# STC SA5871SW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Clark Engineering Service
- Description: 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.
- Status date: January 26, 1985
- Data sheets: 4A26
- Certificate PDF: https://openairdocs.org/files/sha256/cb/c9/cbc9015af586d34f8d0c078e389dc7056b06b5ad0327785b9e3b088665c1af9c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3EDA05EAA0DC2C1785256CC200122C18.0001
- Page: https://openairdocs.org/stc/SA5871SW

## ADs that name it

None.

## Approved models (1)

- The Boeing Company 707-300B (TCDS 4A26)

## 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.

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

## Every issue (1)

- January 26, 1985: Issued, Current. [certificate](https://openairdocs.org/files/sha256/cb/c9/cbc9015af586d34f8d0c078e389dc7056b06b5ad0327785b9e3b088665c1af9c)

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