Cirrus VISION SF50 Airplane Flight Manual

Aircraft serials sf50-0005 and subsequent

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FAA APPROVED

AIRPLANE FLIGHT MANUAL

for the CIRRUS VISION SF50

Aircraft Serials SF50-0005 and Subsequent

FAA Approved in Normal Category based on FAR 23. This document must

be carried in the airplane at all times and be kept within the reach of the

pilot during all flight operations.

THIS MANUAL INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO

THE PILOT BY FAR PART 23 AND ADDITIONAL INFORMATION PROVIDED BY

CIRRUS AIRCRAFT AND CONSTITUTES THE FAA APPROVED AIRPLANE

FLIGHT MANUAL.

Model - Serial #:

Registration #:

P/N 31452-001

Cover Page-i

Revision 2

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Summary of Contents for Cirrus VISION SF50

Page 1 THIS MANUAL INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE PILOT BY FAR PART 23 AND ADDITIONAL INFORMATION PROVIDED BY CIRRUS AIRCRAFT AND CONSTITUTES THE FAA APPROVED AIRPLANE FLIGHT MANUAL. Model - Serial #:...
Page 3 IRRUS IRPLANE LIGHT ANUAL SF50 ISION FFECTIVE AGES List of Effective Pages Use this page to determine the current effective date for each page in the AFM. Supplements are issued individually and are controlled by the Log of Supplements Page in Section 9. Dates of original issue and revised pages are: Original Issue..
Page 4 IRPLANE LIGHT ANUAL IRRUS SF50 IST OF FFECTIVE AGES ISION List of Effective Pages (Cont.) Page Status Page Status Page Status 2-93 Revision 4 3-42 Revision 4 3A-15 Revision 4 2-94 Revision 4 3-43 Revision 4 3A-16 Revision 4 2-95 Revision 4 3-44 Revision 4...
Page 5 IRRUS IRPLANE LIGHT ANUAL SF50 ISION FFECTIVE AGES List of Effective Pages (Cont.) Page Status Page Status Page Status 3A-70 Revision 4 4-23 Revision 4 5-46 Revision 4 3A-71 Revision 4 4-24 Revision 4 5-47 Revision 4 3A-72 Revision 4 4-25 Revision 4 5-48...
Page 6 IRPLANE LIGHT ANUAL IRRUS SF50 IST OF FFECTIVE AGES ISION List of Effective Pages (Cont.) Page Status Page Status Page Status 5-101 Revision 4 5-156 Revision 4 8-31 Revision 4 5-102 Revision 4 5-157 Revision 4 8-32 Original Issue 5-103 Revision 4 5-158 Revision 4...
Page 7 IRRUS IRPLANE LIGHT ANUAL SF50 ISION FFECTIVE AGES List of Effective Pages (Cont.) Page Status Page Status Page Status 10-14 Original Issue P/N 31452-001 LOEP-5 Revision 4...
Page 8 IRPLANE LIGHT ANUAL IRRUS SF50 IST OF FFECTIVE AGES ISION List of Effective Pages (Cont.) Page Status Page Status Page Status Intentionally Left Blank LOEP-6 P/N 31452-001 Revision 4...
Page 9 OREWORD Foreword This Airplane Flight Manual (AFM) has been prepared by Cirrus Aircraft to familiarize operators with the aircraft. Read this AFM carefully. It provides operational proce- dures that will assure the operator obtains the perfor- mance published in the AFM, data designed to allow the...
Page 10 OREWORD IRRUS SF50 OREWORD ISION storage. Tabbed dividers throughout the AFM allow quick reference to each section. Logical and convenient Tables of Contents are located at the beginning of each section to aid in locating specific data within that section. The AFM is divided into ten sections as follows: Section 1 ..............
Page 11: Identifying Revised Material
“Original Issue” at this location. In the event that the majority of pages in the AFM are revised, Cirrus Aircraft may deter- mine that it is more effective to reissue the AFM. Reissued pages will be identified by the word “Reissue”...
Page 12 AFM. Revisions to the Airplane Flight Manual AFM revisions, temporary revisions, and supplements can be downloaded from Cirrus Aircraft at www.cirrusaircraft.com, or from the Authorized Service Center website. Paper copies of AFM revisions and supplements can be purchased from Cirrus Connection at www.cirrusconnection.com.
Page 13 The “Log of Supplements” page can be utilized as a “Table of Contents” for Section 9. If the airplane is modified at a non Cirrus Aircraft facility through an STC or other approval method, it is the owner’s responsibility...
Page 14 OREWORD IRRUS SF50 ETENTION OF ISION Retention of Data In the event a new title page is issued, the weight and balance data changes, the equipment list changes, or the “Log of Supplements” is replaced, the owner must ensure that all information applicable to the airplane is trans- ferred to the new pages and the aircraft records are current.
Page 15: Warnings, Cautions, And Notes
IRRUS OREWORD SF50 ISION ARNINGS AUTIONS OTES Warnings, Cautions, and Notes Warnings, Cautions, and Notes are used throughout this AFM to focus attention on special conditions or proce- dures as follows: • WARNING • Warnings are used to call attention to operating procedures which, if not strictly observed, may result in personal injury or loss of life.
Page 16 OREWORD IRRUS SF50 ARNINGS AUTIONS OTES ISION Intentionally Left Blank Front Matter-8 P/N 31452-001 Original Issue...
Page 17: Table Of Contents
1: G IRRUS ECTION ENERAL SF50 ISION ABLE ONTENTS Section 1: General Table of Contents Introduction..................3 The Airplane ..................7 Engine ....................7 Fuel ....................7 Approved Fuel Grades ..............7 Oil ...................... 8 Oil Capacity ..................8 Landing Gear Hydraulic Fluid & Brake Fluid ........8 Ice Protection System (IPS) Fluid .............
Page 18 1: G ECTION ENERAL IRRUS SF50 ABLE ONTENTS ISION Intentionally Left Blank P/N 31452-001 Revision 3...
Page 19: Introduction
1: G IRRUS ECTION ENERAL SF50 ISION NTRODUCTION Introduction This section contains information of general interest to pilots and owners. You will find the information useful in acquainting yourself with the airplane, as well as in loading, fueling, sheltering, and handling the airplane during ground operations.
Page 20 1: G ECTION ENERAL IRRUS SF50 NTRODUCTION ISION Figure 1-1: Airplane Three View 30.7 ft (9.4 m) 10.9 ft (3.3 m) 11.1 ft (3.4 m) 18.3 ft (5.6 m) NOTE: • Wing Area = 195.7 sq. ft. (18.2 sq. m) •...
Page 21 1: G IRRUS ECTION ENERAL SF50 ISION NTRODUCTION Figure 1-2: Airplane Interior Dimensions 61.0" 44.0" 46.4" 16.6" 48.8" 34.7" 29.6" 12" 80" 24.6" 23.0" 49.4" 19.3" 17.6" 24.9" BAGGAGE DOOR CABIN DOOR SF50_FM01_0014A OPENING OPENING Location Length Width Height Volume Cabin 137.8”...
Page 22 1: G ECTION ENERAL IRRUS SF50 NTRODUCTION ISION Figure 1-3: Turning Radius GROUND TURNING CLEARANCE 26.1 ft. (7.9 m) RADIUS FOR WING TIP (3.5 m) 11.6 ft. RADIUS FOR NOSE GEAR 0.5 ft. (0.2 m) RADIUS FOR INSIDE GEAR 11.7 ft. (3.6 m) RADIUS FOR OUTSIDE GEAR 20.7 ft.
Page 23: The Airplane
1: G IRRUS ECTION ENERAL SF50 ISION IRPLANE The Airplane Engine Number of Engines .............. 1 Engine Manufacturer ..... Williams International Engine Model ............FJ33-5A Engine Type................Twin spool, turbofan engine with a single-stage fan and a three-stage axial compressor direct-driven by a two-stage turbine, a single-stage centrifugal compressor driven by a single-stage turbine, an annular combustor, a full length bypass duct, and an exhaust mixer.
Page 24: Oil
1: G ECTION ENERAL IRRUS SF50 IRPLANE ISION Oil Capacity Oil Tank Total Volume......3 Quarts (2.8 L) Oil Tank FULL Volume......2.2 Quarts (2.1 L) Oil Tank ADD Volume......1.6 Quarts (1.5 L) Oil Tank Usable Volume ......1.5 Quarts (1.4 L) The oil tank total volume represents the volume at which the filler port will overflow.
Page 25: Ice Protection System (Ips) Fluid
1: G IRRUS ECTION ENERAL SF50 ISION IRPLANE Ice Protection System (IPS) Fluid • IPS Fluid (AL-5) DTD-406B IPS Fluid Capacity Total Tank Capacity ..... 3.1 U.S. gallons (11.7 L) Usable ..........3.0 U.S. gallons (11.4 L) Unusable ..........0.1 U.S. gallon (0.4 L) Maximum Certificated Weights Max.
Page 26: Noise Characteristics
1: G ECTION ENERAL IRRUS SF50 IRPLANE ISION Noise Characteristics The following noise levels comply with 14 CFR Part 36, Appendix B, Stage 4 maximum noise level requirements and were obtained by analysis of approved data from noise tests conducted under the provisions of part 36, Amendment 36-28.
Page 27: Terminology
1: G IRRUS ECTION ENERAL SF50 ISION IRPLANE Terminology Table 1: General Airspeed Terminology General Airspeed Terminology Terminology Definition KCAS Knots Calibrated Airspeed is the indicated airspeed corrected for position and instrument error. KIAS Knots Indicated Airspeed is the speed shown on the airspeed indicator.
Page 28 1: G ECTION ENERAL IRRUS SF50 IRPLANE ISION General Airspeed Terminology (Continued) Terminology Definition Operating Maneuvering Speed is the maximum speed at which application of full control movement will not overstress the airplane. Maximum Landing Gear Operating Speed LO_EXT (Extension) is the maximum speed at which it is safe to extend the landing gear.
Page 29 1: G IRRUS ECTION ENERAL SF50 ISION IRPLANE General Airspeed Terminology (Continued) Terminology Definition Minimum final approach speed is the airspeed equal to the landing 50-foot point speed with flaps 100% (IPS OFF) or with flaps 50% and landing gear extended. For emergency and abnormal procedures, it is the airspeed equal to the 50-foot point speed with flaps in landing position as...
Page 30 1: G ECTION ENERAL IRRUS SF50 IRPLANE ISION Table 2: Meteorological Terminology Meteorological Terminology Terminology Definition Instrument Meteorological Conditions are meteorological conditions expressed in terms of visibility, distance from cloud, and ceiling less than the minima for visual flight defined in FAR 91.155. International Standard Atmosphere (standard day) is an atmosphere in which (1) the air is a dry perfect gas, (2) the...
Page 31 1: G IRRUS ECTION ENERAL SF50 ISION IRPLANE Meteorological Terminology (Continued) Terminology Definition Pressure Altitude is the altitude read from the altimeter when the altimeter’s barometric adjustment has been set to 29.92 inHg (1013.21 mb) corrected for position and instrument error. In this AFM, altimeter instrument errors are assumed to be zero.
Page 32 1: G ECTION ENERAL IRRUS SF50 IRPLANE ISION Table 3: Engine Power Terminology Engine Power Terminology Terminology Definition Thrust Lever Angle is the position of the thrust lever. Takeoff thrust is the maximum installed thrust that the engine will produce. This is obtained when Thrust Lever Angle (TLA) is in Takeoff (T/O) position.
Page 33 1: G IRRUS ECTION ENERAL SF50 ISION IRPLANE Engine Power Terminology (Continued) Terminology Definition Inter-Turbine Temperature is the exhaust temperature measured between the HP and LP turbines. P/N 31452-001 1-17 Original Issue...
Page 34 1: G ECTION ENERAL IRRUS SF50 IRPLANE ISION Table 4: Performance and Flight Planning Terminology Performance and Flight Planning Terminology Terminology Definition One “g” is a quantity of acceleration equal to that of earth’s gravity. Demonstrated Demonstrated Crosswind Velocity is the Crosswind velocity of the crosswind component for Velocity...
Page 35 1: G IRRUS ECTION ENERAL SF50 ISION IRPLANE Table 5: Weight and Balance Terminology Weight and Balance Terminology Terminology Definition Reference Reference Datum is an imaginary Datum vertical plane from which all horizontal distances are measured for balance purposes. Fuselage Station Fuselage Station (FS) is a location along the airplane fuselage measured in inches from the reference datum and expressed...
Page 36 1: G ECTION ENERAL IRRUS SF50 IRPLANE ISION Weight and Balance Terminology (Continued) Terminology Definition Maximum Maximum Ramp Weight is the Ramp Weight maximum weight approved for ground maneuver and includes the weight of the fuel used for startup and taxi. Maximum Gross Maximum Gross Weight is the Weight...
Page 37 2: L IRRUS ECTION IMITATIONS SF50 ISION ABLE ONTENTS Section 2: Limitations Table of Contents Introduction..................5 Certification Status ................5 Taxiing, Takeoff, and Landing Limitations........... 6 Operational Limits ................6 Airspeed Limitations ................7 Operating Speeds ................7 Minimum Maneuvering Speeds ............8 Flap Speeds ..................
Page 38 Navigation and Communication Equipment ........82 Attitude and Heading Reference System (AHRS) ......82 Cirrus Perspective Touch by Garmin Avionics System ....83 Cirrus Perspective Touch by Garmin GPS Navigation System ..83 Weather ................... 86 Garmin GSR 56 Iridium Datalink ........... 86 Other Limitations ................
Page 39 2: L IRRUS ECTION IMITATIONS SF50 ISION ABLE ONTENTS Tire Inflation Pressure (nominal) ............. 93 Circuit Breakers................93 In-Flight Entertainment ..............93 Exterior Windows ................93 Placards ..................94 Interior Placards ................94 Exterior Placards ................. 103 Electronic Placards..............106 P/N 31452-001 Revision 4...
Page 40 2: L ECTION IMITATIONS IRRUS SF50 ABLE ONTENTS ISION Intentionally Left Blank P/N 31452-001 Original Issue...
Page 41: Introduction
2: L IRRUS ECTION IMITATIONS SF50 ISION NTRODUCTION Introduction The limitations included in this Section of the Airplane Flight Manual (AFM) are approved by the Federal Avia- tion Administration. This section provides operating limitations, instrument markings, and basic placards required by regulation and necessary for the safe operation of the aircraft and its standard systems and equipment.
Page 42: Taxiing, Takeoff, And Landing Limitations
2: L ECTION IMITATIONS IRRUS SF50 AXIING AKEOFF ANDING IMITATIONS ISION Taxiing, Takeoff, and Landing Limitations Operational Limits For taxiing operations, the lower cabin door must be closed. Takeoffs and landings are limited to paved or concrete surfaces. Maximum Tailwind..........10 knots P/N 31452-001 Revision 3...
Page 43: Airspeed Limitations
2: L IRRUS ECTION IMITATIONS SF50 ISION IRSPEED IMITATIONS Airspeed Limitations Operating Speeds Operating Maneuvering Speed (V ) ....150 KIAS Max. Operating Speed (V )......250 KIAS Max. Operating Mach Number (M ) ....0.53 Mach • WARNING • Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw, as they may result in loss of control in flight and/or structural failures at any speed,...
Page 44: Minimum Maneuvering Speeds
2: L ECTION IMITATIONS IRRUS SF50 IRSPEED IMITATIONS ISION Minimum Maneuvering Speeds FLAP CONFIGURATION SPEED 100% • N • These speeds are based on up to 40° angle of bank and are independent of thrust settings. Flaps UP is an abnormal landing configuration, approved for use in the event of an emergency.
Page 45: Airspeed Indicator Markings
2: L IRRUS ECTION IMITATIONS SF50 ISION IRSPEED NDICATOR ARKINGS Airspeed Indicator Markings Value Marking (KIAS/Mach) Remarks Red Line 250 KIAS/ Maximum Operating Speed 0.53 Mach ) and Maximum Operating Mach Number (M ≥ 210 KIAS Landing Gear: DOWN ≥ 190 KIAS FE_50% ≥...
Page 46: Powerplant Limitations
OWERPLANT IMITATIONS ISION Powerplant Limitations Operational Limits The Cirrus Perspective Touch™ by Garmin® avionics system provides dynamic gage markings for engine instruments. Markings are automatically determined based on current conditions and mode of operation (start, climb, etc.). Automated markings are designed to reduce pilot work- load and eliminate pilot error;...
Page 47 2: L IRRUS ECTION IMITATIONS SF50 ISION OWERPLANT IMITATIONS • N • High oil temperatures and associated low oil pres- sures can occur when returning to ground idle from high power. Therefore, ground operation at or near Takeoff thrust should be limited in dura- tion to avoid oil temperatures rising above 194 °F 90 °C) or perform a partial power cooldown prior to returning to ground idle.
Page 48: Engine Limit Exceedances
Long term changes in N1 and N2 or ITT readings can be useful in tracking trends in engine health. Therefore, the pilot should monitor engine trend data and notify Cirrus Aircraft of any sudden or gradual changes over time. Fuel •...
Page 49: Oil
2: L IRRUS ECTION IMITATIONS SF50 ISION OWERPLANT IMITATIONS Fuel Left Right Total 149.25 U.S. gal 149.25 U.S. gal 298.5 U.S. gal Total Capacity (1009 lb) (1009 lb) (2018 lb) 148 U.S. gal 148 U.S. gal 296 U.S. gal Usable (1000 lb) (1000 lb) (2001 lb)
Page 50: Landing Gear Hydraulic Fluid And Brake Fluid
2: L ECTION IMITATIONS IRRUS SF50 OWERPLANT IMITATIONS ISION Landing Gear Hydraulic Fluid and Brake Fluid Only the following approved hydraulic fluid shall be used for the landing gear and brakes: Specification ..........MIL-PRF-87257 2-14 P/N 31452-001 Revision 3...
Page 51: Engine Start
2: L IRRUS ECTION IMITATIONS SF50 ISION OWERPLANT IMITATIONS Engine Start Engine Start (General) Minimum oil temperature......-40 °F (-40 °C) Minimum temperature for Battery 1 start ..0 °F (-18 °C) Minimum voltage for Battery 1 start ....23.5 VDC Min.
Page 52: Start Abort Criteria
2: L ECTION IMITATIONS IRRUS SF50 OWERPLANT IMITATIONS ISION Start Abort Criteria Abort start if any of the following are observed: • Failure to accelerate after 30 seconds. • No N1 indication at 25% N2. • Low oil pressure after start. •...
Page 53: Starter Generator Limits (Start Mode)
2: L IRRUS ECTION IMITATIONS SF50 ISION OWERPLANT IMITATIONS Starter Generator Limits (Start Mode) The starter duty cycle is limited as follows: 30-second maximum first start attempt followed by a 30-second minimum spool down and cool down period. 30-second maximum second start attempt followed by a 5-minute minimum spool down and cool down period.
Page 54 2: L ECTION IMITATIONS IRRUS SF50 OWERPLANT IMITATIONS ISION Figure 2-3: Danger Areas During Start and Ground Operation MAX POWER VELOCITY DROPS TO 20 mph (32 kph) AND TEMPERATURE IS 10 °F (-12 °C) 20 ft (6 m) OVER AMBIENT radius 85 ft (26 m)
Page 55: Engine Instrument Markings & Annunciations
Associated Warning and Caution annunciations are shown in capitalized text. Powerplant The Cirrus Perspective Touch by Garmin avionics system provides dynamic gage markings for engine instruments. Markings are automatically determined based on current conditions and mode of operation (start, climb, etc.).
Page 56 2: L ECTION IMITATIONS IRRUS & A SF50 NGINE NSTRUMENT ARKINGS NNUNCIATIONS ISION High Low Operating High Instrument Operating Limit Range Limit (Range & Range (Red (Green Arc (Red Units) (Green Arc Line) Bottom) Line) Top) N2 < 80% 23 psi N2 <...
Page 57: Fuel
2: L IRRUS ECTION IMITATIONS SF50 & A ISION NGINE NSTRUMENT ARKINGS NNUNCIATIONS Fuel Yellow Green Yellow Arc/Bar Arc/Bar Arc/Bar Arc/Bar Arc/Bar Instrument Min. Max. (Range & Caution Normal Caution Units) Min. Range Range Range Max. Fuel Flow –– –– 0 –...
Page 58: Electrical
2: L ECTION IMITATIONS IRRUS & A SF50 NGINE NSTRUMENT ARKINGS NNUNCIATIONS ISION Electrical Yellow Yellow Green Arc/Bar Arc/Bar Arc/Bar Arc/Bar Arc/Bar Instrument (Range & Min. Max. Normal Units) Caution Min. Caution Max. Range Range Range Ess. Bus Voltage –– <...
Page 59: Weight Limits
2: L IRRUS ECTION IMITATIONS SF50 ISION EIGHT IMITS Weight Limits • Note • The airplane must be operated in accordance with the approved loading schedule. Max. Takeoff Gross Wt. (MTOGW) ..6000 lb (2722 kg) Maximum Landing Weight (MLW) ..5550 lb (2517 kg) Maximum Ramp Weight (MRW)..6040 lb (2740 kg) Max.
Page 60: Center Of Gravity Limits
2: L ECTION IMITATIONS IRRUS SF50 ENTER OF RAVITY IMITS ISION Center of Gravity Limits CG Envelope Weight (lb) FS (inches) Forward Light 4000 189.44 Forward Intermediate 4700 189.44 Forward Gross 6000 192.55 Aft Gross 6000 198.15 Aft Intermediate 5200 198.15 Aft Light 3600...
Page 61 2: L IRRUS ECTION IMITATIONS SF50 ISION ENTER OF RAVITY IMITS Figure 2-4: Center of Gravity Envelope 6500 FS 192.55 Max. Ramp Weight FS 198.15 6000 lb 6040 lb 6000 lb 6000 5500 Max. Landing Weight 5550 lb Max. Zero Fuel Weight 4900 lb FS 198.15 5000...
Page 62: Maneuver Limits
2: L ECTION IMITATIONS IRRUS SF50 ANEUVER IMITS ISION Maneuver Limits Acrobatic maneuvers are strictly prohibited. Spins are strictly prohibited. This airplane is certified in the normal category and is not designed for acrobatic operations. Only those operations incidental to normal flight are approved. These opera- tions include normal stalls, chandelles, lazy eights, and turns in which the angle of bank is limited to 60°.
Page 63: Flight Load Factor Limits
2: L IRRUS ECTION IMITATIONS SF50 ISION LIGHT ACTOR IMITS Flight Load Factor Limits Flaps UP, any weight........+3.6g, -1.44g Flaps 50%, any weight ..........+2.0g, 0g Flaps 100%, any weight.......... +2.0g, 0g Landing Gear (V )......... +3.6g, -1.44g Landing Gear (V ) ..........
Page 64: Kinds Of Operation
2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation This airplane is equipped for day and night, VFR and IFR operations, and flight in icing conditions when the required equipment is installed as defined within the Kinds of Operations Equipment List.
Page 65: Symbols
2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION The systems and equipment list does not include specific flight, emergency, and radio-navigation equipment required by local operating rules. It also does not include components obviously required for the airplane to be airworthy such as wings, primary flight controls, empennage, engines, control panels etc.
Page 66 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Symbol Definition This symbol indicates a requirement for a specific operations procedure which must be accomplished in planning for and/or operating with the listed item inoperative. Normally, these procedures are accomplished by the flightcrew;...
Page 67 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes AIR CONDITIONING Avionics Cooling 1 / 1 1 / 1 1 / 1 1 / 1 1 / 1 Bleed Bias 1 / 1 1 / 1 1 / 1 1 / 1 1 / 1 Valve...
Page 68 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes (O) May be inoperative provided: CABIN PRESS 1 circuit breaker is pulled and collared, CABIN PRES- SURE DUMP switch is...
Page 69 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes May be inoperative provided: Air Condi- tioning System is deac- tivated, and power-on ground operations are...
Page 70 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes AUTO FLIGHT GMC 707 (AFCS 1 / 1 1 / 1 1 / 1 1 / 1 1 / 1 Mode Controller) Autopilot...
Page 71 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes COMMUNICATIONS Audio Panel 1 / 1 1 / 1 1 / 1 1 / 1 1 / 1 (GMA 36) Any in excess of those required by 14 CFR...
Page 72 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes ELECTRICAL POWER Battery 1 1 / 1 1 / 1 1 / 1 1 / 1 1 / 1 Battery 2 1 / 1 1 / 1 1 / 1 1 / 1 1 / 1 Generator 1 1 / 1 1 / 1 1 / 1 1 / 1 1 / 1...
Page 73 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes FIRE PROTECTION Smoke Goggles - / 0 - / 0 - / 0 - / 0 - / 0 (Optional) Portable Fire Extin-...
Page 74 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes (O) May be inoperative provided: Aileron Trim Tab is visually checked for full range of opera- tion, Aileron Trim...
Page 75 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes (O) May be inoperative provided: STICK SHAKER circuit breaker is pulled and collared, Stick stall warning...
Page 76 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes FUEL Fuel Control 1 / 1 1 / 1 1 / 1 1 / 1 1 / 1 Switch Fuel Control...
Page 77 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes May be failed OFF provided ENGINE IPS switch is OFF for all operations.
Page 78 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes May be inoperative provided ENGINE IPS switch is OFF for all operations.
Page 79 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes Right pitot heater may be inoperative provided pitot heater is not required by 14 CFR.
Page 80 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes INDICATING/RECORDING SYSTEMS (O) May be inoperative Flight provided flight time is Hours 1 / 0 1 / 0 1 / 0 1 / 0 1 / 0 tracked by alternate...
