| Tittel: | F-27 : Aeroplane Flight Manual | | Forfatter: | Braathens | | Materialtype: | Manual/Sivil | | Signatur: | 21-A-5 | | Utgitt: | Amsterdam : Fokker Aircraft B.V., [1959] | | Omfang: | upag. | | Emneord: | Aeroplane Flight Manual / Braathens / Fokker 27 | | Lokal Note (gave): | Braathens | | Materialbetegnelse: | Technical Handbook | | Materialbetegnelse: | Perm | | Note: | Published Feb 17/59 (first entry). Last revision, revison no. 352, dated Nov 8/76.
Last Addenda, Addenda No. 35, dated March 29/73
Written inside the cover of the binder: "No: 6 Captain N. Ringdal", and on the back
of the binder: "6 F. 27" | | Innhold: | TABLE OF CONTENTS:
Distribution List
Introduction
Foreword
Purpose and Scope
Index System
Issuance of Manuals
Revisions and Addenda
General
Record of Revisions
Record of Addenda
CHAPTER I - DESCRIPTION AND DESIGN CHARACTERISTICS
1.1 General
1.1.1 Certification Particulars
1.1.2 Aircraft Dimension
1.1.3 Powerplant Data
1.1.4 Engine Auxiliaries
1.1.5 Pneumatic
CHAPTER II - LIMITATIONS AND PROCEDURES
2.1 Limitations
2.1.1 Weight Limitations
2.1.2 Powerplant Limitations
2.1.3 Fuel and Oil System Limitations
2.1.4 Airspeed Limitations
2.1.5 Miscellaneous Limitations
2.2 Procedures
2.2.1 Flight Characteristics
2.2.2 Handling
2.2.3 Checklist
2.2.4 Minimum Equipment
2.2.5 ATC Procedures
CHAPTER III - TECHNICAL
3.1 Accommodation and Equipment
3.1.1 Accommodation
3.1.2 Equipment
3.2 Power Plant
3.2.1 Engine Description
3.2.2 Water/Methanol
3.2.3 Propeller Description
3.2.4 Engine and Propeller Control
3.2.5 Oil System
3.2.6 Engine Fire-warning and Extinguishing System
3.2.7 Normal Operation
3.3 Flying Controls
3.3.1 General
3.3.2 Gust Locks
3.4 Flaps Control System
3.4.1 Description
3.4.2 Emergency Operation
3.5 Pre-stall Warning
3.5.1 General
3.6 Landing Gear System
3.6.1 Introduction
3.6.2 Main Landing Gear
3.6.3 Nose Landing Gear
3.6.4 Control and Signaling
3.6.5 Brakes
3.7 Pneumatic System
3.7.1 Main System
3.7.2 Landing Gear Circuit
3.7.3 Nosewheel Steering Circuit
3.7.4 Wheel Brake Circuit
3.7.5 Emergency System
3.7.6 Normal Operation
3.7.7 Emergency Operation
3.7.8 Diagram
3.8 Fuel System
3.8.1 Description
3.8.2 De-icing Description
3.8.3 Normal Operation
3.8.4 Emergency Operation
3.8.5 Miscellaneous
3.9 Water/Methanol
3.9.1 Description
3.9.2 Operation
3.9.3 Miscellaneous
3.10 Instruments
3.10.1 General
3.10.2 Flight Instruments
3.10.3 Gyroscopic Instruments
3.10.4 Navigation Instruments
3.10.5 Powerplant Instruments
3.10.6 Miscellaneous
3.11 De-icing System
3.11.1 General
3.11.2 Airframe De-icing
3.11.3 Power Plant De-icing
3.11.4 Wing Air Intake Anti-icing
3.11.5 Fuel Filter De-icing
3.11.6 Windshield De-icing
3.11.7 Pitot Head and Stall Warning Anti-icing
3.11.8 Miscellaneous
3.12 Electrical System
3.12.1 Description
3.12.2 Normal Operation
3.12.3 Start and Relight System
3.12.4 Lighting Circuits
3.12.5 Emergency Operation
3.13 Pressurization and Air Conditioning
3.13.1 Pressurization
