IAE V2527-A5
Service difficulty reports · 8,009
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 = 'V2527A5' 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.
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 = 'V2527A5' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA2014081191934Light · malfunctionedRIGHT SIDE FLIGHT DECK DOME LIGHT INOPERATIVE ON BATTERY POWER. CYCLED SIDES 1 & 2, ACP LIGHT TESTED OK.SDR CALA2014080691739Warning System · false activationAT GATE WITH NO ENGS RUNNING. ENG 2 FAIL ECAM. ACCOMPLISHED TSM 73-00-00 -810-856-A NO HELP. CHECKED FDEC 2A & 2B GND REPORTS & SELF-TEST BOTH TESTS NORMAL WITH NO FAULTS. CYCLED NR 2 ENG FIRE SWITCH, NO HELP. DEPOWERED ACFT & REPOWERED, MSG CLEARED. RANSDR CALA2014080691740Slide · faultedEPSU 10WL DOOR 1R FAILED WITH EXTERIOR LIGHTS FAULT. REPLACED SLIDE ASSEMBLY DUE TO EXTERNAL LOAD FAULT DOOR 1R IAW 25-62-44.SDR YENA20140729143Fmu · failedCREW DECLARED AN EMERGENCY AND ACFT RETURN TO DEPARTURE. ENG 1 STALL, ECAM & LOSS OF THRUST CLIMBING 12000/300KTS. ENG 1 DECREASED TO IDLE THRUST: EGT 440 N2-59 PERCENT, EPPR .927 EF 700 N1-25 PERCENT THRUST DID NOT INCREASE WITH THROTTLE ADVANCEMENT, GEN 1 SDR CALA2014080191585Engine · making metalMETAL FOUND IN TAIL PIPE AFTER ENG 2 HAD 3 SELF-RECOVERING STALLS IN CRUISE. REPLACED NR 2 ENG IAW MT 71-017. ENG RUNS & OPERATIONS CHECKED.SDR CALA2014072891554Door Frame · corrodedRIGHT FWD EMER EXIT FOUND CORROSION OUT OF LIMITS INTERNAL DOOR FRAME LOWER BAYS. R & R PN D5227902820600, D5227905420400 & D5227902820451 IAW SRM 51-4 2-11. NO FURTHER INSPECTIONS REQUIRED AT THIS TIME.SDR SOKF20140730005Servo Control · damagedVIBRATION AFTER TAKEOFF & CLIMB IAW TSM 05-50-00-810-802-A. PERFORMED CHECK OF THE LOAD REPORT PARAMETER AFTER HARD & OVERWEIGHT LANDING IAW AMM 31-37-00-200-001-A & NO OVERWEIGHT LANDING CONDITION WAS FOUND. CHECKED OK IAW TSM 05-50-00-810-801-A & TSM 27-2SDR CALA2014072891548Skin · damagedMLG DOOR HINGE FITTINGS LT & RT WERE REMOVED TO FIND SEVERAL ELONGATED HOLES AT MATING SURFACE OF HINGE FITTING & KEEL BEAM BOTTOM SKIN. REPAIRED BOTH LT & RT BOTTOM KEEL BEAM SKINS AT HINGE FITTING SURFACES IAW ECRA 5336-01 017. NO DEVIATIONS, NO FURTHER ACSDR CALA2014072891549Door · corrodedRIGHT AFT EMER EXIT OVERWING DOOR CORROSION FOUND ON STRUCTURE LOWER 3 BAYS. R & R PN D5227902820451, D5227902820600 & D5227905420400. NO FURTHER ACTION NECESSARY.SDR CALA2014072891550Structure · corrodedLEFT AFT