Boeing 757-232
Service difficulty reports · 15,843
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 = '757232' 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 = '757232' 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 DU4R2007002Floor Support · tool damageFLOOR SUPPORT STRINGER HAS DRILL BIT DAMAGE BS 594 LBL 11 FWD CARGO COMPT. CUT OUT DRILLED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED 2 ANGLES 9" BY 1" BY 1" FROM 7075-T6 .050" AND 2 ANGLES 10" BY 1" BY 1" FROM 2024-T3 .040" IAW B757 SRM 51-70-12, FIGSDR DU4R2007001Floor Support · damagedFLOOR SUPPORT STRINGER HAS DRILL BIT DAMAGE BS 590 LBL 11 FWD CARGO COMPT. CUT OUT DRILLED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED 2 ANGLES 10" BY 1" BY 1" FROM 7075-T6 .050" AND 2 ANGLES 8" BY 1" BY 1" FROM 2024-T3 .040" IAW B757 SRM 51-70-12, FIGSDR DALA1133780682Actuator · unknownHORIZONTAL STAB TRIM ACTUATOR REPLACED IAW EA 06-086621-03, ME01.SDR DL757061046Engine · leakingSTRONG ODOR ON T/OFF ROLL WITH FORWARD LAV SMOKE DETECTOR CHIRPING, 10-15 SECONDS SMELL DISSIPATED BUT IS STILL DETECTABLE. MX INSPECTED ENGINE. FOUND EVIDENCE OF OIL LEAK FWD CLOSED ENGINE COWLING SERVICED LEFT ENGINE WITH 10 PINTS. PREPARED A/C FOR FERRY SDR DL757061042Engine · failedWINDING UP FOR T/O HEARD AUDIBLE ENGINE SURGE/STALL PASSENGERS OBSERVED FLAMES COMING FROM LEFT ENGINE. A/C RETURNED TO GATE. MTC INSPECTED TAIL PIPE FOUND BB SIZED DEBRIS. WILL NEED ENGINE CHANGE. REPLACED NR 1 ENG PER ROUTINE CARD DECK TRANS 6T103.SDR DU4R2007004Seat Track · corrodedLT O/B SEAT TRACK CORRODED AT BS 810 AND 830. CUT OUT SECTION OF TRACK FROM BS 780 TO BS 879. FABRICATED AND INSTALLED REPAIR TRACK SECTION BAC1520-792 IAW DWG NR 143N5116, 53-00-52 AND 51-40-02.SDR DU4R2006709Skin · corrodedFOUND CORROSION ON SKIN UNDER AFT LAV SERVICE PAN BS 1681 AND S-26R TO S-29R. FABRICATED AND INSTALLED DOUBLER REPAIR 19.5" BY 18" BY 22" BY 15.75" FROM 2024-T3 .063" AND FILLER IAW DELTA ERA 458954-14 REV ORIG DATED 12-05-06.SDR DL757061043Skin · crackedTHE FUSELAGE SKIN HAS CRACK INDICATIONS IN EXISTING HOLES IN THE L1 DOOR OPENING, FORWARD UPPER CORNER. THE CRACKED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.SDR DL757061035Collar · crackedREPORTED TO MTC 4R DOOR WILL NOT STAY OPEN. FOUND 4R DOOR GUST LOCK COLLAR BROKEN/CRACKED. REPLACED GUST LOCK COLLAR PER AMM 52-11-08.SDR DU4R2006710Skin · dentedLEFT LWR FUSELAGE HAS A DENT AT BS 640 S-17L. CUT OUT DENTED AREA. FABRICATED AND INSTALLED DOUBLER REPAIR 9.20" BY 8.75" BY 11.10" BY 5.10" FROM CLAD 2024-T3 .050" AND 2 SHIMS 8.5" BY 4.5" BY 10.6" AND 9.7" BY 1.45" BY 10.7" FROM CLAD 2024-T3 .040" IAW B757SDR DU4R2006708Stringer · corrodedCORROSION ON AFT PIT S-29L BS 1405. CUT OUT CORRODED SECTION OF STRINGER AND FRAME. FABRICATED AND INSTALLED DOUBLER REPAIR FROM 7075-T6 .071", DRILLED AND INSTALLED CHANNEL NR 4 P/N NR 727-6982, CHANNEL NR 6 P/N 654N0010-135, ANGLE NR 7 P/N BAC1493-791 ANSDR DL757070040Wedge · damagedTRAILING EDGE WEDGE REPLACED REF SRM57-43-02D, FIG 202. WORKED ON SON W59082. SLAT WAS REMOVED FROM AIRCRAFT AND SENT TO STOCK WHEN SERVICEABLE.SDR DL757061032Flap System · malfunctionedT/E FLAP DISAGREE MSG WHEN EXTENDING FLAPS FROM 15DEG TO 20DEG USED ALT FLAPS SYS TO EXTEND FLAPS 20DEG PER QRH. FOUND LT I/B XMSSN INDICATOR POPPED. RESET INDICATOR. LUBED FLAPS INSPECTED ROLLER AND TRACKS--NTF. OPERATED FLAPS. ALL CKS NORMAL. SERVICED SDR DL757061027Light · inoperativeON APP GEAR SELECTED DOWN LEFT GEAR GREEN LIGHT DID NOT ILLUMINATE CHECKED LIGHT TEST BULB WAS OK AFTER GA. QRH PROCEDURE FOLLOWED AFTER RECYCLE OF GEAR LIGHT REILLUMINATED LND NML. NO ASSOCIATED EICAS ON CONFIG WARN NOTED. DEBRIEFED CREW FOUND LT GEAR GREESDR DU4R2006696Floor Support · corrodedCORROSION AFT PIT FLOOR SUPPORT ANGLE BETWEEN BS 1500 - BS 1520 AND LBL 5. FABRICATED AND INSTALLED REPAIR ANGLE 6-1/4" BY 1-1/4" BY 5" FROM BAC1517-2226 IAW B757 SRM 51-40-05, 51-20-01 AND 51-40-0.SDR DU4R2006694Frame · corrodedCORROSION ON FRAME AND DOUBLER UNDER AFT LAV SERVICE PAN. FABRICATED AND INSTALLED DOUBLER 1.0" BY 2.1" BY 15.0" BY .5" FROM 2024-T3 .040" AND 2 CHANNELS 16" FROM 2024-T3 032" IAW B757 SRM 53-00-01, 51-40-2, 51-21-03 AND DWG 146N3650.SDR DU4R2006695Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN AT BS 457 S-7R - S-8R. CUT OUT LIGHTNING STRIKE AREA. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER 10.4" BY 9" FROM 2024-T3 .071" IAW B757 SRM 53-00-01 FIG 201 REPAIR 2.SDR DL757061011Skin · puncturedSKIN PUNCTURE FS 1840, BETWEEN S25R AND S27R. DAMAGE CUTOUT AND REPAIR DOUBLER INSTALLED.SDR DL757061029Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT BS 1682 BETWEEN S-28R AND S-29R UNDER LAV SERVICE PAN. THE CORRODED SKIN WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED.SDR DL757061002Line · looseLEFT ENGINE OIL PRESSURE DECREASED TO RED BAND. LEFT ENGINE OIL QTY ZERO. SHUTDOWN ENGINE PER QRH. LANDED BDA. FOUND NR 5 BEARING SCAVENGE LINE AT SCAVENGE PUMP LOOSE. RESTORED AND WIRE LOCKS OIL LINE. CARRIED OUT WINDMILL INSPECTION MAIN OIL FILTER AND SDR DALA1134750682Floor Panel · gougedAFT GALLEY FLOOR AT BS 1682, BL-54L GOUGES REPAIRED IAW SRM 53-00-51, 51-20-01, 53-60-51 FIG 201.SDR DU4R2006702Floorboard · corrodedCORROSION ON AFT GALLEY FLOOR AT BS 1680 - BL 48R CABIN COMPARTMENT. FABRICATED AND INSTALLED REPAIR DOUBLER 5-1/2" BY 7-1/2" FROM 2024-T3 .063" BAC1517-2226 IAW B757 SRM 51-10-02, 53-00-51, 51-20-01, AND 53-60-51 FIG 201.SDR DU4R2006701Floorboard · corrodedCORROSION ON GALLEY FLOOR AT BS 1720 - BL 36R CABIN COMPARTMENT. FABRICATED AND INSTALLED REPAIR DOUBLER 5-1/2" BY 7-1/2" FROM 2024-T3 .063" BAC1517-2226 IAW B757 SRM 51-10-02, 53-00-51, 51-20-01, AND 53-60-51 FIG 201.SDR DU4R2006700Floorboard · corrodedCORROSION ON GALLEY FLOOR AT BS 1720 - BL 20R CABIN COMPARTMENT. FABRICATED AND INSTALLED REPAIR DOUBLER 18-3/4" BY 7-1/2" FROM 2024-T3 .063" BAC1517-2226 IAW B757 SRM 