N525NK

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,572 hrs · 27,851 cycles

DIRTY SOCK SMELL IN DESCENT BELOW 10000 APROX 30 SEC DURATION UNABLE TO ISOLATE. ACCR W/IDLE POWER FLT DECK ONLY. SUSPECT PACK 1 -PERFORMED AQE ISOLATION PER AMM 05-50-810-831,COUND NOT CONFIRM SOURCE OR RECREATE,NO HISTORY,OK FOR SVC

Part: BATTERY — FAILED (EPSU 10WL) · airframe 58,413 hrs · 26,838 cycles

EPSU BATT 10WL BAD-R&R EPSU BATT AT 10WL IAW AMM 33-51-38 OPS CHECK GOOD

Part: NOT REPORTED — NOT REPORTED · airframe 54,079 hrs · 24,837 cycles

FA "A" MEGAPHONE NOT DISPLAYING GREEN INDICATOR LIGHT-R/R FWD F/A "A" MEGAPHONE IAW A319 EMERGENCY EQUIPMENT LAYOUT DRAWING# A319-EMER EQUIP

Part: UNKNOWN — ODOR (CABIN) · airframe 53,417 hrs · 24,558 cycles

STRONG SMELL OF OZONE AFTER TAKEOFF. CLEARED SHORTLY AFTER ( POTABLE WATER SYSTEMS )-FILLED,DRAINED, AND REFILLED POTABLE WATER SYSTEM IAW AMM 12-15-38. TESTED WATER SYSTEM WITH TEST STRIPS FOR FREE CHLORINE IAW AMM 38-10-00. TEST OK, NO DISIFENCTANT DETECTED, R/R GALLEY WATER FILTERS IAW AMM 38-12-023. MDDR 15346 IS CLEARED.MOC NOTIFIED, PLACARD REMOVED.

Part: UNKNOWN — VIBRATION (FUSELAGE) · airframe 52,531 hrs · 24,206 cycles

VIBRATION FELT DURING CLIMB DESCENT AND APPROACH WITH AUTO PILOT 1 OR 2 ON IT STOPPED WITH AP. OFF AND SLIGHT RUDDER PRESSURE. PERFORMED GVI OF TAIL SECTION NO DISCREPANCIES NOTED. PERFORMED OPS TEST OF RUDDER TRIM PER 27-22-00 OPS TEST GOOD. PER TSM 05-50-00-810-801-A INTERPRETED VIBRATION SHEET ON THE DECISION TABLE AND RESULTS POINT TO THE RUDDER NEXT TASK TO BE PERFORMED IS 27-20-00-810-802-A (AIRFRAME VIBRATION DUE TO THE RUDDER) REF LOG PAGE 2773151-1 FOR CONTINUE TROUBLESHOOTING.

Part: CONTROLLER — MALFUNCTIONED (PITOT HEAT) · airframe 51,964 hrs · 23,966 cycles

IN CRUISE GOT ECAM ANTI ICE CAPT L STAT AND CAPT R STAT. 2 MINS PRIOR WE BOTH SMELLED A FUNNY ODOR-POSSIBLE FIRE AND OR SMOKE- WENT AWAY AFTER ABOUT 10 MINS-ACCOMPLISHED TSM 30-31-00-810-807-A FAULT CONFIRMED, R STATIC PROBE 8DA1 AND CHECK STATIC PHC 1 SUPPLY. CHECKED R STATIC PROBE 8DA1 RESISTANCE BETWEEN PIN 2 AND PIN 1, 12.0 OHMS (NORMAL RANGE). REF TSM 30-31-00-810-806-A CB 5DA1 CLOSED AND 28VDC AT PIN A M OF THE PHC 1 (6DA1) PER BOTH TSM NEXT STEP IS REPLACEMENT OF THE PHC 1 (6DA1) R&R PHC 1 (6DA1) IAW AMM 30-31-34. PHC 1 IS THE SOURCE OF THE ODOR/INTERNAL FAIL. OPERATIONAL TEST OF THE PROBE ICE PROTECTION SYSTEM OK NO FURTHER FAULTS NOTED. AC OK FOR RETURN TO SERVICE. MOC NOTIFIED.

Part: UNKNOWN — ODOR (AFT CABIN) · airframe 51,894 hrs · 23,934 cycles

FA REPORTS FUME WHEN WE STARTED DESCENT IN AFT PART OF AIRCRAFT-ACCOMPLISHED TSM 05-50-00-810-831. ISOLATED PACKS 1 & 2 WITH ENGINES AND APU BLLED. NO ODOR NOTED. ACFT OK FOR SERVICE

Part: GUSSET — DAMAGED (FRM 68 S16L) · airframe 51,862 hrs · 23,918 cycles

REF TC# ZL-100-02-1 FR68 STR16L GUSSET @ RAF01 OPENED REF HEACO NRI # 20326-REPAIRED FR68 STR 16L GUSSET ATTACH HOLES 1-5 IAW AIRBUS RD/80524669/007/2019 #D REF EO 5341-2116 CAT B REPAIR REQUIRES REINSPECT AT 37100 FC/7430 FH INTERVAL OF 2300FC/4600FH PER RDAF 80916460/003/2021 #A. REF HAECO N/R 20326

Part: SPAR — CORRODED (RT WING) · airframe 51,862 hrs · 23,918 cycles

REF MWI 2482736-1 PERFORM PERMANENT REPAIR OF CORROSION AT FWD SPAR BETWEEN RIB 5-6. RAF 01 OPENED. REF HAECO NRI 20139-ACCOMPLISHED REPAIR OF CORROSION AT RH WING FRONT SPAR TOP SURFACE BETWEEN RIBS 5 & 6 PER REPAIR DRAWING R572-58616 ISSUE K REF EO 5721-2108. THIS IS A CAT B REPAIR REQUIRES REINSPECT AT 56600 FC/113200 FH PER RDAF 80706541/024/2021 #A. REF HAECO N/R 20139

