4.  
Secure the push-pull cable in this position by tightening screws on clamps.  The stop should be lubricated and free to swivel without excessive play.

5.  
Push on seat back with stop assembly in an engaged position to check engagement. Rotate the seat back release handle and check for disengagement of seat back.

LUMBAR SEATS  (Refer to Figure 25-2.) DESCRIPTION
Lumbar pilot and co-pilot seat installations are available as an option.  The installation consists of an inflatable bladder attached to the seat back filler and a inflation bulb located under and on the inboard side of each pilot and co-pilot seat.
25-10-00 Page 25-5 Revised: February 28, 2002
REMOVAL OF LUMBAR BLADDER.
To remove the lumbar bladder for repair or replacement:
1.  
Remove seat from airplane.

2.  
Loosen velcro securing seat back filler cover.

3.  
Remove only enough of seat back filer cover to expose lumbar bladder.

— Note —
Inflation tube may be removed before or after bladder is removed from seat back filler.  Tube is not glued to nipple attachment; it can be removed by carefully pulling on tube.
4.  Remove inflation tube from bladder.
— CAUTION —
DO NOT USE A CHEMICAL SOLVENT TO REMOVE BLADDER. SOLVENT MAY DAMAGE SEAT BACK FILLER
— CAUTION —
TO AVOID OR MINIMIZE DAMAGE TO SEAT BACK FILLER DURING REMOVAL, USE ONE HAND TO RETAIN SEAT BACK FILLER IN PLACE, WHILE GENTLY  REMOVING BLADDER WITH OTHER HAND.
5.  Starting at either right or left edge of bladder, carefully and slowly pull bladder and pad assembly from seat back filler.
INSTALLATION OF LUMBAR BLADDER.
— Note —
An installation kit is required for airplanes not previously equipped with a lumbar support Refer to Piper's Illustrated Parts Catalog for kit part number.
1.  If necessary to assemble pad and bladder:
a.  
Apply a layer of 3M 847 cement to smooth side of bladder pad.

b.  
Apply a layer of 3M 847 cement to back side of bladder (side away from inflation tube nipple).

c.  
Attach bladder pad to bladder.

— Note —
While cement does not set immediately, there is no need to wait before attaching bladder and pad to seat back filler.
2.  
Apply a layer of 3m 847 cement to rough side of bladder pad.

3.  
Apply a layer of 3m 847 cement to seat back filler where bladder is to be located.

4.  
Attach bladder and pad assembly to seat back filler.  Depending on temperature and humidity, allow

0:30 minutes to 1:00 hour for cement to set.
5.  
Install seat back filler cover and secure velcro fastenings.

6.  
Install seat in airplane.

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Figure 25-2. Lumbar Seat Bladder Installation 
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EMERGENCY

— WARNING —
FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION(S), WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT, MAY RENDER THE AIRCRAFT UNAIRWORTHY. (SEE INTRODUCTION - SUPPLEMENTARY PUBLICATIONS.)
This section contains information necessary to perform operational checks of the Emergency Locator Transmitter (ELT), with and without a pilot's remote switch.  Included are the appropriate removal and installation instructions to facilitate battery replacement.
EMERGENCY LOCATOR TRANSMITTER (ELT). DESCRIPTION.
The electrical power for the ELT is supplied by its own self-contained battery.  FAA regulations require the battery be replaced at the expiration printed on the battery. The battery must also be replaced if the transmitter has been used in an emergency situation or if accumulated test time exceeds one hour
PILOT'S REMOTE SWITCH.
Refer to the appropriate Pilot’s Operating Handbook for description, operation, testing and inadvertent activation of the ELT pilot’s remote switch.
ARTEX ELT 110. 
The Artex ELT-110 transmits on 121.5 mHz and 243.0 mHz, and is designed to meet or exceed the requirements of TSO C91a and FAR Part 91.
The Artex ELT 110 cannot be accidently activated by dropping the unit, handling it roughly, or during shipping. However, when properly mounted, and locked into its mounting tray, the ELT will activate in a crash, regardless of the cockpit remote switch and ELT switch position.  The normal position of the ELT switch is in the down or OFF position.  The normal position of the remote cockpit switch is in down or ARM position
　
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