EMER EXIT OVERWING DOOR FOUND CORROSION ON STRUCTURE LOWER BAYS. R & R PN`S D52279055203, D5227905204 & D52279055202 IAW SRM 51-42-11. NO FURTHER ACTION NECESSARY.SDR CALA2014072891551Structure · corrodedLEFT FWD EMER OVERWING DOOR STRUCTURE FOUND CORROSION IN BOTTOM 3 BAYS. R & R PN`S D52279028206, D52279028204, D52279054202 & D52279055200 IAW SRM 51-42-11. NO FURTHER ACTION NECESSARY.SDR CALA2014072891552Skin · corrodedADF ANTENNA CUT OUT FOUND CORRODED FUSELAGE FRAME 44 - 45 STRINGER 1L - 1R. REMOVED CORROSION FROM UPPER SKIN SURFACE NEAR ADF CUT OUT.\O-T\0.087. DEPTH OF REMOVED MATERIAL =.077\W=2.5\ SRM 53-31-11 PARAGRAPH 3 TABLE 101 PARAGRAPH 4 A NOTE 1 DIAGRAM 101. ACSDR CALA2014072891553Stringer · corrodedCORROSION FOUND INTERNAL BILGE FRAME 31 - 32 STRINGER 41R. MORE THAN 50% MATERIAL LOSS. CORROSION REMOVED & INSTALLED REPAIR IAW SRM 53-21-13 TABLE 202 PARAGRAPH 5 A FIG 202 SHEETS 2-4. REINSPECT AT 60000 PTC IAW SRI 53-21-13-2-002-00. REPAIR APPLIED TO STSDR CALA2014072591513Door Sill · corrodedMAJOR REPAIR. R2 DOOR SILL AFT END CORRODED. BLENDED CORROSION ON AFT END OF DOOR SILL. AFTER BLENDING AFT SECTION MEASURED 0.030 & FWD SECTION MEASURED 0.042. ORIGINAL THICKNESS = 0.070. MAX MATERIAL LOSS ALLOWED =0.017. R & R RT 2 DOOR SILL.SDR CALA2014072591515Stringer · corrodedMAJOR REPAIR. STRINGER 42L CORROSION REPAIR ACCOMPLISHED BETWEEN FRAME 57 - 59. STRINGER SPLICE REPAIR REQUIRES INSPECTION AT 60,000 FLIGHT CYCLES AFTER REPAIR EMBODIMENT. DAMAGE WAS REMOVED & NDT ACCOMPLISHED IAW NTM51 -10-08. NO CRACKS FOUND. THE REPAISDR CALA2014072291502Cleat · corrodedFORWARD PIT CLEAT CORRODED AT BETWEEN FRAMES 27 & 28 AT STRINGER 38L. REPLACED CLEAT IAW SRM 51-42-11 PAGE 23 & 24.SDR CALA2014072291503Door · gougedMAJOR REPAIR. AFT AVIONICS COMPARTMENT DOOR HANDLE CUT OUT GOUGED ADJACENT TO HANDLE RELEASE PUSH BUTTON. BLENDED MINOR DAMAGE. DIMENSIONS AFTER BLENDING ARE AS FOLLOWS. E=.3 D=.159 E BY D =1.886 > 1.5. WITHIN LIMITS IAW SRM 52-41-00 FIG 101 SH 2. THIS RESDR CALA2014072291504Door · gougedMAJOR REPAIR. LEFT LATERAL AVIONICS COMPARTMENT DOOR HANDLE CUT OUT GOUGED ADJACENT TO HANDLE RELEASE PUSH BUTTON. REPAIRED MINOR GOUGE. AFTER BLENDING DIMENSIONS ARE AS FOLLOWS. E=.4 D = .159 E BY D = 2.515 > 1.5. WITHIN LIMITS IAW SRM 52-41-00 FIG 101 SHSDR CALA2014072291505Door · gougedMAJOR REPAIR. RT LATERAL AVIONICS COMPARTMENT DOOR GOUGED AT HANDLE CUT OUT ADJACENT TO RELEASE PUSH BUTTON. BLENDED MINOR