STC ST00016IB

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

IMPORT ST00016IB PMV Engineering 140 IMPASSE DE LISBONE 82000 MONTAUBAN FRANCE Part 25 Title 14 Code of Federal Regulations A53EU ATR – GIE Avions de Transport Régional ATR72-202, ATR72-212, ATR72-212A

1. Installation of Bulk Freighter Conversion (BFC), by Converting a passenger configuration into a full Class "E" cargo configuration, including floor reinforcements, cargo crash net, new lining, smoke detection system and other associated modifications for ATR72-202 and ATR72-212, in accordance with BCF Type Design Definition, Alenia Aeronautica document No. 54/NT/0000/N316C/040148, Issue 1, dated December 1, 2004 or later EASA approved revisions and for ATR72-212A, in accordance with ASI Innovation Data (See Description of Type Design Change Continued on Page 3 of 4)

1. The aircraft must be operated in accordance with the "Limitations" section of "Airplane Flight Manual Supplement" (AFM) for ATR72-202 and ATR72-212, Alenia Aeronautica document ATR72 Cargo BCF, (See Limitations and Conditions Continued on Page 3 of 4) January 29, 2021 July 12, 2021 Anthony E, Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 4

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

IMPORT ST00016IB 4

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

IMPORT ST00016IB Date of Issuance: July 12,2021

Description of Type Design Change (continued):

List ASI-SDL-0458-01, Revision 01, dated Dec. 5, 2016 or later EASA approved revisions.

2. PMV Engineering "Instructions for Continued Airworthiness", document ref.

P2F-00090-ICA-S02, Revision R00, dated February 23, 2021 or later EASA accepted revisions is required with this modification.

3. Airplane Flight Manual AFM Supplement for ATR72-202 and ATR72-212, Alenia Aeronautica document ATR72 Cargo BCF, Initial Issue, Revision 00, dated December 2004 or later EASA approved revisions and for ATR72-212A, ASI Innovation Document No. ASI‐AFM‐0458, issue 00, dated September 2016 or later EASA approved revisions, are required with this installation.

Initial Issue, Revision 00, dated December 2004 or later EASA approved revisions and for ATR72-212A, ASI Innovation Document No. ASI‐AFM‐0458, issue 00, dated September 2016 or later EASA approved revisions.

2. The EASA approved Airworthiness Limitations section of Instructions for Continued Airworthiness, PMV Engineering "Instructions for Continued Airworthiness", document ref. P2F-00090-ICA-S02, Revision R00, dated February 23, 2021 or later EASA accepted revisions, is mandatory.

3. No items or equipment may be carried or installed in the forward cargo barrier net expansion zone.

4. The access to main deck cargo compartment is prohibited in all phases of the flight.

5. This STC is applicable to all serial numbers for ATR models ART72-202, ART72-212 and ATR72-212A.

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

7. If the holder agrees to permit another person to use the certificate to alter the product, the holder shall give the other person written evidence of that permission.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

IMPORT ST00016IB Date of Issuance: July 12,2021

Certification Basis:

Based on 14 CFR §21.115 and §21.101, and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for ATR72-202, -212, -212A BCF is as follows:

a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A53EU.

b. The modification certification basis for parts changed or affected by the change since the reference date of application to EASA, October 29, 2004, is based upon part 25 as amended by Amendment 25-115 as follows:

Regulations at the latest amendment 25-0 through 25-115:

25.1, 25.2, 25.23, 25.25, 25.27, 25.31, 25.301, 25.303, 25.305, 25.307, 25.561, 25.571,

25.581, 25.601, 25.603, 25.605, 25.609, 25.611, 25.613, 25.619, 25.621, 25.623,

25.625, 25.787, 25.793, 25.831, 25.843, 25.851, 25.853, 25.855, 25.857, 25.858,

25.869, 25.1301, 25.1309, 25.1322, 25.1351, 25.1353, 25.1357, 25.1439, 25.1441,

25.1445, 25.1501, 25.1519, 25.1525, 25.1529, 25.1541, 25.1557, 25.1581, 25.1583,

25.1585 Regulations at the amendment level in TCDS A53EU:

25.321, 25.331, 25.341, 25.345, 25.349, 25.351, 25.373, 25.391, 25.393, 25.395,

25.397, 25.399, 25.405, 25.407, 25.409, 25.415, 25.427, 25.445, 25.457, 25.459,

25.471, 25.473, 25. 477, 25.479, 25.481, 25.483, 25.485, 25.487, 25.489, 25.491,

25.493, 25.495, 25.497, 25.499, 25.503, 25.507, 25.509, 25.511

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