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 07FDEA03054Skin Panel · damagedLT SIDE OF FUSELAGE HAS A DIVOT IN THE SKIN AND RUNNING INTO A RIVET AT STATION 700, APPROXIMATELY 5" ABOVE STRINGER 23L. MEASURED THE DAMAGED AREA PER SRM 53-00-01 AND SRM 53-00-01. OUT OF LIMITS IAW SRM 53-30- 01. ACCOMPLISHED REPAIR IAW EA F-5310-110755SDR USAA920070801Floor Support · corrodedBFM - MAJOR REPAIR - C-04 CHECK - CORROSION FOUND ON LT HAND TUNNEL ABOVE NLG FLOOR SUPPORT WEB, BS 310 - BS 324, LBL 20. REPLACED LT HAND TUNNEL ABOVE NLG FLOOR SUPPORT WEB, BS 310 - BS 324, LBL 20 IAW 757-200 SRM 51-40-02, SRM 51-42-08, AND SRM 51-40-02.SDR BB07068Charger · failedMAINTENANCE FOUND THE AFT RIGHT EMERGENCY LIGHT BATTERY AND CHARGER INOPERATIVE. REPLACED BATTERY AND CHARGER. NO FURTHER FAULTS.SDR 07FDEA02963Skin · corrodedNR 2 STRUT, RT SIDE, SIDE SKIN AT APPROXIMATELY NAC STA 144 INTERNAL, IS CORRODED ON SKIN AND UNDER LOWER FRAME/CHORD. REMOVED CORROSION FROM INTERNAL SKIN AS MARKED PER SRM 54-50-01. ORIGINAL SKIN THICKNESS (DOUBLER SIDE) .090", AFTER REWORK .075" AT LOWESDR BB07066Filter · deterioratedFLIGHT 725, SNN-PHL: AFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED INSULATION LIKE MATERIAL COMING FROM OVERHEAD VENTS. FLIGHT RETURNED TO SNN. MAINTENANCE FOUND THAT THE LEFT RECIRC FILTER HAD BROKEN DOWN, ALLOWING MATERIAL FROM FILTER INTO THE DUCT SYSTEM. TSDR 07FDEA02871Bushing · misalignedACCOMPLISHED DVI OF THE LT WING OUT BOARD DRAG FITTING AND FOUND THE INBOARD SIDE BUSHING MIGRATED .060 INCH. REMOVED BUSHINGS IAW SOPM 20-50-03. HFEC INSPECTED FITTING IAW NTM 51-00-16, PT.6. NO DEFECTS NOTED. HONED, CHAMFERED AND FLAP PENNED LUG BORES IASDR 07FDEA02869Bushing · misalignedRT WING OUTBOARD UPPER LINK FITTING HAS MIGRATING BUSHINGS. REMOVED BUSHINGS PER SOPM 20-50-03. INSPECTED FITTING PER NTM 51-00-00, PT.6, NO DEFECTS NOTED. HONED, CHAMFERED FLAP PEENED AND SWAGED PER F-5450-108892 FINAL DIA OF THE LUG BORE IS 1.7507. TRESDR BB07064Charger · inoperativeMAINTENANCE FOUND THE L4 AND R4 DOOR ESCAPE SLIDE LIGHTS INOPERATIVE. REPLACED THE BATTERY CHARGER. NO FURTHER FAULTS.SDR 07FDEA02825Skin · corrodedNUMBER ONE STRUT/PYLON, LT SIDE SKIN, AT APPROXIMATE NAC STA 144, INTERNAL, IS CORRODED ON SKIN AND UNDER LOWER FRAME/CHORD. REMOVED CORROSION IAW SRM 54-50-01. ORIGINAL MATERIAL THICKNESS WAS .090", AFTER REWORK REMAINING MATERIAL THICKNESS WAS .079", OUT OSDR BB07057Controller · failedFLIGHT 724, PHL-SNN: TWENTY MINUTES INTO FLIGHT, COCKPIT TEMPERATURE BEGAN TO RISE. WHEN TEMPERATURE REACHED 97F, THE CAPTAIN ELECTED TO PHL. MAINTENANCE REPLACED THE ZONE TEMP CONTROLLER.SDR BB07055Socket · inoperativeMAINTENANCE FOUND THE FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LIGHT SOCKET. NO FURTHER DIFFICULTIES.SDR BB07054Light · brokenMAINTENANCE FOUND THE R4 DOOR EMERGENCY LIGHT BROKEN. REPLACED LIGHT ASSEMBLY.SDR 07FDEA02518Stringer · damagedAFT PIT - BS 1640 S27L, DRILL MARKS IN STRINGER (4 EACH HOLES) BLENDED DRILL MARKS ON STRINGER 27L IAW SRM 53-00-03. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, FIG 101, SHEET 1. NO HOLES ALLOWED. REMOVED DAMAGE IAW SRM 53-00-03, FIG 201. FABRICATED REPAIRSDR 07FDEA02517Skin · corrodedBULK CARGO - BILGE AREA, BS 1580, BETWEEN S27R AND 28R, SHEAR TIE AND SKIN EXFOLIATED. REMOVED AND REPLACED SHEAR TIE AS IT HAD 100 PERCENT MATERIAL LOSS IAW SRM 51-40-02. SHEAR TIE WAS FABRICATED ON MAE TRAVELER T7/689492 IAW SRM 51-10-01. REMOVED CORROSIOSDR 07FDEA02509Stringer · damagedAFT PIT, STATION 1660 AT STRINGER 27R, HAS TOOLING MARKS ON STRINGER. BLENDED TOOL MARKS FROM STRINGER IAW SRM 53-00-03. FOUND TO BE OUT OF LIMITS PER SRM 53-00-03, FIG 101. REMOVED DAMAGED SECTION OF STRINGER IAW SRM 53-00-03, FIG 201. FABRICATED REPAIR STSDR 07FDEA02507Skin · dentedEXTERNAL FUSELAGE HAS A LARGE DENT AT STATION 1507 ON STRINGER 2R. FOUND TO BE OUT OF LIMITS PER SRM 53-00-01, FIG 101. CUT OUT DAMAGE ON SKIN PER SRM 53-00-01, FIG 201. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED DOUBLER IAW SRM 51-20-01.SDR 07FDEA02508Stringer · damagedAFT PIT, BS 1660, S26R DAMAGED. BLENDED DAMAGE ON STRINGER IAW SRM 53-00-03. FOUND TO BE OUT OF LIMITS PER SRM 53-00-03, FIG 101. REMOVED DAMAGED SECTION OF STRINGER IAW SRM 53-00-03. FABRICATED REPAIR STRINGER. FABRICATED FILLER IAW SRM 53-00-03, FIG 201SDR BB07051Light · missingMAINTENANCE FOUND THE L4 DOOR EMERGENCY LIGHT MISSING. REPLACED LIGHT ASSEMBLY.SDR USAA920070793Skin · crackedBMH - MAJOR REPAIR - C-4 CHECK - NR 6000784, RIGHT WING LEADING EDGE SLAT NR 9 INNER SKIN CRACKED, WS 623.5. REPLACED RIGHT WING LEADING EDGE SLAT NR 9 INNER SKIN CRACKED, WS 623.5 IAW B757 SRM 51-40-02.SDR USAA920070792Floorbeam · corrodedBFM - MAJOR REPAIR - C-4 CHECK - NR 6000701, CORROSION ON CABIN FLOORBEAM, BS 365, RBL 20 - RBL 25, WL 208. REPAIRED CABIN FLOORBEAM, BS 365, RBL 20 - RBL 25, WL 208 IAW USAIRWAYS TYPICAL REPAIR 53-15-01.SDR BB07044Electrical Box · smokeFLIGHT 1729, BOS-CLT: ON DESCENT INTO CLT, SMOKE BEGAN TO FILL THE CABIN. CREW ACCOMPLISHED SMOKE IN CABIN PROCEDURES AND THE CABIN CLEARED. MAINTENANCE FOUND THE SEB AT ROW 10AC TO BE THE SOURCE. REMOVED SEB AND CABLE. RELEASED PER MEL. [07-10-07] REPLSDR BB07045Power Supply · inoperativeMAINTENANCE FOUND THE R1 SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY.SDR BB07042Bracket · damagedMAINTENANCE FOUND GIRT BAR ENGAGEMENT LIGHT EXTINGUISHED WITH THE EVACUATION SLIDE ARMING LEVER IN THE ARMED POSITION AT DOOR 4L. FOUND GIRT BAR WOULD NOT ENGAGE DUE TO WORN/MISSING PARTS ON DOOR MECHANISM. REPAIRED BRACKET FOR GIRT BAR. NO FURTHER FAULTS NSDR