N517NK
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
91 reports on file, 2007-10-11 – 2024-01-11.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,533 hrs · 28,135 cycles
L1 DOOR ASSIST BOTTLE REQUIRES SERVICING.-SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001-A.
Earlier reports · 2007–2023 · 90 reports
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,368 hrs · 28,053 cycles
DURING SERVICE CHECK FOUND L1 DOOR ASSIST BOTTLE LOW-SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00
Part: MEGAPHONE — INOPERATIVE (ZONE 900) · airframe 58,431 hrs · 27,101 cycles
FORWARD FA MEGAPHONE INOP-R+R FWD FA MEGAPHONE IAW NKS DRAWING NO. A319-EMER EQUIP REV.3 AND AMM 25-65-00. OPS CHECK GOOD
Part: HOSE — LEAKING (MLG LOCK STAY AC) · airframe 58,019 hrs · 26,909 cycles
GREEN HYD LOST-UPON FURTHER EVAL FOUND PRESSURE HOSE ON L/H LOCK STAY ACTUATOR LEAKING. R&R MLG LOCK STAY ACTUATOR HOSE IAW AMM 32-11-22. PERFORMED FUNC. CHECK OF THE MLG ACTUATING CYLINDER IAW AMM 32-31-00-710-007. FUNC. CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME. SERVICED GREEN HYD. SYST. IAW AMM 12-12-29. NO LEAKS NOTED. A/C OK FOR SERV.
2021
Part: SKIN — DENTED (FRMS 11-12) · airframe 53,818 hrs · 24,916 cycles
"DENT FOUND ON LATERAL FWD FUSELAGE UPPER CROWN RH FR11-12 STR RH & LATERAL EDGE/ STRUCTURE -Y511. RAF01 2871823-01 CREATED-COMPLIED WITH E.O 5311-2149"
Part: SKIN — DENTED (FR 3-4) · airframe 54,818 hrs · 24,916 cycles
"DENT FOUND ON LATERAL FWD FUSELAGE SKIN FR3-4 STR RH & LATERAL EDGE/ STRUCTURE -Z250. RAF01 2871822-02 CREATED-COMPLIED WITH E.O. 25311-2147"
Part: SKIN — CORRODED (RIB 12&14 & STR1) · airframe 53,818 hrs · 24,916 cycles
"CORROSION FOUND ON TOP SKIN PNL, RIB12+14 & STR11. RAF01 2871822-01 CREATED-REPAIRED CORRODED AREA IAW REO L23533 CAT B REINSPECT 30,000 FC OR 41,900 FH FROM EMBODIMENT AND A INTERVAL OF 25,000 FC OR 34,900 FH METHOD DETAILED EXTERNAL IAW AIRBUS RDAF 80992698 / 007 / 2021 REV A."
Part: NONE — NONE · airframe 53,817 hrs · 24,915 cycles
L1 DOOR ASSIST REQUIRES SERVICING -SERVICED L1 DOOR ASSIST IAW AMM 52-10-00
2020
Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 53,614 hrs · 24,827 cycles
L1 DOOR ASSIST BOTTLE LOW PRESSURE -SERVICED L1 DOOR ASSIST BOTTLE PER AMM 52-10-00
Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 53,381 hrs · 24,723 cycles
L1 DOOR ASSIST BTL LOW. SERVICED L1 DOOR ASSIST BTL IAW AMM 52-10-00.
Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 53,339 hrs · 24,706 cycles
L1 DOOR ASSIST ACCUMULATOR LOW-SVCD L1 DOOR ASSIST ACCUMULATOR IAW AMM 52-22-00.
Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 52,191 hrs · 24,224 cycles
L1 DOOR ASSIST BOTTLE LOW-SVCD L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00
2019
Part: UNKNOWN — ODOR (CABIN) · airframe 51,448 hrs · 23,867 cycles
CABIN FUMES ODER IN CRUISE DURINF PRECIP + DURING DESCENT BOTH PACKS AFFECTED-PERFORMED TSM 05-50-00-810-831-A. FOR FUME EVENT ISOLATION FOUND NO FAULTS. A/C OK FOR SERVICE.
Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 51,080 hrs · 23,690 cycles
"AFTER TAKEOFF HAD ECAM: VENT SKIN VALVE FAULT. UNABLE TO PRESSURIZE (THIS IS AN SDR ITEM) ACCOMPLISH TSM 21-26-00-810-804-A, FOUND (22HQ) OUTLET VALVE AT FAULT, R+R OUTLET VALVE PER AMM 21-26-53, OPS CK GOOD. REF. LG PG# 2457820-01 & -02 FOR FURTHER WORK CAL TOOL: NK828 DUE: 28,NOV,19".
Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 51,005 hrs · 23,647 cycles
L1 DOOR ASSIST BOTTLE LOW-SERVICED R2 DOOR ASSIST AND AMM 52-10-00
Part: UNKNOWN — ODOR (COCKPIT) · airframe 50,960 hrs · 23,628 cycles
ELECTRICAL SMELL IN COCKPIT DURING CLIMB OUT, OBSERVED BY FIRST OFFICER.-UPON ARRIVAL N COCKPIT/ NO ELECTRICAL SMELL NOTED, PERFORMED TSM 05-50-00-810-031-A,STILL COULD NOT DUPLICATE. A/C OKAY FOR CONTINUE SERVICE.
Part: MEGAPHONE — INOPERATIVE (AFT CABIN) · airframe 50,776 hrs · 23,546 cycles
REAR RIGHT MEGAPHONE INOP-R/R REAR RIGHT MEGAPHONE IAW 25-65-51. OPS CHECK GOOD
Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 50,636 hrs · 23,459 cycles
L1 DOOR ASSIST BOTTLE REQ SVC. SVCD L1 DOOR PER AMM 52-10-00.
Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 50,085 hrs · 23,210 cycles
"L1 DOOR DOOR ASSIST PRESSURE IS LOW -SERVICED DOOR ASSIST BOTTLE IAW AMM 52-110-00-614-001 LEAK CK GOOD."
Part: UNKNOWN — ODOR · airframe 49,906 hrs · 23,138 cycles
POSSIBLE FUME EVENT PACK NR 2 -T/S PER TSM 05-50-00. REVIEWED CABIN ODER FORM. CREW REPORTED EVENT HAPPEND ON THE GATE WITH GROUND AIR CONNECTED WITH APU, PACK1 & 2 OFF. DISCONNECTED GROUND AIR RAN APU AND PACK 1 & PACK 2 SMELL DISSIPATED. NO ABNORMAL ODERS EMMITED FROM PACK SYSTEM. OPS CKS GOOD IAW AMM 21-00-00. OK FOR CONTINUED SERVICE.
Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 49,512 hrs · 22,980 cycles
L1 DOOR ASSIST BOTTLE PRESSURE BELOW WEEKLY LEVEL -SERVICED L1 DOOR ASSIST BOTTLE TO PROPER PRESSURE IAAW AMM 52-10-00
Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 48,684 hrs · 22,656 cycles
L1 DOOR ASSIST BOTTLE LOW PRESS.-SVCD L1 DOOR ASSIST BOTTLE PER AMM 52-10-00. NO DEFECT NOTED.
2018
Part: A/C PACK — CONTAMINATED (NR 2) · airframe 48,328 hrs · 22,521 cycles
FA REPORTS BACK OF AIRCRAFT HAS LIGHT DIRTY SOCK SMELL. TURNED PACK 2 OFF, ISOLATION CLOSED, SMELL IMPROVING. -PERFORMED DECONTAMINATION OF PACK 1 + 2 , WITH APU PER AMM 21-00-00. NO ODOR NOTED AT THIS TIME
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 46,748 hrs · 21,853 cycles
FWD MEGAPHONE INOP. R&R FWD MEGAPHONE IAW AIRCRAFT DRAWING NK319-132-EQ OPS TEST IS GOOD AT THIS TIME.
Part: MEGAPHONE — INOPERATIVE (FWD CABIN) · airframe 46,008 hrs · 21,522 cycles
DURING A WEEKLY CHECK, FOUND THE FWD MEGAPHONE INOPERATIVE. REMOVED AND REPLACED THE MEGAPHONE IAW DRAWING NKS 319-132-EQ. OPS CHECKED GOOD.
Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 45,565 hrs · 21,323 cycles
L1 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED THE L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00.
Part: SKIN — DAMAGED (RUDDER) · airframe 45,320 hrs · 21,211 cycles
RUDDER, RT SIDE SKIN SHELL DENTED AND DEBONDING.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 45,320 hrs · 21,211 cycles
A CRACK WAS FOUND IN THE LT WINDSHIELD, FRAMES 3-4 LT. EO 5311-1812 HAS BEEN ACCOMPLISHED.
