THRUSH S2R-H80 Flight Manual
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THRUSH S2R-H80 Flight Manual

Single & dual cockpit
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Summary of Contents for THRUSH S2R-H80

  • Page 2 Atlanta, GA July 2, 2013 Added Document Control “# AFM H8001 SINGLE & DUAL COCKPIT” to document. Replaced the picture to reflect an S2R-H80 model airplane. Cover Updated Log of Revision to reflect Revision A. Log of Effective Pages: updated for revised page numbering & all pages affected due to v-vi Document Control # added.
  • Page 3 09/03/2015...

  • Page 4: Table Of Contents

    INTRODUCTION ..............................VIII WARNINGS, CAUTIONS & NOTES DEFINED ...................... IX 3-VIEW OF S2R-H80 SINGLE COCKPIT ....................... X DIMENSIONAL 3-VIEW OF S2R-H80 SINGLE COCKPIT ..................XI 3-VIEW OF S2R-H80 DUAL COCKPIT ......................... XII DIMENSIONAL 3-VIEW H80 DUAL COCKPIT ....................XIII GLOSSARY OF TERMS & ABBREVIATIONS ....................XIV SECTION 1 LIMITATIONS: ............................
  • Page 5 SECTION 5: WEIGHT & BALANCE ........................... 66 5.1. WEIGHT & BALANCE PROCEDURE ....................... 66 5.2. S2R-H80 SINGLE AND DUAL COCKPIT C.G. ENVELOPE ..............67 5.3. WAM - EXAMPLE ............................68 5.5. USING FORWARD BALLAST TO MANAGE AFT EMPTY CG POSITION FOR THE DUAL COCKPIT CONFIGURATION.
  • Page 6 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL LOG OF EFFECTIVE PAGES PAGE FAA APPROVAL DATE PAGE FAA APPROVAL DATE ……………………… ……………………… Cover 3/19/15 3/19/15 ……………………… ……………………… 9/03/15 3/19/15 ……………………… ……………………… 9/03/15 3/19/15 ……………………… ……………………… 3/19/15 3/19/15 ……………………… ……………………… 3/19/15 3/19/15 ………………………...
  • Page 7 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL LOG OF EFFECTIVE PAGES PAGE FAA APPROVAL DATE PAGE FAA APPROVAL DATE ……………………… 8/05/14 ……………………… 8/05/14 ……………………… 8/05/14 ……………………… 8/05/14 ……………………… 8/05/14 ……………………… 8/05/14 SECTION 5: WEIGHT & BALANCE ……………………… ……………………… ………………………...

  • Page 8: Introduction

    RESTRICTED CATEGORY and flight maneuvers shall be limited to those normally performed in special purpose operations and approved by Administrator. The S2R-H80 Turbo Thrush is approved for day and night VFR flight. Flight into or near thunderstorms or into known icing conditions is PROHIBITED. The observance of limitations, performance, and weight &...

  • Page 9: Warnings, Cautions & Notes Defined

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL WARNINGS, CAUTIONS & NOTES DEFINED: WARNING weaning A WARNING IS DEFINED AS AN OPERATING PROCEDURE, PRACTICE, CONDITION OR STATEMENT, WHICH IF NOT CORRECTLY FOLLOWED, COULD RESULT IN PERSONAL INJURY OR LOSS OF LIFE.

  • Page 10: 3-View Of S2R-H80 Single Cockpit

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 3-VIEW OF S2R-H80 SINGLE COCKPIT AFM H8001 SINGLE & DUAL COCKPIT Revision A Page x FAA APPROVAL DATE: 8/05/2014...

  • Page 11: Dimensional 3-View Of S2R-H80 Single Cockpit

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL DIMENSIONAL 3-VIEW OF S2R-H80 SINGLE COCKPIT AFM H8001 SINGLE & DUAL COCKPIT Revision A Page xi FAA APPROVAL DATE: 8/05/2014...

  • Page 12: 3-View Of S2R-H80 Dual Cockpit

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 3-VIEW OF S2R-H80 DUAL COCKPIT AFM H8001 SINGLE & DUAL COCKPIT Revision A Page xii FAA APPROVAL DATE: 8/05/2014...

