STC SR09930AC

Supplemental type certificate · Aero-Seats and Systems Inc

Holder
Aero-Seats and Systems Inc · United States
Status
Current · Issued
Status date
September 21, 2022
Applied
May 11, 2020
Product
Aircraft · Rotorcraft
Certification basis
Part 21, Part 29
Data sheet
TCDSH4EU

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation Rear-View Mirror

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

29 Federal Aviation Regulations SR09930AC Aero Seats and Systems, Inc.

340 Thomas Place, Everman, Texas 76140 H4EU Airbus Helicopters AS332C, AS332C1, AS332L, AS332L1, and EC225LP Description of Type Design Change:

Installation of the Aero Seats and Systems, Inc. ASI-225-M2 Rear-View Mirror in accordance with Master Drawing List (MDL) document number ASI-225M2-MDL-001 Rev B, dated August 05, 2020, or later FAA approved revision. Rotorcraft Flight Manual Supplement (RFMS) ASI-225M2-FMS-001 Rev XX, dated September 14, 2022, or later FAA approved revision is required. Instructions for Continued Airworthiness, ASI-225M2-ICA-001, Rev IR, dated August 10, 2020, or later FAA accepted revision is required to be made available at installation.

1. The ASI-225-M2 Rear-View Mirror requires prior installation of the mounting provisions for the Airbus P/N:

332A84-1222 Forward Floats, however, the ASI-225-M2 installation is not compatible with the Airbus Float Installation.

(continued on 3 of 3 pages)

September 21, 2022 May 11, 2020 3 S. Frances Cox, Acting Manager Compliance & Airworthiness Division Aircraft Certification Service

SR09930AC 3

FAA Form 8110-2 (03/21) Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR09930AC 3 3 ---------------------------------------------------------------------------------END-------------------------------------------------------------------------------- Limitations and Conditions:

2. The installer must determine whether this design change is compatible with previously approved modifications.

3. 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.

Certification Basis:

The modification certification basis for parts changed or affected by the change is based upon Part 29 as amended by Amendment 29-47 as follows:

Regulations at the latest amendment 29-0 through 29-47

29.1, 29.65, 29.67, 29.141, 29.171, 29.251, 29.301, 29.303, 29.305(a)(b)(1), 29.307(a),

29.337(a), 29.601, 29.603, 29.605(a), 29.609(a), 29.611(a)(b), 29.613(a)(b)(c)(d), 29.619,

29.623, 29.625(a)(b)(c), 29.1301(d), 29.1501, 29.1503(a), 29.1505(a)(c), 29.1529, 29.1581(a)

(b)(d), 29.1585(a), Appendix A: A29.1, A29.2, A29.3, and Appendix B: B29.4, B29.6.

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 5

MakeModelData sheet
Airbus HelicoptersAS332CH4EU
Airbus HelicoptersAS332C1H4EU
Airbus HelicoptersAS332LH4EU
Airbus HelicoptersAS332L1H4EU
Airbus HelicoptersEC225LPH4EU