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 UALA2012030101275Computer · faultyELECTRICAL ODOR, FLIGHT DIVERTED. ACCOMPLISHED VISUAL INSPECTION OF AREA INCLUDING HARNESS AND CONNECTORS PHC NR 2 THAT WAS FOUND TO BE OVERHEATED. STRONG ACRID ODOR COMING FROM PHC NR 2. NO OTHER DEFECTS NOTED. SEE SEQ 0662001 FOR REPLACEMENT OF PHC NR 2SDR UALA2012022901257Switch · dirtyENG 1 AGENT DISCHARGE LIGHT ILL. DISCHARGE LIGHT ON INTERMITTENTLY WITH PUSH OF TEST BUTTON ON OVERHEAD FIRE PANEL. CLEANED TEST SWITCH AND ACCOMPLISHED TEST OF ENG-1 LOOP-SQUIB OPERATIONAL TEST. TESTS NORMAL.SDR UALA2012022901246Switch · faultyENG 1 AGENT DISCHARGE LIGHT ILL. DISCHARGE LIGHT ON INTERMITTENTLY WITH PUSH OF TEST BUTTON ON OVERHEAD FIRE PANEL. CLEANED TEST SWITCH AND ACCOMPLISHED TEST OF ENG-1 LOOP-SQUIB OPERATIONAL TEST. TESTS NORMAL.SDR UALA2012030101273Wire · damagedROW 37 A-C EMERGENCY LIGHT WIRING CUT. FOUND THE INSULATION ON ONE WIRE WAS DAMAGED. INSTALLED ELECTRICAL TAPE. NO STRANDS OF WIRE WERE CUT. REPAIR THE CABLE PER MM 20-53-20.SDR UALA2012030101287Converter · faultyCAPT WIPER MOTOR INOP, REMOVED CAPT WIPER MOTOR, STDBY INSTRUMENTS BACKED BUT NOT RMV'D. OLD PART IS IN COCKPIT. RPL'D CAPTS WIPER MOTOR CONVERTER PER MM. REPLACED CAPTS WIPER ARM, OPERATES NORMALLY.SDR UALA2012030101278Slide · misinstalledDOOR 1L SLIDE PACK IS IMPROPERLY INSTALLED ON LOWER PIN OR PIN IS DAMAGED CAUSING SLIDE TO LIFT UP. REMOVED AND REPLACED SAME SLIDE PER MM.SDR UALA2012022801238Structure · damagedMAJOR REPAIR. INSTALL DOUBLER AT FORMER LT ANTENNA LOCATION PER 4079C AND SRM 53-00-11 FIG 238. INSTALLED DOUBLER REPAIR. MUST BE RE-INSPECTED AT 60000C FROM REPAIR EMBODIMENT. CURRENT PTC 22274.SDR UALA2012022901261Skin · damagedINSTALL DOUBLER REPAIR AT FORMER RT ANTENNA LOCATION PER 40795C AND SRM AND ECRA 5341-01012. MAJOR REPAIR: INSTALLED DOUBLER REPAIR PER SRM AND ECRA 5341-01012. MUST BE RE-INSPECTED AT 59900C PER SRI 53-00-11 TABLE 246 PG 355. CURRENT PTC22193.SDR UALA2012022901262Structure · damagedINSTALL DOUBLER AT FORMER LT ANTENNA LOCATION PER 40795C AND SRM. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. MUST BE RE-INSPECTED AT 60,000C FROM REPAIR EMBODIMENT. CURRENT PTC 22193.SDR UALA2012022801239Doubler · damagedFORMER VERIZON ANTENNA LOCATION HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. MUST BE RE-INSPECTED AT 59900C PER S RI 53-00-11 TABLE 246. CURRENT PTC 22274.SDR UALA2012022901249Skin · corrodedFUSELAGE SKIN CORROSION AT WASTE TANK VENT FR 69-70 RT SIDE. MAJOR REPAIR ACCOMPLISHED. MAINT TEXT: INSTALLED REPAIR PER SRM. REQUIRES RE-INSPECTION PER SRI. INSTALLED DOUBLER REPAIR PER SRM. INSPECT AT 53900 PER REPAIR EMBODIMENT. CURRENT PTC 22274.SDR UALA2012022801232Battery · dischargedEPSU BATTERY AFT L MESSAGE DISPLAYED ON EMERGENCY LIGHT TEST. REPLACED