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 SWAA2022090941819Angle · crackedCRACK SUPPORT ANGLE AT LEVEL ORSS 282 TRAILING EDGE AT RT WING 2022-427080 / [01] REPLACED SUPPORT ANGLE AND FASTENERS LOC. AT LEVEL ORSS 282 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND B737-700 DWG 115A3700 SHEET 27 REV -.SEE INDIVIDUAL SIGNS-OFF BSDR SWAA2022090941820Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE AT LEVEL ORSS 274 RT WING 2022-427081 / [01] REPLACED SUPPORT BRACKET ON TRAILING EDGE AT LEVEL ORSS 274 AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG #115A2930 SHEET 8 AND REV -. MEASURE OF CRACK IS 0.470'. TOOL USED IS CALSDR VNAA202208149993Slat Track · corrodedPITTING CORROSION ON SLAT TRACKS 1-1, 1-3 UPPER SURFACE & SLAT TRACK 1-2 UPPER/LOWER SURFACE; SLAT #1 LH WINGSDR REXA2022100302163Bracket · wornRIGHT INBOARD FLAP INBD ATTACHMENT BRACKET ON THE INBD HINGE ARM CHAFED FOUND TO BE OUT OF LIMITS IAW CRJ 200 SRM 57-54-00, INSTALLED NEW ATTACHMENT BRACKET P/N: 601R14116-85 CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-45-00SDR SWAA2022090941315Access Panel · crackedCRACK ACCESS PANEL 661BB AROUND FASTENERS HOLES AT RT WING 2022-426980 / [01] TOOL USED CALIPER PN: 500-197-30; SN: 15120589; D/D: 28/NOV/22.;[02] TOOL USED HOT BONDER P/N: HCS9200B; S/N: 16122983; DUE DATE: 16-JAN-23.;[03] TOOL USED SCALE P/N: 91847; S/N: AE-SDR SWAA2022083139530Angle · crackedCRACK SUPPORT ANGLE ON ACCESS PANEL 651GB AT RT WING 2022-418567 / [01] REPLACED SUPPORT ANGLE ON ACCESS PANEL 651GB AT RT WING I.A.W B737-700 SRM 51-10-02 AND SRM 51-40-02; MEASURE OF CRACK ON DAMAGED SUPPORT ANGLE IS: 3.027 INCHES; NOMINAL THICKNESS OF SUPPOSDR SWAA2022083139314Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT RT WING 2022-418557 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT RT IAW B737-700 SRM 51-10-02 AND DRAWING # 115A2781 REV:- . SEE INDIVIDUAL SING-OFF BELOW;[02] REPLACED CORRUGATED PSDR SWAA2022082439030Attach Bracket · crackedAT PANEL 551EB LOCATION; I/B ANGLE SUPPORT FWD ATTACH BRACKET CRACKED; AT LOWER L/W T/E FRONT SPAR CORRECTION -- IS AFT SPAR / [01] REMOVED AND REPLACED PANEL 551EB ANGLE SUPPORT FWD ATTACH BRACKET AT LOWER L/W T/E SPAR REF. SRM 51-40-02-0G-0; AND DRAWING #115SDR SWAA2022083138740Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 204 AT RT WING 2022-418467 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 204 AT RT WING IAW B737-700 SRM 51-10-02 AND DRAWING# 115A2781 REV: -SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED CORRUGATEDSDR P5CA2022072000154Flap · peelingLH W - #9 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)SDR P5CA2022072000155Flap · peelingLHW - #8 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)SDR P5CA2022072000156Flap · peelingLH W - #7 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)SDR SWAA2022082637766Fairing · brokenRT WING T/E PANEL 551FB LOWER I/B END FAIRING IS BROKEN (MARKED) RT WING T/E PANEL 651FB LOWER I/B END FAIRING IS BROKEN (MARKED) / [01] REMOVED AND REPLACED BROKEN LOWER