Søk i Norsk luftfartsmuseum
  • Portal
  • Søk
    v
  • Mine lån
  • Utlån
  • Innlevering
  • Gi vurdering
  • Reserver
  • Fjernlån
  • Marcdata
  • RIS
Tittel:Braathens S.A.F.E : 767 FAA APPROVED AIRPLANE FLIGHT MANUAL
Forfatter:Braathens S.A.F.E
Materialtype:Manual/Sivil
Signatur:21-A-2
Utgitt:Seattle, Washington : The Boeing Commercial Airplane Company, 1982
Omfang:upag.
Serie:Document No. ; D6T11320
Emneord:Boeing 767 / Braathens / FAA / Manual
Lokal Note (gave):Braathens
Materialbetegnelse:Perm
Materialbetegnelse:Technical Handbook
Note:Gift from former Braathens
Published 07-30-82, Revised 10-28-82
Written insidet of binder: "KAPTEIN EINAR DANIELSEN"
Innhold:TABLE OF CONTENTS: (Titles shown in capital letters are charts. Titles shown in
lower case letters are text)
Log of Pages, Appendix Applicability
Revision Highlights
Log of Pages
Appendix Applicability
Contents

SECTION 1 - CERTIFICATE LIMITATIONS
Weight Limitations
Performing Operating Weights
Performance Configuration
Operational Limits
CENTER OF GRAVITY LIMITS
Certification Status
Kind of Airplane Operation
Flight Maneuvering Load Acceleration Limits
Flight Crew
Maximum Operation Limit Speed (Vmo/Mmo)
MAXIMUM AIRSPEED LIMITS
Fuel System
Engines
Engine Thrust
Engine RPM
Engine EGT
Engine Limit Display Markings
Engine Indicating and Crew Alerting System (EICAS)
Engine Fuel System
Engine Ignition
Engine Oil Systen
Reverse Thrust
Operating in Icing Conditions
Engine Anti-Ice System
Cabin Pressurization
Autopilot - Flight Director
Flight Management Computer System (FMCS)
ILS/DME Tuning
Flap Operation
Passenger Evacuation
Cargo Fire
Noise Characteristics
Configuration Deviation List (CDL)

SECTION 2 - EMERGENCY PROCEDURES
Emergency Procedures
Fire
Engine Fire, Severe Engine Damage, or Separation
APU Fire
Cargo Fire (FWD/AFT)
Electrical Smoke or Fire
Wheel Well Fire
Smoke Removal (Cockpit or cabin source)
Loss of Both Engines
AC Bus(es) Off
Rapid Depressurization
Descent
Ditching
Passenger Evacuation
Autopilot Elevator Malfunction

SECTION 3 - OPERATING PROCEDURES
3.1 Normal Procedures
Contents
General
Fuel Tank Capacity
Reverse Thrust
Windshield Rain Repellent
Turbulence Avoidance
Severe Turbulent Air Penetration
Autopilot-Flight Director System
Inertial Reference System
Flight Management Computer System (FMCS)
Operation in Icing Conditions
Auxiliary Power Unit
3.2 Non-normal Procedures
Contents
General
Hydraulic Systems
Pump Overheat
Pump Low Pressure
System(s) Low Pressure
Automatic Wheel Brakes
Engine Oil System
Low Oil Pressure
High Oil Temperature
Oil Filter Bypass
Low Fuel Quantity
Electronic Engine Control (EEC) Inoperative
Fuel Filter Bypass
Engine Overheat
Engine Inoperative Landing
Inadvertent Reverse Thrust in Flight
Stabilizer Trim Fault
Unscheduled Stabilizer Trim
Spoilers Fault
Rudder Ratio
Yaw Damper
Automatic Speed Brakes
Leading Edge Slat Asymmetrical
Trailing Edge Flaps Asymmetrical
Flap/Slat Disagree
Flap Load Relief
Alternate Landing Gear Extension
Window Heat
Equipment Cooling System
Ground Proximity Warning-Glide Slope Deviation Alerting System

