What it approves
Installation of Pratt & Whitney AC L PT6A-20, -27 engine and airplane modifications to increase the maximum takeoff gross weight to 8,000 pounds.
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.
ttnitd goto if 2UKriea Beparrmcnt of transportation federal atriation administration Supplemental 'Cpe Certificate <Sutm<v0r' SA4678SW Southeastern Resources Corp.
2201 Scott Avenue Fort Worth, TX 76103 ^^JA&^^ 4*r*<vn>/mc^^^ 3 ClVll Air &MtM A20SO PA31-350 Installation of Pratt & Whitney ACL PT6A-20, -27 engines and airplane modifications to increase the maximum takeoff gross weight to 8,000 Ibs. according to Drawing List No. 60,OOOL (Rev.
9) dated 7/31/84, or later FAA approved revision. Installation ofEdo-Aire Mitchell Century III Autopilot Model AK560 according to STC SA3086SW-D. Installation of Edo-Aire Mitchell Yaw Damper System Model YK849 according to STC SA3388SW-D.
"See'C'oritlnuat'iofT"Sheet, page 2 of this STC. Compatibility of this modification with previously installed equipment must be determined by installer.
4e***^ £Xe/rn*ruti&a£>r-^.4&e June 1981 1982 : 12/30/82, 3/3/88, 8/9/88 .8/9/83; 10/5/83; 1/30/85 $/v/Jc/t/rf<c&&n;^£ri^£:j£arnj/rit&lr<i/^ ^/O/*? // — ^/•S, C^^^Qg^ L. B.
Manager, Rotorcraft Directorate, Aircraft Certification Service (Title)
FAA Fout SI 10-2 (10-68)
ttnittd £tatu of anrerica Bepartment of Importation— Jfetol 2ttnation administration Supplemental Itgpe Certificate(Continuation &heet) SA4678SW Rev. 3 Limitations and Conditions:
1. FAR Approved Pilot's Operating Handbook (POH) dated May 19, 1982, (Revision 1 dated December 30, 1982) is required for Pratt & Whitney ACL PT6A-20, -27 engines and airplane modifications to increase the Waodinum takeoff gross weight.
2. EAA Approved Airplane Flight Manual Supplement dated August 9, 1983, is required with Edo-Aire Mitchell Century III Autopilot Model 2KE60.
3. FAA Approved Airplane Flight Manual Supplement dated August 9, 1983, is required with Edo-Aire Mitchell Yaw Damper System Model YK849.
4. STC SA3086SW-D is required for installation of Edo-Aire Mitchell Century III Autopilot Model AK560.
5. STC SA3388SW-D is required for installation of Edo-Aire Mitchell Yaw Damper System Model YK849.
6. Compatibility of this modification with other previously approved modifications must be determined by the installer.
-END- Atir alteration of this certificate is punishable by a fine of not exceeding SI,000, or imprisonment not exceeding 3 years, or both.
i AA FORM Biio-2-1 (10-69) This certificate may be transferred in accordance with i'AR ~1.-I7 PAGE 2 OF 2 PAGES
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and <7/> code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and <7P code) 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.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Piper Aircraft Inc. | PA-31-350 | A20SO |