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 SWAA990809Strap · crackedDURING SCHEDULED 1/4D CHECK, FOUND LT WING UPPER STRAP FWD OF AILERON CRACKED. REMOVED AND REPLACED STRAP PER SRM.May 4, 1999 · N323SW · Boeing 7373H4SDR DHL9980229CAngle · crackedC-CHECK, RT WING AT NR 1 HINGE AREA XW 5 & FS 980 APPROX CRACKED ANGLE. DOT 641.59. REMOVED DAMAGED ANGLE AT RT WING NR 1 HINGE AREA XW 5 FS 940 IAW DC-8 51-1-21 PG 1 PAR 1. FABRICATED NEW ANGLE PER DC-8 SRM 53-8-3 PG 5/6 FIG 1 2024-T3 050 14X3. TREATED & May 3, 1999 · N802DH · Doug DC873FSDR DHL9980226CFitting · crackedC-CHECK, LT WING, I/B FLAP, I/B HINGE, 2 INCH CRACK UNDER FLAP FITTING ATTACH POINT WING STA XW 5.000. STOP DRILLED END CRACK .25 AT LT WING I/B FLAP I/B HINGE UNDER FLAP FITTING ATTACH POINT IAW DC-8 SRM 51-3-2 PG 1 PAR 1. FABRICATED ANGLE REPAIR 2024-T3 05May 3, 1999 · N802DH · Doug DC873FSDR DHL9980224CAngle · crackedC-CHECK, RT WING AT NR 1 HINGE AREA XW 5 & 980 APPROX CRACKED ANGLE DOT 641-59. REMOVED DAMAGED ANGLE AT RT WING NR 1 HINGE AREA XW 5 FS 940 PER DC-8 SRM 51-1-21 PG 1 PAR 1. FABRICATED NEW ANGLE PER DC-8 SRM 53-8-3 PG 5/6 FIG 1 2024-T3 050 14 X 3. TREATED &May 3, 1999 · N802DH · Doug DC873FSDR DHL9980219CFitting · crackedC-CHECK, LT WING, L/B HINGE, 2 INCH CRACK UNDER FLAP FITTING ATTCH POINT WING STA: XW 5.000. STOP DRILLED END CRACK .25 AT LT WING L/B FLAP L/B HINGE UNDER FLAP FITTING ATTACH POINT IAW DC-8 SRM 51-3-2 PG 1 PAR 1. FABRICATED ANGLE REPAIR 2024-T3 050. 6 X 3 IMay 3, 1999 · N802DH · Doug DC873FSDR UF6A990510Tip · crackedSBN - LEFT FORWARD WING TIP END CAP HAS A CRACKED RIB ASSEMBLY. MAINTENANCE REPAIRED DAMAGED AREA AND INSTALLED DOUBLER IAW BAE ATP SRM 51-60-04. AREA WAS ALODINED AND PRIMED. (M)May 1, 1999 · N857AW · Bag ATPSDR UF6A990509unknownSBN - LEFT AFT WING TIP END CAP HAS CORROSION AT ATTACHMENT HINGE. MAINTENANCE REPAIRED DAMGED AREA AND FABRICATED DOUBLER IAW BAE ATP SRM 51-60-04. AREA WAS ALODINED AND PRIMED. (M)May 1, 1999 · N857AW · Bag ATPSDR DHL9980231CBracket · crackedC-CHECK, LT WING STA SRS 693 THRU PLATE DOOR NR 518B BRACKET CRACKED. DOT 381. STOP DRILLED END CRACK AT LT WING I/E RIB STA WRS 693 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3.050 3 X 1 X 4 IAW DC-8 SRM 57-2-0 PG 10 FIG 2. TREATED & PRMay 1, 1999 · N802DH · Doug DC873FSDR DHL9980248CAngle · crackedC-CHECK, ABOUT XCW 46.00 BELOW LT WING IS CRACKED DOT 382627. REMOVED DAMAGED ANGLE AT LT WING XW 46.00 IAW DC-8 SRM 51-1-21 PG 1 PAR 1. FABRICATED NEW ANGLE .071 2024T3 12 X 6 IAW DC-8 SRM 51-1-4 PG 1 PAR 1. TREATED & PRIMED PER DC-8.Apr 29, 1999 · N802DH · Doug DC873FSDR DHL9980246CAngle · crackedC-CHECK, ABOUT XTS 6.000 BELOW LT WING IS A CRACK SEE MARK DOT 38262. REMOVED CRACKED ANGLE FROM WING ABOUT STA XRS 6.000 IAW DC-8 SRM 51-1-21 PAR 1 FIG 32. FABRICATED NEW ANGLE SAME MATERIAL & THICKNESS 2024-T3 0.050 (20 X 11) IAW DC-8 SRM 57-3-1 FIG 25. Apr 29, 1999 · N802DH · Doug DC873FSDR DHL9980213CBracket · crackedC-CHECK, BELOW LT WING ABOUT X 46.000 STA 880 BRACKET CRACKED. REMOVED