N503NK

Part: OUTFLOW VALVE — FAULTED · airframe 60,706 hrs · 28,105 cycles

AFTER T.O VENT SKIN VALVE FAULT FOLLOWED BY BLOWER FAULT AND EXTRACT FAULT-REACTIVATED SKIN AIR OUTLET VLV CURRENTLY ON MEL MDDR 40498 PER AMM 21-26-00. R&R AEVC PER AMM 21-26-34. PERF AEVC TEST PER AMM 21-26-00. TEST OKAY. REF LBP 2862508-1 FOR SKIN AIR OUTLET VLV R&R

Part: NONE — NONE · airframe 60,553 hrs · 28,027 cycles

FA STATED THAT DURING THE DESCENT SHE NOTICED A "BURNING SMELL" IN THE AFT GALLEY, BUT COULD NOT FIND THE SOURCE-REF TSM 05-50-00 APU VERIFIED NO LEAKS, PERCONDITIONAL AC WITH APU AND ENG 1&2. NO SMELL NOTED. ISOLATED PACK 1&2. NO SMELL NOTED. AC OK FOR SERVICE IAW AMM 21-61-00, 49-00-00 &72-00-00

Part: NONE — NONE · airframe 60,264 hrs · 27,888 cycles

F/A'S REPORT SWEATY SOCKS SMELL DURING FINAL DECENT INTO ACY. STRONGEST AT REAR OF CABIN-PERFORMED MANUAL ENGINE START IAW AMM 71-00-00. T/S WITH ENGINE BLEEDS AND PACK 1&2. NO DEFECTS NOTED. REF L/P 2900080-1. APU CONFIRMED SOURCE OF CONTAMINATION. REF L/P 2900080-2. APU ON DEFERRAL. A/C OK FOR CONTINUED SERVICE. AIRCRAFT STATUS NORMAL.

Part: NONE — NONE · airframe 59,905 hrs · 27,715 cycles

FUME EVENT IN FLIGHT. ISOLATED PACK #2 AND ALTERNATY PACK#1 AND SMELL DID NOT GO AWAY OR DISIPATED-PERFORMED IDLE RUN ON ENG #1 & ENG #2 WITH PACK #1 ON IAW AMM 7100-00. NO SMELL NOTED AT THIS TIME.

Part: NONE — NONE · airframe 59,472 hrs · 27,496 cycles

DURING CLIMB RADAR WAS PAINTING GROUND REGARDLESS OF TILT IN MANUAL MODE. RADAR THEN COMPLETLY FAILED TWICE, AFTER 2 RESETS-TS IAW TSM 34-41-00-810-802-A. R&R XCVR WEATHER RADAR IAW AMM 34-41-33. BITE TEST NORMAL A/C OK FOR CONTINUE SERVICED

Part: SLIDE — BLOWN (ZONE 600) · airframe 58,252 hrs · 26,956 cycles

RIGHT WING EMER SLIDE BLOWN-R/R RH OFF WING ESCAPE SLIDE AND RH DISCHARGE INFLATION RESERVOIR PER AMM 25-62-46

Part: A/C PACK — ODOR (NR 2) · airframe 57,737 hrs · 26,751 cycles

FUME EVENT SHORT FINAL-REF TSM 05-50-00-810-831-A. FAULT ISOLATION PROCESS IDENTIFIED PACK 2 AS SOURCE OF SMELL. REF LP 2825432-1 FOR CORRECTIVE ACTION

Part: A/C PACK — CONTAMINATED (NR 2) · airframe 57,687 hrs · 26,730 cycles

FLIGHT ATTENDANTS REPORTING DIRTY SOCK SMELL ON DECENT NO SMELL IN FLIGHT DECK. ( PACKS A319 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - AT OR BELOW FL 370 )-ERFORMED DECONTAMINATATION OF PACK 2 IAW AMM 21-00-00. OPS CHECK GOOD, NO ODOR PRESENT.

Part: NONE — NONE (ZONE 800) · airframe 57,482 hrs · 26,647 cycles

"FOUND L1 DOOR SLIDE UNRAVELED, BLOCKING SIGHT GLASS OF PRESSURE GAUGE-DISARMED EMERGENCY CONTROL HANDLE ON L1 DOOR IAW AMM 52-10-00 SLIDE REMOVED IAW AMM 25-62-44 (JM67501) . RE INSTALLED L1 DOOR SLIDE OPS CHECK OK .PIN REMOVED. DOOR ASIST REACTIVATED."

