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 CALA9801716Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN OUTBOARD TRAILING EDGE ATTACH ANGLE AT RT WING NR 8 FLAP TRACK. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-40-3, 51-10-2, AND MM 51-20-11.Sep 12, 1998 · N14788 · Boeing 727232SDR UPS98827875Bracket · crackedINSPECTION TYPE-C2, RT WING LEADING EDGE NR 3 PNEU SHUT-OFF AFT ATTACH BRACKET AT XW223 CRACKED. REMOVED BROKEN BRACKET IAW DC8 SRM 51-3-0. MAT ID FOR NEW BRACKET 302 STAINLESS STEEL .063 IN ANNEALED CONDITION IAW DAC DWG NR 5802881 AND DC8 SRM 51-9-0. FAB Sep 11, 1998 · N798UP · Doug DC871FSDR CALA9801714Beam · corrodedINSPECTION FOUND CORROSION IN BOLT HOLES OF LT MLG ATTACH BEAM. REPAIRED IAW DOUGLAS DRAWINGS 90-57-1017 AND 90-57-1018.Sep 11, 1998 · N68060 · Doug DC1030SDR CALA9801713Beam · corrodedINSPECTION FOUND CORROSION IN UPPER HOLES OF RT MLG WING ATTACH BEAM. REPAIRED IAW DOUGLAS DRAWINGS 90-57-1017 AND 90-57-1018.Sep 11, 1998 · N68060 · Doug DC1030SDR CALA9801705Angle · crackedINSPECTION FOUND A 4 INCH CRACK IN ANGLE AND DOUBLER AT RT WING FIXED LEADING EDGE RIB AT SLAT STA 0. THE DOUBLER WAS REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND 51-40-3, FSep 10, 1998 · N93738 · Boeing 727224SDR CALA9801700Pad · corrodedINSPECTION FOUND BOTTOM SURFACE OF SPOILER BEAM PAD CORRODED WHERE NR 3 FLAP TRACK MOUNTS. THE FLAP TRACK MOUNT PAD WAS REMOVED AND REPLACED IAW SRM 51-10-2, PAGE 1 AND 51-30-2, PAGE 14.Sep 10, 1998 · N93738 · Boeing 727224SDR CALA9801687Beam · crackedINSPECTION FOUND A .375 INCH CRACK IN RT WING J BEAM FORWARD OF SPOILER NR 8 ACTUATOR MOUNT FITTING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW ECRA 5750-07914.Sep 10, 1998 · N15790 · Boeing 727232SDR DL72S981868Stiffener · crackedFOUND ON F1 LETTER CK, NR 6 SLAT O/B TRACK O/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21.Sep 9, 1998 · N528DA · Boeing 727232SDR C2XA98IA331Support · crackedIAH - DURINC C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT BRACKET NR 1 AT RIB 21 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,16Sep 8, 1998 · N22727 · Emb EMB120RTSDR C2XA98IA330Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT BRACKET NR 2 AT RIB 22 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,16Sep 8, 1998 · N22727 · Emb EMB120RTSDR C2XA98IA329Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT BRACKET NR 3 AT RIB 22 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT BRACKET IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TCSep 8, 1998 · N22727 · Emb EMB120RTSDR C2XA98IA328Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT BRACKET NR 2 AT RIB 21 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,16Sep 8, 1998 · N22727 · Emb EMB120RTSDR UPS98827702Doubler · crackedINSPECTION TYPE-C, LT WING NR 2 MAIN TANK AFT UPPER ACCESS PANEL DOUBLER IS CRACKED. REPAIRED AREA IAW SRM 57-2-1 FIG 36.Sep 3, 1998 · N709UP · Doug DC871FSDR DHL9870829CAngle · crackedAT C-CHECK, L/W LE SLAT FRONT SPAR CAVITY UPPER WEB SUPPORT ANGLE IS CRACKED AT UPPER CORNER WS 344. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-10-1, 3 X 18. N/R 1696Sep 3, 1998 · N708DH · Boeing 72725SDR DHL9870828CAngle · crackedAT C-CHECK, RT WING I/B L/E COVE WBL 92.8 ANGLE REPAIR JUST BELOW TOP SKIN CRACKED. REMOVED ANGLE AND REPLACED PER SRM 51-30-2, 16 X 6. N/R 2374Sep 3, 1998 · N708DH · Boeing 72725SDR DHL9870827CWeb · crackedAT C-CHECK, RT WING LOWER L/E ANGLE TO WEB CRACKED 2 PLACES WBL 92.8. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 25 X 2 X 2. N/R 2375Sep 3, 1998 · N708DH · Boeing 72725SDR AALA981636Angle · corrodedTUL - THREE INCH CORROSION SPOT LOWER CHORD BOTTOM SIDE SURFACE AT NR 8 FLAP TRACK ATTACH AREA REAR SPAR. REMOVED CORROSION, ALODINED AND PRIMED. INSTALLED 2024 T-3 .071 THICK DOUBLER USING EXISTING PATTERN, THREE ROWS HIGH LOCKS .375 AROUND BLEND AREA, REF Sep 3, 1998 · N889AA · Boeing 727223SDR 98ZZZX3671Angle · corrodedDURING ROUTINE INSPECTION, SEVERAL AREAS OF INTERGRANULAR CORROSION IN UPPER SPAR ANGLES P/N 0523020-1 AND 2 WERE DISCOVERED. AFTER REMOVAL, THE ANGLES WERE BROKEN IN TWO WITH LIGHT HAND PRESSURE. DETECTION WAS DIFFICULT AS THERE ARE VERY FEW INSPECTION HOLESep 1, 1998 · N7248A · Cessna 172SDR RAAA98E9021Angle · brokenDURING SCHEDULED NR 3 CHECK WHILE GAINING ACCESS TO REPAIR FUEL LEAK (M-54 NR 11), RT MLG RIB FORGING LOWER NR 4 WING PANEL ATTACH ANGLE INADVERTENTLY BROKEN OFF AT WS 167. REPAIRED PER LDS DWG 188339. M-54 NR 293.Aug 29, 1998 · N1968R · Lkheed 188CSDR UPS98827674Angle · crackedINSPECTION TYPE:C, LT WING L/E I/B SLOT BOX, O/B AFT VERTICAL ANGLE IS CRACKED AT THE BOTTOM, (STA.XS246.089). REMOVED AND REPLACED ANGLE IAW DWG 9753293.Aug 28, 1998 · N706UP · Doug DC871FSDR UPS98827660Angle · crackedINSPECTION TYPE:C RT WING I/B SLOT O/B VERTICAL ANGLE CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20 AND DWG 9753293.Aug 28, 1998 · N706UP · Doug DC871FSDR UPS98827678Doubler · crackedINSPECTION TYPE-C, RT WING FUEL TANK ACCESS PANEL LAND IS CRACKED AT THE AFT O/B CORNER (XCW 78.5). REPAIRED AREA IAW SRM 57-2-1 FIG 36.Aug 27, 1998 · N706UP · Doug DC871FSDR P5CA9801370Beam · crackedLEFT WING TRAILING EDGE BEAM UPPER CHORD INBOARD END CRACKED. REPAIRED PER SRM 51-40-14 FIG 2.Aug 27, 1998 · N859FT · Boeing 747123SDR CALA9801576Channel · crackedINSPECTION FOUND A 1.25 INCH CRACK IN CHANNEL INSIDE TRAILING EDGE AT UPPER SKIN OUTBOARD END OF AFT FALSE SPAR ABOVE NR 3 FLAP TRANSMISSION. A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-2.Aug 27, 1998 · N32725 · Boeing 727224SDR CALA9801553Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN J BEAM AT CUTOUT AREA ABOVE NR 7 SPOILER. THE J BEAM WAS REPAIRED IAW ECRA 5780-02914.Aug 27, 1998 · N32725 · Boeing 727224SDR CALA9801546Angle · crackedINSPECTION FOUND LT WING INBOARD NR 7 SPOILER ACTUATOR SUPPORT FITTING LOWER ANGLES (TWO EACH) RIB PANEL SUPPORTS CRACKED. THE CRACKS WERE .5 INCH LONG. THE INBOARD AND OUTBOARD ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-10-1 AND 51-30-2.Aug 27, 1998 · N32725 · Boeing 727224SDR CALA9801538Beam · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING TRAILING EDGE J BEAM JUST ABOVE NR 8 SPOILER MOUNT. REPAIR PARTS WERE INSTALLED IAW ECRA 5720-01676.Aug 26, 1998 · N32725 · Boeing 727224SDR CALA9801534Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN L-ANGLE OF LT WING J-BEAM ABOVE NR 7 SPOILER ACTUATOR. