STC SE00026EN

Supplemental type certificate · Pratt & Whitney Engine Services Inc.

Holder
Pratt & Whitney Engine Services Inc. · United States
Status
Current · Reissued
Status date
October 22, 2007
Applied
December 7, 1998
Product
Engine
Certification basis
Part 33
Data sheet
TCDSE1GL

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

What it approves

Installation of Pratt & Whitney Engine Services Inc. IntelliStart Plus Electronic Control Unit (ECU), P/N DPU-K-010 on specified 250 engine models.

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: SE00026EN This certificate issued to: Pratt & Whitney Engines Services, Inc.

249 Vanderbilt Ave.

Norwood, MA 02062 Part 33 of the Federal Aviation Regulations.

Original Product Type Certificate Number : E1GL Make: Rolls Royce Allison Engine Company (Formerly Allison Engine) Model: 250-C28, 250-C28B, 250-C28C, 250-C30, 250- C3OS, 250-C30P, 250-C30M, 250-C30L, 250-C30R, 250-C30G, 250-C30U, 250-C30G/2, and 250-C30R/1 Description of Type Design Change: Installation of Prant & Whitney Lingine Services, Inc. Intellistart Plus +T Hectronic Control Unit (ECU), P/N DPU-K-010 on the specified 250 engine models. Airframe installation of the Mtair Avionies Corporation - AlliedSignal Aerospace Intellitart Plus + TM to be accomplished in accordance with applicable airframe STC.

Limitations and Conditions: 1) The IntelliStart Plus 'T FCU is designed to limit start temperatures and to provide an electronic aid for recording engine trend and cycle data. 2) The Intellistart Plus *TM ECT is designed as non-essential, ground use only equipment and cannot be used to replace pilot monitoring during start as required by FAN approved operating instructions for the aircraft.

This system does not climate any Rotocraft Flight Manual monitoring requirements or limitations during engine starts or the requirement for manual recording of engine operating data required by the FAN approved operating specifications or maintenance programs. 3) This approval shall not be incorporated in any engines of these models on which other previously approved modifications are incorporated, unless it is determined that the inter-relationship between this change and any previously approved modification will introduce no adverse effect upon the airworthiness of those aircraft. 4) 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 Reissued: . August 21, 2002, October 22, 2007 Date of Application: December 07, 1998 Date of Issuance: January 19, 2000 Date Amended: .

By Direction of the Administrator FEDERAL AVIATION (Signature) Diane M. Cook Manager, Engine Certification Branch TOMINSTRATO Aircraft Certification Office (Title) Any alteration of FAA Form

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 · 12

MakeModelData sheet
Rolls-Royce Corporation250-C28E1GL
Rolls-Royce Corporation250-C28BE1GL
Rolls-Royce Corporation250-C28CE1GL
Rolls-Royce Corporation250-C30E1GL
Rolls-Royce Corporation250-C30GE1GL
Rolls-Royce Corporation250-C30G/2E1GL
Rolls-Royce Corporation250-C30ME1GL
Rolls-Royce Corporation250-C30PE1GL
Rolls-Royce Corporation250-C30R (T703-AD-700)E1GL
Rolls-Royce Corporation250-C30R/1 (T703-AD-700B)E1GL
Rolls-Royce Corporation250-C30SE1GL
Rolls-Royce Corporation250-C30UE1GL