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MD Helicopters MD 530F PLUS Flight Manual
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MD Helicopters MD 530F PLUS Flight Manual

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CSP−FF−1, Rotorcraft Flight Manual
Manual:
530F–Plus (369FF) Helicopter
Model:
Ressue #1:
14 August 1998
Revision 5:
3 October 2003
FILING INSTRUCTIONS:
NOTE: Ensure that Revision 4 to Reissue #1 of CSP–FF–1 has been inserted into your manu-
al before posting Revision 5.
REMOVE PAGES
F−i thru F−xiv
4−15 & 4−16
5−11 & 5−12
R
FRONT MATTER:
SECTION I
All pages
SECTION II:
2−5 & 2−6
SECTION III
All pages
SECTION IV:
4−5 & 4−6
SECTION V:
SECTION VII:
All pages
SECTION VIII:
All pages
SECTION IX:
All pages
369 Series
RFM Revision
INSERT PAGES
F−i thru F−xiv
New Revision 5 Pages
2−5 & 2−6
New Revision 5 Pages
4−5 & 4−6
4−15 & 4−16
5−11 & 5−12
New Revision 5 Pages
New Revision 5 Pages
New Revision 5 Pages
A/(B blank)

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  • Page 1 369 Series RFM Revision CSP−FF−1, Rotorcraft Flight Manual Manual: 530F–Plus (369FF) Helicopter Model: Ressue #1: 14 August 1998 Revision 5: 3 October 2003 FILING INSTRUCTIONS: NOTE: Ensure that Revision 4 to Reissue #1 of CSP–FF–1 has been inserted into your manu- al before posting Revision 5.
  • Page 3 THE ‘‘AIRWORTHINESS LIMITATIONS’’ LISTED IN SECTION 04−00−00 OF CSP−HMI−2 SHALL BE COMPLIED WITH. THIS MANUAL MUST BE KEPT IN THE HELICOPTER AT ALL TIMES. Copyright E 1999−2003 by MD Helicopters, Inc. All rights reserved under the copyright laws. Revision 4...
  • Page 4 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) LOG OF REVISIONS BY DATE FAA / NON–FAA REVISIONS REVISION DATE/NUMBER Original Issue . . . 25 October 1985 Revision 1 ..11 April 1990 Revision 2 .

  • Page 5: Table Of Contents

    ROTORCRAFT FLIGHT MANUAL MD 530F Plus CSP–FF–1 (Model 369FF) TABLE OF CONTENTS PARAGRAPH PAGE Cover ..............

  • Page 6: Paragraph Page

    CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) PARAGRAPH PAGE 2−9. Starter Limitations ........... .
  • Page 7 ROTORCRAFT FLIGHT MANUAL MD 530F Plus CSP–FF–1 (Model 369FF) PARAGRAPH PAGE 4−7. Cruise ............. . .
  • Page 8 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) PARAGRAPH PAGE Section VII – Handling, Servicing, and Maintenance 7−1. Helicopter Components ..........
  • Page 9 ROTORCRAFT FLIGHT MANUAL CSP–FF–1 MD 530F Plus (Model 369FF) SUMMARY OF REVISIONS TO THE ROTORCRAFT FLIGHT MANUAL NOTE: Revisions are listed below by number with appropriate remarks. REVISION REMARKS NUMBER Revision 5 Section I: Removed company logo from all pages and replaced refer ences to McDonnell Douglas with MDHI.

  • Page 10: F−Ii

    CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) LIST OF EFFECTIVE PAGES FAA APPROVED NON FAA APPROVED SECTION PAGE NUMBER REVISION NUMBER REVISION NUMBER FRONT Cover − − − − − − − − Revision 3 MATTER F−i Revision 5 −...
  • Page 11 ROTORCRAFT FLIGHT MANUAL CSP–FF–1 MD 530F Plus (Model 369FF) LIST OF EFFECTIVE PAGES FAA APPROVED NON FAA APPROVED SECTION PAGE NUMBER REVISION NUMBER REVISION NUMBER 1−13 − − − − − − − − Revision 5 1−14 − − − − − − − −...
  • Page 12 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) LIST OF EFFECTIVE PAGES FAA APPROVED NON FAA APPROVED SECTION PAGE NUMBER REVISION NUMBER REVISION NUMBER 3−3 Revision 5 − − − − − − − − 3−4 Revision 5 − − − − − − − −...
  • Page 13 ROTORCRAFT FLIGHT MANUAL CSP–FF–1 MD 530F Plus (Model 369FF) LIST OF EFFECTIVE PAGES FAA APPROVED NON FAA APPROVED SECTION PAGE NUMBER REVISION NUMBER REVISION NUMBER 4−7 Revision 4 − − − − − − − − 4−8 Revision 4 − − − − − − − −...