SECTION 4 - PERFORMANCE
4.1 General
Contents
Regulatory Compliance
Standard Performance Conditions
Performance Configuration
Definitions
Airspeed
Temperature
Wind
Icing
Takeoff Path
Takeoff Flight Path
Maximum Crosswind
Buffet Onset Characteristics
Performance Conditions and Procedures
Takeoff
Refused Takeoff
Climbout
Obstacle Clearance
Landing Field Length
Flap Retraction Speed Schedule
Takeoff Weight Determination Procedure
Introduction
Filed Length Limited Performance
Climb Limited Performance
Tire Speed Limited Performance
Obstacle Clearance Limited Performance
Takeoff Weight Determination Procedure Flow Diagram
Takeoff Weight Determination Procedure
ENVIRONMENT ENVELOPE
WIND COMPONENT
RECOMMENDED TAKEOFF STABILIZER SETTING
Position Corrections - Primary Static Source
- ALTERNATE STATIC SOURCE (FLAPS UP)
- ALTERNATE STATIC SOURCE (ALL FLAPS)
TEMPERATURE CONVERSION
STALL SPEEDS
GEAR UP
GEAR DOWN
CRUISE MANEUVERING CAPABILITY
4.2 Engine Data
Contents
General
Takeoff Power Setting
Go-Around Power Setting
Inflight Power Setting
TAKEOFF EPR
GO-AROUND EPR (INFLIGHT TAKEOFF)
INFLIGHT EPR (MCT)
INFLIGHT RESTART ENVELOPE
Noise Characteristics
Noise Levels
Noise Certification Procedures
Engine Intermix
Package "A" Engines
Certificated Noise Levels
Package "B" Engines
Certificated Noise Levels
4.3 Runway Length Corrections
Contents
General
Corrected Runway Length Determination
Corrected Runway Length Determination Procedure Flow Diagram
ALL ENGINES OPERATING CORRECTED RUNWAY LENGTH
(FLAPS 1, 5, 15, 20)
ENGINE INOPERATIVE CORRECTED TAKEOFF DISTANCE
(FLAPS 1, 5, 15, 20)
CORRECTED ACCELERATE-STOP DISTANCE (FLAPS 1, 5, 15, 20)
RUNWAY LENGTH & V1 ADJUSTMENTS ALTITUDE-TEMPERATURE REGIONS
RUNWAY LENGTH & V1 ADJUSTMENTS (REGION A)
(FLAPS 1)
(FLAPS 5)
(FLAPS 15)
(FLAPS 20)
RUNWAY LENGTH & V1 ADJUSTMENTS (REGION B)
(FLAPS 1)
(FLAPS 5)
(FLAPS 15)
(FLAPS 20)
4.4 Field Length Limits
Contents
General
Takeoff Field Length
FIELD LENGTH LIMITS WEIGHT ADJUSTMENTS
FIELD LENGTH LIMITS (FLAPS 1) A/C PACKS ON
A/C PACKS OFF
FIELD LENGTH LIMITS (FLAPS 5) A/C PACKS ON
A/C PACKS OFF
FIELD LENGTH LIMITS (FLAPS 15) A/C PACKS ON
A/C PACKS OFF
FIELD LENGTH LIMITS (FLAPS 20) A/C PACKS ON
A/C PACKS OFF
4.5 Takeoff Climb Limits
Contents
General
Takeoff Climb Limits
Final Takeoff Climb Limits
TAKEOFF CLIMB LIMITS
(FLAPS 1) - A/C PACKS ON
- A/C PACKS OFF
(FLAPS 5) -A/C PACKS ON
- A/C PACKS OFF
(FLAPS 15) - A/C PACKS ON
- A/C PACKS OFF
(FLAPS 20) - A/C PACKS ON
- A/C PACKS OFF
FINAL TAKEOFF CLIMB LIMITS
4.6 Tire Speed Limits
Contents
General
TIRE SPEED LIMITS (225 MPH TIRES)
4.7 Takeoff Speeds
Contents
General
Takeoff Speed Restrictions
