N4873U

Part: CAP — MISSING (FUEL PANEL) · airframe 52,459 hrs · 32,971 cycles

FUEL CAP IS MISSING REPORTED FUELER TO OPS. TOMC BROADSTONE UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INSPECT FUEL CAP FOR LEAK AND APPLY CDL MAC METER INITIATED FOR WITH VENDOR ID V925027. NSPECTED COUPLING FOR LAEKS AND INSTALLED PLACARD. INSPECTED COUPLING FOR LAEKS AND INSTALLED PLACARD 4380493 REF CDL 28A DISPATCH DESK: S02 NAME: R.C. DATE: 20-APR-23-DEFERRED DIRECTLY BY TOMC CAP, COUPLING R OFF 31-2825-9-0001 0225 ON 0000 CAP, COUPLING R OFF 31-2825-9-0001 0225 ON 31-2825-9-0001 7010. REPLACED MISSING FUEL CAP. REF AMM 28-25-41.

Part: FITTING — CRACKED (R MLG) · airframe 52,012 hrs · 32,770 cycles

RMLG DOOR ACTUATOR FITTING CONNECTING PLATE HAS A CRACK INDICATION AT AFT LUG CONNECTION FWD FACE LOWER FASTENER CRACK MEASURES 7/16'' OTBD AND 1/D'' INBD DIRECTION PER HAECO LCQ NR 9292006/4400 6 GENERATED BY V061671 AD RELATED TASK (2015-02-14) ACTUATOR FITTING AND HINGE FITTING ATTACH AREA PER PART 3 OF THE 32970 TOTAL AIRCRAFT FLIGHT CYCLES. LATEST REVISION OF ECRA 5330-07061 ON OR BEFORE AIRCRAFT REACHES INTERIM REPAIR ACCOMPLISHED IAW ECRA 5330-07061. ACCOMPLISH A PERMANENT REPAIR ON THE REPAIRED HOLES AT RH KEEL BEAM MLG ACCOMPLISH A PERMANENT REPAIR ON THE REPAIRED HOLES AT THE RH TOMC-APPROVAL FROM SC1ELBYC COMMENT KEEL BEAM MLG ACTUATOR FITTING AND HINGE FITTING ATTACH AREA PER PART 3 OF THE LATEST REVISION OF ECRA 5330-07061 ON OR BEFORE THE AIRCRAFT REACHES 32,970 TOTAL AIRCRAFT FLIGHT CYCLES. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. QC QC REVIEWED

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 51,505 hrs · 32,497 cycles

EPSU BATTERY AFT L FAILS DURING OPERATIONAL CHECK OF EMERGENCY POWER SUPPLY UNITS BY BITE CHECK. SUPPORT TASK NSA EMX N/R 00009. REMOVED PART NO AD 3214-31 SN 17434 AFT LEFT EMERGENCY POWER SUPPLY UNIT 13WL IAW AMM 33-51-38-000-002. DISPLACED LOWER PSU FOR ACCESS TO EPSU 13WL IAW A319 AMM AFT LEFT EMERGENCY POWER SUPPLY UNIT 13WL IAW AMM NOTED. REMOVED PART IAW 33-51-38-400-002-A. LIFTED AND ENGAGED PSU PANEL 13WL. LEFT EMERGENCY POWER SUPPLY UNIT 13WL IAW AMM AMM 35-21-41-400-001-A. PERFORMED OPS CHECK IAW AMM 33-51-38-000-002. INSTALLED PART NUMBER AD-3214-31 SN 293714 33-51-00-710-001-A AND A319 AMM 33-51-00-710-006-A. NO ISSUES INSPECTION COMPLETE

Part: BATTERY PACK — NO TEST (M1672) · airframe 49,369 hrs · 31,422 cycles

LAPTOP POWER OUTLET INOPERATIVE AT 21D 21E 21F REQUEST DEFERRAL.QUICK TURN. C/W MEL.PLACARDED BOTH OUTLETS. OK TO DEFER

Part: LANYARD — MISSING (FUEL CAP) · airframe 49,115 hrs · 31,284 cycles

PDA 3 REF LP7920135 FUEL CAP LANYARD MISSING CDL APPLIED .LANYARD PRESENT , REPLACED SPLIT RING.