Part: FITTING — CORRODED · airframe 45,320 hrs · 21,211 cycles
BOTTOM SKIN CORRODED, AT LT RIB 5. REMOVED CORROSION ON THE LT FWD DOOR AND AFT GIRT BAR FITTING AREAS IAW SRM 53-11-14-283-005 R121.
Part: SKIN — CORRODED (WS 5512) · airframe 45,320 hrs · 21,211 cycles
CORROSION FOUND ON THE TOP SKIN PANEL, WS 5512 RIB 10. REPAIR CLASSIFIED AS MAJOR.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 45,320 hrs · 21,211 cycles
CRACK FOUND IN THE RT WINDSHIELD, FRAMES 3- 4R. EO 5311-1810 AND HAS BEEN ACCOMPLISHED.
Part: UNKNOWN — ODOR (CABIN) · airframe 45,000 hrs · 21,079 cycles
FLIGHT ATTENDANT AT SEATS B & C REPORTED A CHEMICAL BASED ODOR IN AFT PORTION OF ACFT. PERFORMED TSM 05-60-00-810-831-A PROCEDURES FOR CABIN ODOR IDENTICATION. NO DEFECTS NOTED. NO ORDER DETECTED IN ACFT. ACFT OK FOR SERVICE.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 44,912 hrs · 21,041 cycles
DURING WEEKLY C CHECK, FOUND THE FWD MEGAPHONE INOPERATIVE. R & R FWD MEGAPHONE IAW NK 319-132-EQ, OPS CHECKED GOOD.
2017
Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 44,203 hrs · 20,744 cycles
L1 DOOR ASSIST BOTTLE REQUIRES SERVICE. SERVICED THE DOOR ASSIST BOTTLE IAW AMM 52-10-00, LEAK CHECKED GOOD.
Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 43,673 hrs · 20,520 cycles
L1 DOOR ASSIST CYLINDER REQUIRES SERVICING. CHARGED THE CYLINDER TO A PROPER LEVEL IAW AMM 52-22-00. LEAK CHECKED GOOD.
Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 43,596 hrs · 20,485 cycles
L1 DOOR ASSIST REQUIRES SERVICE. SERVICED L1 DOOR ASSIST IAW AMM 52-010-00-614-001-A. LEAK CHECKED GOOD.
Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 42,765 hrs · 20,116 cycles
L1 DOOR ASSIST BOTTLE LOW . SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00.
Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 42,494 hrs · 20,002 cycles
L1 DOOR ASSIST BOTTLE LOW. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-22-00.
Part: CABIN PRESSURE — MALFUNCTIONED · airframe 42,221 hrs · 19,884 cycles
CABIN DE-PRESSURIZED DURING DECENT OUT OF FL290, CABIN ALTITUDE REACHED 13800FT. OPERATIONAL CHECK OF THE PRESSURE CONTROL AND MONITORING SYS ACCOMPLISHED FOR CPC 1 AND CPC 2 IAW AMM 21-31-00-710-002A. BOTH CPC 1 AND CPC 2 CHECK NORMAL.
Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 42,186 hrs · 19,868 cycles
BOTH AFT FLIGHT ATTENDANTS REPORTED AN ODOR OF DIRTY SOCKS WHILE DESCENDING THROUGH 10,000 FT OR BELOW. R & R BOTH CABIN AIR RECIRCULATION FILTER'S IAW AMM 21-21-41. FOUND THE NR 1 & 2 ENGINES WITH OIL LEAKS AT DEOILER DUCT. R & R THE NR 1 ENGINE DEOILER CARBON SEAL ASSY & MATING RING IAW AMM 72-60-31. LEAK TESTED, NO LEAKS NOTED. NO ODOR IN CABIN.
Part: UNKNOWN — ODOR (CABIN) · airframe 42,184 hrs · 19,867 cycles
FLIGHT ATTENDANT REPORTED AN ODOR OF FORMALDYHDE WHILE DECSENDING THROUGH 10,000FT. THE ODOR DISAPATED AFTER LANDING. COMPLIED WITH ENGINE RUNS. RAN ENGINE 1 AND PACK 1 AND 2. COMPLIED WITH PACK BURNOUT. ALL THIS IAW AMM 05-50-00-810-831-A. NO ODORS. ACFT OK TO CONTINUE.