Part: FRAME — CRACKED (FRM 20 S10-11L) · airframe 51,862 hrs · 23,918 cycles

FOUND DURING TC 531155-02-01L: CRACK ON FR 20 STR 10-11-LH. RAF 01 OPENED. REF HAECO NRI 20269-REPAIRED HOLES #5 & 6 AT FR20 STR 10-11 L/H DOUBLE JOGGLE AREA PER DRW R531-13041 REF EO 5311-2117 CAT B REPAIR REQUIRES REINSPECT AT 8900 FC-FH NOT RELEVANT. INTERVAL 6300FC/FH NOT RELEVANT PER RDAF 80916895/003/2021 #A. REF HAECO N/R 20269

Part: SKIN — DENTED (FRMS 68-69 S19L) · airframe 51,862 hrs · 23,918 cycles

FOUND ON WALKAROUND: DENT AT FR 68-69 STR 19 LH MEASURES 2.75 LENGTH 1.5 WIDTH AND .035 DEPTH. RAF-01 2760207-01 OPENED-ACCOMPLISHED PERMANENT REPAIR OF FUSELAGE SKIN LH FR68+4.5" STR 19L IAW A319 SRM 53-41-11-300-095. REF REO 5341-2115 CAT A REPAIR NO REINSPECT REQUIRED REF HAECO N/R 20277

Part: UNKNOWN — FUMES · airframe 50,962 hrs · 23,587 cycles

FUME EVENT PACK 1 ISULATED DURNING DECENT-IAW TASK TSM 05-50-00-810-831 NO FUMES OR SMELL NOTED THROUGH OUT TASK AERO TRACER NO INDICATIONS OF FUMES OK TO CONTINUE

Part: MEGAPHONE — MISSING (CABIN) · airframe 48,857 hrs · 22,666 cycles

AFT MEGAPHONE QC12 MISSING. R/R AFT MEGAPHONE IAW CMM 25-60-01.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 47,445 hrs · 22,026 cycles

FWD F/A STATION MEGAPHONE NOT WORKING. REPLACED FWD F/A STATION MEGAPHONE IAW EMERGENCY EQUIPMENT LAYOUT AND AMM 25-65-51 OPS TEST GOOD.

Part: EPR SYSTEM — MALFUNCTIONED (NR 2 ENGINE) · airframe 46,970 hrs · 21,826 cycles

A+ CRUISE FL360 ENGINE NR 2 EPR MODE FAULT DEGRADE MODE PER COM TURNED ON N1 MODE FOR ENGINE 1AND 2-PERFORMED TSM 73-22-009-810-818-B INSPETED HARNESS EEC(4000KS) TO P2/T2 SENSOR CONNECTOR AND CONNECTS AND P2 NEUMATIC LINE NO DEFECT NOTED. PER MX REQUEST R/R P2/T2 SENSOR IAW AMM 73-21-11 OPS CHECK GOOD NO DEFECT NOTED THIS IA AN SDR ITEM.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 46,275 hrs · 21,546 cycles

HYD FLUID COULD BE SMELLED IN CABIN AND FLIGHT DECK-PERFORMED INSPECTION OF CABIN ODOR WHILE PACKS 1 & 2 RUNNING. COULD NOT DUPLICATE HYD FLUID SMELLS/ODOR IAW AMM 05-50-00-810-831-A.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,666 hrs · 20,441 cycles

F/A REPORTED A DIRTY SOCK ODOR TOWARD THE AFT CABIN, COCKPIT CREW COMPLIED WITH QRM, SHUT OFF THE NR 2 PACK, ODOR REMAINED AND DID NOT DISSAPATE. PERFORMED TSM 05-50-00 NO ODOR NOTED, OIL LEVELS CHECKED OK. NO LEAKS DETECTED. ACFT OK FOR SERVICE

Part: SKIN — CORRODED (LT WING) · airframe 43,551 hrs · 20,390 cycles

CORROSION FOUND ON THE LT WING PANEL 2 TOP. DAMAGED 80MM L X 40MM W X 4.22MM D, REPAIRED IAW R572-58616 ISSUE H.

Part: SKIN — CORRODED (RT WING) · airframe 43,551 hrs · 20,390 cycles

CORROSION FOUND ON THE RT WING PANEL 2, TOP AT WS 970, RIBS 17-18.

Part: HINGE ARM — DISTORTED (VERTICAL STAB) · airframe 43,551 hrs · 20,390 cycles

DISTORTION FOUND ON THE HINGE ARMS AT RIB 5, VERTICAL STAB.

Part: ECS — CONTAMINATED · airframe 43,206 hrs · 20,265 cycles

COCKPIT ODOR DURING DECENT LEVELING AT 5000'. ODORS DETECTED IN COCKPIT. DISAPPEARED AS SOON AS PACK 1 WAS SHUT OFF. ISOLATED TO PACK 1 LOCKED OUT DUE TO FUME EVENT. REACTIVATED PACK 1 IN ORDER TO FACILITATE OTHER MX IAW AMM 21-51-51. OPS CHECK GOOD. PERFORMED THOROUGH INSPECTION OF BLEED AIR. NO EVIDENCE OF OIL CONTAMINATION FOUND. RAN ENGINES IAW AMM 71-00-00. NO SMELL NOTED. PERFORMED DECONTAMINATION OF ENVIRONMENTAL CONTROL SYSTEM IAW AMM 21-00-00. NO SMELL NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,153 hrs · 20,243 cycles

AFT FLIGHT ATTENDANT REPORTED FUMES DURING DECENT, PERFORMED TSM 05-50-00-810-831-A. COULD NOT DUPLICATE THE ODOR ON GROUND. POSSIBLE TYPE 9 CAUSE IAW TSM 05-50-00. AIRCRAFT OK FOR CONTINUED SERVICE.

Part: SEAL — LEAKING (DEOILER) · airframe 43,034 hrs · 20,191 cycles

ODOR DURING DESCENT. ABLE TO ISOLATE TO THE NR 2 PACK. MUSTY SOCK ODOR. REPLACED THE DEOILER CARBON SEAL IAW AMM 72-60-31 AND PERFORMED DECONTAMINATION OF ECS IAW 21-00-00.