  • Page 13: Dimensional 3-View H80 Dual Cockpit

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL DIMENSIONAL 3-VIEW H80 DUAL COCKPIT AFM H8001 SINGLE & DUAL COCKPIT Revision A Page xiii FAA APPROVAL DATE: 8/05/2014...

  • Page 14: Glossary Of Terms & Abbreviations

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL GLOSSARY OF TERMS & ABBREVIATIONS To the Rear C.G. Center of Gravity Capacity Inertial Multiplier: 1G = Weight Maximum Permitted G’s G LIMITS Gallons Generator Indicated Air Speed Instrument Flight Rules Inter-Turbine Temperature...

  • Page 15: Limitations

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL SECTION 1 LIMITATIONS: 1.1. POWERPLANT LIMITS: ENGINE General Electric Model GE-H80-100 FUEL JET A 1 acc. To AST< D 1655 89 or DERD 2494 JET A acc. to ASTMD 1655 89 ...
  • Page 16 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL STARTER: Maximum starter engagement duration is 30 seconds followed by a 60 second cool-down period; a total of 3 cycles to be followed by a 30 minute starter cool-down period. FUEL PUMPS: Continuous simultaneous operation of both fuel pumps is prohibited due to high fuel pressure.

  • Page 17: Powerplant Instrument Markings

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 1.2. POWERPLANT INSTRUMENT MARKINGS The following conventions represent the colors used in the MVP-50T Glass Panel Engine Monitoring display panel: You have exceeded a limit and an immediate action is required. Exceeding any limit will cause the indication display color to change to RED and flash, as well as illuminate a flashing Master Warning Light.
  • Page 18 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL LIMITS FEATURES MEANING RED Radial Minimum -20 to +20 YELLOW Arc Caution Range OIL TEMP (°C) 20 to 85 GREEN Arc Normal Range RED Radial Maximum RED Radial Minimum 18 to 26...

  • Page 19: Airspeed Limits

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 1.3. AIRSPEED LIMITS Speed Limits (MPH) Remarks Stall speed at maximum gross weight with 1. Flaps down stall speed – V flaps full down (15ᵒ) Stall speed at maximum gross weight with 2.

  • Page 20: Altitude Limitations: 12,000 Msl

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 1.4. ALTITUDE LIMITATIONS: 12,000 MSL 1.5. MAXIMUM WEIGHT AND CENTER OF GRAVITY LIMITS NOTE: DATUM is the leading edge of the wing. For Single and Dual Cockpit Maximum Weight: 10,500 lbs. Maximum Landing Weight: 7600 lbs.

  • Page 21: Using Forward Ballast To Manage Aft Empty Cg Position For The Dual Configuration

    1.8. TYPES OF OPERATION The model S2R-H80 aircraft is approved for day and night VFR flight conditions. Flight into or near thunderstorms or into known icing conditions is PROHIBITED. GROUND OPERATION: Ground operation is approved at ground idle power with the propeller feathered for 30 minutes.

  • Page 22: Placards

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 1.11. PLACARDS 1.11.1. SINGLE COCKPIT/SINGLE CONTROL Located on Right Hand lower instrument panel: “THE OPERATION OF THIS AIRPLANE IS LIMITED TO DAY AND NIGHT VFR FLIGHT CONDITIONS. FLIGHT INTO OR NEAR THUNDERSTORMS OR INTO KNOWN ICING CONDITIONS IS PROHIBITED.
  • Page 23 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL Located on the forward Lower Corner of Each side door window: “DO NOT OPEN DOOR IN FLIGHT.” “DO NOT OPEN DOOR ON THE GROUND WITH THE ENGINE RUNNING UNLESS HEADED OUT OF THE WIND WITH PROPELLER FEATHERED.”...
  • Page 24 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL LocatedbelowMVP-50Tscreen: “USEABLE FUEL 114 U.S. GAL.PER TANK. FUEL ABOVE 82 GAL. IS UNGAGEABLE” Locate inside baggage compartment on floor near baggage compartment doors: “100 POUNDS MAXIMUM BAGGAGE” Locate at hopper rinse port: ”HOPPER RINSE FILLER PORT”...
  • Page 25 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL Locate above main fuel filler caps: “FUEL LEVEL INDICATOR 110 U. S. GAL 100 U. S. GAL 88 U. S. GAL 66 U. S. GAL” Locate below main fuel filler caps: “FUEL TANKS ARE INTERCONNECTED.