3.13.2 Air Conditioning
3.14 Oxygen System
3.14.1 Description
3.15 Radio
3.15.1 Description and Location
3.15.2 VHF Transmitter/Receiver Type 17L-7/51x-2
3.15.3 VHF Navigation Receivers Type 51x-2
3.15.4 75 MC/s Marker Beacon Type 51z-2
3.15.5 Glideslope Receiver Type 51v-3
3.15.6 Interphone System
3.15.7 Public Address System
3.15.8 Audio Control Panel
3.15.9 ADF Receiver Type 51y-1
3.15.10 Emergency System
3.15.11 ATC Transponder
3.15.12 Distance Measuring Equipment (DME)
3.16 Auto Pilot
3.16.1 General
3.16.2 Description and Location of Components
3.16.3 Electrical and Pneumatic Supplies
3.16.4 Normal Operation
CHAPTER IV - FLIGHT PREPARATIONS
4.1 Flight Planning
4.1.1 General
4.1.2 Fuel Planning Tables
01 Altitude 6.000 ft.
02 Altitude 7.000 ft.
03 Altitude 8.000 ft.
04 Altitude 9.000 ft.
05 Altitude 10.000 ft.
06 Altitude 11.000 ft.
07 Altitude 12.000 ft.
08 Altitude 13.000 ft.
09 Altitude 14.000 ft.
10 Altitude 15.000 ft.
11 Altitude 16.000 ft.
12 Altitude 17.000 ft.
13 Altitude 18.000 ft.
14 Altitude 19.000 ft.
15 Altitude 20.000 ft.
16 Optimum Fuel, Time and Economic Altitudes
4.1.3 Miscellaneous
01 Fuel Consumption During Holding
02 Required Quantity of Water/Methanol for Take-off - Flap 16.5° - Wet
Take-off Power
03 Required Quantity of Water/Methanol for Take-off - Flap 0° - Wet
Take-off Power
04 Required Quantity of Water/Methanol for Landing
4.2 Weight and Balance
4.2.1 Release Load
4.2.2 Loading
4.2.3 Loading Table
CHAPTER V - PERFORMANCE
5.1 Performance Information
5.1.1 General
5.1.2 Take-off
5.1.3 Take-off Flight Path
5.2 Instrument Corrections
5.2.1 Airspeed Calibration, Normal System
5.3 Characteristic Airspeeds
5.3.1 Power Off Stalling Speed Vs
5.3.2 Flap Retraction Speed & Single Engine. Final Take-off and En Route Climb
Speed
5.3.3 Target Threshold Speed Flaps 40°
5.3.4 Approach and Landing Climb Speeds
5.4 Take-off
5.4.1 Flap 16.5° Wet Take-off Power
5.4.2 Flap 16.5° Dry Take-off Power
5.4.3 Flap 0° Wet Take-off Power
5.4.4 Flap 0° Dry Take-off Power
5.5 Take-off Flight Path
5.5.1 Maximum Continuous Power
5.6 En Route
5.6.1 Climb Performance
5.7 Landing
5.7.1 Landing Weight Permitted by Climb Requirements - Wet Take-off Power and
Maximum Continuous Power
5.7.2 Required Landing Runway Lenght
5.7.3 Climb Performance
5.7.4 Water Methanol Requirement for Landing
5.8 Airport Gross Weight Charts
5.8.1 General
5.8.2 Tabulations
CHPATER VI - EMERGENCY
6.1 Location of Equipment
6.1.1 Emergency Equipment Layout
6.1.2 Emergency Equipment
6.2 Emergency Procedures
6.2.1 Engine Failures
6.2.2 Fire-Drills
6.2.3 Technical Failure
6.2.4 Explosive Decompression
6.2.5 Emergency Landing and Evacuation
6.2.6 Emergency Drill
6.2.7 Tabulated Crew Drill
CHPATER VII - MISCELLANEOUS
7.1 Ground Handling
7.1.1 Parking F-27 Friendship
7.1.2 De-icing on Ground
7.1.3 Technical Inspections
7.1.4 Engine Winterization | | Eier: | Norsk Luftfartsmuseum | | |
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