Salt River Aviation, LLC 175 S. Hamilton Place #112 Gilbert, AZ Phone: (480) Fax: (480) B APU MINI PACK

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1 Salt River Aviation, LLC 175 S. Hamilton Place #112 Gilbert, AZ Phone: (480) Fax: (480) B APU MINI PACK APU Model/ Part Number B/ APU Serial Number P-1301 Total Time since New 35,817 Total Cycles since New 21,382 Date of Last Shop Visit June 2, 2016 Time Since Overhaul: 0 Hrs Cycles Since Overhaul: 0 Cycles Commercial Trace Singapore Airlines All Technical Data included in this Mini Pack is based on information provided by FAA/OEM approved repair stations and the Operators Maintenance Program. Honeywell removed all PMA and DER parts from this APU during the last shop visit. All material is OEM only. Aaron M Putman 10/4/2016 Aaron M. Putman Date

2 TO WHOM IT MAY CONCERN com scr/os/2o15/88 I b.luly zots ACCTDENT & INCIDENT STATEMENT - BOEING 777-2OO AIRCRAFT: 9V-OTB (MSN 28508) ("Aircraft") FITTED WITH MLG SERIAL NUMBERS MC0252P0122 AND MC0251P0122, NLG SERIAL NUMBER MCOOglPOO86 AND APU SERIAL NUMBER P.l301. The Aircraft was delivered new f rom Boeing Commercial Airplane Group on 18 July 1997 and had been in operation with Singapore Airlines Limited ("SlA") until its delivery to SCOOT Pte. Ltd. ("SCOOT") on 21 August Subsequytly, SCOOT had operated the Aircraft until its delivery to AerSale lncorporated ("AerSale") on O July This statement certifies that the Aircraft has not been subjected to any Accident or lncident as defined in ICAO Annex 13, subjected to sudden impact, severe stress, fire, severe temperature, immersion in sa1 water or exposure to corrosive agents. ln addition, the Aircraft has not been operated by the Government of Singapore or been in military service. We hereby conf irm that, to the best of our knowledge and belief and, based on the review of available records that the above referenced Aircraft has been operated within its Airplane Flight Manual operational limits throughout the period of operation. This letter does not constitute a warranty, guarantee or representation by SCOOT and no legal obligation, whether arising in contract or tort is assumed by SCOOT to AerSale, its affiliates, officers, emfloyees or agents or any third party and no liability shall be imposed on SCOOT as a consequence of the statements made in this letter. This letter is also declared based on the understanding that the aircraft will not be used by AerSale in the operation of service revenue flights. The legal relationship between you and SCOOT under which this letter is provided is governed solely by theierms of the purchase Agreement, datedajune 2015 as amended. Yours lly Khoong Wei Jack Manager Quality WE ACKNOWLEDGE RECEIPT OF THIS LETTER PBN KA S4 NB4QN '4TYr1 SR, ryla-o Aq e R RO F47 and on behalf of AerSale lncorporated Scoot Pte Ltd Changi Airport Post Office, PO Box 89, Singapore Reg. No.: 20' W

3 SINGAPORE AIRLINES LIMITED M TO WHOM IT MAY CONCERN vpq/m/169r-r 21 August 2012 STATEMENT OF NON INCIDENCE AND ACCIDENT @ AIRCRAFT:9V-SQB (MSN: 28508) ("Aircraft" FITTED WITH ROI-LS ROYCE TRENT 884 ENGINES (SN: AND (Engines) The aircraft was delivered new from Boeing Commercial Airplane Group on 18 July 1997 and has been in operation with Singapore Airlines Limited ("SlA") until its delivery 2l August 2012 to SCOOT Pte. Ltd. 2 This is to indicate that to the best of our knowledge and belief, after review of all the available Aircraft and Engine records, the above stated aircraft and its installed engine had not experienced any major incident or accident that had required to undergo major structural repair. 3 This letter does not constitute a warranty, guarantee or representation and no legal obtigation whether arising in contract or tort to SCOOf Pte. Ltd., its affiliates, officers, employees or agents or any third party shall be imposed on SIA as a consequence of the statements made in this letter. The legal relationship between you and us for the sale of the Aircraft is governed solely by the terms of the Sale Agreement, as amended. Yours faithfully (&, Lawrence Lim Vice President Quality WE RECEIPT OF THIS LETTER. KHaaNQ LEl J ACK fdlrrgq.ffi 62*1*tffY on behalf of SCOOT PTE. LTD Airmail Tiansit Centre P o Box 501, Singapore Cable: SINAIRLINE Telex: Airline House,25 Airline Road, Shgapore Telephone: (65) singaporc Company Registration No: 19720O078R s r ngoporcor r. com A S- l Ai i i \.r MtlvB:I1

