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 TWAA0016001Light · brokenTHE EGRESS LIGHT STRIP AT SEAT ROW 29 WAS INOPERATIVE. REPLACED THE FLEX-LAMP. CHECK-C 9-27-99 LAX.SDR TWAA0014601Light · damagedEGRESS LAMP WAS INOPERATIVE IN THE MIDDLE OF FIRST CLASS AND THE BEGINNING OF COACH. REPLACED FLEX LAMP STRIP. CHECK-C 9-27-99 LAX.SDR TWAA0014502Wire · shortedTHE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 19 TO THE LT AFT LAV. FOUND JUMPER CABLE SHORTED AND BROKEN. REPLACED CABLE. CHECK-C 7-31-99 LAX.SDR TWAA0014003Video Unit · overheatedTHE VIDEO MONITOR AT ROW 27 ABC OVERHEATED. A SMALL AMOUNT OF SMOKE WAS OBSERVED AND IT WAS WARM TO TOUCH. VIDEO SYSTEM WAS DISABLED BY PULLING THE CIRCUIT BREAKER. THE VIDEO SCREEN WAS REPLACED. CHECK-C 9-27-00 LAX.SDR TWAA0011802Computer · malfunctionedTHE LEFT AUTOPILOT SELF-ENGAGED DURING TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. THE LEFT AUTOPILOT WAS DEACTIVATED AND DEFERRED PER MEL. CHECK-C 2-20-00 LAX. ---OPEN--- S/D. THE AUTOFLIGHT CONTROL SYSTEM MODE CONTROL PANEL (MCP) WAS REPLACED. TSDR TWAA0011304Skin · dentedDURING CHECK-C MAINT, THE LT WING I/B TRAILING EDGE FLAP, ON THE BOTTOM TOWARDS THE TRAILING EDGE, A DENT AND SCRATCH WAS FOUND APPROX 1 IN BY 1 IN BY .0625 IN DEEP. EDDY CURRENT FOUND A .75 INCH CRACK. INSTALLED A 4 INCH DIAMETER METAL HOT BOND REPAIR PER SSDR TWAA0010703Light · inoperativeTHE RT SIDE NR 3 CABIN DOOR EXIT LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 11-20-99 LAX. ---CLOSED---SDR TWAA0009501Wire · disconnectedDURING ROUTINE INSPECTION, IT WAS NOTED THAT EGRESS FLOOR LIGHTING WAS INOP. SPLICED IN REPLACEMENT JUMPER CABLE. AC06 05-18-00 LAX.SDR TWAA0006807Light · inoperativeTHE RT SIDE NUMBER 4 CABIN DOOR SLIDE LIGHT DID NOT ILLUMINATE WHEN ARMED. RELAMPED AND CLEANED THE PROX SWITCH. CHECK-C 2-20-00 LAX.SDR TWAA0006804Panel · gougedDURING CHECK-C MAINT, THE LT HORIZ STAB L/E REMOVABLE PANEL 3320L, TOP SIDE HAD A 3.5 FOOT BY. 125 INCH WIDE BY.0625 INCH DEEP GOUGE. REMOVED GOUGE PER SRM 55-10-01, PAGE 103 DETAIL II AND BLENDED AND ALODINED.SDR TWAA0004503Connector · wornCABIN EGRESS LIGHTS LOOSE CONNECTION IN FIRST CLASS FWD OF THE LAV. REMOVED AND REPLACED JUMPER CABLE TWA (P/N 91-8055). CHECKS MADE TO ASSURE NORMAL PERFORMANCE, OPS CK EGRESS LTS. AC 02 12-23-00 LAX.SDR TWAA0004401Engine · failedJUST AFTER TAKEOFF AT 900 FT AGL, THE LEFT ENGINE SURGED. TOWER REPORTED MOMENTARY FIRE OUT THE ENGINE, THE ENGINE WAS SHUT DOWN. THERE WAS NO FIRE WARNING BUT THE CREW ELECTED TO FIRE ONE FIRE BOTTLE. FLIGHT RETURNED TO MCO. BORESCOPE REVEALED COMPRESSOR