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 FDEA201003210970Angle · crackedLT WING T/E FALSE SPAR CHORD ANGLE CRACKED WBL 118. TRIMMED OUT DAMAGE, FABRICATED NEW INBD WEB SECTION USING 7075T-6 .032 PO NR 9009201 DIMS 12 1/8 INCH BY 9 1/2 INCH, FABRICATED NEW LWR CHORD SECTION USING BAC1514-1437 7075T-6 PO NR 2911884, FABRICATED 2 ANSDR FDEA201003200948Deflector · delaminatedRT WING T/E COVE PANEL NR 4 LOWER SURFACE METAL TAPE PEELING/MISSING REPAIRED IAW EA 6-5720-136631. REMOVED PANEL TO FOM. REMOVED ALUMINUM FOIL AND HARDWARE. APPLIED NEW ALUMINUM FOIL AND INSTALLED HARDWARE IAW EA 6-5720-136631,"WINGS - WING FLAP HINGE DESDR FDEA201003200947Deflector · delaminatedRT WING T/E COVE PANEL NR 3 LOWER SURFACE METAL TAPE PEELING/MISSING REPAIRED IAW EA 6-5720-136631. REMOVED AND REINSTALLED HARDWARE IAW SRM 51-40-00. N/R N00389 FOR ORIGINAL EA. N/R N01255 FOR THE APPLICATION OF THE WITNESS MARK.SDR KCSA101014Support · crackedLEFT WING LOWER L/E FUEL ACCESS DOOR HAS A CRACK IN THE SUPPORT STRUCTURE AT WS 807.SDR USAA2010031290566Pin · corrodedPIT - C11 - MAJOR REPAIR - RIGHT PINTLE PIN HAS STEP WEAR & CORROSION. REPLACED RIGHT PINTLE PIN IAW JOB CARD 26T00032001.SDR SIMA201006707Torque Box · damagedDURING THE MAINTENANCE BASE VISIT THE RIGHT LOWER WING TORQUE BOX RIB WAS FOUND TO HAVE AN OVERSIZED HOLE OUTBOARD FORWARD OF THE HOLE WITH BUSHING INSTALLED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED, FABRICATED AND INSTALLED BUSHING ON THE RIGHT LOWERSDR FDEA201003030626Stiffener · crackedRT WING UPPER L/E PANEL 616 ET INNER SURFACE HAS 3 EA CRACKED STIFFENERS. PANEL 616 ET REQUIRES SRM REPAIR IAW SRM 57-10-00, VOL I. MATERIAL VERIFICATION 7075-0 0.040, PO NR 657517.2. FORMED REPAIR STIFFENERS AND FABRICATED REPAIR STIFFENERS IAW SRM 57-10-SDR A6WA201040214Seal · crackedLT WING FLIGHT SPOILER, METAL SEAL BETWEEN CTR HINGES ON WING IS CRACKED. R & R UNSERVICEABLE SEAL IAW SRM 51-42-06 & 51-42-21.SDR FDEA201003020592Stiffener · crackedLT WING UPPER L/E PANEL 516 ET HAS 3 EA INNER STIFFENERS CRACKED. RECEIVED MATERIAL ID 7075-0 0.040 TO FORM 3 REPAIR STIFFENERS AND HEAT TREAT TO 7075-T6 0.040 IAW SRM 57-10-00, PG 83, VOL I. FABRICATED 3 REPAIR STIFFENERS IAW SRM 57-10-00, PG 83, VOL I. APSDR DL76L100679Tee Fitting · misinstalledLT AND RT TEE CLIPS FOR UPPER LINK FITTING IAW SB 767-54-0080 FOUND TO HAVE INCORRECT EDGE DISTANCE, REPAIRED IAW ERA 480782-14AD.SDR IPXA10658814Stiffener · crackedINSPECTION TYPE:C, RT WING - L/E OFSS821 FRONT SPAR STIFFENER FOUND CRACKED. RT WING L/E OFSS821 FRONT SPAR STIFFENER REPLACED AND INSTALLED IAW RS R57-00-36628. ORG MAT'L IS BAC1503-100631-7075T6511 EXTRUSION CRACK LENGTH IS .3750". THIS