# STC SA01643SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: BAS Inc, United States
- Description: Installation of BAS, Inc. shoulder harness with inertia reel
- Applied: March 22, 2005
- Status date: December 2, 2010
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13), [TCDS A3SO](https://openairdocs.org/tcds/A3SO), [TCDS A7SO](https://openairdocs.org/tcds/A7SO)
- Certificate PDF: https://openairdocs.org/files/sha256/b6/54/b6546ed416eb7fb50ab205d97cdc83ddf49b80b06feeeeceac1e3e3f8b6f4701
- Approved model list and other attachments: [AML SA01643SE.pdf](https://openairdocs.org/files/sha256/ba/aa/baaaf200e40e85c184aa243920fea060dad94c99d131900c8bcfb842bc95419f)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/41605CF07009CEE2862577FB005EC121.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01643SE

## ADs that name it (0)

None.

## Approved models (34)

- Piper Aircraft Inc. PA-28-140 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-150 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-151 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-160 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-161 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-181 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-235 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-236 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-200 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-201 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28RT-201 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28RT-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28S-160 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28S-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-32-260 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32-301 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32-301FT ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32-301T ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32-301XTC ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32R-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32R-301 (HP) ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32R-301 (SP) ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32R-301T ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32RT-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32RT-300T ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32S-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-34-200 ([TCDS A7SO](https://openairdocs.org/tcds/A7SO))
- Piper Aircraft Inc. PA-34-200T ([TCDS A7SO](https://openairdocs.org/tcds/A7SO))
- Piper Aircraft Inc. PA-34-220T ([TCDS A7SO](https://openairdocs.org/tcds/A7SO))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

UnilzlliMolmIi Ammm ~ ofQrnttllllllll1nti1JlromdAuinlinnAbministmtinn

• See Attached FAA Approved Model List SA01643SE for List of Approved Airplane Models and Applicable Airworthiness Regulations ./Yttnz&, SA01643SE BAS, Inc.

411 Super Cub Drive North PO Box 190 Eatonville, WA 98328

c.r'/'Itj!~.1 IAn! 1J1:..rA~.//~Y'tp1/1 IA~ Iy//(P.(M.1rjr/" /f'r tk /b/CJI/N/Ij/ //;YNbICIIPtll! I/t: &/I/Iatio/M (Uta c-t'J/Uhtio/l4 Ih'./~~.,..a.j ;Ylrrtj!f(,/.(F,PO}//- /?I~~/:J d,. lu/-'tum-'lh/lr:J.J n'~/((;Y/llr/I/.J ~%/Y 23 tJ/d'~ Federal Aviation ,9t-j'lIdtl/o/l..1.

(f:J;'tjt(,(a/'9'm(;;(d -0;V('<'?5;,rIt/{caleA{(//(~,r.' .&k.' Jt>,;;,/ 91cJrnitli'V( ,,/ik'c .~(,< 9J"'Jtjt" '6".&z/~,<.'Installation of BAS, Inc. shoulder harness with inertia reel in accordance with BAS, Inc. Report 1006, dated October 15, 2005, or later FAA-approved revision .

.51//(/lali'VlJam/'{?,'a,;;/(,wJ.' Approval of this change in type design applies to the above model aircraft only.

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

A copy of this certificate and FAA Approved Model List SA01643SE must be maintained as part of the permanent records for the modified aircraft.

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 .

.50~Jrr/'Itjlrn/~ u/II'/ lit, J/~~/~/"lt./1? ahta luh:C£/,j lA;,J:-M/.Jj/<ro/ru'tJ{J.(7/Jlfnlf? /Y//lfl";;'1- iN #ct N/tli/' IN/''/YINkl'rr'; JI/"Y,rllrkr,; rn10brL ('.if a vnIU/U:I/(:(,V/ I'b-I/f /J ",lk/Y£"JI'" /'JINtfI/JA:rd tfJttA',.W'tk/u/u'Jlra/tif o/!h .:J?;rk/w/.~Jia//(:'/I ~~~N///{.Jtra//(?/I.

