N220NV

Part: EPSU — NO TEST (ZONE 200) · airframe 54,418 hrs · 33,944 cycles

(AIRCRAFT NOT GROUNDED) FAILED BATTERY CAPACITY TEST / REMOVED AND REPLACED EPSU WO532858"

Part: COVER — OUT OF POSITION (ZONE 800) · airframe 56,210 hrs · 34,800 cycles

(AIRCRAFT NOT GROUNDED) FA REPORTS FORWARD GALLEY SLIDE PACK COVER ON WRONG DOOR. REMOVED, SWAPPED, AND INSTALLED FWD RIGHT AND LEFT SLIDE PACK COVERS TO PROPER CONFIGURATION PER AMM 25-62-44-000-002-A, AMM 25-62-44-400-006-A AND AMM 25-62-44-000-802-A & AMM 25-62-44-400-802-A.

Part: TAB — MISSING (ZONE 800) · airframe 56,205 hrs · 34,798 cycles

(AIRCRAFT NOT GROUNDED) BOTH EMERGENCY EGRESS TABS MISSING OFF BLOW OUT PANEL IN COCKPIT. REPLACED COCKPIT DOOR EGRESS PINS IAW AMM 52-51-11-960-002-A.

Part: LIGHT — MALFUNCTIONED (ZONE 200) · airframe 56,003 hrs · 34,706 cycles

(AIRCRAFT GROUNDED) LEFT OVERWING EMERGENCY EXIT SIGNS ARE INOP WITH AC BUSSES OFF. / PERFORMED OPS CK OF EMERGENCY LIGHTS REF AMM 33-51-00-710-007-A. OPS CK GOOD AT THIS TIME. A/C OK FOR SVC / "

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 55,872 hrs · 34,648 cycles

(AIRCRAFT NOT GROUNDED) EPSU BATTERY MID R ON EMERGENCY LIGHT TEST. REMOVED AND REPLACED EPSU BATTERY AT LOCATION 12WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A, OPS CHECK GOOD.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 55,597 hrs · 34,534 cycles

(AIRCRAFT NOT GROUNDED) FAILED OPERATIONAL LIGHT TEST. / REMOVED AND REPLACED EPSU REF WO521139"

Part: SENSOR — FALSE INDICATION (ZONE 800) · airframe 55,271 hrs · 34,393 cycles

(AIRCRAFT NOT GROUNDED) RT SIDE OVERWING SLIDE NOT ARMED / RESET DOOR AND SENSORS, OPS CHECK GOOD, PER AMM AMM25-62-42 AND AMM 52-22-00-220-003-A"

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 55,233 hrs · 34,375 cycles

(AIRCRAFT NOT GROUNDED) EMERG LIGHT AFT CABIN FAILED, FIN 13WL / REPLACED BATTERY PACK @ @13WL, OPS CHECK GOOD, REF AMM 33-51-38-400-002-A"

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 54,463 hrs · 33,968 cycles

(AIRCRAFT GROUNDED) FWD EPSU BATTERY (10WL) REQUIRES REPLACEMENT FOR CAPACITY CHECK / REMOVED AND REPLACED EPSU (10WL), OPS CHECK GOOD REF AMM 33-51-38-400-002-A AND 33-51-38-000-002-A."

Part: RIB — DAMAGED (ZONE 500) · airframe 54,273 hrs · 33,860 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 5000-0013: 33284-23 LH WING TRAILING EDGE, RIBLET E AT RIB 13 CORRODED / AT LH WING TRAILING EDGE , RIBLET E AT RIB 13 REPLACED AS PER AIRBUS DOSSIER 81427484 AND REPAIR DRAWING R575-40263#B. REPAIR IS CATEGORY A AS PER AIRBUS RDAF/81427484/006/2024#A. REPAIR IS MAJOR DUE TO PSE ITEM. NO FURTHER ACTION REQUIRED. SEE AWS FOR DETAILS AND NDT REPORT MWO 58564-10. RIBLET PN: D5755907120039 PO:2076190 REF AAY ERO: R5751-0052 R.00"

