JASC 5750
Service difficulty reports · 1,158
Reports filed under 5750 · Wing, Control Surfaces, newest first.
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 jasc_code = '5750' 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 jasc_code = '5750' 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 FDEA202204130973Attach Fitting · crackedFOUND CRACK 1.75 INCHS LONG ON I/B UPPER WINGLET L/E ATTACH FLANGE ON RIGHT-HAND WING REPAIR IAW EA 1-5750-T0368013 PART 1SDR FDEA202204130948Panel · noneEXISITING REPAIR LOCATED ONR/WING INBD FLAP, L/E NOSE PANEL, INBD OF MF STA,153.43 REQUIRES REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS PER AGING AIRCRAFT EO F-5100-7-5001-PT1. EVALUTED EXISTING REPAIR LOCATED ON ONR/WING INBD FLAP, L/E NOSE PANEL, INBSDR FDEA202204130947Unknown · unknownEXISITING REPAIR LOCATED ONL/WING OUTBD AFT FLAP, UPPER SKIN, APPROX WBL 350, REQUIRES REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS PER AGING AIRCRAFT EO F-5100-7-5001-PT1. EVALUTED EXISTING REPAIR LOCATED ON L/WING OTBD AFT FLAP, UPPER SKIN, APPROX WBLSDR FDEA202204120931Flap · noneEXISTING COMPOSITE REPAIR LOCATED ON L/WING INBD MAIN FLAP, UPPER SURFACE, 63" FROM OTBD EDGE AND 41" FROM T/E, REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA EVALUATED EXISTING COMPOSITE REPAIR AND FOUND REPAIR TO CONFORM TSDR FDEA202204090908Skin · damagedLEFT HAND WING - INBOARD FLAP ASSEMBLY, INBOARD UPPER MID SEGMENT STATION XIFH 160 FOUND OIL CANNING. LEFT HAND WING INBOARD FLAP ASSEMBLY INBOARD UPPER MID SEGMENT DAMAGE SKIN AT STATION XIFH 160 REPAIRED IN ACCORDANCE WITH SRM 57-00-01-2R REPAIR 1 FIGURESDR SWAA2022041892599Panel · delaminatedPANEL 551BB LOCATED L/H WING LOWER SURFACE FORWARD OF GEAR CUT OUT HAS A DENT WITH SAME AREA OF DELAMINATION. / [01] PANEL 551BB REMOVED FROM A/C. REQUIRES PANEL P/N 115A2711-7. IPC 24-51-00-12 ITEM 1;[02] P/N CHANGED TO 654A0004-1261.;[03] LOCATED; DRILLED; ASDR YENA2022041200356None · noneDURING HEAVY MAINTENANCE, CORROSION LOCATED ON RIB 10 PLUS 5 INCH UPPER SKIN LOWER SURFACE TRAILING EDGE LH WING; ACCOMPLISHED PER JB EA 57-0091-22SDR YENA2022041200355None · noneDURING HEAVY MAINTENANCE, CORROSION TE RIB 10-11 OVERHANG LH WING; ACCOMPLISHED PER JETBLUE EA 57-0091-22SDR REXA2022052700904Panel · chafedCHAFING DAMAGE ON PANEL 684GB. FOUND CHAFING DAMAGE ON 684GB OUT OF LIMITS, REMOVED AND REPLACED PANEL IAW CRJ 900 SRM 51-40-11-001-001-A01.SDR FDEA202204070888None · delaminatedRH WING OUTBOARD FLAP LOWER SKIN WITH DENT AT WBL: 435. RH WING OUTBOARD FLAP LOWER SKIN WITH DENT AT WBL 435 THAT WAS REPAIRED IAW SRM 57- 53-01-2R FIG. 201 PAGE 1-6 TABLE II AND SRM 51-70-17-0G-0 FIG. 10 PAGE 1, 24, 25, 36, 48 PARA. 4.A. REV. 82 DEC15/20SDR FDEA202204060874Skin · noneAGING AIRCRAFT - EXISTING SKIN SPLICE REPAIR FOUND AT LEFT HAND WING INBOARD FLAP CENTER BOX LOWER SURFACE BETWEEN XIFH 249- XIFH 255. EXISTING SKIN SPLICE REPAIR ON LEFT HAND WING INBOARD FLAP CENTER BOX LOWER SURFACE BETWEEN XIFH 249 - XIFH 255 EVALUATEDSDR FDEA202204050918Rib · crackedRIGHT HAND INBOARD FLAP, INBOARD LEADING EDGE CAVITIE HAS A ONE INCH TEAR IN LOWER FORWARD LIGHTNING HOLE. BLENDED DAMAGE AND APPLIED DOUBLER REPAIR IAW SRM 57-00-00-2R FIG 201, SEE ALSO EA 1-5750-T0368054SDR FDEA202204050862None · noneLH WING LE AT STA OSS441 RIVETS LOOSE REPLACED FASTENERS REF B767 SRM 51-40-02 AND E.A. TH-5750-T0367852 P1SDR SWAA2022050291068Access Panel · crackedCRACK ACCESS PANEL 661BB TRAILING EDGE AROUND HOLES RT WING 2022-192583 / [01] TOOL USED: CALIPER P/N: 500-464 S/N: 15331932 DUE DATE: 26-OCT-22.;[02] CORRECTIVE ACTION 1 ENTERED BY ERROR CORRECTED TOOL IS CALIPER P/N: 500-464 S/N: 15331926 