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Piper PA-28-161 Maintenance Manual

Piper PA-28-161
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PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 15
Nov 30/06
3H15
34-20-00
(c) Place the aircraft on the South compass rose heading. Rotate the indicator card to South
using the manual slave buttons on the slaving control. With a non-magnetic screwdriver in
the N/S opening on the slaving control, adjust to remove one-half (1/2) of the existing
deviation shown by the slave meter.
(d) Place the aircraft on the West compass rose heading. Rotate the indicator card to West
using the manual slave buttons on the slaving control. With a non-magnetic screwdriver in
the E/W opening on the slaving control, adjust to remove one-half (1/2) of the existing
deviation shown by the slave meter.
(e) If deviation (difference between actual magnetic heading and what compass indicates on
that particular heading) exceeds ± 10° on any heading, instrument replacement may be
necessary. To verify, do the following:
1 Check whether any magnetic metals are near compass (tools, flashlights, pocket
knives, wristwatches, etc.)
2
Check to be sure screwdriver being used to make adjustments is either fiber or a
non-magnetic metal, such as brass.
3
When satisfied that errors in excess of 10° are the fault of the instrument, replace
instrument. After installing a new instrument, repeat procedures (1) and (2).
(f) After all adjustments are completed, the indicator shall read within ± 2° of any compass
rose heading on which the aircraft is placed.
B. S-TEC ST-180 Slaved Compass (with HSI)
The S-TEC ST-180 HSI Slaved Compass System may be installed as an option in non-EFIS
equipped airplanes, S/N’s 2842064 and up.
(1) Flux Detector (See Figure 4.)
A flux detector installed in the wing tip of the left wing is used to provide heading data to the HSI.
(a) Removal
CAUTION: PERFORM MAGNETIC HEADING COMPENSATION / CALIBRATION,
BELOW, WHENEVER THE FLUX DETECTOR IS CHANGED.
1 Remove the left wing tip fairing to expose the flux detector.
2 Disconnect the wiring harness from the top of the flux detector to be removed.
3 Unscrew and remove the three brass screws and washers and remove the flux
detector.
(b) Installation
CAUTION: THE FLUX DETECTOR IS SECURED TO THE MOUNTING BRACKET
WITH BRASS SCREWS. ENSURE ONLY BRASS SCREWS ARE USED
WHEN REINSTALLING.
1 Place the flux detector into position on its mounting bracket and secure with brass
screws and washers (3 ea.)
2 Connect wiring harness to the connector on top of the flux detector.
3
Reinstall the Left wing tip.
NO
TE: Ensure correct hardware is used when reinstalling wing tip over flux detector.

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Piper PA-28-161 Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelPA-28-161 Warrior II
EngineLycoming O-320-D3G
Horsepower160 hp
Seating Capacity4
Wingspan35 ft (10.7 m)
Length24 ft 0 in
Maximum Speed127 knots
Cruise Speed122 knots
Maximum Takeoff Weight2, 325 lb (1, 055 kg)
Fuel Capacity48 US gallons (182 L)

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