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 MEX2003386Engine · malfunctionedFLT 494 - MID-MEX - AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER RIGHT ENGINE STARTED, IT SHUT DOWN. RIGHT ENGINE AND EICAS MESSAGES WERE CHECKED IAW 72-00-00 AND RIGHT ENGINE WAS RESTARTED, ALL CORRECT. DURING OVERNIGHT SERVICE, RIGHT ENGINE WAS SDR MEX2003387Shutoff Valve · malfunctionedDURING PUSH BACK AND LEFT ENGINE STARTING, ENGINE VALVE LIGHTS TURNED ON, SPAR VALVE DID NOT GO OFF AND N2 WAS BETWEEN 25 PERCENT AND 30 PERCENT WITHOUT EGT INCREMENTATION. THE SPAR VALVE AND FUEL SHUTOFF VALVE WERE RESET IAW MM 73-10-01, ALL TEST CORRECT. DSDR MEX2003360Shutoff Valve · failedAIRCRAFT RETURN TO PLATFORM AFTER LEFT ENGINE WAS STARTED. THE LT FUEL SPAR VALVE LIGHT COME ON AND THE LEFT ENGINE SHUTDOWN WITH CODE 282209. DURING REVISION, WAS DETECTED FUEL SHUTOFF VALVE ACTUATOR DAMAGED, THE FUEL SHUTOFF VALVE ACTUATOR WAS REPLACED IAWSDR ZW0A0306101Spring · brokenDURING CHECK-C THE EVACUATION SLIDE GIRT BAR LEAF RETENTION SPRING WAS FOUND BROKEN AND REPLACED AT THE L1 AND R1 CABIN DOORS. THE SPRINGS WERE FOUND DEFORMED AND REPLACED AT THE L2, R2, L4 AND R4 CABIN DOORS.SDR ZW0A0306001Spring · deformedTHE EVACUATION SLIDE GIRT BAR LEAF RETENTION SPRING AT THE R1, L2, AND R4 DOOR WERE DEFORMED AND ADJUSTED. THE RETENTION SPRING AT THE L4 DOOR WAS REPLACED ACCOUNT DEFORMED.SDR MEX2003280Module · malfunctionedAIRCRAFT RETURNED TO GATE, EICAS STATUS MESSAGE ELEV ASYM. FIM PROCEDURE WAS PERFORMED WITH NEGATIVE RESULTS IAW 27-09-00 FIG 106 PAGE 150. THE STAB/TRIM ALL LOCK AND ASYM MODULE WAS INTERCHANGED IAW FIM PROCEDURE 27-09-00, ALL TESTS CORRECT. (M)SDR MEX2003276Regulator · failedAIRCRAFT AIR TURN BACK DUE TO (RT ENGINE BLEED OFF) AND (RT PACK OFF) MESSAGES AT 310 FT, LOOSING CABIN PRESSURE AND APPEARING MESSAGE OF CABIN ALTITUDE WITH AUDIBLE ALARM. AIRCRAFT WAS SENT TO THE HANGAR. PILOT PRESSURE REGULATOR AND TEMPERATURE SENSOR OFSDR MEX2003273Antenna · failedAIRCRAFT ARRIVED WITH CAPTAIN REPORT RADAR OUT OF SERVICE. DURING REVISION WAS DETECTED WAVE GUIDE WITH DAMAGE. AIRCRAFT WAS SENT TO THE HANGAR, AND THE WAVE GUIDE WAS REPLACED IAW 34-40-01. ADDITIONALLY AS A PREVENTIVE ACTION ANTENNA RADAR WAS REPLACED, ALSDR MEX2003325Turbine · damagedMEX-TIJ - FLT 176 - AIRTURN BACK, DURING TAKEOFF RIGHT ENGINE HAD 600 DEGREES CELSIUS REDUCING THRUST TO MAINTAIN TEMPERATURE ON LIMITS. DURING EHM ANALYSIS WAS DETECTED R EGT YELLOW MESSAGE AND AIRCRAFT WAS SENT TO THE HANGAR. DURING REVISION