AFT LEFT EPSU BATTERY.SDR UALA2012022901264Oxygen Mask · misinstalledOXYGEN MASKS DROPPED AT ROW 31 DEF. COMPLIED WITH MAINT TIP 35-003 DROP TEST DUE IN 3D. INSTALLED MASK O2 PROPERLY CHECK CONTAINER O2 MASK ALL OK AND PERFORMED OPERATIONAL CHECK IAW AMM.SDR UALA2012022901265Floorboard · damagedFLOOR IN FIRST CLASS CABIN IS SOFT AND SPONGY. REPLACED FLOORBOARD.SDR UALA2012022801219Doubler · damagedPRE-EXISTING EXTERNAL DOUBLER REPAIR BETWEEN FRAMES 29-30 AT STR 31L-25L. MAJOR REPAIR ACCOMPLISHED. REPLACED EXTERNAL DOUBLER. RE-INSPECTION REQUIRED PERM SRI 53-21-11 TABLE 208. AT 60,000 C. FROM REPAIR EMBODIMENT. CURRENT PTC 22193.SDR UALA2012022801223Wire · brokenCABIN - NR 2 RT PAX-CREW DOOR SLIDE- RAFT P/N MR25115-028 ELECTRICAL WIRES ARE BROKEN. FROM BASE WRITE-UP L3760M. (NOTE: WIRES APPEAR TO HAVE BEEN BROKEN WHILE SLIDE RAFT WAS IN STORAGE DURING DOOR MAINTENANCE. REPLACED 2R DOOR SLIDE.SDR UALA2012022701169Seat · defectiveCAP SEAT RECLINE INOP DEFECTIVE RATCHETS AND DIFFICULT TO ADJUST. REPLACED SEAT IN REF TO AMM, OPS CHECK NORMAL.SDR UALA2012022901258Computer · faultySPOILERS ARMED DID NOT DEPLOY ON TOUCHDOWN. SAMC TEXT: PERFORM EFCS GRD SCAN PER MM AND OPS TEST OF SEC 3 PER AMM. REPLACED SEC 3 PER AMM, TESTED OKAY.SDR UALA2012022701192Actuator · leakingNR 2 ENG PH-LP ACTUATOR IS LEAKING FUEL FROM ACTUATOR. REPLACED ACTUATOR, LEAK CHECKED GOOD.SDR UALA2012022701155Container · crackedLT OFF WING EMERGENCY ESCAPE SLIDE CONTAINER IS CRACKED, ALONG AFT EDGE. REPLACED LT OVERWING SLIDE IAW MM, OPS CHECK GOOD. ACCOMPLISH RII INSPECTION OF AMIS ITEM 8252008: RPLC'D LT OVERWING SLIDE IAW MM. OPS CHECK GOOD. ACP RII PER AMM 25-62-42.SDR UALA2012022701156Stringer · damagedAFT PIT, AT FRAME 65, STR 31R IS EXFOLIATED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED STR. INSTALLED NEW STRINGER.SDR UALA2012022801214Bearing · wornACFT OUT OF TRIM AFTER TEST HOP. RT AILERON STILL HAS .300" UPWARD PLAY. MAX UPWARD TRAVEL IS .078". AILERON HINGES 1-3 WORN. REPLACED 1, 2 AND 3 HINGE SUPPORT SLEEVES AND BEARING REF MT57-016. REPLACED RT NR 2 O/B HINGE FITTING BUSHING PER GNMM. REPLACSDR UALA2012022701185Door · damagedUNABLE TO CLOSE DOOR TO F/O`S O2 MASK, IT IS STUCK BEHIND SLIDING WINDOW. REPAIRED BY REPOSITIONING O2 MASK DOOR.SDR UALA2012022401124Oxygen Mask · leakingF/O'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). CREW COMMENTS: HARNESS CLIP IS BROKEN HARNESS NOT ATTACHED AT TOP LEFT TEMPLE. SWAP F/O MASK WITH 2ND OBSERVER MASK. COMPLY WITH MEL FOR 2ND OBS SEAT. SWAPPED F/O WITH 2ND OBSERVER MASK. 2ND OBS SEAT BSDR UALA2012022301092Cover · crackedRUDDER PEDALS JAMMED DURING FLARE. INORDINATE FORCE REQ'D TO MOVE PEDALS. UNSAFE FOR FLIGHT. RUDDER PEDAL ADJUSTMENT FOOTREST IS LOOSE AND PUSHES PEDALS AT TIMES. FIRST OFFICERS RUDDER PEDALS WILL NOT