Part: UNKNOWN — ODOR (CABIN) · airframe 57,238 hrs · 26,541 cycles

FUME EVENT DIRTY SOCK SMELL ON DESCENT THROUGH 10,000. PACK 2 TURNED OFF AND WENT AWAY TIL SHORT FINAL, THEN RETURNED. ( PACKS A319 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - AT OR BELOW FL 370 )-PERFORMED DECONTAMINATION OF THE ECS IAW AMM 21-00-00. PERFORMED OPS CHECK OF PACK 2 IAW AMM 21-00-00. OPS CHECK GOOD. NO ODOR DETECTED. THIS CLOSES DMI # 2843038-1. DMI LOG UPDATED, PLACARD REMOVED, MOC NOTIFIED.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 57,233 hrs · 26,359 cycles

FWD F/A I/B SEAT FLASHLIGHT INOP.-R/R FWD F/A I/B SEAT FLASHLIGHT IAW SPIRIT AIRLINES A319 EMERGENCY EQUIPMENT LAYOUT DRAWING # A319-EMR EQUIP. OPS CHECK GOOD. THIS CLOSES DMI # 284303201. DMI LOG UPDATED, PLACARD REMOVED, MOC NOTIFIED.

Part: UNKNOWN — ODOR (CABIN) · airframe 56,823 hrs · 26,362 cycles

FUME/ODOR DIRTY SOCKS ON SHORT FINAL W/BOTH PACKS ON.-PER TSM 05-50-00-810-831-A FOR CAUSE OF CABIN ODORS OR SMOKE. RAN APU, PACKS ENGINES WITH NO EVIDENCE OF LEAKS OF ODORS AT THIS TIME AIRCRAFT OK FOR SERVICE.

Part: SKIN — DAMAGED (WING) · airframe 55,076 hrs · 25,667 cycles

WSC FOUND LH RAF#250456802.-PERFORMED PERM REPAIR REF TO LTPR 5000996082-0010,5000996087-0010,100317329-0010 AND SPIRIT EO 5751-2005. AS PER RDAS 80779132/003/2020 THE REPAIR IS PERMANENT CAT B WITH RE INSP REQ TOP SKIN AT SRT 11 B/W RIBS 3-4 THR 30000FD/40900FH INT 25000FC/34900FH BUTT STRAP RIB 3-4 THR 38100FC/67100FH; INT-TBD; RIB 9-10 THR 40000FC

Part: COWLING — DAMAGED (NR 2 ENGINE) · airframe 55,076 hrs · 25,667 cycles

#2 ENGINE INLET COWL DAMAGE.RAF # 250456202.SDR-PERFORMED PERMANENT REPAIR FOR ALL WORK PERFORMED REF TO LTPR 1003177291-0010 SPIRIT EO 5412-2001 REPAIR IS PERMANENT CAT A NO RE-INPS RQRD AS PER RDAS ROHR/S168/2020

Part: WINDOW FRAME — DAMAGED (COCKPIT) · airframe 55,076 hrs · 25,667 cycles

RH WINDSHIELD FRAME DAMAGED RAF # 250456801.-PERFORMED PERMANENT REPAIR FOR ALL WORK PERFORMED REWF TO LTPR DO 5000999744-0010/1003177290-0010 SPIRIT EO 5311-2038. REPAIR IS CAT A PERMANENT NO RE-INSPECTION RQRD REF RDAS 80784402-003-2020

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 55,076 hrs · 25,667 cycles

RAF #2504561-2 ENTERED FOUND LH WINDSHIELD CENTER POST CRACKED.SEE NR ITEM 5000996328-0010-BOTH CONTINUITY FITTINES REPLACED. FOR ALL WORK PERFORMED PLEASE REF TO LTPR 5000996328-0010 10033173811-0010 AND SPIRIT AIRLINES EO 5311-2027

Part: UNKNOWN — ODOR (CABIN) · airframe 51,523 hrs · 24,127 cycles

DIRTY SOCK FUME SMELL WITH AMP BLEED ON, AT GATE NO ENGINE RUNNING-PERFORMED TSM 05-50-00 CABIN ODOR OR SMOKE IDENTIFICATION.

Part: A/C PACK — ODOR (NR 2) · airframe 51,470 hrs · 24,102 cycles

DURING CLIMBOUT IN HEAVY RAIN. FA'S REPORTED ODOR OF SOCKS. RAN SUP PROCEDURE-PERFORMED TSM 05-51-00-810-831-A AND FOUND PACK 2 TO BE SOURCE OF ODOR.. NO ODOR. NO ODOR PRESENT FROM ANY OTHER SOURCE SEE LP # 2436418-2 FOR MX ACTION (PACK 2)

Part: A/C PACK — ODOR (AC BAY) · airframe 51,220 hrs · 24,009 cycles

"FA SMELLS DIRTY SOCKS ON SHORT FINAL AND TAXI-TROUBLESHOOTING DONE IAW TSM 05-50-00-810-831-A AND FOUND PACK 2 AT FAULT. SEE LOG PAGE #2415732-2 FOR PACK DEFERRAL. ONE TIME AUTHORIZATION.

