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Bell BHT-206L3-FM-1 LongRanger-III, Руководство по эксплуатации самолета

Bell BHT-206L3-FM-1 LongRanger-III - вертолет долгого радиуса действия с уникальной возможностью полета. Полное руководство по эксплуатации включено в Полетное Руководство, которое можно бесплатно скачать на manualshive.com. Обеспечивает безопасный и уверенный полет для пилотов всех уровней квалификации.

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Содержание BHT-206L3-FM-1 LongRanger-III

Страница 1: ...TEXTRON INC AND BELL HELICOPTER TEXTRON CANADA LTD ALL RIGHTS RESERVED BHT 206L3 FM 1 MODEL 206L3 28 OCTOBER 1992 REVISION 6 26 APRIL 2005 ROTORCRAFT FLIGHT MANUAL THIS MANUAL SHALL BE IN THE HELICOPT...

Страница 2: ...CE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron Inc P O Box 482 Fort Worth Texas 76101 0482 PN BHT 206L3...

Страница 3: ...vision 11 25 MAY 90 Reissued 0 28 OCT 92 Revision 1 09 AUG 93 Revision 2 14 SEP 95 Revision 3 04 JUN 97 Revision 4 03 MAR 99 Revision 5 18 DEC 01 Revision 6 26 APR 05 LOG OF PAGES REVISION REVISION NO...

Страница 4: ...sion 2 12 DEC 83 Revision 3 26 OCT 84 Revision 4 14 MAR 85 Revision 5 21 OCT 86 Revision 6 24 JUL 87 Revision 7 09 MAY 88 Revision 8 14 OCT 88 Revision 9 12 SEP 89 Revision 10 04 DEC 89 Revision 11 25...

Страница 5: ...sion 2 12 DEC 83 Revision 3 26 OCT 84 Revision 4 14 MAR 85 Revision 5 21 OCT 86 Revision 6 24 JUL 87 Revision 7 09 MAY 88 Revision 8 14 OCT 88 Revision 9 12 SEP 89 Revision 10 04 DEC 89 Revision 11 25...

Страница 6: ...onjunction with the Flight Manual The manual is divided into four sections Section 1 WEIGHT AND BALANCE Section 2 SYSTEMS DESCRIPTION Section 3 OPERATIONAL INFORMATION Section 4 HANDLING SERVICING MAI...

Страница 7: ...r of Gravity Direct Current Decrease Environmental Control System Emergency Locater Transmitter Engine Fahrenheit Foot Feet Generator Governor Hd Hg HP HYDR IDLE REL IFR IGE IN INCR INST LT KCAS kg LB...

Страница 8: ...AA APPROVED BHT 206L3 FM 1 SL Sea Level TOT or Turbine Outlet Temperature TURB OUT TEMP T R Tail Rotor TRANS Transmission VFR Visual Flight Rules Vne Never Exceed Velocity WRN Warning XMSN Transmissio...

Страница 9: ...EED ALTITUDE AMBIENT AIR TEMPERATURE MANEUVERING ELECTRICAL GENERATOR POWERPLANT GAS PRODUCER RPM POWER TURBINE RPM TOT TURBINE OUTLET TEMPERATURE ENGINE TORQUE FUEL PRESSURE ENGINE OIL PRESSURE ENGIN...

Страница 10: ...BHT 206L3 FM 1 FAA APPROVED Figure Number LIST OF FIGURES Title Page Number 1 1 Gross weight center of gravity 1 5 1 2 Placards and decals 1 6 1 3 Instrument markings 1 12 1 2...

Страница 11: ...Torque events shall be recorded A torque Refer to appropriate Flight Manual event is defined as a takeoff or a load lift Supplement s for additional limitations internal or external procedures and per...

Страница 12: ...ity chart in the maintenance manual Selective passenger loading does not apply and the ALTERNATE placard shall be installed The pilot is responsible for determining weight and balance to ensure gross...

Страница 13: ...FAA APPROVED BHT 206L3 FM 1 119 2 3026 Figure 1 1 Gross weight center of gravity 1 5...

Страница 14: ...ble if Technical Bulletin 206L 01 209 has not been accomplished Airspeed limits shown are valid only for the corresponding altitudes and temperatures Dashes indicate conditions which exceed approved t...

Страница 15: ...is applicable when Technical Bulletin 206L 01 209 has been accomplished Airspeed limits shown are valid only for the corresponding altitudes and temperatures Dashes indicate conditions which exceed ap...

Страница 16: ...TC APPROVED BHT 206L3 FM 1 26 APR 2005 Rev 6 1 7 Figure 1 2 Placards and Decals Sheet 3 of 3 AVOID CONT OPS 71 8 TO 91 5 N2 Location Instrument panel 206L3FM_1_0001...

Страница 17: ...B OUT TEMP OR 100 TORQUE CAN CAUSE GAS PRODUCER TOPPING WITH RESULTANT ROTOR RPM DROOP Continuous operation 0 to 90 DC LOAD Maximum 90 DC LOAD Continuous operation 63 to 105 Maximum 105 Maximum transi...

Страница 18: ...conds above 100 Intentional use prohibited 100 105 1 22 FUEL PRESSURE Minimum Continuous operation 4 PSI 4 to 25 PSI Maximum 25 PSI BHT 206L3 FM 1 Minimum Continuous operation 4 PSI 4 to 25 PSI Maximu...

Страница 19: ...Seconds ON 30 Minutes OFF 30 Minutes OFF 1 27 TRANSMISSION 1 26 TRANSMISSION OIL PRESSURE Minimum Continuous operation Maximum 30 PSI 40 to 70 PSI 70 PSI 1 29 TRANSMISSION OIL TEMPERATURE Continuous o...

Страница 20: ...o Allison Operation and intenance Manual for cold weather fuel and blending instructions Re Ma 1 35 ENGINE OIL Turbine oil MIL L 7808 may be used at all ambient temperatures DOD L 85734 AS or MIL L 23...

Страница 21: ...s operation 130 PSI Maximum ENGINE OIL TEMPERATURE m 0 to 107oc Continuous operation Maximum TRANSMISSION OIL PRESSURE 30 PSI Mmlmum 40 to 70 PSI Continuous operatlo 70 PSI Maximum TRANSMISSION OIL TE...

Страница 22: ...m for start and shutdown 1 second max TOT between 770 and 927 C longer than 10 seconds or TOT above 927 C NOTE Range Mark at 999 C Any one of the two turbme outlet temperature gages may be mstalled I...

Страница 23: ...usable L LUAU I 90 Maximum FUEL PRESSURE 4 PSI Minimum 4 to 25 PSI Continuous operatio I 25 PSI Maximum I NOTE Either indicator may be installed m DC LOAD n Maximum FUEL PRESSURE m 4PSI Minimum 0 25...

Страница 24: ...CENTER RIGHT SIDE FUSELAGE AFT RIGHT SIDE FUSELAGE FULL AFT FUSELAGE AFT LEFT SIDE FUSELAGE CABIN LEFT SIDE FUSELAGE FRONT INTERIOR AND PRESTART CHECK ENGINE STARTING PRELIMINARY HYDRAULIC SYSTEMS CH...

Страница 25: ...planned adequately to ensure safe operations and to provide the pilot with the data to be used during flight Check type of mission to be performed and destination Select appropriate performance chart...

Страница 26: ...BHT 206L3 FM 1 FAAAPPROVED Figure 2 1 Preflight check sequence 2 4...

Страница 27: ...riveshaft forward coupling Condition security and grease leakage Check Temp Plates four places for evidence of elevated temperature indicated by dot changing color to black SIDE 1 2 3 4 5 2 10 Right s...

Страница 28: ...ine Condition security of attachments Evidence of oil leakage c Engine mounts Condition and security d Throttle linkage Condition security and freedom of operation e Fuel control and mechanical fuel p...

Страница 29: ...grease leakage and overheating 9 Oil cooler blower Clear of obstruction and condition 10 Oil cooler Condition and leaks BHT 206L3 FM 1 11 Oil cooler access door Secured 12 Aft fairing Secured 13 Bagga...

Страница 30: ...plate Condition security of attachment bolts and locking hardware 7 Forward fairing and access door Secured 6 Cabin doors and hinge pins Condition and security 9 Windows Condition and security 2 8 Rev...

Страница 31: ...If the INST LT switch Is on the caution lights can be dimmed and may not be visible Effective helicopter S N 51390 and subsequent With the INST LT switch rheostat on and CAUTION LIGHT switch position...

Страница 32: ...C AND 768 C WITH START TIMES LESS THAN 40 SECONDS NOTE At the appropriate GAS PRODUCER RPM and TURB OUT TEMP introduce fuel with the throttle to obtain the initial TURB OUT TEMP rise Observe the 927...

Страница 33: ...d control movement or motoring with hydraulic system off may indicate hydraulic system malfunction HYDRAULIC SYSTEM switch OFF then ON 5 Check normal operation of cyclic control by moving cyclic in an...

Страница 34: ...light and navigation instruments Check Maximum pressure altitude is 20 000 feet For high altitude operation refer to appropriate 6 FUEL QTY Note indication operating rules for oxygen requirements 9 FU...

Страница 35: ...wo minutes ELT if installed Check for inadvertant transmission Radios and navigation equipment OFF IDLE REL button Press and hold TO ENSURE ENGINE CUTOFF HOLD THROTTLE IN CLOSED POSITION UNTIL GAS PRO...

Страница 36: ...c gross weight of helicopter 4 Helicopter to be left unattended Perform the following 1 Moor aft main rotor blade with tiedown assembly by drawing blade FAA APPROVED down lightly against the static st...

Страница 37: ...ND EFFECT ENGINE RESTART ENGINE OVERSPEED ENGINE UNDERSPEED ENGINE COMPRESSOR STALLS ENGINE OIL PRESSURE LOW HIGH OR FLUCTUATING ENGINE OIL TEMPERATURE HIGH HYDRAULIC SYSTEM FAILURE TAIL ROTOR FAILURE...

Страница 38: ...duration of flight are at the discretion of the pilot Extended flight beyond the nearest approved landing area is not recommended The following terms are used to describe the operating condition of a...

Страница 39: ...TRANS OIL PRESS XMSN OIL pressure is below minimum TRANS OIL TEMP XMSN OIL temperature is at or above red line BATTERY RLY Battery relay has malfunctioned to closed position with BAT switch OFF Batte...

Страница 40: ...nd below 6 000 feet pressure pump assembly failed altitude if flight permits Land as soon as practical 3 4 ENGINE EMERGENCIES 3 5 ENGINE FIRE DURING START OR SHUTDOWN INDICATIONS 1 Excessive TURB OUT...

Страница 41: ...Engine out audio if functional activated when GAS PRODUCER drops below 55 RPM ROTOR RPM decreases with ROTOR LOW caution light and audio on when ROTOR drops below 90 RPM Engine instruments indicate p...

Страница 42: ...D SMOOTHLY WHILE MAINTAINING CYCLIC IN NEUTRAL OR CENTERED POSITION EXCESSIVE GROUND RUN WITH COLLECTIVE UP OR ANY TENDENCY TO FLOAT FOR LONG DISTANCE PRIOR TO GROUND CONTACT SHOULD BE AVOIDED 3 9 ENG...