DUE DATE: 28-SEP-22SDR FDEA202203310791Skin · noneAGING AIRCRAFT - EXISTING DOUBLER REPAIR AT LEFT HAND WING DROOP LEADING EDGE ASSEMBLY . INBOARD AREA XDLE 309.934. EXISTING DOUBLER REPAIR AT LEFT HAND WING DROOP LEADING EDGE ASSEMBLY INBOARD AREA XDLE 309.934 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WSDR FDEA202203290729Support · corrodedLEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (D) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (D) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 5SDR FDEA202203290733Support · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (D) ECCENTRIC HOLE CORRODED. HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-SDR FDEA202203290732Support · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (C) ECCENTRIC HOLE CORRODED. HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-SDR FDEA202203290731Support · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (E) ECCENTRIC HOLE CORRODED. HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MDSDR FDEA202203290728Support · corrodedLEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (C) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (C) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-SDR FDEA202203290727Support · corrodedLEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (E) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (E) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-SDR FDEA202203290726Support · corrodedLEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- SDR FDEA202203280723Flap · tornRH WING INBOARD AFT FLAP WITH NICK LOWER SURFACE AT WBL -152 RH WING INBOARD AFT FLAP TRAILING EDGE LOWER SKIN AT IFS 162.65 WAS REPAIRED IAW SRM 57-53-01-2R TABLE I FIGURE 201 AND SRM 51-70-03-0G PAR. 5.L. FIGURE 16 REV.82 DEC 15/2021SDR FDEA202203280722Flap · unknownPREVIOUS COMPSITE MAJOR REPAIR RW O/B FLAP, UPPER SURFACE, APPROX. 52" FROM THE I/B END AND 5.5" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND PERDORMED PERMANENT REPAIR IAW B757 SSDR FDEA202203280717Support · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY . INBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP ASSEMBLY . INBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE REWORKED AND FOUND EXCEED LIMIT AS PER MDSDR FDEA202203280712Bracket · corrodedLEFT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-52-03 AND E.A.SDR FDEA202203280710Bracket · corrodedRIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE (F AND G HOLE) REWORKED AND FOUND EXCESDR FDEA202203250694Flap · unknownPREVIOUS COMPOSITE MAJOR REPAIR RW O/B FLAP UPPER SURFACE APPROX 53" FROM I/B END AND 9.5" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND PERFOMED PERMANENT REPAIR IAW B757 SRM: SDR FDEA202203250693Flap · unknownPREVIOUS COMPOSITE MAJOR REPAIR R/W O/B FLAP UPPER SURFACE APPROX 95" FROM I/B END AND 7.5" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND PERFORMED PERMANENT REPAIR IAW B757 SRMSDR FDEA202203250689Flap · unknownPREVIOUS COMPOSITE MAJOR REPAIR. L/W O/B FLAP UPPER SURFACE APPROX 36" FROM I/B END AND 10" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIRS IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND APPLIED NEW REPAIR IAW B757 SRM 57-53-SDR FDEA202203250688Flap · unknownPREVIOUS COMPOSITE MAJOR REPAIR. L/W O/B FLAP UPPER SURFACE APPROX 83" FROM I/B END AND 8" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIRS IS IN ACCORDANCE WITH APPROVED DATA REMOVED PREVIOUS REPAIR AND APPLIED NEW REPAIR IAW B757 SRM 57-53-01SDR FDEA202203250687Flap · unknownPREVIOUS COMPOSITE MAJOR REPAIR. L/W O/B FLAP UPPER SURFACE APPROX 98" FROM I/B END AND 