# STC SR01397LA

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: California Shock/Truma Air Rescue (CALSTAR), United States
- Description: Installation of Honeywell (Lycoming) LTS 101-750C-1 engines to replace Honeywell (Lycoming) LTS 101-650C-2, -3, -3A engines in accordance with CALSTAR Master Drawing List No. CAL 101, Revision A, dated September 10, 2002, or later FAA approved revisions. FAA Approved Rotorcraft Flight Manual Supplement No. CAL 104, Revision N/C, dated October 25, 2002, or later FAA approved revision is required with this installation. (See Page 3)
- Applied: September 17, 2001
- Status date: October 28, 2002
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H9SW](https://openairdocs.org/tcds/H9SW)
- Certificate PDF: https://openairdocs.org/files/sha256/35/e5/35e5da288afb4fa94407223a44097de728d5f06b4fb2df03fc34f9c537855149
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1C8AAF0A91D5A9F686256E75004E6819.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01397LA

## ADs that name it (0)

None.

## Approved models (1)

- Bell Helicopter Textron (Canada) 222 ([TCDS H9SW](https://openairdocs.org/tcds/H9SW))

## 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.

This Certificate issued to California Shock/Trauma Air Rescue (CALSTAR) 20876 Corsair Boulevard, Suite B Hayward, California 94545

Part 29 of the Federal Aviation Regulations.

H9SW Bell Helicopter Textron Bell 222 Description of Type Design Change: Installation of Honeywell (Lycoming) LTS 101- 750C-1 engines to replace Honeywell (Lycoming) LTS 101-650C-2, -3, -3A engines in accordance with CALSTAR Master Drawing List No. CAL 101, Revi sion A, dated September 10, 2002, or later FAA approved revisions. FAA Approved Rotorcraft Fli ght Manual Supplement No. CAL 104, Revision N/C, dated October 25, 2002, or later FAA approved revision is required with this installation. (See Page 3)

Limitations and Conditions: Approval of this change in ty pe design applies to the above model rotorcraft only. This appr oval should not be extended to rotorc raft of this model on which other alterations are incorporated unless it is determined th at the relationship between this change and any of those other alterations will introduce no adverse e ffect upon the airworthiness of that rotorcraft.

Maintenance Manual Supplement CAL 103, dated Ma y 15, 2002, or later FAA accepted revision, is required with this installation. A copy of this STC must be included in the permanent records of the modified rotorcraft. 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.

Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (United States Of America Continuation Sheet)

Date ofapplication: September 17, 2001 Date of issuance : October 28, 2002

/s/ Eric Smith

( Signature) Manager, Propulsion Branch Los Angeles Aircraft Certification Office ( Title)

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (United States Of America Continuation Sheet)

Number SR01397LA

NOTE: Noise characteristics - This modification was determined not to increase the noise level and was not considered an “acoustical change” as defined in paragraph § 21.93(b), amendment 21- 73 of the Federal Aviation Regulations.

-END-

## Every issue (1)

- October 28, 2002: Issued, Current. [certificate](https://openairdocs.org/files/sha256/35/e5/35e5da288afb4fa94407223a44097de728d5f06b4fb2df03fc34f9c537855149)

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