STC ST04732NY

An (Ref. 1414 CFR 21.120).

FAAAA 8110-2 (10/24) Page 1 of ___ ST04732NY Space Exploration Technologies Corp./Starlink Aviation 8550 Case Road McGregor, TXTX76657 2525 Title 1414 Code ofof Federal Regulations A46NM Airbus SAS A330-200 Series, A330-300 Series

(1) The installer must determine whether this design change isis compatible with previously approved modifications.

(2) IfIf the holder agrees totopermit another person toto use the certificate totoalter the product, the holder must give the other person written evidence ofof that permission.

(Limitations and Conditions Continued onon Page 3)3) December 23, 2022 June 21, 2024 June 14, 2024 January 22, 2025 February 27, 2026 6 Installation ofof DualSpaceX Starlink Aviation Systeminin accordance with (1) Master DataList (MDL) SPX-00005895, ver5.0, dated February 26,2026, ororlater FAA approved revision. (2.1)Instructions for Continued Airworthiness (ICA) SPX-00005689, ver 6.0,dated February 25,2026, ororlater FAA accepted revision. (2.2)ICA for STC DeModification SPX-00006554, ver2.0, dated December 19, 2024,ororlater FAA accepted revision. The applicable ICA shallbebe made available toto theoperator atatthe time ofofinstallation and bebe incorporated intothe operatorsmaintenance program.

(Description ofofType Design ChangeContinued ononPage 3)3) ODA Administrator, ODA-635882-NM Digitally signed by: Sally Robinson DN: CN = Sally Robinson email = sally.robinson@aeromechinc.co m C = US OU = AeroMech ODA Date: 2026.02.27 18:02:11 -08'00' Sally Robinson

: The transfer endorsement below may be used to notify the appropriate FAA Aircraft Certification Office of the transfer of this Supplemental Type Certificate. The FAA will reissue the certificate in the name of the transferee and forward it to him.

(Name and address of transferee):

(Name and address of grantor):

An (Ref. 1414 CFR 21.120).

An (Ref. 1414 CFR 21.120).

(3.1)AircraftFlightManualSupplement(AFMS)U10-0720,RevIR,datedJune13,2024,ororlaterFAA approvedrevision(3.2)AircraftFlightManualSupplement(AFMS)SPX-00011036,Rev1.0,dated February25,2026,ororlaterFAAapprovedrevision.Theconfiguration-specificAFMSisisrequiredand mustbebecarriedduringallflights.

LimitationsandConditions(continuedfromPage1):

(3)ThisSTCisisapplicabletotoallserialnumbersofofAirbusSASModelA330-200SeriesandA330-300 Seriesaircraft.

(4)ThesysteminstalledbybythisSTCisisintendedtotoprovideanon-essential,non-requiredinternet connectiontotoportableelectronicdevices(PED).Useofofthissystemforanyotherpurposeororconnection ofofthissystemtotootheronboardequipmentmayrequireadditionalregulatoryapproval.

(5)OperationalapprovaltotopermituseofofPortableElectronicDevices(PED)isisnotpartofofthisSTC.

CertificationBasis(A330-200Series):

Basedonon1414CFR§21.115and§21.101,andtheFAApolicyfordesignchangesthatareidentifiedasas notsignificantininFAAOrder8110.48,thecertificationbasisforAirbusSASModelA330-200Seriesisis asasfollows:

(1)ThetypecertificationbasisforpartsnotchangedorornotaffectedbybythechangeisisshownononTCDS A46NM.

(2)Themodificationcertificationbasisforpartschangedororaffectedbybythechangeisisasasfollows:

CertificationBasis(A330-200Series)continuedononpage4 3 6

An (Ref. 1414 CFR 21.120).

FAA 8110-2 (10/24) Page of ___ ST04732NY February 27, 2026 CertificationBasis(A330-200Series):(continuedfrompage3)3) 1414CFRPart2525regulationsatattheamendmentlevelininTCDSA46NM:

1414CFR25.29,25.121(a)(b)(c)(d),25.123(b),25.251(a)(b)(c)(d),25.301(a)(b),25.303,25.307(a),

25.337(a)(b)(c),25.581,25.601,25.603(a)(b)(c),25.605(a),25.609(a)(b),25.611,25.623,

25.625(a)(b)(c),25.629,25.771(a),25.773(a)(2),25.777(a),25.789(a),25.1301,25.1307(c),25.1309(a),

25.1351(a)(1),25.1357(a)(c),25.1381(a)(b),25.1401(b),25.1419(a),25.1501(a)(b),25.1529,

25.1541(a)(1)(b),25.1555(a),25.1581(a)(2)(d),25.1587(b).