DETECTED MISINGSDR MEX2003261Fmc · inoperativeDURING TRANSIT CHECK WAS DETECTED BOTH INTERNAL SYSTEM OUT SERVICE IN ANY SELECTION. THE BOTH FMC COMPUTER SYSTEM WERE DEFERRED IAW MEL. FMC COMPUTERS WERE REPROGRAMMED IAW MM 34-21-00, ALL TESTS CORRECT.SDR ZW0A0305705Spring · brokenAN EVACUATION SLIDE GIRT BAR LEAF RETENSION SPRING WAS BROKEN AND REPLACED AT THE L1 AND R1 DOORS.SDR ZW0A0305702Spring · deformedTHE EVACUATION SLIDE GIRT BAR RETENSION LEAF SPRINGS WERE ADJUSTED ACCOUNT DEFORMED ON THE L1, R1, L2, R2, L4, AND R4 CABIN DOOR.SDR MEX2003237Indicator · failedAIRCRAFT RETURN TO PLATFORM DUE TO TCAS NR 1 BLOCKED WITH INDICATION IN DISPLAY. THE INDICATOR VSI/TRA DISPLAY WAS REPLACED IAW 34-22-06, ALL TEST CORRECT.SDR MEX2003236Packing · failedAIRCRAFT ARRIVED WITH CAPTAIN REPORT WITH 1 QUART OF OIL IN ENGINE NR 2. DURING REVISION WAS DETECTED LEAK IN RIGHT HYDRAULIC PUMP. THE RIGHT HYDRAULIC PUMP PACKING WAS REPLACED IAW MM. DURING OVERNIGHT SERVICE RIGHT HYDRAULIC PUMP WAS REPLACED IAW 29-11-40SDR MEX2003222Shaft · brokenFLT 402 - MEX-JFK - AIRCRAFT RETURN TO PLATFORM, ENGINE NR 1 DID NOT START. DURING REVISION, THE STARTER SHAFT WAS BROKEN. THE STARTER WAS REPLACED IAW MM 80-11-01, ALL TESTS CORRECT. (M)SDR MEX2003220Bypass Valve · leakingFLT 494 - MID-MEX - AIRCRAFT RETURN TO GATE, HYDRAULIC LEAK AT LEFT COMPARTMENT RESERVOIR AND DURING ENGINES STARTING THE 'LIGHT RUDDER PCU' EICAS STATUS MESSAGE TURN ON. THE LEFT SLATS BYPASS VALVE WAS REPLACED IAW MM, TASK CARD 27-81-09-024-001 AND 27-81-09SDR MEX2003193Recorder · failedDURING TRANSIT CHECK, FLT REC OFF LIGHT TURNED ON. ASSOCIATED BRAKES WERE RESET BUT FAIL CONTINUES. WIRING WAS CHECKED IAW WDM 31-31-03, ALL CORRECT. FLIGHT DATA RECORDER AND FDAU WERE REPLACED IAW MM 31-31-03, ALL TESTS CORRECT. (M)SDR MEX2003174Engine · malfunctionedAIRCRAFT RETURN TO PLATFORM DUE TO NR 1 ENGINE DID NOT START. STARTER VALVE WAS CHECKED AND IGNITION WAS CORRECT. TESTS PERFORMED IAW MM 74-21-0. AFTER THIS CHECK LEFT ENGINE STARTING WAS CORRECT IAW MM 80-10-00.SDR ZW0A0304802Bulb · inoperativeTHE EXTERNAL EMERGENCY LIGHT AT THE LEFT SIDE NUMBER 4 CABIN DOOR WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 5-27-02 MCI.SDR MEX2003212Inlet · damagedFLT 6444 - MEX-HMO - DURING TRANSIT CHECK, DETECTED FAN INLET GUIDE DAMAGED BY AND FOD. IN THE HANGAR THE FAN INLET GUIDE WAS REWORKED, TEST PERFORMED IAW 72-00-00, ALL CORRECT. (M)SDR MEX2003159Warning Light · illuminatedAIRCRAFT RETURNED TO PLATFORM DUE TO MACH SPEED TRIM MESSAGE ILLUMINATION. THE