Страница 43: ...ions If the GAS PRODUCER RPM can be controlled with throttle then a power turbine governor failure or power turbine accessory drive failure is indicated If the GAS PRODUCER RPM and POWER TURBINE RPM a...

Страница 44: ...pilot elects to shut down engine 7 Throttle Closed 1 Engine pops 8 FUEL VALVE switch OFF 2 High or erratic TURB OUT TEMP 9 Collective Adjust as required to 3 Decreasing or erratic GAS maintain 90 to...

Страница 45: ...malfunctions The key to successful handling of a tail rotor emergency lies in the pilot s ability to quickly recognize the type of malfunction that has occurred 3 17 COMPLETE LOSS OF TAIL ROTOR THRUS...

Страница 46: ...r is reduced Power and AIRSPEED should be adjusted to a value where a comfortable yaw angle can be maintained If AIRSPEED is increased the vertical fin will become more effective and an increased left...

Страница 47: ...rom the forward fuel cells and maintain the helicopter within CG limits For night operation approximately one hour of battery power will be available 4 Land as soon as practical 3 22 FUEL TRANSFER FAI...

Страница 48: ...ION Figure Number LIST OF FIGURES Title 4 l 4 2 4 3 4 4 4 5 4 6 4 7 4 6 4 9 Power assurance check Density altitude chart Hover ceiling in ground effect Hover ceiling out of ground effect Critical rela...

Страница 49: ...r power check may be 2 below that shown on figure 4 1 and still achieve predicted flight manual performance Record the following information from cockpit instruments HP Example 10 000 ft I OAT Example...

Страница 50: ...TAPPROVED LEVEL FLIGHT POWER TURBINE 100 RPM DC LOAD 17 5 MODEL 206L3 POWER ASSURANCE ALLISON 250 C3OP F 85 TO 105 KIAS NOT TO EXCEED VNE ENGINE ANTI ICING OFF HEATER EM OFF Figure 4 11 Power assuranc...

Страница 51: ...a Enter the bottom of the chart at 15 C b Move vertically upward to the 6000 foot pressure altitude line c From this point move horizontally to the left and read a density altitude of 4000 feet BHT 20...

Страница 52: ...BHT 206L3 FM 1 FAA APPROVED...

Страница 53: ...D EFFECT 25 C TO 51 51 7 C TAKEOFF POWER POWER TURBINE 100 RPM DC LOAD 17 5 SKID HEIGHT 2 5 FT 0 7 METER ENGINE ANTI ICING OFF 30 20 10 0 10 20 30 40 50 26 20 30 32 34 36 38 40 42 44 I Figure 4 3 Hove...

Страница 54: ...C POWER SEENOTEBELOW POWER TURBINE 100 RPM DC LOAD 17 5 SKID HEIGHT 2 5 FT 0 7 METER ENGINE ANTI ICING Oh NOTE THIS HELICOPTER CAN BE HOVERED IGE AT MAXIMUM GROSS WEIGHT WITH LESS THAN TAKEOFF POWER...

Страница 55: ...FF POWER POWER TURBINE 100 RPM DC LOAD 17 5 HOVER CEILING OUT OF GROUND EFFECT 25 C TO 51 7 C SKID HEIGHT 40 FT 12 2 METERS1 ENGINE ANTI ICING OFF GROSS WEIGHT kg X 100 Figure 4 4 Hover ceiling out of...

Страница 56: ...A APPROVED I 1 I HOVER CEILING OUT OF GROUND EFFECT 25 C TO 5 C TAKEOFF POWER POWER TURBINE 100 RPM DC LOAD 17 5 SKID HEIGHT 40 FT 12 2 METERS ENGINE ANTI ICING ON Hover ceiling out of ground effect S...

Страница 57: ...t hover capability could be expected at a site having the following conditions H 10 000 ft OAT 30 C From the appropriate IGE chart obtain A maximum of 3550 pounds 1610 kilograms for all allowable wind...

Страница 58: ...14 000 feet pressure altitude curve From this point move horizontally to the right to intersect the 3600 pound gross weight line Drop vertically and read a rate of climb of 1530 feet per minute 4 5 R...

Страница 59: ...FAA APPROVED BHT 206L3 FM 1 RATE OF CLIMB TAKEOFFPOWER POWER TURBINE 100 RPM DC LOAD 17 5 57 KIAS ENGINE ANTI ICING OFF Rate of climb Sheet 1 of 4 4 13...

Страница 60: ...PROVED RATE OF CLIMB TAKEOFF POWER POWER TURBINE 100 RPM DCLOAD 17 5 57 KIAS ENGINE ANTI ICING ON 60 40 20 0 20 0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 OAT C RATE OF CLIMB Figure 4 6 Rate of cli...

Страница 61: ...06L3 FM 1 RATE OF CLIMB MAXIMUM CONTINUOUS POWER POWER TURBINE 100 RPM DC LOAD 17 5 57 KIAS ENGINE ANTI ICING OFF 60 40 20 0 20 40 60 0 2 4 6 6 10 12 14 16 16 20 22 24 26 OAT Figure 4 6 Rate of climb...

Страница 62: ...BHT 206L3 FM 1 FAA APPROVED RATE OF CLIMB MAXIMUM CONTINUOUS POWER POWER TURBINE 100 RPM DC LOAD 17 5 57 KIAS ENGINE ANTI ICING ON 60 Figure 4 6 Rate of climb Sheet 4 of 4 4 16...

Страница 63: ...FAA APPROVED 500 450 I Figure 4 7 Height velocity diagram BHT 206L3 FM 1 4 17...

Страница 64: ...BHT 206L3 FM 1 FAA APPROVED Figure 4 8 Altitude vs gross weight limits for height velocity diagram 4 18...

Страница 65: ...UMENT ERROR POSITION ERROR KCAS NOTE This chart assumes zero instrument error KNOTS KNOTS INDICATED AIRSPEED CALIBRATED AIRSPEED KIAS KCAS 35 32 5 45 42 5 50 47 55 52 50 57 70 55 5 80 75 5 90 86 5 100...

Страница 66: ...ssued Particle Separator Engine 3 Mar 99 Air Induction System BHT 206L3 FMS 4 206 706 341 December 11 1981 Reissued 2000 Pound Capacity 8 Nov 99 Cargo Hook BHT 206L3 FMS 5 206 705 001 July 21 1982 Rei...

Страница 67: ...n Addendum for 2000 Pound Capacity Cargo Hook BHT 206L3 FMS CAA Supplement for United Kingdom Registered Helicopters BHT 64 IAF 206L3 FMS 1 Engine Fire Detection System and Heated Pitot Tube BHT 84 IA...

Страница 68: ...ht Manual Supplements for Optional Equipment Cont DATE CURRENT NAME OF EQUIPMENT KIT NUMBER CERTIFIED REVISION BHT 84 IAF 206L3 FMS 4 Instrument Panel Radio Console Circuit Breaker Panel 10 15 84 Reis...

Страница 69: ...Information contained herein supplements information of basic Flight Manual For Limitations Procedures and Performance Data not contained in this supplement or other applicable supplements consult bas...

Страница 70: ...APPROVED NOTICE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron Inc P 0 Box 482 Fort Worth Texas 76101 0482...

Страница 71: ...28 OCT 92 Revision 14 MAR 87 Reissue 0 08 NOV 99 Revision 2 15 MAY 87 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title NP 0 C D 0 A B 0 1 6 0 NOTE Revised text is indicated by a black vertical lin...

Страница 72: ...REVISIONS Original 0 16 DEC 81 Reissue 0 28 OCT 92 Revision 14 MAR 87 Reissue 0 08 NOV 99 Revision 2 15 MAY 87 APPROVED DATE 1 Aov f9 CHIEF FLIGHT TEST FOR DIRECTOR AIRCRAFT CERTIFICATION BRANCH DEPAR...

Страница 73: ...BHT 206L3 FMS 1 LOG OF FAA APPROVED REVISIONS Original 0 16 DEC 81 Reissue 0 280CT92 Revision 14 MAR 87 Reissue 0 08 NOV 99 Revision 2 15 MAY 87 November 8 1999 CID...

Страница 74: ...IAS 60 MPH daily prior to performing over water operations Maximum allowable airspeed floats inflated 61 KIAS 70 MPH 1 2 WEIGHT CG 1 2 WEIGHT CG Maximum autorotation airspeed floats inflated 52 KIAS 6...

Страница 75: ...witch temperature and altitude Refer to POWER guard open placard on cylinder Check electrical connectors for security 2 FLOAT ARMED light Illuminated 2 2 INTERIOR AND PRESTART CHECK CAUTION 2 3 PREFLI...

Страница 76: ...imately 3 2 AFTER EMERGENCY 500 feet per minute WATER LANDING NOTE 1 After landing inspect the helicopter for possible damage If floats are inflated in level flight If malfunction was cause of there i...

Страница 77: ...PPROVED Section 4 4 1 HOVER CEILING effect hover performance is shown on the 4FLOATS STOWED following charts FLOATS STOWED Out of ground effect hover performance is the same as basic helicopter In gro...

Страница 78: ...2 5 FT 0 7 METER POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 15 000 FT HD LIMIT OAT C 4250 LB 1928 kg 30 20 10 0 10 20 30 40 50 26 28 30 32 34 36 38 40 42 44 LB X 100 OAT C 12 13 14 15 16...

Страница 79: ...AA APPROVED HOVER CEILING IN GROUND EFFECT WITH STANDARD INLET TAKEOFF POWER POWER TURBINE 100 RPM DC LOAD 17 5 SKID HEIGHT 2 5 FT 0 7 METER ENGINE ANTI ICING ON Hover ceiling in ground effect Sheet 2...

Страница 80: ...information of basic Flight Manual For Limitations Procedures and Performance Data not contained in this supplement or other applicable supplements consult basic Flight Manual Bell Helicopter Textron...

Страница 81: ...APPROVED NOTICE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron Inc P 0 Box 482 Fort Worth Texas 76101 0482...

Страница 82: ...1 11 JUN 82 Reissue 0 28 OCT 92 Revision 2 08 FEB 83 Reissue 0 29 NOV 99 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title NP 0 i ii 0 A B 0 1 20 0 CID 0 21 22 0 NOTE Revised text is indicated by a...

Страница 83: ...SIONS Original 0 20 JAN 82 Revision 3 14 MAR 85 Revision 1 11 JUN 82 Reissue 0 28 OCT 92 Revision 2 08 FEB 83 Reissue 0 29 NOV 99 APPROVED DATE CHIEF FLIG FOR DIRECTOR AIRCRAFT CERTIFICATION BRANCH DE...

Страница 84: ...BHT 206L3 FMS 2 LOG OF FAA APPROVED REVISIONS Original 20 JAN 82 Revision 3 14 MAR 85 Revision 1 11 JUN 82 Reissue 0 28 OCT 92 Revision 2 08 FEB 83 Reissue 29 NOV 99 November 29 1999 CID...

Страница 85: ...e bleed air heater 206 706 141 consists of two basic subsystems bleed air and heater ventilation air Bleed air flows from the engine through bleed lines to the mixing valve and into the cabin in the f...

