IAE V2527-A5
Service difficulty reports · 8,009
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 CALA2013090290908Armrest · looseARMREST CONSOLE LOOSE AT 7F. PERFORMED AN INTERIM REPAIR IAW ECRA 2000-01279. REPLACED NEW ARMREST END CAP.SDR CALA2013090290909Sliding Window · delaminatedDELAMINATION FRONT EDGE APPROXIMATELY 2 IN X 14 IN. R & R CAPTAIN'S SLIDING WINDOW IAW AMM 56-12-11-400-002-A UP TO STEP 5A. (LINING INSTALLATION)SDR CALA2013090290912Bracket · looseUPON OPENING NR 1 ENGINE FOR ACCESS FOUND LANYARD BRACKET FOR CORE COWL LATCH ACCESS LOOSE FROM DOOR ASSEMBLY. REPAIRED LANYARD BRACKET, CHECKED NORMAL.SDR CALA2013090290927Panel · damagedNR 2 ENGINE NOSE COWL INNER PANEL HAS 2 AREAS OF DAMAGE AT APPROXIMATELY 5 O'CLOCK 1 APPROXIMATELY 2" X .50" & 1 AT 6 O'CLOCK 2" X .50". PREVIOUS REPAIR IS COMING LOOSE APPROXIMATELY 5" X 5" & ENTIRE PANEL FROM NOSE LIP TO FAN ATTRITION LINER FROM EDGE OF PRESDR CALA2013090290942Floor Panel · puncturedRAMP FOUND 1X1 INCH SQUARE PUNCTURE AFT PIT MAIN FLOOR PANEL AFT OF CARGO DOOR. PUNCTURE TAPED OVER PER MT-53-007.SDR CALA2013090290911Unknown · faultySTATIC INVERTER WILL NOT TEST. REPLACED STATIC INVERTER & STATIC INVERTER CONTACTOR 2XB PER MM 24-28-51 & MM 24-28- 55 WITH NO HELP. ALSO REPLACED RELAYS 30XU1 & 30XU2 WITH NO HELP. REPLACED RELAY 7XB, 13XC, 14XC, & CNTOR- AC ESS BUS SWITCHING (15- XE), NO SDR CALA2013083090873Shaft · shearedCONT MAX N1 WAS 8 PERCENT BOTH STARTS. REPLACED ENGINE STARTER, FOUND SHAFT SHEARED, REPLACED ENGINE START VALVE. OPERATIONS CHECKED. START 3 TIMES ALL GOOD.SDR CALA2013083090874Screw · looseVERY LOUD SQUEAL ROW 1-2 NEAR WALL-FLOOR. PRESSURIZED ACFT IAW AMM 05 -53-00-780-03. FOUND CAPTAINS AOA SENSOR ATTACHMENT SCREWS LOOSE, SECURED. FIRST OFFICERS AOA BLANKING PLATE CLOCKED WRONG. REINSTALLED IAW MM. NO NOISE NOTED.SDR CALA2013082990839Panel · dentedDENT FORWARD CARGO DOOR BY HANDLE. REMOVED LOWER PANEL 825AR FROM FORWARD CARGO DOOR. PANEL PLACED ON PAC ORDER NR N5708. CDL IAW 52UR PARTS: 110-0461 D5237173500000 PANEL.SDR CALA2013082990840Skin · crackedNR 2 ENGINE RT THRUST REVERSER OUTER SKIN HAS 7-10 RIVETS PULLING THREW SKIN WITH A CRACK 5.75 INCHES LONG AT 1 O-CLOCK POSITION.SDR CALA2013082990842Mount Bracket · brokenCOCKPIT CRASH AXE HAS A BROKEN SADDLE MOUNTING BRACKET. INSTALLED NEW BRACKET.SDR CALA2013082990845Hinge · brokenLAVATORY DOOR WON'T OPEN OR CLOSE AT AFT CABIN LT FORWARD LAVATORY. HINGE BROKE, DAMPER IS MISSING FROM DOOR. DOOR OPERATED GOOD IPC 25-43-41-62C ITEM H PARTS: 110-0012 192856 DAMPER LOB: N 110-0011, A225400288-508 DOOR LOB: NSDR CALA2013083090859Nut Plate · brokenFASTENER MISSING ON RT PANEL 191KB OUTBOARD EDGE FOURTH FASTENER FROM FORWARD CORNER. CORRECTION LT PANEL 191KB NUTPLATE