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 CALA2015030993397Door 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 CALA2015030993398Skin · gougedTHREE EA 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 PG 15.SDR CALA2015022693174Frame · crackedLEFT FRAME 43 IS CRACKED AT HOLE NR 3 1 LONG. CRACK CHECKED BY HFEC. REPAIRED FRAME IAW ECRA 5330-05075. THIS REPAIR FOUND TO BE PERMANENT REPAIR.SDR CALA2015022693177Frame · corrodedRIGHT FRAME 68 FWD FACE JUST ABOVE FLOOR LEVEL IS CORRODED. ORIGINAL THICKNESS .098 INCHES, MATERIAL LOSS OF .035 INCHES IS OUT OF LIMITS IAW SRM 53-41-12 FIG 102. REPAIRED IAW SRM 53-41-12 PAR 5A FIG 201. DOUBLER INSTALLED.SDR CALA2015022093166Fluid · lowGREEN HYD SYS FAILURE, CREW PLANNED MANUAL GEAR EXTENSION, BUT ABLE TO EXIT RNWY & TOWED TO GATE. FOUND ALL 3 HYD QTY LOW. SERVICED & RAN ALL 3 SYS & OPERATED ALL FLIGHT CONTROLS, NO LEAKS.SDR CALA2015022093159Stop Fitting · gougedR2 DOOR CUT OUT FRAME 68 DOOR STOP FITTING NR 2, ALL 4 ATTACH HOLES HAVE GOUGES. REAMED UPPER INBD & OTBD TO .263 INCHES, LOWER INBD TO .26 3 INCHES, LOWER OTBD .265 INCHES. REPAIRED IAW SRM 53-41-12 PAR 5 D.SDR CALA2015022093160Door Frame · damagedR2 DOOR CUT OUT FRAME 68 DOOR STOP FITTING NR 5 LOWER INBD HOLE IS OUT OF ROUND IN THE FRAME WEB. REAMED TO .265 INCHES. REPAIRED IAW SRM 53-41-12 PAR 5 D.SDR CALA2015022093161Door Frame · damagedR2 DOOR CUT OUT FRAME 66 RT DOOR STOP FITTING NR 5 UPPER INBD HOLE IS CRACKED IN THE WEB AT 2 O'CLOCK POSITION. REAMED TO .278 INCHES & REPAIRED IAW SRM 53-41-12 PAR 5 D.SDR CALA2015022093162Door Frame · crackedR2 DOOR CUT OUT FRAME 66 DOOR STOP FITTING NR 6 LOWER INBD HOLE IS CRACKED IN THE WEB AT 2 O'CLOCK POSITION. REAMED HOLE TO .268 INCHES. REPAIRED IAW SRM 53-41-1 2 PAR 5 D.SDR CALA2015022093165Door Frame · crackedL2 DOOR CUT OUT FRAME 66 LOWER STOP LOWER INBD HOLE HAS A CRACK. ACCOMPLISHED REPAIR IAW REO-L18732 & ECRA 5340-01644. HOLE WAS REAMED & FREEZE PLUG INSTALLED. INTERIM APPROVED IAW RDAS 80025005-003-2015 ISSUE A FOR 50C. NEW RDAS PROVIDING PERM APPROVAL MUSDR CALA2015021293121Door Frame · damagedR2 DOOR CUT OUT FRAME 68 SECOND FROM LOWER STOP, OTBD UPPER HOLE HAS AN ELONGATION INDICATION OUT OF LIMITS IN FRAME. REPAIRED IAW SRM 53-41-12 PAR 5 E FIG 204.SDR CALA2015021293122Door Frame · crackedR2 DOOR CUT OUT FRAME 68 LOWER STOP LOWER INBD HOLE HAS A CRACK INDICATION IN FRAME AT 6 O'CLOCK POSITION. REPAIRED IAW SRM 53-41-12 PAR 5 E FIG 204.SDR CALA2015021293123Door Frame · crackedL2 DOOR CUT OUT FRAME 68 LOWER STOP LOWER INBD HOLE HAS A CRACK INDICATION IN FRAME AT 6 O'CLOCK & 12 O'CLOCK POSITION. REPAIRED IAW SRM 53-41-12 PAR 5 E FIG 204.SDR CALA2015021293129Battery · dischargedEMERGENCY LIGHTS OPERATIONAL TEST FAILED. REPLACED LT EMER BATTERY LOCATED BY EMER EXIT IAW AMM 33-51-38, TESTED OK.SDR CALA2015021293137Battery · dischargedCABIN EMER LIGHT CHECK FAILED. GRIPES EPSU FWD LT IAW A CHECK JC 4-2020 STEP 26. REPLACED ESPU BATTERY 10WL IAW MM 33-51-38-000-002-A & 33-51-38-400-002-A. INSTALLED PN AD -3214-30.SDR CALA2015021293138Battery · dischargedFAILED EMER LIGHT BATTERY CAP TEST. GRIPES BATTERY CAP AFT LT IAW A CHECK JC 4-2020 STEP 33. REPLACED EPSU BATTERY 13W LT IAW MM 33-51-38-000-002-A & 33-51-38-400-002-A. INSTALLED PN AD-3214-31. CAP TESTED GOOD.SDR CALA2015021093074Stringer · corrodedAFT CARGO COMPARTMENT STRINGER 43L CORRODED AT FRAME 56 - 59, TOP SURFACE & UNDERSIDE AROUND FLANGE. ACCOMPLISHED STRINGER REPAIR ON NR 9710677 IAW SRM 53-00-13 FIG 201 PG 211 DETAIL H. STRINGER REPLACED FROM FRAME 56 - 59.SDR CALA2015020693068Slide · defectiveEMERGENCY LIGHTS OPERATIONAL TEST DOES NOT PASS DURING 2 SERVICE CHECK. MESSAGE ATA 33-51-38 EXT LOADS FWD LT. TRIED NEW EPSU, NO HELP IAW TSM31-51-00-810-808A. REPLACED DOOR 1R SLIDE ASSEMBLY IAW AMM-25-62-44-400-006-A. PERFORMED EMER LIGHT TEST, SYS OPERSDR CALA2015020393064Eec · malfunctionedCREW REPORT ENG 2 SENSOR FAULT & ENG 2 STALL MSG ON ECAM. HELD AT FL 160 & PERFORMED QRH PROCEDURES, NO STALL OBSERVED. CREW ELECTED TO RETURN. R & R NR 2 EEC IAW AMM 73-22-34-400-010-A13. COMPLIED WITH STEPS 3 THRU 5D.SDR CALA2015020293050Skin · saturatedRIGHT ELEVATOR UPPER SKIN HAD 2 WATER FINDINGS FROM THERMOGRAPHY INSPECTION. 102.5 INCHES FROM INBD END & 4 INCHES FROM TE. 74 INCHES FROM INBD END & 4.5 INCHES FROM TE. BOTH AREAS REPAIRED IAW SRM 55-21-11 REPAIR PGS 234 - 236 FIG 205. REPAIR AREAS WERE BSDR CALA2015020293061Skin · damagedRIGHT WING TANK ACCESS PLATE 640PB HAS DAMAGED FASTENER HOLE ON LANDING. HOLE WAS REPAIRED IAW HAECO REO-L187 08 & CONSIDERED CAT B REPAIR IAW -B RDAS 80022401-003-2015. HOLE WAS OVERSIZED & BUSHING WAS INSTALLED. IAW CRA THRESHOLD SUPPLEMENTAL INSPECTIONS TSDR USAA2015020200022Shear Pin · corrodedNUMBER 1 ENG AFT MOUNT INBD UPPER INNER SHEAR PIN HAS SLIGHT PITTING ALONG FULL LENGTH OF PIN APPROX 60 DEGREES OF RADIUS. REPLACED NR 1 AFT MOUNT INBD UPPER INNER SHEAR PIN IAW AMM 71-22-11-200-804-A.SDR CALA2015020293054Skin · damagedRIGHT FUEL TANK ACCESS LANDING, TWO EACH HOLES HAS ELONGATION 640HB. R & R BUSHING HOLE 565 & INSTALLED BUS HINGE HOLE 562 IAW A320. SRM 57-21-11 PG 210-216 PAR B.SDR CALA2015012893034Strut · defectiveLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO FIELD. FAULTS WITH PROXIMITY SENSORS 21GA & 23GA. STRUT IS SHOWING A 250 PSI DIFFERENCE BETWEEN UPPER & LOWER CHAMBERS, 25 PSI IS GENERAL DIFFERENCE LIMIT. ADJUSTED PROXIMITY SENSOR. PERFORMED FULLSDR CALA2015012793030Battery · dischargedEMERGENCY LIGHTS, OPERATIONAL TEST FAILED, BATTERY FWD LT DISPLAYED. REPLACED NR 1 BATTERY FWD LT. LIGHTS CHECKED GOOD IAW AMM 33-51-38-400-02.SDR CALA2015012793033Door Sill · corrodedR2 DOOR SILL BEAM HAS CORROSION ON