Page 81 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes LIGHTS May be inoperative provided: remaining lighting system lights are sufficient to clearly illuminate all required instruments, controls, and other devices for...
Page 82 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes May be inoperative for Day operations provided: remaining lighting system lights are sufficient to clearly illuminate all required instruments, controls,...
Page 83 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes May be inoperative provided: remaining lighting system lights are sufficient to clearly illuminate all required Cockpit instruments, controls,...
Page 84 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes May be inoperative Landing provided at least one 4 / 0 4 / 1 4 / 0 4 / 1 4 / 0 Lights wingtip landing light is operative.
Page 85 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes The second primary air data computer (GDC#2) may be inoperative provided: MD302 standby unit is OPERATIVE, there are no...
Page 86 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes OAT sensor #2 may be inoperative. Outside Air Tempera- NOTE: OAT sensor #1 2 / 1 2 / 1 2 / 1 2 / 1 2 / 1 ture (OAT) data is provided to...
Page 87 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes The second primary attitude and heading reference system (GRS#2/GMU#2) may be inoperative provided: MD302 standby...
Page 88 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes (M) May be inoperative provided: TCAS-I system is deacti- System 1 / 0 1 / 0 1 / 0 1 / 0 1 / 0 vated and secured, and (Optional)
Page 89 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes Any in excess of those (Distance required by 14 CFR Measuring may be inoperative 1 / 0 1 / 0 1 / 0 1 / 0 1 / 0...
Page 90 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes Pilot (Left Seat) 1 / 1 1 / 1 1 / 1 1 / 1 1 / 1 Oxygen Mask May be inoperative...
Page 91 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes (M) May be inoperative for operations not requiring oxygen provided: operations do not require a second in Passenger...
Page 92 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes (M)(O) One per occupied seat provided: Passenger affected mask is Oxygen placarded "INOPERA- Masks,...
Page 93 2: L IRRUS ECTION IMITATIONS SF50 ISION INDS OF PERATION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes (O) May be inoperative provided: BLEED AIR switch is in the OFF/FRESH position for ground operations, takeoff, and landing,...
Page 94 2: L ECTION IMITATIONS IRRUS SF50 INDS OF PERATION ISION Kinds of Operation System, # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes Touch- screen 3 / 3 3 / 3 3 / 3 3 / 3 3 / 3 Controllers (GTCs) Integrated...
Page 95 Faults) with the times - / - - / - - / - - / - - / - established in Cirrus Vision SF50 Airplane Maintenance Manual and Williams FJ33-5A Line Maintenance Manual. Fuel Flow May be inoperative Indication provided fuel quantity...
Page 96 # Installed / # Required Instrument Remarks, Exceptions, and/or Limitations, and/or Equipment Night Night Icing Notes RECOVERY Cirrus Airframe Parachute 1 / 1 1 / 1 1 / 1 1 / 1 1 / 1 System (CAPS) 2-60 P/N 31452-001 Revision 4...
Page 97: Maximum Operating Altitude Limit
2: L IRRUS ECTION IMITATIONS SF50 ISION AXIMUM PERATING LTITUDE IMIT Maximum Operating Altitude Limit Maximum Airport Elevation ......10,000 ft MSL Maximum Operating Altitude........FL280 Minimum Airport Elevation......-1000 ft MSL Maximum Positive Cabin Differential Pressure ...6.4 psid 1. For operations at altitudes below sea level, use Mean Sea Level (MSL) values.
Page 98: Outside Air Temperature Limits
2: L ECTION IMITATIONS IRRUS SF50 UTSIDE EMPERATURE IMITS ISION Outside Air Temperature Limits Takeoff Temperatures Minimum Takeoff Temperature ....-40 °F (-40 °C) Maximum Takeoff Temperature ....122 °F (50 °C) Operating Temperatures Min. Operating Temp. (up to 20,000 ft)..-65 °F (-54 °C) Min.
Page 99 2: L IRRUS ECTION IMITATIONS SF50 ISION UTSIDE EMPERATURE IMITS • N • Windshield IPS performance is degraded below -40 °F (-40 °C). Avionics that have been cold soaked for two or more hours at an ambient temperature of -40 °F (-40 °C) or lower must be allowed to warm up for at least 20 minutes after power on prior to takeoff.
Page 100 2: L ECTION IMITATIONS IRRUS SF50 UTSIDE EMPERATURE IMITS ISION Figure 2-5: Outside Air Temperature Limits 2-64 P/N 31452-001 Revision 4...
Page 101: Minimum Crew Requirements
2: L IRRUS ECTION IMITATIONS SF50 ISION INIMUM EQUIREMENTS Minimum Crew Requirements The minimum crew requirement for all operations is one appropriately rated pilot. P/N 31452-001 2-65 Revision 4...
Page 102: Maximum Passenger Seating Limits
2: L ECTION IMITATIONS IRRUS SF50 AXIMUM ASSENGER EATING IMITS ISION Maximum Passenger Seating Limits Occupancy of this airplane is limited to seven persons - the pilot and six passengers. The two optional outboard XC seats are weight-limited to 90 lb (40 kg). If this weight restriction for the XC seats cannot be met, or if the XC seats are not installed, these seats cannot be used and occupancy is thus limited to five persons.
Page 103: Child Restraint System Limits
2: L IRRUS ECTION IMITATIONS SF50 ISION HILD ESTRAINT YSTEM IMITS Child Restraint System Limits Rear seat configuration for LATCH-compliant child seats is limited to Seats 3, 4, and 5. Installation of child seats in Seats 1, 2, 6, and 7 is prohibited.
Page 104: Seat Belt Limits
2: L ECTION IMITATIONS IRRUS SF50 IMITS ISION Seat Belt Limits Seat belts must be worn and tightened snug and low on the waist. 2-68 P/N 31452-001 Revision 4...
Page 105: Seat Handling Limitations
2: L IRRUS ECTION IMITATIONS SF50 ISION ANDLING IMITATIONS Seat Handling Limitations • WARNING • If a seat is unoccupied, buckle the seat belt. Do not move (or remove) the passenger seat while the aircraft is moving; do so when the aircraft is stationary.
Page 106: Systems And Equipment Limits
2: L ECTION IMITATIONS IRRUS SF50 YSTEMS AND QUIPMENT IMITS ISION Systems and Equipment Limits Flight Controls Flaps Approved Takeoff Settings ........... 50% Approved Approach and Landing Settings..UP, 50%, 100% • N • Flaps UP is an abnormal landing configuration, approved for use in the event of flap failure.
Page 107: Traffic Alert And Collision Avoidance System (Tcas-1)
2: L IRRUS ECTION IMITATIONS SF50 ISION YSTEMS AND QUIPMENT IMITS Traffic Alert and Collision Avoidance System (TCAS-1) TCAS-1 is for advisory use only to aid in visually acquiring traffic. TCAS-1 traffic information must not be the only basis for avoidance maneuvers.
Page 108: Electrical System
QUIPMENT IMITS ISION Electrical System The Cirrus Perspective Touch by Garmin avionics system provides dynamic gage markings for engine instruments. Markings are automatically determined based on current conditions and mode of operation (start, climb, etc.). Automated markings are designed to reduce pilot work- load and eliminate pilot error;...
Page 109: Icing Conditions
2: L IRRUS ECTION IMITATIONS SF50 ISION YSTEMS AND QUIPMENT IMITS Icing Conditions Icing conditions are defined as visible moisture and OAT ≤ 41 °F (5 °C) or visible ice accumulations on the airframe. Visible moisture is defined as any cloud, fog with visibility of one mile (1.6 km) or less, mist, rain, sleet, or snow.
Page 110: Operation
2: L ECTION IMITATIONS IRRUS SF50 YSTEMS AND QUIPMENT IMITS ISION • Unusually extensive ice accumulation on the airframe or windshield in areas not normally observed to collect ice. • Accumulation of ice on the wing surface, aft of the deice boots.
Page 111: Tactile Inspection
2: L IRRUS ECTION IMITATIONS SF50 ISION YSTEMS AND QUIPMENT IMITS Takeoff is prohibited with any frost (polished or not), ice, snow, or slush adhering to the wings, stabilizers, control surfaces, engine inlet, or fuselage forward of the engine inlet. When holding in icing conditions, higher speed will result in increased ice accretion rate.
Page 112: Ips Activation
2: L ECTION IMITATIONS IRRUS SF50 YSTEMS AND QUIPMENT IMITS ISION This check must be performed whenever the OAT is below 41 °F (5 °C), or when the wing fuel temperature is not above 32 °F (0 °C), and visible moisture is present, or the airplane was exposed to visible moisture since the previous landing, or the difference between the dew point temperature and the OAT is 6 °F (3 °C) or less, or water is...
Page 113: Ice Protection System (Ips) Fluid
2: L IRRUS ECTION IMITATIONS SF50 ISION YSTEMS AND QUIPMENT IMITS • N • The left wing leading edge is the primary reference area for determining if ice is accumulating on the aircraft. Ice may be visible on other areas of the aircraft as well, such as the forward windshield.
Page 114: Use Of Autopilot In Icing Conditions
2: L ECTION IMITATIONS IRRUS SF50 YSTEMS QUIPMENT IMITS ISION Use of Autopilot in Icing Conditions In light- to moderate-icing conditions, autopilot use with periodic checks (disconnect and hand fly) is permitted. However, autopilot use is prohibited in the following conditions: •...
Page 115: Autopilot
YSTEMS QUIPMENT IMITS Autopilot The appropriate revision of the Cirrus Perspective Touch by Garmin Cockpit Reference Guide must be immedi- ately available to the pilot during flight. The system software version stated in the Cockpit Refer- ence Guide must be appropriate for the system software version displayed on the equipment.
Page 116 2: L ECTION IMITATIONS IRRUS SF50 YSTEMS QUIPMENT IMITS ISION • Autopilot Minimum-Use Height: – Takeoff and Climb ......400 ft AGL – Enroute and Descent ....1000 ft AGL – Approach (GP or GS Mode).. Higher of 200 ft AGL or Approach MDA, DA, DH –...
Page 117 2: L IRRUS ECTION IMITATIONS SF50 ISION YSTEMS QUIPMENT IMITS • Use of VNAV is not supported during an approach with a teardrop course reversal. VNAV will be disabled at the beginning of the teardrop. • If Stall Warning is inoperative, Autopilot Under- speed Protection (USP) will not be provided in Alti- tude Critical Modes (ALT, GS, GP, T/O and GA).
Page 118: Navigation And Communication Equipment
2: L ECTION IMITATIONS IRRUS SF50 YSTEMS QUIPMENT IMITS ISION Navigation and Communication Equipment Attitude and Heading Reference System (AHRS) The airplane must not operate in the regions listed below. Flying in these regions may lead to loss of attitude or heading information, and possibly even loss of aircraft control.
Page 119: Cirrus Perspective Touch By Garmin Avionics System
ECTION IMITATIONS SF50 ISION YSTEMS QUIPMENT IMITS Cirrus Perspective Touch by Garmin Avionics System The avionics system has the following limitations: • Use of VNAV is prohibited during the intermediate segment of an approach that includes a teardrop course reversal.
Page 120 2: L ECTION IMITATIONS IRRUS SF50 YSTEMS QUIPMENT IMITS ISION • Barometric VNAV is approved to enroute and terminal descents, as per AC 20-129. Guidance is provided up to the FAF waypoint when there is no procedure for vertical guidance following the FAF. Guidance is provided up to the waypoint preceding the FAF (FAF-1) when there are provisions for vertical guidance (ILS or GPS WAAS) following the...
Page 121 2: L IRRUS ECTION IMITATIONS SF50 ISION YSTEMS QUIPMENT IMITS The GPS navigation system has the following limitations: • GPS-based IFR enroute, oceanic, and terminal navi- gation is prohibited unless the pilot verifies the currency of the database or verifies each selected waypoint for accuracy by reference to current approved data.
Page 122: Weather
2: L ECTION IMITATIONS IRRUS SF50 YSTEMS QUIPMENT IMITS ISION approach not approved for GPS overlay is not authorized. • Operation in airspace referenced to a datum other than WGS-84 or NAD-83 is prohibited. • RNP operations are not authorized except as noted in the Operational Approvals Section.
Page 123: Other Limitations
2: L IRRUS ECTION IMITATIONS SF50 ISION THER IMITATIONS Other Limitations Oxygen The oxygen system is serviced with Oxygen, Aviator’s Breathing, Liquid And Gas (MIL-O-27210, Type I - Gaseous). It is prohibited to use technical/medical oxygen. Minimum dispatch pressure is per table on following page.
Page 124 2: L ECTION IMITATIONS IRRUS SF50 THER IMITATIONS ISION • WARNING • Ensure that the crew oxygen mask can be donned quickly without any interferences (i.e. eyewear, head- sets, hats, hairstyles). Ensure that the passenger oxygen masks are donned during an emergency descent to an altitude not re- quiring supplemental oxygen.
Page 125: Fill Pressure Vs. Temperature
2: L IRRUS ECTION IMITATIONS SF50 ISION THER IMITATIONS Fill Pressure vs. Temperature OXYGEN FILL PRESSURE VERSUS TEMPERATURE TEMP °F TEMP °C FILL TO PSI MIN. DISPATCH 1321 1141 1370 1181 1418 1221 1466 1261 1515 1300 1563 1340 1611 1379 1659 1418...
Page 126: Altitude Vs. Hours Of Available Oxygen
2: L ECTION IMITATIONS IRRUS SF50 THER IMITATIONS ISION Altitude vs. Hours of Available Oxygen Pilot Oxygen Mask Mode: NORM The information in the tables below is based on the following: • The pilot quick-don mask set to NORM, and •...
Page 127: Pilot Oxygen Mask Mode: 100
2: L IRRUS ECTION IMITATIONS SF50 ISION THER IMITATIONS Pilot Oxygen Mask Mode: 100% • CAUTION • With 100% flow, endurance can be substantially lower than with diluted flow. The information in the tables below is based on the following: •...
Page 128: Crew Headset
2: L ECTION IMITATIONS IRRUS SF50 THER IMITATIONS ISION Crew Headset One headset with a boom microphone is required for pilot use. Smoking Smoking is prohibited in this airplane. Brakes • WARNING • Brake assemblies, discs, and pads can be VERY HOT. Approach slowly and cautiously to detect the amount of radiant heat before proceeding with tactile inspec- tion (hands on surface).
Page 129: Tire Inflation Pressure (Nominal)
2: L IRRUS ECTION IMITATIONS SF50 ISION THER IMITATIONS After each cool down period, inspect for damaged or overheated components. • N • Refer to Section 8: Handling and Servicing, "Brake Overheat Inspection". Tire Inflation Pressure (nominal) Nose Tire 5.00 x 5 (10 PR)....88±5 psi (607±34 kPa) Main Tires 18 x 5.5 (8 PR)...
Page 130: Placards
2: L ECTION IMITATIONS IRRUS SF50 THER IMITATIONS ISION Placards Interior Placards Figure 2-6: Oxygen Fill Chart OXYGEN FILL CHART FILL TEMPERATURE PRESSURE TEMPERATURE PSIG 1321 -40.0 1370 -34.4 1418 -28.9 1466 -23.3 1515 -17.8 1563 -12.2 1611 - 6.7 1659 - 1.1 1707...
Page 131 2: L IRRUS ECTION IMITATIONS SF50 ISION THER IMITATIONS Figure 2-7: Landing Gear V Placard SF50_FM02_0025 Figure 2-8: Fasten Seat Belts/No Smoking NO SMOKING FASTEN SEATBELTS SF50_FM02_0026 Figure 2-9: Cargo X-Tend CARGO X-TEND WEIGHT LIMIT: 40 LBS (18 KG) INCLUDE WEIGHT IN TOTAL BAGGAGE WEIGHT CALCULATION.
Page 132 2: L ECTION IMITATIONS IRRUS SF50 THER IMITATIONS ISION Figure 2-10: Baggage Compartment Limitations TOTAL BAGGAGE COMPARTMENT WEIGHT LIMIT: 300 LBS (136 KG) 50 LB/FT MAXIMUM (244 KG/M LOAD IN ACCORDANCE WITH AFM. REFER TO AFM FOR BAGGAGE TIE-DOWN, WEIGHT AND BALANCE INFORMATION. SF50_FM02_0028 Figure 2-11: Seats 3, 4, 5 -Locate seat per AFM.
Page 133 2: L IRRUS ECTION IMITATIONS SF50 ISION THER IMITATIONS Figure 2-13: Lavatory This is not an approved seat. Do not use during ground operations, takeoff, or landing. Weight: SF50_FM02_0040A Figure 2-14: Flap Positions/Airspeeds SF50_FM02_0037 Figure 2-15: Pitch Trim Direction SF50_FM02_0035 P/N 31452-001 2-97 Revision 4...
Page 134 2: L ECTION IMITATIONS IRRUS SF50 THER IMITATIONS ISION Figure 2-16: Thrust Position SF50_FM02_0036 Figure 2-17: Fuel Selector FUEL CONTROL AUTO LEFT RIGHT SF50_FM02_0039 2-98 P/N 31452-001 Revision 4...
Page 135 2: L IRRUS ECTION IMITATIONS SF50 ISION THER IMITATIONS Figure 2-18: Emergency Panel SF50_FM02_0038B P/N 31452-001 2-99 Revision 4...
Page 136 2: L ECTION IMITATIONS IRRUS SF50 THER IMITATIONS ISION Figure 2-19: CAPS Safety Pin Flag REMOVE BEFORE FLIGHT INFORM PASSENGERS OF CAPS PROCEDURES USE FOR EMERGENCIES ONLY SEAT BELTS MUST BE WORN AT ALL TIMES WARNING CAPS ® AVOID ACCIDENTAL ACTIVATION This aircraft is equipped with a Pyrotechnic-deployed Emergency parachute system...
Page 137 2: L IRRUS ECTION IMITATIONS SF50 ISION THER IMITATIONS Figure 2-20: Emergency Exit EMERGENCY EXIT 2. ROTATE 1. PULL SF50_FM02_0042 Figure 2-21: Door Operation, Upper TO EXIT: 1. PUSH BUTTON 2. ROTATE HANDLE SF50_FM02_0044 Figure 2-22: Door Operation, Lower EXIT: LIFT AND ROTATE HANDLE SF50_FM02_0045 Figure 2-23: IFE Screen Stowage...
Page 138 2: L ECTION IMITATIONS IRRUS SF50 THER IMITATIONS ISION Figure 2-24: Oxygen PULL FOR OXYGEN SF50_FM02_0079 Figure 2-25: Egress EGRESS Push Forward Here SF50_FM02_0081 2-102 P/N 31452-001 Revision 4...
Page 139: Exterior Placards
2: L IRRUS ECTION IMITATIONS SF50 ISION THER IMITATIONS Exterior Placards Figure 2-26: Emergency Exit EMERGENCY EXIT 1. PULL 2. ROTATE 39326-001 SF50_FM02_0041 Figure 2-27: Door Operation OPEN CLOSE SF50_FM02_0043 Figure 2-28: External Power EXTERNAL POWER, 28VDC SF50_FM02_0052 Figure 2-29: Tire Pressure, Nose NOSE TIRE: 88 PSI ±...
Page 140 2: L ECTION IMITATIONS IRRUS SF50 THER IMITATIONS ISION Figure 2-30: Tire Pressure, Main MAIN TIRE: 105 PSI ±5 PSI 724 kPa ±34 kPa Refer to AFM SF50_FM02_0023 Figure 2-31: Fuel Tank Capacity and Fuel Type SF50_FM02_0021 2-104 P/N 31452-001 Revision 4...
Page 141 2: L IRRUS ECTION IMITATIONS SF50 ISION THER IMITATIONS Figure 2-32: TKS Fluid SF50_FM02_0024A P/N 31452-001 2-105 Revision 4...
Page 142: Electronic Placards
150 KIAS Seats must be in normal upright position for takeoff and landing. Completely lock all seats in position before flight. Aircraft is equipped with: Cirrus Airframe Parachute System (CAPS), Garmin Electronic Stability and Protec- tion (ESP). 2-106 P/N 31452-001...
Page 143 3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION ABLE ONTENTS Section 3: Emergency Procedures Table of Contents Introduction..................5 Crew Alert System (CAS) Messaging ..........6 Warnings ..................6 Preflight Planning ................6 Preflight Inspections/Maintenance ............ 7 Methodology..................7 Maintain Aircraft Control ..............7 Analyze the Situation...............
Page 144 3: E ECTION MERGENCY ROCEDURES IRRUS SF50 ABLE ONTENTS ISION Emergency Descent ................ 35 Emergency Landing w/o Power............36 Flameout / Precautionary Approach ..........38 Landing Without Aileron Control............39 Landing Without Elevator Control............ 39 Landing Without Rudder Control ............. 39 CAPS Activation ................
Page 145 3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION ABLE ONTENTS OIL FILTER BYPASS Warning - On Ground ........79 OIL PRESSURE Warning ............... 80 OIL TEMPERATURE Warning ............80 STALL WARNING ................81 STICK PUSHER Warning ............... 81 TAKEOFF PITCH TRIM Warning - On Ground ....... 82 THR LEVER CALIBRATION Warning - On Ground ......
Page 146 3: E ECTION MERGENCY ROCEDURES IRRUS SF50 ABLE ONTENTS ISION Intentionally Left Blank P/N 31452-001 Original Issue...
Page 147: Introduction
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION NTRODUCTION Introduction This section provides procedures for handling emergen- cies and critical flight situations that may occur while operating the aircraft. Although emergencies caused by airplane, systems, or engine malfunctions are rare, the guidelines described in this section should be considered and applied as necessary should an emergency arise.
Page 148: Crew Alert System (Cas) Messaging
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 NTRODUCTION ISION Crew Alert System (CAS) Messaging Warnings Displayed in red against a black background, Warning CAS messages arise during emergency situations that require immediate flight crew awareness and immediate flight crew response. •...
Page 149: Preflight Inspections/Maintenance
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION NTRODUCTION Preflight Inspections/Maintenance In-flight mechanical problems in the aircraft will be extremely rare if proper preflight inspections and mainte- nance are practiced. Always perform a thorough walk-around inspection before any flight to ensure that no damage occurred during the previous flight or while the airplane was on the ground.
Page 150: Analyze The Situation
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 NTRODUCTION ISION Analyze the Situation Once you are able to maintain control of the aircraft, assess the situation. Read all warning and caution messages. Evaluate the engine parameters. Consider all aircraft operational information at your disposal. Take Appropriate Action In many situations, the procedures listed in this section will either correct or mitigate the aircraft problem or...
Page 151: Circuit Breakers
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION NTRODUCTION Circuit Breakers Some procedures involve manipulating circuit breakers (CBs). The following criteria should be followed during “Circuit Breaker” steps: • Intentional pulling of circuit breakers during flight, other than as required in specific procedures, is prohibited.
Page 152: Procedure Division Symbols
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 NTRODUCTION ISION Procedure Division Symbols For procedures requiring pilot decision, conditional steps are indented with a symbol to designate sub-sections within the procedure. On condition, the pilot makes a decision to identify the applicable sub-section. Following the initial decision, a further sub-division of the proce- dure may occur.
Page 153: Landing Guidance
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION NTRODUCTION Landing Guidance Land as soon as practicable Extended flight is not recommended and the pilot should proceed to land the plane, but not necessarily at the first or closest landing location. The landing location and duration of flight remains at the discretion of the pilot in command, after considering all factors related to the safety of the flight.
Page 154: Airspeeds For Emergency Operations
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 IRSPEEDS FOR MERGENCY PERATIONS ISION Airspeeds for Emergency Operations Maneuvering Speed 6000 lb (2721 kg)............ 150 KIAS Emergency Landing Flaps UP ..............100 KIAS Flaps 50% ..............95 KIAS Flaps 100% ............... 90 KIAS Best Glide (Gear and Flaps: UP) 6000 lb (2722 kg)............
Page 155: Glide
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION IRSPEEDS FOR MERGENCY PERATIONS Glide Conditions Example Power Altitude 20,000 ft. AGL Flaps Glide Distance 48.4 NM Wind Zero Gear Figure 3-1: Maximum Glide Ratio ~ 14.7: 1 28000 24000 20000 16000 12000 8000 4000...
Page 156: Emergency Procedures
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION Emergency Procedures Engine Emergency On Takeoff - Speed Below V • N • Includes emergencies such as engine failure or fire. Brakes .....MAX. PILOT EFFORT W/O SKIDDING Thrust Lever..............IDLE Engine Knob ..............OFF Engine Button ......PRESS (MOMENTARY) ◆...
Page 157 3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION MERGENCY ROCEDURES (Continued) After airplane comes to a complete stop: Brakes ............COOL DOWN Procedure Complete • CAUTION • For maximum brake effectiveness, retract flaps, hold side stick control full back, and bring the airplane to a stop by smooth, even application of the brakes.
Page 158: Engine Fire On Takeoff - Low Altitude
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION Engine Fire On Takeoff - Low Altitude Land as soon as possible. Procedure Complete ◆ If immediate landing is not possible: a. Perform ENGINE FIRE Warning - In Flight checklist. Procedure Complete •...
