ALLWAYS REFER TO AFM FOR MANUFACTURER PROCEDURES
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1 HB-XYA BELL 206 JET RANGER CHECKLIST EMERGENCY CHECKLIST LIMITATIONS PERFORMANCES PREFLIGHT CHECKLIST ALERT CHECKLISTE SECURITY AROUND W&B COMPUTATION SAMPLES The pilot is responsible for correct operation of the helicopter according the AFM. This summary is provided only as additional material for preflight preparation. Heli-Lausanne declines all responsability in case of non respect of any official manufacturer limitations(afm). ALLWAYS REFER TO AFM FOR MANUFACTURER PROCEDURES Version /16
2 BELL 206 B III - NORMAL PROCEDURES / CHECKLISTS 0. Rotor blades free Cockpit Preparation 1. Frictions... off 2. Flight Controls... freedom of movement 3. Frictions... on 4. Throttle... check freedom & idle stop operation 5. Rotor brake (if installed)... secured 6. Circuit breakers... all in 7. Overhead switches... off 8. Cabin heater... off 9. Generator... off 10. Altimeter... set 11. Engine gauges... zero 12. Flight instruments... static/zero 13. Fuel valve switch... on 14. Comm / Nav / Transponder (master switch)... off 15. Hydraulic switch... on 16. Engine Anti-Ice switch... off 17. Landing light... off Engine Pre-Start 1. Battery switch (for battery and GPU start)... on (for battery cart start... off) (for GPU start on) 2. Engine Out Horn... audible 3. Fuel pumps... check 4. Fuel pressure... check 5. Fuel quantity... check 6. Warning lights... press to test 7. TOT light... check 8. Rotor Low RPM... light and audio Version /16
3 Engine Start 1. Anti-Collision light... on 2. Collective... down Caution! 3. Throttle... closed 4. Rotor... free 5. Area... clear Caution! Monitor TOT in case of inadvertent throttle opening! TOT must stay steady or decrease when starter is engaged! If TOT rise before throttle opening close throttle immediately! 6. Starter... engage 7. Engine Oil Pressure... increase 8. Throttle... open to flight idle at 15% N1 and TOT <150 C N1 Starting Speed N1 RPM... TEMP C 15%... Above 7 C 13% to +7 C 12%... Below 18 C If N1 remains below 12%... abort start Caution! Abort start if TOT reaches either 927 C or remains maximum 10 seconds between 810 C and 927 C 9. TOT... monitor 10. Rotor... turning at 25% N1 11. Starter... release at 58% N1 Version /16
4 12. Idle (60%-62% N1) (If more than 15 minutes shutdown)... 1 minute 13. Engine gauges... within limits 14. (GPU disconnect; Battery... on) 15. Throttle... open to 70% N1 16. Generator Switch... on 17. Loadmeter... below red line 18. Avionic master switch (if installed)... on 19. Position lights... as required 20. Standby horizon (if installed)... on 21. Strobe light... on 22. Defog Blower... check, on as required 23. GPS (if installed)... on 24. FLARM (if installed)... on 25. COMM / NAV... set as required 26. Transponder... set as required 27. ELT... check for inadvertent xmission Engine Run-Up 1. Throttle... increase to full open psn Caution! Do not exceed 40% Torque during accelaration Avoid N 2 range % when torque is greater than 33 % 2. N2 Governor...check range % 3. Engine Anti-Ice... check for TOT rise, then off 4. Hydraulic system... check 5. Engine relight (if installed)... test, reset, then on 6. Directional gyro (if installed)... set Version /16
