N502NK

Part: NONE — NONE · airframe 58,275 hrs · 26,911 cycles

R2 DOOR ASSIST REQUIRED SERVICING.-R2 DOOR ASSIST SERVICED IAW AMM 52-10-00

Part: NONE — NONE · airframe 57,779 hrs · 26,728 cycles

R2 DOOR ASSIST BOTTLE REQUIRE SERVICE.-SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 12-14-00

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 52,217 hrs · 25,647 cycles

PASSENGER / CREW R2 DOOR REQUIRE SERVICING -SERVICED PASSENGER / CREW DOORS ASSIST BOTTLE AT R2 IAW AMM 52-10-00-210-004

Part: UNKNOWN — ODOR (CABIN) · airframe 55,184 hrs · 25,634 cycles

FA "A" REPORTS DIRTY SOCK SMIELL. IN THE CABIN. COMPLETED PROCEDURE FOR ELIMINATED OF ODOR CABIN COM 3.226.1 PACK 2 ISOLATED SMELL WENT AWAY COMPLETELY. ( 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 PACK BURN IAW AMM 21-00-00. TEST PERFROMED FOR 30 MINS. ALTERNATIG BETWEEN HOT AND COLD TEMPS/ NO DEFECTS OR SMELLS NOTED AT THIS TIME. THIS CLEARS DMI#26022370-1. PLACARDS REMOVED. MOC NOTIFIED, MX LOG UPDATED

Part: UNKNOWN — ODOR (CABIN) · airframe 54,847 hrs · 25,501 cycles

CABIN FUME EVENT DESCENDING BELOW 10KFT. FLT ATTENDANT A REPORTED A DIRTY SOCK SMELL IN THE FWD AND AFT CABIN AS WE DESCENDED ON THE ARRIVAL INTO RSW. ( PACKS A319 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - AT OR BELOW FL 370 )--

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 54,730 hrs · 25,444 cycles

R2 DOOR ASSIST BOTTLE LOW PER WEEKLY CHECK -SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 54,326 hrs · 25,274 cycles

MEGAPHONE INOP. R+R FWD MEGAPHONE IAW EQUIPMENT EMERGENCY DRAWINGS.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 53,127 hrs · 24,773 cycles

FUME EVENT REPORTED IN COCKPIT ON APPROACH TO LANDING. PERFORMED OPS CHECK OF A/C SYSTEM OF AIR CONDITIONING PACKS IAW AMM 12-33-21 NO ODORS NOTED AT THIS TIME.

Part: A/C PACK — CONTAMINATED (AC BAY) · airframe 53,132 hrs · 24,776 cycles

"DIRTY SOCK" SMELL DESCENDING THROUGH 7,000 FT. SHUT OFF PACK 1. SMELL WENT AWAY. ( PACKS 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 PACK 1 IAW AMM 21-00-00-615-002. NO DIRTY SMELL PRESENT AT THIS TIME. THIS CLEARS DMI # 2457702-1. PLACARD REMOVED. MOC NOTIFIED.

Part: UNKNOWN — ODOR (CABIN) · airframe 53,027 hrs · 24,812 cycles

DURING DESCENT FLIGHT ATTENDANTS COULD SMELL A SWEET SMELL LIKE TRANSMISSION FLUID. TROUBLESHOOTING ACCOMPLISHED IAW TSM 05-50-00-810-831-A. PERFORMED WALKAROUND NO FLUID LEAKS NOTED. PERFORM PACK BURNOUT (1 & 2 INDIVIDUALLY) NO SMELLS NOTED. CAUSE OF COS IS MISC TYPE 9, NO ODOR SMELLED IN AFT LAV, GALLEY CABIN. A/C OK FOR SVC.

