N523NK

Part: SEAL — FAILED (DEOILER) · airframe 57,366 hrs · 26,301 cycles

ODOR DETECTED ON TAKEOFF IN COCKPIT. DISAPPATED QUICKLIY. DESCENDING FRO CRUISE ALTITUDE DETECTED STRONGER ODOR IN COCKPIT STARTING AROUND 26,000FT HAD AGAIN DISAPPATED BEFORE ODOR CHECKLIST COULD BE COMPLETED.-FOUND BOTH #1 & #2 DEOILER SEALS BAD, REPLACED #1 & #2 ENG DEOILER SEALS IAW AMM 12-60-31. RAN ENGS IAW AMM 71-00-00. PERFORMED TSM 21-00-00, MNO FURTEHR DEFECTS NOTED, A/C OKAY FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 57,321 hrs · 26,282 cycles

STRON MUSTYODOR ON T/U GOES AWAY AT THRUST REDUCTION REAPPEARS LATER IN THE FLIGHT ON DESCENT.-THE AIR EVENT TSM 05-50-00-810-831-A ACCOMPLISHED INSPECTION OF APU AND BOTH ENG'S CARRIED OUT. NO LEAKS NOTED PACKS ON GROUND NO ODOR NOTED.

Part: NONE — INOPERATIVE (1SQ1) · airframe 56,437 hrs · 25,845 cycles

WX RADAR INOP-R&R WEATHER RADAR TRANSCEIVER IAW AMM 34-41-33, OP`S CHECK GOOD.

Part: NONE — NONE · airframe 56,258 hrs · 25,747 cycles

AFT RIGHT FA'S FLASHLIGHT INOP.-REMOVED AND REPLACED AFT R FA'S FLASHLIGHT IAW CMM 25-60-02. FUNCTION CHECK OK.

Part: NONE — NONE · airframe 55,507 hrs · 25,420 cycles

FOUL ODOR ON APPROACH FROM PACK 1-PERFORMED ENG #1 PACK BURNOUT IAW AMM 21-00-00-615-004. AC OK FOR CONTD SVC. AEROTRACER UTILIZED THROUGHOUT CABIN.

Part: NONE — NONE · airframe 53,915 hrs · 24,759 cycles

FWD MEGA PHONE INOP-REMOVED AND REPLACED FWD MEGA PHONE IAW AMM 25-65-51

Part: UNKNOWN — ODOR (CABIN) · airframe 52,151 hrs · 24,052 cycles

SMELL OF WET PAINT DESCENDING THROUGH 10,000 FT BOTH PILOT AND F/O REPORTED SMELL. PACKS A319 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD 30626/MP K6443 (ENHANCED ECS)-AT OR BELOW FL 370). DURING TROUBLESHOOTING, THE PRIMARY ASSUMPTION AWS A "TYPE 10" ODOR REPORT. DURING INVESTIGATION, IAW TSM 05-50-00. FOUND NO DEFECTS AT THIS TIME, NO ODOR NOTED. THIS CLEARS DMI 2647867-2 DMI LOG UPDATED MOC NOTIFIED PACK 1 ACTIVATED.

Part: UNKNOWN — ODOR (CABIN) · airframe 50,706 hrs · 23,478 cycles

MUSTY SMEEL DURING DESCENT @ 9000' ENGINES IDLE. FLIGHT ATTENDANTS AND COCKPIT CREW HAD THE SAME EXPERINCE. WE SUSPECTED PACK 1 SO WE TURNED IT OFF. WE ARE NOT SURE IF TURNING PACK 1 OFF HELPED OR WE JUST GOT USED TO THE SMELL TOO CLOSE TO LANDINE TO TOUBLE SHOOT.-ACCOMPLISHED TI 2100-1706 "DATA COLLECTION OF INSPECTION RESULTS OF A/C PNEUMATIC! A.C. SYS AFTER ODOR CCURENCE. NO CONTAMINATION SENSED WITH AERO TRACER. DMI # 260285901 RAMINS OPE. A/C OK FOR SVC."