  • Page 14 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) LIST OF EFFECTIVE PAGES FAA APPROVED NON FAA APPROVED SECTION PAGE NUMBER REVISION NUMBER REVISION NUMBER 5−8 Revision 4 − − − − − − − − 5−9 Revision 4 − − − − − − − −...
  • Page 15 ROTORCRAFT FLIGHT MANUAL CSP–FF–1 MD 530F Plus (Model 369FF) LIST OF EFFECTIVE PAGES FAA APPROVED NON FAA APPROVED SECTION PAGE NUMBER REVISION NUMBER REVISION NUMBER 6−13 − − − − − − − − Revision 4 6−14 − − − − − − − −...
  • Page 16 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) LIST OF EFFECTIVE PAGES FAA APPROVED NON FAA APPROVED SECTION PAGE NUMBER REVISION NUMBER REVISION NUMBER VIII 8−i/(8−ii blank) − − − − − − − − Revision 5 8−1 − − − − − − − −...
  • Page 17 Table 1−2. Fuel System: Optional Self−Sealing Fuel Tanks ....1−13 Figure 1−1. MD 530F Plus Principal Dimensions − Standard Landing Gear 1−14 1−15. Conversion Charts and Tables .
  • Page 19 Refer to Section IX for Optional Equipment. MDHI optional equipment items and STC items which are FAA approved for the MD 530F Plus may be installed and used. Revision 5 1–1...
  • Page 20 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General 1–5. PILOT’S BRIEFING Prior to flight, passengers should be briefed on the following. Approach and depart the rotorcraft from the front in full view of the pilot, being aware of the main and tail rotor.
  • Page 21 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General SECTION III − EMERGENCY AND MALFUNCTION PROCEDURES (FAA Approved) Problems which could be encountered in flight are defined and the proce dures necessary to cope with or alleviate them are discussed. The data is recommended by MDHI.
  • Page 22 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General 1–7. METHOD OF PRESENTATION General information in the various sections is provided in narrative form. Oth er information is given in step−by−step procedures, graphs, charts, or tabular form. The information in the step−by−step procedure is presented in the imperative mode;...
  • Page 23 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General mand. However, the nature of the specific problem or malfunction may dictate termination of the flight before reaching the destination. 1–9. ABBREVIATIONS Extend; External Air Conditioner Fahrenheit Above Ground Level Federal Aviation Alternate;...
  • Page 24 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General Imperial Out of Ground Effect INST Instrument Inches Panel INST(R) Instrument POSN Position IVSI Instantaneous Vertical Primary Speed Indicator PRESS Pressure Pounds per Square Inch Kilogram Power KCAS Knots Calibrated Airspeed...
  • Page 25 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General Best Rate of Climb Speed Water Line U.S. United States XMSN Transmission XPNDR Transponder 1–10. TECHNICAL PUBLICATIONS A file of technical publications is available to aid in obtaining maximum utili zation of your rotorcraft.
  • Page 26 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General New and revised publications are available through MDHS Subscription Ser vice. Further information may be obtained by contacting: MD Helicopters, Inc. M615−G048 4555 E McDowell Rd Mesa, AZ 85215−9734 or your local Service Center, Distributor, or Sales Company.
  • Page 27 Helicopter interior: The standard MD 530F Plus requires a minimum crew of one pilot seated on the left side of the cockpit. The passengers sit to the right, abreast of the pilot. Seat belts are provided for all positions. In the military version, the center seat is eliminated.
  • Page 28 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General Limiting the maximum power to less than the maximum rated power pro vides a higher engine critical altitude. The power turbine governor provides automatic constant speed control of rotor RPM.
  • Page 29 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General 1–12. ELECTRICAL SYSTEM The 530F Plus electrical system is a direct current (DC) system with electrical power supplied by a 24 volt battery and a 28 volt, 200 amp generator driven by the aircraft’s powerplant.
  • Page 30 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General 1–13. AUTO REIGNITION SYSTEM The automatic reignition system provides automatic actuation of the ignition exciter in the event that power is lost as a result of engine flameout. The system senses signals from the engine power out warning unit and con sists of a indicator light (RE IGN P RST) on the instrument panel, a RE−IGN...
  • Page 31 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General 1–14. CAPACITIES AND DIMENSIONS Table 1–1. Fuel System: Standard Non Self–Sealing Fuel Tanks Imp. U.S. Pounds/ Fuel Type Liters Kilograms Jet−A Usable 51.7 62.1 421.9/191.4 Unusable 13.1/5.9 Total 53.3 64.0 435.0/197.3...
  • Page 32 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General F04−001 Figure 1–1. MD 530F Plus Principal Dimensions – Standard Landing Gear 1–14 Revision 5...
  • Page 33 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General 1–15. CONVERSION CHARTS AND TABLES EXAMPLE: CONVERT 100 KNOTS TO MPH AND TO KM/HR: ENTER CHART AT 100 KNOTS AND FOLLOW ARROW TO SLOPING LINE. TO FIND MPH, MOVE LEFT AND READ 115 MPH.
