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 P5CA2022012800031None · noneLHW O/B MID FLAP CTR L/E FOUND DELAMINATION (127" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A </P>)SDR P5CA2022012800032None · noneLHW O/B FORE FLAP L/E FOUND DELAMINATION (77" TO O/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A </P>)SDR P5CA2022012800033None · noneLHW O/B MID FLAP L/E FOUND DELAMINATION (235" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A </P>)SDR YENA2022031500196Skin Panel · corrodedDURING HEAVY MAINTENANCE, CORROSION AROUND FASTENER R-WING UPPER SURFACE AFT SPAR FASTENER LINE WSTA 7300; C/W FAS EA 21089 REV IR DATED 24 JAN 22 R-WING /SKIN PANEL #2/ BETWEEN RIB 11 AND 13 AT REAR SPAR DATUM/ CORROSION. CLASSIFICATION MAJOR CAT C REPAIR POSSDR YENA2022031500195Skin Panel · corrodedDURING HEAVY MAINTENANCE, CORROSION L WING UPPER SURFACE WSTA 6699 10 IN AFT OF MID STRINGER; C/W FAS EA 21086 REV IR P1-P15 ACCOMPLISHED REPAIR AT L WING TOP SKIN PNL 2 UPPER SURFACE BETWEEN RIBS 11-13 AND STRINGER 11-16 IAW FAS EA 21086REV IR CLASSIFICATIONSDR YENA2022031500194Skin Panel · corrodedDURING HEAVY MAINTENANCE, CORROSION L-WIN UPPER SURFACE REAR SPAR FASTENER ROW WSTA 4862; CW FAS EA REV IR ACCOMPLISHED REPAIR L-WIN TOP SKIN PNL 2 BTW RIB 6-13 AT REAR SPAR DATUM 5 EA CLASSIFICATION MAJOR CAT C REPAIR POST REPAIR LIFE LIMITATION 6 MONTHS RDASDR FDEA202201310170Slat · cracked#3 SLAT COVE SKIN CRACKED AT O/B MAIN TRACK ATTACH FITTING. REMOVED AND REPLACED #3 SLAT COVE SKIN AT O/B MAIN TRACK ATTACH FITTING IAW SRM 51- 40-02, MAJOR REPAIR AND DWG. #114N4077 AND SRM 57-43-01-OI, FIG.1..SDR IPXA2022013178468None · noneINSPECTION TYPE:N/ALEFT WING OTBD T/E FLAP LOWER SKIN DENTS REPAIRREPAIRED LT O/B FLAP ASSY LOWER SKIN IAW UPS EO B767-5750-81837-B ON NRC 676430.SDR REXA2022042000670None · corrodedCORROSION FOUND ON INBOARD CLOSING RIB FROM RT HAND WING FLAP J/C:900-57-690-506 - REMOVED AND REPLACED I/B CLOSING RIB ON O/B FLAP IAW CRJ AMM 57-53-32-400-801SDR SWAA2022030172441Plate · looseLH WING REAR SPAR LOWER CHORD WAFFLE PLATE LOOSE AND HOLES ELONGATED JUST IB OF #3 FLAP TRACK (MARKED) / [01] REPLACED PLATE PER SRM 51-10-02 & SRM 51-40-02.;[02] INSPECTION C/W TASK CARDSDR SWAA2022022364691Support · elongatedLH WING DEFLECTION RIB UPPER SHELF PANEL SUPPORT WORN AND HOLES ELONGATED ; / [01] REMOVED DAMAGED AREA IN DEFLECTION RIB PER ARM 57-51-02-2R-4; [02] REMOVED DAMAGED AREA IN DEFLECTION RIB PER ARM 57-51-02-2R-4; [03] ACCOMPLISHED HFEC OF CUTOUT AREA PER 737NDTSDR SWAA2022022364708Plate · looseLH WING REAR SPAR LOWER CHORD WAFFLE PLATE LOOSE AND HOLES ELONGATED JUST IB OF #3 FLAP TRACK (MARKED) ; / [01] REPLACED PLATE PER SRM 51-10-02 & SRM 51-40-02.; [02] INSPECTION C/W TASK CARDSDR SWAA2022022864467Plate · crackedLEFT WING T/E WIGGLE PLATE AT ORSS 261 IS CRACKED. ; / [01] REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE AT ORSS 261 IAW SRM 51-40- 02-0G-0; PARA. 4.; [02] VERIFIED JOB