1414CFRPart2525regulationsatatananintermediateamendmentlevel:

1414CFR25.111(c)(1)(3)(i)amdt25-94,25.119(a)amdt25-94,25.341(a)amdt25-86,

25.365(a)(b)(d)(e)amdt25-87,25.571(a)(b)(e)(1)amdt25-96,25.853(a)amdt25-83,

25.869(a)(4)amdt,25-113,25.901(c)amdt25-126,25.903(c)amdt25-140,25.1353(a)(d)amdt25-113.

1414CFRPart2525regulationsatatamendmentlevel25-0through25-153:

1414CFR25.115(b)(1),25.305(a)(b)(e)(f),25.321,25.333(a),25.335,25.561(a)(b)(3)(c),25.613(a)(b),

25.899,25.1431(c),25.1583(c)(1),25.1585(a)(1)(b)(2).

(3)Compliancehasbeendemonstratedtoto1414CFRPart26.11(c)amdt26-7and1414CFRpart26.47(c) amdt26-7.

(4)EquivalentLevelofofSafetyFindingshavebeenmadeforthefollowingregulation(s):§25.251 Vibrationandbuffeting(documentedininP&SELOSMemoADC-0137-F-1).

(5)EquivalentLevelofofSafetyFindingshavebeenmadeforthefollowingregulation(s):§25.773(a)(2), PilotCompartmentView(documentedininP&SELOSMemoODA-ADC-0137-SE-1).

An (Ref. 1414 CFR 21.120).

Basedonon1414CFR§21.115and§21.101,andtheFAApolicyfordesignchangesthatareidentifiedasas notsignificantininFAAOrder8110.48,thecertificationbasisforAirbusSASModelA330-300Seriesisis asasfollows:

(1)ThetypecertificationbasisforpartsnotchangedorornotaffectedbybythechangeisisshownononTCDS A46NM.

(2)Themodificationcertificationbasisforpartschangedororaffectedbybythechangeisisasasfollows:

1414CFRPart2525regulationsatattheamendmentlevelininTCDSA46NM:

1414CFR25.29,25.123(b),25.251(a)(b)(c)(d),25.301(a)(b),25.303,25.337(a)(b)(c),25.581,25.601,

25.603(a)(b)(c),25.605(a),25.609(a)(b),25.611,25.623,25.629,25.771(a),25.777(a),25.789(a),

25.1301,25.1309(a)(b),25.1357(a)(c),25.1401(b),25.1501(a)(b),25.1529,25.1541(a)(1)(b),25.1555(a),

25.1587(b).

1414CFRPart2525regulationsatatananintermediateamendmentlevel:

1414CFR25.111(c)(1)(3)(i)amdt25-94,25.119(a)amdt25-94,25.121(a)(b)(c)(d)amdt25-84,

25.307(a)amdt25-72,25.341(a)amdt25-86,25.365(a)(b)(d)(e)amdt25-87,

25.571(a)(b)(e)(1)amdt25-96,25.773(a)(2)amdt25-72,25.853(a)amdt25-83,

25.869(a)(4)amdt25-113,25.901(c)amdt25-126,25.903(c)amdt25-140,25.1353(a)(d)amdt25-113,

25.1419(a)amdt25-72.

1414CFRPart2525regulationsatatamendmentlevel25-0through25-153:

1414CFR25.115(b)(1),25.305(a)(b)(e)(f),25.321,25.333(a),25.335,25.561(a)(b)(3)(c),25.613(a)(b),

25.625(a)(b)(c),25.899,25.1431(c),25.1307(c),25.1351(a)(1),25.1381(a)(b),25.1581(a)(2)(d),

25.1583(c)(1),25.1585(a)(1)(b)(2).

CertificationBasis(A330-300Series)continuedononpage6 5 6

An (Ref. 1414 CFR 21.120).

(3)Compliancehasbeendemonstratedtoto1414CFRPart26.11(c)amdt26-7and1414CFRpart26.47(c) amdt26-7.

(4)EquivalentLevelofofSafetyFindingshavebeenmadeforthefollowingregulation(s):§25.251(b) Vibrationandbuffeting(documentedininELOSMemorandumAMI-PRG-0411-02-T-25.251).

----------------------------------------------------END----------------------------------------------------- 6 6