Part: HYDRAULIC LINE — DAMAGED (Y SYSTEM) · airframe 48,927 hrs · 31,192 cycles

*EMERGENCY DECLARED* ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD FOUND RED RUBBER COATED HYD LINE JUST ABOVE ENGINE ABD JUST FOUND LINE LEAKING IPC 29-13-06-2D ITEM # 260 PN D2901010201200 UPDATED WITH PICTURE ON DATA PLATE ON LINE FUP WRITTEN TO REPL 9HB FLOW SENSOR WHICH IS THE SENSOR FOR DISREGARD LAST UPDATE FOR FLOW SENSOR. WRONG LOG PAGE UPDATED UNDER PYLON SPLIT LEAKING FLUID PACK 2. CORRECT SENSOR 10HB IS PACK 1 WHICH IS THE SENSOR WE WILL REPLACE. PARTIALLY REMOVED HYDRAULIC LINE IRW AIPC 29-13-06-02D ITEM 260. REMOVED DAMAGED HYD LINE ITEM #260 NEED TO CONTINUE WITH REMOVAL OF HYDRAULIC LINE. ADD EMP:285099 INSTALLED HYD LINE REF AMM78-37-51 AND AIPC 29-13-06-02D. LEAK CHK GOOD.

Part: STRINGER — CORRODED (FRMS 26-30 S38L) · airframe 47,674 hrs · 30,573 cycles

FWD CGO COMPT SLOPE AREA FR26-FR30 STGR38L STRINGER FND CORROSIO N REF HAECO NON-ROUTINE NO.9439870,ORIGINATED BY EMP V906550,SPE C NO.A3NB-53-3-6105. PERFORMED BY EMP V906550,FWD CGO COMPT SLOPE AREA FR29-FR30 STR 38L STRINGER REPAIRED AS PER ECRA 5341-01249 REV -.THIS ECRA PROVIDES PERMANENT REPAIRED INSTRUCTIONS FOR THE STRINGER CORROS ION.NO FURTHER ACTION REQ. RII BY TA327.

Part: SKIN — CORRODED (FR 26-30 S37-38L) · airframe 47,674 hrs · 30,573 cycles

FWD CGO COMPT SLOPE AREA FR26-FR30 STGR38L-STGR37L INTERNAL SKIN FND CORROSION REF HAECO NON-ROUTINE NO.9439977,ORIGINATED BY EM P V906550,SPEC NO.A3NB-53-3-6105. PERFORMED BY EMP V906550,FWD COMPT SLOPE AREA FR29-FR30 STGR38L- STGR37L INTERNAL SKIN CORROSION AREA REPAIRED AS PER ECRA 5341-0 1249 REV -.THIS ECRA PROVIDES PERMANENT REPAIR INSPECTIONS FOR S KIN CORROSIONS,NO FURTHER ACTION REQUIRED. RII BY TA327.

Part: DOOR SILL — CORRODED (FRM 66) · airframe 47,674 hrs · 30,573 cycles

CABIN FR66 RH DOOR SILL PANEL FND CORROSION REF HAECO NON-ROUTIN E NO.9438973,ORIGINATED BY EMP V902597,SPEC NO.A3NB-53-3-6187. PERFORMED BY EMP V902597,CABIN FR66-FR68 RH DOOR SILL PANEL (BEA M) REPLACED AS PER SRM 51-42-11 REV135 AND DWG E5347250000 ISSUE AF AND DWG D53480505006 ISSUE EQ. RII BY TA570.

