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Piper Aircraft Corporation PA-24-260 Flight Manual
Piper Aircraft Corporation PA-24-260 Flight Manual

Piper Aircraft Corporation PA-24-260 Flight Manual

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PIPER AIRCRAFT CORPORATION
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-2/ =260
SUPPLEMENT NO. 1 TO PIPER
|
THIS
DOCUMENT MUST BE ATTACHLD
Approval Basls
CAR 3 and 410
TO THE BASIC ATRPLANE FLIGHT
Approved June 30,
1965
MANUAL AND KIPT IN THY ATIRPLANE
Piper Model PA-2£—26O
WHILN THEE
ITEM
OF
EQUIPMINT
Equipped with
Plper Altimatic
DESIGNATED BELOW IS
INSTALLED.
II with Automatic
Trim
Normal
Category Only
INSTALLATION OF PIPER ALTIMATIC MODEL AKO89 WITH AUTOMATIC TRIM
Placards:
*(1)
Below the directional gyro:
PULL TO SELECT HEADING
(2)
To the right of the control console:
PIPER ALTIMATIC PILOT
INSTRUCTIONS
LIMITATIONS:
1.
Pilot off during take-off and landing.
2.
Pilot off above 180 MPH.
NORMAL OPERATION:
1.
Refer to
Flight Manual.
1.
Disengage
Altimatic
Controls
2.
Altimatic may be
overpowered manually.
(3)
To the right of the Pitch Control Knob:
PULL
(4)
To the left of the PITCH CONTROL KNOB:

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