What it approves
Installation of Pratt & Whitney Canada PT6C-67D, engine in accordance with DynCorp International Master Drawing List Report Number D1H-MDL-100, Revision IR, dated April 17, 2007, or later FAA approved revision. DynCorp International Rotorcraft Flight Manual Supplement (RFMS) Report Number DIER-0012, Revision 0, dated January 17, 2008, or later FAA approved revision, is required. Instructions for Continued Airworthiness (ICAs) DIER-0003, Revision 1, dated August 30, 2007, or later revision is required. Airworthiness Limitations section of ICA DIER-0003, approved on August 30, 2007 or later approved revision is required.
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.
14 CFR 21.120)
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 1 OF 3
Number: SR09492RC This certificate issued to:
Installation of Pratt & Whitney Canada PT6C-67D, engine in accordance with DynCorp International Master Drawing List Report Number D1H-MDL-100, Revision IR, dated April 17, 2007, or later FAA approved revision. DynCorp International Rotorcraft Flight Manual Supplement (RFMS) Report Number DIER-0012, Revision 0, dated January 17, 2008, or later FAA approved revision, is required.
Instructions for Continued Airworthiness (ICAs) DIER-0003, Revision 1, dated August 30, 2007, or later revision is required. Airworthiness Limitations section of ICA DIER-0003, approved on August 30, 2007 or later approved revision is required.
TALON Aerospace Inc.
15387 Doran Rd.
Acme, Washington 98220
Original Product Type Certificate Number: R00002RC
Make: GHTI Model: UH-1H
Date of application: January 09, 2007
Date of issuance: January 17, 2008 Date reissued: June 28, 2010; August 22, 2022
August A. Asay Title: Manager, Anchorage ACO Branch
Part 29 of Federal Aviation Regulations.
14 CFR 21.120)
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 2 OF 3
Number: SR09492RC
Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SR09492RC
14 CFR 21.120)
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 3 OF 3
Date of issuance: March 01, 2004 Date reissued: June 28, 2010; August 22, 2022 Date amended:
Number: SR09492RC
Limitations and Conditions: (continuation from page 1 of 3) The installer must determine whether this design change is compatible with previously approved modifications.
Certification Basis:
FAR 29 Amendment 1: 29.1, 29.21, 29.25, 29.27, 29.29(b), 29.45, 29.65(a), 29.71, 29.73(b), 29.79 (a)
(b) (2), 29.141, 29.143, 29.161, 29.171, 29.173, 29.175, 29.251, 29.301, 29.303, 29.305, 29.307 (a)
(b) (1) (4) (6), 29.309 (a) (g), 29.321, 29.337, 29.361 (a), 29.399, 29.549 (c) (d), 29.561 (a) (b),
29.601 (a), 29.603, 29.605, 29.607, 29.609, 29.611, 29.613 (a) (b) (d), 29.625, 29.671, 29.675 (a) (b)
(c), 29.681, 29.683, 29.685, 29.771 (a) (b) (c), 29.777, 29.831 (b) (c) (d), 29.833, 29.859, 29.861 (b),
29.863, 29.901, 29.903 (a), 29.907, 29.917 (a), 29.923 (a) (b) (c) (d) (e) (f) (g), 29.927, 29.931,
29.935, 29.951, 29.955, 29.961 (a), 29.993, 29.995, 29.997, 29.1011 (a) (b) (e), 29.1013 (c) (d),
29.1015, 29.1017, 29.1019, 29.1021, 29.1023, 29.1025, 29.1041, 29.1043 (a) (b), 29.1047 (b),
29.1049, 29.1093 (a), 29.1103, 29.1105 (b) (c) (d), 29.1121, 29.1123, 29.1141, 29.1143 (a) (c),
29.1163, 29.1165, 29.1181, 29.1183, 29.1185, 29.1187 (a) (b) (c) (d), 29.1191, 29.1193 (a) (b) (c) (d),
29.1203, 29.1301, 29.1305 (a) (6) (7) (8) (9) (10) (11) (c), 29.1307 (d) (e), 29.1309 (a) (b) (c),
29.1321 (a) (b) (c) (e) (f), 29.1337 (d), 29.1351(a) (1) (b), 29.1353 (a) (b), 29.1355 (a) (b) (2) 29.1357
(a) (c) (d) (e), 29.1359, 29.1381, 29.1401, 29.1431 (a), 29.1435, 29.1501, 29.1517, 29.1519, 29.1521
(a) (b) (c) (1) (d) (e), 29.1523, 29.1525, 29.1541, 29.1543 (b), 29.1549, 29.1551, 29.1555 (a) (b) (1)
(d), 29.1557 (c), 29.1559, 29.1581, 29.1583 (a) (b) (c) (e), 29.1585, 29.1587 (b) (2) (4) (5) (6).
FAR 29 Amendment 3: 29.1091 (a) (b) (c) (f).
FAR 29 Amendment 12: 29.397(b) (2), 29.1322 (a) (b).
FAR 29 Amendment 20: 29.1529.
FAR 29 Amendment 26: 29.1027, 29.1189 (a) (d) (e) (f).
Special conditions 29-015-SC (HIRF) Dated November 7, 2007.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Global Helicopter Technology Inc. | UH-1H | R00002RC |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| August 22, 2022 | Reissued, current | Certificate |
| June 28, 2010 | Reissued, earlier issue | Certificate |