Pma Supplements Index Heico
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PMA Supplements Index:ARTICLE NUMBER ARTICLE NAME PMA SUPP. DATE ISSUED DEC6713‐85 SHIM TK232 JULY 15, 2010DEC6763‐01884 GUIDE, SPRING TK253 JAN 25, 2012DEC6763‐02300 VALVE, OVER PRESSURE, S/A DEC6773‐61 GUIDE, CLAPPER ODA‐TK‐022 MARCH 23, 2016 DEC6773‐68 CLAPPER HEICO Aerospace Corporation PMA Supplements Index:ARTICLE NUMBER ARTICLE NAME PMA SUPP. DATE ISSUED TK232 JULY 15, 2010 DEC6713‐85 SHIM TK253 JAN 25, 2012 ODA‐TK‐022 MARCH 23, 2016 HEICO Aerospace Corporation FAA – PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENTTurbine Kinetics, Inc. PMA NO.: PQ0816NEA HEICO Aerospace Company SUPPLEMENT No.: ODA-TK-02260 Sequin Drive DATE: March 23, 2016Glastonbury, CT 06033Article Article Approved Approval Basis and Make/TCH Model/SeriesName Number Replacement Approved Design Data Eligibility Eligibility for Article NumberLatch 740-0352-505DEC Goodrich Tests and Computations per Airbus A319 Model -131Assembly- Aerostructures 14 CFR § 21.303, A319 Model -132Auxiliary P/N: Dwg No.: A319 Model -133 740-0352-505 740-0352-505DEC, Rev.: B, A320 Model -231 Dated: 8/6/13, A320 Model -232 or later FAA approved A320 Model -233 revisions
A321 Model -131 A321 Model -231 A321 Model -232Housing 740-0353-505DEC Goodrich Tests and Computations per Airbus A319 Model -131 Aerostructures 14 CFR § 21.303, A319 Model -132 P/N: Dwg No.: A319 Model -133 740-0353-505 740-0353-505DEC, Rev.: B, A320 Model -231 Dated: 8/7/13, A320 Model -232 or later FAA approved A320 Model -233 revisions
A321 Model -131 A321 Model -231 A321 Model -232Fitting-End 740-0354-507DEC Goodrich Tests and Computations per Airbus A319 Model -131 Aerostructures 14 CFR § 21.303, A319 Model -132 P/N: Dwg No.: A319 Model -133 740-0354-507 740-0354-507DEC, Rev.: B, A320 Model -231 Dated: 8/7/13, A320 Model -232 or later FAA approved A320 Model -233 revisions
A321 Model -131 A321 Model -231 A321 Model -232 Page 1 of 15 HA Form F712.1 FAA – PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENTTurbine Kinetics, Inc. PMA NO.: PQ0816NEA HEICO Aerospace Company SUPPLEMENT No.: ODA-TK-02260 Sequin Drive DATE: March 23, 2016Glastonbury, CT 06033Article Article Approved Approval Basis and Make/TCH Model/SeriesName Number Replacement Approved Design Data Eligibility Eligibility for Article NumberFitting-End 740-0355-507DEC Goodrich Tests and Computations per Airbus A319 Model -131 Aerostructures 14 CFR § 21.303, A319 Model -132 P/N: Dwg No.: A319 Model -133 740-0355-507 740-0355-507DEC, Rev.: B, A320 Model -231 Dated: 8/7/13, A320 Model -232 or later FAA approved A320 Model -233 revisions