SDR TWAA0003603Power Supply · overheatedVIDE O PLAYER INOP. RED FAIL LIGHT ON BOTTOM UNIT ILLUMINATED. SMELLS OF ELECTRICAL. REMOVED AND REPLACED VTR1 AND VTR2. AC09 12-01-99 LAX.SDR TWAA0003010Static Port · lightning strikeDURING CHECK-C MAINTENANCE, THE LEFT SIDE PRIMARY CAPTAINS AND FIRST OFFICERS STATIC PORTS HAD .1875 BY 0.008 DEEP LIGHTNING STRIKE ABOVE PORTS, APPROX STA 490 BETWEEN STRINGERS 20L AND 21L. BURNISHED AND FOUND TO BE WITHIN LIMITS OF SRM 51-10-01 PAGE 27. ALSDR TWAA0002202Light · looseDURING CRUISE, CABIN ATTENDANT FOUND EGRESS LIGHT STRIP DETACHED FROM THE FLOOR. MAINTENANCE RESECURED THE LIGHT STRIP.SDR TWAA0001607Rivet · corrodedTHE LEFT WING HAD 48 RIVETS WITH CORROSION REMOVED PER SRM 57-20-01 FIG 101. ONE RIVET REMOVED AND REPLACED AT STRINGER 4 WBL 326, ONE RIVET REMOVED AND REPLACED AT S-5 WBL 333. ONE RIVET REMOVED AND REPLACED AT S-5 WBL 328 PER SRM 51-40-02, PAGE 9. CHECK-CSDR TWAA0000801Battery Pack · dischargedTHE EMERGENCY LIGHT OVER SEAT ROW 12, RT SIDE OF CABIN, WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 9-12-99 LAX.SDR TWAA0001606Rivet · corrodedTHE RT WING HAD 126 RIVETS WITH CORROSION AT TOP WING SKIN FROM WBL 300 TO WBL 336, FROM FRONT SPAR TO REAR SPAR. REMOVED CORROSION PER SRM 57-20-01, FIG 106. SEVEN FASTENERS REPLACED PER SRM 51-40-02, PAGE 9 AT STRINGER 2, WBL 317, WBL 308, AFT SPAR AFT ROWSDR TWAA9915401Fuse · blownTHE RIGHT SIDE NUMBER 1 CABIN DOOR SLIDE LIGHT WAS INOPERATIVE. REPLACED FUSE AND IT BLEW AGAIN. REPOSITIONED THE LIGHT ASSEMBLY AND INSULATED THE CENTER BULB WIRE CONTACT, THEN REPLACED THE FUSE AGAIN. CHECK-C 7-31-99 LAX.SDR TWAA9914903Skin · corrodedFOUND CORROSION ON LT WING SKIN SURFACE FROM FRONT TO REAR SPAR UNDER THE BLACK ICE DETECTION STRIPE, STA 300 TO 360. REMOVED BLACK ICE DETECTION STRIPE. CLEANED CORROSION FROM SURFACE OF WING SKIN AND REPLACED TWO FASTENERS DUE TO CORROSION. CLEANED HOLES SDR TWAA9914902Skin · corrodedFOUND CORROSION AROUND MANY FASTENERS AND ON RT WING SKIN SURFACE UNDER BLACK ICE DETECTION STRIPE, FRONT TO REAR SPAR, STA 300 TO 360. REMOVED BLACK ICE DETECTION STRIPE. CLEANED CORROSION FROM SURFACE OF WING SKIN. REMOVED AND REPLACED 235 FASTENERS AND CSDR TWAA9913605Wire · brokenTHE EGRESS LIGHTS WERE INOPERATIVE AT THE MID LAVATORY AND AT ROW 5. REPAIRED BROKEN WIRES AT THE MID LAV, AND REPLACED TWO LAMPS AT ROW 5. CHECK-C 10-24-98 LAX.SDR TWAA9912902Skin · corrodedDURING CHECK-C MAINT, FOUND APPROX 200 RIVETS WITH STAGE 2 CORROSION ON TOP OF THE LEFT WING UNDER THE ICE DETECTION STRIPE, STA 341.5 THRU 425.5. *S/D* CORROSION WAS REMOVED BY