51-10-02, 53-00-51, 51-20-01, AND 53-60-51 FIG 201.SDR DU4R2006699Floorboard · corrodedCORROSION ON GALLEY FLOOR AT BS 1720 - BL 0 TO BL 8R CABIN COMPARTMENT. FABRICATED AND INSTALLED REPAIR DOUBLER 18-1/2" BY 7-1/2" FROM 2024-T3 .063" BAC1517-2226 IAW B757 SRM 51-10-02, 53-00-51, 51-20-01, AND 53-60-51 FIG 201.SDR DU4R2006698Floorboard · corrodedCORROSION ON GALLEY FLOOR AT BS 1720 - BL 12L CABIN COMPARTMENT. FABRICATED AND INSTALLED REPAIR DOUBLER 17-1/2" BY 6-5/8" FROM 2024-T3 .063" BAC1517-2226 IAW B757 SRM 51-10-02, 53-00-51, 51-20-01, AND 53-60-51 FIG 201.SDR DU4R2006697Floorboard · corrodedCORROSION ON GALLEY FLOOR AT BS 1720 - BL 4L CABIN COMPARTMENT. FABRICATED AND INSTALLED REPAIR DOUBLER 17-1/2" BY 6-5/8" FROM 2024-T3 .063" BAC1517-2226 IAW B757 SRM 51-10-02, 53-00-51, 51-20-01, AND 53-60-51 FIG 201.SDR DU4R2006693Floor Panel · gougedGOUGES ON AFT GALLEY FLOOR AT BS 1682 BL-54L IN CABIN COMPARTMENT. FABRICATED AND INSTALLED REPAIR DOUBLER 9-1/2" BY 5-3/4" FROM 2024-T3 .063" IAW B757 SRM 53-00-51, 51-20-01, 53-60-51 FIG 201.SDR DALA1134770682Skin · corrodedAFT PIT LWR SKIN AT BS 1290, S-27L TO S-28L CORROSION REPAIRED IAW SRM 51-20-01 AND 53-00-01.SDR DU4R2006707Skin · corrodedCORROSION AFT PIT LWR SKIN BS 1290 BETWEEN S-27L AND S-28L. REMOVED CORRODED SKIN SECTION. FABRICATED AND INSTALLED DOUBLER 12-11/16" BY 12-1/2" FROM 2024-T3 .125" IAW B757 SRM 51-20-01 AND 53-00-01.SDR DALA1134760682Floorbeam · corrodedFWD CABIN FLOORBEAM AND HAT AT BS 377.7, RBL 10 CORROSION REPAIRED IAW SRM 53-10-51 AND 51-30-2.SDR DU4R2006705Crease Beam · corrodedCORROSION MAIN CABIN LT CREASE BEAM BS 1020. REMOVED CORRODED ANGLE. FABRICATED AND INSTALLED L ANGLE REPAIR 3-3/4" BY 3-1/2" BY 1-1/4" FROM 7075-T6 .090" IAW B757 SRM 51-70-11, 51-20-01 AND 51-40-02.SDR DU4R2006704Channel · corrodedCORROSION FWD CABIN FLOORBEAM AND HAT SECTION AT BS 377.7 RBL 10. REMOVED HAT SECTION. FABRICATED AND INSTALLED HAT SECTION FROM 3" BY 3"7075-T6 EXTRUSION IAW B757 SRM 53-10-51 AND 51-30-2.SDR DL757060997Fitting · gougedTHE LT WING SIDE LOAD FITTING HAS TWO HOLES THAT WERE OVERSIZED TO CLEAN UP TOOL DAMAGE. THE HOLES WERE OVERSIZED AND OVERSIZED FASTENERS WERE INSTALLED.SDR DL757060986Selector Valve · bypassingMULTIPLE LEFT HYDRAULIC SYSTEM MALFUNCTIONS. NOSE GEAR NOT EXTENDING IN NORMAL MODE. ALT OK. LEFT HYDRAULIC SYSTEM OVERHEAT INDICATION ALSO. FOUND LANDING GEAR SELECTOR VLV BYPASSING. ALSO, ACMP AND EDPCASE RETURN FILTERS WITH DEBRIS. REPLACED ACMP, EDP SDR DU4R2006692Skin · dentedLOWER FUSELAGE BS 1540 S-27L - S-28L DENTED NEXT TO STRINGER. CUT OUT DENTED AREA, PERFORMED HFEC IAW B757 NTM PT. 6 51-10-00. FABRICATED AND INSTALLED SKIN REPAIR 16.5" BY 10.5" FROM 2024-T3 .080" IAW B757 SRM 53-00-01.SDR DU4R2006706Shear Tie · corrodedCORROSION AND DAMAGE LEVELING COMPOUND AFT CARGO BS 1620 FROM S-29L TO S-29R. REMOVED CORRODED SHEAR TIE. FABRICATED AND INSTALLED SHEAR TIE .75" BY 1.5" BY 1.5" BY 1.5" BY 4" FROM 7075-T6 .040" IAW B757 SRM 51-30-01 AND 51-40-02, AMM 51-21-03 AND PS 900-3-6SDR DU4R2006703Floorbeam · corrodedCORROSION CABIN FLOORBEAM AT BS 365.25 12" LEFT OF B/L 0. CUT OUT CORRODED SECTION OF FLOOR BEAM. FABRICATED AND INSTALLED FLOORBEAM REPAIRS 12" BY 1" FROM 7075-T6 .063", 12" BY 1" FROM 7075-T6 .090", 12" BY 1" FROM 7075-T6 .125" AND EXTRUDED TEE 12" BY 3" BSDR DALA1134690682Skin · corrodedCORROSION AFT PIT LOWER SKIN BS 1290 BETWEEN S-27L AND S-28L REPAIRED PER SRM.SDR DALA1134680682Skin · corrodedCORROSION ON SKIN UNDER AFT LAV SERVICE PANEL BS 1681 AND S-26R TO S-29R REPAIRED PER SRM.SDR DU4R2006691Floorbeam · corrodedCORROSION IN AFT CABIN BS 1640 S-10R FLOOR SUPPORT. FABRICATED AND INSTALLED FLOORBEAM REPAIR 10.5 BY 1 BY 1/2" FROM 7075-T6 .071 AND STRAP 13" BY 2" FROM 7075-T6 .050" IAW B757 SRM 51-20-1, AND 53-00-51 FIG 201.SDR DU4R2006680Skin · dentedFUSELAGE SKIN BS 1400 BETWEEN S-30R AND S-29R SKIN DENTED. CUT OUT DENTED AREA, HFEC SKIN CUT OUT, NO CRACKS NOTED. FABRICATED AND INSTALLED REPAIR FILLER 3-3/4" BY 2-1/4" FROM 2024-T3 .071" AND DOUBLER 12-3/4" BY 5" FROM 2024-T3 .080" IAW DELTA ERA 458714-1SDR DU4R2006690Floor Panel · corrodedCORROSION IN AFT CABIN BS 1720 S-20R FLOOR PANEL. FABRICATED AND INSTALLED REPAIR FILLER 21 BY 7.5 FROM 2024-T3 .063 IAW B757 SRM 51-10-2, AND 53-60-51 FIG 201.SDR DL757060958Skin · dentedDURING CURRENT HMV AT TIMCO LCQ, A DENT WAS NOTED ON THE BELLY SKIN AT FS 1398, FROM S-30 TO S-29R. THE DENT IS IN CLOSE PROXIMITY OF THE CIRCUMFERENTIAL BUTT SPLICE AT FS 1401. A BOEING APPROVED REPAIR WAS INSTALLED PER 458714-14.SDR DL757060957Skin · dentedA DENT AND GOUGE WERE FOUND IN THE SKIN AFT OF FS 1260 BELOW S-14R. THE DAMAGED SKIN IS WITHIN 3 INCHES OF THE SKIN SPLICE. THE DAMAGED AREA WAS CUTOUT AND A BOEING APPROVED REPAIR WAS INSTALLED PER 456588-14SDR DL757060975Fitting · damagedTHE NR 1 AND NR 2 PYLON OUTBOARD SIDE LOAD FITTINGS WERE FOUND WITH 2 AND 1 FASTENER HOLES DAMAGED. THE HOLES WERE OVERSIZED AND OVERSIZED BUSHINGS WERE INSTALLED.SDR DL757060956Keelbeam · corrodedCORROSION WAS FOUND ON THE KEEL BEAM CHORD BETWEEN FS 660 AND FS 680, S-28R. THE CORROSION WAS REMOVED AND A BOEING APPROVED REPAIR INSTALLED PER 456557-14SDR DL757060955Skin · dentedA DENT WAS FOUND ON THE SKIN AT FS 223.50 BETWEEN WL200 AND WL 210, NEAR THE ANGLE OF ATTACH SENSOR. BOEING WAS CONTACTED AND AN APPROVED EXTERNAL REPAIR WAS INSTALLED PER 456555-14SDR DL757060954Sill · corrodedCORROSION WAS FOUND ON THE NR 2 CARGO DOOR LOWER MAIN SILL OUTBOARD CHORD ON THE UPPER FACE OF THE OUTBOARD SURFACE OF THE HORIZONTAL FLANGE FROM APPROXIMATELY FS 1400 TO 1440. THE CORROSION WAS BLENDED PER SRM REQUIREMENTS WITH A MAXIMUM DEPTH OF 0.065", ANDSDR DL757060953Frame · corrodedCORROSION WAS FOUND ON THE FRAME ON THE INSIDE CHORD AT FS 729.6 ABOVE WL 210. THE DAMAGE WILL BE TRIMMED OUT AND BOEING APPROVED REPAIR ANGLE INSTALLED PER 456268-14.
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