Страница 86: ...ch HEAT and OFF NOTE VENT position is not applicable TURB OUT TEMP increases with 2 1 INTERIOR AND bleed air heater operating 2 1 I N T E R IO R A N D Observe TURB OUT TEMP PRESTART CHECK limitations...

Страница 87: ...INSTALLED S E PA R ATOR A N D S N OW To determine rate of climb performance DEFLECTOR INSTALLED with PARTICLE SEP PRG switch OFF use the rate of climb chart in this section and To determine hover cei...

Страница 88: ...00 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON WITH ENGINE ANTI ICING ON ABOVE 12 000 FT Hp G W IS 150 LB 68 kg LESS BELOW 12 000 FT NO CORRECTION IS NECESSARY 15 000 FT HD LIMIT OAT C 4250 LB 19...

Страница 89: ...2 5 FT 0 7 METER POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp G W IS 150 LB 68 kg LESS BELOW 10 000 FT NO CORRECTION ISNECESSARY OAT...

Страница 90: ...GHT 3 5 FT 1 1 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON WITH ENGINE ANTI ICING ON ABOVE 12 000 FT Hp G W IS 150 LB 68 kg LESS BELOW 12 000 FT NO CORRECTION IS NECESSAR...

Страница 91: ...ERGENCY FLOAT LANDING GEAR TAKEOFF POWER SKID HEIGHT 40 FT 12 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp G W IS 120 LB 54...

Страница 92: ...EATER ON WITH ENGINE ANTI ICING ON ABOVE 12 000 FT Hp G W IS 150 LB 68 kg LESS BELOW 12 000 FT NO CORRECTION ISNECESSARY 15 000 FT HD LIMIT OAT C AREA B I AR MAXIMUM INTERNAL GROSS WEIGHT LIMIT 4150 L...

Страница 93: ...100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp G W IS 160 LB 73 kg LESS BELOW 10 000 FT NO CORRECTION IS NECESSARY 15 000 FT HD LIMIT OAT C AREA A 4...

Страница 94: ...RPM ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON WITH ENGINE ANTI ICING ON ABOVE 12 000 FT Hp G W IS 150 LB 68 kg LESS BELOW 12 000 FT NO CORRECTION IS NECESSARY 15 000 FT HD LIMIT OAT C MAXIMUM INTE...

Страница 95: ...R TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp G W IS 130 LB 59 kg LESS BELOW 10 000 FT NO CORRECTION IS NECESSARY 15 000 FT HD LIMIT I MAX...

Страница 96: ...ANTI ICING OFF DC LOAD 17 5 HEATER ON PARTICLE SEP PURGE OFF WITH ENGINE ANTI ICING ON ABOVE 12 000 FT Hp G W IS 150 LB 68 kg LESS BELOW 12 000 FT NO CORRECTION ISNECESSARY 15 000 FT HD LIMIT OAT C M...

Страница 97: ...ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON PARTICLE SEP PURGE ON WITH ENGINE ANTI ICING ON ABOVE 12 000 FT Hp G W IS 150 LB 68 kg LESS BELOW 12 000 FT NO CORRECTION IS NECESSARY 15 000 FT HD LIMIT O...

Страница 98: ...CING OFF DC LOAD 17 5 HEATER ON PARTICLE SEP PURGE OFF WITH ENGINE ANTI ICING ON ABOVE 12 000 FT Hp G W IS 150 LB 68 kg LESS BELOW 12 000 FT NO CORRECTION ISNECESSARY OAT C 15 000 FT HD LIMIT 20 MAXIM...

Страница 99: ...100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON PARTICLE SEP PURGE ON WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp G W IS 160 LB 73 kgl LESS BELOW 10 000 FT NO CORRECTION IS NECESSARY OAT C 15 0...

Страница 100: ...0 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON PARTICLE SEP PURGE OFF WITH ENGINE ANTI ICING ON ABOVE 12 000 FT Hp G W IS 150 LB 68 kg LESS BELOW 12 000 FT NO CORRECTION ISNECESSARY 1 5 000 FT H D...

Страница 101: ...INE ANTI ICING OFF DC LOAD 17 5 HEATER ON PARTICLE SEP PURGE ON WITH ENGINE ANTI ICING ON ABOVE 12 000 FT Hp G W IS 150 LB 68 kgl LESS BELOW 12 000 FT NO CORRECTION IS NECESSARY 15 000 FT HD LIMIT OAT...

Страница 102: ...FT 12 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON PARTICLE SEP PURGE OFF WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp G W IS 130 LB 59 kg LESS BELOW 10 000 FT NO CORREC...

Страница 103: ...TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON PARTICLE SEP PURGE ON WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp G W IS 130 LB 59 kg LESS BELOW 10 000 FT NO CORRECTION ISNECESSARY 15 00...

Страница 104: ...Y SKID OR FLOAT LANDING GEAR POWER SEE BELOW 57 KIAS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF OR ON DC LOAD 17 5 HEATER ON MAXIMUM CONTINUOUS POWER 0 LU 50 TO 10 C OAT 26 28 30 32 34 36 38 40 42LB...

Страница 105: ...per minute feet and 20 C on chart hover gross less than that determined with the Rate of weight will be 90 pounds 40 8 kg less Climb Decrease chart figure 4 2 and than the weight determined on the Hov...

Страница 106: ...E ANTI ICING ON OR OFF HEATER ON NO PURGE SWITCH INSTALLED OR PURGE SWITCH ON 18 000 NOTE For points above is 90 Lbs less and 170 ft min less 12 000 10 000 For points below 2000 curve being used no pe...

Страница 107: ...attached to Model 206L 3 Flight Manual when Particle Separator Engine Air Induction System kit has been installed Information contained herein supplements information of basic Flight Manual For Limita...

Страница 108: ...c Disclosure reproduction or use of these data for any purpose other than helicopter operation is forbidden without prior written authorization from Bell Helicopter Textron inc NP Additional copies of...

Страница 109: ...8 OCT 92 Revision 2 28 OCT 82 Reissued 3 MAR 99 Revision 3 14 MAR 85 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title 0 21 22 0 NP 0 A B 0 MANUFACTURER S DATA C D 0 i ii 0 23 24 0 1 20 0 NOTE Revi...

Страница 110: ...HT 206L3 FMS 3 LOG OF DOT APPROVED REVISIONS Original 0 21 DEC 81 Reissued 0 14 OCT 88 Revision 1 21 JUL 82 Reissued 0 28 OCT 92 Revision 2 28 OCT 82 Reissued 0 3 MAR 99 Revision 3 14 MAR 85 APPROVED...

Страница 111: ...BHT 206L3 FMS 3 LOG OF FAA APPROVED REVISIONS Original 0 21 DEC 81 Reissued 0 14 OCT 88 Revision 1 21 JUL 82 Reissued 0 28 OCT 92 Revision 2 28 OCT 82 Reissued 0 15 MAR 99 Revision 3 14 MAR 85 CID...

Страница 112: ...to a restricted inlet flow With this switch ON engine bleed air is used to purge debris further affecting performance Performance charts contained in this supplement provide data for each of these co...

Страница 113: ...ns at idle power twist grip at idle shall not exceed five 5 minutes If five 5 minutes idle power time is exceeded or ground and hover operations exceed 20 minutes total helicopter shall be shut down a...

Страница 114: ...or baffles and engine air intake areas All areas checked must be clean and free of accumulated snow slush and ice before each flight 2 Check engine air plenum chamber through the plexiglass windows on...

Страница 115: ...result of bleed air being taken from the engine To determine the minimum torque available when the Particle Separator is installed refer to the Power Assurance chart in BHT 206L3 FM 1 From the minimu...

Страница 116: ...EILING IN GROUND EFFECT WITH STANDARD SKID LANDING GEAR TAKEOFF POWER SKID HEIGHT 2 5 FT 0 7 METER POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 PARTICLE SEP PURGE OFF Figure 4 1 Hover ceil...

Страница 117: ...NG IN GROUND EFFECT WITH STANDARD SKID LANDING GEAR TAKEOFF POWER POWER TURBINE 100 RPM DC LOAD 17 5 SKID HEIGHT 2 5 FT 0 7 METER ENGINE ANTI ICING OFF PARTICLE SEP PURGE ON 15 000 FT Figure 4 l Hover...

Страница 118: ...CT WITH STANDARD SKID LANDING GEAR POWER SEE NOTE BELOW SKID HEIGHT 2 5 FT 0 7 METER POWER TURBINE 100 RPM ENGINE ANTI ICING ON DC LOAD 17 5 PARTICLE SEP PURGE OFF NOTE THIS HELICOPTER CAN BE HOVERED...

Страница 119: ...ING IN GROUND EFFECT WITH STANDARD SKID LANDING GEAR POWER SEE NOTE BELOW POWER TURBINE 100 RPM DC LOAD 17 5 SKID HEIGHT 2 5 FT 0 7 METER1 ENGINE ANTI ICING ON PARTICLE SEP PURGE ON Figure 4 l Hover c...

Страница 120: ...ND EFFECT WITH HIGH SKID OR EMERGENCY FLOTATION LANDING GEAR TAKEOFF POWER POWER TURBINE 100 RPM DC LOAD 17 5 SKID HEIGHT 2 5 FT 0 7 METER ENGINE ANTI ICING OFF PARTICLE SEP PURGE OFF GROSS WEIGHT Fig...

Страница 121: ...VED HOVER CEILING IN GROUND EFFECT WITH HIGH SKID OR EMERGENCY FLOTATION LANDING GEAR TAKEOFF POWER SKID HEIGHT 2 5 FT 0 7 METER POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 PARTICLE SEP P...

Страница 122: ...N DC LOAD 17 5 PARTICLESEP PURGE OFF OC 20 TO 10 25 5 t MAXIMUM INTERNAL F 1 I 1 In 1 1 1GROSS WEIGHTLIMIT i I I Y 4150 LB 1882 kg y ff t GROSS WEIG MAXIMUM EXTERNAL iHT LIMIT 4250 LB 1928 kg L I I I...

Страница 123: ...G ON DC LOAD 17 5 PARTICLESEP PURGE ON OAT 7 15 000 FT HD LIMIT 20 TO 5 l f I GROSS WEIGHT LIMIT 8 0 LB 1882 kg e i i j i MAXIMUM EXTERNAL GROSS WEIGHT LIMIT I 4250 LB 1928 kq _ Y JETTISCiNABL v 0 1 I...

Страница 124: ...STANDARD FLOAT LANDING GEAR POWER SEE NOTE BELOW FLOAT HEIGHT 3 5 FT 1 1 METERS1 POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 PARTICLE SEP PURGE OFF NOTE THIS HELICOPTER CAN BE HOVERED IG...

Страница 125: ...I METERS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 PARTICLE SEP PURGE ON IVIYI I I I I I I I I I I I I I I I 30 20 10 0 10 20 30 40 50 26 28 30 32 34 36 38 40 42 44 I I I I I I I OAT C...

