Boeing 757-2Q8
Service difficulty reports · 2,798
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 aircraft_model_key = '7572Q8' 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 aircraft_model_key = '7572Q8' 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 ASMF200503020Inlet Guide Vane · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF CAPTAIN REPORTED APU PNEUMATIC PRESSURE DOWN TO 8 PSI WHEN LEFT ENGINE STARTED INSULATION VALVE WAS OPENED. ENGINES WERE STARTED WITH A GPU AND REPORT WAS DEFERRED IAW MEL 49-11-01. DURING OVERNIGHT SERVICE, SDR ASMF200503014Control Valve · failedAIRCRAFT RETURNED TO PLATFORM AFTER ENGINES STARTED WITH CROSSED FEEDING, EICAS MESSAGES R HYD R SUR PRESS, R ENG REV CONE, L ENG REV CONE, L ENG FIRE LOOP 2, EPR DET LOOP 2 INCHES AND (RT ENGINE EPR OUT OF SERVICE) WERE SHOWN AND PNEUMATIC AUXILIARY POWER UNISDR ASMF200502005Control Module · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER ENGINES STARTED, EICAS MESSAGES STAB TRIM" WAS SHOWN. REPORT WAS DEFERRED IAW MEL 27-41-2. DURING TRANSIT CHECK AT MEX, LEFT STAB TRIM CONTROL MODULE WAS REPLACED IAW MM 27-41-05, TESTED CORRECT, DEFERRESDR ASMF200502002Control Module · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER ENGINES STARTED, EICAS MESSAGES "STAB TRIM" WAS SHOWN. REPORT WAS DEFERRED IAW MEL 27-41-2. DURING TRANSIT CHECK AT MEX, LEFT STAB TRIM CONTROL MODULE WAS REPLACED IAW MM 27-41-05, TESTED CORRECT, DEFERSDR ASMF200501016Fuel Control · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXING AND AFTER RIGHT ENGINE STARTING AUTO-SHUTDOWN WITHOUT ANY APPARENT CAUSE. CAPTAIN PERFORMED CLEANING PROCEDURE FOR ENGINE REVISION. ENTRANCE, EXHAUST AND MASTER CHIP DETECTOR OF RIGHT ENGINE WERSDR ASMF200501014A/C Pack · inoperativeAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LT AIR CONDITIONING PACK WAS OUT OF SERVICE. AT PLATFORM, BOTH AIR CONDITIONING SYSTEMS WERE CHECKED BEING CORRECT. DURING CHECK, LT ENGINE BLEED AIR OFF LIGHT TURNED ON, LIGHT WAS DEFERRED IAW MM 36-11-1. SDR ASMF200501015Valve · failedDURING TRANSIT CHECK WAS DETECTED A HYDRAULIC LEAK IN THE LEFT ENGINE FILTERS MODULE TUBE, TUBE WAS TIGHTENED AND ENGINE WAS MOTORIZED, BUT DURING THE PROCESS A NEW LEAK WAS DETECTED IN THE DE-OILER. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICSDR ASMF200501006Valve · leakingDURING FUEL SERVICE WAS DETECTED HIGH SUPPLY PRESSURE ON FUEL DISPENSER (80 PSI), PROMOTING FUEL LEAK ON RT CENTRAL TANK VALVE. AIRCRAFT WAS FUELED THROUGH LT VALVE AND RT VALVE WAS DEFERRED IAW MEL 28-21-1. DURING OVERNIGHT SERVICE RT FUEL VALVE WAS REPLACED SDR ASMF200412009Pump · damagedCAPT REPORTED LT HYD SYSTEM LOST, LT HYD QTY AT EICAS FAULT CODE 291106-01, LT HYD ELECTRIC PUMP FAULT CODE 291133-01, PTU