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 ZW0A0209302Skin · crackedDURING CHECK-C MAINT THE NR 2 ENGINE PYLON, FWD ACCESS HOLE TO INTERIOR OF THE PYLON, APPROXIMATE NACELLE STA 162, THE OTBD SIDE HAD A CRACK 1.625 INCHES LONG. THE CRACK WAS LOCATED TOP FWD SECTION, AND VISIBLE ON OTBD TO INBD OF THE SKIN. ACCOMPLISHED BOEINSDR MEX2002145Warning System · activatedFLT 902 - MEX-MTY - AIRCRAFT RETURN TO GATE DUE TO CENTRAL AND LEFT HYDRAULIC SYSTEM RSVR LIGHT CAME ON. SUPPLY LINES AND DEPRESSURIZATION VALVES WERE CHECKED NO DAMAGE WAS FOUND. NITROGEN SYSTEM WAS SERVICED AND WAS TESTED IAW MM 29-11-00. DURING OVERNIGHTSDR MEX2002266Warning System · activatedAT START OF RT ENGINE, ALL THE FIRE ALARMS ACTIVATED. FUEL CONTROL WAS DISCONNECTED AND MASTER WARNING WAS ADJUSTED, CREW REQUESTED TO PERFORM A VISUAL INSPECTION TO CONFIRM FIRE PRESENCE. FIRE HANDLE WAS PULLED AND FIRE ALARM CONTINUED AFTER 30 SEC. THE FISDR ZW0A0208202Light · inoperativeEGRESS LIGHTS OUT ROW 14 AND 15 DUE TO WEAR. RELAMPED AT ROW 14. OPS CHECKED NORMAL. LAST CHECK-C LAX 6/12/01.SDR ZW0A0207901IndicatorLT MLG POSITION INDICATOR LOOSE IN SOCKET AND WILL NOT STAY LATCHED IN. R & R LT MLG POS IND 26-1424. OPS CK POS IND OK. LAST CHECK C PERFORMED LAX 8/3/01. --CLOSED--SDR MEX2002216Fan · malfunctionedFLT 490 - MEX-LAX - CAPTAIN ABORTED TAKEOFF, RADAR FAILED, OVERHEAT LIGHT WAS ON AND BURNING SMELL WAS DETECTED. DURING CHECK RADAR AND EICAS MESSAGES WERE OK AND BURNING SMELL DISAPPEARED. AIR CONDITIONING PACKS, TRIM VALVES WERE CHECKED, ALL OK. AIRCRAFT SDR ZWOA0207002Bulb · burned outEGRESS LIGHTING AT SEAT 19C INOP. RELAMPED LIGHT. LAST CHECK C PERFORMED 10/14/2000 AT LAX. --CLOSED--SDR ZW0A0206903Skin · crackedDURING CHECK-C MAINT ON THE RT PYLON THE FWD INBD SIDE LIGHTNING HOLE ON NUMBER 2 PYLON WAS CRACKED 1/2 INCH LONG. CONFIRMED BY NDT. REPAIRED PER SERVICE BULLETIN 757-54-0037, AND EMLR 73125. --CLOSED--SDR ZW0A0206902Structure · crackedDURING CHECK-C MAINT ON RT PYLON, THE FWD OTBD SIDE LIGHTNING HOLE ON THE NUMBER 2 PYLON WAS CRACKED ABOUT 1/2 INCH LONG. CONFIRMED BY NDT. REPAIRED PER SERVICE BULLETIN 757-54-0037 AND EMLR 73125. --CLOSED--SDR ZW0A0206901Skin · crackedDURING CHECK-C MAINT ON NUMBER 1 PYLON FOUND A 1 7/8 INCH CRACK EXTENDING FROM UPPER FORWARD CORNER OF FORWARD LIGHTNING HOLE IN LT SIDE SKIN OF PYLON. CONFIRMED BY EDDY CURRENT. INSTALLED FORWARD DOUBLER ON OTBD SIDE PER SERVICE BULLETIN 757-54-0037 AND EMLSDR ZW0A0206401FanOILY SMOKE WAS REPORTED THROUGHOUT THE CABIN DURING TAKEOFF. THE LH AIR CONDITIONING PACK WAS SHUT OFF AND SMOKE DISSIPATED. THE LH PACK WAS PLACARDED INOPERATIVE PER MEL AND THE AIRCRAFT WAS OPERATED TO ANOTHER STATION WHERE THE LH RECIRCULATION FAN WAS REPLSDR MEX2002187Slide · out of adjustFLT 170 - MEX-TIJ - CAPTAIN REPORTED THAT THE DOOR NR 1 SLIDE WAS NOT ARMED. DURING CHECK WAS DETECTED THAT THE ARMED LIGHT