BITE TEST ON P61 ADC WAS ACCOMPLISHED AND LIGHT ILLUMINATION IN OVERHEAD P11. FLIGHT CONTROLS TEST WAS ACCOMPLISHED AND LT ELEV PCU MESSAGE ILLUMINATED. THE MESSAGE APPEARED ONLYSDR MEX2003155Actuator · inoperativeAIRCRAFT RETURN TO PLATFORM DUE TO RUDDER PCA EICAS MESSAGE. THE RUDDER MODULE WAS VERIFIED AND THE ALARM WAS FOUND IN RIGHT RUDDER RATIO. IN HANGER THE FIM 27-21-00 PROCEDURE WAS ACCOMPLISHED. BEING ALL CORRECT.SDR MEX2003150Control Unit · failedDURING TRANSIT CHECK CAPTAIN REPORTED NORM ANTI-SKID AND ALTN ANTI-SKID MESSAGES IN EICAS. MESSAGE APPEARED EVERY TIME THAT THE PARKING BRAKES WERE USED. FIM PROCEDURE WAS ACCOMPLISHED BUT NO FAILURE CODE APPEARS. AIRCRAFT WAS SENT TO THE HANGAR. ANIT-SKIDSDR MEX2003149Shutoff Valve · failedAIRCRAFT SUSPENDS TAKE OFF DUE TO EICAS (L FLT CONT HYD) MESSAGE. THE HYDRAULIC SHUTOFF VALVE WAS VERIFIED AND IT WAS CORRECT. FIM PROCEDURE WAS ACCOMPLISHED AND NON FAILURE INDICATION WAS DETECTED. DURING OVERNIGHT SERVICE THE HYDRAULIC SHUTOFF VALVE WAS RSDR MEX2003137Arm · jammedCAPTAIN REPORTED THAT WAS NOT POSSIBLE TO ARM THE EMERGENCY SLIDE OF DOOR NR 4 IT WAS JAMMED. AIRCRAFT WAS SENT TO THE HANGAR WHERE WAS TESTED AND ADJUSTED THE MECHANISM WAS ADJUSTED IAW MM 52-11-20, ALL CORRECT. (M)SDR ZW0A0303604Light · inoperativeTHE MOST FORWARD EGRESS LIGHT STRIP IN THE FIRST CLASS CABIN WAS INOPERATIVE. REPAIRED BROKEN FEEDER SYSTEM. CHECK-C 11-14-01 MCI.SDR MEX2003092Valve · malfunctionedMEX-TIJ - AIRCRAFT RETURNED TO GATE, NOSE WHEEL TURN TO THE RIGHT DURING TAKEOFF AND IT WAS ABORTED, DURING REVISION WAS DETECTED METER VALVE VERY HOT. IN HANGAR, NOSE WHEEL STEERING VALVE WAS REPLACED IAW MM 32-51-00, TESTS CORRECT. (M)SDR MEX2003089Valve · malfunctionedTIJ-MEX - AFTER LANIDNG IN GROUND TO TURN THE STEERING WHEEL TO THE RT WAS VERY HARD, WITH CODE OF FAIL 32-51-07-04. IN HANGAR NOSE WHEEL STEERING SYSTEM ADJUSTMENT AND TEST WERE PERFORMED IAW MM 32-51-00, TESTS CORRECT. (M)SDR MEX2003055Girt Bar · stuckAIRCRAFT RETURNED TO PLATFORM DUE TO LEFT AFT SLIDE DOOR NR 4 WAS NOT ARMED, ARMED AND DISARMED SYSTEM, AFT SLIDE DOOR 4 WAS CHECKED AND IT WAS STUCK. AIRCRAFT WAS SENT TO THE HANGAR. EMERGENCY MECHANISM WAS ADJUSTED IAW MM, TEST CORRECT.SDR ZW0A0302704Light · dislodgedON ARRIVAL EMERGENCY STRIP BY MID LAV PULLED UP. REINSTALLED EGRESS LIGHT SYS PN 5774-1 TWA 91-8032. OPS CHECKED NORMAL PER MM33-51-11. CHECK-C MCI 10-12-02.SDR ZW0A0302403Battery · dischargedDURING CRUISE EMERGENCY EXIT LIGHTS AND AISLE STRIP LIGHTS COME ON