A321 Model -131 A321 Model -231 A321 Model -232Fire Seal DEC59-032-501 Boeing P/N: Tests and Computations per Boeing 747-200B SeriesAssembly 314U2100-15 14 CFR § 21.303, 747-300 Series Dwg No.: DEC59-032, 747-400 Series Rev.: L, 747-400D Series Dated: 4/15/15, 747-400F Series or later FAA approved revisions. 767-200 Series 767-300 Series 767-300F Series 767-400ER SeriesRetainer DEC59-032-003 Boeing P/N: Tests and Computations per Boeing 747-200B Series 314U2100-18 14 CFR § 21.303, 747-300 Series Dwg No.: DEC59-032, 747-400 Series Rev.: L, 747-400D Series Dated: 4/15/15, 747-400F Series or later FAA approved revisions. 767-200 Series 767-300 Series 767-300F Series 767-400ER Series Page 2 of 15 HA Form F712.1 FAA – PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENTTurbine Kinetics, Inc. PMA NO.: PQ0816NEA HEICO Aerospace Company SUPPLEMENT No.: ODA-TK-02260 Sequin Drive DATE: March 23, 2016Glastonbury, CT 06033Article Article Approved Approval Basis and Make/TCH Model/SeriesName Number Replacement Approved Design Data Eligibility Eligibility for Article NumberFireseal, Fwd DEC59-032-005 Boeing P/N: Tests and Computations per Boeing 747-200B Series 314U2100-19 14 CFR § 21.303, 747-300 Series Dwg No.: DEC59-032, 747-400 Series Rev.: L, 747-400D Series Dated: 4/15/15, 747-400F Series or later FAA approved revisions. 767-200 Series 767-300 Series 767-300F Series 767-400ER SeriesFireseal, DEC59-032-007 Boeing P/N: Tests and Computations per Boeing 747-200B SeriesAft 314U2100-20 14 CFR § 21.303, 747-300 Series Dwg No.: DEC59-032, 747-400 Series Rev.: L, 747-400D Series Dated: 4/15/15, 747-400F Series or later FAA approved revisions. 767-200 Series 767-300 Series 767-300F Series 767-400ER Series Page 3 of 15 HA Form F712.1 FAA – PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENTTurbine Kinetics, Inc. PMA NO.: PQ0816NEA HEICO Aerospace Company SUPPLEMENT No.: ODA-TK-02260 Sequin Drive DATE: March 23, 2016Glastonbury, CT 06033Article Article Approved Approval Basis and Make/TCH Model/SeriesName Number Replacement Approved Design Data Eligibility Eligibility for Article NumberValve, DEC6763-02300 Liebherr P/N: Tests and Computations per CFM CFM56-5A1Overpressure, 6763-02300 14 CFR § 21.303, International CFM56-5A1/FS/A Dwg No.: CFM56-5A3 DEC6763-02300, CFM56-5A4 Rev.: H, CFM56-5A4/F Dated: 5/27/15, CFM56-5A5 or later FAA approved CFM56-5A5/F revisions
CFM56-5B1 CFM56-5B1/P CFM56-5B1/2P CFM56-5B2 CFM56-5B1/3 CFM56-5B2/3 CFM56-5B3/3 CFM56-5B3/3B1 CFM56-5B2/P CFM56-5B2/2P CFM56-5B3/P CFM56-5B3/P1 CFM56-5B4/3 CFM56-5B4/3B1 CFM56 -5B5/3 CFM56-5B6/3 CFM56-5B3/2P CFM56-5B3/2P1 CFM56-5B4 CFM56-5B4/P CFM56-5B4/P1 CFM56-5B4/2P CFM56-5B4/2P1 CFM56-5B5 CFM56-5B5/P CFM56-5B6 CFM56-5B6/P CFM56-5B6/2P CFM56-5B7 CFM56-5B7/P CFM56-5B8/P CFM56-5B9/P CFM56-5B7/3 CFM56-5B8/3 CFM56-5B9/3 CFM56-5B9/2P Page 4 of 15 HA Form F712.1 FAA – PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENTTurbine Kinetics, Inc. PMA NO.: PQ0816NEA HEICO Aerospace Company SUPPLEMENT No.: ODA-TK-02260 Sequin Drive DATE: March 23, 2016Glastonbury, CT 06033Article Article Approved Approval Basis and Make/TCH Model/SeriesName Number Replacement Approved Design Data Eligibility Eligibility for Article NumberValve, DEC6763-02300 Liebherr P/N: Tests and Computations per International V2500-A1Overpressure, 6763-02300 14 CFR § 21.303, Aero V2522-A5S/A Dwg No.: Engines V2524-A5 DEC6763-02300, V2527M-A5 Rev.: H, V2527-A5 Dated: 5/27/15, V2527E-A5 or later FAA approved V2530-A5 revisions. V2533-A5 Page 5 of 15 HA Form F712.1 