N516NK

Part: NONE — NONE · airframe 55,889 hrs · 25,862 cycles

FUME EVENT DESCENDING THROUGH 10000 SMELL RESEMBLED A CHEMICAL SMELL, TURNED 1 PACK OFF SMEL DISSIPATED ( PACKS A319 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - AT OR BELOW FL 370 )-REACTIVATED PACK 1 IAW AMM 21-51-00. PERFORMED OPERATIONAL TEST OF PACK 1 IAW AMM 21-52-00. NO ODOR DETECTED. PACK 1 OK FOR CONTINUED SERVICE. THIS CLOSES DMI # 2921953-1. DMI LOG UPDATED, PLACARD REMOVED, MOC NOTIFIED.

Part: NONE — NONE · airframe 55,397 hrs · 25,635 cycles

FOUND FWD F/A STA. MEGAPHONE VOLUME CONTROL KNOB MISSING.-REMOVED AND REPLACED FWD F/A STA. MEGAPHONE IAW CMM 25-60-01 AND SPIRIT AIRLINES DRAWING A319 EMER. EQUIPMENT LAYOUT. OPS CHECK GOOD IAW AMM 25-65-51-710-002-A.

Part: UNKNOWN — ODOR · airframe 52,666 hrs · 24,467 cycles

FUME EVENT ON DESCENT PASSING FL230. CHECK LIST COMPLETE, SMELL WAS GONE-PERFORMED DECCONTAMINATION OF ECS IAW AMM 21-00-00. OPS CHECK GOOD. NO DEFECT NOTED AT THIS TIME.

Part: FILTER — ODOR (AC BAY) · airframe 52,391 hrs · 24,354 cycles

DIRTY SOCK FOUL ODOR SMELL ON APPROACH. PACK 1 SUSPECTED. SMELL PERSISTED THROUGHOUT CABIN. -PER TSM 05-50-00-810-831-A PERFORMED DECONTAMINATION OF PACK 1 SYSTEM. R&R RECIRCULATION FILTERS AND GARLOCK SEAL ON ENG #1 IAW AMM 21-00-00-615-002. FOUND NO SIGNS OF ODOR AT THIS TIME A/C OK FOR CONTINUED SERVICE

Part: UNKNOWN — ODOR (CABIN) · airframe 51,678 hrs · 24,073 cycles

"STRONG ODOR IN A/C CABIN-PERFORMED TSM 05-51-00-810-831-A INSP APU CMPARTMENT NO DEFECTS NOTE ODOR DISSAPATTED WHILE PERFORMING INS NO ODOR PRESENT A/C OK FOR SVC"

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 51,628 hrs · 24,052 cycles

DURING WEEKLY CHECK FOUND FWD MEGAPHONE NOT TESTING -R&R FWD MEGAPHONE OPS CHECK OK IAW AMM 25-65-00.

Part: CONDENSER — ODOR (NR 2 A/C PACK) · airframe 51,310 hrs · 23,908 cycles

CABIN FUMES-REPLACED #2 PACK CONDENSER PER AMM 21-52-32. OPS NORMAL. REPLACED BOTH RECIRC.FILTERS PER AMM 21-21-41. PERFORMED PACK BURN OUT ON #2 PACK PER 21-00-00 WITH ENG. NO ODOR AT THIS TIME. FOR OTHER CORRECTIVE ACTIONS SEE L/P 2504258-2, 2504259-1 AND -2.

Part: UNKNOWN — ODOR (CABIN) · airframe 49,609 hrs · 23,081 cycles

FLIGHT ATTENDANTS DESCRIBED AN ODOR THAT BUILT IN INTENSITY DURING DESCENT FROM 10000 TO 3000'. STARTED AS A BURNING SMELL GRADUATING TO A SWEET / BLEACH ODOR. ORIGINATED NEAR L2 DOOR AND SPREAD FWD TO ROW 26.-PERFORMED TSM 05-50-00-810-831-A FOR CAUSE OF CABIN ODOR, EXTERIOR AC INSPECTION SHOWED NO SIGNS OF OIL LEAKAGE AT ENGS OR APU. AC PACK INLETS CLEARED. PACK OPS WITH APU , ENG1, ENG 2 BLEED, NO ODOR NOTICED. AIRCRAFT OK FOR CONTINUED SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 48,836 hrs · 22,768 cycles

STRONG ODOR IN COCKPIT, MAKES EYES AND THROAT BURN-PERFORMED PACK 1 & 2 BURN OUT IAW AMM: 21-00-00. OPS CHECK GOOD. NO LEAKS FOUND. NO STRONG ODOR.