Part: BEAM — CORRODED (ZONE 200) · airframe 54,272 hrs · 33,860 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 2000-0070: (1684-027) AT R1 DOOR SILL BEAM FOUND CORRODED AROUND FASTENER HOLE AT AFT GIRT BAR FITTING AREA. / R 1 DOOR LOWER SILL BEAM CORROSION REMOVED AS PER SRM 51-74-00 REV 149 AND FOUND WITHIN LIMIT PER SRM 53-11-14 283 005 REV 149.REPAIR MAJOR CATEGORY B WITH FUTURE INSPECTION LISTED IN SRI 53-11-14-205-001 REV. 149 THRESHOLD FROM 1ST FLIGHT AT 60000FC/FH NOT RELEVANT, INTERVAL; TBD. METHOD; TBD SEE AWS FOR DETAILS AND NDT REPORT MWO 585564-36."

Part: FRAME — CRACKED (ZONE 100) · airframe 54,273 hrs · 33,860 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 2000-0082: S/M PASSENGER CABIN, CRACK FOUND AT FR 68 STR 22 RH CRACK FOUND ON WEB HORIZONTAL FLANGE / PASSENGER CABIN FR 68 AT STR 22R/H & STOP FITTING #1 REPAIRED AS PER AIRBUS DOSSIER 81431174 IN COMPLIANCE WITH SRM 53-41-12-300-022 REV. 149. REPAIR CLAISSIFED MAJOR CATEGORY B AS PER RDAF 81431174/004/2024#A ALL REPEAT INSPECTION THRESHOLD FROM 1ST FLIGHT AT 1-EXTERNAL SURFACES OF THE FRAME WEB (FWD FACE) AND REPAIR PART WEB (AFT FACE) EXCEPTING UNDERNEATH THE SEAL PROFILE AND THE BRACKETS AT 71600TFC / FH NOT RELEVANT. INTERVAL: TBD METHOD: TBD. 2- FASTENER HOLES AT FRAME WEB, MACHINED REPAIR PART AND SEAL PROFILE / BRACKETS ATTACHMENTS AT 95000 FC / FH NOT RELEVANT INTERVAL: TBD METHOD TBD. SEE AWS 14 FOR THE CONTINUATION OF THIS CORRECTIVE ACTION. REF AAY ERO R5341E0131 R.OO"

Part: SKIN — CORRODED (ZONE 600) · airframe 54,273 hrs · 33,860 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 6000-0032: S/M RHWING TRAILING EDGE OVERHANG BETWEEN RIB 13-14 RIBLET E CORRODED OUT OF ADL / AT RH WING TRAILING EDGE, RIBLET E BETWEEN RIB 13 AND RIB 14 REPLACED AS PER AIRBUS DOSSIER 81430186 AND REPAIR DRAWING R575-40263 ISSUE B. REPAIR IS CATEGORY A AS PER AIRBUS RDAF 81430186/005/2024#A. REPAIR IS MAJOR DUE TO PSE ITEM. NO FURTHER ACTION REQUIRED. SEE AWS FOR DETAILS AND NDT REPORT MWO 58564-62. RIBLET PN: D5755907120139 AND PO: 2030626. REF AAY ERO R5751-0048 R.00"