  • Page 34 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General TEMPERATURE ° ° EXAMPLE: CONVERT °F TO °C KNOWN: TEMPERATURE = 50° F METHOD: ENTER AT 50° F READ 10° C ACROSS ON °C SCALE METHOD MAY BE REVERSED TO FIND ° F WHEN ° C IS KNOWN –10...
  • Page 35 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General Table 1–3. Liquid Measure – U.S. Gallons to Liters U.S. Liters Liters Liters Liters Liters Liters Liters Liters Liters Liters Gallons – 3.785 7.571 11.356 15.142 18.927 22.713 26.498 30.283 34.069...
  • Page 36 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General Table 1–5. Linear Measure – Feet to Meters Feet Meters Meters Meters Meters Meters Meters Meters Meters Meters Meters – 0.305 0.610 0.914 1.219 1.524 1.829 2.134 2.438 2.743 3.048 3.353...
  • Page 37 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General KNOTS METERS/SEC EXAMPLE CONVERT KNOTS TO METERS/SEC KNOWN: WIND SPEED = 25 KT METHOD: ENTER CHART AT 25 KT READ APPROXIMATELY 13 METERS/SEC ACROSS ON METERS/SEC SCALE METHOD MAY BE REVERSED TO FIND KNOTS WHEN METERS/SEC ARE KNOWN F03–005...
  • Page 38 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General EXAMPLE 1: 29.44 IN. HG = 997 MBAR EXAMPLE 2: 30.18 IN. HG = 1022 MBAR 29.5 30.5 31.1 29.4 30.4 31.0 29.3 30.3 30.9 29.2 30.2 30.8 29.1 30.1 30.7...
  • Page 39 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) General Table 1–7. Standard Atmosphere Table Standard Sea Level Conditions: Temperature: 59°F (15°C) Pressure: 29.921 in. Hg (1013.25 mbar) Density: 0.0023769 slugs/ft (1.225 kg/m TEMPERATURE ALTITUDE ALTITUDE DENSITY DENSITY PRESSURE PRESSURE PRESSURE...
  • Page 41 ROTORCRAFT FLIGHT MANUAL CSP–FF–1 MD 530F Plus (Model 369FF) Limitations 2–7. POWERPLANT LIMITATIONS Engine torque limits: Maximum takeoff (5 minute): 59.6 psi torque. Maximum continuous: 48.9 psi torque Transient torque limits: None. Turbine outlet temperature limits: Maximum takeoff (5 minute): 768°C Maximum continuous: 694°C...
  • Page 42 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) Limitations 2–8. ELECTRICAL SYSTEM LIMITATIONS Generator limits: Maximum continuous: 140 amps 140 to 200 amps: 10 minutes Battery limits: Flight following a battery overtemperature of 160°F (71°C) or above is pro hibited until the battery has been inspected.
  • Page 43 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures I I I E C T I O N MERGENCY AND ALFUNCTION ROCEDURES TABLE OF CONTENTS PARAGRAPH PAGE 3−1. General ............. .
  • Page 44 MD 530F Plus CSP–FF–1 ROTORCRAFT FLIGHT MANUAL (Model 369FF) Emergency and Malfunction Procedures PARAGRAPH PAGE Anti−Torque Failure ..........
  • Page 45 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures SECTION III EMERGENCY AND MALFUNCTION PROCEDURES 3–1. GENERAL The procedures contained in this section are recommendations to be followed in the event of an emergency or malfunction that may potentially affect the safety of the aircrew, passengers, aircraft, or personnel on the ground.
  • Page 46 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures 3–2. WARNING AND CAUTION INDICATORS Warning and caution indicators are located at the top of the instrument panel. A red warning or yellow caution indicator will illuminate and in some cases, an audible warning will sound announcing a failure or malfunction.
  • Page 47 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures 3–3. ENGINE FAILURE COMPLETE POWER LOSS ENGINE Indications: Red warning indicator ON and audible warning in headset. Left yaw (due to a reduction in torque) Drop in engine speed.
  • Page 48 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures The maximum glide distance with power off will be attained at 80 KIAS and 410 N Glide distances attained during an actual engine out autorotation may be less than...
  • Page 49 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures Procedures: Engine Failure − Above 12 Feet and Below 500 Feet AGL The Height − Velocity Diagram (Ref. Section V) depicts the combinations of air speeds vs. altitudes wherein a successful autorotation landing can be made in the event of an engine failure.
  • Page 50 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures 3–4. AIR RESTART – ENGINE Because the exact cause of engine failure cannot be determined in flight, the decision to attempt a restart will depend on aircraft altitude, time available, rate of descent, and potential landing areas.
  • Page 51 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures 3–5. LOW ROTOR SPEED ENGINE Indications: Red warning indicator ON and audible warning in headset. Drop in rotor RPM. Change in noise level. NOTE : The LOW ROTOR warning is activated when N falls below 453.