Part: MEGAPHONE — INOPERATIVE (AFT CABIN) · airframe 52,743 hrs · 24,573 cycles

AFT EMERGENCY MEGAPHONE INOPERATIVE. REPLACED THE MEGAPHONE IAW CMM 25-60-01.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 51,549 hrs · 24,062 cycles

R2 DOOR ASSIST ACCUMULATOR LOW. SERVICED R2 DOOR ASSIST ACCUMULATOR TO PROPER PRESURE IAW AMM 52-10-00.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 50,149 hrs · 23,507 cycles

CRACK FOUND ON LH WINDSHIELD LOWER FRAME, FRAME LH4 LH WINDSHIELD LOWER SECTION, MAX DAMAGE LENGTH X1=6MM X WIDTH 6MM X X3=2MM, CAT B. RAF01 227692802 OPENED. REF LTPR NRI 1002575575-0010.-REVIEWED LTPR ROUTINE CARD 1002575575-0010 (EO 5311-1870)AND HAS BEEN ACCOMPLISHED.REQUIRED INSPECTION FROM EMBODIEMENT. 31400FC,TBD FH

Part: ENGINE — FAILED (NR 2) · airframe 49,980 hrs · 23,430 cycles

ON APPROACH ENG 2 FAIL. DID NOT RESTART. DID NOT RESTART DURING THE AUTOMATIC RESTART. ENGINE WAS SHUT DOWN-BORESCOPED HP COMPRESSOR AND HPT IAW AMM 72-00-00. NO DEFECTS FOUND. PERFORMED FUNCTIONAL TEST OF THE HPC STAGE 7 BLEED VALVE AND SOLENIODS IAW AMM 75-32-52. LEAK AND OPS CHECK GOOD. PER MOC REMOVED AND REPLACED UPPER RIGHT 7 STAGE HPC BLEED VALVE IAW AMM 75-32-52

Part: MEGAPHONE — MALFUNCTIONED (CABIN) · airframe 49,670 hrs · 23,283 cycles

FA REPORTED AFT MEGAPHONE ALARM WENT OFF. -R/R AFT GALLEY MEGAPHONE IAW 25-65-51.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 47,679 hrs · 22,385 cycles

R2 DOOR ASSIST BOTTLE LOW. SERVICED THE ASSIST BOTTLE IAW AMM 52-10-00. NO LEAKS NOTED.

Part: SERVO — MALFUNCTIONED (NLG STEERING) · airframe 47,031 hrs · 22,128 cycles

NLG STEERING FAULT. REMOVED AND REPLACED NOSE WHEEL STEERING SERVO CONTROL IAW AMM 32-51-51-401. OPS & LEAK CHECKED GOOD. NO FURTHER DEFECTS IAW AMM 32-51-51-720-051-A.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,753 hrs · 22,011 cycles

DURING APPROACH, ODOR IN THE CABIN. TROUBLESHOT IAW TSM 05-50-00-810-831-A, PERFORMED GVI OF THE NR 1 & 2 ENGINES. NO LEAKS NOTED. PERFORMED GVI OF APU. NO LEAKS NOTED. NO FUMES NOTED. ACFT OK FOR SERVICE.

Part: SKIN — GOUGED (L2 DOOR) · airframe 43,338 hrs · 20,498 cycles

GOUGE FOUND ON L2 DOOR SKIN PANEL. REPAIRED IAW EO 5213-1701.

Part: RIB — NICKED (LT WING) · airframe 43,338 hrs · 20,498 cycles

FOUND A NICK ON RIB 23 LT WING. REPAIR CORRECTED AS PER EO 5721-1702. BLEND OUT REPAIR COMPLETED.

Part: STRINGER — CORRODED (FRAMES 60-61) · corrosion level 2 · airframe 43,338 hrs · 20,498 cycles

FOUND CORROSION ON STRINGER 32L FRAMES 60-61. DEFECT CORRECTED IAW SRM TASK 53-00-13-3000-001 AND EO5341-1702.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 43,304 hrs · 20,482 cycles

L1 DOOR ASSIST BOTTLE REQUIRES SERVICE. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 25-10-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,218 hrs · 20,436 cycles

DIRTY SOCK ODOR THROUGH THE ENTIRE AIRCRAFT. OCCURED ON SEVEN MILE DESCENT. ACCOMPLISHED FAULT ISOLATION PROCEDURE IAW TSM 05-50-00-A10-831-A AND ENVIREMENTAL CONTROL SYSTEM PROCEDURE IAW AMM 21-00-00-615-001 NO ODORS NOTED/ FAULTS .A/C OK TO CONTINUE SERVICE.