Part: UNKNOWN — FUMES · airframe 41,892 hrs · 19,742 cycles
FUME EVENT THRU 3000FT DURING DECENT. PERFORMED OPS CHECK OF PACK SYSTEMS 1 AND 2 IAW AMM 21-51-00 NO ODOR NOTED. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE
Part: SKIN — CORRODED (RT WING) · airframe 41,873 hrs · 19,734 cycles
FOUND THE TOP SKIN AT RIB 6 ON THE RT WING CORRODED. PERFORMED SHIM WASHER AND SEALANT REPAIR IAW EO 5721-1712.
Part: SKIN — DENTED (FRAMES 23-24) · airframe 41,873 hrs · 19,734 cycles
SKIN PANEL DENTED FRAMES 23 - 24, STRINGERS 24 - 25L. PERFORMED DOUBLER REPAIR IAW EO 5311-1723.
2016
Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 39,918 hrs · 18,918 cycles
5 ABC O2 MASK DROPPED. RE-PACKED O2 MASK BOX ASSY DROP CHECK GOOD REF AMM 35-21-43
Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 39,719 hrs · 18,827 cycles
FIRST OFFICER OXYGEN MASK HARNESS PUNCTURED. R & R MASK IAW AMM 35-12-41. OPS CHECKED GOOD.
Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 38,198 hrs · 18,119 cycles
F/A O2 MASK FELL AFTER TAKEOFF AFT OF A/C. REPACKED OXY O2 MASK IAW AMM 35-21-00.
2015
Part: OXYGEN MASK — UNWANTED DEPLOY (GALLEY) · airframe 36,495 hrs · 17,373 cycles
AFT GALLEY F/A O2 MASK DROPPED. STOWED AFT GALLEY F/A O2 MASK IAW AMM 35-21-43. PERFORMED OPS CHECK OF MANUAL MASK RELEASE IAW AMM 35-23-00. OPS CHECK GOOD.
Part: BLEED VALVE — FAILED (NR 1 ENGINE) · airframe 35,924 hrs · 17,108 cycles
NR 1 ENGINE FAILED, PRIOR HAD NR 1 ENGINE COMPRESSOR VANE ECAM. ACCOMPLISHED TROUBLESHOOTING IAW TSM 71-00-00-810-808-A. R & R ALL 7TH AND 10TH STAGE BLEED VALVES AND SOLENOIDS ON NR 1 ENGINE, REF LOG PAGES 71099-1, 71099-2, 71100-1, 71100-2, 99751-1, 99751-2, 99752-1, AND 99752-2. PERFORMED 3 HIGH POWER ASSURANCE CHECKS IAW AMM 71-00-00-710-013C. OPS CHECK GOOD.
Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 33,801 hrs · 16,128 cycles
DURING EPSU EMERGENCY LIGHT CHECK FOUND EPSU, 12WL, EMERGENCY RT FAULT. R & R RT EPSU BATTERY IAW AMM 33-51-00. OPS CHECK GOOD.
2014
Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 30,988 hrs · 14,780 cycles
DURING EPSU SYS TEST. EPSU FWD LEFT FAILED MESSAGE. FOUND POWER SUPPLY BATTERY FAILED. R & R IAW AMM 33-51-38. TESTED OK IAW 33-51-00-710-001-A.
Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT ROW 5) · airframe 30,640 hrs · 14,629 cycles
PAX OXYGEN MASK PANEL OPENED ON LANDING, ROW 5. REPACKED OXYGEN MASK IAW AMM 35-23-00.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 30,586 hrs · 14,605 cycles
AFT MEGAPHONE INOPERATIVE. R & R MEGAPHONE IN AFT GALLEY IAW AMM 25-65-51-920-001, MM 25-60-01. OPS CHECKED GOOD.
Part: MEGAPHONE — INOPERATIVE (GALLEY) · airframe 30,482 hrs · 14,565 cycles
F/A FOUND ON PREFLIGHT, MEGAPHONE IN AFT GALLEY INOPERATIVE. R & R AFT MEGAPHONE IAW CMM 25-60-01. OPS CHECKED NORMAL.
2013
Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 28,360 hrs · 13,639 cycles
REAR MEGAPHONE INOPERATIVE. R & R MEGAPHONE BATTERIES IAW AMM, MEGAPHONE OPS CKD GOOD.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 28,233 hrs · 13,582 cycles
FOWARD MEGAPHONE INOPERATIVE. R & R FWD MEGAPHONE IAW AMM.