I/B END FAIRING ON PANEL 651FB PER BOEING DRAWING 115A2200. FLAG NOTES 7. AND 8.;[02] REMSDR SWAA2022083137798Angle · crackedCRACK ON SUPPORT ANGLE LOCATED ORSS 261 OF TRAILING EDGE LT WING 2022-418347 / [01] REPLACED SUPPORT ANGLE LOCATED ORSS 261 OF TRAILING EDGE LT WING I.A.W B737-700 SRM 51-10-02 ; SRM 51-40-02;[02] REPLACED SUPPORT ANGLE LOCATED ORSS 261 OF TRAILING EDGE LT WINSDR SWAA2022082637358Support Beam · brokenRT WING T/E PANEL 661AB AFT SUPPORT BEAM IS BROKEN ON I/B END / [01] FOUND NO APPLICABLE SRM REPAIR FOR BROKEN RT WING ACCESS PANEL 661AB AFT SUPPORT BEAM; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9. REMOVED AND INSTALLED NEW SUPPORT BSDR SWAA2022081840978Frame · deterioratedDETERIORATED FLAP TRACK FAIRING CANOE 6 BUSHING FWD O/B SIDE AT RT WING 2022-365957 / [01] INSTALLED NEW FRAME AND FASTENERS ON FLAP TRACK CANOE #6 IAW B737-700 SRM 51-40-02 AND DRAWING 113A9150 SHEET 3 REV.C;[02] REPLACED FRAME AND FASTENERS ON FLAP TRACK CANSDR SWAA2022080135913Bracket · crackedUPPER SHELF PANEL SUPPORT BRACKET INBOARD OF DEFLECTION RIB CRACKED ON RIGHT WING TRAILING EDGE. / [01] REMOVED AND REPLACED BRACKET PER SOPM 20-50-01;[02] C/W INSPECTION.SDR REXA2022091302056Angle · corrodedLEFT WING INTERNAL REAR SPAR TO AUXILIARY SPAR ACCESS PANEL MOUNT FLANGE BELOW FQGC CONNECTOR IS CORRODED REPLACED PARTSDR SWAA2022082935580Panel · elongatedRIGHT WING LWR PANEL 661CB HAS ELONGATED/ CRACKED HOLES. CORRECT PANEL IS 621CB / [01] PERFORMED VISUAL INSPECTION AND TAP-TEST INSPECTION AT ACCESS PANEL 661CB; ELONGATED HOLES FOUND; NO WATER NOTE AND NO DELAMINATION FOUND. REF B737-700 SRM 51-70-04-2R-9 PARSDR REXA2022081201864Panel · chafedLHIB FLAP PANEL 584GB CHAFED. BLENDED CHAFE, DIMENSIONS AS FOLLOWS. 2.0" X 1.0" X .027" DEEP REMOVED AND REPLACED ACCESS PANEL 584GB.SDR IXXA202272810Wing Root · corrodedLEFT WING ABOVE MAIN LANDING GEAR ACTUATOR ATTACHMENT POINT SS267 CORROSION UNDER NUTPLATES.SDR UIEA2022072100769Beam · corrodedAGING A/C INSP - AREAS OF MINOR CORROSION ON THE RH WING T/E CLOSE OUT PANEL ATTACH ANGLE BETWEEN THE O/B FAIRINGS, MULTIPLE AREAS ALONG THE ANGLE (CORROSION FOUND IN MULTIPLE AREAS AROUND NUTPLATES MEASURING 1.0"L X 1.0" W X .015" D ALONG FULL LENGTH OF BEAM.SDR REXA2022081201856Panel · chafedLHIB FLAP PANEL 584EB CHAFED. BLENDED CHAFE, DIMENSIONS AS FOLLOWS. 3.0" X 1.5" X .042" DEEP REMOVED AND REPLACED ACCESS PANEL 584EB.SDR SWAA2022080830803Fairing · delaminated#6 FLAP TRACK AFT FAIRING HAS DELAMINATED AREA AT O/B SIDE / [01] IDENTIFIED #6 AFT FLAP TRACK FAIRING PANEL 642BB IAW SRM 57-53-70-0I-3 FIGURE 1-2; 4 AND 14; ITEM 1; TABLE 3 AND 12<BR><BR>DAMAGE IS OUT OF ALLOWABLE LIMITS IAW SRM 57-53-70-1A-1 FIGURE 101 AND SDR SWAA2022081629990Plate · crackedCRACK PLATE ASSY REAR SPAR LOCATED IRSS 215 APPROX AT RT WING 2022-368386 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N:A21043226; DUE DATE: 10-AUG-22.;[02] REPLACED PLATE ASSY AND FASTENERS REAR SPAR LOCATED IRSS 215 APPROX AT RT WING IAW B737-700 SRSDR SWAA2022081629995Plate · crackedCRACK