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 K11A2008121672009Stiffener · crackedRT WING FRONT SPAR VERTICAL STIFFENER CRACKED.SDR IXXA07SMN268SSupport · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE INTERNAL PART SUPPORT CRACKED AT STATION XFS 430.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SUPPORT. FABRICATED SUPPORT CLEANED, TREATED AND PRIMED AREA AND NEWSDR KCSA071522Angle · corrodedRIGHT WING L/E CAVITY I/B OF FS-1318 HAS CORROSION ON ANGLE AT L/E WEB DOUBLER LOWER AT ATTACH POINT.SDR 07FDEA04769Support · crackedHFEC OPEN HOLE INSPECTION CARRIED OUT FOUND 1 EACH HOLE CRACK AT LEFT WING OUTBOARD FLAP HINGE LOWER OUTBOARD HOLE SUPPORT COMMON TO THE ARC4008 SUPPORT. REMOVED AND REPLACED AS PER AMM 27-50-30-4. OUTBOARD FLAP VANE ADJUSTMENT CARRIED OUT AS PER AMM 27-50SDR 07FDEA04768Support · crackedHFEC OPEN HOLE INSPECTION CARRIED OUT FOUND 1 HOLE CRACK AT RIGHT WING OUTBOARD FLAP HINGE SUPPORT LOWER OUTBOARD HOLE COMMON TO THE ARC4008 SUPPORT AND ARC4009. REMOVED AND REPLACED AS PER AMM 27-50-30-4. OUTBOARD FLAP VANE ADJUSTMENT CARRIED OUT AS PER ASDR 07FDEA04743Angle · crackedLT OTBD AILERON BAY BAFFLE SEAL IS CRACKED AT INBD ANGLE (MKD) TO FASTENER HOLE REMOVED AND REPLACED AILERON BAY BAFFLE ANGLE REF DWG 65-19289 AND SRM 51-30-2. APPLIED PN FX 65-19289-17 REF FED EX GMM 7-0-1001.SDR 07FDEA04718Fitting · crackedFOUND ON LOWER JUNCTION FITTING LT CENTER TANK, INTERNAL, SEVERAL HOLES WITH CRACK FINDINGS. REPAIR PERFORMED BY REAM UP UNTIL DAMAGE REMOVAL IAW EA 6-5710-114908 AND RAS/054537/070/2007 ISS A.SDR 07FDEA04717Fitting · crackedFOUND ON LOWER JUNCTION FITTING CENTER TANK INTERNAL SEVERAL HOLES WITH CRACK FINDINGS REPAIR PERFORMED BY REAM UP UNTIL DAMAGE REMOVAL IAW EA 6-5710-114908 AND RAS/054537/070/2007 ISS A.SDR 07FDEA04701Duct · crackedLT WING, LEADING EDGE UPPER SURFACE TELESCOPING DUCT CUTOUT I/B AND O/B CORNERS FOUND CRACK. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-116509, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 5700Stiffener · corrodedLEFT WING REAR SPAR VERTICAL STIFFENER CORRODED AT LOWER END W.S. 200SDR TRAX200701599Plate · crackedLEFT WING BOX FR 28, FACE PLATE CRACKED. LT WING BOX FR 28 FACE PLATE REPLACED IAW SRM 51-25-01.SDR TRAX200701560Plate · crackedRIGHT WING BOX FR 28A FACE PLATE CRACKED. REPLACED IAW SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01.SDR TRAX200701559Angle · crackedRIGHT WING BOX FR 28A ANGLE CRACKED.SDR TRAX200701550Nut · brokenLEFT WING AND RIGHT WING 3 ANCHOR NUT FOR BUTTE DOOR (594SB, 594PB, 694LB) BROKEN.SDR HYIA12140Support Bracket · corrodedRUDDER SPRING TAB LEVER SUPPORT ASSEMBLY CORRODED. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IN ACCORDANCE WITH SRM.SDR HNAA0700242Plate · crackedCRACK AT FORWARD INBOARD CORNER OF LADDER PLATE ON PANEL 522AT WAS FOUND DURING INSPECTION. REPAIRED IAW EO 8-57-07-0242.SDR TRAX200701518Hinge Fitting · crackedLT MFS HINGE FITTING OUTBOARD AT WS 216.95 CRACKED. 10-29-07 R & R LT MFS FITTING IAW CRJ 700 SB 670-BA-57-010. REMOVED BUTTE DOORS FROM LT WING. BEGAN REMOVING HINGE FITTING IAW BOMBARDIER SB 70BA-57-010. INSTALLED LT WING MFS PCU PER CRJ 700 AMM 27-62-SDR 07FDEA04639Retainer · crackedRIGHT WING LOWER TRAILING EDGE PANEL JUST BELOW NR 11 FLIGHT SPOILER ACTUATOR BULB SEAL RETAINER CRACKED. REPLACED SEAL RETAINER REF 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR MASA200700701Shroud · looseFOUND 1 MISSING RIVET ON RT WING OUTBOARD MFS SHROUD FITTING AT WING STATION 231.23. PERFORMED PERM REPAIR.SDR CA071015003Bracket · cracked(CAN) DURING THE ACCOMPLISHEMENT OF A PRE CHECK, A SPACE WAS OBSERVED BETWEEN THE SPOILER ACTUATOR AND THE SPOILER ACTUATOR BRACKET. FURTHER INVESTIGATION FOUND THAT THE BRACKET WAS CRACKED. (TC NR 20071015003)SDR USAA920071114Structure · crackedCLT - MAJOR REPAIR - C16 CHECK, RIGHT WING LOWER WING CHORD CRACKED, WS 135.5. REPAIRED RIGHT WING LOWER CHORD, WS 135.5 IAW USAIRWAYS EA 98943.SDR 2007UALA04215Support Fitting · damagedFUEL LEAKING AT AFT SPAR JUST OUTBOARD OF LEFT MAIN GEAR, FROM UPPER REAR SPAR CHORD REINFORCEMENT DOUBLER LOCK FASTENER. BEAM LEFT SUPPORT FITTING HAS 6 ELONGATED HOLES IN UPPER SKIN.SDR 07FDEA04575Intercostal · crackedMD10 TO ACF MODIFICATION FOUND RT WING TRAILING EDGE LOWER SIDE STA XORS 241 ABOUT INTERCOSTAL WITH CRACK. REPLACED INTERCOSTAL FOR SRM 51-35-01.SDR COEA0735821Shim · corrodedFOUND DURING HEAVY CHECK. MAJOR REPAIR. CORROSION ON RT WING UPPER SPAR SHIM, REPLACED SHIM WITH NEW MACHINED SHIM. WO 72241, NR 602033. (K)SDR 07FDEA04534Plate · delaminatedDELAMINATION ON LT WING OUTER SHROUD BOX FLAP DEFLECTOR PLATE, AROUND THE ROLLER SUPPORT. REPAIR PERFORMED BY REMOVING DAMAGED PLIES AND INSTALLING REPAIR PLIES USING PRINCIPLES OF SRM 51-77-12/PARA.2A(3), ALL IAW EA 6-5755-106530 AND RAS/BAE/1005093/2007 ISSSDR 07FDEA04500Plate · delaminatedFOUND DELAMINATION ON LT WING INNER SHROUD BOX DEFLECTOR PLATE AROUND ROLLER SUPPORT REPAIR PERFORMED BY BONDING REPAIR IAW EA 6-5755-112536 AND RAS//BAE/1005280/2007 ISS A.SDR 07FDEA04480Channel · crackedTHE RT AFT WING TIP SECTION HAS A BROKEN NUT PLATE CHANNEL IN THE LOWER AFT END. THIS DISCREPANCY WAS FOUND DURING A "B" CHECK. REPAIRED NUTPLATE CHANNEL PER EA NR 7-5730-115028SDR 07FDEA04444Fitting · corrodedFOUND AT C47 INTERNAL CENTER WING RT VERTICAL FLANGE FITTING HOLE NR U, NR I AND NR H WITH CORROSION. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CORROSION REMOVAL IAW EA 6-5710-106533 AND RAS 052780/019/2007 ISS A.SDR 07FDEA04443Fitting · corrodedFOUND AT C47 INTERNAL CENTER WING RT VERTICAL FLANGE FITTING HOLE NR A, NR E, NR F, NR G, NR P, NR Q AND NR S WITH CORROSION. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CORROSION REMOVAL IAW EA 6-5710-106533 AND RAS 052780/019/2007 ISS A.SDR 07FDEA04442Fitting · corrodedFOUND AT C47 INTERNAL CENTER WING LT VERTICAL FLANGE HOLE NR G, NR S AND NR T WITH CORROSION. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CORROSION REMOVAL IAW EA 6-5710-106533 AND RAS 052780/019/2007 ISS A.SDR 07FDEA04441Fitting · corrodedFOUND AT C47 INTERNAL CENTER WING LT VERTICAL FLANGE HOLE NR I AND NR U WITH CORROSION. REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVAL AND CUT EXTERNAL FITTING AT HOLE NR I IAW SB 57-6049 IAW EA 6-5710-106533 AND RAS 052780/019/2007 ISS A.SDR 07FDEA04375Angle · crackedLT WING FIXED LEADING EDGE, XOS 602, LOWER ANGLE FOUND CRACKED. 10-9-07 REMOVED ANGLE AS PER SRM 51-33-01 VOLUME II AND FABRICATED NEW ANGLE DOUBLER AS PER DRAWING ARB 2933. INSTALLED NEW ANGLE DOUBLER AT LT WING FIXED LEADING EDGE , XOS 602, LOWERSDR 07FDEA04374Support Bracket · crackedLEFT WING FIXED LEADING EDGE, XORS 542 (OUTBOARD OF ACCESS PANEL 518FB), LOWER LONGITUDINAL SUPPORT BRACKET FOUND CRACKED. 10-16-07 CRACKED SUPPORT BRACKET AT LT WING FIXED LEADING EDGE XOS 542 (OUTBOARD OF ACCESS PANEL 518FB) LOWER AREA REMOVED AND RSDR SIMA200727402Fairing · looseNOISE FROM UNDER FLOOR AT ROWS 11 - 13/VIBE HEARD IN COCKPIT AND FELT IN YOKE. WHILE PERFORMING VIBRATION INSPECTION WC 05-005 FOUND LEFT AND RIGHT FLAP STAB FAIRINGS LOOSE. RESECURED LEFT AND RIGHT FLAP STAB FAIRINGS IAW CRJ AMM 53-82-82. C/W VIBRATION WORSDR 07FDEA04358Plate · crackedFOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 7, FWD OF FRONT SPAR, UPPER SKIN, RT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 7 RT IAW SRM 51-72-10.SDR 07FDEA04357Plate · crackedFOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 7, FWD OF FRONT SPAR, UPPER SKIN, LT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 7 LT IAW SRM 51-72-10.SDR 07FDEA04356Plate · crackedFOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 6, FWD OF FRONT SPAR, UPPER SKIN, LT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 6 LT IAW SRM 51-72-10.SDR TRAX200701445Angle · crackedRIGHT WING PRESSURE DECK ANGLE FR 27 CRACK FOUND IN Y AXIS. 10-16-07 HFEC PERFORMED W/O 37536. CRACK CONFIRM, DOES NOT EXTEND BEYOND FASTENER. PRC 870 APPLIED IAW SRI DO/TS-4165/07-9309 INSPECTED PRESSURE DECK ANGLE AND EXISTING CRACK PER TC EO 72-53-SDR HALA0700417Fairing · crackedCRACK ON RT WING TRAILING EDGE UPPER FIXED FAIRING SUPPORT BEAMS AT WS 1030, WS 1100, AND WS 1178 ABOVE AND FWD OF OUTER AILERON. REPAIRED BY REPLACEMENT WITH REF TO 767-300 SRM 51-40-02 AND BOEING DWG 