FAA – PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENTTurbine Kinetics, Inc. PMA NO.: PQ0816NEA HEICO Aerospace Company SUPPLEMENT No.: ODA-TK-02260 Sequin Drive DATE: March 23, 2016Glastonbury, CT 06033Article Article Approved Approval Basis and Make/TCH Model/SeriesName Number Replacement Approved Design Data Eligibility Eligibility for Article NumberShim DEC6713-85 Liebherr P/N: Tests and Computations per CFM CFM56-5A1 6713-85 14 CFR § 21.303, International CFM56-5A1/F Dwg No.: CFM56-5A3 DEC6713-85, CFM56-5A4 Rev.: D, CFM56-5A4/F Dated: 5/27/15, CFM56-5A5 or later FAA approved CFM56-5A5/F revisions
CFM56-5B1 CFM56-5B1/P CFM56-5B1/2P CFM56-5B2 CFM56-5B1/3 CFM56-5B2/3 CFM56-5B3/3 CFM56-5B3/3B1 CFM56-5B2/P CFM56-5B2/2P CFM56-5B3/P CFM56-5B3/P1 CFM56-5B4/3 CFM56-5B4/3B1 CFM56 -5B5/3 CFM56-5B6/3 CFM56-5B3/2P CFM56-5B3/2P1 CFM56-5B4 CFM56-5B4/P CFM56-5B4/P1 CFM56-5B4/2P CFM56-5B4/2P1 CFM56-5B5 CFM56-5B5/P CFM56-5B6 CFM56-5B6/P CFM56-5B6/2P CFM56-5B7 CFM56-5B7/P CFM56-5B8/P CFM56-5B9/P CFM56-5B7/3 CFM56-5B8/3 CFM56-5B9/3 CFM56-5B9/2P Page 6 of 15 HA Form F712.1 FAA – PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENTTurbine Kinetics, Inc. PMA NO.: PQ0816NEA HEICO Aerospace Company SUPPLEMENT No.: ODA-TK-02260 Sequin Drive DATE: March 23, 2016Glastonbury, CT 06033Article Article Approved Approval Basis and Make/TCH Model/SeriesName Number Replacement Approved Design Data Eligibility Eligibility for Article NumberShim DEC6713-85 Liebherr P/N: Tests and Computations per International V2500-A1 6713-85 14 CFR § 21.303, Aero V2522-A5 Dwg No.: Engines V2524-A5 DEC6713-85, V2527M-A5 Rev.: D, V2527-A5 Dated: 5/27/15, V2527E-A5 or later FAA approved V2530-A5 revisions. V2533-A5 Page 7 of 15 HA Form F712.1 FAA – PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENTTurbine Kinetics, Inc. PMA NO.: PQ0816NEA HEICO Aerospace Company SUPPLEMENT No.: ODA-TK-02260 Sequin Drive DATE: March 23, 2016Glastonbury, CT 06033Article Article Approved Approval Basis and Make/TCH Model/SeriesName Number Replacement Approved Design Data Eligibility Eligibility for Article NumberBody, Valve DEC6763-239 Liebherr P/N: Tests and Computations per CFM CFM56-5A1 6763-239 14 CFR § 21.303, International CFM56-5A1/F Dwg No.: CFM56-5A3 DEC6763-239, CFM56-5A4 Rev.: J, CFM56-5A4/F Dated: 5/27/15, CFM56-5A5 or later FAA approved CFM56-5A5/F revisions
CFM56-5B1 CFM56-5B1/P CFM56-5B1/2P CFM56-5B2 CFM56-5B1/3 CFM56-5B2/3 CFM56-5B3/3 CFM56-5B3/3B1 CFM56-5B2/P CFM56-5B2/2P CFM56-5B3/P CFM56-5B3/P1 CFM56-5B4/3 CFM56-5B4/3B1 CFM56 -5B5/3 CFM56-5B6/3 CFM56-5B3/2P CFM56-5B3/2P1 CFM56-5B4 CFM56-5B4/P CFM56-5B4/P1 CFM56-5B4/2P CFM56-5B4/2P1 CFM56-5B5 CFM56-5B5/P CFM56-5B6 CFM56-5B6/P CFM56-5B6/2P CFM56-5B7 CFM56-5B7/P CFM56-5B8/P CFM56-5B9/P CFM56-5B7/3 CFM56-5B8/3 CFM56-5B9/3 CFM56-5B9/2P Page 8 of 15 HA Form F712.1 FAA – PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENTTurbine Kinetics, Inc. PMA NO.: PQ0816NEA HEICO Aerospace Company SUPPLEMENT No.: ODA-TK-02260 Sequin Drive DATE: March 23, 2016Glastonbury, CT 06033Article Article Approved Approval Basis and Make/TCH