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.

SDR 99ZZZX2686Stiffener · crackedRT WING T/E SHROUD TOP STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 9 AND 10. REPAIRED PER BAE FAX JM/RJ0317/97 USING 2024T3 .040 INCH AND AW FAX HC/142-97 AND DJR/RJ0630-98.Aug 18, 1998 · N610AW · Bag BAE146200ASDR 99ZZZM478Stiffener · crackedRIGHT WING TE SHROUD TOP STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 5/6. REMOVED AND REPLACED RIGHT WING TE SHROUD TOP STIFFENER. (M)Aug 18, 1998 · N610AW · Bag BAE146200ASDR 99ZZZM476Rivet · looseRIGHT WING TE SHROUD TOP STIFFENER BETWEEN RIB 4/5 HAS LOOSE RIVET, AFT END. REMOVED AND REPLACED LOOSE RIVET. (M)Aug 18, 1998 · N610AW · Bag BAE146200ASDR 99FDEA00306Doubler · corrodedN0235 - DURING A/C P-F CONV AT AERONAVALI, CORROSION WAS FOUND ON LT UPPER WING AND MLG DOUBLER, TYPICAL PER DC10 SRM 57-00-01, FIG 8. THE AMOUNT OF DAMAGE FOUND ON PN ARB0866-1 IS NOT COVERED BY SRM. REPAIR REMOVES ALL CORROSION BY CUTTING OUT DAMAGE AND THAug 18, 1998 · N364FE · Doug DC1010SDR MWEA98938Tee Cap · replacementRIGHT SIDE TEE CAP REPLACEMENT AT STATION XCW 58 5. MTC REMOVED AND REPLACED TEE CAP.Aug 17, 1998 · N400ME · Doug DC914SDR MWEA98937Tee Cap · damagedLEFT SIDE TEE CAP REPLACEMENT AT STATION XCW 58 5. MTC REMOVED AND REPLACED LEFT TEE CAP.Aug 17, 1998 · N400ME · Doug DC914SDR MWEA98921Web · crackedWEB AT UPPER WING TRAILING EDGE IS CRACKED AT OUTBOARD END NUMBER 2 SPOILER PANEL. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.Aug 17, 1998 · N400ME · Doug DC914SDR MWEA98910Clip · unapproved partFOUND MATERIAL SUBSTITUTION CLIP ON RIGHT WING ANTENNA STATION XRS 111.5 BETWEEN STRINGER 13 AND 14. MTC FABRICATED AND INSTALLED STRINGER CLIP.Aug 17, 1998 · N400ME · Doug DC914SDR DHL9880327CCover · crackedAT C CHECK, RT T/E FLAP O/B FLAP I/B HINGE SUPPORT BRACKET STA 204.125, UPPER AREA RUB COVER IS CRACKED. REMOVED AND FABRICATED AND REPLACED COVER PER SRM 51-3-0. N/R 1023.Aug 17, 1998 · N803DH · Doug DC873FSDR DHL9880326CAngle · crackedAT C CHECK, RT WING T/E FLAP WELL LOWER AREA AT STA 178. FOUND CRACK ON ANGLE SUPPORT INBOARD AREA NEXT TO FAIRING CUTOUT. REMOVED AND FABRICATED NEW ANGLE PER SRM 51-1-21. N/R 1022.Aug 17, 1998 · N803DH · Doug DC873FSDR ABXA9801078Intercostal · corrodedRIGHT WING LEADING EDGE CORROSION ON INTERCOSTAL AND INNER DOUBLER AT STATION XFS 13.250. REPAIRED IAW ABX REA D857-17831.Aug 16, 1998 · N847AX · Doug DC861SDR CALA9801461Angle · crackedINSPECTION FOUND TWO ATTACH ANGLES CRACKED UNDER OUTBOARD END OF NR 12 SPOILER AT SUPPORT ROD LOWER ATTACH POINT OF RT WING TRAILING EDGE. THE ATTACH ANGLES WERE REMOVED. TWO NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM Aug 15, 1998 · N14788 · Boeing 727232SDR CALA9801460Angle · crackedINSPECTION FOUND A CRACK ON THE INBOARD SIDE OF L/E CAVITY BULKHEAD LOWER ANGLE APPROXIMATELY TWENTY INCHES AFT OF KRUEGER FLAP HINGE LINE AT LT WING LEADING EDGE STA 130. THE ANGLE WAS REMOVED AND