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6 Honeywell Aerospace Trading APU SUMMARY SHEET SERIAL MODEL: B PART NUMBER: P-1301 NUMBER: CONDITION: Overhaled TRACE TO : SCOOT CERTIFIED BY: Honeywell CERTIFIED DATE: June 2, 2016 LOCATION: Raunheim PRESERVATION: Yes, June 2, 2018 APU TIMES TSN: CSN: TSO: 0 CSO: 0 TSR: 0 CSR: 0 PART NUMBER SERIAL NUMBER DESCRIPTION TSN CSN LIMIT TIME REMAIN CYCLES REMAIN LC IMPELLER CYC N/A ST IMPELLER CYC N/A ND IMPELLER CYC N/A ST TWHEEL CYC N/A ND T WHEEL CYC N/A RD T WHEEL CYC N/A INTERNAL REF : NOTES : Learn more For additional information, please visit or contact:

7 Engineering Disposition Report B P Honeywell Aerospace GmbH DE Prepared By: Frauke Frahm Printed On : Page 1 Of 6

8 Model Number : B Serial Number : P-1301 Notification : Repair Facility : Maintenance Organization # : Honeywell Aerospace GmbH DE FINAL - FINDINGS REPORT Customer : Honeywell Aerospace Trading Customer P/O : Notification : Induction Date : Model No : GTCP B Installed Date : Part Number : Series : 33 Removal Date : Serial No In : P-1301 Mods : Mod to S/N : P-1301 TIMES / CYCLES HH.DD (HH:MM) Time Since New: (35817:33) Cycles Since New: Time Since Repair: (654:55) Cycles Since Repair: Time Since Last Shop Visit: (654:55) Cycles Since Installation: AIRCRAFT INFORMATION CUSTOMER INFORMATION Sales Order No: Aircraft/Application Model: BOEING B777 REMOVAL INFORMATION Low Time Removal: No Removal Type: Not unscheduled(other) RETURN REASON Primary Removal Reason: REPAIR AS NECESSARY TO CERTIFY OVERHAUL.. INDUCTION FINDINGS General Information Engine nameplates missing No Page 2 Of 6

9 Model Number : B Serial Number : P-1301 Notification : Repair Facility : Honeywell Aerospace GmbH Maintenance Organization # : DE Engine nameplate data mismatch Additional customer hardware received QEC parts installed Generator assy installed Findings 1st external condition APU rotation Missing APU Hardware No Yes No No Clean and dry condition Rotating free Yes Oil System Investigation APU received with oil Lube filter element missing Lube filter element condition Gen scavenge filter element missing Gen scavenge filter element condition Gearbox oil sump MCD condition Gen scavenge MCD condition Midframe scavenge MCD condition Turb brg scavenge MCD condition Air turb starter MCD condition Speed monopols condition Oil tubes condition No No No Normal/Clean Normal/Clean Normal/Clean Normal/Clean Normal/Clean Tips in good condition Fuel System Investigation Fuel filter element missing Fuel filter element condition Fuel tubes/hoses/nozzles condition No Normal/Clean Outline Investigation Findings on inlet plenum Findings on grounding straps Findings on inlet screen Findings on bleed duct Findings on bleed duct clamps Findings on surge ducts Findings on surge duct clamps Findings on surge control valve Findings on pneumatic tubes Findings on bleed check valve Findings on ATS duct Findings on air turbine starter Dry Inlet plenum straps torn / frayed Dry Dry Page 3 Of 6

