JASC 5720
Service difficulty reports · 13,638
Reports filed under 5720 · Wing Miscellaneous Structure, 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 = '5720' 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 = '5720' 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 IPXA2020022652470Stiffener · crackedINSPECTION TYPE:SEGR/H WING ACCESS PANEL 613AB LANDING HAS CRACKREPAIRED IAW SRM 53-15-63 FIG. 201SDR SWAA2020021984150Plate · crackedL/H WING TRAILING EDGE WIGGLE P LATTE AT IRSS. 216 CRACKED. / R&R WIGGLE PLATE IAW SRM.SDR HALA2020021000032Insert · missingRIGHT WING NUT PLATE INSERT MISSING AT WING FWD SPAR OUTBOARD OF # 1 SLAT TRACK. // REMOVED AND REPLACED NUT PLATE, REF. A330 SRM 51-42-11.SDR SWAA2021082094315Support · crackedLEFT WING TRAILING EDGE PANEL SUPPORT CRACKED RSS 288 WL 200. / REPLACED CRACKED LEFT WING TRAILING EDGE PANEL SUPPORT AT RSS 288 WL 200 IAW SRM 51-40-02; SRM 51-40-05 AND IPC 57-50-00-17SDR SWAA2021060918750Attach Angle · brokenSHELF PANEL NUTPLATE BEAM ATTACH CLIP ON AFT SPAR OF RIGHT WING AT STA. 220 BROKEN. / R&R'D CLIP (MPN #115A5552U2) IAW SRM 51-40-02.SDR SWAA2020021941466Plate · crackedR/H WING TRAILING EDGE WIGGLE PLATE CRACKED JUST OUTBOARD OF PANEL 651DB / R&R WIGGLE PLATE IAW SRM & DWG.SDR ABXA2020021409027Support · corrodedLH WING, TE, WS 870, UPPER DECK SUPPORT CORRODED. THE AIRPLANE WAS GROUNDED.SDR ABXA2020021409026Bracket · corrodedBRACKET CORRODED ABOVE RH MLG FWD TRUNNION. THE AIRPLANE WAS GROUNDED.SDR CALA2020021200394Fitting · crackedSHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540, RBL 40.87. IAW B7 37 700. SRM 51-60-02 AND DWG NO. 111A 2000. SSFR REPORT, FORM 46 -0024, ENTERED BY UAL INSPECTIONU241010, 2/8/2020 INSPECTION ACCEPTEDSDR EE4Y2020020710630Angle · crackedRH WING, TRAILING EDGE CAVITY ANGLE WITH CRACK AT WBL 449.5. NOTE: THE TRAILING EDGE ANGLE WAS REPLACED AS PER B737-300 SRM INSTRUCTIONS. (REF: JOB: A1H267 ITEM: 6-6).SDR SWAA2021081713691Bracket · crackedLT. WING T/E PANEL 551GB T/E BRACKET CRACKED. (MARKED) / REMOVED AND REPLACED T/E BRACKET ON PANEL 551GB IAW SOPM 20-50-01 59675U 02/11/20SDR SWAA2021072122768Stiffener · crackedLEFT MLG WHEEL WELL STA 663 LBL28 WL 148; VERTICAL STIFFENER IS CRACKED. / REMOVED AND REPLACE LH MLG WHEEL WELL STA 663 LBL 28 WL 148 VERTICAL STIFFENER IAW SRM 51-40-02-0G-0 & 51-40-05-0G-0 & DWG 111A100 REV -SDR SWIA2020032649357Angle · cracked* R/H BATT RIB AT WS48.30 TOP ANGLE IS CRACKED, MARKED IN RED. (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED NEW R/H BATT RIB AT WS48.30 TOP ANGLE P/N 600-10389-2 REF BOMBARDIER DWG AND CRJ200 SRM. RESTORED FINISH CRJ200 SRM.SDR SWIA2020032649356Angle · cracked* L/H BATT RIB AT WS48.30, TOP ANGLE IS CRACKED, MARKED IN RED. (C-CHECK) RO 3/25/2020 REMOVED CRACKED LH BATT RIB TOP AFT ANGLE AND