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BHT-206L3-FM-1

APPROVED:

DATE:

CHIEF, FLIGHT TEST

FOR

DIRECTOR — AIRCRAFT CERTIFICATION

TRANSPORT CANADA

LOG OF TC APPROVED REVISIONS

Original ....................0 ....................... 09 DEC 81
Revision ...................1 .......................29 NOV 82
Revision ...................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 MAY 90
Reissue.................... 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

26 APR 2005 Rev. 6

C/D

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Summary of Contents for BHT-206L3-FM-1 LongRanger-III

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

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

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

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 232: ......

Page 233: ......

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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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