Part: ECS — CONTAMINATED (AC BAY) · airframe 46,296 hrs · 21,711 cycles

FUME EVENT ON LANDING / TAXI IN, CHEMICAL / GLYCOL LIKE ODOR. PERFORMED DECONTAMINATION OF ENVIRONMENTAL CONTROL SYSTEM (ECS) IAW AMM 21-00-00-615-002-A. NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,277 hrs · 21,704 cycles

FLIGHT ATTENDANT REPORTED OIL / CHEMICAL SMELL IN AFT GALLEY-PER TSM05-50-00-810-831-A. PREFORMED ENG RUNS WITH FLIGHT CREW NO ODOR DETECTED ON PACK 1 OR 2 WITH ENG'S 1 & 2 RUNNING. NO HISTORY OF ODOR A/C OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,574 hrs · 21,406 cycles

STRONG ELECTRICAL ODOR IN THE COCKPIT AND FWD CABIN. CONTINUED LG PG 2371999-01, ACCOMPLISHED TSM 24-00-00-810-823-A, PFM WAS CLEAN. NO BURNING ODOR NOTED IN THE E&E BAYS IAW AMM 52-41-00. ACCOMPLISHED AVEC TEST IAW AMM 21-26-00, TESTED OK. PERFORM TEMP CONTROL TEST AMM 21-61-00, TESTED OK. PERFORM CIDS POWER UP TEST IAW AMM 23-73-00, SIDEWALL LIGHTS INOPERATIVE AT 22 LT, 15 RT & 16 LT, R & R THE SIDEWALL LIGHTS IAW AMM 33-21-11, OPS CHECKED GOOD. ACCOMPLISHED AN ENGINE RUN FOR NR 1 & 2 IAW 71-00-00, TESTED OK, NO ODOR NOTED THROUGH OUT CABIN & FLIGHT DECK. ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (FRAMES 40-41) · airframe 44,909 hrs · 21,110 cycles

SKIN PANEL CRACKED, FRAME 40, AND 41, STRINGER 20R. REPAIRED IAW EO 5331-1811.

Part: DOOR SILL — CORRODED (FRAME 16) · airframe 44,909 hrs · 21,110 cycles

FWD DOOR SILL CORRODED, FRAME 16,20, STRINGER 23R. REWORKED AND EVALUATED THE CORROSION. FOUND OUT OF LIMITS IAW EO 5311-1813 AND ACCOMPLISHED.REPAIR.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,733 hrs · 21,043 cycles

DURING CRUISE DIRTY SOCKS SMELL REPORTED ON ROW 8. COM SUPPLEMENTAL PROCEDURE SMELL WENT AWAY NO SMELL FELT IN THE COCKPIT. PERFORMED GVI OF A/C ENGINE 1 AND 2 AND PACKS INLETS 1 AND 2 NO CONTAMINATION NOTED OR OIL LEAKS IAW TSM 05-50-00. PERFORMED ENGINE RUN TO ISOLATE ODOR. ENGINE 1 AND 2 BLEED WITH PACK 1 NO ODOR NOTED PER FLIGHT CREW REPORT PACK 2 WILL BE PLACED ON DEFERRAL SEE ITEM 2.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 44,679 hrs · 21,026 cycles

DURING DESCENT THROUGH 6000FT. THE COCKPIT HAD A DIRTY SOCK ODOR. PERFORMED CSAS DECONTAMINATION OF THE NR 1 & 2 PACKS IAW AMM 21-00-000, AND TSM 05-50-60. FOUND NO ODOR OR SIGNS OF FUMES. ACFT OK TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,395 hrs · 20,909 cycles

DURING DESCENT THRU 5000FT ON APPROACH. THE APU WAS OFF DURING EVENT SYMPTOMS FELT IN THE COCKPIT AND CABIN. RAM AIR INLET WAS OPENED BY THE CAPTAIN. . THE ODOR WAS STRONG. PERFORMED COCKPIT AND CABIN ODOR ISOLATION IAW TSM 05-50-00-810-831-A. RAN THE NR 1 & 2 PACKS INDIVIDUALLY USING APU, NR 1 & 2 ENGINES FOR 15 MINUTES EACH. NO ODOR NOTED. ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (APU) · airframe 44,381 hrs · 20,901 cycles

ODOR THROUGHOUT ENTIRE PLANE, ON SELECTING APU BLEED ON. ACCOMPLISHED DECONTAMINATION & PACK BURNOUT OF BOTH PACKS USING APU BLEED & ISOLATION OF ENGINE AS BLEED SOURCE. NO ODORS NOTED IAW TSM 21-00-00. CHECKED FOR EXTERNAL APU OIL LEAKAGE IAW AMM 49-11-11. NO LEAKS FOUND.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,379 hrs · 20,899 cycles

FLT ATTENDANTS SMELLED FUMES DURING TAKEOFF AND INITIAL DESCENT. PERFORMED A CABIN ODOR ISOLATION IAW TSM 05-50-00. NO ORDER NOTED ACFT OK FOR SERVICE.

Part: ELEMENT — OVERHEATED (WINDOW HEAT) · airframe 44,215 hrs · 20,837 cycles

ODOR JUST BEFORE DESCENT. BURNED FINGERS PUTTING SHADE DOWN ON CAPTAIN'S SIDE WINDOW. SMALL CRACKS NEAR HEATING ELEMENT. ODOR OF BRUNING OR HOT ELECTRICAL. CAPTAIN'S SLIDING WINDOW OVERHEATING AND CAUSING ODOR. PERFORMED INSPECTION OF THE CAPTAIN`S SLIDING WINDOW IAW AMM 56-12-11 & FOUND FOUR SMALL CRACKS, LESS THAN 0.5' EACH AROUND THE HEATING ELEMENT.

