STC SR00113BO

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
September 20, 1998
Product
Aircraft · Rotorcraft
Certification basis
Part 21, Part 27
Data sheet
TCDSH2SW

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

What it approves

Installation of a Pratt & Whitney Engine Services, Inc. AlliedSignal Aerospace IntelliStart Plus+ Electronic Control System P/N DPU-K-010.

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.

249 Vanderbilt Ave.

Norwood, MA 02062

Part 6, 21, 27 of the Civil Air/Fed Aviation Regulations.

Original Product Type Certificate Number : Bell Helicopter Textron (Canada) Make : 206 Series

Model : See Attached Eligibility List Dated January 20, 2000

Installation of a Pratt & Whitney Engine Services, Inc. – AlliedSignal Aerospace IntelliStart Plus +™ Electronic Control System P/N DPU-K-010 in accordance with Pratt & Whitney Engine Services, Inc. – AlliedSignal Aerospace Installation Manual, DPU-I-010-2, Revision E, dated January 14, 2000, or later FAA-approved revisions.

1. Aircraft must have engine modifications as shown on the Eligibility List.

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 20, 1998

Date of issuance : January 20, 2000 Date reissued : August 15, 2002, October 22, 2007

( Signature) Robert G. Mann Manager, Boston Aircraft Certification Office

( Title)

FAA Form 8110-2-1(10-69) Page 2 of 2

Number SR00113BO Limitations and Conditions (Cont’d):

2. Compatibility of this design change with previously approved modifications must be determined by the installer.

3. Pratt & Whitney Engine Services, Inc. Rotorcraft Flight Manual DPU-T-250-1 dated January 20, 2000, or later FAA-approved revision, is required.

4. This system is designed as an electronic aid for engine “hot start” prevention and for recording engine trend and cycle data.

This system does not eliminate any rotorcraft Flight Manual monitoring requirements or limitations during engine starts or the requirement for manual recording of engine operating data required by the FAA-approved operating specifications and maintenance programs.

Eligibility List January 20, 2000

Model TC Engine STC Required

206A H2SW SE00027EN 206A-1 H2SW SE00027EN 206B H2SW SE00027EN 206L H2SW SE00027EN 206L-1 H2SW SE00026EN 206L-3 H2SW SE00026EN 206L-4 H2SW SE00026EN

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 · 7

MakeModelData sheet
Bell Helicopter Textron (Canada)206AH2SW
Bell Helicopter Textron (Canada)206A-1 (OH-58A)H2SW
Bell Helicopter Textron (Canada)206BH2SW
Bell Helicopter Textron (Canada)206LH2SW
Bell Helicopter Textron (Canada)206L-1H2SW
Bell Helicopter Textron (Canada)206L-3H2SW
Bell Helicopter Textron (Canada)206L-4H2SW