6 Jim Reeves Manager, Atlanta M anufdg Inspection District Office. PMA No. PQ1682CE
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1 U.S. mpament of Transportatiod Wedera! Aviation Administration Smdl Airplane Directorate Atlanta Manufadaring bspection DPstdc4 W ~ c e One Cmwn Center, Suite Ph~nix~Boulevard, AtImta, GA June 29,2007 PMA No. PQ1682CE A='P~ 40 1 Century Ct Piney Flats, TN FEDERAL AVIATION ADIMIMSTRATION-PAm MANUFACTURER APPROVAL Per 14 CFR part 21, Subpart K, we found design data submitted with your letters dated (6ea) December 8,2006 and (2ea) January 15,2007, to meet the airworthiness requirements of the ~gu1ations for the products on which the^ parts are to be installed. We based our finding on test and computation. Also, we detded that your company set up the fabrication inspection system at, 401 Century Court, Piney Flats, Temesee a4 required by 14 CFR, (h). Therefore, we.grant parts m ~ ~ rapproval e r (PMA), which authorizes you to produce the replacement parts in the enclosed Supplement No. 3. We remind you that the provisions of 14 CFR, noted in our PMA letter of approval dated Jmm , also apply to the enclosed PMA Listing-Supplement Please keep the enclosed supplement with the original PMA letter as ewidence of approval to produce the psrtsconoerned. Sincerely, 6 Jim Reeves Manager, Atlanta M anufdg Inspection District Office
2 FEDERAL AVIATION ADMINISTRATION-PARTS MANUFACTURER APPROVAL ADpma, LLC 401 Century Ct. Piney Flats, TN PMA NO. PQ1682CE SUPPLEMENT NO, 29 DATE: 06/27/2007 part Name J%rt &~rnved Replacement Number For Part Number ADP Honeywell PM Spring, ADP Honeywell PM Washer - Spring, ADP I Honeywell P/N Was her - spring, Washer - ADP I Honeywell P/N Approved Basis and Ma kc MOM Approved Design Data Eli~ibllCtv McDonnell pet 14 CFR QWG NO_: ADP49146 =A m: 01/05/07 or later 28O[D], PM bstalled A319Model-111, per 14 CFR A3 19 Model , DWG NO; ADP49147 A319 Model -1 14, - A3 19 Model DATE: 08/16/06 or later , , A320 Mode1-2 12, A320 Made1-2 14, -23 1, -232, A320 M.odet -233 A321 Modd -1 I I, A32 1 Madel -1 12, A32 1 Model -2 1 I, SOO[A], Pm's , Jnstallcd, per 14 CFR When Honeywe11 ADP N/C BAIT$: 08/16/06 or later 28O[B], PM Instiilled. Test and computations McDomell per 14 CFR # 21,303 P-WG NO: ADP DATE: 08/I 6/06 or later Model CfTCP36-280[D], P/N I Installed.
3 Part Name ~ssembly - Part Number Anproved Re~lacernent For Part Number HoneywelI PM Basis and Apprm-peflign Data per 14 CFR $ I,Wg NO; ADP DATE: 01/09/07 or later _I - - Model Make Eliaibilitv Elt~ibility A319 Model -1 11, A319 Model -1 12, A319 Model -1 14, A319 Model -132 A320 Mode , A3 20 Model , -2 12, -2 14, -23 1, -232, -233 A32 1 Model -1 I J, A321 Madel -1 12, A321 Model -13 1, A321 Model , A321 Modal [A], PM's 4 Installed, Assembly Honeywell PM per 14 CFR DWG WO: ADP DATE: 01/09/07 or later Model QTCP36-280[B], PN hstalled. Assembly Honeywell PM per 14 CFR 22,303 DWG NO: ADP DATE: 0 1/09/07 or later McDonnell 280[D], PM Assembly Honeywell PM per 14 CFR 5 21,303 PWG NO; ADP49148 N/C DATE: 01/09/07 or later A319Model-111, A319 Model -1 12, A3 19 Model -1 14, A3 19 Model -132
