Boeing 757-236
Service difficulty reports · 2,544
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 = '757236' 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 = '757236' 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 FDEA2020060541134Actuator · crackedON TAKEOFF GEAR WOULD NOT RETRACT. RAN QRH, PROBLEM RESOLVED. NOTED AUTOBRAKES "RTO" DID NOT MOVE TO THE "OFF" POSITION AFTER LIFTOFF. AMM: 32-32-15-4 REMOVED AND REPLACED RIGHT MAIN GEAR TRUCK POSITIONER ACTUATOR REF AMM 32-32-15-4. LEAK AND OPS CHECKS GOSDR FDEA202006031120Floorbeam · crackedDURING CLEAN UP FOR INSTALLATION OF SEAT TRACK, FOUND FLOORBEAM AT STA 580 CRACKED. REPLACED STA 580 FLOORBEAM SECTION IN REF TO SRM 51-40-02 AND DRAWING SR57-53-004.SDR FDEA2020052621033Charger · inoperativeEMERGENCY EXIT SIGN OVER R1 DOOR WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY CHARGER ASSY (POWER SUPPLY) M730 REF AMM 33-51-07-2. REMOVED AND REPLACED R1 EMERGENCY EXIT SIGN REF AMM 33-51-01-2. EMERGENCY LIGHTS OPS CHECK SDR FDEA2020051320923Lanyard · out of positionL1 SLIDE LIGHT WILL NOT ILLUMINATE FOUND L1 DOOR SLIDE LANYARD HANGING DOWN- STOWED LANYARD-DOOR SLIDE ARMS AND DISARMS NML- REF: B757 M/M 25-66-10-2SDR FDEA202005040888Floorbeam · corrodedMAIN CABIN FLOOR FRAME UPPER CAP SHOWS EVIDENCE OF POSSIBLE CORROSION BL0 TO BL20R BS 1020. REMOVED CORR ON FLOOR SUPPORT STA 1020 BLO TO BL20R IAW B757 SRM 51-10-02. FOUND TO BE OUT OF LIMITS DUE TO EXFOILATION IAW B757 SRM 53-00-51-1A FIG 101. REMOVED FLSDR FDEA2020050430885Shear Web · corrodedMAIN CABIN COMPT. SHEAR WEB HAS CORROSION, BETWEEN LBL.34", AND LBL.46", FROM BS. 1711, TO BS. 1715. REMOVED CORR ON SHEAR WEB 1711 TO 1715 LBL34 AND LBL46 IAW B757 SRM 51-10-02. LOWEST REMAINING .052 FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-60-51-2R REP SDR FDEA2020051510870Skin · crackedR/H WING # 9 SLAT LOWER COVE PANEL SKIN HAS A CRACK AT WS 594. REMOVED AND REINSTALLED #9 LEADING EDGE SLAT IAW B757 AMM 27-81-02-4, FABRICATED AND INSTALLED LOWER COVE PANEL IAW B757 SRM 51-40-02-06 AND B, DWGS. 114N4003, REV. E AND REV. B, B DWG : 114NSDR FDEA2020050410870Skin · crackedR/H WING # 9 SLAT LOWER COVE PANEL SKIN HAS CRACK AT WS 594.SDR FDEA2020051390839Filler · corrodedCORROSION FORWARD WET AREA STA 375 LBL 20 FLOOR SUPPORT CORRIER AREA. REMOVED CORROSION FWD WET AREA STA 375 LBL 20 FILLER IAW B 757 SRM 51-10-02-OG ORIGINAL MATERIAL .071",MAT REM .058",MAT LOSS .013" FOUND TO BE OUT OF LIMITS IAW B 75 757 SRM 53-00-51-1SDR FDEA202004300839Filler · corrodedCORROSION FORWARD WET AREA STA 375 LBL 20 FLOOR SUPPORT CORRIER AREA. REMOVED CORROSION FWD WET AREA STA 375 LBL 20 FILLER IAW B 757 SRM 51-10-02-OG