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 CALA2015050793687Battery Pack · dischargedDOOR 2L EMER LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.SDR CALA2015050793688Power Supply · inoperativeDOOR 2L EMER LIGHT & POWER SUPPLY INOPERATIVE. REPLACED POWER SUPPLY. SYS OPERATIONS CHECKED NORMAL.SDR CALA2015050793689Battery · dischargedEMERGENCY LIGHT BATTERY PACK AT DOOR 1L IS DEAD. REPLACED BATTERY & POWER SUPPLY. OPERATIONS CHECKED OK.SDR CALA2015050793690Power Supply · inoperativeLOST GND POWER AT GATE. TURNED ON EMER LIGHTS TO ARMED, GOT LIGHTS ONLY AT EMER EXIT AISLE SEATS. TURNED SWITCH TO ON, ONLY LIGHTS AT EMER EXIT AISLE SEATS. FOUND FWD, AFT & LT POWER SUPPLIES NOT POWERING EMER LIGHTS WITH POWER OFF. REPLACED FWD & AFT POWESDR CALA2015050893698Fan · seizedCREW REPORTED FAINT SMELL OF SMOKE FOLLOWED BY EXTRACT FAN FAULT & CB AE2 POPPED. FOUND AEVC EXTRACT FAN SEIZED & SOURCE OF SMOKE. R & R EXTRACT FAN IAW 21-26-51. OPERATIONS CHECKED IAW AMM 21-26-00-710-001-A.SDR CALA2015050693661Skin · crackedFUSELAGE SKIN FRAME 35 & CM10 THE LT AFT LOWER HOLE NR 2 HAS CRACK INDICATION 5:00 POSITION. REPAIRED NR 2 HOLE & INSTALLED FASTENER LT FRAME 35 IAW ECRA 53-30-04940 & THIS IS TEMP REPAIR. REPAIR OF CRACKED & ELONGATED FASTENER HOLE FRAME 35 BELOW STRINGER 3SDR CALA2015050493652Battery · dischargedFORWARD LT & AFT LT EMER LIGHT BATTERIES FAIL CAPACITY TEST. REPLACED 10WL & 13WL BATTERIES IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A. CAPACITY TESTED OK IAW AMM 33-51-00-710-003.SDR CALA2015050493651Hydraulic Line · unknownG RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN AT FL 360. EMER DECLARED & DIVERTED. REPLACED NR 1 ENG HYD PRESS LINE.SDR CALA2015050193645Door Sill · corrodedR2 DOOR SILL HAS CORROSION AT FRAME 66 - 68, STRINGER 22R - 23R. R & R R2 DOOR SILL IAW SRM 51-72-11.SDR CALA2015050193646Frame · corrodedFRAME 68 RT SIDE HAS CORROSION BETWEEN STRINGER 23R & 22R. FABRICATED REPAIR FITTING IAW SRM 53-41-12. INSTALLED FITTING IAW SRM 53-41-12 PAR 5 FIG 201.SDR CALA2015050193638Compressor Blade · damagedABORTED TAKEOFF, ENG 1 STALL NEVER EXCEEDED 1.2 EPR, FLAMES REPORTED. PER CREW AUDIBLE STALL, TRAILING ACFT REPORTED VISUAL STALL. NR 1 ENG HAS MULTI 3RD STAGE HPC BLADES DAMAGE BEYOND REPAIR LIMITS. ENG CHANGE SCHEDULED.SDR CALA2015050693657Skin · corrodedCORROSION AROUND AFT LAVATORY EXHAUST VENT. INSTALLED DOUBLER REPAIR IAW SRM 53-41-11 FIG 205.SDR CALA2015042093582Unknown · malfunctionedREFERENCE LOG 1, SLIDE INDICATION FOR LT OVERWING EXITS, NOT ILLUMINATED ON ECAM DOOR PAGE. WHEN REMOVING DOOR COVERS, SLIDE ARMED LIGHT LOCATED BETWEEN DOORS DOES NOT COME ON WHEN REMOVING LT AFT COVER. SUSPECT PROBLEM IS WITH LT AFT SLIDE ARMED SYS. ACFT SDR CALA2015042093581Skin · dentedFROM CF 9001 REPAIR DENT AT STRINGER 41, FRAME 