Страница 126: ...ANTI ICING ON DC LOAD 17 5 PARTICLESEP PURGE OFF OR ON NOTE THIS HELICOPTER CAN BE HOVERED IGE AT THE INDICATED GROSS WEIGHTS WITH LESS THAN TAKEOFF POWER 16 000 FT HD LIMIT tW i ii i i i i i i i i i...

Страница 127: ...3 HOVER CEILING OUT OF GROUND EFFECT WITH ANY SKID OR FLOAT LANDING GEAR TAKEOFF POWER SKID HEIGHT 40 FT 12 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 Hover ceiling out of grou...

Страница 128: ...LING OUT OF GROUND EFFECT WITH ANY SKID OR FLOAT LANDING GEAR TAKEOFF POWER SKID HEIGHT 40 FT 112 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 PARTICLE SEP PURGE ON Hover ceiling...

Страница 129: ...ILING OUT OF GROUND EFFECT WITH ANY SKID OR FLOAT LANDING GEAR TAKEOFF POWER SKID HEIGHT 40 FT 12 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING ON DC LOAD 17 5 PARTICLE SEP PURGE OFF Hover ceiling...

Страница 130: ...ING OUT OF GROUND EFFECT WITH ANY SKID OR FLOAT LANDING GEAR TAKEOFF POWER POWER TURBINE 100 RPM DC LOAD 17 5 SKID HEIGHT 40 FT 12 2 METERS ENGINE ANTI ICING ON PARTICLE SEP PURGE ON GROSS WEIGHT LIMI...

Страница 131: ...IAS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 PARTICLE SEP PURGE OFF WITH ENGINE ANTI ICING ON ABOVE 12 000 FT Hp RATE OF CLIMB IS 220 FT MIN LESS BELOW 12 000 FT NO CORRECTION IS NECES...

Страница 132: ...OFF POWER 57 KIAS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 PARTICLE SEP PURGE ON WITH ENGINE ANTI ICING ON ABOVE 12 000 FT Hp RATE OF CLIMB IS 220 FT MIN LESS BELOW 12 000 FT NO CORREC...

Страница 133: ...OWER 57 KIAS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 PARTICLE SEP PURGE ON OR OFF WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp RATE OF CLIMB IS 235 FT MIN LESS BELOW 10 000 FT NO CORR...

Страница 134: ...MANUFACTURER S DATA BHT 206L3 FMS 3 MANUFACTURER S DATA No change from basic manual Section2 MANUFACTURER S DATA ON BRT OFF DIM Figure 2 1 Miscellaneous control panel 23 24...

Страница 135: ...in supplements information of basic Flight Manual For Limitations Procedures and Performance Data not contained in this supplement or other applicable supplements consult basic Flight Manual Bell Heli...

Страница 136: ...APPROVED NOTICE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron Inc P O Box 482 Fort Worth Texas 76101 0482...

Страница 137: ...95 Revision 1 14 Mar 85 Reissue 0 08 Nov 99 Reissue 0 28 Oct 92 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title i ii 0 NP 0 1 4 0 A B 0 5 6 0 C D 0 NOTE Revised text is indicated by a black verti...

Страница 138: ...D APPROVED REVISIONS Original 11 Dec 81 Reissue 0 13 Sep95 Revision 14 Mar 85 Reissue 0 08 Nov 99 Reissue 0 28 Oct 92 APPROVED DATE CHIEF FLIGHT TEST FOR DIRECTOR AIRCRAFT CERTIFICATION BRANCH DEPARTM...

Страница 139: ...BHT 206L3 FMS 4 LOG OF FAA APPROVED APPROVED REVISIONS Original 0 11 Dec 81 Reissue 13 Sep 95 Revision 1 14 Mar 85 Reissue 0 08 Nov 99 Reissue 0 28 Oct 92 November 8 1999 C D...

Страница 140: ...cargo The hook has a rated capacity of 2000 pounds 907 2 kg The kit contains electrical and manual releases both operated from the pilots seat Cargo hook is located at FS 121 0 The external cargo hoo...

Страница 141: ...CARRYING EXTERNAL CARGO Actual weight change shall be determined A THE HANDLING after cargo hook is installed and ballast CHARACTEISTICS MAY BE AFFECTED BY THE SIZE readjusted if necessary to retain e...

Страница 142: ...G USE OF INAPPROPRIATELY SIZED LOAD RINGS MAY RESULT IN LOAD HANG UP WHEN LOAD RING IS TOO SMALL OR USE OF MULTIPLE RINGS SLINGS RING IS TOO SMALL OR OR SHACKLES ON THE LOAD INADVERTENT LOAD RELEASE I...

Страница 143: ...ht path As required to BEFORE TAKEOFF avoid flight with external load over any person vehicle or CARGO HOOK circuit breaker In structure TAKEOFF DESCENT AND LANDING 1 Flight path and approach angle As...

Страница 144: ...S SECTION DIMENSION MAXIMUM CROSS SECTION OF SECONDARY MEMBER TOLOAD S SEE TABLE 2 1 INCORRECT RIGGING INCORRECT RIGGING LOAD BEAM PRIMARY RING MULTIPI E LOAD RINGS MULTIPLE BEAM SECONDARY RINGS TOLOA...

Страница 145: ...argo hook will not of an electrical failure release sling when CARGO RELEASE switch is pressed proceed as follows Section 4 Refer to BHT 206L3 FM 1 or the Performance may be affected by size and appro...

Страница 146: ...Y 21 1982 This supplement shall be attached to Model 206L 3 Flight Manual when IFR Configuration kit has been installed Information contained herein supplements information of basic Flight Manual For...

Страница 147: ...isclosure reproduction or use of these data for any purpose other than helicopter operation is forbidden without prior written authorization from Bell Helicopter Textron Inc Additional copies of this...

Страница 148: ...late indicators used to detect overtemperature conditions of grease lubricated driveshaft couplings Insert these temporary revision pages next to like numbered pages in Flight Manual Supplement after...

Страница 149: ...BHT 206L3 FMS 5 Temporary 23 Nov 93 PAGE Title A B 7 LOG OF REVISIONS LOG OF PAGES REVISION NO PAGE FLIGHT MANUAL Temporary Temporary Temporary REVISION NO TEMPORARY REVISION 23 NOV 93 A...

Страница 150: ...4 September 12 1969 Revision 2 December 12 1963 Reissued 0 October 26 1992 LOG OF PAGES PAGE REVISION NO FLIGHT MANUAL Title NP 0 A B 0 i ii 0 l 36 0 REVISION PAGE NO MANUFACTURER S DATA 37 46 0 47 48...

Страница 151: ...HT 206L3 FMS 5 LOG OF APPROVEDREVISIONS Temporary 23 Nov 93 APPROVED MANAGER ROTORCRAFTCERTIFICATIONOFFICE FEDERAL AVIATION ADMINISTRATION FT WORTH TX 761934170 TEMPORARYREVISION23 NOV 93 FAA APPROVED...

Страница 152: ...nal 0 July 21 1962 Revision 3 March 14 1965 Revision 1 January 24 1963 Revision 4 September 12 1969 Revision 2 December 12 1963 Reissued 0 October 26 1992 APPROVED MANAGER ROTORCRAFT CERTIFICATION OFF...

Страница 153: ...l fully redundant electricat system In addition to allowing single pilot IFR capabilities the system can also be used to relieve pilot workload in VFR conditions aid in normal navigation and assist in...

Страница 154: ...ted in basic attitude retention mode or coupled in all IFR maneuvers All coupled modes shall be disengaged below 60 KIAS although attitude retention mode may be used in VFR conditions at all approved...

Страница 155: ...to bring empty weight CG within allowable limits 1 8 CENTER OF GRAVITY LONGITUDINAL Center of gravity limits for IFR operation are from station 118 0 2997 mm to 127 0 3226 mm however these limits are...

Страница 156: ...FAA APPROVED BHT 206L3 FMS 5 Gross weight center of gravity Sheet 1 of 2...

Страница 157: ...BHT 206L3 FMS 5 FAA APPROVED...

Страница 158: ...missions 2 2 BEFORE EXTERIOR CHECK 1 Flight planning Completed 2 Publications Checked I 3 Gross weight and CG Computed 4 Helicopter servicing Completed 5 Battery Connected 2 3 EXTERIOR CHECK 2 4 FUSEL...

Страница 159: ...FAA APPROVED Figure 2 l Preflight check sequence...

Страница 160: ...MAINTENANCE PERSONNEL SHALL ASSIST IN DETERMINING AlRWORTHlNESS PER ALERT SERVICE BULLETIN 206L 93 9 SHT 206L3 FMS 5 19 Power lan Area a Main driveshaft aft coupling Condition security and grease lea...

Страница 161: ...DRAIN button Press drain sample then release NOTE Forward fuel cells can be drained manually as desired BHT 206L3 FMS 5 15 A F fuel filter Drain and check before first flight of the day as follows a F...

Страница 162: ...ion and security 5 Sync elevator Check lateral freedom bearing play and clear of obstructions Tail rotor driveshaft cover Condition and security 4 Horizontal stabilizer and position light Condition an...

Страница 163: ...ft restraint damper b Transmission oil filter bypass button Ensure not visible C d e BHT 206L3 FMS 5 Main driveshaft forward coupling Condition and evidence of grease leakage Check paint strip for evi...

Страница 164: ...bin loading Refer to BHT 206L3 MD 1 to maintain CG within limits FAA APPROVED 6 Copilot seat belt Secured if solo 7 Doors Secured 6 Flight controls Loosen frictions check freedom of travel position fo...

Страница 165: ...djust as desired 32 BAT switch ON for battery start If external power is used for starting BAT switch OFF Observe ENG OUT TRANS OIL PRESS ROTOR LOW RPM and GEN FAIL caution lights illuminated 33 Exter...

Страница 166: ...tenance Manual if limits are exceeded or if TURB OUT TEMP warning light illuminates 6 TURB OUT TEMP Monitor Do not exceed 10 seconds above 768 C or a maximum of 927 C IF MAIN ROTOR IS NOT ROTATING BY...

Страница 167: ...em If abnormal forces unequal forces control binding or motoring are encountered it may be an indication of a malfunctioning flight control actuator 2 15 HYDRAULIC SYSTEMS CHECK 1 2 3 4 5 Collective F...

Страница 168: ...LIC CONTROL MAY MOTOR TO STOPS IF AUTOPILOT IS LEFT ENGAGED WHILE HELICOPTER IS ON GROUND 12 Cyclic stick Move fore aft and laterally ensure that autopilot override Is possible Center cyclic stick 13...

Страница 169: ...obtain 100 POWER TURBINE RPM This will maintain POWER TURBINE RPM within limits during low power descents however the GOV RPM switch should be positioned to INCR as collective is increased Refer to P...

Страница 170: ...S PRODUCER RPM decreasing NOTE It is not necessary to turn FUEL VALVE switch OFF since neither 10 Cyclic Apply as required to minimize mast bumping during rotor coast down 11 Rotor brake Engage betwee...

Страница 171: ...ing any autopilot mode of operation with the following exceptions Fore aft movement of ATTD TRIM switch will disengage ALT mode Pitch trim will be inoperative in APPR mode after computer has switched...