ORIGINAL MATERIAL .071",MAT REM .058",MAT LOSS .013" FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-51-1A FISDR FDEA202004300817Web · crackedMAIN CABIN INTERIOR, UPPER LOBE STRUCTURE WEB IS CRACKED, BS. 720 STR. 4R. REMOVED WEB STA 720 STR 4R, FABRICATED, LOCATED, DILLED AND INSTALLED NEW WEB IAW B757 SRM 51-40-02, 51-40-05 AND BOEING DWG 143N8323 REV M, REV C AND REV -SDR FDEA2020043080816Frame · crackedFWD CARGO PIT-R/H SIDE,FRAME 846 AT STR 22 RT. CRACKED AT FASTENER HOLE. REMOVED,FABRICATED AND INSTALLED STANCHION STUB (FRAME) ON FWD CARGO PIT R/H SIDE AT STA 846 BETWEEN STR-21R TO STR-26R IAW B 757 SRM 51-40-02-OG AND B. DWG : 143N5811, REV : - , RESDR FDEA2020042760791Floorbeam · corrodedMAIN CABIN FLOOR FRAME UPPER CAP SHOWS EVIDENCE OF POSSIBLE CORROSION BL0 TO RBL20 BS 1060. REMOVED CORR ON FLOOR SUPPORT STA 1060 BL0 TO BL20R IAW B757 SRM 51-10-02 100% MAT. LOSS OUT OF LIMITS IAW B757 SRM 53-00-51 FIG 101. REMOVED SUPPORT IAW B757 SRM SDR FDEA2020042760794Seat Track · corrodedMAIN CABIN, CORROSION ON SEAT TRACK FLANGE BETWEEN STA. 365 AND 377 RBL-44. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5310-T0353677 P1 FUSELAGE - MAINFRAME - RBL 45.50 SEAT TRACK CORROSION REPAIR FROM STA 365 TO 377SDR FDEA2020042760793Stringer Clip · crackedMAIN CABIN INTERIOR, UPPER LOBE STRUCTURE STRINGER CLIP IS CRACKED\GOUGED BS. 720 STR. 3R REMOVED, FABRICATED AND INSTALLED MAIN CABIN INTERIOR, UPPER LOBE STRUCTURE STRINGER CLIP AT STA 720 STR. 3R IAW BOEING DWG # 140N2001, REV D AND REV. BN, B757 SRM SDR FDEA2020042760790Seat Track · corrodedSEAT TRACK AT STA 1180 LBL44.5 HAS EXFOILATION CORROSION EVALUATED SEAT TRACK STA 1180 LBL 44.5 FOUND OUT OF LIMITS DUE TO 100% MATERIAL LOSS DUE TO EXFOILATION IAW B757 SRM 53-00-52. REMOVED, TRIMMED, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK IAW B757SDR FDEA2020042760789Crease Beam · corrodedMAIN CABIN BETWEEN STA 860-879 CREASE BEAM CORRODED. REMOVED CORR ON RH CREASE BEAM STA 860-879 IAW B757 SRM 51-10-02. ORIG MAT .071 LOWEST REM .054 LOSS .017 FOUND OUT OF LIMITS IAW B757 SRM 53-30-13-1A. REPAIRED CREASE BEAM IAW B757 SRM 53-00-13-2R REP 1SDR FDEA2020042760788Seat Track · corrodedSEAT TRACK RBL 44.5 STA 1320 TO 1540 HAS CORROSION ENTIRE LENGHT REMOVED CORR ON SEAT TRACK RBL 44.5 STA 1320 TO 1540 IAW B757 SRM 51-10-02. 