STC SA1239SW

Supplemental type certificate · George D. Merrell

Holder
George D. Merrell · United States
Status
Current · Reissued
Status date
November 22, 1998
Applied
August 14, 1970
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21
Data sheet
TCDSA1EA

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of Rajay turbosupercharges and Lycoming IO-360-C1C or IO-360-C1F engines.

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.

Jttittttb of Qlrmtspcrtatfrnt - Of .Amttica (Afriattmt (Abmttrtstrjrtiim (Esrtifttate SA1239SW George D. Merrell, an Individual DBA George Merrell. Co.

Hwy 1431 West at Pacific Loop Kingsland, TX 78639 Civil Air A1EA Piper PA-30, PA-39 Installation of Rajay turbochargers and Lycoming IO-360-C1C or IO-360-C1F engines in accordance with J. w. Miller Drawing List No. 28,000 dated August 11, 1970, revised September 10, 1972; or later PAA approved revision.

(See continuation sheet 3 of 3) .-August 14, 1970 January 04, 1971 22, 1998 10/16/72; 1/17/73;

10/2/73; 3/14/83 Rev. 4 ._1 / ^f ~—^ (Signature) S. Frances Cox Manager, Special Certification Office, Southwest Region (Title) Any *JtBrfltion of thia certificate if punltfhdbl* by d flna o/ not exceeding $1,000. or itopriBonp&flt not exceeding 3 PAA rofit aiiD-2no-6S) page ] 01 JMX ho transferred in accordance with PAR 21.47-

Jtmtrfl £fctift* flfH , of Srmtspirrfcittmt - Jfr&tral ^A&tjittott jWmthristraittm (Eerttftcate ((Emtttnuatttm SA1239SW Date of Issuance: January 04, 1971 Date of Reissuance: November 22, 1998 (Continued):

1. The following FAA Approved Airplane Flight Manual Supplements are required:

a. Supplement dated January 4, 1971, revised October 2, 1973, with Lycoming IO-360-C1C engines;

b. Supplement dated October 16, 1972, with Lycoming IO-360-C1F;

c. Supplement dated January 17, 1973, revised October 2, 1973, with Lycoming IO-360-C1F engines and aircraft modified by STC SA2312WE.

2. Dorsal fin provided with STC SA1112SW or STC SA2312WE is required.

3. For Model PA-30 rudder aileron interconnect system per STC SA1154SW or Piper interconnect system is required.

4. Loading instructions for individual aircraft is required.

5. Compatibility of this modification with other previously approved modifications must be determined by the installer.

-END- Any fllteraUon of thJfl csrMfJc-its is punJahabJw by a flu* of not &#ce&ding Sl,000, or Inpfleomrent not exceeding 3 years, or tto FAA Form 9110-2-l(io-«9) Page 3 of 3 This csrtlfJcare nay Jw trAflflf#rrfld in fccordanca with FAB 21.

INSTKUC ['IONS: The iransfcr ciKlorsc mml hcluiv m;iy he usorf in mil if v the a|>|ji<>|>riat<* FAA }' ogional Olh< <• of the transfer of ihis Siipplciiicnial Type Ccriilu-atr ['In- I-'A A will ri-issiK1 ihi- tcrtitii aic in the n,um- ot thr iransli-ree and lonvai'tl il lo him.

TRANSFER ENDORSEMENT Transfer (he ownership of Supplemental Type Certificate Number __ to (Namf of transferee) _. .

(Address of transferee) r and iticct) (City, SlaU, a;

from (Name vf grantor) (Print or type) ..

(Address ofgrantw) f Number anil tlrtrt) , Slalt, and %IP cud,) Extent of Authority (if licensing agreement):

Signature of grantor (In ink).

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 · 2

MakeModelData sheet
Piper Aircraft Inc.PA-30A1EA
Piper Aircraft Inc.PA-39A1EA