Part: UNKNOWN — ODOR (CABIN) · airframe 42,780 hrs · 20,223 cycles

ENROUTE, CHEMICAL ODOR MID CABIN. TURNED OFF THE NR 2 PACK, NO CHANGE REPORTED. DIVERTED. PERFORMED GVI OF ENGINES PACKS AND APU AREA NO DEFECTS NOTED. NO DEFECTS OR ODORS

Part: RAIL — GOUGED (SLIDING WINDOW) · airframe 41,373 hrs · 19,595 cycles

RIGHT SLIDING WINDOW LOWER RAIL HAS MULTIPLE GOUGES. C/W EO 5311-1719, BLEND OUT ON THE SPOTS.

Part: HINGE FITTING — DAMAGED (RUDDER) · airframe 41,373 hrs · 19,595 cycles

RUDDER HINGE NR 7, FOUND WITH ELONGATED HOLES. OVERSIZED THE HOLE IAW EO 5536-1704

Part: SKIN — DENTED (FRAME 58) · airframe 41,373 hrs · 19,595 cycles

SKIN DENTED FRAME 58, STRINGERS 5 - 6L. PERFORMED A DOUBLER REPAIR IAW EO 5341-1718.

Part: RAIL — GOUGED (SLIDING WINDOW) · airframe 41,373 hrs · 19,595 cycles

LEFT SLIDING WINDOW LOWER RAIL HAS MULTIPLE GOUGES. C/W EO 5311-1721 BLENDED OUT ON THE SPOTS.

Part: UNKNOWN — ODOR (CABIN) · airframe 41,006 hrs · 19,429 cycles

ODOR IN COCKPIT AND CABIN ON CLIMBOUT FROM 4000 TO 15000 FT. RETURNED ON APPROACH AND TAXI IN. PERFORMED TROUBLESHOOTING OF ODOR IAW TSM 05-50-00-810-831-A . NO ODOR NOTED. R & R THE RECIRCULATION FILTERS IAW AMM 21-21-41-PB 401. A/C OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 40,963 hrs · 19,409 cycles

CABIN REPORTED FUMES ON SHORT FINAL SMELLING LIKE RUBBER CEMENT & AMMONIA. SMELL DISSIPATED AFTER SHUTTING OFF PACKS. TROUBLESHOT PER TSM 05-90-00 NO DEFECTS NOTED. ALSO 4 MECHANICS WERE ONBOARD A/C DURING FLIGHT AND NOTED NO SMELL PRESENT DURING FLIGHT SEATS 4A,4B, 11A, 11F

Part: UNKNOWN — ODOR (CABIN) · airframe 40,755 hrs · 19,312 cycles

DURING DESCENT, AFT FA REPORTED AN ODOR DURING DESCENT. DURING TAXI THE ODOR CHANGED TO A WET DOG ODOR AND INCREASED. SECURED THE NR 2 ENGINE AND NR 2 PACK AND THE ODOR DIMINISHED. PERFORMED ECS DECONTAMINATION. NO DEFECTS NOTED IAW AMM 21-00-00 -615-002 004.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 40,588 hrs · 19,236 cycles

CAPTAIN`S OXYGEN MASK INOPERATIVE. R & R THE OXYGEN MASK IAW AMM 35-12-41. OPS CHECKED OK.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 24 DEF) · airframe 38,160 hrs · 18,117 cycles

ROW 24 DEF, O2 MASK FELL DOWN, PASSENGER OXYGEN STORAGE PASSENGER OXYGEN MODULES. PERFORMED OPERATION CHECK OF MANUAL MASK CHECK AND RELEASE, DROP TEST, IAW AMM 35-23-00-710-001-A, OPS TEST GOOD.

Part: MEGAPHONE — NO TEST (CABIN) · airframe 37,470 hrs · 17,805 cycles

FWD MEGAPHONE WILL NOT TEST. R & R FWD MEGAPHONE IAW SPIRIT EMERGENCY EQUIPMENT DWG NK320-232-EQ.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 37,288 hrs · 17,731 cycles

CAPTAIN`S O2 MASK HEAD STRAP DOES NOT LEAK, SWAPPED CAPT AND 2ND OBS O2 MASK. CAPTAIN`S CXS NORMAL REF AMM 35-12-41. R & R SECOND OBSERVER SEAT 02 MASK IAW AMM 35-12-41-00-002-A/400-002-A, OPS AND LEAK CHECK GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (GALLEY) · airframe 34,354 hrs · 16,416 cycles

OXYGEN MASKS JUMP SEAT FWD GALLEY DEPLOYED. STOWED O2 DOOR IAW AMM 35-23-00 MASKS DID NOT DEPLOY.

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 33,884 hrs · 16,206 cycles

F/O O2 MASK WEBBING RUPTURED LT SIDE. R & R MASK IAW AMM 35-12-41-000-002-A AND 35-12-41-400-002-A. OPS CKS GOOD.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 33,596 hrs · 16,083 cycles

CAPT O2 MASK INOP. R & R CAPT'S FULL-FACE/ QUICK DONNING O2 MASK, REF AMM 25-12-41; OP - TEST OK.

