DEPARTMENT OF TRANSPORT ATIONFEDERAL AVIATION ADMINISTRATION
Los Angeles Manufacturing Inspection District Office3960 Paramount Boulevard Suite-l 00Lakewood, California 90712-4137
U.S Departmentof Transportation
Federal AviationAdministration
October 19,2012
Mrs. Nancy Johnson, General ManagerNew Horizons308 East Franklin Avenue #BEI Segundo, California 90245 ,~
~FEDERAL AVIATION ADMINISTRATION - PARTS MANUFACTURER APPROVAL
Dear Mrs. Johnson:
In accordance with the provisions of Title 14, Code of Federal Regulations (14 CFR), Part 21,Certification Procedures for Products, Articles, and Parts, subpart K, the FAA has found that thedesign data, based on Test & Computations submitted by New Horizons, with your letter datedJuly 12, 2012, meets the airworthiness requirements of the regulations applicable to the productson which the parts are to be installed. Additionally, the FAA has determined thatNew Horizons has established the fabrication inspection system required by § 21.307 at308 East Franklin Avenue #B, EI Segundo, California 90245. Accordingly, Parts ManufacturerApproval (PMA) is hereby granted for production of the replacement parts listed in the enclosedAmended Supplement No.6.
You are reminded that the provisions of 14 CFR, parts 21 and 45, noted in our PMA letter ofapproval dated May 27, 2008, also apply to the enclosed Amended PMA Listing-SupplementNo.6. The enclosed supplement should be retained with the original PMA letter as evidence ofapproval to produce the parts concerned.
Sincerely,
Aure SilvaLos Angeles Manufacturing InspectionDistrict Office, ANM-l 08L
Enclosure:Amended PMA Listing Supplement No.6
Page 1 of2
FEDERAL AVIATION ADMINISTRATION - PARTS MANUFACTURER APPROVAL
NEW HORIZONS PMA NO: PQ2039NM308 EAST FRANKLIN AVENUE #B SUPPLEMENT NO: 6EL SEGUNDO, CALIFORNIA 90245 DATE: OCTOBER 12,2012
APPROVEDREPLACDIENT
PART FOR APPROVAL BASIS AND MAKE MODELPART NAME ~Vl\lBER PART :'tIl;MBER APPROVED DESIGN DATA ELlGIRILlTY ELIGIBILITY
Kit, Ignition SOS218NH SOS218 Test & Computation per 14 CFR Engine Alliance GP7200Lead § 21.303
DwgNo: SOS218NHRev: NoneDate: 7/9/12, or later FAAapproved revisions
Kit, Ignition 9043876NH 9043876 Test & Computation per 14 CFR CFM International CFMS6-2A, -28, -2C,Lead § 21.303 -38, -3C, -SA, -S8, -SC
DwgNo: 9043876NH ;-Rev: None
t
Date: 7/9/12, or later FAAapproved revisions
Kit, Ignition 9043877NH 9043877 Test & Computation per 14 CFR CFM International CFMS6-78Lead § 21.303
DwgNo: 9043877NHRev: NoneDate: 7/9/12, or later FAAapproved revisions
Kit, Ignition KSI2688NH KS12688 Test & Computation per 14 CFR General Electric CF34-IOALead § 21.303
DwgNo: K512688NHRev: NoneDate: 7/9/12, or later FAAapproved revisions
Kit, Ignition 503883NH 503883 Test & Computation per 14 CFR General Electric CF34-IOELead § 21.303
Dwg No: 503883NHRev: NoneDate: 7/9/12, or later FAAapproved revisions
Kit, Ignition 510889NH 510889 Test & Computation per 14 CFR General Electric GEnx-2867, -28678Lead § 21.303
DwgNo: 510889NHRev: NoneDate: 7/9/12, or later FAAapproved revisions
Page 2 of2
FEDERAL AVIATION ADMINISTRATION - PARTS MANUFACTURER APPROVAL
NEW HORIZONS308 EAST FRANKLIN AVENUE #BEL SEGUNDO, CALIFORNIA 90245
PMA NO: PQ2039NMSUPPLEMENT NO: 6DATE: OCTOBER 12,2012
PART NAMEI'ART
:'oIl'MBER
APPROVF])REPLACEMENT
H)RPART N{!MBER
APPROVAL BASIS A"InAPPROVEn nESIG~ nATA
MAKEELIGIBILITY
MonELELIGIBILITY
Kit, IgnitionLead
9043875NH 9043875 Test & Computation per 14 CFR§ 21.303Dwg No: 9043875NHRev: NoneDate: 7/9/12, or later FAAapproved revisions
General Electric CF6-50, -80A I/A21A3-80C2A II A21A31A5IA8, -80C2A5F,-80C28 1/82,84/86,-80C28 IF/82F/84FI86F/86FA/87F,-80C2DIF, -80C2LIF
Kit, IgnitionLead
9043884NH 9043884 Test & Computation per 14 CFR§ 21.303Dwg No: 9043884NHRev:
General Electric CF6, -6, -50
Date:None7/9/12, or later FAA
.;I
approved revisions
Kit, Ignition 9043878NH 9043878 Test & Computation per 14 CFR General Electric GE90-768, -778, -858,Lead § 21.303 -908, -948, -11081,
DwgNo: 9043878NH -1138,-1158Rev: NoneDate: 7/9/12, or later FAAapproved revisions
Kit, Ignition 9043889NH 9043889 Test & Computation per 14 CFR International Aero V2500-A I, -A5, -05Lead § 21.303 Engines
DwgNo: 9043889NHRev: NoneDate: 7/9/12, or later FAAapproved revisions
NOTE:
1) Provide minor design changes in a manner as determined by the ACO. Handle major design changes to drawingsand specifications in the same manner as that for an original FAA-PMA.
2) The FAA approved ICA for the above parts with their designs. These ICA may refer to those of the respectiveparts from the holders of type certificates. Otherwise, provide supplementallCA for differences in thereplacement parts. Make referral statements or supplementallCA readily available per 14 CFR 21.50./lM,(' / j
, : l!!lLt(~f{~ Wanda A. Kimuraomas A. Enyart
Manager, Propulsion BranchLos Angeles Aircraft Certification Office
Manager, Los AngelesManufacturing Inspection District Office