Part: UNKNOWN — ODOR (CABIN) · airframe 50,698 hrs · 23,473 cycles

DIRTY SOCK SMELL IN CABIN AT FL390 WHILE FLYING THRU MED. TURBULANCE. TURNED OFF PACK 2 + FUMES DISSIPATED. THEN FUMES AGAIN IN COCKPIT + CABIN ON APPROACH -PERFUMED TSM 05-50-00-810-931A . CHECKED DEOILER CASING FOUND NO EVIDENCE OF OIL LEAK IN BOTH #1 & #2 ENGINES DISSASSEMBLE TUBES FOR CONDENSORS IN BOTH PACK 1 & 2 . CONT LOG 2602852-1

Part: UNKNOWN — FUMES · airframe 50,340 hrs · 23,312 cycles

"FUME EVENT ON DESCENT TURNED OFF PACK # 1 ODOR WENT AWAY. ( 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: A/C PACK — ODOR (NR 1) · airframe 50,228 hrs · 23,263 cycles

FUME EVENT- DESCENDING THROUGH 10,000 FT FA'S REPORTED A DIRTY SOCK /MUSTY SMELL IN THE FORWARD CABIN. TURNED OFF PACK 1 & BLEED 1 AND THE FUMES SEEM TO DISSIPATE. -COMPLY WITH TSM 05-50-00-810-831-A IDENTIFICATION OF CABIN , SMOKE OR FUME FOUND NO 1 PACK TO BE THE CAUSE OF ODOR.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 49,408 hrs · 22,866 cycles

DIRTY SOCK SMELL COMING INTO THE COCKPIT FROM THE APU BLEED. ACCOMPLISHED TSM 05-50-00-810-831. FOR CABIN ODOR. RAN BOTH PACKS ON APU BLEED. ISOLATED PACKS NO SIGN OF CONTIMINATION INSPECTED PACKS AND APU AREAS NO SIGNOFF POSSIBLE CAUSE. A/C OK FOR SVC.

Part: UNKNOWN — ODOR (CABIN) · airframe 48,703 hrs · 22,543 cycles

DIRTY SOCK SMELL PASSING 10000 ' IN CABIN ON APROACH. DISSIPATED WITHIN 2 MINS OF TURNING PACK 2 OFF ( PACKS 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 OUT PER AMM 21-00-00-615-004-A OPS CHECK LEAK CHECK GOOD NO ODORS NOTED THIS DMI 252927001 MOC NOTIFIED PLACARD REMOVED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 47,775 hrs · 22,161 cycles

DURING RON CHECK FOUND CAPT FLASHLIGHT (11MM) TO BE INOPERATIVE-REMOVED AND REPLACED FLASHLIGHT (11MM) IAW AMM 25-65-00.

Part: A/C PACK — CONTAMINATED · airframe 47,724 hrs · 22,144 cycles

FUME EVENT ON DESCENT THROUGH 11000 IN COCKPIT -PERFORMED TSM 05-50-00-810-801, VISUALLY INSPECTED APU FOR SIGNS OF OIL IAW TSM 49-00-00-801-921A. NO DEFECTS NOTED. INSPECTED ENG 1 AND ENG 2 FOR OIL IAW TSM 71-00-00-810-801. NO OIL NOTED. PERFORMED DECONTAMINATION OG PACK 1 AND PACK 2WITH ENGINES IAW AMM 21-00-00-615-004A. NO SMELL NOTED AC OK FOR SERVICE

Part: ECS — CONTAMINATED (AC BAY) · airframe 46,838 hrs · 21,798 cycles

FUME EVENT DESCENDING THROUGH FL 220AT IDLE FA REPORTED STRONG DIRTY SOCK SMELL AFT CABIN PACK 2 ISOLATED SMELL DISSIPATED ( PACKS WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - AT OR BELOW FL 370 )-ACCOMPLISHED DECONTAMINATION OF THE ENVIRONMENTTAL CONTROL SYSTEM WHEN THE TEMPERATURE IS BELOW 24 DEG C. (APU) IAW AMM 21-00-00-615-001-A. OPS CHECK GOOD, LEAK CHECK GOOD. NO CABIN ODOR AT THIS TIME. THIS CLEARS DMI 241483501. MOC NOTIFED. PLACARD REMOVED.