USAA070464Angle · corrodedBS 719.6 - 745.6 RBL 62.45 ANGLE HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-30-15, 51-10-02, 51-40-02, DEFECT SIZE: 6 X 1 INCHES.SDR USAA070465Support · corrodedBS 720 - 740 RBL 62.45 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-30-15, 51-10-02, 51-40-02, DEFECT SIZE: 6 X 1 INCH.SDR USAA070466Support · corrodedBS 680-700, RBL 62.45, GUTTER SUPPORT ASSEMBLY HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-30-15, 51-10-02; 51-40-02, DEFECT SIZE: 4 X 1 INCH.SDR USAA070416Floor Support · corrodedCABIN FLOOR SUPPORT LBL 0, STA 345.0-395 HAS CORROSION. BLENDED AT STA 374 BL 0, REMOVED & REPLACED FLOOR SUPPORT AT STA 324-395 AT BL 0 PER SRM 53-00-51, DEFECT SIZE: 4.5"L X 2"W X .016"D.SDR USAA070398Floorbeam · corrodedSTA 345, LBL 0 - LBL 20, CABIN FLOORBEAM CORRODED. BLENDED AREA & INSTALLED DOUBLERS PER TYP REP 53-15-02, 51-20-01, CORR TASK C53-221-03; LEVEL 1, DEFECT SIZE: 1"L X 1"W X .013"D.SDR USAA070399Floorbeam · corrodedRBL 14-17 STA 1660 CABIN FLOORBEAM FASTENER HOLES CORRODED. INSTALLED FAB'D NUT PLATE STRIP ANGLE PER TYP REP 53-15-02, 51-40-02, CORR TASK C53-251-03; LEVEL 1, DEFECT SIZE: 3"L X .800"W X .025"D.SDR BB07037Brake · crackedFLIGHT 0728, PHL-GLA: AFTER TAKEOFF, HYDRAULIC QUANTITY STARTED DROPPING ON BOTH LEFT AND RIGHT SYSTEMS. RETURNED TO PHL. MAINTENANCE FOUND THE NUMBER 7 BRAKE HOUSING CRACKED. REPLACED BRAKE.SDR USAA070259Angle · corrodedBS 740-800, WL 208.1, RBL 64.40 HAS CORROSION. REMOVED, FABRICATED & INSTALLED CHORD IAW BOEING DWG 143N5520 & SRM 51-40-02, PARA 7(D) FIG 12, DEFECT SIZE: 15 X 1 INCH.SDR USAA070258Support · corrodedR2 DOOR CUTOUT BS 720-740 HAS CORROSION. REMOVED, FABRICATED & INSTALLED SUPPORT PER SRM 51-40-02, FIG 3 & 8, DEFECT SIZE: 3 X 1 INCH.SDR BB07029Windshield · crackedFLIGHT 888, LAS-FLL: IN CRUISE, 1R WINDOW DEVELOPED EXTENSIVE SPIDERWEB CRACKING. FLIGHT DIVERTED TO PHX. MAINTENANCE REPLACED THE WINDSHIELD ASSEMBLY AND THE HEAT CONTROLLER.SDR BB07021Relay · faultyDEN - FLT773 EN ROUTE FROM PHL TO LAS, CREW REPORTED, LOST THE NR 2 ENGINE IDG AND WERE UNABLE TO START THE APU. CREW DECLARED AN EMERGENCY AND DIVERTED TO DEN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE K176 APU DOOR INLETSDR BB07017Apu · failedFLIGHT 1026, TPA-CLT: ON TAXI OUT, CABIN BEGAN TO FILL WITH SMOKE AND THE LAV SMOKE DETECTORS BEGAN TO SOUND. FLIGHT RETURNED TO GATE. MAINTENANCE FOUND THE APU HAD CONTAMINATED THE A/C SYSTEM WITH OIL. ACCOMPLISHED DE-CONTAMINATION OF AIR DISTRIBUTION SYSSDR USAA070086Mount · corrodedAFT GALLEY RIGHT OUTBOARD MOUNTS 2 EA AROUND BARREL NUT HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER BOEING DWG 415N40C2; CORR LEVEL 1; TASK JL-58-5316, DEFECT SIZE: 1 INCH.SDR USAA070087Mount · corrodedAFT GALLEY LEFT OUTBOARD MOUNTS 2 EA AROUND