  • Page 52 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures Level aircraft and apply full collective pitch as contact is made with the water. When aircraft begins to roll, lower collective to full down to minimize blades skipping off the water.
  • Page 53 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures 3–7. FIRE The safety of the helicopter occupants is the primary consideration when a fire occurs. Therefore, if airborne, it is imperative that the pilot maintain control of the aircraft and land immediately.
  • Page 54 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures Procedures: Aircraft Evacuation A thorough preflight passenger briefing is essential for a quick and safe evacuation of passengers and crew when fire is involved. How to release...
  • Page 55 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures Conditions: Engine compartment fire Procedures: Twistgrip CUTOFF Fuel shutoff valve PULL TO CLOSE BAT/EXT switch Passengers/crew EVACUATE IF TIME AND SITUATION PERMIT: Rotor brake (if installed) APPLY...
  • Page 56 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures Conditions: At high altitude (AGL) Procedures: Prevailing circumstances such as altitude (AGL), available landing areas, and confirmation of engine fire must be considered in order to determine whether to execute a power−on approach, as described for low altitude...
  • Page 57 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures Conditions: In flight Procedures: Land immediately POWER ON APPROACH AND LANDING WITHOUT DELAY Air vents VENTILATE CABIN AS NECESSARY Twistgrip CUTOFF–AS SOON AS HELICOPTER IS ON GROUND...
  • Page 58 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures 3–8. ENGINE FUEL CONTROL SYSTEM MALFUNCTIONS FUEL CONTROL OR POWER TURBINE GOVERNOR FAILURE Indications: Failure is indicated by an instrument needle fluctuation. A rise or drop of: Torque Conditions: Failure Producing an Overspeed.
  • Page 59 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures Conditions: Failure Producing an Underspeed: Indications: decaying. Possible left yaw. Possible low rotor warning indication. Procedures: Lower collective to maintain rotor RPM in the green (410−508) and at tempt level flight at 60 knots IAS.
  • Page 60 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures 3–9. OTHER ENGINE CAUTION INDICATIONS ENGINE CHIP DETECTOR ENGINE Indications: Yellow indicator ON. CHIPS Conditions: Metal contamination of oil. Procedures: Land as soon as possible. LOW ENGINE OIL PRESSURE Indications: Oil pressure decreasing below normal operating range (Ref.
  • Page 61 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures 3–10. MAIN ROTOR AND TAIL ROTOR TRANSMISSION MALFUNCTIONS M/R TRANSMISSION OIL PRESSURE XMSN Indications: Red indicator ON. PRESS Conditions: Transmission oil pressure low. Procedures: Land as soon as possible.
  • Page 62 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures 3–11. FLIGHT CONTROL MALFUNCTIONS ANTI−TORQUE FAILURE Different types of failure may require slightly different techniques for optimum success in recovery. Therefore, it is not possible to provide a standardized solu tion for an anti−torque emergency.
  • Page 63 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures Conditions: Anti−torque failure, fixed tail rotor pitch setting. Procedures: Adjust power to maintain 50 to 60 knots airspeed. Perform a shallow approach and running landing to a suitable area, touching down into wind at a speed between effective translational lift and 30 knots.
  • Page 64 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures CYCLIC TRIM FAILURE Indications: Inability to reduce cyclic forces with the cyclic trim switch. The failure will be one of the following types. Control of the helicopter is the primary consideration of a pilot WARNING confronted with any type of trim motor or switch malfunction.
  • Page 65 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures Conditions: Runaway trim Indications: An uncommanded longitudinal or lateral cyclic trim actuation. The cyclic may move to a full travel position or some intermediate position resulting in cyclic forces up to the maximum. Uncommanded movement can occur after cyclic trim switch actuation or as a result of an electrical short.
  • Page 66 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures 3–12. ABNORMAL VIBRATIONS Indications: Sudden, unusual or excessive vibrations occurring during flight. Conditions: The onset of unusual or excessive vibrations in the helicopter may be an indication of problems in the rotor or drive train systems.
  • Page 67 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures FUEL LOW FUEL Indications: Yellow indicator ON when approximately 35 pounds of fuel LEVEL (22.5 LBS usable) remain in fuel tank. Never use the FUEL LEVEL LOW light as a working indication of CAUTION fuel quantity.
  • Page 68 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures 3–14. ELECTRICAL SYSTEM MALFUNCTIONS BATTERY OVERTEMPERATURE Indications: Red indicator ON. TEMP 160° Conditions: Battery overtemperature at 160°F (71°C) or above. Procedures: Battery switch: OFF. NOTE : On helicopters equipped with the ‘‘generic’’ electrical system, the battery hi–temp relay removes the battery from the DC electrical bus when battery...
  • Page 69 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures GENERATOR MALFUNCTION Indications: Yellow indicator ON, and ammeter indicating zero. Generator (GEN) switch tripped to OFF (‘‘early generic’’ configuration only) NOTE : See Sections I and IV to determine which version of the electrical system is installed in the aircraft.
