STC SA2064CE-D

Supplemental type certificate · Honeywell International Inc

Holder
Honeywell International Inc · United States
Status
Current · Reissued
Status date
March 24, 2020
Applied
March 24, 1986
Product
Aircraft · Small Airplane
Certification basis
Part 21, Part 23
Data sheet
TCDSA8SW

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

What it approves

Installation of Bendix 3 tube or 5 tube EFS-10 electronic flight instrument 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: SA2064CE-D This certificate issued to: Honeywell International Inc.

21111N 19th Ave Phoenix, Arizona 85027 Part 23of the Federal Aviation Regulations Original Product – Type Certificate Number: Make: Fairchid Model: SA227-AC, SA227-BC A8SW

Configurations A & B(Model SA227-AConly): Installation of Bendix 3 tube or 5 tube EFS10 Electronic Flight Instrument System.

REQUIRED DATA: 1. King Master Drawing List 155-9364-00Rev. 1 dated 11-17-86and 2a. Airplane Flight Manual Supplement 006-0450-00dated 1-15-87for the 3 tube EFS10 System or 2b. Airplane Flight Manual Supplement 006-0450-01dated 1-15-87for the 5 tube EFS10 System or later FAA approved revision to 1, 2a or 2b.

This approval included an evaluation of the interface between the Bendix EFS10 Electronic Flight Instrument System, the King KNS660 Flight Management System (SA2062CE-D) and the King KFC400 Automatic Flight Control System (SA2060CE-D).

Date of Application: 3-24-86 Date Reissued: 2-28-95; 2-28-00; 3-24-20

Date of Issuance: 1-15-87 Date Amended:

3-16-89; 7-6-90

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: SA2064CE-D

Description of Type Design Change: (continued) REQUIRED DATA:

Configuration C(Models SA227-ACand SA227-BC):

Installation of Bendix 4 tube EFS10 Electronic Flight Instrument System.

REQUIRED DATA: (3) King Master Drawing List 155-9541-00Rev. 3 dated 7-90 and (4) Airplane Flight Manual Supplement 006-0450-02Rev.2, dated 7-6-90 for or later FAA approved revision to (3) or (4).

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 other 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.

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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
Fairchild Aircraft CorporationSA227-AC (C-26A)A8SW
Fairchild Aircraft CorporationSA227-BC (C-26A)A8SW

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
March 24, 2020Reissued, currentCertificate
February 28, 2000Reissued, earlier issueCertificate