Part: UNKNOWN — ODOR (CABIN) · airframe 50,900 hrs · 23,885 cycles

FLIGHT ATTENDANTS REPORT REPORT " DIRTY SOCK" ODOR DURING DESCENT PROCEDURE NOT APPLIED NOTIFIED UPON ARRIVAL AT GATE-PER TSM 05-50-00-810-831-A, RUN # 1 AND # 2 ENGINES PER AMM 71-00-00. NO SMELL NOTED USING EITHER PACK # 1 AND # 2. PERFORMED VISUAL INSPECTION OF A/C FUSELAGE AND ENGINES AND NO LEAKS WERE FOUND AT THIS MOMENT PER AMM 05-00-00. AIRCRAFT IS GOOD FOR CONTINUE SERVICE

Part: UNKNOWN — ODOR (CABIN) · airframe 50,399 hrs · 23,684 cycles

FUME EVENT AT 15000 FT WITH ENGINES AT IDLE FA (A) REPORTED A STRONG OILY SMELL. WE TURNED PACK 1 OFF AND THE SMELL DIDNT GO AWAY. WE THEN TURNED OFF PACK 2 AND THE FA'S REPORTED THAT THE SMELL WENT AWAY-PERF TSM 05-50-00-810-931A FOR CAUSE OF ODOR. PER TSM AND REPORTING SHEET PACK 2 WILL BE PLACED ON DEFERRAL.SEE L/P 2396065-2.

Part: UNKNOWN — ODOR (CABIN) · airframe 50,159 hrs · 23,585 cycles

FA REPORTS ODOR IN CABIN LIKENED TO DIRTY SOCKS-C/W TSM 05-50-00-810-831-A IDENTIFICATION OF THE CAUSE OF CABIN ODOR OR SMOKE NO DEFECS NOTED CK ENG. NO BIRD INGESTION RAN PACK WITH ENG ALO WITH APU INSP ARE FRAME INSP CARGO INSP E&E COMP INSP APU AND CABIN COCKPIT NO FAULT NOTED.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 50,053 hrs · 23,541 cycles

L1 FA JUMPSEAT FLASHLIGHT INOP ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) )-R&R L1 F/A FLASHLIGHT IAW AMM 25-65-01 OPS CK GOOD THIS CLEARS DMI#241524301. MOC NOTIFIED LOG UPDATED

Part: SEAL — LEAKING (DEOILER) · airframe 47,787 hrs · 22,527 cycles

SOCK ODOR, EVALUATED THE NR 1 PACK AS WELL AS THE NR 2. CONCLUDED THERE WAS OIL CONTAMINATION IN EACH. FOUND THE OIL CONTAMINATION SOURCE TO BE THE DEOILER SEALS FOR THE NR 1 & 2 ENGINES. R & R THE DEOILER SEALS IAW AMM 72-60-31.

Part: SEAL — LEAKING (DEOILER) · airframe 47,064 hrs · 22,218 cycles

ODOR IN COCKPIT AND CABIN DURING CLIMB OUT AND DESCENT. PERFORMED TSM 71-00-00-810-801-A, ODOR DUE TO AN ENGINE LEAKAGE. FOUND THE NR 2 ENGINE DEOILER OVERBOARD VENT WITH EXCESIVE OIL. REPLACED THE DEOILER CARBON SEAL IAW AMM 72-60-31. RAN ENGINES & PACKS AND COULD NOT DUPLICATE ODOR. ACFT OK TO CONTINUE SERVICE.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 46,919 hrs · 22,153 cycles

FWD MEGAPHONE INOP. R&R FWD MEGAPHONE IAW EMERGENCY EQUIPMENT LAYOUT DRAWING: NK319-132-EQ.

Part: DUCT — ODOR · airframe 45,228 hrs · 21,428 cycles

DESCENDING THROUGH 12,000 FEET, ON APPROACH. A DIRTY SOCK ODOR WAS INTENSE. TURNED THE NR 1 PACK OFF AND HAD NO EFFECT ON THE ODOR. TURNED THE NR 2 PACK OFF, IT ALSO HAD NO EFFECT ON THE ODOR. DURING VISUAL INSPECTIONS IAW TSM 05-50-00-810-831-A, FOUND HAT IN THE PACK 2 RAM AIR INLET / INLET BYPASS DUCT. REMOVED HAT AND INSPECTED PACK 2 RAM AIR INLET / INLET BYPASS DUCT IAW AMM 21-58-61-000-802-A / 400-802-A AND FOUND TO BE GOOD AT THIS TIME. RAN ENGINE 1 AND ENGINE 2 ISOLATING PACK 1 AND PACK 2 ON ENGINE BLEED 1 AND ENGINE BLEED 2. CABIN ODORS ISOLATED...

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 44,919 hrs · 21,284 cycles

EMERGENCY DECLARED, MAINTENANCE. AC 503 FLT 860 MCO-BDL SENT ACARS ADVISED EMERGENCY DESCENT DUE LOSS OF CABIN PRESSURE AT (370FL). BOTH CPC HAVE BEEN REPLACED PER TSM. AND OPERATIONAL TEST OK. OUTFLOW REPLACED AS PRECAUTIONARY PER MOC; R&R OUTFLOW VALVE IAW AMM 21-31-00 OPS CHECK GOOD

Part: PUMP — FAILED (HYD SYSTEM) · airframe 44,684 hrs · 21,185 cycles

YELLOW HYD RESERVOIR OVERHEAT, EMERGENCY GATE RETURN. AS A PRECAUTION, CHANGED YELLOW NR 2 ENGINE HYD PUMP IAW AMM 29-13-51. OPS AND LEAK CHECKED GOOD.