10 Model Number : B Serial Number : P-1301 Notification : Repair Facility : Honeywell Aerospace GmbH Maintenance Organization # : DE Findings on ATS clutch shaft Findings on electrical starter motor Findings on e-starter clutch shaft Findings on oil cooler Findings on wiring harness Findings on ignition box Findings on ignition lead (short) Findings on ignition lead (long) Findings on igniter plug (2ea) Findings on thermocouples Findings on exhaust pipe Findings on gearbox vent tube Normal wear Wiring harness slightly oil and dirt con Lightly contaminated with oil Gearbox Investigation Generator pad rubber seal missing Generator pad cover missing Findings on gearbox (external) Findings on clutch housings Findings on clutch gears Findings on air/oil separator seal rotor No Yes Port oil wetted Load Compressor Investigation Findings on load compressor (external) Findings on IGV assembly No Power Section Investigation Findings on engine mount adaptation Findings on thermal blankets Findings on turbine bearing area Boroscope Inspection Borescope Required? No FAILURE DATA Failure Description : The APU was received for overhaul following a change of ownership. The APU was completely disassembled and inspected to zero time. All life limited parts were replaced by new hardware due to customer Page 4 Of 6

11 Model Number : B Serial Number : P-1301 Notification : Repair Facility : Honeywell Aerospace GmbH Maintenance Organization # : DE request.. Part Number Part Name Condition Findings Primary Failure IMPELLER, Low YES COMPRESSOR, LOAD TURBINE ROTOR Low YES ASSY 3RD STAGE ROTOR ASSY TURB - Low YES 2STG ROTOR ASSY 1STG Low YES IMPELLER, COMPRESSOR, SECOND STAGE Low YES DISPOSITION SUMMARY Work Accomplished: 1) Disassembled power section completely and performed parts inspection per applicable manual zero time requirements. 2) Replaced all life limited parts due to customer request. 3) Disassembled load compressor completely and performed parts inspection per applicable manual zero time requirements. 4) Disassembled gearbox completely and performed parts inspection per applicable manual zero time requirements. 5) Modified gearbox assembly per SB ) Performed parts inspection of remaining disassembled hardware per applicable manual continuous time requirements. 7) Performed final test per applicable manual requirements. Power Section Workscope Performed: Gearbox Workscope Performed: Load Compressor Workscope Performed: General Workscope Performed: DISPOSITION SUMMARY. Heavy Heavy Heavy Heavy Page 5 Of 6

12 Model Number : B Serial Number : P-1301 Notification : Repair Facility : Honeywell Aerospace GmbH Maintenance Organization # : DE Customer Confirmed Removal Reason: Yes FINDINGS As Received Condition: APU S/N P-1301 was returned for overhaul following change of ownership. The APU was received in externally clean condition. The inspection of the APU outline did not revealy and significant findings. The inspection of the oil system did not reveal any findings with regard to contamination. A borescope inspection was not performed since the overhaul requirement did call for a complete disassembly of the APU.. One Line Findings: Overhaul unit Page 6 Of 6

