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 SWAA2022040847406Bracket · crackedLT. WING PANEL 551FB AFT BRACKET CRACKED.(MARKED) / REMOVED CRACKED BRAKET & REINSTALLED W/NEW IAW B737 SRM 51-40-02-0G-0 & BOEING ENGINEERING DOCUMENT 115A2710 DWG 0004SDR SWAA2022022210243Plate · crackedR/H WING T/E WAFFLE BRACKET JUST OBD OF PYLON CRACKED THROUGH FASTENER HOLE. / REMOVED AND REPLACED PLATE PER SRM 51-40-02SDR SWAA2022040610230Slat · cracked#8 SLAT NOSE SKIN HAS CRACK AT ACTUATOR ATTACH FITTING; (OUTBOARD AFT FASTENER) HFEC VERIFIED / REPAIR #8 SLAT NOSE SKIN PER SRM 57-42-01-2R-8.SDR SWAA2022022247165Plate · crackedLH WING LOWER INBOARD TRAILING EDGE CAVITY; WAFFLE PLATE OUTBOARD OF PANEL 551DB (STA IRSS 217)IS CRACKED; MARKED. / REMOVED AND REPLACED WAFFLE PLATE O/B OF PANEL 551DB STA IRSS 217; IAW SRM 57-40-02-0G; DWG 115A2781 REV B AMM 51-21-73-370-801 AMM 51-21-72-37SDR SWAA2022022247180Plate · crackedLH WING; I/B REAR SPAR; WAFFLE PLATE CRACKED I/B END (JUST O/B OF WING ROOT) / REMOVED WIGGLE PLATE @ L/H WING; I/B REAR SPAR; I/B END (JUST O/B OF WING ROOT). RECEIVED NEW WIGGLE PLATE P/N 115A2781-12 SI# 7570568. LOCATED & DRILLED NEW WIGGLE PLATE. INSTALLEDSDR FDEA2019101762659Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE(#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57SDR SWAA2022040582300Angle · crackedLEFT WING FIXED TE UPPER PANEL HAS AFT SUPPORT ANGLE CRACKED / REMOVED AND REPLACED PER SRM 51-40-02SDR SWAA2022022208969Plate · crackedRIGHT HAND WING AFT TRAILING EDGE EDGE CAVITY ABOVE ACCESS PNL 651GB WIGGLE PLATE INBD OF #2 ENGINE SAIL TAIL IS CRACKED / REMOVED R/H WING AFT TRAILING WIGGLE PLATE ABOVE ACCESS PANEL 651GB INBD # 2 ENG SAIL TAIL I.A.W B737-700 SRM 51-40-02-0G-0; VERIFIED NEWSDR FDEA201910102582Hinge Bracket · corrodedRIGHT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), OUTBOARD ACTUATOR HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0SDR SWAA2022040408966Spoiler · delaminatedR/W #12 SPOILER UPPER SURFACE HAS DELAMINATION 7.0' FROM AFT EDGE AND 7.0' FROM I/B EDGE / REPAIRED RIGHT WING #12 SPOILER UPPER SURFACE DELAM 7.0' FROM AFT EDGE AND 7.0' FROM INBOARD EDGE I.A.W B737-700 SRM'S 51-70-10-2R-0 REV 68 & 51-70-10-2R-2 REV 68 & 57-7SDR SWAA2022040408965Spoiler · delaminatedR/W #9 SPOILER UPPER SURFACE HAS DELAMINATION 2.5' FROM FWD EDGE AND 5.5' FROM O/B EDGE / REPAIRED DELAM ON #9 SPOILER UPPER SURFACE 6' FROM I/B END 14' FROM AFT EDGE I/A/W SRM 51-70-10-212-0 REV 68; SRM 51-70-10-2R-2 REV 68 PER SRM 57-70-01-2R-1 FIG 201 REV 6SDR SWAA2022040408964Spoiler · delaminatedR/W #9 SPOILER UPPER SURFACE HAS DELAMINATION 9.0' FROM AFT EDGE AND 7.0' FROM O/B EDGE / REPAIRED DELAM AND R/H #9 SPOILER UPPER SURFACE 9' FROM AFT EDGE AND 7' FROM O/B WDGE I/AW SRM 51-70-010-2R-0 REV 68L SRM 51-70-10-2R-2 REV 68; PER SRM 57-70-01-2R-1 FIG SDR SWAA2022040408963Spoiler · delaminatedR/W # 8 SPOILER UPPER SURFACE HAS DELAMINATION 2.5' FROM FWD EDGE AND 5.5' FROM O/B EDGE / REMOVED AND REPLACED #8 FLIGHT SPOILER IAW AMM 27-61-11-000-801 AND 27-61-11-400-801. PERFORMED FLIGHT SPOILER SYSTEM TEST IAW AMM 27-61-00-730-801.SDR SWAA2022022210833Plate · crackedR/H WING TRAILING EDGE CAVITY INBD WIGGLE PLATE ABOVE SAIL TAIL HAS FASTENERS SHEARED AND PLATE IS CRACKED / REMOVED AND REPLACED RH WING TRAILING EDGE CAVITY I/B WIGGLE PLATE P/N 115A2781-14 (7570259) WN6612 IAW B 737-700 AIPC 57-50-00-30 & SRM 51-40-02-0G-0SDR SWAA2019102138026Plate · crackedL/H WING LOWER TRAILING EDGE STRUCTURE WAFFLE PLATE CRACKED OUTBOARD OF PANEL 551DB, INBOARD OF PYLON. / REPAIRED WAFFLE PLATE PER SRM.SDR SWAA2022032952777Angle · cracked: RT WING UPPER T/E PANEL LOWER WEB ATTACH ANGLE CRACKED AT FLAP DEFLECTION ARM ATTACH POINT. / REMOVED AND REPLACED ANGLE PER SRM 51-40-02SDR SWAA2022022210784Plate · crackedR/H WING TRAILING EDGE CAVITY INBD WIGGLE PLATE ABOVE SAIL TAIL HAS FASTENERS SHEARED AND PLATE IS CRACKED / R/H TRAILING EDGE ACVITY I/B PLATE ABOVE SAIL TAIL REMOVED IAW B-737-700 SRM 51-40-02-0G-0 AND REPLACED NEW IAW -737-700 SRM 51-40-05-0G-0 & SRM 51-40-SDR SWAA2022032996838Fairing · cracked#3 CANOE FAIRING TAL CORE HAS CRACK I/B SIDE MEASURES 3.25'L 3.5' FROM TRAILING EDGE 3' FROM UPPER JOINT / REF DMA#0177934 INSTALLED NEW TAIL FAIRING ON #3 CANOE REF AMM 27-51-18 CLR# 91774SDR SCNA20190907155Panel · damagedTHE INNER SIDE OF PANEL 661AB IS DAMAGED. REPAIRED THE INNER SIDE OF PANEL 661 A/B.SDR SWAA2022022241475None · crackedLEFT WING T/E I/B OF PYLON SAIL TAIL; WIGGLE PLATE IS CRACKED. / REMOVED AND REPLACED L/H WING T/E I/B OF PYLON SAIL TAIL IAW SRM 51-40-02-0G-0; 51-40-05-0G-0; AND DWG 115A2714 SHT 1 REV BSDR SWAA2022022241439Plate · crackedLEFT WING LOWER TRAILING SKIN WIGGLE PLATE JUST INBOARD OF #3 FLAP TRACK IS CRACKED / REMOVED AND REPLACED L/H WING LOWER TRAILING SKIN WIGGLE PLATE JUST I/B OF #3 FLAP TRACK IAW SRM 51-40-02-0G-0; 51-40-05-0G-0; AND DWG 115A2713 SHT REV BSDR SWAA2022031505758Nut Plate · crackedAT LEFT WING TRAILING EDGE NUT PLATE BEAM BELOW #5 SPOILER PANEL IS CRACKED / REMOVED AND REPLACED NUT PLATE BEAM AT LEFT WING TRAILING EDGE; BELOW #5 SPOILER PANEL IAW SRM 51-40-02-G0-0 AND DRAWINGS 115A3758; 115A3712 59796C 30AUG19SDR SWAA2022022205730Plate · crackedRIGHT WING TRAILING EDGE WIGGLE PLATE JUST O/B OF SWING DOWN PANEL CRACKED / REMOVED WIGGLE PLATE RIGH WING JUST O/B OF SWING DOWN PANEL IAW SRM 51-40-02-0G-01 89813U 08-31-19 LEAD 286 8/31/19 REPLACED WIGGLE PLATE RIGHT WING TRAILING EDGE JUST O/B OF SWING DOSDR SWAA2022022209435Plate · crackedR/H WING AFT TRAILING EDGE CAVITY WIGGLE PLATE ABOVE BOTTOM ACCESS PNL 651GB IS CRACKED / R/H WING AFT TRAILING EDGE CAVITY WIGGLE PLATE ABOVE BOTTOM ACCESS PNL 651 GB WAS REMOVED DUE TO CRACK REPLACED VERIFIED P/N 115A2781-14 A TAG WN6612 LOCATED DRILLED AND SDR SWAA2022022209436None · crackedR/H WING AFT TRAILING EDGE CAVITY ABOVE #6 FLAP TRACK ASSY WIGGLE PLATE IS CRACKED / REMOVED AND REPLACED #6 FLAP TRACK ASSY WIGGLE