COMPLETE; [03] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2022022172418Plate · crackedLEFT WING T/E WIGGLE PLATE AT ORSS 261 IS CRACKED. / [01] REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE AT ORSS 261 IAW SRM 51-40- 02-0G-0; PARA. 4.;[02] VERIFIED JOB COMPLETE;[03] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2022022164488Plate · crackedLT WING T/E LOWER WIGGLE PLATE CRACKED INBD OF #3 FLAP TRACK. / [01] REMOVED AND REPLACED LT WING T/E LOWER WIGGLE PLATE PER SRM 51-40-02 .SDR IPXA2022012478222None · dentedINSPECTION TYPE:N/ASMALL DENT ON RIGHT WING INBOARD FLAP LOWER SURFACE T/E AREA BETWEEN STA XIFH 124 AND XW 291MAJOR REPAIR COMPLETED PER E.O. MD11-575080336-A SEE NR 676429 FOR DETAIL PERTAINING TO REPAIR THIS CLEARS D715183SDR FDEA202201240125Slat · crackedRH WING, SLAT #8, TRAILING EDGE WITH WEAR AND CRACK (2EA) RH WING SLAT #8, TRAILING EDGE WAS REPAIRED IAW B767 SRM 57-43-02-2R PAG. 1-2 FIG.201 (SHEET 1) AND SRM 51-70-10-2R REP. 4 PAG. 149, 162, 163 REV.82 15 DEC 21SDR FDEA202201240124Retainer · crackedL/W #3 SPOILER I/B SEAL RETAINER IS CRACKED REMOVED AND REPLACED PER BOEING DWG # 113N4605SDR FDEA202201220277Flap · crackedRH WING INBD FLAP OUTBD SIDE UPPER SURFACE FOUND 1EA CRACKED REPAIRED RH WING INBD FLAP OUTBD SIDE UPPER SURFACE PER B757 SRM57-53-01-2R REPAIR 1 & SRM51-70-10-2R REPAIR 4. TRACKING EA: F-5750-T0366627 P1 WAS ISSUED, TITLE: WING - FLIGHT SURFACES - RH INBOSDR FDEA202201190082Spoiler · delaminatedLH WING #5 SPOILER CENTER I/B & O/B HINGE ARM LWR SURFACE FOUND DELAMINATION. SIZE: (1) 20MM*20MM, DEPTH: 1.9MM (2) 40MM*20MM, DEPTH: 2.2MM COMPLIED WITH EA: 6-5750-T0366401 P1. TITLE: WING - FLIGHT SURFACES - LH 5# SPOILER CENTER HINGE ARMS LOWER SURFACSDR FDEA202201190097None · crackedL/W #3 FLAP TRACK AFT PHENOLIC RUB BLOCKS CRACKED REMOVED AND REPLACED 2EA RUB PLATES PER BOEING DWG # 113N2156 REV ASDR IPXA2022021078844None · crackedINSPECTION TYPE:CLH WING O/B FLAP INTERNAL STRUCTURE RIB 25 HAS CRACK BETWEEN THREE FASTENERS HOLEREPAIRED PER SRM 57-50-00SDR SWAA2022020961777Bracket · cracked90 DEGREE ANGLE BRACKET ON PANEL 651FB IS CRACKED AT THE BEND RADIUS. ; / [01] REMOVED THE BRACKET PER SRM 51-40-02.; [02] INSTALLED NEW BRACKET PER SRM 51-40-02.; [03] INSTALLED NEW BRACKET PER SRM 51-40-02.SDR SWAA2022013161419Beam · wornA-061 R/H WING DEFLECTION CONTROL RIB UPPER TAB AND SUPPORT BEAM WORN AT 2 EA FASTENER HOLES ; / [01] EVALUATED WEAR - DEFLECTION CONTROL RIB UPPER TAB LOSS OF .051'; MAX ALLOWED .040' OUT OF LIMITS<BR>EVALUATED WEAR - SUPPORT BEAM ORIGINAL THICKNESS .090' LOSSDR FDEA202201130064Slat · delaminatedLH WING SLAT #4 CREASE IN L.E. NOSE SKIN OSS: 666. SLAT #4 TRAILING EDGE WEDGE UPPER SKIN AT POSITION OSS 649-664 WAS REPAIRED I.A.W. SRM 51-70-10-2R PAG. 149-154 FIG. 201 PAR. 3.D. AND SRM 57-43-02-2R PAG. 1-2 FIG. 201 REV. 82 DEC 15/ 2021SDR FDEA202201130063Slat · wornLH WING SLAT #5 WITH WEAR IN LOWER SKIN OSS: 439. LH WING SLAT #5 IN LOWER AND UPPER SKIN AT OSS 439 WERE REPAIRED IAW, SRM 51-70-10-2R REP. 