13 P Data Conversion For ENGINE S/N P1301 WINDMM.EXE Version B Production Version Item Count NUMBER ENTRIES IN DMM 2 SW Version ECB SOFTWARE VERSION 3 APUser.pre P P APU SERIAL NUMBER PREFIX 4 APUser.num APU SERIAL NUMBER (FIRST 2 DIGITS) 5 APUser.num APU SERIAL NUMBER (NEXT 2 DIGITS) 6 APUser.num APU SERIAL NUMBER (NEXT 2 DIGITS) 7 APUser.num APU SERIAL NUMBER (LAST 2 DIGITS) 8 APUser.suf APU SERIAL NUMBER (SUFFIX 2 DIGITS) 9 APUhours HOURS 10 APUminutes MINUTES 11 APUcycles CYCLES 12 ATSSTRT NUMBER OF ATS STARTS 13 FLTSTRT NUMER OF INFLIGHT STARTS 14 ABSTRT NUMBER OF UNSECCESSFUL STARTS 15 ABATSSTRT NUMBER OF ATS UNSUCCESSFUL STARTS 16 ABFLTSTRT NUMBER OF UNSUCCESSFUL INFLIGHT STARTS 17 TURBHOUR HOURS SINCE TURBINE REPAIR 18 LCHOUR HOURS SINCE LOAD COMPRESSOR REPAIR 19 ECHOUR HOURS SINCE ENGINE COMPRESSOR REPAIR 20 ECSHOUR OPERATING HOURS IN ECS 21 ECSMINUTES OPERATING MINUTES IN ECS 22 NMES NUMBER OF MES 23 ADPTIM OPERATING HOURS IN ADP 24 ADPECSTIM OPERATING HOURS IN ADP & ECS 25 FLTTIM OPERATING HOURS INFLIGHT 26 HOTTIM OPERATING HOURS T2 > 100 DEGF 27 CLDTIM OPERATING HOURS T2 < 0 DEGF 28 HISTRT "START ATTEMPTS > 25,000 FT" 29 BRR START ATTEMPTS TOIL < 0 DEGF 30 BRRRR 0 0 START ATTEMPTS TOIL < -40 DEGF 31 NLOP 0 0 NUMBER OF LOP SHUTDOWNS 32 N3LOP 0 0 NUMBER OF 3 CONSECUTIVE LOP SHUTDOWNS 33 NCLOP 0 0 NUMBER OF CURRENT CONSECUTIVE LOP SDNS 34 NHOT NUMBER OF HIGH OIL TEMP SHUTDOWNS 35 NFLTSD NUMBER OF INFLIGHT AUTO SHUTDOWNS 36 AKWECS(1) AVERAGE GEN LOAD ECS KW * 37 AKWECS(2) AVERAGE GEN LOAD ECS KW 38 AKWMES(1) AVERAGE GEN LOAD MES KW * 39 AKWMES(2) AVERAGE GEN LOAD MES KW 40 AKWADP(1) AVERAGE GEN LOAD ADP KW * 41 AKWADP(2) AVERAGE GEN LOAD ADP KW 42 AKWAE(1) AVERAGE GEN LOAD ADP & ECS KW * 43 AKWAE(2) AVERAGE GEN LOAD ADP & ECS KW 44 AKWFLT(1) AVERAGE GEN LOAD INFLIGHT KW * 45 AKWFLT(2) AVERAGE GEN LOAD INFLIGHT KW 46 AT4ECS(1) AVERAGE T4 ECS DEG F* 47 AT4ECS(2) AVERAGE T4 ECS DEG F 48 AT4MES(1) AVERAGE T4 MES DEG F* 49 AT4MES(2) AVERAGE T4 MES DEG F 50 AT4ADP(1) AVERAGE T4 ADP DEG F* 51 AT4ADP(2) AVERAGE T4 ADP DEG F 52 AT4AE(1) AVERAGE T4 ADP & ECS DEG F* 53 AT4AE(2) AVERAGE T4 ADP & ECS DEG F 54 AT4FLT(1) AVERAGE T4 INFLIGHT DEG F* 55 AT4FLT(2) AVERAGE T4 INFLIGHT DEG F 56 T HOURS T4 > 1900 DEG F 57 T HOURS T4 > 1950 DEG F 58 T HOURS T4 > 2000 DEG F 59 T HOURS T4 > 2050 DEG F 60 T HOURS T4 > 2100 DEG F 61 RECT4R HIGHEST T4 ONSPEED DEGF 62 RECT4S HIGHEST T4 DURING START DEGF Seite 1