PLATE AT R/H WING AFT TRAILING EDGE CAVITY IAW SRM 51-40-02-0G-0; BOEING DRAWING 115A2781 REV -. RESTORED FINISH ON AREA IAW AMMSDR SWAA2019082736353Plate · crackedL/H WING AFT TRAILING EDGE CAVITY ABOVE #3 FLAP TRACK ASSEMBLY WIGGLE PLATE ASSEMBLY CRACKED INBOARD SIDE CORNER. / R&R WIGGLE PLATE IAW SRM & DWG.SDR SWAA2022022209593Plate · crackedWIGGLE PLATE IS CRACKED ABOVE THE NUMBER 6 FLAP TRACK / R/R WIGGLE PLATE PER SRM 51-40-02. SEE NRC FOR INDIVIDUAL SIGN-OFFS.SDR SWAA2022022228063Plate · crackedLEFT WING LOWER TRAILING EDGE SKIN WIGGLE PLATE ASSY IS CRACKED JUST INBOARD OF #3 FLAP TRACK / REMOVED AND REPLACED WIGGLE PLATE INBOARD OF #3 FLAP TRACK IAW SRM 51-40-02. P/N 115A2781-3 A TAG #WN3797SDR SWAA2022031449308Fairing · delaminatedLH WING TO BODY FAIRING 195CL HAS DELAMINATION SPOT 19INCHES FROM AFT SIDE OF PANEL (MARKED) / REPAIRED PER SRM 53-60-70-2R-1 AND SRM 51-70-05. SEALED PER SRM 51-70-08; RESTORED FINISH PER AMM 51-21-73SDR SWAA2022022231144Plate · crackedRIGHT WING; TRAILING EDGE WAFFLE PLATE PANEL SUPPORT; UNDER THE #8 SPOILER ACTUATOR; IS CRACKED. / REMOVED AND REPLACED RIGHT WING; T/E WAFFLE PLATE PANEL SUPPORT I/A/W BOEING DWG 115A3760 REV. A REV B; 737-700 SRM 51-40-02-0G-0; 737-700 SRM 51-40-05-0G-0; ANDSDR SWAA2022022231146Plate · crackedRIGHT WING; TRAILING EDGE WAFFLE PLATE PANEL SUPPORT; UNDER THE #7 FLAP TRANSMISSION; IS CRACKED. / RIGHT WING; TRAILING EDGE DAMAGED WAFFLE PLATE PANEL SUPPORT; UNDER THE #7 FLAP TRANSMISSION REMOVED AND REPLACED NEW IAW B-737-700 SRM 51-40-02-0G-0. FASTENER SDR SWAA2022022283832Plate · brokenR/W T/E WIGGLE PLATE BROKEN COMMON TO FORWARD EDGE OF PANEL 651BB / REMOVED AND REPLACED WIGGLE PLATE ASSY R/W T/E COMMON TO FORWARD EDGE OF PANEL 651BB IAW SRM 51-40-02-0G-0; DWG 115A2781 AND IPC 57-50-00-27 83802U 10AUG19SDR FDEA2019071761593Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE (#10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZEDSDR SWAA2022022207753Plate · crackedRIGHT WING AFT TRAILING EDGE CAVITY; OUTBD WIGGLE PLATE FOR ACCESS PNL 651GB IS CRACKED AT INBD FASTENER HOLE AREA / REMOVED AND REPLACED RIGHT WING AFT TRAILING EDGE CAVITY OUTBOARD WIGGLE PLATE FOR ACCESS PANEL 651GB IAW SRM 51-40-02-0G-0 AND BOEING DRAWING SDR SWAA2022022207755Plate · crackedRIGHT WING AFT TRAILING EDGE CAVITY; ABOVE ACCESS PNL 651EB WIGGLE PLATE ABOVE #6 FLAP TRACK ASSY IS CRACKED AS MARKED / REMOVED DAMAGED WIGGLE PLATE AT R/WING AFT TRAILING EDGE CAVITY ABOVE PANEL 651EB AND REPLACED NEW IAW SRM 51-40-02-0G-0; 51-0-05; AND 51-4SDR FDEA201906251484Skin · unknownEXISTING REPAIR ON RH WING 1# SLAT LOWER SKIN BETWEEN RIB9 AND RIB10 REQUIRES EVALUATION FOR CONFORMITY THE
EXISTING REPAIR ON RH WING 1# SLAT LOWER SKIN BETWEEN RIB9 AND RIB10 WAS EVALUATED AND FOUND NO REPAIR