CRACKED BRACKET FROM LT WING AT STA 880 IAW DC-8 SRM 51-1-20D & 51-1-21 PAR 1. FABRICATED NEW BRACKET SAME MATERIAL & THICKNESS 2024-T3 0.0063 DC-8 SRM 53-8-3 FIG 2. CLEANED BRACKET AREApr 29, 1999 · N802DH · Doug DC873FSDR LR7A9973Web · damagedDURING SCHEDULED C1 INSPECTION LT WING OWS 545 TO 562 FWD SPAR WEB DUE REPLACEMENT TO CORRECT DAMAGE FROM INCIDENT 6/27/98 AND TERMINATE REPETITIVE INSPECTION REQUIREMENT. WEB REPLACED FROM OWS 545 TO 562 IAW SRM 583-57-30-22. DRC-0001-SM.Apr 28, 1999 · N402LC · Lkheed 382GSDR 99ZZZX2109Cap · crackedCRACK FOUND IN LEFT GEAR WELL AFT OF MAIN SPAR ON INBOARD SIDE OF THE CAP IN THE VICINITY OF THE NACELLE SPLICE PLATE.Apr 26, 1999 · N95WA · Beech 99SDR ABXA9900468Clip · crackedLEFT CENTER LEADING EDGE INTERCOSTAL ATTACH CLIP CRACKED AT STATION XOLDI 6.225. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 5769857.Apr 23, 1999 · N816AX · Doug DC863SDR ABXA9900467Angle · crackedRIGHT WING LEADING INBOARD SIDE STATION XS250.089 RIB VERTICAL ANGLE CRACKED AT BOTTOM. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 97532938.Apr 21, 1999 · N816AX · Doug DC863SDR A6WA9900055Stiffener · crackedUPPER WING SKIN TRAILING EDGE STIFFENER IS CRACKED AT FORWARD END LOCATED BETWEEN RIBS 9 AND 10, LEFT WING. REPAIRED LT WING SKIN TRAILING EDGE UPPER WING SKIN STIFFENER BETWEEN RIBS 9 AND 10 IAW BAE FAX DJR/RJ0630-98. (X)Apr 21, 1999 · N463AP · Bag BAE146100ASDR 99T64R262ARShim · crackedNR 2680 - LT WING BOTTOM FRONT SPAR CAP SHIM PLATE CRACKED XS 510.222. REMOVED SHIM, BLENDED SMOOTH THE CRACKED SURFACE, ALODINED AND PRIMED. RE-INSTALLED SHIM AND SEALED WITH PR 1422 B 1/2 PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARApr 21, 1999 · N1808E · Doug DC862SDR 99T64R263ARShim · crackedNR 2681 - RT WING BOTTOM FRONT SPAR CAP SHIM PLATE CRACKED APPROXIMATELY 1 FOOT INBOARD NR 4 PYLON XS 510.222. REMOVED SHIM, BLENDED SMOOTH THE CRACKED SURFACE, ALODINED AND PRIMED. RE-INSTALLED SHIM AND SEALED WITH PR 1422 B 1/2 PER EO 99-061 WITH APPROVED Apr 20, 1999 · N1808E · Doug DC862SDR UPS99829578Angle · crackedINSPECTION TYPE:C2, THE RT STA 98 FLAP ACTUATOR ATTACH FITTING INBD MOUNT ANGLE IS CRACKED AT THE LWR END. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 3643319 AND SRM 51-1-20D AND 51-3-0.Apr 19, 1999 · N880UP · Doug DC873FSDR UPS99829521Fitting · crackedINSPECTION TYPE:C2 RT LONG 24 UPPER FITTING AT FS 879 HAS CRACK AT ATTACHMENT HOLES. REMOVED CRACK FITTING, LOCATE NEW FITTING, DRILL, AND REAM EXISTING HOLES IN FITTING IAW DC-8 SRM 51-3-2 AND INSTALLED IAW DC-8 SRM 51- 1-20D.Apr 19, 1999 · N819UP · Doug DC873FSDR UPS99829520Fitting · corrodedINSPECTION TYPE:C2 LONG 24 RT UPPER FITTING AT FS 940 HAS CORROSION AT BOTTOM ATTACHMENT HOLES. REMOVED CORRODED FITTING, LOCATE NEW FITTING DRILL REAMED EXISTING HOLES IN FITTING IAW DC-8 SRM 51-3-2 AND INSTALLED IAW DC-8 SRM 51-1 -20D,CPCP.Apr 19, 1999 · N819UP · Doug DC873FSDR UPS99229372Chord · crackedINSPECTION TYPE:SI, UPPER RIB FLANGE CRACKED AT LT WING (FUEL TANK) UPPER STRINGER