Checklist Flight Manual

 

 

 

 

 

Die folgende Checkliste basiert auf dem “Flight Manual P 149 D” mit Stand vom 1. Juli 1983. Es werden zunächst nur die “Normal Procedures” auf den Seiten 1-3 vorgestellt.

Beachte bitte die ‘Haftungshinweise’ am Seitenende.

 

 

 

 

 

PREFLIGHT CHECK

 

 

BEFORE EXTERIOR INSPECTION

Ignition key

OUT

Battery switch

OFF

All circuit breakers

OFF

Flight controls

LOCKED

Elevator and rudder trim tabs  

NEUTRAL

Flap lever

REST 1

Landing gear switch

DOWN

Oil quantity

CHECK 8 ltr

Oil filler cap

CLOSE

Fuel quantity

CHECK

Filler caps of both tanks

CLOSE

EXTERIOR INSPECTION

160327NormalProceduresBild01

LEFT WING

Wing

CHECK condition, no skin wrinkles and leakages

Flap

CHECK condition, hinges secured

Aileron an trim tab

CHECK condition, rods and hinges secured

Wing tip and position light

CHECK condition

Pitot tube

Cover removed - CHECK condition

Landing light

CHECK condition

LEFT LANDING GEAR

Wheel

CHOCKED

Wheel and tire

CHECK condition, slippage marks and tire pressure

Landing gear strut

CHECK for damage and extension (approx. 5,5 cm)

Electrical cables and micro switch

CHECK for damage

Break and hydraulic lines

CHECK for leakage

Landing gear and landing gear fairing

CHECK condition

NOSE WHEEL

Wheel and tire

CHECK condition, slippage marks and tire pressure

Landing gear strut

CHECK for damage and extension (approx. 10 cm)

Landing gear and fairing

CHECK condition

POWER PLANT SECTION

Propeller

CHECK for exessive play, oil leaks, nicks

Governor linkage

SECURED

Engine cowling

SECURED

Intake ducts and exaust

CLEAR

Power plant

CHECK for oil and fuel leakages

RIGHT LANDING GEAR
Refer to left landing gear
 

RIGHT WING

Landing light

CHECK condition

Wing tip and position light

CHECK condition

Aileron and trim tab

CHECK condition, hinges secured

Flap

CHECK condition, hinges secured

Wing

CHECK condition, no sking wrinkles and leakage

FUSELAGE (RIGHT SIDE)

Fuselage

CHECK general condition

Inspection doors

CLOSED

Fuel vent

CLEAR

Loop antenna housing

CHECK condition

Anticollision lights

CHECK condition

EMPANNAGE

Horizontal and vertical fin

CHECK condition

Elevator and rudder

CHECK condition, hinges secured

Trim tabs

NEUTRAL

Tail position light

CHECK condition

FUSELAGE (LEFT SIDE)

Fuselage

CHECK general condition

Anticollision lights

CHECK condition

Static ports

CLEAR

First aid kit

ABOARD

Radio communication system crystals

CHECK

Radio access door

CLOSE

Antenna and loop antenna housing

CHECK condition

INTERIOR INSPECTION

WARNING
Do not enter or leave the aircraft with engine running

Cockpit

CHECK for loose objects

Baggage compartment

CHECK for loose object, beggage secured

Canopy emergency jettison handle

Safety wired, CHECK seal intact

Flight controls

UNLOCK, CHECK for free and proper movement

Parking break

SET

Seat

ADJUST

Safety belts

FASTEN, CHECK for locking and unlocking function

Ignition key

INSERT

Fuel shutoff knob

IN

Landing gear circuit breaker

IN

Landing gear position indicator circuit breaker

IN

Carburetor heatcontrol knob

COLD

Cowlflap handle

REST 3

Stopcock

OUT

Landing light switches

OFF

Fuses / caps

TIGHT

Cabin heat and ventilation system

CLIMATIC

Trim system

CHECK full travel

Fuel tank selector

L/H tank

Flap lever

CHECK all six rests

Flap lever

REST 0

Landing gear emergency handcrank



 

STOWED, safety wired, seal intact

NOTE
Make sure that the handcrank is fully down and the microswitch is depressed

STARTING ENGINE

Propeller control lever

FULL FINE

Throttle

OPEN 1/10

External power source

CONNECTED or Battery switch on

Voltmeter

24 V

Anticollision lights

ON

Fire warning light

PRESS to test

Generator circuit breaker

IN

Starter an fuel quantity, oil pressure and oil temperatur gages circuit braker

ON

Landing gear position indication

CHECK down

Fuel

CHECK quantity

Primer

Actuate 3 to 5 times (relock primer)

Electrical fuel pump

ON

NOTE
Fuel pressure indication must be within the green range

Propeller

CLEAR

Ignition switch

M1

Starter button

PRESS

Immediately after the engine has fired
- Stopcock
- Ignition switch



 


Fully IN
M1 + M2

NOTE
If engine stops, stopcock immediately OUT

Throttle

1200 to 1500 RPM

Oil pressure


 

 

Within limits

CAUTION
If oilpressure is not indicated within 30 sec, stop the engine and determine the reason

Electrical fuel pump

OFF, CHECK pressure

If external power is used

APU disconnect, Battery switch ON

 

 

 

 

 

continue checklist, Page 2

 

 

HAFTUNGSHINWEIS

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