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 SWAA2023041923389Panel · delaminatedL/T WING I/B LOWER FAIRING ACEESS PANEL # 194CL HAS SEVERALS FASTENER HOLES BULGING/CRACKED<[01] PREPARED PANEL #194CL FOR REPAIR PER B737 SRM 51-70-06-2R-9 PARA 4.D<BR>APPLIED REPAIR IN DAMAGED AREA AT ACEESS PANEL # 194CL AROUND FASTENER HOLES. AS PER REF B7SDR SWAA2023040621139Panel · crackedRH WING LOWER PANEL 651CB IS CRACKED; AFT INBOARD SIDE NEAR NUT PLATE.<[01] R&R RH WING OWNER PANEL 651CB PER AMM 32-11-00SDR SWAA2023033121125Skin · crackedLEFT WING LOWER SKIN HAS A POSSIBLE CRACK AT FASTENER HOLE LOCATED O/B SIDE OF PYLON FAIRING & COMMON TO RUBSTRIP AT RIB 7, STR 10. INDICATION WAS SEEN WHILE PERFORMING NDT MANUAL PART 4 57-10-15. POSSIBLE CRACK HAD AN INDICATION OF APPROX. 45% FSH & WAS TO SDR SWAA2023032720727Panel · elongatedRH WING LOWER SKIN FIXED TRAILING EDGE PANEL HAS FIVE ENLARGED FASTENER HOLES<[01] REPAIRED IAW SRM 57-51-01-2R-1 AND SRM 51-70-05 2R-8 AND SRM 51-70-14. PERFORMED A NDT TEST PER 737 NDT PART 1 51-01-01. NO DELAMINATION FOUND.;[02] REFINISH REPAIR AREA PER SRMSDR SWAA2023042022885Panel · crackedLEFT WING LOWER MID T/E ACCESS PANEL # 561BB HAS BULGING/CRACKED AROUND FASTENER HOLES<[01] REPAIRED DAMAGED AREA AT LEFT WING LOWER MID T/E ACCESS PANEL # 561BB REF B737 SRM 51-70-04-2R-9-A00753 (REPAIR 9);[02] VERIFIED ALL STEPSSDR SWAA2023042022086Panel · crackedLEFT WING LOWER L/E ACCESS PANEL # 521UB CRACKED/EXPOSED COMPOSITE<[01] REMOVED DAMAGE AREA PANEL 521 UB. AS PER B737 SRM 51-70-06-2R-9 REPARED AREA AND FABRIC REPAIR PANEL 521UB ; AS PER B737 SRM 51-70-06-2R-9 REPAIRED PANEL 521UB; AS PER B737 SRM 51-70-06-2RSDR SWAA2023041922885Panel · crackedLEFT WING LOWER MID T/E ACCESS PANEL # 561BB HAS BULGING/CRACKED AROUND FASTENER HOLES<[01] REPAIRED DAMAGED AREA AT LEFT WING LOWER MID T/E ACCESS PANEL # 561BB REF B737 SRM 51-70-04-2R-9-A00753 (REPAIR 9);[02] VERIFIED ALL STEPSSDR SWAA2023032720320Fairing · pulledRIGHT WING #6 AFT FLAP CANOE AFT TIP FAIRING SIDE FASTENERS PULLED THRU.<[01] REMOVED AND REPLACED AFT FAIRING REF AMM 27-51-18.SDR FDEA202303230496Flap · dentedLH OB FLAP LWR SURFACE FROM OB TO IB 162INCH CROSS TE TO LE 6INCH FOUND ONE DENT LH OB FLAP LWR SURFACE FROM OB TO IB 162INCH CROSS TE TO LE 6INCH DENT WITH DELAMINATION L X W=3.4" X 2.3", OUT OF ALLOWABLE LIMIT PER B777 SRM 57-53-01-1A ALLOWABLE DAMAGE 2,SDR FDEA202303230495Flap · dentedLH OB FLAP LWR SURFACE FROM IB TO OB 177INCH CROSS TE TO LE 15.8INCH FOUND ONE DENT LH OB FLAP LWR SURFACE FROM IB TO OB 177INCH CROSS TE TO LE 15.8INCH DENT WITH DELAMINATION L X W=3.1" X 2.5", OUT OF ALLOWABLE LIMIT PER B777 SRM 57-53-01-1A ALLOWABLE DAMSDR SWAA2023041919291Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT LT WING 2023-191912<[01] ET EQUIPMENT P/N: NORTEC 600D; S/N: 220272712; DUE DATE: 17-DEC-23;[02] REMOVED AND RE-INSTALLED CORRUGATED PLATE AND FASTENERS LOCATED ON TRAILING EDGE AT ORSS261 LT WING IAW B73SDR SWAA2023041919294Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS281 AT LT WING 2023-191913<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS281 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2781; SHEET 7; REV -. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] COMPLETE TASK CSDR FDEA202303210563Skin · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 11~13 T/E-9". COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CSDR FDEA202303210562Skin · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 11~13 T/E-9". COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CSDR FDEA202303210561Skin · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPR SKIN BTW RIB 1C~5,STGR 2.1~2.2. COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS SDR SWAA2023041918449Plate · crackedRT WING T/E N/P STRIP (WIGGLE PLATE) O/B OF 651DB CRACKED.<[01] REMOVED PART 57-50-00-22-270 WIGGLE PLATE PART IS ON ORDER;[02] REPLACED R/H WING NUTPLATE STRIP (WIGGLE PLATE) OTBD OF 651DB IAW SRM 51-40-02SDR FDEA202303170453Slat · wornRH WING, SLAT# 8, TRAILING EDGE, LOWER SURFACE WITH WEAR (TWO PLACES). RH WING, SLAT 8, TRAILING EDGE LOWER SURFACE WAS REPAIRED IAW SRM 57-43-02-2R PAG 1,FIG 201 AND SRM 51-70-10-2R PAG 150, 163 FIG 202 REV 85 DEC 15/2022.SDR SWAA2023041717485Bracket · crackedCRACK REAR SPAR BRACKET IRSS 211 AT RT WING 2023-185520<[01] REAPLACED BRACKET ON REAR SPAR IRSS 211 AT RT WING IAW B737-700 SRM 51-49-92 AND MEASURES OF CRACK ARE: L: 0.500 INCH TOOK MECHANICALLY TOOL USED CALIPER P/N : 500-750-20 S/N: B21015879 DUE DATE: 13-SDR FDEA202303160437Doubler · crackedLEFT HAND WING FIXED LEADING EDGE FOUND BEADED DOUBLER AT STATION XOS 580 CRACKED. LEFT HAND WING FIXED LEADING EDGE DOUBLER AT STATION XOS 580 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR SWAA2023050116654Panel · crackedR/H WING LOWER ACCESS PANEL 661CB LOWER SKIN SURFACE FASTENER HOLES HAS CRACKS. (18-027)<[01] PREPARED REPAIR AND REPAIRED R/H WING ACCESS PANEL 661 CB .AS PER B737 SRM 51-70-04 -2R-9 PARAGRAPH.4 .MATERIAL USED PO.1738579 AND PO.1800550. APPLIED PRIMER PANEL 6SDR FDEA202303150622Skin · unknownEXISTING REPAIR ON RH WING #1 SLAT TAIL SECTION UPR SKIN, T/E-8.5" POSITION, BTW RIB 22~24, EVALUATE TO DETERMINE WHETHER IT IS ACCOMPLISHED BY APPROVED DATA DUE TO NO EXISTING DOCUMENTATION SUPPORTING THIS REPAIR, REMOVED THE EXISTING REPAIR AND PERFORMEDSDR FDEA202303150621Skin · unknownEXISTING REPAIR ON RH WING #1 SLAT TAIL SECTION UPR SKIN, T/E-11.5" POSITION, BTW RIB 8~9, EVALUATE TO DETERMINE WHETHER IT IS ACCOMPLISHED BY APPROVED DATA DUE TO NO EXISTING DOCUMENTATION SUPPORTING THIS REPAIR, REMOVED THE EXISTING REPAIR AND PERFORMED SDR SWAA2023041916330Panel · elongatedRIGHT WING DEFLECTION RIB HAS ELONGATED HOLES AT SHELF PANEL ATTACH POINT.<[01] REMOVED DAMAGE FROM FIXED UPPER RIB PER SRM 57-51-02-2R-1.