  • Page 26: Dual Cockpit/Single Control

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 1.11.2. DUAL COCKPIT/SINGLE CONTROL All placards listed in 1.11.1 for the single cockpit/single control with these additional placards for dual cockpit/single control: Locate in rear cockpit on extrusion. Part of Padding installation.
  • Page 27 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL Locate in the center of rear instrument panel: “STABILIZED GROUND OPERATION IS PROHIBITED BETWEEN 400 AND 1100 RPM. THE PROPELLER MAY BE OPERATED WHEN FEATHERED AT OR BELOW 400 RPM.” Locate below MVP-50T screen on rear instrument panel: “USEABLE FUEL 114 U.S.

  • Page 28: Kinds Of Operation Equipment List

    * ½ indicates that 2 only required if rear seat occupied. Numbers in represent a required item per FAR 91.205 Numbers in GREEN represent a required item per Thrush Aircraft Type Design. Abbreviations: SC/SC Single Cockpit/Single Control DC/SC Dual Cockpit/Single Control DC/DC Dual Cockpit/Dual Control Required for Commercial Ag Operations.

  • Page 29: Normal Procedures

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL SECTION 2: NORMAL PROCEDURES: 2.1. PRE-FLIGHT VISUAL INSPECTION EXTERIOR INSPECTION ROUTE SINGLE AND DUAL COCKPIT CONFIGURATIONS AFM H8001 SINGLE & DUAL COCKPIT Revision B Page 15 FAA APPROVAL DATE: 3/19/2015...
  • Page 30 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL Visually check the aircraft for general condition during the walk around inspection. Verify that all skin panel Camlocs are fastened. In cold weather, remove all accumulations of frost, ice, or snow from wing, tail and control surfaces. Check that control surfaces contain no internal accumulations of ice.
  • Page 31 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL NOTE: Position 4, 6 and 1 SHALL be sequenced as shown below to prevent introduction of air in the fuel system during fuel system check. Position 4: a. Wing Tie Down REMOVE b.
  • Page 32 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL NOTE: When Rear Seat of Dual Cockpit S2R-H80 is to be occupied in flight, check that hopper rinse tank is full. CAUTION The owner and pilot are responsible for keeping the airplane’s CG within allowable limits.
  • Page 33 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL NOTE: Keep the wing leading edge clean. An excessive build-up of dirt, bugs, and chemicals can have the same negative effect on lift as an accumulation of ice or frost. b. Pitot Mast CHECK for blockage of opening.

  • Page 34: Mvp-50T Glass Panel Engine Monitoring System

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 2.2. MVP-50T GLASS PANEL ENGINE MONITORING SYSTEM MVP-50T MAIN SCREEN PROCEDURES The MVP-50T Main Engine Screen displays the primary engine and aircraft instruments, but not flight instruments. This screen is displayed on electrical power-up and should be monitored throughout the flight.
  • Page 35 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL To assist the pilot in identifying the current operating band (green, yellow, red or white), the MVP-50T displays the digital value for each function in its appropriate color band. In addition, annunciators are provided across the top of the display. When a function reaches a red or yellow operating band, blinking digits for that function and an annunciator will alert the pilot.

  • Page 36: Operating Checklist

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 2.3. OPERATING CHECKLIST Before Starting the Engine: Visual Inspection COMPLETE Flaps Seat ADJUST Rudder Pedals ADJUST and LOCK Seat Belt & Shoulder Harness ADJUST and LOCK All Switches Altimeter Avionics Door Latches...
  • Page 37 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL Auto Start Enable switch Fuel Condition Lever IDLE Start switch FORWARD to Start position and HOLD for three seconds, then release CAUTION There is a maximum number of three unsuccessful start attempts allowed. The fuel drain accumulator must be drained prior to any additional attempts.

