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 UALA2011120106610Oxygen System · leakingCREW OXYGEN SYSTEM LOW 1120 PSI. FOUND SLIGHT LEAK AT F/O O2 MASK BOX AND BOX WOULD TEST INTERMITTENTLY. REPLACED BOX AND MASK ASSY.SDR UALA2011112906538Thrust Reverser · debondedNR 1 ENG RT REV HALF FWD EDGE HAS DISBONDED FROM 6 O'CLOCK TO 11 O'CLOCK, SHEETMETAL UNDER BLOCKER DOORS HAS TORN BACK APPROX 4\ DEEP FROM FWD EDGE. REPLACED NR 1 ENG INBOARD REV HALF PER MM WITH UNIT ROBBED FROM AC 4628.SDR UALA2011120106611Control Panel · malfunctionedCIDS FAULT LIGHT. FAULTED FWD FLIGHT ATTENDANT PANEL. REPLACED F/A PANEL FAULT CLEARED, ALL OPS NORMAL.SDR UALA2011112906539Switch · stickingAFT LAVATORY DOESN’T STOP FLUSHING, THE PROBLEM IS THE FLUSH BUTTON, IT STICKS IN THE 'ON' POSITION, RESET TOILET VACUUM SYS CIRCUIT BREAKER, OPS CHECKED OKAY.SDR UALA2011112906560Oxygen Mask · defectivePORTABLE OXYGEN BOTTLE MASK DEFECTIVE - OXYGEN CREW COMMENTS: AFT BOTTLE MISSING FACE MASK, HAS CANULA. REPLACED AND SECURED.SDR UALA2011112906537Shoulder Belt · damagedFLIGHT ATTENDENT JUMPSEAT AT L1 DOOR NEEDS NEW SHOULDER HARNESS. REPLACED SHOULDER HARNESS.SDR UALA2011112706480Buffer · faultyF/O RUDDER PEDALS DO NOT SELF ADJUST OUT. REPLACED RUDDER PEDAL POSITION BUFFER, OPS CHECKED OKAY.SDR UALA2011112706528Buffer · stuckCAPTAIN'S RUDDER PEDAL ADJUSTMENT RESET IS STICKING. REPLACED CAPTAIN RUDDER PEDAL POSITION BUFFER, OPS CHECKED OKAY.SDR UALA2011112906552Computer · malfunctionedWHILE ON THE GATE LEFT TANK FUEL QTY IN BOTH INNER AND OUTER TANKS WENT INOP. SAMC TEXT: ALSO HAVE TXFR VALVE OPEN ECAMS WHEN QTY GOES INOP. REPLACED FQIC COMPUTER. ALL INDICATIONS NORMAL & ECAM MESSAGES CLEARED.SDR UALA2011112906553Drain Valve · not seatedFUEL DRIPPING NEAR NACA OUTLET ON LEFT WING. FOUND FUEL LEAKING FROM THE OUTBOARD FUEL WATER DRAIN VALVE. RESEATED VALVE. NO LEAK NOTED AFTER 5 MIN. THIS WAS THE LEFT WING SURGE TANK WATER DRAIN VALVE.SDR UALA2011112706523Lamp · inoperativeAPU FIRE LIGHT ON EXT SERVICE PANEL INOPERATIVE. RELAMPED, OPS CHECKED OKAY.SDR UALA2011112706467Oxygen Mask · no testOXYGEN MASKS DROPPED, COMPLIED WITH MAINT TIP 35-03. ACCOMPLISHED MASK DROP REF AMM 35-23-00-710-001. 23ABC AND AFT FLIGHT ATTENDANT PANELS DID NOT DEPLOY - REPACKED. AFTER REPACK TESTED CABIN TWICE MORE AND ALL MASKS DEPLOYED.SDR UALA2011112706473Seat · failedCAPTAIN'S SEAT LUMBAR ADJUSTMENT, STICKS AND IS INOPERATIVE. MECHANISM BROKEN INSIDE. REPLACED CAPTAINS SEAT ASSY PER AMM. OPERATIONAL CHECKED NORMAL. INSTALLED SAFETY VEST IN NEW SEAT ASSY.SDR UALA2011112706520Oxygen Mask · failedF/O FORWARD O2 MASK WILL NOT INFLATE. REPLACED F/O'S FULL FACE O2 MASK AND O2 BOX PER AMM. OPS CHECKED GOOD.SDR UALA2011112706521Windshield Wiper · inadequateCAPTAINS WINDSHIELD WIPER BLADE DOES NOT CLEAR RAIN FROM GLASS. NO CONTACT ON 3 