Part: APU — ODOR (APU BAY) · airframe 42,950 hrs · 20,321 cycles

FUME EVENT NOTED INITIALLY AT TOP OF DESCENT FOR 1-2 MIN THEN C LEVEL OFF 6000 WITH ADVANCEMENT OF POWER COMPLETED ELIMINATION OF ODOR FUME IN COCKPIT CABIN CHECKLIST COULD NOT DETERMINE WHICH ENG. PAC SMELL WAS COMING FROM MAYBE BOTH FUMES IN COCKPIT AND CABIN NOT NOTED FROM APU. PERFORMED TROUBLESHOOTING OF CABIN ODOR IAW TSM 05-50-00-810-831-A FOUND APU TO BE THE SOURCE OF SMELL. ENG RUNS VERIFIED NO ENG/PACKS WERE SOURCE OS SMELL DURING OPERATION.

Part: APU — CONTAMINATED · airframe 42,812 hrs · 20,268 cycles

FUME EVENT, NOTED INITIALLY ON GROUND. PERFORMED TSM 05-50-00-810-831-A, FOUND CAUSED TO BE APU BLEED SYSTEM. IAW TSM 49-00-00-810-921-A; PERFORMED EXTERIOR INPECTION OF APU COMPARTMENT. FOUND OIL LEVEL SLIGHTLY BELOW FULL, OIL CAP SECURED & SCUPPER WAS CLEAN.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 42,789 hrs · 20,257 cycles

L1 DOOR ASSIST BOTTLE REQUIRES SERVICE. SERVICED L1 DOOR ASSIST BOTTLE WITH NITROGEN AS REQUIRED IAW AMM 52-10-00-614-001-A.

Part: DAMPER — LOW PRESSURE (L1 DOOR)

L-1 DOOR LOW PRESSURE DOOR ASSIST ACCUMULATOR. SERVICED L-1 DOOR ASSIST ACCUMULATOR TO PROPER PRESSURE IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 42,177 hrs · 19,981 cycles

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

Part: SEAL — DIRTY (R1 DOOR) · airframe 40,726 hrs · 19,325 cycles

SHORTLY AFTER TOP OF CLIMB, F/A REPORTED VIBRATION AND THE SOUND OF AIR AT THE L/E OF DOOR R1. VERIFIED BY BOTH PILOTS SOUND LASTED FOR THE REMAINDER OF THE FLIGHT. PERFORMED TSM 52-11-00-810-826-A INSPECTION OF THE DOOR SEAL, NO DAMAGE NOTED. ACCOMPLISHED STRUCTURAL LEAKAGE TEST IAW AMM 05-53-00-780-003-A01, LEAK TEST GOOD NO LEAK NOTED ACFT PLACED BACK INTO SERVICE.

Part: DOOR SEAL — DIRTY (R2 DOOR) · airframe 38,408 hrs · 18,284 cycles

FLIGHT ATTENDANTS REPORT LOUD SQUEAL AROUND DOOR R2 DURING DESCENT. STARTED JUST BEFORE SEAT BELT SIGN TURNED ON, APPROX 18,000 FT. INSPECTED & CLEANED R2 DOOR SEAL, NO DEFECTS OR FAULTS NOTED. PERFORMED LEAK TEST IAW AMM 05-55-00-780-003A, NO LEAKS NOTED. ACFT OK TO CONTINUE SERVICE.

Part: BUTTON — CRACKED (MASK TEST) · airframe 37,370 hrs · 17,778 cycles

F/O O2 MASK TEST PUSH BUTTON CRACKED. R & R F/O FULL FACE/QUICK DONNING MASK STOWAGE BOX IAW AMM 35-12-41 PB 401. OPS AND LEAK CHECKED GOOD.

Part: WINDOW — SCRATCHED (L2 DOOR) · airframe 34,744 hrs · 16,568 cycles

L2 DOOR WINDOW SCRATCHED. R & R L2 DOOR WINDOW IAW AMM 56-31-13.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 34,174 hrs · 16,287 cycles

AFT MEGAPHONE GREEN LIGHT NOT ILLUMINATED. REPLACED AFT MEGAPHONE IAW AMM 25-65-920-001-A. OPS CK GOOD IAW AMM 25-65-51-710-002-A.