Part: ECS — CONTAMINATED · airframe 43,036 hrs · 20,192 cycles

DURING DESCENT AT 5000 FT, AN ODOR OF DIRTY SOCKS & OIL IN THE COCKPIT AND CABIN. PERFORMED TSM 05-50-00-810-A, AND TSM 71-00-00-810-801. PERFORMED DECONTAMINATION OF THE ENVIROMENTAL CONTROL SYSTEM. NO ODOR NOTICED.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 43,031 hrs · 20,189 cycles

FUME EVENT DURING DESCENT, UNABLE TO ISOLATE. PERFORMED TSM 05-50-00-810-831-A, NO ODOR PRESENT AFTER THE NR 1 & 2 ENGINE IDLE RUN . PERFORMED OPERATIONAL CHECK OF THE NR 1 &2 PACKS WITH APU AND ENGINE BLEED SOURCE. NO ODOR PRESENT. ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 41,853 hrs · 19,703 cycles

F/A REPORTED DIRTY SOCK SMELL ON DESCENT . PERFORMED CABIN ODOR IDENTIFICATION AND RUN BOTH PACKS 1 AND 2 WITH NO ODORS TO REPORT IAW AMM 05-50-00-710-079-A NO SIGNS OF LEAKAGE ON ENGINES OR APU.

Part: SEAL — LEAKING (NR 1 ENGINE) · airframe 41,854 hrs · 19,704 cycles

DIRTYSOCK/FUNGUS SMELL ON DESCENT, SHUT PACK 2 OFF, SMELL REMAINED PACK 2 BACK ON SHUT PACK 1 OFF & SMELL WENT AWAY. PER TSM 05-50-00-810-831-A AND CAPTAIN DEBRIEFING POINT TO PACK NR 1 AND ENG NR 1 FOR SOURCE OF SMELL. PER TSM TI-00-510-801-A FOUND ENG NR 1 DE-OILER SEAL LEAKING. R&R DE OILER SEAL IAW AMM 72-60-31 AND MAKING RING IAW 72-60-29. ACCOMPLISHED ENG IDLE RUN IAW AMM 71-00-00 NO LEAKS OR OIL NOTED AT THIS TIME. REF LOG PAGE 2292916-2 FOR NR 1 PACK DEFERRAL.

Part: UNKNOWN — UNKNOWN (CABIN) · airframe 41,218 hrs · 19,415 cycles

DIRTY SOCK ODOR REPORTED DURING CLIMB AROUND 10000 FT, FROM AFT FLT ATT. WE PERF COM PROC + TURNED OFF # 2 PACK. SMELL WENT AWAY UNTIL PARKING AT GATE AND THEN THE SMELL RETURNED EVEN STRONGER.IDENTIFICATION OF THE COST OF CABIN ODORS WAS PERFORMED IAW ISM-05-50-00-810-831-A. ENGINE RUN AND APU TEST WAS PERFORMED. NO ODORS DETECTED.

Part: BATTERY PACK — INOPERATIVE (MEGAPHONE) · airframe 41,115 hrs · 19,371 cycles

R2 JUMPSEAT MEGAPHONE IS INOPERATIVE. REPLACED DEAD BATTERIES IN R2 JUMPSEAT MEGAPHONE IAW AMM 25-65-51, OPS CHECKED OK.

Part: FAN — MALFUNCTIONED (AFT) · airframe 40,998 hrs · 19,328 cycles

FA REPORTED AN ALARM TYPE SOUND IN AFT GALLEY DURING FLIGHT, SOUND CONTINUED ON GROUND AFTER ENGINE SHUTDOWN. REMOVED & REPLACED THE LAVATORY & GALLEY EXTRACT FANS IAW AMM 21-23-51. PERFORMED OPS TEST OF THE PACK TEMP-CONTROL SYSTEM IAW AMM 21-61-00. TESTED OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 40,316 hrs · 19,040 cycles

SUSPECTED ODOR FROM NR 1 PACK . PERFORMED DECONTAMINATION OF THE NR 1 PACK IAW AMM 21-00-00-615-002-A. RAN NR 1 ENGINE IAW AMM 71-00-00 WITH THE NR 1 PACKON, NO ODORS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 39,710 hrs · 18,762 cycles

AFT F/A REPORTS ODOR SIMILAR IN THE AFT GALLEY SIMILAR TO A "WET SOCK SMELL" "MUSTY SMELL" IN CRUISE AT FL 370. TROUBLESHOOTING CARRIED OUT WITH TSM 05-50-00-810-831-A, UNABLE TO DUPLICATE ODOR FROM BOTH PACK SYSTEM AND ODOR ISOLATED AS TYPE 9 IN AFT GALLEY AREA ONLY. CLEANING CREW CLEANED AREA AND ODOR NO LONGER PRESENT IN AIRCRAFT.

Part: COMPUTER — MALFUNCTIONED (BLEED AIR SYS) · airframe 39,297 hrs · 18,581 cycles

NR 1 IAW AMM 36-11-00 OPS CHECK GOOD. NO FAULTS AT THIS TIME. SWAPPED BMC NR 1 WITH BMC NR 2 FOR TROUBLESHOOTING PURPOSES. BITE TEST GOOD IAW AMM 36-11-00. BMC NR 1 P/N 785002-9 S/N 2845 IS IN NUMBER 2 POSITION. BMC NR 2 P/N 785002-8 S/N 6360 IS IN NUMBER 1 POSITION.

Part: UNKNOWN — ODOR · airframe 39,291 hrs · 18,577 cycles

FUME EVENT, ON DECENT AROUND 5000FT NOTICED FOUL SMELL. TURNED OFF PACK 1 SMELL WENT AWAY. PERFORMED TSM 05-50-00-810-831-A. THE COSRS IDENTIFIED ENG 1 OR PACK 1 INSPECTED ENG 1 IAW TSM 71-00-00-810-801. NO DEFECTS NOTED. PERFORMED TSM 21-00-00-810-801 NO DEFECTS NOTED. PERFORMED PACK BURN IAW AMM 21-00-00-615-003. NO ODOR PRESENT AT THIS TIME. A/C IS APPROVED FOR CONTINUED SERVICE.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 39,121 hrs · 18,505 cycles

ODOR DUIRNG TAKEOFF, CLIMB, AND CRUISE WITH NR 2 PACK OFF THE ODOR DECREASED. REACTIVATED THE NR 2 PACK IAW AMM 21-51-00, PERFORMED VISUAL INSPECTION OF THE NR 2 PACK ASSEMBLY, FOUND NO LEAKS OR ABNORMAL DISCOLORATION. PERFORMED OPS CHECK OF THE NR 2 PACK WITH APU & NR 2 ENGINE IAW AMM 21-00-00, NO ODOR NOTED AT THIS TIME.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 39,053 hrs · 18,477 cycles

ROW 25 ABC O2 MASKS DROPPED. REPACKED AND STOWED OXYGEN MASKS AT SEAT ROW 25 ABC IAW 35-21-43. OPS CHECK GOOD.