Part: SENSOR — FAULTED (HYD SYSTEM) · airframe 44,675 hrs · 21,180 cycles

AFTER TAKEOFF AT APPROXIMATLEY 60 FT, HYD Y RESERVOIR OVERHEAT ILLUMINATED, RETURNED TO DEPARTURE. FOUND A FAULTED SENSOR 3151GN IAW TSM 29-13-00-810-805. R & R THE SENSOR IAW AMM 29-32-12. OPS AND LEAK CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,358 hrs · 21,033 cycles

DEAD HEADING FLIGHT ATTENDANT REPORTED DIRTY SOCK ODOR IN CABIN DURING DECENT. CAPTAIN DID NOT NOTICE ANY UNUSUAL ODORS ONLY NORMAL PACK ODOR. WALKROUND AND PACK BURN IAW AMM 05-50-00-810-831-A. NO ODOR NOTED, ACFT FOR SERVICE.

Part: A/C PACK — MALFUNCTIONED (AC BAY) · airframe 44,213 hrs · 20,969 cycles

BAD PUNGENT SMELL IN COCKPIT AND CABIN ON SHORT FINAL, FUME REPORT FILLED OUT. TROUBLESHOOTING DONE IAW TSM 05-50-00-810-831-A AND ISOLATED PACK 1 AS SOURCE OF CABIN ODOR SEE LOG PAGE 2247435-1+2 FOR DEFERRAL.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 44,177 hrs · 20,948 cycles

R2 DOOR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. OPERATIONAL TEST OF THE EMERGENCY LIGHT WAS PERFORMED IAW AMM 33-51-00 TEST OK.

Part: OXYGEN MASK — NO TEST (FIRST OFFICER'S) · airframe 43,569 hrs · 20,661 cycles

FIRST OFFICER`S OXYGEN MASK AUDIO WILL NOT TEST PROPERLY. REMOVED AND REPLACED OXYGEN MASK STORAGE BOX IAW AMM 35-12-41, PB 401. OPS AND LEAK CHECKED GOOD.

Part: FRAME — CRACKED (FRM 43) · airframe 43,460 hrs · 20,612 cycles

CRACK FOUND ON FRAME 43. REPAIRED IAW EO 5331-1713.

Part: SKIN — CORRODED (WING) · airframe 43,460 hrs · 20,612 cycles

SIX AREAS OF WING SKIN CORROED. REPAIRED IAW EO 5721-1707.

Part: SPAR — CORRODED (RT) · airframe 43,460 hrs · 20,612 cycles

RIGHT THS FWD SPAR OTBD TIP WEIGHT HAS CORROSION. BLENDED IAW EO 5514-1702.

Part: SHIELD — CRACKED (FRAME 8) · airframe 4,346,036 hrs · 20,612 cycles

A CRACK WAS FOUND ON THE LT EROSION SHIELD, FRAME 8. PERFORMED BLENDED IAW EO 5311-1715

Part: FITTING — NICKED (PYLON TO WING) · airframe 43,460 hrs · 20,612 cycles

NICK FOUND ON THE NR 1 ENGINE PYLON TO WING FITTING. REPAIRED IAW EO 5451-1704.

Part: SKIN — DAMAGED (NR 1 INLET) · airframe 4,346,036 hrs · 20,612 cycles

DAMAGE FOUND ON NR 1 ENGINE INLET COWL. REPAIRED IAW EO 5412-1712.

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 43,460 hrs · 20,612 cycles

RIGHT OTBD FLAP, ZONE 2, LOWER SURFACE HAS DISBONDED. PERFORMED EXTERNAL DOUBLER REPAIR IAW EO 5753-1708.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 43,460 hrs · 20,612 cycles

CRACK ON RT WINDSHEILD FRAME. REPAIRED IAW EO 5311-1714.

Part: FLANGE — CRACKED (FRAME 43) · airframe 43,460 hrs · 20,612 cycles

A CRACK WAS FOUND ON THE SIDE BOX FLANGE Y1292 FRAME 43, STRINGER 15L. INSTALLED FREEZE PLUG IAW EO 5331-1713

Part: UNKNOWN — ODOR (CABIN) · airframe 43,456 hrs · 20,610 cycles

DESCENDING THRU 8,000' COCKPIT FWD CABIN HAD A STRONG ACRID SMELL TURNED OFF BOTH PACKS SMELL RESIDED.

