What it approves
Install KAP-100 single axis, KAP-150 two or three axis or KFC-150 two or three axis flight control system, optional KAS-297B vertical speed and altitude selector and KFC-150 system with optional flight director displays.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)
Number: SA1575CE-D This certificate issued to: Honeywell International Inc.
21111N 19th Ave Phoenix, Arizona 85027 Part 23of the Federal Aviation Regulations.
Original Product – Type Certificate Number: Make: Piper Model:
A7SO PA-34-200T, PA-34-220T
Install KAP100 single axis, KAP150 two or three axis, or KFC150 two or three axis Flight Control System, KAS297B Vertical Speed and Altitude Selector and KFC150 system with optional dual Flight Director displays.
(See Continuation Sheet for Required Data)
This approval should not be extended to other specific airplanesof this model on which other previously approved modificationsare incorporated, unlessit isdetermined that the interrelationship between this change and any of those other previously approved modificationswill introduce no adverse effect upon the airworthinessof that airplane.
If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
Date of Application: December 9, 1982 February 28, 1995, February 28, 2000, Date Reissued: March 25, 2020 Date of Issuance: February 11, 1983
September 4, 1984, December 23, 1987
Signature
Title Richard B. Sleigh ODA Administrator, ODA-602216-NM
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)
To (Name and address of transferee)
From (Name and address of grantor)
FAA Form 8110-2 (5/14) Page 3 of 3
(Continuation Sheet) Number: SA1575CE-D
Description of Type Design Change: (continued) REQUIRED DATA:
KAP100 Single Axis Flight Control System
1. Master Drawing List 155-9275-00, dated 1-3-83 for Field Installation.
2. Airplane Flight Manual Supplement 006-0417-00, dated 2-11-83.
KAP150 and KFC150 Two or Three Axis Flight Control System 1a. Master Drawing List 155-9275-00, dated 1-3-83 for Field Installation.
1b. Master Drawing List 155-9275-01, Rev. 1, dated 1-28-83for Piper Factory Installation.
2. Airplane Flight Manual Supplement 006-0417-01, dated 2-11-83.
Optional KAS297BVertical Speed and Altitude Selector 1a. Master Drawing List 155-9275-00, Rev. 2, dated 8-24-84for Field Installation.
1b. Master Drawing List 155-9275-01, Rev. 3, dated 9-4-84 for Piper Factory Installation.
2. Airplane Flight Manual Supplement 006-0417-02, dated 9-4-84.
KFC150 System with Optional Dual Flight Director Displays
1. Master Drawing List 155-9275-02, Rev. 1, dated 12-22-87for Piper Factory Installation.
2. Airplane Flight Manual Supplement 006-0479-01, dated 12-23-87.
Later FAA approved revisionsto above listed data are incorporated without further revision to the Supplemental Type Certificate.
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ADs that name this STC · 1
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 2
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| March 25, 2020 | Reissued, current | Certificate |
| February 28, 2000 | Reissued, earlier issue | Certificate |