Part: CONTAINER — DEFECTIVE (CABIN) · airframe 39,001 hrs · 18,455 cycles

ROW 7 SEATS DEF O2 MASKS DEPLOYED ON LANDING. R&R EMERGENCY OXYGEN CONTAINER ON ROW 7DEF IAW AMM 35-21-41. DROP CHECK OK IAW MAM 35-23-00. THIS CLEARS DMI 2123608-1. MOC NOTIFIED PLACARD REMOVED

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 38,995 hrs · 18,453 cycles

ROW 8 DEF OXY DOOR OPEN AND MASK DEPLOYED. R&R EMERGENCY O2 CONTAINER

Part: OXYGEN MASK — UNWANTED DEPLOY (SEATS 8 DEF) · airframe 38,980 hrs · 18,447 cycles

FA REPORTED THE OXYGEN MASKS AT SEATS 8D, 8E, AND 8F DROPPED, CALLED DURING TAXI IN. PERFORMED OPERATIONAL CHECK OF THE MASK RELEASE IAW AMM 35-23-710-001-A. OPS CHECKED GOOD.

Part: SEAL — LEAKING (DE OILER) · airframe 38,767 hrs · 18,348 cycles

DIRTY SOCK ODOR DURING APPROACH AND TAXI IN. ODOR WAS IN CABIN AND COCKPIT. FOUND SOURCE OF ODOR TO BE COMING ENGINE BLEEDS VIA DEOILER SEALS IAW TSM 71-00-00-810-801-A. R & R DEOILER SEALS IAW AMM 72-60-31. NO FURTHER ODORS NOTED.

Part: FILTER — ODOR (RECIRCULATION) · airframe 38,666 hrs · 18,307 cycles

STRONG HYDRAULIC FLUID ODOR IN COCKPIT DURING FLIGHT, FA'S ADVISED ODOR IN CABIN ALSO. REMOVED AND REPLACED THE RT CABIN RECIRCULATION FILTER IAW AMM 21-21-41 PB401 PERFORMED NR 2 PACK BURNOUT IAW AMM 21-00-00. NO FUMES OR ODOR NOTED.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 4 ABC) · airframe 38,183 hrs · 18,098 cycles

AFTER LANDING, FA REPORTS OXYGEN MASKS DROPPED FROM SEAT 4 ABC. RESTOWED THE MASKS AND MANUAL TESTED GOOD IAW AMM 35-21-43 AND AMM 35-23-00.

Part: OXYGEN MASK — UNWANTED DEPLOY (GALLEY) · airframe 38,163 hrs · 18,089 cycles

FWD GALLEY OXYGEN MASK FELL DOWN. STOWED FWD GALLEY OXYGEN MASK IAW AMM 35-21-43. NO DEFECTS NOTED. DROP TESTED OKAY.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 8) · airframe 38,163 hrs · 18,089 cycles

ROW 8 RIGHT SIDE OXYGEN MASKS DROPPED. STOWED MASK PER AMM 35-21-43

Part: OXYGEN MASK — DEPLOYED (CABIN)

ON LANDING O2 MASKS ROW 12DEF DEPLOYED. PASSENGER OXYGEN STORAGE PASSENGER OXYGEN MODULES.

Part: OIL SYSTEM — LEAKING (APU) · airframe 37,850 hrs · 17,958 cycles

FUMES ODOR IN CABIN AND COCKPIT. PERFORMED PACK BURNOUT IAW AMM 21-00-00 FOUND FUMES ONLY COMING FROM APU. PERFORMED APU INSPECTION AND FOUNDLOP OIL PRESSUE SWITCHLEAKING. R&R LOP OIL PRESSURE SWITCH IAW AMM 49-94-14. LEAK CHECK GOOD PERFORMED DECONTAMINATION OF ENVIROMENTAL CONTROL SYSTEM IAW AMM 21-00-00 NO SMELL NOTICED AT THIS TIME.

Part: OXYGEN MASK — MALFUNCTIONED (COCKPIT) · airframe 37,844 hrs · 17,956 cycles

CAPTAIN OXYGEN MASK OPERATING IRREGULARLY. VIBRATION WHEN BREATHING. R & R THE OXYGEN MASK IAW AMM 35-12-41

Part: DUCT — CONTAMINATED (CABIN AIR) · airframe 36,243 hrs · 17,206 cycles

COCKPIT AND CABIN HAS AN OVERWHELMING ODOR OF URINE. CLEANERS SPRAYED AIR FRESHENER AND DEODERIZERS IN CABIN AND LAV, BUT EVEN WITH THE EXIT DOORS OPEN AND APU AIR TO VENTILATE, THE ODOR IS NOT REMOVED. REMOVED FWD PIT AFT WALLS. NOTED RESIDUAL WASTE FLUID BELOW RECIRCULATION DUCTING. CLEANED AREA. R & R RECIRCULATION FILTERS IAW AMM 21-21-41 PB401. INSTALLED PANELS IAW AMM 25-54-12.

Part: SMOKE DETECTOR — FAULTED (CARGO BAY) · airframe 369,218 hrs · 17,193 cycles

CLASS II MESSAGE SMOKE AND CARGO SMOKE DETECTOR FAULT IN FLT. CREW DISCHARGED FIRE AGENT FOR CARGO. R & R CARGO FIRE BOTTLE ASSY IAW AMM 26-23-42. CHECK OF FIRING CIRCUIT CONTINUITY C/W IAW AMM 26-23-00. CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 35,674 hrs · 16,958 cycles

R1 DOOR SLIDE ASSIST BOTTLE PRESSURE BELOW LIMITS. SERVICE R1 DOOR SLIDE ASSIST BOTTLE TO PROPER LIMITS.