FOUND BROKEN. CERTIFIED FOR 10 CYCLES. REPLACED MISSING FASTENER IAW IPC 53-35-03.SDR CALA2013083090860Rub Strip · loosePIECE OF RUBBER SEAL MATERIAL PROTRUDING FROM BOTTOM OF LT ENGINE. REMOVED AN 8IN. PIECE OF TEFLON WEAR STRIP FROM THE FORWARD REVERSER SLEEVE ACCESS PANEL AT THE 6:00 POSITION, IAW MT 78-016. ENGINE OKAYED FOR CONTINUED SERVICE. PANEL SECURED.SDR CALA2013082890812Servo Valve · faultySYSTEM ONE FAULT DISPLAYED ON UPPER ECAM SCREEN. ECAM AFTER LANDING. PFR FAULTS "ALT BRK SERVO VLV 41GG", PCN 644-2121, IAW AMM 32-43-27 FOR R&R. NO FAULTS NOTED, CLEANED CONNECTOR 41GG BITE TEST BSCU IAW AMM, CHECKED OKAY.SDR CALA2013082990821Oxygen Mask · leakingCAPTAINS OXYGEN MASK FOUND LEAKING ON ARRIVAL INTO ORD FLIGHT 354-26, COULD HEAR AUDIBLE LEAK WITH OXYGEN ON. REPLACED CAPTAINS OXYGEN MASK & OXYGEN BOX. AFTER MASK & BOX REPLACED LT OXYGEN ON & NO PRESSURE DROP IN 3 HOURS..SDR CALA2013082990843Wire Harness · shortedLGCIU 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND WIRE A1009 IN UPPER HARNESS 1M SHORTED TO GROUND. REPLACED NLG HARNESS 1M IAW AMM. ACP NOSE GEAR LANDING, TAXI, TURNOFF LIGHT CHECKED GOOD, ALSO ACP NOSE GEAR WHEEL STEERING OPERATIONS & LGCIU 1 & 2 BITE TESDR CALA2013082890813Valve · leakingHYDRAULIC LEAK COMING FROM RIGHT PARKING BRAKE VALVE. REPLACED PARKING BRAKE VALVE.SDR CALA2013082790784Uplock · malfunctionedLANDING GEAR RETRACT, RETURN TO FIELD. REPLACE RT UPLOCK.SDR CALA2013082890808Exciter · faultyAUXILIARY POWER UNIT WILL NOT START. R & R AUXILIARY POWER UNIT IGNITER BOX. R & R AUXILIARY POWER UNIT PLUGS. R & R AUXILIARY POWER UNIT IGNITER PLUG LEADS, OPERATIONS CHECKED NORMAL.SDR CALA2013082890814Oxygen Mask · unsecurePASSENGER SEAT OVERHEAD 02 MASK FELL AT 32 ABC, IAW MT 35-003. MASKS WERE STOWED. NEEDS MANUAL MASK RELEASE OPERATIONAL CHECK IAW AMM ON OR BEFORE 3 DAYS MAX LIMIT.SDR CALA2013082990841B-Nut · looseG RESERVOIR LOW AIR PRESSURE DISPLAYED ON UPPER ECAM SCREEN. FOUND 'B'-NUT LOOSE AT RESERVOIR PRESSURE GAUGE SERVICED SYSTEM LIGHT OUT AT UPPER ECAM SCREEN. OPERATION CHECKED GOOD IAW MM.SDR CALA2013082690722Switch · inoperativeFWD FLIGHT ATTENDANT CALL CHIME FROM COCKPIT INOP-INTERMITTENT. REPLACED FWD FLIGHT ATTENDATNT PUSH BUTTON SWITCH INSIDE COCKPIT, OPERATIONS CHECKED GOOD.SDR CALA2013082690740Receptacle · defectiveFASTENER LOOSE ON PANEL FORWARD OF RAM AIR TURBINE. DEFERED MISSING SCREW IAW AMM 53-35-00 OK FOR 10 CYCLES. RECEPTACLE IS BROKEN ON PANEL 191KB, TRAILING EDGE, CENTER. REPLACED CYLINDER LOCKING RECEPTICAL FASTNER OPERATIONS CHECKED GOOD.SDR CALA2013082690754Controller · faultyCABIN PR#1 MESSAGE AT DEPARTURE TIME. REPLACED NR 1 CABIN PRESSURE CONT IAW TO MM & BITE TEST, NO FAULT.SDR CALA2013082690767Screw · missingCAPTAINS