100% MAT. LOSS DUE TO EXFOILIATION OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101. REMOVED SEAT TRACK, FABRICATED, SDR FDEA2020042760787Support · crackedR1 DOOR LOWER SILL UPPER SURFACE HAS CORROSION ON THE THRESHOLD SUPPORT STA. 338 REMOVED CORROSION FROM R1 DOOR LOWER SILL UPPER SURFACE SUPPORT STA 338, FOUND OUT OF LIMITS WITH THE ORIGINAL MAT. .050 REMAINING MATERIAL .043, REMOVED, FABRICATED AND INSSDR FDEA2020042760786Support · corrodedR-1 DOOR LOWER SILL UPPER SURFACE CORROSION ON THE TOP SIDE OF THRESHOLD SUPPORT AT STA 354. REMOVED CORROSION FROM R-1 DOOR LOWER SILL UPPER SURFACE, FOUND OUT OF LIMITS WITH ORIGINAL MATERIAL .050 REMAINING MATERIAL .040, REMOVED, FABRICATED AND INSTALLED NESDR FDEA2020042310768Plate · corrodedMAIN CABIN FLOOR FRAME UPPER CAP SHOWS EVIDENCE OF POSSIBLE CORROSION AT BL20L TO BL40L BS 1020. REMOVED CORR ON FLOOR FRAME UPPER CAP (PLATE) IAW SRM 51-10-02. 100% MAT LOSS OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AND INSTALLED IAW SRM 51-40-02SDR FDEA2020042310763Skin · dentedOBSERVED SMALL DENT AND SCRATCH ON FUSELAGE. LEFT HAND SIDE BELOW CAPTS L2 WINDOW. REF WRI 56-10-5113, HFEC THE DENT ON NOSE SECTION OF AIRCRAFT, LEFT SIDE BELOW L3 WINDOW. MEASURED SDR FDEA202004200762Intercostal · corrodedCORROSION WEB SUPPORT AFT PIT STA. 1420 - 1440 STR 29R-30. DOT 88-010. REMOVED FABRICATED AND INSTALLED AFT CARGO INTERCOSTAL AT BS1400-1420 29R-30 IAW B757 SRM 51-40-02-0G AND BOEING DWG 146N5398 REV A , REV P.SDR FDEA202004200761Shear Tie · corrodedCORROSION SHEAR TIE AFT PIT STA. 1440 STR 29R TO STR. 30. DOT 88-014. REMOVED FABRICATED AND INSTALLED AFT CARGO SHEAR TIE AT BS1440 STR 29R TO STR 30 IAW B757 SRM 51-40-02-0G AND BOEING DWG 146N1101 REV - , REV B.SDR FDEA2020041760753Door Frame · crackedRH #2 DOOR UPPER HINGE CUTOUT IS CRACKEDSDR FDEA2020041750748Element · failedAPU WHEN PUT ON LINE FIRE BOTTLE BLEW, APU FIRE WARNING LIGHT HORN ON CONSTANT, SHUT OFF APU RESET THE HORN FIRE WARNING. LIGHT OUT BUT FIRE BOTTLE SQUIBS FIRED. [APU FIRE LP1 STATUS] APU BTL [ECAS MSG]. REMOVED AND REPLACED LWR APU FIRE DET ELEMENT REF MM 26SDR FDEA202004080719Unknown · malfunctionedCRZ FL340, CABIN ALTITUDE WARNING. CABIN APPROX 10,000FT WITH APPROX 200FPM CLIMB, DIFFERENTIAL 6.4 DESCENDED TO FL320 NO HELP DUCT PRESSURE OVER 40PSI. DECDENSDR FDEA2020040870715Warning System · false activationFL360 AFT CARGO FIRE EICAS AND MASTER WARNING EICAS RESOLVED ITSELF BEFORE QRH AND AGENT DISCHARGE COULD BE COMPLETED. REFERENCE WRI 26-12/4866 FOR CORRECTIVE MAINTENANCE ACTION AND REMOVE/INSTALL PARTS INFO FOR THIS WRI, ALSO. ALL INFO APPLIES TO BOTSDR FDEA2020040870714Circuit Card · malfunctionedEICAS AND MASTER WARNING EICAS RESOLVED ITSELF BEFORE QRH AND AGENT DISCHARGE COULD BE COMPLETED. UPON ARRIVAL AT SGF, IT WAS NOTED THAT THE FWD AND AFT CARGO COMPARTMENTS WERE LOADED WITH BULK FREIGHT, ALL THE WAY TO THE CEILINGS IN BOTH COMPARTMENSDR FDEA2020032980612Warning System · false activationINTERMITTANT R EMER DOOR ADVISORY AT BLOCK - IN