BHT-206B3-FM-1 - JET RANGER III FLIGHT MANUAL - MODEL ...

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FAA APPROVED HOVER CEILING OUT-OF-GROUND-EFFECT TAKEOFF POWER O° TO 46°C GENERATOR 22 3 AMPS ANTI-ICE OFF SKID HEIGHT 40 FT (12 2 METERS, N2 ENGlNE RPM 100% WITH ANT-ICE ON GROSS WEIGHT IS 295 LBS (133 8 Kg) LESS
206B 250-C20B/C20J ENGINE ROTORCRAFT FLIGHT MANUAL BHT-206B3-FMS-18 SUPPLEMENT ENGINE (AUTOMATIC) RE-IGNITION 206-706-038 CERTIFIED AUGUST 11, 1977 This supplement shall be attached to Model 206B3 Flight Manual when Engine (Automatic) Re-Ignition kit has been installed. 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 basic Flight Manual. Bell Helicopter itIfl COPYRIGHT NOTICE A Subsidlary of Textron Inc. COPYRIGHT 2000 BELL A HELICOPTER TEXTRON INC. POST OFFICE BOX 482 * FORT WORTH. TEXAS 76101 AND BELL HELICOPTER TEXTRON INC. A DIVISION OF TEXTRON CANADA LTD. ALL RIGHTS RESERVED REISSUE 6 OCTOBER 2000
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BHT-206B3-FM-1 MODEL JET R 250-C20B
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FAA APPROVED FUEL SHUTOFF NOTICE VA
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LOG OF REVISIONS BHT-206B3-FM-1 Ori
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LOG OF FAA APPROVED REVISIONS BHT-2
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BHT-206B3-FM-1 DOT APPROVED USE OF
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BHT-206B3-FM-1 FAA APPROVED Paragra
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BHT-206B3-FM-1 FAA APPROVED l-6 Rev
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BHT-206B3-FM-1 FAA APPROVED l-6 IN.
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I BHT-206B3-FM-1 FAA APPROVED GAS P
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BHT-206B3-FM-1 FAA APPROVED 50% to
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BHT-206B3-FM-1 1-14 Rev. 2 FAA APPR
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BHT-206B3-FM-1 INSTRUMENT MARKINGS
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BHT-206B3-FM-1 FAA APPROVED PLACARD
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BHT-206B3-FM-1 PLACARDS (Cont) l-20
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FAA APPROVED BHT-206B3-FM-1 Section
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I DOT APPROVED BHT-206B3-FM-1 Hydra
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FAA APPROVED BHT-206B3-FM-1 Forward
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FAA APPROVED BHT-206B3-FM-1 indicat
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THESE RESTRICTIONS ARE IN CONJUNCTI
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BHT-206B3-FM-1 TC APPROVED TAIL ROT
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BHT-206B3-FM-1 TC APPROVED CAUTION
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a3AOUddV D1 i-W--go-90ZiH :::::: *.
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BHT-206B3-FM-1 TC APPROVED RATE OF
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BHT-206B3-FM-1 TC APPROVED RATE OF
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BHT-206B3-FM-1 FAA APPROVED HOVER C
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BHT-206B3-FM-1 FAA APPROVED 4-12 HO
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180 CRITICAL RELATIVE WIND AZIMUTH
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BHT-206B3-FM-1 FAA APPROVED Table 4
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BHT-20663-FM-1 FAA APPROVED ALTITUD
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Figure 4-8. Density altitude and te
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Appendix A BHT-206B3-FM-1 OPTIONAL
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BHT-206B3-FM-1 Table A-1. Flight Ma
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INE ROTORCRAFT FLIGHT MANUAL SUPPLE
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FAA APPROVED BHT-206B3-FM-1 LOG OF
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FAA APPROVED BHT-206B3-FMS-1 Sectio
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COPYRIGHT NOTICE COPYRIGHT ROTORCRA
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FAA APPROVED BHT-206B3-FM-2 Origina
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FAA APPROVED BHT-206B3-FMB-2 LITTER
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LITTER LOCATION WEIGHT ALLOWABLE CH
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LITTER LOCATION WEIGHT REQUIRED CHA
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COPYRIGHT NOTICE COPYRIGHT AU RIGHT
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FAA APPROVED BHT-206B3-FM-3 - LOG O
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FAA APPROVED TYPE OF OPERATION Hois
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NOTES: HOIST LOADING NOMOGRAPH METR
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BHT-206B3-FMS-4 FAA APPROVED SUPPLE
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FAA APPROVED SUPPLEMENT Section 1 T
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FAA APPROVED SUPPLEMENT ’ Section
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BHT-206B3-FMS-5 PROPRIETARY RIGHTS
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FAA `APPROVED BHT-206B3-FM-5 GENERA