HAND MIC HAS TWO SCREWS MISSING BOTTOM FALLS OUT. RESECURED &TIGHTENED SCREWS ON CAPTAIN`S MICROPHONE OKAY.SDR CALA2013082990844Screw · looseLOUD SQUEAL ABOVE SEAT 2A. REMOVED PSU ABOVE SEATS 2A & 2B, REMOVED SIDEWALL CEILING PANELS ABOVE ROWS 2 & 3 LT SIDE. AIR ESCAPING FROM RISER DUCT WHERE IT ATTACHES TO INDIVIDUAL AIR SUPPLY DUCT ABOVE SIDEWALL AT ROW 3, ADJUSTED & SECURED CLAMP, NO NOISE NOTSDR CALA2013082690705Rivet · damagedLIGHTNING STRIKE ON FASTENER BS 1085 STRINGER 35. NO DAMAGE NOTED ON REMOVAL OF PAINT TOP COAT. REPLACED RIVET, PRIMED & PAINTED. IAW SRM 51-10-10 & MT 53-013. DUE TO RIVET IN RVSM AREA.SDR CALA2013082690706Rivet · damagedLIGHTNING STRIKE ON FASTENERBS 9855 STRINGER 35. NO DAMAGE NOTED ON REMOVAL OF PAINT TOP COAT. REPLACED RIVET, PRIMED & PAINTED. IAW SRM 51-10-10 & MT 53-013. DUE TO RIVET IN RVSM AREA.SDR CALA2013082690716Deu · faultyINTERCOM RECEPTION AT AFT FLIGHT ATTENDANT STATION VERY WEAK. COMPLIED WITH MEL. REPLACED DIGITAL ELECTRONIC UNIT B ABOVE DOOR 2L. INTERCOM OPERATIONS CHECKED NORMAL.SDR CALA2013082690717Nut Plate · damagedONE FASTENER WILL NOT SECURE ON WING TO BODY FAIRING 191BB, FASTENER IN TOP EDGE 5TH FROM LEADING EDGE. TAPED OVER FASTENER, TO BE REPAIRED WITHIN CYCLES, PTC IS 20387. REPLACED DAMAGED NUTPLATE.SDR CALA2013082690719Valve · faultyAFT CARGO HEAT FAULT DISPLAYED ON UPPER ECAM SCREEN. VERIFIED HOT AIR PRSOV CLOSED. REPLACED TRIM AIR VALVE PER AMM & CARGO HEAT CONTROLLER PER AMM. OPERATIONS CHECKED OK, NO FAULT MESSAGE.SDR CALA2013082690741Display · defectiveLOWER ECAM DISPLAY UNIT INOPERATIVE EIS FLASHES WITH DIAGONAL WHITE LINE. REPLACED LOWER ECAM DISPLAY, TESTED OKAY.SDR CALA2013082690742Handset · damagedFORWARD PASSENGER ADDRESS HANDSET CABLE IS DAMAGED & HANDSET IS INOPERATIVE. REPLACED HANDSET.SDR CALA2013082690707Structure · damagedLW FUEL TANK LANDING 540KB HAS FOUR OVER SIZED FASTENER HOLES. REPAIRED LT WING FUEL TANK LANDING 540KB IAW REO-L01412 & EC-RA 5720-02442. THIS REPAIR HAD BEEN APPROVED AS CAT 'B' VIA RDAS 70581393-003- 2013 ISSUE A.SDR CALA2013082690720Seat · defectiveFIRST OFFICER SEAT MANUAL ADJUSTMENT, RECLINE DEFECTIVE. SEATBACK WILL NOT RETURN TO UPRIGHT ON ITS OWN. REPLACED SEAT PER AMM.SDR CALA2013082690721Blade · nickedNR 2 ENGINE FAN BLADE HAS NICK ON LEADING EDGE. BLENDED BLADE PER AMM 72- 31-11. IDT INSPECTION WAS ACCOMPLISHED. NICK WAS ON LEADING EDGE OF BLADE APPROX 1 -32ND OF AN INCH.SDR CALA2013082690723Blade · damagedNR 21 FAN BLADE, NR 1 ENGINE, FAILED TRANSIENT ACOUSTIC PROPAGATION TEST PER JOB CARDNR 4-2215. REMOVED & REPLACED NR 21 FAN BLADE PER AMM 72-31-11. PERFORMED NR 1 ENGINE RUNUP VIBRATION TEST PER AMM 71-00-00, VIBRATIONS WITHIN SERVICEABLE LIMITS.SDR CALA2013082690739Switch · looseFIRST