  • Page 70 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures Procedures: FILTER BYPASS control handle: OPEN SCAV AIR: OFF Service particle separator prior to next flight (Ref. HMI). To prevent compressor erosion avoid operation in a dirty or dusty CAUTION environment with the filter bypass door open.
  • Page 71 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Emergency and Malfunction Procedures 3–16. EMERGENCY EGRESS Pilot compartment doors: Pilot doors function as primary and emergency exits. Cabin doors: Passenger doors function as primary and emergency exits. EXIT OPEN LOCK...
  • Page 73 ROTORCRAFT FLIGHT MANUAL CSP–FF–1 MD 530F Plus Normal Procedures (Model 369FF) TAILBOOM/TAIL ROTOR Tailboom CHECK: NO DAMAGE ALLOWED Position and anti collision lights CHECK Stabilizers (vertical, horizontal and end plates) CHECK: NO DAMAGE ALLOWED Tail skid CHECK Tailboom extension to tailboom attachment for security and...
  • Page 74 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus Normal Procedures (Model 369FF) Tail rotor drive shaft coupling CHECK: NO DAMAGE ALLOWED Rock tail rotor back and forth in plane of rotation and check main rotor blades for coincidental movement. Main rotor blades for condition and abrasion strip for...
  • Page 75 ROTORCRAFT FLIGHT MANUAL CSP–FF–1 MD 530F Plus Normal Procedures (Model 369FF) 4–3. ENGINE START Cyclic stick − trimmed neutral; friction ON RECHECK Do not attempt engine start with cyclic stick in positions other than neutral. Damage to rotor head and controls will result.
  • Page 76 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus Normal Procedures (Model 369FF) During starts, overtemperatures above 826°C for 10 seconds or less with a momentary peak at 927°C for not more than 1 second are CAUTION permited. Consult Allison Engine Operation and Maintenance Man- ual if these limits are exceeded.
  • Page 77 ROTORCRAFT FLIGHT MANUAL CSP–FF–1 MD 530F Plus (Model 369FF) Performance Data F40−037A Figure 5–6. Hover Ceiling IGE, 3.5–Foot Skid Clearance Extended Landing Gear, Standard Engine Inlet FAA Approved Revision 5 5–11...
  • Page 78 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus Performance Data (Model 369FF) F40–039 Figure 5–7. Hover Ceiling IGE, 3.5–Foot Skid Clearance, Standard Landing Gear, Particle Separator Inlet with Mist Eliminator FAA Approved 5–12 Revision 4...
  • Page 79 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) E C T I O N ANDLING, ERVICING AINTENANCE TABLE OF CONTENTS PARAGRAPH PAGE 7−1. Helicopter Components ..........
  • Page 81 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Handling, Servicing and Maintenance SECTION VII HANDLING, SERVICING, AND MAINTENANCE 7–1. HELICOPTER COMPONENTS The major components of the helicopter are shown in Figure 7−1. 7–2. USE OF EXTERNAL POWER An external receptacle is located at the right side of the pilot’s compartment seat structure.
  • Page 82 CSP–FF–1 MD 530F Plus ROTORCRAFT FLIGHT MANUAL (Model 369FF) Handling, Servicing and Maintenance HORIZONTAL STABILIZER MAIN ROTOR INSTALLATION VERTICAL STABILIZER TAIL ROTOR TRANSMISSION FLIGHT CONTROLS INSTALLATION TAILBOOM AFT SECTION INSTALLATION TAIL ROTOR ASSEMBLY ENGINE FORWARD SECTION INSTALLATION INSTALLATION MAIN TRANSMISSION...
  • Page 83 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Handling, Servicing and Maintenance 7–4. GROUND HANDLING WHEELS Standard ground handling wheels, available as a special tool for helicopters not equipped with floats, are used for moving helicopter by hand and for towing helicopter (Ref.
  • Page 84 CSP–FF–1 MD 530F Plus ROTORCRAFT FLIGHT MANUAL (Model 369FF) Handling, Servicing and Maintenance 7–5. MOVING AND TOWING HELICOPTER Manual moving: Excessive lead–lag load applied to the main rotor blades during CAUTION ground handling can result in damage to the elastomeric damper buns and failure of the damper assembly.
  • Page 85 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Handling, Servicing and Maintenance 7–6. PARKING AND MOORING Parking (Ref. Figure 7−3): To prevent rotor damage from blade flapping (droop stop pounding) CAUTION as a result of air turbulence from other aircraft landing, taking off or taxiing or sudden wind gusts, rotor blades should be secured whenever helicopter is parked.
  • Page 86 CSP–FF–1 MD 530F Plus ROTORCRAFT FLIGHT MANUAL (Model 369FF) Handling, Servicing and Maintenance BLADE SOCK (5 PLACES) TIEDOWN TETHER CABLE OR MANILA ROPE MOORING ANCHOR (4 PLACES) ENGINE EXHAUST COVER ZIPPER AIR INLET FAIRING COVER PITOT TUBE COVER DOOR TIE CORD...