ADJUST. RUDDER PEDAL ADJ IS NOT AFFECTED, COVER BETWEENSDR UALA2012022301103Interface Unit · faultyNR 2 ENG FIRE LIGHT AT ENG MASTER SWITCH DOES NOT ILLUMINATE DURING TEST. REF TSM 26-12-00, AWM 26- 12-02, MM33-14-33 AND MM 33-14-00, FOUND ANNUNCIATOR LIGHT TEST AND INTERFACE BOARD AT FAULT. INSTALLED NEW BOARD AND TESTED, OP CK'S NORMAL.SDR UALA2012030501328Fire Loop · defectiveINTERMITTANT DISPLAY OF ECAM ENG2 FIRE LOOP 'A' FAULT. MEASURED RESISTANCE AT FDC 2 BTWN PIN J AND K, OHMS READ 1510, IS WITHIN LIMIT NEED MORE T-S TIME. NO HARD FAULT. VISUAL INSPECTION OF FIRE LOOPS CHECKS GOOD. REPLACED FIRE LOOP 4001WD2. OPS CHECKS GSDR UALA2012022101055Window · out of toleranceLT FIREX WINDOW DAMAGED. REMOVED AND REPLACED LT FIREX WINDOW.SDR UALA2012022101063Sliding Window · delaminatedCAPTAIN'S SLIDING WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS, DELAMINATION EXTENDS 3.5 INCH FROM EDGE. OUT OF SERVICEABLE LIMITS PER MM. REPLACED CAPTAIN'S SLIDING WINDOW PER AMM.SDR UALA2012022101065Actuator · out of adjustIN CLIMB AND CRUISE, ACFT FLYS IN 1 DEGREE RT BANK. RUDDER TRIM AT L1.7 DEGREES. AUTOPILOT ON. RUDDER TRIM GRIPE AND MT 27-018 FOUND RUDDER NEUTRAL POSITION NOT ALIGNING WITH REFERENCE TRIANGLE. WITH ALL RIG PINS INSTALLED FOUND RUDDER NOT ALIGNED, INSTALLSDR UALA2012022001007Stringer · corrodedAFT PIT STRINGER 42L AT FRAME FR 57 IS CORRODED BEYOND LIMITS OF SRM. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOUND MATERIAL REMAINING TO BE BEYOND LIMITS OF SRM 53-00-00. REMOVED DAMAGED STRINGER SECTION, FABRICATED A NEW STRINGER AND SPLICE SECTISDR UALA2012022001043Slide · unsecureON LANDING, SLIDE AT L2 DOOR CAME LOOSE FROM DOOR. TO REPLACED L2 DOOR SLIDE PER AMM. RIG AND OPS CHECKED IAW AMM. REF ICS GROUP NR 1 OP AND INDICATION NORMAL.SDR UALA2012022101044Stringer · corrodedAFT PIT CENTERLINE STRINGER 43 BETWEEN FRAMES FR 54 TO FR 56 IS CORRODED. REMOVED CORROSION AND FOUND MATERIAL REMAINING TO BE OUT OF LIMITS PER SRM. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED A NEW STRINGER SECTION AND SPLICE ANGLES AND INSTALLED.SDR UALA2012022101045Container · no testRT SEAT ROWS NR 1 & 2 - O2 CONTAINER FAILED TO OPERATE DURING MANUAL RELEASE TEST. REPLACED CONTAINER ASSY PER MM. OPS CHECKED GOOD.SDR UALA2012022101046Stringer · corrodedAFT PIT STRINGER 42R BETWEEN FRAMES FR 63 AND FR 64 IS CORRODED. REMOVED CORROSION AND FOUND MATERIAL REMAINING TO BE OUT OF LIMITS PER SRM. REMOVED DAMAGED STRINGER SECTION, FABRICATED A NEW STRINGER SECTION AND SPLICE ANGLES AND INSTALLED PER SRM.SDR UALA2012022101054Tip Cap · damagedLEFT WING TIP ASSY SUSTAINED DAMAGE. REPLACED WINGTIP PER AMM.SDR UALA2012022001000Unknown · malfunctionedGEAR NOT DOWNLOCKED DISPLAYED ON UPPER ECAM SCREEN - L-G CREW COMMENTS: ON TAKEOFF AFTER AIRBORNE GOT MOMENTARY L-G GEAR