[j)11/(",,/a/'/ll!roll/J/I.' f;ji}al, rYt".J.J///NIO"" March 22, 2005 February 13, 2006 fiji'll."..pn".J.JllrrL.

9'11", a/N('/('/"'d:' December 02,2010 ..:::8yd~;'."diNII"/lb .r;</rkM('''(''( Il, so•••• C-I~ "("f:<Ji.*nature)Actin Mana er Seattle' I raft Certification Office ([; Ie) 000, or imprisonment not exceeding 3years, orboth,

fAA FORM 8110.2 (10~)

FAA APPROVED MODEL LIST (AML) No. SA01643SE BAS, Inc.

SHOULDER HARNESS INSTALLATION 6UKI\;;INAL I::;::;U~ UA I~: reDruary 1J, ZUUt NUMBER NUMBER Or Later FAA-Approved Revision PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-28S-160, PA-28S-180, PA-28R-180, CAR 3, and Revision New, dated1 Piper Aircraft, Inc, PA-28R-200, PA-28-151, 2A13 Type Certificate DS 2A13 Report NO.1006 October 15, 2005 December 02,2010PA-28-161, PA-28-181, PA-28R-201, PA-28R-20n, PA-28-236, PA-28RT-201, PA-28RT-20n, PA-28-20n PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300, PA-32RT-300T, 2 Piper Aircraft, Inc PA-32-301FT, PA-32-301XTC, A3S0 CAR 3, and Report NO.1006 Revision New, dated December 02, 2010PA-32R-301 (SP), Type Certificate DS A3S0 October 15, 2005 PA-32R-301 (HP), PA-32R-30n, PA-32-301, PA-32-30n 3 Piper Aircraft, Inc PA-34-200, PA-34-200T, AlSO FAR 23 Report NO.1006 Revision New, dated December 02,2010PA-34-220T , October 15, 2005 FAAApproved: '--t/Acting Manager, Se .IeAircraft Certification Office Reissued:

Amended: December 02,2010 Page 1of 1

### AML SA01643SE.pdf

FAA APPROVED MODEL LIST (AML) No. SA01643SE BAS, Inc.

for

SHOULDER HARNESS INSTALLATION 6UKI\;;INAL I::;::;U~ UA I~: reDruary 1J, ZUUt ORIGINAL FAA ApPROVEDDRAWINGI DRAWINGLIST ITEM AIRCRAFTMAKE AIRCRAFTMODEL TYPE CERTIFICATION BASIS FOR AML AMENDMENTDATECERTIFICATE ALTERATION ReVISION No. AND DATE NUMBER NUMBER Or Later FAA-Approved Revision PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-28S-160, PA-28S-180, PA-28R-180, CAR 3, and Revision New, dated1 Piper Aircraft, Inc, PA-28R-200, PA-28-151, 2A13 Type Certificate DS 2A13 Report NO.1006 October 15, 2005 December 02,2010PA-28-161, PA-28-181, PA-28R-201, PA-28R-20n, PA-28-236, PA-28RT-201, PA-28RT-20n, PA-28-20n PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300, PA-32RT-300T, 2 Piper Aircraft, Inc PA-32-301FT, PA-32-301XTC, A3S0 CAR 3, and Report NO.1006 Revision New, dated December 02, 2010PA-32R-301 (SP), Type Certificate DS A3S0 October 15, 2005 PA-32R-301 (HP), PA-32R-30n, PA-32-301, PA-32-30n 3 Piper Aircraft, Inc PA-34-200, PA-34-200T, AlSO FAR 23 Report NO.1006 Revision New, dated December 02,2010PA-34-220T , October 15, 2005 FAAApproved: '--t/Acting Manager, Se .IeAircraft Certification Office Reissued:

Amended: December 02,2010 Page 1of 1

UnilzlliMolmIi Ammm ~ ofQrnttllllllll1nti1JlromdAuinlinnAbministmtinn

• See Attached FAA Approved Model List SA01643SE for List of Approved Airplane Models and Applicable Airworthiness Regulations ./Yttnz&, SA01643SE BAS, Inc.