NR 16 WS 171.5. REMOVED AND REPLACED CHORD PER SRM 51-30-2. CHORD REPLACEMENT LOCATED AT UPPER STRINGER 16 WS 171.5 AT LT WING.Apr 19, 1999 · N937UP · Boeing 72725CSDR UPS99229371Chord · crackedINSPECTION TYPE:SI, RT WING TANK UPPER CHORD CRACKED AT STRINGER 21 STA 171.5. REMOVED AND REPLACED THE CHORD IAW SRM 51-30-2. CHORD REPLACEMENT LOCATED AT RT WING, STRINGER 21 WS 171.5.Apr 19, 1999 · N937UP · Boeing 72725CSDR RAIA990428Screw · incorrect partFLT 7364 - STL - 15 DEGREES HEADING SPLIT. MAINTENANCE REMOVED MAGNETIC SCREWS AND INSTALLED NON-MAGNETIC SCREWS IN BOTH WING TIPS. (M)Apr 19, 1999 · N875JX · Bag JETSTM3201SDR ABXA990393Splice · corrodedDURING D-CHECK, FOUND RIGHT WING LOWER SPAR CAP SPLICE CORRODED. REPLACED SPLICE IAW DC9 SRM 51-30-5.Apr 19, 1999 · N974AX · Doug DC941SDR ABXA9900394Fitting · crackedDURING D-CHECK, FOUND SLAT ACTUATOR ASSEMBLY INBOARD MOUNT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.Apr 19, 1999 · N974AX · Doug DC941SDR AALA990560Splice · corrodedTUL - FOUNS STRINGER SPLICE CORRODED. INSTALLED NEW STRINGER SPLICE AT STATION 680 STRINGER 27L PER SRM 51-10-1. (M)Apr 16, 1999 · N6835 · Boeing 727223SDR 99ZZZX1922Bolt · misinstalledWHILE C/W 5 YEAR WING BOLT INSPECTION, FOUND FITTINGS DAMAGED DUE TO IMPROPER INSTALLATION OF RIGHT, LOWER, FORWARD AND LEFT, LOWER FORWARD WING BOLTS. WASHERS WERE INSTALLED BACKWARDS WHICH DEFORMED THE WING FITTINGS.Apr 15, 1999 · N86FD · Beech B100SDR ABXA9900399Splice · corrodedDURING D-CHECK, FOUND LEFT WING UPPER SPAR CAP SPLICE CORRODED LEVEL 2 CORROSION. REPLACED T-ANGLE IAW DC9 SRM 51-10-4 AND DACO DWG NR 9910010.Apr 14, 1999 · N974AX · Doug DC941SDR ABXA9900313Angle · corrodedDURING C-CHECK, FOUND RIGHT TRAPEZOIDAL PANEL ATTACH ANGLE EXFOLIATED. REPLACED ATTACH ANGLE IAW DC9 SRM 57-30-1.Apr 14, 1999 · N943AX · Doug DC931SDR ABXA9900311Doubler · corrodedFOUND RIGHT WING TRAILING EDGE DOUBLER CORRODED JUST INBOARD OF INBOARD SPOILER PANEL. REPLACED DOUBLER IAW DACO DWG 5912156 AND DC9 SRM 57-31-3.Apr 14, 1999 · N943AX · Doug DC931SDR ABXA9900310Tip · corrodedDURING C-CHECK, FOUND RIGHT WING TIP, UPPER AND LOWER INTERIOR SURFACE CORRODED. REPLACED WING TIP.Apr 14, 1999 · N943AX · Doug DC931SDR CALA9900400Angle · crackedINSPECTION FOUND A 2.75 INCH CRACK IN LT WING REAR SPAR O/B SUPPORT ANGLE WHERE NR 2 SPOILER ACTUATOR AND FLAP DRIVE CASTING MOUNTS. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.Apr 13, 1999 · N17402 · Boeing 727243SDR 99T64R255ARWeb · damagedNR 2484 - LT FLAP WELL WEB DAMAGED XCW 69.5 BS 980 - BS 1020. REMOVED WEB, FABRICATED NEW WEB AND INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)Apr 13, 1999 · N1808E · Doug DC862SDR 99ZZZX1785Retainer · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON RIGHT WING TRAILING EDGE PANEL SEAL RETAINER (APPROXIMATELY WS 220).Apr 12, 1999 · N79754 · Boeing 727227SDR UPS99829525Fitting · crackedINSPECTION TYPE:C3 INBD SIDE OF THE XRS 74.5 BULKHEAD, THE STR 51 FWD END FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20 AND 