Part: OXYGEN MASK — FAILED (COCKPIT) · airframe 33,573 hrs · 16,074 cycles

CAPT O2 MASK CONNECTION FAILED IN FLIGHT. RE CONNECTED FLEXIBLE HOSE TO CAPT O2 MASK IAW AMM 35112-41-400-002-A. OPS CHECK GOOD IAW AMM 35-12-41-710-001.

Part: DOOR — LEAKING (L2) · airframe 30,461 hrs · 14,642 cycles

L2 DOOR MADE LOUD NOISE AFTER 10,000 FT. REMOVED TORN STRIP, INSTALLED NEW STRIP IAW AMM 52-13-18. PRESSURIZED ACFT ON GROUND, NO LEAKS NOTED IAW AMM 21-31-00.

Part: HARNESS — BROKEN (OXYGEN MASK) · airframe 28,768 hrs · 13,929 cycles

CAPTAIN`S OXYGEN MASK HEAD HARNESS RETENTION TUBE IS BROKEN. R & R OXYGEN MASK IAW AMM. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,635 hrs · 13,871 cycles

RIGHT EXIT ROW EPSU BATTERY INOPERATIVE. R & R RT EXIT ROW EPSU BATTERY IAW AMM.

Part: DOOR SEAL — DAMAGED (RT OVERWING) · airframe 28,635 hrs · 13,871 cycles

RIGHT OVERWING EXIT DOOR HAS SQUEAL WHEN ACFT PRESSURIZED. R & R HATCH SEAL IAW AMM. ALSO, PERFORMED PRESSURIZATION CHECK. NO LEAKS NOTED. ACFT OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,635 hrs · 13,871 cycles

LEFT EMERGENCY EXIT ROW EPSU BATTERY INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: ENGINE — FIRE (NR 1) · airframe 28,634 hrs · 13,870 cycles

AIR RETURN DUE TO NR 1 ENGINE FIRE. ENGINE SHUTDOWN IN FLIGHT, SMOKE IN COCKPIT. NR 1 ENGINE CHANGED IAW AMM.

Part: CABLE — DAMAGED (DOOR SLIDE) · airframe 28,631 hrs · 13,868 cycles

FWD RT DOOR ESCAPE SLIDE ARM/DISARM FLEXIBLE CABLE HAS BURST/TORN SHEATH. R & R RT DOOR ESCAPE SLIDE CABLE IAW AMM 52-11-22 AND OPS CHECK GOOD IAW AMM 25-62-44.

Part: CABLE — DAMAGED (DOOR SLIDE) · airframe 28,631 hrs · 13,868 cycles

FWD LT DOOR ESCAPE SLIDE ARM/DISARM FLEXIBLE CABLE HAS BURST/TORN SHEATH. R & R FWD LT DOOR ESCAPE SLIDE CABLE IAW AMM 52-11-22. OPS CHECK GOOD IAW AMM 25-62-44, WORK CLEARED ON NON-ROUTINE 7240N00505.

Part: CABLE — DAMAGED (DOOR SLIDE) · airframe 28,631 hrs · 13,868 cycles

AFT RT DOOR ARM, DISARM FLEXIBLE CABLE HAS BURST. R & R AFT RT DOOR ARM, DISARM CABLE IAW AMM 52-13-22. OPS CHECK GOOD IAW AMM 25-62-44. CLEARED ON NON-ROUTINE 7240N00498.

Part: SKIN — CORRODED (RT WING) · airframe 28,631 hrs · 13,868 cycles

NDT/PHASED ARRAY INSPECTION, IDENTIFIED CORROSION ON RT WING TOP SKIN BEHIND REAR SPAR AT RIB-9, FWD R2 SPOILER.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 28,501 hrs · 13,805 cycles

L1 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED BOTTLE IAW AMM 52-10-00-614-001.

Part: ACCUMULATOR — LOW PRESSURE (L1 DOOR) · airframe 28,352 hrs · 13,728 cycles

L1 DOOR EMERGENCY ACCUMULATOR PRESSURE LOW, SERVICED L1 DOOR EMERGENCY ACCUMULATOR AS REQ IAW AMM. NO FURTHER DEFECTS NOTED.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 28,233 hrs · 13,672 cycles

L1 DOOR EMERGENCY ACCUMULATOR REQUIRES SERVICE. SERVICED DOOR ACCUMULATOR AS REQ IAW AMM. NO FURTHER DEFECTS NOTED.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 27,291 hrs · 13,205 cycles

L1 DOOR ASSIST ACCUMULATOR HAS LOW N2 PRESSURE. SERVICED L1 DOOR ASSIST ACCUMULATOR IAW MM.

Part: DAMPENER — LOW PRESSURE (L1 DOOR ASSIST) · airframe 27,277 hrs · 13,198 cycles

L-1 DOOR ASSIST BOTTLE HAS LOW PRESSURE. SERVICED IAW ACFT MM.

Part: CONTAINER — BROKEN (LIFE VEST) · airframe 27,241 hrs · 13,183 cycles

5D LIFEVEST POCKET BROKEN. ACCOMPLISHED MX PROCEDURES IAW ACFT MM.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 27,191 hrs · 13,163 cycles

L1 DOOR ASSIST BOTTLE HAS LOW PRESSURE. SERVICED L1 DOOR ASSIST TO PROPER PRESSURE IAW ACFT MM. LEAK CHECKED GOOD.