WAS INOPERATIVE AND THE ACTIVATION MECHANISM WAS IN AN ABNORMAL POSITION. TECHNICAL PERSONNEL TRIED TO REMOVED THE DOOR COVER AND THE SDR ASM2002F00002Actuator · failedDURING INSPECTION, DETECTED A LEAK IN THE RIGHT FUEL TANK. THE LEAK WAS AT THE RIGHT SHUTOFF VALVE. RIGHT TANK WAS SEALED. DURING OVERNIGHT SERVICE THE O-RINGS OF SHUTOFF VALVE ACTUATOR WAS REPLACED IAW MM.SDR MEX2002123Panel · failedFLT 902 - MEX-MTY - AIRCRAFT GOT PLATFORM WITHOUT AUDIBLE FIRE ALARMS. PERFORMED A FIRE DETECTION TEST IAW FIM 26-11-00 AND WEU AUDIBLE SYSTEM TEST IAW FIM 31-51-00. M100 ELECTRONIC CARD WAS CHANGED AND TESTS WERE PERFORMED IAW MM 31-51-04. DURING OVERNIGHTSDR MEX2002105Probe · failedFLT 404 - MEX-JFK - AIRCRAFT WAS SENT TO THE HANGAR FOR HIGH EGT ON NR 2 ENGINE (930 GRADES). PERFORMED A FIM PROCEDURE DETECTED THE PROBES T/C 2 T/C 6 OUT OF LIMITS. THEY WERE CHANGED AND AN EGT TEST WAS PERFORMED DURING ENGINE RUNNING IAW MM 77-21-01. (M)SDR ZW0A0203601Lamp · burned outRIGHT FWD AND LEFT FWD EMERGENCY DOOR SLIDE LIGHTS INOP. RELAMPED RIGHT FWD AND LEFT FWD EMERGENCY SLIDE LIGHTS. LAST CHECK C PERFORMED 14NOV2001 MCI --CLOSED--SDR ZW0A0203202Splice · damagedTHE EGRESS LIGHT AT CABIN ROW 12 WAS INOPERATIVE. REPAIRED THE SPLICE AT ROW 12.SDR MEX2002067Panel · failedFLT 941 - MTY-MEX - CABIN CREW REPORTED OTU OF SERVICE THE LANDING ALTITUDE SELECTOR, AS CONSEQUENCE OF SPARE PARTS MISSING IN MTY, MEX SENT SUCH PARTS IN FLT 944. AT ARRIVING, THE SELECTOR PANEL WAS SWAPPED, TEST OK, IAW MM 21-31-01. AT RON MEX 13/14 TESTS SDR ZW0A0201902Lamp · missingDURING LAYOVER SERVICING, EGRESS LAMP MISSING AT FIRST CLASS SEAT - ROW 2L. INSTALLED MISSING LAMP, OPS CHECK NORMAL. CHECK-C 12/12/01. ---CLOSED---SDR ZW0A0201901Connector · detachedDURING LAYOVER SERVICE, THE EGRESS LIGHTING STRIP FOUND INOP AT -D- LAVATORY DOOR. REPAIRED ELECTRICAL CONNECTION TO MAIN POWER SUPPLY FOR -D- LAV DOOR AND OPS CHECK NORMAL. CHECK-C 12/12/01. ---CLOSED---SDR MEX2002027Actuator · failedFLT 402 - MEX-NYC - DURING TRANSIT CHECKED ENGINE NR 1 AND THE REVERSER WAS FOUND DEACTIVATED. THE WIRE BUNDLE OF THE REVERSER CONTROL VALVE WAS CHAFED AGAINST THE WIRE BUNDLE OF THE FIRE DETECTOR. WIRE BUNDLES WERE ISOLATED, REVERSERS WORKED OK AND NO SCREESDR MEX2002026Controller · failedFLT 906 - MEX-MTY - AIRCRAFT RETURNED TO PLATFORM AFTER A PRESSUATIZATION FAIL MESSAGE. MAINT TESTED BOTHE PRESSURE CONTROLLERS AND FOUND THAT THE ACTUATOR FAILED. REPLACE ACTUATOR IAW MM. REPLACED BOTH CONTROLLERS.SDR MEX2002025Valve · failedFLT 913 - MTY-MEX - AIRCRAFT RETURNED TO PLATFORM, EICAS MESSAGE LEFT HYD RSVR PRESS WARNING. THREE QUARTERS OF HYDRAULIC FLUID WAS ADDED, RVSR WAS DISCONNECTED AND CLEANED, AFTER ENGINE WAS STARTED FAIL APPEARED AGAIN, AIRCRAFT TOOKOFF IN THAT CONDITION. HYSDR MEX2002024Valve · leakingFLT 913 - MTY-MEX - AIRCRAFT ARRIVED TO PLATFORM WITH HYDRAULIC FLUID LEAK IN THE LEFT