5 Check before Departure 1. Frictions... off 2. Throttle... full open 3. RRPM % 4. All warning lights... off 5. Engine gauges... green 6. Fuel quantity... checked 7. Engine anti-ice (4,4 C and below + visble moisture =ON) as required 8. Heater... off 9. Landing light... on (apt. only) 10. Comm / Nav setting... checked Check in Ground Effect 1. RRPM % 2. Torque/TOT/N1... within limits 3. Take-off axis... clear 4. Wind... check Climb check 1. Speed... adjusted 2. Vertical speed... positive 3. Engine Anti-Ice (4 C and below + visble moisture =ON)... as required 4. Pitot heat... as required Check for Approach 1. Throttle... full open 2. RRPM % 3. All warning lights... off 4. Engine gauges... green 5. Fuel quantity... checked 6. Engine Anti-Ice (4 C and below + visble moisture =ON)... as required 7. Heater... off 8. Landing light... on (apt) only Final Check 1. Speed kt. 2. Vertical speed... <500ft/Min. 3. Decision... land/go around Version /16
6 Engine Shut Down 1. Throttle... idle for 2 min 2. Frictions... on 3. Landing light... off 4. Avionics master switch (if installed)... off 5. Position lights... off 6. Heater... off 7. Strobe light (if installed)... off 8. Gyro / standby horizon... off 9. GPS (if installed)... off 10. FLARM (if installed)... off 11. Com/Nav/XPDR (if no master switch)... off 12. ELT (if installed)... check for inadvertent xmission After 2 minutes cool-down 13. Generator... off 14. Throttle... close 15. Rotor brake (if installed)... apply 38%-30% RRPM 16. Beacon... off 17. Battery switch (if TOT stabilized and N1=0%)... off Version /16
7 BELL 206 B III - EMERGENCY PROCEDURES ENGINE FAILURE - Enter autorotation immediately TAIL ROTOR CONTROL FAILURE Complete Loss of Thrust - Close throttle - Enter autorotation - Maintain minimum airspeed 50 knots (58 mph) Fixed Pitch Failure - Adjust power to minimise excessive yawing - Adjust airspeed to minimise excessive yawing FUEL CONTROL/GOVERNOR FAILURE - Control power with Throttle if engine overspeeds - Maintain RPM with collective pitch if engine underspeeds - Establish autorotation if power is too low or engine must be shut down - Prepare for power-off landing HYDRAULIC SYSTEM FAILURE - Reduce airspeed to knots (70-80 mph) - HYD BOOST c/b: ON (OFF if power is not restored) - Land as soon as practical and investigate - (A run-on landing at knots (12-17 mph) is recommended GENERATOR FAILURE - Cycle GENerator switch. If power is not restored: OFF - All electrical equipment: OFF (to conserve battery) - Required electrical equipment: ON (only as needed) - Reduce altitude to below 6000 feet (1830 m) BOOST PUMP FAILURE - Descend to below 6000 feet (1830 m) CAUTION : UNUSABLE FUEL: 10 U.S. GALLS (38 LITERS) ENGINE FIRE DURING FLIGHT - Close throttle - Enter autorotation immediately - FUEL VALVE switch: OFF - BATTery switch: OFF - GENerator switch: OFF - Execute autorotational landing Version /16
8 ENGINE FIRE DURING START - Close throttle - Continue to motor engine with starter FUEL VALVE switch: OFF - ENGINE AIR START - Establish steady autorotation - GENerator switch: OFF - Perform normal engine starting procedures CAUTION:DO NOT ATTEMPT AIR-RESTART ABOVE 12'000 FEET (3660 M) RED L I G H T S ENG OUT (audio and light) BATTERY HOT Engine failure. Enter autorotation Land as soon as possible (Do not use helicopter battery for restart) A M B E R L I G H T S ROTOR LOW RPM (audio and light) TRANS TEMP TRANS PRESS TRANS CHIP ENG CHIP T/R CHIP FUEL FILTER A/F FUEL FILTER FUEL PUMP FUEL LOW BATTERY TEMP GEN FAIL 1. Reduce collective pitch 2. Check throttle full open Land as soon as possible Land as soon as possible Land as soon as possible Land as soon as possible Land as soon as possible Land as soon as practical Land as soon as practical 1. Descend to below 6000 feet (1830 m) CAUTION: UNUSABLE FUEL: 10 U.S. GALLS. Plan landing (approx. 20 Galls left) 1. Move battery switch to OFF until battery cools and light extinguishes 2. BATTery switch: ON 1. Gen switch RESET; then ON 2. If power not restored Gen switch OFF 3. All unnecessary equipment off 4. Reduce altitude to below 6000 ft PA 5. Land as soon as practical Version /16