Page 159: Engine Failure On Takeoff - Low Altitude
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION MERGENCY ROCEDURES Engine Failure On Takeoff - Low Altitude Best Glide or Landing Speed ....... 100 KIAS Landing Gear..............A/R Flaps..................A/R Land straight ahead. ◆ If time permits: a. Engine Knob..................OFF b. Engine Button ..........PRESS (MOMENTARY) c.
Page 160 3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION (Continued) • N • When determined that a forced landing is the safest option, a suitable landing site should be chosen as early as possible so that maximum time will be available to plan and execute the forced landing.
Page 161: Rejected Takeoff
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION MERGENCY ROCEDURES Rejected Takeoff Brakes ..... MAX. PILOT EFFORT W/O SKIDDING Thrust Lever ..............IDLE After airplane comes to a complete stop: Brakes ............COOL DOWN Procedure Complete • CAUTION • For maximum brake effectiveness, retract flaps, hold side stick control full back, and bring the airplane to a stop by smooth, even application of the brakes.
Page 162: Engine Failure In Flight
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION Engine Failure In Flight Pitch for air start ....AIRSPEED 120 - 200 KIAS Turn toward possible landing site(s). Oxygen Masks (above 15,000 ft)....DON, 100% MIC SELECT Switch ........MASK MIC •...
Page 163 CAPS activation may be the safest option. Refer to the CAPS Activation checklist in this section. Refer to Section 10: Safety Information, "Cirrus Airframe Parachute System (CAPS)" for CAPS deployment scenarios and landing considerations. P/N 31452-001...
Page 164: Uncontained Engine Failure (Rotor Burst In Flight)
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION Uncontained Engine Failure (Rotor Burst in Flight) Pitch for 120 KIAS (APPROX.) Turn toward possible landing site(s). Oxygen Masks (above 15,000 ft)....DON, 100% MIC SELECT Switch ........MASK MIC ENGINE FIRE ACKNOWLEDGE Switch....LIFT GUARD, TOGGLE Left &...
Page 165 3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION MERGENCY ROCEDURES (Continued) • N • This condition is identified by complete loss of thrust accompanied by the following: Loud bangs, knocks, vibration, or other noise, or Engine Fire Indication (CAS Warning and/or FIRE light), or Fire Detector Fail (CAS Caution), or Erratic engine indications, such as the following:...
Page 166: Loss Of All Flight Displays
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION Loss of All Flight Displays EMER BATT Switch............ON • N • With the EMER BATT Switch turned ON and GEN 1 and GEN 2 inoperative, the autopilot and the displays on the MFD and GTC 3 will be unavailable.
Page 167 3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION MERGENCY ROCEDURES (Continued) • Landing gear control (To lower landing gear, perform Alternate Gear Extension checklist) • Flaps control (Perform Flaps Inoperative Approach/Landing checklist) • Cabin pressure control (Perform CABIN PRESSURE CTRL FAIL Caution checklist) •...
Page 168: Loss Of Thrust Control
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION Loss of Thrust Control Shut down engine, if required. Flaps ................. A/R Landing Gear ..............A/R Land as soon as practicable. Procedure Complete ◆ If the thrust lever is stuck at, or near, the T/O detent: a.
Page 169: Abnormal Engine Start
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION MERGENCY ROCEDURES Abnormal Engine Start Engine Knob..............OFF Engine Button ... PRESS AND HOLD 15 - 30 SECONDS See Powerplant Limitations and Outside Air Tempera- ture Limits in Section 2: Limitations for corrective actions.
Page 170: Air Start
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION Air Start Airspeed ............120 - 200 KIAS Altitude...............< 18,000 FT Thrust Lever..............IDLE Engine reset: Engine Knob ..............OFF Engine Button ......PRESS (MOMENTARY) N2............WAIT UNTIL < 24% ◆ If time permits: a.
Page 171 3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION MERGENCY ROCEDURES (Continued) • CAUTION • Probability of engine restart is greater when N2 < 16%. Do not attempt a restart until N2 < 24%. See Section 2: Limitations, Engine Start (In flight) for Engine Air Start envelope.
Page 172: Smoke Removal
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION Smoke Removal Crew Oxygen Mask(s)........DON, EMER Smoke Goggles (if equipped) ........DON MIC SELECT Switch ........MASK MIC Instruct passenger(s) to don mask(s). DEFOG Button ............... ON CABIN PRESSURE DUMP Button......PRESS •...
Page 173 3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION MERGENCY ROCEDURES (Continued) Land as soon as possible. Oxygen Masks ........ADJUST TO NORM AT OR BEFORE 10 MINUTES OF 100% USAGE Procedure Complete • WARNING • Regardless of smoke evidence, if there is no visual confirmation that fire has been extinguished following fire suppression and/or smoke evacuation, land as soon as possible.
Page 174: Cabin Fire In Flight
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION Cabin Fire In Flight Crew Oxygen Mask(s)........DON, 100% Smoke Goggles (if equipped) ........DON MIC SELECT Switch ........MASK MIC BAT 1 Switch ..............OFF GEN 1 and GEN 2 Switches .........OFF Fire Extinguisher............
Page 175 3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION MERGENCY ROCEDURES (Continued) • N • With BAT and GEN switches OFF, engine will continue to run. However, no electrical power will be available. If the airplane is in IMC, turn GEN 1, GEN 2, and BAT 1 switches OFF.
Page 176: Ditching
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION Ditching Radio......TRANSMIT (ATC OR 121.5 MHZ) MAYDAY WITH LOCATION & INTENTIONS Transponder ..........SQUAWK 7700 ELT..................ON Landing Gear ..............UP Flaps ......... 100% (RECOMMENDED) CABIN PRESSURE DUMP Button......PRESS Airspeed .................V Rate of Descent....200 - 300 FEET PER MINUTE Align approach parallel to swells and attempt to touch- down along a wave crest or behind it.
Page 177: Emergency Descent
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION MERGENCY ROCEDURES (Continued) Airplane............EVACUATE • WARNING • Evacuate via either egress window or main cabin door. However, main cabin door evacuation shall be done only via the upper cabin door. To avoid flooding the airplane, do not open lower cabin door.
Page 178: Emergency Landing W/O Power
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION Emergency Landing w/o Power Airplane Control ..........MAINTAIN Pitch for glide speed. Turn toward nearest practical landing site. Radio......TRANSMIT (ATC OR 121.5 MHZ) MAYDAY WITH LOCATION & INTENTIONS Transponder ..........SQUAWK 7700 ◆...
Page 179 Refer to the CAPS Activation checklist in this section. Refer to Section 10: Safety Information, "Cirrus Airframe Parachute System (CAPS)" for CAPS deployment scenarios and landing considerations. When determined that a forced landing is the safest...
Page 180: Flameout / Precautionary Approach
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION Flameout / Precautionary Approach POSITION ALTITUDE AIRSPEED High-Key 3000 ft AGL 115-130 KIAS Low-Key 1500 ft AGL 120 KIAS Base Leg 1000 ft AGL 120 KIAS • N • Gear down and flaps when landing is assured. Airspeed 110 KIAS (minimum until short final).
Page 181: Landing Without Aileron Control
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION MERGENCY ROCEDURES Landing Without Aileron Control Flaps................50% Trim................V Thrust Lever ..............A/R Use rudder as necessary to align the aircraft with the runway. Procedure Complete Landing Without Elevator Control Use manual trim wheel to control pitch attitude. Flaps.................
Page 182: Caps Activation
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION CAPS Activation • WARNING • The recommended CAPS activation speed is one that is less than 135 KIAS and 145 KTAS, whichever is lower, which will result in immediate parachute deployment once the CAPS handle is pulled.
Page 183 3: E IRRUS ECTION MERGENCY ROCEDURES SF50 ISION MERGENCY ROCEDURES • WARNING • Jerking or rapidly pulling the CAPS activation handle will greatly increase the pull forces required to activate the rocket. Use a firm and steady pulling motion – a “chin-up” type pull ensures successful activation.
Page 184: Emergency Ground Egress
3: E ECTION MERGENCY ROCEDURES IRRUS SF50 MERGENCY ROCEDURES ISION • N • In the event the cabin remains pressurized at touchdown, the egress hatch may not be removable. After touchdown with the landing gear up, the lower half of the clamshell cabin door will not completely open with the belly of the aircraft resting on the ground.
Page 185: Emergency Cas Procedures
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES Emergency CAS Procedures AUTO DESCENT Warning AUTO DESCENT Aircraft descending to 14,000FT. To cancel auto descent, disconnect the autopilot: a. AP Disconnect ..........PRESS AND RELEASE Procedure Complete CABIN ALTITUDE HIGH Warning CABIN ALTITUDE HIGH Cabin high altitude detected.
Page 186: Cabin Diff Pressure High Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION CABIN DIFF PRESSURE HIGH Warning CABIN DIFF PRESSURE HIGH Cabin differential pressure is too high. Oxygen Masks ........... DON, 100% BLEED Switch ............FRESH L / R MIC Switches ........... MASK MIC Perform Emergency Descent checklist as required.
Page 187: Cabin Dump Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES CABIN DUMP Warning CABIN DUMP Cabin pressure dump activated. • N • If the CABIN PRESSURE DUMP Button was inadver- tently activated, it should be deactivated immediately. Autopilot Emergency Descent Mode (EDM) is disabled when the cabin dump switch is activated.
Page 188: Caps Activated Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION CAPS ACTIVATED Warning CAPS ACTIVATED CAPS sequence has been activated. ◆ If message is displayed due to CAPS activation (pulling of CAPS Activation Handle): a. Refer to CAPS Activation procedure. Procedure Complete •...
Page 189: Door Open Baggage Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES DOOR OPEN BAGGAGE Warning DOOR OPEN BAGGAGE Baggage door is open. ◆ If in flight: a. Land as soon as practicable. Procedure Complete ◆ If on ground: a. Verify baggage door is closed. Procedure Complete P/N 31452-001 3-47...
Page 190: Door Open Main Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION DOOR OPEN MAIN Warning DOOR OPEN MAIN Main door is open. ◆ If in flight: a. Airplane Control ..............MAINTAIN b. Airspeed ..............LIMIT TO 150 KIAS c. Altitude ............AS LOW AS PRACTICAL d.
Page 191: Emer Bus Volts Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES EMER BUS VOLTS Warning EMER BUS VOLTS Operating on emergency power. ◆ If GENERATOR 1 CURRENT OR GENERATOR 2 CURRENT CAS is also displayed: a. Perform GENERATOR 1 CURRENT OR GENERATOR 2 CURRENT procedure prior to performing remainder of EMER BUS VOLTS procedure.
Page 192 3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION (Continued) • N • FUEL VALVE #2 FAIL Caution will be displayed during normal tank AUTO selection since the secondary valve is not powered by emergency power. With EMER BATT switched on and GEN 1 and GEN 2 inoperative, power will be removed from the entire main bus, including the essential bus and hydraulic power- pack.
Page 193 3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES (Continued) • Optional equipment (such as Traffic/TCAS, XPonder2, Radar, EVS, ADS-B/UAT,115VAC PWR, Iridium WIFI Data, DME, ADF, XM Data, and Yaw Damper) • Autopilot Servos, Roll Trim, and Pitch Trim •...
Page 194 3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION Emergency Bus Circuit Breakers CIRCUIT BREAKER CIRCUIT BATT1 HOT BUS CONV LIGHTS Interior Lights Controller CAPS A Primary CAPS COPILOT CIRCUIT BREAKER PANEL (ROW D) FUEL VALVE 1 (D5) Fuel Control Valve 1 LANDING GEAR IND (D6) L MLG WOW Sensor...
Page 195 3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES CIRCUIT BREAKER CIRCUIT PILOT CIRCUIT BREAKER PANEL (ROW A) CABIN PRESS 2 (A10) Manual Dump SW & Controller Solenoid Pwr AP CTRL (A7) AP Controller (GMC 707) FIRE PROT 1 (A9) Fire Bottle 1 Fire Prot.
Page 196: Engine Fire Warning - In Flight
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION ENGINE FIRE Warning - In Flight ENGINE FIRE Engine fire detected. Thrust Lever..............IDLE Pitch for 120 KIAS (APPROX.) Wait 15 seconds. ◆ If ENGINE FIRE Warning remains on, or secondary fire indications are present –...
Page 197 3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES (Continued) ◆ If ENGINE FIRE Warning goes out and secondary fire indications are not present – probable bleed leak: a. Thrust Lever .......REDUCE (MINIMUM REQUIRED) b. Land as soon as possible. If time permits: c.
Page 198: Engine Fire Warning - On Ground
ENGINE START N1 N1 is not indicating rotation. ENGINE START N1........ABORT START ◆ If in flight: a. Increase airspeed and retry start procedure. Procedure Complete ◆ If on ground: b. Contact Cirrus for disposition. Procedure Complete 3-56 P/N 31452-001 Revision 4...
Page 199: External Power Connected Warning - On Ground
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES EXTERNAL POWER CONNECTED Warning - On Ground EXTERNAL POWER CONNECTED External power is connected, set park brake. Parking Brake or Brakes ......SET OR HOLD Disconnect external power. Procedure Complete •...
Page 200: Fadec Ctrl Degraded Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION FADEC CTRL DEGRADED Warning FADEC CTRL DEGRADED Reference FADEC Fault Code Messages. FADEC Reset via MFD Controller: a. From Home, touch Aircraft Systems. b. Touch the FADEC Stale Fault Reset Button. ◆...
Page 201: Fadec No Dispatch Warning - On Ground
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES FADEC NO DISPATCH Warning - On Ground FADEC NO DISPATCH Reference FADEC Fault Code Messages. FADEC Reset via MFD Controller: a. From Home, touch Aircraft Systems. b. Touch the FADEC Stale Fault Reset Button. ◆...
Page 202: Flaps Ice Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION FLAPS ICE Warning FLAPS ICE Full flaps prohibited in icing conditions. Flaps ............SET UP OR 50% Procedure Complete • WARNING • Maximum flap deflection in icing conditions is limited to 50%.
Page 203: Fuel Filter Bypass Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES FUEL FILTER BYPASS Warning FUEL FILTER BYPASS Fuel filter diff press too high, bypass impending. Thrust Lever ...REDUCE (MINIMUM REQUIRED) Altitude........MAINTAIN AS POSSIBLE Land as soon as possible. Procedure Complete •...
Page 204: Fuel Imbalance Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION FUEL IMBALANCE Warning FUEL IMBALANCE Fuel imbalance is ≥ 50 gallons. Fuel Quantity/Fuel Remaining ......COMPARE a. Refer to EIS for fuel quantity (based on level sensors). Fuel Control Switch .........FULLEST TANK Airspeed ....MAINTAIN FOR ADEQUATE ROLL CONTROL ◆...
Page 205: Fuel Low Left/Right/Total Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES FUEL LOW LEFT/RIGHT/TOTAL Warning FUEL LOW LEFT FUEL LOW RIGHT FUEL LOW TOTAL Left fuel tank is nearly empty, OR Right fuel tank is nearly empty, OR Total fuel quantity is low. Fuel Quantity............
Page 206: Fuel Pressure Low Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION FUEL PRESSURE LOW Warning FUEL PRESSURE LOW FDU fuel inlet pressure is low. Fuel Control Switch ... SWITCH TO OTHER TANK a. Refer to EIS for current tank selection (AUTO selection shown in white;...
Page 207: Fuel Temp Low Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES FUEL TEMP LOW Warning FUEL TEMP LOW Fuel temperature below operating limit. Fuel Temperature (L / R)........CHECK ◆ If in flight: a. Land as soon as practicable. •...
Page 208: Fuel Valves Both Fail Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION FUEL VALVES BOTH FAIL Warning FUEL VALVES BOTH FAIL Both fuel control valves have failed. Fuel Quantity............CHECK Airspeed ....MAINTAIN FOR ADEQUATE ROLL CONTROL Land as soon as possible. Procedure Complete •...
Page 209: Generator 1 Current Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES GENERATOR 1 CURRENT Warning GENERATOR 1 CURRENT Generator 1 current is too high. GEN 1 Switch ..............OFF GCU Reset via MFD Controller: a. From Home, touch Aircraft Systems. b.
Page 210 3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION (Continued) • N • With Battery 1 and Generator 1 switched off, power will be removed from the entire main bus, including the hydraulic powerpack. The following equipment will also be inoperative: •...
Page 211: Generator 1 Overvoltage Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES GENERATOR 1 OVERVOLTAGE Warning GENERATOR 1 OVERVOLTAGE Generator 1 voltage is high. GEN 1 Switch ..............OFF GCU Reset via MFD Controller: a. From Home, touch Aircraft Systems. b. Touch the GCU Reset Button. ECS DISABLE .............PRESS GEN 1 Switch ..............
Page 212 3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION Main Bus Circuit Breakers CIRCUIT BREAKER CIRCUIT PILOT CIRCUIT BREAKER PANEL (ROW B) Bleed Air Flow Control Valve BLEED AIR FLOW CTRL (B2) Stick Shaker Motor STICK SHAKER (B3) Landing Gear Hydraulics Power LANDING GEAR HYD Control...
Page 213 3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES CIRCUIT BREAKER CIRCUIT AFT CIRCUIT BREAKER PANEL (ROW K) IFE USB (K1) In-Flight Entertainment FADEC A Maintenance Panel, FADEC PANEL (K2) FADEC B Maintenance Panel TRAFFIC (K3) TCAS-1 ADF, DME ADF (K4) FADEC B (K5)
Page 214: Generator 2 Current Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION GENERATOR 2 CURRENT Warning GENERATOR 2 CURRENT Generator 2 current is too high. GEN 2 Switch ............CYCLE GEN 2 Amps......CHECK WITHIN LIMITS ◆ If GEN 2 amps are within limits: a.
Page 215: Generator 2 Overvoltage Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES GENERATOR 2 OVERVOLTAGE Warning GENERATOR 2 OVERVOLTAGE Generator 2 voltage is high. GEN 2 Switch ............CYCLE ◆ If message persists: a. GEN 2 Switch ..................OFF • N •...
Page 216: Itt Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION ITT Warning ITT limits exceeded. ◆ If in flight: a. Thrust Lever................REDUCE b. ITT ...................MONITOR ❍ If message persists: Land as soon as practicable. Procedure Complete ◆ If on ground: a.
Page 217: Ldg Gear Is Up Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES LDG GEAR IS UP Warning LDG GEAR IS UP Landing gear is not down and locked for landing. ◆ If in flight: a. Landing Gear..............CHECK DOWN ❍ If message persists: Perform Alternate Gear Extension checklist.
Page 218: Ldg Gear Selected Up Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION LDG GEAR SELECTED UP Warning LDG GEAR SELECTED UP Ldg gear should be selected down while on ground. ◆ If on ground: a. Do not taxi. b. Landing Gear ..............SELECT DOWN Procedure Complete ◆...
Page 219: N1 Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES N1 Warning N1 speed exceeded. ◆ If in flight: a. Thrust Lever ................REDUCE b. Monitor N1. ❍ If message persists: Land as soon as practicable. Procedure Complete ◆ If on ground: a.
Page 220: N2 Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION N2 Warning N2 speed exceeded. ◆ If in flight: a. Thrust Lever................REDUCE b. Monitor N2. ❍ If message persists: Land as soon as practicable. Procedure Complete ◆ If on ground: a.
Page 221: Oil Chip Detect Warning - On Ground
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES OIL CHIP DETECT Warning - On Ground OIL CHIP DETECT Engine oil debris detected. Shut down engine. Do not dispatch. Procedure Complete • N • Frequent oil chip detect messages during flight may cause the OIL CHIP DETECT Warning to occur on a subsequent flight.
Page 222: Oil Pressure Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION OIL PRESSURE Warning OIL PRESSURE Engine oil pressure exceedance. ◆ If in flight: a. Monitor oil system pressure and temperature. ❍ If message persists: Thrust Lever....REDUCE (MINIMUM REQUIRED) Avoid abrupt thrust lever movements.
Page 223: Stall Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SF50 CAS P ISION MERGENCY ROCEDURES STALL WARNING STALL WARNING Stall warning active. AOA.................REDUCE Thrust Lever ..............T/O Procedure Complete STICK PUSHER Warning STICK PUSHER Stick pusher active. AOA.................REDUCE Thrust Lever ..............T/O Procedure Complete •...
Page 224: Takeoff Pitch Trim Warning - On Ground
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SF50 MERGENCY ROCEDURES ISION TAKEOFF PITCH TRIM Warning - On Ground TAKEOFF PITCH TRIM Pitch trim not in takeoff configuration. Takeoff............... ABORT Pitch Trim ..ADJUST TO TAKEOFF (GREEN BAND) Procedure Complete THR LEVER CALIBRATION Warning - On Ground THR LEVER CALIBRATION...
Page 225 3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 ISION ABLE ONTENTS Section 3A: Abnormal Procedures Table of Contents Introduction..................5 Crew Alert System (CAS) Messaging ..........5 Cautions ..................5 Advisories ..................6 Abnormal Procedures Guidance ............6 Circuit Breakers................. 7 Locating Circuit Breakers ..............
Page 226 3A: A ECTION BNORMAL ROCEDURES IRRUS SF50 ABLE ONTENTS ISION AOA HEAT FAIL Caution ..............27 BLEED AIR Caution ................ 28 BLEED LEAK Caution ..............29 BLEED OFF Caution ............... 30 BLEED OPEN Caution ..............30 BLEED OVERPRESSURE Caution ..........31 CABIN LFE NOT SET Caution ............
Page 227 3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 ISION ABLE ONTENTS FUEL VALVE #1 FAIL Caution............57 FUEL VALVE #2 FAIL Caution............58 FUEL VALVE AUTO FAIL Caution..........59 GENERATOR 1 CURRENT Caution..........60 GENERATOR 2 CURRENT Caution..........63 GROUND IDLE FAIL Caution - On Ground ........64 HYDRAULIC OVERHEAT Caution ..........
Page 228 3A: A ECTION BNORMAL ROCEDURES IRRUS SF50 ABLE ONTENTS ISION STARTER ENGAGED Advisory ............92 STICK PUSHER FAIL Caution ............93 SURFACEWATCH FAIL Advisory........... 94 TAKEOFF FLAPS Caution - On Ground ......... 94 TAKEOFF PITCH TRIM Advisory - On Ground....... 94 TAKEOFF THRUST Caution ............
Page 229: Introduction
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 ISION NTRODUCTION Introduction This section provides procedures for handling abnormal system and/or flight conditions which, if followed, will maintain an acceptable level of airworthiness or reduce operational risk. The guidelines described in this section are to be used when an abnormal condition exists, and should be considered and applied as necessary.
Page 230: Advisories
3A: A ECTION BNORMAL ROCEDURES IRRUS SF50 NTRODUCTION ISION Advisories Displayed in white against a black background, Advisory CAS messages arise during situations that require flight crew awareness and that may require subsequent flight crew response. Abnormal Procedures Guidance Although this section provides procedures for handling most abnormal system and/or flight conditions that could arise in the aircraft, it is not a substitute for proper flight training, thorough knowledge of the airplane, and recog-...
Page 231: Circuit Breakers
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 ISION NTRODUCTION Circuit Breakers Some procedures involve manipulating circuit breakers (CBs). The following criteria should be followed during “Circuit Breaker” steps: • Intentional pulling of circuit breakers during flight, other than as required in specific procedures, is prohibited.