Part: ACCUMULATOR — LOW PRESSURE (L1 DOOR) · airframe 26,748 hrs · 12,963 cycles

L1 DOOR ASSIST ACCUMULATOR PRESSURE LOW. SERVICED L1 DOOR ASSIST ACCUMULATOR TO CORRECT PRESSURE IAW MM.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 26,097 hrs · 12,641 cycles

L1 DOOR ACTUATOR PRESSURE LOW. SERVICED L1 DOOR ACTUATOR WITH NITROGEN IAW AMM.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 26,001 hrs · 12,591 cycles

L1 DOOR ASSIST BOTTLE HAS PRESSURE LOW. SERVICED L1 DOOR ASSIST BOTTLE ACCUMULATOR IAW MM.

Part: BOTTLE — LOW PRESSURE (PAX DOOR ASSIST) · airframe 25,872 hrs · 12,528 cycles

PAX DOOR L1 ASSIST BOTTLE LOW PRESSURE. SERVICED L1 DOOR ACCUMULATOR ASSIST BOTTLE TO PROPER LEVEL IAW AMM.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 25,579 hrs · 12,391 cycles

L1 DOOR LOW AIR PRESSURE. SERVICED L1 DOOR TO PROPER AIR PRESSURE IAW ACFT MM.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 25,051 hrs · 12,120 cycles

L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED L1 DOOR PAMBER/EMERGENCY OPERATION CYLINDER IAW AMM 52-10-00-614-051-A. NO LEAKS NOTED.

Part: BOTTLE — LOW (L2 DOOR ASSIST) · airframe 24,334 hrs · 11,753 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 23,820 hrs · 11,498 cycles

EMERGENCY EXIT LIGHT FWD OF THE OVERWING EMERGENCY EXIT ON ADFT RT IS MISSING ITS COVER. REATTACHED LENS IAW AMM 33-51-15-400-001-A. OPS CK GOOD.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 23,807 hrs · 11,491 cycles

L1 DOOR ASSIST BOTTLE LOW. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001-A.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 23,488 hrs · 11,321 cycles

L1 DOOR ASSIST B0TTLE PRESSURE LOW. C/A: SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00 PB. 301. LEAK CK OK.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 23,079 hrs · 11,121 cycles

EMERGENCY LIGHTS BATTERY FAILED CAP TEST. R & R 10WL BATTERY AMM 33-51-38-000-001-A +33-51-38-400-001-A, OPS TESTED OK.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 22,593 hrs · 10,880 cycles

L1 DOOR PASSENGER DOOR, ASSIST ACTUATOR PRESSURE INDICATOR LESS THAN 1100 PSI ON DIAL GAUGE. SERVICED L1 DOOR PASSENGER DOOR ASSIST WITH NITROGEN IAW AMM 52-10-00-614-001-A. NO LEAKS DETECTED.

Part: ACCUMULATOR — LOW PRESSURE (L1 DOOR) · airframe 22,452 hrs · 10,810 cycles

L1 DOOR ACCUMALATOR HAS LOW PRESSURE. SERVICED L1 DOOR ACCUMALATOR TO PROPER LEVEL IAW AMM 52-10-00-614-001.

Part: STRUCTURE — CONTAMINATED (VERTICAL STAB) · airframe 22,315 hrs · 10,749 cycles

DURING THE INSPECTION PROCESS, FOUND THE VERTICAL STABILIZER, RUBBER PANEL HOIST POINT NR 3 LT SIDE WITH TRAPPED FLUID. HOIST POINT REQUIRED A MINOR REPAIR IAW GUIDELINES.

Part: FITTING — CORRODED (ZONE 500) · airframe 22,315 hrs · 10,749 cycles

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

Part: FITTING — CORRODED (ZONE 600) · airframe 22,315 hrs · 10,749 cycles

RIGHT WING REAR SPAR AFT FACE RETRACTION JACK ANCHORAGE FITTING CORRODED AROUND T BORE AND LOWER SURFACE. DAMAGED PART GOING TO BE REPAIRED FOLLOWING REPAIR INSTRUCTIONS.

Part: SKIN — DENTED (ZONE 100) · airframe 22,315 hrs · 10,749 cycles

LOWER FUSELAGE BETWEN FR-60 AND FR-61 AND BETWEEN STR 39 AND STR41 SKIN WITH DENT AND REWORK. DAMAGED REPORT GOING TO BE REPAIRED FOLLOWING REPAIR INSTRUCTIONS.

Part: STRUCTURE — CONTAMINATED (VERTICAL STAB) · airframe 22,315 hrs · 10,749 cycles

DURING THE INSPECTION PROCESS, FOUND THE VERTICAL STABILIZER, RUBBER PANEL HOIST POINT NR 1 RT SIDE WITH TRAPPED FLUID. HOIST POINT REQUIRED A MINOR REPAIR IAW GUIDELINES.

