STC SE00768LA

Supplemental type certificate · Aero-Engines Inc.

Holder
Aero-Engines Inc. · United States
Status
Current · Amended
Status date
March 23, 1999
Applied
December 21, 1998
Product
Engine
Data sheet
TCDS5E-2

From FAA DRS, with our copy of the certificate PDF. DRS record last changed September 3, 2026.

What it approves

Installation of the AN4100 or AN4101 fuel pump on above mentioned series reciprocating engine model.

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: SE00768LA This certificate issued to: AERO-ENGINES-INC.

3033 NORTH COOLIDGE AVENUE LOS ANGELES, CALIFORNIA 90039 Part 13 of the Civil Air Requlations.

Original Product Type Certificate Number: 5E-2 Make: Pratt & Whitney Model: R-1340 Series Description of Type Design Change: Installation of the AN4100 or AN4101 fuel pump on Pratt & Whitney R-1340 series reciprocating engine mödel must be in accordance with FAA approved Aero-Engines-Inc.'s Master Drawing List No. 1000, Rev. N/C, dated February 23, 1999, or later FAA approved revisions. This STC establishes the eligibility of the R-1340 series engine for operation with the AN4100 or AN4101 fuel pump in accordance with the engine operating limitations specified.

Limitations and Conditions: This approval should not be extended to other specific engines of these models on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of that engine. This approval covers engine fuel pump compatibility only, and a separate FAA approval is required for the installation on an aircraft. A copy of this STC must be included in the permanent records of the modified engine. 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 (Cont. Page 3).

Date of Application: December 21, 1998 Date Reissued:

Date of Issuance: February 24, 1999 Date Amended: March 23, 1999 FEDERAL AVIATION By Direction of the Administrator , (Signature) TOMINSTRATO Manager, Propulsion Branch Los Angeles Aircraft Certification Office (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE00768LA Limitations and Conditions: Continued:

Fuel Pressure Limits - normal operation Make: 6 psi Min: 3 psi -END-

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 · 1

MakeModelData sheet
Pratt & Whitney DivisionR-1340 Series5E-2

Every issue · 2

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

DateStatusFiles
March 23, 1999Amended, currentCertificate
March 23, 1999Amended, earlier issueCertificate