Page 232: Locating Circuit Breakers
3A: A ECTION BNORMAL ROCEDURES IRRUS SF50 NTRODUCTION ISION Locating Circuit Breakers Each circuit breaker panel row and column is labeled for easy reference. Each row is individually labeled A through C (on the Pilot CB panel) and D through F (on the Copilot CB panel).
Page 233: Procedure Division Symbols
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 ISION NTRODUCTION Procedure Division Symbols For procedures requiring pilot decision, conditional steps are indented with a symbol to designate sub-sections within the procedure. On condition, the pilot makes a decision to identify the applicable sub-section. Following the initial decision, a further sub-division of the proce- dure may occur.
Page 234: Landing Guidance
3A: A ECTION BNORMAL ROCEDURES IRRUS SF50 NTRODUCTION ISION Landing Guidance Land as soon as practicable Extended flight is not recommended and the pilot should proceed to land the plane, but not necessarily at the first or closest landing location. The landing location and duration of flight remains at the discretion of the pilot in command, after considering all factors related to the safety of the flight.
Page 235: Abnormal Procedures
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 ISION BNORMAL ROCEDURES Abnormal Procedures Dry Motoring Engine • • NOTE Dry motoring is used to clear the engine of residual fuel following a failed engine start. Thrust Lever ..............IDLE Engine Knob..............OFF BLEED Switch ............FRESH Engine Button ..PRESS AND HOLD 15 - 30 SECONDS Procedure Complete...
Page 236: Flaps Inoperative Approach/Landing
3A: A ECTION BNORMAL ROCEDURES IRRUS SF50 BNORMAL ROCEDURES ISION Flaps Inoperative Approach/Landing ........REFER TO GREEN DONUT Landing Gear ....... DOWN AND LOCKED Procedure Complete • N • Refer to Section 5: Performance Data, "Flaps: UP" for Flaps UP landing distance requirements. 3A-12 P/N 31452-001 Revision 2...
Page 237: Landing With Failed Brakes
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 ISION BNORMAL ROCEDURES Landing With Failed Brakes ◆ If one brake is inoperative: a. Land on the side of runway corresponding to the inoperative brake. b. Maintain directional control using rudder and operational brake. c.
Page 238: Landing With Flat Tire
3A: A ECTION BNORMAL ROCEDURES IRRUS SF50 BNORMAL ROCEDURES ISION Landing With Flat Tire • • WARNING If a flat tire is suspected, do not retract landing gear since it may cause difficulties in extending the gear. Additionally, landings with the gear up are poten- tially more hazardous than with the gear down.
Page 239: Alternate Gear Extension
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 ISION BNORMAL ROCEDURES Alternate Gear Extension Airspeed ..........BELOW 210 KIAS LANDING GEAR HYD CB (B4) ......PULL Landing Gear Handle..........DOWN Alternate Gear Extension Handle ..PULL TO STOP, RESTOW Verify 3 Green, DOWN / LOCKED indications. ◆...
Page 240: Pitch Trim Runaway / Failure
3A: A ECTION BNORMAL ROCEDURES IRRUS SF50 BNORMAL ROCEDURES ISION Pitch Trim Runaway / Failure Red PTRM annunciator on PFD. Grip side stick firmly. AP/TRIM DISC Button......PRESS AND HOLD Pitch Trim ......A/R (MANUAL TRIM WHEEL) PITCH TRIM CB (A1)..........PULL AP/TRIM DISC Button........RELEASE Procedure Complete Roll Trim Runaway / Failure Grip side stick firmly.
Page 241: Jammed Elevator Trim Tab
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 ISION BNORMAL ROCEDURES Jammed Elevator Trim Tab ◆ During Cruise: a. Thrust Lever ..................A/R b. Landing Gear..................A/R c. Airspeed ....MAINTAIN LAST TRIMMED AIRSPEED OR A/R d. Flaps........... UP OR A/R FOR CONDITIONS e.
Page 242: Gear Indication(S) Not Down/Locked
3A: A ECTION BNORMAL ROCEDURES IRRUS SF50 BNORMAL ROCEDURES ISION Gear Indication(s) Not Down/Locked ◆ If in flight: a. Landing Gear ..........CYCLE UP, THEN DOWN ❍ If Landing Gear is down and locked: Monitor landing gear indications. Procedure Complete ❍...
Page 243: Communications Failure
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 ISION BNORMAL ROCEDURES Communications Failure Switches, Controls ........... CHECK Frequency ............. CHANGE Circuit Breakers .............. SET Headset........CHANGE OR SPEAKER Attempt to use oxygen mask microphone or hand-held microphone and cabin speakers. ◆ If Precipitation-static is experienced during flight: a.
Page 244: Flight Through Volcanic Ash
3A: A ECTION BNORMAL ROCEDURES IRRUS SF50 BNORMAL ROCEDURES ISION Flight Through Volcanic Ash • • CAUTION Avoid flying through volcanic ash where possible. Engine Parameters ..........MONITOR ◆ If engine parameters cannot be kept within limits: a. Land as soon as possible. Procedure Complete Abnormal Engine Shutdown On Ground...
Page 245: Afcs Alerts
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 AFCS A ISION LERTS AFCS Alerts For more information on AFCS alerts, refer to SF50 Garmin Cockpit Reference Guide. Autopilot Abnormal Disconnect Red AP flashing on PFD; continuous high-low aural tone. AP DISC Button ......PRESS AND RELEASE Airplane Control ..........MAINTAIN Procedure Complete Autopilot Failure...
Page 246: Pitch Axis Failure
3A: A ECTION BNORMAL ROCEDURES IRRUS AFCS A SF50 LERTS ISION Pitch Axis Failure Red PTCH annunciator on PFD. • N • If the pitch axis fails while autopilot is engaged, the autopilot will disengage as indicated by the red AP flashing on the PFD.
Page 247: Yaw Axis Failure
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 AFCS A ISION LERTS Yaw Axis Failure Red YAW annunciator on PFD. • N • The yaw damper will disconnect, but the autopilot may still be used for vertical and lateral guidance. Some lateral mistrim may become apparent, and manual rudder inputs may be required for turn coordination.
Page 248: Elevator Mistrim Down
3A: A ECTION BNORMAL ROCEDURES IRRUS AFCS A SF50 LERTS ISION Elevator Mistrim Down Yellow (down arrow) ELE annunciator on PFD. • N • Be prepared for out of trim condition if AP is disengaged. Manipulate elevator trim up to eliminate the mistrim condition.
Page 249: Aileron Mistrim Left/Right
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 AFCS A ISION LERTS Aileron Mistrim Left/Right Yellow (left/right arrow) AIL annunciator on PFD. • N • Be prepared for out of trim condition if AP is disengaged. Manipulate aileron trim as required to eliminate the mistrim condition.
Page 250: Abnormal Cas Procedures
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION Abnormal CAS Procedures AOA FAIL Caution AOA FAIL AOA signal invalid. Airspeed .....REFER TO V SPEEDS TABLE Avoid stalls, low airspeed, and uncoordinated or abrupt control inputs. Land as soon as practicable. Procedure Complete Speeds (KIAS) FLAPS...
Page 251: Aoa Heat Fail Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES (Continued) • • WARNING The aircraft is not stall protected. Stalls must be avoided when the AOA is inoperative. Excessive altitude loss may result if the aircraft is stalled. Departure from controlled flight or spin may occur during stall with uncoordinated aileron/rudder inputs.
Page 252: Bleed Air Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION BLEED AIR Caution BLEED AIR ECS bleed air system pressure low or failed. BLEED Switch ......CYCLE FRESH, BLEED WITHIN < 1 SEC Cabin Altitude ............MONITOR ◆ If message extinguishes: a.
Page 253: Bleed Leak Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES BLEED LEAK Caution BLEED LEAK Bleed leak detected in tailcone. Oxygen Masks ..........DON, NORM BLEED Switch ............FRESH L / R MIC Switches........... MASK MIC Wait 15 seconds. ◆ If message extinguishes: a.
Page 254: Bleed Off Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION BLEED OFF Caution BLEED OFF Bleed air is switched to OFF/FRESH. ◆ If bleed is desired OFF: a. No further action required. Procedure Complete ◆ If bleed is not desired OFF: a.
Page 255: Bleed Overpressure Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES BLEED OVERPRESSURE Caution BLEED OVERPRESSURE ECS bleed air system pressure high. ◆ If message extinguishes within 15 seconds and does not recur: a. No further action required. Procedure Complete ◆...
Page 256: Cabin Lfe Not Set Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION CABIN LFE NOT SET Caution CABIN LFE NOT SET Landing field elevation is not set. Input destination airport in flight plan. Manually set Landing Field Elevation on GTC. Procedure Complete CABIN PRESSURE CTRL FAIL Caution CABIN PRESSURE CTRL FAIL...
Page 257: Caps Autopilot Inop Advisory
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES CAPS AUTOPILOT INOP Advisory CAPS AUTOPILOT INOP Minimize CAPS deployment speed. ◆ If in an emergency situation: a. Airspeed ..........MANUALLY REDUCE BELOW 135 KIAS AND 145 KTAS BEFORE DEPLOYING PARACHUTE Procedure Complete CAPS MISCOMPARE Advisory CAPS MISCOMPARE...
Page 258: Door Open Advisory - On Ground
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION DOOR OPEN Advisory - On Ground DOOR OPEN One or more doors are open. Advisory only. No further action required. Procedure Complete DOOR OPEN EMER EXIT Caution DOOR OPEN EMER EXIT Emergency exit door is open.
Page 259: Ecs Bleed Hot Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES ECS BLEED HOT Caution ECS BLEED HOT Bleed supply temperature is too hot. Cabin Temp Knob ...........FULL COLD ◆ If message extinguishes: a. No further action required. Procedure Complete ◆...
Page 260: Ecs Bleed Overheat Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION ECS BLEED OVERHEAT Caution ECS BLEED OVERHEAT Bleed supply temperature is too hot. Cabin Temp Knob .......... FULL COLD ◆ If message extinguishes: a. No further action required. Procedure Complete ◆...
Page 261: Ecs Control Fail Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES ECS CONTROL FAIL Caution ECS CONTROL FAIL ECS controller has failed, OR All cabin temperature sensors have failed, OR All ECS fans in cabin have failed, OR Bleed duct temperature sensor has failed. TEMP BACKUP ............SELECT Cabin Temp Knob ..
Page 262: Ecs Temp Backup Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION ECS TEMP BACKUP Caution ECS TEMP BACKUP Environmental control temperature backup mode. ◆ If TEMP BACKUP mode engaged intentionally: a. Cabin Temp Knob ......ADJUST FOR CABIN COMFORT b. Monitor for ECS BLEED HOT or ECS BLEED OVERHEAT cautions.
Page 263: Edm Disabled Advisory
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES EDM DISABLED Advisory EDM DISABLED Emergency Descent Mode is disabled. Advisory only. No further action required. Procedure Complete EMER BATTERY FAIL Caution EMER BATTERY FAIL Emergency battery power unavailable. Exit IMC as soon as practical.
Page 264: Engine Start Volts Caution - On Ground
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION ENGINE START VOLTS Caution - On Ground ENGINE START VOLTS Battery 1 is below minimum starting voltage. Battery service, preheat and/or charging is required. Procedure Complete ESS BUS VOLTS Caution ESS BUS VOLTS Essential power bus voltage is low, OR Loss of forward essential power bus voltage.
Page 265: External Power Connected Caution - On Ground
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES EXTERNAL POWER CONNECTED Caution - On Ground EXTERNAL POWER CONNECTED External power is connected. • • NOTE Indicates external power is connected. Ensure external power is removed before moving airplane.
Page 266: Fadec No Dispatch Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION FADEC NO DISPATCH Caution FADEC NO DISPATCH Reference FADEC Fault Code Messages. ENG. IPS Switch (OAT < 50 °F) ....VERIFY ON a. Allow sufficient time for ice to clear from inlet probes. FADEC Reset via MFD Controller: a.
Page 267: Fire Detector Fail Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES FIRE DETECTOR FAIL Caution FIRE DETECTOR FAIL Engine fire detector loop low pressure. ◆ If in flight: a. Land as soon as practicable. Procedure Complete ◆ If on ground: a.
Page 268: Fire Ext Low L Advisory
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION FIRE EXT LOW L Advisory FIRE EXT LOW L Pressure is low in the left fire extinguisher. Continue flight. Service aircraft as soon as practical. Procedure Complete FIRE EXT LOW R Advisory FIRE EXT LOW R Pressure is low in the right fire extinguisher.
Page 269: Flaps Disagree Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES FLAPS DISAGREE Caution FLAPS DISAGREE Flaps are not within commanded position limits. • • WARNING Flaps motion is inhibited when a flap position disagree condition exists. Flaps......CYCLE TO DESIRED POSITION ◆...
Page 270: Flaps Fail Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION FLAPS FAIL Caution FLAPS FAIL Flaps system inoperative, OR Flaps position sensor miscompare, OR Flaps sensors failed, position unknown, OR Flaps have not reached the selected position. Place flaps in last known or safe position. FLAPS CB (C2) ............CYCLE ◆...
Page 271: Flight Idle Fail Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES FLIGHT IDLE FAIL Caution FLIGHT IDLE FAIL Engine idle N2 is too low. Maintain at least 70% N2. Land as soon as practicable. Procedure Complete • • CAUTION When N2 <...
Page 272: Fuel Imbalance Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION FUEL IMBALANCE Caution FUEL IMBALANCE Fuel imbalance is ≥ 15 Gallons. Fuel Control Switch ........... AUTO Fuel Quantity/Fuel Remaining ......COMPARE a. Refer to EIS for fuel quantity (based on level sensors). Fuel Control Switch .........FULLEST TANK Airspeed ....MAINTAIN FOR ADEQUATE ROLL CONTROL...
Page 273: Fuel Low Left/Right/Total Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES FUEL LOW LEFT/RIGHT/TOTAL Caution FUEL LOW LEFT FUEL LOW RIGHT FUEL LOW TOTAL Left fuel quantity is low, OR Right fuel quantity is low, OR Total fuel quantity is low. Fuel Quantity............
Page 274: Fuel Pump On Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION FUEL PUMP ON Caution FUEL PUMP ON Fuel pump is ON due to low fuel pressure. Fuel Control Switch ... SWITCH TO OTHER TANK a. Refer to EIS for current tank selection (AUTO selection shown in white;...
Page 275: Fuel Pump On Advisory
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES FUEL PUMP ON Advisory FUEL PUMP ON Fuel pump is ON for normal operations. Advisory only. No further action required. Procedure Complete • N • Fuel pump has been activated due to normal operations, either due to pilot action (selecting L or R tank) or by the avionics due to entering Start Mode.
Page 276: Fuel Selector Fail Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION FUEL SELECTOR FAIL Caution FUEL SELECTOR FAIL Cannot determine fuel selector position. Fuel Control Switch ..CHECK LEFT/AUTO/RIGHT ◆ If control is inoperable in all switch positions: a. Land as soon as possible. Procedure Complete •...
Page 277: Fuel Shutoff Advisory
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES FUEL SHUTOFF Advisory FUEL SHUTOFF Fuel shutoff valve is closed. ENGINE FIRE ACKNOWLEDGE Switch.... CLOSE GUARD Procedure Complete • N • The above procedure opens the fuel shutoff valve. Disregard if fuel shutoff has been intentionally activated.
Page 278: Fuel Shutoff Fail Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION FUEL SHUTOFF FAIL Caution FUEL SHUTOFF FAIL Fuel shutoff valve not in commanded position. ◆ If during normal flight and engine is running: a. Land as soon as practicable. Procedure Complete ◆...
Page 279: Fuel Tank Balanced Advisory
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES FUEL TANK BALANCED Advisory FUEL TANK BALANCED Fuel tank quantity balance has been detected. Advisory only. No further action required. Procedure Complete P/N 31452-001 3A-55 Revision 4...
Page 280: Fuel Temp Low Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION FUEL TEMP LOW Caution FUEL TEMP LOW Fuel temperature is low, increase OAT. Fuel Temperature (L / R) ........CHECK ◆ If in flight: a. Climb or descend to warmer conditions. •...
Page 281: Fuel Valve #1 Fail Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES FUEL VALVE #1 FAIL Caution FUEL VALVE #1 FAIL Fuel Control Valve #1 has failed. Fuel Quantity............CHECK Fuel Control Switch......... FULLEST TANK Fuel Quantity........MAINTAIN BALANCE Land as soon as practicable. Procedure Complete •...
Page 282: Fuel Valve #2 Fail Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION FUEL VALVE #2 FAIL Caution FUEL VALVE #2 FAIL Fuel Control Valve #2 has failed. Fuel Quantity............CHECK Fuel Control Switch ........... AUTO Land as soon as practicable. Procedure Complete •...
Page 283: Fuel Valve Auto Fail Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES FUEL VALVE AUTO FAIL Caution FUEL VALVE AUTO FAIL Auto fuel tank selection failure, use Manual mode. Fuel Quantity............CHECK Fuel Control Switch......... FULLEST TANK Fuel Quantity........MAINTAIN BALANCE Land as soon as practicable.
Page 284: Generator 1 Current Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION GENERATOR 1 CURRENT Caution GENERATOR 1 CURRENT Generator 1 current is low. GEN 1 Switch ..............OFF GCU Reset via MFD Controller: a. From Home, touch Aircraft Systems. b.
Page 285 3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES Main Bus Circuit Breakers CIRCUIT BREAKER CIRCUIT PILOT CIRCUIT BREAKER PANEL (ROW B) Bleed Air Flow Control Valve BLEED AIR FLOW CTRL (B2) Stick Shaker Motor STICK SHAKER (B3) Landing Gear Hydraulics Power LANDING GEAR HYD Control...
Page 286 3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION CIRCUIT BREAKER CIRCUIT AFT CIRCUIT BREAKER PANEL (ROW K) IFE USB (K1) In-Flight Entertainment FADEC A Maintenance Panel, FADEC PANEL (K2) FADEC B Maintenance Panel TRAFFIC (K3) TCAS-1 ADF, DME ADF (K4) FADEC B (K5)
Page 287: Generator 2 Current Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES GENERATOR 2 CURRENT Caution GENERATOR 2 CURRENT Generator 2 current is low. GEN 2 Switch ............CYCLE GEN 2 CB (C3) ..........CHECK, SET ◆ If GEN 2 resets: a.
Page 288: Ground Idle Fail Caution - On Ground
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION GROUND IDLE FAIL Caution - On Ground GROUND IDLE FAIL Ground idle is unavailable. Do not dispatch. Procedure Complete • • CAUTION With increased idle speed, idle thrust will be greater than normal.
Page 289: Hydraulic Overheat Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES HYDRAULIC OVERHEAT Caution HYDRAULIC OVERHEAT Landing gear hydraulic power pack has overheated. ◆ If HYDRAULIC OVERHEAT Caution CAS is accompanied by LDG GEAR FAIL Caution CAS: a. Refer to LDG GEAR FAIL Caution checklist. Procedure Complete ◆...
Page 290 3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION (Continued) • N • FUEL VALVE #2 FAIL Caution CAS will be periodi- cally displayed during normal tank AUTO selection since the secondary valve is not powered by emergency power.
Page 291 3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES CIRCUIT BREAKER CIRCUIT COPILOT CIRCUIT BREAKER PANEL (ROW F) YAW SAS (F8) Yaw Servo Convenience Power Relay IFE CTRL (F7) Wi-Fi Datalink, Iridium Satellite IRIDIUM WIFI DATA (F6) AHRS 2, ADC 2 AHRS 2 ADC 2 (F5)
Page 292 3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION CIRCUIT BREAKER CIRCUIT AFT CIRCUIT BREAKER PANEL (ROW l) 115 VAC PWR (L12) DC-AC Inverter ECS BOOST FAN (L1) ECS Booster Fan ECS GROUND FAN (L2) ECS Ground Fan NOSE CIRCUIT BREAKER PANEL (ROW M) NOSE LAND LIGHT Nose Landing Light...
Page 293: Ips Bleed Overheat Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES IPS BLEED OVERHEAT Caution IPS BLEED OVERHEAT Ice protection bleed cooling failure. WING/STAB IPS Switch ..........OFF Thrust Lever ............REDUCE Avoid/exit icing conditions. Procedure Complete IPS ENG INLET OFF Caution IPS ENG INLET OFF Engine IPS should be on.
Page 294: Ips Eng Inlet On Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION IPS ENG INLET ON Caution IPS ENG INLET ON Engine IPS should be off, OR Shutoff solenoid failed to close. ◆ If Engine IPS should be off: a. ENGINE IPS Switch ................OFF Procedure Complete ◆...
Page 295: Ips Eng Inlet Overheat Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES IPS ENG INLET OVERHEAT Caution IPS ENG INLET OVERHEAT Inlet temp higher than required for anti-ice, OR Inlet temp higher than safe levels. ENGINE IPS Switch ..........CYCLE Procedure Complete ◆...
Page 296: Ips Eng Inlet Underpress Advisory - On Ground
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION IPS ENG INLET UNDERPRESS Advisory - On Ground IPS ENG INLET UNDERPRESS Engine IPS bleed flow low with engine at idle. ◆ If in icing conditions: a. Increase engine thrust to extinguish message. Procedure Complete IPS FLUID LOW Caution IPS FLUID LOW...
Page 297: Ips Fluid Low Advisory - On Ground
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES IPS FLUID LOW Advisory - On Ground IPS FLUID LOW IPS fluid below minimum dispatch quantity. Fill IPS fluid as desired. Procedure Complete • N • This CAS message is displayed when IPS fluid quantity ≤...
Page 298: Ips Wing/Stab Fail Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION IPS WING/STAB FAIL Caution IPS WING/STAB FAIL Wing/Stabilizer IPS low system pressure, OR Wing/Stabilizer IPS zonal pressure failure, OR Wing/Stabilizer IPS controller failure, OR Low system pressure, Wing/Stab IPS inoperative. Avoid/exit icing conditions.
Page 299: Ldg Gear Fail Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES LDG GEAR FAIL Caution LDG GEAR FAIL Landing gear didn't reach the selected position. Landing Gear Indications..VERIFY POSITION/LOCK Landing Gear............. CYCLE • N • Even though the gear assemblies are functioning properly, the root cause may be a failure of the gear sensors to indicate properly (Down/Up or Locked/Unlocked).
Page 300: Ldg Gear Selector Fail Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION LDG GEAR SELECTOR FAIL Caution LDG GEAR SELECTOR FAIL Cannot determine landing gear selector position. Landing Gear .............CYCLE ◆ If message extinguishes: a. No further action required. Procedure Complete ◆...
Page 301: Main Bus Volts Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES MAIN BUS VOLTS Caution MAIN BUS VOLTS Loss of forward main power bus voltage, OR Main power bus voltage is low. Perform Checklist. GENERATOR 1 CURRENT Caution Procedure Complete •...
Page 302: Mute Active Advisory
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION MUTE ACTIVE Advisory MUTE ACTIVE Master silence muting is active. Advisory only. No further action required. Procedure Complete OIL FILTER BYPASS Caution OIL FILTER BYPASS Oil filter diff press too high, bypass impending. Avoid abrupt thrust lever movements.
Page 303: Oxygen Off Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES OXYGEN OFF Caution OXYGEN OFF Oxygen has not been turned on. OXYGEN MASTER Switch ......VERIFY ON ◆ If OXYGEN MASTER Switch on bolster panel is switched ON: a.
Page 304: Oxygen On Caution - On Ground
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION OXYGEN ON Caution - On Ground OXYGEN ON Oxygen is on. OXYGEN MASTER Switch......VERIFY OFF ◆ If message persists: a. OXYGEN CREW CB (E7)............ VERIFY SET b. OXYGEN CREW CB (E7).............CYCLE c.
Page 305: Oxygen On Advisory - On Ground
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES OXYGEN ON Advisory - On Ground OXYGEN ON Oxygen is on. Advisory only. No further action required. Procedure Complete • N • This CAS message is displayed while taxiing after landing.
Page 306: Oxygen Pressure Dispatch Caution - On Ground