Part: HOSE — DETACHED (OXYGEN MASK) · airframe 34,106 hrs · 16,257 cycles

CAPTAIN`S OXYGEN MASK HOSE CAME OFF MASK. R & R CAPTAIN`S OXYGEN MASK IAW MM 35-12-41-000-002 AND 35-12-41-400-002. OPS CHECKED OK IAW 35-12-41-710-001.

Part: OXYGEN MASK — UNWANTED DEPLOY (AFT GALLEY) · airframe 32,942 hrs · 15,733 cycles

OXYGEN MASKS IN AFT GALLEY DROPPED. PERFORMED OXYGEN MASK DROP TEST IAW AMM 35-23-00 NO DEFECTS NOTED.

Part: OXYGEN MASK — UNWANTED DEPLOY (GALLEY) · airframe 32,905 hrs · 15,718 cycles

OXYGEN MASKS IN AFT GALLEY DROPPED. CLOSED AND SECURED AFT GALLEY OXYGEN COMPARTMENT. PERFORMED OPS CHECK OF MANUAL MASK RELEASE IAW AMM TASK 35-23-00-710-001-A. DROP TEST OK.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 32,699 hrs · 15,641 cycles

CORROSION DETECTED FROM PHASED ARRAY INSPECTION ON LT WING SKIN PANEL NR 2 OVERHANG AT RIB 17. REF NRI 7337N00135 IAW SRM 51-74-00. REMOVED CORROSION TOP SKIN AND RE-MEASURED WITHIN ALLOWABLE SRM 57-21-1 LIMITS. TREATED, PREPPED, PRIMED AND PAINTED IAW SRM. MWI 080410103, OPENED FOR APPROPRIATE REINSPECTION INTERVALS.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 32,699 hrs · 15,641 cycles

CORROSION DETECTED FROM PHASED ARRAY INSPECTION ON LT WING SKIN PANEL NR 2 OVERHANG BETWEEN RIBS 15 AND 16. REMOVED CORROSIONIAW SRM 57-21-1. TREATED, PREPPED AND TOP COATED IAW SRM.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 32,699 hrs · 15,641 cycles

CORROSION DETECTED FROM PHASED ARRAY INSPECTION ON LT WING SKIN PANEL NR 2 OVERHANG BETWEEN RIBS 10 AND 11. REF NRI 7337N00131 IAW SRM 51-74-00. REMOVED CORROSION TOP SKIN AND RE-MEASURED WITHIN ALLOWABLE SRM 57-21-1 LIMITS. TREATED, PREPPED AND TOP COATED IAW SRM.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 32,699 hrs · 15,641 cycles

CORROSION DETECTED FROM PHASED ARRAY INSPECTION ON LT WING SKIN PANEL NR 2 OVERHANG BETWEEN RIBS 17 AND 18. REF NRI 7337N00136 ER SRM 51-74-00. REMOVED CORROSION TOP SKIN AND RE-MEASURED WITHIN ALLOWABLE SRM 57-21-1 LIMITS. TREATED, PREPPED, PRIMED AND PAINTED IAW SRM. MAW 080410002 OPENED FOR APPROPRIATE REINSPECTION INTERVALS.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 32,699 hrs · 15,641 cycles

CORROSION DETECTED FROM PHASED ARRAY INSPECTION ON LT WING SKIN PANEL NR 2 OVERHANG BETWEEN RIBS 14 AND 15. REF NRI 7337N00132 IAW SRM 51-74-00. REMOVED CORROSION TOP SKIN AND RE-MEASURED WITHIN ALLOWABLE SRM 57-21-1 LIMITS. TREATED, PREPPED AND TOP COATED IAW SRM.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 32,699 hrs · 15,641 cycles

CORROSION DETECTED FROM PHASED ARRAY INSPECTION ON LT WING SKIN PANEL NR 2 OVERHANG BETWEEN RIBS 16 AND 17.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 32,673 hrs · 15,632 cycles

R2 DOOR ASSIST BOTTLE PRESS LOW. SERVICED R2 (842) DOOR ASSIST BOTTLE WITH NITROGEN IAW AMM.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 32,673 hrs · 15,632 cycles

L2 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED L2 DOOR ASSIST BOTTLE WITH NITROGEN IAW AMM.

