Boeing 757-2B7
Service difficulty reports · 3,730
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 = '7572B7' 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 = '7572B7' 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 USAA051226Floor Support · corrodedSTA 310.5-324 LBL 18.75 & WL 208.10; CORROSION LEVEL 1; TSK C53-221-003. FABRICATED & INSTALLED NEW FLOOR SUPPORT PEER SRM 53-00-00, 51-40-02 & DWG 141N5170, DEFECT SIZE: 3.0 X 2.75 X 0.050 INCH AREA.SDR USAA051224Plate · corrodedSTA 1680, LBL 12, LBL 32; CORROSION LEVEL 1; TSK C53-252-03. BLEND OUT PLUS DOUBLER & CUTOUT PLUS DOUBLER PER SRM 51-10-02, 53-00-51, DEFECT SIZE: 1.2"L X 2"W X .043"D, 1.3"L X 1.4"W X .019".SDR USAA051222Web · corrodedSTA 397-418 RBL 63 WL 208.10; LEVEL 1 CORROSION; TASK C53-222-03. REMOVED & INSTALLED NEW FLOOR WEB PER SRM 53-00-51, 51-40-02, DEFECT SIZE: 4.6 X 1.5 X 0.044 INCH.SDR USAA051225Support · corrodedSTA 1675 UNDER DOOR 4L THRESHOLD LBL 62; LEVEL 1 CORROSION; TASK C53-251-03. REMOVED & REPLACE SUPPORT, FABRICATED PART PER SRM 53-60-15, 51-10-02, 51-40-02, DWG 146N8712, DEFECT SIZE: .5" W X 2.0"L X .063"D.SDR USAA051206Crease Beam · corrodedMAIN CABIN BS 310 - 324, RBL 62, R1 DOOR AREA; NO LEVEL OR TASK. REPLACED CREASE BEAM WITH NEW FABRICATED BEAM ASSY PER SRM 53-00-51, FIG 101, 53-30-13. DEFECT SIZE 6 INCHES LONG X 1.5 INCH WIDE X .040 INCH DEEP.SDR USAA051207Intercostal · corrodedMAIN CABIN, BS 310-324, RBL 45 CORRODED. REPLACED CHANNEL INTERCOSTAL WITH NEW FABRICATED ASSY PER SRM 53-00-51, 51-40-02. DEFECT SIZE, 11 INCHES LONG X 5 INCHES WIDE X .025 INCH DEEP.SDR USAA051208Skin · erodedRIGHT AILERON UPPER SURFACE I/B EDGE ERRODED. REPAIRED AILERON (COMPOSITE) TIME LIMITED REPAIR PER EA 96922, SRM 51-60-01, 51-70-03. DEFECT SIZE NOT DOCUMENTED.SDR BB05087Lanyard · out of adjustTPA - FOUND ESCAPE SLIDE D-RING LANYARDS NOT VISIBLE ON L1, L2, R1, R2, AND R4 DOORS. ALSO, FOUND R2 DOOR D-RING TANGLED ON GIRT BAR. MAINTENANCE REMOVED SLIDE COVERS AND CORRECTED ROUTING OF LANYARDS ON L1, L2, R1, R2, AND R4 DOORS.SDR BB05082Sequence Valve · malfunctionedFLL FLT 365 EN-ROUTE CLT TO FLL - AFTER TAKE-OFF, AND UPON GEAR RETRACTION, RECEIVED EICAS MESSAGE "GEAR DOOR" WITH THE GEAR HANDLE UP. ALSO, THE LEFT GEAR DOOR LIGHT ILLUMINATED. HOWEVER, THE GEAR AMBER LIGHT AND ALL GREEN LIGHTS WERE EXTINGUISHED. THE CSDR BB05081Socket · failedCLT - MAINTENANCE REPORTED THE L4 EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD.SDR USAA051071Bulkhead · damagedMID BULKHEAD O/B FWD UPPER BOLT HOLE PP STA 164.3 DAMAGED. REAMED HOLE, INSTALLED SLEEVE BUSHING, REAMED PER EA 96822, DEFECT SIZE: .8810.SDR USAA051070Fitting · gougedNR 2 PYLON UPPER SPAR, AFT HOLE, OUTER SURFACE GOUGE. SPOT FACED DAMAGED AREA HFEC