Rotation Speed
Brake Energy Limits
Minimum V1 For Control On the Ground
Air Minimum Control Speed
Takeoff Decision Speed, V1, Determination
V1 Determination Procedure Flow Diagram
Selection of V1
When a High V1 Is Selected
When a Low V1 Is Selected
TAKEOFF SPEEDS
(FLAPS 1)
(FLAPS 5)
(FLAPS 15)
(FLAPS 20)
BRAKE ENERGY LIMITS
(FLAPS 1)
(FLAPS 5)
MINIMUM V1 FOR CONTROL ON THE GROUND
AIR MINIMUM CONTROL SPEED
REFERENCE SPEEDS
4.8 V1 (MCG) Limited Takeoff
Contents
General
Takeoff Speeds
Basic Takeoff Speeds
Speed Increase Required
4.9 Obstacle Clearance
Contents
Takeoff Flight Path
Presentation
TAKEOFF FLIGHT PATH (EXAMPLE)
Assumed Climb Technique
FLIGHT PATH OPTIONS
Flight Path Chart Presentation
Takeoff Climb
Close-In Obstacles Clearance
Distant Obstacle Clearance
Obstacle Distance Trade Lines
Maximum Level-Off Height
Third Segment Distance
Final Takeoff Climb Chart
Gradient Corrections
Gross Height-Pressure Altitude Conversion
Obstacles Clearance Analysis Procedure Flow Diagram
Flow Diagram
Obstacles Clearance Analysis Procedure
Sloped Runway Effect On Obstacle Clearance
Construction of Obstacle Distance Trade Lines
On Obstacle Clearance Chart
Obstacle Clearance With Speed Increase
4.10 Improved Climb Performance
Contents
General
Chart Presentation
Improved Climb Performance
Takeoff Weight Analysis With Improved Climb Performance Procedure
Corrected Runway Length Required With Improved Climb Performance Procedure
IMPROVED CLIMB PERFORMANCE
(TAKEOFF WEIGHT LIMITS/TAKEOFF SPEEDS)
(FLAPS 1)
(FLAPS 5)
(FLAPS 15)
(FLAPS 20)
TAKEOFF SAFETY SPEED (Flaps 1, 5, 15, 20)
TAKEOFF CLIMB, IMPROVED CLIMB PERFORMANCE
4.11 Enroute Climb
Contents
General
Electronic Engine Control (EEC) Thrust Limit Error
ENROUTE CLIMB WEIGHTS FOR POSITIVE NET GRADIENTS
1 ENGINE INOPERATIVE
ENROUTE CLIMB, 1 ENGINE INOPERATIVE
ISA + 10 DEG C AND BELOW
ISA + 15 DEG C
ISA + 20 DEG C
ISA + 35 DEG C
ENROUTE CLIMB SPEEDS, 1 ENGINE INOPERATIVE
4.12 Approach and Landing Climb
Contents
General
APPROACH CLIMB
(FLAPS 5)
(FLAPS 15)
LANDING CLIMB
(FLAPS 25)
(FLAPS 30)
MAXIMUM LANDING WEIGHT, CLIMB LIMITS
APPROACH FLAPS 5, LANDING FLAPS 25
APPROACH FLAPS 15, LANDING FLAPS 30
4.13 Landing Field Length and Speed
Contents
General
Automatic Landing
Automatic Wheel Brakes
LANDING SPEEDS
LANDING FIELD LENGTH, ANTISKID OPERATIVE
(FLAPS 25)
LANDING FIELD LENGTH CORRECTIONS, ANTISKID INOPERATIVE
(FLAPS 25)
LANDING FIELD LENGTH, ANTISKID OPERATIVE
(FLAPS 30)
LANDING FIELD LENGTH CORRECTIONS, ANTISKID INOPERATIVE
(FLAPS 30)
MAXIMUM QUICK TURNAROUND WEIGHT
(FLAPS 25)
(FLAPS 30)
STOPPING DISTANCE WITH AUTOMATIC WHEEL BRAKES
LANDING FIELD LENGTH CORRECTIONS FOR AUTOLAND