Part: SWITCH — DIRTY (LT OVERWING) · airframe 31,967 hrs · 15,334 cycles

LEFT OVERWING EMERGENCY EXIT INDICATED UNLOCKED ON FINAL AT 1100 FT. APPLIED TSM 52-21-00-810-806-A, RESET SYSTEM CLIMB'S FOUND AREA OF PROXIMITY SWITCH 21WV1 DUST & DEBRIS, CLEANED, CLEARANCE CHECKS OK, FUNCTIONAL TEST OK, ALL INDICATIONS NORMAL ON ECAM/FAP AT THIS TIME, ALL IAW AMM.

Part: BRACKET — BROKEN (COCKPIT O2 MASK) · airframe 30,688 hrs · 14,757 cycles

PRIMARY OBSERVER OXYGEN MASK INOPERATIVE DUE TO BROKEN BRACKET.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 29,623 hrs · 14,258 cycles

R2 DOOR ASSIST BOTTLE HAS LOW PRESSURE (1400 PSI). SERVICED ASSIST BOTTLE AT R2 DOOR IAW ACFT MM.

Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 29,323 hrs · 14,119 cycles

R-2 DOOR SLIDE LOW PRESSURE & HAS STARTED TO UNFOLD. R & R R2 DOOR ESCAPE SLIDE RAFT PACK ASSY IAW ACFT MM. OPS CHECKED OK.

Part: DOOR — NOISY (EMERGENCY EXIT) · airframe 29,308 hrs · 14,114 cycles

F/A REPORTED A SQUEALING NOISE FROM RT EMERGENCY OVERWING EXIT IN CRUISE. PERFORMED DETAILED VISUAL INSPECTION OF RT OVERWING EMERGENCY EXIT DOOR IAW ACFT MM. NO LOOSE HARDWARE OR DEFECTS NOTED. ACFT RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — DIRTY (EMERGENCY EXIT) · airframe 27,965 hrs · 13,460 cycles

LT EMERGENCY DOOR OPEN LIGHT RIGHT AFTER TAKE-OFF. RETURNED TO DEPARTURE. PERFORMED OPS TEST OF DOOR WARNING SYS IAW ACFT MM. PROXIMITY SWITCH CLEANED.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 27,568 hrs · 13,253 cycles

RT AFT DOOR EMERGENCY BOTTLE LOW. SERVICED DOOR EMERGENCY BOTTLE RT AFT IAW AMM 52-10-00-614-001-A.

Part: STRUCTURE — CONTAMINATED (RUDDER) · airframe 27,163 hrs · 13,040 cycles

VERTICAL STABILIZER RUDDER HOISTING POINTS 1, 2, 3 AT RT SIDE AND 2 AND 3 AND LT SIDE WERE FOUND WITH TRAPPED FLUID. REPAIRED IAW DISPOSITION TD K4S2394852012, ISSUE A,.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 26,673 hrs · 12,793 cycles

EPSU CAP TEST FOUND FWD LT EPSU FAILED CAP TEST. (10WL) P.O.O MRF 67209 BATTERY FAILED. REMOVED ACCESS PANEL TO 10WL. PERFORMED TEST AT EPSU UNIT BATTERY FAIL LIGHT ON. REMOVED BATTERY IAW AMM 33-51-38-000-002-A. INSTALLED IAW 33-51-38-400-002-A. TEST OK PANEL. R & R IAW AMM -25-23-42-00-001.

Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 26,076 hrs · 12,487 cycles

STRONG ODOR OF PLASTIC BURNING AFTER TAKE OFF, IN COCKPIT AND CABIN THAT DISSIPATED AFTER A FEW MINUTES. ODOR RETURNED ON DESCENT IN AFT CABIN AREA. PERFORMED VISUAL INSPECTION OF ENGINE INLET CORE. INSPECTED ALL E&E COMPARTMENTS. RAN BLEED AND PACKS WITH APU. RAN NR 1 AND NR 2 ENGINE. OPERATED BLEED AND PACKS OFF THEN ON. NO EVIDENCE OF LEAKS ON ENGINE OR APU. INSPECTED ALL CABIN LIGHTING AND SIGNS. INSPECTED GALLEY AND LAV ELECTRICAL CONNECTIONS. INSPECTED ALL OVER COCKPIT. INSPECTED ALL C/B FOR POPPED CONDITION. ALL IAW TSM 24-00-00-810-823-A. FIREFIGHTER INSPECTED ACFT FOR HOT SPOTS. NONE FOUND. COULD NOT FIND ANY UNUSUAL ODOR DURING INSP PROCESS. NO SMOKE OR HAZE OR BURNED ODOR FOUND. ACFT OK FOR SERVICE AT THIS TIME. PILOT VERIFIED ALL ENGINE PARAMETERS NORMAL IN FLIGHT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,433 hrs · 12,172 cycles

EPSU TEST FAILED. PERFORMED TSM 33-51-00-810-859A SWAP LT AND RT EPSU NO HELP FOUND 1 LIGHT AT 62WL INOPERATIVE. R & R BULB IAW 33-51-15-420-050A. OPS CHECKED OK EPSU BACK TO ORIGINAL POSITION.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 24,929 hrs · 11,922 cycles

R2 DOOR SLIDE POPPED. R & R SLIDE AT R2 IAW AMM 52-62-44-000-011-A. 52-62-44-400-006-A & REPLACED DIAPHRAM IN THE PERCUSSION MECHANISM OF DOOR DAMPER IN AND SERV IAW AMM 52-10-00-610-001A. OPS AND LEAK CHECKED GOOD.

Part: CYLINDER — LOW PRESSURE (PAX DOOR) · airframe 24,713 hrs · 11,806 cycles

DOOR ASSIST BOTTLES REQUIRES SERVICING. SERVICED DOOR ASSIST BOTTLES TO PROPER PRESSURE IAW AMM 52-10-00-PB 301.

Part: LOCK — INOPERATIVE (L1 HOLD OPEN) · airframe 24,058 hrs · 11,491 cycles

L1 DOOR WILL NOT LATCH OPEN. INSTALLED NEW SPRING & BUSHING ON DOOR LOCKING MECHANISM IAW AMM 52-11-12-400-001. ADJUSTED L-1 DOOR BUFFER IAW AMM SUB TASK 52-11-12-820-051. OPENED & CLOSED L-1 PAX DOOR IAW AMM 52-10-00-010-001 & AMM 52-10-00-410-001. DOOR OPS CORRECTLY, ACFT OK FOR SVC.

Part: ACCUMULATOR — LOW PRESSURE (R2 DOOR) · airframe 24,046 hrs · 11,484 cycles

R2 DOOR ACCUMULATOR LOW PRESSURE. R2 DOOR ACCUMULATOR SERVICED TO PROPER PRESS IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 23,644 hrs · 11,287 cycles

R2 DOOR EMERGENCY ASSIST BOTTLE PRESSURE LOW. SERVICED R2 DOOR EMERGENCY BOTTLE PRESSURE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 23,160 hrs · 11,048 cycles

R2 DOOR ACCUMULATOR PRESSURE LOW. SERVICED AS REQUIRED IAW AMM 52-10-00-64-001. NO OTHER DEFECTS.

Part: CYLINDER — LOW PRESSURE (R2 DOOR ASSIST) · airframe 22,961 hrs · 10,952 cycles

R2 DOOR ASSIST REQUIRES SERVICING. SERVICED R2 DOOR ASSIST IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 22,796 hrs · 10,875 cycles

R2 DOOR ASSIST BOTTLE LOW PRESSURE. SERVICED ASSIST/EMERGENCY OPERATION CYLINDER IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R2 DOOR ASSIST) · airframe 22,383 hrs · 10,684 cycles

R2 DOOR EMERGENCY CYLINDER ACCUMULATER PRESSURE LOW.