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION OXYGEN PRESSURE DISPATCH Caution - On Ground OXYGEN PRESSURE DISPATCH Oxygen below required dispatch pressure. Fill oxygen bottle per Section 2: Limitations, Fill Pressure vs. Temperature. • N •...
Page 307: Park Brake Caution - On Ground
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES PARK BRAKE Caution - On Ground PARK BRAKE Parking brake is set. Parking Brake ..............A/R Procedure Complete PROBE HEAT FAIL L Caution PROBE HEAT FAIL L Left probe heat failure. PROBE HT LEFT CB (A8)........
Page 308: Probe Heat Fail R Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION PROBE HEAT FAIL R Caution PROBE HEAT FAIL R Right probe heat failure. PROBE HT RIGHT CB (E4) ........CYCLE ◆ If message extinguishes: a. No further action required. Procedure Complete ◆...
Page 309: Probe Heat Off Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES PROBE HEAT OFF Caution PROBE HEAT OFF Probe heat is required. Probe Heat Switch ............ON ◆ If message extinguishes: a. No further action required. Procedure Complete ◆ If message persists, and icing encountered: a.
Page 310: Sfd Alt Miscompare Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION SFD ALT MISCOMPARE Caution SFD ALT MISCOMPARE SFD altitude miscompare. DISPLAY BACKUP Button ......... SELECT Altitude ......CROSSCHECK SFD WITH PFD Altitude ... CROSSCHECK PFD ADC #1 WITH ADC #2 •...
Page 311: Sfd Ias Miscompare Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES SFD IAS MISCOMPARE Caution SFD IAS MISCOMPARE SFD airspeed miscompare. DISPLAY BACKUP Button ........SELECT Airspeed ....... CROSSCHECK SFD WITH PFD Airspeed .. CROSSCHECK PFD ADC #1 WITH ADC #2 •...
Page 312: Sfd Pitch Miscompare Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION SFD PITCH MISCOMPARE Caution SFD PITCH MISCOMPARE SFD pitch miscompare. DISPLAY BACKUP Button ........SELECT Attitude ......CROSSCHECK SFD WITH PFD Attitude....CROSSCHECK PFD AHRS #1 WITH AHRS #2 •...
Page 313: Sfd Roll Miscompare Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES SFD ROLL MISCOMPARE Caution SFD ROLL MISCOMPARE SFD roll miscompare. DISPLAY BACKUP Button ........SELECT Attitude ......CROSSCHECK SFD WITH PFD Attitude ....CROSSCHECK PFD AHRS #1 WITH AHRS #2 •...
Page 314: Stall Speed High Advisory
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION STALL SPEED HIGH Advisory STALL SPEED HIGH Stall protection system adjusted for icing. ◆ If airframe is no longer ice contaminated: a. IPS Stall Offset Reset via MFD Controller: From Home, touch Aircraft Systems.
Page 315: Stall Warning Fail Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES STALL WARNING FAIL Caution STALL WARNING FAIL Stall warning failure. Airspeed ........ MAINTAIN ABOVE 1.3 V Avoid stalls, low airspeed, and uncoordinated or abrupt control inputs. Land as soon as practicable. Procedure Complete •...
Page 316: Starter Engaged Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION STARTER ENGAGED Caution STARTER ENGAGED Starter will not disengage (start relay stuck). Start ................ABORT GCU Reset via MFD Controller: a. From Home, touch Aircraft Systems. b. Touch the GCU Reset Button. BAT 1 Switch ..............
Page 317: Stick Pusher Fail Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES STICK PUSHER FAIL Caution STICK PUSHER FAIL Stick pusher failure. Airspeed ........ MAINTAIN ABOVE 1.3 V Avoid stalls, low airspeed, and uncoordinated or abrupt control inputs. Land as soon as practicable. Procedure Complete •...
Page 318: Surfacewatch Fail Advisory
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION SURFACEWATCH FAIL Advisory SURFACEWATCH FAIL SurfaceWatch failed. • N • SurfaceWatch is unavailable. Procedure Complete TAKEOFF FLAPS Caution - On Ground TAKEOFF FLAPS Flaps not in takeoff configuration. Flaps ............CHECK POSITION Procedure Complete TAKEOFF PITCH TRIM Advisory - On...
Page 319: Takeoff Thrust Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES TAKEOFF THRUST Caution TAKEOFF THRUST 5 minute takeoff thrust limitation exceeded. Thrust Lever ..............MCT Procedure Complete • • CAUTION Engine operating costs are predicated on a maximum of 2 minutes of takeoff thrust on an average flight.
Page 320: Takeoff Thrust Advisory
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION TAKEOFF THRUST Advisory TAKEOFF THRUST Engine is in takeoff thrust. Thrust Lever..............MCT Procedure Complete • • CAUTION Engine operating costs are predicated on a maximum of 2 minutes of takeoff thrust on an average flight. Exceeding 5 minutes of takeoff thrust may disproportionately increase engine operating costs.
Page 321: Tcv Control Fail Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES TCV CONTROL FAIL Caution TCV CONTROL FAIL TCV motor controller has failed. Cabin Temperature ........... MONITOR • N • TCV will typically fail open resulting in colder than normal cabin temperatures.
Page 322 3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION (Continued) ◆ If message persists and cabin temperature is colder than acceptable: a. Altitude..DESCEND TO WARMER OUTSIDE AIR TEMPERA- TURE, IF PRACTICAL b. Land as soon as practicable. Procedure Complete •...
Page 323: Throttle Servo Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES THROTTLE SERVO Caution THROTTLE SERVO Throttle servo has failed. • N • Automatic thrust functions, including thrust lock, will be unavailable. CAPS activation will require manual retard of thrust lever to IDLE.
Page 324: Wow Disagree Advisory
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION WOW DISAGREE Advisory WOW DISAGREE WOW indicating opposite on ground/in air states. Continue flight. Procedure Complete • N • When WOW disagrees, avionics determines ground/in-air state based on airspeed. Expect GROUND IDLE FAIL Caution after landing.
Page 325: Wow Fail Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SF50 CAS P ISION BNORMAL ROCEDURES WOW FAIL Caution WOW FAIL WOW is indicating on ground state. Maintain at least 70% N2. Land as soon as practicable. Procedure Complete • • WARNING If above 10,000 ft, expect CABIN ALTITUDE Warning and aircraft to depressurize.
Page 326: Yaw Sas Servo Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SF50 BNORMAL ROCEDURES ISION YAW SAS SERVO Caution YAW SAS SERVO Yaw SAS servo has failed. ◆ If in flight: a. Limit flaps to 0% or 50% in landing configuration. Flaps Inoperative Approach/Landing b.
Page 327: Section 4: Normal Procedures
4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION ABLE ONTENTS Section 4: Normal Procedures Table of Contents Introduction..................3 Normal Procedures ................4 Preflight Inspection................4 Before Engine Start ................. 14 Engine Start..................15 Before Taxi ..................18 Before Takeoff................. 20 Normal Takeoff................
Page 328 4: N ECTION ORMAL ROCEDURES IRRUS SF50 ABLE ONTENTS ISION Intentionally Left Blank P/N 31452-001 Revision 3...
Page 329: Introduction
IRRUS ECTION ORMAL ROCEDURES SF50 ISION NTRODUCTION Introduction This section provides amplified procedures for normal operation of the Vision SF50 aircraft. • • NOTE Refer to Section 9: Log of Supplements for optional equipment Normal Procedures. P/N 31452-001 Original Issue...
Page 330: Normal Procedures
4: N ECTION ORMAL ROCEDURES IRRUS SF50 ORMAL ROCEDURES ISION Normal Procedures Preflight Inspection • • WARNING Before carrying out preflight inspections, ensure that all required maintenance has been accomplished. Review your flight plan and compute weight and balance and performance requirements. Throughout the walk-around: check all hinges, hinge pins, and bolts for security;...
Page 331 4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION ORMAL ROCEDURES (Continued) Figure 4-1: Recommended Walk-Around Sequence SF50_FM04_0010 (Continued on next page) P/N 31452-001 Original Issue...
Page 332 4: N ECTION ORMAL ROCEDURES IRRUS SF50 ORMAL ROCEDURES ISION (Continued) Cabin a. Cabin Door ... CHECK HINGE, LATCH AND SEAL CONDITION AND OPERATION b. Egress Window......SECURED AND PIN REMOVED c. Seats ............SECURED AND LOCKED Crew Seats ..LATCHED (FLIGHT RANGE POSITION) Passenger Seats ..GRAB TOP, ROCK FORWARD AND AFT Seat Levers, Latches.........VISUALLY INSPECT Latch Pins (Child Seats) ......VISUALLY INSPECT...
Page 333 4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION ORMAL ROCEDURES (Continued) p. BAT 1 Switch..................ON Verify ENGINE START VOLTS CAS message not present. • • NOTE If ENGINE START VOLTS CAS message is displayed, perform ENGINE START VOLTS Caution - On Ground checklist.
Page 334 4: N ECTION ORMAL ROCEDURES IRRUS SF50 ORMAL ROCEDURES ISION (Continued) aa. Fuel Control Switch ..............AUTO Verify white L or R selection box is displayed in the fuel section of the EIS. ab. BAT 1 and BAT 2 Switches ..............OFF •...
Page 335 4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION ORMAL ROCEDURES (Continued) Left Wing Trailing Edge and Left Main Gear a. LH Aileron, Roll Trim Tab......CONDITION, MOTION b. LH Wing BLE Top, Bottom (if installed) ........ CHECK c. LH Aileron Fence (if installed) ..........CHECK d.
Page 336 4: N ECTION ORMAL ROCEDURES IRRUS SF50 ORMAL ROCEDURES ISION (Continued) Left Fuselage a. Baggage Circuit Breaker Panel ....... CHECK AND SET b. Baggage............... CHECK, SECURE c. Baggage Door ................SECURE d. External Power Service Door ...........SECURE e. Static Ports ..................CLEAR f.
Page 337 4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION ORMAL ROCEDURES (Continued) Empennage a. Engine Nozzle ................INSPECT b. Second LP Turbine ..............INSPECT • N • When inspecting the LP Turbine, look for Foreign Object Damage (FOD), overall damage, cracks, defor- mation, and evidence of pooled liquid (water, fuel, oil, etc.).
Page 338 4: N ECTION ORMAL ROCEDURES IRRUS SF50 ORMAL ROCEDURES ISION (Continued) Right Wing Trailing Edge and Right Main Gear a. RH MLG Brakes, Wheel and Tire........CONDITION Brake Pads..........VISUALLY INSPECT FRICTIONAL MATERIAL Center channel indicates thickness is greater than wear limit. Edges are free from voids or large sections of material missing.
Page 339 4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION ORMAL ROCEDURES (Continued) Right Wing Tip a. RH Wing Tip, Strobe/Nav Lights.....CONDITION, SECURITY b. Pitot Probe..........CLEAR, COVER REMOVED Right Forward Wing a. RH Fuel Cap ......CHECK FUEL LEVEL AND SECURE b. RH Fuel Tank Drain..............SAMPLE c.
Page 340: Before Engine Start
4: N ECTION ORMAL ROCEDURES IRRUS SF50 ORMAL ROCEDURES ISION Before Engine Start • • CAUTION Before starting engine, ensure batteries that have been cold soaked for 2 hours or more at an ambient temperature of 0 °F (-18 °C) or lower are preheated above 0 °F (-18 °C).
Page 341: Engine Start
4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION ORMAL ROCEDURES Engine Start • • CAUTION Point nose of the aircraft into the wind. If this is not possible (and if the speed of the tailwind component exceeds 10 knots), do not operate engine N1 speed above 60% until the aircraft rolling speed is greater than the tailwind component.
Page 342 4: N ECTION ORMAL ROCEDURES IRRUS SF50 ORMAL ROCEDURES ISION (Continued) Strobe Lights ..............ON CAS Messages............CHECK Thrust Lever..............IDLE Brakes ................. HOLD Engine Knob ..............RUN Fuel Pump ..............CHECK a. Verify FUEL PUMP ON Advisory CAS is displayed. b.
Page 343 4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION ORMAL ROCEDURES (Continued) EIS..........CHECK ALL NORMAL External GPU ..........DISCONNECT Engine IPS................A/R • N • The BLEED switch should not be set to BLEED until BAT 1 and BAT 2 have been ON for 2 minutes or more. BLEED Switch ............BLEED ECS Control Panel............SET P/N 31452-001...
Page 344: Before Taxi
4: N ECTION ORMAL ROCEDURES IRRUS SF50 ORMAL ROCEDURES ISION Before Taxi • • WARNING When operating aircraft on the ground in snow or icing conditions, N2 should be increased to 70% for 30 seconds every 10 minutes to ensure the inlet remains clear of ice.
Page 345 4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION ORMAL ROCEDURES (Continued) Trim................CHECK Flaps................. 50% Electric Roll Trim ..VERIFY MOTION, LEFT AND RIGHT TO/GA Button ............PRESS GEN 1 and GEN 2 Switches ......... OFF BAT 2 Switch..............OFF EIS........CHECK EMER BUS VOLTAGE •...
Page 346: Before Takeoff
4: N ECTION ORMAL ROCEDURES IRRUS SF50 ORMAL ROCEDURES ISION Before Takeoff • • WARNING When operating aircraft on the ground in snow or icing conditions, N2 should be increased to 70% for 30 seconds every 10 minutes to ensure the inlet remains clear of ice.
Page 347 4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION ORMAL ROCEDURES (Continued) • • WARNING Takeoff is prohibited with any frost (polished or not), ice, snow, or slush adhering to the wings, stabi- lizers, control surfaces, engine inlet, or fuselage forward of the engine inlet. A tactile inspection in accordance with Section 2, Limitations, must be accomplished no more than 5 minutes prior to takeoff when operating in ground icing conditions.
Page 348: Normal Takeoff
4: N ECTION ORMAL ROCEDURES IRRUS SF50 ORMAL ROCEDURES ISION Normal Takeoff Brakes ................. HOLD Thrust Lever..............T/O Thrust Setting (N1% Indicator) ..ALIGNED w/ BUG (T) Engine Instruments ......CHECK NORMAL Brakes ..............RELEASE ................ 80-90 KIAS Pitch Attitude ..............5° Landing Gear ..UP w/ POSITIVE RATE OF CLIMB Flaps ....UP AT 115 KIAS, CLEAR OF OBSTACLES Airspeed ..........PER CLIMB TABLES...
Page 349: Climb
4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION ORMAL ROCEDURES Climb • • CAUTION Thrust set to Takeoff thrust is limited to 5 minutes maximum. If practical, reduce to MCT within 2 minutes of selecting Takeoff thrust. Engine life and maintenance costs are contingent upon observing the 2-minute limit of Takeoff thrust for every 72 minutes of flight.
Page 350: Descent
4: N ECTION ORMAL ROCEDURES IRRUS SF50 ORMAL ROCEDURES ISION Descent Thrust Lever..............A/R Landing Field Elevation ......... CHECK Ice Protection..............A/R Altimeter Transition Altitude .....LOCAL SETTING Seats and Seat Belts ..........SECURE Brake Pressure ............CHECK Approach Approach Briefing .......... COMPLETE All seats must be in normal upright position.
Page 351: Before Landing
4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION ORMAL ROCEDURES Before Landing Landing Gear....... DOWN AND LOCKED Flaps..................A/R Cabin Pressure Diff ........... ~0 PSI WINDSHLD IPS Switch..........OFF • N • IPS fluid decreases flight visibility. Autopilot................. OFF Airspeed ..........V TO V Brake Pressure............
Page 352 4: N ECTION ORMAL ROCEDURES IRRUS SF50 ORMAL ROCEDURES ISION Table 1: Landing Considerations Normal, Gusty, and Crosswind Landing Considerations • Maintain V +10 for all flap configurations Normal (UP, 50%, and 100%). Approaches • AFM weight-adjusted V or green donut on ASI tape are suitable for determining V speed.
Page 353: Go-Around
4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION ORMAL ROCEDURES Go-Around Thrust Lever ..............T/O TO/GA Button ............PRESS Pitch Attitude ..............7 Flaps................. 50% Landing Gear..UP w/ POSITIVE RATE OF CLIMB Airspeed ................V Flaps.... UP AT 115 KIAS, CLEAR OF OBSTACLES Climb Out ....
Page 354: Shutdown
4: N ECTION ORMAL ROCEDURES IRRUS SF50 ORMAL ROCEDURES ISION Shutdown • N • Allow engine to remain at ground idle for 2 minutes (minimum) prior to shutdown for hot section compo- nent temperatures to equalize. Thrust Lever..............IDLE ENGINE IPS Switch ............OFF BLEED Switch ............FRESH OXYGEN MASTER Switch..........OFF Lights ................OFF...
Page 355: Icing Conditions
4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION CING ONDITIONS Icing Conditions Preflight Inspection • • WARNING In cold weather, remove all frost (polished or not), ice, snow, or slush from fuselage, wing, stabilizers, control surfaces, and engine inlet. Ensure that control surfaces are free of internal ice or debris.
Page 356: Before Takeoff
4: N ECTION ORMAL ROCEDURES IRRUS SF50 CING ONDITIONS ISION (Continued) c. Engine Inlet................INSPECT Cabin a. PROBE HEAT Switch ..ON AND CHECK NO CAS THEN OFF b. ICE Light .....................OFF c. BAT 1 and BAT 2 Switches..............OFF Before Takeoff ENGINE IPS Switch ...
Page 357: Ips Activation
4: N IRRUS ECTION ORMAL ROCEDURES SF50 ISION CING ONDITIONS IPS Activation OAT ≤ 41 °F (5 °C) with visible moisture or visibility < 1 mile (1.6 km) In Flight: PROBE HEAT Switch ..........ON ENGINE IPS Switch ..........ON WING/STAB IPS Switch ........OFF WINDSHLD IPS Switch ........
Page 358 4: N ECTION ORMAL ROCEDURES IRRUS SF50 CING ONDITIONS ISION PROBE HEAT Switch ........... ON ENGINE IPS Switch ..........ON WING/STAB IPS Switch ........ON • N • Verify STALL SPEED HIGH CAS Advisory is present. WINDSHLD IPS Switch ........ON •...
Page 359 5: P IRRUS ECTION ERFORMANCE SF50 ISION ABLE ONTENTS Section 5: Performance Data Table of Contents Introduction..................5 Standard Charts .................. 6 Associated Conditions Affecting Performance ........6 Temperature Conversion..............7 OAT for International Standard Atmosphere (ISA) Condition.... 8 Pressure Conversion - Inches of Mercury to Millibars ....... 9 Fuel Quantity Conversion - U.S.
Page 360 5: P ECTION ERFORMANCE IRRUS SF50 ABLE ONTENTS ISION Aircraft Weight: 6000 lb (2722 kg) ..........63 Aircraft Weight: 5500 lb (2495 kg) ..........64 Aircraft Weight: 5000 lb (2268 kg) ..........65 Aircraft Weight: 4500 lb (2041 kg) ..........66 ISA....................
Page 361 5: P IRRUS ECTION ERFORMANCE SF50 ISION ABLE ONTENTS Flaps: 100%, Dry Runway ............153 Flaps: 100%, Wet Runway ............155 Flaps: 50%, Dry Runway ............. 157 Flaps: 50%, Wet Runway ............159 Flaps: 50% (Ice Contaminated Airframe/STALL SPEED HIGH Advi- sory), Dry Runway ..............
Page 362 5: P ECTION ERFORMANCE IRRUS SF50 ABLE ONTENTS ISION Intentionally Left Blank P/N 31452-001 Revision 4...
Page 363: Introduction
5: P IRRUS ECTION ERFORMANCE SF50 ISION NTRODUCTION Introduction Performance data in this section are presented for opera- tional planning so that you will know what performance to expect from the airplane under various ambient and field conditions. Performance data are presented for takeoff, climb, cruise (including range &...
Page 364: Standard Charts
5: P ECTION ERFORMANCE IRRUS SF50 TANDARD HARTS ISION Standard Charts Associated Conditions Affecting Performance Computed performance data in this section are based upon data derived from actual flight testing with the airplane and engine in good condition and using average piloting techniques.
Page 365: Temperature Conversion
5: P IRRUS ECTION ERFORMANCE SF50 ISION TANDARD HARTS Temperature Conversion Temp to Convert Temp to Convert Temp to Convert °C or °F °C or °F °C or °F °C < > °F °C < > °F °C < > °F P/N 31452-001 Revision 4...
Page 366: Oat For International Standard Atmosphere (Isa) Condition
5: P ECTION ERFORMANCE IRRUS SF50 TANDARD HARTS ISION OAT for International Standard Atmosphere (ISA) Condition Press -30 °C -15 °C +15 °C +30 °C Feet °C °F °C °F °C °F °C °F °C °F 1000 2000 3000 4000 5000 -25 -13 -10 6000...
Page 367: Pressure Conversion - Inches Of Mercury To Millibars
5: P IRRUS ECTION ERFORMANCE SF50 ISION TANDARD HARTS Pressure Conversion - Inches of Mercury to Millibars Inches Of Inches Of Millibars Millibars Mercury Mercury 28.0 29.6 1002 28.1 29.7 1006 28.2 29.8 1009 28.3 29.9 1012 28.4 30.0 1016 28.5 30.1 1019...
Page 368: Fuel Quantity Conversion - U.s. Gallons To Liters
5: P ECTION ERFORMANCE IRRUS SF50 TANDARD HARTS ISION Fuel Quantity Conversion - U.S. Gallons to Liters • N • Fuel mass provided for reference assuming nominal 6.76 lb/gallon at 59 °F (15 °C). U.S. Gallons U.S. Gallons Lb (Kg) Lb (Kg) (Liters) (Liters)
Page 369: Weight Conversion - Pounds To Kilograms
5: P IRRUS ECTION ERFORMANCE SF50 ISION TANDARD HARTS Weight Conversion - Pounds to Kilograms Pounds Kilograms Pounds Kilograms 6500 2948 4900 2223 6400 2903 4800 2177 6300 2858 4700 2132 6200 2812 4600 2087 6100 2767 4500 2041 6000 2722 4400 1996...
Page 370: Distance Conversion: Feet To Meters
5: P ECTION ERFORMANCE IRRUS SF50 TANDARD HARTS ISION Distance Conversion: Feet to Meters Feet Meters Feet Meters 1000 2000 3000 4000 1219 5000 1524 6000 1829 7000 2134 8000 2438 9000 2743 10,000 3048 5-12 P/N 31452-001 Original Issue...
Page 371: Length Conversion: Inches To Centimeters
5: P IRRUS ECTION ERFORMANCE SF50 ISION TANDARD HARTS Length Conversion: Inches to Centimeters Inches Centimeters Inches Centimeters 2.54 50.8 5.08 76.2 7.62 101.6 10.16 12.70 142.4 15.24 177.8 17.78 203.2 20.32 228.6 22.86 25.40 27.94 30.48 P/N 31452-001 5-13 Revision 4...
Page 372: Static Source Error Correction
5: P ECTION ERFORMANCE IRRUS SF50 TANDARD HARTS ISION Static Source Error Correction Airspeed Correction Conditions: • Thrust for level flight or MCT, whichever is less. • N • Indicated airspeed values assume zero instrument error. KCAS KIAS Flap Deflection 100% 5-14 P/N 31452-001...
Page 373: Altitude Correction, Flaps: 0
5: P IRRUS ECTION ERFORMANCE SF50 ISION TANDARD HARTS Altitude Correction, Flaps: 0% Conditions: • Thrust for level flight or MCT, whichever is less. • N • Add correction to desired altitude to obtain indicated altitude to fly. Indicated airspeed values assume zero instrument error.
Page 374: Altitude Correction, Flaps: 50
5: P ECTION ERFORMANCE IRRUS SF50 TANDARD HARTS ISION Altitude Correction, Flaps: 50% Conditions: • Thrust for level flight or MCT, whichever is less. • N • Add correction to desired altitude to obtain indicated altitude to fly. Indicated airspeed values assume zero instrument error.
Page 375: Altitude Correction, Flaps: 100
5: P IRRUS ECTION ERFORMANCE SF50 ISION TANDARD HARTS Altitude Correction, Flaps: 100% Conditions: • Thrust for level flight or MCT, whichever is less. • N • Add correction to desired altitude to obtain indicated altitude to fly. Indicated airspeed values assume zero instrument error.
Page 376: Stall Speeds
5: P ECTION ERFORMANCE IRRUS SF50 TANDARD HARTS ISION Stall Speeds STALL SPEEDS (KCAS) AT IDLE Bank Angle Flap Deflection 100% 6000 lb 5550 lb 5200 lb 4800 lb 5-18 P/N 31452-001 Revision 4...
Page 377: Wing/Stab Ips: On
5: P IRRUS ECTION ERFORMANCE SF50 ISION TANDARD HARTS Stall Speeds (Ice Contaminated Airframe/STALL SPEED HIGH Advisory) WING/STAB IPS: ON • N • Actual stick pusher speed is dependent on physical ice accretion. STALL SPEEDS (KCAS) AT IDLE Bank Angle Flap Deflection 6000 lb 5550 lb...
Page 378: Wind Components
5: P ECTION ERFORMANCE IRRUS SF50 TANDARD HARTS ISION Wind Components Example: Runway Heading............... 10° Wind Direction ..............60° Wind Velocity ............15 Knots • N • Maximum demonstrated crosswind is 16 knots for 100% flaps, and 18 knots for 50% flaps. Reduced flap settings enable higher crosswind limits.
Page 379: Takeoff Power Setting (N1)
5: P IRRUS ECTION ERFORMANCE SF50 ISION TANDARD HARTS Takeoff Power Setting (N1) • N • FADEC PT2 and TT2 values are displayed on the FUEL SYNOPTIC page. P/N 31452-001 5-21 Revision 4...
Page 380 5: P ECTION ERFORMANCE IRRUS SF50 TANDARD HARTS ISION Figure 5-2: Takeoff N1, Engine Anti-Ice: OFF Engine Anti-Ice OFF 10 psi 11 psi 12 psi 13 psi 14 psi 9 psi 15 psi 16 psi 17 psi 18 psi TT2 ~ Total Inlet Temperature (°C) SF50_FM05_0049 5-22 P/N 31452-001...