DAMAGE. DIMENSIONS AFTER BLENDING ARE AS FOLLOWS E=.4 D=.159 E BY D= 2.515 >1.5. WITHIN LIMITS IAW SRM 52-41-00 FIG 101 SH 2. THIS RSDR CALA2014072291501Door · gougedMAJOR REPAIR. FWD AVIONICS COMPARTMENT DOOR HAS GOUGE AT HANDLE CUT OUT ADJACENT TO PUSH RELEASE BUTTON. REWORKED DAMAGED AREA & REMOVED DAMAGE IAW SRM 52-41-00 PG 107 FIG 101 SH 2. REWORKED AREA IS IN ZONE 1 E BY D =2.51 > 1.5. HFEC REVEALED NO CRACKS. MASDR CALA2014072191479Power Supply · inoperativeLEFT EPSU FAILED EMER LIGHT TEST. FOUND PSU INOPERATIVE. REPLACED IAW AMM 33-50-51, GND CHECKED NORMAL.SDR CALA2014072191480Battery · dischargedAFT EPSU FAIL EMER LIGHT TEST FOUND BATTERY WOULD NOT STAY CHARGED. REPLACED BATTERY AMM 33-51-38, GND CHECKED NORMAL.SDR CALA2014072291497Shear Tie · corrodedFORWARD PIT FRAME 30 SHEAR TIES CORRODED. REPLACED SHEAR TIES AT FRAME 30 STRINGER 44 LT & 44 RT IAW SRM 57-42-11 PG 29.SDR CALA2014072291498Shear Tie · corrodedFORWARD CARGO HAS CORRODED SHEAR TIE AT FRAME 32. REPLACED SHEAR TIE AT FRAME 32 STRINGER 42 RT.SDR CALA2014072291499Shear Tie · corrodedFORWARD CARGO COMPARTMENT SHEAR TIE CORRODED AT FRAME 33. REPLACED CLEAT AT FRAME 33 STRINGER 40 RT.SDR CALA2014072291500Stringer Splice · corrodedFORWARD CARGO HAS CORRODED STRINGER SPLICES AT FRAME 31 - 30 STRINGER 41L - 42R. REPLACED STRINGER SPLICES AT FRAME 30 - 31 STRINGER 41 LT - 42 RT.SDR CALA2014071591474Beam · corrodedDOOR 2L SILL BEAM CORRODED AT FASTENER HOLES FOR FWD GIRT BAR FITTING. REMOVED CORROSION & INSTALLED REPAIR IAW SRM 53-41-14 FIG 201. THIS IS A CATEGORY A REPAIR.SDR CALA2014071591475Door Sill · corrodedL1 DOOR SILL SHOWS EVIDENCE OF CORROSION AT FWD & AFT GIRT FITTING HARD MOUNTS. QTY 2 FWD & QTY 1 AFT. DAMAGE FOUND WITHIN ALLOWABLE REWORK LIMITS IAW SRM 53 -11-14 PARA 3 TABLE 101. REWORK ACCOMPLISHED IAW SRM 53-11-14 PARA 4 E FIG 108 SHEETS 1 - 5. FIRSTSDR CALA2014071591476Door Sill · corrodedR1 DOOR SILL SHOWS EVIDENCE OF CORROSION AT GIRT BAR FITTING HARD MOUNTS. FWD QTY 4 & AFT QTY 2. DAMAGE FOUND WITHIN ALLOWABLE RE-WORK LIMITS IAW SRM 53-11-14 PARA 3 TABLE 101. RE-WORK ACCOMPLISHED IAW SRM 53-11-14 PARA 4 E FIG 108 SHEETS 1 - 5. FIRST REQUSDR CALA2014071591465Skin · damagedDOUBLER REPAIR ACCOMPLISHED ON EXTERNAL FUSELAGE SKIN JUST AFT OF FRAME 1 & AT Y-330 RT. ORIGINAL SKIN THICKNESS 0.055INCHES. REPAIR ACCOMPLISHED IAW SRM 53-00-11 TBL 203 PARA 4 W FIG 239. REPAIR REQUIRES INSPECTION IAW SRI 53-00-11-2-017-00 PARA 3 L TBL 22SDR