[05] FABRICATED AND LOCATED REPAIR PARTS PER SRM 57-51-02-2R-4 TABLE 102; ITEMS 1 THRU 4 AND VENDOR PO# P6895661 AND P6895SDR SWAA2023041715730Angle · corrodedCORROSION ANGLE OUTBOARD TRAILING EDGE LOCATED BTW SPOILER 3 AND SPOILER 4 ORSS 354 LT WING 2023-185285<[01] REPLACED ANGLE OUTBOARD TRAILING EDGE LOCATED BTW SPOILER 3 AND SPOILER 4 ORSS 354 LT WING I.A.W B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG#SDR SWAA2023041715724Panel · crackedCRACK ACCESS PANEL 661BB AROUND HOLE AT RT WING 2023-185257<[01] TOOL USED: CALIPER P/N:500-197-30; S/N:B2018941; DUE DATE:19-DEC-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 24/SEP/23.;[03] TOOL USED: SCALE P/N: SPX621 S/N:834022544SDR SWAA2023041715725Panel · crackedCRACK ACCESS PANEL 661AB AROUND HOLE AT RT WING 2023-185259<[01] TOOL USED: CALIPER P/N:500-197-30; S/N:B20189416; DUE DATE:19-DEC-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 24/SEP/23;[03] TOOL USED: CALIPER P/N: 500-193-30 S/N: 00SDR SWAA2023041715632Panel · crackedCRACK ACCESS PANEL 561CB TRAILING EDGE AROUND HOLES LT WING 2023-185210<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189416 DUE DATE: 19-DEC-23;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 24/SEP/23;[03] TOOL USED: SCALE P/N: SPX621 S/NSDR SWAA2023041715649Panel · crackedCRACK ACCESS PANEL 561AB TRAILING EDGE AROUND HOLES LT WING 2023-185218<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189416 DUE DATE:19-DEC-23;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 24/SEP/23.;[03] TOOL USED: SCALE P/N: SPX621 S/NSDR SWAA2023041715654Panel · crackedCRACK ACCESS PANEL 561BB TRAILING EDGE AROUND HOLES LT WING 2023-185220<[01] TOOL USED: CALIPER PN: 500-197-30; SN: B20189416; DUE DATE: 19-DEC-23;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 24/SEP/23.;[03] TOOL USED: SCALE P/N: SPX621 SDR SWAA2023031313383Bracket · crackedRIGHT WING - MIDSPAN BULKHEAD SEAL WEB CRACKED.<[01] REPLACED MIDSPAN BULKHEAD SEAL WEB SUPPORT ANGLE BRACKET. I.A.W. SRM 51-40-02;[02] INSPECTED THE REPLACED MIDSPAN BULKHEAD SEAL WEB SUPPORT ANGLE BRACKET. I.A.W. SRM 51-40-02SDR SWAA2023031313405Tab · brokenLEFT WING DEFLECTION BEAM UPPER SHELF PANEL ATTACH POINT (SERRATED PLATE) BROKEN.<[01] REPAIRED LEFT WING TRAILING EDGE DEFLECTION UPPER TAB PER S/R/M 57-51-02-2R-3 (REPAIR 3)SDR FDEA202303080392Aileron · dentedLH WING AILERON TRAILING EDGE WEDGE UPPER SURFACE FOUND SMALL DENTS COMPLIED WITH EA: 6-5750-T0373267 P1. TITLE: WING - FLIGHT SURFACES - LH AILERON TRAILING EDGE WEDGE UPPER SURFACE REPAIR. AND REFER TO A300-600 SRM51-77-12-201 PARA.4.B FIGURE 218 & AMM57SDR SWAA2023041713702Plate · crackedAFTER REMOVED LEFT WING LOWER INBOARD FIXED TRALING EDGE PANEL #551GB FOUND GIGGLE PLATE AT INNER WING EDGE WITH CRACK<[01] REMOVED; REPLACED AND INSTALLED GIGGLE PLATE AT WING PANEL #551GB.SDR SWAA2023041713697Support · crackedAFTER REMOVED LEFT WING INBOARD LOWER TREALING EDGE PANEL 561AB; FOUND SUPPORT TO ATTACH PANEL WITH 0.500'CRACK AT END AREA<[01] REMOVED AND REPLACED SUPPORT.SDR FDEA202303070645Slat · unknownAGING AIRCRAFT ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON RH WING #3 SLAT NOSE SKIN O/B END. DUE TO NO APPROVED DOCUMENTATION TO SUPPORT THE REPAIR, REMOVED ALL REPAIR PARTS AND PERFORMED NEW REPAIR TO THE AREA I.A.W. EA# T6-5750-T0373565 P1, TITLSDR FDEA202303070631Skin · noneEXISTING FLUSH DOUBLER REPAIR FOUND ON RH WING #3 SLAT NOSE SKIN O/B END. DUE TO NO APPROVED DOCUMENTATION TO SUPPORT THE REPAIR, REMOVED ALL REPAIR PARTS AND PERFORMED NEW REPAIR TO THE AREA I.A.W. EA# T6-5750-T0373565 P1, TITLE: WINGS- FLIGHT SURFACES-RSDR