  • Page 38: Dry Motoring Run

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 2.4. DRY MOTORING RUN Dry motoring run is used for draining of residual fuel and vapor from the flow path whenever it is necessary, or if undesirable combustions might occurs after engine shutdown or when lubrication system is to be filled.

  • Page 39: Before Take-Off

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 2.7. BEFORE TAKE-OFF Before proceeding with a ground run-up, be sure that the propeller system is purged, by feathering the propeller once or twice with the Power Lever in the idle position. Items a –...
  • Page 40 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL Climb Maintain maximum continuous power as necessary After obstacles are cleared a power reduction and a propeller speed reduction for noise may be desirable. NOTE: Maximum engine efficiency is achieved at 1900 propeller RPM.
  • Page 41 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL After clearing the runway: Flaps RETRACT Engine Shutdown: NOTE: Engine must be cooled down for 5 (five) minutes at ground idle before engine shutdown. Parking Brakes Power Lever IDLE NOTE: Allow the engine to stabilize at idle for a minimum of 5 (five) minutes before shutting down for maximum engine longevity.

  • Page 42: 2.9. Engine Re-Start Procedures On The Ground

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 2.9. ENGINE RE-START PROCEDURES ON THE GROUND 2.9.1 ENGINE RE-START PROCEDURES ON THE GROUND FOR ALL AIRCRAFT WITH ENGINES NOT!!!! LISTED IN TABLE 1 BELOW: 2.9.2 USE NORMAL ENGINE START PROCEDURES DEFINED IN SECTION 2.3 OF THIS DOCUMENT.
  • Page 43 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL Immediately before starting, perform “Dry motoring” as described in this document. Then wait 2 minutes to cool down starter generator. Start engine using procedures described in this document. Engine restart more than 60 minutes.

  • Page 44: Emergency Procedures

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL SECTION 3: EMERGENCY PROCEDURES 3.1. INTRODUCTION The urgency of certain emergencies requires immediate and instinctive action by the pilot. The most important single consideration is aircraft control. All procedures are subordinate to this requirement: “Never stop flying the aircraft”.
  • Page 45 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL WARNING FAULT/ADVISORY LIGHTS Illuminates approximately 5 – 10 mph above Stall Speed, Buzzer will STALL also sound Engine Oil Pressure is Low as indicated by low oil pressure switch, confirm low oil pressure with gauge, if low.
  • Page 46 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL ANNUNCTIATION LIGHTS LISTED BELOW CAN BE EITHER YELLOW OR RED, BASED ON CONVENTIONS OUTLINED IN SECTION 1.2 - INSTRUMENT MARKINGS: G METER Aircraft being flown in caution range or above. NG not within parameters...

  • Page 47: Ground Engine Fire

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 3.5. GROUND ENGINE FIRE See “DRY MOTORING RUN”, Section 2 3.6. IN-FLIGHT ENGINE FIRE In case of an in-flight fire, the following procedures should be used: Reduce power to minimum level to sustain flight.

  • Page 48: Emergency Hopper Dump

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL Prepare for forced landing. If terrain is rough, turn on Battery Switch “BATT” and extend flaps as desired, then turn off “BATT” switch. Side-slip to prevent fire from reaching cockpit. LAND AS SOON AS POSSIBLE 3.7.

  • Page 49: Engine Failure In-Flight

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL ENGINE FAILURE IN-FLIGHT Engine failure symptoms could include any or all of the following: Loud noises followed by heavy vibration and loss of power, smoke and/or flame. Rapid loss of power with unusual noises, vibration or sudden increase of ITT.

  • Page 50: Engine Flameout

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 3.10. ENGINE FLAMEOUT The indications of any engine flameout will be a drop in the ITT (inter-turbine temperature), torque pressure and RPM. The flameout may result from the engine running out of fuel or possibly by unstable engine operation.

