Piper Aircraft, Inc. PA-46R-350T: certification basis
Basis entries as written on the TCDS
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OTHER
Type Certificate No. A25SO issued September 27, 1983.
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OTHER
Date of application for Type Certificate, August 22, 1979.
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◆ SPECIAL
Special Conditions No. 23-ACE-53, Docket No. 082CE.
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REG
For the Avidyne Entegra system installation (See Piper Report VB-1954) and modifications to that installation (See Piper Report VB-2008) the following additional requirements are applicable: FAR 23.1529 as amended by Amendment 23-26, effective 14 October 1980; FAR 23.1523 as amended by Amendment 23-34, effective 17 February 1987; FAR 23.1322, 23.1331, 23.1357 (a)(2), (b), (c), (d) as amended by Amendment 23- 43, effective 10 May 1993; FAR 23.305, 23.613, 23.773 (a)(2), 23.1525, 23.1549 (a) as amended by Amendment 23-45, effective 7 September 1993; FAR 23.301, 23.337 (a)(1), (b)(1), 23.341 (a), 23.473, 23.561 (b)(3), (e), 23.571 (a), 23.607, 23.611, as amended by Amendment 23-48, effective 11 March 1996; FAR 23.1303 (a), (b), (f), 23.1307, 23.1309 (a), (a)(1), (a)(2), (b),(e), 23.1311 (a)(2), (a)(3), (a)(4), (a)(5), (a)(6), (a)(7), (b), (c), 23.1321 (a), (c), (d), (e), 23.1323 (a), (c), 23.1329, 23.1351 (a)(1), (a)(2)(i), (b)(2), (b)(3), 23.1353 (d), (h), 23.1359 (c), 23.1365 (a), (b), (d), (e), (f), 23.1431 (a), (b) as amended by Amendment 23-49, effective 11 March 1996; FAR 23.1325 (a), (b)(1), (b)(2)(ii), (b)(3), (c), (e), 23.1543 (b), (c), 23.1545(a), (b)(3), (b)(4), (c), 23.1555 (a), (b), 23.1563, 23.1581 (a), (b)(2), (b)(3), (f), 23.1583 (m), 23.1585 (j) as amended by Amendment 23-50, effective 11 March1996; FAR 23.777 (a), (b), 23.1337 as amended by Amendment 23-51, effective 11 March 1996; FAR 23.1305 (a)(1), (a)(2), (a)(3),
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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◆ SPECIAL
(b)(2), (b)(3), (b)(4), (b)(5), (b)(6)(i) as amended by Amendment 23-52, effective 25 July 1996 Special Condition for HIRF (Docket # CE215, Special Condition 23-154-SC), January 7, 2005.
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REG
For modifications specific to the PA-46R-350T airplane (see Piper Report VB-2008) the following additional requirements are applicable: FAR 23.1529 and Appendix G (Sec G23.1 and G23.2) as amended by Amendment 23-26, effective 14 October 1980; Appendix G (Sec G23.3) as amended by Amendment 23-34 effective 17 February 1987;
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
FAR 23.2 as amended by Amendment 23-36 effective 14 September 1988; Appendix G (Sec G23.4) as amended by Amendment 23-37, effective 18 August 1990; FAR 23.831 as amended by Amendment 23-42, effective 4 February 1991; FAR 23.905, 23.1357, 23.1441, 23.1443, and 23.1445 as amended by Amendment 23-43, effective 10 May 1993; FAR 23.613, 23.773, 23. 851, and 23.1527 as amended by Amendment 23-45, effective 7 September 1993; FAR 23.561, 23.572,, 23.575, 23.607, and 23.611 as amended by Amendment 23-48, effective 11 March 1996; FAR 23.775, 23.783, 23.853, 23.1309, 23.1311, 23.1321, 23.1323, 23.1351, 23.1447, 23.1451, 23.1453, and Appendix F (Sec F23) as amended by Amendment 23-49, effective 11 March 1996; FAR 23.25, 23.1325, 23.1543, 23.1545, and 23.1589 as amended by Amendment 23-50, effective 11 March 1996; FAR 23.907 and 23.1191 as amended by Amendment 23-51, effective 11 March 1996; and FAR Part 36, effective December 1, 1969, as amended by Amendment 36-1, dated December 1, 1969 through Amendment 36-28, dated 3 February 2006
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
23.907 as amended by Amendment 23-59, effective 24 October 2008.