FDEA202303070384Spoiler · delaminatedLH WING 4# SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE & CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATED (1) (S:10MM*15MM D:1.52MM) (2) (S:10MM*15MM D:1.52MM) REPAIRED LH WING 4# SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE DELAMINATION & CENSDR FDEA202303070383Spoiler · delaminatedRH WING #3 SPOILER I/B CENTER HINGE ARM O/B FOUND DELAMINATION. SIZE: 10MM*18MM , DEPTH: 1.59MM. REPAIRED THE RH WING #3 SPOILER I/B CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION PER FEDEX EA: 6-5750-T0373206 P1 & SB A300-57-6082 R03 FIGURE 2 SHEET 2 & 4 SDR SWAA2023032412899Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED ON ACCESS PANEL 651FB AT RT WING 2023-165233<[01] REPLACED SUPPORT BRACKET LOCATED ON ACCESS PANEL 651FB AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2710; SHEET 6; REV: B;[02] REPLACED SUPPORT BRACKET SDR SWAA2023032412558Plate · crackedCRACK TRAILING EDGE CORRUGATED PLATE LOCATED ORSS 261 AT LT WING 2023-165210<[01] REPLACED CORRUGATED PLATE AND LOCATED ON ORSS 261 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 22 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] RESDR FDEA202303030483Aileron · damagedLH WING AILERON UPPER SKIN DEFORMED AT RIB1 & REAR SPAR-17" ACCOMPLISHED THE DOUBLER REPAIR, THIS IS CAT.A REPAIR I.A.W A300-600F SRM 57-61-11-201, PARA.4D, PAGE.213-PAGE.216, FIG.204 MAJOR REPAIRSDR FDEA202303030365Spoiler · delaminatedLH WING #3 SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 40MM*10MM, DEPTH: 1.7MM COMPLIED WITH EA: 6-5750-T0373146 P1. TITLE: WING - FLIGHT SURFACES - LH 3# SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE LH WISDR IPXA2023041592889Filler · crackedINSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 26REPAIRED PER UPS EO A300-5750-86564-A AND FINAL EA 300-5750-27-A3180 REVSDR IPXA2023041592888Plate · crackedINSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 26REPAIRED PER UPS EO A300-5750-86564-A AND FINAL EA 300-5750-27-A3180 REVSDR IPXA2023041592887Doubler · crackedINSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 26REPAIRED PER UPS EO A300-5750-86564-A AND FINAL EA 300-5750-27-A3180 REVSDR IPXA2023041592886Filler · crackedINSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 27REPAIRED PER UPS EO A300-5750-86564-A AND FINAL EA 300-5750-27-A3180 REVSDR IPXA2023041592885Filler · crackedINSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 27REPAIRED PER UPS EO A300-5750-86564-A AND FINAL EA 300-5750-27-A3180 REVSDR IPXA2023041592884Plate · crackedINSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 27REPAIRED PER UPS EO A300-5750-86564-A REVSDR IPXA2023041592883Doubler · crackedINSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 27REPAIRED PER UPS EO A300-5750-86564-A AND FINAL EA 300-5750-27-A3180 REVSDR SIMA20230302002Unknown · unknownRH WING FLAP TRACK 3 UPPER FWD OTBD GUIDE PLATE CRACKED AT SCREW HOLE.-C/A-COMPLETE:REMOVED AND REPLACED THE RH WING FLAP TRACK 3 UPPER FWD OTBD GUIDE PLATE IAW EMB 175 AMM 20-10-01. TORQUE WRENCH #7409
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