Model/SeriesName Number Replacement Approved Design Data Eligibility Eligibility for Article NumberBody, Valve DEC6763-239 Liebherr P/N: Tests and Computations per International V2500-A1 6763-239 14 CFR § 21.303, Aero V2522-A5 Dwg No.: Engines V2524-A5 DEC6763-239, V2527M-A5 Rev.: J, V2527-A5 Dated: 5/27/15, V2527E-A5 or later FAA approved V2530-A5 revisions. V2533-A5 Page 9 of 15 HA Form F712.1 FAA – PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENTTurbine Kinetics, Inc. PMA NO.: PQ0816NEA HEICO Aerospace Company SUPPLEMENT No.: ODA-TK-02260 Sequin Drive DATE: March 23, 2016Glastonbury, CT 06033Article Article Approved Approval Basis and Make/TCH Model/SeriesName Number Replacement Approved Design Data Eligibility Eligibility for Article NumberGuide, Spring DEC6763-01884 Liebherr P/N: Tests and Computations per CFM CFM56-5A1 6763-01884 14 CFR § 21.303, International CFM56-5A1/F Dwg No.: CFM56-5A3 DEC6763-01884, CFM56-5A4 Rev.: G, CFM56-5A4/F Dated: 6/17/15, CFM56-5A5 or later FAA approved CFM56-5A5/F revisions
CFM56-5B1 CFM56-5B1/P CFM56-5B1/2P CFM56-5B2 CFM56-5B1/3 CFM56-5B2/3 CFM56-5B3/3 CFM56-5B3/3B1 CFM56-5B2/P CFM56-5B2/2P CFM56-5B3/P CFM56-5B3/P1 CFM56-5B4/3 CFM56-5B4/3B1 CFM56 -5B5/3 CFM56-5B6/3 CFM56-5B3/2P CFM56-5B3/2P1 CFM56-5B4 CFM56-5B4/P CFM56-5B4/P1 CFM56-5B4/2P CFM56-5B4/2P1 CFM56-5B5 CFM56-5B5/P CFM56-5B6 CFM56-5B6/P CFM56-5B6/2P CFM56-5B7 CFM56-5B7/P CFM56-5B8/P CFM56-5B9/P CFM56-5B7/3 CFM56-5B8/3 CFM56-5B9/3 CFM56-5B9/2P Page 10 of 15 HA Form F712.1
SUPPLEMENT No.: ODA-TK-022 DATE: March 23, 2016 Page 1 of 15 HA Form F712.1 Article Name Article Number Approved Replacement for Article Number Approval Basis and Approved Design Data Make/TCH Eligibility Model/Series Eligibility Latch Assembly- Auxiliary 740-0352-505DEC Goodrich Aerostructures P/N: 740-0352-505
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Frequently Asked Questions
What is pma supplement under review?
A PMA supplement is the submission required for a change affecting the safety or effectiveness of the device for which the applicant has an approved PMA; additional information provided to FDA for PMA supplement under review are amendments to a supplement.
What is a pma pma amendment?
A PMA amendment includes all additional submissions to a PMA or PMA supplement before approval of the PMA or PMA supplement OR all additional correspondence after PMA or PMA supplement approval.
How do i find a pma article?
We maintain listings of Parts Manufacturer Approval (PMA) articles in the FAA Dynamic Regulatory System (DRS). In DRS, under the "Design and Production Approvals" section, you may search PMAs by PMA holder, PMA article name, number, approval basis, as well as make and model on which the PMA part can be installed.
What types of changes must an applicant submit a pma supplement?
Changes for which an applicant must submit a PMA supplement include, but are not limited to, the following types of changes if they affect the safety or effectiveness of the device: the use of a different facility or establishment to manufacture, process, or package the device;