Page 381 5: P IRRUS ECTION ERFORMANCE SF50 ISION TANDARD HARTS Figure 5-3: Takeoff N1, Engine Anti-Ice: ON Engine Anti-Ice ON 10 psi 11 psi 12 psi 13 psi 14 psi 9 psi 15 psi 16 psi 17 psi 18 psi TT2 ~ Total Inlet Temperature (°C) SF50_FM05_0050 P/N 31452-001 5-23...
Page 382: Takeoff Distance
5: P ECTION ERFORMANCE IRRUS SF50 AKEOFF ISTANCE ISION Takeoff Distance Takeoff Weight: 6000 lb (2722 kg) Engine Anti-Ice: A/R Winds ................Calm Runway............Dry, Level, Paved Thrust Lever ..............T/O Landing Gear .............DOWN Flaps.................. 50% BLEED Switch ..............ON Headwind: Subtract 7% from the ground run and 6% from the total distance for every 10 knots of headwind.
Page 383 5: P IRRUS ECTION ERFORMANCE SF50 ISION AKEOFF ISTANCE Takeoff Weight: 6000 lb (2722 kg) Press TEMPERATURE ~°C Distance Feet -20 -10 Feet Gnd Roll 1780 1851 1924 1999 2231 2757 3418 4284 2036 Total 2789 2900 3014 3133 3519 4415 5561 7093 3192 Gnd Roll 1855 1928 2005 2084 2386 2947 3652 4591 2106 1000 Total...
Page 384: Takeoff Weight: 5500 Lb (2495 Kg)
5: P ECTION ERFORMANCE IRRUS SF50 AKEOFF ISTANCE ISION Takeoff Weight: 5500 lb (2495 kg) Engine Anti-Ice: A/R Winds ................Calm Runway............Dry, Level, Paved Thrust Lever ..............T/O Landing Gear .............DOWN Flaps.................. 50% BLEED Switch ..............ON Headwind: Subtract 7% from the ground run and 6% from the total distance for every 10 knots of headwind.
Page 385 5: P IRRUS ECTION ERFORMANCE SF50 ISION AKEOFF ISTANCE Takeoff Weight: 5500 lb (2495 kg) Press TEMPERATURE ~°C Distance Feet -20 -10 Feet Gnd Roll 1632 1697 1763 1833 2045 2528 3133 3927 1867 Total 2458 2555 2656 2761 3099 3885 4887 6227 2812 Gnd Roll 1700 1768 1838 1911 2187 2702 3348 4209 1931 1000 Total...
Page 386: Takeoff Distance: 5000 Lb (2268 Kg)
5: P ECTION ERFORMANCE IRRUS SF50 AKEOFF ISTANCE ISION Takeoff Distance: 5000 lb (2268 kg) Engine Anti-Ice: A/R Winds ................Calm Runway............Dry, Level, Paved Thrust Lever ..............T/O Landing Gear .............DOWN Flaps.................. 50% BLEED Switch ..............ON Headwind: Subtract 7% from the ground run and 6% from the total distance for every 10 knots of headwind.
Page 387 5: P IRRUS ECTION ERFORMANCE SF50 ISION AKEOFF ISTANCE Takeoff Weight: 5000 lb (2268 kg) Press TEMPERATURE ~°C Distance Feet -20 -10 Feet Gnd Roll 1483 1542 1603 1666 1859 2298 2848 3570 1697 Total 2147 2232 2320 2412 2706 3388 4257 5417 2457 Gnd Roll 1546 1607 1671 1737 1988 2456 3044 3826 1755 1000 Total...
Page 388: Enroute Climb
5: P ECTION ERFORMANCE IRRUS SF50 NROUTE LIMB ISION Enroute Climb Climb Gradient Thrust Lever ..............MCT Flaps..................UP Landing Gear ..............UP Anti-ice ................OFF Airspeed ....Per subsequent Climb Gradient table • N • Climb performance data provided results in approximately 95% best rate of climb.
Page 389 5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE LIMB Aircraft Weight Press 6000 lb 5500 lb 5000 lb 4500 lb °C Grad Grad Grad Grad KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 1052 1051 1050 1049 1055 1053 1050 1010 P/N 31452-001 5-31...
Page 390 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE LIMB ISION Aircraft Weight Press 6000 lb 5500 lb 5000 lb 4500 lb °C Grad Grad Grad Grad KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 1042 1041 1040 1037 1035 1033 2000 1029 5-32 P/N 31452-001...
Page 391 5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE LIMB Aircraft Weight Press 6000 lb 5500 lb 5000 lb 4500 lb °C Grad Grad Grad Grad KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 1019 1019 1017 1014 1012 4000 1019 1021 6000 P/N 31452-001...
Page 392 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE LIMB ISION Aircraft Weight Press 6000 lb 5500 lb 5000 lb 4500 lb °C Grad Grad Grad Grad KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 8000 10,000 5-34 P/N 31452-001 Revision 4...
Page 393 5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE LIMB Aircraft Weight Press 6000 lb 5500 lb 5000 lb 4500 lb °C Grad Grad Grad Grad KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 12,000 14,000 P/N 31452-001 5-35 Revision 4...
Page 394 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE LIMB ISION Aircraft Weight Press 6000 lb 5500 lb 5000 lb 4500 lb °C Grad Grad Grad Grad KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 16,000 18,000 5-36 P/N 31452-001 Revision 4...
Page 395 5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE LIMB Aircraft Weight Press 6000 lb 5500 lb 5000 lb 4500 lb °C Grad Grad Grad Grad KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 20,000 22,000 24,000 P/N 31452-001 5-37 Revision 4...
Page 396 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE LIMB ISION Aircraft Weight Press 6000 lb 5500 lb 5000 lb 4500 lb °C Grad Grad Grad Grad KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 26,000 28,000 5-38 P/N 31452-001 Revision 4...
Page 397: Rate Of Climb
5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE LIMB Rate Of Climb Thrust Lever ..............MCT Flaps..................UP Landing Gear..............UP Anti-ice ................OFF Airspeed ......Per Rate Of Climb table below Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS...
Page 398 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE LIMB ISION Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ MIN) MIN) MIN) MIN) 187 2616 187 2922 186 3296 185 3746 187 2591 187 2894 186 3264 185 3710 187 2531 186 2839 186 3189 185 3625 187 2472 186 2773 186 3115 185 3540 187 2419 186 2713 186 3048 185 3465...
Page 399 5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE LIMB Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ MIN) MIN) MIN) MIN) 187 2616 186 2935 186 3299 185 3751 187 2590 186 2906 185 3280 185 3714 187 2531 186 2840 185 3204 185 3629 187 2471 186 2773 185 3129 185 3544 187 2417 186 2712 185 3061 185 3466...
Page 400 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE LIMB ISION Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ MIN) MIN) MIN) MIN) 186 2358 185 2656 184 3007 184 3415 186 2336 185 2631 185 2966 184 3383 186 2280 185 2568 184 2908 184 3302 186 2227 185 2509 184 2841 183 3239 186 2178 185 2453 184 2776 183 3165...
Page 401 5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE LIMB Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ MIN) MIN) MIN) MIN) 176 1979 175 2249 174 2566 173 2946 176 1960 175 2228 174 2542 173 2917 176 1915 175 2175 174 2482 173 2849 176 1872 175 2127 174 2426 173 2785 176 1830 175 2079 174 2372 173 2722...
Page 402 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE LIMB ISION Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ MIN) MIN) MIN) MIN) 165 1643 164 1891 163 2181 162 2527 165 1627 164 1872 163 2159 162 2501 165 1587 164 1827 163 2106 162 2440 165 1549 164 1783 163 2056 162 2381 16,000...
Page 403 5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE LIMB Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ MIN) MIN) MIN) MIN) 157 1347 155 1576 154 1843 153 2159 157 1333 155 1560 154 1824 153 2136 157 1299 155 1521 154 1778 152 2094 157 1268 155 1484 153 1744 152 2043 20,000...
Page 404 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE LIMB ISION Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ MIN) MIN) MIN) MIN) 144 1162 143 1404 142 1687 144 1134 143 1370 142 1647 144 1104 142 1342 141 1613 26,000 138 1079 137 1309 137 1569...
Page 405 5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE ONTAMINATED LIMB Enroute Ice Contaminated Climb Climb Gradient Thrust Lever ..............MCT Flaps..................UP Landing Gear..............UP Airspeed ......Per Climb Gradient table below Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) Grad Grad Grad...
Page 406 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE ONTAMINATED LIMB ISION Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) Grad Grad Grad Grad (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 138 1054 138 1057 138 1057 138 1055 2000 138 1054 138 1049...
Page 407: Enroute Ice Contaminated Climb
5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE ONTAMINATED LIMB Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) Grad Grad Grad Grad (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 6000 8000 P/N 31452-001 5-49 Revision 4...
Page 408 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE ONTAMINATED LIMB ISION Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) Grad Grad Grad Grad (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 10,000 12,000 5-50 P/N 31452-001 Revision 4...
Page 409 5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE ONTAMINATED LIMB Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) Grad Grad Grad Grad (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 14,000 16,000 P/N 31452-001 5-51 Revision 4...
Page 410 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE ONTAMINATED LIMB ISION Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) Grad Grad Grad Grad (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 18,000 -137 20,000 -105 -153 -113 5-52 P/N 31452-001 Revision 4...
Page 411 5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE ONTAMINATED LIMB Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) Grad Grad Grad Grad (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 22,000 -175 -137 24,000 -149 -109 -202 -167 -133 -101 26,000...
Page 412 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE ONTAMINATED LIMB ISION Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) Grad Grad Grad Grad (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ 28,000 -191 -157 -124 -241 -212 -185 -163 5-54 P/N 31452-001 Revision 4...
Page 413: Rate Of Climb (Ice Contaminated)
5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE ONTAMINATED LIMB Rate Of Climb (Ice Contaminated) Thrust Lever ..............MCT Flaps..................UP Landing Gear..............UP Airspeed ......Per Rate Of Climb table below Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS...
Page 414 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE ONTAMINATED LIMB ISION Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ MIN) MIN) MIN) MIN) 140 1932 139 2200 138 2514 138 2888 140 1914 139 2180 138 2490 138 2861 139 1871 139 2131 138 2435 137 2797 139 1828 139 2082 138 2379 137 2733...
Page 415 5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE ONTAMINATED LIMB Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ MIN) MIN) MIN) MIN) 138 1659 138 1908 137 2197 136 2541 138 1644 138 1890 137 2177 136 2518 138 1606 138 1847 137 2128 136 2461 138 1571 137 1807 136 2081 136 2406...
Page 416 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE ONTAMINATED LIMB ISION Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ MIN) MIN) MIN) MIN) 137 1299 134 1526 132 1785 132 2091 137 1287 134 1512 133 1769 132 2072 137 1258 134 1478 133 1729 132 2025 137 1232 134 1447 133 1692 132 1981...
Page 417 5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE ONTAMINATED LIMB Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ MIN) MIN) MIN) MIN) 132 1134 130 1362 129 1629 132 1123 130 1349 129 1614 132 1097 130 1318 129 1576 132 1071 130 1287 129 1539 16,000...
Page 418 5: P ECTION ERFORMANCE IRRUS SF50 NROUTE ONTAMINATED LIMB ISION Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ MIN) MIN) MIN) MIN) 126 1168 126 1156 126 1129 126 1103 20,000 -319 -178...
Page 419 5: P IRRUS ECTION ERFORMANCE SF50 ISION NROUTE ONTAMINATED LIMB Aircraft Weight (lb) Press 6000 5500 5000 4500 (°C) (Feet) KIAS (FT/ KIAS (FT/ KIAS (FT/ KIAS (FT/ MIN) MIN) MIN) MIN) 26,000 -436 -291 -146 -694 -566 -440 -332 -744 -619 -497...
Page 420: Time, Fuel, & Distance To Climb
5: P ECTION ERFORMANCE IRRUS , & D SF50 ISTANCE TO LIMB ISION Time, Fuel, & Distance to Climb Thrust Lever ..............MCT Landing Gear ..............UP Flaps..................UP Anti-ice ................OFF Airspeed ..........Per subsequent tables 5-62 P/N 31452-001 Revision 4...
Page 421: Aircraft Weight: 6000 Lb (2722 Kg)
5: P IRRUS ECTION ERFORMANCE SF50 , & D ISION ISTANCE TO LIMB ISA -10 Aircraft Weight: 6000 lb (2722 kg) ISA -10 Altitude Time Fuel Fuel Distance KIAS (ft) (°C) (min) (U.S. gal) (lb) (nm) 2000 4000 6000 8000 10,000 12,000 14,000...
Page 422 5: P ECTION ERFORMANCE IRRUS , & D SF50 ISTANCE TO LIMB ISION Aircraft Weight: 5500 lb (2495 kg) ISA -10 Altitude Time Fuel Fuel Distance KIAS (ft) (°C) (min) (U.S. gal) (lb) (nm) 2000 4000 6000 8000 10,000 12,000 14,000 16,000 18,000...
Page 423: Aircraft Weight: 5000 Lb (2268 Kg)
5: P IRRUS ECTION ERFORMANCE SF50 , & D ISION ISTANCE TO LIMB Aircraft Weight: 5000 lb (2268 kg) ISA -10 Altitude Time Fuel Fuel Distance KIAS (ft) (°C) (min) (U.S. gal) (lb) (nm) 2000 4000 6000 8000 10,000 12,000 14,000 16,000 18,000...
Page 424: Aircraft Weight: 4500 Lb (2041 Kg)
5: P ECTION ERFORMANCE IRRUS , & D SF50 ISTANCE TO LIMB ISION Aircraft Weight: 4500 lb (2041 kg) ISA -10 Altitude Time Fuel Fuel Distance KIAS (ft) (°C) (min) (U.S. gal) (lb) (nm) 2000 4000 6000 8000 10,000 12,000 14,000 16,000 18,000...
Page 425: Isa
5: P IRRUS ECTION ERFORMANCE SF50 , & D ISION ISTANCE TO LIMB Aircraft Weight: 6000 lb (2722 kg) Altitude Time Fuel Fuel Distance KIAS (ft) (°C) (min) (U.S. gal) (lb) (nm) 2000 4000 6000 8000 10,000 12,000 14,000 16,000 18,000 20,000 22,000...
Page 426: Aircraft Weight: 5500 Lb (2495 Kg)
5: P ECTION ERFORMANCE IRRUS , & D SF50 ISTANCE TO LIMB ISION Aircraft Weight: 5500 lb (2495 kg) Altitude Time Fuel Fuel Distance KIAS (ft) (°C) (min) (U.S. gal) (lb) (nm) 2000 4000 6000 8000 10,000 12,000 14,000 16,000 18,000 20,000 22,000...
Page 427: Aircraft Weight: 5000 Lb (2268 Kg)
5: P IRRUS ECTION ERFORMANCE SF50 , & D ISION ISTANCE TO LIMB Aircraft Weight: 5000 lb (2268 kg) Altitude Time Fuel Fuel Distance KIAS (ft) (°C) (min) (U.S. gal) (lb) (nm) 2000 4000 6000 8000 10,000 12,000 14,000 16,000 18,000 20,000 22,000...
Page 428: Aircraft Weight: 4500 Lb (2041 Kg)
5: P ECTION ERFORMANCE IRRUS , & D SF50 ISTANCE TO LIMB ISION Aircraft Weight: 4500 lb (2041 kg) Altitude Time Fuel Fuel Distance KIAS (ft) (°C) (min) (U.S. gal) (lb) (nm) 2000 4000 6000 8000 10,000 12,000 14,000 16,000 18,000 20,000 22,000...
Page 429: Isa +10
5: P IRRUS ECTION ERFORMANCE SF50 , & D ISION ISTANCE TO LIMB ISA +10 Aircraft Weight: 6000 lb (2722 kg) ISA +10 Altitude Time Fuel Fuel Distance KIAS (ft) (°C) (min) (U.S. gal) (lb) (nm) 2000 4000 6000 8000 10,000 12,000 14,000...
Page 430: Aircraft Weight: 5500 Lb (2495 Kg)
5: P ECTION ERFORMANCE IRRUS , & D SF50 ISTANCE TO LIMB ISION Aircraft Weight: 5500 lb (2495 kg) ISA +10 Altitude Time Fuel Fuel Distance KIAS (ft) (°C) (min) (U.S. gal) (lb) (nm) 2000 4000 6000 8000 10,000 12,000 14,000 16,000 18,000...
Page 431: Aircraft Weight: 5000 Lb (2268 Kg)
5: P IRRUS ECTION ERFORMANCE SF50 , & D ISION ISTANCE TO LIMB Aircraft Weight: 5000 lb (2268 kg) ISA +10 Altitude Time Fuel Fuel Distance KIAS (ft) (°C) (min) (U.S. gal) (lb) (nm) 2000 4000 6000 8000 10,000 12,000 14,000 16,000 18,000...
Page 432: Aircraft Weight: 4500 Lb (2041 Kg)
5: P ECTION ERFORMANCE IRRUS , & D SF50 ISTANCE TO LIMB ISION Aircraft Weight: 4500 lb (2041 kg) ISA +10 Altitude Time Fuel Fuel Distance KIAS (ft) (°C) (min) (U.S. gal) (lb) (nm) 2000 4000 6000 8000 10,000 12,000 14,000 16,000 18,000...
Page 433: Cruise Performance
5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Cruise Performance ** MCT * Max Range Cruise (No Wind) Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 89.6** 25.7 84.6 27.2 79.2 28.7 74.2* 29.3 92.1**...
Page 434 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 89.5** 25.8 83.8 27.8 77.5 29.5 71.8* 30.3 92.1** 24.7 85.3 27.2 77.8 29.7 70.7* 30.9 5000 5500 93.6**...
Page 435 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 89.5** 83.3 28.2 76.4 30.3 70.0* 31.3 92.1** 24.8 84.9 27.5 76.9 30.3 69.2* 31.9 5000 5000 93.4** 23.9...
Page 436 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 89.5** 26.1 82.9 28.6 75.4 68.3* 32.4 92.1** 24.9 84.3 75.4 31.2 66.8* 32.9 5000 4500 93.2** 24.1 84.6...
Page 437 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 91.7** 29.1 87.4 30.6 82.9 78.5* 32.7 94.4** 27.7 88.7 30.1 82.6 32.2 76.8* 33.3 10,000 6000 97.2** 26.1...
Page 438 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 91.7** 29.3 86.5 31.3 33.1 75.7* 33.9 94.4** 27.8 87.9 30.6 33.2 74.2* 34.4 10,000 5500 97.2** 26.2 89.4...
Page 439 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 91.7** 29.5 85.5 31.9 34.2 72.8* 35.2 94.4** 27.9 87.2 31.2 79.4 34.3 71.7* 35.8 10,000 5000 97.2** 26.3...
Page 440 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 91.7** 29.6 84.8 32.6 77.2 35.3 70.1* 36.6 94.4** 86.4 31.7 77.6 35.4 69.0* 37.3 10,000 4500 96.9** 26.4...
Page 441 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 93.0** 33.3 89.5 34.7 85.7 35.9 82.3* 36.4 95.8** 31.7 90.7 85.5 36.1 80.7* 15,000 6000 98.1** 29.9 91.8...
Page 442 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 93.0** 33.6 88.6 35.5 83.9 37.1 79.7* 37.8 95.8** 31.9 89.9 34.8 83.9 37.3 78.3* 38.5 15,000 5500 98.0**...
Page 443 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 93.0** 33.8 36.2 82.7 38.3 77.7* 39.3 95.7** 89.3 35.4 82.6 38.4 76.1* 15,000 5000 98.0** 30.1 90.5 34.4...
Page 444 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 93.0** 34.1 37.1 80.7 39.8 74.4* 95.7** 32.2 88.6 39.7 73.5* 41.7 15,000 4500 98.0** 30.2 89.7 35.1 80.7...
Page 445 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 93.5** 35.2 90.3 36.5 37.6 83.9* 96.1** 33.5 91.7 35.7 87.2 37.7 82.9* 38.7 17,000 6000 98.5** 31.4 92.9...
Page 446 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 93.4** 35.6 89.5 37.3 85.3 38.9 81.5* 39.5 96.1** 33.8 90.7 36.5 85.2 39.1 80.1* 40.2 17,000 5500 98.4**...
Page 447 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 93.4** 35.9 88.7 38.2 83.7 40.2 79.1* 41.1 96.1** 33.9 37.3 83.6 40.4 77.6* 41.8 17,000 5000 98.4** 31.7...
Page 448 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 93.4** 36.1 82.3 41.5 76.8* 42.9 96.1** 34.1 89.3 38.1 41.8 74.9* 43.6 17,000 4500 98.4** 31.8 90.7 36.8...
Page 449 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 93.9** 37.2 91.3 38.2 88.5 39.3 85.8* 39.7 96.5** 35.5 92.4 37.5 88.3 39.5 84.4* 40.4 19,000 6000 99.4**...
Page 450 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 93.9** 37.6 90.4 39.3 86.7 40.7 83.3* 41.3 96.5** 35.8 91.5 38.4 86.4 40.9 81.7* 19,000 5500 99.3** 93.1...
Page 451 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 93.9** 37.9 89.5 40.3 84.9 42.2 80.6* 96.4** 90.7 39.3 84.9 42.3 79.4* 43.7 19,000 5000 99.3** 33.1 92.3...
Page 452 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 93.8** 38.2 88.6 41.2 83.1 43.8 77.9* 44.9 96.4** 36.2 89.9 40.1 83.2 43.8 76.7* 45.7 19,000 4500 99.3**...
Page 453 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 94.4** 39.3 91.9 40.2 89.4 41.1 87.0* 41.4 97.0** 37.4 93.1 39.5 41.4 85.4* 42.1 21,000 6000 100.0** 34.7...
Page 454 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 94.4** 39.8 91.3 41.2 88.3 42.5 85.3* 43.1 96.9** 37.7 92.5 40.3 87.9 42.7 83.6* 43.8 21,000 5500 100.0**...
Page 455 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 94.3** 40.2 90.3 42.4 86.1 44.2 82.2* 44.9 96.9** 91.6 41.3 86.1 44.4 81.0* 45.7 21,000 5000 100.0** 35.1...
Page 456 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 94.3** 40.5 89.5 43.4 84.5 45.9 79.8* 96.9** 38.3 90.6 42.3 84.2 46.1 78.0* 47.8 21,000 4500 99.9** 35.2...
Page 457 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 94.8** 41.6 93.1 91.2 42.7 89.5* 43.1 97.5** 39.3 94.3 41.3 90.8 42.9 87.6* 43.9 23,000 6000 100.5** 36.9...
Page 458 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 94.7** 42.1 43.3 89.1 44.5 86.5* 97.4** 39.6 93.3 42.4 88.9 44.7 84.9* 45.8 23,000 5500 100.4** 37.1 94.3...
Page 459 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 94.7** 42.6 44.6 87.4 46.3 84.0* 97.4** 39.9 92.5 43.4 87.4 46.4 82.6* 47.8 23,000 5000 100.4** 37.3 93.7...
Page 460 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 94.6** 43.1 90.1 45.8 85.6 48.2 81.2* 49.2 97.4** 40.2 91.6 44.5 85.5 48.3 79.7* 23,000 4500 100.4** 37.5...
Page 461 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 95.3** 43.9 93.9 44.1 92.1 44.6 90.5* 44.9 97.6** 41.6 94.9 43.5 91.7 44.9 88.8* 45.7 25,000 6000 100.5**...
Page 462 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 95.2** 44.6 92.8 45.5 90.2 46.5 88.0* 46.9 97.6** 44.7 46.7 86.5* 47.7 25,000 5500 100.5** 39.7 94.6 43.4...
Page 463 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 95.2** 45.1 91.9 46.8 88.7 48.4 85.6* 49.1 97.6** 42.4 93.2 45.8 88.3 48.6 84.0* 25,000 5000 100.5** 39.9...
Page 464 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 95.1** 45.7 91.1 48.1 87.1 50.4 83.3* 51.4 97.6** 42.7 92.4 46.9 86.7 50.6 81.4* 52.3 25,000 4500 100.5**...
Page 465 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 95.6** 46.5 94.7 46.3 93.4 46.6 92.2* 46.7 97.7** 44.3 95.3 45.6 92.8 90.4* 47.5 27,000 6000 100.4** 42.3...
Page 466 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 95.5** 47.3 93.7 47.8 91.6 48.6 89.6* 48.9 97.6** 44.8 94.6 47.1 91.2 48.9 88.1* 49.8 27,000 5500 100.4**...
Page 467 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 95.5** 92.7 49.3 89.8 50.7 87.3* 51.3 97.6** 45.2 93.7 48.5 89.3 85.5* 52.2 27,000 5000 100.5** 42.9 94.1...
Page 468 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 95.5** 48.6 91.8 50.8 88.1 84.7* 53.9 97.6** 45.6 49.6 83.5* 54.8 27,000 4500 100.5** 43.2 93.5 48.3 87.1...
Page 469 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 95.7** 47.8 95.3 47.4 94.3 47.6 93.4* 47.7 98.4** 45.3 46.5 93.7 91.4* 48.5 28,000 6000 100.4** 43.9 96.1...
Page 470 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 95.7** 48.7 94.2 92.5 49.6 90.8* 49.9 98.3** 45.9 48.1 91.8 50.1 88.7* 50.8 28,000 5500 100.4** 44.2 95.1...
Page 471 5: P IRRUS ECTION ERFORMANCE SF50 ISION RUISE ERFORMANCE Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 95.6** 49.5 93.1 50.7 90.3 87.9* 52.4 98.2** 46.4 94.2 49.6 90.1 52.2 86.4* 53.4 28,000 5000 100.4** 44.6...
Page 472 5: P ECTION ERFORMANCE IRRUS SF50 RUISE ERFORMANCE ISION Specific Aircraft Δ ISA Fuel Flow Airspeed Range Weight °C °C KTAS 10 U.S. Gal 95.6** 50.2 52.4 88.4 54.4 85.2* 55.2 98.1** 46.9 93.7 50.9 88.9 54.1 84.6* 56.1 28,000 4500 100.4** 44.8...
Page 473: Takeoff Climb Gradient
5: P IRRUS ECTION ERFORMANCE SF50 UP, F ISION LAPS Gear UP, Flaps 50% Takeoff Climb Gradient ................91 KIAS Thrust Lever ..............T/O Flaps.................. 50% Landing Gear..............UP Engine Anti-Ice: A/R Aircraft Weight (LB) Press 6000 5500 5000 4500 (°C) Feet Climb Gradient (Feet per Nautical Mile) 1232...
Page 474 5: P ECTION ERFORMANCE IRRUS UP, F SF50 LAPS ISION Engine Anti-Ice: A/R Aircraft Weight (LB) Press 6000 5500 5000 4500 (°C) Feet Climb Gradient (Feet per Nautical Mile) 1232 1422 1642 1903 1233 1423 1643 1904 1231 1421 1640 1901 1231 1420...
Page 475 5: P IRRUS ECTION ERFORMANCE SF50 UP, F ISION LAPS Engine Anti-Ice: A/R Aircraft Weight (LB) Press 6000 5500 5000 4500 (°C) Feet Climb Gradient (Feet per Nautical Mile) 1243 1435 1657 1921 1243 1435 1657 1920 1242 1434 1656 1919 1241 1432...
Page 476 5: P ECTION ERFORMANCE IRRUS UP, F SF50 LAPS ISION Engine Anti-Ice: A/R Aircraft Weight (LB) Press 6000 5500 5000 4500 (°C) Feet Climb Gradient (Feet per Nautical Mile) 1052 1225 1426 1663 1052 1225 1426 1663 1050 1224 1424 1661 1049 1222...
Page 477 5: P IRRUS ECTION ERFORMANCE SF50 UP, F ISION LAPS Engine Anti-Ice: A/R Aircraft Weight (LB) Press 6000 5500 5000 4500 (°C) Feet Climb Gradient (Feet per Nautical Mile) 1074 1251 1455 1697 1073 1250 1454 1696 1072 1248 1452 1693 1070 1246...
