IAE V2522-A5

Service difficulty reports · 3,460

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'V2522A5'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA2014123092871Connector · damagedEMERGENCY SYS AT33-51-38 EPSU BATTERY FWD LIGHT MSG DURING EMER LIGHT OPERATIONAL CHECK. REPLACED BATTERY IAW AMM 33-51-38-400-002-A NO HELP. REINSTALLED OLD BATTERY & REPLACED CHARGER IAW AMM 33-51-38-000-002-A NO HELP. REPLACED DECODER & ENCODER IAW AMM 2Dec 26, 2014 · N831UA · Airbus A319131 · Light System WiringSDR CALA2014123092875Battery · failed11WL EPSU BATTERY FAILED. REPLACED BATTERY IAW AMM 33-51-38.Dec 23, 2014 · N828UA · Airbus A319131 · Emergency LightingSDR CALA2014122392862Slide · defectiveEPSU EXT LOAD FWD LIGHT MSG APPEARS ON PTP PANEL AFTER EMER LIGHT TEST. REPLACED DOOR 1L SLIDE IAW AMM 25-62-44-400-006A. EMER LIGHT TESTED GOOD, NO MSGS.Dec 21, 2014 · N812UA · Airbus A319131 · Escape SlideSDR CALA2014122392863Oxygen Mask · unwanted deployO2 MASKS DROPPED ROW 32ABC. INSPECTED PAX O2 PANEL IAW MT 35-003, NO DAMAGE NOTED. REPACKED O2 COMPARTMENT & SECURED PANEL DOOR. MANUAL MASK RELEASE OPERATIONAL CHECK IAW AMM 35-23-00- 710-001 WITHIN 3 DAYS.Dec 21, 2014 · N825UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2014123092870Oxygen Mask · unwanted deployO2 MASKS DROPPED ROW 32ABC. INSPECTED PAX O2 PANEL IAW MT 35-003, NO DAMAGE NOTED. REPACKED O2 COMPARTMENT & SECURED PANEL DOOR. MANUAL MASK RELEASE OPERATIONAL CHECK IAW AMM 35-23-00- 710-001 WITHIN 3 DAYS.Dec 21, 2014 · N825UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2014122392861Hydraulic Line · leakingHYD Y ENG 2 PUMP LOW PRESS ECAM & YELLOW HYD LOW PRESS ECAM WARNINGS. OBSERVED YELLOW HYD QTY LOW. FOLLOWED QRH, SELECTED NR 2 ENG HYD PUMP OFF, PRESS & QTY STABILIZED. PERFORMED ENG RUNS, NO FAULTS ON ECAM FOUND HYD LINE IN RIGHT WW LEAKING. REPLACED LINEDec 20, 2014 · N823UA · Airbus A319131 · Hydraulic System, MainSDR CALA2014122692867O-Ring · blownSYSTEM Y HYD QTY LOST IN FLIGHT. RESERVOIR QTY DROPPED WITH NO SYS PRESS. DIVERTED & FOUND PTU O RINGS BLOWN OUT. REPLACED CHECK VLV ASSEMBLY & O RINGS FOR PTU. OPERATIONS CHECKED & LEAK GOOD. SERVICED SYS TO NORMAL.Dec 20, 2014 · N803UA · Airbus A319131 · Hydraulic System, MainSDR CALA2014122392860Battery · failedEMERGENCY BATTERY PACKS 11WL & 12WL FAIL TEST. REPLACED EPSU BATTERIES IAW AMM 33-51-38-400-002-A.Dec 19, 2014 · N810UA · Airbus A319131 · Emergency LightingSDR CALA2014122392857Fan · faultyFLIGHT ATTENDANT`S REPORTED SMOKE & BURNING SMELL. ACCOMPLISHED AMM TASK 05- 51-10-S00-801C1. DETERMINED THAT NR 2 CABIN RECIRC FAN 14HG IS AT FAULT IAW SEQ 1032003 FOR PART CHANGE.Dec 18, 2014 · N840UA · Airbus A319131 · Air Distribution FanSDR CALA2014122392851Skin · damagedLEFT WING FUEL TANK ACCESS PANEL 540K B HAS 3 EACH ELONGATED