4 PAG. 149-159 FIG. 202(SHEET 5) AND SRM 57-43-02-2R PAG. 1-2 FIG. 201 REP. 1 REV. 82 DEC 15/2021SDR SWAA2022013160819Plate · crackedWIGGLE PLATE ON RIGHT WING AT STATION ORSS 375 + 27 PHENOLIC STRIPE CRACKED IPC 57-50-00-20 ITEM 253 ; / [01] REMOVED AND REPLACED WIGGLE PLATE ON RIGHT WING AT STATION ORSS 375 + 27 PER SRM 51-40-02; [02] C/WSDR FDEA202201120059None · noneRH WING. INBOARD FLAP, LEADING EDGE WITH 01 DENT MEASURES L=80MM, W=35MM D=0.3MM AT 334MM OF THE OUTBOARD CLOUSING RIB. RH WING INBOARD FLAP LEAADING EDGE WAS REPAIRED I.A.W. SRM 57-53-01-2R REP. 1 TABLE I PAG. 5 FIG. 201 AND SRM 51-70-03-0G PARA. 5.A. PAGSDR FDEA202201110040None · noneAGING AIRCRAFT - EXISTING REPAIR AT RIGHT HAND WING - INBOARD FLAP LOWER SURFACE SKIN STATION XIFH 183.3 TO XIFH 201.3. EXISTING REPAIR AT RIGHT HAND WING - INBOARD FLAP LOWER SURFACE SKIN STATION XIFH 183.3 TO XIFH 201.3 EVALUATED AND FOUND NOT IN ACCORDASDR FDEA202201110047Slat · wornRH WING SLAT #8 SKIN AFT FACE WITH WEAR ON TWO LOCATIONS OSS-430 AND OSS-495. RH WING, SLAT #8, LOWER SKIN, WEAR AT OSS 495 WAS EVALUATED AND STRUCTURAL DAMAGE NOT FOUND, ONLY PAINT DAMAGE, PAINT WAS RESTORED AND WEAR AT OSS 432 WAS REPAIRED IAW B767 SRM 5SDR FDEA202201050278Flap · delaminatedRH WING INBD FLAP TRAILING EDGE MID DELAMINATION REPAIRED RH WING INBD FLAP TRAILING EDGE MID SKIN PER B757 SRM57-53-01-2R REPAIR 1 & SRM51-70-10-2R REPAIR 4. TRACKING EA: F-5750-T0366626 P1 WAS ISSUED, TITLE: WING - FLIGHT SURFACES - RH INBOARD MAIN FLAPSDR FDEA202201050008None · wornLEFT WING I/B FWD FLAP L/E AREA LOWER SKIN WORN. ACCOMPLISHED PERMANENT REPAIR TO L/W I/B FWD FLAP L/E BY BONDING AN ALUMINUM DOUBLER IAW FED EX EA# F-5750-TO366153-P1 WING-FLIGHT SURFACEES-LH INBD FORE FLAP, LOWER OOUBD LEADING EDGE SKIN, MF STA 235, DOUBSDR REXA2022021000221Panel · chafedPANEL 684ET IS CHAFED
"BLENDING REMOVED AREA FOUND OT BE OUT OF LIMITS REMOVE AND REPLACED
PRE PAD FASTENER HOLES AND INSTALLED 4EA FASTENERS AND PAINTED PANEL
684ET IAW CRJ 900 SRM 57-52-01-001-001-A01, 51-77-00-001-001-A01,
51-40-11-001-001-A01, 51-4SDR FDEA202112293155None · cracked#8 SLAT I/B TRACK I/B SIDE COVE PANEL CRACKED REMOVED AND REPLACED COVE PANEL PER BAC DWG #114N4004 REV FSDR REXA2022020900184Cap · chafed"L/H WING INBOARD FLAP VANE IS CHAFED BETWEEN W.S.88 TO W.S. 108 CHAFE
IS APPROX 0.750 LONG, 0.500 WIDE & 0.015 DEEP. "
"REPLACED VANE CAP LH BTWN W.S. 88 TO 108 IAW CRJ900 SRM 51-25-00-001-
001-A01, 51-42-11-001-001-A01, 51-40-11-001-SDR IPXA2021122777284Flap · noneINSPECTION TYPE:N/ADAMAGE TO FLAP LOWER SKINACCOMPLISHED REPAIR IAW EO 82022-BSDR FDEA202112233129Skin · crackedLEFT HAND WING # 8 SLAT LOWER SURFACE ( COVE PANEL ) ZONE 624 STATION XOS 1097 FOUND CRACK BETWEEN TRACK # 17 AND # 18. LEFT HAND WING # 8 SLAT LOWER SURFACE ( COVE PANEL ) ZONE 624 STATION XOS 1097 CRACKED BETWEEN TRACK # 17 AND # 18 REPAIR CARRIED OUT ASSDR DALA2021122908129None · none**THIS LOG REPLACES LOG 2010626.