CALA2014071591466Spar · wornNUMBER 2 PYLON LOWER SPAR HAD WEAR SPOT FROM CONTACT WITH THE CNA AT RIB 5. THE BLEND OUT IS .003 INCHES DEEP & 0.100 INCHES WIDE. AN ANTI-CHAFE PLATE WAS INSTALLED IAW SRM 54-51-12 PARA 5 B FIG 202. REQUIRES RE-INSPECTION IAW SRI 54-51-12-2-001-00 PARA 3 ASDR CALA2014071591467Spar · wornNUMBER 1 PYLON LOWER SPAR HAD WEAR SPOT FROM CONTACT WITH THE CNA AT RIB 5. THE BLEND OUT IS .019 INCHES DEEP & 0.400 INCHES WIDE. AN ANTI-CHAFE PLATE WAS INSTALLED IAW SRM 54-51-12 PARA 5 B FIG 202. REQUIRES RE-INSPECTION IAW SRI 54-51-12-2-001-00 PARA 3 ASDR CALA2014071591462Stringer Splice · corrodedSTRINGER 41R SPLICE PLATE CORRODED AT FRAME 58. R & R STRINGER SPLICE PLATES.SDR CALA2014071591463Stringer · corrodedSTRINGER FOUND CORRODED BETWEEN FRAME 58 & 60. STRINGER SECTION REPLACED FROM FRAME 58 TO 64.SDR CALA2014071191442Computer · malfunctionedFMGC NR 1 INOPERATIVE. R & R NR 1 FMGC IAW MM 22-83-34-000-001-A & 22-83-34-400-001-G. PERFORMED OPERATIONS TEST OF LAND CAT III CAPABILITIES IAW 22-97-00-710-001-A. LAND TEST PASSED, ACFT REMAINS FULLY CAT CAPABLE.SDR CALA2014071191444Beam · crackedLEFT MLG WW SIDE BOX BEAM FLANGE CRACKED AFT SIDE OF FASTENER, JUST FWD OF FRAME 43. REPAIRED THE CRACK ON LT WW SIDE BOX BEAM FLANGE JUST FWD OF FRAME 43 IAW ECRA 5330-04874. NO SRI INSPECTION REQUIRED IAW ECRA.SDR CALA2014071191445Structure · crackedRIGHT WW SIDE BOX FLANGE CRACKED AFT SIDE OF FASTENER JUST FWD OF FRAME 43. REPAIRED RT WW SIDE BOX FLANGE CRACK IAW ECRA 5330-04874. NO SRI INSPECTION IS REQUIRED IAW ECRA.SDR CALA2014071191446Control System · malfunctionedHOT AIR FAULT DISPLAYED ON UPPER ECAM SCREEN. RESET PACK CONTROL SYS 1 & 2 PACKS, FAULT CLEARED.SDR CALA2014071191448Mechanism · lack of lubeON TAXI, ENG 1 EGT BEGAN PULSING AMBER THEN RED. EGT OBSERVED AT 642, SHUTDOWN ENG, DURATION WAS 10 SECONDS. FOLLOWED FAILURE MSG IAW AMM75-32-42. LUBRICATED THE VSV MECHANISM IAW AMM75-32-42-640 -010. ALSO REPLACED THE HP COMPRESSOR SOLENOID VLV 7A IAW 75SDR CALA2014071191443Bonding Strap · damagedBOTH LT & RT WING FUEL TANKS ALL ELEC BONDING CABLES SHOWS SIGNS OF AGEING & BRITTLENESS. ACCOMPLISHED LT WING FUEL TANK ALL BONDING WIRE REPLACEMENT.SDR CALA2014071191447Stringer · corrodedAFT CARGO COMPARTMENT BILGE AREA FRAME 60 - 64 RT HAS CORROSION. AFT CARGO STRINGER 42R CORRODED BEYOND LIMITS. FRAME 60 - 64 REPAIRED BY SPLICING IN NEW STRINGER SECTION SRM 53-00-13 FIG 202. THIS SRM REFERS TO SRI 53-00-13 