Страница 172: ...matically computed after course capture This procedure takes approximately 120 seconds to function properly Approaches should be planned to allow ample time for crosswind correction function to stabil...

Страница 173: ...y engage new mode selected Go around pitch attitude may be adjusted then by moving ATTD TRIM switch fore and aft or by pressing cyclic TRIM REL switch NOTE When using autopilot for go around following...

Страница 174: ...and reduce AIRSPEED to minimum IFR speed of 60 KIAS 69 MPH and turn into wind Verify failure from gages GAS PRODUCER less than 55 RPM and POWER TURBINE decreasing If ample altitude remains investigate...

Страница 175: ...r to non essential bus Check main generator functioning normally Check STBY GEN FIELD OVLD and RESET circuit breakers in STBY GEN switch RESET then on If power is not restored STBY GEN switch OFF PLAC...

Страница 176: ...ROACH 140 FEET 1 Sudden disturbance in helicopter attitude 2 Illumination of red AP WRN light when the helicopter attitude reaches the malfunction monitor trip limits 3 Autopilot failure audio warning...

Страница 177: ...luminated after cyclic TRIM REL switch has been released PROCEDURE NOTE With TRIM REL switch in OVERRIDE position the autopilot or force trim will be engaged and operation will be normal except that c...

Страница 178: ...ON TO PROTECT BATTERY POWER IN THIS CONDITION ONLY ESSENTIAL BUS 1 WILL BE POWERED 1 NON ESS bus switch NORM 2 MAIN GEN FIELD 24 3 MAIN GEN and STBY GEN switches RESET then on 4 Reduce electrical load...

Страница 179: ...follows 3 13 ESSENTIAL BUS 1 FAILURE BHT 206L3 FMS 5 4 Loss of autopilot No 1 radios and all other equipment on the essential bus 1 1 Helicopter attitude Correct with cyclic 2 VM SELECT switch ESS BU...

Страница 180: ...UE as follows NOTE These recommended TORQUE settings should maintain AIRSPEED within I approved IFR limits 4 Land as soon as practical 3 18 STATIC PORT ICING Delayed or inactive vertical speed and alt...

Страница 181: ...A APPROVED BHT 206L3 FMS 5 Section4 Refer to appropriate performance charts in on use of primary NORMAL static air accordance with optional equipment source installed All performance charts are based...

Страница 182: ...WER POWER TURBINE 100 RPM DC LOAD 17 5 80 KIAS ENGINE ANTI ICING OFF WITH ENGINE ANTI ICING ON ABOVE 12 000 FT Hp RATE OF CLIME IS 220 FT MIN LESS BELOW 12 000 FT NO CORRECTION IS NECESSARY 26 60 40 2...

Страница 183: ...DARD INLET MAXIMUM CONTINUOUS POWER POWER TURBINE 100 RPM DC LOAD 17 5 80 KIAS ENGINE ANTI ICING OFF WITH ENGINE ANTI ICING ON ABOVE 12 000 FT Hp RATE OF CLIMB IS 230 FT MIN LESS BELOW 12 000 FT NO CO...

Страница 184: ...C LOAD 17 5 60 KIAS ENGINE ANTI ICING OFF WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp RATE OF CLIMB IS 220 FT MIN LESS BELOW 10 000 FT NO CORRECTION IS NECESSARY 60 40 20 60 40 20 0 0 20 40 20 40 0 0...

Страница 185: ...MAXIMUM CONTINUOUS POWER POWER TURBINE 100 RPM DC LOAD 17 5 80 KIAS ENGINE ANTI ICING OFF WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp RATE OF CLIME IS 235 FT MIN LESS BELOW 10 000 FT NO CORRECTION I...

Страница 186: ...ITH PARTICLE SEPARATOR TAKEOFF POWER 80 KIAS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 PARTICLE SEP PURGE ON WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp RATE OF CLIMB IS 220 FT MIN LES...

Страница 187: ...R MAXIMUM CONTINUOUS POWER 80 KIAS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 PARTICLE SEP PURGE ON WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp RATE OF CLIMB IS 235 FT MIN LESS BELOW 10...

Страница 188: ...R 80 KIAS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 PARTlCLE SEP PURGE OFF WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp RATE OF CLIMB IS 220 FT MIN LESS BELOW 10 000 FT NO CORRECTION IS...

Страница 189: ...L3 FMS 5 AIRSPEED SYSTEM CALIBRATION LEVEL FLIGHT CLIMB AND DESCENT 1000 FPM IAS INST ERROR POSITION ERROR VCAL ASSUME ZERO INSTRUMENT ERROR INDICATED AIRSPEED KNOTS Figure 4 2 Airspeed system calibra...

Страница 190: ...LIBRATION ALTERNATE STATIC SOURCE LEVEL FLIGHT CLIMB AND DESCENT 1000 FPM IAS INST ERROR POSITION ERROR V CAL 140 120 20 0 I I I I I NOTE ASSUME ZERO INSTRUMENT ERROR INDICATED AIRSPEED KNOTS Figure 4...

Страница 191: ...ilot using the cyclic ATTD TRIM switch or TRIM REL switch When HDG mode is selected autopilot will maneuver helicopter to turn to and maintain a selected heading When ALT mode is selected autopilot wi...

Страница 192: ...topilot System status Mode selection switches on mode control panel are push on push off type and when illuminated indicate which mode is selected All remote annunciators are located in upper right co...

Страница 193: ...opic precession To set gyro compass quickly to correct heading press auto slave switch to make it pop out thereby gaining manual compass control Then press N S or E W compass rotation switch as requir...

Страница 194: ...ertical speed indicator 30 Altimeter 31 Marker beacon receiver 32 Alternate static sir source switch 33 Vent control knob 34 Radio call placard 35 Standby attitude indicator switch 36 DME selector pan...

Страница 195: ...BHT 206L3 FMS 5 Figure 2 2 Miscellaneous control panel 41...

Страница 196: ...BHT 206L3 FMS 5 Figure 2 3 Overhead console...

Страница 197: ...BHT 206L3 FMS 5 Figure 2 4 Lower circuit breaker panel 43...

Страница 198: ...BHT 206L3 FM 5 44 MODE...

Страница 199: ...BHT 206L3 FMS 5 Figure 2 6 Cyclic grip and collective 45...

Страница 200: ...DME ESS 2 VM FUEL BOOST RIGHT MKR SPKR VHF 2 COMM VHF 2 NAV Course indicator only XPNDER NON ESSENTIAL BUS ANTI COLL LT DEFOG BLOWER ICS INSTR LT MAIN GEN RESET LDG LT incl voltmeter PRI ATTD IND NON...

Страница 201: ...BHT 206L3 FM 5 Section3 MANUFACTURER S DATA No change from basic manual Section4 MANUFACTURER S DATA No change from basic manual 47 48...

Страница 202: ...be attached to Model 206L 3 Flight Manual when Environmental Control System Cabin Temperature Control kit has been installed Information contained herein supplements information of basic Flight Manua...

Страница 203: ...HT 206L3 FM 6 NOTICE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron P 0 Box 402 Fort Worth Texas 76101 0482...

Страница 204: ...1961 Reissued 0 October 28 1992 Revision 1 March 14 1965 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title NP 0 1 2 0 A B 0 3 4 0 i ii 0 NOTE Revised text is indicated by a black vertical line Inse...

Страница 205: ...BHT 206L3 FMS 6 FAA APPROVED LOG OF APPROVED REVISIONS Original 0 December 11 1961 Reissued 0 October 26 1992 Revision 1 March 14 1985 APPROVED FEDERAL AVIATION ADMINISTRATION FT WORTH TX 76193 0170 B...

Страница 206: ...is designed for heating and cooling as well as removing moisture from the air supplied to the cabin area The system runs off bleed air from the engine Installation of this system and the distribution...

Страница 207: ...y to return empty weight CG to within allowable limits Section2 2 1 INTERIOR AND PRESTART CHECK 12 C TO PREVENT DAMAGE TO ECS ECS switch OFF 2 3 BEFORE TAKEOFF 2 2 GROUND OPERATION 1 ECS circuit break...

Страница 208: ...ead and lower outlets should be closed during windshield defogging 2 5 DESCENT AND LANDING ECS switch OFF for landing 2 ECS flow switch ECS LOW ECS HIGH as desired I 3 1 OPERATING EMERGENCIES ECS swit...

Страница 209: ...ASE DUE TO ENVIRONMENTAL CONTROL SYSTEM WITH ANY INLET WITH ANY SKID OR FLOAT LANDING GEAR POWER TAKEOFF OR MAXIMUM CONTINUOUS 57 KIAS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF OR ON DC LOAD 17 5 80...

Страница 210: ...rein supplements information of basic Flight Manual For Limitations Procedures and Performance Data not contained in this supplement or other applicable supplements consult basic Flight Manual Bell He...

Страница 211: ...APPROVED NOTICE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron Inc P 0 Box 482 Fort Worth Texas 76101 0482...

Страница 212: ...ion 1 05 MAR 93 Revision 2 28 OCT 82 Revision 2 04 JAN 95 Reissued 0 14 OCT 89 Reissue 0 08 NOV 99 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title 0 C D NP 0 i ii 0 A B 0 1 18 0 NOTE Revised text...

Страница 213: ...EC 81 Reissued 0 28 OCT 92 Revision 1 03 JUN 82 Revision 1 05 MAR 93 Revision 2 28 OCT 82 Revision 2 04 JAN 95 Reissued 0 14 OCT 89 Reissue 0 08 NOV 99 APPROVED DATE CHIEF FLIG FOR DIRECTOR AIRCRAFT C...

Страница 214: ...LOG OF FAA APPROVED REVISIONS Original 0 21 DEC 81 Reissued 0 28 OCT 92 Revision 1 03 JUN 82 Revision 1 05 MAR 93 Revision 2 28 OCT 82 Revision 2 04 JAN 95 Reissued 0 14 OCT 89 Reissue 0 08 NOV 99 Nov...

Страница 215: ...e Snow Deflector Kit 206 706 208 consists of two deflectors that mount on either side of transmission fairing just forward of engine air inlets The kit adds approximately 5 pounds 2 kilograms to the e...

Страница 216: ...oval is after kit is installed and ballast readjusted accomplished if necessary to return empty weight CG to within allowable limits Refer to Center of 2 Ground operations and hover Gravity vs Weight...

Страница 217: ...r baffles and engine air inlet areas All areas checked shall be clean and free of accumulated snow WARNING slush and ice before each flight FAILURE TO INSTALL ENGINE NOTE INLET COVERS COULD ALLOW FALL...

Страница 218: ...PARTICLE SEPARATOR AND SNOW DEFLECTOR 4 2 POWER ASSURANCE INSTALLED CHECK This supplement contains two Power To determine performance when snow Assurance Check charts Figure 4 5 The deflector and part...

Страница 219: ...BHT 206L3 FMS 7 DOT APPROVED RATE OF CLIMB TAKEOFF POWER 57 KIAS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 Figure 4 1 Rate of climb Sheet 1 of 4 4 November 8 1999...

Страница 220: ...F CLIMB TAKEOFF POWER 57 KIAS POWER TURBINE 100 RPM ENGINE ANTI ICING ON DC LOAD 17 5 60 40 20 0 20 0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 OAT C RATE OF CLIMB FT MIN X 100 Figure 4 1 Rate of cl...

