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 CALA2014042590894Skin · corrodedFORWARD PIT FWD FRAME 34 BETWEEN STRINGER 43R & 42R HAS CORROSION AROUND FASTENERS ON INNER SURFACE OF SKIN. REMOVED .014 OF.071 SKIN IAW SRM 53-21-11 FIG 114 SHEET 1 P149. REMOVED LESS THAN 25% & FOUND TO BE IN LIMIT.SDR CALA2014042590895Skin · corrodedFORWARD PIT FWD FRAME 34 BETWEEN STRINGERS 42L & 40L, CORROSION AROUND FASTENERS ON INNER SURFACE OF SKIN. REMOVED .012 OF.071 SKIN IAW SRM 53-21-11 FIG 114 SHEET 1 P149, REMOVED LESS THAN 25% & FOUND TO BE IN LIMIT.SDR CALA2014042590896Skin · corrodedFORWARD PIT FWD FRAME 34 BETWEEN STRINGERS 42R & 41R HAS CORROSION AROUND FASTENERS ON INNER SURFACE OF SKIN. REMOVED .011 OF .091 SKIN IAW SRM 53-21-11 FIG 114 SHEET 1 P149. REMOVED LESS THAN 25% & FOUND TO BE IN LIMIT.SDR CALA2014042590897Seal · wornNR 2 PYLON BOTTOM METAL SEAL WORN. REMOVED WORN CHAFE STRIP & STRAP. MATERIAL LOSS <.002 ON LOWER SPAR. NR 2 PYLON LOWER SPAR REPAIRED WITH EXTENDED CHAFE PLATE.SDR CALA2014042590898Seal · wornNR 1 PYLON BOTTOM METAL SEAL WORN. REMOVED STRAP & CHAFE PLATE ON LOWER SPAR. MATERIAL LOSS ON LOWER SPAR .005. BLENDED CHAFE MARK SMOOTH. HFEC IAW NTM 51-10-20 PB6 NO CRACKS. FABRICATED EXTENDED ANTI-CHAFING PLATE IAW SRM 54-51-12 FIG 202. INSTALLED REPSDR CALA2014042590905Landing Gear · malfunctionedCREW REPORTS NLG WILL NOT RETRACT AFTER TAKEOFF. RETURN TO FIELD, OVERWEIGHT LANDING.SDR CALA2014042190873Unknown · malfunctionedPASSENGER ADDRESS INOPERATIVE. SEVERE FEEDBACK IN REAR CABIN OVER PA. ACCOMPLISH CHRONIC REVIEW, OPERATIONS CHECKED GOOD PA FROM REAR OF CABIN.SDR CALA2014042190875Fan · failedSMOKING ELEC BURNING SMELL REPORTED BY FLIGHT ATTENDANT AT ROW 6 - 7 & 1L. CABIN FAN FAULT INDICATION ON COND AIR PAGE ON LOWER ECAM SYS PAGE. BREAKER FOR RT FAN SUPPLY POPPED. OPERATIONS CHECKED RT FAN LOUD GRINDING HEARD & BREAKER POPPED AGAIN. VERIFIED RTSDR CALA2014042190876A/C Pack · faultedMAINTENANCE STATUS MSG PACK DISPLAYED ON THE LOWER ECAM SCREEN. CREW COMMENTS, PACK 2.SDR CALA2014041790844Unknown · malfunctionedWILL NOT PASS THE EMERGENCY LIGHTS TEST. REPLACED TB 7225VT IAW AW WM 33-51-02. PERFORMED EMERGENCY LIGHT TEST, TEST PASSED.SDR CALA2014041490818Stringer · corrodedCORROSION IN AFT PIT BILGE AREA ON LOWER LT SKIN STRINGER 40L BETWEEN FRAME 56 & FRAME 58. CORROSION WAS BEYOND LIMITS IAW SRM 53-41-13 PG 101. INSTALLED STRINGER REPAIR & SPLICE ON STRINGER 41L IAW SRM 53-00-13 PG 211-212 & FIG 201.SDR CALA2014041490819Stringer · corrodedFRAME 63 - FRAME 64 & STRINGER 42L HAS CORROSION IN AFT CARGO COMPARTMENT. BLENDED CORROSION & FOUND THE AREA BEYOND LIMITS IAW SRM 51-72-11 PG 11. CUT OUT CORRODED AREA OF STRINGER & INSTALLED STRINGER REPAIR & SPLICE ON STRINGER 42L FROM FRAME 62.5 - FRAMESDR CALA2014041490820Adapter · corrodedRIGHT WING MANUAL REFUELING ADAPTER APERTURE HAS PITTING CORROSION RIB 19 - RIB 20. BLENDED THE AREA & MEASURED REMAINING THICKNESS.SDR CALA2014041490821Adapter · corrodedLEFT WING MANUAL REFUELING ADAPTER APERTURE HAS PITTING CORROSION RIB 19 - RIB 20. BLENDED CORROSION & MEASURED THE AREA.SDR CALA2014041490815Valve · failedNO WATER PRESS ON ENTIRE ACFT BUT WATER IS FULL. FOUND OVERFLOW DRAIN VLV IN THE OPEN POSITION AT FWD WATER DRAIN PANEL. NEEDS VLV REPLACEMENT, REPLACED OVERFLOW VLV IAW AMM 38-14-44, LEAK CHECKED & OPERATIONS CHECKED NORMAL. WATER PRESS OK.SDR CALA2014041490816Igniter · faultyECAM MSG APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN, APU. APU AUTO SHUTDOWN ON TWO ATTEMPTED STARTS. PLACED ON MEL 49-10B. SHOWS IGNITION & FUEL CONTROL FAULT. TROUBLE SHOT APU TO PLUGS IAW THE MX MSG. R & R APU IGNITER PLUGS IAW AMM 49-41-41.SDR CALA2014041490817Skin · dentedEXTERNAL FUSELAGE SKIN DENTED AT FRAME 61 & STRINGER 42L - 43L. MEASURED THE DENTED AREA & FOUND IT TO BE OUT OF LIMITS IAW SRM 53-41-11 DIA 103. CUT OUT DENTED AREA & INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 53-00-11 FIG 209.SDR CALA2014041490823Battery · dischargedPER A CHECK, FOUND EPSU FAULT AFT LT. REPLACED AFT LT EPSU BATTERY, OPERATIONS CHECKED GOOD.SDR CALA2014041490822Oxygen Mask · unsecurePASSENGER SEAT OVERHEAD 02 MASK FELL AT 2E & 2F. REQUIRES MASK DROP AMM35- 23-00-710-001.SDR CALA2014041090796Sill · corrodedR2 DOOR SILL IS CORRODED ON FWD GIRT BAR PLATE & AT AFT AREA. DOOR SILL WAS WORN OUT OF LIMITS IAW SRM 53-41-11. R & R R2 DOOR SILL IAW SRM 51-42-11 PGS 1, 7 & 25.SDR CALA2014040890772Wire · damagedREF 2 SVC EMERGENCY LIGHTS OPERATIONAL TEST MSG DISPLAYED WHEN TEST FAILED. ATA 33-51-38 EXT LOADS FWD L. TESTED AT EPSU, STILL FAILED. ALSO FAILED WITH TESTER CONNECTED AT EACH FWD SLIDE. RANG WIRING FROM 2871VC ON DOOR 1L TO GND & NO GND FOUND. BETWEEN SDR YENA20140407073Tube · failedDURING TAKEOFF ROLL NR 1 ENGINE LOST APPROXIMATELY 15 TO 20 PERCENT POWER. CREW CONTINUED TAKEOFF, DECLARED AN EMERGENCY AND ACFT RETURNED TO DEPARTURE. FOUND RT P4.9 PRESSURE TUBE SEVERED. R & R IAW AMM 73-22-51.SDR CALA2014040890773Skin · saturatedLEFT ELEVATOR UPPER SKIN HAS A TRAPPED WATER INDICATION 143 INCHES FROM INBD END & 17 INCHES FROM TE, 1 INCH DIAMETER. REPAIRED LT ELEVATOR UPPER SKIN AT AREA NOTED. DRILLED WITNESS HOLES & FOUND WATER. CUT OUT & REMOVED WATER, APPLIED REPAIR & RESTORED FINISDR CALA2014040890774Skin · saturatedLEFT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATION 145 INCHES FROM INBD END & 14 INCHES FROM TE, 1 INCH DIAMETER. REPAIRED LT ELEVATOR UPPER SKIN AT AREA NOTED. DRILLED WITNESS HOLES & FOUND WATER. CUT OUT & REMOVED WATER, APPLIED REPAIR & RESTOREDSDR CALA2014040890775Skin · saturatedLEFT