Part: ECS — CONTAMINATED · airframe 46,263 hrs · 21,565 cycles

FUME EVENT ON DESCENT-REF TSM 05-50-00-810-831-A ACCOMPLISHED DECONTAMINATION OF THE ECS WITH ENGINES, FOUND NO SIGNS OF ODOR WITH AEROTRACER. A/C OK FOR SERVICE IAW AMM 21-00-00-615-004-A, 71-00-00AMM.

Part: COMPUTER — MALFUNCTIONED (NR SFCC) · airframe 45,766 hrs · 21,332 cycles

IN CRUISE FLIGHT ECAM "F/CTL SLATS LOCKED - WING TIP BRAKE ON " ACCOMPANIED BY FLASHING AMBER " S. LOCKED " ABOVE SLAT/FLAP POSITION INDICATOR. ON APPROACH + LANDING SLATS EXTENDED TO POSITIONS 1, 2, + 3 AS FLAP HANDLE SELECTOR WAS MOVED TO POSITION 1, 2, + 3.-RESET WING TIP BRAKES IAW AMM 27-80-00. PERFORMED BITE TEST OF SFCC 1+ 2 IAW AMM 27-81-00. PERFORMED OPS TEST OF SLAY SYS IAW AMM 27-84-00. NO FAULTS FOUND. CHECKED ALL TORQUE LIMITERS, NO TRIPS PRESENT IAW AMM 27-80-00. R/R SFCC2 IAW AMM 25-51-34. OPS TEST GOOD. PERFORMED LC3CT IAW AMM 22-97-00. A/C IS CAT III DUAL CAPABLE. SDR REPORTABLE.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,880 hrs · 20,907 cycles

FA REPORTED FUMES IN MAIN CABIN DURING DECENT, APPROXIMATELY 8000 FT. PERFORMED TSM 05-50-00-810-831-A, PERFORMED VISUAL INSPECTION OF APU NO LEAKS FOUND. PERFORMED VISUAL CHECKS ON BOTH ENGINES, AND THE NR 2 DEOILER SEALS, NO EVIDENCE OF LEAKS, COULD NOT DUPLICATE THE ODORS.

Part: SEAL — LEAKING (NR DEOILER) · airframe 43,755 hrs · 20,436 cycles

FUMES IN CABIN, TROUBLESHOT IAW TSM 5-50-00-810-831-A. FOUND THE NR 2 DEOILER SEAL LEAKING. R & R IAW AMM 72-60-31.

Part: SEAL — DAMAGED (NR 2 DEOILER) · airframe 43,755 hrs · 20,436 cycles

FUMES IN CABIN. T/S IAW TSM 5-50-00-810-831-A FOUND NR 2 DEOILER SEAL LEAKING, R&R. ALSO R&R NR 1 DEOILER AS PRECAUTION IAW AMM 72-60-31 NO ODORS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,663 hrs · 20,397 cycles

FUMES DURING DECENT THRU 8000 FT, F/A REPORTED A BURNING ODOR OF OIL. PERFORMED DECONTAMINATION OF THE ECS, CAN NOT DUPLICATE ODOR ON GROUND. CHECKED APU BLEED AIR DUCT, NO OIL CONTAMINATION FOUND IAW TSM 05-50-00-810-831A, & AMM 21-00-00-615-002A/004A.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,583 hrs · 20,362 cycles