REPLACED WITH NEW L/H BATT RIB TOP AFT ANGLE AT WS.48.30 WITH NEW FASTENERS PER CRJ200 SRM AND BOMBARD. DWG. COMPLIED WISDR SWIA2020031049248Bracket · crackedCONNECTING BRACKET/BRIDGE FOR CANOE PANEL 697AB IS CRACKED. (C CHECK) RO 3/7/2020 INSTALLED NEW CONNECTING BRACKET TO CANOE PANEL # 697AB AS REQUIRED PER REF: CRJ200 SRM.SDR REXA2020020100153Strap · damagedWHILE INCORPORATING SB 670BA-57-020, FOUND 4 EA 2ND OVERSIZE FASTENERS IN THE COLD WORK ZONE. (HST254). ON LH WING PLANK STRAP. REPAIRED LH WING PLANK OVERSIZE FASTENERS IAW REO 690-57-21-341 REV--DATED 2020-01-30.SDR SWAA2021052509352Bracket · crackedLEFT WING MLG CONDUIT GUIDE BRACKET HAS CRACK IN RADIUS. LOCATED JUST OTBD OF AFT TRUNNION BEARING AND TOWARD TOP OF WING SURFACE. MARKED. / REMOVED & REPLACED CONDUIT GUIDE BRACKET ABOVE LEFT MLG JUST OTBD OF AFT TRUNNION BEARING AND TOWARD TOP OF WING SURFACSDR RAIA2020021630003Bracket · crackedR/H L/E #1 HORSE SHOE BRACKET IS CRACKED............... REMOVED AND REPLACED R/H #1HORSE SHOE BRACKETSDR REXA202002123200Skin · corrodedLH WING LOWER WING PLANK ACCESS HOLE CORRODED UNDER PANEL 540BB
REPAIRED WING PLANK HOLE 540BB IAW REO 601R-57-21-030 REV L. WVAC STAMP EMP# 717 MTCSDR SWIA2020031649275Angle · cracked*LH WING BATT RIB WS48.30 IN MLG WELL, UPPER WEB ANGLE CRACKED (MARKED) (C-CHECK) RO 3/13/2020 REMOVED AND REPLACED DAMAGED ANGLE (P/N 601R10204-33) AT LH WING BATT RIB WS48.30 IN MLG WELL REF DWG CRJ200 SRM. COMPLIED WITH TASK CARD.SDR SWIA2020031649274Angle · cracked*LH WING BATT RIB WS48.30 IN MLG WELL, CAP CRACKED (MARKED) (C-CHECK) RO 3/13/2020 REMOVED AND REPLACED CAP ANGLE AT LH WING BATT RIB WS48.30 REF CRJ-200 SRM, BOMBARDIER DWG , COMPLIED WITH SKYWEST TASK CARDSDR SWIA2020031649273Angle · cracked* RIGHT WING BATT RIB WS53.6 ANGLE IS CRACKED IN THE RADIUS OF THE UPPER CORNER. (MARKED) (C-CHECK) RO 3/13/2020 REMOVED AND INSTALLED NEW RIGHT WING BATT RIB @ WS53.6. REF CRJ200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD. ALL CHECKS GOOD.SDR SWAA2020013140950Plate · crackedLT WING REAR SPAR LOWER CHORD 10" INBOARD OF #3 FLAP TRACK WIGGLE PLATE HAD EVIDENCE OF A CRACK AT FASTENER HOLE. R&R WIGGLE PLATE IAW SRM.SDR IPXA2020012981504Support · crackedINSPECTION TYPE:SEG, LT WING T/E RIN WEB OTBD OF NR 4 SPOILER CRACKED AT FWD L ATTACHMENT. R&R THE SUPPORT IAW SRM 51-40-11 & SRM 51-40-21.SDR SWAA2020012940871Plate · crackedLT WING TRAILING EDGE PANEL 551GB WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM & DWG.SDR COEA2020032617801Fitting · corrodedWO 209330 NR 600051 HEAVY CHECK COE/MAJOR REPAIR: R/H LOWER WING AT JUNCTION RIB 13 BOLT HOLE #14 OB SPOT FACE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0114756_01...16108 ISSUE A, DATED 3/20/2020.SDR SWAA2021081320125Angle · crackedLT WING SEAL ANGLE FWD OF TRANSVERSE WEB