INSPECTED, SHOT PEENED, TREATED & INSTALLED FASTENER PER EA 96808. DEFECT SIZE: .045 INCH DEEP, 15.5 PERCENT MATERIAL LOSS.SDR BB05076Warning Light · false activationCLT - FLT 1123 EN ROUTE, PIT TO CLT, AFTER TAKEOFF, A "GEAR DOORS" EICAS MESSAGE APPEARED WITH THE GEAR HANDLE UP. ALSO, RECEIVED A "DOORS" AMBER LIGHT. THE "GEAR" AMBER LIGHT AND ALL GREEN DOWN LIGHTS EXTINGUISHED. CREW CYCLED THE GEAR AND ALL INDICATIONSSDR BB05075Warning Light · false activationCLT - FLT 667, EN ROUTE CLT TO LAS - AFTER TAKEOFF, RECEIVED AN EICAS MESSAGE "GEAR DOOR" WITH THE LANDING GEAR HANDLE UP. ALSO, RECEIVED AN AMBER "DOORS" LIGHT. THE GEAR LIGHT AND ALL THREE GREEN DOWN AND LOCKED LIGHTS EXTINGUISHED. THE CREW CYCLED THE GEASDR BB05072Charger · faultyCLT - THE AFT DOORS EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. SYSTEM CHECKS OK.SDR BB05071Battery · dischargedCLT - BATTERY FOR THE AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE AFT EMERGENCY LIGHT. SYSTEM CHECKS OK.SDR BB05070Charger · faultyTHE L-2 EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK CHARGER ASSEMBLY. OPERATIONALLY CHECKS OK.SDR BB05068Girt Bar · dislodgedCLT - MAINTENANCE FOUND THE L-4 DOOR SLIDE GIRT BAR PARTIALLY DISLODGED. MAINTENANCE REMOVED THE GIRT BAR, LUBED, AND THEN INSTALLED THE SAME GIRT BAR. OPERATIONALLY CHECKS OK.SDR BB05065Smoke Warning · activatedFLT 310 - EN ROUTE BWI TO CLT - IN FLIGHT, THE MID LAVATORY SMOKE DETECTOR BEGAN ALARMING. CREW NOTICED AN OIL ODOR IN FLIGHT. FLIGHT CONTINUED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE LEFT PACK ON MEL. PERFORMED A SATISFACTORY PASDR BB05066Haze · detectedEN-ROUTE, THE MID LAV SMOKE DETECTOR BEGAN TO ALARM DURING FLIGHT. THE CABIN CREW NOTED A LIGHT HAZE THROUGHOUT THE CABIN. THE FLIGHT CREW SHUT DOWN THE LT PACK AND CONTINUED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING.SDR BB05064Battery Pack · dischargedCLT - THE OVERHEAD EMERGENCY LIGHT AT ROW 13DEF WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECKS OK.SDR USAA050986Skin · corrodedBFM - C3 - SKIN, 2.5 INCH X 2.0 INCH X .048 INCH, 2.0 INCH X 2.5 INCH X .037 INCH, CORROSION; NO TASK OR LEVEL, STA 490-493, S-27 TO S-28L, STA 500, S27-S28L. INSTALLED DOUBLER IAW EA AND SRM. (K)SDR BB05063Slide · reads lowPHL - THE R-3 DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE R-3 DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE.SDR SA05058Slide · reads lowPHL - RIGHT OFF THE WING SLIDE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE RIGHT WING SLIDE BOTTLE. OK FOR SERVICE.SDR USAA050939Floorbeam · corrodedBFM - C3 -CHORD, 11 INCH X .90 INCH, CORROSION, STA 303-379, RBL 55. REPLACED FLOOR SUPPORT CHORD IAW SRM. (K)SDR USAA050919Channel · crackedBFM - C3 - U CHANNEL, 1.2 