Part: ANCHOR — CORRODED (ZONE 600) · corrosion level 2 · airframe 20,233 hrs · 9,820 cycles

RT WING REAR SPAR AREA, MACHINING JACK ANCHORAGE WITH CORROSION AROUND THE BORE UPPER, LOWER SURFACE AND AT BORE INNER SURFACE. THE CORROSION REQUIRED MAJOR REPAIR IAW MFG INSTRUCTIONS.

Part: SKIN — CORRODED (NR 1 NACELLE) · airframe 20,720 hrs · 9,902 cycles

NR 1 ENGINE PYLON AFT LOWER SECTION INBD AND OTBD SKIN WITH CORROSION. REPLACED NR1 ENGINE PYLON AFT FAIRING SECTION INBD AND OTBD SKIN PANEL FROM PYLON STA 819 TO PYLON STA 1005 IAW SRM 51-72-11, PARA 4 AND 6.

Part: SKIN — CORRODED (NR 2 NACELLE) · airframe 20,720 hrs · 9,902 cycles

NR 2 ENGINE PYLON AFT LOWER SECTION OTBD AND INBD SKIN WITH CORROSION. REPLACED NR2 ENGINE PYLON AFT FAIRING SECTION INBD AND OTBD SKIN PANEL FROM PYLON STA829 TO PYLON STA1005 IAW SRM 51-72-11, PARA 4 AND 6.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,720 hrs · 9,902 cycles

UPPER FUSELAGE PAX CABIN AFT ENTRANCE AREA STA 2835, -Y 76.5 FLOOR SUPPORT WITH CORROSION. THE DAMAGED PART WAS REPLACED IAW SRM 51-72-11, PARA 4 AND 6.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,720 hrs · 9,902 cycles

UPPER FUSELAGE PAX CABIN AFT ENTRANCE AREA FROM STA 2800 TO STA 2870 BETWEEN -Y 116 AND -Y 129 FLOOR SUPPORT WITH CORROSION. THE DAMAGED PART WAS REPLACED IAW SRM 51-72-11, PARAGRAPH 4 AND 6.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,720 hrs · 9,902 cycles

UPPER FUSELAGE PAX CABIN AFT ENTRANCE AREA STA 2765, -Y 129 SEAT TRACK FLOOR SUPPORT WITH CORROSION. THE DAMAGED PART IS GOING TO BE REPLACED IAW SRM 51-72-11, PARAGRAPH 4 AND 6.

Part: STRUCTURE — CORRODED (ZONE 500) · corrosion level 2 · airframe 20,720 hrs · 9,902 cycles

LEFT WING REAR SPAR AREA, MACHINING JACK ANCHORAGE WITH CORROSION AROUND THE BORE UPPER AND LOWER SURFACE AND AT THE BORE INNER SURFACE. REQUIRE A MAJOR REPAIR.

Part: STRAP — CORRODED (ZONE 600) · corrosion level 2 · airframe 20,720 hrs · 9,902 cycles

RIGHT WING AILERON T/E LOWER SURFACE STRAP WITH CORROSION AT RIVET HEAD AREA. THE FASTENERS REPLACED.

Part: BRACKET — CRACKED (ZONE 100) · airframe 20,720 hrs · 9,902 cycles

LOWER FUSELAGE LATERAL AVIONIC COMPARTMENT BRACKET CRACKED. PART REPLACED.

Part: SKIN — CORRODED (ZONE 100) · airframe 20,720 hrs · 9,902 cycles

LOWER FUSELAGE FWD CARGO COMPARTMENT FLOOR CAVITY BETWEEN FR24 AND FR34 STR, RIVETS WITH CORROSION. FASTENERS REPLACED.

Part: SHEAR WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,720 hrs · 9,902 cycles

UPPER FUSELAGE PAX CABIN AFT ENTRANCE AREA FROM STA 2936 TO STA 2992, -Y125 LATERAL SHEAR WEB WITH CORROSION AND LOOSE RIVETS. REPLACED.