WING. IT WAS CHECKED AND THE LEAK WAS FOUND AT SPOILER PCA NR 3 LEFT SIDE, EHSV BODY. CANCELLED THE PRESSURE AND RETURN PORTS AND DISCONNECTED THE ELECTRIC CONNECTOR OF THSDR MEX2002015Wire Harness · damagedFLT 239 - GDL-MEX - CREW REPORTED THAT DURING THE ENGINE STARTING, THE ENGINE 1 WAS NOT STABILIZED, THE RPM'S REMAINED AT 42 PERCENT AND MAINTENANCE AREA REPORTED THE PRESENCE OF FLAME IN SUCH ENGINE. AT CHECKING IT WAS FOUND A DAMAGE IN THE WIRE BUNDLE NEAR SDR ZW0A0112402Skin · crackedDURING CHECK-C MAINT THE WINDOW BELT LOWER LAP SEAM AT STA 1618, BELOW STRINGER 14R, HAD SKIN DAMAGE. THE LOWER INNER SKIN WAS CRACKED. REPAIRED PER ARA 17863, PAGE 1 THRU 6.SDR ZW0A0200105Skin · corrodedDURING CHECK-C MAINT FOUND TWO STATIC BURN PITS WITH 3 INCH CIRCLE OF LIGHT CORROSION. AREA HAD BEEN GROUND APPROX 0.025 DEEP, LOCATED CENTER OF LAP SEAM, STRINGER 4L AND STA 1223. REPAIRED PER ARA 17864.SDR ZW0A0111901Light · inoperativeTHE EMERGENCY LIGHT AT SEAT ROW 2D, AND THE EGRESS LIGHTS ROW 14 TO 18, WERE INOPERATIVE. REPLACED THE LAMP, PN 8074-1, AT ROW 2D, AND REPLACED SPLICE, PN 65801-003, AT ROW 14 FOR THE EGRESS LIGHTS AT ROW 14 TO 18.SDR ZW0A0110501Cable · brokenTHE EGRESS LIGHTS AT THE REAR LAVATORY WOULD NOT TEST. REPLACED THE FLEX CABLE.SDR ZW0A0108613Flap · puncturedDURING CHECK-C MAINT ON LT WING THE LOWER SURFACE OF THE INBD FOREFLAP, MIDDLE SECTION, HAD .25 INCH WIDE PUNCTURE AND 1 INCH LONG DENT, LOCATED JUST OTBD AND AFT OF THE INBD CANOE FAIRING. INSTALLED HOT BOND REPAIR AND PRIMED AND PAINTED PER SRM 51-70-10.SDR ZW0A0108704Doubler · delaminatedDURING CHECK-C MAINT THE TOP SURFACE JUST AFT OF L/E AND 6 FT OTBD OF FUSELAGE, FOUND PATCH DELAMINATED WITH RAGGED EXPOSED EDGE. INSTALLED 4 .5 INCH DIAMETER METAL TO METAL HOT BOND REPAIR ON UPPER LEFT HORIZONTAL STABILIZER PANEL PER SRM 55-10-01, PAGE 1, ASDR ZW0A0108703Skin · crackedDURING CHECK-C MAINT FOUND AT STA 1365 AND STRINGER 23L, 2 DAMAGE AREAS WITHIN 6 INCHES OF STATIC PORT. GOUGE AND DENT ABOVE PORT. SHOWS EDDY CURRENT CRACK. INSTALLED 1 INCH ROUND REPAIR, FLUSH TYPE, PER SRM 53-00-01, FIG 208 PAGE 225.SDR ZW0A0108612Bar · wornDURING CHECK-C MAINT ON THE NUMBER 1 INBD PYLON, THE EQUALIZER BAR HOLE IN THE PYLON FWD OF AFT REVERSER MOUNT, THE FWD EDGE OF THE HOLE WAS WORN. CLEANED AND SMOOTHED OUT AREA PER SRM 54-5-01.SDR ZW0A0108611Skin · wornDURING CHECK-C MAINT ON THE NUMBER 1 PYLON, THE AFT REVERSER EQUALIZER BAR HAD WEAR SPOT AT CONTACT POINT WITH INBOARD SKIN. CLEANED UP AND SMOOTHED OUT AREA PER SRM 54-51-01.SDR ZW0A0108102Power SupplyWHEN ELECTRICAL POWER WAS LOST THE FLOOR AND CEILING EMERGENCY LIGHTS IN THE MID AND AFT CABIN STAYED ON AND WOULD NOT RESET. REPLACED THE POWER SUPPLY. CHECK-C 7-22-00 LAX. --CLOSED--SDR ZW0A0106302Skin · dentedDURING MAINTENANCE SMALL DENTS WERE DISCOVERED AT FLIGHT STATION 640 AND WL 200. REMOVED OLD EXTERNAL DOUBLER ALSO REMOVED