PLATE ASSY REAR SPAR LOCATED ORSS 270 APPROX AT RT WING 2022-368388 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-752-20; S/N: B21038254; DUE DATE: 11-AUG-22;[02] REPLACED PLATE ASSY AND FASTENERS LOCATED REAR SPAR LOCATED ORSS 270 APPROX AT RT WING IAW B73SDR SWAA2022081629996Plate · crackedCRACK PLATE ASSY REAR SPAR IRSS 245 APPROX AT RT WING 2022-368390 / [01] TOOL USED DIGITAL CALIPER P/N:500-752-20. S/N:B21038254 DUE DATE:11/AUG/22;[02] REPLACED PLATE ASSY REAR SPAR IRSS 245 APPROX AT RT WING IAW B737-700 SRM 51-40-02 AND DWG # 115A2781 REV: SDR SWAA2022081629986Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 280 APPROX LT WING 2022-368360 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-752-20; S/N: B21038254; DUE DATE: 11-AUG-22.;[02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 280 APPROX LT WING IAW B737-700 SRM 51-10-02; SRM 51-40SDR SWAA2022081729688Angle · crackedCRACK ANGLE TRAILING EDGE DEFLECTION CONTROL RIB LOCATED ORSS 278 AT RT WING 2022-368300 / [01] REPLACED ANGLE TRAILING EDGE DEFLECTION CONTROL RIB LOCATED ORSS 278 AT RT WING IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A6200 SHEET 7 REV:A;[02] SDR SWAA2022072929573Plate · crackedMICARTA 'WIGGLE PLATE' I/B OF #7 FLAPTRACK AND COMMON TO WING TRAILING EDGE PANEL 661AB IS CRACKED. / [01] R&R WIGGLE PLATE PER SRM 51-10-02;[02] C/W INSPECTION.SDR REXA2022072001617Panel · wornRH WING PANEL 684DT WORN. EVALUATED AND REPLACED PANEL PER CRJ200 SRM 57-52-00.SDR SWAA2022071828193Support Bracket · crackedRIGHT WING LOWER SHELF PANEL INBOARD SUPPORT BRACKET IS CRACKED. UNDER #8 SPOILER. / [01] REMOVED AND REPLACED RIGHT WING LOWER SHELF PANEL INBOARD SUPPORT BRACKET UNDER #8 SPOILER PER AMM 20-50-11 AND SRM 51-40-02.SDR FDEA202207131713None · delaminatedLH WING 5# SPOILER O/B HINGE ARM O/B END FOUND DELAMINATION SIZE:80MM X 25MM X 1.45MM PERFORMED THE REPAIR ON LH WING 5# SPOILER O/B HINGE ARM O/B END AS PER FEDEX EA # : 6-5750-T0315012 A P2 TITLE: WING - FLIGHT SURFACES - LH WING 5# SPOILER LOWER SURFSDR FDEA202207111707None · delaminatedLH WING 3# SPOILER O/B HINGE LOW SURFACE FOUND DELAMINATION SIZE:20MM X 10MM X 1.6MM PERFORMED THE REPAIR ON LH WING 3# SPOILER O/B HINGE AS PER FEDEX EA # : 6-5750- T0369055 P1 TITLE: WING - FLIGHT SURFACES - LH 3# SPOILER CENTER HINGE ARM LOWER SURFACESDR SWAA2022072527641Bracket · crackedRIGHT WING I/B TE/ LOWER ACCESS PANEL #651FB O/B INNER BRACKET WITH .500' CRACKED AT RADIUS AREA (MKD) / [01] CERTIFIED;[02] REMOVED AND REPLACED BRACKED AS PER B-737-700 SR # 51-40-02-OG-0;[03] VERIFIED STEP #2.SDR SWAA2022080227373Plate · crackedCRACK REAR SPAR CORRUGATED PLATE LOCATED BETWEEN WS204 TO WS228 AT LT WING 2022-373088 / [01] REPLACED REAR SPAR CORRUGATED PLATE LOCATED BETWEEN WS204 TO WS228 AT LT WING I.A.W. B737-700 DWG 115A2001 REV: A AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN-OFF BELSDR SWAA2022080227374Plate · crackedCRACK REAR SPAR CORRUGATED PLATE LOCATED BETWEEN WS228 TO WS253 AT RT WING 2022-373087 / [01] REPLACED CORRUGATED PLATE LOCATED