What it approves
Installation of Dual Universal Nav UNS-1 Integrated Flight Management/Navigation System with Triple Honeywell LASEREF IRS Sensors Model HG1075AB02, Dual Sperry Electronic Flight Instrument System, Sundstrand Data Control Mark II Ground Proximity Warning System, Dual Sperry AZ800 Digital Air Data Computer with Single VW-801 VNAV Controller, Canadian Marconi CMA-776 Status Display System, Category II Operations, and a Dual HF Beckar System HF-3800-11 and Audio VCS-221
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 $tates of america ©epartment of transportation— Jpederal atoiation administration Supplemental t^pe Certificate SA3502SW P/N 190-9001 OWW-192 dark Engineering Service 312 E. Main Street Lancaster, Texas 75146 <^^ 25 ^'.3&& Federal Aviation A21EA CL-600-1A11/-2A12 Universal Nav ONS-1 Integrated Flight Managenent/Navigatjbon System with Triple Honeywell IASEREF IPS Sensors Model B31075AB02, Dual Sperry Electronic Flight Instruraent Systam, Sundstrand Data Control Mark II Ground Proximity Warning System, Dual Sperry AZ800 Digital Air Data Ocoiwter with Single VW-801 VNAV Controller, Canadian Marconi GMA-776 Status Display System, Category II Operations, and a Dual HF Bedcer System HF-3800-11 and Audio VCS-221 in acoordance with dark Engineering Data List DL-850723, Ravisixxi C dated January 15, 1988, or later FAA approved revision.
See OOTtinuation sheet, page 2 of this STC.
Goniatibility of this raadif ication with other previously approved modifications must be ftet^r^lny' by the installer.
,^^^.de4^ S^^n^/ntti 12, 1983 September 27, 1985 ^^^^^^ 1/21/86, 10/16/86, 1/15/88 L. B. anarieaen—r%na/ur,,—————————Manager, Aircraft Certification Division Southwest Region (Title)
FAAFo«M8110-2(10-68)
tinted $tatu of amenta Bepartmcnt of transportation— federal atriation administration Supplemental t^pe Certificate(Continuation £heet) SA3502SW Revision 3 Limitations and Conditions;
The following FAA Approved Airplane Flight Manual Supplements are required:
1. Supplement AFMS 850820 dated September 27, 1985, Revision A dated January 21, 1986, is required for Dual Universal Nav UNS-1 Integrated Flight Management/Navigation Syfetem with Triple Honeywell LASEREF IPS Sensors Model HG1075AB02.
2. Supplement AFMS 850821 dated September 27, 1985, ftsvision A dated January 21, 1986, is required for Sperry Electronic Flight Instrument System.
3. Supplement AFMS 850822ddfcted September 27, 1985, is required for Sundstrand Data Control Mark II Ground Proximity Warning System.
4. Supplement AFMS 850824 dated September 27, 1985, is required for Dual Sperry AZ800 Digital Air Data Computer "with Single VN-801 VNAV Controller.
5. Supplement AFMS 850825 dated September 27, 1985, is required for Canadian Marconi CMA.-776 Status Display System.
6. Supplement AFMS 850823 dated September 27, 1985, is required for Category II Operations.
alteration nf this certificate is punishable by a fine of not exceeding SI,000, or imprisonment not exceeding 3 years, or both.
FORM aiio-2-i (10-69) This certificate may be transferred in accordance with 1'AK I.'/.-/.7 PAGE 2 OF2 PAGES
be used to notify the appropriate FAA Regional Office ofINSTRUCTIONS: The transfer endortement below may the transfer of thi* Supplemental Type Certificate.
The FAA will reiuue the certificate in the name 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). (.\umttr *nt stntlj from (Name of grantor) (Print or type).
(Address of grantor) __ (Cify, Extent of Authority (if licensing agreement):
Signature of grantor (In ink):
4V it « r. o n ««««-««»-n»°
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