** DENTS LEFT UPPER FLAP MOVEABLE VANE. SUMMARY OF NRC 00049: LEFT UPPER FLAP MOVEABLE VANE WAS REPAIRED PER B-717-200 SRM 51-70-02-0G PROCEDURE GENERAL ON REFERENCE OF B-717-200 SRM 57-53-01-2R-1 PAR. 4. PERFORM DECAL INSP CONDSDR SWAA2021122254615Plate · crackedLT WING LOWER T/E SHELF PANEL 551GB FWD SUPPORT BRACKET(WIGGLE PLATE) CRACKED. ; / [01] REMOVED AND REPLACED LT WING LOWER T/E SHELF PANEL 551GB FWD SUPPORT BRACKET(WIGGLE PLATE) PER SRM 51-40-02 AND 20-50-11; [02] REMOVED AND REPLACED LT WING LOWER T/E SHELF SDR FDEA202112173095Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-09 AND FOUND BARREL NUT WALL THICKNESS USDR FDEA202112173096Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-08 AND FOUND BARREL NUT WALL THICKNESS UPPERSDR SWAA2022011253499Support Beam · elongatedRIGHT WING ACCESS PANEL 651GB UPPER SUPPORT BEAN FASTENER HOLE ELONGATED ( MARKED) ; / [01] PERFORMED HFEC INSP. IAW B737 NDT<BR>PART 6; 51-00-00; PROCEDURE 23. NO CRACKS <BR>TOOL: NORTEC 600 B/C: 166316 DUE: 10/08/22; [22] REPAIR ACCOMPLISHED PER EA-22-157-00SDR FDEA202112153091Skin · crackedLEFT HAND WING # 8 SLAT LOWER SURFACE ( COVE PANEL ) ZONE 624 STATION XOS 1097 FOUND CRACK BETWEEN TRACK # 17 AND # 18. LEFT HAND WING # 8 SLAT LOWER SURFACE ( COVE PANEL ) ZONE 624 STATION XOS 1097 CRACKED BETWEEN TRACK # 17 AND # 18 REPAIR CARRIED OUT ASSDR 2021F00352Spoiler Panel · corrodedSPOILER WAS RECEIVED WITH SKIN AND DOUBLERS INTERNALLY DISBONDED FORM HONEYCOMB CORE DUE TO CORROSION. SPOILER WAS REPAIRED IAW DELTA ERS#562089-14SDR 2021F00351Spoiler Panel · corrodedSPOILER WAS RECEIVED FOR REPAIR AND INSPECTION WAS PERFORED IAW CMM 27-60-02. CORROSION OF HONEYCOMB CORE WAS FOUND INTERNALLY BETWEEN THE SKINS (UPPER/LOWER) AND DOUBLERS. COMPLETE DISASSEMBLY AND REBONDING WAS ACCOMPLISHED IAW DELTA ERA#562089-14.SDR SWAA2022010352933Balance Weight · corrodedON THE RIGHT WING AT THE TIP; THE INSTALLED WEIGHTS HAVE EVIDENCE OF CORROSION. ; / [01] C/W EA; [02] C/W EA 21-157-03731; [03] C/W EA 21-157-03731SDR SWAA2021121452162Tie Rod · brokenSUPPLEMENTAL INFORMATION: L/H FIXED LOWER TE PANEL 551FB HAS BROKEN SUPPORT STUTS AT LEADING EDGE INBOARD SIDE. ; / [01] R/R TWO BROKEN TIE RODS ON INBOARD FIXED TRAILING EDGE LOWER PANEL PER AMM 57-50-02SDR FDEA202112103078Support · corrodedLEFT HAND WING OUTBOARD FLAP VANE # 4 TEE FITTING TRACK ATTACH HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE # 4 TEE FITTING TRACK ATTACH HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPASDR FDEA202112103077Support · corrodedLEFT HAND WING OUTBOARD FLAP VANE # 3 TEE FITTING TRACK ATTACH HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE # 3 TEE FITTING TRACK ATTACH HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPASDR FDEA202112103076Support · corrodedLEFT HAND WING OUTBOARD FLAP VANE # 2 TEE FITTING TRACK ATTACH HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE # 2 TEE FITTING TRACK ATTACH HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPA
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