Part: STRUCTURE — CONTAMINATED (VERTICAL STAB) · airframe 22,315 hrs · 10,749 cycles

DURING THE INSPECTION PROCESS, FOUND THE VERTICAL STABILIZER, RUBBER PANEL HOIST POINT NR 2 LT SIDE WITH TRAPPED FLUID. HOIST POINT REQUIRED A MINOR REPAIR IAW GUIDELINES.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 10,749 hrs · 22,315 cycles

LOWER FUSELAGE LEFT LATERAL AVIONIC COMPARTMENT AT C16 WASTE WATER VACUUM DUCT CLAMP SUPPORT CRACKED. DAMAGED PART WAS REPLACED IAW SRM 51-72-11, PAR 4 AND PAR 6 REQUIREMENTS. UNDER THE NON ROUTINE ITEM: WO A1A055, SUBJOB 1, ITEM 1.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 10,749 hrs · 22,315 cycles

AFT CARGO COMPARTMENT FR58, BETWEEN STGR 38LT AND STR 38RT PROFILE JOINT WITH CORROSION. DAMAGED PART WAS REPLACED IAW THE SRM REQUIREMENTS, UNDER THE NON ROUTINE ITEM: WO A1A055, SUBJOB 1, ITEM 68.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 10,749 hrs · 22,315 cycles

PAX CABIN BETWEEN FR69 TO FR70 +Y65 FLOOR SUPPORT WITH CORROSION. DAMAGED PART WAS REPLACED IAW SRM REQUIREMENTS UNDER THE NON ROUTINE ITEM: WORK ORDER A1A055, SUBJOB 2, ITEM 142.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 10,749 hrs · 22,315 cycles

AFT CARGO COMPARTMENT FR52 THRU FR55A STGR 38RT PROFILES WITH CORROSION. DAMAGED PART WAS REPLACED IAW SRM REQUIREMENTS, UNDER THE ROUTINE ITEM: WO A1A055, SUBJOB 1, ITEM 72.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 10,749 hrs · 22,315 cycles

AFT CARGO COMPARTMENT FR58 TO FR59 LT, STR 38L FLOOR SUPPORT WITH CORROSION. DAMAGED PART WAS REPLACED IAW SRM REQUIREMENT, UNDER THE NON ROUTINE ITEM: WO A1A055, SUBJOB 1, ITEM 67.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 10,749 hrs · 22,315 cycles

AFT CARGO COMPARTMENT FR56 THRU FR58, STGR 38LH PROFILES CORNER WITH CORROSION. DAMAGED PART WAS REPLACED IAW THE SRM REQUIREMENTS, UNDER THE NON ROUTINE ITEM: WORK ORDER A1A055, SUBJOB 1, ITEM 69.

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 10,749 hrs · 22,315 cycles

LOWER FUSELAGE ACCESS DOOR 191CB CUT OUT MOUNTING RING IS CRACKED. DAMAGED PART WAS REPLACED IAW SRM REQUIREMENTS, UNDER THE NON ROUTINE ITEM: WORK ORDER A1A055, SUBJOB 1, ITEM 89.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 10,749 hrs · 22,315 cycles

UPPER FUSELAGE PAX CABIN BETWEEN FR68 - FR70 FLOOR SUPPORT WITH CORROSION. DAMAGED PART WAS REPLACED IAW SRM REQUIREMENTS UNDER THE NON ROUTINE ITEM: WO A1A055, SUBJOB 2, ITEM 114.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 22,263 hrs · 10,724 cycles

L1 DOOR ASSIST BOTTLE REQUIRE SERVICING. SERVICED L-1 DOOR ASSIST BOTTLE TO PROPER PRESSURE IAW AMM 52-10-00-614-007.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 22,125 hrs · 10,669 cycles

L1 DOOR LOW PRESSURE. SERVICED L1 DOOR TO PROPER PRESSURE IAW AMM 52-10-00-614-001.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,981 hrs · 10,597 cycles

ACFT HAS DIVERTED DUE TO A SMOKE ECAM WARNING AND FLT ATTENDANT CONFIRMED FOUL ODOR. DECLARED EMERGENCY AND DIVERTED. PERFORMED TSM 26-15-00-810-804A. NO FAULTS FOUND. RAN APU WITH PACKS. NO ODORS DETECTED. RAN NR 1 & 2 ENG WITH PACKS. NO ODORS FOUND. SUSPECT AFT LAVATORY WATER HEATER. TRANSFERRED TO DMI - ITEM NR 2, CLEANED.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 21,795 hrs · 10,513 cycles

L1 DOOR ASSIST BOTTLE LOW PSI. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-050.

Part: ACCUMULATOR — LOW PRESSURE (PAX DOOR) · airframe 21,594 hrs · 10,411 cycles

FWD LT PASSENGER DOOR ACCUMULATOR LOW PRESS. SERVICED FWD LT PASSENGER DOOR ACCUMULATOR TO CORRECT PRESS IAW AMM-52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 21,268 hrs · 10,264 cycles

NR1 - L DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED NR 1-L DOOR ASSIST BOTTLE PRESSURE LOW.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 21,150 hrs · 10,202 cycles

L -1 DOOR ASSIST BOTTLE READS 1400 PSI. SERVICED L -1 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 21,068 hrs · 10,161 cycles

L1 DOOR EMERGENCY DAMPER LOW. SERVICED WITH NITROGEN AS REQUIRED IAW AMM 52-10-00-614-050. LEAK CHECKED OK.