ELEVATOR UPPER SKIN SURFACE HAS A WATER INGRESS INDICATION AT 67 INCHES FROM INBD END & 5 INCHES FROM TE 3 INCH DIAMETER. DRILLED WITNESS HOLES, NO EVIDENCE OF WATER. APPLIED REPAIR IAW TC 4R5517310 PAR 3.5 & 3.6 & SRM 51-75-12 PAR 3 P3. LT ELEVATOR RESDR CALA2014040890776Seal · wornNUMBER 2 PYLON BOTTOM METAL SEAL WORN. REMOVED WORN CHAFE STRIP & STRAP. MATERIAL LOSS <.002 INCHES ON LOWER SPAR. HFEC OF WORKED AREA IAW NTM 51-10-20 PB6 NO CRACKS FOUND. FABRICATED EXTENDED ANTI-CHAFING PLATE IAW SRM 54-51-12 FIG 202. INSTALLED EXTENDESDR CALA2014040890777Stringer · corrodedCORROSION IN AFT PIT BILGE AREA ON STRINGER 42R FROM FRAME 63 - 64. REPAIR REQUIRES SRI INSP AT DEFINED INTERVALS. REMOVED SECTION OF STRINGER 42R BETWEEN FRAME 62 - 63. INSTALLED FABRIC REPAIR STRINGER 42 BETWEEN 62 - 64 & INSTALLED FABRICATED SPLICE STRINGSDR CALA2014040890778Stringer · corrodedCORROSION IN AFT PIT BILGE AREA ON LT SKIN STRINGERS & FASTENERS BETWEEN FRAMES 53 - 55 & STRINGER 41 - 44L. REMOVED FACTORY SPLICE AT FRAME 53. REMOVED STRINGER 41L FROM FRAME 53 TO FRAME 59. INSTALLED NEW STRINGER 41L FROM FRAME 53 TO FRAME 59 & FACTORY SSDR CALA2014040890779Stringer · corrodedCORROSION IN AFT PIT BILGE AREA ON STRINGER 41L FROM FRAME 63 - 64. REPLACED SECTION OF STRINGER 41L BETWEEN FRAME 62 - 63L TO FRAME 64, NEW SPLICE BETWEEN FRAME 61 - 63 & CLEAT FRAME 63 STRINGER 61 IAW SRM 53-00-13 FIG 201 & SRM 51-42-11 PG 25-27. REPAIR ATSDR CALA2014040890780Seal · wornNUMBER 1 PYLON BOTTOM METAL SEAL WORN. REMOVED STRAP & CHAFE PLATE ON LOWER SPAR. MATERIAL LOSS ON LOWER SPAR .005 INCHES. BLENDED CHAFE MARK SMOOTH. HFEC IAW NTM 51-10-20 PB6 NO CRACKS. FABRICATED EXTENDED ANTI-CHAFING PLATE IAW SRM 54-51-12 FIG 202. INSTSDR CALA2014040890781Skin · saturatedLEFT ELEVATOR UPPER SKIN SURFACE AREA HAS A WATER INGRESS INDICATION 35 - 43 FROM INBD END, 6 INCHES FROM TE, 7.75 X 5 INCHES DIAMETER. REPAIRED LT ELEVATOR UPPER SKIN AT LOCATION NOTED. DRILLED WITNESS HOLES & FOUND NO EVIDENCE OF WATER. APPLIED REPAIR IAWSDR CALA2014040890782Skin · saturatedRIGHT ELEVATOR UPPER SKIN SURFACE HAS A WATER INGRESS INDICATION 39 INCHES FROM INBD END, 3 INCHES FROM TE, 3.5 INCHES DIAMETER. REPAIRED RT ELEVATOR UPPER SKIN AT LOCATION NOTED. DRILLED WITNESS HOLES & FOUND WATER. CUT OUT, SANDED AREA & REMOVED WATER. APSDR CALA2014040890783Oxygen Mask · unsecureCREW REPORTS 02 MASKS FELL AT ROW 12ABC. REPACK MASK ON ROW 12ABC IAW AMM 35-21-43 & CHECK 02 GEN AMM 35-21-42 DROP TEST ACP ON TASK CARD 4R3590171 SEQ 546.SDR CALA2014040890784Epsu · failedPER 2 SVC EMERGENCY LIGHT TEST FAILS AFT 2L. REPLACED EPSU 13WL & BATTERY PACK IAW AMM 33-51-38-000-001-A.SDR CALA2014040390750Potable Water · leakingPOTABLE WATER LEAKING FROM BELLY OF ACFT NEXT TO HYD RESERVOIR FILLING PANEL.SDR