Part: DOOR SILL — CORRODED (ZONE 200) · airframe 54,273 hrs · 33,860 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 2000-0072: (1684-029) AT R2 DOOR, SILL BEAM FOUND CORRODED AT FWD GIRT BAR FITTING AREA AT ANCHOR NUT LOCATION. / R2 DOOR, SILL BEAM REPIRED IAW SRM 53-41-14-300-001 REPAIR PRINCIPLE 11 REV. 149. THIS REPAIR IS MAJOR CATEGORY A NON FURTHER ACTION REQUIRED. ANGLE P/N: ANGLE #7 RH-RAW PO: 1569232. FILLER P/N: 2024T3.090 PO: 2070859. HILOCK P/N: HL10VF6-5 PO:2064098, HILOCK P/N: HL10VF6-3 PO: 2056607. HILOCK P/N: HL10VF6-4 PO: 2025158. HILOCK P/N: HL11VF6-7 PO: 2071812. HILOCK P/N: DAN6-6-5 PO: 2014791. HILOCK P/N: HL10VF6-6 PO: 1771915. COLLAR P/N: HL70-6 PO: 2064166 NUT PLATE P/N: MS21060L3 PO: 2035625. SEALANT P/N: PRC870B1/2 PO: 2068700."

Part: SIGN — BROKEN (FWD CABIN) · airframe 54,272 hrs · 33,860 cycles

(AIRCRAFT NOT GROUNDED) NRC 2000-0067: 165-59 PASS CABIN RH FWD ENTRY EMERGENCY EXIT SIGN BROKEN. / EMERGENCY EXIT SIGN REPLACED IN PASSENGER CABIN AT FWD RH ENTRY AS PER AMM 33-51-13-400-001-A".

Part: WING ROOT — CORRODED (ZONE 500) · airframe 54,273 hrs · 33,860 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 6000-0005: R/H WING TRAILING EDGE CORROSION FOUND AT WING ROOT OVERWING PANEL BETWEEN INBD JOINT STRIP AND NUT STRIP RETAINERS. / RH WING TRAILING EDGE OVERHANG BETWEEN RIB 1-2 AT OVERWING PANEL GANG-CHANNEL REPAIRED AS PER AIRBUS DOSSIER 81430471. REPAIR CLASSIFED MAJOR CATEGORY B WITH FUTURE INSPECTION AS PER RDAF/81430471/004/2024#A FROM REPAIR REPAIR EMBODIMENT AT 10200 FC / 20400 FH. INTERVAL 10200 FC / 20400 FH METHOD: DETAIL INSPECTION. SEE AWS FOR DETAILS AND NDT REPORT MWO 58564-6/37"

Part: RIB — CORRODED (ZONE 500) · airframe 54,273 hrs · 33,860 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 5000-0012: 33284-20 LH WING TRAILING EDGE , RIBLET L BETWEEN RIB 18 AND RIB 19 CORRODED / AT LH WING TRAILING EDGE , RIBLET L BETWEEN RIB 18 AND RIB 19 REPLACED AS PER AIRBUS DOSSIER 81427483 AND REPAIR DRAWING R575-40250 ISSUE C. REPAIR IS CATEGORY A AS PER AIRBUS RDAF/81427483/006/2024#A. REPAIR IS MAJOR DUE TO PSE ITEM. NO FURTHER ACTION REQUIRED. SEE AWS FOR DETAILS AND NDT REPORT MWO 58564-15. RIBLET PN: D5754017020039 AND PO: 2076190.REF AAY ERO R5751-0053 R.00"

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,235 hrs · 32,880 cycles

FOUND CRACK EXTENDING FROM RIVET HEAD AFT AT FR 14 BETWEEN STRINGER 12 & 13 SEE NR01165111 AND NR01167609 / REPAIRED CRACK. REMOVED CRACK, CUT-OUT SKIN IAW SRM TASK 53-11-11-300-041 PERMANENT EXTERNAL REPAIR FOR SKIN THICKNESS. PERFORMED NDT-EDDY CURRENT SKIN AND HOLES FOR VERIFICATION OF CRACK REMOVAL REF NR 1165378, 1165505, 1166720, 1166864, 1166866, 1167521, 1167522 AND 1167609."