ABOVE AFT STRUT FAIRING TIP IS CRACKED / REMOVED AND REPLACED LT WING SEAL ANGLE FWD OF TRANSVERSE WEB ABOVE AFT STRUT FAIRING IAW SRM 51-40-02-0G-0 84036U 23JAN20SDR SWAA2021081917967Bracket · crackedLT WING; STABILIZER LINK BRAKET CRACK AT FWD SIDE STABILIZER ACCESS PANEL 551 AT / REMOVED AND REPLACED LT. WING STABILIZER LINK BRACKET REF SRM 51-40-02SDR SWAA2021081927445Stiffener · crackedL/H WING O/B FIXED L/E; INTERNAL STRUCTURE; FOUND STIFFENER WITH CRACKED TAB / REMOVED AND REPLACED L/H WING O/B FIXED L/E; INTERNAL STIFFENER P/N 116A4530-1 IAW DRAWING 11619 4008 REV A AND SRM 51-40-02-0G-0. REMOVED AND REINSTALLED ACCESS PANEL 511AB IAW AMMSDR IPXA2020030952867Angle · crackedINSPECTION TYPE:A300RH WING ANGLE CRACKED UPPER FIXED PANEL OUTBRD OF AND FORWARD OF#3 SPOILER ATTACH POINTREMOVED CRACKED ANGLE @ RH WING UPPER FIXED PANEL IAW A300 SRM 51-40-21 INSTALLED NEW ANGLE PN A572400 7120100 IAW A300 SRM 51-40-21SDR SWAA2020012240653Stiffener · crackedL/H WING OUTBOARD FIXED LEADING EDGE, INTERNAL STRUCTURE, FOUND STIFFENER WITH CRACKED TAB. / R&R STIFFENER IAW DWG, AMM, AND SRM.SDR A6WA2020011647111Angle · crackedO/B ANGLE P/N 600-12045-12, ON RIGHT WING AT PANEL 620ML, IS CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ANGLE IAW SRM 51-41-02.SDR SWIA2020030348953Angle · cracked*RH MLG WELL BATT RIB AT APPROXIMATELY WS53.00 RH POSSIBLE CRACK UPPER SMALL ANGLE (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED RH MLG WELL BATT RIB ANGLE AT APPROX. WS 53.00 (P/N 601R10202-25) REF DWG, CRJ200 SRM. COMPLIED WITH TASK CARD.SDR SWIA2020030348952Angle · cracked*LH MLG WELL BATT RIB AT APPROXIMATELY WS53.00 LH POSSIBLE CRACK UPPER SMALL ANGLE ON FWD SIDE (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED DAMAGED ANGLE AT APPROXIMATELY LH WS53.00 REF DWG AND CRJ200 SRM. COMPLIED WITH TASK CARD.SDR DALA2020011500302Shim · migratedMIGRATED SHIMS 1B AND 1D (2EA), ON OUTBOARD ENG DRAG FITTING AT RT WING. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV. ORIGINAL. SECTION I: PERMANENT REPAIR.SDR RAIA2020012412009Support Bracket · crackedLH W/W FWD O/B CORNER @ WING T/E NUTPLATE 'L'ANGLE SUPPORT BRACKET IS CRACKED- REMOVED CRACKED SECTION OF THE LH W/W O/B CORNER BELLY FAIRING ATTACH ANGLE & INSTALLED REPAIR. NUTPLATES NEED TO BE LOCATED & INSTALLED. LOCATED NUTPLATES AND INSTALLED ONSDR DALA2020011500301Fitting · scratchedSCRATCHES ON HOLES 1, 2, 3, 6, 7, 8, 9 LOCATED ON RT ENG DRAG FTG CLAMP-UP & DIAG BRACE. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV. ORIGINAL. SECTION I: PERMANENT REPAIR. AND ETI-57-19-201 REV. 10.SDR DALA2020011500300Fitting · corrodedSEVERAL POINTS OF FRETTING CORROSION WERE FOUND ON FRONT SPAR SETTLEMENT AREA OF INBOARD AND OUTBOARD ENG DRAG FITTINGS AT RT WING IN REF ETI-57-19-201 REV. 4 STEP 23. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV. ORIGINAL. SECTION I: PERMANENT REPAIR SDR DALA2020011500299Fitting · corrodedSEVERAL POINTS OF FRETTING CORROSION WERE FOUND ON OUTBOARD ENG DRAG FITTING AT RT WING IN REF ETI-57-19-201 REV. 4 STEP 23 (AD). CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV. ORIGINAL. SECTION I: PERMANENT REPAIR. AND ETI-57-19-201 REV. 10.SDR DALA2020011500298Fitting · corrodedSEVERAL POINTS OF FRETTING CORROSION WAS FOUND ON INBOARD ENG DRAG FITTING AT RT WING IN REF ETI-57-19-201 REV 4 STEP 23. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV ORIGINAL. SECTION I: PERMANENT REPAIR. AND ETI-57-19-201 REV. 10.SDR DALA2020011500293Fastener · looseLOOSE FASTENERS NR 4, 5, AND 10, ON RT ENG DRAG FITTING (AD). CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV ORIGINAL. SECTION I: PERMANENT REPAIR. AND ETI-57-19-201 REV 10.SDR DALA2020011400269Fitting · damagedCORROSION: ELONGATED HOLES WAS FOUND ON OUTBOARD ENG DRAG FITTING, OUTBD HOLES TO ATTACH FITTING TO DRAG FITTING AT RT WING IN REF ETI-57-19-201 REV 4 STEP 23. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV ORIGINAL. SECTION I: PERMANENT REPAIR, AND ETI-SDR DALA2020011400266Fitting · corrodedHIDDEN CORROSION: NICKS WAS FOUND ON COUNTERSINK AREA OF FITTING, LOWER HOLES TO ATTACH FITTING TO FRONT SPAR AT RT WING. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV ORIGINAL. SECTION I: PERMANENT REPAIR AND ETI-57-19-201 REV 10.SDR DALA2020011400265Fastener · looseLOOSE FASTENERS NR 15, ON RT ENG DRAG FITTING. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV. ORIGINAL. SECTION I, PERMANENT REPAIR AND ETI-57-19-201 REV 10.SDR SWAA2021081301959Angle · crackedR/H UPPER WING PANEL ABOVE GEAR I/B FWD SUPPORT BEAM FWD ATTACH '2' ANGLE IS CRACKED / REMOVED AND REPLACED RH MLG UPPER WING PANEL I/B FWD SUPPORT BEAM FWD ATTACH '2' ANGLE PER SRM 51-40-02SDR SWAA2020109925874Support Bracket · crackedLEFT WING T/E ABOVE PYLON SAIL TAIL; UPPER SEAL SUPPORT BRACKET IS CRACKED. / REMOVED & REPLACED LEFT WING T/E ABOVE PYLON SAIL TAIL; UPPER SEAL SUPPORT BRACKET IAW SRM 51-40-02-0G-0 & AIPC 57-50-0-25 A TAG: A95950SDR SWAA2020012040519Plate · crackedLT WING TRAILING EDGE PANEL WIGGLE PLATE CRACKED ATA IRSS 218. R&R WIGGLE PLATE PER SRM.SDR VNAA2020010981101Panel · missingPANEL 642BT MISSING FROM A/C. INSTALLED R/H MLG DOWN-LOCK ACTUATOR PANEL 642BT IAW CRJ 900 AMM.SDR AALA202001079013Sealant · deterioratedAIRCRAFT WAS GROUNDED: FUEL LEAKING FROM LEFT INBOARD WING. CLEANED AND RESEALED LT INBD FWD SPAR PER SRM 51-76-12. SUPPLEMENTAL ACTION: SECT. 3, TT/TC.SDR SWAA2020011440464Plate · crackedRT WING TRAILING EDGE FLAP WELL LOWER INSPAR SKIN WIGGLE PLATE CRACKED BETWEEN RSS 270 TO RSS 276. R&R WIGGLE PLATE IAW DWG & SRM.
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