Part: STRINGER SPLICE — CORRODED (FRMS 60-59 S41L) · airframe 47,674 hrs · 30,573 cycles

AFT CGO COMPT BILGE AREA FR60-FR59STG41L SPLICE FND CORROSION REF HAECO NON-ROUTINE LP:9440977 SPEC NO.A3NB-53-4-6179. AFT CGO COMPT BILGE AREA FR59-60 STR41L STRINGER SPLICE REPLACED AS PER ECRA 5341-01248 REV A.

Part: STRINGER SPLICE — CORRODED (FRMS 60-59 S42L) · airframe 47,674 hrs · 30,573 cycles

AFT CGO COMPT BILGE AREA FR60-FR59 STGR42L SPLICE FND CORROSION REF HAECO NON-ROUTINE LP:9440976 - ORIGINATED BY EMP V906550, SPEC NO.A3NB-53-4-6179. AFT CGO COMPT BILGE AREA FR59-60 STR42L STRINGER SPLICE REPLACED AS PER ECRA 5341-01248 REV A.

Part: FRAME — DAMAGED (FRM 68) · airframe 47,674 hrs · 30,573 cycles

CHECK THE LH FR68 FASTENER HOLE DIAMETER FOUND MORE THAN STARTIN G HOLE DIAMETER.REQUIRED TO CHECK REPAIR RECORD REFER HAECO NON- ROUTINE NO.9439811 ORIGINATED BY EMP V926739,EA5340-01724 REV C OP002. THE LH FR/68 #1 STOP FITTING LOWER OUTBOARD HOLE WAS PERFORMED P REVIOUSREPAIR AS PER CSN REPAIR LIST INTERNAL REPAIR ITEM 53-019 AS THE REQUIREMENT OF UAL. RE-DONE THE REPAIR AS PER SRM 53-41-12-300-010 REV 136. THE REPAIR APPROVED AS CATAGORY B REPA IR. REQUIREDTO PERFORM REPEAT INSPECTIONWITH THRESHOLD FROM REPA IR EMBODIMENT24500 FLIGHT CYCLESAND SUBSEQUENT INSPECTION AT ROTOTEST AS PER SRI 53-41-12-205-009 REV 137. INTERVALS OF 10700 FLIGHT CYCLES INSPECTION METHOD WITH HFEC AND OKAY TO DIP TO PERFORM REPEAT INSPECTION WITH THRESHOLD FROM REPA IR EMBODIMENT IS 24500 FLIGHT CYCLES AND SUBSEQUENT INSPECTIONS AT INTERVALS OF 10700 FLIGHT CYCLES PER SRI 53-41-12-205-009 TOMC-APPROVAL FROM SC1ELBYC COMMENT REVIEWED QC REVIEWED RECORDS UPDATE....SP INIT: 47238 TAFC (24500 FC FROM REPAIR EMBODIMENT) (INIT WILL TRIGGER TO RIR -2417) RIR : 10,700 FC...SP/U366013

Part: STRINGER — CORRODED (FRMS 60-61 S44) · airframe 47,674 hrs · 30,573 cycles

AFT CGO COMPT BILGE AREA FR60-FR61 STGR44 STRINGER FND CORROSION REF HAECO NON-ROUTINE NO.9439511, SPEC NO.A3NB-53-4-6179. ,AFT CGO COMPT BILGE FR60-61 STGR44 CORRODED STRINGER REPAIRED AS PER SRM 53-00-13-300-001 REV 135,THIS REPAIR APPROVED AS CAT B REPAIR REQUIRED REPEAT INSPECTION THRES HOLD FROM TIME OF REPAIR EMBODIMENT 60000FC/120000FH SUBSEQUENT INSPECTION AT INTERVALS OF TBD,INSPECTION METHOD:TBD AS PER SRI 53-00-13-205-001 REV135.

