STC SA00529SE

Supplemental type certificate · Central Airlines Inc

Holder
Central Airlines Inc · United States
Status
Current · Amended
Status date
November 17, 1998
Applied
May 28, 1996
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDS6A1

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

What it approves

Modification, inspection, and repair of the wing to fuselage attachment straps, wing leading edge close outs, and wing station 24.0 ribs.

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.

1tuftd'a ~rt 1\mmm &pmltntttt llf wnmspnrtnlinn---1'1.00l:ml .Nmt1inn i\hministndinn hpplttntntnl mwt Cl!trtifiattt /lit,.m,/'eF SAP0529SE Central Airlines, Inc.

411 Lou Holland Drive Kansas City, MO 64116 oe,ct/f'ej eke ck o~1n, cllc ty;w dej~JG, cllcjG!f6tLJ-in;?po-dace tLJ-tt.4 ck dm,t'tacio-n.1 and'00-ndttio-n.1 c~jG,aJ :ywot/f'edllcn:o-nme&t"j cllc IZY'tLJ-o-4/!vzejj n:~avenwn/"j o-/Y'CV'c 3 o-/ck Civil Air !lfcpahio-n.1.

&,~$0-daoc-~ ~,cFak /Yttm#'e;-.· 6A1 .A:de.· Twin Commander ~de/:- 500, 500A, B, S, U, 560A, and E 9'ejortJ7,cio-n o-/cllc ~9'ej~ W~.- Modification, inspection and repair of the wing to fuselage attachment straps, wing leading edge close outs, and wing station 24.0 ribs in accordance with Central Airlines, Inc. Service Bulletin No. CA223-TKS, Revision 3, dated June 30, 1998, or later FAA approved revision.

NOTE: This STC has been determined to be an acceptable alternate method of compliance with Airworthiness Directive (AD) 98-08-19, Part I and II only. Accomplishment of Part Ill of the AD is still required .

.2'tmttacio-n.1 and' Wo.ndttio-n.1.· Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of these models 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 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.

!JZ"J oe.dtj{oaCe an,d'Clfc jUfZjW.f'Ctn;? afata tLJ-lft:o_,{ t°d Clfc ,fa,jt,"j /Gr 0/1fY'IJ-IHZ/jk.f/re/7UU/2, in, e;ff;oeU,.12,/"i/'ju,­ n:naen:d ja:ywnded /'e{I-O-.i'ed 0-/-' a CernunaCio-n ala& t,"j o-cllc,tLJ-t°de e.Mdibllcd tfi, cllc Jtft/4-wu"Jcraco-r o-/de .9;dera/'Jtfu.uzko-n Jtf~crat"io-n.

May 28, 1996 Acting Manager, Seattle Aircraft Certification Office June 19, 1998 (Signature) (Title) Any alteration ofthis certificate is punishable by a fine ofnot exceeding $1,000, or imprisonment not exceeding 3 years, or both.

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 · 7

MakeModelData sheet
Twin Commander Aircraft Corporation5006A1
Twin Commander Aircraft Corporation500-A6A1
Twin Commander Aircraft Corporation500-B6A1
Twin Commander Aircraft Corporation500-S6A1
Twin Commander Aircraft Corporation500-U6A1
Twin Commander Aircraft Corporation560-A6A1
Twin Commander Aircraft Corporation560-E6A1