What it approves
Installation of a Pratt & Whitney Engine Services, Inc. IntelliStart+ Electronic Control System and Engine Trend Monitor P/N DPU-K-010-14.
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 27 of the Federal Aviation Regulations.
Original Product Type Certificate Number : 4H12 Make : Schweizer Aircraft Corporation Model : 269D
Installation of a Pratt & Whitney Engine Services, Inc. IntelliStart+ Electronic Control System and Engine Trend Monitor P/N DPU- K-010-14 in accordance with Pratt & Whitney Engine Services, Inc. IntelliStart+ Installation Instructions DPU-I-010-6, Revision A, dated October 12, 2005, or later FAA-approved revision.
1. Engine must be modified in accordance with STC SE00027EN. Reference STC SE00027EN for any additional limitations applicable to the engine installation.
2. Pratt & Whitney Engine Services, Inc. Rotorcraft Flight Manual Supplement DPU-T-250-4, dated November 1, 2005 or later FAA-approved revision, is required and must be carried during all flights.
3. Pratt & Whitney Engine Services, Inc. Instructions for Continued Airworthiness DPU-T-260-6, dated November 1, 2005 or later FAA accepted revision, shall be made available to the operator at the time of installation.
(See Continuation Sheet 2 of 2) 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 : April 7, 2005
Date of issuance : November 1, 2005 Date reissued : 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 SR00220BO
Limitations and Conditions (Cont’d):
4. This system is designed as an electroni c 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 data as required by the FAA-approved operating specifications and maintenance programs.
5. Compatibility of this design change with previously appr oved modifications must be determined by the installer.
Certification Basis :
14 CFR Part 27: 27.1301, 27.1309, 27.1322, 27.1357, 27.1367, 27.1529, 27.1581
….END….
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Schweizer Aircraft Corporation | 269D | 4H12 |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| October 22, 2007 | Reissued, current | Certificate |
| November 1, 2005 | Issued, earlier issue | Certificate |