STC SA1033WE

Supplemental type certificate · United Airlines Inc

Holder
United Airlines Inc · United States
Status
Current · Reissued
Status date
November 30, 2011
Applied
October 25, 1965
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21
Data sheet
TCDS4A25

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

What it approves

Installation of either single or dual Collins AL-101 Radio Altimeter System(s) in accordance with FAA Approved United Air Lines Report Nos. F-1038 and No. F-1054.

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.

This Certificate issued to United Air Lines, Inc.

600 Jefferson Street Houston, Texas 77002 Part 4b of the Civil Air Regulations.

Original Product Type Certificate Number : 4A25 Make: Boeing Model: DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-51, DC-8-52, DC-8-53, DC-8F-54, DC-8-55 Description of Type Design Change: Installation of either single or dual Collins AL-101 Radio Altimeter System(s) in accordance with FAA Approved United Air Lines Report Nos. F-1038 and No. F-1054.

Limitations and Conditions : This approval should not be extended to ot her aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. The DC-8-51, -52, -53, DC-8F-54, and DC-8F-55 aircra ft which have the Douglas wiring & installation provisions for the dual Sperry radio a ltimeter system only. The approval of this change in type design is in accordance with UAL Report F-1054 and applies basically to the DC-8-51, -52, -53, -21, -31, -33, DC-8F-54 & DC-8F-55 which do not have previous altimeter system wiring. A copy of this STC must be included in the permanent records of the modified aircraft. 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.

Date of application : October 25, 1965

Date of issuance : August 19, 1965

Date reissued : November 30, 2011

Date amended : September 14, 1965; October 13, 1965;

August 9, 1966; October 31, 1975; November 19, 1975

( Signature) Haifa Haj-Eid Supervisor, Technical & Administrative Support Staff Los Angeles Aircraft Certification Office ( Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP Code)

from (Name of grantor) (Print or type)

(Address of grantor) (Number and street)

(City, State, and ZIP Code)

Signature of grantor (In ink):

U.S. GPO 1987-763-28

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 · 9

MakeModelData sheet
The Boeing CompanyDC-8-214A25
The Boeing CompanyDC-8-314A25
The Boeing CompanyDC-8-324A25
The Boeing CompanyDC-8-334A25
The Boeing CompanyDC-8-514A25
The Boeing CompanyDC-8-524A25
The Boeing CompanyDC-8-534A25
The Boeing CompanyDC-8-554A25
The Boeing CompanyDC-8F-544A25