| Tittel: | Braathens S.A.F.E : FAA APPROVED AIRPLANE FLIGHT MANUAL BOEING MODEL 737/737C | | Forfatter: | Braathens S.A.F.E | | Materialtype: | Manual/Sivil | | Signatur: | 21-A-6 | | Utgitt: | Seattle, Washington : The Boeing Commercial Airplane Company, 1967 | | Omfang: | upag. | | Emneord: | Airplane flight manual / Boeing 737 / Boeing 737C | | Materialbetegnelse: | Technical Handbook | | Materialbetegnelse: | Perm | | Lokal Note (gave): | Braathens | | Note: | 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" | | Innhold: | 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 | | Eier: | Norsk Luftfartsmuseum | | |
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