Part: SEAL — BROKEN (HYD SERVICE DOOR) · airframe 35,614 hrs · 16,932 cycles

HYD SERVICE DOOR SEAL BROKEN, LOOSE. RESECURED SEAL AND INPSECTED LT HYDRAULIC DOOR IAW AMM 52-42-22, DOOR OPS NORMAL AT THIS TIME. OK TO CONTINUE SERVICE.

Part: SERVICE DOOR — UNSECURE · airframe 34,689 hrs · 16,498 cycles

BAD VIBRATION FELT DURING CLIMB NOTED IN COCKPIT AND AFT F/A REPORTED, MECHANIC IN MIDDLE OF ACFT DID NOT FEEL. PERFORMED VIBRATION INSPECTION IAW TSM 05-50-00-810-801 FOUND HYD SERVICE DOOR 197CB, OPEN UPON ARRIVAL FURTHER INSPECTION FOUND BELLY PANEL 191KB AND 192KB LOOSE. RESECURED SERVICE DOOR 197CB, RESECURED BELLY PANEL 191KB AND 192KB IAW AMM 53-35-13. NO FURTHER DAMAGED FOUND. OPS CHECK OF DOOR 197CB. OK IAW AMM 52-42-22.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW E-F) · airframe 32,396 hrs · 15,422 cycles

O2 MASK DROP ROW 3 E&F. REPACKED MASKS, PERFORMED OPS CHECK OF MANUAL MASK RELEASE IAW AMM 35-23-00-710-001-A. DROP CHECK GOOD. THIS CLEARS DMI 25213-1; PLACARD REMOVED.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 7 L) · airframe 29,055 hrs · 13,905 cycles

ROW 7L OXYGEN MASK DROPPED. PACKED OXYGEN MASK IAW AMM 35-21-43, DROP CHECKED OK IAW AMM 35-23-00.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 3DEF) · airframe 29,044 hrs · 13,901 cycles

OXYGEN MASKS ROW 3DEF DROPPED ON LANDING ROLL OUT. PACKED OXYGEN MASKS AT ROW 3DEF IAW AMM 35-21-43-550-050-B.

Part: OXYGEN MASK — LOOSE (CABIN) · airframe 28,483 hrs · 13,649 cycles

AFT F/S OXYGEN MASK DEPLOYED NEEDS TO BE RESTOWED. REPACKED F/A MASK IAW MEL 35-21-43-550-801-A.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 28,451 hrs · 13,635 cycles

DURING PHASE CHECK ARRAY INSPECTION OF LT WING, FOUND CORROSION AT TOP SKIN T/E IR SURFACE JUST OTBD IR RIB 14.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 28,451 hrs · 13,635 cycles

DURING PHASED ARRAY INSPECTION, CORROSION FOUND ON LT WING T/E LWR SURFACE INBD RIB 15. REMOVED CORROSION IAW SRM 51-74-00. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-21-11. RESTORED FINISH IAW SRM 51-75-11.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 28,451 hrs · 13,635 cycles

DURING PHASED ARRAY INSPECTION, CORROSION FOUND ON RT WING TOP SKIN T/E LOWER SURFACE BETWEEN RIBS-11-12. REMOVED CORROSION IAW SRM 51-74-00. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-21-11.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 28,451 hrs · 13,635 cycles

DURING PHASED ARRAY INSPECTION, CORROSION FOUND ON RT WING TOP SKIN LWR SURFACE AT RIB 14. REMOVED CORROSION IAW SRM 51-74-00. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-21-11. RESTORED FINISH IAW SRM 51-75-11.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 28,451 hrs · 13,635 cycles

DURING PHASE ARRAY INSPECTION, CORROSION FOUND ON RT WING TOP SKIN T/E LOWER SURFACE BETWEEN RIBS-14-15. REMOVED CORROSION IAW SRM 51-74-00. WITHIN LIMITS IAW SRM 57-21-11.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT ROW 7DEF) · airframe 27,997 hrs · 13,455 cycles

SEAT ROW 7DEF BLOCKED DUE TO OXYGEN MASK DEPLOYMENT. PERFORMED OXYGEN MASK TEST IAW AMM 35-23-00-710-001-A. OP TESTED OK.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 27,769 hrs · 13,362 cycles

CAPTAIN O2 MASK HEADSTRAP LEAKS AND WILL NOT INFLATE. R & R FULL FACE QUICK DONNING IAW AMM. OPS CHECK GOOD.

Part: HINGE — DAMAGED (OXYGEN MASK BOX) · airframe 27,655 hrs · 13,314 cycles

AFT GALLEY F/A OXYGEN MASK FELL. FOUND AFT GALLEY OXYGEN MASK BOX DOOR HINGE QUICK RELEASE NOT LOCKED & SEATED IN PLACE. SECURED DOOR HINGE IAW CMM. OPS CHECKED GOOD IAW AMM.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 27,623 hrs · 13,301 cycles

AFT GALLEY F/A OXYGEN MASK FELL. MADE SEVERAL ATTEMPTS TO STOW AND SECURE OXYGEN COMP. REPEATEDLY REOPENED ORDERED CONTAINER ASSY FOUND AFT GALLEY OXYGEN MASK BOX DOOR HINGE QUICK RELEASE NOT LOCKED/SEATED IN PLACE. RESECURED DOOR HINGE IAW AMM. OPS CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (GALLEY) · airframe 27,539 hrs · 13,259 cycles

AFT GALLEY OXYGEN MASK DROPPED ON LANDING. REPACKED MASKS AND PERFORMED DROP CHECKED OK IAW AMM 35-23-00-710-001-050A, 35-21-43-550-050A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,357 hrs · 13,187 cycles

EPSU BATTERY PACKS AT 10WL AND 13WL FAILED CAP CHECK. REPLACED BATTERY PACKS AT 10WL AND 13WL IAW AMM.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT ROW 10) · airframe 27,295 hrs · 13,158 cycles

ROW 10, OXYGEN MASK FELL. PERFORMED OPS CHECK OF MANUAL RELEASE IAW AMM. OPS CHECKED GOOD.