REPAIR IS CLASSIFSDR UIEA201000025Support · crackedLT WING LOWER SURFACE ADJACENT TO NR 5 SPOILER OTBD AREA UPPER SURFACE FIXED PANEL SUPPORT STRUCTURE CRACKED. UPPER SURFACE SUPPORT FITTING REPLACED IAW SRM 51-10-02, 51-40-02 AND AMM 57-22-01.SDR DHLA201000007Door · gougedRT OTBD WING SLOT DOOR HAS A DEEP GOUGE IN OUTER PLATING LOWER SURFACE APPROX AT WS XS 493.0. ACCOMPLISHED EXTERNAL DOUBLER REPAIR TO PN 5769946-502 SLOT DOOR IN AFFECTED AREA IAW EVA D857-00321 REV IR AND SRM 57-2-0, FIG 2A TR 57-84. REFERENCE ASSOCIATED FASDR IPXA10658878Support · crackedINSP TYPE:C, LT WING L/E LES675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP FOUND CRACKED, CRACK .2500" IN LENGTH. LT WING L/E LES675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP, REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.SDR UALA2010022300667Fairing · puncturedLT WING INBD FLAP TRACK WING TO BODY FAIRING PUNCTURED. APPROX ONE HALF INCH SQUARE. SUPPLEMENTAL DATA UPDATE HOLE WITHIN LIMITS REF SRM. 2 SHIFT SLOT REQUESTED. REQUIRED FOR ACCESS. REPAIRED HOLE REF MM.SDR ASAA1077406Bracket · crackedRT WING FIXED TRAILING EDGE FIXED BULKHEAD STA 289 BRACKET FIXED TRAILING EDGE IS CRACKED. REMOVED CRACKED BRACKET AND INSTALLED NEW BRACKET.SDR A6WA201040127Seal · chafedLT FLAP FAIRING (HINGE) 592BB IB METAL SEAL IS CHAFED. REMOVED DAMAGED SEAL AND REPLACED WITH METAL SEAL SRM 51-12-00.SDR ASAA1057400Support Angle · crackedSEAL RETAINER SUPPORT ANGLE CRACKED LT WING REAR SPAR. REMOVED AND REPLACED SUPPORT ANGLE.SDR IPXA10658553Stiffener · crackedINSP TYPE:6C, FWD CARGO WING CENTER SECTION FRONT SPAR VERTICAL STIFFENER UPPER AREA FOUND CRACKED JUST AT STA 785.9 LBL 32.94. STIFFENER REPAIRED IAW HX RS. R57-10-36618 REV A & EO NR B767-5710-36713-A. ORIN. MAT'L 1518-749-2024T3511, CRK LENGTH 3.25", CUTOSDR UVVR2010021200003Strip · chafedRT WING L/E ASSY INBD RIB (1A) IS CHAFING AGAINST THE FWD WING/FUSELAGE FAIRING SUPPORT STRIP. THE SUPPORT STRIP IS FLUSH RIVETED TO THE OTBD WEB OF THE WING/FUSELAGE FAIRING AND SANDWICHES A SEAL. THE SUPPORT STRIP AND SEAL WERE INSTALLED OVER THE TOP OF MS20SDR UVVR2010021200002Strip · chafedLT WING L/E ASSY INBD RIB (1A) IS CHAFING AGAINST THE FWD WING/FUSELAGE FAIRING SUPPORT STRIP. THE SUPPORT STRIP IS FLUSH RIVETED TO THE OTBD WEB OF THE WING/FUSELAGE FAIRING AND SANDWICHES A SEAL. THE SUPPORT STRIP AND SEAL WERE INSTALLED OVER THE TOP OF MS20SDR WRLA20100211343Fitting · crackedDURING PERFORM TASK CARD WA5750, FOUND RT WING LOWER WINGLET FWD FITTING (ARB7772-70) CRACKED, ISSUED NRC U01048. REMOVED AND KEPT THE WINGLET AND THE ATTACHING PARTS, REPLACE THE WINGLET FWD FITTING ACCORDING EI W2010A57B-494 REV 00, INSTALL