Страница 221: ...MS 7 DOT APPROVED RATE OF CLIMB MAXIMUM CONTINUOUS POWER 57 KIAS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 60 40 20 0 20 40 0 2 4 6 8 10 12 14 16 18 20 22 24 26 6 November 8 1999 6 Nove...

Страница 222: ...CLIMB MAXIMUM CONTINUOUS POWER 57 KIAS POWER TURBINE 100 RPM ENGINE ANTI ICING ON DC LOAD 17 5 F 60 40 20 0 20 0 2 4 6 8 10 12 14 16 18 20 22 24 26 OAT C RATE OF CLIMB FT MIN X 100 Figure 4 1 Rate of...

Страница 223: ...ON WITH SNOW DEFLECTOR AND PARTICLE SEPARATOR INSTALLED ENGINE ANTI ICING ON OR OFF NO PURGE SWITCH INSTALLED OR PURGE SWITCH ON 18 000 N TE NOTE For points above 50 40 30 20 10 0 10 20 30 OAT C 0 Fig...

Страница 224: ...FF POWER SKID HEIGHT 2 5 FT 0 7 METER POWER TURBINE 100 RPM ENGINE ANTJ ICING OFF DC LOAD 17 5 15 000 FT HD LIMIT OAT C 30 20 10 0 1020 30262830323436 38404244 LB X 100 OAT 0 C 12 13 14 15 16 17 18 19...

Страница 225: ...D HEIGHT 2 5 FT 0 7 METER POWER TURBINE 100 RPM ENGINE ANTI ICING ON DC LOAD 17 5 15 000 FT HD LIMIT OAT C AREA A MAXIMUM EXTERNAL 30 20 10 0 10 26 28 30 32 34 36 38 40 42 44 LBX 100 OAT C 12 13 14 15...

Страница 226: ...R SKID HEIGHT 2 5 FT 0 7 METER POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 OAT C 10 15 000 FT HD LIMIT 20 30 20 10 0 10 20 30 26 28 30 32 34 36 38 40 42 44 LB X 100 OAT CC 12 13 14 15 16...

Страница 227: ...AKEOFF POWER SKID HEIGHT 2 5 FT 0 7 METER POWER TURBINE 100 RPM ENGINE ANTI ICING ON DC LOAD 17 5 OAT C 15 000 FT HD LIMIT 20 TO 10 30 20 10 0 10 26 28 30 32 34 36 38 40 42 44 LB X 100 OAT C 12 13 14...

Страница 228: ...ER FLOAT HEIGHT 3 5 FT 1 1 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 15 000 FT H D LIMIT OAT C 30 20 10 0 10 20 30 26 28 30 32 34 36 38 40 42 44 LB X 100 OAT C 12 13 14 15 16 1 7...

Страница 229: ...3 5 FT 1 1 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING ON DC LOAD 17 5 NOTE THIS HELICOPTER CAN BE HOVERED IGE AT THE INDICATED GROSS WEIGHTS WITH LESS THAN TAKEOFF POWER 15 000 FT HD LIMIT AREA A...

Страница 230: ...ECT WITH ANY SKID OR EMERGENCY FLOAT LANDING GEAR TAKEOFF POWER SKID HEIGHT 40 FT 12 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 15 000 FT HD LIMIT GROSS WEIGHT Figure 4 4 Hover...

Страница 231: ...NCY FLOAT LANDING GEAR TAKEOFF POWER SKID HEIGHT 40 FT 12 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING ON DC LOAD 17 5 20 0 20 40 60 28 32 36 40 44 LB X 100 OAT C 13 14 15 16 17 18 19 kg X 100 GRO...

Страница 232: ......

Страница 233: ......

Страница 234: ...lement shall be attached to Model 206L 3 Flight Manual when Float Landing Gear Standard Type Fixed Floats kit has been installed Information contained herein supplements information of basic Flight Ma...

Страница 235: ...HT 206L3 FMS 8 NOTICE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron P 0 Box 482 Fort Worth Texas 78101 048...

Страница 236: ...September 2 1986 Revision 1 Reissued March 14 1985 0 October 26 1992 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title NP 0 1 6 0 A B 0 7 8 0 i ii 0 NOTE Revised text is indicated by a black vertic...

Страница 237: ...D LOG OF APPROVED REVISIONS Original 0 June 7 1982 Revision 2 September 2 1986 Revision 1 March 14 1985 Reissued 0 October 28 1992 APPROVED ROTORCRAFT CERTIFICATION OFFICE FEDERAL AVIATION ADMINISTRAT...

Страница 238: ...signed for water operations and consists of two streamlined four cell inflatable floats It can be operated at gross weight up to 4000 pounds 1614 4 kilograms within the limits outlined in this supplem...

Страница 239: ...et Hp decrease V 2 6 KIAS 3 MPH per 1000 feet 1 4 ALTITUDE Maximum operating H 15 000 ft 2 1 FLOAT PRESSURE VARIATION Temperature changes when moving from warm hangar to cold outside or vice versa res...

Страница 240: ...BHT 206L3 FMS 8 FAA APPROVED FLOAT PRESSURE VARIATION VERSUS TEMPERATURE AND OR ALTITUDE CHANGE 2...

Страница 241: ...TING AND RUNUP ON WATER ANCHOR OR MOOR HELICOPTER PRIOR TO STARTING ENGINE TO 2 3 TAXIING ON WATER Taxi at slow speed to prevent float bows from nosing under NOTE Safe operation can be accomplished in...

Страница 242: ...ard to the decrement line From this point move left Reduce Rate of Climb chart data from to A RATE OF CLIMB scale at a point of basic Flight Manual or appropriate optional 225 feet Subtract this figur...

Страница 243: ...FAA APPROVED BHT 206L3 FMS 8 RATE OF CLIMB DECREASE DUE TO STANDARD FLOAT LANDING GEAR...

Страница 244: ...ROUND EFFECT I 25 TO 51 7 C POWER SEE NOTE BELOW FLOAT HEIGHT 3 5 FT 1 1 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 NOTE THIS HELICOPTER CAN BE HOVERED IGE AT THE INDICATED GROSS...

Страница 245: ...G IN GROUND EFFECT 25 TO 5 C POWER SEE NOTE BELOW POWER TURBINE 100 RPM DC LOAD 17 5 FLOAT HEIGHT 3 5 FT 1 1 METERS ENGINE ANTI ICING ON NOTE THIS HELICOPTER CAN BE HOVERED IGE AT THE INDICATED GROSS...

Страница 246: ...be attached to the Model 206L 3 Flight Manual when High Skid Landing Gear kit has been installed Information contained herein supplements Information of basic Flight Manual For Limitations Procedures...

Страница 247: ...FM 9 NOTICE PAGE DOTAPPROVED Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron Inc P 0 Box 462 Fort Worth Texas 761...

Страница 248: ...ecember 1961 Reissued 0 3 March 1999 Reissued 0 28 October 1992 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title NP 0 A B 0 CID 0 i ii 0 1 4 0 NOTE Revised text is indicated by a black vertical li...

Страница 249: ...BHT 206L3 FMS 9 LOG OF DOT APPROVED REVISIONS Original 0 11 December 1981 Reissued 0 28 October 1992 Reissued 0 3 March 1999 APPROVED DATE...

Страница 250: ...BHT 206L3 FMS 9 LOG OF FAA APPROVED REVISIONS Original 0 11 December 1981 Reissued 3 March 1999 Reissued 0 28 October 1992 CID...

Страница 251: ...ten inches 25 meters of additional ground clearance over the standard skid gear This enables operations in rough terrain tall grass and other adverse conditions and allows fitting of underslung loads...

Страница 252: ...determined Maintenance Manual after kit is installed and ballast readjusted Section2 DESCENT AND LANDING Tail low run on landings should be avoided to prevent nosedown pitching RUN ON LANDINGS ON OTHE...

Страница 253: ...BHT 206L3 FMS 9 DOT APPROVED 1 Out of ground effect hover performance is same as basic helicopter In ground effect hover performance is shown in figure 4 1...

Страница 254: ...FAA APPROVED BHT 206L3 FMS 9 TAKEOFF POWER ENGINE RPM 100 GENERATOR 17 5 HOVER CEILING IN GROUND EFFECT WITH STANDARD INLET SKID HEIGHT 2 5 FT 0 7 METER ANTI ICE OFF 30 20 10 0 10 20 30 40 50...

Страница 255: ...FF POWER ENGINE RPM 100 GENERATOR 17 5 HOVER CEILING IN GROUND EFFECT WITH STANDARD INLET SKID HEIGHT 2 5 FT 0 7 METER1 ANTI ICE ON OAT C 30 20 10 0 10 26 26 30 32 34 36 38 40 42 44 LB X 100 Hover cei...

Страница 256: ...be attached to Model 206L 3 Flight Manual when Rotor Brake kit has been installed Information contained herein supplements information of basic Flight Manual For Limitations Procedures and Performance...

Страница 257: ...206L3 FM 10 NOTICE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron P 0 Box 462 Fort Worth Texas 76101 0482...

Страница 258: ...ision 2 March 3 1987 Revision 1 March 14 1985 Reissued 0 October 26 1992 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title NP 0 i ii 0 A B 0 1 2 0 NOTE Revised text is indicated by a black vertical...

Страница 259: ...OF APPROVED REVISIONS Original 0 December 11 1981 Revision 2 March 3 1987 Revision 1 March 14 1985 Reissued 0 October 28 1992 APPROVED MANAGER ROTORCRAFT CERTIFICATION OFFICE FEDERAL AVIATION ADMINIS...

Страница 260: ...des a means of positive stopping of the main and tail rotor The brake is a completely self contained hydraulic system and is operated by a handle located to the right of the overhead console The kit a...

Страница 261: ...determined after kit is installed and ballast readjusted ENGAGE ROTOR BRAKE BETWEEN 36 30 ROTOR RPM INTERIOR AND PRESTART ON ICE OR OTHER SLIPPERY OR CHECK LOOSE SURFACE TO PREVENT ROTATION OF HELICOP...

Страница 262: ...BHT 206L3 FMS 10 FAA APPROVED Section3 No change from basic manual No change from basic manual 2...

Страница 263: ...ched to Model 206L 3 Flight Manual when Area Navigation System kit has been installed Information contained herein supplements information of basic Flight Manual For Limitations Procedures and Perform...

Страница 264: ...206L3 FMS 11 NOTICE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron P O Box 402 Fort Worth Texas 76101 0482...

Страница 265: ...11 1981 Reissued 0 Revision October 26 1992 1 March 14 1985 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title NP 0 i ii 0 A B 0 1 2 0 NOTE Revised text is indicated by a black vertical line Insert...

Страница 266: ...BHT 206L3 FMS 11 FAA APPROVED LOG OF APPROVED REVISIONS Original 0 December 11 1961 Reissued 0 October 26 1992 Revision 1 March 14 1965 APPROVED B...