4 Part Name - Part Approved Re~lacement Approved Basis and Number For Part Number Approved Dcslpn Data - Make Model Eli~ibllitv Eiipibilitv A321 Model -1 11, A321 Model - t 12, A32 1. Model - t 3 1, A32 1 Model , 3DO[A], PM's 3, , Instssllcd, Assembly ADP Honeywell PM per 14 CFR 5 21,303 BWG-NO: ADP49148 DATE: 01/09/07 or later When Iihneyvell Auxiliq Power Unit 2&0[13], PM i6- Assembly ADP Honeywell P/N per 14 CFR $ DWG NO: ADP49148 DL$=,:. 01/09/07 or later McDomell Men Honeywell Model GTCP [D], PM Nut ADP Honeywell P/N per 14 CFR DWG-NO: ADP PA-TE: 12/7/06 or later A319 Model-111, A3 19 Model , A3 19 Model , A3 19 Model A320 Mods1 A320 Mod01 A320,Model A32 1 Model , A321 Model -1 12, A32 1 Model , Awiliary Power Unit 300[A], P/N's 38002'78-3,
5 Part Name Part Amroved Replacement -is and Number For.Par$$amb.er, &proved Desipn Data Nut ADP Honeywe l P/N per 14 CFR i - ADP49153 PEV; N/C PATE: 12/7/06 or later Nut ADP49 t 53-1 Honeywell PM T~st and Computations pet 14 CFR 21,303 DWG NO: APP REV; N/C DATE: 12/7/06 or later ' Carbon ADP Honeywell P/N per 14 CFR $ DWG NO: ADP49155 DATE: 01/ 15/07 or later Carbon ADP Honeywell PM Test and Cornputations per 14 CFR PWG NO: ADP49155 BEY: N/C DATE; 0 1'1 5/07 or later Carbon Am Honeywell PM per 14 CFR QWG NO: ADP PAE 01/15/07 or later - Make Ellpibilitv McDonneIl McDonnell - Model Eliqibilib When Honeywe11 2SO[B], PM When Honeywe1 l Auxiliq Power Unit Model QTCP36-280[Dl, PM A319 Model -1 11, A319 Model -112, A3 19 Model -1 1'4, A319 ModeI , -2 1 I, -2 12, -214, -23 1, A320 ModeI +232, -233 A321 Modal -1 11, A32 t Model , A321 Model -21 1, When Honeywall ModeI GTCP [A], P/N's When Honeywe11 Awiiiary Power Unit Model GTCP [8], P/N Installed, Whan Honoywell Awciliruy Power Unit Model GTCP [D], P/N
6 Part Name Part Approved Replacement Number Por Part Number Shim, ADP Honeywell P/N Cornpressor Anproved Basis and Approved Design Data pet 14 CFR DWG NO; ADP491S6 REV: WC DATE: 08/ 16/06 or tater - - Make Model Eligibilit~ Eliyib&y A319 Model -t 11, A319 Model -1 12, A3 19 Model -1 14, A319 Model , -2 1 '1, , -2 14, -23 1, -232, -233 A321 Model -1 11, A321 Model -1 12, A32 1 Model -2 i 1,. Auiliary Power Unit 300[A]], P/NYs , Shim, ADP Honeywe11 P/N Test a11d Computations per 14 CFR QWG NO: APP CII ' DATE4 08/16/06 or later 280[B], PM Shim, ADP Honeywell P/N Shim, ADP491S6-2 Honeywell PM per 14 CFR DWG NO1 ADP DAm: 08/16/06 or later per 14CER DWG NO: ADP49156 DAn: 08/16/06 or later McDonnell 28O[P], PM A319 Model -1 11, A3 19 Model -1 12, A319 Model -114, A3 19 Model , -211, -212, -214, A320 M~de1-23 1, -232, -233
7 Part Mame Part Amroved Replacement Number For Part Number &,proved Basis ahd Make Model -inn Data EIi~lblllhr Eli~ibilitv A321 Model -1 11, A32 1 Model -1 12, A321 Model -13 1, A32 1 Model -27 1, 300[A], PM's , Installed, Shim, ADP Honeywell PM per 14 CFR $ DWG NO: ADP49156 DATE: 08/16/06 or later Series. 280[B], P/N Shim, ADP Honeywall PM Shim, ADP HoneywellP/N per 14 CFR DWG NO: ADP DATE,: 08/16/06 or later par 14 CFR DWG NO: ADP DATE: 08/16/06 or later McDonnell Auxiliq Power Unit 28O[b], PN Installed, A3 19 Model -1 11, A319 Model -112, A3 19 Model - 114, A319 Model , M20 Model , -2 12, A320 Modal , -23 1, -232, -233 A32 1 Model - 1 I I, A321 Model -1 12, A322 Model , A321 Made JOO[A], P/N's 4 Instatled.