Part: FASTENER — MISSING (OXYGEN MASK) · airframe 43,427 hrs · 20,601 cycles

CA O2 MASK MISSING FASTENER ON NOSE BRIDGE. R&R O2 MASK IAW AMM 35-12-41. OPS CKS NORMAL. NO DEFECTS NOTED.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 43,209 hrs · 20,501 cycles

F/A AND COCKPIT CREW SMELLED A LIGHT DIRTY SOCK ODOR ON APPROACH INTO LAX, SECURED PACK 2 ODOR DID DISIPATE. OPS TESTED IAW TSM 05-50-00-810-831-A NO SMELL DETECTED ALL CHECKS GOOD THIS CLEARS DMI PLACARD REMOVED MOC NOTIFIED RAN ENG LEAKAGE FOR PACK ODOR FOR PACK ODOR IAW TSM 71-00-00-810-801-A RAN APU WITHOUT MOTORS AND PACKS ON IAW 21-00-00-810-801-A NO SMELLS DETECTED

Part: A/C PACK — ODOR · airframe 43,205 hrs · 20,500 cycles

FA REPORTED STRONG DIRTY SOCK ODOR AFER TAKEOFF, ODOR LASTED ON 3-4 MINUTES THEN DISSIPATED. NO FURTHER ODOR UNTIL SHORT FINAL MCI. SECURED PACK 2 PER OB -16-52. ODOR DID NOT DISSIPATE. ODOR WAS NOTICEABLE IN FLIGHT DECK. ACCOMPLISHED STEPS IN TSM 05-50-810-831. DECISION TABLE PONTS TO #1 ENGINE AS CAUSE OF ODOR RAN ENG 1 AND 2 ENG WITH CREW IAW AMM 71-00-00. NO ODOR NOTED. RAN PACKS 1 AND 2 WTIH APU IAW AMM 12-33-21 NO ODOR NOTED. A/C OK FOR SERVICE

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,052 hrs · 20,435 cycles

EMERGENCY BATTERY PACK ESPU 11WL FAILED SYSTEM TEST. R&R BATTERY OF THE ESPU AT 11WL IAW AMM 33-51-38-400-002A. OPS CHCK GOOD PER SUBTASK 33-51-38-710-052B.

Part: STOWAGE BOX — DEFECTIVE (COCKPIT) · airframe 43,036 hrs · 20,429 cycles

FO O2 MASK WILL NOT TEST. R&R FO O2 MASK STORAGE BOX ASSY. IAW AMM 35-12-41 OPS OK. NO LEAKS NOTED

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 42,054 hrs · 20,004 cycles

FORWARD MEGAPHONE INOPERATIVE. REMOVED AND REPLACED THE MEGAPHONE IAW DRAWING NK319-132-EQ REV 6. OPS CHECKED GOOD.

Part: SEAL — LEAKING (DEOILER) · airframe 42,012 hrs · 19,985 cycles

DIRTY SOCK, OIL ODOR IN ALL PHASES OF FLIGHT. R & R DEOILER SEAL ASSEMBLY IAW AMM 72-60-31. DECONTAMINATION OF THE ECS ONLY LEFT PACK ACCOMPLISHED IAW AMM 21-00-00-615-004. R & R RECIRCULATION FILTERS AS PRECAUTION IAW AMM 71-00-00. NO ODOR AT THIS TIME WITH BOTH PACKS RUNNING

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 38,611 hrs · 18,482 cycles

AFT GALLEY MEGA PHONE TEST ALARM INOPERATIVE. R & R AFT GALLEY MEGAPHONE IAW EMERGENCY EQUIPMENT LAYOUT DWG NK319-132-EQ, REV 6.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 38,283 hrs · 18,341 cycles

FWD MEGAPHONE INOPERATIVE. R & R FWD MEGAPHONE IAW ACR CMM 25-60-01, OPS CHECK GOOD AT THIS TIME.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 38,238 hrs · 18,341 cycles

CABIN HI ALT WARNINGS, INITIATED EMERGENCY DECENT TO 10,000 FT REQUESTED 7,000 FT, SAFETY VALVE, OPENED AC PRESS STABILIZED AT 7,000 MSL. TS IAW TSM 21-30-810-808-A, 21-31-00-810-809-A, AND 21-31-00-810-810-A. IAW ECS 19 REPORT AND MFG RECOMMENDATION LETTER 80079145/009, R & R CPC 1 & 2 L/I 35626-1. NO DEFECTS NOTED, CABIN PRESS CONTROL AND MONITORING OK FOR CONTINUED SERVICE IAW AMM 21-31-00-710-002-A.

Part: OXYGEN SYSTEM — MALFUNCTIONED (ROW 16DEF) · airframe 38,270 hrs · 18,335 cycles

ROW 16 DEF PSU FAILED TO OPEN, FORCED OPEN. R & R OXYGEN CONTAINER ASSY AT 16DEF IAW AMM 35-21-41. OP'S CHECKED OK.

Part: SAFETY VALVE — FAILED (CABIN PRESSURE) · airframe 38,270 hrs · 18,335 cycles

CABIN ALTTITUDE HIGH ADV INDICATION FOLLOWED BY EMERGENCY DESCENT, OXYGEN MASKS IN CABIN DEPLOYED. R & R BOTH SAFETY VALVES, REF LP 358607-2. R & R OUTFLOW VALVE LP 35608-2. PERFORMED OPS CHECK, REF LP 35607-1.