  • Page 87 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Handling, Servicing and Maintenance 7–7. SERVICING – GENERAL Servicing helicopter includes replenishment of fuel, changing or replenishment of oil and other such maintenance functions. Fuels, oils, other servicing materials and capacities are listed in Table 7−1.
  • Page 88 CSP–FF–1 MD 530F Plus ROTORCRAFT FLIGHT MANUAL (Model 369FF) Handling, Servicing and Maintenance Specification Material Manufacturer Turbonycoil NYCO S.A. 600) 66, Champs−Elysees−51 Rue De Ponthieu F−75008 Paris, France Aeroshell/Royco Turbine Royal Lubricants Company, Oil 500 Inc. River Road, P.O. Box 518...
  • Page 89 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Handling, Servicing and Maintenance 5. Fuel Cells − Standard Nonself−sealing, Capacity: 64.0 US Gal (242 liters), 416 pounds Optional Self−sealing, Capacity: 62.0 US Gal (234 liters), 402 pounds. Refer to Rolls−Royce 250 Series Operations Manual for complete fuel specifications.
  • Page 90 CSP–FF–1 MD 530F Plus ROTORCRAFT FLIGHT MANUAL (Model 369FF) Handling, Servicing and Maintenance One−Way Lock Continued Specification Material Manufacturer MIL–PRF–6083 Brayco Micronic 783 Castrol Industrial North America Inc. Royco 783 Royal Lubricants Company, Inc. Hydraunycoil FH−6 NYCO, S.A. 9. Battery (NiCad) − Capacity: As required...
  • Page 91 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Handling, Servicing and Maintenance OIL FILTER BYPASS INDICATOR (369F5100 M/R TRANSMISSION ONLY) TRANSMISSION OIL LEVEL SIGHT GAUGE MAIN TRANSMISSION FILLER BATTERY MAIN TRANSMISSION DRAIN VALVES LIQUID LEVEL SIGHT GAGE OVERBOARD OIL DRAIN LINE ONE−WAY LOCK...
  • Page 92 CSP–FF–1 MD 530F Plus ROTORCRAFT FLIGHT MANUAL (Model 369FF) Handling, Servicing and Maintenance ENGINE WASH ENGINE OIL FITTING TANK DRAIN MAIN TRANSMISSION OIL COOLER DRAIN ENGINE OIL COOLER DRAIN SCAVENGE OIL FILTER STATION 137.50 BULKHEAD OIL FILTER BYPASS INDICATOR ENGINE OIL FILTER...
  • Page 93 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Handling, Servicing and Maintenance 7–8. FUEL SYSTEM – SERVICING Refueling vehicle should be parked a minimum of 20 feet from helicopter dur ing fueling operation. Before starting fueling operation, always ground fueling nozzle or fuel truck to GROUND HERE receptacle (Ref.
  • Page 94 CSP–FF–1 MD 530F Plus ROTORCRAFT FLIGHT MANUAL (Model 369FF) Handling, Servicing and Maintenance Fuel draining: Fuel draining should be accomplished with helicopter as level as possible. The fuel system may be defueled in two ways: One is to defuel through the filler port, using a pump.
  • Page 95 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Handling, Servicing and Maintenance Tail rotor transmission: A liquid level sight gauge for checking oil level is located on the rear of the transmission housing. Check oil level by viewing sight gauge.
  • Page 96 CSP–FF–1 MD 530F Plus ROTORCRAFT FLIGHT MANUAL (Model 369FF) Handling, Servicing and Maintenance 7–13. CLEANING AIRCRAFT EXTERIOR AND ROTOR BLADES Use care to prevent scratching of aluminium skin when cleaning CAUTION main rotor blades. Never use volatile solvents or abrasive materials.
  • Page 97 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Handling, Servicing and Maintenance NOTE : On transmission input gear oil seals with less that 2 hours of operation, some seepage or wetting of adjacent surfaces is normal until seal is wetted and worn–in (seated).
  • Page 98 CSP–FF–1 MD 530F Plus ROTORCRAFT FLIGHT MANUAL (Model 369FF) Handling, Servicing and Maintenance Start engine (Ref. Section IV). After idle stabilizes, accelerate engine to 103 percent N . Operate until oil temperature shows an increase and ammeter reads zero. Shut down engine (Ref. Section IV).
  • Page 99 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Handling, Servicing and Maintenance DOOR FRAME PILOT’S DOOR PASSENGER/CARGO COMPARTMENT DOOR (LH SHOWN, RH SIMILAR) FUSELAGE STRUCTURE HINGE PIN DOOR HINGE DOOR STRUCTURE F60–043 Figure 7–5. Pilot and Passenger/Cargo Door Removal Revision 5 7–19...