FAULT CODE 292201-00 AND RT ELECTRIC PUMP OVERHEAT AT EICAS FAULT CODE 291113-02; THEREFORE LANDING GEAR WAS OPERATED IN ALTERNATE MODE. SDR ASMF200412003Shutoff Valve · failedCAPTAIN REPORTED THAT WHEN LEFT THRUST LEVER WAS LOCATED IN IDLE POSITION THE AIR-CONDITIONING PACK WAS SHUTDOWN AND "HI STAGE" LIGHT TURNED ON. DUAL VALVE WAS REPLACED IAW MM 36-11-08, ALL CORRECT. DURING ENGINE STARTING, "HI STAGE" LIGHT DID NOT TURNED OFF,SDR AALA20041215Wire · brokenDFW - EMERGENCY LIGHTS IN FRONT OF R3 LAVATORY TRACK STRIP BROKEN. REPLACED BROKEN TRACK CABLE FROM ROW 18 TO LAVATORY D FOR EMERGENCY LIGHTS IN FRONT OF R3 LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20041214Light · inoperativeDFW - EMERGENCY ESCAPE PATH LIGHT BETWEEN ROW 21 AND 22 INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT STRIP BETWEEN ROWS 21 AND 22. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20041179Light · inoperativeAFT PORTION OF EMERGENCY FLOOR TRACK LIGHT AT 2AB INOPERATIVE. REPLACED EMERGENCY FLOOR TRACK LIGHT ASSEMBLY AT ROW 2AB. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20041172Light · inoperativeDFW - EMERGENCY ESCAPE PATH LIGHT AT ROWS 11 TO 14 INOPERATIVE. EMERGENCY TRACK LIGHT AT 24D MISSING END CAP AND BROKEN CABLE. REPLACED EMERGENCY ESCAPE PATH LIGHT SEGMENTS AT ROWS 11 TO 14. REPLACED EMERGENCY TRACK LIGHT END CAP AT 24D AND REPLACED EMERGENSDR ASMF200411004Blade · nickedDURING OVERNIGHT SERVICE, BOROSCOPE INSPECTION WAS PERFORMED ON RIGHT ENGINE AND NICKS WERE DETECTED ON ONE BLADE OF 11TH STAGE, OUT OF LIMITS IAW MM 72-00-00. RIGHT ENGINE WAS REPLACED IAW MM 71-00-00, TEST CORRECT.SDR ASMF200410017Mechanism · out of adjustAIRCRAFT REJECTED TAKEOFF AT 80 KTS, AFT CABIN DOOR LIGHT TURNED ON. CAPTAIN REPORTED THAT DURING TAXING, LIGHT TURNED OFF AND TURNS ON AGAIN AT PLATFORM. CAPTAIN REQUESTED TO FLT ATTENDANTS TO CHECK THE DOOR, LINKING THE SLIDE BAR TURNING OFF THE LIGHT. AIRSDR ASMF200410016Idg · failedCAPTAIN REJECTED TAKEOFF AT 70 KTS, RT GENERATOR WAS OUT OF ITS BAR AND DRIVE LIGHT TURNED ON. STARTED THE APU AND RESEATED THE SYSTEM RECOVERING THE GENERATOR. PERFORMED A SECOND ATTEMPT BUT AT 80 KTS REJECTED TAKEOFF DUE TO THE GENERATOR WAS OUT OF ITS BARSDR ASMF204410010Fan · odorDURING TRANSIT CHECK, CAPTAIN REPORTED STRONG ELECTRICAL CABLE BURNED ODOR. TECHNICAL PERSONNEL PERFORMED BITE TO APU CONTROL UNIT SHOWING MESSAGE CURRENT LAS RUN LOW OIL PRESS. APU WAS DEFERRED IAW MEL 49-11-1. BURNED ODOR IN PILOTS CABIN AND GALLEY. SMOKE INSDR AALA20041099Connector · unsecureDFW - EMEREGNCY EXIT FLOOR PATH LIGHTS IN AFT CABIN INOPERATIVE. RESECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20040968End Plug · missingEND PLUG MISSING FOR EMERGENCY ESCAPE PATH LIGHTING TO THE RIGHT OF