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 52,120 hrs · 32,820 cycles

AFT LEFT(13WL) AND MID LEFT(11WL) EPSU BATTERY FAILED CIDS EMERGENCY LIGHT TEST / REMOVED AND REPLACED AFT LEFT AND MID LEFT EPSU BATTERIES REF AMM 33-51-38-000-002-A AND 33-51-38-400-002-A OPS CHECK GOOD"

Part: EPSU — UNKNOWN · airframe 51,833 hrs · 32,678 cycles

MID RH EMERGENCY BATTERY (12WL) FAILED EMER BATTERY TEST, REQS R/R. / NO BATTERIES IN STOCK. R/R EPSU AND BATTERY ASSY W/REF TO AMM 33-51-38-400-001-A. ALL OPS OK."

Part: NONE — NONE · airframe 50,751 hrs · 32,162 cycles

NRC 0000-0004:THIS NRC IS RAISED TO COMPLY WITH ALLEGIANT M313 DIGITAL FORM COMPLIANCE, REFER 5000-0038 CORROSION FOUND ON LH WING UPPER SKIN UPPER SURFACE AT RIB 8 REAR SPAR AREA. / PROCESS FORM M313 ACCOMPLISHED, M313 ATTACHED.CORROSION REMOVED AS PE SRM 51-74-00 REV 142 AND FOUND STRUCTURALLY ACCEPTALE AS PER AIRBUS REPAIR INSTRUCTIONS R572-58616 PARA E, ISSUE L AND AIRBUS TD/70525679/055/2022/C. AIRBUS WILL EVALUATE AND PROVIDE RESPONSE WITHIN 6 MONTHS."

Part: NONE — NONE · airframe 50,751 hrs · 32,162 cycles

NRC 0000-0003: THIS NRC IS RAISED TO COMPLY WITH ALLEGIANT M313 DIGITAL FORM COMPLIANCE, REFER 6000-0029 R/H WING T/E AT RIB 7, CORROSION FOUND ON UPPER SKIN LOWER SURFACE / PROCESS FOR M313 CARD ACCOMPLISHED, M313 ATTACHED.CORROSION REMOVED AS PER SRM 51-74-00, AND REPAIRED AS PER TD/70566294/030/2022/G AND AIRBUS REPAIR INSTRUCTIONS R572-58616 PARA E, ISSUE L. AIRBUS WILL EVALUATE AND PROVIDE RESPONSE WITHIN 6 MONTHS."

Part: NONE — NONE

NRC 5000-0025: 193-22. CORROSION FOUND ON LH WING UPPER SKIN LOWER SURFACE AT TRAILING EDGE AREA RIB 22./LH WING UPPER SKIN LOWER SURFACE AT TRAILING EDGE AREA RIB 22, CORROSION REMOVED AT BLEND AREA NO.1 AND REPAIRED AND AS PER TD/70525679/055/2022#C AND AIRBUS REPAIR INSTRUCTION R572-58616 PARA E. ISSUE L AND COMPLY WITH ERO: R 5721-0122 REV 00 . REPAIR CLASSIFIED MAJOR, CATEGORY: NOT DEFINED, SOLUTION LIFE OR LIMITATION: 6 MONTHS AS PER RDAF 70525679/048/2022#A. PRIOR TO TO THE EXPIRATION OF THIS LIFE LIMITATION, AIRBUS WILL ACCOMPLISH THE FULL FATIGUE AND DAMAGE TOLERANCE ANALYSIS AND AUTOMATICALLY DELIVER AN UP-ISSUED RDAF. NO ACTION IS REQUIRED ON THE PART OF ALLEGIANT AIR. SEE AWS AND NDT REPORT MWO52444-18 FOR MORE DETAILS."