THE RIGHT WING LSDR IPXA10M58588Support · crackedINSP TYPE:1C, RT WING FIXED L/E COMP'T SPLICE STRAP SUPPORT CRACKED AT STA XOS789 CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR STRAP AND FILLER REF STASA EA 011-5720-01-A2178 AND EO MD11-5720-36726-ASDR UIEA201000002Fairing · missingON WALK AROUND, FOUND NR 5 CANOE MISSING. ALSO FOUND DAMAGE TO RT FUSELAGE SKIN AND LONGERON BOX. INSTALLED NR 5 CANOE AND OPERATIONAL CHECK OK. ALSO, ACCOMPLISHED REPAIR REF EO4453A333, FUSELAGE SECTION 44-LONGERON BOX, BS 1442.41 - BS 1480 FUSELAGE SKIN DSDR WRLA20100204337Fitting · crackedDURING PERFORM TASK CARD WA3007, FOUND RT WING TIP FITTING ARB7602-R CRACKED. PER AMM 20-50-02-900-801 REV 66 REPLACED THE FITTING, CONDITION SATISFACTORY.SDR SWIA201023944Angle · crackedRIGHT INBOARD WING FUEL TANK LOWER ANGLE CRACKED FORWARD OF DEFUEL PANEL. (C CHECK) REPLACED ANGLE PER SRM.SDR A6WA201040080Angle · crackedATTACH ANGLE AT INBD END OF WING L/E 530JL CRACKED (PN 600-12045-11).SDR FOTR20006NR4905Skin · crackedLT MLG WING DOOR AT AFT HINGE AREA, SKIN IS CRACKED AFT OF SEAL RETAINER. REPAIRED ON FASI WO 20006, N/R 04905. REMOVED AND REPLACED PREVIOUS REPAIR TO LT MLG WING DOOR AT AFT HINGE AREA WBL 124 IAW S/B 727-32-318 FIG 4, REV IR. MATERIAL USED: DOUBLER; 2024SDR IXXA10SMN028SWeb · crackedDURING ROUTINE C-CHECK INSP FOUND LT WING INBD LOWER SLOT DOOR WEB BROKEN. REMOVED DAMAGED WEB. FABRICATED NEW WEB. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 51-3-0, SRM 57-1-0 PAGE 1, SRM 57-3-3 FIGURE 22 ITEM "G", DPS 4.7SDR AALA20100123TUL01Angle · corrodedFOUND CORROSION ON ANGLE IN RIGHT WHEEL WELL. REMOVED AND REPLACED ANGLE UNDER 57-10-00-13A.SDR AALA20100122TUL05Casting · crackedFOUND PULLEY BRACKET SUPPORT CASTING CRACKED ON FORWARD WING SPAR. REMOVED CASTING PER SRM 51-01.SDR FDEA201001140137Support · crackedRT WING T/E UPPER PANEL SUPPORT IS CRACKED FROM RIB 6A TO RIB 7. REMOVED CRACKED SUPPORT/STIFFENER IAW SRM 51-40-21, PARA 7. MACHINED NEW STIFFENER IAW DWG A57241059. ACCOMPLISHED FPI IAW DWG A57241059 IAW PROCESS 526.2501 AND ABP 6-5230. NO CRACKS NOTED. SDR N93A01132010ABolt · corrodedMOST CADMIUM PLATED HARDWARE INSTALLED IN WING INTERGRAL FUEL TANKS HAVE DEVELOPED CORRSION. HARDWARE REQUIRES REPLACEMENT MULTIPLE PNS AFFECTED.SDR FDEA201001110069Intercostal · crackedLT WING L/E FOUND CRACK ON OLD REPAIR OF INTERNAL INTERCOSTAL. REPAIRED INTERNAL INTERCOSTAL IAW SRM 57-00-01 FIG.10 SH.1 VOL.1SDR A6WA201040158Angle · crackedRT MIDDLE WING L/E. INBD ATTACH ANGLE IS CRACKED. REPLACED ANGLE PN 600-12025-8 IAW SRM 51-41-02, 51-40-11.SDR A6WA201040155Angle · crackedLT WING CTR L/E INBD ATTACH ANGLE CRACKED. REMOVED DAMAGED ANGLE, LOCATED