Page 478 5: P ECTION ERFORMANCE IRRUS UP, F SF50 LAPS ISION Engine Anti-Ice: A/R Aircraft Weight (LB) Press 6000 5500 5000 4500 (°C) Feet Climb Gradient (Feet per Nautical Mile) 1071 1247 1451 1691 1071 1247 1451 1691 1021 1192 1390 1624 1120 1311...
Page 479: Takeoff Rate Of Climb
5: P IRRUS ECTION ERFORMANCE SF50 UP, F ISION LAPS Takeoff Rate of Climb ................91 KIAS Thrust Lever ..............T/O Flaps.................. 50% Landing Gear..............UP Engine Anti-Ice: A/R Aircraft Weight (LB) Press 6000 5500 5000 4500 (°C) Feet Rate of Climb (Feet per Minute) 2099 2421 2795...
Page 480 5: P ECTION ERFORMANCE IRRUS UP, F SF50 LAPS ISION Engine Anti-Ice: A/R Aircraft Weight (LB) Press 6000 5500 5000 4500 (°C) Feet Rate of Climb (Feet per Minute) 2126 2452 2832 3281 2081 2401 2772 3212 2037 2350 2714 3145 1997 2304...
Page 481 5: P IRRUS ECTION ERFORMANCE SF50 UP, F ISION LAPS Engine Anti-Ice: A/R Aircraft Weight (LB) Press 6000 5500 5000 4500 (°C) Feet Rate of Climb (Feet per Minute) 2193 2531 2923 3387 2145 2476 2859 3314 2101 2425 2800 3246 2058 2375...
Page 482 5: P ECTION ERFORMANCE IRRUS UP, F SF50 LAPS ISION Engine Anti-Ice: A/R Aircraft Weight (LB) Press 6000 5500 5000 4500 (°C) Feet Rate of Climb (Feet per Minute) 1898 2211 2573 3001 1857 2164 2518 2937 1818 2119 2466 2876 1780 2074...
Page 483 5: P IRRUS ECTION ERFORMANCE SF50 UP, F ISION LAPS Engine Anti-Ice: A/R Aircraft Weight (LB) Press 6000 5500 5000 4500 (°C) Feet Rate of Climb (Feet per Minute) 1981 2308 2685 3131 1939 2259 2628 3064 1899 2211 2573 3000 1859 2165...
Page 484 5: P ECTION ERFORMANCE IRRUS UP, F SF50 LAPS ISION Engine Anti-Ice: A/R Aircraft Weight (LB) Press 6000 5500 5000 4500 (°C) Feet Rate of Climb (Feet per Minute) 2025 2357 2742 3196 1982 2307 2683 3128 1852 2163 2521 2945 1700 1993...
Page 485: Landing Distance
5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE Landing Distance Speeds (KIAS) FLAPS 4000 lb 4500 lb 5000 lb 5550 lb 6000 lb* UP or UNKNOWN 50% (Ice Contaminated Airframe /STALL SPEED HIGH Advisory) 100% * Maximum Landing Weight (MLW) is 5550 lb (2495 kg). •...
Page 486 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ISION Aircraft Weight: 5550 lb (2517 kg) Flaps: 100% ................85 KIAS Winds ................Calm Runway............Dry, Level, Paved Thrust Lever ..............IDLE Headwind: Subtract 8% from the ground run and 7% from the total distance for every 10 knots of headwind.
Page 487 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE Aircraft Weight: 5550 lb (2517 kg); Flaps: 100% Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 1543 1600 1656 1713 1769 1628 Total 2889 2970 3052 3134 3217 3011 Gnd Roll 1600 1659 1717 1776 1835 1677 1000 Total...
Page 488 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ISION Flaps: 50% ................96 KIAS Winds ................Calm Runway............Dry, Level, Paved Thrust Lever..............IDLE Headwind: Subtract 7% from the ground run and 6% from the total distance for every 10 knots of headwind. Tailwind: Add 39% to the ground run and 36% to the total distance for every 10 knots of tailwind.
Page 489 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE Aircraft Weight: 5550 lb (2517 kg); Flaps: 50% Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 2173 2253 2332 2412 2492 2571 2293 Total 3199 3296 3393 3490 3587 3685 3345 Gnd Roll 2254 2336 2419 2501 2584 2666 2361 1000 Total...
Page 490 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ISION Flaps: 50% (Ice Contaminated Airframe/STALL SPEED HIGH Advisory) ................. 115 KIAS Winds ................Calm Runway............Dry, Level, Paved Thrust Lever ..............IDLE Headwind: Subtract 6% from the ground run and 5% from the total distance for every 10 knots of headwind.
Page 491 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE Aircraft Weight: 5550 lb (2517 kg); Flaps: 50% (Ice Contaminated) Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 2706 2813 2920 3026 Total 4949 5116 5283 5451 Gnd Roll 2806 2916 3027 3138 1000...
Page 492 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ISION Flaps: UP ................. 104 KIAS • N • To calculate Flaps UP landing distance, add 35% to the total distance of Flaps 50%. Refer to Section 2: Limitations, "Brakes" for high-energy braking events. Refer to Section 10: Safety Information, "Taxiing, Steering, and Braking Practices".
Page 493 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE Aircraft Weight: 4500 lb (2041 kg) Flaps: 100% ................76 KIAS Winds ................Calm Runway............Dry, Level, Paved Thrust Lever ..............IDLE Headwind: Subtract 8% from the ground run and 7% from the total distance for every 10 knots of headwind. Tailwind: Add 46% to the ground run and 43% to the total distance for every 10 knots of tailwind.
Page 494 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ISION Aircraft Weight: 4500 lb (2041 kg); Flaps: 100% Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 1543 1600 1656 1713 1769 1826 1628 Total 2307 2380 2454 2528 2602 2676 2417 Gnd Roll 1600 1659 1717 1776 1835 1893 1677 1000 Total...
Page 495 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE Flaps: 50% ................87 KIAS Winds ................Calm Runway............Dry, Level, Paved Thrust Lever ..............IDLE Headwind: Subtract 7% from the ground run and 6% from the total distance for every 10 knots of headwind. Tailwind: Add 39% to the ground run and 37% to the total distance for every 10 knots of tailwind.
Page 496 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ISION Aircraft Weight: 4500 lb (2041 kg); Flaps: 50% Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 2173 2253 2332 2412 2492 2571 2293 Total 2751 2844 2937 3030 3123 3217 2890 Gnd Roll 2254 2336 2419 2501 2584 2666 2361 1000 Total...
Page 497 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE Flaps: 50% (Ice Contaminated) ................. 104 KIAS Winds ................Calm Runway............Dry, Level, Paved Thrust Lever ..............IDLE Headwind: Subtract 6% from the ground run and 5% from the total distance for every 10 knots of headwind. Tailwind: Add 32% to the ground run and 30% to the total distance for every 10 knots of tailwind.
Page 498 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ISION Aircraft Weight: 4500 lb (2041 kg); Flaps: 50% (Ice Contaminated) Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 2706 2813 2920 3026 Total 3939 4082 4225 4369 Gnd Roll 2806 2916 3027 3138 1000...
Page 499 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE ACTORED Landing Distance - Factored Data The landing distance data in the subsequent tables includes a 1.67 factor for dry pavement and a 1.92 factor (1.67 × 1.15) for wet pavement. Aircraft Weight: 5550 lb (2517 kg) Flaps: 100%, Dry Runway Headwind: Subtract 8% from the ground run and 7%...
Page 500 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ACTORED ISION Aircraft Weight: 5550 lb (2517 kg); Flaps: 100%; Runway: Dry Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 2577 2672 2766 2861 2954 2719 Total 4825 4960 5097 5234 5372 5028 Gnd Roll 2672 2771 2867 2966 3064 2801...
Page 501 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE ACTORED Flaps: 100%, Wet Runway Headwind: Subtract 8% from the ground run and 7% from the total distance for every 10 knots of headwind. Tailwind: Add 46% to the ground run and 41% to the total distance for every 10 knots of tailwind.
Page 502 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ACTORED ISION Aircraft Weight: 5550 lb (2517 kg); Flaps: 100%; Runway: Wet Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 2963 3073 3180 3290 3397 3127 Total 5548 5704 5861 6019 6178 5783 Gnd Roll 3073 3186 3297 3411 3524 3221...
Page 503 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE ACTORED Flaps: 50%, Dry Runway Headwind: Subtract 7% from the ground run and 6% from the total distance for every 10 knots of headwind. Tailwind: Add 39% to the ground run and 36% to the total distance for every 10 knots of tailwind.
Page 504 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ACTORED ISION Aircraft Weight: 5550 lb (2517 kg); Flaps: 50%; Runway: Dry Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 3630 3762 3895 4028 4161 4294 3829 Total 5343 5504 5666 5828 5991 6154 5585 Gnd Roll 3764 3901 4039 4177 4315 4452 3943 1000 Total...
Page 505 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE ACTORED Flaps: 50%, Wet Runway Headwind: Subtract 7% from the ground run and 6% from the total distance for every 10 knots of headwind. Tailwind: Add 39% to the ground run and 36% to the total distance for every 10 knots of tailwind.
Page 506 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ACTORED ISION Aircraft Weight: 5550 lb (2517 kg); Flaps: 50%; Runway: Wet Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 4174 4327 4480 4632 4785 4938 4403 Total 6145 6330 6516 6703 6890 7077 6423 Gnd Roll 4328 4487 4645 4803 4962 5120 4534 1000 Total...
Page 507 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE ACTORED Flaps: 50% (Ice Contaminated Airframe/STALL SPEED HIGH Advisory), Dry Runway Headwind: Subtract 6% from the ground run and 5% from the total distance for every 10 knots of headwind. Tailwind: Add 32% to the ground run and 29% to the total distance for every 10 knots of tailwind.
Page 508 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ACTORED ISION Aircraft Weight: 5550 lb (2517 kg); Flaps: 50% (Ice Contaminated); Runway: Dry Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 4519 4697 4876 5054 Total 8265 8543 8822 9102 Gnd Roll 4685 4871 5056...
Page 509 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE ACTORED Flaps: 50% (Ice Contaminated Airframe/STALL SPEED HIGH Advisory), Wet Runway Headwind: Subtract 6% from the ground run and 5% from the total distance for every 10 knots of headwind. Tailwind: Add 32% to the ground run and 29% to the total distance for every 10 knots of tailwind.
Page 510 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ACTORED ISION Aircraft Weight: 5550 lb (2517 kg); Flaps: 50% (Ice Contaminated); Runway: Wet Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 5196 5402 5607 5812 Total 9505 9824 10,145 10,468 Gnd Roll 5388 5601 5814...
Page 511 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE ACTORED Aircraft Weight: 4500 lb (2041 kg) Flaps: 100%, Dry Runway Headwind: Subtract 8% from the ground run and 7% from the total distance for every 10 knots of headwind. Tailwind: Add 46% to the ground run and 43% to the total distance for every 10 knots of tailwind.
Page 512 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ACTORED ISION Aircraft Weight: 4500 lb (2041 kg); Flaps: 100%; Runway: Dry Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 2577 2672 2766 2861 2954 3049 2719 Total 3853 3975 4098 4222 4345 4469 4036 Gnd Roll 2672 2771 2867 2966 3064 3161 2801 1000 Total...
Page 513 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE ACTORED Flaps: 100%, Wet Runway Headwind: Subtract 8% from the ground run and 7% from the total distance for every 10 knots of headwind. Tailwind: Add 46% to the ground run and 43% to the total distance for every 10 knots of tailwind.
Page 514 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ACTORED ISION Aircraft Weight: 4500 lb (2041 kg); Flaps: 100%; Runway: Wet Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 2963 3073 3180 3290 3397 3507 3127 Total 4431 4571 4713 4855 4997 5139 4642 Gnd Roll 3073 3186 3297 3411 3524 3636 3221 1000 Total...
Page 515 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE ACTORED Flaps: 50%, Dry Runway Headwind: Subtract 7% from the ground run and 6% from the total distance for every 10 knots of headwind. Tailwind: Add 39% to the ground run and 37% to the total distance for every 10 knots of tailwind.
Page 516 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ACTORED ISION Aircraft Weight: 4500 lb (2041 kg); Flaps: 50%; Runway: Dry Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 3629 3763 3894 4028 4162 4294 3829 Total 4594 4749 4905 5060 5215 5372 4826 Gnd Roll 3764 3901 4040 4177 4315 4452 3943 1000 Total...
Page 517 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE ACTORED Flaps: 50%, Wet Runway Headwind: Subtract 7% from the ground run and 6% from the total distance for every 10 knots of headwind. Tailwind: Add 39% to the ground run and 37% to the total distance for every 10 knots of tailwind.
Page 518 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ACTORED ISION Aircraft Weight: 4500 lb (2041 kg); Flaps: 50%; Runway: Wet Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 4173 4327 4479 4632 4786 4938 4404 Total 5283 5462 5641 5819 5998 6178 5550 Gnd Roll 4329 4486 4646 4803 4963 5120 4534 1000 Total...
Page 519 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE ACTORED Flaps: 50% (Ice Contaminated Airframe/STALL SPEED HIGH Advisory), Dry Runway Headwind: Subtract 6% from the ground run and 5% from the total distance for every 10 knots of headwind. Tailwind: Add 32% to the ground run and 30% to the total distance for every 10 knots of tailwind.
Page 520 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ACTORED ISION Aircraft Weight: 4500 lb (2041 kg); Flaps: 50% (Ice Contaminated); Runway: Dry Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 4519 4697 4876 5054 Total 6578 6816 7056 7295 Gnd Roll 4685 4871 5056...
Page 521 5: P IRRUS ECTION ERFORMANCE SF50 ISION ANDING ISTANCE ACTORED Flaps: 50% (Ice Contaminated Airframe/STALL SPEED HIGH Advisory), Wet Runway Headwind: Subtract 6% from the ground run and 5% from the total distance for every 10 knots of headwind. Tailwind: Add 32% to the ground run and 30% to the total distance for every 10 knots of tailwind.
Page 522 5: P ECTION ERFORMANCE IRRUS SF50 ANDING ISTANCE ACTORED ISION Aircraft Weight: 4500 lb (2041 kg); Flaps: 50% (Ice Contaminated); Runway: Wet Press TEMPERATURE ~°C Distance Feet Feet Gnd Roll 5196 5402 5607 5812 Total 7564 7839 8114 8390 Gnd Roll 5388 5601 5814...
Page 523: Section 6: Weight And Balance
6: W IRRUS ECTION EIGHT AND ALANCE SF50 ISION ABLE ONTENTS Section 6: Weight and Balance Table of Contents Introduction..................3 Weight and Balance Record..............4 Weight and Balance Data..............4 Loading Instructions ................4 Weight and Balance Determination for Flight........7 Weight and Center of Gravity Limit ...........
Page 524 6: W ECTION EIGHT AND ALANCE IRRUS SF50 ABLE ONTENTS ISION Intentionally Left Blank P/N 31452-001 Original Issue...
Page 525: Introduction
6: W IRRUS ECTION EIGHT AND ALANCE SF50 ISION NTRODUCTION Introduction This section describes the procedure for establishing the basic empty weight and center of gravity of the airplane. Sample forms are provided for reference. A comprehen- sive list of all equipment available for this airplane is included at the back of this section.
Page 526: Weight And Balance Record
6: W ECTION EIGHT AND ALANCE IRRUS SF50 EIGHT AND ALANCE ECORD ISION Weight and Balance Record Weight and Balance Data Refer to “As-Delivered” Weight and Balance Data. Loading Instructions It is the responsibility of the pilot to ensure that the airplane is properly loaded and operated within the prescribed weight and center of gravity limits.
Page 527 6: W IRRUS ECTION EIGHT AND ALANCE SF50 ISION EIGHT AND ALANCE ECORD Middle Row Inboard Seat (Seat 4) – Enter total weight and moment/1000 for the middle row seat from the Loading Data. • N • Seat 4 may be located in any of three locations (forward, mid, and aft).
Page 528 6: W ECTION EIGHT AND ALANCE IRRUS SF50 EIGHT AND ALANCE ECORD ISION Ramp Condition (weight and moment of aircraft before taxi) – Subtotal the weight and moment/1000. Fuel for start, taxi, and run-up – This value is pre-entered on the form. Normally, fuel used for start and taxi before takeoff is approximately 40 lb (6 U.S.
Page 529: Weight And Balance Determination For Flight
6: W IRRUS ECTION EIGHT AND ALANCE SF50 ISION EIGHT AND ALANCE ETERMINATION FOR LIGHT Weight and Balance Determina- tion for Flight Weight and Center of Gravity Limit Figure 6-1: Center of Gravity Envelope 6500 FS 192.55 Max. Ramp Weight FS 198.15 6000 lb 6040 lb...
Page 530: Weight/Fuselage Station (Fs) Chart
6: W ECTION EIGHT AND ALANCE IRRUS SF50 EIGHT AND ALANCE ETERMINATION FOR LIGHT ISION Weight/Fuselage Station (FS) Chart Weight FS - Min. FS - Max. Weight FS - Min. FS - Max. (lb) (inches) (inches) (lb) (inches) (inches) 3500 189.44 196.28 4800...
Page 531: Weight And Balance Loading Form
6: W IRRUS ECTION EIGHT AND ALANCE SF50 ISION EIGHT AND ALANCE ETERMINATION FOR LIGHT Weight and Balance Loading Form • N • The Takeoff Condition Weight must not exceed 6000 lb (2722 kg). The Takeoff Condition Moment must be within the Minimum Moment to Maximum Moment range at the Takeoff Condition Weight.
Page 532 6: W ECTION EIGHT AND ALANCE IRRUS SF50 EIGHT AND ALANCE ETERMINATION FOR LIGHT ISION FS Inches Moment/1000 Weight Item Description [(Moment/1000) (Weight*FS)/ *1000]/Weight 1000 4. Middle Row 178.4 Outboard Seat Occupants (Seats 3 & 5) 5. Middle Row 183.2 (Fwd) Inboard Seat (Seat 197.2 (Mid) 211.2 (Aft)
Page 533 6: W IRRUS ECTION EIGHT AND ALANCE SF50 ISION EIGHT AND ALANCE ETERMINATION FOR LIGHT FS Inches Moment/1000 Weight Item Description [(Moment/1000) (Weight*FS)/ *1000]/Weight 1000 11. Zero Fuel Condition Weight Subtotal item 1 thru 9 4900 lb maximum 12. Fuel Loading 296 U.S.
Page 534: Weight & Balance Record
6: W ECTION EIGHT AND ALANCE IRRUS & B SF50 EIGHT ALANCE ECORD ISION Weight & Balance Record Use this form to maintain a continuous history of changes and modifications to airplane structure or equipment affecting weight and balance: Page Serial Num: Reg.
Page 535 6: W IRRUS ECTION EIGHT AND ALANCE SF50 & B ISION EIGHT ALANCE ECORD Page Serial Num: Reg. Num: __ of __ Running Weight Change Basic Item No. Added (+) or Description Empty Removed (-) of Article Weight Date Modification MOM/ 1000 P/N 31452-001...
Page 536: Equipment List
6: W ECTION EIGHT AND ALANCE IRRUS SF50 QUIPMENT ISION Equipment List This list will be determined after the final equipment has been installed in the aircraft. 6-14 P/N 31452-001 Original Issue...
Page 537: Section 7: Systems Description
7: S IRRUS ECTION YSTEMS ESCRIPTION SF50 ISION Section 7: Systems Description • N • Content for Section 7: Systems Description is located in the Pilot’s Information Manual (PIM). P/N 31452-001 Original Issue...
Page 538 7: S ECTION YSTEMS ESCRIPTION IRRUS SF50 ISION Intentionally Left Blank P/N 31452-001 Original Issue...
Page 539 Airworthiness Directives ..............8 Airplane Inspection Periods..............9 Hour Meters..................9 Annual Inspection................10 100-Hour Inspection ................ 10 Cirrus Aircraft Progressive Inspection Program ......11 Ground Handling ................12 Application of External Power ............12 Towing..................... 14 Taxiing..................... 16 Parking .................... 18 Tie Down ..................
Page 540 8: H ECTION ANDLING AND ERVICING IRRUS SF50 ABLE ONTENTS ISION Cleaning Interior Surfaces ..............64 Interior Windshield and Windows ............ 65 Instrument Panel and Electronic Display Screens......68 Headliner and Trim Panels .............. 69 Leather Upholstery and Seats ............70 Carpets ....................
Page 541: Introduction
This section provides general guidelines for handling, servicing, and maintaining your aircraft. In order to ensure continued safe and efficient operation of your airplane, keep in contact with your Authorized Cirrus Service Center to obtain the latest information pertaining to your aircraft.
Page 542 NTRODUCTION ISION • CAPS Component Maintenance Manual (CMM) - Maintenance Manual with Illustrated Parts List prepared to enable an authorized Cirrus Aircraft CAPS technician to restore the system to a func- tional condition. • Engine Operators and Maintenance Manual –...
Page 543: Obtaining Publications
8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION NTRODUCTION Obtaining Publications AFMs and aircraft service publications can be obtained from Cirrus Aircraft at www.cirrusaircraft.com, or the Cirrus Connection at www.cirrusconnection.com. P/N 31452-001 Original Issue...
Page 544: Airplane Records And Certificates
8: H ECTION ANDLING AND ERVICING IRRUS SF50 IRPLANE ECORDS AND ERTIFICATES ISION Airplane Records and Certifi- cates The Federal Aviation Administration (FAA) requires that certain data, certificates, and licenses be displayed or carried aboard the airplane at all times. Additionally, other documents must be made available upon request.
Page 545 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION IRPLANE ECORDS AND ERTIFICATES Table 1: Required Documents Required Documents Note Airworthiness Must be displayed at all times. Certificate FAA Form 8100-2 Registration Must be in the aircraft for all Certificate operations.
Page 546: Airworthiness Directives
AD. Operators should periodi- cally check with Cirrus Service Centers or A&P mechanic to verify receipt of the latest issued AD for their airplane. P/N 31452-001...
Page 547: Airplane Inspection Periods
8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION IRPLANE NSPECTION ERIODS Airplane Inspection Periods • N • FAR 1.1 defines time in service, with respect to maintenance time records, as “the time from the moment an aircraft leaves the surface of the earth until it touches it at the next point of landing.”...
Page 548: Annual Inspection
Airframe and Powerplant (A&P) mechanic holding an Inspection Authorization (IA). Annual inspections can only be performed by facilities approved by Cirrus Aircraft. The inspection is listed, in detail, in Chapter 5 of the Airplane Maintenance Manual. 100-Hour Inspection...
Page 549: Cirrus Aircraft Progressive Inspection Program
Progressive Inspection Program in accordance with the Federal Aviation Regulation Part 91.409(d). The Cirrus Aircraft Progressive Inspection Program provides for the complete inspection of the airplane utilizing a five-phase cyclic inspection program. 400 flight hours: A total of eight inspections are accom- plished over the course of 400 flight hours, with an inspection occurring every 50 flight hours.
Page 550: Ground Handling
8: H ECTION ANDLING AND ERVICING IRRUS SF50 ROUND ANDLING ISION Ground Handling Application of External Power An external power receptacle, located on the LH wing fairing behind the baggage door, permits the use of an external power unit for cold weather starting and mainte- nance procedures.
Page 551 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION ROUND ANDLING Refer to Section 2: Limitations, "Engine Start (General)" for external power unit start limita- tions. Ensure external power unit is regulated to 28 VDC. Verify BAT 1, BAT 2, GEN 1, and GEN 2 power switches are set to OFF.
Page 552: Towing
Towing provisions are included in the nose wheel axle; 0.556 inch (1.412 cm) outer diameter. Recommended Towing Equipment ITEM P/N or SPEC DESCRIPTION SUPPLIER Tow Bar Tow airplane. Any Supplier Wheel Chocks. WCK1001 Block wheels. Cirrus 8-14 P/N 31452-001 Revision 4...
Page 553 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION ROUND ANDLING To Tow Airplane • N • Be especially cognizant of hangar door clearances. Refer to Section 1: General, Airplane Three View for turning radius clearances. Attach tow bar/adapter onto the nose wheel axle •...
Page 554: Taxiing
8: H ECTION ANDLING AND ERVICING IRRUS SF50 ROUND ANDLING ISION Taxiing • CAUTION • Only rated pilots and mechanics should taxi the aircraft or run the engine. Verify that taxi area is clear before beginning taxi. Do not operate the engine at high thrust when running up or taxiing over ground containing loose stones, gravel, or any loose material that may cause damage to aircraft.
