STC SA222SW

Supplemental type certificate · Hutchinson Aircraft Svc

Holder
Hutchinson Aircraft Svc · United States
Status
Current · Reissued
Status date
October 17, 1973
Applied
July 12, 1962
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDS2A13

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of propeller and cowl rework.

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 £tatrs of America Btpartment of Transportation — federal Sloiation administration Supplemental TCpe Certificate *-Sl0QAt£a<&0n&'-.

tSMvrnvetp' SA222SW Hutchlnson Aircraft Service P. 0. Box 1070 Borger, Texas 3 'Mf Civil Air Ptper PA-28-150, PA-28-160, PA-28-180, PA-28-140 PA..?8-140, PA-28-150, and PA- 28- 160 installation of Hartzell HC-82XL-6N/7636D 4 or HC~82XL-6N/8^33-12 propeller and coT'l rework in accordance with Drawing List revised 4/28/67 and packing list revised 10/29/64. ?. For PA-?8-180 Installation of KcCauley ?D36C14/78»1- 4 or Hartzell HC-92-ZK-8D/8447A-12A propeller and co^l rer-ork in accordance with Drawing List revised 4/28/67 and packing list revised 10/29/64, and Installation Instructions Supplement revised 7/24/64.

See Continuation Sheet, page 2, a part of this STC.

^b& jjf^a/ift&fji&f July 12, 1962 May 20, 1963 '. 12/11/64; 5/12/67( 10/17/73 Revision 3 (Signature) Glen W. Welsh Chief, Engineering and Manufacturing Branch (Tale)

FAAFow,81IO-Z(10-AB)

Unlttfl Stattt of Slmirica ©tpartmtnt of transportation— idetal Station administration Supplemental t^pe Certificate(Continuation SA222SW Revision 3 Limitations and Conditions!

1. For PA-28-150, PA-28-160, and PA-28-140 with 0-320-E2A engines only.

a. FAA Approved Airplane Flight Manual Supplement appropriate to the engine installed dated 5/13/63 is required.

b. Spinner installed per item 3(a) of Spec. IAIO is required,

c. Piper engine cooling kit per drawing SKVB-240 Rev. 8/2/6? required.

d. Lycoming 0-320 Series engines converted for controllable pitch props per FAA approved service bulletins eligible.

e. Prop pitch settings 12° low 26° high.

£. Loading instructions dated 7/24/64 required.

2. For PA-28-180.

a. FAA Approved Airplane Flight Manual Supplement dated 8/14/63 is required.

b. Lycoralng 0-360 series engines converted for controllable pitch props per FAA approved service bulletins eligible.

c. Prop pilch settings 12.7° low ?7.5° high.

d. Loading instructions dated 7/24/64 required.

•1. Eligible on Serial Numbers 28-1760 and below.

FAA FORM 8110-2-1 (io-69) PAGE ? OF IMAGES FAA AC 7B-4435

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 4

MakeModelData sheet
Piper Aircraft Inc.PA-28-1402A13
Piper Aircraft Inc.PA-28-1502A13
Piper Aircraft Inc.PA-28-1602A13
Piper Aircraft Inc.PA-28-1802A13