BLENDING PER SRM 57-30-1 FIG 6, AT A 10:1 REMOVAL RATIO. ALL BLEND OUT AREAS WESDR 99ZZZX3574Blade · failedENGINE SURGED WITH OVERTEMP - METAL IN BLEEDS. DISASSEMBLED, INSPECTION DISCLOSED FAILURE OF 6TH STAGE COMPRESSOR BLADE. BLADES WILL BE FORWARDED TO P&W ENGINEERING FOR ANALYSIS. CYCLES, 2,867.SDR TWAA9912303Wire · brokenFOUND SECTION OF EGRESS LIGHTS OUT ROW 1 THROUGH 6. REPAIRED A BROKEN WIRE. CC01 12-11-99 LAX.SDR TWAA9911701Light · inopTHE CABIN EGRESS LIGHTS WERE INOPERATIVE AT THE RT AFT LAVATORY. CLEANED THE EGRESS STRIP. CHECK-C 1-20-99 LAX.SDR TWAA9909803Bearing · failedDURING TAKEOFF FROM STL, THE LEFT NOSE WHEEL ASSEMBLY SEPARATED FROM THE AIRCRAFT. FLIGHT OPERATED AND LANDED AT MCO WITHOUT INCIDENT. CHECK-C 1-20-99 LAX. INVESTIGATION FOUND THE OUTER BEARING OF THE LEFT NOSE GEAR WHEEL FAILED. THIS COMPROMISED THE RETENSDR TWAA9906102Connector · contaminatedFOUND THE EGRESS LIGHTS DIM AT ROWS 26 TO 34. DRIED OUT THE POWER SUPPLY CABLE AND THE LAMP CONNECTIONS. CHECK-C 5-9-98 LAX.SDR TWAA9904703Bulb · failedTHE EVACUATION SLIDE LIGHT WAS INOPERATIVE AT THE NUMBER 4 DOOR, RT SIDE OF THE AIRCRAFT. REPLACED THE LAMP. CHECK-C 12-11-98 LAX.SDR TWAA9901002Bulb · failedFOUND THE LEFT SIDE NUMBER 4 CABIN DOOR SLIDE LIGHT INOPERATIVE ON TEST. REPLACED THE LAMP AND SECURED THE LAMP IN THE SOCKET. CHECK-C 5-9-98 LAX.SDR TWAA9900202Skin · tornTHE FUSELAGE SKIN WAS TORN 6 INCHES BY 3 INCHES, BETWEEN S28 AND S29 ON LEFT SIDE AT STA 1806. EXTERNAL DOUBLER REPAIR INSTALLED PER MCIER RELEASE AND 757 SRM 53-00-01, FIG 204. CHECK-C 5-9-98 LAX.SDR TWAA9819002Wire · looseFOUND FIRST CLASS FLOOR EGRESS LIGHT STRIP INOPERATIVE. FOUND STRIP UNPLUGGED. SECURED CABLE. CHECK-C 7-19-98 LAX.SDR TWAA9818404Skin · crackedDURING CHECK-C MAINT, FOUND LEFT WING LEADING EDGE. BULLNOSE CRACK 10 INCH LONG ON COMPOSITE PANEL LOCATED AFT OF AND BETWEEN NR 3 AND 4 LEADING EDGE SLATS. INSTALLED 3 IN BY 10 IN HOT BOND REPAIR PER SRM 57-41-01 AND 51-70-07.SDR TWAA9814604Connector · looseEGRESS LIGHT INOP BY L-1 DOOR. SECURED CONNECTOR AND TRACK COVER. CHECK-C 01, 7-19-98 LAX.SDR TWAA9814603Connector · damagedEGRESS LIGHTS INOP IN FRONT OF LAV DOOR LT BEHIND FIRST CLASS. REPAIRED FLEX CABLE ASSY CONNECTORS MFG PN'S 65801-003 AND 97F9705. CHECK-C 01.SDR TWAA9814602Lamp · failedEMERGENCY AISLE LIGHT INOP AT ROW 17 FED, RELAMPED. CHECK-C 01, 7-19-98 LAX.SDR TWAA9811501Panel · crackedDURING CK-C01, FOUND LT WING TOP L/E PANEL AT OTBD END OF NR 4 L/E SLAT HAS A 7 INCH CRACK. DRESSED OUT DAMAGED AREA AND INSTALLED HOT BOND REPAIR PER SRM 51-70-07 PG 40 AND SRM 57-41-01 PG 20. (X)SDR TWAA9808203Acm · failedBWI - FLT 176 - DURING APPROACH, LT AIR CYCLE MACHINE MADE A BURNED SMELL IN THE CABIN. REPLACED THE LT AIR CYCLE MACHINE MFG PN 680640-4-3. OP-15. 