AFT F/A REPORT A SLIGHT SMELL OF BURNING PLASTIC AT APPROX 10,000'. AFTER INSPECTING THE RT/LT ENGINE, APU, PACK NR 1 & NR 2 , HYD SYSTEM, CABIN ITEMS AND COCKPIT ITEMS I FOUND NO INDICATION OF SMOKE IAW TSM 05-50-00-810-831-A

Part: UNKNOWN — ODOR (CABIN) · airframe 42,932 hrs · 20,113 cycles

BURNING RUBBER SMELL REPORTED BY FLIGHT ATTENDANT BEGINNING AT INITAL DESCENT AND CONTINING TO LANDING FROM ROW 14 AND BACK. ACCOMPLISHED TSM 05-50-00-810-831 PERFORMED APU OPS CHECK ALSO ISO #1 ENG AND #2 ENG BLEED SYSTEM,COUL NOT DUPLICATE SMELL ALL CHECKS GOOD A/C OK FOR SERVICE ALSO USED AMM 70-00-00 AND AMM 49-00-00

Part: SEAL — DIRTY (L2 DOOR) · airframe 41,138 hrs · 19,331 cycles

L2 DOOR LEAKING. INSPECTED THE DOOR SEAL IAW AMM 52-13-00. FOUND DEBRIS ON BOTTOM AFT CORNER. CLEANED AS REQUIRED. NO FUTHER DEFECTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 40,189 hrs · 18,921 cycles

CAPT FLASHLIGHT INOP. REPLACED FLASHLIGHT IAW AMM 25-65-00.

Part: SEAL — LEAKING (NR 1 ENGINE) · airframe 28,923 hrs · 18,382 cycles

DURING DESCENT EXPERIENCED DIRTY SOCKS SMELL COMPLIED WITH OS AFTER PACK 1 SHUTOFF SMELL DISSIPATED. PERFORMED INSPECTION AND PACK BURNOUT IAW AMM 21-00-00, FOUND THE NR 1 ENG DE-OILER CASING SEAL ASSEMBLY LEAKING OIL. REMOVED AND REPLACE THE DE-OILER CASING SEAL ASSY IAW AMM 72-60-31. OPS CHECK GOOD, NO DEFECT OR SMELL NOTED AT THIS TIME.

Part: STOWAGE BOX — INOPERATIVE (OXYGEN MASK) · airframe 37,764 hrs · 17,839 cycles

FIRST OFFICER`S OXYGEN MASK TEST FUNCTION BROKEN. R & R OBSERVER'S OXYGEN MASK STOWAGE BOX W/SERVICEABLE UNIT IAW AMM 35-12-41.

Part: PROXIMITY SWITCH — MALFUNCTIONED (R2 DOOR) · airframe 31,143 hrs · 14,815 cycles

R2 DOOR INDICATES OPEN WHEN IT IS CLOSED. R & R PROXIMITY SWITCH IAW AMM 52-71-11, APPLIED TSM 52-13-00-810-804-A. OPS CHECKED OK.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 29,326 hrs · 13,964 cycles

DURING PHASED ARRAY INSPECTION, CORROSION FOUND ON LT WING AT RIB-10. REMOVED CORROSION IAW 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 57-21-11. PERFORMED REPAIR DOUBLER IAW RIR 572-58944 & TD 51-52-22045. REPAIRED TO BE INSPECTED AT 27700FC/49600FH WITHIN INTERVALS OF 15000FC/15000FH.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 6 DEF) · airframe 28,786 hrs · 13,746 cycles

ROW 6DEF OXYGEN MASKS FELL. RESTOWED MASKS IAW AMM 35-21-43-550-801-A. PERFORMED DROP TEST IAW AMM 35-23-00-710-001-A. DROP TESTED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 6 DEF) · airframe 2,874 hrs · 13,731 cycles

