FAA PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENT Turbine Kinetics, Inc. 60 Sequin Drive Glastonbury, CT 06033 PMA NO.: PQ0816NE SUPPLEMENT No.: ODA-TK-012 DATE: February 19, 2016 Name Approved Replacement for Approval Basis and Approved Design Data Make/TCH Model/Series DEC59-110-502 P/N: 452T1204-2 Dwg No.: DEC59-110, Rev.: H, Dated: 6/20/11,. DEC59-110-511 P/N: 452T1204-11 Dwg No.: DEC59-110, Rev.: H, Dated: 6/20/11,. DEC59-110-512 P/N: 452T1204-12 Dwg No.: DEC59-110, Rev.: H, Dated: 6/20/11,. DEC59-110-515 P/N: 452T1204-15 Dwg No.: DEC59-110, Rev.: H, Dated: 6/20/11,. Pedal DEC59-111-511 P/N: 452T1205-11 Dwg No.: DEC59-111, Rev.: E, Dated: 7/26/12,. Page 1 of 5 HA Form F712.1
FAA PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENT Turbine Kinetics, Inc. 60 Sequin Drive Glastonbury, CT 06033 PMA NO.: PQ0816NE SUPPLEMENT No.: ODA-TK-012 DATE: February 19, 2016 Name Approved Replacement for Approval Basis and Approved Design Data Make/TCH Model/Series Cam DEC59-112-507 P/N: 452T1207-7 Dwg No.: DEC59-112, Rev.: E, Dated: 7/26/12,. Restraint DEC59-113-501 P/N: 452T1208-1 Dwg No.: DEC59-113, Rev.: G, Dated: 7/26/12,. Pawl DEC59-114-512 P/N: 452T1212-12 Dwg No.: DEC59-114, Rev.: C, Dated: 11/9/06,. Pawl DEC59-115-511 P/N: 452T1610-11 Dwg No.: DEC59-115, Rev.: C, Dated: 11/9/06,. Shaft DEC59-116-504 P/N: 452T1614-4 Dwg No.: DEC59-116, Rev.: D, Dated: 11/9/06,. Page 2 of 5 HA Form F712.1
FAA PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENT Turbine Kinetics, Inc. 60 Sequin Drive Glastonbury, CT 06033 PMA NO.: PQ0816NE SUPPLEMENT No.: ODA-TK-012 DATE: February 19, 2016 Name Approved Replacement for Approval Basis and Approved Design Data Make/TCH Model/Series Restraint DEC59-117-501 P/N: 452T1640-1 Dwg No.: DEC59-117, Rev.: D, Dated: 11/9/06,. Pin DEC59-124-511 P/N: 452T1218-11. Pin DEC59-124-512 P/N: 452T1218-12. Pin DEC59-124-513 P/N: 452T1218-13. Pin DEC59-124-514 P/N: 452T1218-14. Page 3 of 5 HA Form F712.1
FAA PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENT Turbine Kinetics, Inc. 60 Sequin Drive Glastonbury, CT 06033 PMA NO.: PQ0816NE SUPPLEMENT No.: ODA-TK-012 DATE: February 19, 2016 Name Approved Replacement for Approval Basis and Approved Design Data Make/TCH Model/Series Pin DEC59-124-515 P/N: 452T1218-15. Pin DEC59-124-522 P/N: 452T1218-22. 777-200 Series Screw DEC59-139-101 P/N: 116080-3 Dwg No.: DEC59-139-101, Rev.: D, Dated: 6/8/15,. 767-300F Series 757-200 Series 757-200PF Series Latch Assy DEC59-139-501 P/N: HA142-2 HA142-3 HA142-5 H3225-3 H3225-5 S313T310-4 10-61334-9 10-61334-10 10-61334-12 10-61334-16 10-61334-17 10-61334-18 9284-4 9675-10 9675-12 91049-16 91049-17 91049-18 Dwg No.: DEC59-139, Rev.: R, Dated: 8/16/13,. 767-300F Series 757-200 Series 757-200PF Series Page 4 of 5 HA Form F712.1