INTERMITTANTLY WITH COCKPIT EMERGENCY LIGHT SW IN BOTH ARMED AND OFF POSITIONS DUE TO LOW BATTERY. REPLACED BATTERY, OPS CHECKED NORMAL. CHECK-C 7/7/02.SDR MEX2003029Slide · stuckAIRCRAFT RETURNED TO PLATFORM, LEFT AFT SLIDE WAS NOT ARMED. ARMED AND DISARMED MECHANISM OF LEFT AFT SLIDE WAS CHECKED, IT WAS STUCK. BAR WAS REMOVED AND REINSTALLED IAW MM, TESTS CORRECT.SDR MEX2003016Warning System · malfunctionedFLT 600 - MEX-ALT - AIRCRAFT RETURNED TO PLATFORM, DURING ENGINES STARTING, MESSAGE EICAS STATUS MAIN BATTERY CHARGE. RESET PROCEDURE WAS PERFORMED AND MESSAGES WAS ERASED, BUT WHEN BATTERY AND BARS WERE DISCONNECTED MESSAGES EICAS STATUS LEFT AND RIGHT CONTRSDR ZW0A0301002Scavenge Pump · leakingDURING CRUISE OIL QTY DROPPED FROM 11 QTS TO 5 QTS WITH CONTINUING DROP UNTIL RIGHT ENGINE OIL PRESSURE EICAS MESSAGE. PERFORMED ENGINE FAILURE CHECKLIST. SHUT DOWN ENGINE AND DIVERTED TO TAMPA. FOUND OIL LEAKING FROM SCAVENGE PUMP NIPPLE. REPLACED SCAVENGE PSDR MEX2002367Indicator · failedAIRCRAFT RETURNED DUE TO FIRST OFFICER AIRSPEED INDICATOR OUT OF SERVICE, CAPTAIN PERFORMED ABNORMAL PROCEDURES AND FAIL CONTINUED DURING DESCENT, AIRSPEED INDICATOR STARTED FUNCTIONING AND WARNING INDICATIONS STOPPED. FIRST OFFICER AIRSPEED INDICATOR AND CASDR ZW0A0212401CylinderTHE LEFT SIDE NUMBER 2 CABIN DOOR, THE ASSIST BOTTLE PRESSURE WAS LOW. REPLACED THE CYLINDER. CHECK-C 12-10-02 MCI. --CLOSED--SDR ZW0A0212101MonitorTHE PASSENGER ENTERTAINMENT MONITOR AT CABIN ROW 27, LEFT SIDE, OVERHEATED AND CAUSED AN ELECTRICAL ODOR. FLIGHT MADE AN UNSCHEDULED LANDING AT JAX. THE ELECTRICAL CONNECTOR WAS REMOVED FROM THE MONITOR AND THE AIRCRAFT OPERATED MINIMUM EQUIPMENT. THE MONITSDR MEX2002347Panel · failedCAPTAIN REPORTED THAT THE RT ENGINE BLEED VALVE SWITCH WAS OUT OF SERVICE PANEL WAS REMOVED AND SWITCH WAS UNCLOGGED AND PNEUMATIC SYSTEM WAS LET OUT OF SERVICE IAW MM. DURING TRANSIT PANEL ASSEMBLY BLEED AIR WAS REPLACED IAW MM.SDR MEX2002346Indicator · malfunctionedFLT 171 - JIJ- DURING TAKEOFF EPR INDICATIONS WAS BLANK RIGHT ENGINE AND N1 WITH FLUCTUATIONS AT REDUCE POWER ON RIGHT ENGINE AFTER 5 MINUTES INDICATIONS WAS NORMAL. AFTER 35 MINUTES IN FLIGHT RETURNED TO AIRPORT. AT PLATFORM, TECHNICAL PERSONNEL CHECKED CHPSDR ZW0A0211821Battery · dischargedSECTION OF EGRESS LIGHTING INOPERATIVE, REPLACED BATTERY AND POWER SUPPLY UNIT. LAST CHECK C PERFORMED MCI 10/12/2002SDR ZW0A0211201Power Supply · dischargedTHE EMERGENCY LIGHTS AT THE RH SIDE NUMBER 3 CABIN DOOR, AND AT THE MID LAVATORY