STC SA5703SW

Supplemental type certificate · Clark Engineering Service

Holder
Clark Engineering Service · United States
Status
Current · Amended
Status date
September 19, 1984
Applied
September 12, 1983
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21
Data sheet
TCDSA21EA

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

What it approves

Installation of avionics systems.

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.

ttnttrd Starts of amtrica ©epartmcnt of Transportation federal Situation Administration Supplemental 'Cgpe Certificate

• -/l&a4dix f-Jrtainat iJ&ociitcf —— • SAE705SW dark Engineering Service 312 E. Main Street Lancaster, Texas 75146 Project T6399SW-DS JWW-190 ,^^ ^5 ^./nv Federdl Aviation Ac! LA : Canadalr CL-600-1A11/-2A12 '—f^e^ua^i' ~Sia'na4' :

InstallRtion of Avionics Systems 1n accordance with dark Engineering Data List DL-840418 dated 4/18/84, Revised 8/20/84, or later FAA approved revision.

See Continuation Sheet, page 2, of this STC.

Je*<iri*M^^ September 12, 1983 May 7, 1984 AW?

9/19/84 Revision 1 WatSOn (S-fnature) lanager, Aircraft Certification Division outhwest Region (Title)

FAA tout 8110-2 (10-68)

tinitrd $tatu of amcrira Bcpartmcnt of Importation— federal atriation administration Supplemental tigpe Certificate(Continuation £heet) SA5703SW Revision 1 Limitations and conditions:

1. FAA Approved Airplane Flight Manual Supplement dated May 7, 1984, is required for the Dual UNS-1 Integrated Flight Management/NavigationSystem.

2. FAA Approved Airplane Flight Manual Supplement dated August 24, 1984, is required for the Carousel Six Inertial Navigation System.

3. FAA Approved Airplane Flight Manual Supplement dated August 24, 1984, is required for the Global GNS-500A Series 3 VLF/Omega Navigation System.

4. FAA Approved Airplane Flight Manual Supplement dated August 24, 1984, is required for the Sperry VA-100 Voice Advisory System.

5. Compatibility of this modification with other previously approved modifications must be determined by the installer.

.•Iff) iil/fru/ion of this certificate is punishable by a fine oj not exceeding S],000, or imprisonment not exceeding 3 years, or both ' AA FORM 8110-2-1 (1O-69) This certificate may be transferred in accordance with i'AR -1.-I7 PAGE 2OF 2PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (A ddress of transferee) (Number and street) (City, State, and <?/> code) from (Name of grantor) (Print or type) (Address of grantor) (Number and 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.

No AD in this release names this STC

Approved models · 2

MakeModelData sheet
Bombardier Inc.CL-600-1A11 (CL-600)A21EA
Bombardier Inc.CL-600-2A12 (CL-601)A21EA