A NEW REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40Aug 15, 1998 · N14788 · Boeing 727232SDR ABXA9800745T-Cap · crackedDURING C-CHECK, FOUND LEFT T-CAP CRACKED AT STATION XCW-58.500. REPLACED LEFT WING T-CAP IAW ABX EA 12182 AND DC9 SRM 51-30-5.Aug 15, 1998 · N983AX · Doug DC932SDR 99ZZZM482Stiffener · crackedRIGHT WING TE SHROUD TOP STIFFENER CRACKED AT FORWARD END AND RIVET POPPED (AFT END) BETWEEN RIBS 3/4. REPLACED RIGHT WING TRAILING EDGE SHROUD TOP STIFFENER BETWEEN RIBS 3/4. (M)Aug 14, 1998 · N610AW · Bag BAE146200ASDR 99ZZZM479Stiffener · crackedTE RIGHT WING TOP SHROUD STIFFENER OUTBOARD CRACKED AT FORWARD END BETWEEN RIB 8/9. REPLACED RIGHT WING TRAILING EDGE SHROUD TO STIFFENER BETWEEN RIBS 8/9. (M)Aug 14, 1998 · N610AW · Bag BAE146200ASDR 99ZZZX2676Rivet · looseNUMEROUS LOOSE RIVETS AT LT WING T/E LOWER SKIN, AFT OF REAR SPAR. REMOVED AND REPLACED NUMEROUS LOOSE RIVETS ON LT WING T/E LOWER SKIN AFT OF REAR SPAR.Aug 13, 1998 · N610AW · Bag BAE146200ASDR ABXA9800789Angle · crackedRIGHT WING LEADING EDGE AT STATION 778.500 UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DWG K 05056-7003.Aug 12, 1998 · N803AX · Doug DC862SDR 99ZZZM483Stiffener · crackedLEFT WING TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 7/8 IS CRACKED AT FORWARD END. REMOVED AND REPLACED TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 7/8. (M)Aug 12, 1998 · N610AW · Bag BAE146200ASDR VJ9800390Tip · gougedAT WS XW536.8 ON LT WING TIP THERE IS A GOUGE IN THE TRAILING EDGE. BLENDED GOUGE AT STA 536.8 IAW DC-9 SRM 51-10-3. MAT LOSS 100 PERCENT AND OUT OF LIMITS IAW DC9 SRM 57-01 FIG 1. FABRICATED NEW SECTION OF T/E OUT OF 2024 T 3 .020 IAW DC9 SRM 57-31-3 AND Aug 11, 1998 · N934VV · Doug DC932SDR CALA9801446Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING TRAILING EDGE UPPER ATTACH ANGLE ABOVE NR 6 GEARBOX FOR FLAP. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-10-6.Aug 11, 1998 · N66734 · Boeing 727224SDR SWAA981714Angle · corrodedDURING SCHEDULED SERVICE CHECK, FOUND O/B STABILIZER BAR SUPPORT ANGLE CORRODED ON LUG FACE. REMOVED AND REPLACED PER BOEING SRM.Aug 10, 1998 · N130SW · Boeing 7372T4SDR CALA9801436Web · crackedINSPECTION FOUND A .5 INCH CRACK IN WEB PANEL NEXT TO BOOST PUMP INSIDE NR 2 FUEL TANK AT LT WS 171.50. THE WEB PANEL WAS REPAIRED IAW SRM 51-40-2, FIGURE 1.Aug 10, 1998 · N32725 · Boeing 727224SDR DHL9880317DDump Well · crackedAT C CHECK, FUEL DUMP WELL AREA CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR PER SRM 51-1-21, .5 BY 5.5, N/R 755.Aug 9, 1998 · N803DH · Doug DC873FSDR UPS98227528Clip · crackedINSPECTION TYPE-D, WING CENTER SECTION FWD TANK FWD WALL SHEAR TIE CLIP CRACKED AT RBL 25. REPLACED SHEAR TIE CLIP IAW DRW 64-08333.Aug 7, 1998 · N905UP · Boeing 72751CSDR UPS98227527Clip · crackedINSPECTION TYPE-D, WING CENTER SECTION FWD TANK FWD WALL SHEAR TIE CLIP CRACKED AT LBL 25. REPLACED SHEAR TIE CLIP IAW DRAWING 64-08333.Aug 7, 1998 · N905UP · Boeing 72751CSDR TWAA9812901Tip · damagedTHE RT WING TIP AND TIP TRAILING EDGE WERE DAMAGED WHEN STRUCK ON THE GROUND. REPLACED WING TIP ASSY AND INSTALLED NEW TRAILING EDGE, PER SRM 51-30-1 AND STANDARD MAINT PRACTICES.Aug 7, 1998 · N9620D · Doug DC983SDR CALA9801428Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN FORWARD ANGLE AT RT WING LEADING EDGE FLAP WELL LOWER STIFFENER, FS 150. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.Aug 7, 1998 · N32725 · Boeing 727224SDR CALA9801425Angle · crackedINSPECTION FOUND A .15625 CRACK IN SUPPORT ANGLE FOR LT WING TRAILING EDGE PANEL FORWARD OF OUTBOARD AILERON, OUTBOARD OF AILERON LOCKOUT. THE CRACKED AREA WAS ROUTED OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-40-1 AND 51-10-2.Aug 7, 1998 · N32725 · Boeing 727224SDR 98FDEA00492Bolt · shearedFOUND 3 BOLTS SHEARED AT BS XCW 118 TO XCW 115 RT AFT SPAR TOP SURFACE. *S/D* REMOVED AND REPLACED BOLT AND TORQUED. INSP AND NDT, MEASURE BOLT HOLE, SPOT FACE AREA.Aug 7, 1998 · Doug DC1010FSDR UPS98827644Fitting · crackedINSPECTION TYPE C-CK, INSIDE NR 3 MAIN TANK O/B OF XRS 74 STINGER 51 THE FWD SPLICE FITTING IS CRACKED. REMOVED CRACKED FITTING, FABRICATED NEW FITTING IAW DAC DWG 3704841. INSTALLED FITTING IAW DC8 SRM 51-3-0, 51-1-20D, 51-1-23.Aug 6, 1998 · N806UP · Doug DC873FSDR UPS98827643Fitting · crackedINSPECTION TYPE C-CK, INSIDE NR 3 MAIN TANK O/B OF XRS 74 STRINGER 51 AFT SPLICE FITTING IS CRACKED. REMOVED CRACKED FITTING HAD NEW ONE FABRICATED IAW DAC DWG 3724841 AND INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, 51-1-20D, 51-1-23.Aug 6, 1998 · N806UP · Doug DC873FSDR UPS98827642Fitting · crackedINSPECTION TYPE C-CK, INSIDE NR 3 MAIN TANK JUST I/B OF XRS 74 STRINGER 51 AFT SPLICE FITTING CRACKED. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51-1-20D. FABBED FITTING IAW DAC CWG 3724841.Aug 6, 1998 · N806UP · Doug DC873FSDR CALA9801409Tip · crackedINSPECTION FOUND LT WING TIP INBOARD ACCESS PANEL 8112 DEFORMED AND CRACKED. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-20-01.Aug 6, 1998 · N14788 · Boeing 727232SDR C2XA98IA300Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND A WING SKIN SUPPROT CRACKED AT FRAME 19, LEFT WING. MAINTENANCEE REMOVED AND REPLACE THE SUPPORT IAW EMB120ER SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Aug 6, 1998 · N16723 · Emb EMB120RTSDR CALA9801392Angle · crackedINSPECTION FOUND 2.5 INCH CRACK AT CURVED ANGLE AT OUTBOARD SIDE OF LT WING FIXED LEADING EDGE RIB SLAT STA 0. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-40-3.Aug 5, 1998 · N66734 · Boeing 727224SDR CALA9801387Web · crackedINSPECTION FOUND CRACKS IN CENTER WING BOX WEBS AT STA XCWR46, XCWL46, XCWR17, AND XCWL18. ALL CRACKS WERE TRIMMED AND BLENDED OUT. REWORKED AREAS AND REINFORCED WITH DOUBLERS AND FILLERS IAW SRM 57-00-01, FIGURE 1, 51-21-03, AND 51-30-02.Aug 5, 1998 · N68043 · Doug DC1010SDR QXEA9801162Angle · crackedLEFT-HAND WING UPPER LEFT-HAND MLG CONNECTION ANGLE (FROM WING TO MLG) CRACKED IN RADIUS. REPAIRED IAW FOKKER SRM 57-02-05.Aug 1, 1998 · N498US · Fokker F28MK4000SDR UPS98827396Angle · crackedINSPECTION TYPE:D LT WING L/E AT STA XS 250.089, THE VERTICAL STIFFNENER ANGLE IS CRACKED AT THE LWR END. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5769859 AND SRM 51-1-20D.Jul 30, 1998 · N755UP · Doug DC871FSDR CALA9801363Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN ANGLE TO RT WING INBOARD BUTE DOOR STIFFENER ATTACHMENT POINT. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, FIGURE 1.Jul 29, 1998 · N15525 · Doug DC932SDR AU980911Bracket · cracked(AUS) WING BRACKET CRACKED.Jul 29, 1998 · Cessna 310RSDR 98ZZZX3184Bracket · crackedWHILE C/W AD 75-17-32-R2 - LANDING GEAR OPERATING MECHANISM, A CRACK WAS FOUND IN THE RIGHT INTERNAL WING RIB BRACKET. THE CRACK WAS LOCATED AT THE UPPER RADIUS AND WAS APPROXIMATELY .75 INCH IN LENGTH. SUBMITTER STATED THE CRACK WAS MOST LIKELY CAUSED BY IMPJul 29, 1998 · N729WA · Mrchti S20522RSDR UPS98827333Angle · corrodedINSPECTION TYPE:C, WING CENTER SECTION ( UPPER ) AT FS 798 RBL 44, CHORD ANGLE HAS HEAVY CORROSION. REMOVED AND REPLACED CHORD ANGLE IAW SRM 51-1-20D.Jul 28, 1998 · N715UP · Doug DC871FSDR VJ9800280Angle · crackedSPAR CAP XRS AT INBRD FLAP HINGE STUD HOLE HAS A .25 INCH CRACK ON FWD FACE RUNNING VERTICALLY FROM TOP EDGE OF HOLE. FABRICATED ANGLE FROM 2024, 26 1/4 BY 3 INCHES. LOCATED AND DRILLED TWO OTHER ANGLES. INSTALLED REPAIRS IAW DC9 SRM 51-30-5 AND DWG J0602T1Jul 27, 1998 · N912VV · Doug DC932SDR ABXA9800752Doubler · crackedRIGHT WING LEADING EDGE AT STATION XOL 6.225, INTERNAL DOUBLER IS CRACKED ON EACH SIDE OF TRIPLER. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 5769589.Jul 27, 1998 · N803AX · Doug DC862SDR ABXA9800751Doubler · crackedRIGHT WING TRAILING EDGE RIB IS CRACKED IN 2 PLACES AT FLAP STATION 3.00. INSTALLED NEW RIB DOUBLER INTERCOSTAL IAW DC8 SRM 51-1-21, 51-1-20D AND 57-2-0.Jul 27, 1998 · N803AX · Doug DC862SDR ABXA9800750Angle · crackedLEFT INBOARD SLOT BOX, AFT OUTBOARD VERTICAL ANGLE IS CRACKED. FABRICATED AND INSTALLED REPLACEMENT VERTICAL ANGLE IAW DC8 SRM 51-1-20D AND DWG 9753293.Jul 27, 1998 · N803AX · Doug DC862SDR UPS98827406Doubler · corrodedINSPECTION TYPE:C LT WING L/E INTERNAL DOUBLER HAS HEAVY CORROSION AT STA XFS 728. 750 AND XFS741.250. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 3641257 AND SRM 51-1-20D.Jul 25, 1998 · N715UP · Doug DC871FSDR UPS98827334Doubler · corrodedINSPECTION TYPE:C, RT WING L/E AT W/S XFS 797.500, THE INTERNAL DOUBLER HAS HEAVY CORROSION AT O/B END OF ACCESS PANEL. REMOVED AND REPLACED DOUBLER IAW SRM 51-1-21.Jul 25, 1998 · N715UP · Doug DC871FSDR UPS98827320Doubler · corrodedINSPECTION TYPE:C, RT WING L/E AT W/S XFS 828.75, THE INTERNAL DOUBLER HAS HEAVY CORROSION AT FWD END OF ACCESS PANEL. REMOVED AND REPLACED DOUBLER IAW SRM 51-1-20.Jul 25, 1998 · N715UP · Doug DC871F
Back to JASC 5720