Part: CYLINDER DAMPER — UNDERSERVICED (ZONE 800) · airframe 27,984 hrs · 13,464 cycles
DOOR DAMPER CYLINDER HAS LOW PRESSURE. SERVICED DOOR DAMPER CYLINDERS IAW ACFT MM.
Part: DOOR — LEAKING (EMERGENCY EXIT) · airframe 26,661 hrs · 12,835 cycles
HISSING SOUND HEARD FROM OVERWING EXIT DOOR ACFT RT DURING FLT. REMOVE RT EMERGENCY EXIT HATCH AND INSPECTED HATCH SEAL IAW ACFT MM. NO DEFECTS NOTED.
2012
Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 25,501 hrs · 12,286 cycles
R2 PAX DOOR LOW PRESSURE, SERVICED R2 IAW DOOR TO PROPER PRESSURE IAW ACFT MM.
Part: CYLINDER — LOW PRESSURE · airframe 23,019 hrs · 11,039 cycles
R-2 DOOR ASSIST BOTTLE REQUIRES SERVICE. SERVICED R-2 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001-A.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 22,951 hrs · 11,010 cycles
EMERGENCY LIGHTS REMAIN ON IN CABIN. WILL NOT TURN OFF WITH SWITCHES ON COCKPIT OVERHEAD. CIDS RESET UNSUCCESSFUL. RESET CIDS 1 & 2 DIR PERFORMED OPS TEST OF CABIN EMERGENCY LIGHTING SYS IAW AMM 33-51-00-710-001-A, TEST OK.
Part: FITTING — CORRODED (ZONE 500) · airframe 22,426 hrs · 10,753 cycles
LT MLG RETRACTION JACK ANCHORAGE FITTING WITH CORROSION. REPAIRED THE JACK ANCHORAGE FITTING IAW GUIDELINES.
Part: BEARING — WORN (RUDDER HINGE) · airframe 22,426 hrs · 10,753 cycles
EMPENNAGE VERTICAL RUDDER HINGES BEARING NR 1 THRU NR 5 AND NR 7 WITH PLAY AND RUST. REPLACED RUDDER HINGE BEARING FITTING 1 THRU 5 AND 7 DUE TO PLAY IAW AMM TASK 55-36-41-000-001A AND TASK 55-36-41-400-001-A.
Part: STRAP — WORN (NOSE COWL) · airframe 22,426 hrs · 10,753 cycles
NR 2 ENGINE NOSE COWL IN THE 1 O`CLOCK POSITION CAPPING STRAP WORN. REPAIRED NR 2 ENGINE NOSE COWL CAPPING STRAP AT 1 O`CLOCK POSITION DUE TO WEAR IAW SRM 54-10-00 REPAIR 30.
Part: PAD — WORN (THRUST REVERSER) · airframe 22,426 hrs · 10,753 cycles
NR 1 ENGINE LT AND RT THRUST REVERSER COWLS, INSIDE UPPER SECTION, PAD PLATES WITH WEAR. REPAIRED NR 1 ENGINE THRUS REVERSE LT AND RT BUMPER PAN DOW DUE TO WEAR IAW SRM 51-30-00, REPAIR 38.
Part: PANEL — DAMAGED (RUDDER) · airframe 22,426 hrs · 10,753 cycles
EMPENNAGE VERTICAL STABILIZER RUDDER SIDE PANEL HOIST POINT NR 2 LT WITH TRAPPED FLUID. REPAIRED THE HOIST POINT IAW GUIDELINES.
Part: STRAP — WORN (NOSE COWL) · airframe 22,426 hrs · 10,753 cycles
NR 1 ENGINE NOSE COWLING REAR SECTION, CAPPING STRAP WITH WEAR AT 1 O`CLOCK AND AND 11 O'CLOCK POSITION. REPAIRED NR 1 ENGINE NOSE COWLING REAR SECTION, CAPPING STRAP AT 1 O`CLOCK AND AND 11 O'CLOCK DUE TO WEAR IAW SRM 54-10-00, REPAIR 30.
Part: PAD — WORN (THRUST REVERSER) · airframe 22,426 hrs · 10,753 cycles
NR 2 ENGINE INBD AND OTBD COWLS CHOCKING PAD WEAR. REPAIRED NR 2 ENGINE THRUS REVERSE INBD AND OTBD BUMPER PAN DOW DUE TO WEAR, SRM 51-30-00, REPAIR 38.