  • Page 51: Air Starts

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL After power is restored and you have climbed to a safe altitude, reduce the engine power lever to idle and continue the flight to a safe place to land using the Fuel Condition Lever as you would normally use the Engine Power Lever.
  • Page 52 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL NOTE: Propeller feathering is dependent on circumstances and is at the discretion of the pilot. Fine pitch selection will pump air through the engine, and therefore increase the gas generator motoring speed during the Air Start procedure. Regardless of where the prop control lever is, loss of engine oil pressure will cause the prop to feather.

  • Page 53: Aborted Take-Off

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 3.13. ABORTED TAKE-OFF Should the pilot deem it necessary to abort a takeoff, the following steps are advised: Power Control Lever: Full Beta or Reverse as necessary. Brakes: Apply as permitted by aircraft attitude and directional control.

  • Page 54: Forced Landings

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 3.14. FORCED LANDINGS Forced Landing with engine power remaining: Maintain 107 MPH IAS and once landing area is assured, apply full flaps Select a safe area to dump hopper if possible. Dump the hopper load and...

  • Page 55: Emergency Egress

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 3.15. EMERGENCY EGRESS If it is necessary to remove the cockpit door from its hinges, do the following: KNOCK OUT the oval panel below the window. REACH through the hole and PULL UP the flexible hinge pin.

  • Page 56: Performance

    4.1. INTRODUCTION The intent of this Performance Supplement is to provide the operator of the Thrush Aircraft Inc. S2R-H80 Aircraft with performance information when the aircraft is loaded to weights in excess of 6000 pounds up to and including 10,500 lbs. (Refer to C.G. Limits on page 1.6 of this manual.)
  • Page 57 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL INTERNATIONAL STANDARD ATMOSPHERE (ISA) TEMPERATURES The International Standard Atmosphere (ISA) is used in most aircraft operations and is standard throughout the industry. Temperature values for this atmosphere are provided below for ease in navigating the following series of performance charts. Values are provided in degrees Celsius.

  • Page 58: Airspeed Calibration

    4.2. AIRSPEED CALIBRATION The following charts provide the airspeed calibration for the Thrush S2R-H80 at a takeoff gross weight of 10,500 lbs and at a light weight of 6850 lbs. To use these charts to determine Calibrated Airspeed, enter the chart at the value of Indicated Airspeed, proceed vertically until the line is encountered.
  • Page 59 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT Revision A Page 45 FAA APPROVAL DATE: 8/05/2014...
  • Page 60 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT Revision A Page 46 FAA APPROVAL DATE: 8/05/2014...
  • Page 61 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT Revision A Page 47 FAA APPROVAL DATE: 8/05/2014...
  • Page 62 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT Revision A Page 48 FAA APPROVAL DATE: 8/05/2014...

  • Page 63: Stalling Speed Versus Aircraft Weight

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 4.3. STALLING SPEED VERSUS AIRCRAFT WEIGHT The following two charts provide the Aircraft Stalling Speeds for both the Flaps Up and Flaps 15ᵒ cases. EXAMPLE: To determine the Stalling Speed at an Aircraft Weight of 8500 pounds, enter the Flaps Up chart at that weight.
  • Page 64 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT Revision A Page 50 FAA APPROVAL DATE: 8/05/2014...
  • Page 65 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT Revision A Page 51 FAA APPROVAL DATE: 8/05/2014...

  • Page 66: Installed Engine Horsepower

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 4.4. INSTALLED ENGINE HORSEPOWER The first of the following four charts provides the Installed Torque Available for several ISA values up to the maximum torque limit of 2020 Ft. Lbs. This chart was used to determine...
  • Page 67 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT Revision A Page 53 FAA APPROVAL DATE: 8/05/2014...
  • Page 68 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT Revision A Page 54 FAA APPROVAL DATE: 8/05/2014...
  • Page 69 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT Revision A Page 55 FAA APPROVAL DATE: 8/05/2014...
  • Page 70 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT Revision A Page 56 FAA APPROVAL DATE: 8/05/2014...

