Braathens S.A.F.E : FAA APPROVED AIRPLANE FLIGHT MANUAL BOEING MODEL 737/737C
Braathens S.A.F.E
Bok · Engelsk · 1967
| Utgitt | Seattle, Washington : The Boeing Commercial Airplane Company , 1967
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| Omfang | upag.
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| Opplysninger | Gift from former Braathens Date of approval: December 15, 1967. Revised 03-01-77. Last revision No 28 to D6-8737. 205 dated 06-24-86 Written in front of binder: "Bind I", and on the back of the binder: "Basic App. 27 AT. 4OK, 63, 66". - TABLE OF CONTENTS: SECTION 1 - CERTIFICATE LIMITATIONS Weight Limitations Performance Configuration Limitations Operational Limits Center of Gravity Limits Fuel System Limitations Engine Limitations Anti-Ice System Limitations Maximum Operating Limit Speed Mach Trim System Limitations Maximum Airspeed Limitations Certification Status Type of Airplane Operation Flight Maneuvering Load Acceleration Limits Flight Crew Cabin Pressurization Limitations Auxiliary Power Unit (APU) Limitations Window Heat Limitations Miscellaneous Limitations SECTION 2 - EMERGENCY PROCEDURES Fire Rapid Depressurization Emergency Descent Ditching Reverse Thrust Autopilot SECTION 3 - NORMAL PROCEDURES Abbreviated Procedures Maximum Operating Altitude Pre-Takeoff Approach and Landing Warning Horn Reverse Thrust Go-Around Procedure Turbulence Avoidance Severe Turbulent Air Penetration Hydraulic System Operation Braking with Accumulator Pressure only Unsymmetrical or no Leading Edge devices Unsymmetrical Trailing Edge Flaps Jammed Controls Manual Flight Control Runaway Stabilizer Jammed Stabilizer Landing Alternate Flap Operation Manual Landing Gear Extention Landing Gear Lever Unable to Place in Up Position after Takeoff Fuel System Engine Oil System Windshield Rain Repellent System Operation in Icing Conditions Auxiliary Power Unit (APU) Operation Cabin Pressurization Cockpit Window Failure One Generator Operation Instrument System Autothrottle Autopilot Electrical and Electronics SECTION 4 - PERFORMANCE General Regulatory Compliance Standard Performance Conditions Variable Factors Affecting Performance Airspeed Systems Definitions Takeoff Data Gradient of Climb Demonstrated Crosswind Minimum Control Speed Performance Conditions Performance Configuration Relation of Temperature to ISA Temperature Conversion Wind Component Takeoff EPR Takeoff N1 Inflight EPR Inflight N1 Recommended Takeoff Stabilizer Setting Position Correction, Flaps Down Position Correction, Flaps Up, Alternate Static Source Position Correction, Flaps Down, Alternate Static Source Temperature Conversion Total Air - Static Air Ground Minimum Control Speed, Vmcg Stall Speeds, Calibrated Airspeed Stall Speeds, Indicated Airspeed Cruise Maneuvering Capability Takeoff Procedures Maximum Allowable Takeoff Weight Flap Position 1: Runway Length and V1 Adjustment Runway Length and V1 Adjustment Maximum Takeoff Weight Field Length Limits Field Length Limits Field Length Limits Climb Limits Tire Speed of 200 MPH Maximum Takeoff Weight and Speed, Improved Climb Performance Takeoff Speeds, V1, Vr, V2 Takeoff Speeds (Improved Climb Performance) Brake Energy Limits Takeoff Climb Obstacle Clearance (Close-in Obstacle) Obstacle Clearance (Distant Obstacle) Maximum Level-Off Height Third Segment Distance Flap Position 5: Runway Length and V1 Adjustment Maximum Take-Off Weight (Field Length Limits) Maximum Take-Off Weight (Field Length Limits) Maximum Take-Off Weight (Climb Limits) Maximum Take-Off Weight and Speed, Improved Climb Performance Take-Off Speeds Take-Off Climb Obstacle Clearance (Close-in Obstacle) Obstacle Clearance (Distant Obstacle) Maximum Level-Off Height Third Segment Distance Flap Position 15: (Same Content as in Flap Position 5) Flap Position 25: (Same Content as in Flap Position 5) Final Takeoff Climb Final Takeoff Climb Wind Effect on Gradient Gross Height - Pressure Altitude Conversion Enroute Enroute Climb, 1 Engine Inoperative Enroute Climb Weights (Positive Net Gradient - Engine Inoperative) Approach and Landing Flaps 25 Approach/40 Landing: Approach Climb, Flap Position 25 Landing Climb, Flap Position 40 Maximum Landing Weight (Climb Limits) Landing Field Length and Speed, Autmatic and Manual Speed Brakes Flaps 15 Approach/30 Landing: Approach Climb, Flap Position 15 Landing Climb, Flap Position 30 Maximum Landing Weight (Climb Limits) Landing Field Length and Speed, Autmatic and Manual Speed Brakes Maximum Quick Turnaround Weight Flaps 1 Approach/25 Landing (Same as Flaps 15 Approach/30 Landing(with 1 and 25)) APPENDIX 27AT: Operation at JT8D-17 Engine Rating (Goodyear Anti-Skid System) APPENDIX 40K: Operation at JT8D-15 Engine Rating APPENDIX 63: JT8D-17 Engine Operation with Intermix APPENDIX 66: JT8D-15A Engine Operation with Intermix
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