IAE V2527-A5

Service difficulty reports · 8,009

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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.

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.Feb 25, 2015 · N405UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 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.Feb 25, 2015 · N405UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 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.Feb 24, 2015 · N453UA · Airbus A320232 · Fuselage Main, FrameSDR 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.Feb 23, 2015 · N405UA · Airbus A320232 · Fuselage Main, FrameSDR 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.Feb 17, 2015 · N425UA · Airbus A320232 · Hydraulic System, MainSDR 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.Feb 16, 2015 · N419UA · Airbus A320232 · Fuselage Main, StructureSDR 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.Feb 16, 2015 · N419UA · Airbus A320232 · Fuselage Main, StructureSDR 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.Feb 16, 2015 · N419UA · Airbus A320232 · Fuselage Main, StructureSDR 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.Feb 16, 2015 · N419UA · Airbus A320232 · Fuselage Main, StructureSDR 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 MUFeb 15, 2015 · N414UA · Airbus A320232 · Fuselage Main, StructureSDR 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.Feb 11, 2015 · N414UA · Airbus A320232 · Fuselage Main, StructureSDR 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.Feb 11, 2015 · N414UA · Airbus A320232 · Fuselage Main, StructureSDR 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.Feb 11, 2015 · N414UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2015021293129Battery · dischargedEMERGENCY LIGHTS OPERATIONAL TEST FAILED. REPLACED LT EMER BATTERY LOCATED BY EMER EXIT IAW AMM 33-51-38, TESTED OK.Feb 11, 2015 · N413UA · Airbus A320232 · Emergency LightingSDR 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.Feb 8, 2015 · N415UA · Airbus A320232 · Emergency LightingSDR 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.Feb 8, 2015 · N415UA · Airbus A320232 · Emergency LightingSDR 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.Feb 7, 2015 · N495UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 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 OPERFeb 4, 2015 · N428UA · Airbus A320232 · Escape SlideSDR 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.Feb 1, 2015 · N493UA · Airbus A320232 · Fuel Control/Turbine EnginesSDR 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 BJan 31, 2015 · N404UA · Airbus A320232 · Elevator, Plate/SkinSDR 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 TJan 30, 2015 · N406UA · Airbus A320232 · Wing, Plate/SkinSDR 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.Jan 30, 2015 · N675AW · Airbus A320232 · Engine Mount SectionSDR 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.Jan 29, 2015 · N406UA · Airbus A320232 · Wing, Plate/SkinSDR 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 FULLJan 27, 2015 · N423UA · Airbus A320232 · Landing Gear SystemSDR 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.Jan 26, 2015 · N417UA · Airbus A320232 · Emergency LightingSDR 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.Jan 26, 2015 · N406UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 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%.Jan 24, 2015 · N421UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2015012793026Plate · corrodedNUMBER 2 RT AFT DOOR SILL PLATE HEAVY CORROSION. NR 2 RT AFT DOOR SILL PLATE REPLACED IAW SRM 51-72-11.Jan 24, 2015 · N441UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 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.Jan 23, 2015 · N451UA · Airbus A320232 · Emergency LightingSDR CALA2015012393009Door Sill · corrodedR2 DOOR SHAPE SILL HAS CORROSION AROUND FASTENERS. REPLACED DOOR SHAPE SILL IAW SRM 51-73-11.Jan 23, 2015 · N406UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2015012393010Fitting · corrodedR2 DOOR AFT SHAPE SILL CORNER FITTING FOUND CORROSION DURING REMOVAL. R & R CORNER FITTING IAW SRM 51-44-11 & 51-75-12.Jan 23, 2015 · N406UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2015012393017Epsu · faultedEMERGENCY LIGHT FAILED TEST, FAULTS CTR LT EPSU. REPLACED CTR LT EPSU & BATTERY IAW AMM 33-51-38, TESTED OK.Jan 22, 2015 · N482UA · Airbus A320232 · Emergency LightingSDR CALA2015012393020Charger · inoperativeD1L EMER EXIT LIGHT CHARGER INOPERATIVE, CICS. CHANGED CHARGER & BATTERY IAW MM33-51-38-401. OPERATIONS CHECKED GOOD.Jan 21, 2015 · N444UA · Airbus A320232 · Emergency LightingSDR CALA2015012393019Stringer · corrodedSTRINGER 31R AT FRAME 65 BELOW OUTFLOW VLV IS CORRODED. REPLACED FACTORY SECTION OF STRINGER IAW SRM 51-72-11.Jan 20, 2015 · N423UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 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.Jan 18, 2015 · N418UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 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.Jan 18, 2015 · N418UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 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.Jan 18, 2015 · N418UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 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.Jan 18, 2015 · N418UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 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.Jan 18, 2015 · N418UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 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 Jan 13, 2015 · N473UA · Airbus A320232 · Wing, Plate/SkinSDR 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.Jan 10, 2015 · N472UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 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 Jan 6, 2015 · N449UA · Airbus A320232 · Elevator, Plate/SkinSDR 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 INCHESJan 6, 2015 · N449UA · Airbus A320232 · Elevator, Plate/SkinSDR 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.Dec 22, 2014 · N652AW · Airbus A320232 · Fuel Control/Turbine EnginesSDR 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.Dec 21, 2014 · N634JB · Airbus A320232 · AC Generator-AlternatorSDR 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.Dec 21, 2014 · N478UA · Airbus A320232 · Engine (Turbine/Turboprop)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 DDec 21, 2014 · N476UA · Airbus A320232 · Turbine Engine Oil SystemSDR 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 HEDec 19, 2014 · N468UA · Airbus A320232 · Fuel System WiringSDR 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.Dec 18, 2014 · N446UA · Airbus A320232 · Wing, Plate/SkinSDR 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.Dec 15, 2014 · N652AW · Airbus A320232 · Engine Indicating System Wiring
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