  • Page 71: Takeoff Distance To 50 Feet Above Ground Level

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 4.5. TAKEOFF DISTANCE TO 50 FEET ABOVE GROUND LEVEL The Takeoff Distance to 50 feet above ground level in no wind conditions is provided in the following two charts. The first chart provides the takeoff distance to 50 feet above ground level at a takeoff gross weight of 10,500 lbs.
  • Page 72 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT Revision A Page 58 FAA APPROVAL DATE: 8/05/2014...
  • Page 73 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT, Revision A Page | 59 FAA APPROVAL DATE: 08/05/2014...

  • Page 74: Climb Performance

    AIRPLANE FLIGHT MANUAL 4.6. CLIMB PERFORMANCE The following two charts provide Climb Performance of the S2R-H80 at various temperatures, altitudes and weights. Best Rate of Climb Speed, VY, at 10,500 lbs. gross weight varies linearly from 106 MCAS at Sea Level to 105 MCAS at 10,000 ft.
  • Page 75 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL Note: Flaps at 15° AFM H8001 SINGLE & DUAL COCKPIT, Revision A Page | 61 FAA APPROVAL DATE: 08/05/2014...
  • Page 76 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT, Revision A Page | 62 FAA APPROVAL DATE: 08/05/2014...

  • Page 77: Landing Distance From 50 Feet Above Ground Level

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 4.7. LANDING DISTANCE FROM 50 FEET ABOVE GROUND LEVEL The Landing Distance from 50 feet above ground level in no wind conditions is provided in the following two charts. The first chart provides the landing distance from 50 feet above ground level at the maximum landing weight of 7600 lbs.
  • Page 78 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT, Revision A Page | 64 FAA APPROVAL DATE: 08/05/2014...
  • Page 79 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL AFM H8001 SINGLE & DUAL COCKPIT, Revision A Page | 65 FAA APPROVAL DATE: 08/05/2014...

  • Page 80: Section 5: Weight & Balance

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL SECTION 5: WEIGHT & BALANCE 5.1. WEIGHT & BALANCE PROCEDURE NOTE: DATUM is the leading edge of the wing Maximum Weight: 10,500 lbs in any configuration. This is the baseline certified weight and does not include any overload.

  • Page 81: S2R-H80 Single And Dual Cockpit C.g. Envelope

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 5.2. S2R-H80 SINGLE AND DUAL COCKPIT C.G. ENVELOPE AFM H8001 SINGLE & DUAL COCKPIT Revision A Page | 67 FAA APPROVAL DATE: 8/05/2014...

  • Page 82: Wam - Example

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 5.3. WAM - EXAMPLE Balance of an aircraft is a simple formula, it can be remembered simply as WAM, or: Weight X Arm = Moment. Weight is in pounds, Arm is the location where the weight is taken, in inches, when measured from the Datum which in this case is the leading edge of the wing.
  • Page 83 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL EXAMPLE 1: Let’s work an example weight and balance calculation for a single cockpit version or dual cockpit with the rear seat empty.  Aircraft empty taken from the original weight and balance form is 4750 lbs with an arm of 25.02 inches and a total moment of 118,845.
  • Page 84 S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL EXAMPLE 2: Dual Cockpit Version:  200 lbs. of cargo at an arm of 114.0. FIRST LOADING  200 lbs. for a passenger at an arm of 127.0. SECOND LOADING Sample loading with cargo in the aft cockpit:...
  • Page 85 Any compartment behind the wing leading edge has a positive arm. NOTE: In the dual cockpit S2R-H80, the hopper rinse tank is utilized for ballast when the rear cockpit is occupied. Whenever a crewmember occupies the rear seat, the hopper rinse tank must be filled with water.

  • Page 86: Using Forward Ballast To Manage Aft Empty Cg Position For The Dual Cockpit Configuration

    S2R-H80 Single & Dual Cockpit AIRPLANE FLIGHT MANUAL 5.5. USING FORWARD BALLAST TO MANAGE AFT EMPTY CG POSITION FOR THE DUAL COCKPIT CONFIGURATION. A second battery is standard and will be used as permanent Ballast. A Hopper Rinse System is standard equipment and must be filled with water whenever the rear seat is occupied by a crewmember.

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