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 UALA2011040801701B-Nut · leakingUPON REMOVING OIL CAP TO SERVICE NR 2 ENG OIL FOUND VERY STRONG FUEL SMELL COMING FROM OIL TANK. ACP'D INSPECTION AND CHECK OF FUEL OIL COOLER, NO PROBLEMS NOTED. FOUND MAIN FUEL SUPPLY LINE B-NUT WITH SMALL SEEPAGE. TIGHTENED B-NUT AND IDLE LEAK CHECKED GOSDR UALA2011040701687Rod End · faultyAIRFRAME VIBRATION STARTED 16000FT (300 KNOTS). SW1416 ASSIGNED RUDDER INTEGRITY CHECK. SAMC TEXT: CREW DID NOT FILL OUT VIBE FORM BUT WAS DEBRIEFED AND SAID THAT THE VIB WAS LATERAL IN NATURE IN THE AFT GALLEY AREA POINTING AT THE RUDDER. PERFORMED SW1416SDR UALA2011040601658Fan Blade · debondedENG 2 N1 VIBES HIGH, CHECKED ALL CHIP DETECTORS ON NR 2 ENG, NO DEBRIS FOUND. POS 2 FAN BLADE TAP TEST REQ'D DUE TO HIGH N1 VIBE. PER T-S NEED TAP TEST PER AMM. ACP'D TAP TEST PER MM. FAILED ONE EA MARKED BLADE WITH 2979 DB PER SEC. NEED TO REPLACE N1 VIBRSDR UALA2011040501632Unknown · smokeSMOKE IN COCKPIT, RTFLSDR UALA2011040501644Seat · unserviceableCAPTAIN SEAT UNUSEABLE. PEDESTAL COMES COMPLETELY OUT OF BASE. R & R CAPT SEAT IAW AMM 25-11-51, OPS CHECKED NORMAL.SDR UALA2011040601666Blade · bird ingestionLEFT ENGINE BIRD STRIKE. CONFERRED WITH ENGINE DESK. ENGINE WILL NEED TO BE REPLACED. REPLACED NR 1 ENGINE ACCT ONE 6TH STG HPC BLADE HAS A TEAR IN A BLADE TIP CURL. RPL'D ENGINE PER MT71-01SDR UALA2011040401606Light · failedEMERGENCY LIGHT TEST FAILED. FAULT IS EXT LOADS EMER L. LT AFT OVERWING EXTERIOR LIGHT FWD LIGHT IS INOP. RELAMPED, NO HELP, NEEDS NEW LIGHT ASSY. REPLACED AFT LEFT OVERWING EXTERIOR LIGHT ASSY, OPS CHK GOOD.SDR UALA2011040401627Bungee · defectiveF/O FOOT PEDAL ADJUSTMENT STICKY. NEEDS LUBE. RUDDER PEDAL MOVEMENT IS NOT EFFECTED BY RUDDER PEDAL ADJ. PEDALS DO NOT STICK OR BIND, PEDALS ARE WEAK TO RETURN WHEN RELEASE ADJ LEVER IS PULLED. CONFIRMED WITH OPBLM PARTS NEEDED ARE (644-0296) PART IS LOB INSDR UALA2011040401590Coffeemaker · faultyELEC SMELL IN GALLEY, FLIGHT DIVERTED. INVESTIGATED AFT GALLEY, FOUND NO EVIDENCE OF FIRE DAMAGE RELATED TO OVENS, ELECTRICAL PANELS, LIGHT PANELS AND LIGHT FIXTURES. DID FIND EVIDENCE OF ELECTRICAL ARCING BEHIND COFFEEMAKERS IN AFT GALLEY. ELECTRICALLY ISOSDR UALA2011040401615Insulation · damagedAFT CARGO DOOR ECAM, RTFL. CURRENT LEG REPORT IS FAULTING AFT CARGO DOOR SAFETY MECH PROX SENSOR 32WV TGT POS. VISUAL INSPECTION OF MECHANICAL SHOWS NO IRREGS. DEFFERED PER MEL. FOUND INSULATION DAMAGED ON HARNESS TO SENSOR 32WV, DOESNT APPEAR TO HAVE ANY SDR UALA2011040601665Power Supply · faultyEMERGENCY LIGHT TEST RESULTS IN EPSU COMM EMERGENCY LIGHT. REPLACED FWD EPSU AND BATTERY AND SYSTEM TEST NOW OK.SDR UALA2011033001525Computer · faultyCTR TK PUMP 1 LOW ECAM, FLT DIVERTED. FUEL INNER QTY INDICATION IS LOCKED UP, LEFT INNER APPEARS INACCURATE. REMOVED AND REPLACED FQIC IAW AMM. BITE CHECKS NORMAL. OPERATED CROSSFEED VALVE MULTIPLE