  • Page 100 CSP–FF–1 MD 530F Plus ROTORCRAFT FLIGHT MANUAL (Model 369FF) Handling, Servicing and Maintenance 7–19. SPECIAL OPERATIONAL CHECKS AND PROCEDURES Cleaning engine compressor: Water wash provisions are incorporated in current configuration helicopters (Ref. Figure 7−4). Engine compressor cleaning should be performed by qualified personnel in accordance with the HMI and the Engine Operation and Maintenance Manual.
  • Page 101 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Handling, Servicing and Maintenance Procedures: Ensure engine anti−ice, cabin heat, and scav air (if installed) are off prior to engine wash or rinse. Water injection will be started three seconds prior to starter engagement.
  • Page 103 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Additional Operations and Performance Data VIII E C T I O N DDITIONAL PERATIONS ERFORMANCE TABLE OF CONTENTS PARAGRAPH PAGE 8−1. Hover Ceiling − Out of Ground Effect (OGE) ......
  • Page 105 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Additional Operations and Performance Data SECTION VIII ADDITIONAL OPERATIONS AND PERFORMANCE DATA 8–1. HOVER CEILING – OUT OF GROUND EFFECT (OGE) Select the appropriate hover performance chart for the type of CAUTION engine inlet installed.
  • Page 106 MD 530F Plus CSP–FF–1 ROTORCRAFT FLIGHT MANUAL (Model 369FF) Additional Operations and Performance Data F40–034 Figure 8–1. Hover Ceiling, OGE, Standard Engine Air Inlet 8–2 Revision 5...
  • Page 107 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Additional Operations and Performance Data F40–035 Figure 8–2. Hover Ceiling, OGE, Engine Air Particle Separator Inlet Revision 5 8–3...
  • Page 108 MD 530F Plus CSP–FF–1 ROTORCRAFT FLIGHT MANUAL (Model 369FF) Additional Operations and Performance Data F40–036 Figure 8–3. Hover Ceiling, OGE, Engine Air Particle Separator Inlet with Mist Eliminator 8–4 Revision 5...
  • Page 109 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Optional Equipment E C T I O N PTIONAL QUIPMENT TABLE OF CONTENTS PARAGRAPH PAGE 9−1. General Information ..........
  • Page 111 OPTIONAL EQUIPMENT 9–1. GENERAL INFORMATION This section provides general supplemental information on optional equipment for the MD 530F Plus Helicopter. The information includes a listing of usable optional equipment. Supplemental data is prepared and included in this section whenever the in...
  • Page 112 MD 530F Plus CSP–FF–1 ROTORCRAFT FLIGHT MANUAL (Model 369FF) Optional Equipment Table 9–1. Optional Equipment – Model 369FF Helicopter Publication Equipment *Pitot heat CSP−FF−1 *Extended landing gear CSP−FF−1 *Rotor brake CSP−FF−1 *Engine air particle separator filter CSP−FF−1 Cargo hook CSP−FF−1 Section IX Emergency floats CSP−FF−1 Section IX...
  • Page 113 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Optional Equipment Cargo Hook Kit 9–4. OPERATING INSTRUCTIONS: CARGO HOOK KIT PART I GENERAL The MDHI Cargo Hook Kit consists of a cargo hook which attaches to the fuse lage keel beam, electrical connections to provide the pilot with cargo release or jettison capability using a switch on the cyclic stick, and a manual backup re lease mechanism.
  • Page 114 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) Optional Equipment Cargo Hook Kit PART II LIMITATIONS Weight Limitations: Maximum takeoff and landing gross weight 3100 pounds. Weight CAUTION in excess of 3100 pounds must be external and jettisonable. Maximum Rotorcraft − Load Combinations operating gross weight 3750 pounds (FAR 133).
  • Page 115 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Optional Equipment Cargo Hook Kit EXTERIOR LOAD IAS (KNOTS) PRESS ALT x 1000 GROSS WT = 3200 LB OR LESS °C –30 –20 –10 FLIGHT EXTERIOR LOAD IAS (KNOTS) PRESS ALT x 1000 GROSS WT = 3201 TO 3750 LB °C...
  • Page 116 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) Optional Equipment Cargo Hook Kit PART III EMERGENCY AND MALFUNCTION PROCEDURES ENGINE FAILURE: The presence of an external load may further complicate a failed engine condition. Release of loads attached through the cargo hook should be ac complished as soon as practical;...
  • Page 117 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Optional Equipment Cargo Hook Kit PART IV NORMAL PROCEDURES Normal Operation: Preflight Place battery switch in BAT position and check that HOOK circuit breaker is in. Push cargo load ring (D−ring or suitable substitute) into hook throat.
  • Page 118 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) Optional Equipment Cargo Hook Kit EXTERNAL RELEASE (TURN CLOCKWISE) ELECTRICAL WIRE HARNESS KEEPER MANUAL RELEASE CABLE HOOK (LOAD BEAM) F40–049 Figure 9–3. Cargo Hook PART V PERFORMANCE DATA Refer to Section V for IGE hover performance or Section VIII for OGE hover performance to assist in planning operations with the cargo hook.