INCHES+. REPLACED WIPER BLADE.SDR UALA2011112706522Unknown · odorF/A REPORT AN ELECTRICAL ODOR WHEN PACKS ARE TURNED ON WITH APU PROVIDING AIR. RAN PACK 2 WITH AC DOOR CLOSE AND NO ODOR NOTICED.SDR UALA2011112706514Buffer · failedF/O RUDDER PEDALS DON`T ADJUST PROPERLY. REPLACED F/O RUDDER PEDAL ADJUSTMENT BUFFER, OPS CHECKED OKAY.SDR UALA2011112706505Fairing · unsecureFOUND LEFT WING INBD FLAP TRACK FAIRING LATERAL MOVEMENT OUT OF LIMITS. LATERAL MOVEMENT MEASURES (.562 INCHES) LIMIT IS .449 INCHES. REMOVED PANEL 531AT DISCONNECTED CONTROL AND SIDESTAY RODS MOVEABLE FLAP TRACK FAIRING LOWERED AND HELD UP IN POSITION WITH SDR UALA2011112706506Fairing · unsecureFOUND LEFT WING NR 3 FLAP TRACK FAIRING LATERAL MOVEMENT OUT OF LIMITS PER MM. LATERAL MOVEMENT MEASURES (.437 INCHES) LIMIT IS .189 INCHES. REMOVED PANEL 532 AT DISCONNECTED CONTROL AND SIDESTAY RODS MOVABLE FLAP TRACK FAIRING LOWERED AND HELD UP IN POSITIOSDR UALA2011112706507Bushing · wornFOUND LEFT WING OUTBD FLAP TRACK FAIRING (NR 4) LATERAL MOVEMENT OUT OF LIMITS PER MM. LATERAL MOVEMENT MEASURES (.375 INCHES) LIMIT IS .158 INCHES. REMOVED PANEL 533AT DISCONNECTED CONTROL AND SIDESTAY RODS MOVABLE FLAP TRACK FAIRING LOWERED AND HELD UP INSDR UALA2011112706508Bushing · wornFOUND RIGHT WING NR 3 FLAP TRACK FAIRING LATERAL MOVEMENT OUT OF LIMITS PER MM. LATERAL MOVEMENT MEASURES (.230 INCHES) LIMIT IS .189 INCHES. REMOVED PANEL 632AT DISCONNECTED CONTROL AND SIDESTAY RODS MOVABLE FLAP TRACK FAIRING LOWERED AND HELD UP IN POSITIOSDR UALA2011112706509Bushing · wornFOUND RIGHT WING OUTBD FLAP TRACK FAIRING LATERAL MOVEMENT OUT OF LIMITS PER MM. LATERAL MOVEMENT MEASURES (.250 INCHES) LIMIT IS .158 INCHES. REMOVED PANEL 633 AT DISCONNECTED CONTROL AND SIDESTAY RODS MOVEABLE FLAP TRACK FAIRING LOWERED AND HELD UP IN POSTSDR UALA2011112306444Line · leakingGREEN HYD LOW LEVEL ECAM, FLIGHT DIVERTED. CREW REPORTED GREEN HYD QTY DOWN TO ZERO, FOLLOWED ECAM PROCEDURE AND GREEN PUMP SELECTED TO OFF. LT PYLON HYD LINE FAILED. OLD LINE REMOVED FROM PYLON OF NUMBER ONE ENGINE. DUE TO DAMAGE AND LEAKING. REPLACED HYDSDR UALA2011112306447Motor · faultyLEFT WINDSHIELD WIPER INOP - ANTI-ICE. CREW COMMENTS: CAPT WIPER NOT MOVING THRU FULL ARC. MOTION IS VERY ERRATIC. DOES NOT CLEAR WINDSHIELD. REPLACED MOTOR ASSY.SDR UALA2011112206415Rivet · failedFAILED RIVET ON LEFT ENGINE EXHAUST NOZZLE 12 O'CLOCK POSITION REF MT 78-001 MISSING RIVETS ALLOWED, MUST BE REPAIRED. REPLACED WITHIN 50 HRS. OK TO CF PER THIS MAINT TRIP. REPLACED MISSING RIVET.SDR UALA2011112206439Control Panel · faultyCREW REPORTS SMOKE ODOR IN CABIN AND PES CIRCUIT BREAKER 5 TRIPPED AT 2000 VU PANEL. CAPT NOTED THAT THE EMERGENCY CALL BUTTON WAS ILLUMINATED WITH NO ONE CALLING AND THAT THE EMERGENCY CALL CHIME WAS GOING OFF. CIRCUIT BREAKER 21MK COLLARED. REMOVED AND RESDR