OFFICER`S SIDESTICK COMMUNICATIONS TRIGGER VERY LOOSE. RESECURED FIRST OFFICER`S PUSH TO TALK, OPERATIONS GOOD.SDR CALA2013082390688Sill · corrodedR2 FWD GIRT BAR FITTING HAS CORROSION UNDER IT. REMOVED & REPLACED R2 DOOR SILL, SILL FWD SPLICES, AFT CORNER FITTING & SIDEWALL ATTACH ANGLES IAW A320 SRM 51-42-11 PARA 5,6,7 &13.SDR CALA2013082390689Skin · damagedFORWARD CARGO DOOR EXTERIOR SKIN LOWER AREA HAS LIGHTNING STRIKE. REPAIRED LIGHTING STRIKE ON FWD CARGO DOOR SKIN FASTENER IAW SRM 52-00-00 FIG 213. REPAIR WORK PERFORMED PER FIG 213 SHEET 2C IIR 52-00-00-2-003-00 & PAGES 211 212 TABLE 204. AT TIME OF 1ST SDR CALA2013082390694Indicator · failedEIS 2 WOULD NOT TEST. REPLACED CFDIU REF AMM 31-32-34. MR31333-71 "ON" SN C12860007285 "OFF" REF TSM 31-32-00 MX MESSAGE NO DMC 2 DATA STILL PRESENT. FOUND NO CONTINUITY BETWEEN CFDIU AB 6F AND DMC2 AB 1C. REPAIRED WIRE 3132-7386 AND REINSTALLED ORIGINAL CFDSDR CALA2013082690718Control Valve · faultyTRIM AIR SYSTEM FAULT - COCKPIT TRIM VALVE DISPLAYED ON UP PER ECAM SCREEN - COND. REPLACED TRIM AIR VALVE & OPERATIONS CHECKED GOOD.SDR CALA2013082190621Fluid · leakingCLEANED UP RED FLUID OFF THE BELLY FROM THE AFT CARGO DOOR TO THE REAR OF THE AIRCRAFT. FOUND RED-FLUID UNDER THS ACTUATOR, FLUID IS LEAKING OUT ACCESS PANEL BOTTOM OF TAIL & RUNNING FORWARD. CLEANED OFF RED FLUID FOUND NO LEAK OR TROUBLE. AUDIO CONTROL PANSDR CALA2013082290651Skin · damagedFWD RT FUSELAGE SKIN FASTENERS HAVE SEVEN EACH LIGHTING STRIKES BETWEEN FRAME 09-24 & STR 37-39. REPAIRED SEVEN EACH LIGHTING STRIKES FWD LOWER RT FUSELAGE SKIN FM 9-24 STR 37-39 IAW SRM 53-11 -11 FIG 211.SDR CALA2013082290657Slide · faulty2SV EMERGENCY. LIGHTING CHECK HAD FAULT EXT LOADS AFT L. USING MT33-001 REMOVED CONNECTOR FOR SLIDE LIGHT ON LT DOOR & INSTALLED TEST PLUG & STILL HAD FAULT, REINSTALLED CONNECTOR & TRIED TEST PLUG ON RT DOOR & FAULT WENT AWAY. REPLACED SLIDE. EMERGENCY LIGHSDR CALA2013082290658Fastener · missingINBOUND PAX SAY RIVETS MISSING AT ENGINE 1 CONNECTION TO WING. SKIN OF WING LIFTS UP. REPLACED MISSING FASTENERS.SDR CALA2013082290659Thrust Reverser · delaminatedLT ENGINE RT THRUST REV HALF HAS APPROXIMATELY 35 SQ IN OF DELAMINATION ON ACOUSTIC SCREEN AT 3-OCLOCK. CLEANED & APPLIED SPEED TAPE. REF MT78-010.SDR CALA2013082290660Wire Harness · faultyIAW DF333 - BEGAN REPLACEMENT OF FIRE LOOP HARNESS. BEGAN AT THE 6 0'CLOCK POSITION & CONTINUED UP THE LT SIDE OF ENGINE. HARNESS IS COMPLETE TO ABOVE THE GROUNDS ON THE LT SIDE OF ENGINE. COMPLETED WIRE HARNESS REPLACEMENT. RECONNECTED DISCONNECT CONNECTORSSDR CALA2013082190619Potentiometer · failedSPEAKER HAS STATIC OFF OR ON. REPLACED CAPTAIN`S SPEAKER POTENTIOMETER.
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