INCH X 1 INCH CRACK, STA 326, RBL43 INCH. REPLACED FLOOR SUPPORT U CHANNEL IAW SRM. (K)SDR USAA050918Channel · corrodedBFM - C3 - U CHANNEL, 14 INCH X 2.5 INCH X .04 INCH, CORROSION; NO LEVEL OR TASK STA 324-345, LBL 18 INCH. REPLACED FLOOR SUPPORT U CHANNEL IAW SRM. (K)SDR USAA050917Skin · corrodedBFM - SKIN - 2 INCH X 2 INCH X .022 INCH D - CORROSION; NO TASK OR LEVEL STA 1316, BET STR 28R AND 30, REPAIRED 1AW SRM AND EA. (K)SDR USAA050916Floorbeam · corrodedBFM - C3 - FLOORBEAM CAP, 6 INCHES L X 2.5 INCHES W X .05 INCH, CORROSION; NO LEVEL OR TASK, STA 324, RBL 40-46. REPAIRED IAW SRM AND EA. (K)SDR USAA050915Floorbeam · corrodedBFM - C3 - FLOORBEAM CAP 4.2 INCH X .020 INCH, 2 INCH X 2 INCH X .027 INCH, 2 INCH X 3 INCH X .020 INCH, 3.5 INCH X 2 INCH X .020 INCH, CORROSION; NO LEVEL OR TASK, STA 365, RBL 4 INCH/ RBL, 14 INCH/RBL 55 INCH/RBL 61. REPAIRED IAW EA. (K)SDR BB05056Slide · defectiveMCO - THE L-1 DOOR "SLIDE ARMED" LIGHT FAILED TO ILLUMINATE WHEN THE DOOR WAS ARMED. MAINTENANCE FOUND THE SPRING ON THE GIRT BAR DEFORMED AND INTERFERING WITH ARMING. MAINTENANCE REPLACED THE GIRT BAR AND ESCAPE SLIDE ON THE L-1 DOOR. OK FOR SERVICE.SDR BB05053Odor · detectedCLT FLIGHT 791 EN-ROUTE SJU TO CLT - DURING TAKE-OFF, FROM ROTATION UNTIL INITIAL CLIMB, A STRONG ODOR OF JET FUEL WAS NOTICED IN THE COCKPIT. AFTER FIVE SECONDS, THE ODOR WENT AWAY. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECSDR BB05054Odor · detectedDURING TAKE-OFF, FROM ROTATION UNTIL INITIAL CLIMB, A STRONG ODOR OF JET FUEL WAS NOTICED IN THE COCKPIT. AFTER FIVE SECONDS, THE ODOR WENT AWAY. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED FOR FUEL LEAKS AND FOUND NONE. ACSDR USAA050894Support · corrodedPIT - FOUND GAL SUPPORT FITTING CORRODED 2 INCH BY .75 INCH BY .03 INCH, MAIN CABIN STATION 368 RBL 12. REMOVED AND REPLACED WITH NEW PART PER SRM 53-00-51, 51-40-02. (M)SDR USAA050896Support · corrodedBFM - FOUND GAL SUPPORT CORRODED, 2.5 INCHES BY 1 INCH BY .05 INCH, MAIN CABIN STATION 398 RBL 12. REMOVED AND REPLACED WITH NEW PART PER SRM 53-00-51, 51-40-02. (M)SDR USAA050895Mount · corrodedBFM - FOUND LAV MOUNT CORROSION 1.5 INCH BY .075 INCH BY .05 INCH, MAIN CABIN STATION 324 LBL 12. REMOVED AND REPLACED WITH NEW PART PER SRM 53-00-51, 51-40-02. (M)SDR BB05049O-Ring · leakingIND FLT 634 EN ROUTE, LAS TO PHL. THE FLIGHT CREW NOTICED A 2400 LB PER HOUR FUEL LOSS. THE FIRST OFFICER CONFIRMED THAT THERE WAS A VAPOR COMING FROM THE RIGHT ENGINE PYLON AREA. THE CREW DIVERTED TO IND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SDR USAA050728Web · corrodedBFM - C4 - WEB, 3.0 INCH L X 2.0 W X .04 D, CORROSION; LEVEL 1; TASK C53-251-03 BETWEEN STA 1620, LBL 60. REMOVED WEB, FAB NEW IAW DWG AND SRM. (K)SDR