8 Part Name Part &a rgved Realacem ent: Number For Part Number Shim, ADP Honeywel PM Approved Basis and, eoved Desipn Data per 24 CFR pwg,no: ADP48156 MV: N/C DATE: 08/16/06 or Iater Make Elieibi& Model: Elipibllitv Series Model GTCP [B], P/N Shim, ADF Honeywell PM per 14 CFR DWG NO: ADP DATE: 08/16/06 or later F M Approved revisions McDannelI When Honeyivell 280[D], PM Shim, ADP Honeywell PM Test and ~omputatians per 14 CFR PWG NQ; ADP49156 WVi N/C BATE: OE/l6/06 or later A3 19 Model -1 1 I, A319Model-112,. A3 19 Model , A319 Model , , A3 20 Model , -2 14, -23 1, -232, -233 A321 Model -1 11, A32 1 Model , A321 Model-131, A32 1 Model , A32 1 Model -23 I 300[Aj, PM's Shim, ADP Honeywell PM per 14 CFR $ DWG NO: ADP49156 ] DATE: 08/16/06 or Iater Boehg 737~300 Series 280[B], P/N
9 part.,name Part Ap~r9ve.d &$lacement Number For Part Number Shim, ADP Honeywell P/N Approved Basis and Approved De~ien Data per 14 CFR # DWG NO: APP49156 DATE: 08/16/06 or later Make gli~ib.i,iiw McDomoll - Model Elipibility When H~rtopvcll 280[D], PN Washer - ADP I Honeywell P/N Wavespring pet 14 CFR PWG NO: ADP RE JI.; N/C DATE: 08/17/06 or later A319 Model-1 11, A3 19 Mod , A319 Model dl 14, A3 19 Model , -21 I, -212, A320 Mod@! -2 14, -231, -2'32, ' -233 A321 Model-111, A32 1 Modd , A32 1 Model -I 3 1, A32 1 Model , A32 1 Model -23 I 300[A], P/N1s Washer - ADP Honeywell PM Wavespring Washer - A M 157- t Honeywell PM Wavespring per 14 CFR ADP49157 plv; N/C PATE: 08/17/06 Qr later per 14 CFR DWG NO: ADP DATE: 08/17/06 or later McDonnell Series When Honeywel 280[B], P/N Auxiliary Power U~it 280[D], P/N Gasket, ADP Honeywell PM Metal Test and Cornputati~ns per 14 CFR DWG NO: ADP TCEV: N/C PA=: 08/17/06 or later FAA Approved revisioss A319 Model -1 11, A319 Mode1-1 12, A3 19 Model -1 14, A3 29 Model -1 32
10 Part Name Part Amroved Re~Iacernent Approved Basis and Make - Model Number For Part Number A~vroved Desipn Data Eligibilitv Eliei bilitv A321 Model -1 11, A321 Mod , A321 Model -21 1, A321 Model Auxiliq Powct Unit 300[A],PM9s.. Gasket, ADP Honeywell Y/N Baeing Metal per 14 CFR DWG NO; ADP49158 REV: NIC DATE: 08/17/06 or later Gasket, ADP Honeywell PCN McDonnell Metal per 14 CFR $ DWG NO: ADP49158 P-V; NIC -' DATEa 08/17/06 or lator When Honeywet1 Auxiliary Power Uliit 280[B], PN I Installed, Awciliay Power Unit 280[D], P/N hstalled. NOTE: 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. If TC holder's ICA applies to these replacement parts, provide a statement noting such. If not, provide supplementary ICA per 14 CFR m/q, A9.r lj in D. Taylor, Manager Atlanta Jim Reeves, Manager Atlanta r - Aircraft Certification Office Manufacturing Inspection District Office
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Page 1 2009-26-03 BOEING Amendment 39-16138 Docket No. FAA-2009-0911; Directorate Identifier 2002-NM-12-AD PREAMBLE Effective Date (a) This AD becomes effective February 1, 2010. Affected ADs (b) None.
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[Federal Register: November 4, 2002 (Volume 67, Number 213)] [Rules and Regulations] [Page 67104-67106] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr04no02-6] DEPARTMENT
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[Federal Register Volume 81, Number 112 (Friday, June 10, 2016)] [Rules and Regulations] [Pages 37492-37494] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
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[Federal Register Volume 83, Number 211 (Wednesday, October 31, 2018)] [Rules and Regulations] [Pages 54663-54665] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR
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2013-18-09 Honeywell ASCa Inc.: Amendment 39-17582. Docket No. FAA-2013-0707; Directorate Identifier 2013-NM-158-AD. (a) Effective. Date This AD becomes effective October 3, 2013. (b) Affected ADs None.
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[Federal Register Volume 76, Number 101 (Wednesday, May 25, 2011)] [Rules and Regulations] [Pages 30253-30254] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc
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