Part: NONE — NONE

NRC 5000-0026: 193-26. CORROSION FOUND ON LH WING UPPER SKIN LOWER SURFACE AT TRAILING EDGE AREA BETWEEN RIB 7-9/ L/H WING UPPER SKIN LOWER SURFACE AT TRAILING EDGE AREA BTW RIB 7-9 CORROSION REMOVED AT BLEND AREA (A-C-D) AND REPAIRED AS PER TD/70525679/055/2022#C AND AIRBUS REPAIR INSTRUCTION R572-58616 PARA E. ISSUE L AND COMPLY WITH ALLEGIANT ERO: R 5721-0122 REV 00. REPAIR CLASSIFIED MAJOR CATEGORY: NOT DEFINED, SOLUTION LIFE OR LIMITATION: 6 MONTHS AS PER RDAF 70525679/048/2022#A. PRIOR TO TO THE EXPIRATION OF THIS LIFE LIMITATION, AIRBUS WILL ACCOMPLISH THE FULL FATIGUE AND DAMAGE TOLERANCE ANALYSIS AND AUTOMATICALLY DELIVER AN UP-ISSUED RDAF. NO ACTION IS REQUIRED ON THE PART OF ALLEGIANT AIR. SEE AWS AND NDT REPORT MWO52444-19 FOR MORE DETAILS."

Part: NONE — NONE

NRC 6000-0029: 962-11 R/H WING T/E AT RIB 7, CORROSION FOUND ON UPPER SKIN LOWER SURFACE / R/H WING UPPER SKIN LOWER AND UPPER SURFACE AT TRAILING EDGE AREA RIB 7-9, CORROSION REMOVED AT BLEND AREAS (2-3-4 LOWER SURFACE)(2A UPPER SURFACE) AND REPAIRED AS PER TD/70566294/030/2022#G, REPAIR INSTRUCTION R572-58616 PARA D AND E. ISSUE L AND COMPLY WITH ALLEGIANT ERO: R 5721-0121 REV. 00. REPAIR CLASSIFIED MAJOR, CATEGORY NOT DEFINED, SOLUTION LIFE OR LIMITATION: 6 MONTHS PER RDAF 70566294/024/2022#A. PRIOR TO THE EXPIRATION OF LIFE LIMITATION, AIRBUS WILL ACCOMPLISH FULL FATIGUE AND DAMAGE TOLERANCE ANALYSIS AND AUTOMATICALLY DELIVER UP-ISSUED RDAF. NO ACTION IS REQUIRED ON THE PART OF ALLEGIANT. SEE AWS AND NDT REPORT MWO52444-20 FOR MORE DETAILS."

Part: NONE — NONE

NRC: 6000-0024 962-06 R/H WING T/E AT RIB 16, CORROSION FOUND ON UPPER SKIN LOWER SURFACE. / R/H WING UPPER SKIN LOWER SURFACE AT TRAILING EDGE AREA AT RIB 16, CORROSION REMOVED AT BLEND AREA (5-6-7-8) AND REPAIRED AS PER TD/70566294/030/2022#G, REPAIR INSTRUCTION R572-58616 PARA E. ISSUE L, REPAIR INSTRUCTIONS R572-58961,ISSUE C AND COMPLY WITH ALLEGIANT ERO: R 5721-0121 REV 00 . REPAIR CLASSIFIED MAJOR CATEGORY: NOT DEFINED, SOLUTION LIFE OR LIMITATION: 6 MONTHS PER RDAF 70566294/024/2022#A. PRIOR TO THE EXPIRATION OF LIFE LIMITATION, AIRBUS WILL ACCOMPLISH FULL FATIGUE AND DAMAGE TOLERANCE ANALYSIS AND AUTOMATICALLY DELIVER AN UP-ISSUED RDAF. NO ACTION IS REQUIRED ON THE PART OF ALLEGIANT AIR. SEE AWS AND NDT REPORT MWO52444-17 FOR MORE DETAILS."

