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 FDEA202305030801Unknown · delaminatedDISBOND INDICATION FOUND ON UPPER SURFACE OF #8 SLAT, MOST OUTBOARD EDGE. REPAIRED #8 SLAT UPPER SURFACE IAW FEDEX EA # F-5750-T0374114-P1-FLIGHT SURFACES-#8 SLAT,TRAILING EDGE WEDGE, DELAMINATION-SRM REPAIR DEVIATION.SDR SWAA2023052443893Plate · crackedLT WING T/E WIGGLE PLATE CRACKED O/B OF PANEL 551DB.<[01] REMOVED CRACKED L/H WAFFLE PLATE OTB OF PANEL 551DB PER SRM 51-40-02.;[02] INSTALLED REPLACEMENT WIGGLE PLATE PER SRM 51-40-02. RESTORED EXTERIOR FINISH PER AMM 51-21-99.;[03] VERIFIED WORK COMPLETED.SDR SWAA2023052443901Plate · crackedCRACKED WAFFLE PLATE OTBD. OF LOWER PANEL 651 DB<[01] REMOVED CRACKED R/H WAFFLE PLATE OTB OF PANEL 651DB PER SRM 51-40-02.;[02] REMOVED AND INSTALLED NEW WAFFLE PLATE PER SRM 51-40-02.;[03] VERIFIED WORK COMPLETED.SDR SWAA2023052341474Fairing · cracked#2 FLAP FAIRING # 543BB FWD EDGE SMALL CRACK.<[01] OK TO APPLY REPAIR.;[02] APPLIED REPAIR AT #2 FLAP FAIRING 543BB ON FWD EDGE PER B737 SRM 51-70-04-2R-0 PARAGRAPH 4.L.7 MATERIAL USED RESIN EY3804 PO#1800550 AND FIBERGLASS PO#1738579;[03] VERIFIED ALL STEPSSDR SWAA2023052530607Panel · pulledR/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED MATERIAL OF PANEL 661BB IAW SRM 57-51-01-0I-1 FIGURE 1 AND 3; ITEM 9; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 TABLE 101; PARA 4.B(5)<BR><BR>REPSDR SWAA2023050130204Bracket · crackedPANEL 551EB: FWD INBOARD ATTACH WAFFLE BRACKET IS CRACKED AND FASTENER IS LOOSE.<[01] REMOVED AND REPLACED WAFFLE BRACKET PER SRM 51-40-02.;[02] COMPLETESDR SWAA2023052530114Plate · crackedLEFT OUTBOARD WING REAR SPAR - WIGGLE PLATE HAS A CRACK ORSS 228 (MARKED)<[01] REMOVED AND REPLACED LEFT OUTBOARD WING REAR SPAR - WIGGLE PLATE AT ORSS 228; P/N 115A3760-29 IAW SRM 51-40-02 AND AIPC 57-50-00-17;[02] VERIFIED CORRECTIVE ACTION ITEM; CARD COMPLESDR IPXA2023051393214Flap · crackedINSPECTION TYPE:5Y*MAJOR REPAIR* RIB 27 ON CENTER FLAP FOUND CRACKEDREPAIRED RIB 27 PER UPS EO A300-5750-8612-A AND VTMAE FINAL EA 300-5750-27-A3212-ASDR SWAA2023052529591Bracket · crackedR/H WING PANEL 651FB HAS A CRACKED BRACKET ON THE SEAL RETAINER.<[01] R/R R/H WING PANEL 651FB BRACKET IAW SRM 51-40-02.;[02] INSPECTED C/A 1. ANDY HERNANDEZ (TECHNICIAN); 27-APR-2023 03:46 UTC<BR>R/R R/H WING PANEL 651FB BRACKET IAW SRM 51-40-02.SDR SWAA2023052529771Plate · crackedLEFT WING TRAILING EDGE PANEL ATTACHMENT PLATE(WIGGLE) CRACKED JUST OUTBOARD OF LEFT WING PANEL 551DB.