STC SA1041NE

Supplemental type certificate · ESL Incorporated

Holder
ESL Incorporated · United States
Status
Current · Reissued
Status date
September 28, 1993
Applied
September 9, 1992
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21
Data sheet
TCDSA20EA

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

What it approves

Installation of passenger cabin floor upgrade. (DHC-7-102 S/N 048, DHC-7-103 S/N 104)

What the certificate saysOCR

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America 8103 Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA104INE This certificate issued to: ESL Incorporated C/O Avtel Services, Inc.

1434 Flight Line, Building 58 Mojave, CA 93501-1666 Purt 25 of the Federal Aviation Regulations.

Original Product - Type bortificate Number: A20EA Маке: DeHavilland Model:

DHC-7-102, s/n 048 Description of Type Design Change: DHC-7-103, s/n 104 Installation of Passenger Cabin Floor Upgrade in accordance with Field Aviation Co. Inc., Drawing List No. 33667, Issue 2, dated October 19, 1992, or later approved revisions.

1. Field Aviation Co. Inc. Maintenance Manual Supplement, p/n FACi-6700-116, Rev. 2, DOT approved October 28, 1992, or later approved revisions, is required with this modification.

Date of Application: September 9, 1992 Jute missued: September 28, 1993 Date of Issuance: February 1, 1993 Date Amended:

FEDERAL AVIATION By Direction of the Administrator I. Brumen Irwin SiS Blumer TMINISTRAIO Manager, New York Aircraft Certifieptine, Office

47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA1041NE Date Reissued: February 1, 1993 Reissued: September 28, 1993 Limitations and Conditions: (Cont.):

2. This approval should not be incorporated in any aircraft of these specific models on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated approved modifications will not introduce any adverse effect upon the airworthiness of the aircraft.

- - -END- - - 47 PAGE 2 OF 2 PAGES

- 82-03578

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-Rotax GmbHDHC-7-102A20EA
Bombardier-Rotax GmbHDHC-7-103A20EA