What it approves
Installation of Collins FCS-80 flight control system with ADS-80 air data system and ALT-50 or ALT-55 altimeter.
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 grata of amrrica Bcpartmcnr of Transportation federal Stoiation administration >upplemcntal 'Cjp Certificate SA2777SW Proj tfo. 190-343 CRW - 191 £ari Falcon Jet Corporation P. O. Box 967 Little itock, Arkansas 72203 c/ir,,,,,, -in f'/yfif't6tAiat:S'-i- /n • tfwitirj /ifif i>?i>.'tnft& //if 'iiri>frf/i>'nfJM.;rty.m'ffr>,<**& A33EU Dassault-Breguet Faloon 10
- 'Wa af/.
25 ,J t/ii Federal Aviation Installation of Collins PCS-80 Flight Control System with ADS-80 Air Data System and ALT-50 or ALT-55 Altimeter in accordance with Falcon Report No. 27034, Revision AE, dated 6-17-86, or later FAA approved revision.
Continuation Sheet, page 2 of this STC.
iM/rfafa^j>th^ i?it3 SKI// july 19, 1977 7, 1978 8/3/78; 3/27/80; 10/29/80;
3/5/81; 12/28/81; 8/30/83; 6/12/86 Revision 7 Don P. WatSOn (Xignatmr) Manager, Aircraft Certification Division Southwest Region (Title) Any alteiglion of this certificate i"j punishable by a fine of not exceeding 57,000, or imprisonment not exceeding 3years, or bulk.
This certificate may be tramfund in accordant! with FAR 21.17.
FAAFot. Bt 10-2 (10-66)
IHnittd gtatu of SLmmra Bepartmtnt of "Cransportation -.federal atriation administration Supplemental lEuje Certificate,™ .. t, fy. „. Proj. No. 190-343 (Continuation £heet) SA2777SW Revision 7 Limitations and Conditions:
1. The following FAA Approved Airplane Flight Manual Supplements are required:
a. Supplement dated May 17, 1978, revised August 3, 1978, is required for aircraft modified according to Report 27034, Rev. K.
b. Supplement dated March 5, 1980, is required for aircraft modified according to Report 27034, Rev. S.
c. Supplement dated October 29, 1980, is required fcr aircraft modified according to Report 27034, Rev. V.
d. Supplement dated December 28, 1981, FJC Report 35168 Rev. D is required for aircraft modified according to Report 27034, Rev. X dated November 2, 1981.
e. Supplement dated August 30, 1983, FJC Report 35168 Rev. E is required for aircraft modified according to Report 27034, Rov. Z dated August 24, 1983.
f . Supplement dated November 30, 1984, FJC Report 35168 Rev, F is required for aircraft modified according to Report 27034, Rev. Z dated August 24, 1983.
g. Supplement dated June 12, 1986, FJC Report 35168 Rev. G is required for aircraft modified according to Report 27034 Rev. AE dated June 17, 1986.
2 . Compatibility of this modification with other previously approved modifications must be determined by the installer.
'd altriittuin of ifiis (trlifictilt is pumthabie by a fine of not exceeding Si,WO, or imfiritonmfttl mil etcrcdins, .3 years, f" hnlh.
A A. FORM ai lo-z-1 OO-S9) Tfiit etrttJKott may be tiantjtrud in accordanfi it-itlt i'AK .'I 1~
PAGE OF PAGES
Tha FAA will reissue the certificate in the nama of the transferee and forward it to him.
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP codej from (Name of grantor)(Print or type) (Address of grantor) (Number £ street) (City, State, and ZIP 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 |
|---|---|---|
| Dassault Aviation | Falcon 10 | A33EU |