SEAT 1B AND BEHIND SEAT 24D. INSTALLED END PLUGS FOR EMERGENCY ESCAPE PATH LIGHTING AT SEAT 1B AND BEHIND SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR ASMF200409004Heat Exchanger · leakingDURING TRANSIT CHECK, A LEAK WAS DETECTED ON OIL TANK TUBE SCUPPER AND FUEL/OIL HEAT EXCHANGER. LT ENGINE WAS STARTED AND LEAK INCREASED. FUEL/OIL HEAT EXCHANGER WAS REPLACED IAW MM 79-21-00, TEST CORRECT. DURING OVERNIGHT SERVICE, ENGINE RUNNING WAS PERFORMESDR ASMF200408021Actuator · failedAIRCRAFT PERFORMED REJECTED TAKE OFF, DURING TAKE OFF RT AUTOMATIC THRUST LEVER WAS JAMMED. DURING MAINTENANCE REVISION, AUTOMATIC THRUST LEVER MOVEMENT WAS CHECKED AND SYSTEM WAS DEFERRED IAW MEL 22-30-1. DURING OVERNIGHT SERVICE, RT THRUST LEVER INTERLOCK WASDR ASMF200408009A/C Pack · inoperativeCAPTAIN REPORTED, AFTER ENGINE STARTED (LT ENGINE BLEED) LIGHT TURNED ON AND LT AIR CONDITIONING PACKAGE WAS INOPERATIVE. ENGINE WAS ACCELERATED, BLEED SWITCH WAS RESEATED AND FAIL CONTINUE. ENGINE BLEED SWITCH WAS RESEATED AGAIN AND ENGINE WAS ACCELERATED, (SDR ASMF200407028Controller · failedCAPTAIN REPORTED RT AIR CONDITIONING (PACK OFF) LIGHT TURNED ON CONTINUALLY AFTER ENGINE START AND WHEN ENGINE WAS IN IDLE POSITION, PNEUMATIC BLEED OF RT ENGINE WAS SHUTDOWN. PILOT CONTROLLER OF 14TH STAGE WAS REPLACED IAW MM 36-11-19, TEST CORRECT.SDR ASMF200407015Bleed Valve · failedCAPTAIN REPORTED WHEN STARTING CLIMB FROM FL350 TO FL390 THE RT ENGINE EPR'S INDICATION FLUCTUATE SEVERALLY AND ENGINE PANCAKING AND NOT CLIMBING. AIRCRAFT WAS SENT TO THE HANGAR AND BOROSCOPE INSPECTION AND FIM TESTS WAS PERFORMED TO RT ENGINE IAW MM 72-00-0SDR AALA20040704Charger · inoperativeDFW - EMERGENCY LIGHTS ON RIGHT HAND FIRST CLASS BAGGAGE BINS INOPERATVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY LIGHTS ON RIGHT HAND FIRST CLASS BAGGAGE BINS. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR ASMF200406028Circuit Breaker · trippedAIRCRAFT RETURNED TO PLATFORM, "CTL HYDRAULIC PUMP" LIGHT TURNED ON AND EICAS MESSAGE, ENGINES WERE SHUTDOWN. DURING MAINTENANCE CHECK, HYDRAULIC PUMP BREAKER K24 WAS ACTIVATED AND REESTABLISHED, FIM PROCEDURE 29-11-00 WAS PERFORMED, ALL CORRECT.SDR ASMF200405027Valve · failedAIRCRAFT RETURNED TO PLATFORM, LT ENGINE WAS SHUTDOWN AND (FUEL CONT) AND (SPAR VALVE) LIGHTS TURNED ON. STATUS DISPLAY MESSAGES, APU PERFORMANCE AND ABNORMAL STATUS WERE CHECKED, ALL CORRECT. LT SPAR FUEL SHUTOFF VALVE WAS OPERATED MANUALLY AND IT WAS WITH FASDR ASMF200405021Valve · leakingDURING REFUELING A FUEL LEAK WAS DETECTED IN LT MAIN GEAR DOOR. LT CENTRAL TANK VALVE WAS DETECTED WITH LEAK AND FUEL VALVE WAS REPLACED IAW MM 28-10-00, TEST CORRECT.SDR AALA20040553Power Cable · brokenDFW - EMERGENCY ESCAPE PATH LIGHT AT LEFT HAND AISLE