Part: CYLINDER — LOW PRESSURE (L1 DOOR ASSIST) · airframe 20,677 hrs · 9,960 cycles

L1 DOOR BOTTLE LOW PRESS. SERVICED L-1 DOOR BOTTLE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L1 DOOR ASSIST) · airframe 20,461 hrs · 9,857 cycles

L1 DOOR BOTTLE LOW PRESSURE. SERVICED L1 DOOR BOTTLE, NO LEAKS NOTED REF TO AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 20,106 hrs · 9,682 cycles

DOOR L1 REQUIRES SERVICE FOR ASSIST BOTTLE. SERVICED DOOR ASSIST CYLINDER AT DOOR L1 IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 20,073 hrs · 9,669 cycles

L-1 DOOR BOTTLE PRESSURE LOW. SERVICED PAX DOOR ACCUMULATOR AS REQ IAW 52-10-00-614-001. NO FURTHER DEFECTS NOTED.

Part: ACCUMULATOR — LOW PRESSURE (L1 DOOR ASSIST) · airframe 19,812 hrs · 9,539 cycles

L1 DOOR ACCUMULATOR LOW. SERVICE L1 DOOR IAW AMM 52-10-00-614-001.

Part: GIRT BAR — STUCK (L1 DOOR) · airframe 17,835 hrs · 8,630 cycles

BIRT BAR STUCK IN DOWN POSITION. REMOVED DEBRIES FROM GIRT BAR.

Part: FLOOR SUPPORT — CORRODED (BS 2884) · airframe 17,224 hrs · 8,339 cycles

UPPER FUSELAGE PAX CABIN AFT SERVICE AREA STA 2884 BETWEEN +Y 130 AND -Y 130 FLOOR SUPPORT STRAP WITH CORROSION. REPLACED FLOOR SUPPORT STRAP ON STA 2884 BETWEEN +Y 130 AND -Y 130 IAW A319 SRM 51-72-11 PAR 4 AND 6.

Part: FLOOR SUPPORT — CORRODED (BS 2800-2870) · airframe 17,224 hrs · 8,339 cycles

UPPER FUSELAGE PAX CABIN AFT SERVICE AREA FROM STA 2800 TO STA 2870 +Y1292, LATERAL FLOOR SUPPORT WITH CORROSION. REPLACED FUSELAGE LATERAL FLOOR SUPPORT FROM STA 2800 TO STA 2870 BETWEEN +Y1162.5 AND +Y1292 DUE TO CORROSION IAW A319 SRM 51-72-11 PAR 4 AND 6. INSTALLED SCREWS, BOLTS AND NUTS IAW A319 SRM 51-42-11 PAR 5B AND 5C PAGE 1. INSTALLED HI-LOCK IAW A319 SRM 51-42-11 PAR 7B.

Part: PANEL — CORRODED (NR 2 PYLON) · airframe 17,224 hrs · 8,339 cycles

ENGINE NR2, PYLON LT LATERAL PANEL, BETWEEN STA 829 AND STA 928, SKIN PANEL WITH EROSION (PANEL PN: D54530052203). THE EROSION REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 2884) · airframe 17,224 hrs · 8,339 cycles

UPPER FUSELAGE PAX CABIN AFT SERVICE AREA STA 2884 BETWEEN -Y 450 FLOOR SUPPORT STRAP WITH CORROSION. REPLACED FLOOR SUPPORT STRAP ON STA 2884 BETWEEN -Y 200 AND -Y 4520 IAW SRM 51-72-11, PAR 4 AND 6.

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,224 hrs · 8,339 cycles

UPPER REAR FUSELAGE, PAX CABIN, AFT SERVICE AREA FROM STA 2800 TO STA 2870, -Y1292 BEAM CORRODED (FLOOR STRUCTURE BEAM PN: D53472172205). NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 2800-2870) · corrosion level 2 · airframe 17,224 hrs · 8,339 cycles

UPPER REAR FUSELAGE, PAX CABIN, AFT SERVICE AREA FROM STA 2800 TO STA 2870, +Y1292 BEAM CORRODED.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,224 hrs · 8,339 cycles

UPPER REAR FUSELAGE, PAX CABIN, AFT SERVICE AREA FROM STA 2936 TO STA 2992, -Y1300 SHEAR PLATE CORRODED (FLOOR STRUCTURE SHEAR PLATE PN: D53471124200). NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,224 hrs · 8,339 cycles

UPPER REAR FUSELAGE, PAX CABIN, AFT SERVICE AREA FROM STA 2800 TO STA 2884, -Y765 BEAM CORRODED (FLOOR STRUCTURE BEAM PN: D53472193200). NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,224 hrs · 8,339 cycles

UPPER REAR FUSELAGE, PAX CABIN, AFT SERVICE AREA FROM STA 2870 TO STA 2884, -Y1292 BEAM CORRODED (FLOOR STRUCTURE BEAM PN: D53472189202). NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.