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PROPRIETARY RIGHTS NOTICE These dat
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FAA APPROVED BHT-206B3-FM-8 GENERAL
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Pressure changes, when moving from
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BHT-206B3-FMS-8 FAA APPROVED Sectio
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6 800 600 20 22 24 26 28 30 (9.1) (
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BHT-206B3-FM-9 FAA APPROVED LOG OF
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FAA APPROVED CARGO RELEASE (LOCATED
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BHT-206B3-FMS-9 FAA APPROVED EXTERI
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HOVER CEILING IN GROUND EFFECT TAKE
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FAA APPROVE HOVER CEILING OUT OF GR
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206B 250-C20B/C20J ENGINE ROTORCRAF
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. Original LOG OF REVISIONS BHT-206
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ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
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FAA APPROVED LOG OF REVISIONS BHT-2
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FAA APPROVED BHT-206B3-FMS-11 -- Se
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FAA APPROVED HOVER CEILING IN GROUN
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MODEL 250-C20B/C20J ENGINE ROTORCRA
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P - ROTORCRAFT FLIGHT MANUAL SUPPLE
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FAA APPROVED BHT-206B3-FMS-13 - Sec
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BHT-206B3-FMS-22
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BHT-206B3-FMS-22 FAA APPROVED CARGO
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BHT-206B3-FMS-22 FAA APPROVED CARGO
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BHT-206B3-FMS-22 FAA APPROVED HIGH
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BHT-206B3-FMS-22 FAA APPROVED PARTI
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BHT-206B3-FMS-22 GENERATOR 22.3 AMP
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BHT-206B3-FMS-22 FAA APPROVED PARTI
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FAA APPROVED BHT-206B3-FMS-22 PARTI
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FAA APPROVED BHT-206B3-FMS-22 PARTI
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BHT-206B3-FMS-22 FAA APPROVED BLEED
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BHT-206B3-FMS-22 FAA APPROVED - 30
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BHT-206B3-FMS-22 FAA APPROVED BLEED
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- - COPYRIGHT NOTICE COPYRIGHT 1993
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- LOG OF REVISIONS BHT-206B3-FMS-26
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- FAA APPROVED BHT-206B3-FMS-26 GEN
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PLACARDS FLOAT ARMING/INFLATION ABO
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BHT-206B3-FMS-26 DESCENT AND LANDIN
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BHT-206B3-FMS-26 6 FAA APPROVED HOV
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FLIGHT MANUAL SUPPLEMENT BHT-206B3-
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FAA APPROVED Section 1 AIRCRAFT LOG
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-- CAA APPROVED BHT-206B3-CAA-FMS-2
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CAA APPROVED BHT-206B3-CAA-FM-29 CA
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- CAA APPROVED BHT-206B3-CAA-FMB-29
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BHT-206B3-CAA-FMS-29 6 GLIDE DISTAN
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BHT-206B3-FMS-30 PN PROPRIETARY RIG
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FAA APPROVED BHT-206B3-FMS-30 GENER
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BHT-206B3-FMS-30 2 No change from b
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BHT-206B3-FMS-CAN-31 PN PROPRIETARY
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FAA APPROVED FOR DOT BHT-206B3-FMS-
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BHT-206B3-FMS-32 FAA APRROVED LOG O
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NOTICE PAGE PROPRIETARY RIGHTS NOTI
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NOTICE This publication is being re
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DOT APPROVED
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MANUFACTURER’S DATA BHT-206B3-FMS
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- ROTORCRAFT FLIGHT MANUAL SUPPLEME
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FAA APPROVED BHT-206B3-FM-34 AIRSPE
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ROTORCRAFT FLIGHT MANUAL BHT-206B3-
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- BHT-206B3-FM-36 AIRSPEED decrease
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BHT-206B3-FMS-36 10 RATE OF CLI MB
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Figure 4-3. Rate of 14 I I Maximum
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Figure 4-5. Rate of climb - Maximum
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