STC ST00182LA-D

Historical

Supplemental type certificate · Hollingsead International

Holder
Hollingsead International · United States
Status
Historical · Surrendered
Status date
June 23, 2009
Applied
September 17, 1997
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 25

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of provisions for avionics upgrade.

What the certificate saysOCR

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST00182LA-D Certificate This certificate issued to: Hollingsead International SURRENDERED 2226 Goodyear Avenue 6-23-09 Ventura, CA 93003 on _ Certifies that the change in the type design for the following product with the limitation's and condition's therefor as specified hereen meets the airworthiness requirement's of Part *25 of the *

•Federal Aviation Regulations. *Certification basis set forth in Type Certificate Data Sheet Original Product Type Certificate Number: A20WE Make Boeing Abodel 747-200B, -200F, -300 Series Description of Type Design Change: Installation in Provisions for Avionics Upgrade in accordance with Hollingsead Intl Master Data List 12041-01, Rev. C, dated November 18, 1997, or later FAA approved revision.

FAA Approved Flight Manual Supplement, Document No. 2852-AFM-1, Revision NC, dated March 29, 2006, or later FAA approved revision is required as part of this installation.

Limitations and Conditions: This installation is limited to aircraft with Maximum Gross Takeoff Weight of 832,692 Ibs. This installation has been determined not to increase the noise level and is not considered an "acoustical change" as defined in 14 CFR Part 21.93(b), Amdt.25-81. This approval should not be incorporated on any certificated product of this model on which other approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any of those previously approved modifications will not introduce any adverse effect upon the airworthiness of that aircraft. A copy of this STC must be included in the permanent record 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: September 17, 1997 Date Reissued: April 1, 1998, June 27, 2005 Date of Issuance: November 18, 1997 Date Amended: April 20, 2006 FEDERAL AVIATION By Direction of the Administrator Maklidantha TOMINISTRATIOR Project Manager, Systems and Equipment Branch (Signature) Los Angeles Aircraft Certification Office (Title)

TRANSFER ENDORSEMENT Transter the ownership of the Supplemental Type Certificate Number to (Name of transferee)_ (Address of transfer) (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) 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 · 5

MakeModelData sheet
The Boeing Company747-200 SeriesA20WE
The Boeing Company747-200B SeriesA20WE
The Boeing Company747-200F SeriesA20WE
The Boeing Company747-300 SeriesA20WE
The Boeing Company757-300 SeriesA2NM

Every issue · 4

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

DateStatusFiles
June 23, 2009Surrendered, earlier issueCertificate
April 20, 2006Reissued, earlier issueCertificate
April 20, 2006Amended, earlier issueCertificate
June 27, 2005Reissued, earlier issueCertificate