AREA, WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT POWER SUPPLY AT THE R3 DOOR. CHECK-C 11-14-01 MCI. --CLOSED--SDR ZW0A0211101Battery Pack · dischargedTHE LEFT SIDE NUMBER 4 CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. THE POWER SUPPLY AND BATTERY PACK WERE REPLACED.SDR MEX2002309Engine · bird ingestionFLT 490 - MID-MEX - DURING TAKEOFF AFTER THE ROTATION MOVEMENT, LEFT ENGINE HAD A BIRD STRIKE, THE ENGINE MOMENTARILY STALLED BUT IT RECOVERED ALL PARAMETERS ITSELF. AT MEX, PERFORMED BORESCOPE INSPECTION TO SUCH ENGINE IAW MM 71-05-00 FIG 103. ENGINE WAS FOSDR MEX2002300Warning System · false activationAIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF THE LIGHT (OIL FILTER CLOGGING) TURNED ON DURING LT ENGINE STARTING. TECH PERFORMED AN ERASER PROCEDURE AND THE ENGINES WERE STARTED AGAIN, MESSAGE DID NOT APPEAR AGAIN AND PARAMETERS WERE, OK.SDR MEX2002299Fuel Control · failedFLT 600 - MEX-ATL - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF AN STARTING FAILED OF THE RIGHT ENGINE. AT POSITION 24, TECHNICIANS TRIED STARTING AGAIN AND ENGINE REACHED 52 PERCENT OF N2 BUT EGT'S WERE HIGH. AT HANGAR, THE FMC WAS REPLACED IAW MM 73-21SDR MEX2002297Hydraulic Line · leakingFLT 405 - JFK - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF AN HYDRAULIC LEAKAGE IN THE RIGHT SYSTEM. TECHNICIAN REVIEWED SUCH SYSTEM AND FOUND LEAKAGE IN A PIPELINE FROM THE FILTERS TO THE WHEELS. PIPELINE WAS REPLACED IAW MM 29-11-17, TESTS OK. (M)SDR ZW0A0209604Skin · crackedDURING CHECK-C MAINT FOUND CRACKS IN PYLON DURING REPAIR. FWD ACCESS HOLE NACELLE STA 116.5 EMITTING FWD APPROX 1.5 INCHES, INBD AND OTBD SIDES. ACCOMPLISHED REPAIR PER EMLR 73252 AND SB 757-54-0037.SDR ZW0A0209603Skin · crackedDURING CHECK-C MAINT CRACKS FOUND ON NUMBER 2 PYLON THE FWD ACCESS HOLE AT NACELLE STA 116.5, OTBD AND INBD OF PYLON, CRACKS 1.625 INCHES LONG AT TOP FWD SECTION OF ACCESS HOLE. CRACK IS VISIBLE ON OTBD AND INBD SIDE OF SKIN. ACCOMPLISHED BOEING SERVICE BULLSDR ZW0A0209602Skin · crackedDURING CHECK-C MAINT IN THE NUMBER 2 PYLON, THE FWD ACCESS HOLE TO INTERIOR AT APPROX NAC STA 116.5, THE OTBD SIDE OF PYLON HAD CRACK 1.625 INCHES LONG. CRACK LOCATED TOP FWD SECTION OF ACCESS HOLE. CRACK IS VISIBLE ON OTBD AND INBD SIDE OF SKIN.SDR ZW0A0209403Skin · crackedDURING CHECK-C MAINT ON NUMBER 2 PYLON 1.5 INCH CRACKS GOING AFT WERE FOUND INBD AND OTBD FORWARD ACCESS HOLE AT NACELLE STA 120 BETWEEN STA 116.05 AND 128. ACCOMPLISHED EMLR 73249.
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