UALA2011112106390Wire Harness · faultyTHE 21ABC EEL LIGHT INOP. REPAIRED SEAT HARNESS AND LIGHT CHECKED OK. FOUND BROKEN WIRE ON SEAT HARNESS TO LIGHT SOCKET HARNESS. NEEDS EITHER A NEW HARNESS OR TO BE RE-PINNED. COMPLIED WITH MEL. ALL ADJ LIGHTS OPERATE NORMALLY. PLZ ID PARTS NEEDED AND IPSDR UALA2011112106348Lanyard · faultyDOOR 1L IS HARD TO ARM. FOUND LANYARD HANGING DOWN 2" RESTRICTING GIRT BAR. REPACKED LANYARD PER AMM.SDR UALA2011112106411Battery · dischargedBATTERY 1 LOW VOLTAGE AND FAILS PREFLIGHT AMPERAGE CHECK. REPLACED NR 1 BATTERY & NR 1 BATTERY CHARGE LIMITER.SDR UALA2011112106410Attach Fitting · defectiveCREW REPORT: 31ABC WHOLE ROW OFF TRACKS. REPLACED THE AFT ATTACH FITTING SECURED SEAT.SDR UALA2011111706290Cable · brokenFOUND WIRES BROKEN ON CAPT SLIDING WINDOW AT LOWER END OF CONDUIT TUBE. OPEN AND TAGGED CB'S 13X,14X,ON 122VU. REMOVED CABLE ASSY PCN-565-2286. WILL NOT BE ABLE TO CHECK OUT NEW CABLE DUE TO TR2 BEING REMOVED (MR24501 REF SMC3).SDR UALA2011112106404Buffer · defectiveCAPT RUDDER PEDALS FAIL TO MOVE FORWARD FROM MOST EXTENDED POSITION AS WELL AS MOST. REPLACED RUDDER PEDAL BUFFER, OPS CHECK GOOD.SDR UALA2011111606274Controller · faultyALL TOILETS INOP, FLIGHT DIVERTED. SAMC TEXT: CFDS SHOWS '38-31-62 LIQUID LEVEL XMTR'. OPBLM -- AND CREW REPORTS FWD ATTEND PNL LAV WASTE QTY SHOWS 'ZERO'. REPLACED VACUUM SYSTEM CONTROLLER PER AMM. ALL 3 LAVS FLUSH NORMALLY.SDR UALA2011111606280Buffer · defectiveF-O RUDDER PEDALS FAIL TO SPRING FORWARD FROM MOST EVERY POSITION FROM A LOCKED POSITION. REPLACED BUFFER PER MM, OPS CHECK GOOD.SDR UALA2011111506260Cover Plate · out of positionCREW REPORT: F/A REPORTS VIBRATION ON FLOOR IN AFT GALLEY CONTINUED IN CLIMB AND CRUISE REPEAT GRIPE. ISOLATED LAV AND GALLEY EXTRACT FAN, NO VIBRATION WHEN OPERATED. CF FOR 3 CYCLES PER MT 53-005 FOR FLIGHT CREW DATA CAPTURE VIA VIB REPORTING SHEET. CHECKESDR UALA2011111706304Fire Bottle · dischargedLAV 'D' WASTE BIN FIRE EXTINGUISHER EMPTY. NEED PCN 635-0002 NOT IN STOCK AT MEXJL. APPLIED MEL. LAV MAY BE USED SMOKE DETECTION SYST OKAY. PART DID NOT ARRIVE. REPLACED EXTINGUISHER PER AMM.SDR UALA2011111506240Light · faultyEMERGENCY LIGHT TEST SHOWS EXT LOADS EMERGENCY RT FAULT. RELAMPED RT AFT EXT OVERWING EMERGENCY EXIT LIGHT, CHECKED OK.SDR UALA2011111406210Panel · unsecureRT AFT EMER EXIT DISPLAYED ON UPPER ECAM SCREEN - DOOR. CREW COMMENTS: INTERIOR PANEL FELL OFF AND TRIGGERED ECAM. SECURED INTERIOR PANEL FOR RT EMER EXIT, NO MESSAGE DISPLAYED ON ECAM.SDR UALA2011111506261Tab · bentCREW REPORT: PIECE OF FLAT METAL PROTRUDING FROM BOTTOM OF RIGHT ENGINE AFT OF BOTTOM LATCH. NR 1 LATCH TAP FOR LATCH OPEN IND BENT. STRAIGHTENED TAB. VERIFIED T-R HALVES SHUT PER MM. FAN COWLS SECURED CLOSED PER MM.SDR UALA2011111406192Generator · inoperativeLAVS NOT FLUSHING. VACUUM GENERATOR POPS