56RT. REPAIRED IAW SRM 53-41-11 FIGURE 204 SHEET 4. SRI53-41-11-2-012-00 TABLE 215 REQUIRES FIRST INSPECTION AT 45,800C FROM REPAIR EMBODIMENT. THEN SUBSEQUENT INSPECTION AT 11,40 0C INTERVALS THEREAFTER. THENSDR CALA2015041393523Valve · faultedRETURNING TO FIELD DUE TO UNABLE TO PRESSURIZE. SKIN VLV FAULT. ALSO REF DF96 SKIN EXCH INLET BYPASS VLV CURRENTLY ON MEL. PFR SHOWS SEVERAL FAULTS VENT AVNCS SYS FAULT, VENT SKIN VLV FAULT & VENT BLOWER FAULT. CFDS MSGS, INLET BYPASS V16HQ, SKIN AIR OUTLESDR AALA201504089004Fmu · inoperativeAFTER TAKEOFF, THE CREW RECEIVED A NR 2 FUEL CONTROL FAULT. DEFERRING TO THE QRH, WHICH TOLD THEM TO PULL ENG BACK TO IDLE. PROCEDURE WAS FOLLOWED, BUT THE SAME ISSUE WAS ACTIVE. THE FLIGHT WAS DIVERTED, AN EMERGNECY WAS DECLARED. RECEIVED AN NR 2 ENG ADSDR USAA2015040200010Bleed Valve · faultyON TAKEOFF AT ABOUT 1500 FT, CREW HAD NR 2 ENG COMPRESSOR STALL & HIGH EGT. FLIGHT RETURNED TO FIELD WITH NO EMER DECLARED & WITH NO FURTHER INCIDENT. TROUBLE SHOT IAW TSM 71-00-00-810-809A & PERFORMED FUNCTIONAL CHECK OF THE HPC 7TH & 10TH STAGE BLEED VLV &SDR USAA2015040200011Solenoid Valve · faultyON TAKEOFF AT ABOUT 1500 FT, CREW HAD NR 2 ENG COMPRESSOR STALL & HIGH EGT. FLIGHT RETURNED TO FIELD WITH NO EMER DECLARED & WITH NO FURTHER INCIDENT. TROUBLE SHOT IAW TSM 71-00-00-810-809A & PERFORMED FUNCTIONAL CHECK OF THE HPC 7TH & 10TH STAGE BLEED VLV &SDR CALA2015040293498Interface Unit · malfunctionedLEFT MLG FAILED TO INDICATE DOWN & LOCKED. CYCLED GEAR IAW CHECKLIST. LT MAIN GEAR UNSAFE, CRANKED GEAR DOWN, MANUAL GEAR EXTENSION. GREEN LIGHT NOT ILLUMINATED, NO ECAM MSGS. REPLACED FIN 9LP IAW MM 33-14-33-000 400-001A PN 35-OFS-1000 & LGCIU 1 IAW MM 32SDR CALA2015040293503Hydraulic Line · damagedDIVERT, YELLOW SYS HYD LOW PRESS FLUID LOSS, YELLOW SYS ACCUMULATOR LOSING PSI. REPLENISHED YELLOW SYS HYD DUE TO FLUID LOSS FROM PRESS LINE HOLE. R & R LINE, PRESS RESTORED.SDR CALA2015033093486Door Sill · corrodedL2 DOOR SILL FRAME 66 HAS TWO EACH CORRODED FASTENER HOLES. REPAIRED IAW SRM 53- 41-14 PAR 5 A FIG 201.SDR CALA2015033093487Door Sill · corrodedR1 DOOR SILL FRAME 16 - 20 FWD & AFT GIRT BAR FITTING ATTACH AREAS HAVE CORROSION AT FASTENER HOLES. REWORKED IAW SRM 53-11-14 PAR 4 E FIG 108.SDR CALA2015033093485Stringer · corrodedSTRINGER 31R AT FRAME 64 - 67 HAS CORROSION. REPLACED IAW SRM 51-72-11.SDR CALA2015033093490Starter · faultyAPU ALTITUDE NO START, COLD SOAK. APU HANGS BETWEEN 0 - 19% DURING START, 3 ATTEMPTS, ALL THREE FAULTED, MAX RPM WAS 26. R & R APU STARTER IAW AMM 49-41-01.SDR CALA2015033093489Battery · failedEMERGENCY LIGHT BATTERY CAP TEST FAILS. REPLACED 10WL & 12WL IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A. CAPACITY TEST OK IAW AMM 33-51-00-710-003.SDR CALA2015032093453Battery · failedDOOR 1L EMER LIGHT