113T1913, P/N 113T1913-24 AND 113T913-26.SDR KCSA071420Web · gougedRIGHT WING I/B AILERON O/B HINGE SUPPORT WEB GOUGED AT WS 807.SDR 07FDEA04307Support Angle · crackedRT WING ROOT UPPER TE COMPOSITE PANEL INBD SUPPORT ANGLES (2EA ) ARE CRACKED, WBL 70. REMOVED CRACKED ANGLES, REF SRM 51-30-2, DRILLED NEW ANGLES TO FIT, REF 51-10-1. INSTALL, REF 51-030-2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 07FDEA04304Plate · noneFOUND OLD REPAIR AT CLOSING RIB TO TRACK NR 1 LT WING (LHT GLB S868048 AND REPORT 34624), PERMANENT REPAIR HAVE TO BE PERFORMED AT NEXT D-CHECK. REPAIR PERFORMED BY INSTALLING NEW ORIGINAL PARTS IAW DWG A572-42993, A572-42285 AND SRM 51-72-10.SDR 07FDEA04303Angle · noneFOUND OLD REPAIR AT CLOSING RIB TO TRACK NR 1 LT WING (LHT GLB S868048 AND REPORT 34624), PERMANENT REPAIR HAVE TO BE PERFORMED AT NEXT D-CHECK. REPAIR PERFORMED BY INSTALLING NEW ORIGINAL PARTS IAW DWG A572-42993, A572-42285 AND SRM 51-72-10.SDR 07FDEA04298Fitting · crackedCRACK FINDINGS AT LT CENTER WING C 47 VERTICAL FLANGE ANGLE FITTING HOLE NR H (A=33MM,B=31MM) AND NR I (A=12MM,B=10MM) REPAIR PERFORMED BY OVERSIZING HOLE NR H, I UNTIL CRACK AND CUT THE EXTERNAL FITTING REMOVAL IAW EA 6-5710-112497 AND RAS/053592/015/2007.SDR 07FDEA04297Fitting · crackedCRACK FINDINGS AT RT CENTER WING C 47 VERTICAL FLANGE ANGLE FITTING HOLE NR H (A=55MM,B=30MM) AND NR N (A=32MM,B=31MM) AND NR 39 WITH BUSH REPAIR AND INCORRECT FASTENER INSTALLED. REPAIR PERFORMED BY OVERSIZING HOLE NR H, N UNTIL CRACK REMOVAL AND INSTALLING SDR 07FDEA04274Deflector · damagedFOUND DAMAGED EDGE BAND OF DEFLECTOR DOOR 572CB AT LT WING. BONDING REPAIR PERFORMED IAW SRM 51-77-12, APPROVED BY EA 6-5755-112454 AND RAS/BAE/1005223/2007 ISSUE A.SDR 07FDEA04273Bracket · crackedRT WING, OTBD FLAP, INBD FLAP TRACK FAIRING IS CRACKED, AT CHANNEL SUPPORT ANGLE 16 INCHES AFT OF FWD EDGE, RT SIDE REMOVED DAMAGED TEE AND INSTALLED NEW ONE IAW SRM 51-30-2 AND 51-30-5 PG 5. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR WRLA2007094Vertical Support · crackedDURING C-5 CHECK, RT WING FIXED TRAILING EDGE 1 EACH VERTICAL SUPPORT CRACKED AT STA XORS 164-192. N/R 66448. 10-12-07 REPAIRED ACCORDING TO DWG ARC0295.SDR COEA0710821Skate Angle · corrodedFOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION ON PREVIOUS REPAIR TO THE RT NACELLE, IB SKATE ANGLE. BLENDED OUT CORROSION IAW SRAS DO/TS-3872/07-9231 REPAIR INSTRUCTIONS. SHEET REFERENCE: DO/TS-3872/07-4247. (K)SDR 07FDEA04137Panel · crackedCRACK FINDING DURING INSPECTION IAW SB 57-6086 HOLE NR F -1MM IN BOTTOM PANEL AND HOLE NR G-8MM IN FWD FITTING. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CRACK REMOVAL IAW EA 6-5710-73898 AND RAS/AS/310/2003 ISS A.
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