# STC SA3810SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Installation of Precise Pulselite control unit Model 2400-25-4-4.
- Applied: May 27, 1987
- Status date: January 23, 2017
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A3EU](https://openairdocs.org/tcds/A3EU)
- Certificate PDF: https://openairdocs.org/files/sha256/3d/3e/3d3ebeffa8ac0a1d24f1ab4c3032ed19b21302a30e72957fb67560179be98446
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CE5CD50B32B5B3C2862581590050E7BD.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3810SW

## ADs that name it (0)

None.

## Approved models (4)

- Beechcraft Corporation BAe.125 Series 800A ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))
- Beechcraft Corporation Hawker 800 ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))
- Beechcraft Corporation Hawker 800XP ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))
- Beechcraft Corporation Hawker 850XP ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))

## 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.

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 3 SA3810SW-D Civil Air Regulations.

4b The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

Hawker Beechcraft Corporation BAe. 125 Series 800A; Hawker 800; Hawker 800XP; Hawker 850XP; Hawker 900XP All installations Except -103 Installation:

Models: BAe.125 Series 800A; Hawker 800; Hawker 800XP; Hawker 850XP Installation of Precise Pulselite Control Unit Model 2400-25-4-4 in accordance with Drawing List No. 800-048 Rev. F dated May 5, 1989 or later FAA approved revision. FAA approved Airplane Flight Manual Supplement dated 6/30/87, or Revision A dated 2/24/89, or Revision B dated 6/2/89, or later FAA approved revision is required.

(see continuation sheet 3 of 3) November 19, 2001; May 9, 2007;

October 19, 2007; January 23, 2017 February 24, 1989; June 2, 1989; November 18, 2002; June 29; 2006; September 13, 2007 May 27, 1987 June 30, 1987 A3EU Mark Fuller STC ODA administrator ODA-100129-CE

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

To (Name and address of transferee)

From (Name and address of grantor)

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

Date of Issuance: June 30, 1987 Date Amended: September 13, 2007 Date Reissued: January 23, 2017

Description of Type Design Change (continued):

-103 Installation Only:

Model: Hawker 800XP; Hawker 850XP; Hawker 900XP Installation of a Precise Pulselite Control Unit in accordance with STC Master Drawing List No. 800-048 (-103), Rev. X, dated 10/29/02, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement 800-231, Rev. 10, dated 9/13/07, or later FAA approved revision is required.

-- END -- SA3810SW-D 3

## Every issue (3)

- January 23, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3d/3e/3d3ebeffa8ac0a1d24f1ab4c3032ed19b21302a30e72957fb67560179be98446)
- May 9, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/84/a6/84a6578a2f791d586ecbf8ca874dc605cf2189fa936a7c9b08473d118c657079)
- June 29, 2006: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/75/52/755223e0e31ba77f8141d9aacd49b4c00671c9388bddd96b6a4ee7873bfaaede)

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