BETWEEN WS 228 TO WS 253 AT RT WING IAW SRM B737-700 51-40-02 AND DRAWING 115A2001 REV:-;[02] REPLACED CORRUGATED PLATE LOCATED BETWSDR SWAA2022080227375Bracket · crackedCRACK REAR SPAR ON SUPPOR BRACKET LOCATED IRSS270 AT RT WING 2022-373086 / [01] REPLACED SUPPOR BRACKET AND FASTENERS LOCATED ORSS270 AT RT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPOR BRACKET SDR SWAA2022072927398Plate · crackedTHE WAFFLE PLATE JUST OB OF PANEL 651DB IS LOOSE AND CRACKED. / [01] REMOVED AND REPLACED WAFFLE PLATE PER SRM 51-40-02 AND RESTORED FINISH PER AMM 51-21-99.;[02] INSPECTED THE WORK PERFORMED ON C/A #1; NO DEFECTS NOTED.SDR SWAA2022072931435Panel · elongatedPANEL 661BB HAS SEVERAL FASTENER HOLES ELONGATED AND CRACKED (MARKED) / [01] REPAIRED FASTENER HOLE PER SRM 51-70-04-2R REPAIR #9.;[02] INSPECTED REPAIRED FASTENER HOLES;[03] REPAIRED PER SRM 51-70-04-2R-9 REPAIR #9; RESTORED FINISH PER M/M 51-21-99.SDR REXA2022072801703Panel · chafedRHIB FLAP PANEL 684GB CHAFED, BLENDED CHAFE DIMENSIONS AS FOLLOWS, 2.5" X 1.0" X .030" DEEP. REMOVED AND REPLACED PANELSDR REXA2022072801686Panel · wornRHIB FLAP PANEL 684EB CHAFED, BLENDED CHAFE DIMENSIONS AS FOLLOWS, 2.5" X 1.5" X .021" DEEP. REMOVED AND REPLACED PANELSDR REXA2022072701685Panel · wornRHIB FLAP VANE ACCESS PANEL 684FT CHAFED. BLENDED CHAFE DIMENSIONS AS FOLLOWS 3.0" X 1.5" X .021" DEEP. REMOVED AND REPLACED ACCESS PANEL 684FT.SDR REXA2022072701684Panel · wornRHIB FLAP VANE ACCESS PANEL 684GT CHAFED. BLENDED CHAFE DIMENSIONS AS FOLLOWS 3.0" X 1.25" X .018" DEEP. REMOVED AND REPLACED ACCESS PANEL 684GT.SDR REXA2022071301557Panel · chafedPANEL 584ET IS CHAFED. RECEIVED LOCATED AND DRILLED NEW PANEL ASSY, VANE ACCESS, FLAP INBD. PN#CC670-140027-3. REF CRJ900 SRM 51-40-11-001-001-A01.SDR SWAA2022080426753Bracket · elongatedELONGATED HOLE ON SUPPORT BRACKET LOCATED ORSS 251 AT LT WING 2022-398199 / [01] REPLACED SUPPORT BRACKET LOCATED ORSS 251 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] TASK COMPLETEDSDR SWAA2022080426731Plate · crackedCRACK ON CORRUGATE PLATE LOCATED ORSS 261 OF TRAILING EDGE RT WING 2022-355183 / [01] REPLACED CORRUGATE PLATE AND FASTENERS LOCATED ORSS 261 OF TRAILING EDGE RT WING IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9; AND B737-700 DWG 115A2001 SHEET 29 RSDR SWAA2022071126407Panel · crackedRT WING FIXED TE PANEL FITTING CRACKED AT APPR WS 278.5 / [01] R&R PANEL AS PER SRM 51-40-02SDR SWAA2022082226423Fairing · crackedL/W FLAP TRACK FAIRING 543BB HAS CRACK ON FWD EDGE / [01] IDENTIFIED L/W FLAP TRACK FAIRING 543BB IAW SRM 57-53-70-0I-2 FIGURE 4; SHEET 1; TABLE 3; ITEM 1. <BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-53-70-1A-1 PAR 4B(2).<BR><BR>REPAIR TOSDR SWAA2022080425884Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED ON ORSS 273 OF TRAILING EDGE AT RT WING 2022-354692 / [01] REPLACED SUPPORT BRACKET LOCATED ON ORSS 273 OF TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.;[02] CORRECTED STEP 1 REPLACED SUPPORT BRACK
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