CALA2014040390755Strut · faultyLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. CREW REPORTED HEARING THUMP, THEN GEAR RETRACTED. ACFT DOWN LINKED CFDS FAULT MAG LT LG EXT PROXIMITY SENSOR 23 GA & LT LG EXT SENSOR 21GA. REPACKED LT MLG STRUT, PERFORMED ADJUSTMENT TEST, OPERATIONS CHECKED GOSDR CALA2014040390751Stringer · corrodedCORROSION IN AFT PIT BILGE AREA STRINGER 43LT BETWEEN FRAME 55 - 56. R & R STRINGER 43LT FROM FRAME 53 - 60 IAW SRM 51-42-11.SDR CALA2014040390752Stringer · corrodedCORROSION IN AFT PIT BILGE AREA ON STRINGERS & FASTENERS AT DOUBLER CUT OUTS FROM FRAME 63 - 64 & STRINGER 41R. R & R STRINGER 41R FROM FRAME 58 - 64 IAW SRM 51-42-11.SDR CALA2014033190726Seal · damagedNLG LEAKING AFT SIDE BELOW COLLAR. REPLACED SEALS ON FWD & AFT STEERING RACK PISTONS IAW CMM 32-27-20, 32-27-19.SDR CALA2014033190727Power Supply · faultyLT EMERGENCY LIGHTS PSU FAULTED. REPLACED PSU IAW AMM 33- 51-38-000-001-A, OPERATIONS NORMAL.SDR CALA2014040390754Strut · defectiveON ARRIVAL, FOUND NLG STRUT TO BE OVER EXTENDED, 20 MINUTES LATER, STRUT WAS FLAT. ATTEMPTED NITROGEN SERVICE, NLG WILL NOT HOLD PRESS.SDR CALA2014033190729Deu · defectiveSTATIC IN CABIN SPEAKERS WITH CIDS CAUTION LIGHT ON. PERFORMED TROUBLESHOOTING 23-73-00-81 0-835A. FOUND BAD DEU A 200RH06. REPLACED & PERFORMED CIDS CHECK, ALL NORMAL.SDR CALA2014033190728Door · leakingEXTREMELY LOUD PRESS SQUEAL ROW 20. PRESSURIZED ACFT FOUND LEAK AT BOTTOM AFT CORNER ON FWD EMERGENCY EXIT HATCH. SMOOTHED REN IN SUSPECT AREA RE PRESSURIZED ACFT, CHECKED OK.SDR CALA2014032790702Skin · damagedLEFT WING FUEL TANK LANDING 540PB OTBD OF RIB 19 HAS DAMAGE AT HOLE N & F. REAMED BOTH HOLES TO 0.297 IAW SRM 57-21-11 PGS 201 - 220, FIG 202. FABRICATED NEW BUSHINGS & INSTALLED IN HOLES N & F IAW SRM 51-72-12 PGS 1-8, FIG 2. TSDR CALA2014032690696Autopilot Sys · malfunctionedDIVERT TO LAX DUE TO AUTO FLIGHT CONTROL ISSUE.SDR CALA2014032790700Stringer · corrodedCORROSION AFT CARGO PIT STRINGER 41R, FRAME 62 TO FRAME 63, NO CORROSION ALLOWABLE. R & R STRINGER 41R FROM FRAME 58 TO FRAME 64 IAW SRM 51-4 2-11 PAGE 23.SDR CALA2014032790701Stringer · corrodedCORROSION AFT CARGO PIT STRINGER 42R, FRAME 62 TO FRAME 63. R & R STRINGER 42R, FRAME 60 TO FRAME 64 IAW SRM 51-42-11 PG 7 & 23.SDR CALA2014032790704Oxygen Mask · unsecureCREW REPORTS 02 MASKS FELL AT ROW 12ABC. STOWED MASKS IAW MT 35- 003, DROP TEST TO BE COMPLIED WITH WITHIN 3 DAYS.SDR CALA2014032890714Control Unit · faultedON CLIMB OUT, ACFT ENCOUNTERED A NOSE WHEEL SENSOR FAULT, BRAKE STEERING CONTROL UNIT FAULT. FLIGHT CONTINUED, EMERGENCY DECLARED.SDR CALA2014032490677Wire · chafedIAW TO EM4478-1 SEQ 3512011 FOUND CHAFED WIRE IN 90 DEGREE CONNECTOR 4021KS-A, WIRE GOES TO SOCKET E WIRE 5B416B20.
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