<[01] REPLACED WIGGLE PLATE ASSY. 52-50-00-22-205. PER SRM 51-40-02;[02] REPLACED WIGGLE PLATE ASSY. 115A2781-3 PER SRM 51-40-02;[03] INSPECTION COMPLETE ON CSDR SWAA2023052529273Panel · crackedLT WING T/E PANEL 561AB HAS CRACKS AROUND FSATENER HOLES ALONG T/E<[01] IDENTIFIED MATERIAL OF PANEL 561AB IAW SRM 57-51-01-0I-1 FIGURE 1 AND 3; ITEM 5; TABLE 3<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 TABLE 101; PARA 4.B(5)<BR><BRSDR SWAA2023051728476Panel · crackedAT FWD O/B SIDE #3 FLAP TRACK AFT FAIRING PANEL (532CL) CRACKED CORRECTION TO PANEL: (542CL)<[01] REMOVED AND REPLACED AT FWD O/B SIDE #3 FLAP TRACK AFT FAIRING PANEL (532CL) IAW AMM 20-50-11-201-NG;[02] UPDATED MEASUREMENT TABLE;[03] PANEL REPLACED PER SRM 51SDR SWAA2023051943850Panel · delaminatedLOWER RT WING TO BODY FAIRING PANEL 192BR DELAMINATED<[01] REMOVED AND REAPPLIED GLASS FABRIC PLIES; PRIMED AND TOPCOATED PANEL 192BR. REF B737 SRM 53-40-70-2R-1 AND SRM 51-70-04-2R-1 REPAIR 1 PARAGRAPH 4; AMM 51-21-72-370-804; AMM 51-21-73-370-803<BR>MATERIALSDR SWAA2023041726995Panel · crackedLEFT WING SLAT PANEL 521QB IS CRACKED ON THE FWD INBOARD SCREW HOLE<[01] REMOVED AND REPLACED LEFT WING SLAT PANEL 521QB. REF AMM 57-50-01 AND SRM 51-40-02.SDR YENA2023041300373Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE REAR FALSE SPAR AT LEVEL OF RIB 8 OVERHAND ARE A ON RH WING; REF AEROMAN NR 2023-68541 WO 2023 1/1 REPAIRED MULTI-SITE CORROSION SPOTS FOUND ON THE TRAILING EDGE OVERHANG TOP SKIN PANEL 2 ON THE RH WING BETWEENSDR YENA2023041300372Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOCATED ON TOP SKIN TRAILING EDGE OVERHANG AREA LOWER SURFACE E AT LEVEL RIB 16 PLUS 12.800 IN RH WING; REF AEROMAN NR 2023-69019 WO 2023 1/1 REPAIRED MULTI-SITE CORROSION SPOTS FOUND ON THE TRAILING EDGE OVERHANG TOP SKIN PSDR YENA2023041300371Unknown · unknownDURING HEAVY MAINTENANCE: SECONDARY FINDING: WEAR LOCATED TOP SKIN PANEL TRAILING EDGE OVERHANG AREA AT LEVEL RIB 4 RH WING; REF AEROMAN NR 2023-69030 WO 2023 1/1 REPAIRED MULTI-SITE CORROSION SPOTS FOUND ON THE TRAILING EDGE OVERHANG TOP SKIN PANEL 2 ON THE RSDR YENA2023041300370Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOCATED AT LEVEL RIB 7A TOP SKIN TRAILING EDGE OVERHANG LOWE R SURFACE AREA RH WING; REF AEROMAN NR 2023-69065 WO 2023 1/1 REPAIRED MULTI-SITE CORROSION SPOTS FOUND ON THE TRAILING EDGE OVERHANG TOP SKIN PANEL 2 ON THE RH WISDR YENA2023041300369Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOCATED ON TOP SKIN TRAILING EDGE OVERHANG AREA LOWER SURFACE E AT LEVEL RIB 16 PLUS 12.800 IN RH WING; REF AEROMAN NR 2023-69019 WO 2023 WO 1/1 REPAIRED MULTI-SITE CORROSION SPOTS FOUND ON THE TRAILING EDGE OVERHANG TOP SKISDR YENA2023041300368Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION TOP SKIN TE OVERHANG RIB 13 PLUS 17" LH WING; REF AEROMAN NR 2023-69037 WO 2023 1/1 REPAIRED PER EC A23-242-01.SDR YENA2023041300367Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION TOP SKIN TE OVERHANG RIB 15 LH WING; REF AEROMAN NR 2023-69039 CORRECTIVE ACTION: REPAIR CORROSION STOPS AFFECTING THE TOP SKIN PANEL #2 TRAILING EDGE OVERHANG BETWEEN RIB 13-16, RIB 18-20 AND WX3494-WX-4010 ON THE LH WING ISDR