9 BELL 206 BIII - LIMITATIONS (summary from AFM) MTOW Internal load Maximum 3200 lbs With external load 3350 lbs Cargo hook 1500 lbs Speed (VNE) Power-on </= 3000 lbs MTOW Maximum 130 kts above 3000 ft -3.5 kts/1000 ft Alt Power-on > 3000 lbs MTOW Maximum 122 kts above 3000 ft -7.0 kts/1000 ft Alt Power-off Maximum 100 kts Aft Doors removed Maximum 87 kts Forward Doors removed Maximum 69 kts LH Sliding door opening Maximum 87 kts LH Sliding door closing Maximum 87 kts Altitude </= 3000 lbs Maximum ft PA > 3000 lbs ft DA Temperature OAT Below 4,4 C and visible Moist Anti Ice ON Main Rotor Power-on In stabilized flight 97% 100% RPM Maximum transient (5 sec) 95% -97% RPM Power-off Maximum 107% RPM Minimum 90% RPM Rotor brake Maximum 38% RPM Torque Maximum continuous 85 % IAS < 80 kts Maximum take-off (5 min) 100 % Maximum transient (5 sec) 110 % (intentional use prohibited) Gas Producer (N1) Flight Maximum continuous 60% -105% Maximum 105% Maximum transient (15 sec) 106% Idle Minimum Ng = 60%-62% TOT Engine start Maximum transient (10 sec) 810 C -927 C Take-off Maximum (5 min) 738 C 810 C Power transient Maximum (6 sec) 810 C 843 C (intentional use prohibited) In-flight Continuous 100 C 738 C Engine Oil Pressure Min. (N1 < 78.5%) 50 psi Min. (N1 < 78.5%) 90 psi Min. (N1 > 94.2%) 115 psi Maximum 130 psi Temperature Maximum 107 C Xmsn Oil Pressure Minimum 30 psi Continious 30 psi -50 psi Maximum 70 psi Temperature Maximum 110 C Fuel Pressure Minimum 4.0 psi Maximum 30.0 psi Pilot & Pax Pilot Minimum lbs< 75 usg 200 lbs> 75 usg Persons carried Maximum 5 (pilot included) Heater Bleed Air Heater Switch OFF for T/O and landing Version /16
10 PERFORMANCES HOGE Version /16
11 BELL 206 B III - NORMAL PROCEDURES PREFLIGHT CHECK Version /16
12 Version /16
13 Version /16
14 Version /16
15 Version /16
16 EQUIPAGE Bell 206 Jet Ranger HB-XYA QUI QUAND QUOI COMMENT CONTACT Immédiat 1 Alerte - REGA - Ambulance - Police - Pompiers 1414 canal K/R Immédiat 2 Secours - sécuriser le site de l accident - actions pour sauver les vies - information aux sauveteurs Immédiat 3 Information Communication externe EXCLUSIVEMENT par le management de la COMPAGNIE. Aucune information aux médias ou tiers 021 / piquet Heli-Lausanne - Management compagnie - Responsable des opérations - Management technique Protocole - noter tous les appels et messages Les principes les plus importants lors de l alerte Alerte Proches Information Que s est-il passé Où cela s est-il passé (lieu, rue, montagne, altitude, coordonnées, etc.) Quand cela s est-il passé Qui est concerné (nombres personnes, blessés, décès, etc.) Hélicoptère et immatriculation Quelles mesures ont été prises Tous les appels, messages et mesures prises ont été enregistrées jusqu à ce que le management prenne le relais Les proches sont informées exclusivement par le management ou une personne autorisée par le management L information à des tiers et aux médias est effectuée exclusivement par le management ou une personne autorisée par le management Version /16
17 Version /16
HB-XLB. Hughes 300 CBi HB-XLB ALLWAYS REFER TO AFM FOR MANUFACTURER PROCEDURES
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