# STC SH3890SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Apical Industries, Inc. dba Dart Aerospace
- Description: Installation of 155 gallon capacity external auxiliary fuel system on high skid landing gear configured helicopters or 140/145-gallon capacity external auxiliary fuel system on low skid landing gear configued helicopters.
- Status date: August 19, 2014
- Data sheets: H1SW, H1SW
- Certificate PDF: https://openairdocs.org/files/sha256/8f/ae/8fae3ab1bcfb3c6b26bc14cb42f54b22e1b07fc45c12467ee57cf752a8ffed32
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CC4C35F247D5AED886257D69006CE24C.0001
- Page: https://openairdocs.org/stc/SH3890SW

## ADs that name it

None.

## Approved models (2)

- Bell Helicopter Textron Inc. 205A (TCDS H1SW)
- Bell Helicopter Textron Inc. 205A-1 (TCDS H1SW)

## 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 APICAL INDUSTRIES, INC.

D/B/A DART AEROSPACE 3030 ENTERPRISE COURT, SUITE A VISTA, CALIFORNIA 92018 Part 7 of the Civil Air Regulations.

H1SW Bell Helicopter Textron, Inc.

205A, 205A-1, S/N 3301-33107 only Description of Type Design Change: Installation of 155 gallon capacity external auxiliary fuel system for high skid landing gear configured helicopters or 140/145 gallon capacity external auxiliary fuel system on low skid landing gear configured helicopters in accordanc e with ERA Drawing 41228-2000, Revision L, dated April 3, 1991, or later FAA approved revisions.

Limitations and Conditions: For high skid gear configured helicopters FAA Approved Rotorcraft Flight Manual (RFM) Supplement Revision 1, dated June 6, 1988, or later FAA approved revisions is required. For low skid gear configured helicopters, FAA Approved RFM Supplement dated August 20, 1991, and for 140 gallon auxiliary fuel system or RFM dated November 3, 1988, for 145 gallon auxiliary fuel system, or later FAA approved revision is required. 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 shall give the other person written evidence of that permission.

Date of application : May 5, 1987

Date of issuance : December 17, 1987

Date reissued : 12/28/88, 7/9/92, 5/20/05, 12/29/06, 8/19/14

Date amended : 11/3/88, 2/11/91, 8/28/91

(Signature) Supervisor, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office (Title)

NOTE:

**DO NOT DELETE THIS PAGE.**

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

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

Number

## Every issue (3)

- August 19, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/8f/ae/8fae3ab1bcfb3c6b26bc14cb42f54b22e1b07fc45c12467ee57cf752a8ffed32)
- December 29, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f2/89/f2893db1563fa795b10b781f4507e5b04ecf4148267ab3011bd61a4aeb1256cb)
- May 20, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f1/fa/f1faf69590eb749f5f33e767797c4e68c20bbdc04661e64052c4069f6a4841f4)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.