# STC SR00780LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Apical Industries Inc. dba Dart Aerospace, United States
- Description: Installation of Apical Emergency Float Kit, P/N 20498.
- Applied: September 3, 1998
- Status date: August 19, 2014
- Product: Aircraft, Rotorcraft
- Certification basis: Part 29
- Data sheets: [TCDS R0001RD](https://openairdocs.org/tcds/R0001RD)
- Certificate PDF: https://openairdocs.org/files/sha256/b9/1b/b91b54db09b9352d4c77a39cceb78787c060d801cf99bce6e64837b9d4ec0ab6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140375663620240202192430.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR00780LA

## ADs that name it (1)

- [AD 2024-20-07](https://openairdocs.org/ad/2024-20-07): Emergency Equipment; Emergency Flotation Section · Apical Emergency Float Kit, P/N 20498 (STC SR00780LA or 12 others). Effective Dec 5, 2024. Named in the applicability

## Approved models (1)

- Airbus Helicopters EC120B ([TCDS R0001RD](https://openairdocs.org/tcds/R0001RD))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SRO0780LA This certificate issued to:

Apical Industries, Inc. dba Dart Aerospace 3030 Enterprise Court, Suite A Vista, CA 92081 Part 27* of the Federal Brialion Requlutions.

*Certification basis is set forth in Type Certificate Data Sheet.

Original Product Type Certificate Nuntier: R0001RD Make: Airbus Helicopters Model: EC120B Description of Type Design Change: Installation of Apical Emergency Float Kit, Part Number 20498, in accordance with FAA approved Apical Industries, Inc., Master Document List MD120-1, Revision D, dated March 18, 1999, or later FAA approved revision. FAA approved Apical Industries, Inc. Rotorcraft Flight Manual Supplement FMS-120(1), Revision N/C, dated March 19, 1999, or later FAA approved revision is Limitations and Conditions: This approval requires the inspections and overhaul schedules to be performed as mandated by the Instructions for Continued Airworthiness, ICA120-1, Revision N/C, dated January 21, 1999, or later FAA approved revision. This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. 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.

suspended, reucked or a termination date is otherwise established by the Administrater of the Federal Aviation Administration Lute of appliculion: September 3, 1998 Jule reissued: August 19, 2014 Date of Issuance: March 19, 1999 Date Amended:

FEDERAL AVIATION By divotion of the Anderinistenten a (Signature) Supervisor, Technical & Administrative Support Staff TOMINISTRATO Los Angeles Aircraft Certification Office (Title)

## Every issue (1)

- August 19, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/b9/1b/b91b54db09b9352d4c77a39cceb78787c060d801cf99bce6e64837b9d4ec0ab6)

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