6 DEF OXYGEN MASK DROPPED DURING TAXI IN. REPACKED MASK AT ROW 6 DEF AND TESTED UNIT IAW AMM. OP'S CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (F/A SEAT) · airframe 28,744 hrs · 13,731 cycles

AFTER TAKEOFF FWD F/A OXYGEN MASKS DEPLOYED. STOWED MASKS AND PERFORMED DROP TEST IAW AMM 35-23-00-710-001A AND 35-21-43-550-801A.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 28,368 hrs · 13,570 cycles

CAPTAIN`S OXYGEN MASK LEAKING AND WILL NOT SEAL PROPERLY. R & R SECOND OBSERVER`S OXYGEN MASK IAW AMM 35-12-41. OPS CK & LEAK CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 6 DEF) · airframe 27,801 hrs · 13,325 cycles

OXYGEN MASKS DROPPED ON ROW 6 SEATS D E F. RESTOWED OXYGEN MASKS AT SEAT 6 D IAW AMM. NO FURTHER FAULTS REPORTED.

Part: SLIDE — FAILED (L4 DOOR) · airframe 26,970 hrs · 12,975 cycles

L4 DOOR SLIDE UNRAVELED/DEPLOYED. R & R L4 SLIDE PACK IAW AMM. OPS CHECKED OK IAW W/O 67765, ELEMENT NR 1.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 26,875 hrs · 12,931 cycles

L1 DOOR ASSIST ACTUATOR PRESSURE LOW. SERVICED L1 DOOR ASSIST IAW AMM.

Part: RESERVOIR — LOW PRESSURE (ESCAPE SLIDE) · airframe 26,822 hrs · 12,909 cycles

MAIN DOOR OPENING INDICATE CHECK SLIDE PRESSURE AMBER RIGHT OVERWING EXIT. R & R RIGHT OVERWING ESCAPE SLIDE RESERVOIR IAW TSM AND AMM. OPS CK GOOD.

Part: OXYGEN MASK — CHATTERING (COCKPIT) · airframe 26,445 hrs · 12,722 cycles

F/O’S OXYGEN MASK, WHEN INHALING, DOES NOT FLOW SMOOTHLY, IT CHATTERS. R & R F/O O2 MASK IAW AMM 35-12-41-000-001-A AND 35-12-410-001-A. OPS CHECKED GOOD.

Part: MEGAPHONE — NO TEST (CABIN) · airframe 25,828 hrs · 12,432 cycles

FWD MEGAPHONE WONT TEST. R & R FWD MEGAPHONE REF ACFT MM.

Part: COVER — UNSECURE (O2 MASK) · airframe 25,536 hrs · 12,294 cycles

L1 O2 MASK COVER IS FALLING. L1 O2 MASK DID NOT OPEN. ONLY MISALIGNED. RESECURED L1 O2 COVER IAW ACFT MM.

Part: SEAL — DIRTY (ZONE 800) · airframe 24,429 hrs · 11,781 cycles

SQUEAL COMING FROM ACFT RT OVERWING EXIT. REMOVED RT WING EMERGENCY EXIT LATCH IAW ACFT MFG MANUAL. CLEANED HATCH SEAL, DEACTIVATED & REACTIVATED RT WING INFLATION RESERVOIR IAW MFG MANUAL.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 24,061 hrs · 11,589 cycles

CABIN EMERGENCY LIGHT BATTERY CAPACITY CHECK . AFT LT EPSU BATTERY FAULT (13WL). INSTALLED EMERGENCY BATTERY PACK IAW MM. OPS CHECKED GOOD OK FOR SERVICE.

Part: LATCH — LACK OF LUBE (L2 DOOR) · airframe 22,981 hrs · 11,049 cycles

L2 DOOR WILL NOT LATCH TO OPEN POSITION. LUBRICATED DOOR GUST LOCK. PERFORMED OPS CHECK IAW AMM 52-10-00-010-001 AND 52-10-00-410-001. OPS CHECKED OK, NO DEFECTS.