BREAKER, INOPED GENERATOR ^12NOV DEN CQT- :VACUUM GENERATOR PCN SPA 565-9025 IPC 38-31-04. -RPL- :REPLACED VACUUM GENERATOR IAW MM. OP CHECKS GOOD.SDR UALA2011111406223Starter · faultyPUSH CREW REPORTS SPARKS COMING FROM NR 1 ENGINE FAN COWL AREA. REPLACED NR 1 ENGINE STARTER PER MM. OPS CHECK OKAY. FOUND OLD STARTER OIL LOW AND BURNT.SDR UALA2011111106163Structure · wornREF DAMAGED BULKHEAD CONNECTOR, SMC7. IPC SHOWS A DOTTED CUTOUT OF STRUCTURE FOR ATTACHMENT OF CONNECTOR. ITEMS 135 AND 120 ARE USED TO SECURE CONNECTOR. THE STRUCTURE IS WORN AWAY. THERE IS NOTHING TO ATTACH TO. REMOVED 1 EA FWD HI-LOKS IN FUEL TANK. PSDR UALA2011111006138Light · faultyELECTRICAL SMELL ROW 32. PROG TEXT: - ITEM ROLLED FORWARD. SAMC TEXT CONTACT SAMC, ALSO CHECK UNDER SEAT WIRING HARNESSES IN AREA FOR ANY EVIDENCE OF ELECTRICAL DAMAGE. INSPECTED AREA FOR DAMAGE. FOUND SIDEWALL LIGHT AT SEAT ROW 32ABC INOP. REPLACED SIDEWSDR UALA2011111006145Snubber · wornCAPT'S & FO'S RUDDER PEDAL BUFFER IS WORN OUT. REPLACED CAPT SIDE RUDDER PEDAL BUFFER. LUBRICATED F/O SIDE, NO HELP. REPLACED F/O'S RUDDER PEDAL SNUBBER IAW MM, OPS OKAY.SDR UALA2011111106165Wire Harness · damagedWHILE WORKING CH2153 (0 TIME) FOUND ENG NR 2 FIRE DETECTION HARNESS DAMAGED ABOVE FAN AIR VALVE 9HA2. WIRING HARNESS ACCESS VERY LIMITED. REFERENCE IPC'S 24-92-06-15A AND 71-52-41-81A. PCN 565-0654, PN- 745-5967-517, OSTF P2946. FIRE LOOP BRACKET WITH MISSISDR UALA2011110906132Engine · vibrationCREW REPORT: NOTICEABLE LOUD ROAR AND VIBRATION ON NR 2 ENGINE THROUGHOUT FLIGHT SAMC TEXT: PER CREW. HIGHEST VIBRATION NR 2 ENGINE WAS 2.0. THROTTLES BROUGHT TO IDLE, VIBS DECREASED. FELT ON FLOOR. FBO TO ACCOMPLISH INLET AND EXHAUST CHECK PER MT 72-021 ANSDR UALA2011111006133Transceiver · faultyWX RADAR FAILURE, RTFL WX RADAR INOP: CAPTS SCREEN PAINTS RED AND F-O SCREEN PAINTS PURPLE. ATTEMPTED RESET IN FLIGHT AND NO HELP. DEBRIEFED CREW. PWR SYSTEM UP GOT RT FAIL MESSAGE ON BOTH SCREENS. REPLACE WX TRANSCEIVER IAW AMM. OPS CHECK'D NORMAL. BISDR UALA2011110906108Hydraulic Line · leakingGREEN SYS HYD LOSS, FLIGHT DIVERTED. ACCOMPLISHED A MANUAL GEAR EXTENSION. AFT HYD PRESS LINE IN NR 1 PYLON REMOVED DUE TO HOLE WORN IN LINE UNDER AFT CLAMP. INSTALLED HYD LINE AND SECURED FRONT BULKHEAD FITTING, B-NUT AND MOST FORWARD CLAMP ASSY. FWD B-NUT SDR UALA2011111106176Wire · chafedFORWARD ENGINE LT JUST ABOVE AND INSIDE OF OIL TANK, 4 EACH WIRES CHAFED AND INSULATION DAMAGED. WIRE 6A411 BETWEEN J3 OF EEC AND PIN 32 & 16 4008VCA DAMAGED AND WIRE 6A445 REF AWM71-51-06 J2 PIN U&T TO PIN 11 & 24 4008VCA HAS DAMAGE. ID AND ORDERED NEW WIRESDR UALA2011110906095Tire · low pressureAIRCRAFT PULLS RIGHT WILL NOT TRACK STRAIGHT. FOUND RT NOSE TIRE 40 PSI LOWER THAN THE LT NOSE TIRE. REPLACED BOTH NOSE TIRES PER AMM.
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