APPENDIX 1 - OPERATION AT REDUCED THRUST
Introduction
SECTION 1 - CERTIFICATE LIMITATIONS
General Limitations
Operational Limits
Engine Limitations
SECTION 2 - EMERGENCY PROCEDURES
SECTION 3 - OPERATING PROCEDURES
SECTION 4 - PERFORMANCE
Reduced Thrust Performance Limits
Determination of the Assumed Temperature
MINIMUM ALLOWABLE EPR FOR REDUCED THRUST

APPENDIX 2K - LANDING GEAR EXTENDED JT9D-7R4D
Introduction
SECTION 1 - CERTIFICATE LIMITATIONS
General
Type of Airplane Operation
Operational Limits
Maximum Operatin Limit Speed (Vmo)
SECTION 2 - EMERGENCY PROCEDURES
Emergency Descent
SECTION 3 - OPERATING PROCEDURES
Severe Turbulent Air Penetration
SECTION 4 - PERFORMANCE
Performance Adjustments
SECTION 4.1 - GENERAL
General
Performance Configuration
Performance Conditions and Procedures
Takeoff
Flap Retraction Speed Schedule
Takeoff Weight Determination Procedure
SECTION 4.5 - TAKEOFF CLIMB LIMITS
General
TAKEOFF CLIMB LIMITS
FINAL TAKEOFF CLIMB LIMITS
SECTION 4.9 - OBSTACLE CLEARANCE
Assumed Climb Technique
Flight Path Chart Presentation and Obstacle Clearance Analysis Procedure
General
Takeoff Climb
CLOSE-IN OBSTACLE CLEARANCE
DISTANT OBSTACLE CLEARANCE
OBSTACLE DISTANCE TRADE LINES
MAXIMUM LEVEL-OFF HEIGHT
THIRD SEGMENT DISTANCE
FINAL TAKEOFF CLIMB
GRADIENT CORRECTIONS
SECTION 4.11 - ENROUTE
Contents
General
Electronic Engine Control (EEC) Thrust Limit Error
ENROUTE CLIMB WEIGHTS (FOR POSITIVE NET GRADIENTS)
ENROUTE CLIMB
ISA + 10° C AND BELOW
ISA + 15° C
ISA + 20° C
ISA + 35° C
ENROUTE CLIMB SPEEDS
SECTION 4.12 - APPROACH AND LANDING CLIMB
General
MAXIMUM LANDING WEIGHT, CLIMB LIMITS
APPROACH FLAPS 5, LANDING FLAPS 25
APPROACH FLAPS 15, LANDING FLAPS 30

APPENDIX 3K - EXAMPLE PROBLEMS
Introduction
General
Problem Solving Procedures
Procedures
GENERAL TAKEOFF ANALYSIS
Example Problem 1
TAKEOFF ANALYSIS WITH IMPROVED CLIMB PERFORMANCE
Example Problem 2
OBSTACLE LIMITED TAKEOFF WEIGHT ANALYSIS
Example Problem 3
DISTANT OBSTACLE LIMITED TAKEOFF WEIGHT ANALYSIS
Example Problem 4
OBSTACLE LIMITED TAKEOFF WEIGHT WITH OBSTACLE IN FINAL SEGMENT
Example Problem 5
TAKOFF FLIGHT PATH EXAMPLE
OBSTACLE LIMITED TAKEOFF WEIGHT ANALYSIS WITH IMPROVED CLIMB PERF.
Example Problem 6
V1 (MCG) LIMITED TAKEOFF
Example Problem 7
BRAKE ENERGY LIMITED TAKEOFF WEIGHT ANALYSIS
Example Problem 8
ALL ENGINES OPERATING CORRECTED RUNWAY LENGTH
(FLAPS 1, 5, 15 & 20)
ENGINE INOPERATIVE CORRECTED TAKEOFF DISTANCE
(FLAPS 1, 5, 15 & 20)
CORRECTED ACCELERATE-STOP DISTANCE
(FLAPS 1, 5, 15 & 20)
RUNWAY LENGTH & V1 ADJUSTMENTS
(FLAPS 1 & 15)
(FLAPS 15)
FIELD LENGTH LIMITS
(FLAPS 1) - A/C PACKS ON
(FLAPS 15) - A/C PACKS ON
TAKEOFF CLIMB LIMITS (FLAPS 1) - A/C PACKS ON
TAKEOFF CLIMB LIMITS (FLAPS 15) - A/C PACKS ON
TIRE SPEED LIMITS (225 MPH TIRES)
TAKEOFF SPEEDS (FLAPS 1)
TAKEOFF SPEEDS (FLAPS 15)
BRAKE ENERGY LIMITS (FLAPS 1)
MINIMUM V1 FOR CONTROL ON THE GROUND (V1 (MCG))
IMPROVED CLIMB PERFORMANCE (FLAPS 15)
TAKEOFF CLIMB (IMPROVED CLIMB PERFORMANCE)
TAKEOFF SAFETY SPEED (FLAPS 1, 5, 15, 20)
TAKEOFF CLIMB (FLAPS 15) - A/C PACKS ON
CLOSE-IN OBSTACLE CLEARANCE (ALL FLAPS)
DISTANT OBSTACLE CLEARANCE (ALL FLAPS)
OBSTACLE DISTANCE TRADE LINES
MAXIMUM LEVEL-OFF HEIGHT (FLAPS 15)
THIRD SEGMENT DISTANCE (FLAPS 15)
FINAL TAKEOFF CLIMB (FLAPS UP) - A/C PACKS ON
GRADIENT CORRECTIONS (TAKEOFF/FINAL TAKEOFF CLIMB)
DISTANT OBSTACLE CLEARANCE - ALL FLAPS
END OF EXTENDED SECOND SEGMENT - 5 MINUTE LIMIT