Part: FITTING — CORRODED (RT WING) · airframe 22,426 hrs · 10,753 cycles
RT MLG RETRACTION JACK ANCHORAGE FITTING WITH CORROSION. THE JACK ANCHORAGE FITTING IAW GUIDELINES.
Part: SKIN — DENTED (ZONE 200) · airframe 22,426 hrs · 10,753 cycles
UPPER FUSELAGE EXTERIOR FROM FR-23 TO FR-24 BTW STR-21 LT AND STR-22 SKIN WITH DENT. REPAIRED FUSELAGE SKIN SECTION FROM FR23+9.250 TO FR23+17.250, BETWEEN STR-21LH AND STR-23LH IAW SRM 5311-11, PARA 5H TABLE 202, FIG 211.
Part: PANEL — CORRODED (RUDDER) · airframe 22,426 hrs · 10,753 cycles
EMPENNAGE RUDDER TIP PANEL 326 AT WITH CORROSION. REPLACED EMPENNAGE RUDDER TIP PANEL IAW SRM 51-72-11, PARAG 4 AND 6.
Part: CHANNEL — CORRODED (NR 1 NACELLE) · airframe 22,426 hrs · 10,753 cycles
NR 1 ENGINE CNA FIRE PROOF BULKHEAD LT AND RT CHANNELS CRACKED. REPLACED LT AND RT CHANNELS IAW SRM 51-72-11, PARAG 4 AND 6.
Part: CHANNEL — CRACKED (NR 1 NACELLE) · airframe 22,426 hrs · 10,753 cycles
NR 1 ENGINE,PYLON, PRECOOLER CASE, WITH CRACKS IN BOTH CORNERS. REPAIRED PRECOOLER CASE LT AND RT LATERAL CHANNELS AT NR 7 AND NR 8 RIBS IAW SRM 54-12 FIG 209.
Part: SKIN — CORRODED (PYLON) · airframe 22,426 hrs · 10,753 cycles
ENGINE, PYLON AFT LOWER SECTION INBD AND OTBD SKIN WITH CORROSION. REPLACED NR 2 ENGINE PYLON AFT LOWER OUTBD SKIN PANEL IAW SRM 54-54-11 PB 101 PARAG 4B DIAGRAM 101 TABLE A.
Part: STRAP — CORRODED (NR 2 NOSE COWL) · airframe 22,426 hrs · 10,753 cycles
NR 2 ENGINE, NOSE COWL IN THE 1 O`CLOCK POSITION CAPPING STRAP WITH WEAR. REPAIRED NR 2 ENGINE, NOSE COWL IN THE 1 O`CLOCK POSITION CAPPING STRAP IAW SRM 54-10-00, REPAIR 30.
Part: CHANNEL — CORRODED (NR 1 NACELLE) · airframe 22,426 hrs · 10,753 cycles
NR 1 ENGINE CNA FIRE PROOF BULKHEAD LT AND RT CHANNELS CRACKED. REPLACED LT AND RT CHANNELS IAW SRM 51-72-11, PARAG 4 AND 6.
Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 22,426 hrs · 10,753 cycles
UPPER FUSELAGE PAX CABIN BTW FR-69 NAD FR-70 AT -Y1060 SHEAR WEB WITH CRACK. REPLACED THE SHEAR PLATE IAW SRM 51-72-11 PARG 4 AND 6 AND DWG D53474180.
2011
Part: CYLINDER — LOW PRESSURE (ESCAPE SLIDE) · airframe 20,584 hrs · 9,843 cycles
RIGHT EXIT ROW SLIDE PRESSURE LOW. R & R OFFWING ESCAPE SLIDE RESERVOIR (7507 MM ) IAW AMM 25-62-46-000-001 & AMM 25-62-46-400-001. OPS CK GOOD.
Part: ACM — FAILED (NR 1) · airframe 20,218 hrs · 9,657 cycles
HIGH SPEED ABORT AT 125KTS DUE TO CABIN SMOKE RETURNED TO GATE. CONFIRMED CABIN SMOKE DUE TO ACM NR 1 FAILURE. ACCOMPLISHED HIGH POWER RUN CONFIRMED NO SMOKE DETECTED. COMPLIED WITH 05-51-16-200-001 INSP AFTER BRAKE EMERGENCY APPLICATION NO FAULT NOTED. ACFT OK FOR CONTINUED SERVICE.