Part: MEGAPHONE — INOPERATIVE (FWD CABIN) · airframe 36,839 hrs · 17,645 cycles

FWD MEGA - PHONE INOPERATIVE. R & R FWD MEGAPHONE IAW ACFT DWGS NK 319-132. EQ REV 6. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,476 hrs · 17,473 cycles

DURING WEEKLY CHECK STEP 19. OPERATIONAL CHECK OF THE CABIN EMERGENCY LIGHTS. FAULT EPSU (12WL) EMERGENCY R SHOWED UP. R & R EPSU, 12WL, BATTERY PACK IAW AMM 33-51-38. TEST CHECKS OK. NO FURTHER FAULTS AT THIS TIME.

Part: LIGHT — INOPERATIVE (MEGAPHONE) · airframe 33,096 hrs · 15,887 cycles

MEGAPHONE GREEN "ON LIGHT" INOPERATIVE. R & R AFT MEGAPHONE IAW AMM. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 32,453 hrs · 15,634 cycles

CORROSION ON CABIN FLOOR SUPPORT, LBL 52 AFT OF C66 BEAM, AT SPLICE. DOCUMENTED ON NRI 7335N00365. R & R FLOOR SUPPORT, REF NRI 7335N00365.

Part: RIB — CORRODED (LT WING) · airframe 32,453 hrs · 15,634 cycles

PERFORM PHASED ARRAY INSPECTION OF LT WING, FOUND EVIDENCE OF CORROSION AT RIBS 17-18. ALL CORROSION WAS REMOVED BY BLENDING WITH MINIMUM DEPTH REPORTED AS 3.90 MM AT L1 AND 3.62 MM AT L2, NORMAL THICKNESS IS 5.0MM. ALL REPAIR PLATES WERE MANUFACTURED AND INSTALLED WITH OVERSIZE FASTENER. REINSPECT.

Part: DOOR SEAL — LEAKING (EMERGENCY EXIT) · airframe 32,458 hrs · 15,633 cycles

LEFT SIDE OVERWING EXIT DOOR SEAL HAS SEVERE LEAK. REMOVED LT EMERGENCY EXIT HATCH. CLEANED AND INSPECTED SEAL. NO DEFECTS NOTED. RE-INSTALLED EXIT HATCH. OPS CHECK GOOD. NO LEAKS NOTED. ALL WORK PERFORMED IAW AMM 52-21-11, PB 401.

Part: RIB — CORRODED (LT WING) · airframe 32,453 hrs · 15,634 cycles

DURING MAINTENANCE VISIT, PERFORM PHASED ARRAY INSPECTION OF LT WING, FOUND EVIDENCE OF CORROSION AT RIBS 11-12. ALL CORROSION WAS REMOVED BY BLENDING WITH MINIMUM DEPTH REPORTED AS 2.87 MM AT L1, NORMAL THICKNESS IS 5.00 MM. ALL REPAIR PLATES WAS MANUFACTURED AND INSTALLED WITH OVERSIZE FASTENER. SRI REQUIRE REINSPECT AT 20000, FC/3580, FH WITH SUBSEQUENT INSPECTIONS AT 9000FC AND 12000 AFTER FIRST INSPECTION IAW A319 57-21-11-1-007-00.

Part: RIB — CORRODED (RT WING) · airframe 32,453 hrs · 15,634 cycles

DURING MAINTENANCE VISIT, PERFORM PHASED ARRAY INSPECTION OF RT WING, FOUND EVIDENCE OF CORROSION AT RIBS 9-11. ALL CORROSION WAS REMOVED BY BLENDING WITH MINIMUM DEPTH REPORTED AS 2.87 MM AT L1, NORMAL THICKNESS IS 5.00 MM. ALL REPAIR PLATES WERE MANUFACTURED AND INSTALLED WITH OVERSIZE FASTENERS. REINSPECT AT 27700.

Part: RIB — CORRODED (LT WING) · airframe 32,453 hrs · 15,634 cycles

PERFORM PHASED ARRAY INSPECTION OF LT WING FOUND EVIDENCE OF CORROSION AT RIBS 10-11. ALL CORROSION WAS REMOVED BY BLENDING WITH MINIMUM DEPTH REPORTED AS 3.90 MM AT L1 AND 3.62MMM AT L2, NORMAL THICKNESS IS 5.0MM, ALL REPAIR PLATES WAS MANUFACTURED AND INSTALLED WITH OVERSIZE FASTENER. REINSPECT.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 32,453 hrs · 15,634 cycles

DURING MAINTENANCE VISIT, CORROSION ON CABIN FLOOR SUPPORT, LBL 52 FWD OF C66 BEAM AT SPLICE. R & R FLOOR SUPPORT IAW NRI 7335N00327.