Part: BLEED AIR SYS — FAILED · airframe 22,489 hrs · 10,816 cycles

BOTH ENGINE BLEEDS LOST. PERFORMED EMERGENCY DESCENT TO 10000 FT, MASKS DEPLOYED. PERFORMED AIR RETURN.

Part: GUST LOCK — BROKEN (R2 DOOR) · airframe 21,855 hrs · 10,507 cycles

R2 DOOR CLOSED BUT SHOWS OPEN ON ECAM AND GUST LOCK NOT WORKING. ACCOMPLISHED OPS CHECK OF DOOR WARNING SYS IAW AMM 52-71-00-710-001-A. OPS CHECK GOOD ACCOMPLISHED DOOR OPS CHECK IAW AMM 52-11-00-820-001-A. DOOR LATCHED IN FULL OPEN POSITION.

Part: SKIN — CONTAMINATED (RUDDER) · airframe 21,498 hrs · 10,341 cycles

EMPENNAGE VERTICAL STABILIZER RUDDER LT SIDE PANEL WITH TRAPPED FLUID AT HOISTING POINT NR 1. A PERMANENT REPAIR WAS INSTALLED AT DAMAGED AREA IAW REPAIR GUIDELINES 70561617/006 AND 70561617/007 UNDER THE NON ROUTINE ITEM; WO: A1A093, SUBJOB: 3, ITEM: 37.

Part: SUPPORT BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,498 hrs · 10,341 cycles

PAX CABIN BETWEEN FR 66 - 67, -Y50 FLOOR SUPPORT BEAM WITH CORROSION. DAMAGED PART WAS REPLACED IAW THE SRM 51-72-11, PARAGRAPH 4 AND 6.

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

PAX CABIN BETWEEN FR 68-70, Y30 FLOOR SUPPORT CORRODED. PART REPLACED IAW SRM 51-72-11,

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,498 hrs · 10,341 cycles

AFT CARGO BAY PROFILE ASSY CORRODED, FROM FWD BULKHEAD TO FR 52, S38R. PART REPLACED IAW SRM 51-42-11.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,498 hrs · 10,341 cycles

AFT CARGO BAY PROFILE ASSY CORRODED, FROM FR 58 TO FR 59, S38L. PART REPLACED IAW THE SRM 51-42-11.

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

AFT CARGO BAY PROFILE ASSY CORRODED, FROM FR 52 TO FR 55A, S38R. PART REPLACED IAW SRM 51-42-11.

Part: ANCHOR FITTING — CORRODED (ZONE 600) · airframe 21,498 hrs · 10,341 cycles

RT WING, OUTER WING REAR SPAR JACK FITTING WITH CORROSION. THE CORRODED FITTING WAS REPAIRED IAW MESSAGE 70561498/007 AND TECH DISPOSITION: TDJ1S2196832012, ISSUE A, UNDER THE NON ROUTINE ITEM; WO A1A093, SUBJOB: 6, ITEM: 8.

Part: ANCHOR FITTING — CORRODED (LT WING) · airframe 21,498 hrs · 10,341 cycles

LT WING, OUTER WING REAR SPAR JACK FITTING WITH CORROSION. THE CORRODED FITTING WAS REPAIRED IAW MESSAGE 70561498/007 AND TECH DISPOSITION TDJ1S2196832012 ISSUE A, UNDER THE NON ROUTINE ITEM; WO: A1A093, SUBJOB: 5, ITEM: 2.

Part: CYLINDER — LOW PRESSURE (PAX DOOR) · airframe 19,048 hrs · 9,105 cycles

L1 DOOR ASSIST BOTTLE REQUIRE SERVICE. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001.

