IAE V2527-A5
Service difficulty reports · 8,011
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 2006UALA00219Skin · damagedDOOR 2R PUSHED WAS UP BY GROUND EQUIPMENT CAUSING A 2.5 INCH HIGH AND 30 INCH LONG BEND IN THE LOWER AFT EDGE OF THE DOOR. LOWER EDGE OF THE DOOR WAS ALSO BENT INBOARD 1 INCH. PERFORMED A DOUBLER REPAIR PER SRM 52-10-00-201. MAJOR REPAIR ON A PSE PER UNITEDSDR 2006UALA00148Battery · no testDURING 3 SVC EMERGENCY LIGHTS FAILED TEST, HAD EPSU BATT EMER L MESSAGE.SDR 2006UALA00138Skin · damagedPUNCTURE TO FUSELAGE SKIN FOUND ON LT SIDE BETWEEN BODY STATION 11100 TO 12167. APPROX FRAME 27 TO FR 29. DAMAGE ENCOMPASSES A 40 INCHES LONG HORIZONTAL INDENTATION, 21.5 INCH LONG X 15 PUNCTURE. DAMAGE IS ALONG SKIN LAP. MAJOR REPAIR DOUBLER INSTALLED IN ASDR 2006UALA00095Fuel Sys · unknownFLIGHT DIVERTED DUE TO UNPLANNED/UNEXPLAINED FUEL BURN. NO FUEL LEAK INDICATIONS NOTED. TASKS ACCOMPLIHSED WERE: DRIP STICK READINGS TAKEN ON ALL AIRCRAFT FUEL TANKS AND RESULTED IN ALL WITHIN LIMITS. REVIEWED POST FLIGHT REPORT FOR SIGNS OF FAULTS AND RESSDR 2006UALA00094Bracket · looseDIVERTED FLIGHT DUE TO NUMEROUS INSTRUMENT FAILURE MESSAGES. NOSE LANDING GEAR (NLG) TARGET 24GA AND 25GA MOUNTING BRACKET WAS FOUND EXTREMELY LOOSE. MAINTENANCE REPLACED UPPER BOLT TO NLG PROXIMITY SENSOR ASSEMBLY. ALL SYSTEMS WERE THEN TESTED WITH NO FURTHESDR 2006UALA00089Stop · out of adjustDOOR 2R NOISY AND ECAM SHOWED SLIDE DISARMED FOR SHORT TIME DURING DESCENT. FLIGHT ATTENDANTS REPORTED A DOOR SQUEAL STARTED AT THE SAME TIME. ADJUSTED DOOR STOPS PER AMM TO IMPROVE SEAL COMPRESSION AND IMPROVE DOOR HANDLE SECURITY. BOTH IMPROVEMENTS WOULD SDR 2006UALA00086Light · no testEMERGENCY LIGHTS FAIL 3 SERVICE TEST.SDR 2006UALA00062Light · inoperativeEMERGENCY LIGHTS EEL LT SIDE 5 ROWS OF SEATS.SDR 2006UALA00060Seal · leakingFLIGHT DIVERTED DUE TO LOSS OF GREEN SYSTEM HYDRAULIC PRESSURE. LOSS OF GREEN HYD SYSTEM. FOUND EDP LEAKING AT MATING FLANGE. REPLACED PUMP REF MM29-11-51. RAN ENG, NO LEAKS, LEVELS NORMAL.SDR 2006UALA00056Skin · damagedFOUND DAMAGE APPROX 4 FEET AFT OF AFT CARGO DOOR AT STA 29896-FR63 BETWEEN STRINGERS 39R AND 41R. MAJOR REPAIR. REPAIRED STR 39R BETWEEN FR 62 & 63 PER SRM 53-00-13 FIG201. INSTALLED SKIN DOUBLER REPAIR PER SRM 53- 00-11 FIG 209 & 211.SDR 2006UALA00068Skin · dentedFWD FUSELAGE IS DENTED 24 INCHES BELOW CAPTAINS SLIDING WINDOW. INSTALLED DOUBLER PER SRM 53-00-11.SDR 2006UALA00037Light · no testEMERGENCY LIGHT TEST FAILED WITH - INT LOAD AFT LT .SDR AWXA200600016Power Supply · unknownDURING OVERNIGHT INSPECTION, DISCOVERED THE RT CABIN AND OVER WING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT CABIN EPSU AND BATTERY IAW TASK CARD R1C33303. OPERATIONAL CHECKS WERE GOOD. DID NOT CONFIRM FAULT. UNIT WAS INSPECTED ASDR AWXA200600017Power Supply · inoperativeDURING OVERNIGHT INSPECTION DISCOVERED THE LT OVERWING EMERGENCY POWER SUPPLY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT CABIN EPSU AND BATTERY IAW AMERICA WEST AIRLINES TASK CARD R1C333034. OPERATIONAL CHECKS WERE GOOD. VENDOR COULD NOT CONFIRM FSDR 2006UALA00021Battery · inoperativeEMERGENCY LIGHT TEST FAILS -AFT LT BATTERY FAULT- MSG SHOWN.SDR 2006UALA00008Engine · leakingFLIGHT DIVERTED DUE TO NR 1 ENGINE OIL LEAK. NUMBER 5 BEARING CARBON SEAL HOUSING WAS FOUND TO BE OUT OF DIMENSION, DEFLECTED, AND SCORED. IT PERMITTED AN OIL PATH TO EXIST AT THE HOUSING/TURBINE EXHAUST CASE(TEC) ATTACHMENT FLANGE. ONCE PAST THE FLANGE OILSDR YENA200590Electrical Box · malfunctionedEGT IND FLUCTUATED BETWEEN 190-490 DEGREES AFTER TAKEOFF, WENT AS LOW AS 75 DEGREES DURING RETURN. T/S IAW AMM 77-21-43-05. REPLACED JUNCTION BOX IAW 77-21-43-04. OPERATED LEFT ENG AT VARIOUS POWER SETTINGS, ALL EGT PARAMETERS NORMAL. OK FOR SERVICE.SDR YENA200589Bleed Valve · failedAFTER TAKEOFF EN ROUTE TO LGB EXPERIENCED NR 1 ENGINE STALL WITH FULL RECOVERY. A/C AT 11,000 FEET AND 300 KTS. RETURNED TO JFK. PERFORMED TSM TASK 71-00-810-808. CHECKED 7A, 7B, 7C BLEED VALVE AND SOLENOID REF AMM 75-32-52. FOUND 7B VALVE FAILED. REPLACSDR 2005UALA01502Uplock · failedGEAR NOT UPLOCKED DISPLAYED ON UPPER ECAM SCREEN. REPLACED LANDING GEAR SEL. VALVE 40GA PER MM32-31-12.OPS CKS GOOD IND. CKS GOOD.ACPD NORMAL GEAR RETRACT-EXTEND 10 TIMES.ACPD ALT. GEAR EXT. ALL CKS GOOD.SDR 2005UALA01510Servo Valve · oscillatesRETURNED TO FIELD DUE TO AILERON VIBRATION. RT GREEN AILERON SERVOCONTROL SERVO VALVE WAS FOUND OSCILLATING, THUS CAUSING INFLIGHT AILERON VIBRATION. REPLACEMENT OF THE SERVOVALVE RESOLVED THE PROBLEM. NO FURTHER ANOMALY WAS REPORTED.SDR AWXA200501606Servo · inoperativeEMERGENCY LANDING, CREW REPORTED NOSE WHEEL FAULT, PERFORMED TWO FLYBYS TO VERIFY NOSE GEAR LOCATION AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED AND WAS TOWED TO THE GATE. NO FURTHER EVENTS OCCURRED. MAINTENANCE REMOVED AND REPLACED THE NLG SERVO CONTROLSDR 2005UALA01479Battery · no testDURING 3 SVC EMERGENCY LIGHT TEST RECEIVED FAILURE, BATTERY EMERGENCY RT. REPLACED BATTERY PACK. REPLACED BATTERY PACK.SDR 2005UALA01499Lanyard · disconnectedAFT RT DOOR SLIDE GIRT BAR HANDLE RELEASE PIN & LANYARD WERE NOT CONNECTED. DOOR R2 SLIDE ASSY MR25614-1275 WAS INSTALLED IN DEN ON 12/9/2004 TO REPLACE SLIDE ASSY MR25614-158, WHICH HAD TO BE REMOVED DUE TO TIME. PER AMIS, THE SLIDE REPLACEMENT WAS ACCOMPLSDR 2005UALA01472Skin · corrodedLEFT AIRPHONE ANTENNA SKIN MATING SURFACE HAS MINOR SURFACE CORROSION. INSTALLED DOUBLER REPAIR PER SRM 53-00-11 FIG 203.SDR 2005UALA01473Odor · detectedSTRONG ELECTRICAL SMELL IN THE COCKPIT AND IN THE CABIN. JUST PRIOR TO SMELL, BOTH MCDU'S DUMPED ALL INFO. AFTER DESCENT, RECEIVED PITOT HEAT MSG FOR THE CAPT & F/O SIDE. ACCOMPLISHED HIGH POWER RUN BOTH ENGINES PER JET RUN-UP HANDBOOK. NO SMELLS OR SMOKE WSDR 2005UALA01471Skin · scratchedLARGE DEEP SCRATCHES APPROXIMATLEY 24-28 INCHES LONG APPROXIMATELY 8 INCHES BEHIND FWD FUSELAGE