PREVIOUS REPAIR & FRAME 68, JUST FWD OF THE AFT GIRT BAR FITTING PLATE. R & R DOOR SILL IAW SRM 51-42-11.SDR CALA2015012793024Engine · vibrationAT CLIMB POWER ENG 2 N1 VIB 2.7 WITH ENG 1 AT 0.4. ALSO ENG 2 EGT 570 DEGREES & ENG 1 AT 519 DEGREES. ACCOMPLISHED ON SHOT TRIM BALANCE IAW MT71-010, MM 72-31-11 & MM 71-00-00. TESTED NR 8. ALL INDICATIONS NORMAL, MAX N1 VIBE WAS 0.4 AT 85%.SDR CALA2015012793026Plate · corrodedNUMBER 2 RT AFT DOOR SILL PLATE HEAVY CORROSION. NR 2 RT AFT DOOR SILL PLATE REPLACED IAW SRM 51-72-11.SDR CALA2015012393007Battery · dischargedEMERGENCY LIGHT BATTERY CAPACITY TEST FAILED, EPSU BATTERY CAPACITY AFT LT. REPLACED AFT LT BATTERY 13WL. PN AD-3214-31. BATTERY CAPACITY TESTED OK.SDR CALA2015012393009Door Sill · corrodedR2 DOOR SHAPE SILL HAS CORROSION AROUND FASTENERS. REPLACED DOOR SHAPE SILL IAW SRM 51-73-11.SDR CALA2015012393010Fitting · corrodedR2 DOOR AFT SHAPE SILL CORNER FITTING FOUND CORROSION DURING REMOVAL. R & R CORNER FITTING IAW SRM 51-44-11 & 51-75-12.SDR CALA2015012393017Epsu · faultedEMERGENCY LIGHT FAILED TEST, FAULTS CTR LT EPSU. REPLACED CTR LT EPSU & BATTERY IAW AMM 33-51-38, TESTED OK.SDR CALA2015012393020Charger · inoperativeD1L EMER EXIT LIGHT CHARGER INOPERATIVE, CICS. CHANGED CHARGER & BATTERY IAW MM33-51-38-401. OPERATIONS CHECKED GOOD.SDR CALA2015012393019Stringer · corrodedSTRINGER 31R AT FRAME 65 BELOW OUTFLOW VLV IS CORRODED. REPLACED FACTORY SECTION OF STRINGER IAW SRM 51-72-11.SDR CALA2015012393012Lug · chafedFORWARD CARGO DOOR FUSELAGE FITTING AT NR 6 LATCHING ROLLER, AFT LUG CHAFED. BLENDED CHAFED AREA IAW SRM 53-26-00 FIG 101. MATERIAL REMAINING WITHIN LIMITS. THIS ALLOWABLE DAMAGE MUST BE INSPECTED AT DEFINED INTERVALS IAW SRI 53-26-00-1-1.SDR CALA2015012393013Lug · chafedFORWARD CARGO DOOR FUSELAGE FITTING AT NR 5 LATCHING ROLLER, AFT LUG CHAFED. BLENDED CHAFED AREA IAW SRM 53-26-00 FIG 101. MATERIAL REMAINING IS WITHIN LIMITS. THIS ALLOWABLE DAMAGE MUST BE INSPECTED AT DEFINED INTERVALS IAW SRI 53-26-00-1-1.SDR CALA2015012393014Lug · chafedFORWARD CARGO DOOR FUSELAGE FITTING AT NR 3 LATCHING ROLLER, FWD LUG CHAFED. BLENDED CHAFED AREA IAW SRM 53-26-00 FIG 101. MATERIAL REMAINING IS WITHIN LIMITS. THIS ALLOWABLE DAMAGE MUST BE INSPECTED AT DEFINED INTERVALS IAW SRI 53-26-00-1-1.SDR CALA2015012393015Lug · chafedFORWARD CARGO DOOR FUSELAGE FITTING AT NR 2 LATCHING ROLLER, FWD LUG GOUGED. BLENDED GOUGE IAW SRM 53-26-00 FIG 101. MATERIAL REMAINING IS WITHIN LIMITS. THIS ALLOWABLE DAMAGE MUST BE INSPECTED AT DEFINED INTERVALS IAW SRI 53-26-00-1-1.SDR CALA2015012393016Lug · chafedFORWARD CARGO DOOR FUSELAGE FITTING AT NR 4 LATCHING ROLLER, AFT LUG GOUGED. BLENDED GOUGE IAW SRM 53-26-00 FIG 101. MATERIAL REMAINING IS WITHIN LIMITS. THIS ALLOWABLE DAMAGE MUST BE INSPECTED AT DEFINED INTERVALS IAW SRI 53-26-00-1-1.SDR CALA2015011692985Plate · damagedFIVE EACH HOLES FOUND DAMAGED ON LT WING LOWER SKIN PANEL NR 3 PYLON SYS MOUNTING PLATE. HOLES REPAIRED REO L18663 REV IR & ECRA 5720-02626. RECEIVED A - B RDAS 80018161-003-2014 ISSUE A THAT THIS IS AN INTERIM REPAIR APPROVED FOR 6 MONTHS. A NEW RDAS MUST SDR CALA2015011392940Door Sill · corrodedCORROSION ON R2 DOOR SILL BEAM AROUND AFT FLOORBOARD NUTPLATE HOLES. BLENDED CORROSION ON AFT FLOORBOARD NUT PLATE HOLES & INSTALLED REPAIR IAW SRM 53 -41-14 FIG 201PARA 5A PRINCIPLE 5.SDR CALA2015010992930Skin Panel · damagedLEFT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATIONS AT THE FOLLOWING LOCATIONS: 82 INCHES FROM INBD, 5 INCHES FROM TE, 3.5 INCHES X 3 INCHES, 170 INCHES FROM INBD, 13 INCHES FROM TE, 2.5 INCHES DIAMETER 27 INCHES FROM INBD, 29 INCHES FROM TE, 1.5 X 2 SDR CALA2015010992931Skin Panel · damagedRIGHT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATION AT THE FOLLOWING LOCATIONS: 27 INCHES FROM INBD, 28 INCHES FROM TE, 2 INCHES DIAMETER: 17 INCHES FROM INBD, 26 INCHES FROM TE, 2.5 INCHES DIAMETER: 12 INCHES FROM INBD, 8 INCHES FROM TE, 25 INCHESSDR USAA2014122300005Eec · inoperativeDIVERTED TO PIT WHEN STATUS MSG WAS RECEIVED THAT ENG 2 TR & THR WAS INOPERATIVE. REPLACED NR 2 ENG EEC IAW JOB CARD 26L40073002.SDR YENA20141221280Stator · failedENROUTE, NR 2 ENGINE FADEC ALTERNATOR ILLUMINATED ON ECAM. ACFT RETURNED TO DEPARTURE,. FOUND NR 2 ENGINE DEDICATED ALTERNATOR STATOR BAD. R & R ALTERNATOR. ACCOMPLISHED ENGINE RUN, GOOD REF AMM 72-22-38-000-010-B. OPS CHECK GOOD.SDR CALA2014122692866Engine · malfunctionedNUMBER 2 ENG OIL QTY LOW & DECREASING EVENTUALLY TO ZERO. PRESS & TEMP GOOD. ENG SHUTDOWN INFLIGHT. SUSPECTED ENG OIL PUMP HOUSING FAILURE. NR 2 ENG R & R. ACCOMPLISHED AMM TASK 72-00-00-200-021-BM INFLIGHT SHUTDOWN PROCEDURE.SDR CALA2015012693022Unknown · leakingNUMBER 2 ENG OIL QTY SHOWING ZERO WITH PIL PRESS & TEMP GOOD. NR 2 ENG SHUTDOWN INFLIGHT. OPENED FAN COWLS & FOUND OIL RESIDUE COVERING EVERYTHING. WIPED UP OIL & RECHECKED AREA, OIL PUMP CONTINUING TO LEAK. SUSPECT OIL PUMP HOUSING FAILURE. ENG REMOVED DSDR CALA2014123192878Wire · burnedRIGHT FUEL TANK 1 PUMP INOPERATIVE. LOW PRESS IN CLIMB WITH 2.6 IN RT WING TANK. FOUND PUMP TRIPPING THE CB, REPLACED NR 1 RT FUEL PUMP IAW AMM 28-21-51, NO HELP. PUMP DOES NOT OPERATE WITH SWITCH ON. REPLACED 18QA CONNECTOR, 54QA CONNECTOR & CB 2QA. NO HESDR CALA2014122392858Skin · damagedRIGHT WING TANK ACCESS CUT OUT AT 640HB HAS 1 EACH ELONGATED HOLE. IAW ECRA 5720-02624, INSTALLED BUSH REPAIR CATEGORY A REPAIR WITH NO RE INSPECTION REQUIREMENTS.SDR USAA2014121600001Connector · dirtyON TAKEOFF ENG 2 SENSOR FAULT, DECISION TO RETURN. FOUND RESIDUE IN CONNECTOR ON EGT HARNESS FWD OF JUNCTION BOX. CLEANED ENG 2 EGT HARNESS CONNECTOR FWD OF JUNCTION BOX.
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