FASTENER HOLES IN SERVICEABLE ANGLE AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-41-02.SDR SWIA201023517Angle · crackedLEFT WING BATT ANGLE AT WS 53 AND WS 48 CRACKED. (C CHECK) REPAIRED PER REO.SDR IPXA10558108Angle · crackedINSPECTION TYPE:C2 LT WING TRUNNION FAIRING NR 571BB OTBD AFT FAIRING STIFFENER ANGLE CRACKED 2 INCHES FWD OF THE AFT END OF THE STIFFENER. ANGLE WAS REPLACED IAW SRM 51-40-02-0G.SDR FDEA200912224496Intercostal · crackedLT WING L/E FOUND CRACK ON INTERNAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 57-00-01 FIG.10 SH.1 VOL.1SDR ASAA0957151Support Angle · crackedRETAINER SUPPORT ANGLE CRACKED ON LT WING TRAILING EDGE. REMOVED AND REPLACED SUPPORT ANGLE.SDR ASAA0957150Support Angle · crackedRETAINER SUPPORT ANGLE CRACKED ON RT WING TRAILING EDGE. REMOVED AND REPLACED SUPPORT ANGLE.SDR QXEA2009121601058Fitting · chafedC5 CHECK - LT SIDE STAY FITTING HAS CHAFE DAMAGE TO UPPER OTBD SIDE. BLENDED OUT CHAFE IAW REO 670-57-11-043. PERFORMED LPI ON BLEND IAW LPI NDTM 51-20-08. PERFORMED ROTO PEEN ON WORKED AREA IAW REO 670-57-11-043.SDR QXEA2009121601057Fitting · chafedC5 CHECK - RT SIDE STAY FITTING HAS CHAFE DAMAGE TO UPPER OTBD SIDE. BLENDED OUT CHAFE IAW REO 670-57-11-043. PERFORMED LPI ON BLEND IAW LPI NDTM 51-20-08. PERFORMED ROTO PEEN IAW REO 670-57-11-043.SDR A6WA2010400004Angle · crackedLT WING OTBD ATTACH ANGLE UNDER ACCESS PANEL 520ML IS CRACKED. REMOVED CRACKED ATTACH ANGLE FROM LT WING OTBD UNDER ACCESS PANEL 520ML AND INSTALLED SERVICEABLE BRACKET PN 600-12045-11 IAW SRM 51-41-061.SDR A6WA201040004Angle · crackedLT WING OTBD ATTACH ANGLE UNDER ACCESS PANEL 520 ML CRACKED. REMOVED CRACKED ATTACH ANGLE FROM LT WING, OTBD UNDER ACCESS PANEL 520 ML AND INSTALLED SERVICEABLE BRACKET PN 600-12045-11, IAW SRM 51-41-061. (K)SDR SWAA097647Stiffener · crackedDURING SCHEDULED 12Y CHECK, FOUND STIFFENER CRACKED AT BS 540, LBL 33. REPAIRED STIFFENER PER SRM.SDR UHLA2009121400077Structure · crackedMAJOR REPAIR: LT WING LEADING EDGE DAMAGE WITH VISUAL CRACK 7.3750 IN LONG. DAMAGE WAS REPAIRED IAW EMBRAER ETD2009-170/09477 REV 1.SDR FDEA200911294215Support Angle · crackedRT WING INSIDE PANEL, 641MB, HAS A CRACKED VERTICAL SUPPORT L ANGLE WS STA 537.5 APPROX 4" ABOVE LWR SKIN. CRACKED L-ANGLE AT WS 537.5 REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR USAA2009122193391Support Fitting · crackedMAJOR REPAIR - CRACK ON RT WING RIB 5 SUPPORT FITTING. REPLACED RT WING RIB 5 SUPPORT FITTING IAW EA 113958. (K)SDR ABXA201003290023Panel · crackedPANEL 551TB OUTBOARD OF LT MLG CORNER IS CRACKED. REMOVED AND RE-INSTALLED PANEL 551TB IAW B767 SRM 51-40-02. P/N 113T1615-25, .5 CRACK LENGTH.
Back to JASC 5720