Applies to: For the PA-46R-350T Matrix aircraft equipped with Hartzell propeller HC-I3Y1R- 1N/N7605+2 or HC- I3Y1R-1N/N7605K+2 or HC-I3Y1R-1N/N7605C+2 or HC-I3Y1R- 1N/N7605CK+ (See Piper Report VB-2132) the additional certification basis for installation specific items only is
Includes 14 CFR 23 §23.907 through 23-59 · current is 23-63, 3 revisions later
Expands to 1 provision link · shown below
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OTHER
Eligible Serial Numbers: 4692123 & up.
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REG
14 CFR 23.23 14 CFR 23.25 14 CFR 23.251 14 CFR 23.301 (a), (b), (c) 14 CFR 23.305 14 CFR 23.337 14 CFR 23.341 14 CFR 23.397 (a) 14 CFR 23.473 14 CFR 23.561 (a), (b)(3), (e) 14 CFR 23.607 14 CFR 23.611 14 CFR 23.613 14 CFR 23.677 (b), (d) 14 CFR 23.773 (a)(l), (a)(2) 14 CFR 23.777 (a), (b), (d) 14 CFR 23.867 14 CFR 23.1141 (a), (b), (c), (d) 14 CFR 23.1303 (a), (b), (c), (f) 14 CFR 23.1305 (a)(l), (a)(2), (a)(3), (b)(2), (b)(4)(i), (b)(5), (b)(6)(i) 14 CFR 23.1307 14 CFR 23.1308 (a) (1), (a)(2), (a)(3), (b), (c) 14 CFR 23.1309 (a) (1), (a)(2), (b), (c), (e) 14 CFR 23.1311 (a)(l), (a)(2), (a)(3), (a)(4), (a)(5), (a)(6), (a)(7), (b), (c) 14 CFR 23.1321 (a), (c), (d)(5), (e) 14 CFR 23.1322 (a), (b), (c), (d), (e) 14 CFR 23.1323 (a), (c) 14 CFR 23.1325 (a), (b)(l), (b)(2)(i) 14 CFR 23.1326
Applies to: For PA-46R-350T aircraft equipped with Piper factory installed Garmin G1000 system and GFC 700 AFCS (See Piper Drawing 106900), the additional certification basis for installation specific items only as amended by Amendment 23-59 dated December 23, 2008, is
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
14 CFR 23.1329 (a) (1), (b), (d), (e), (f), (g), (h), 14 CFR 23.1331 (a), (b), (c) 14 CFR 23.1337 (b)(l), (b)(4) 14 CFR 23.1351 (a)(l), (a)(2)(i), (b)(l)(i) 14 CFR 23.1353 (h) 14 CFR 23.1357 (a)(2), (b), (c), (d) 14 CFR 23.1359 (c) 14 CFR 23.1365 (a), (b), (d), (e), (f) 14 CFR 23.1431 (a), (b), (e) 14 CFR 23.1441 (b), (c), (e) 14 CFR 23.1507 14 CFR 23.1523 14 CFR 23.1525 14 CFR 23.1529 14 CFR 23.1543 (b)(c) 14 CFR 23.1545 (a), (b) (1), (b)(2), (b)(3), (b) (4) 14 CFR 23.1549 (a), (b), (c) 14 CFR 23.1553 14 CFR 23.1555 (a), (b), (d)(2) 14 CFR 23.1559 (c) 14 CFR 23.1563 (a) (b) 14 CFR 23.1567 (a) 14 CFR 23.1581 14 CFR 23.1583 14 CFR 23.1585 14 CFR 23.1589 Eligible Serial Numbers: 4692134 and up
Applies to: For PA-46R-350T aircraft equipped with Piper factory installed Garmin G1000 system and GFC 700 AFCS (See Piper Drawing 106900), the additional certification basis for installation specific items only as amended by Amendment 23-59 dated December 23, 2008, is
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
- Equivalent level of safety findings: none recorded.
- Exemptions: none recorded.
Entry 8 expanded
Powerplant 14 CFR 23 1 section
| Section | Title | Cut-off | Text version | Changed since | Status |
|---|---|---|---|---|---|
| §23.907 | Propeller vibration and fatigue. General | 23-59 | 23-59 | 0 | ✓ Text available |