TIMES WITH ALL INDICATION NORMAL. RAN BOTH ENGINES IAW THSDR UALA2011033001510Windshield · crackedCAPT'S WINDSHIELD CRACKED, RTFL. CAPT'S WINDSHIELD WAS HISSING. RPLD WINDSHIELD PER AMM. ACCOMPLISHED PRESSURIZATION CHK PER JRH, NO LEAKS NOTED. ALSO ACCOMPLISHED CPC 1 & 2 CHK. TEST PASSED, NO FAULTS.SDR UALA2011032901502Oxygen Mask · out of positionO2 MASK HANGING AT 11D. SEATS 12DEF INOP DUE TO O2 MASK DOWN AT SEAT 12D. ACP TEST PER MM. RAN TEST PER AMM. NO DEFECTS NOTED, RETURNED SEATS TO SERVICE.SDR UALA2011032801484Bottle · low pressureDOOR 2R EMERGENCY DOOR CYL-ACCUM PRESSURE LOW. SERVICED BOTTLE TO 1750 PSI.SDR UALA2011032901495Filter · dirtyOIL SMELL IN CABIN. REPLACED FILTERS PER MM. OKAY FOR SERVICE.SDR UALA2011032901503Trim System · malfunctionedACCOMPLISHING AN OPERATIONAL TEST OF TRIMMABLE HORIZONTAL STABILIZER. TEST FAILS STEP 7 OF AMM. THS ACTUATOR NEVER STOPS. ON THE LEFT AND RIGHT THS ACTUATOR CONTROL SHAFT THE LOCKWIRE AND CAPS ARE REMOVED. PARTS IN COCKPIT. STILL COULDN'T GET EITHER LT NOSDR UALA2011032901504Computer · faultyBOTH AP'S INOP WITH RUDDER TVL LIMITER FAULT, BOTH PFD'S ON SAME FAC MESSAGE. FAC 1 IS FAULTED IN CFDS. SWAPPED FAC 1 AND 2. CHECKED NORMAL. REPLACED TAT PROBE 1, ALL SYST CKD NORMAL. CAT III CKD NORMAL IAW AMM. CURRENT POSITIONS. FAC 1, MR22675-126, FACSDR UALA2011032801483Ram Air Turb · faultyRAT FAILS TEST. GREEN LIGHT WON'T COME ON AND STAY ON. FIRST TEST FAILED. REPLACED HYD PUMP ASSY RAT HYD PUMP ASSY OP CHECKS GOOD, NO LEAKS.SDR UALA2011032801481Manifold · leakingON WALKAROUND FOUND HYD LEAK RT MAIN GEAR. REMOVED AND INSTALLED NEW RT NORMAL BRAKE MANIFOLD ASSY. MANIFOLD SECURED SAFTIED, LINES SECURED TIGHT, CONNECTOR SECURED SAFTIED. PICK UP FROM PG 419 D2 DID BLEEDING OF BRAKES SYS AND TESTED 1 AND 2 PG 419 AND TESSDR UALA2011032801486Servo Control · malfunctionedAIL SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. - F- CTL. TROUBLESHOOTING FAULTS R G AIL POS XDCR 33CES. DEACTIVATED RG AILERON SERVO 33CES. REPLACED RIGHT WING AIL, SERVO CONTROL 33CE2.SDR UALA2011032501417Servo · faultyFLIGHT ATTENDANT REPORTS VIBRATION IN BACK OF ACFT STRONG. CLIMBING BETWEEN 24000 & 36000 FT, SPEED 300 KTS PITCH SET AT 4 DEG NOSE UP, VIB FELT IN FWD & AFT, LOWERING NOSE TO 3 DEG PITCH UP DECREASED VIB. REPLACED LEFT BLUE AND GREEN ELEV SERVO CONTROL EYE SDR UALA2011032401403Control Unit · faultyBSCU 2 NW STEERING FAULT ON LANDING. BRAKES - ANTI SKID FAULT ON APPROACH AND LOSS OF NWS FUNCTION. REPLACED BSCU PER MM. OPS ARE GOOD.SDR UALA2011032501442Acoustic Liner · tornTHREE SMALL TEARS IN THE ACOUSTIC MATERIAL INSIDE THE NUMBER ONE ENG COWLING. SAMC TEXT: REF MT 71-006. TEAR IN SKIN 3.5 INCHES LONG. EXCEEDS MT LIMITS. ACP REPAIR NR 1 PER MT 71-006.SDR UALA2011032501443Cylinder · leakingAFT NOSE STEERING CYLINDER LEAKING WITH HYD PRESSURE OFF. PACKINGS ON ANTI SHIMMY VALVE. OP CHECKED STEERING, NO LEAKS NOTED.SDR