Страница 267: ...ALINFORMATION BHT 206L3 FMS 11 The Area Navigation System 206 705 005 Collins ANS 351 RNAV consists of a computer and a remote annunciator adjacent to HSI RNAV operates in conjunction with VHF NAV 1 r...

Страница 268: ...within allowable limits Section2 NOTE For operating procedures refer to ANS 351 Area Navigation System Pilot Guide printed by Collins Radio Group Rockwell International For operation in RNAV mode RNA...

Страница 269: ...BHT 206L3 FMS 11 FAA APPROVED Section4 No change from basic manual...

Страница 270: ...shall be attached to Bell Helicopter Model 206L 3 Flight Manual when 206 706 343 Litters Kit is installed Information contained herein supplements information of basic Flight Manual For Limitations Pr...

Страница 271: ...206L3 FMS 12 NOTICE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron Inc P 0 Box 402 Fort Worth Texas 76101 0...

Страница 272: ...1 DEC 81 Reissue 0 28 OCT 92 Reissue 0 02 SEP 97 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title NP 0 i ii 0 A B 0 1 2 0 C D 0 NOTE Revised text is indicated by a black vertical line Insert lates...

Страница 273: ...BHT 206L3 FMS 12 LOG OF DOT APPROVED REVISIONS Original 0 11 DEC 81 Reissue 0 28 OCT 92 Reissue 0 02 SEP 97 APPROVED DATE DIRECTOR AIRCRAFT CERTIFICATION BRANCH DEPARTMENT OF TRANSPORT B...

Страница 274: ...BHT 206L3 FMS 12 LOG OF FAA APPROVED REVISIONS Reissue 0 04 AUG 97 CID...

Страница 275: ...r the capability of carrying up to two patients on litters with room and access for medical attendants The kit contains aluminum litters with patient restraints and all necessary hardware for proper i...

Страница 276: ...ined be removed and stowed when litters are after kit is installed and ballast readjusted if necessary to return empty weight CG to installed within allowable limts Patients must be restrained by litt...

Страница 277: ...T MUST BE INSTALLED WHEN THIS SUPPORT IS REMOVED Located on lower litter support COVER MUST BE INSTALLED WHEN LOWER SUPPORT IS REMOVED ONE OR BOTH LITTER SUPPORTS MUST BE IN PLACE DURING FLIGHT FOR ST...

Страница 278: ...ched to Model 206L 3 Flight Manual when Increased Power Operations kit has been installed Information contained herein supplements information of basic Flight Manual For Limitations Procedures and Per...

Страница 279: ...206L3 FMS 13 NP NOTICE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron P 0 Box 482 Fort Worth Texas 76101 0...

Страница 280: ...0 1982 Reissued 0 October 28 1992 Revision 1 March 15 1983 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title NP 0 i ii 0 A B 0 1 18 0 NOTE Revised text is indicated by a black vertical line Insert...

Страница 281: ...3 FAA APPROVED LOG OF APPROVED REVISIONS Original 0 July 20 1982 Reissued 0 October 26 1992 Revision 1 March 15 1983 APPROVED ROTORCRAFT CERTIFICATION OFFICE FEDERAL AVIATION ADMINISTRATION FT WORTH T...

Страница 282: ...L3 FMS 13 The Increased Power Kit 206 706 045 allows for an increased transmission limit of 456 shp and an increased engine TORQUE of 104 8 for 5 minutes Restrictions pertaining to this increased limi...

Страница 283: ...AIRSPEED of 60 KIAS or less 1 2 POWERPLANT 1 3 ENGINE TORQUE KIT NO 206 706 045 ONLY Continuous operation 0 to 65 Maximum continuous 65 5 Minute takeoff range 65 to 104 6 Maximum for takeoff 104 6 Ma...

Страница 284: ...I BHT 206L3 FMS 13 FAA APPROVED Figure l l Instrument markings...

Страница 285: ...CAUTION SHOULD BE EXERCISED WHEN OPERATING AT LOW AIRSPEEDS ABOVE PUBLISHED PERFORMANCE CHART ALTITUDES TAIL ROTOR EFFECTIVENESS COULD BE MARGINAL AT HIGH POWER SETTINGS UNDER THESE CONDITIONS 4 2 PER...

Страница 286: ...zontally to known OAT If intersection of known H and OAT is below the known anti ice curve Example A 3000 FAA APPROVED feet H and 3O C there is not any performance variation If intersection of known H...

Страница 287: ...FAA APPROVED HOVER CEILING OUT OF GROUND EFFECT WITH STANDARD INLET TAKEOFF POWER POWER TURBINE 100 RPM DC LOAD 17 5 SKID HEIGHT 40 FT 12 2 METERS ENGINE ANTI ICING OFF...

Страница 288: ...BHT 206L3 FMS 13 FAA APPROVED HOVER CEILING OUT OF GROUND EFFECT WITH STANDARD INLET TAKEOFF POWER POWER TURBINE 100 RPM DC LOAD 17 5 SKID HEIGHT 40 FT 12 2 METERS ENGINE ANTI ICING ON...

Страница 289: ...UT OF GROUND EFFECT WITH SNOW DEFLECTOR WITH ANY SKID OR FLOAT LANDING GEAR TAKEOFF POWER SKID HEIGHT 40 FT 12 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 Hover ceiling out of gr...

Страница 290: ...ND EFFECT WITH SNOW DEFLECTOR WITH ANY SKID OR FLOAT LANDING GEAR TAKEOFF POWER SKID HEIGHT 40 FT 12 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING ON DC LOAD 17 5 I I GROSS WEIGHT Figure 4 1 Hover...

Страница 291: ...TAKEOFF POWER SKID HEIGHT 40 FT 112 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp G W IS 120 LB 54 kg LESS BELOW 10 000 FT N...

Страница 292: ...R AND BLEED AIR HEATER WITH ANY SKID OR FLOAT LANDING GEAR TAKEOFF POWER SKID HEIGHT 40 FT 112 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 HEATER ON WITH ENGINE ANTI ICING ON ABO...

Страница 293: ...AA APPROVED BHT 206L3 FMS 13 HOVER CEILING OUT OF GROUND EFFECT WITH PARTICLE SEPARATOR WITH ANY SKID OR FLOAT LANDING GEAR TAKEOFF POWER Figure 4 1 Hover ceiling out of ground effect Sheet 7 of 12 11...

Страница 294: ...OUND EFFECT WITH PARTICLE SEPARATOR WITH ANY SKID OR FLOAT LANDING GEAR TAKEOFF POWER SKID HEIGHT 40 FT 12 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING OFF DC LOAD 17 5 PARTICLE SEP PURGE ON I Fig...

Страница 295: ...MS 13 HOVER CEILING OUT OF GROUND EFFECT WITH PARTICLE SEPARATOR WITH ANY SKID OR FLOAT LANDING GEAR TAKEOFF POWER SKID HEIGHT 40 FT 12 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING ON DC LOAD 17 5...

Страница 296: ...S 13 HOVER CEILING OUT OF GROUND EFFECT WITH PARTICLE SEPARATOR WITH ANY SKID OR FLOAT LANDING GEAR TAKEOFF POWER SKID HEIGHT 40 FT 12 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING ON DC LOAD 17 5...

Страница 297: ...WITH PARTICLE SEPARATOR WITH ANY SKID OR FLOAT LANDING GEAR TAKEOFF POWER SKID HEIGHT 40 FT 12 2 METERS POWER TURBINE 100 RPM ENGINE ANTI ICING ON DC LOAD 17 5 PARTICLE SEP PURGE ON 20 0 20 40 60 26...

Страница 298: ...R TURBINE 100 RPM DC LOAD 17 5 SKID HEIGHT 40 FT 12 2 METERS1 ENGINE ANTI ICING OFF HEATER ON PARTICLE SEP PURGE OFF WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp G W IS 130 LB 59 kg LESS BELOW 10 000...

Страница 299: ...ANDING GEAR TAKEOFF POWER POWER TURBINE 100 RPM DC LOAD 17 5 SKID HEIGHT 40 FT 12 2 METERS ENGINE ANTI ICING OFF HEATER ON PARTICLE SEP PURGE ON WITH ENGINE ANTI ICING ON ABOVE 10 000 FT Hp G W IS 130...

Страница 300: ...FAA APPROVED BHT 206L3 FMS 13 PERFORMANCE VARIATION WITH SNOW DEFLECTOR AND PARTICLE SEPARATOR INSTALLED ENGINE ANTI ICING ON OR OFF HEATER OFF NO PURGE SWITCH INSTALLED OR PURGE SWITCH ON 16 000...

Страница 301: ...CE VARIATION WITH SNOW DEFLECTOR AND PARTICLE SEPARATOR INSTALLED ENGINE ANTI ICING ON OR OFF HEATER ON NO PURGE SWITCH INSTALLED OR PURGE SWITCH ON 16 000 I 12 000 30 20 10 0 10 20 30 OAT C Figure 4...

Страница 302: ...ed to Model 206L 3 Flight Manual when External Hoist kit has been installed Information contained herein supplements information of basic Flight Manual For Limitations Procedures and Performance Data...

Страница 303: ...sclosure reproduction or use of these data for any purpose other than helicopter operation is forbidden without prior written authorization from Bell Helicopter Textron Inc Additional copies of this p...

Страница 304: ...ctober 28 1992 Revision 1 July 26 1988 LOG OF PAGES PAGE REVISION REVISION NO PAGE NO FLIGHT MANUAL MANUFACTURER S DATA Title NP 0 A B 0 i ii 0 1 3 0 4 6 0 7 8 0 NOTE Revised text is indicated by a bl...

Страница 305: ...APPROVED LOG OF APPROVED REVISIONS Original 0 September 15 1983 Reissued 0 October 28 1992 Revision 1 July 26 1988 APPROVED MANAGER ROTORCRAFT CERTIFICATION OFFICE FEDERAL AVIATION ADMINISTRATION FT...

Страница 306: ...stallation Winch unit contains 110 feet 33 5 meters of usable cable Winch unit when actuated has a rate of cable travel of 50 feet 15 2 meters per minute Control panel is edge lit and contains a POWER...

Страница 307: ...st and external cargo hook is prohibited 1 2 FLIGHT CREW Crewmember in passenger compartment is required during hoist operations 1 3 WEIGHT CG Actual weight change shall be determined after kit is ins...

Страница 308: ...position I 3 HOIST OVERHEAT WARNING light if installed Press to test 4 5 6 7 6 HOIST switch pilot cyclic DN down to lower hook approximately 2 feet then UP to raise hook POWER switch located on HOIST...

Страница 309: ...ter completing hoist operation NOTE Use care to prevent hook to fuselage fouling during hoist operation I I BHT 205L3 FMS 14 6 Pilot or crewmember Ensure hook firmly seated against bumper pad 2 8 AFTE...

Страница 310: ...Right Aft Facing Passenger 12 9 Left Aft Row Forward Facing Passenger 15 6 I Center Aft Row Forward Facing Passenger 0 Right Aft Row Forward Facing Passenger 15 8 Fuel All Amounts 0 Hoist Load 25 0 Gi...