YENA2023041300366Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION EXTERNAL SKIN TOP SKIN TE OVERHANG RIB 18 + 6.5" LH WING; REF AEROMAN NR 2023-69044 WO 2023 1/1 CORRECTIVE ACTION: REPAIR CORROSION STOPS AFFECTING THE TOP SKIN PANEL #2 TRAILING EDGE OVERHANG BETWEEN RIB 13-16, RIB 18-20 ASDR YENA2023041300365Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION EXTERNAL SKIN TE OVERHANG RIB 19 + 8.5" LH WING; REF AEROMAN NR 2023-69045 WO 2023 1/1 CORRECTIVE ACTION: REPAIR CORROSION STOPS AFFECTING THE TOP SKIN PANEL #2 TRAILING EDGE OVERHANG BETWEEN RIB 13-16, RIB 18-20 AND WX3494-SDR FDEA202304120629Flap · dentedRH WING, OUTBOARD FLAP, LOWER SURFACE, WITH DENT (NEAR TO INBOARD FLAP TRACK). RH WING, OUTBOARD FLAP, LOWER SURFACE, WAS REPAIRED IAW B767 SRM 57-53-01-2R PAG. 1-9 AND B767 SRM 51-70-10-2R REP. 4 PAG. 150-151 FIG. 201 REV. 85 DEC15/2022SDR YENA2023041300352Unknown · unknownDURING HEAVY MAINTENANCE: LH WING TE AREA, LOWER SKIN HAS 2 EACH CRACK O/B PYLON; REF: TOMX W/O 2191 NR-00014 REPAIRED PER ETI-190-23-535 REV 3 AND ETD-2023-190-008554 REV B. NO SPECIFIC OR ADDITIONAL INSPECTIONS ARE NECESSARY. TOMX MECH 10000726 INSP 325718.SDR FDEA202304100618Slat · wornRH WING, SLAT #8, TRAILING EDGE, LOWER SURFACE WITH WEAR (ABOVE OF INBOARD AUXILIARY SLAT TRACK). R.H. WING, SLAT # 8, TRAILING EDGE, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-43-02- 2R, FIG 201 SHEET 1-2 AND SRM 51-70-10-2R REP 4, FIG 202 SHEET 8, PAG 150SDR SWAA2023050124982Panel · elongatedL/H WING PANEL 567BT HAS ELONGATED FASTENER HOLE AT I/B UPPER ROW. MRKD<[01] REPAIRED L/H WING PANEL 567BT ELONGATED FASTENER HOLE PER EA 23-157-01346;[02] COMPLIED WITH EA 23-157-01346SDR SWAA2023050124878Panel · crackedRIGHT WING FWD INBOARD ATTACH PINT FOR PANEL 651GB IS CRACKED. (WAFFLE PLATE)<[01] REMOVED AND INSTALLED NEW WAFFLE PLATE WITH ATTENDERS PER SRM 51-40-02.;[02] VERIFIED WORK PERFORMED.SDR FDEA202304080593Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (F AND G HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-0SDR FDEA202304080592Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52SDR FDEA202304080590Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (F AND G HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52SDR FDEA202304080589Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-SDR FDEA202304070585Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED REPAIR BUSHINSDR FDEA202304070584Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-4SDR FDEA202304070583Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-SDR FDEA202304070582Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED REPAIR BUSHISDR FDEA202304070581Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-4SDR FDEA202304070580Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMMSDR FDEA202304070579Support · failedRIGHT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING- OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM57-50-02-2R SDR FDEA202304070578Support · corrodedRIGHT WING- OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING- OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM57-50-02-2R SDR FDEA202304060569Spoiler · delaminatedRH WING #5 SPOILER CENTER I/B & O/B HINGE ARM LWR SURFACE FOUND DELAMINATION SIZE: (1) 20MM * 25MM, DEPTH: 2.1MM (2) 25MM * 60MM, DEPTH: 2.2MM PERFORMED THE REPAIR ON RH WING #5 SPOILER CENTER I/B & O/B HINGE ARM LWR SURFACE AS PER FEDEX EA: 6-5750-T037383SDR SWAA2023041223900Slat · delaminatedSLAT #3 UPPER IB CORNER ON TE AREA IS DELAMINATED. .<[01] REMOVED DELAMINATED EXISTING FILLER REPAIR; AND PREPARED AREA FOR REBOUNDING NEW FILLER REPAIR ON L/W L/E #3 SLAT I/B CORNER T/E AS PER B737 SRM 57-42-01-2R-6. REBOUNDED FILLER REPAIR AS MARKED ON #3 L/SDR GTIA2023040637098Box Beam · dentedDENT LOWER SURFACE OB FLAP ON RH WING RAF 3069146-01 GENERATED -PERFORMED PERMANENT REPAIR ON OB FLAP LOWER SURFACE OH RH WING IAW EC# EA 5753-2319 REVISION 00, EA # 57-0117-23 #1 COVER EA 57-0117-23 PART #1 AND A320 SRM 57-53-00-300-055 THIS REPAIR IS CATEGORSDR VNAA202304061112Unknown · unknown12€? SCRATCH WITH A MAX DEPTH OF .002€? IN THE LEADING EDGE OF THE #2 RH SLAT LEADING EDGE SKIN. PERMANENT REPAIR WAS C/W PER REO 690-57-42-972 INSTRUCTIONS.SDR IPXA2023042793010Balance Weight · corrodedINSPECTION TYPE:3CR/H WING O/B AILERON 2ND WEIGHT FROM O/B HAS CORROSION IN LIGHTING HOLE AT STA XOA=975.REPAIRED CORRODED BALANCE WEIGHT AT THE R/H WING O/B AILERON AT STA XOA=975 IAW EO MD11-5750-29342-F (MINOR)SDR VNAA202304270019Lug · corrodedCORROSION ON BORE LUGS AT HINGE FITTING #2 (I/B AND O/B) & HINGE FITTING#3 (O/B), RH AILERONSDR SWAA2023042023724Web · crackedL/H WING WEB INBD OF DEFLECTION RIB AND BELOW FIXED T/E PANEL HAS A CRACK AT O.B. FASTENER HOLE<[01] REMOVED WEB AND DRILLED NEW WEB PER SRM 51-40-02;[02] C/W INSPECTION.;[03] INSTALLED T/E PANEL PER SRM 51-40-02.SDR SWAA2023040722918Rib · elongatedRH WING INB FLAP DEFLECTION RIB (2 EACH) ELONGATED FASTENER HOLES AT ATTACHMENT TO FIXED T/E.<[01] ACCOMPLISHED REPAIR AT RIGHT WING I/B FLAP DEFLECTOR RIB PER SRM 57-51-02-2R-4 REPAIR 4SDR SWAA2023041722492Bracket · elongatedELONGATED HOLE ON SUPPORT BRACKET TRAILING EDGE AREA ORS 255 AT LT WING 2023-185590<[01] REPLACED SUPPORT BRACKET TRAILING EDGE AREA ORS 255 AT LT WING;[02] CORRECTED STEP 1 <BR>REPLACED SUPPORT BRACKET TRAILING EDGE AREA ORS 255 AT LT WING I.A.W SRM B737-700 SDR U2RA2023040300018Unknown · unknownDURING ROUTINE INSPECTION, FOUND RIGHT INBOARD MID FLAP WITH GROUND DAMAGE (DENTED). ACCOMPLISHED A TIME LIMITED MAJOR REPAIR PER FLIGHT VEHICLES CONSULTING ENGINEERING ORDER 23069-1. DATA APPROVED ON FAA FORM 8110-3 DATED 3/31/2023 BY R. MANASHI DERT-876272
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