HAD NO "R EMER DOOR" ADVISORY. VISUALLY CHECKED DOOR AND VERIFED IT WAS CLOSED WITH HANDLE LOCK PLATED STILL INSTALLED REF B757 AMM 52-21-01-2. COMPLETED #3 R EMER EXIT DOOR SENSOR TARGET TEST OF PSEU WISDR FDEA202003200596Static Line · looseUPON CLOSING THE MAIN ENTRY DOOR COULDNT GET THE SECURE LIGHT ON (SLIDE LIGHT ON). FOUND SLIDE STATIC LINE LOOSE -RESTOWED SAME- L1 DOOR GIRT BAR AND LIGHT CHECKS GOOD- REINSTALLED DOOR SLIDE COVER- DOOR SLIDE AND DOOR ASSIST BOTTLES SAFETIES RMVD- REF: SDR FDEA202003170579Battery · dischargedEMERGENCY LIGHTS IN CTR COURER AREA, ABOVE R1 DOOR, AND R1DOOR EXTERIOR LIGHTS ARE INOP. AMM: 33-51-07-2 REMOVED AND REPLACED EMERGENCY PACK HOLDER ASSY REF B757 AMM 33-51-07-2. OPS SDR FDEA2020030530483Fire Warning · false activationL ENG FIRE WARNING L ENG OVHT RAN ENGINES TO POWER FOR APPROX 5 MIN. TAXIED A/C PER JRH NO WARNINGS COMPLIED WITH PNEUMATIC BLEED DUCT LEAK CHECK USING ALUMINUM FOIL WRAP DURING POWER RUNS NO LSDR FDEA2020021090297Hook And Loop · wornVELCRO EVAS STRIP ON CAPTAIN GLARE SHIELD IS SEPERATING. REPLACED VELCRO LOOP FASTENER. REF AMM 25_62_00_8_0 A/C OK FOR SERVICE.SDR FDEA2020021090296Hook And Loop · wornEVAS VELCRO STRIP ON F/O GLARE SHIELD MISSING REPLACED VELCRO LOOP FASTENER. REF AMM 25_62_00_8_0 A/C OK FOR SERVICE.SDR FDEA202002070281Skin · dentedR/H HORIZONTAL STAB UPPER SKIN AUX SPAR PREVIUS REPAIR APROX.. 4" 3/4 CIRCUNFERENCE DELAM AT STA 78.00 REMOVED EXISTING REPAIR AND ACCOMPLISHED PERMENENT REPAIR ON R/H HORIZONTAL STAB UPPER SKIN AT STA 78 IAW B757 SRM 55-10-01-1A AND IAW B757 SRM 51-70SDR FDEA20200130236Beam · gouged3EA SMALL GOUGES - MAIN CARGO DOOR VERTICAL BEAM INBD CHORD INTERIOR SURFACE - APPROX STA 490,BETWEEN WATER LINE 210 - 215. REMOVED GOUGES ON MAIN CARGO DOOR VERTICAL BEAM I\B CHORD APPROX STA 490 BETWEEN WL 210-215 IAW B757 SRM 51-40-02. FOUND TO BE OUT SDR FDEA2020013090238Shear Tie · corrodedAFT LOWER CARGO COMPARTMENT, CORROSION, SHEAR TIE STA 1480 BETWEEN STR 28R AND STR 29R. REMOVED CORROSION ON SHEAR TIE AT STA 1480 BETWEEN STR 28R-29R IAW SRM 51-10-02-0G. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101 DET 2. REMOVED SHEAR TIE IAW SRM 5SDR FDEA2020012320198Floorbeam · corrodedMAIN DECK STA 1055 BETWEEN BL0-RBL 24.75 FLOOR SUPPORT CORRODED. ACCOMPLISHED IAW EA F-5310-T0352036 P1 FUSELAGE - MAINFRAME -MAIN CARGO FLOOR SUPPORT STA 1055 CORRODED, NEW PART FABRICATION TEMPER ATERATION, REMOVED CORR IAW SRM 51-10-02-OG, FOUND TO BE OUT LSDR FDEA202001210190Seat Track · corrodedMAIN DECK SEAT TRACK FLANGE CORRODED BETWEEN STA 1180 - 1200 RBL 45.5. REMOVED CORROSION ON SEAT TRACK FLANGE AT STA 1180 TO 1200, RBL 45.5 IAW SRM 