HOLES AT 4:00, 7:00 &11:00 POSITIONS. REWORKED & REPAIRED LANDING IAW ECRA 5720-02626. ACCOMPLISH INITIAL REQUIREMENTS IAW PART 2 OF ECRA BEFORE ACFT REACHES 85800T OR 4290 0C WHICHEVER COMES FIRSTDec 15, 2014 · N811UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2014122392844Door Sill · corrodedR2 DOOR SILL HAS CORROSION FRAME 66 - 68. R & R NEW DOOR SILL IAW SRM 51-42-11 PARA 5, 6, & 8.Dec 14, 2014 · N811UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014122392845Shear Plate · corrodedRIGHT AFT SHEAR PLATE HAS CORROSION. REMOVED & INSTALLED NEW SHEAR PLATE & FRAME SUPPORT IAW SRM 51-42-11 PG 7, 23, 24 & 30 - 32 & 46 - 48.Dec 14, 2014 · N811UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014122392846Door Frame · corrodedAFT FUSE R2 DOOR CUT OUT FRAME 68 AT STRINGER 23R FRAME HAS CORROSION. CUT OUT DAMAGE & INSTALLED REPAIR IAW SRM 53-41-12 FIG 202. CATEGORY B REPAIR SRI 53-41-12-2-002-00 REQUIRES FIRST INSPECTION AT 64000C AFTER ACFT DELIVERY. CURRENT 22528C, FIRST INSPECTDec 14, 2014 · N811UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2014122392843Skin Panel · damagedLEFT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATIONS IN 5 LOCATIONS. 1. 73 INCHES FROM INBD, 8 INCHES FROM TE & 3 INCHES IN DIAMETER. 2. 101 INCHES FROM INBD, 5 INCHES FROM TE & 5 INCHES IN DIAMETER. 3. 204 INCHES FROM INBD, 5.5 INCHES FROM TE & Dec 13, 2014 · N811UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2014120992799Door Sill · corrodedL2 DOOR SILL HAS CORROSION AT FRAME 68. INSTALLED REPAIR IAW SRM 53-41-14 FIG 201 SHEET 3 PRINCIPLE 4.Dec 8, 2014 · N811UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014120992813Light · inoperativeEMERGENCY LIGHTS FAIL MSG FOUND DURING 2 SVC CHECK. MSG READS, EPSU EXT LOAD RT. REPLACED EPSU & BATTERY FOR 12WL, NO HELP. REPLACED ALL FOUR LAMPS AT LIGHTS 60WL & 62WL. OPERATIONS CHECKED GOOD IAW AMM 33-51-15-400-0.Dec 7, 2014 · N837UA · Airbus A319131 · Emergency LightingSDR CALA2014120292758Unknown · odorDURING FLIGHT, ACFT HAS A SMELL SIMILAR TO PLASTIC MELTING IN OVEN. SEEMS TO WORSEN WITH POWER INCREASE. PERFORMED NR 2 ENG WASH. REPLACED LT & RT RECIRCULATION FILTERS. PERFORMED HIGH POWER ENG RUN TO BURN OUT SMELL IAW JRH-2-40-35. NO ODOR AT THIS TIME.Nov 29, 2014 · N818UA · Airbus A319131 · Air Distribution SystemSDR CALA2014120292754Battery · dischargedEMERGENCY LIGHT TEST FAILED ON 2 SVC. REPLACED FWD BATTERY. OPERATIONS CHECKED GOOD IAW MM 33-51-00.Nov 27, 2014 · N841UA · Airbus A319131 · Emergency LightingSDR CALA2014111492700Connector · not seatedEMERGENCY LIGHT TEST FAILED IAW NR 2 SVC. EPSU BATTERY EMER LT. RESEATED CONNECTOR ON LT MID EMER POWER SUPPLY IAW AMM 33-51-11 TEST PASSED.Nov 13, 2014 · N834UA · Airbus A319131 · Light System WiringSDR CALA2014111092675Contact · dirtyEMERGENCY LIGHT TEST