14 P NNUDGE_ERR NUMBER OF OCCURANCES OF NUDGE ERR 64 PREV_MVTRIM FUEL METERING VALVE TRIM ADJ % 65 IGVPERFADJ IGV PERFORMANCE ADJUSTMENT DEG 66 SCSETADJ 0 0 SURGE CONTROL SCHEDULE ADJ LB P SEC 67 CT5MESF FILTERED AVERAGE CT5 DURING MES D 68 MDNCT5MES MAIDEN CT5 DURING MES DEGF 69 CT5MES CT5 DURING MES AT 500 HOURS DEGF 70 CT5MES CT5 DURING MES AT 1000 HOURS DEGF 71 CT5MES CT5 DURING MES AT 1500 HOURS DEGF 72 CT5MES CT5 DURING MES AT 2000 HOURS DEGF 73 CT5MES CT5 DURING MES AT 2500 HOURS DEGF 74 CT5MES CT5 DURING MES AT 3000 HOURS DEGF 75 CT5MES CT5 DURING MES AT 3500 HOURS DEGF 76 CT5MES CT5 DURING MES AT 4000 HOURS DEGF 77 CT5MES CT5 DURING MES AT 4500 HOURS DEGF 78 CT5MES CT5 DURING MES AT 5000 HOURS DEGF 79 CT5MES CT5 DURING MES AT 5500 HOURS DEGF 80 CT5MES CT5 DURING MES AT 6000 HOURS DEGF 81 CT5MES CT5 DURING MES AT 6500 HOURS DEGF 82 CT5MES CT5 DURING MES AT 7000 HOURS DEGF 83 CT5MES CT5 DURING MES AT 8000 HOURS DEGF 84 CT5MES CT5 DURING MES AT 9000 HOURS DEGF 85 CT5MES CT5 DURING MES AT HOURS DEG 86 CT5COOLF FILTERED AVERAGE CT5 DURING COOLD 87 MDNCT5COOL MAIDEN CT5 DURING COOLDOWN DEGF 88 CPTMESF FILTERED AVERAGE CPT DURING MES PSIA 89 MDNCPTMES MAIDEN CPT DURING MES PSIA 90 CPTMES CPT DURING MES AT 500 HOURS DEGF 91 CPTMES CPT DURING MES AT 1000 HOURS DEGF 92 CPTMES CPT DURING MES AT 1500 HOURS DEGF 93 CPTMES CPT DURING MES AT 2000 HOURS DEGF 94 CPTMES CPT DURING MES AT 2500 HOURS DEGF 95 CPTMES CPT DURING MES AT 3000 HOURS DEGF 96 CPTMES CPT DURING MES AT 3500 HOURS DEGF 97 CPTMES CPT DURING MES AT 4000 HOURS DEGF 98 CPTMES CPT DURING MES AT 4500 HOURS DEGF 99 CPTMES CPT DURING MES AT 5000 HOURS DEGF 100 CPTMES CPT DURING MES AT 5500 HOURS DEGF 101 CPTMES CPT DURING MES AT 6000 HOURS DEGF 102 CPTMES CPT DURING MES AT 6500 HOURS DEGF 103 CPTMES CPT DURING MES AT 7000 HOURS DEGF 104 CPTMES CPT DURING MES AT 8000 HOURS DEGF 105 CPTMES CPT DURING MES AT 9000 HOURS DEGF 106 CPTMES CPT DURING MES AT HOURS DEGF 107 LCFLC(1) LCF LOAD COMPRESSOR STAGE 1* 108 LCFLC(2) LCF LOAD COMPRESSOR STAGE LCFEC1(1) LCF ENGINE COMPRESSOR STAGE 1* 110 LCFEC1(2) LCF ENGINE COMPRESSOR STAGE LCFEC2(1) LCF ENGINE COMPRESSOR STAGE 2* 112 LCFEC2(2) LCF ENGINE COMPRESSOR STAGE LCFTUR1(1) LCF TURBINE STAGE 1* 114 LCFTUR1(2) LCF TURBINE STAGE LCFTUR2(1) LCF TURBINE STAGE 2* 116 LCFTUR2(2) LCF TURBINE STAGE LCFTUR3(1) LCF TURBINE STAGE 3* 118 LCFTUR3(2) LCF TURBINE STAGE SR1(1) S-R TURBINE STAGE 1* 120 SR1(2) S-R TURBINE STAGE SR2(1) S-R TURBINE STAGE 2* 122 SR2(2) S-R TURBINE STAGE SR3(1) S-R TURBINE STAGE 3* 124 SR3(2) S-R TURBINE STAGE APU_OPTIONS APU OPTIONS BIT 0: TRUE Oil Heater BITE Disable Seite 2

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