RECORD WAS AVAILABLE. THE EXISTING REPAIR PITCHSDR LR7A2019062402104Rib · warpedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND RT ATTACHMENT RIB WARPED AND EXCEEDED CUT OUT AT OWS255. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6610.SDR SWAA2022022231497Plate · crackedRIGHT WING T/E I/B OF #6 FLAP TRACK; WIGGLE PLATE IS CRACKED. / REMOVED AND REPLACED WIGGLE PLATE AT R/W T/E I/B OF #6 FLAP TRACK I.A.W. B737 SRM 51-40-02-0G-0; 51-40-05-0G-0; SRM 51-20-01-0G-0 A.M.M. 51-21-72-370-804 AMM 51-21-99-300-801SDR SWAA2022031028433Retainer · crackedLEFT WING TRAILING EDGE MIDSPAN BULKHEAD AFT CURVED SEAL RETAINER ANGLE IS CRACKED / INSTALLED NEW LEFT WING TRAILING EDGE MIDSPAN BULKHEAD AFT CURVED SEAL RETAINTER. P/N 115A2953-1 IAW 51-40-02-0G-0 (SRM) ATAG A70616SDR SWAA2022022208830Plate · crackedRIGHT WING TRAILING WIGGLE PLATE IS CRACKED AT RSS 261 / WIGGLE PLATE RW T/E IS TO BE REPLACED ON CARD # T938670.SDR SWAA2022022202564Plate · crackedRIGHT WING T/E BELOW #8 SPOILER ACTUATOR; WIGGLE PLATE IS CRACKED. / REMOVED AND REPLACED R/H WING T/E BELOW #8 SPOILER ACTUATOR WAFFLE PLATE IAW SRM 51-40-02-0G-0 AND BOEING DWG 115A3700 SHT 6 REV: B.SDR SWAA2022022227701Plate · crackedWAFFLE PLATE CRACKED INBD OF #3 FLAP TRANSMISSION SUPPORT / REMOVED AND REPLACED WAFFLE PLATE INBOARD OF #3 FLAP TRANSMISSION SUPPORT PER SRM 51-40-02.SDR SWAA2022022206822Plate · brokenLH WING WIGGLE PLATE FOR 561BB I/B CORNER IS BROKEN / REMOVED; FABRICATE; AND INSTALLED SERVICEABLE WIGGLE PLATE ON LW LWR SKIN AT T/E; I/B END OF PANEL 561BB PER BOEING DWG 115A3750; AMM 51-21-41-370-802; STEP 3E; AMM 51-21-72-370-804 STEP 5.E; AMM 51-21-99-3SDR FDEA201905221107Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT INBOARD HOLE BORE (#2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44SDR SWAA2022022490365Strip · crackedR/W T/E WIGGLE STRIP AT ORSS 261 HAS SHEARED RIVETS AND IS CRACKED.. / REMOVED & REPLACED R/W T/E WIGGLE STRIP PER SRM 51-40-02-0G-0 STEPS 4.A.& B.SDR SWAA2022022207610Plate · brokenRIGHT WING LOWER T/E; WIGGLE PLATE I/B OF PYLON SAIL TAIL HAS SHEARED FASTENERS AND BROKEN NUTPLATE. / REMOVED BROKEN RIGHT WING LOWER T/E; WIGGLE PLATE I/B OF PYLON SAIL TAIL AND REPLACED WITH NEW WIGGLE PLATE P/N 115A2781-14 IAW SRM 51-40-02; IPC 57-50-00-30SDR SWAA2022022205860Plate · crackedR/H WING; WIGGLE PLATE JUST INBOARD OF #6 FLAP TRACK ON REAR SPAR IS CRACKED. / R&R WIGGLE PLATE PER SRM 51-40-02SDR SWAA2022030746193Spoiler · delaminated#4 SPOILER HAS 1 EACH DISBOND LOCATED 21' FROM OUTBD SIDE; 14' FROM L/E MARKED IN RED / REPAIRED 1EA DISBONDED ON #4 SPOILER LOCATED 21' FROM O/B SIDE 14' FROM L/E PER SRM 51-70-10-2R-2 AND SRM 51-70-10-2R-0.SDR SWAA2022022405722Plate · crackedR/H WING LOWER SHELF PANEL WIG PLATE CRACKED WS 278.50. / R&R WIGGLE PLATE PER SRM 51-40-02SDR SWAA2022022225981Plate · crackedLFET WING LOWER TE WIGGLE PLATE CRACKED AT FASTENER PANEL 651GB REJECTION: LOWER WING SURFACE DECORATIVE FINISH NOT RESTORED / REJECTED INSP 390 4-12-19 RESTORED LOWER WING SURFACE DECORATIVE FINISH IAW. AMM 51-21-99-300-801; REMOVED AND REPLACED LEFT WING LOW
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