Part: PSU — UNSECURE (SEAT 24E) · airframe 2,713 hrs · 13,074 cycles

OXYGEN MASK COMPARTMENT OVER SEAT 24E HAS COME LOOSE. SECURED PSU SEALANT CORD IAW AMM. OPS CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 27,093 hrs · 13,064 cycles

OXYGEN MASK, PSU DROPED AFT LAV. AND AFT GALLEY MASK. REPACKED OXYGEN MASK IAW AMM PERFORMED DROP TEST OF ALL MASKS IAW AMM ALL CHECKED OK.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 14 DEF) · airframe 27,093 hrs · 13,064 cycles

OXYGEN MASK FELL OUT, ROW 14 SEATS DEF. RESET OXYGEN MASK AND PERFORMED OPS CHECK OF MANUAL MASK RELEASE IAW AMM, OPS CHECKED GOOD.

Part: CABLE — DISCONNECTED (OVERWING SLIDE) · airframe 26,564 hrs · 12,841 cycles

ON ARRIVAL, UNABLE TO INSERT SAFETY PIN INTO RT OVERWING SLIDE BOTTLE, CABLE WAS DISCONNECTED. REPLACED RT OVERWING CABLE IAW EO 5273-1301, REV ORIGINAL. OK FOR SERVICE.

Part: ACM — SEIZED (NR 1) · airframe 26,158 hrs · 12,664 cycles

STRONG BURN ODOR AND SMOKE IN COCKPIT AND CABIN, RETURNED TO DEPARTURE. PERFORMED TROUBLESHOOTING IAW TSM 05-50-00-810-831-A. FOUND AIR PACK 1 TO BE THE CAUSE ECAM " AIR PACK 1 REGUL FAULT". TROUBLESHOT IAW TSM 21-61-00-810-824-A. ON GCI INSPECTION OF PACK 1, FOUND ACM TO BE SEIZED CAUSING HOT AIR BURNING ODOR GOING INTO CABIN. R & R PCMCIA CARD IAW AMM 36-00-000-001A & 31-00-400-001A.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 26,158 hrs · 12,664 cycles

ROW 7ABC, OXYGEN MASKS DEPLOYED. PACKED PAX OXYGEN MASKS & PERFORMED OPS CHECK OF MANUAL MASK RELEASE IAW AMM 35-23-00-710-001-A. OPS CHECKED GOOD IAW AMM 35-21-43-550-801-A.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 25,738 hrs · 12,460 cycles

L2 DOOR ASSIST CYLINDER HAS PRESSURE LOW. SERVICED BOTTLE TO PROPER PSI IAW AMM.

Part: LIFE VEST — TORN (CABIN) · airframe 23,135 hrs · 11,206 cycles

INFANT SPARE LIFEVEST TORN. R & R LIFE VESTS IAW ACFT MM.

Part: SLEEVE — CORRODED (THRUST REVERSER) · airframe 26,766 hrs · 12,946 cycles

NR 1 ENGINE LT THRUST REVERSER C-DUCT EXTERNAL SURFACE SKIN WITH SPOT CORROSION AT AFT MID SECTION. DAMAGED AREA WAS REPAIRED IAW CV12-4525 DTD SEP 25, 2012 UNDER NON ROUTINE ITEM, WO A1A232, SUBJOB: 4, ITEM: 111.

Part: ACCUMULATOR — LOW PRESSURE (L2 DOOR) · airframe 21,535 hrs · 10,392 cycles

L2 DOOR ACCUMULATOR PRESSURE LOW. SERVICED L2 DOOR ACCUMULATOR PRESSURE IAW AMM 52-10-00-400-001.

Part: LIGHT — FAILED (ZONE 200) · airframe 20,902 hrs · 10,053 cycles

UPPER FUSELAGE PAX CABIN ILLUMINATION TEST SHOWS CLASS 3, FAILURE. REPLACED AND TESTED PAX CABIN READING LIGHTS AT POSITIONS 25C AND 25D IAW THE AMM TASK REF: 23-73-64-000-001-A AND 23-73-64-400-001-A SASTISFACTORY CONDITION.

Part: LAMP — FAILED (ZONE 200) · airframe 20,902 hrs · 10,053 cycles

UPPER FUSELAGE RIGHT FWD OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED AND TESTED RT FWD OVERWING EXTERIOR EMERGENCY LIGHT LAMP IAW THE AMM TASK REF: 33-51-15-000-001-A, PARA 1 THROUGH 4A,STEP 2 AND 33-51-15-400-001-A PARA 1 THROUGH 4B, STEP 2 AND 4E SASTIFACTORY CONDITION.

Part: SKIN — DENTED (ZONE 200) · airframe 20,902 hrs · 10,053 cycles

UPPER FUSELAGE FR 64+12.5 AT STR 12 RT, SKIN PANEL DENTED OUT OF SRM LIMITS. DAMAGED AREA WAS REPAIRED IAW THE SRM 53-00-11, FIG 204.

Part: SUPPORT ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

UPPER FUSELAGE PAX CABIN LAVATORY A LOWER SUPPORT ANGLE CORRODED. ANGLE REPLACED IAW AMM TASK 25-41-41-400-001-A PARA 4C STEPS G AND H.

Part: FRAME — CRACKED (ZONE 100) · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE FR 34 STR 31LT SUPPORT FRAME CRACKED. SUPPORT FRAME REPLACED IAW SRM 51-72-11.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE AFT CARGO COMPARTMENT BETWEEN FR47 AND FR55 LOWER SECTION TIE DOWN CORRODED. TIE DOWN REPLACED IAW AMM TASK 25-55-41-400-001-A.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWERFUSELAGE AFT CARGO COMPARTMENT BETWEEN FR55 AND FR59 LOWER SECTION TIE DOWN CORRODED. TIE DOWN REPLACED IAW AMM 25-55-41-400-001-A.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEM FR25 TO FR28 LOWER SECTION TIE DOWN CORRODED. TIE DOWN REPLACED IAW AMM TASK 25-54-41-400-001-A.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE AFT CARGO COMPARTMENT BETWEEN FR47 AND FR55 LOWER SECTION TIE DOWN CORRODED. TIE DOWN REPLACED IAW AMM TASK 25-55-41-400-001-A.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEN FR25 TO FR28 LOWER SECTION TIE DOWN WITH CORROSION. TIE DOWN WAS REPLACED IAW AMM TASK 25-54-41-400-001-A .