411 Super Cub Drive North PO Box 190 Eatonville, WA 98328

c.r'/'Itj!~.1 IAn! 1J1:..rA~.//~Y'tp1/1 IA~ Iy//(P.(M.1rjr/" /f'r tk /b/CJI/N/Ij/ //;YNbICIIPtll! I/t: &/I/Iatio/M (Uta c-t'J/Uhtio/l4 Ih'./~~.,..a.j ;Ylrrtj!f(,/.(F,PO}//- /?I~~/:J d,. lu/-'tum-'lh/lr:J.J n'~/((;Y/llr/I/.J ~%/Y 23 tJ/d'~ Federal Aviation ,9t-j'lIdtl/o/l..1.

(f:J;'tjt(,(a/'9'm(;;(d -0;V('<'?5;,rIt/{caleA{(//(~,r.' .&k.' Jt>,;;,/ 91cJrnitli'V( ,,/ik'c .~(,< 9J"'Jtjt" '6".&z/~,<.'Installation of BAS, Inc. shoulder harness with inertia reel in accordance with BAS, Inc. Report 1006, dated October 15, 2005, or later FAA-approved revision .

.51//(/lali'VlJam/'{?,'a,;;/(,wJ.' Approval of this change in type design applies to the above model aircraft only.

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

A copy of this certificate and FAA Approved Model List SA01643SE must be maintained as part of the permanent records for the modified aircraft.

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 .

.50~Jrr/'Itjlrn/~ u/II'/ lit, J/~~/~/"lt./1? ahta luh:C£/,j lA;,J:-M/.Jj/<ro/ru'tJ{J.(7/Jlfnlf? /Y//lfl";;'1- iN #ct N/tli/' IN/''/YINkl'rr'; JI/"Y,rllrkr,; rn10brL ('.if a vnIU/U:I/(:(,V/ I'b-I/f /J ",lk/Y£"JI'" /'JINtfI/JA:rd tfJttA',.W'tk/u/u'Jlra/tif o/!h .:J?;rk/w/.~Jia//(:'/I ~~~N///{.Jtra//(?/I.

[j)11/(",,/a/'/ll!roll/J/I.' f;ji}al, rYt".J.J///NIO"" March 22, 2005 February 13, 2006 fiji'll."..pn".J.JllrrL.

9'11", a/N('/('/"'d:' December 02,2010 ..:::8yd~;'."diNII"/lb .r;</rkM('''(''( Il, so•••• C-I~ "("f:<Ji.*nature)Actin Mana er Seattle' I raft Certification Office ([; Ie) Any alteration of this certificate is punishable by a fine of not exceeding $1.000, or imprisonment not exceeding 3years, orboth, This certificate may be transferred inaccordance with FAR 21.47.

fAA FORM 8110.2 (10~)

## Every issue (2)

- December 2, 2010: Amended, Current. [certificate](https://openairdocs.org/files/sha256/b6/54/b6546ed416eb7fb50ab205d97cdc83ddf49b80b06feeeeceac1e3e3f8b6f4701), [AML SA01643SE.pdf](https://openairdocs.org/files/sha256/ba/aa/baaaf200e40e85c184aa243920fea060dad94c99d131900c8bcfb842bc95419f)
- February 13, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/58/b8/58b8fd7a7eb80286a7ca0a8d9cc4f8bd66e6bccdbe2d84c46f56d74aae01a84c), [SA01643SE_AML.pdf](https://openairdocs.org/files/sha256/ae/b3/aeb3f425a8f9a1c0c40262d0d81e27dfcade7cf9e35b65d98c964c2065a34dc9)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.