BATTERY FAILED TEST. REPLACED EPSU BATTERY IAW AMM 33-51-38-000-002.SDR CALA2015031793425Strut · low pressureUNABLE TO RAISE GEAR HANDLE. HAVE ASSOCIATED FAULTS, AIR GND SENSE ISSUES. ACCOMPLISHING SEVERAL EXTENSIONS & COMPRESSIONS VIA JACKS TO CONFIRM NO EXTEND ISSUES, GEAR SWING IAW AMM 32-31-00-720-002. FOUND STRUT PRESS LOW, SERVICED LT MLG STRUT & PERFORMED MSDR CALA2015031793441Epsu · malfunctionedEPSU BATTERY EMER RT MSG AFTER PERFORMING EMER LIGHTS OPERATIONAL TEST. REPLACED EPSU IAW AMM 33-51-38-000-001-A. OPERATIONS CHECKED OK.SDR YENA20150313045Fmu · failedDIVERTED AT CRUISE NR 1 ENGINE ROLLED BACK TO IDLE THRUST. ECAM REPORTED NR 1 ENGINE FAILED. FOLLOWED ECAM AND SHUTDOWN NR 1 ENGINE. T/S IAW TSM 73-00-00-810-904. R & R NR 1 ENGINE FMU AMM 73-22-52. R & R NR 1 ENGINE FADEC IAW AMM 73-22-01. OPS AND LEAK CHECKSDR CALA2015031793439Stop Fitting · crackedFRAME 68 AT R2 DOOR LOWER AFT STOP FITTING, INBD LOWER HOLE IS CRACKED AT 6 O’CLOCK. HOLE WAS REPAIRED IAW SRM 53-41-12 PG 222 WITH FREEZE PLUG. THIS IS A CAT B REPAIR & REQUIRES SRI INSPECTION IAW SRM 53-41-12 TABLE 202 ON PAGE 203.SDR CALA2015031793440Stop Fitting · crackedFRAME 66 AT R2 DOOR, 3RD STOP FITTING FROM BOTTOM, INBD LOWER HOLE IS CRACKED AT 5 O`CLOCK. HOLE WAS REPAIRED IAW SRM 53-41-12 PG 222 WITH FREEZE PLUG. THIS IS A CAT B REPAIR & REQUIRES SRI INSPECTION IAW SRM 53-41-12 TABLE 202 ON PAGE 203.SDR YENA20150312042Compressor · stalledON CLIMBOUT, ENGINE 1 COMPRESSOR VANE ON ECAM. FOLLOWED QRH. IN CLIMB EPR FLEX EGT NR 1 100 DEGREES HIGHER THAN ENGINE 2. NR 1 ENGINE N2 PERCENT 86.6 AND ON NR 2, 84.4. R & R ENGINE NR 1. ALL OPS CHECK FOUND OK. NOTE: ON APPROACH INTO PBI PILOT DECLARED AN ESDR CALA2015031793429Connector · not seatedINTERIOR LOADS EMER R FAULT WHEN PERFORMING EMER LIGHTS TEST. REMOVED & INSTALLED SAME BATTERY PACK & RESEATED CONNECTOR ON POWER SUPPLY UNIT. RETESTED & CHECKED OKAY.SDR USAA2015030900006Actuator · defectiveENGINE 1 COMPRESSOR VANE FAULT ON TAKEOFF ROLL APPROX 50 KIAS. AVOIDED TAKEOFF & SHUTDOWN ENG 1 IAW ECAM. REPLACED VSV ACTUATOR ON NR 1 ENG IAW AMM 75-32-41 & 71-00-00-710. OPERATIONAL CHECKS ACCOMPLISHED WITH NO DEFECTS NOTED.SDR CALA2015030993417Skin · debondedRIGHT ELEVATOR UPPER SKIN HAS A DISBOND 23" FROM INBD, 25" FROM TE, 2" DIA. REMOVED UNBONDED AREA & APPLIED REPAIR IAW SRM 55-21-11 PARA 5E.SDR CALA2015030993410Door Frame · crackedL2 DOOR FRAME 66 STOP FITTING 1IB UPPER MOUNT HOLE HAS A CRACK INDICATION. REPAIRED WITH A FREEZE PLUG IAW SRM 53-41-12 PARA 5E FIG 204.SDR CALA2015030993411Door Frame · crackedL2 DOOR FRAME 68 STOP FITTING NR 7 MOUNT HOLE HAS A CRACK INDICATION. REPAIRED WITH FREEZE PLUG IAW SRM 53- 41-12 PARA 5E FIG 204.SDR CALA2015030993412Door Frame · crackedAFT RT PAX DOOR FRAME 68 RT NR 7 FITTING LOWER OTBD HOLE HAS CRACK INDICATION. CLEANED