Part: DOOR SEAL — DIRTY (EMERGENCY EXIT) · airframe 32,385 hrs · 15,601 cycles

LOUD NOISE AT ACFT LEFT EMERGENCY EXIT. OVERWING EXIT. REMOVED LEFT OVERWING EXIT AND CLEANED SEAL. INSTALLED OVERWING EXIT IAW AMM.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 32,269 hrs · 15,555 cycles

OXYGEN MASK FELL DOWN FROM R1 DOOR. REPACKED OXYGEN MASK IAW AMM. PERFORMED DROP TEST IAW AMM. OPS CHECKED GOOD.

Part: EPSU — NO TEST (EMERGENCY LIGHT) · airframe 30,821 hrs · 14,900 cycles

FAILED BATTERY EPSU EMERGENCY LIGHT TEST. R & R EPSU, BATTERY IAW AMM. OPS CHECKED OK.

Part: SKIN — DAMAGED (LT AILERON)

EVIDENCE OF LIGHTNING STRIKE DAMAGE ON LT AILERON. PERFORMED LIGHTNING STRIKE INSPECTION IAW W/C. INSPECTED FUSELAGE, WINGS, RUDDER, ELEVATORS. FOUND 2 BURN MARKS ON LT AILERON PREPPED AND PAINT 2 MARKS LT AILERON IAW ACFT MM. COMPLETED LIGHTNING STIKE INSPECTION. NO OTHER DAMAGES NOTED AT THIS TIME.

Part: COVER — DAMAGED (L2 DOOR) · airframe 28,612 hrs · 13,854 cycles

L2 DOOR HANDLE HAS PIECE MISSING. INSTALLED L2 DOOR HANDLE COVER IAW ACFT MM.

Part: SLIDE — DEFECTIVE (ZONE 800) · airframe 28,557 hrs · 13,824 cycles

RT WING EMERGENCY EXIT AMBER HANDLE PULLED, SLIDE DID NOT DEPLOY. PERFORMED TEST OF DOOR WARNING SYS. INSTALLED HANDLE TO CLOSED POSITION & COVER INSTALLED IAW MM. NO FAULTS DETECTED ECAM NORMAL.

Part: SKIN — CORRODED (RT WING) · airframe 26,766 hrs · 12,946 cycles

RT WING LOWER SURFACE BETWEEN RIBS 25-&26 HAS CORROSION DAMAGE. PERFORMED PERMANENT BLEND OUT REPAIR OF CORROSION DAMAGE IAW EA 57-20-1219 REV ORIGINAL DATE 9-26-2012.

Part: STRUCTURE — CORRODED (RUDDER) · corrosion level 2 · airframe 26,766 hrs · 12,946 cycles

RUDDER LT AND RT SIDE WITH CORROSION AT THE TIP AREA. DAMAGED AREA WAS REPAIRED IAW MESSAGE 70567398/006.

Part: SKIN — CORRODED (RT WING) · airframe 26,766 hrs · 12,946 cycles

RIGHT WING LOWER SURFACE T/E AREA, STRAP WITH LIGHT CORROSION AT SEVERAL PLACES. DAMAGED AREAS WERE REPAIRED IAW MESSAGE 70567430/007 DTD SEP 23,2012 AND TD-J1-S2-21150-2012 ISSUE A, UNDER THE NON ROUTINE ITEM WO: A1A232, SUBJOB: 6, ITEM: 19.

Part: RUDDER — CONTAMINATED (ZONE 300) · airframe 26,766 hrs · 12,946 cycles

VERTICAL STABILIZER RUDDER HOISTING POINTS 1LT, 2LT, 3LT AND 3RT WITH TRAPPED FLUID. DAMAGED AREAS WERE REPAIRED IAW MESSAGE 70567288/006 DTD SEP 19, 2012 AND TD-K4-S2-39630-2012, ISSUE A, UNDER THE NON ROUTINE ITEM, WO: A1A232, SUBJOB: 3, ITEM: 1.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 26,637 hrs · 12,874 cycles

EPSU (13WL) AFT LT FAILED. R & R EPSU BATTERY (13WL) IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002. OPS CHECKED OK.

Part: LANDING GEAR — INTERMITTENT (ZONE 700) · airframe 20,665 hrs · 9,911 cycles

ON APPROACH, DID NOT GET 3 GREEN FOR LANDING GEAR. FLIGHT EXECUTED GO-AROUND. RE-CYCLED GEAR AND ALL OK - 3 GREEN. FLIGHT LANDED SAFELY AT 1901 LOCAL.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,454 hrs · 9,820 cycles

UPPER FUSELAGE PAX CABIN, FLOORBEAM UPPER CHORD WITH CORROSION FROM STA X39510 TO STA X400030, +Y116. DAMAGE PART IS GOING TO BE REPLACED IAW SRM 51-72-11, PARA 4 AND 6.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,454 hrs · 9,820 cycles

UPPER FUSELAGE PAX CABIN, FLOORBEAM UPPER CHORD WITH CORROSION FROM STA X39019 TO STA X39510, -Y76. DAMAGED PART IS GOING TO BE REPLACED IAW SRM 51-72-11, PARA 4 AND 6.