FAILED ON 2 SVC. REMOVED & CLEANED BATTERY CONTACTS IAW MM 33-51-00. OPERATIONS CHECKED GOOD.Nov 9, 2014 · N822UA · Airbus A319131 · Emergency LightingSDR CALA2014102992625Chiller · malfunctionedREPORT OF EXHAUST SMELL NEAR FWD AFT LAVATORY, AFT GALLEY AREA. FOUND AFT GALLEY FWD CHILLER BLUE POWER LIGHT FLASHING, WITH LITTLE OR NO AIRFLOW FROM CHILLER. UNIT SHUTS OFF & RESTARTS. REPLACED AFT GALLEY FWD CHILLER, CLEANED FILTER. NO SMELL AFTER REPLAOct 28, 2014 · N835UA · Airbus A319131 · Buffet/GalleysSDR CALA2014102992624Mount · corrodedRIGHT PYLON ENG MOUNT HAS SURFACE CORROSION. PERFORMED ECRA 5450-02273 NO DEFAULTS FOUND. OK TO CONTINUE.Oct 27, 2014 · N803UA · Airbus A319131 · Engine Mount SectionSDR CALA2014102392556Fairing · looseAIRFRAME VIBRATION ONCE AIRBORNE, EMER DECLARED, RETURNED. SECURED & APPLIED TAPE TO FILLET FAIRING ON LT SIDE OF FUSELAGE. COMPLETED INSPECTION OF FUSELAGE, NO DEFECTS FOUND.Oct 22, 2014 · N824UA · Airbus A319131 · Aerodynamic FairingsSDR CALA2014101692456Battery · dischargedEMERGENCY LIGHT OPERATIONAL TEST FAILED. EPSU BATTERY AFT LT DISPLAYED AFTER TEST. RESET AFT LT EPSU BATTERY. TESTED GOOD.Oct 12, 2014 · N814UA · Airbus A319131 · Emergency LightingSDR CALA2014121692830Oxygen Bottle · unserviceableAFT CABIN LT SIDE BEHIND LAST ROW OF SEATS HAVE BOTH PORTABLE O2 BOTTLE CANNULA TIGHTLY TIE WRAPPED TO BOTTLES RENDERING BOTTLES USELESS. REMOVED TIE WRAPS FROM BOTH BOTTLES & REPLACED UPPER BOTTLE.Oct 12, 2014 · N809UA · Airbus A319131 · Portable Oxygen SystemSDR CALA2014101692434Slide · defectiveEMERGENCY LIGHTS TEST FAILS WITH MSG EPSU EXT LOAD FWD L. R & R DOOR 1R ESCAPE SLIDE PACK IAW AMM 25-62-44. EMER LIGHTS TESTED OK.Oct 10, 2014 · N812UA · Airbus A319131 · Escape SlideSDR CALA2014101392396Flap · dentedDENT IN RT INBD FLAP NEAR FUSELAGE. DAMAGE WITHIN ALLOWABLE LIMITS IAW SRM 57-52-00 PAR 8. AREA FREE FROM CRACKS IAW NDT IAW NT M51-10-08.Oct 9, 2014 · N845UA · Airbus A319131 · Trailing Edge FlapsSDR CALA2014101392394Slat · dentedNUMBER 2 LT SLAT HAS DENT AT INBD END THAT IS OUT OF LIMITS. DAMAGE REMOVED & DOUBLER REPAIR INSTALLED IAW SRM 57-40-00. HFEC IAW NTM 51-10-08 PB6.Oct 8, 2014 · N835UA · Airbus A319131 · Leading Edge DevicesSDR CALA2014100792374Door Sill · corrodedR2 DOOR SILL HAS CORROSION AT NUTPLATE HOLES AT AFT INBD END. REMOVED CORROSION & FOUND BEYOND SRM ALLOWABLE LIMITS. REPAIR AT R2 DOOR SILL IAW SRM 53-41-14 FIG 201 SHEET 3, REPAIR PRINCIPLE 4.Oct 5, 2014 · N835UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014100792375Door Sill · corrodedR2 DOOR SILL HAS CORROSION, AFT SIDE FRAME 68 STRINGER 23R. AFTER BLENDING FOUND BEYOND SRM ALLOWABLE LIMITS. R & R FILLER IAW SRM 51-41-14 FIG 201 PARA 5 A PRINCIPLE 5.Oct 5, 2014 · N834UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014092992321Actuator · failedNR 1 ENGINE EGT OVERLIMIT DURING TAKEOFF. FAULTED 2.5 BLEED ACTUATOR. EXCEEDANCE RECORDED WAS 640 FOR 8 SECONDS. REPLACED 2.5 BLEED ACTUATOR IAW AMM 75-31-42-400-010-B13Oct 2, 2014 · N816UA · Airbus A319131 · Engine Bleed Air SystemSDR CALA2014100792367Battery · not seatedEMERGENCY LIGHT TEST FAILED ON 2 SVC. RESEATED EPSU BATTERY IN AFT CABIN IAW AMM 33-51-38. EMER LIGHT TEST PASSED.Oct 2, 2014 · N808UA · Airbus A319131 · Emergency LightingSDR CALA2014091892245Skin · saturatedLEFT ELEVATOR UPPER SURFACE HAS WATER INGRESS AT THREE EACH LOCATIONS IN ZONE 3. REMOVED DAMAGE & REPAIRED IAW SRM 55-21-11 PARA 5 E FIG 205. REPAIR REQUIRES SRI INSPECTIONS IAW SRI 55-21-11-2-002-00 PARA 3 - B TABLE 203. FIRST INSPECTION DUE AT 48000FC & 6Sep 16, 2014 · N854UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2014091892234Door Sill · corrodedL2 DOOR SILL CORRODED BETWEEN STRINGER 22L & 23L AT FRAME 68. BLENDED CORROSION AT FRAME 68 ON L2 DOOR SILL BEAM IAW SRM 51-41-14 FIG 101. AFTER REMOVAL FOUND OUT OF LIMITS IAW SRM. R & R L2 DOOR SILL BEAM IAW SRM 51-72--11 PG 6 D & SRM 51-42-11 PARA 6 & 7.Sep 13, 2014 · N854UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014091892235Attach Fitting · corrodedFORWARD CARGO BILGE BELLY FAIRING ATTACH HAS CORROSION AROUND RIVETS ON SKIN FRAME 30 - 31 STRINGER 42L. CORROSION REMOVED IAW SRM 53-21-11DIAGRAM 105 PARA 4 E.Sep 13, 2014 · N854UA · Airbus A319131 · Aerodynamic FairingsSDR CALA2014091292110Battery · dischargedRIGHT EMER BATTERY MSG ON PTT PANEL DURING EMER SYS LIGHT TEST. REPLACED EMER BATTERY, RESET CIDS & LIGHT TESTED OK.Sep 10, 2014 · N829UA · Airbus A319131 · Emergency LightingSDR CALA2014091292107Door Sill · corrodedR2 DOOR SILL HAS CORROSION FRAME 66 - 68 STRINGER 22R - 23R. DOOR SILL REPLACED IAW SRM 51- 42-11.Sep 9, 2014 · N854UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014090992094Battery · not seatedEMERGENCY LIGHT TEST FAILED ON 2 SVC. RESEATED EPSU BATTERY AT AFT LT IAW AMM 33-51-38, EMER LIGHT TEST NOW PASSES.Sep 6, 2014 · N813UA · Airbus A319131 · Emergency LightingSDR CALA2014090392050Battery · dischargedDURING SERVICE CHECK OF EMER LIGHTS FOUND EPSU FWD L DISPLAYED ON FWD FLIGHT ATTENDANT PANEL. REPLACED THE EPSU & BATTERY ON 10WL IAW MM 33-51-38-401.Aug 30, 2014 · N846UA · Airbus A319131 · Emergency LightingSDR CALA2014090392052Epsu · malfunctionedEMERGENCY LIGHTS TEST FAILS NO GREEN LIGHT & MSG EPSU BATTERY EMER R. RESET EPSU & SYS BITE CHECKED GOOD IAW MM 33-51-38 & EMER LIGHT TEST PASSED.Aug 30, 2014 · N804UA · Airbus A319131 · Emergency LightingSDR CALA2014090392053Epsu · faultyEMERGENCY LIGHTS TEST FAILS NO GREEN LIGHT & MSG EPSU UNIT FWD L. REPLACED EPSU & BATTERY IAW MM 33-51-38. SYS BITE TESTS GOOD & EMER LIGHT TEST PASSED.Aug 30, 2014 · N804UA · Airbus A319131 · Emergency