Part: NONE — NONE

NRC 5000-0038: 193-32. CORROSION FOUND ON LH WING UPPER SKIN UPPER SURFACE AT RIB 8 REAR SPAR AREA. / LH WING UPPER SKIN UPPER SURFACE AT RIB 8 REAR SPAR AREA, CORROSION REMOVED AT BLEND AREA B AND REPAIRED AND AS PER TD/70525679/055/2022#C AND AIRBUS REPAIR INSTRUCTION R572-58616 PARA D. ISSUE L AND COMPLY WITH ERO: R 5721-0122 REV 00 . REPAIR CLASSIFIED MAJOR, CATEGORY: NOT DEFINED, SOLUTION LIFE OR LIMITATION: 6 MONTHS AS PER RDAF 70525679/048/2022#A. PRIOR TO TO THE EXPIRATION OF THIS LIFE LIMITATION, AIRBUS WILL ACCOMPLISH THE FULL FATIGUE AND DAMAGE TOLERANCE ANALYSIS AND AUTOMATICALLY DELIVER AN UP-ISSUED RDAF. NO ACTION IS REQUIRED ON THE PART OF ALLEGIANT AIR. SEE AWS AND NDT REPORT MWO52444-21 FOR MORE DETAILS."

Part: NONE — NONE

NRC 1000-0006: 429-7 L/H MLG DOOR ACTUATOR TO KEEL BEAM ATTACHMENT FITTING FWD LUG BUSHING MIGRATED. / ON L/H MLG DOOR ACTUATOR TO KEEL BEAM ATTACHMENT FITTING, FWD LUG BORE REWORKED AND NEW OVERSIZE PLAIN BUSHING INSTALLED AS PER ERO NO.R5336-0017 REV 01. INSTALLATION OF ACTUATOR COVERRED BY TASK CARD NO.53-140-002. ERO R5336-0017, REV 01, N220NV - AAR - MLG DOOR ACTUATOR FITTING ON KEEL BEAM (SB53-1195) - LH, ACCOMPLISHED"

Part: NONE — NONE

NRC 1000-0007: 429-8 R/H MLG DOOR ACTUATOR TO KEEL BEAM ATTACHMENT FITTING AFT LUG BUSHING MIGRATED. / ON R/H MLG DOOR ACTUATOR TO KEEL BEAM ATTACHMENT FITTING, AFT LUG BORE REWORKED AND NEW OVERSIZE PLAIN BUSHING INSTALLED AS PER ERO NO.R5336-0018 REV 00. INSTALLATION OF ACTUATOR COVERRED BY TASK CARD NO.53-140-002."

Part: MEGAPHONE — INOPERATIVE · airframe 50,027 hrs · 31,822 cycles

FORWARD MEGAPHONE INOP / REMOVED & REPLACED FWD MEGAPHONE IAW AMM 25-65-51. OPS CHECKED GOOD"

Part: NONE — NONE · airframe 49,524 hrs · 31,544 cycles

R2 DOOR ARMING LEVER WILL NOT STAY DOWN. IT SLOWLY WORKS ITS WAY UP TO THE UNARMED POSITION. / CLEANED & LUBRICATED & OPS CHECK OF THE SLIDE ARMING MECHANISM REF AMM 52-13-22. OPS CHECK GOOD. NO DISCREPANCIES NOTED AT THIS TIME"

Part: LOCK — FAILED (MLG) · airframe 48,555 hrs · 31,022 cycles

RT SIDE STAY LOCK FAILED / RT MLG & MLG RT ACTUATOR REPLACED ON FEAM WO# MIA WA-055. VERIFIED W.O. COMPLETED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,539 hrs · 31,013 cycles

SEVERAL EMERGENCY LIGHT DOOR SIGN MARKING TO BE RELAMP. / ALL DEFFECTIVE EMERGENCY LIGHT DOOR SIGN WARNING RELAMPED AND TESTED SERVICEABLE IAW AMM 33-51-16-400-001-A AND AMM 33-51-17-400-001-A"

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 46,278 hrs · 29,803 cycles

EMERGENCY LIGHT BATTERIES FAILED A CHECK. R & R ALL FOUR BATTERIES.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 46,168 hrs · 29,752 cycles

FWD MEGAPHONE INOP/ R&R MEGAPHONE BATTERIES"

Part: SIGN — MISSING (CABIN)

EMERGENCY EXIT SIGN IN ROW 12F MISSING. INSTALLED EMERGENCY EXIT SIGN. OPS CHECK GOOD. A/C OK FOR SERVICE."