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE AFT CARGO COMPARTMENT BETWEEN FR55 AND FR59 LOWER SECTION TIE DOWN CORRODED. TIE DOWN REPLACED IAW AMM TASK 25-55-41-4000-001-A.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE AFT CARGO COMPARTMENT BETWEEN FR59 AND FR69 LOWER SECTION TIE DOWN CORRODED. TIE DOWN REPLACED IAW AMM TASK 25-55-41-400-001-A.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE AFT CARGO COMPARTMENT BETWEEN FR55 AND FR59 LOWER SECTION TIE DOWN CORRODED. TIE DOWN REPLACED IAW AMM TASK 25-55-41-400-001-A.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE FWD CARGO COMPARTMENT FR25 TO FR28 LOWER SECTION TIE DOWN CRACKED. TIE DOWN REPLACED IAW AMM TASK 25-54-41-400-001-A.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE AFT CARGO COMPARTMENT BETWEEN FR55 AND FR59 LOWER SECTION TIE DOWN CORRODED. TIE DOWN REPLACED IAW AMM TASK 25-55-41-400-001-A.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE AFT CARGO COMPARTMENT BETWEEN FR55 AND FR59 LOWER SECTION TIE DOWN CORRODED. TIE DOWN REPLACED IAW AMM TASK 25-55-41-400-001-A.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE AFT CARGO COMPARTMENT BETWEEN FR59 AND FR69 LOWER SECTION TIE DOWN CORRODED. TIE DOWN REPLACED IAW AMM TASK 25-55-41-400-001-A.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEN FR28 AND FR30 LOWER SECTION TIE DOWN CORRODED. TIE DOWN REPLACED IAW AMM TASK 25-54-41-400-001-A.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 20,902 hrs · 10,053 cycles

LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEN FR28 AND FR30 LOWER SECTION TIE DOWN CORRODED. TIE DOWN REPLACED IAW AMM TASK 25-54-41-400-001-A.

Part: SKIN — CONTAMINATED (RUDDER) · airframe 20,902 hrs · 10,053 cycles

DURING THERMOGRAPHIC INSPECTION METHOD, VERTICAL STABILIZER RUDDER, RT SIDE PANEL HAS TRAPPED FLUID AT HOISTING POINT NR 2. DAMAGED AREA WAS REPAIRED IAW REPAIR INSTRUCTIONS NR 70561884/006 AND 70561884/007.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 20,513 hrs · 9,865 cycles

PAX L2 DOOR ACCUMULATOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED PAX L2 DOOR ACCUM ASSIST BOTTLE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 20,236 hrs · 9,721 cycles

L2 DOOR EMERGENCY DAMPER HAS LOW PRESSURE. SERVICED TO PROPER PRESSURE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 19,834 hrs · 9,530 cycles

L2 DOOR AIR PRESSURE LOW. SERVICED L2 DOOR TO PROPER LEVEL OF AIR PRESS IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (PAX DOOR) · airframe 19,562 hrs · 9,396 cycles

L-2 DOOR EMERGENCY DAMPER IS LOW. PRESS AT 1.300 PSI. SERVICED L-2 DOOR EMERGENCY DAMPER IAW AMM 52-10-00-614-001, NO LEAKS NOTED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 19,482 hrs · 9,357 cycles

EMERENCY EXIT LIGHTS STUCK IN "ON" REGARDLESS OF SWITCH POSITION. OPS CHECK OF EMERGENCY EXIT LIGHTS & SIGNS IAW AMM 33-51-00-710-004. ALL INDICATIONS NORMAL.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 19,359 hrs · 9,288 cycles

L2 DOOR EMERGENCY DAMPER LOW. SERVICED L2 DOOR EMERGENCY DAMPER IAW AMM 52-10-00-614-001. LEAK CHECKED GOOD.

Part: CYLINDER — LOW PRESSURE · airframe 18,775 hrs · 9,017 cycles

DOOR ASSIST BOTTLE NEEDS SERVICING. SERVICED DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001. LEAK CHECKED OK.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 18,678 hrs · 8,964 cycles

DOOR L2 ASSIST BOTTLE REQUIRES SERVICE. SERVICED L2 DOOR ASSIST BOTTLE AS REQUIRED IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L2 DOOR ASSIST) · airframe 18,311 hrs · 8,777 cycles

L2 DOOR ASSIST BOTTLE LOW. SERVICED L2 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 17,974 hrs · 8,614 cycles

R2 DOOR LOW AIR PRESSURE. SERVICE R2 DOOR TO PROPER AIR PRESSURE IAW AMM 52-10-00-614-001.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

PAX CABIN, AFT SERVICE AREA, UPPER REAR FUSELAGE FROM STA 2936 TO STA 2992 +Y120 SHEAR PLATE CORRODED (SHEAR PLATE PN: D5347112420200) NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

PAX CABIN, AFT SERVICE AREA, UPPER REAR FUSELAGE FROM STA 2805 TO STA 2870 BETWEEN -Y960 TO -Y1292 FLOOR STRUCTURE BEAM CORRODED: CORROSION REQUIRES A MAJOR REPAIR.

Part: BUMPER BLOCK — WORN (THRUST REVESER) · airframe 15,487 hrs · 7,446 cycles

ENGINE NR 1, INBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. BUMPER WEAR REQUIRES A MAJOR REPAIR.

Part: BUMPER BLOCK — WORN (THRUST REVERSER) · airframe 15,487 hrs · 7,446 cycles

(EE4Y) ENGINE NR 2, OTBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE BUMPER WEAR REQUIRES A MAJOR REPAIR.

