# STC SE00768LA - Type: Supplemental type certificate - Status: Current, Amended - Holder: Aero-Engines Inc., United States - Description: Installation of the AN4100 or AN4101 fuel pump on above mentioned series reciprocating engine model. - Applied: December 21, 1998 - Status date: March 23, 1999 - Product: Engine - Data sheets: TCDS 5E-2 - Certificate PDF: https://openairdocs.org/files/sha256/61/64/6164b106233c25e2bea616cacf3a5367cef45716c4fd2c171a24452ea063040f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132141999220260903154219.0001 - DRS record last changed: September 3, 2026 - Page: https://openairdocs.org/stc/SE00768LA ## ADs that name it (0) None. ## Approved models (1) - Pratt & Whitney Division R-1340 Series (TCDS 5E-2) ## What the certificate says 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- ## Every issue (2) - March 23, 1999: Amended, Current. [certificate](https://openairdocs.org/files/sha256/61/64/6164b106233c25e2bea616cacf3a5367cef45716c4fd2c171a24452ea063040f) - March 23, 1999: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/94/9a/949ae9a09fb9a779dad09bcb91a1c8eb98e65eb0d38f52c950f870fd1b0b0a33) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.