TBL 205 PG 205. RE-INSP AT 6000SDR CALA2014071191422Access Panel · gougedLEFT WING FUEL PANEL 540MB HAS TWO EACH GOUGED FASTENER S HOLES. REAMED TWO EACH HOLES ON PANEL 540MB, COLD WORKED HOLES & REAMED. FABRICATED TWO BUSHINGS & INSTALLED ON PANEL. BRIDGE PLATE INSTALLED WET IAW SRM 57-21-11 PARA 5 B FIG 202. PANEL REQUIRES RESDR CALA2014071191423Stringer · corrodedAFT CARGO COMPARTMENT BILGE AREA STRINGER FRAME 61 - 64 STRINGER 40 RT HAS CORROSION. OUT OF LIMITS REPAIR EXTENDS PASSED 2 BAYS IAW SRM 53 -41-13 & 53-00-13 FIG 202 SHEET 2. REMOVED DAMAGED STRINGER 40 FRAME 61 - 64 APPROX 51.25 INCHES SRM53-00-13 FIG 202. SDR CALA2014071191424Stringer · corrodedAFT CARGO STRINGER 39 RT CORROSION ON OUTER FLANGE BETWEEN FRAME 62 - 63 & STRINGER 39. REMOVED CORROSION STRINGER 39 AFT CARGO FRAME 62 - 63 IAW SRM 53-00-13 FIG 202. HFEC ACCOMPLISHED NO CRACKS NOTED IAW NTM 51-10-04. INSTALLED REPAIR IAW SRM53-00-13 FIG SDR CALA2014071191426Warning Light · illuminatedCOCKPIT DOOR FAULT LIGHT & DOOR CONTROLLER TOP STRIKE OR LOWER STRIKE LIGHT IS ON. LOWER STRIKE LIGHT ON RESET COCKPIT DOOR CB & PERFORMED OPERATIONAL TEST IAW AMM 52-51-00. OPERATIONS CHECKED OK.SDR CALA2014071191413Ils System · faultedILS 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ACCOMPLISHED CHRONIC REVIEW. ACCOMPLISHED MT 34-001. OPERATIONS CHECKED GOOD.SDR CALA2014071191417Stringer · corrodedAFT CARGO JUST AFT OF FRAME 56 STRINGER 40 CORROSION STRINGER. REMOVED DAMAGED SECTION OF STRINGER 40L & FRAME 56. FABRICATED & INSTALLED STRINGER SPLICE REPAIR. REPAIR HAS SRI AT 60000 FC & 7500 WITH SUBSEQUENT INSP & METHOD TBD.SDR CALA2014071191418Stringer · corrodedSTRINGERS 41L & 42L CORRODED IN AFT CARGO COMPARTMENT BETWEEN FRAME 63 & 64. REMOVED CORRODED SECTIONS OF STRINGERS & REPLACED WITH NEW STRINGERS. FABRICATED NEW STRINGER SPLICES & INSTALLED. REPAIR REQUIRES RE-INSPECTION. FIRST INSPECTION DUE AT 60000FC ASDR CALA2014071191419Stringer · corrodedSTRINGER 42L CORRODED IN AFT PIT AFT OF FRAME 56. REMOVED CORRODED SECTION OF STRINGER & REPLACED WITH A NEW STRINGER. FABRICATED NEW STRINGER SPLICE & INSTALLED. REPAIR REQUIRES SRI INSPECTION. FIRST INSPECTION DUE AT 60000FC & 75000FH AFTER REPAIR EMBODIMSDR CALA2014071191420Fitting · crackedFRAME 43 WING BAY CORD, TORSION BOX & MLG FREE FALL BRACKET AFT HOLE HAS A CRACK RT SIDE. R & R LT & RT REINFORCEMENT FITTINGS TORSION BOX LOWER SIDE SHELL.
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