Part: SHEAR PLATE — CORRODED (BS 2936-2992) · airframe 17,224 hrs · 8,339 cycles

UPPER FUSELAGE PAX CABIN AFT SERVICE AREA FROM STA 2936 TO STA 2992, -Y120, LATERAL SHEAR PLATE WITH CORROSION. REPLACED FUSELAGE LATERAL SHEAR PLATE FROM STA 2936 TO STA 2992 BETWEEN -Y1162.5 AND -Y1330, DUE TO CORROSION IAW SRM 51-72-11 PAR 4 AND 6. INSTALLED SOLID RIVETS IAW SRM 51-42-11, PAR 6B.

Part: FLOOR SUPPORT — CORRODED (BS 2870-2884) · airframe 17,224 hrs · 8,339 cycles

UPPER FUSELAGE PAX CABIN AFT SERVICE AREA FROM STA 2870 TO STA 2884, -Y 1292, LATERAL FLOOR SUPPORT WITH CORROSION. REPLACED FUSELAGE LATERAL FLOOR SUPPORT FROM STA 2754 TO STA 3026, -Y 1162.5 DUE TO CORROSION, IAW SRM 51-72-11 PAR 4 AND 6. INSTALLED HI-LOCK IAW SRM 51-42-11 PAR 7B. INSTALLED SCREWS, BOLTS AND NUTS IAW SRM 51-42-11, PAR 5B AND PAR 5C PAGE 7

Part: FLOORBEAM — CORRODED (BS 2884) · airframe 17,224 hrs · 8,339 cycles

UPPER FUSELAGE PAX CABIN AFT SERVICE AREA STA 2884 BETWEEN -Y 800 AND -Y 1020 FLOOR SUPPORT STRAP WITH CORROSION. REPLACED FLOOR SUPPORT STRAP ON STA 2884 BETWEEN -Y 800 AND -Y 1020 IAW A319 SRM 51-72-11 PAR 4 AND 6.

Part: FLOOR SUPPORT — CORRODED (BS 2800-2870) · airframe 17,224 hrs · 8,339 cycles

UPPER FUSELAGE PAX CABIN AFT SERVICE AREA FROM STA 2800 TO STA 2870, -Y 1292 LATERAL FLOOR SUPPORT WITH CORROSION. REPLACED FUSELAGE LATERAL FLOOR SUPPORT FROM STA 2800 TO 2870 BETWEEN -Y 1162.5 AND -Y 1292, DUE TO CORROSION, IAW SRM 51-72-11 PAR 4 AND 6. INSTALLED HI-LOCK IAW SRM 51-42-11, PAR 7B. INSTALLED SCREWS, BOLTS AND NUTS IAW SRM 51-42-11 PAR 5B AND 5C PAGE 7.

Part: FLOOR SUPPORT — CORRODED (BS 2800-2884) · airframe 17,224 hrs · 8,339 cycles

UPPER FUSELAGE PAX CABIN AFT SERVICE AREA FROM STA 2800 TO STA 2884, -Y 765, LATERAL FLOOR SUPPORT WITH CORROSION. REPLACED FUSELAGE LATERAL FLOOR SUPPORT FROM STA 2800 TO STA 2992, -Y 765, DUE TO CORROSION IAW SRM 51-42-11, PAR 4 AND 6. INSTALLED HI-LOCK IAW SRM 51-42-11 PAR 7B. INSTALLED SCREWS, BOLTS AND NUTS IAW SRM 51-42-11, PAR 5B AND 5C PAGE 7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,224 hrs · 8,339 cycles

UPPER FUSELAGE PAX CABIN AFT SERVICE AREA STA 2884 BETWEEN -Y 500 AND -Y 750 FLOOR SUPPORT STRAP WITH CORROSION. REPLACED FLOOR SUPPORT STRAP ON STA 2884 BETWEEN -Y 500 AND -Y 750 IAW A319 SRM 51-72-11 PAR 4 AND 6.

Part: SLIDE — NO TEST (LT WING) · airframe 16,293 hrs · 7,889 cycles

DURING MX, LT WING SLIDE PARTIALLY DEPLOYED. REPLACED LT OVERWING SLIDE ASSY.

Part: FLOORBEAM — CORRODED (BS 765) · corrosion level 2 · airframe 4,948 hrs · 2,492 cycles

FLOORBEAM AT Y STATION 765 BETWEEN FR 66 AND FR 70 CORRODED. REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (BS 1292) · corrosion level 2 · airframe 4,948 hrs · 2,492 cycles

FLOORBEAM AT Y STATION -1292 AT FR 68 CORRODED. REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (BS 765) · corrosion level 2 · airframe 4,948 hrs · 2,492 cycles

FLOORBEAM BETWEEN Y STATIONS -765 AND -254 AT FR 68 CORRODED. REPLACED DAMAGED AREA.

Part: FLOORBEAM — CORRODED (BS 765) · corrosion level 2 · airframe 4,948 hrs · 2,492 cycles

FLOORBEAM AT Y STATION -765 AND FR 68 CORRODED. REPAIRED FLOORBEAM.

Part: SEAT TRACK — CORRODED (BS 765) · corrosion level 2 · airframe 4,948 hrs · 2,492 cycles

FOUND SEAT TRACK AT Y STATION -765 AT FR 66 CORRODED. REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,948 hrs · 2,492 cycles

AFT FLOORBEAM UNDER AFT GALLEY CORRODED. REPAIRED FLOORBEAM UNDER AFT GALLEY.