# STC SR00113BO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Pratt & Whitney Engine Services Inc., United States
- Description: Installation of a Pratt & Whitney Engine Services, Inc.  AlliedSignal Aerospace IntelliStart Plus+  Electronic Control System P/N DPU-K-010.
- Applied: September 20, 1998
- Status date: October 22, 2007
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/76/b3/76b3e58f9e1f05f585c46e1bc4bff3fd7a89ac8c665a69e6e5d78220673081ee
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8FFC7FBC1E48F7968625738B007FADA7.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00113BO

## ADs that name it (0)

None.

## Approved models (7)

- Bell Helicopter Textron (Canada) 206A ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206A-1 (OH-58A) ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can 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

## Every issue (1)

- October 22, 2007: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/76/b3/76b3e58f9e1f05f585c46e1bc4bff3fd7a89ac8c665a69e6e5d78220673081ee)

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