6.5" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIRS IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND APPLIED NEW REPAIR IAW B757 SRM 57-53SDR FDEA202203250686Flap · unknownPREVIOUS COMPOSITE MAJOR REPAIR, L/W O/B FLAP UPPER SURFACE APPROX 42" FROM I/B END AND 5.5" FROM T/E; REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND APPLIED NEW REPAIR IAW B757 SRM 57-53-SDR FDEA202203240669Slat · dentedRH WING #12 SLAT I/B T/E UPPER SURFACE FOUND DENT. REPAIRED RH WING #12 SLAT I/B T/E UPPER SURFACE DENT PER B767 SRM57-43-02-2R & SRM51-70-10-2R REPAIR 4. TRACKING EA: H-5750-T0367602 P1 WAS ISSUED, TITLE: WINGS - CONTROL SURFACES - RH WING ,#12 SLAT, T/SDR FDEA202203240668Slat · dentedRH WING #11 SLAT O/B T/E UPPER SURFACE FOUND DENT. REPAIRED RH WING #11 SLAT O/B T/E UPPER SURFACE DENT PER B767 SRM57-43-02-2R & SRM51-70-10-2R REPAIR 4. TRACKING EA: H-5750-T0367601 P1 WAS ISSUED, TITLE: WINGS - CONTROL SURFACES - RH WING ,#11 SLAT, T/ESDR SWAA2022042687036Angle · crackedCRACK REAR SPAR ANGLE LOCATED BETWEEN WS253 TO WS278 AT RT WING 2022-158299 / [01] REPLACED REAR SPAR ANGLE LOCATED BETWEEN WS253 TO WS278 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A6200;[02] REPLACED REAR SPAR ANGLE LOCATED BETWEEN SDR FDEA202203230661Flap · unknownEXISTING COMPOSITE REPAIR ON R/WING OTBD FLAP, UPPER SURFACE, APPROX. 30" FROM INBD END AND 2.5" FROM T/E EXISTING COMPOSITE REPAIR ON R/WING OTBD FLAP, UPPER SURFACE, APPROX. 30" FROM INBD END AND 2.5" FROM T/E IS LOCATED ON A PRIMARY STRUCTURE PER B757-2SDR FDEA202203230656Doubler · chafedR/W O/B FLAP L/E HAS A WORN AREA ON REPAIR DOUBLER 11IN I/B FROM O/B EDGE REPAIRED PER FEDEX EA # F-5750-T0322968 ASDR FDEA202203210613Skin · damagedAGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND AT RIGHT HAND WING INBOARD FLAP LOWER SEGMENT UPPER SKIN XIFH 288.14 EXISTING REPAIR DOUBLER AT RIGHT HAND WING INBOARD FLAP LOWER SEGMENT UPPER SKIN XIFH 288.14 EVALUATED AND FOUND REPAIR DOUBLER DAMAGED ANDSDR FDEA202203210612Skin · damagedAGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND AT RIGHT HAND WING INBOARD FLAP LOWER SEGMENT UPPER SKIN XIFH 261.69. EXISTING REPAIR DOUBLER AT RIGHT HAND WING INBOARD FLAP LOWER SEGMENT UPPER SKIN XIFH 261.69 EVALUATED AND FOUND EXISTING REPAIR DOUBLER DASDR FDEA202203200600Skin · crackedLEFT HAND WING # 8 SLAT INTERIOR SURFACE FOUND CRACK. LEFT HAND WING #8 SLAT INTERIOR SURFACE AT STATION XOS 1146.814 CRACKED AREA REPAIR CARRIED OUT AS PER EA 1-5750-T0367711 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR SWAA2022042585514Bracket · brokenACCESS PANEL 551FB FIXED PANE: T/E L BRACKET CRACK / [01] REMOVED AND REPLACED 'L' BRACKET ON L/W T/E PANEL #551FB REF. B737-7 SRM 51-40-02-0G-0; AND DRAWING 115A2710;[02] VERIFIED STEP 1SDR FDEA202203170555Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE (HOLE #8) REWORKED AND SDR FDEA202203170554Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE (HOLE #8) REWORKED AND FOSDR FDEA202203170553Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT BORE (HOLE #7) REWORKED AND FOUND EXCESDR FDEA202203170552Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT BORE (HOLE #7) REWORKED AND FOUND EXCESDR FDEA202203170551Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE (HOLE #3) REWORKED AND FOUNSDR FDEA202203170550Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE (HOLE #3) REWORKED AND FOUND SDR FDEA202203170549Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE (HOLE #4) REWORKED AND FOUND EXCEED LIMIT AS PERSDR FDEA202203170557Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE (HOLE #7) REWORKED AND FOUND E
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