Part: COMPUTER — MALFUNCTIONED (MLG) · airframe 43,779 hrs · 28,504 cycles

LANDING GEAR DID NOT RETRACT DURING DEPARTURE. R & R THE NR 2 LGCIU COMPUTER.

Part: A/C PACK — ODOR (LEFT) · airframe 41,139 hrs · 27,252 cycles

CREW REPORTS VINEGAR FUMES IN THE FLIGHT DECK AND FORWARD CABIN/TS FOUND LH PACK CAUSING ODOR. DEFERRED LEFT PACK. FINAL CORRECTIVE ACTION PENDING"

Part: SENSOR — LEAKING (OIL TEMP) · airframe 39,891 hrs · 26,608 cycles

OIL ODOR IN VENTILATION SYSTEM. TIGHTENED OIL TEMP SENSOR.

Part: O-RING — FAILED (APU) · airframe 39,839 hrs · 26,584 cycles

MUSTY ODOR THROUGH VENTS WITH BOTH PACKS ON. R & R DEFECTIVE O-RING AT APU GEN BASE

Part: NUT — LOOSE (GENERATOR) · airframe 39,799 hrs · 26,564 cycles

FA'S REPORTED AN ODOR IN THE MID-CABIN DURING ENTIRE FLIGHT. FOUND OIL LEAKING FROM GENERATOR FLANGE. TORQUED THE MOUNTING NUTS.

Part: SPRING — BROKEN (GIRT BAR FITTING) · airframe 37,885 hrs · 25,618 cycles

LEFT AFT PASSENGER DOOR, L2 GIRT BAR FITTING SPRING BROKEN. R & R SPRING IAW AMM 52-13-31 AND DWG 18D 53480282.

Part: FDU — FAULTY (APU) · airframe 36,758 hrs · 25,063 cycles

CHECK FIRE DETECTION UNIT, AUXILIARY POWER UNIT FIRE TEST, FAILURE MSG AT POST FLIGHT REPORT. IAW TSM 31-32-00 R & R FIRE DETECTION UNIT IAW AMM 26-13-34. OPERATIONAL TESTED GOOD, NO DISCREPANCY NOTED.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

FLIGHT ATTENDANT REPORTS, AFT FLIGHT ATTENDANT POSITION B, EMER FLASHLIGHT IS INOPERATIVE. INSTALLED NEW FLASHLIGHT BATTERY IAW AMM 25-65-00. OPERATIONS CHECKED GOOD.

Part: ANGLE — CRACKED (FUSELAGE)

RIGHT AFT TI ANGLE CRACKED. R & R RT AFT TI ANGLE IAW SRM 51-12-11, E88 RES T6252 & ERO 5331-004. OPERATIONS & LEAK CHECK GOOD IAW AMM 29-00-00 & 71-00-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

AFT FLIGHT ATTENDANT RT FLASHLIGHT DOES NOT BLINK. R & R AFT FLIGHT ATTENDANT RT FLASHLIGHT BATTERY IAW AMM 25-60-00 & ESPM 20-44-00. OPERATIONS CHECKED GOOD. THIS CLEARS MEL 25-60-08A, DMI 9712. PLACARDS REMOVED.

Part: PROXIMITY SWITCH — OUT OF ADJUST (R1 DOOR)

ON CLIMB OUT FLIGHT ATTENDANT`S OBSERVED RED PRESS LIGHT ON R1 DOOR FLIGHT ATTENDANT`S HEARD ABNORMAL LOUD NOISE. ON ECAM DOORS PAGE HAD R1 DOOR UNARMED, NON-LIGHT, LIGHT SHOWING NOT ARMED NO QRH FOR THIS QRC AOM SUPPLEMENTAL , OR COMPUTER RESETS. RAN LANDING DISTANCE CALCULATION. ADJUSTED R1 ESCAPE SLIDE PROX SWITCH 4WN2 IAW MM 52-71-00-820-053-A , OPERATIONS CHECKED GOOD.