FORWARD OF SEATS 1AB INOPERATIVE. FOUND EMERGENCY LIGHT POWER CABLE BROKEN IN FIRST CLASS. REPLACED EMERGENCY PATH LIGHT POWER CABLE IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR ASMF200405010Proximity Sensor · damagedDURING TRANSIT CHECK, (LANDING GEAR) AND (MAINTENANCE GEAR DOOR) LIGHTS TURNED ON. DURING MAINTENANCE REVISION, PSEU WAS DETECTED WITH DAMAGE ON SENSOR 076. PROXIMITY SWITCH WAS REPLACED IAW MM 32-61-02 AND TEST CORRECT IAW MM 32-61-00.SDR ASMF200405005Warning Light · illuminatedAIRCRAFT SUSPENDED TAKE OFF AT 70 KTS AND RETURNED TO PLATFORM BECAUSE (L ENG BLEED OFF) LIGHT TURNED ON. (L ENG BLEED OFF) LIGHT WAS DEFERRED IAW MEL 36-11-1. FIM 36-10-00 PROCEDURE WAS PERFORMED AND SUSPENDED TAKE OFF INSPECTION WAS ACCOMPLISHED IAW MM 05-5SDR ASMF200404024Tube · damagedDURING TRANSIT CHECK AN HYDRAULIC LEAK WAS DETECTED ON LT ENGINE. DURING MAINTENANCE REVISION AN HYDRAULIC TUBE (P/N 316N3100-28) WAS DETECTED WITH DAMAGE. PROVISIONAL FLEXIBLE HOSE WAS INSTALLED, LEAK TEST WAS PERFORMED, NO LEAK WAS DETECTED. DURING OVERNIGHTSDR ASMF200404021Idg · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT MTY AS A CONSEQUENCE OF APU WAS SHUTDOWN IN FLIGHT AND LT IDG WAS PREVIOUSLY DEFERRED. BITE TO ECU WAS PERFORMED IAW FIM 49-11-00 AND "NO FAME" MESSAGE WAS SHOWN IN FAULT DISPLAY. APU OIL LEVEL WAS VERIFIED AND FOUNSDR AALA20040484Light · brokenLAS - SECTION OF EMERGENCY FLOOR TRACK LIGHTING AT SEAT 1B BROKEN. REPLACED FORWARD EMERGENCY FLOOR TRACK LIGHTING AT SEAT 1B. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20040365Light · inoperativeDFW - EMERGENCY FLOOR TRACK LIGHTING AT FIRST CLASS ROW ONE INOPERATIVE. REPLACED POWER STRIP FOR EMERGENCY FLOOR TRACK LIGHTING AT FIRST CLASS ROW ONE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20040237Cable · inoperativeDFW - EMERGENCY PATH LIGHT STRIP AT MID LAVATORY BY 2L DOOR INOPERATIVE. REPLACED RIBBON CABLE TO EMERGENCY PATH LIGHT STRIP IN FRONT OF MID LAVATORY BY 2L DOOR. SYSTEM GROUND CHECKED NORMAL OPRATION.SDR MEX2004040Line · leakingDURING PUSH BACK, FOUND HYDRAULIC LEAKAGE ON THE LT ENGINE WHEN IT WAS STARTED. AT REVISION WAS FOUND A BROKEN HYDRAULIC LINE, SUCH LINE WAS REPLACED BY AN ALTERNATE PN OF THE SAME PRESSURE CAPACITY AND SYSTEM TESTED IAW FIM.SDR MEX2004026Skin · damagedDURING OVERNIGHT SERVICE, IT WAS DETECTED THAT THE SLAT NR 5 HAD DAMAGES AND MATERIAL LOST IN A 20 X 10 INCH AREA, AND THE WING LEADING EDGE HAD DAMAGES TOO. SLAT NR 5 WAS REPLACED AND THE WING LEADING EDGE WAS REPAIRED IAW MM, ALL CORRECT.SDR MEX2004019Thrust Reverser · failedDURING TRANSIT REVISION, THE LT REVERSER WAS OPEN AND LIGHT AND MESSAGE WAS IN DISPLAY. THE REVERSER WAS REVISED AND ICE AND SNOW WAS DETECTED INTO THE REVERSE. THE REVERSER WAS NOT