BULKHEAD JUST AFT OF NOSE RADOME, FROM BELOW WATER LINE TO JUST BELOW RVSM AREA LT SIDE OF FUSELAGE. MAJOR REPAIR REPORTING. BLENDED SCRATCHED AREA PER SRM 53-11-SDR 2005UALA01452Light · illuminatedEPSU EMER R DISPLAYED AFTER EMERGENCY LIGHT TEST. REPLACED POWER SUPPLY AND BATTERY AT RH OVER WING EXIT.SDR 2005UALA01447Bulkhead · ground damageBULKHEAD DAMAGE AT STATION 350 APPROXIMATELY 14 INCHES RIGHT OF FR 1. DAMAGE CAUSED BY IMPACT WITH GROUND EQUIPMENT. HORIZONTAL STIFFENER REPLACE, BULKHEAD WEB DOUBLER INSTALLED, FRAME REPAIR, AND VERTICAL STIFFENER DOUBLER INSTALLED.SDR AU510001766Hinge Pin · loose(AUS) 103VU PANEL HINGE PIN LOOSE. NO CONTACT WITH ADJACENT ELECTRICAL HARNESS. FOUND DURING INSPECTION IAW AD/A320/175.(AD/SB DESC: AD/A320/175 ) (CASA NR 510001766)SDR AU510002220Valve · faultyNR 2 ENGINE BLEED SYSTEM FAN AIR VALVE SUSPECT FAULTY.SDR 2005UALA01432Smoke · detectedLOUD VIBRATION HEARD FOLLOWED BY SMOKE SMELL IN THE COCKPIT. BLOWER SWITCH DIDN'T GO INTO OVERRIDE ON AVIONICS VENT. ALSO HAD ECAM AMBER INDICATIONS ON PRESS PAGE FOR INLET AND EXTRACT VALVES. SMOKE REPORTED IN FLIGHT DECK AFTERWARDS. SYSTEM DIDN'T GO INTO SDR 2005UALA01433Light · inoperativeEEL LIGHTS AT SEATS 4, 5, 8, 9, 15, 16, 17, 21, 22 AND 23 ARE INOPERATIVE. REPAIRED SHORT UNDER SEAT 8A AND REPLACED 110WL2.SDR 2005UALA01424Unknown · unknownDIVERTED DUE TO NUMEROUS FAULT LIGHTS. SYSTEM TESTS OF FLIGHT WARNING COMPUTERS, RADIO ALTIMETERS AND ENHANCED GROUND PROXIMITY WARNING COMPUTER. RADIO ALTIMETER ANTENNA CHECKED. ENHANCED GROUND PROXIMITY WARNING COMPUTER REPLACED. SYSTEM OPERATION NORMAL TO SDR 2005UALA01412Control Unit · malfunctionedRETURN TO FIELD DUE TO SHOCK ABSORBER FAULT MESSAGE. TROUBLESHOOTING OF NOSE GEAR LOG. JACKED NOSE AND SWUNG GEAR NUMEROUS TIMES, NO FAULTS FOUND. SHOOK OUT WIRING ON NOSE GEAR, NO FAULTS. SEE ITEM FOR SVCING STRUT, PER SFOLM SWANN, REPLACED NR 2 LGCIU PRSDR YENA200585Odor · detectedF/A'S REPORT ACRID BURNING SMELL ON A/C RT AT ROWS 20 OR 21. LIVE TV TURNED OFF, SMELL WAS INTERMITTENT FROM THEN ON. ACCOMPLISHED WITH TSM 23-39-00-810-801 NO DISCREPANCIES NOTED. REMOVED AND REPLACED SB AT 20 AND 21 DEF AND VDU AT 20 DEF AND 21 DEF AS PRECAUSDR AWXA200501482Servo · failedON CLIMB, FELT VIBE IN RUDDER PEDALS. TURNED A/P OFF, INCREASED PITCH OF AC TO SLOW DOWN TO 270 IAS & FL 330, VIBE STOPPED. INSP AC & ELEV SERVO HINGE BRGS FOR CONDITION IAW MM. AC FERRIED BACK FOR REPAIR. DURING FERRY FLT, REPORTED AC CRABBING 2 DEGREES TOSDR AWXA200501574Sill · corrodedSAL - MAJOR REPAIR - DURING BC4 CHECK DISCOVERED CORROSION ON BULK CARGO DOOR SILL, AROUND NUT PLATES, AT FR 61+9.5 AND Y-640. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-44-49 PAGE 403 FIG 101. FABRICATED DOUBLER AND FISDR AWXA200501576Sill · corrodedDURING BC4 CHECK DISCOVERED CORROSION ON THE LOWER SILL AT FR 68-3 INCHES AND Y1732 ON THE LT SIDE OF CABIN. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14 FIG 101. FABRICATED ANGLE AND FILLERS IAW SRM 53-41-14. INSTALLED FABRISDR AWXA200501577Sill · corrodedDURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON THE LOWER SILL, RT SIDE OF CABIN, AT FR 66 AND Y-1732. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14. FABRICATED ANGLE AND FILLERS IAW SRM 53-41-14. INSTALLED FABRICATSDR AWXA200501580Beam · corrodedDURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION LOCATED ON BEAM ASSEMBLY AT FR 68 AND Y-765. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 FIG 102. REMOVED AND INSTALLED NEW BEAM ASSEMBLY FROM FR 66+5 INCHES TO FR 70 ANDSDR AWXA200501581Beam · corrodedDURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION LOCATED ON BEAM ASSEMBLY AT FR 68 AND Y1162. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 FIG 102. REMOVED AND INSTALLED NEW BEAM ASSEMBLY FROM FR 68 TO FR 69 AND Y1162 SRSDR 2005UALA01395Light · brokenEEL LIGHT ASSY BROKEN AT 9C. REPLACED LIGHT ASSY.SDR AWXA200501575Floorbeam · corrodedDURING BC-4 CHECK DISCOVERED CORROSION ON THE FLOORBEAM LOCATED AT FR 16 AND Y254. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 PAGE 109, FIG 104. MAINTENANCE CUT OUT DAMAGED AREA IAW SRM 53-11-14. FABRICATED ANGLES AND SUPPOSDR AWXA200501578Rail · corrodedDURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION LOCATED ON RAIL ASSEMBLY AT FR 16 AND Y503.2. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 103. REMOVED AND INSTALLED NEW RAIL ASSEMBLY AT FR 16 AND Y503.2 IAW SRM 51-SDR 2005UALA01390Cabin Pressure · malfunctionedCABIN PRESSURE PROBLEM. WHILE ON CLIMB OUT FLIGHT EXPERIENCED VENT SKIN VALVE FAULT, WHICH CAUSED A BLOWER FAULT. BLOWER WOULDN'T GO TO OVERRIDE. 'INLET' WORD ON PRESS PAGE IS AMBER. ACCOMPLISHED TSM 21-26-00-810-801 AND REPLACED AEVC (MR21002, 482-9059) PSDR 2005UALA01393Light · inoperativeEMERGENCY LIGHTS AT SEATS 15-17, 20-23 INOPERATIVE. REPLACED EEL POWER SUPPLY.SDR AWXA200501582Seat Track · corrodedDURING BC4 CHECK DISCOVERED CORROSION ON THE RT IB SEAT TRACK AT FR 39+5 INCH AND Y-765. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-31-15 FIG 101, PAGE 102. REMOVED AND INSTALLED NEW SEAT TRACK BETWEEN FR 36 AND FR 41, ALSO AT Y-SDR AWXA200501607Seat Track · corrodedDURING BC4 CHECK DISCOVERED CORROSION ON RT OB SEAT TRACK AT FR42+1 INCH. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-31-15 FIG 101. REMOVED AND INSTALLED NEW SEAT TRACK FROM FR 41 TO FR 47 AND Y-1292 IAW SRM 51-72-11.SDR 2005UALA01384Sill · corrodedAFT RT GALLEY DOOR THRESHOLD SILL PLATE WAS FOUND CORRODED THROUGH AT FASTENER HOLE. REPLACED DOOR SILL PLATE REF SRM 51-42-14.SDR 2005UALA01385Skin · dentedA 4 X 5 X .25 INCH DENT NOTED ON RT SIDE OF FUSELAGE IN THE AREA OF THE RVSM MARKINGS. DENT STARTS APPROX 2.75 INCHES AFT OF 4TH FRAME RIVET ROW AND STOPS .25 INCH FROM 5TH FRAME RIVET ROW. BOTTOM OF DENT TOUCHES WATER LINE RIVET ROW. REPAIR WAS ACCOMPLISHE
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