2010
Part: BEAM — CORRODED (FUSELAGE) · airframe 17,047 hrs · 8,166 cycles
RT Z BEAM AT FRAME 68-69 HAS CORROSION. REMOVED RT Z BEAM, FRAME 68-69 IAW SRM 51-72-11. INSTALLED NEW RT Z BEAM, FRAME 68-69 IAW SRM 51-72-11. PRIMED AND PAINTED ATTACH POINTS OF NEW BEAM IAW SRM 51-75-12.
Part: BEAM — CORRODED (FUSELAGE) · airframe 17,047 hrs · 8,166 cycles
RT Z BEAM AT FRAME 67-68 HAS CORROSION. REMOVED RT Z BEAM, FRAME 67-68 IAW SRM 51-72-11. INSTALLED NEW RT Z BEAM, FRAME 67-68 IAW SRM 51-72-11. PRIMED AND PAINTED ATTACH POINTS OF NEW BEAM - IAW SRM 51-75-12.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 17,047 hrs · 8,166 cycles
FLOORBEAM AT +Y765, FRAME 67-70 HAS CORROSION. REMOVED FLOORBEAM +Y765, FRAME 67-70 IAW SRM 51-72-11. INSTALLED NEW FLOORBEAM +Y765, FRAME 67-70 IAW SRM 51-72-11. PRIMED AND PAINTED ATTACH PINTS OF NEW BEAM IAW SRM 51-75-12.
Part: FLOORBEAM — CORRODED (CABIN) · airframe 1 hrs · 8,166 cycles
FLOORBEAM -Y765, FRAME 66-70 HAS CORROSION. REMOVED FLOORBEAM -Y765, 66-70 IAW A319 SRM 51-72-11. INSTALLED NEW FLOORBEAM IAW SRM 51-72-11. PRIMED AND PAINTED ATTACH POINTS OF NEW BEAM IAW SRM 51-75-12.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 17,047 hrs · 8,166 cycles
FLOOR PANEL 262FF CORRODED. INSTALLED NEW SERVICABLE FLOOR PANEL 262FF IAW AMM 53-42-12-400-002 & AMM 53-42-12-000-002.
Part: BEAM — CORRODED (FUSELAGE) · airframe 17,047 hrs · 8,166 cycles
Z BEAM, LT AT FRAME 68-69 HAS CORROSION. REMOVED LT Z BEAM, 68-69 IAW SRM 51-72-11, 82110. INSTALLED NEW LT Z BEAM, 68-69 IAW SRM 82110. PRIMED AND PAINTED ATTACH POINTS OF NEW BEAM IAW SRM 51-75-12 82095.
Part: FLOORBEAM — CORRODED (CABIN) · airframe 17,047 hrs · 8,166 cycles
FLOORBEAM Y240 FROM FRAME 68-70 HAS CORROSION. REMOVED FLOORBEAM Y240, FRAME 68-70 IAW SRM 51-72-11. INSTALLED FLOORBEAM Y240 IAW SRM 51-72-11. PRIMED AND PAINTED ATTACH POINTS OF NEW BEAM IAW SRM 51-75-12.
Part: ACTUATOR — BINDING (RAM AIR DOOR) · airframe 15,914 hrs · 7,582 cycles
DURING CLIMB PACK 1 OVERHEAT AND PACK 2 FAULT. REPLACED PACK 1 TEMP SENSOR AND LT RAM AIR DOOR INLET ACTUATOR.
2009
Part: COMPUTER — ODOR (ELAC) · airframe 13,442 hrs · 6,442 cycles
ELAC 1 FAILED AND STRONG ODOR OF ELEC BURNING, IDENTIFIED AS ELAC 1.
2008
Part: HORN — NO TEST (SMOKE DETECTION) · airframe 6,476 hrs · 3,178 cycles
MECH CALL HORN FAILED TO COME ON DURING AVX COMPARTMENT SMOKE DETECTION TEST. REPLACED HORN 15WC AND RELAY 4WC. OPS CHECK GOOD.
2007
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 5,083 hrs · 2,521 cycles
FLOORBEAM CORROSION, 6" AFT OF FRAME 67 AT Y765. REPAIRED DAMAGED AREA.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 5,083 hrs · 2,521 cycles
FLOORBEAM CORROSION AT Y-1732 15" AFT OF FRAME 67. REPLACED SECTION OF FLOORBEAM.