What it approves
Installation of Bendix/King EHI 40 electronic horizontal situation indicator 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.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)
Number: SA2318CE-D This certificate issued to: Honeywell International Inc.
21111N 19th Ave Phoenix, Arizona 85027 Part 3 of the Civil Air Regulations Original Product – Type Certificate Number: Make: Mooney Model:
2A3 M20L, M20M
Installation of Bendix/King EHI 40 Electronic Horizontal Situation Indicator System.
REQUIRED DATA: 1. Master Drawing List 155-09559-0000, Rev. 1, dated 9-15-89and 2. Airplane Flight Manual Supplement 006-00495-0000dated 1-17-90or later FAA approved revision to 1 or 2.
This approval included and evaluation and finding of acceptance of the interface between the Bendix/King EHI 40 Electronic Horizontal Situation Indicator System, the Bendix/King KFC150 Automatic Flight Control System (SA2074CE-D & SA2319CE-D) and the Bendix/King KLN 88 Loran System (SA2320CE-D).
Date of Application: 3-23-89 Date Reissued: 2-28-95; 2-28-00; 4-14-20
Date of Issuance: 1-17-90 Date Amended:
Signature
Title Richard B. Sleigh ODA Administrator, ODA-602216-NM
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)
To (Name and address of transferee)
From (Name and address of grantor)
FAA Form 8110-2 (5/14) Page 3 of 3
(Continuation Sheet) Number: SA2318CE-D
Certification Basis:
Additional requirementsasspecified on TCDS2A3 and this STC.
Limitationsand Conditions: (continued) This approval should not be extended to other specific airplanesof this model on which other previously approved modificationsare incorporated, unlessit isdetermined that the interrelationship between this change and any of those previously approved modificationswill introduce no adverse effect upon the airworthinessof that airplane.
If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
------------------------------------------------------------------------------------END--------------------------------------------------------------------------------
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.