Part: SKIN — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 20,454 hrs · 9,820 cycles

NR 2 ENGINE PYLON, PYLON AFT FIXED FAIRING LATERAL PANEL INBD AND OTBD SKIN WITH CORROSION. REPLACED NR 2 ENGINE PYLON AFT FAIRING SECTION INBD AND OTBD SKIN PANEL FROM PYLON STA 829 TO PYLON STA 1005, IAW SRM 51-72-11 PARA 4 AND 6.

Part: ANCHOR FITTING — CORRODED (LT WING) · airframe 20,454 hrs · 9,820 cycles

LEFT OUTER WING REAR SPAR AFT FACE RETRACTION JACK ANCHORAGE FITTING CORRODED AROUND THE BORE UPPER AND LOWER AND IN THE BORE INNER SURFACE. DAMAGED PART IS GOING TO BE REPAIRED FOLLOWING REPAIR INSTRUCTIONS.

Part: SKIN — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 20,454 hrs · 9,820 cycles

NR 1 ENGINE PYLON, PYLON AFT FIXED FAIRING LATERAL PANEL INBD AND OTBD SKIN WITH CORROSION. REPLACED NR 1 ENGINE PYLON AFT FAIRING SECTION INBD AND OTBD SKIN PANEL STA829 TO STA1005, IAW SRM 51-72-11 PARA 4 AND 6.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,454 hrs · 9,820 cycles

UPPER FUSELAGE PAX CABIN, SEAT TRACK WITH CORROSION FROM STA X38600 TO STA X39400, +Y1292. DAMAGED PART IS GOING TO BE REPLACED IAW SRM 51-72-11, PARA 4 AND 6.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,454 hrs · 9,820 cycles

UPPER FUSELAGE PAX CABIN, FLOORBEAM UPPER CHORD WITH CORROSION FROM STA X39019 TO STA 39510, +Y116. DAMAGED PART IS GOING TO BE REPLACED IAW SRM 51-72-11, PARA 3 AND 4.

Part: ANCHOR FITTING — CORRODED (RT WING) · airframe 20,454 hrs · 9,820 cycles

RT OUTER WING REAR SPAR AFT FACE, JACK ANCHORAGE FITTING CORRODED, AROUND THE BORE UPPER AND LOWER SURFACE AND IN THE BORE INNER SURFACE. DAMAGED PART IS GOING TO BE REPAIRED FOLLOWING REPAIR INSTRUCTIONS.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,454 hrs · 9,820 cycles

UPPER FUSELAGE PAX CABIN, FLOORBEAM UPPER CHORD WITH CORROSION FROM STA X39019 TO STA 39510, -Y116. DAMAGED PART IS GOING TO BE REPLACED IAW SRM 51-72-11, PARA 4 AND 6.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,970 hrs · 7,217 cycles

FLOORBEAM CORRODED AT FR69 AT Y254. REMOVED AND REPLACED FLOORBEAM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,970 hrs · 7,217 cycles

FLOORBEAM SEAT TRACK CORRODED -Y765 AT FR66. REMOVED AND REPLACED FLOORBEAM SEAT TRACK -Y765 AT FR66.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,970 hrs · 7,217 cycles

RIGHT HAND CORNER WEB CORRODED -Y1292 AT FR70. REMOVED AND REPLACED CORNER WEB.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,970 hrs · 7,217 cycles

SEAT TRACK CORRODED AT Y765-FR66. REMOVED AND REPLACED SEAT TRACK.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 9,091 hrs · 4,398 cycles

EMERGENCY LIGHT ON DOOR 2R IS INOP. REATTACHED LOOSE CONNECTION, OPS CHK GOOD IAW AMM33-51-16.

Part: PIPE — CRACKED (FIRE EXTING) · airframe 9,091 hrs · 4,398 cycles

ENGINE FIRE EXTINGUISHING PIPE OVER THE HOT SECTION (NR 2 ENG) IS CRACKED. REMOVED AND REPLACED PIPE AFT SECTION IAW A319 AMM 26-21-49.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,091 hrs · 4,398 cycles

FOUND CORROSION ON FLOOR SUPPORT -Y765 BETWEEN STA FR 67 AND FR 70. REMOVED AND REPLACED FLOOR SUPPORT IAW A319 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,091 hrs · 4,398 cycles

FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN ST FR76 7 FR70. REMOVED AND REPLACED FLOOR SUPPORT IAW A319 SRM 51-72-11.

Part: CONTROL UNIT — MALFUNCTIONED (MLG)

FLT 516 - AFTER STARTING 2ND ENGINE RECEIVED ECAM `ALTN BRAKING` INOPERATIVE, RETURNED TO THE GATE, AIRCRAFT TAIL SWAP WITH N822NK. REMOVED AND REPLACED ABCU. ALL SYSTEMS OPS CHECK GOOD. (M)