51-10-02-OG. EVALUATED DAMAGED AREA, ORIG MAT =.070', REM MAT = .040",MAT LOSS = .030" FOUND TO BE OUT LIMITS IASDR FDEA202001200178Gust Lock · damagedDURING SERVICE FOUND LT ENTRY DOOR GUST DOOR LOCK BROKEN. REMOVED AND REPLACED L1 DOOR HOLD OPEN GUST LOCK REF AMM 52-11-08-8. MATERIAL 140N6008-1 COLLAR ASSY MATERIAL 140N6009-1 CATCH ASSY.SDR FDEA2020012170162Fitting · crackedAFT CARGO COMPT SHEAR WEB STRUCTURE CLIP IS CRACKED AT O/B RBL 24.75" AND BS 1715. REMOVED, FABRICATED AND INSTALLED CLIP ON AFT CARGO COMP SHEAR WEB STRUCTURE AT O/B SIDE OF RBL 24.75, STA 1715 IAW SRM 51-40-02-OG AND B DWG 146N5329,REV - AND REV C.SDR FDEA202001170159Shear Tie · crackedFUSELAGE LT EMERGENCY EXIT INTERNAL STRUCTURE AT MID SECTION AFT STIFFENER CRACKED BETWEEN STR 13L TO STR 14L ON STA 1340. (SHEAR TIE) REMOVED AND REPLACED STIFFENER (SHEAR TIE) ON LT EMERGENCY EXIT DOOR AT INTERNAL STRUCTURE MID SECTION AFT SIDE IAW SRM 51-40SDR FDEA202001110112Skin · crackedMAIN CABIN R2 DOOR ENTRY DOOR UPPER HINGE CUT OUT CRACKED. COMPLIED WITH EA #: F-5210-T0351839 P1 TITLE : DOORS - PASSENGER / CREW - R-2 DOOR FOWARD FRAME UPPER HINGE CUT OUT SRM REPAIR - RSC TRACKING AND B 757 SRM 52-10-02-2R FIG 201 REP 1 DET III.SDR FDEA2020011310112Hinge · crackedMAIN CABIN R2 DOOR ENTRY DOOR UPPER HINGE CUT OUT CRACKED. COMPLIED WITH FEDEX EA #: F-5210-T0351839 P1 TITLE : DOORS - PASSENGER / CREW - R-2 DOOR FOWARD FRAME UPPER HINGE CUT OUT SRM REPAIR - RSC TRACKING AND B 757 SRM 52-10-02-2R FIG 201 REP 1 DET III.SDR FDEA2020010980062Seat Track · damagedDAMAGED SEAT TRACK AT STA 560 BL 0 REQUIRES REPAIR OR REPLACE REPAIRED SEAT TRACK AT STA 560 BL 0 IAW FEDEX EA#F-5320-T0351623SDR FDEA2020010640017Control Unit · failedFOUND DURING WRI# 05-50/6574. ANTISKID/AUTOBRAKE CONTROL UNIT HAS MSG "BOX 1-5" THAT WILL NOT CLEAR. DURING TRANSDUCER SPINUP TEST, TRANSDUCER #1 SPINUP DOES NOT RESULT IN RELEASE OF BRAKE #5. REMOVED AND REPLACED ANTISKID/AUTOBRAKE CONTROL SDR FDEA202001020005Door · delaminatedDAMAGE FOUND ON LH MLG DOOR DEPTH = 3.14, L= 27.77 W= 41.37 SEQ NO 000206 WRI 52801178 WO 00076120 PERFORMED REPAIR OF LH MLG DOOR FIBERGLASS PLYS IAW FEDEX REPAIR DRAWING SR 57- 52-01 REV A (SHEETS 1-3) SRM 51-70-00 SRM 52-80-02 AND 51-40-02 MATERIASDR FDEA2019123103332Seat Track · corrodedMAIN CABIN STA 578 RBL 45.50 SEAT TRACK HAS CORROSION. REMOVED DAMAGE AND RESTORED SURFACE PROTECTION IAW SRM 53-30-52-1A, 53-00 00-52-1A AND 51-20-01.SDR FDEA2019123103331Seat Track · corrodedMAIN CABIN BS 788 RBL 24.75 SEAT TRACK HAD CORROSION. REMOVED CORROSION FROM THE SEAT TRACK AT BS 788, RBL 24.75 IAW SRM 53-30-52-1A, AND SRM 51-20-01.
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