UALA2011032501448Tip Cap · damagedLIGHTNING STRIKE DAMAGE AT AFT OUTBOARD CORNER. REPLACED RT ELEVATOR TIP PER AMM AND REMOVED AND RE-INSTALLED RT HORIZ STAB TIP FOR ACCESS.SDR UALA2011032401404Outflow Valve · faultyR AFT CABIN DISPLAYED ON UPPER ECAM SCREEN. DOOR CREW COMMENTS: R AFT CABIN DOOR SHOWED OPEN IN FLIGHT. CABIN PRESSURIZATION CONTROL WAS LOST IN AUTO AND MANUAL. SAMC TEXT: **CREW REPORTED LOST PRESS AT APPROX 8000FT AGL. UNABLE TO REGAIN CONTROL IN AUTOSDR UALA2011032401407Skin · damagedWING LEADING EDGE AT RT SLAT NR 3 AREA HAS A DENT OF 0.125 IN DEPTH AND A SCRATCH OF 0.500 IN BY 0.250 IN. WHILE REMOVING RT LEADING EDGE SKIN FOUND CRACK AT NR 3 SLAT STOP CUTOUT AT FASTENER HOLE. CUT OUT DAMAGE .875 INCH HOLE FOR CIRCULAR PATCH REPAIR. SKSDR UALA2011032201386Selector Valve · faultyLEFT MLG DOOR PROBLEM. DUE TO REPEAT FAULTS OF LEFT MLG DOOR PROX SWITCHES 35GA AND 33GA REPLACE DOOR SELECTOR VALVE 41GA. PCN 644-0025. THIS REQUIRES A DOOR OPS CHECK, NOT A GEAR SWING. REPLACED LT MLG SELECTOR VALVE PER AMM. OPERATION AND LEAK CHECK GOSDR UALA2011032401408Servo · vibrationAIRFRAME VIBRATION FELT IN AFT GALLEY. WENT AWAY W- RUDDER APPLICATION. REPORT FORM COMPLETED. SAMC TEXT: REFERENCE TSM FOR RUDDER TRAILING EDGE PLAY CHECKS. REPLACED ALL THREE RUDDER SERVO CONTROL ROD ENDS. PLAY BEFORE REPLACEMENT: Y=15MM, B=17MM, G=19MMSDR UALA2011032301396Oxygen Mask · unwanted deployOXYGEN MASKS DROPPED AT 18DEF. REPACKED MASKS PER AMM, DROP CHECK PER MM, OPS CHECK GOOD.SDR UALA2011032101361Transducer · faultyNR 2 ENG VIBRATION, RTFL. PERFORMED TRANSIENT ACOUSTIC PROPAGATION TEST OF NR 2 ENG LP COMPRESSOR FAN BLADES PER AMM. ALL BLADES FOUND WITHIN LIMITS. NR 2 ENGINE, REMOVED INLET CONE AND FAIRING FOR INSPECTION OF BLADE RETAINING RING. CHECKED TORQUE OF BLADSDR UALA2011032401409Computer · faultyAT SHUTDOWN ECAM F-CTL SIDESTICK PRIORITY. REPLACED NR 1 ELAC PER MM. ACCOMPLISHED ELAC TEST, REF MM AND AFS TEST, REF MM AND LAND CAT III TEST, REF MM. ALL TESTS PASS.SDR UALA2011032201387Starter · failedPASSENGERS REPORTED SPARKS COMING FROM NR 1 ENG ON START. REPLACED NR 1 ENG STARTER, OPS CHECK GOOD.SDR UALA2011032101331Wire · out of positionCABIN EMERG LIGHTING CHECK RESULT SHOWED ATA 33-51-38 INT LOADS EMER L. FOUND EXT AND INT LIGHTS FLASHING ON 11W EPSU. TRIED NEW BATTERY AND EPSU NO HELP. 11W DISCONNECTED FROM AIRCRAFT. REPLACED EPSU 11W AND BATTERY PACK, NO HELP. FOUND WIRES BELOW SEAT ROWSDR UALA2011032101315Power Supply · inoperativeEMERGENCY FLOOR LIGHTS INOP NEAR ROWS 13-14-18-19+20. REPLACED POWER SUPPLY UNIT. OPS NORMAL.SDR UALA2011032101311Extinguisher · dischargedAFT CABIN HALON FIRE EXTINGUISHER EMPTY. AFT CABIN HALON FIRE EXTINGUISHER EMPTY. REPLACED EXTINGUISHER.SDR UALA2011031701300Computer · faultyVENT SKIN VLV FAULT, RTFL. SKIN AIR VALVE FAULT. INLET FULL OPEN EXTRACT FULL CLOSED. ALSO LOUD HUM IN COCKPIT. SAMC TEXT: CFDS SHOWS "CHK