Page 555 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION ROUND ANDLING To Taxi Airplane Remove chocks. Start engine in accordance with Airplane Flight Manual procedures. Release parking brake. Advance thrust lever to initiate taxi. Immediately after initiating taxi, apply the brakes to determine their effectiveness.
Page 556: Parking
The battery may be recharged using a constant potential charger. Recommended Parking Equipment ITEM P/N or SPEC DESCRIPTION SUPPLIER Wheel Chocks WCK1001 Block wheels. Cirrus 39003-001 Support tail (if required under Tail Stand Cirrus heavy snow conditions). 8-18 P/N 31452-001...
Page 557 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION ROUND ANDLING To Park Airplane Position airplane on level surface and headed into the wind. Retract flaps. • CAUTION • Use care if setting parking brake during cold weather when accumulated moisture may freeze brakes, or when brakes are overheated.
Page 558: Tie Down
Recommended Tie Down Equipment ITEM P/N or SPEC DESCRIPTION SUPPLIER Wheel Chocks WCK1001 Block wheels. Cirrus Inlet Cover JETENGCVR Prevent entry of Bruce’s moisture and/or Custom foreign particles. Covers Pitot Tube...
Page 559 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION ROUND ANDLING Secure gust lock strap to immobilize the side sticks. Retract flaps. Set parking brake in accordance with Parking procedure in this section. Install chocks. Install wing tie-down rings. • N •...
Page 560: Leveling
8: H ECTION ANDLING AND ERVICING IRRUS SF50 ROUND ANDLING ISION Leveling Refer to AMM Chapter 8: Leveling & Weighing, Weighing the Airplane procedures for instructions and illustration. Jacking Refer to AMM Chapter 7: Lifting & Shoring, Jacking the Airplane procedures for list of required tools and for illus- tration.
Page 561: Servicing
8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION ERVICING Servicing Landing Gear Servicing The nose landing gear is an air/oil oleo shock strut; the main landing gear is an air/oil oleo shock strut. The landing gear system is serviced with MIL-PRF-87257 hydraulic fluid and filled with compressed, dry nitrogen.
Page 562 8: H ECTION ANDLING AND ERVICING IRRUS SF50 ERVICING ISION To Replenish Brake Fluid Install chocks. Release parking brake. Remove upper right nose access panel to gain access to hydraulic fluid reservoir. Clean reservoir plug and area around plug before opening reservoir cap.
Page 563 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION ERVICING • Overheated components, such as: • Brake Pads: The profile of the edges is deformed and may include large voids or sections of missing material. • Brake Discs: Surface is irregular and may include large grooves, bumps, or deposits from brake pads.
Page 564: Hydraulic Power Pack Servicing
8: H ECTION ANDLING AND ERVICING IRRUS SF50 ERVICING ISION Hydraulic Power Pack Servicing The hydraulic power pack system is filled with MIL-PRF-87257 hydraulic brake fluid. The fluid level should be checked at every oil change and at the annual/100-hour inspection, replenishing the system when necessary.
Page 565: Tire Inflation
8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION ERVICING Tire Inflation The main landing gear wheel assemblies use 18 × 5.5, 8-ply rating tubeless tires. The nose wheel assembly uses a 5.00 × 5, 10-ply rated tubeless tire. Always keep tires inflated to the rated pressure to obtain optimum perfor- mance and maximum service.
Page 566 8: H ECTION ANDLING AND ERVICING IRRUS SF50 ERVICING ISION An oil filler cap is located at the 2 o’clock position on the right-hand side of the engine, next to the front mounting pad. The sight glass (located at the 3 o’clock position) is marked with two levels: FULL and ADD.
Page 567 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION ERVICING For a list of approved engine lubricants, refer to Section 2: Limitations, "Oil". To Check and Add Oil Open oil check door located on lower RH side of nacelle. Verify oil level via sight glass. If oil level is at or below ADD mark on sight glass, open oil fill door on upper RH side of nacelle.
Page 568: Fuel System Servicing
8: H ECTION ANDLING AND ERVICING IRRUS SF50 ERVICING ISION Fuel System Servicing Fuel Filtration Element A 20-micron disposable fuel filter element is located on the engine FCU. In the event that the fuel filter becomes blocked, a filter bypass valve located adjacent to the filter will allow fuel to bypass the fuel filter for continued engine operation.
Page 569 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION ERVICING • WARNING • During fueling, have a fire extinguisher available. Ground fuel truck or cart to suitable earth ground. Do not fill tank within 100 ft (30.5 m) of any energized electrical equipment capable of producing a spark.
Page 570 8: H ECTION ANDLING AND ERVICING IRRUS SF50 ERVICING ISION Figure 8-1: Fuel Grounding Points LEGEND 1. MLG Ground Tab SF50_FM08_0018A 8-32 P/N 31452-001 Original Issue...
Page 571 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION ERVICING To Refuel Airplane Place fire extinguisher near fuel tank being filled. Connect ground wire from refuel nozzle to airplane ground point, from airplane ground point to fuel truck or cart, and from fuel truck or cart to a suitable earth ground.
Page 572: Fuel Contamination And Sampling
8: H ECTION ANDLING AND ERVICING IRRUS SF50 ERVICING ISION Fuel Contamination and Sampling Typically, fuel contamination results from foreign mate- rial such as water, dirt, rust, and fungal or bacterial growth. Additionally, chemicals and additives that are incompatible with fuel or fuel system components are also a source of fuel contamination.
Page 573 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION ERVICING To help reduce the occurrence of contaminated fuel coming from the supplier or fixed based operator, pilots should ensure that the fuel supply has been checked for contamination and that the fuel is properly filtered. Also, between flights, the fuel tanks should be kept as full as operational conditions permit to reduce condensation on the inside of fuel tanks.
Page 574: Ice Protection System (Ips) Servicing
8: H ECTION ANDLING AND ERVICING IRRUS SF50 ERVICING ISION Ice Protection System (IPS) Servicing IPS Fluid Replenishment The IPS fluid tank is serviced through a filler cap and neck located on the RH side of the fuselage. • WARNING • Only use approved IPS fluids.
Page 575: Battery Service
8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION ERVICING To add IPS fluid Dispense approved IPS fluid into clean measuring container. Remove filler cap. Use funnel to fill fluid tank to desired level. Install filler cap. Battery Service The aircraft is delivered with a maintenance-free, rechargeable, sealed, lead acid primary battery known as Battery #1.
Page 576: Oxygen System Servicing
8: H ECTION ANDLING AND ERVICING IRRUS SF50 ERVICING ISION Oxygen System Servicing • WARNING • To preclude the possibility of fire by sponta- neous combustion, oil, grease, paint, hydraulic fluid, and other flammable material should be kept away from oxygen equipment. Service the oxygen system as follows: Oxygen Supply Cylinder Standard system (22 cu ft)
Page 577: Cleaning Exterior Surfaces
8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING XTERIOR URFACES Cleaning Exterior Surfaces • CAUTION • Waxing, an unapproved cleaning method, may damage the pneumatic deicers due to material incompatibility. Do not wax leading edge pneumatic deicers. Prior to cleaning, place the airplane in a shaded area to allow the surfaces to cool.
Page 578 8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING XTERIOR URFACES ISION Recommended Exterior Cleaning Products Cleaning Cleaning Product Application Supplier Pure Carnauba Painted Exterior Any Source Mothers California Painted Exterior Wal-Mart Stores Gold Pure Carnauba Wax RejeX Painted Exterior Corrosion Technologies WX/Block System...
Page 579 Application Supplier LP Aero Plastics Exterior Aircraft Spruce & Acrylic Polish & Windshield and Specialty Sealant Windows Goodrich Deicer Exterior Cirrus Aircraft Aerospace Cleaner 54023-004 Goodrich Deicer Exterior Cirrus Aircraft Aerospace Protectant 54023-005 Goodrich Deicer Exterior Cirrus Aircraft SILVERboot Polish 54023-006 ICEX®...
Page 580: Care Of Graphics
8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING XTERIOR URFACES ISION Care of Graphics Graphics require care similar to any fine paint finish. Use high quality products designed specifically for use on automobile finishes. Use products in accordance with the manufacturer’s instructions.
Page 581 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING XTERIOR URFACES Rinse thoroughly with clean water. To reduce water spotting, immediately use a sili- cone squeegee to remove water. Dry with a clean microfiber cloth. Pressure Washing Although hand washing is preferred, pressure washing may be used when necessary to remove dirt and contam- inants.
Page 582 8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING XTERIOR URFACES ISION Removing Difficult Contaminants Difficult contaminants such as bugs, bird droppings, or tree sap may require spot cleaning. • CAUTION • To prevent scratching the graphic, refrain from rough scrubbing and the use of abrasive tools. To spot clean difficult contaminants Soften contaminants by soaking with hot, soapy water for several minutes.
Page 583 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING XTERIOR URFACES Cleaning Fuel Spills • CAUTION • Immediately clean fuel spills to avoid degrading the vinyl and adhesive used in the graphic. To clean fuel spills Wipe off spilled fuel. Clean graphic with a wet, non-abrasive detergent such as 3M™...
Page 584 8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING XTERIOR URFACES ISION Graphic Restoration If typical cleaning methods fail to produce satisfactory results, refer to the recommended restoration products and mixtures below to help preserve the condition of the graphics on your aircraft. •...
Page 585 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING XTERIOR URFACES Table 2: Recommended Graphic Restoration Products and Mixtures Film or Finish Type Product or Mixture Smooth Gloss 3M™ Perfect-it™ Show Car Paste Wax 39526; Meguiar's Gold Class™ Carnuaba Plus Premium Liquid Wax Matte or Satin Mixture of two parts isopropyl alcohol to...
Page 586: Exterior Windshield And Windows
8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING XTERIOR URFACES ISION Exterior Windshield and Windows Before cleaning an acrylic window, rinse away all dirt particles before applying cloth or chamois. Never rub dry acrylic. Dull or scratched window coverings may be polished using a special acrylic polishing paste.
Page 587 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING XTERIOR URFACES Apply acrylic cleaner to one area at a time, then wipe away with a soft, cotton cloth. Dry the windows using a dry non-abrasive cotton cloth or chamois. P/N 31452-001 8-49 Original Issue...
Page 588: Engine Compartment
8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING XTERIOR URFACES ISION Engine Compartment The engine exterior and compartment may be cleaned with a dry cleaning solvent, MIL-PRF-680 Type II. To clean the Engine Compartment Remove engine nacelle. Cover fire extinguisher discharge nozzles so as to ensure no water or debris falls into the discharge tubes during cleaning.
Page 589: Heated Inlet
8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING XTERIOR URFACES Flight Near/Over Salt Water A fresh water rinse of the powerplant must be performed after a flight near/over salt water. • CAUTION • Failure to conduct a fresh water rinse after flight near/over salt water may cause engine damage.
Page 590 8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING XTERIOR URFACES ISION To polish the Lipskin (Cosmetic Polish) • CAUTION • Hand polish only. Mechanical polishing is prohibited on all areas of the inlet assembly. Use Teflease tape to mask off painted surfaces beyond the trailing edges of the lipskin.
Page 591: Landing Gear
8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING XTERIOR URFACES Landing Gear Before cleaning the landing gear, place a plastic cover or similar material over the wheel and brake assembly. To clean the Landing Gear Place a pan under the gear to catch waste. Spray or brush the gear area with solvent or a mixture of solvent and degreaser, as desired.
Page 592: Deicers
8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING XTERIOR URFACES ISION Deicers Before cleaning/maintaining the deicers, place a plastic cover or similar material over the surrounding wing or stabilizer surfaces. • N • It is recommended the maintenance process be performed in the following sequence: (i) Clean (ii) Polish (iii) Protect (iv) Apply Ice Adhesion Inhibitor...
Page 593 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING XTERIOR URFACES Deicer Cleaner Application Goodrich Aerospace Cleaner is to be used for frequent routine cleaning of the Silver Urethane Deicers. It may be used as needed for removal of bugs, dirt, and grime. Goodrich Aerospace Cleaner may be used as a spot cleaner as well.
Page 594 8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING XTERIOR URFACES ISION Rinse deicer as needed with clean water and clean, soft, lint-free, cotton cloths; maintain the cloths fully wetted at all times. Ensure cloth is continually wetted with water to avoid abrasion and creating scratches in deicer surface.
Page 595 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING XTERIOR URFACES been in service for 6 to 12 months. Reapplication is suggested at 3 to 12 month intervals as needed. Polish application on new deicers will not cause damage but will not improve cosmetic appearance.
Page 596 8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING XTERIOR URFACES ISION polishing action is seen once the polish cloth becomes saturated. If polish dries prior to buffing, it should be removed by re-polishing. Deicer protectant may be used immediately on top of polish, but is not required.
Page 597 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING XTERIOR URFACES alternately be sprayed directly onto the deicer in addition to spraying the cloth. Overspray should be wiped off. Ensure cloth is continually wetted with Aerospace Protectant to avoid abrasion and creating scratches in deicer surface.
Page 598 8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING XTERIOR URFACES ISION Cosmetic Surface Protectant Application • CAUTION • Avoid scratching the unprotected deicer surface. Use clean, soft, lint-free, cotton cloths. It is important to leave only a thin film of ICEX II. A heavy application can result in a sticky surface that would collect dust and dirt, thereby reducing the product's ice adhesion inhibitor efficiency.
Page 599 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING XTERIOR URFACES Apply ICEX II to clean, soft, lint-free cotton cloth. • CAUTION • Ensure cloth is continually wetted with ICEX II to avoid abrasion and creating scratches on deicer surface.
Page 600 8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING XTERIOR URFACES ISION Ice Adhesion Inhibitor Application When ICEX II is applied to a silver urethane deicer, the resulting surface finish helps protect the deicer from insect impact stains and other forms of surface contami- nation.
Page 601 8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING XTERIOR URFACES Clean deicer with isopropyl alcohol to remove substances that cannot be removed with soap and water. Apply masking tape on leading edge lined up to the aft edge of the conductive edge sealer. Form neat, straight lines to border the application area.
Page 602: Cleaning Interior Surfaces
8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING NTERIOR URFACES ISION Cleaning Interior Surfaces Seats, carpet, upholstery panels, and headliners should be vacuumed at regular intervals to remove surface dirt and dust. While vacuuming, use a fine bristle nylon brush to help loosen particles.
Page 603: Interior Windshield And Windows
8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING NTERIOR URFACES Interior Windshield and Windows Never rub dry acrylic. Dull or scratched window cover- ings may be polished using a special acrylic polishing paste. • CAUTION • Clean acrylic windows with a solvent-free, non-abrasive, antistatic acrylic cleaner.
Page 604 Prist Aerospace and Windows Optimax Display Screens PhotoDon Mild Dishwasher Cabin Interior Any Source Soap (abrasive-free) Leather Care Kit Leather Upholstery Cirrus Aircraft 50689-001 Leather Cleaner Leather Upholstery Cirrus Aircraft 50684-001 Ink Remover Leather Upholstery Cirrus Aircraft 50685-001 8-66 P/N 31452-001...
Page 605 ANDLING AND ERVICING SF50 ISION LEANING NTERIOR URFACES Cleaning Cleaning Product Application Supplier Leather Leather Upholstery Cirrus Aircraft Conditioner 50686-001 Spot and Stain Leather Upholstery Cirrus Aircraft Remover 50687-001 Vinyl Finish Vinyl Panels Cirrus Aircraft Cleaner 50688-001 Vinyl & Leather...
Page 606: Instrument Panel And Electronic Display Screens
8: H ECTION ANDLING AND ERVICING IRRUS SF50 LEANING NTERIOR URFACES ISION Instrument Panel and Electronic Display Screens The instrument panel, control knobs, and plastic trim need only to be wiped clean with a soft, damp cloth. The multifunction display, primary flight display, and other electronic display screens should be cleaned with Optimax - LCD Screen Cleaning Solution as follows: •...
Page 607: Headliner And Trim Panels
8: H IRRUS ECTION ANDLING AND ERVICING SF50 ISION LEANING NTERIOR URFACES Headliner and Trim Panels The airplane interior can be cleaned with a mild detergent or soap and water. Harsh abrasives or alkaline soaps or detergents should be avoided. Solvents and alcohols may damage or discolor vinyl or urethane parts.
Page 608: Leather Upholstery And Seats
Cirrus Aircraft for more stubborn marks and stains. Do not use soaps as they contain alkaline which will alter the leather’s pH balance and cause the leather to age prema-...
Page 609 9: L IRRUS ECTION OG OF UPPLEMENTS SF50 ISION ABLE ONTENTS Section 9: Log of Supplements Table of Contents As Required P/N 31452-001 Original Issue...
Page 610 Issuement is installed or the special operations are to be performed. This Log of Supplements shows all Cirrus Aircraft Supple- ments available for the aircraft at the corresponding date of the revision level shown in the lower left corner. A check mark in the Part Number column indicates that the supple- ment is applicable to the AFM.
Page 611: Section 10: Safety Information
Table of Contents Introduction..................3 Taxiing, Steering, and Braking Practices ..........4 Operating Practices................4 Brake Maintenance ................6 Cirrus Airframe Parachute System (CAPS)......... 7 Deployment Scenarios ..............7 Loss of Thrust.................. 8 Pilot Incapacitation ................9 Other ....................9 General Deployment Information ............
Page 612 10: S ECTION AFETY NFORMATION IRRUS SF50 ABLE ONTENTS ISION Intentionally Left Blank 10-2 P/N 31452-001 Original Issue...
Page 613: Introduction
Cirrus Aircraft strongly recommends that all pilots seek regular recurrent training and that they operate in accordance with the Cirrus Aircraft Flight Operations Manual and Envelope of Safety. In addition, regulations require additional pilot training and proficiency because the SF50 is turbojet-powered (14 CFR 61.58).
Page 614: Taxiing, Steering, And Braking Practices
RACTICES ISION Taxiing, Steering, and Braking Practices The Vision SF50 uses a full-castering nose wheel and relies on differential braking for directional control while taxiing. Proper braking practices are therefore critical to avoid potential damage to the brakes. The most common cause of brake damage and/or failure is the creation of excessive heat through improper braking practices.
Page 615 10: S IRRUS ECTION AFETY NFORMATION SF50 ISION AXIING TEERING RAKING RACTICES power added with the thrust will be absorbed in the brakes to maintain constant speed. Approximately 38% N1 is the required breakaway thrust at 6000 lb (2722 kg). •...
Page 616: Brake Maintenance
10: S ECTION AFETY NFORMATION IRRUS SF50 AXIING TEERING RAKING RACTICES ISION Brake Maintenance The brakes shall be inspected before every flight for general condition, evidence of overheating, and deterio- ration. • N • Refer to Section 8: Handling and Servicing, "Brake Servicing"...
Page 617: Cirrus Airframe Parachute System (Caps)
The primary purpose of CAPS on the Cirrus Vision SF50 is to bring the aircraft occupants safely to the ground following a loss of thrust event, if the pilot has determined the use of CAPS to be safer than a forced landing.
Page 618: Loss Of Thrust
YSTEM ISION Loss of Thrust The primary purpose of CAPS on the Cirrus Vision SF50 is to bring the aircraft occupants safely to the ground following a loss of thrust event or other engine loss, if the pilot has determined the use of CAPS to be safer than a forced landing.
Page 619: Pilot Incapacitation
10: S IRRUS ECTION AFETY NFORMATION SF50 (CAPS) ISION IRRUS IRFRAME ARACHUTE YSTEM Loss of Thrust Enroute While attempting to glide to an airfield to perform a power-off landing, the pilot must be continuously aware of altitude and ability to successfully perform the landing. The pilot must determine by 1000 feet AGL if landing is assured or if CAPS will be required.
Page 620: General Deployment Information
10: S ECTION AFETY NFORMATION IRRUS (CAPS) SF50 IRRUS IRFRAME ARACHUTE YSTEM ISION General Deployment Information Deployment Speed The recommended CAPS activation speed is one that is less than 135 KIAS and 145 KTAS, whichever is lower, which will result in immediate parachute deployment. It is important for the operator to make all reasonable efforts to slow to the minimum possible airspeed prior to CAPS activation.
Page 621: Deployment Attitude
10: S IRRUS ECTION AFETY NFORMATION SF50 (CAPS) ISION IRRUS IRFRAME ARACHUTE YSTEM under the canopy or for the cabin to be secured. A low altitude deployment increases the risk of injury or death and should be avoided if possible. If circumstances permit, it is advisable to activate the CAPS at or above 1000 feet AGL.
Page 622: Emergency Landing Body Position
10: S ECTION AFETY NFORMATION IRRUS (CAPS) SF50 IRRUS IRFRAME ARACHUTE YSTEM ISION The overriding consideration in all CAPS-deployed land- ings is to prepare the occupants for the touchdown in order to protect them as much as possible from injury. Emergency Landing Body Position The most important consideration for a touchdown with CAPS deployed is to protect the occupants from injury,...
Page 623: Water Landings
10: S IRRUS ECTION AFETY NFORMATION SF50 (CAPS) ISION IRRUS IRFRAME ARACHUTE YSTEM If the cabin door is clear, exit via the cabin door. If the cabin door is blocked, or has jammed on impact, exit via the emergency exit (egress window). Depending on altitude and condition of the cabin after touchdown, dumping cabin pressure (in accordance with the CAPS Activation procedure) prior to shutting down...
Page 624: Ground Gusts
10: S ECTION AFETY NFORMATION IRRUS (CAPS) SF50 IRRUS IRFRAME ARACHUTE YSTEM ISION Ground Gusts If it is known or suspected that ground gusts are present in the landing zone, the parachute could drag the airplane after touchdown, especially if the terrain is flat and without obstacles.

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