51-1-23.Apr 9, 1999 · N840UP · Doug DC873FSDR UPS99829454Fitting · crackedINSPECTION TYPE:C3, RT WING O/B OF THE XRS 74.5 BULKHEAD, BOTH STRINGER 51 END FITTINGS ARE CRACKED. REMOVED AND REPLACED FITTINGS IAW SRM 51-1-20D AND 51-3-0.Apr 9, 1999 · N840UP · Doug DC873FSDR UPS99829397Fitting · crackedINSPECTION TYPE:C3 INBD SIDE OF THE STA XRS 74 BULKHEAD, THE STRINGER 51 AFT END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.Apr 9, 1999 · N840UP · Doug DC873FSDR DL72L990775Stiffener · cracked1.25 CRACK ON NR 7 SLAT I/B TRACK O/B SPAR STIFFENER. REPAIRED PER MM 57-20-21.Apr 9, 1999 · N501DA · Boeing 727232SDR UPS99829412Angle · crackedINSPECTION TYPE:C3 LT WING INBD L/E UPPER INBD AFT L/E ATTACH ANGLE IS CRACKED, STA XFS 7.5. REMOVED, FABRICATED, AND INSTALLED ANGLE IAW DWG 5269646 AND SRM 51-3-0.Apr 8, 1999 · N840UP · Doug DC873FSDR UPS99829395Clip · crackedINSPECTION TYPE:C3 LT WING UPPER L/E RIB, ABOVE THE NR 2 PYLON STA XW 239, THE FWD ATTACH CLIP IS CRACKED. REMOVED, FABRICATED, AND INSTALLED CLIP IAW DWG 9753294 AND SRM 51-1-20D.Apr 8, 1999 · N840UP · Doug DC873FSDR UPS99829393Doubler · crackedINSPECTION TYPE:C3 LT WING L/E AT XFS 598, THE LWR SKIN T/E DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND INSTALLED DOUBLER IAW DWG 5641255 AND SRM 51-1-21.Apr 8, 1999 · N840UP · Doug DC873FSDR AU990772Stiffener · corroded(AUS) RIGHT WING FRONT SPAR STIFFENER CONTAINED LEVEL 2 CORROSION.Apr 8, 1999 · Boeing 72777CSDR AALA990507Angle · corrodedTUL - FOUND UPPER SURFACE OF LOWER CHORD ON RIGHT WING L/E BELOW NR 6 SLAT ACT HAS HEAVY CORROSION. REPAIRED PER AARD 57-30-00-2 PAGE 1. (M)Apr 7, 1999 · N862AA · Boeing 727223SDR 99ZZZX1815Bracket · crackedDURING A PHASE INSPECTION, FOUND THAT THE RIGHT MAIN GEAR OUTBOARD UPLOCK HOOK STEEL BRACKET WAS UPWARD TO THE END OF BRACKET. INSTALLED NEW BRACKET.Apr 7, 1999 · N88834 · Cessna 441SDR UPS99829293Fitting · crackedINSPECTION TYPE:C1 WING STA XRS74.0, THE STR 51 END FITTING IS CRACKED (LT WING). REMOVED AND REPLACED FWD AND AFT END FITTINGS IAW DWG 3704841 AND SRM 51-1-20D.Apr 6, 1999 · N797UP · Doug DC871FSDR UPS99829288Fitting · crackedINSPECTION TYPE:C1 RT WING, THE STRINGER 51 END FITTING AT STA XRS74.00 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.Apr 6, 1999 · N797UP · Doug DC871FSDR 99T64R254ARWeb · damagedNR 1253 - RT INBOARD FLAP WELL WEB, FASTENERS PULLED THROUGH XCW 69.5 BS 980 - BS 1020. REMOVED WEB, FABRICATED NEW WEB AND INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)Apr 6, 1999 · N1808E · Doug DC862SDR UPS99829423Fitting · crackedINSPECTION TYPE-C3, RT WING T/E AT WS 5.812. THE FLAP SUPPORT FITTING ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE IAW DWG 4652201 AND SRM 51-1-20D AND 51-3-0.Apr 4, 1999 · N840UP · Doug DC873FSDR UPS99829413Doubler · crackedINSPECTION TYPE:C3 LT WING L/E SKIN ABOVE THE NR 2 PYLON HAS A CRACKED REPAIR DOUBLER. REMOVED, FABRICATED REPAIR DOUBLER IAW SRM 57-2-1A FIG 1.Apr 4, 1999 · N840UP · Doug DC873F
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