What it approves
Installation of dual Global GNS-1000 flight management system with dual Honeywell 1779A inertial reference systems and NDB-2 navigation data bank, Collins FDS-80 dual flight director system, Collins EFIS-86A-1 electronic flight instrument system with Collins WXR-300 weather radar, dual ADS-80K air data system, standby airspeed and altimeter, and standby power system.
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.
Httitri States of America Bepartmcnt of ^transportation —federal 2toiation administration Supplemental 'Cgpe Certificate SA5871SW Project T6729SW-DS JWW-190 clark Engineering Service 312 E. Main Street Lancaster, Texas 75146 (fe *^J&e> Civil Air t .'uaMta-tU'-nA .
£Jf*a*rLa* <Jtrvcu6C/ —— •^u/if^'^e^^tfM^e'^/Yu^neer- 4A26 Boeing 707-300B ^be&c*<A£&n. jx*ls/u/w~l ^e&tan- 'Gi/ui&i&e' :
Installation of Dual Global GNS-1000 Flight Management System with Dual Honeywell 1779A Inertlal Reference Systems and NDB-2 Navigation Data Bank, Collins FDS-80 Dual Flight Director System, Collins EFIS-86A-1 Electronic Flight Instrument System with Collins WXR-300 Weather Radar, Dual ADS-80K Air Data System, Standby Airspeed and Altimeter, and Standby Power System in accordance with Clark Engineering Service Report No. DL-840531 dated 1/21/85, or later FAA approved revision.
See Continuation Sheet 2 of this STC.
Compatibility of this modification with other previously approved modifications must be determined by the installer.
•CW^^J£n^^H2^iMk/<^?^sGfyfl?t&^^ May 31, 1984 January 26, 1985 Don P. WatSOn (Stgnat^e) Manager, Aircraft Certification Division Southwest Region (Title) ___
FAA Fowt S110-2 (10-68)
ttnitrd Starts of amcrira Bepartment of transportation— federal Sttriation administration Supplemental t:j)pe Certificate(Continuation £heet) SA5871SW Limitations and Conditions:
The following FAA Approved Airplane Flight Manual Supplements are required:
1. Dual Global GNS-1000 Flight Management System with Dual Honeywell 1779A Inertial Reference Systems and NDB-2 Navigation Data Bank dated January 26, 1985.
2. Collins FDS-80 Dual Flight Director System dated January 26, 1985.
3. Collins EFIS-86A-1 Electronic Flight Instrument System with Collins WXR-300 Weather Radar dated January 26, 1985.
4. Dual ADS-80K Air Data System dated January 26, 1985.
5. Standby Airspeed and Altimeter dated January 26, 1985.
6. Standby Power System dated January 26, 1985.
.If/! alteration of this certificate is punishable by a fine of not exceeding SI,000, or imprisonment not exceeding 3 years, or both.
I-AA F-ORM aiio-2-i (1O-69) This certificate may be transferred in accordance with l-'AR 21.17 PAGE 2OF 2PAGES
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee).
(Address of transferee). (Mumhtr md Oral) (City. Stall. *ixf from (Name of grantor) (Print or type).
(Address of grantor) (Citf, Suit, utd^lF ndtt Extent of Authority (if licensing agreement):
Signature of grantor (In ink):
A ii < r. o n i«««-««»-n«o
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 |
|---|---|---|
| The Boeing Company | 707-300B | 4A26 |