Part: STRINGER SPLICE — CORRODED (FRMS 59-60 S42L) · airframe 47,674 hrs · 30,573 cycles

AFT CGO COMPT BILGE AREA FR60-FR59STGR42L SPLICE FND CORROSION REF HAECO NON-ROUTINE LP:9440976 - ORIGINATED BY EMP V906550, SPEC NO.A3NB-53-4-6179. PERFORMED BY EMP V906550,AFT CGO COMPT BILGE AREA FR59-60 STR42L STRINGER SPLICE REPLACED AS PER ECRA 5341-01248 REV A. RII BY TA327.

Part: STRINGER — CORRODED (FRMS 60-61 S32L) · airframe 47,674 hrs · 30,573 cycles

AFT CGO COMPT BILGE AREA FR60-FR61 STGR32L STRINGER FND CORROSIO N REF HAECO NON-ROUTINE NO.9439516, SPE C NO.A3NB-53-4-6179. AFT CARGO COMPT BILGE AREA FR60-61 STGR32 L CORRODED STRINGER REPAIRED AS PER SRM 53-00-13-300-001 REV135, THIS REPAIR APPROVED AS CAT B REPAIR,REQUIRED REPEAT INSPECTION THRESHOLD FROM TIME OF REPAIR EMBODIMENT 60000FC/120000FH SUBSEQ UENT INSPECTION AT INTERVALS OF TBD,INSPECTION METHOD TBD AS PER SRI 53-00-13-205-001 REV135.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 47,674 hrs · 30,573 cycles

13WL EPSU BATTERY CAPACITY FOUND LOW CAPACITY REF HAECO NON- ROUTINE LP:9438987 - ORIGINATED BY EMP V903570,SPEC NO.A3NB-33-3 -0004. PERFORMED BY EMP V903570,REPLACED 13WL EPSU BATTERY AND BITE TEST FOUND ''TEST OK'' REF TO AMM 33-51-38-000-002-A REV 111, AMM 33-51-38-400-002-A REV 111.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 47,674 hrs · 30,573 cycles

12WL EPSU BATTERY CAPACITY FOUND LOW CAPACITY REF HAECO NON- ROUTINE. SPEC NO.A3NB-33-3 -0004. REPLACED 12WL EPSU BATTERY AND BITE TEST FOUND NORMAL REFER TO AMM 33-51-38-400-002-A REV 111.

Part: STRINGER SPLICE — CORRODED (FRM 47-51 S43L) · airframe 47,674 hrs · 30,573 cycles

PERFORM GVI INSP FIND AFT CGO COMPT JOINT STRINGER CORROSION AT FR47/51-FR52 S43L REF HAECO NON-ROUTINE NO.9440347,ORIGINATED BY EMP V906550. PERFORMED BY EMP V906550,REPLACED AFT CGO COMPT JOINT STRINGER COUPLING AS PER SRM 51-42-11 REV 137. RII BY TA327.

Part: STRUCTURE — CORRODED (FR60-61 STR44) · airframe 47,674 hrs · 30,573 cycles

REF HAECO LOG PAGE 9439511 AFT CARGO COMPARTMENT BILGE AREA FR60 -61 STGR 44 FOUND CORROSION. REF HAECO LOG PAGE 9439511 AFT CARGO COMPARTMENT BILGE FR60-61 S TGR 44 CORRODED STRING REPAIRED AS PER SRM 53-00-13-300-001 REV 135. THSI REPAIR APPROVED AT CATAGORY B REPAIR. REQUIRED REPEAT INSPECTION THRESHOLD FROM TIME OF REPAIR EMBODIMENT 60000 FC/120000FH SUBSEQUENT INSPECTION AT INTERVALS TBD INSPECTION ME THOD TBD AS PER SRI 53-00-13-205-001 REV135. OKAY TO DIP INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT IS 60000 FC OR 120000 FH WHICHEVER COMES FIRST WITH SUBSEQUENT INSPECTIONS TBD REF SRI 53-00-13-205-001 TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. REVIEWED QC REVIEWED