DOUBLER FROM NEW DAMAGED AREA AND INSTALLED NEW EXTERNAL DOUBLER PER SRM BETWEEN STN. 640 TO 196 AND BETWEEN STN. 196 AND 216.SDR ZW0A0106102Wire · wornDURING PRE FLIGHT EGRESS LIGHT STRIP NEXT TO LAV C WERE INOP DUE TO WEAR. INSTALLED NEW CABLE.SDR ZW0A0105405Skin · dentedDURING CHECK-C MAINT FOUND STATION 650 STRINGER 17L, 4 FOOT FWD OF THE LEFT SIDE NUMBER 2 CABIN DOOR, WITH 2 EACH SMOOTH DENTS. THE FWD DENT WAS .75 IN BY .75 IN BY .1875 IN DEEP. AFT DENT WAS 1 IN BY 1 IN BY .0625 IN DEEP. CUT OUT DAMAGED SKIN AND INSTALLESDR ZW0A0104702Eec · failedIN CLIMB THE RT ENG STALLED THEN SHUT ITSELF DOWN. FLIGHT RETURNED TO STL. REPLACED THE EEC STATOR, P/N 430219, AND THE EEC ROTOR, P/N 46038. CHECK-C 6-12-01 LAX.SDR ZW0A0102703Connector · disconnectedWITH POWER REMOVED FROM THE AIRCRAFT THE EMERGENCY EXIT LIGHTS AT ROWS 24 AND 26 ILLUMINATED. FOUND LOOSE ELECTRICAL CONNECTOR AT M10919 AND SECURED SAME. CHECK-C 7-22-00 LAX.SDR ZW0A0102005Connector · dirtyTHE EGRESS LIGHT AT SEAT ROW 1 WAS INOPERATIVE. CLEANED AND RE-INSTALLED THE LAMP CONNECTOR. CHECK-C 4-12-01 LAX.SDR ZW0A0101602Light · inoperativeTHE EGRESS LIGHT WAS INOPERATIVE AT SEAT 1A. REPLACED THE FLEX LAMP ASSY. CHECK-C 4-12-01 LAX.SDR ZW0A0100602Engine · leakingTHE LEFT ENGINE OIL QUANTITY DECREASED IN FLIGHT. OIL PRESSURE EVENTUALLY DECREASED TO RED LINE. ENGINE WAS SHUT DOWN, AN UNSCHEDULED LANDING MADE AT DTW. CHECK-C 10-17-99 LAX.SDR TWAA0105502Light · inoperativeTHE EGRESS LIGHT WAS INOPERATIVE BY THE LEFT SIDE LAV AND AT SEAT ROW 1 LEFT SIDE. REPLACED THE LAMP AT BOTH LOCATIONS. CHECK-C 5-4-00 LAX.SDR TWAA0104404Door · dentedENGINEERING REQUESTED A PERMANENT REPAIR TO A DENT JUST FWD AND BELOW THE LEFT SIDE NUMBER 4 CABIN DOOR, STA 1610 AND STRINGER 18L. INSTALLED AN EXTERNAL DOUBLER 8 IN BY 10 INCHES USING BLIND FASTENERS PER SRM 53-00-01. CHECK-C 9-27-99 LAX.SDR TWAA0103401Fmc · failedAIRCRAFT RETURNED FROM FLIGHT AT LAX TWICE WITH A DUAL FMC FAILURE. THE FIRST TIME THE RT FMC COMPUTER WAS REPLACED, (P/N 4052506-941-945). THE SECOND TIME THE AIRCRAFT WAS REMOVED FROM SERVICE. CHECK-C 11-20-99 LAX.SDR TWAA0101604Bottle · dischargedTHE LEFT SIDE NUMBER 4 CABIN DOOR EVACUATION SLIDE HAD LOW BOTTLE PRESSURE. REPLACED THE SLIDE ASSEMBLY. CHECK-C 9-27-99 LAX.SDR TWAA0100801Lamp · inoperativeTHE EGRESS SYSTEM SWITCH LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 10-17-99 LAX.SDR TWAA0100301Engine · failedIN CRUISE A LOUD BANG WAS HEARD FROM THE LEFT ENGINE AND IT SPOOLED DOWN. MADE AN UNSCHEDULED LANDING AT MSP. THE ENGINE WAS REPLACED. CHECK-C 12-5-00 LAX.SDR TWAA0019602Video Display · faultySMOKE WAS COMING FROM THE VIDEO MONITOR AT SEAT ROW 23, RT SIDE. CREW PULLED CIRCUIT BREAKER AND SHUT OFF THE VIDEO. MAINTENANCE PULLED ALL CIRCUIT BREAKERS, REMOVED THE CONNECTOR, AND DEFERRED CORRECTIONS PER MEL. THE VIDEO MONITOR WAS LATER REPLACED. CHECK-C
Back to Boeing 757-2Q8