NOT DOWNLOCKED ECAM WITH ASSOCIATED ALARMS. ACCOMPLISHED LANDING GEAR FUNCTIONAL TEST PER MM, NO FAULTS NOTED.SDR UALA2012022001009Slide · misrepairedINBOUND INSPECTION FOUND THE RT OVERWING SLIDE BALL LOCKS PAINTED OVER. WILL NEED SLIDE REPLACED BEFORE NEXT REVENUE FLIGHT. WALKAROUND INSPECTION COMPLETE, NO DEFECTS NOTED. REPLACED RT ESCAPE SLIDE.SDR UALA2012022001011Pan · crackedFWD LAV FLOOR IS CRACKED. GAINED ACCESS TO LAV FLOOR PAN, PER AMM. REPLACED FLOOR PAN AND INSTALLED LAV ASSEMBLY PER MM AND REINSTALLED CEILING BRACKETS PER MM.SDR UALA2012022101056Floor Panel · delaminatedFOUND CARGO PIT ENTRY WAY FLOOR PANEL VERY SOFT AND DELAMINATED APPROX 12 INCHES BY 12 INCHES AREA JUST INBD OF FWD CARGO DOOR AFT JAMB. REPLACED FLOOR BOARD.SDR UALA2012022001021Floor Panel · damagedAFT CABIN FWD LAVATORY FLOOR IS SPONGY. NO EVIDENCE OF LIQUID LEAKING. REMOVED LAVATORY FROM STRUCTURE, ACCOMPLISHED FLOOR PAN REPLACEMENT.SDR UALA2012022000982Pin · missingD' RING MISSING ON COCKPIT DOOR FOR PIN IN ESCAPE PANEL. REMOVED AND REPLACED OUTBOARD PIN, OPS GOOD.SDR UALA2012022000991Frame · corrodedFRAME 58 CORRODED AT STRINGER 43L. MAJOR REPAIR ACCOMPLISHED LNSTALLED REPAIR PER SRM 53-00-12 FIG 201 ON NR #'S V1974J, V1464I BY 395820 AND INSPECTED. MUST BE RE-INSPECTED AT 60000C FROM REPAIR EMBODIMENT CURRENT PTC IS 22107.SDR UALA2012022001028Slide · delaminatedRT OVERWING SLIDE ASSY HAS MULTIPLE POINTS ON OUTER FACE WITH DELAMINATION AND IS DEBONDED. REMOVED AND REPLACED RIGHT OVERWING SLIDE. OP CHECKED GOOD IAW AMM.SDR UALA2012022001029Selector Valve · leakingMLG GEAR DOOR SELECTOR MANIFOLD ASSY LEAKING. REMOVED AND REPLACED MLG DOOR SELECTOR VALVE. LEAK AND OPS CHECKED GOOD IAW MM.SDR UALA2012022000970Battery Pack · dischargedEMERGENCY LIGHT SYSTEM WILL NOT TEST SUCCESSFULLY, GIVES EPSU BATT AFT L ATA 33-51-38 MESSAGE. REPLACE BATTERY PACK.SDR UALA2012022000981Frame · damagedPRE-EXISTING FRAME REPAIR TO FR 76 BETWEEN STR 32L TO 32R. REMOVED EXISTING REPAIR PER SRM. PERFORMED ROCKWELL INSPECTION TEST AND VERIFIED 3 EACH REPAIR ANGLES ARE 2024-T4, REF: GN-MM 1-0-7-003. REINSTALLED SAME REPAIR PARTS PER SRM 53-00-12, FIG 203 ON NONSDR UALA2012022000975Power Supply · inoperativeEMERGENCY EXIT LIGHTS ON WITH SWITCH OFF. REPLACED POWER SUPPLY UNIT PER AMM, OPS GOOD.SDR UALA2012022000980Skin · dentedDENT IN FUSELAGE SKIN BETWEEN FRAME STATIONS FR 63- TO FR 64 RT & STR 31R. EVALUATED DENT AND REWORKED SKIN PER SRM, TABLE 101 AND PARA. 4.I. ACCOMPLISHED HFEC PER NDT 6-51-10-08 AND NO CRACKS FOUND. DOCUMENTED ON NON ROUTINE V1445I. PER SRM 53-41-11, TABLSDR UALA2012022001030Computer · faultedAVIONICS VENT FAULT, FLIGHT DIVERTED. REPLACED AVIONICS EQUIPMENT VENTILATION COMPUTER AND TESTED SEVERAL TIMES WITH NORMAL INDICATION.
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