Part: BRACKET — CRACKED (ZONE 100) · airframe 20,720 hrs · 9,902 cycles

(EE4Y) LOWER FUSELAGE LATERAL AVIONIC COMPARTMENT BRACKET CRACKED. PART REPLACED.

Part: STRUCTURE — CORRODED (ZONE 600) · corrosion level 2 · airframe 20,720 hrs · 9,902 cycles

RT WING REAR SPAR AREA, MACHINING JACK ANCHORAGE WITH CORROSION AROUND THE BORE UPPER AND LOWER SURFACE AND AT THE BORE INNER SURFACE. REQUIRES MAJOR REPAIR.

Part: STRAP — CORRODED (FLOOR) · corrosion level 2 · airframe 15,187 hrs · 7,279 cycles

EVIDENCE OF CORROSION ON FLOOR STRAP ABOVE FRAME C-68 IN AFT CABIN UNDER FLOOR COMPARTMENT / REPLACED FLOOR STRAP IAW SRM 51-2-0

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,187 hrs · 7,279 cycles

FLOORBEAM AT Y160 BETWEEN FR68-FR70 / REMOVED AND REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,531 hrs

FLOORBEAM AT -Y1732 BETWEEN FR 68 AND FR 70 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM ASSY IAW SRM 51-72-11.

Part: BEARING — DISPLACED (L1 DOOR HINGE) · airframe 9,531 hrs · 4,580 cycles

L1 DOOR UPPER HINGE BEARING IS DISPLACED FROM ITS BORE. REPLACED UPPER AND LOWER L1 DOOR HINGE FITTINGS IAW AMM 52-11-00.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,531 hrs · 4,580 cycles

EVIDENCE OF CORROSION ON WEB BEAM Y1292 FR69 THROUGH FR70 RT SIDE. REMOVED AND REPLACED WEB ASSY IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

EVIDENCE OF CORROSION ON BEAM Y1292 FR 66 THROUGH FR 69. REMOVED AND REPLACED FLOORBEAM Y1292 FROM FR 66 THROUGH FR 69 IAW A319 SRM 51-72-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,531 hrs · 4,580 cycles

FLOOR SUPPORT Y254 FROM FR 66 THROUGH FR 68 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT Y254 FROM FR 66 THROUGH FR 68.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,531 hrs · 4,580 cycles

FLOORBEAM AT STATION Y254 BETWEEN FR 66 AND FR 68 CORRODED. REMOVED AND REPLACED FLOORBEAM AT STATION Y254 BETWEEN FR 66 AND FR 68.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,531 hrs · 4,580 cycles

EVIDENCE OF CORROSION ON FLOORBEAM Y1292 FROM FR66 THROUGH FR 68. REMOVED AND REPLACED FLOORBEAM Y1292 FROM FR 66 THROUGH FR 68 IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,531 hrs · 4,580 cycles

EVIDENCE OF CORROSION ON FLOORBEAM Y254 BEAM 175. REPLACED FLOORBEAM Y254 BEAM 175 IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,531 hrs · 4,580 cycles

FLOORBEAM AT STATION Y765 BETWEEN FR 66 AND FR 70 CORRODED. REMOVED AND REPLACED FLOORBEAM AT STATION Y765 BETWEEN FR 66 AND FR 70 IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,531 hrs · 4,580 cycles

FLOORBEAM AT STAT -Y765 CORRODED BETWEEN FR 66 AND FR 70. REMOVED AND REPLACED FLOORBEAM -Y765 BETWEEN FR 66 AND FR 70 IAW SRM 51-72-11.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 8,646 hrs · 4,160 cycles

L2 AND R2 EMERGENCY EXIT LIGHTS INOP ON GROUND. REMOVED AND REPLACED AFT (13WL) EPSU.

Part: VALVE — OPEN (FUELING PANEL)

CAE - CENTER TANK PUMP NR 1 FAULTED DURING CLIMB-OUT. FOUND CENTER TANK REFUEL VALVE LEFT MANUALLY OPEN AT FUELING PANEL, PUT VALVE SWITCH TO NORMAL AND IT CLOSED, OPS CHECK NORMAL. (M)