FEDERAL AVIATION ADMINISTRATION-PARTS MANUFACTURER APPROVAL DEC Technologies, Inc. 136 Industrial Park Road Piney Flats, TN 37686 PMA NO. PQ1469CE SUPPLEMENT NO. 226 DATE: AwriI 22.2010 Part Part Approved Approved Basis and Make Model Name Replacement Approved Design Data For Part Hushing DEC59-110-001 RACB28Y6M048 Roeing 767-200 Smics CFR 8 21,303. Dwg: DEC59-110 - Rev.: Rev D & Or later FAA-approved Rushing DEC59-1 10-002 'I'est and Computation per 14 CFR 4 21.303, kg: DEC59-110 b: Rev D JJ& or later FAA-appmvd Bushing DEC59-11 0-003 Test and Computation per I4 CFR # 21.303, Dwg: DEC59-110 - Rev.: Rev D - Dale: Nov 04,2006 767-300 Scrim Dwg: DEC59-1 10 : RwD m 767.200 Series 1>EG59-110-111 Test and Compumtion per 14 CFR 8 21.303. hg: DEC59-1 I0 Rev.! RtvD - Date DEC59-110-112 CFR 6 21.303, Dw~: DEC59-110 W: RevD
Test and Computation per I4 CFR 21.303, kg: DEC59- i 10 : Rev D DEC59-110-502 CFR # 21.303, Dwg: DECS9-110 : RevD Boting DEC59-110-511 CFR 4 21.303, Dwg; DEC59- I 10 Bf4$: RevD Q& 767-200 Saies DECS9-110-512 CFR 4 21.303, Dwg: DEC59-110 : Rev D Q& Bocing 767.300 Series DEC59-110-515 CFR $21.303, Dw~: DEC59-1 I0 Rev.: Rev D m: Nov09.2006 or later FAA-approvtd 767-2W Series CFR 21.303, Dwg: DEC59.111 &: RevD or later FAA-approvd Bming 767.200 Series 767.300 Series Cam DEC59-112-507 Dw~: DEC59-112 - Rev.: Rev C Date rcvisions 767-300 Sdcs
Restraint DEC59-113-501 CFR 8 21.303. Dw~; DEC59-I 13 : Rev D - Date Pawl DEC59- I 1 4-5 12 CFR # 21.303, Dwg: DEC59-I 14 &,: Rev C or later FAA-approvcd Roeing Pawl DEC59-1 I 5-5 1 1, Bwing CFR f 21.303, Dwg: DEC59-115 Rev.: Rev C - Date Dw~: DEC59- I 16 &: Rev D Date or latcr FAA-approved 767-200 Smie 767.300 Series Restraint DEC59-117-50 1 CFR $21.303, Dw~: DEC59-117 Rev.: Rev D - Date or Iakr FAA-approved Baeing Latch DEC59-139.501 'rest and Computation per 14 Dw~: DEC59-139 : RevK : Aug 29,2008 Botjng 767400F Series 767400ER Series 757-200 Series 757-200PF Series BoIt& Pad DEC59.139-101 Test ad Computation per 14 Dwg: DEC59-139-101 &: RevA : May 30,2006 767-300F Series 757-200 Series 757-200PF Series
Bushing - DEC600-10300-605 600-1 0300-605 Sleeve Rombardicr CL-600-2RI 9 CFR 4 21.303, (Regional Jet Dwg: DECBOU- 10300- Series 100 & 605 440) ; Rev B : Jan 28,2008 Cmk DEC59-120-506 452T2605-6 Asscrnbly CFR 8 21.303. Dwg: DEC59.120 &: RevE : Apr 13.2007 or latcr FAA-approved Rwing Clevis DEC59-12 1-5 1 1 Uwg: DEC59-121. Rev.: Rev C - Date: Apr 13,2007 777-200 Series Paw1 DEC59-122-508 Dwg: DEC59- I22 &: Rev D : Apr 13,2007 e - - - - - - - 3 - - End of Listing ------------------- 777-200 Series NOTE: 1) Provide minor design changes in a manner as determined by the ACO. Handle major design changes to drawings and specifications in the same manner as that for an original FAA-PMA. 2) The FAA approved ICA for the above parts with their designs. If the TC hoider's ICA applies to these repiacement parts, provide a statement noting such. If not, provide supplemental ICA per 14 CFR 5 2 1.SO. Make referral statements or supplemental ICA readily available per 14 CFR 8 21 SO. g Inspection District Ofice