Part: STRUCTURE — CRACKED (FRM 16) · airframe 47,674 hrs · 30,573 cycles

CRACK/BUSH REPAIR AT RH FR 16 DOUBLE JOGGLE AREA OUTER FLANGE FA STENER HOLE CRACK.REF ECRA 5100-03068 CSN INTERNAL REPAIR LIST F IG.5,ITEM 53-005, REFER HAECO NON-ROUTINE NO.9440148 ORIGINATED B Y EMP V905987,LOGPAGE 6259129. GVI ACCOMLISHED WITH NIL FINDING VALIDA TED,THE REPAIR REFERENCE IS RDAS 80294360/003/2017 ISSUE A THIS EXISTING REPAIR WAS RECORDED ON CSN INTERNAL REPAIR LIST FIG 5,I TEM 53-005 AND RE-EVALUATED DURING HMV-2 PER ECRA 5100-03068 REV A,THIS IS PERMANENT REPAIR(CATEGORY B) NEED REPEAT INSPECTION. H NOT RELEVANT). FOR HOLE 3&4 RH TH=5350 FC(FH NOT RELEVANT) IT=5350 FC(F FOR HOLE 5&6 RH TH=3840 FC(FH NOT RELEVANT) IT=3840.

Part: STRINGER — CORRODED (FR 60-61 S32L) · airframe 47,674 hrs · 30,573 cycles

REF HAECO LOG PAGE 9439516 AFT CARGO COMPARTMENT BILGE AREA FR60 -61 STGR 32L FOUND CORROSION. REF HAECO LOG PAGE 9439516 AFT CARG COMPARTMENT BILGE FR60-61 ST GR 32L CORRODED. STRINGER REPIRED AS PER SRM 53-00-13-300-001 RE V 135. THIS REPAIR APPROVED AS CATAGORY B REPAIR. REQUIRED REPEAT INSPECTION THRESHOLD FROM REPAIR EMBODIMENT 60000 FC/1200 00FH SUBSEQUENT INSPECTION AT INTERVALS TBD. INSPECTION METHOD T BD AS PER SRI 53-00-13-205-001 REV 135. OKAY TO DIP INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT IS 60000 FC OR 120000 FH WHICHEVER COMES FIRST WITH SUBSEQUENT INSPECTIONS TBD REF SRI 53-00-13-205-001 TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. REVIEWED QC REVIEWED

Part: FITTING — CORRODED (FRM 35 S40L) · airframe 47,674 hrs · 30,573 cycles

FWD CGO COMPT BILGE AREA FR35 STGR40L STRINGER END FITTING FND C ORROSION REF HAECO NON-ROUTINE NO.9439541,ORIGINATED BY EMP V906 550,SPEC NO.A3NB-53-3-6105. PERFORMED BY EMP V906550,FWD CGO COMPT BILGE AREA FR35 STR40L STRINGER END FITTING REPLACED AS PER SRM 51-42-11 REV135. RII BY TA327.

Part: FITTING — CORRODED (FRM 35 S39L) · airframe 47,674 hrs · 30,573 cycles

FWD CGO COMPT BILGE AREA FR35 STGR39L STRINGER END FITTING FND C ORROSION REFER HAECO NON-ROUTINE NO.9439542 ORIGINATED BY EMP V9 065550,SPEC NO.A3NB-53-3-6105. PERFORMED BY EMP 906550,FWD CGO COMPT BILGE AREA FR35 STGR39L ST RINGER END FITTING REPLACED AS PER SRM 51-42-11 REV.135 & DWG D5 3376035 ISSUE C REFER SWS FOR THE DETAILS. RII BY TA327.

Part: STRINGER — CORRODED (FRM 35 S40L) · airframe 47,674 hrs · 30,573 cycles

FWD CGO COMPT BILGE AREA FR35 STGR40L STRINGER END FITTING FND C ORROSION REF HAECO NON-ROUTINE NO.9439541,ORIGINATED BY EMP V906 550,SPEC NO.A3NB-53-3-6105. FWD CGO COMPT BILGE AREA FR35 STR40L STRINGER END FITTING REPLACED AS PER SRM 51-42-11 REV135.