Страница 311: ...BHT 206L3 FMS 14 TOTAL WEIGHT LEFT HAND SIDE COCKPIT CABIN PILOT WEIGHT RIGHT HAND COCKPIT SEAT MAXIMUM POUNDS POUNDS POUNDS Figure 1 1 Hoist load nomograph English...

Страница 312: ...senger 327 7 Left Aft Row Forward Facing Passenger 401 3 Center Aft Row Forward Facing Passenger 0 Right Aft Row Forward Facing Passenger 401 3 Fuel All Amounts 0 Hoist Load 635 0 copilot 65 kilograms...

Страница 313: ...BHT 206L3 FMS 14 TOTAL WEIGHT LEFT HAND SIDE COCKPIT CABIN PILOT WEIGHT RIGHT HAND COCKPIT SEAT MAXIMUM HOIST KILOGRAMS KILOGRAMS KILOGRAMS Figure 1 2 Hoist load nomograph Metric 7 8...

Страница 314: ...d to Model 206L 3 Flight Manual when SX 16C Nightsun Searchlight kit has been installed Information contained herein supplements information of basic Flight Manual For Limitations Procedures and Perfo...

Страница 315: ...206L3 FMS 16 NOTICE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron P 0 Box 482 Fort Worth Texas 76101 0482...

Страница 316: ...al 0 October 30 1985 Reissued 0 October 28 1992 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title NP 1 2 0 A B 3 4 0 i ii 0 NOTE Revised text is indicated by a black vertical line Insert latest rev...

Страница 317: ...3 FMS 16 FAA APPROVED LOG OF APPROVED REVISIONS Original 0 October 30 1985 Reissued 0 October 26 1992 APPROVED MANAGER ROTORCRAFT CERTIFICATION OFFICE FEDERAL AVIATION ADMINISTRATION FT WORTH TX 76193...

Страница 318: ...sition provides power to lamp and lamp starter gimbal drive motors focusing drive motor circuit and cooling fan located in lamp housing assembly OFF position rem es power to these components START swi...

Страница 319: ...f Nightsun Searchlight is restricted to copilot or operator position 1 4 WEIGHT CG Actual weight changes shall be determined after searchlight is installed and ballast readjusted if necessary to retur...

Страница 320: ...onnected MASTER switch OFF 2 4 IN FLIGHT OPERATIONS 1 NIGHTSUN SEARCHLIGHT MASTER switch ON 2 NIGHTSUN SEARCHLIGHT START switch START hold in this position approximately 5 seconds or until ignition ha...

Страница 321: ...manual Rate of Climb performance is reduced Landing Gear with Emergency Floats approximately 60 feet per minute from that Loudhailer installed on rear crosstubes shown in basic Flight Manual when and...

Страница 322: ...t shall be attached to Model 206L 3 Flight Manual when Alternate Turbine Outlet Temperature Gage Red Triangle at 626 C has been installed Information contained herein supplements information of basic...

Страница 323: ...T 206L3 FMS 17 NOTICE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron P 0 Box 482 Fort Worth Texas 76101 048...

Страница 324: ...NS Original 0 August 9 1993 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO FLIGHT MANUAL A B 0 i ii 0 Title NP 0 1 4 0 NOTE Revised text is indicated by a black vertical line Insert latest revision pa...

Страница 325: ...BHT 206L3 FMS 17 LOGOF APPROVEDREVISIONS Original 0 August 9 1993 APPROVED FAA APPROVED ROTORCRAFT CERTIFICATION OFFICE FEDERAL AVIATION ADMINISTRATION FT WORTH TX 76193 0170 B...

Страница 326: ...revised parameters The start temperature limitations permit unrestricted start modulation up to 626 C This point is identified by a red triangle on the instrument face The initiation point for the 10...

Страница 327: ...continuous 716 C 5 minute takeoff range 716 to 768 C Maximum for takeoff 768 C INTENTIONAL USE OF POWER TRANSIENT TOT ABOVE 766 C IS PROHIBITED Maximum power on transient Do not exceed 10 seconds abov...

Страница 328: ...c Continuous operation 716to76B C 5 minute takeoff range 768 C Maximum for takeoff 826 DC NOTE Beginning of time limited range for Starting 927 C llluminafe when TOT between 826 and 927 cC more than...

Страница 329: ...se modulate throttle to maintain TURB OUT TEMP between 716 C and 826 C This sequence should provide optimum starts in less than 40 seconds from the introduction of fuel If limits are exceeded or TURB...

Страница 330: ...BHT 206L3 FMS 17 FAA APPROVED No change from basic manual...

Страница 331: ...e attached to the Sell Helicopter Model 206L 3 Flight Manual when the 206 899 793 Fire Detection System Kit has been installed Information contained herein supplements information of basic Flight Manu...

Страница 332: ...sclosure reproduction or use of these data for any purpose other than helicopter operation is forbidden without prior written authorization from Bell Helicopter Textron Inc Additional copies of this p...

Страница 333: ...nal 0 7 JAN 94 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO FLIGHT MANUAL MANUFACTURER S DATA Title NP 0 3 4 0 A B 0 1 2 0 NOTE Revised text is indicated by a black vertical line Insert latest revis...

Страница 334: ...BHT 206L3 FMS 18 LOG OF APPROVED REVISIONS Original 0 7 JAN 94 APPROVED ROTORCRAFT CERTIFICATION OFFICE FEDERAL AVIATION ADMINISTRATION FT WORTH TX 76193 0170 B FAA APPROVED...

Страница 335: ...tual weight change shall be determined warning light on the instrument after kit is installed and ballast readjusted panel to illuminate if a fire if necessary to return empty weight CG to within allo...

Страница 336: ...CORRECTIVE ACTION ENG FIRE Overtemperature condition in engine compartment Throttle close Immediately enter autorotation FUEL VALVE switch OFF BATtery switch OFF GENerator switch OFF NOTE Do not resta...

Страница 337: ...BHT 206L3 FMS 18 MANUFACTURER S DATA No change from basic manual Section2 MANUFACTURER S DATA 206L3 FMS 16 2 l Figure 2 1 Caution and warning panel 3...

Страница 338: ...BHT 206L3 FMS 18 MANUFACTURER S DATA No change from basic manual MANUFACTURER S DATA No change from basic manual...

Страница 339: ...BHT 206L3 FM CAN 0 FLIGHT MANUAL ADDENDUM ADDENDUM FOR CANADIAN REGISTERED HELICOPTERS COPYRIGHTNOTICE SEPTEMBER 23 1983 REISSUED OCTOBER 28 1992...

Страница 340: ...these data for any purpose other than helicopter operation and or maintenance is forbidden without prior written authorization from Bell Helicopter Textron Inc Additional copies of this publication m...

Страница 341: ...seding that in the basic document to which it applies Pages contained herein shall be attached to like numbered pages in the Bell Model 206L3 Flight Manual when the helicopter is registered in Canada...

Страница 342: ...BHT 206L3 FM CAN 0 1 4 FAA APPROVED FOR DOT AMBIENT AIR TEMPERATURE Minimum 50 F 45 5 C Maximum 125 F 51 6 C This page applies to Canadian Registered helicopters only...

Страница 343: ...DING WHEN BOTH CREW SEATS ARE OCCUPIED ONLY ONE 1 MID PASSENGER IS PERMITTED UNLESS THERE ARE TWO 2 AFT PASSENGERS WHEN ONLY ONE 1 CREW SEAT IS OCCUPIED NO MORE THAN TWO 2 AFT PASSENGERS ARE PERMITTED...

Страница 344: ...ed to Model 206L 3 Flight Manual when 2000 Pound 907 kilograms Capacity Cargo Hook kit has been installed Information contained herein supplements information of basic Flight Manual For Limitations Pr...

Страница 345: ...ges contained herein shall be attached to like numbered pages in the BHT 206L3 FMS 4 Flight Manual Supplement for 2000 Pound Cargo Hook when the helicopter is registered in Canada Additional copies of...

Страница 346: ...tember 23 1963 Reissued 0 October 26 1992 Revision 1 March 14 1965 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title NP 0 1 2 0 A B 0 NOTE Revised text is indicated by a black vertical line Insert...

Страница 347: ...CAN 4 FAA APPROVED LOG OF APPROVED REVISIONS Original 0 September 23 1983 Reissued 0 October 26 1992 Revision 1 March 14 1985 ROTORCRAFT CERTIFICATION OFFICE FEDERAL AVIATION ADMINISTRATION FT WORTH T...

Страница 348: ...uring external The height velocity diagram in the basic cargo operations unless that person is Flight Manual is not a limitation for external load operation 1 A crewmember 2 A crewmember trainee or 3...

Страница 349: ...shall be attached to the Bell Helicopter Model 206L3 Flight Manual when the helicopter is registered in the United Kingdom Information contained herein supplements information of basic Flight Manual F...

Страница 350: ...206L3 FMS CAA NOTICE PAGE Additional copies of this publication may be obtained by contacting Commercial Publication Distribution Center Bell Helicopter Textron P 0 Box 402 Fort Worth Texas 76101 0482...

Страница 351: ...riginal 0 December 23 1982 Reissued 0 June 12 1992 LOG OF PAGES REVISION REVISION PAGE NO PAGE NO Title PN 0 1 6 0 A B 0 NOTE Revised text is indicated by a black vertical line Insert latest revision...

Страница 352: ...AA CAA APPROVED LOG OF APPROVED REVISIONS Original 0 December 23 1982 Reissued 0 June 12 1992 CIVIL AVIATION AUTHORITY SAFETY REGULATION GROUP AVIATION HOUSE SOUTH AREA GATWICK AIRPORT GATWICK WEST SU...

Страница 353: ...occupants including crew is the lesser of seven and the number of approved seats installed Children under age of two years carried in arms of passengers may be left out of this count 1 3 EXTERNAL FRE...

Страница 354: ...NING LIGHT FIRE FAULT AND REMEDY Overtemperature condition in engine compartment Proceed as follows Throttle Close Immediately enter autorotation FUEL VALVE switch OFF guard closed WARNING LIGHT FAULT...

Страница 355: ...ind factors are not considered Takeoff should be initiated from a stabilized 2 5 foot 0 76 meter skid height hover Increase power smoothly and simultaneously start nosedown pitch rotation so that heli...

Страница 356: ...BHT 206L3 FMS CAA CAA APPROVED TAKEOFF DISTANCE OVER 100 FOOT OBSTACLE CONDITIONS TECHNIQUE ROTOR 100 RPM LEVEL ACCELERATION AIRSPEED 50 KIAS FROM 2 5 FT 0 7 METER...

Страница 357: ...CAA APPROVED BHT 206L3 FMS CAA LANDING DISTANCE OVER 100 FOOT OBSTACLE CONDITIONS AIRSPEED 50 KIAS ROTOR 100 RPM WIND ZERO Figure 4 2 Landing distance over 100 foot obstacle...

Страница 358: ...ED GLIDE DISTANCE ALL GROSS WEIGHTS 48 KCAS ROTOR 100 RPM EXAMPLE Hp 3500 FT OAT 2 C STD OAT 8 C OAT STD OAT 2 8 10 USE CURVE STD 10 C HEIGHT ABOVE GROUND 2000 FT HORIZONTAL GLIDE DIST 1 25 N Ml 10 8...

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