CLOSED COMPLETELY BECAUSE A GAP OF 2 INCHES IS BETWEEN COVERS. THE CABLE BESDR MEX2003560Indicator · leakingFLT 494 - MEX-LAX - AIRCRAFT PERFORMED AN UNSCHEDULED LANDING IN GDL AS CONSEQUENCE OF THE RIGHT QUANTITY INDICATION DECREASE TO .08 QUARTS. AT PLATFORM, THE HYDRAULIC SYSTEM WAS REPLENISHED TO DETECT THE LEAKAGE, THE DIFFERENTIAL PRESSURE INDICATOR WAS REPLASDR AALA20031435Blade · damagedEWR T785/15 EN ROUTE, ON CLIMBOUT AT 20,000 FT EXPERIENCED TWO COMPRESSOR STALLS FROM RT ENGINE. RT ENGINE LT AT IDLE AND LANDED EWR WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION. ON BOROSCOPE OF 6TH STAGE COMPRESSOR BLADES FOUND 18 DAMAGED BLASDR AALA20031399Battery Pack · dischargedSNA SEVERAL AFT GALLEY AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR SEVERAL AFT GALLEY AREA EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR MEX2003539Pump · failedAIRCRAFT RETURNED TO GATE DUE TO LOW OIL PRESSURE INDICATION ON NR 2 ENGINE DURING STARTING. SYSTEM WAS VERIFIED AND THE OIL PUMP WAS REPLACED IAW MM 79-21-04, TESTS WERE PERFORMED IAW MM 71-00-00, ALL OK. DURING THE OVERNIGHT SERVICE. THE ENGINE WAS VERIFISDR MEX2003534Pitot Tube · damagedAIRCRAFT RETURNED TO GATE DUE TO (R AUX PITOT) LIGHT WAS TURNED ON AND THE CABIN TEMPERATURE CONTROL HAD A FAILURE, TEMP REACHED 37 DEGREES CELSIUS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE RELATED PITOT WIRES/CONNECTORS AND THE CABIN SDR MEX2003530Light · inoperativeAIRCRAFT RETURNED TO PLATFORM DURING TAXIING RT AFT SLIDE ARMED LIGHT DID NOT TURN ON. AT PLATFORM, TECH PERSONNEL SWAPPED BOTH AFT SLIDE LIGHTS, AND CLEANED PROXIMITY SENSOR IAW MM 25-10-00, TESTS CORRECT.SDR MEX2003405Warning Light · illuminatedAIRCRAFT ARRIVED WITH CAPTAIN REPORT OF EICAS MESSAGE FLAP-SLAT ELEC. ONCE WE HAVE ADDITIONAL INFORMATION WE WILL SEND YOU AS SUPPLEMENT TO THIS REPORT.(K)SDR MEX2003408Wire · looseAIRCRAFT ARRIVED WITH CAPTAIN REPORT OF (WARN ELEX/ SLAT FLAP ELEC STATUS) MESSAGE IN EICAS. DURING REVISION WAS DETECTED BCPU POPPED DUE TO LOOSE OF WIRE NUMBER 5 TB 5001. THE BCPU C/B 6-14 WAS RESETED AND FSEU POWER OPERATED IN A NORMAL WAY TEST PERFORMED SDR MEX2003400Eec · failedAIRCRAFT RETURN TO PLATFORM, DURING RT ENGINE START WITHOUT EPR AND EGT INDICATIONS ON PRIMARY DISPLAY AND EGT INDICATION ONLY ON SECONDARY DISPLAY WITH CIRCUIT BREAKER THROWN AWAY P6, M16,17,18,22,23 AND 24. DURING REVISION WERE DETECTED EICAS MESSAGES P ADCSDR MEX2003399Eec · failedAIRCRAFT RETURNED TO PLATFORM , DURING TAXI, RT ENGINE SHUT OFF SLOWLY. DURING REVISION WERE DETECTED EICAS MESSAGES R ENG FUEL SOL, R ENG OIL PRESS. R ENG PRI CONT AND R ENG SEC CONT. THE ENGINE WAS CHECK FOR CONDITION AND DETECTING FLAME EVIDENCE IN TURBI
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