# STC SH2541CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Install Bendix/King KAP 150H Flight Control System.
- Applied: August 4, 1987
- Status date: April 16, 2020
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/d2/fa/d2fa99c594af1660d7a516fbc0e3cc661fa91d73bdedd59aae587c97eda2af61
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2464496EFCF3B36586258614005A21BA.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SH2541CE

## ADs that name it (0)

None.

## Approved models (5)

- Bell Helicopter Textron (Canada) 206 ([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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)

Number: SH2541CE This certificate issued to: Honeywell International Inc.

21111N 19th Ave Phoenix, Arizona 85027 Part 6 of the Civil Air Regulationseffective 12-20-56.

Original Product – Type Certificate Number: Make: Bell Model:

H2SW 206, 206L, 206L-1, 206L-3 and 206L-4

Install Bendix/King KAP150H Flight Control System. DATA REQUIRED: (206B only) 1. Master Drawing List for KAP150H installation in Bell 206B, Document Number 155-9464-00, Rev. 2, dated 9-18-89stamped "FAA Approved". 2. FAA Approved KAP150H Flight Manual Supplement 206B dated 9-26-89or later FAA approved revisionsto 1 or 2.

Other Approved Modifications are:

1. Spectrolab Nightsun Model SX 16 Searchlight

2. Breeze-Eastern Corp. Helicopter Rescue Hoist P/N BL-16600-170(mounted on the left side)

3. Breeze Cargo Hook

Date of Application: 8-4-87 Date Reissued: 2-28-00; 4-16-20

Date of Issuance: 9-26-89 Date Amended:

3-6-92; 10-26-93; 11-12-93

Signature

Title Richard B. Sleigh ODA Administrator, ODA-602216-NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 3 of 3

(Continuation Sheet) Number: SH2541CE

Description of Type Design Change: (continued)

3. Master Drawing List for KAP150H Installation in Bell 206L, 206L-1, 206L-3 and 206L-4 Document Number 155-09629-0000, Rev. 2, dated 10-1-93, stamped "FAA Approved".

4. FAA Approved KAP150H Flight Manual Supplement for 206L, 206L-1, 206L-3 and 206L-4, Rev. 1, dated 10-26-93or later FAA approved revisionsto 3 or 4.

DATA REQUIRED: (206L, 206L-1, 206L-3 and 206L-4 only)

5. Master Drawing List for KAP150H Installation in Bell 206L, 206L-1, 206L-3 and 206L-4 Document Number 155-09629-0000, Rev. 2, dated 10-1-93, stamped "FAA Approved".

6. FAA Approved KAP150H Flight Manual Supplement for 206L, 206L-1, 206L-3 and 206L-4, Rev. 1, dated 10-26-93or later FAA approved revisionsto 5 or 6.

Limitationsand Conditions: (continued)

4. Use of either skids or wheels

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.

This approval should not be extended to other specific helicoptersof these models on which other previously approved modificationsare incorporated, unlessit isdetermined by the installer that the interrelationship between this change and any of those other previously approved modificationswill introduce no adverse effect upon the airworthinessof that helicopter.

------------------------------------------------------------------------------------END--------------------------------------------------------------------------------

## Every issue (3)

- April 16, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d2/fa/d2fa99c594af1660d7a516fbc0e3cc661fa91d73bdedd59aae587c97eda2af61)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/c8/58/c8582e8d6b341c07f4c098c04283e8aedd6f6b4247c429faf420fd752d731caf)
- November 12, 1993: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/95/52/9552937f60b600439c9a9c3804879e8e0839c1c796925b391491aaa15abfa54e)

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