| 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 | | Lokal Note (gave): | Braathens | | Materialbetegnelse: | Technical Handbook | | Materialbetegnelse: | Perm | | Note: | Gift from former Braathens
Date of Approval: December 15, 1967. Revised 03-01-77. Last revision No 24 to
D6-8737. 205A dated 06-24-86.
Written in front of binder: "Bind III" | | Innhold: | TABLE OF CONTENTS:
SECTION 1 - CERTIFICATE LIMITATIONS
Weight Limitations
Performance Configuration Limitations
Operational Limits
Automatic Wheel Brakes
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
Ground Proximity Warning System
Reverse Thrust
Autopilot
SECTION 3 - NORMAL PROCEDURES
Abbreviated Procedures
Maximum Operating Altitude
Pre-Takeoff
Takeoff
Approach and Landing
Warning Horn
Ground Proximity Warning System
Glide Slope Deviation Alert System
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
Operation in Icing Conditions
Windshield Rain Repellent System
Auxiliary Power Unit Inflight Start Envelope
Auxiliary Power Unit (APU) Operation
Cabin Pressurization
Cockpit Window Failure
One Generator Operation
Instrument System
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
Takeoff Field Length
Climb Gradients and Obstacle Clearance
Landing Field Length
Performance Configuration
Relation of Temperature to ISA
Temperature Conversion Chart
Wind Component
Takeoff EPR, 0-60 Knots
Takeoff N1, 0-60 Knots
Inflight EPR
Inflight N1
Recommended Takeoff Stabilizer Setting
Inflight Restart Envelope
Position Correction
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
Cruise Maneuvering Capability
Takeoff Procedures
Thrust Setting Procedure
Normal Takeoff Procedures
Climb Out (1 or 2 Engines)
Flap Retraction Speed Schedule
Maximum Allowable Takeoff Weight
Introduction
Field Length and Climb Performance Limits
Definitions
Chart Presentation
Flight Path and Obstacle Clearance
Definitions
Assumed Climb Technique
Constant Thrust Effects on Climb Gradient
Take-Off Flight Path
Normal Take-Off Weight Analysis
Takeoff Weight Analysis with Improved Climb Performance
Takeoff Flap Position Selection
Clearway and Stopway
Selection of V1
V1 Greater than Brake Energy Limit (Flaps Pos 1 or 2)
Minimum VR
Anti-Skid Inoperative
Slippery Runway
Obstacle in First or Second Segment
Sloped Runway Effect on Obstacle Clearance
Obstacle in Third Segment
Extended Second Segment Climb
Obstacle in Final Segment
Example Guide Lines
Illustrative Examples
Takeoff Flight Path (Example)
Runway Length Corrections, All Engines Operating
Runway Length and V1 Adjustment
Runway Length and V1 Adjustment
Runway Length Corrections, Flap Position
Maximum Takeoff Weight, Field Length Limits, A/C on
Maximum Takeoff Weight, Field Length Limits, A/C off
Maximum Takeoff Weight, Climb Limits, A/C on
Maximum Takeoff Weight, Climb Limits, A/C off
Climb Limit Corrections, Flap Position
Maximum Takeoff Weight, for Tire Speed of 200 and 210 MPH
Maximum Takeoff Weight, Improved Climb Performance
Tire Speed Limits, Improved Climb Performance
Takeoff Speeds
Takeoff Speeds, Improved Climb Performance
Brake Energy Limits
Takeoff Climb, A/C on
Takeoff Climb, A/C off
Takeoff Climb Corrections, Flap Position
Obstacle Clearance, Close-in Obstacles
Obstacle Clearance, Field Length Trade Lines
Obstacle Clearance, Distant Obstacles
Maximum Level-Off Height
Third Segment Distance
Final Take-Off Climb
Final Take-Off Climb
Gradient Gorrections, Wind and Gross Height
Gross Height, Pressure Altitude Conversion
Enroute Climb
Enroute Climb (Charts)
Enroute Climb Weights
Approach and Landing
Approach Climb
Landing Climb
Maximum Landing Weight Climb Limits, Flap Pos 10/30
Maximum Landing Weight Climb Limits, Flap Pos 2/15
Landing Speeds
Landing Field Length, Flap Pos 40
Wind Corrections to Landing Weight or Distance, Flap Pos 40
Landing Field Length, Flap Pos 30
Wind Corrections to Landing Weight or Distance, Flap Pos 30
Landing Field Length, Flap Pos 15
Wind Corrections to Landing Weight or Distance, Flap Pos 15
Landing Field Length, Anti-Skid Inoperative
Maximum Quick Turnaround Weight, Flap Pos 40
Maximum Quick Turnaround Weight, Flap Pos 30
Maximum Quick Turnaround Weight, Flap Pos 15
Automatic Wheel Brakes
Stopping Distance with Automatic Wheel Brakes
APPENDICES:
APPENDIX 3: Operation at Reduced Take-Off Thrust
APPENDIX 7C (Revision 8 to Appendix 7C, D6-8737, dated 11-22-83):
SECTION 1 - CERTIFICATE LIMITATIONS
General Limitations
Engine Limitations
Engine Thrust
Lateral Unbalance
Engine Fuel System Limitations
Engine Ignition Limitations
Engine Oil System Limitations
Reverse Thrust
APPENDIX 9C: Operation at JT8D-15 Engine Rating | | Eier: | Norsk Luftfartsmuseum | | |
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