Part: DOOR SILL — CORRODED (FRM S66) · airframe 47,674 hrs · 30,573 cycles

CABIN FR66 LH DOOR SILL PANEL FOUND CORROSION REF HAECO NON- ROUTINE LP:9439144 - ORIGINATED BY EMP V902597,SPEC NO.A3NB-53-3 -6187. PERFORMED BY EMP V902597,CABIN FR66 L/H DOOR SILL PANEL REPAIRED AS PER SRM 53-41-14-300-001 REV 135,THE REPAIR APPROVED AS CAT A REPAIR AS PER SRM 53-41-14-300-001 REV 135. RII BY TA570.

Part: FRAME — CRACKED (FRM 16) · airframe 47,674 hrs · 30,573 cycles

CRACK/BUSH REPAIR AT RH FR16 DOUBLE JOGGLE AREA OUTER FLANGE FA STENER HOLE CRACK REF ECRA 5100-03068 CSN INTERNAL REPAIR LIST FIG 5 ITEM 53-005. REF HAECO NRWC9440148 ACCOMPLISHED GVI WITH NO FINDING VALIDATED REPAIR. REF AIRBUS RDAS 80294360/003/2017 ISSUE A THIS EXISTING WAS RECORDED ON CSN INTERNAL REPAIR LIST FIG 5 ITEM 53-005 AND R RE-EVALUATED DURING HMV-2 PER EC/RA #5100-03068 REV A THIS IS A PERMANENT REPAIR CATEGORY B NEEDS REPAET INSPECTION FOR HOLE #5 AND #6 RH THRESHOLD IS 3840 FLIGHT CYCLES FLIGHT HOURS NOT EFFECTED INITIAL THRESHOLD IS 3840 FLIGHT CYCLES. DIP APPROVED FOR CARRY TO BE RE-EVALUATED DURING HMV-2 PER EC/RA # 5100-03068 REV A THIS IS A PERMANENT REPAIR CATEGORY "B" NEEDS REPEAT INSPECTION FOR HOLE #5 AND #6 RH THRESHOLD IS 3840 FLIGHT CYCLES FLIGHT HOURS NOT EFFECTED INITIAL THRESHOLD IS 3840 FLIGHT CYCLES. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: FRAME — CRACKED (FRM 16) · airframe 47,674 hrs · 30,573 cycles

CRACK/BUSH REPAIR AT RH FRAME 16 DOUBLE JOGGLE AREA OUTER FLANGE FASTNER HOLE CRACK REF EC/RA #5100-03068 CSN INTERNAL REPAIR LIS T FIG 5 ITEM 53-005 REF HAECO NRWC 9440148 ACCOMPLISHED GVI WITH NO FINDINGS VALIDAT ED THE REPAIR REFERENCE RDAS 80294360/003/2017 ISSUE A THIS EXIS TING REPAIR WAS RECORDED ON CSN INTERNAL REPAIR LIST FIG 5 ITEM 53-005 AND RE-EVALUATED DURING HMV-2 PER EC/RA #5100-03068 REV A THIS IS A PERMANENT REPAIR CATAGORY B NEEDS REPEAT INSPECTION. FOR HOLE #3 AND #4 THRESHOLD IS 5350 FLIGHT CYCLES FLIGHT HOURS YCLES. FLIGHT HOURS NOT EFFECTED INITIAL THRESHOLD IS QAT 5350 FLIGHT C DIP APPROVED FOR CARRY BY TOMC TO BE RE-EVALUATED DURING HMV-2 PER EC/RA #5100-03068 REV A THIS IS A PERMANENT REPAIR CATAGORY B NEEDS REPEAT INSPECTION. FOR HOLE #3 AND #4 THRESHOLD IS 5350 FLIGHT CYCLES FLIGHT HOURS NOT EFFECTED INITIAL THRESHOLD IS 5350 FLIGHT C YCLES. TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. QC QC REVIEWED.