  • Page 119 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Optional Equipment Cargo Hook Kit 16000 14000 12000 10000 8000 6000 4000 2000 INDICATED AIRSPEED − KNOTS (CORRECTED FOR INSTRUMENT ERROR) F40–038 Figure 9–4. Speed for Best Rate of Climb FAA Approved Revision 5 9–9...
  • Page 120 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) Optional Equipment Cargo Hook Kit PART VI WEIGHT AND BALANCE DATA The following table of Cargo Hook Loading Data should be used by the opera tor to assist in evaluating the helicopter center of gravity for various hook load weights.
  • Page 121 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Optional Equipment Emergency Floats 9–5. OPERATING INSTRUCTIONS – EMERGENCY FLOATS PART I GENERAL The MDHI Emergency Float Kit, consists of inflatable bag−type floats intended for use in emergency landings only, during over−water operation. It is fur nished with squib−actuated valves and with steel pressure vessels.
  • Page 122 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) Optional Equipment Emergency Floats PART II LIMITATIONS Night flight over water beyond autorotational capability to ground is prohib ited, unless 369D292032 Night Landing Kit is installed. Flight with floats inflated, or at time of inflation, is limited to the conditions of altitude and temperature presented on the EMERGENCY FLOATS INFLATED PLACARD.
  • Page 123 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Optional Equipment Emergency Floats Gross weight limitations: Maximum gross weight is 3000 pounds. Minimum gross weight is 1803 pounds. Center of gravity limits: Longitudinal C.G. Limit Lateral C.G. Limit Gross Weight (lb) (Sta−in.)
  • Page 124 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) Optional Equipment Emergency Floats EMER FLOATS – INFLATED IAS (KNOTS) ° –30 –20 –10 NO FLIGHT FOR AUTOROTATION V REDUCE SPEED BY 22K (85K MIN); DO NOT EXCEED CHART V FLOATS STOWED...
  • Page 125 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Optional Equipment Emergency Floats FLOATS STOWED IAS (KNOTS) ° –30 –20 –10 NO FLIGHT FOR AUTOROTATION V REDUCE SPEED BY 22K (86K MIN); DO NOT EXCEED CHART V MAX V 130 KTS WITH LESS THAN 30 LB FUEL...
  • Page 126 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) Optional Equipment Emergency Floats FLOATS STOWED IAS (KNOTS) PRESS ALT X 1000 GROSS WT = 2201 TO 2300 LB ° –30 –20 –10 NO FLIGHT FOR AUTOROTATION V REDUCE SPEED BY 22K (88K MIN);...
  • Page 127 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Optional Equipment Emergency Floats FLOATS STOWED IAS (KNOTS) PRESS ALT X 1000 GROSS WT = 2401 TO 2500 LB ° –30 –20 –10 NO FLIGHT FOR AUTOROTATION V REDUCE SPEED BY 22K (90K MIN);...
  • Page 128 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) Optional Equipment Emergency Floats FLOATS STOWED IAS (KNOTS) PRESS ALT X 1000 GROSS WT = 2601 TO 2700 LB ° –30 –20 –10 NO FLIGHT FOR AUTOROTATION V REDUCE SPEED BY 22K (92K MIN);...
  • Page 129 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Optional Equipment Emergency Floats FLOATS STOWED IAS (KNOTS) PRESS ALT X 1000 GROSS WT = 2801 TO 2900 LB ° –30 –20 –10 NO FLIGHT FOR AUTOROTATION V REDUCE SPEED BY 22K (94K MIN);...
  • Page 130 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) Optional Equipment Emergency Floats PART III EMERGENCY AND MALFUNCTION PROCEDURES EMERGENCY FLOAT INFLATION If emergency occurs at airspeeds greater than maximum CAUTION permissible float inflation speed, i.e., 81 knots IAS at less than 6,000 feet altitude, 77 knots IAS at 6,000 feet altitude and above, reduce speed to an appropriate value prior to float inflation.
  • Page 131 MD 530F Plus ROTORCRAFT FLIGHT MANUAL CSP–FF–1 (Model 369FF) Optional Equipment Emergency Floats PART IV NORMAL PROCEDURES Preflight checks: Check condition and security of stowed float package. Check pressure gauge in each float package. If the pressure vessel is at 70°F (21.1°C), the pressure should read within 3000 to 3500 psig (Ref.
  • Page 132 CSP–FF–1 ROTORCRAFT FLIGHT MANUAL MD 530F Plus (Model 369FF) Optional Equipment Emergency Floats PRESSURE GAGE INSPECTION WINDOW RIGHT HAND SKID (LEFT HAND SIMILAR) PRESSURE GAGE F04–050 Figure 9–6. Float Pressure Gauge PART V PERFORMANCE DATA Hover Performance with Stowed Floats No change from that of the basic helicopter with extended landing gear.

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