LightingSDR CALA2014082692028Door Sill · corrodedR1 DOOR SILL BEAM WAS CORRODED AROUND THE FWD & AFT GIRT BAR FITTING HOLES & AROUND THE FWD DRAIN HOLE. CORROSION WAS REMOVED & AREA BLENDED AROUND THE DRAIN HOLE. FWD GIRT BAR FITTING AFT OTBD HOLE & ALL 4 HOLES AT THE AFT GIRT BAR FITTING WERE SPOT FACED & Aug 24, 2014 · N855UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014082692029Door Sill · corrodedL1 DOOR SILL BEAM WAS CORRODED AROUND THE FWD GIRT BAR FITTING AFT INBD ATTACH HOLE & THE AFT FITTING AFT INBD & OTBD ATTACH HOLES. HOLES WERE SPOT FACED & REPAIR WASHERS INSTALLED IAW SRM 53-11-14 PARA 4 E FIG 108. MINIMUM MATERIAL THICKNESS AT SPOT FACES IAug 24, 2014 · N855UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014082692025Door Sill · corroded2R DOOR SILL CORRODED UNDER THE GIRT BAR PLATES. DOOR SILL REPLACED IAW SRM 51-42-11 & SRM 51-44-11.Aug 23, 2014 · N855UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014082592014Door Sill · corrodedR2 DOOR SILL & AFT CORNER FITTING CORRODED BETWEEN FRAME 66 & 68. DOOR SILL & AFT CORNER FITTING R & R IAW SRM 51-42-11.Aug 21, 2014 · N855UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014082192002Skin · dentedDENT REPORTED BY FLIGHT CREW & CATERING AFT OF DOOR 2L. FUSELAGE DENTED BETWEEN FRAME 69 & 70 AT STRINGER 21. DENT ABOVE STRINGER IS .040 INCHES DEEP, .23 INCHES FROM NEAREST RIVET ROW, 2.66 INCHES X 1.24 TOTAL AREA. DENT BELOW STRINGER IS 3 X 1.25, .010 IAug 20, 2014 · N855UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2014082192005Epsu · inoperativeNUMEROUS EMER ESCAPE PATH LIGHTS INOPERATIVE THROUGHOUT CABIN DURING HMV TEST. R & R EPSU 10WL IAW AMM 33-5 1-38-000-001-A & 33-51-38-400-001-A. R & R BATTERY PACK 13WL IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A, EEPL LIGHTS OPERATIONS CHECKED GOOD IAW Aug 20, 2014 · N852UA · Airbus A319131 · Emergency LightingSDR CALA2014081891999Battery · dischargedFAILED EMER LIGHT TEST FWD FLIGHT ATTENDANT PANEL. EPSU BATTERY EMER LIGHT REPLACED BOTH LT & AFT LT BATTERIES AMM 33-51. TEST NOW OK.Aug 18, 2014 · N814UA · Airbus A319131 · Emergency LightingSDR CALA2014081891997Door Sill · corrodedL2 DOOR SILL HAS SPOTS OF CORROSION BETWEEN FRAME 66 & 68. BLENDED CORROSION, AFTER BLENDING ALL AREAS WERE WITHIN LIMITS EXCEPT FOR NUTPLATE AT INBD FLANGE ON FRAME 68 IAW SRM 53-41-14 FIG 101.Aug 17, 2014 · N855UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014081891995Stringer · corrodedCORROSION FOUND ON STRINGER 42R AT FRAME 60 IN AFT PIT. UPON FURTHER EVALUATION FOUND STRINGER 42R CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF STRINGER & SPLICED IN NEW SECTION OF STRINGER BETWEEN FRAME 59.5 & 60.5 IAW SRM 53-00-13 FIG 201.Aug 15, 2014 · N852UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
Back to IAE V2522-A5