Part: FITTING — CORRODED (FRM 35 S41L) · airframe 47,674 hrs · 30,573 cycles

FWD CGO COMPT BILGE AREA FR35 STGR41L STRINGER END FITTING FND CORROSION REF HAECO NON-ROUTINE NO.9439539,ORIGINATED BY EMP V90 6550,SPEC NO.A3NB-53-3-6105. PERFORMED BY EMP V906550,FWD CGO COMPT BILGE AREA FR35 STGR41L DAMAGED STRINER END FITTING REMOVED AND REPLACED AS PER SRM 51-4 2-11 REV135 AND DWG D53210054 ISSUE C. RII BY TA327.

Part: FITTING — CORRODED (FRM 35 S41R) · airframe 47,674 hrs · 30,573 cycles

FWD CGO COMPT BILGE AREA FR35 STGR41R STRINGER END FITTING FND CORROSION REF HAECO NON-ROUTINE NO.9439540,ORIGINATED BY EMP V906550,SPEC NO.A3NB-53-3-6105. PERFORMED BY EMP V906550,FWD CGO COMPT BILGE AREA FR35 STGR41R DAMAGED STRINGER END FITTING REMOVED AND REPLACED AS PER SRM 51- 42-11 REV135 AND DWG D53210054 ISSUE C. RII BY TA327.

Part: INTERCOSTAL — DAMAGED (FRM 16) · airframe 47,674 hrs · 30,573 cycles

PLS PROVIDE REPAIR RECORD REFER HAECO NON-ROUTINE LP 9439169. EA5311-02164 REV ORIG OP001 STEP 2.1C) AND STEP 2.2). REPLACED LH 16 NO.7 INTERCOSTAL FTG REF DWG 53114236 REV S,SRM 51-42-11 REV 135,OTHERS FOLLOW UP PER EA5 311-02164 REV ORIG OP001 STEP 2.1 AND STEP 2.2.

Part: INTERCOSTAL — DAMAGED (FRM 16) · airframe 47,674 hrs · 30,573 cycles

PLS PROVIDE REPAIR RECORD REFER HAECO NON-ROUTINE LP 9439170. EA5311-02164 REV ORIG OP002 STEP 2.1 C AND STEP 2.2 C). RH FR16 NO.7 INTERCOSTAL FTG REPLACED REF DWG 53114236 REV S,SRM 51-42-11 REV 135,OTHERS FOLLOW UP PER EA5311-02164 REV ORIG OP002 STEP 2.1 AND STEP 2.2

Part: INTERCOSTAL — DAMAGED (LH 16 NR 7) · airframe 47,667 hrs · 30,570 cycles

PLS PROVIDE REPAIR RECORD REFER HAECO NON-ROUTINE EA5311-02164 REV ORIG OP001 STEP 2.1C) AND STEP 2.2). REPLACED LH 16 NO.7 INTERCOSTAL FTG REF DWG 53114236 REV S,SRM 51-42-11 REV 135,OTHERS FOLLOW UP PER EA5 311-02164 REV ORIG OP001 STEP 2.1 AND STEP 2.2.

Part: INTERCOSTAL — DAMAGED (FRM 16) · airframe 47,667 hrs · 30,570 cycles

PLS PROVIDE REPAIR RECORD REFER HAECO NON-ROUTINE LP 9439170 - ORIGINATED BY EMP V902597 EA5311-02164 REV ORIG OP002 STEP 2.1 C AND STEP 2.2 C). PERFORMED BY EMP V926739 RH FR16 NO.7 INTERCOSTAL FTG REPLACED REF DWG 53114236 REV S,SRM 51-42-11 REV 135,OTHERS FOLLOW UP PER EA5311-02164 REV ORIG OP002 STEP 2.1 AND STEP 2.2 RII BY TA327