5-14-97. NEW. (X)SDR TWAA9802701Oven · failedSTL - FLT 2 - AFT GALLEY NR 3 OVEN HAD ELECTRICAL SMELL WHEN POWER APPLIED. PULLED CB AND DID NOT USE OVEN. REPLACED THE OVEN. (M)SDR TWAA9802204Oven · dirtyJFK - FLT 31 - THREE GALLEY OVENS EMITTED SMOKE WHEN DOOR OPENED AFTER USE. POSITIONS WERE A GALLEY NR 1 AND NR 2 OVENS, AND B-GALLEY NR 2 OVEN. BELIEVED CAUSED BY CLEANING SOLVENTS. REPLACED THE A-GALLEY NR 1 AND NR 2 OVENS, DEACTIVATED AND DEFERRED THE B-SDR TWAA9712202Oven · overheatedJFK - FLT 901 - DURING CRUISE, THE B-6 OVEN OVERHEATED EMITTING SMOKE INTO THE CABIN AND SOUNDED THE ALARM. REMOVED AND REPLACED OVEN, MFG PN 8201-11-0000, MANUFACTURED BY BUDERUS SELL CORPORATION. OPERATIONAL CHECK NORMAL. OP16-7/16/97. (X)SDR 96ZZZM83Charger · inoperativeBOS - EGRESS LIGHTING SYSTEM INOPERATIVE, ROWS 11-19 AND 24-26. REPLACED BATTERY CHARGER ASSEMBLY FOR EGRESS LIGHTING SYSTEM ROW 11-19 AND 24-26. OPS CHECK NORMAL. (M)SDR 96ZZZX653Stator Vanes · crackedMDW - LEFT ENGINE SURGE DURING DECELERATION. ENGINE PARAMETERS NORMAL AFTER SURGE. REMOVED AND REPLACED LEFT ENGINE. FOUND CRACKED STATOR VANES.SDR 95ZZZX5197Eel Battery · dischargedMDW - ON DAILY SERVICE CHECK, FOUND AFT AISLE LIGHTS (EMERGENCY) WOULD NOT ILLUMINATE. REMOVED AND REPLACED AFT POWER SUPPLY PER 33 IN MM. OPS CHECK GOOD.SDR 95ZZZX3071Eel Power Supply · failedMDW - ON DAILY SERVICE CHECK, FOUND AFT AISLE LIGHTS (EMERGENCY) WOULD NOT ILLUMINATE. REMOVED AND REPLACED AFT POWER SUPPLY PER 33 IN MM. OPS CHECK GOOD.SDR 95ZZZX1192Bearing · oil leakPHOG - FLT 578 - DURING CLIMB, COCKPIT FILLED WITH SMOKE. PERFORMED AIR TURN-BACK. PERFORMED INSPECTION OF PACK SYSTEMS, INSPECTED ENGINES FOR LEAKS, NO EICAS MESSAGES. AIRPLANE WAS INSPECTED AND FOUND TO BE SAFE FOR A NON-REVENUE FLIGHT BACK TO MAINLAND USDR 95ZZZZ201Control · malfunctionMDW - CLIMBING OUT OF 30,000 FEET. AIRCRAFT ATTEMPTED TO ROLL RIGHT, RUDDER RATIO FLICKERED, THUMPING FELT IN RUDDER PEDALS AND FLIGHT ATTENDANT HEARD LOUD NOISE IN TAIL SECTION. FLT CONTINUED TO FLL. PERFORMED BITE CHECK OF RUDDER RATIO PER FIN 27-09-00 FISDR 95ZZZX1191Precooler Valve · failedMDW - FLT 575 - AT BEGINNING OF TAKEOFF ROLL WHEN POWER APPLIED, COCKPIT FILLED WITH HEAVY SMOKE. TAKEOFF ABORTED, RETURNED TO GATE FOR MX ACTION. REMOVED AND REPLACED FAN MOD. VALVE IAW MM 36-11-16, PERFORMED OPERATIONAL CHECK TO THE AIR SUPPLY DISTRIBUTION
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