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 SWAA2022070110062Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 273 AT RT WING 2022-265836 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 273 AT RT WING IAW B737-700 SRM 51-40-02 ;51-10-02;[02] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 273 AT RT WINGSDR SWAA2022070109625Access Panel · crackedCRACK ACCESS PANEL 661BB HOLES AT RT WING 2022-265723 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 15331926; DUE DATE: 28-SEP-22.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N:15102320; DUE DATE: 16-JAN-23;[03] TOOL USED: SCALE P/N:CL5000; S/N: AE-408753; DUE SDR REXA2022062001258Stop · chafedLH/S WING IN/B FLAP STOPPER AT AFT SPAR IS CHAFED AND MISSING BUMPER PAD BETWEEN W/S 29.00 - WS 38.00 (INBD SIDE) REMOVED REPLACED STOP ASSY IAW CRJ 900 SRM 51-42-06-001-001-A01 & AMM 20-21-00-910-801-A01.SDR IPXA2022052582486Support Beam · corrodedINSPECTION TYPE:C16CORROSION ON RH WING INBD SPOILER SUPPORT BEAM UPPER CHORD BETWEEN WBL 168 AND 2BL 238REPAIR I.A.W 767-300BCF SRM 57-51-02, ALLOWABLE DAMAGE 1, REV. 43.00.SDR REXA2022062301289Panel · chafedPANEL 684AB IS CHAFED. PANEL REPLACED.SDR REXA2022062201287Angle · corrodedSUPPORT ANGLE FOR PANEL 542 IS CORRODED.. REMOVED AND REPLACED ANGLE IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-40-11-001-001-A01.SDR SWAA2022061608011Support · crackedLOWER BULB SEAL RETAINER SUPPORT IS CRACKED AT RIGHT WING FIXED T/E PANEL JUST AFT OF THE PYLON ORSS 272. MARKED / [01] REMOVED RETAINER SUPPORT FROM RIGHT WING FIXED T/E ORSS 272 SRM 51-40-02.;[02] RECEIVED FITTING P/N 115A2953-2 LOT 1491603-1. LOCATED AND DRSDR SWAA2022061608072Support · crackedBULB SEAL RETAINER SUPPORT IS CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON ORSS 272. MARKED / [01] REMOVED RETAINER SUPPORT (FITTING) FROM LEFT WING T/E PANEL JUST AFT PYLON ORSS 272 PER SRM 51-40-02.;[02] RECEIVED NEW FITTTING P/N 115A2953-1 LOTSDR SWAA2022060907971Beam · brokenBEAM ASSY BROKEN AT I/B END FOR T/E PNL 561AB / [01] REMOVED AND REPLACED BEAM ASSY AT I/B END FOR T/E PNL 561AB IAW SRM 51-40-02-0G-0. <BR>CAL ID:ATS1699<BR>S/N:1505369<BR>DUE:04/2022;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION #2SDR YENA2022051700479Rib · crackedDURING HEAVY MAINTENANCE, WINGS / RH WING / FIXED LEADING EDGE RIB 17 INBOARD SIDE / CRACK - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR).SDR YENA2022051700478Rib · crackedDURING HEAVY MAINTENANCE, WINGS-LH/ FIXED LEADING EDGE RIB 27 OB SIDE/ CRACK- PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR).SDR REXA2022062301288Panel · chafedLEFT INBOARD FLAP LEADING EDGE PANEL 584GB IS CHAFFED. LOCATED, DRILLED, AND INSTALLED NEW PANEL 584GB PER CRJ SRM 51-40-11-001-001-A01SDR SWAA2022060807045Support · crackedLOWER BULB SEAL RETAINER SUPPORT IS CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON ORSS271. MARKED / [01] REMOVED AND REPLACED LOWER BULB SEAL RETAINER SUPPORT AT LH WING FIXED T/E PANEL. IAW SRM 51-40-02 AND IPC 57-50-00-25.;[02] VERIFIED CORRECTISDR FDEA202205111178Rib · crackedRIGHT WING - NUMBER 6 LEADING EDGE SLAT INNER RIB FOUND CRACK AT STATION XOS 858.175. RIGHT HAND WING - NUMBER 6 LEADING EDGE SLAT INNER RIB AT STATION XOS 858.175 REPAIR CARRIED OUT AS PER E.A. # 1-5750-T0368508 P1 TITLE: WINGS Ï¿½ FLIGHT SURFACES Ï¿½ RSDR SWAA2022052306717Fairing · delaminated#6 FLAP TRACK FAIRING 642BB HAS FIBERGLASS PLY SEPARATION AT EXISTING SRM SEAL RETAINER REPAIR. / REPAIRED PER E/A VERIFIED REPAIR PER EASDR SWAA2022061409734Panel · elongatedL/W PANEL 561AB HAS FOUR HOLE SCREW ELONGATED. / [01] PERFORMED VISUAL AND TAP TEST INSPECTION ON PANEL #521VB AND FOUND NO ENTRY OF WATER; OIL; FUEL; OR OTHER UNWANTED MATERIAL PER B737 NDTM 51-05-01;[02] CORRECTION TO STEP 1 PERFORMED VISUAL AND TAP TEST INSSDR SWAA2022060805699Panel · pulledR/W T/E PANEL 661CB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / [01] IDENTIFIED PART AND MATERIAL ID PER SRM 57-51-01-0I-1 FIG.3; SHT.1; TABLE 3; AND ITEM 10. FOUND SEVERAL PULLED FASTENER HOLES TO BE OUT OF ALLOWABLE DAMAGE LIMITS PER SRM 57-51-01-1A-1 PAR.4SDR SWAA2022060805703Panel · pulledL/W T/E PANEL 561BB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / [01] IDENTIFIED PART AND MATERIAL IAW SRM 57-51-01-0I-1 FIGURES 1+3; TABLE 3; ITEM[9].<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PAR 4.B (5) (B).<BR>PERMANENT REPSDR SWAA2022060805704Panel · pulledL/W T/E PANEL 561AB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / [01] IDENTIFIED PART AND MATERIAL ID PER SRM 57-51-01-0I-1 FIG.3; SHT.1; TABLE 3; AND ITEM 10. FOUND SEVERAL PULLED FASTENER HOLES TO BE OUT OF ALLOWABLE DAMAGE LIMITS PER SRM 57-51-01-1A-1 PAR.4SDR SWAA2022060805705Panel · delaminatedL/W L/E PANEL 521DB HAS AREA OF DELAM (MARKED) / [01] IDENTIFIED PANEL 521DB MATERIAL IAW SRM 57-41-01-0I-1 FIGURE 5 TABLE 5 ITEM 2<BR><BR>DAMAGED AREAS EXCEED ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PAR.4 A(2)<BR><BR>DAMAGE IS REPAIRABLE IAW SRM 51-70-0SDR FDEA202205081148Bracket · corrodedLEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. SDR FDEA202205081147Hinge · corrodedLEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.ASDR FDEA202205081146Hinge · corrodedLEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.ASDR FDEA202205081145Hinge Bracket · corrodedLEFT HAND WING - LEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM SDR SWAA2022060805500Panel · pulledR/W T/E PANEL 661AB HAS SEVERAL PULLED FASTENER HOLE (MARKED) / [01] IDENTIFIED PANEL 661AB IAW SRM 57-51-01-0I-1 FIGURE 3; SHEET 1; TABLE 3; ITEM 5. <BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PAR 4B(5).<BR><BR>REPAIR TO BE ACSDR SWAA2022060805501Panel · pulledR/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / [01] IDENTIFIED PANEL 661BB MATERIAL IAW SRM 57-51-01-0I-1 TABLE 3 FIGURE 3 ITEM 9. DAMAGE TO MULTIPLE FASTENER HOLES AS MARKED ARE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PARAGRAPH SDR SWAA2022052305149Bracket · crackedR/H WING UPPER SHELF PANEL I/B SUPPORT BRACKET CRACKED. LOCATED JUST OBD OF #6 SPOILER. / [01] REMOVED AND REPLACED BRACKET PER SRM 51-40-02;[02] PARTS INFO ONLY.SDR REXA2022053100905Panel · chafedPANELS 684ET AND HT HAS CHAFFING DAMAGE. REPAIRED CHAFFING DAMAGE TO PANEL 684ET IAW CRJ 900 SRM 51-12-00-001-001-A01. REPLACED DAMAGED PANEL 684HT IAW CRJ 900 SRM 51-40-11-001-001-A01.SDR SWAA2022052603146Access Panel · elongatedRIGHT WING ACCESS PANEL # 661CB T/E HAS AN ELONGATED ATTACH HOLE AT FWD CORNER I/B SIDE, MEASUREMENTS; CLEANED PANEL AND PREPARED AREA FOR REPAIR ON R/W LOWER ACCESS T/E PANEL 661CB AS PER B737 51-70-04-2R-9;PERFORMED DRY OUT ON DAMAGE AREA FOUND NO WATER AS PSDR SWAA2022052602387Bracket · brokenRT WING LOWER INBRD. PNL. 651FB HAS BROKEN TIE DOWN BRACKET ON OB END. / [01] REMOVED AND REPLACED R/H WING PANEL 651FB TIE DOWN BRACKET REF B-SRM 51-40-02;[02] VERIFIED REPLACED BRACKET. AMT STEP 1.SDR FDEA202204291080Pivot · corrodedRIGHT HAND WING - RIGHT HAND AFTER (FLAP) INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57SDR FDEA202204291079Pivot · corrodedRIGHT HAND AFTER (FLAP) INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5SDR FDEA202204271061Slat · dentedLEFT WING SLAT 4 WITH DENT T/E WEDGE LH WING SLAT #4 WEDGE AT POSITION OSS(648.9-657) UPPER SKIN WAS REPAIRED IAW SRM 57- 43-02-2R PAG. 1-2 FIG. 201 AND SRM 51-70-10-2R REP. 4 PAG. 149, 159-163 FIG. 202 REV. 82 DEC15/2021SDR REXA2022061001133Panel · chafedPANEL 684EB CHAFED NEAR VANE ACTUATOR. REMOVED CHAFED PANEL AND LOCATED AND DRILLED A SERVICEABLE PANEL 684EB IAW CRJ 700 SRM 51-40-11-001-001-A01.SDR SWAA2022052397547Access Panel · crackedCRACK ACCESS PANEL 643CR AT RT WING 2022-211550 / [01] REPLACED ACCESS PANEL 643CR AT RT WING IAW B737-700 AMM 27-51?28-400-804 STEP 9 H(4).;[02] REPLACED ACCESS PANEL 643CR AT RT WING IAW B737-700 AMM 27-51?28-400-804 STEP 9 H(4).SDR IPXA2022042981558Angle · brokenINSPECTION TYPE:CRT WING 2 FLAP O/B END ANGLE BRACKET BROKEN/MISSINGREMOVED AND REPLACED IAW SRM 51-40-21SDR FDEA202204251046Hinge · corrodedLEFT HAND WING - LEFT HAND AFT (FLAP) INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE BORE FOUND COROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-SDR FDEA202204251045Hinge · corrodedLEFT HAND WING - LEFT HAND AFT (FLAP) INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE FOUND COROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03SDR FDEA202204241039Hinge · corrodedRIGHT HAND WING - RIGHT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57- 44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 SDR FDEA202204241038Hinge · corrodedLEFT HAND WING - LEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57- 44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 ANSDR FDEA202204231035Spoiler · failedDUE TO HOLE DAMAGE A/C N986FD FOUND DURING B-CHECK IN IND, MAINTENANCE REPORTED A HOLE ON #10 SPOILER (FROM INBD EDGE 49" & 6" AFT EDGE). SPOILER PANEL IS REPAIRED PER 57-70-01-2R, TABLE I, 200 DEGREE F WET LAYUP. EA F-5750-T0368159 ISSUED TO DOCUMENT THE ESDR FDEA202204211019Skin · crackedL.WING L/E SLAT #2, COVE SKIN IS CRACKED AT OUT BOARD SLAT TRACK. REMOVED SKIN, FABRICATED NEW SKIN PER BAC DWG 114N4076, REINSTALLED NEW SKIN PER BAC DWG 114N4003SDR FDEA202204201006Skin · crackedL.WING L/E #3 SLAT COVE SKIN IS CRACKED. REMOVE SKIN, FABRICATE NEW SKIN AND REINSTALL PER BAC DWG 114N4077 AND 114N4004SDR IXXA2022042704Bracket · crackedLH WING #6 SLAT INNER SUPPORT ANGLE AT APPROX LES 281.12 IS CRACKED. FAS WO N389AZ-02-01 NON ROUTINE 00061SDR IXXA2022042707Bracket · crackedRH WING #7 SLAT INNER SURFACE SUPPORT ANGLE AT APPROX LES 320 IS CRACKED. FAS WO N389AZ-02-01 NON ROUTINE 00072SDR IXXA2022042706Bracket · crackedRH WING #7 SLAT INNER SURFACE SUPPORT ANGLE AT APPROX LES 295 IS CRACKED. FAS WO N389AZ-02-01 NON ROUTINE 00071SDR FDEA202204190996Bracket · crackedRIGHT WING I/B L/E CAVITY SLAT TORQUE TUBE SUPPORT BRACKET CRACKED @ IFSS 282 REMOVED & REPLACED SLAT TORQUE TUBE GUIDE BRACKET IAW BAX DWG 114T1240, SHEET 6, REVISION -SDR FDEA202204190995Bracket · crackedL/H SLAT DRIVE SUPPORT BRACKET CRACKED 3 PLACES UNDER #6 SLAT REMOVED & REPLACED TORQUE TUBE GUIDE BRACKET IAW BAC DWG 114T1240, SHEET 6, REVISION -SDR IPXA2022041781237None · noneINSPECTION TYPE:N/ALEFT OTBD AFT FLAP TRAILING EDGE WEDGE UPPER SKIN REPAIRREPAIRED PER EO B757-5750-83466-ASDR SWAA2022041994984Bracket · crackedL/H WING UPPER PANEL SUPPORT FORWARD 'Z' ANGLE IS CRACKED / [01] R&R L/H WING UPPER PANEL SUPPORT FORWARD 'Z' ANGLE BRACKET IN REF TO SRM 51-40-02. NO FURTHER DEFECTS NOTED.
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