USAA050735Support Fitting · corrodedBFM - C4 - GALLEY SUPPORT FITTINGS, .6 INCH L X .2 INCH W X .032 INCH D, .2 INCH L X .2W X .032, CORROSION; NO LEVEL OR TASK, STA 1686, RBL 6.5 AND LBL6.5. REPLACED GALLEY SUPPORT FITTINGS IAW SRM. (K)SDR USAA050734Sill · corrodedBFM - C4 - UPPER CAP, 3.1 INCH L X .5 INCH W X .2 INCH D; CORROSION, NO LEVEL OR TASK AFT CARGO DOOR LOWER SILL FROM AFT TO FWD DOOR CUTOUT. REMOVED AND REPLACED UPPER CAP. (K)SDR USAA050733Floorbeam · corrodedBFM - C4 - FLOORBEAM, 2.5 IN L X 2 IN W X .027 IN D, 2 IN L X 2 IN W X .016 IN D; CORROSION; LEVEL 1; TASK C53-252-03, STA1640, BL 0-LBL 60. REPAIRED AS OUTLINED. (K)SDR USAA050732Floor Support · corrodedBFM - C4 - FLOOR SUPPORT, 1.5 INCH L X 1.5 INCH W X .06 INCH D, 1.5 INCH L X 2 INCH X .050. CORROSION; LEVEL 1; TASK C53-252-03, BS 1640-1680 RBL 56. (K)SDR USAA050730Support · corrodedBFM - C4- THRESHOLD SUPPORT, 4.0 INCH X 3.4 INCH W X .040 INCH D - 3 AREAS - CORROSION; LEVEL 1; TASK C53-251-03, BS 1640-1680, LBL 60 INCH. REMOVED AND REPLACED THRESHOLD SUPPORTS IAW SRM. (K)SDR USAA050731Floor Support · corrodedPIT - C4 - FLOOR SUPPORT, 6 INCHES L X 1.5 INCHES W X .050 INCH D, 8 INCH L X 2 INCH WIDE X .060 INCH D, CORROSION; LEVEL 1; TASK C53-251-03, BS 1640, LBL 56. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM. (K)SDR USAABB05041Sensor · faultyDURING DESCENT, THE RT ENGINE FLAMED OUT WHEN POWER WAS APPLIED (12.00 FEET AT LEVEL OFF). THE CREW RESTARTED THAT ENGINE, AND LANDED WITH BOTH ENGINES POWERED. MAINTENANCE REPLACED THE TRANSIENT PRESSURE SENSOR.SDR USAA050727Floor Support · corrodedBFM - C4 - FLOOR SUPPORT, 1.0 INCH X 1.3 INCH X .020 INCH. CORROSION; LEVEL 2; TASK C53-221-03, S17L BET STA 365 AND 377 FL. FABRICATED ON TRAVELER NR T5/520007 21R FLOOR SUPPORT IAW SRM. (K)SDR USAA050685Support · corrodedBFM - C4 - THRESHOLD SUPPORT, .028 INCH D X 1.5 INCH WIDE X 1.5 INCH L, CORROSION; LEVEL 1; TASK C53-252-03, BS 1658, RBL 60 R4 DOOR. R & R THRESHOLD SUPPORT IAW SRM. (K)SDR USAA05686Floorbeam · corrodedBFM - C4 - FLOORBEAM UPPER CHORD, 1.5 L X 2.0 W X .020, 1.5: X 2 W X .029, 2L, CORROSION (3 AREAS); LEVEL 1; TASK C53-251-03, STA 1640 FROM BL0 - RBL 60. REPLACED UPPER CHORD SECTION IAW TYP REP. (K)SDR BB05030Engine · noisyFL 750 AT THE END OF CLIMB (FL350), CREW REPORTED THE RT ENGINE EXHIBITING LOUD NOISE VIBRATION. CREW REDUCED THRUST ON THE ENGINE, BUT THE VIBRATION CONTINUED. THE ENGINE WAS SECURED AND THE FLIGHT RETURNED TO CUN. (SET: 30 MINUTES.) MAINTENANCE ANALYSIS PSDR USAA050505Shim · migratedBFM - FOUND PYLON MID BULKHEAD SHIM MIGRATION, NR 1 PYLON MID BULKHEAD SHIMS, UPPER, REPLACEMENT AND REAMNG AFT UPPER HOLE. ACCOMPLISHED PER EO 5402R022A PARTS 2/6. (M)
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