Part: PANEL — CORRODED (ZONE 400) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

NR 2 PYLON AFT FIXED FAIRING, OTBD/RT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

(EE4Y) PAX CABIN, AFT SERVICE AREA, UPPER REAR FUSELAGE FROM STA 2786 TO STA 2796 -Y1292 SEAT TRACK CORRODED (SEAT TRACK PN: D5347219021100) THE CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

(EE4Y) PAX CABIN, AFT SERVICE AREA, UPPER REAR FUSELAGE FROM STA 2805 TO STA 2870 BETWEEN -Y960 TO -Y1292 FLOOR STRUCTURE BEAM CORRODED. CORROSION REQUIRES A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

PAX CABIN, AFT SERVICE AREA, UPPER REAR FUSELAGE FROM STA 2786 TO STA 2796 -Y1292 SEAT TRACK CORRODED (SEAT TRACK PN: D5347219021100) NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.

Part: BUMPER BLOCK — WORN (THRUST REVERSER) · airframe 15,487 hrs · 7,446 cycles

ENGINE NR 2, INBD/LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. BUMPER WEAR REQUIRES A MAJOR REPAIR.

Part: PANEL — CORRODED (ZONE 400) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

NR 1 PYLON AFT FIXED FAIRING, OTBD/LT LATERAL SKIN PANEL WITH CORROSION. THE CORROSION REQUIRES A MAJOR REPAIR.

Part: PANEL — CORRODED (ZONE 400) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

NR 1 PYLON AF FIXED FAIRING, INBD/RT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

PAX CABIN, AFT SERVICE AREA, UPPER REAR FUSELAGE FROM STA 2799 TO STA 2874 BETWEEN -Y960 AND -Y1292 FLOOR STRUCTURE BEAM CORRODED. (BEAM PN: D5347217220500) THE CORROSION REQUIRES A MAJOR REPAIR.

Part: BUMPER BLOCK — WORN (THRUST REVERSER) · airframe 15,487 hrs · 7,446 cycles

ENGINE NR 1, OTBD/LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE WEAR REQUIRES A MAJOR REPAIR.

Part: FAIRING — CORRODED (ZONE 400) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

ENGINE NR1, PYLON AFT FIXED FAIRING, OTBD/LT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.

Part: BUMPER BLOCK — WORN (THRUST REVERSER) · airframe 15,487 hrs · 7,446 cycles

ENGINE NR 1, INBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE BUMPER WEAR REQUIRES A MAJOR REPAIR.

Part: PANEL — CORRODED (ZONE 400) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

NR 2 PYLON AFT FIXED FAIRING, INBD/LT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

PAX CABIN, AFT SERVICE AREA, UPPER REAR FUSELAGE FROM STA 2799 TO STA 2874 BETWEEN -Y960 AND -Y1292 FLOOR STRUCTURE BEAM CORRODED. CORROSION REQUIRES A MAJOR REPAIR.

Part: BUMPER BLOCK — WORN (THRUST REVERSER) · airframe 15,487 hrs · 7,446 cycles

ENGINE NR.2, INBD/LT THRUST REVERESE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE THE BUMPER WEAR REQUIRES A MAJOR REPAIR.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

PAX CABIN, AFT SERVICE AREA, UPPER REAR FUSELAGE FROM STA 2936 TO STA 2992 +Y120 SHEAR PLATE CORRODED. CORROSION REQUIRES A MAJOR REPAIR.

Part: PANEL — CORRODED (ZONE 400) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

ENGINE NR1, PYLON AFT FIXED FAIRING, INBD/RT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.

Part: BUMPER BLOCK — WORN (THRUST REVERSER) · airframe 15,487 hrs · 7,446 cycles

ENG NR 2, OTBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. BUMPER WEAR REQUIRES A MAJOR REPAIR.

Part: PANEL — CORRODED (ZONE 400) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

ENG NR 2, PYLON AFT FIXED FAIRING, OTBD/RT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.

Part: PANEL — CORRODED (ZONE 400) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

ENGINE NR 2, PYLON AFT FIXED FAIRING, INBD/LT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.

Part: BUMPER BLOCK — WORN (THRUST REVERSER) · airframe 15,487 hrs · 7,446 cycles

ENG NR 1, OTBD/ LT THRUST REVERSER C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. WEAR REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

(EE4Y) PAX CABIN, AFT SERVICE AREA, UPPER REAR FUSELAGE, FROM STA 2835 TO STA 2884 +Y76.5 FLOOR STRUCTURE BEAM CORRODED (BEAM PN: D5347219220000) NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

PAX CABIN SERVICE AREA, UPPER REAR FUSELAGE, FROM STA 2835 TO STA 2884 +Y76.5 FLOOR STRUCTURE BEAM CORRODED. CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

PAX CABIN, AFT SERVICE AREA, UPPER REAR FUSELAGE, FROM STA 2936 TO STA 2992 +Y160.5 FLOOR STRUCTURE BEAM CORRODED. CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

PAX CABIN, AFT SERVICE AREA, UPPER REAR FUSELAGE, FROM STA 2936 TO STA 2992 +Y160.5 FLOOR STRUCTURE BEAM CORRODED (BEAM PN: D5347219620000) NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

PAX CABIN, AFT SERVICE AREA, UPPER REAR FUSELAGE, FROM STA 2786 TO STA 2796 +Y76.5 SEAT TRACK CORRODED. CORROSION REQUIRES A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,487 hrs · 7,446 cycles

PAX CABIN, AFT SERVICE AREA, UPPER REAR FUSELAGE, FROM STA 2786 TO STA 2796 +Y76.5 SEAT TRACK CORRODED (SEAT TRACK PN: D5347213320200) THE CORROSION REQUIRES A MAJOR REPAIR.

Part: RELEASE CABLE — INOPERATIVE (OVERWING EXIT) · airframe 10,766 hrs · 5,198 cycles

RT OVERWING EXIT FAILED MANUAL AND AUTOMATIC SLIDE RELEASE CHECK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,853 hrs · 2,373 cycles

AFT GALLLEY FLOORBEAM -Y765 BETWEEN FR 67 AND FR 64 CORRODED. REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,853 hrs · 2,373 cycles

AFT GALLEY FLOORBEAM, Y765 BETWEEN FR 67 AND FR 70 CORRODED. REPLACED FLOORBEAM.