UP HOLE & NDT INSP HFEC IAW NTM 51-10-08 & NO CRACK FOUND. FABRICATED FREEZE PLUG & REPAIR FITTING FOR AFT END & INSTALLED IAW SRM 53-41-12.SDR CALA2015030493184Frame · crackedLEFT FRAME 43 CRACKED AT HOLE NR 3. REPAIRED IAW ECRA 5330-05 076 REV A. THIS IS A PERMANENT REPAIR WITH NO INSPECTION REQUIREMENTS.SDR CALA2015030493207Door Sill · corrodedR2 DOOR SILL HAS CORROSION AT NUTPLATE AT FRAME 68. REPAIRED IAW SRM 53-41-14 FIGURE 201 SHEET 3 PRINCIPLE 4.SDR CALA2015030493208Door Sill · corrodedR2 DOOR SILL FRAME 68 INBD & FWD OF AFT GIRT BAR FITTING, CORROSION AT 7 LOCATIONS. R & R R2 DOOR SILL IAW SRM 51-42-11.SDR CALA2015030993409Door Sill · corrodedR2 DOOR SILL HAS CORROSION AT NUTPLATE AT FRAME 68. REPAIRED IAW SRM 53-41-14 FIGURE 201 SHEET 3 PRINCIPLE 4 ON HAECO NR 35080.SDR CALA2015030493205Door Frame · crackedAFT PAX DOOR CUT OUT, DOOR STOP FITTING HOLES AT FRAME 68 WEB RT POSITION 7 LOWER INBD HOLE IS CRACKED AT APPROX 6 O'CLOCK & 12 O'CLOCK POSITIONS. HOLE WAS OPENED UP TO .417 & CRACK FREE VIA NTM51-10-01-PB6. FINAL REAM TO .438 & FREEZE PLUG INSTALLED IAW SRMSDR CALA2015030493206Skin · damagedLEFT WING LOWER SURFACE OPENING FOR FUEL PANEL 540JB HAS ELONGATED SCREW HOLE. REPAIRED HOLE IAW ECRA 5720-02637. REQUIRES 1ST INSPECTION AFTER ACFT 1ST FLIGHT AT 31.1K FC 54.6K FH & SUBSEQUENT INSPECTIONS A T 3.6K FC 4.5K FH IAW SRI 57-21-11 TBL 203. CURRESDR CALA2015030993407Door Frame · crackedAFT PAX DOOR CUT OUT, DOOR STOP FITTING HOLES AT FRAME 68 WEB, RT POSITION 7 LOWER INBD HOLE IS CRACKED AT APPROX 6 O'CLOCK & 12 O'CLOCK POSITIONS. HOLE WAS OPENED UP TO .417 & CRACK FREE VIA NTM51 -10-01-PB6. FINAL REAM TO .438 & FREEZE PLUG INSTALLED IAW SSDR CALA2015030993408Skin · damagedLEFT WING LOWER SURFACE OPENING FOR FUEL PANEL 540JB HAS ELONGATED SCREW HOLE. REPAIRED HOLE IAW ECRA 5720-02637.SDR CALA2015030493210Power Supply · inoperativeBATTERY EMER RT MSG DISPLAYED AFTER EMER LIGHTS OPERATIONAL TEST. FAILS BATTERY RT POWER SUPPLY, WILL NOT TEST. REPLACED POWER SUPPLY & BATTERY IAW AMM 33-51-38. OPERATIONS CHECKED GOOD.SDR CALA2015030993399Power Supply · inoperativeBATTERY EMER RT MSG DISPLAYED AFTER EMER LIGHTS OPERATIONAL TEST. POWER SUPPLY WILL NOT TEST. REPLACED POWER SUPPLY & BATTERY IAW AMM 33-51-38. OPERATIONS CHECKED GOOD.SDR CALA2015022793180Warning System · false activationABORTED TAKEOFF DUE TO NUMEROUS FMGC RELATED FAULTS. REPORTED AROUND 100 KTS AT REJECT. PERFORMED AFS BITE, NO FAULTS DETECTED.SDR CALA2015030493209Skin · gougedTHREE EACH SKIN GOUGES BETWEEN FRAME 51 - 52 & STRINGER 38 -39R FROM CONTACT WITH WTB FAIRING 198GB. BLENDED GOUGES IAW SRM 53-41-11 F105. NOMINAL SKIN THICKNESS IS .157" IAW SRM 53-41-11 PAGE 15. IAW NTM 51-10-04 PB4 MINIMUM MATERIAL REMAINING OF 3 AREAS A
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