AEVC SUPPLY" AND SKIN AIR VALVE FAULT. FOUND A CIRCUIT BREAKER ON VU49 (D5)FOR THE AEVC COMPUTER POPPED. REPLACED CSDR UALA2011031701293Structure · dentedBIRD STRIKE NR 3 SLAT DAMAGE. DENT STARTS AT RIB COVERING 5 RIVETS GOING 16.5 IN TOWARDS OTBD. CENTER OF DENT STARTS ON TOP AT RIVETS COVERING 10 RIVETS GOING FWD TOWARDS LEADING EDGE. RPL'D NR 3 LT SLAT.SDR UALA2011031601286Control Unit · malfunctionedA-C PULLS TO RIGHT ON TAXI. CONTINUOUS LEFT TILLER REQ TO TRACK STRAIGHT. MAINT TEXT: DURING TAXI TEST LEFT RUDDER TRIM REQUIRED TO KEEP AIRCRAFT STRAIGHT. REPLACED BSCU PER MM. TAXIED AIRCRAFT WITH ALLOWABLE TRIM INPUTS OF UP TO 3 DEGREES TO STEER STRAISDR UALA2011031501231Actuator · faultyNR 1 ENG REV FAULT, FLIGHT DIVERTED. REPLACED NR 1 ENGINE THRUST REVERSER NON LOCKING ACTUATOR ON INBOARD UPPER SIDE (FADAC NR 1B CHANNEL) WAS AT FAULT. REPLACED PER MM. OPS CHECKED NORMAL BOTH STATICALLY AND ENGINE OPERATIONAL, ALL SAFETIES APPLIED AND REMSDR UALA2011031501238Strut · underservicedTOOK 3 TRIES TO GET THE LANDING GEAR HANDLE TO MOVE TO GET THE GEAR TO RETRACT. FOUND BOTH MAIN GEAR STRUT UPPER CHAMBERS LOW. ACP FULL SVC ON MAIN GEAR. ACP GEAR SWING 3 TIMES, OPS GOOD.SDR UALA2011031601252Windshield · failedFIRST OFFICER'S FWD WINDSHIELD FOR INOP HEAT. THE SENSOR AND WHC HAVE ALREADY BEEN REPLACED, NO HELP. REPLACE PER AMM. REPLACED FIRST OFFICER'S WINDSHIELD PER MM.SDR UALA2011031401193Power Supply · out of toleranceEMERGENCY POWER SUPPLY UNIT 11WL IS OUT OF TOLERANCE. REPLACED AND OPS CHECKED EPSU 11WL AT C-03 VISIT. ALL OKAY.SDR UALA2011031401209Control Unit · faultySDCU MAINTENANCE STATUS CLASS II MESSAGE DISPLAYED ON LOWER ECAM. DEFERRED PER PDL. INSTALLED NEW SDCU PER MM, OPS CHECKED GOOD.SDR UALA2011031401192Lens · wrong partSEAT ROW 10ABC HAS A WHITE EMERGENCY EXIT LIGHT LENS INSTEAD OF A RED ONE INDICATING THE OVERWING EXIT PATH. THE LENS IS LOCATED ON THE SEAT AISLEWAY ARMREST SHROUD. REMOVED & REPLACED LENS ASSY. OPS CHECKED REF AMM. ALL CHECKS GOOD.SDR UALA2011031401212Panel · damagedACCOUSTICAL PANEL DAMAGE AT NR 2 ENG. REPLACED RT TRANSLATING COWL ON NR 2 ENGINE. OPS CHECKED REF MM. NO FAULTS NOTED.SDR UALA2011031101177Heater · arcedCAPTAIN'S SLIDING WINDOW ARCING. APPEARS DAMAGED LOWER FWD SIDE, APPROX 12 INCHES LONG. C-B X 14 PULLED IAW ECAM. REPLACED CAPTAIN'S SLIDING WINDOW.SDR UALA2011031001160Light · detachedDOOR 2R EXIT LIGHT CAME OFF WALL. REATTACHED EXIT LIGHT AT 2R. COULD USE NEW ASSY 565-2003. STAYS ON WALL, ALL FUNCTIONS NORMAL. REPAIRED LIGHT ASSY, EMERGENCY LIGHT OPERATES CORRECTLY.SDR UALA2011031101172Bushing · faultyAIRFRAME VIBRATION ON CLIMBOUT APPROX FL300. SEEMS ENG RELATED BUT NO SECONDARY INDICATIONS. ENG1 N1=1.1 N2=.6 ENG2 N1=.6 N2=.3 VIBRATION STRONGEST AT ROW 24 AND AFT. NO CHANGE WITH AIRSPEED BUT DECREASED WITH POWER REDUCTION AT TOP OF CLIMB. CREW REPORTS AS
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