APPENDIX 6 - ALTERNATE THRUST SETTING METHOD (% N1 RPM)
(JT9D-7R4D ENGINES)
General
Thrust Setting
Weight Limitations
Procedures
TAKEOFF N1 POWER SETTING
GO-AROUND N1 POWER SETTING
INFLIGHT N1 POWER SETTING (MAX CONTINUOUS)

APP. 15 - OPERATION WITH INTERMIXED CATEGORY A AND B BRAKES 767-200
Introduction
SECTION 1 - CERTIFICATE LIMITATIONS
General Limitations
SECTION 2 - EMERGENCY PROCEDURES
SECTION 3 - OPERATING PROCEDURES
SECTION 4 - PERFORMANCE
Takeoff Speeds
Brake Energy Limits
Landing Field Length and Speed
Maximum Quick Turnaround Weight
MAXIMUM QUICK TURAROUND WEIGHT ADJUSTMENT CHARTS

APPENDIX CDL - MODEL 767 SERIES CONFIGURATION DEVIATION LIST
General Limitations
SYSTEM 21 - AIR CONDITIONING
Cabin Pressure relief Valve Flapper Doors
Ram Air Inlet Doors
Ram Air Exhaust Doors
Ram Air Inlet and Exhaust Doors
SYSTEM 23 - COMMUNICATIONS
Static Dischargers
SYSTEM 27 - FLIGHT CONTROLS
Inboard Trailing Edge Flap-To-Fuselages Seals
SYSTEM 28 - FUEL
Override Boost Pump Access Panels
Fuel Quantity Measuring Sticks
SYSTEM 32 - LANDING GEAR
Main Landing Gear Wing Door
Tail Skid Fairing
Tail Skid Lever Door
SYSTEM 33 - LIGHTS
Main and Bulk Cargo Door Light Covers
Wing Illumination Light Covers
Nose Gear Taxi Light - Double and Single Configuration
Wing Tip Aft Navigation Light Lens
Wing Tip Strobe Lights
Upper and Lower Body Anti-Collision Lights
External Emergency Escape Light Covers, Overwing and Ground Illumination
SYSTEM 52 - DOORS
Electrical/Electronics External Power Door
Portable Water Service Doors, Standard Configuration
Portable Water Service Doors, Alternate Configuration
Outboard Wing Leading Edge Pressure Fueling Door
Main Cargo Loading Control Doors
SYSTEM 53 - FUSELAGE
Wing Root Jacking Point Access Panels
Aft Toilet Service Door
Main Cargo Doors Control Switch Panels
APU Louvered Pressure Relief Door
Nose Landing Gear Hinge Cover Door
SYSTEM 54 - NACELLE/PYLON
Nacelle Strut-To-Wing Seals
Aft Fairing Primary Nozzle-To-Strut Seals
Nacelle Strut Pressure Relief Door
Nacelle Strut Access Door
SYSTEM 55 - STABILIZER
Horizontal Stabilizer-To-Elevator Seals
Vertical Stabilizer-To-Fuselage Seals
SYSTEM 57 - WINGS
Wing Leading Edge Slat Linkage Fairing Panels
Wing Thermal Anti-Icing Duct Seal
Fixed Leading Edge Seals
Main Landing Gear Trunnion Support Fairings
Trailing Edge Flap Hinge Fairings
SYSTEM 71 - POWER PLANT
Fan Cowl Pressure Relief Access Doors
SYSTEM 78 - EXHAUST
Thrust Reverser Sleeve Actuator Access Panels
Thrust Reverser Track Fairings
Louvered Door at Bottom of Nacelle Low Bifurcation

FINALY SOME COPIES AND REVISIONS OF SOME OF THE FORMER CHAPTERS
Eier:Norsk Luftfartsmuseum


EksemplarStatusNoteEierPlasseringBindHylleFrist
1.exIkke til utlånNorsk LuftfartsmuseumNorsk Luftfartsmuseum21-A-2
Vurdering:
Ikke til utlån