BARREL NUT HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENT PART PER BOEING DWG 415N40C2; CORR LEVEL 1; TASK JL-58-53516, DEFECT SIZE: 1 INCH.SDR USAA070088Floor Support · corrodedAROUND NUT PLATE HOLES (90 PERCENT) CTR FLOOR SUPPORT BL 0 STA 1640-1681.8 HAS CORROSION. REPLACED CHANNELS PER SRM 51-40-02; CORR TASK JL-58-53516; LEVEL 1, DEFECT SIZE: 1 INCH.SDR USAA070089Attach Angle · corrodedTOP, LWR & FWD SIDES OF APU INTAKE DOOR ON 3 ATTACH ANGLES HAS CORROSION. MFG ANGLES PER BOEING DWG 148N3152 & SRM 53-00-07, DEFECT SIZE: 10 SQ INCHES.SDR USAA070081Galley Track · corrodedAFT GALLEY RT OUTBOARD MOUNTS 2 EA HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER BOEING DWG 415N40C2; CORR LEVEL 1; TASK JL-58-5316, DEFECT SIZE: 1 INCH.SDR BB07012Charger · failedMAINTENANCE FOUND EMERGENCY LIGHT ON BULLNOSE 12/13R INOPERATIVE. REPLACED BATTERY CHARGER AT 12R. NO FURTHER DIFFICULTIES.SDR USAA070058Seat Track · wornBS 850-879 LBL 24.75 WORN. REMOVED DAMAGED SECTION OF SEAT TRACK & REPLACED PER SRM 53-00-52, DEFECT SIZE: 1 X 1 INCH.SDR USAA070057Seat Track · wornBS 850-879 LBL 45.5 WORN. REMOVED DAMAGED SECTION OF SEAT TRACK & REPLACED PER SRM 53-00-52, DEFECT SIZE: 1 X 1 INCH.SDR USAA070056Seat Track · wornBS 850 - 879 RBL 24.75 WORN. REMOVED DAMAGED SECTION OF SEAT TRACK, REPLACED PER SRM 53-00-52, DEFECT SIZE: 1 X 5 INCHES.SDR USAA070055Seat Track · wornSEAT TRACK BS 850 - 879 RBL 45.5 WORN. REMOVED DAMAGE SECTION OF SEAT TRACK & REPLACED PER SRM 53-00-52, DEFECT SIZE: .5 X .5 INCH.SDR BB07010Power Supply · inoperativeBDL - MAINTENANCE REPORTED THE AFT SECTION OF EMERGENCY LIGHTS ARE DIM. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK AT POSITION M736. OPERATIONAL CHECK GOOD.SDR USAABB07009Bypass Valve · malfunctionedCLT FLT 722 EN ROUTE CLT TO BWI. ON APPROACH, THE NOSE LANDING GEAR WAS SLOW TO EXTEND. FLIGHT ABORTED APPROACH AND MADE A GO-AROUND. CREW LOWERED THE GEAR BY USING THE ALTERNATE GEAR EXTENSION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS MASDR USAABB07007Valve · failedFLIGHT 704, LAS-CLT: WHEN GEAR WAS EXTENDED ON APPROACH, NOSE GEAR GREENLIGHT DID NOT ILLUMINATE AND AMBER -DOORS- AND -GEAR- LIGHTS REMAINED ON. ABORTED APPROACH, RECYCLED GEAR, RECEIVED THREE GREEN LIGHTS. LANDED WITH NO FURTHER DIFFICULTIES. MAINTENANCESDR USAABB07004Actuator · failedFLIGHT 1827, PHL-FLL: NOSE GEAR GREEN LIGHT FAILED TO ILLUMINATE WITH GEAR HANDLE DOWN. EICAS MESSAGE GEAR DISAGREE AND GEAR DOORS DISPLAYED. DOORS AND GEAR AMBER LIGHTS ILLUMINATED. INDICATIONS WERE NORMAL AFTER ALTERNATE GEAR EXTENSION. FLIGHT LANDED WISDR USAABB07003Charger · inoperativeMAINTENANCE FOUND AFT GALLEY EMERGENCY LIGHT ABOVE R4 DOOR INOPERATIVE. REPLACED BATTERY CHARGER. NO FURTHER FAULTS.
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