Part: HOOK — OBSTRUCTED (R2 DOOR GIRTBAR) · airframe 17,515 hrs · 8,340 cycles

UNABLE TO CLOSE AND ARM R2 DOOR. FOUND DEBRIS IN FWD GIRT FLOOR FITTING HOOK. REMOVED DEBRIS AND CLOSED AND ARMED DOOR IAW AMM 52-13-00 PB 501.

Part: ANGLE — CRACKED (NR 2 NACELLE) · airframe 15,816 hrs · 7,560 cycles

DURING INSPECTION, DISCOVERED THAT THE NR 2 ENGINE PYLON FWD ANGLE SECTION WAS CRACKED AT STA 537. THE SRM DID NOT SPECIFY AN ALLOWABLE REPAIR, THEREFORE A REPLACEMENT OF THE PART WAS ACCOMPLISHED.

Part: BUMPER BLOCK — WORN (THRUST REVERSER) · airframe 15,816 hrs · 7,560 cycles

DURING INSPECTION, DISCOVERED THAT THE NR2 ENGINE THRUST REVERSER, INBD & OTBD C-DUCT/PAN-DOWN BUMBER WEAR WAS BEYOND SRM ALLOWABLE DAMAGE LIMITS. A SRM REPAIR 038 WAS ACCOMPLISHED.

Part: PANEL — CORRODED (NR 2 NACELLE) · airframe 15,816 hrs · 7,560 cycles

DURING INSPECTION, DISCOVERED THAT THE NR2 ENGINE PYLON AFT FIXED FAIRING, INBD PANEL, TO BE CORRODED BEYOND SRM ALLOWABLE LIMITS. A NEW PANEL WAS FABRICATED AND REPLACED.

Part: PANEL — CORRODED (NR 2 NACELLE) · airframe 15,816 hrs · 7,560 cycles

DURING INSPECTION, DISCOVERED THAT THE NR2 ENGINE PYLON AFT FIXED FAIRING, OTBD PANEL, TO BE CORRODED BEYOND SRM ALLOWABLE LIMITS. A NEW PANEL WAS FABRICATED AND REPLACED.

Part: PANEL — CORRODED (NR 1 NACELLE) · airframe 15,816 hrs · 7,560 cycles

DURING INSPECTION, DISCOVERED THAT THE NR1 ENGINE PYLON AFT FIXED FAIRING, INBD PANEL, TO BE CORRODED BEYOND SRM ALLOWABLE LIMITS. A NEW PANEL WAS FABRICATED AND REPLACED.

Part: PANEL — CORRODED (NR 1 NACELLE) · airframe 15,816 hrs · 7,560 cycles

DURING INSPECTION, DISCOVERED THAT THE NR1 ENGINE PYLON AFT FIXED FAIRING, OTBD PANEL, TO BE CORRODED BEYOND SRM ALLOWABLE LIMITS. A NEW PANEL WAS FABRICATED AND REPLACED.

Part: BUMPER BLOCK — WORN (THRUST REVERSER) · airframe 15,816 hrs · 7,560 cycles

DURING INSP, DISCOVERED THAT THE NR1 ENGINE THRUST REVERSER, INBD & OTBD C-DUCT/PAN-DOWN BUMBER WEAR WAS BEYOND SRM ALLOWABLE DAMAGE LIMITS, SRM REPAIR 038 WAS ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (ZONE 900) · corrosion level 2 · airframe 9,769 hrs · 4,701 cycles

SURFACE CORROSION AFT GALLEY AREA FR68 AND Y765. REMOVED AND REPLACED FLOORBEAM FR66.5 TO FR 70 AT STA Y765 IAW SRM 51-72-11.

Part: SLIDE — FAILED (PAX DOOR) · airframe 8,500 hrs · 4,103 cycles

DURING MAINTENANCE OPERATIONAL CHECK OF RT AFT PAX/CREW DOOR SLIDE DEPLOYMENT, THE SLIDE FAILED TO DEPLOY. REMOVED AND REPLACED SLIDE AS REQUIRED.