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-1, PAGE 4 AND 51-30-2.Aug 26, 1998 · N66734 · Boeing 727224SDR CALA9801533Chord · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LOWER FORWARD CHORD OF LT WING BELOW NR 7 SPOILER ACTUATOR. THE CRACKED SECTION WAS CUT OUT, A REPAIR WAS INSTALLED IAW ECRA 5720-01675.Aug 26, 1998 · N66734 · Boeing 727224SDR CALA9801530Chord · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RT WING TRAILING EDGE LOWER CHORD AT NR 8 SPOILER ACTUATOR CASTING. THE CRACKED SECTION OF CHORD WAS REMOVED IAW SRM 51-30-2. A REPAIR WAS INSTALLED IAW SRM 51-10-1 AND ECRA 5720-01675.Aug 26, 1998 · N66734 · Boeing 727224SDR ABXA9800858Angle · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND THE INBOARD ATTACH ANGLE FOR THE CENTER BUTE DOOR CRACKED AT RIGHT WING STATION 164 HINGE BRACKET. REPLACED ATTACH ANGLE IAW DC9 SRM CHAPTER 51-30-01.Aug 26, 1998 · N903AX · Doug DC932SDR ABXA9800857Door · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT WING INBOARD BUTE DOOR CRACKED AT INBOARD CAM ROLLER. REPLACED LEFT INBOARD BUTE DOOR IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-2.Aug 26, 1998 · N903AX · Doug DC932SDR UPS98627570Angle · crackedINSPECTION TYPE:ETOP LEFT WING NR 6 SLAT LOWER TE COVE SUPPORT ANGLES CRACKED AT POSITIONS 3, 4, 5, 6 AND 7 FROM OUTBOARD END. REMOVED CRACKED SUPPORT ANGLES, FABRICATED AND INSTALLED NEW SUPPORT ANGLES IAW SRM 51-30-01, SRM 51-21-01, SRM 51-40-02.Aug 25, 1998 · N310UP · Boeing 76734AFSDR CALA9801519Bracket · crackedINSPECTION FOUND A 0.4 INCH CRACK IN RT WING LEADING EDGE FLAP NR 6 ACTUATOR MOUNT BRACKET. THE MOUNT BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-1.Aug 25, 1998 · N66734 · Boeing 727224SDR CALA9801518Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN J-BEAM APPROXIMATELY 1.5 INCHES ABOVE NR 7 SPOILER ACTUATOR AT CUTOUT ABOVE INBOARD END OF AFT FALSE SPAR. PANELS AND A FITTING WERE REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5740-02914 AND SRM 51-10-2, AND 51-10-6. THE Aug 25, 1998 · N66734 · Boeing 727224SDR CALA9801516Angle · crackedINSPECTION FOUND LT WING FORWARD RIB ATTACH ANGLE CRACKED AT WS 92.8. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 57-20-2, 51-10-2, AND 51-30-2.Aug 25, 1998 · N14788 · Boeing 727232SDR CALA9801515Angle · crackedINSPECTION FOUND TWO .625 INCH CRACKS IN RT WING TRAILING EDGE SUPPORT ANGLE UNDER NR 13 SPOILER OUTBOARD END AT SUPPORT ROD LOWER ATTACH POINT. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-10-2 AND 51-30-2.Aug 25, 1998 · N14788 · Boeing 727232SDR AU981040Angle · cracked(AUS) SPAR CAP ANGLE CRACKED BEYOND THE STOP DRILL HOLE. PART TC: 7,384.Aug 25, 1998 · Parten P68BSDR DL72S981730Chord · crackedDURING ACCOMPLISHMENT OF 4-58560-3AD, A CRACK WAS FOUND IN THE VERT FLANGE OF THE WING TO FUSELAGE UPPER ATTACH CHORD. CRACK PROPAGATES FROM THE EDGE OF THE CHORD ABOVE THE TWO FWD MOST FASTENER HOLES AND TRAVELS DOWN. REPAIRED PER ERA 332062-14AD.Aug 21, 1998 · N405DA · Boeing 727232SDR ABXA9800779Angle · crackedRIGHT WING LEADING EDGE INTERIOR, VERTICAL STIFFENER ANGLE IS CRACKED AT BOTTOM OUTBOARD END OF INBOARD SLOT BOX STATION XS 250.089. REPLACED ANGLE IAW DWG 9753293 AND DC8 SRM 51-1-20 AND 51-1-21.Aug 21, 1998 · N803AX · Doug DC862SDR 99ZZZX2688Stiffener · crackedLEFT WING TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 5 AND 6 IS CRACKED AT FORWARD END. REPAIRED IAW BAE RDO DJR/RJ0630-98. REF: W/C 5035 FOR ALODINE PRIME AND PAINT.Aug 21, 1998 · N610AW · Bag BAE146200ASDR 99ZZZM480Screw · damagedRIGHT WING SHORT STALL BAR PULLING OVER CORNER MOUNT SCREWS. REPAIRED SCREWS AS REQ'D IAW AVRO FAX DJR/RJO638-98, GCB/RJ1344-94, JEN/RJ1331-94. OK FOR SERVICE IAW BAE 146 MM. (M)Aug 21, 1998 · N610AW · Bag BAE146200ASDR CALA9801495Stiffener · crackedINSPECTION FOUND STIFFENER CRACKED AT LT WING TRAILING EDGE FALSE SPAR WHERE FLAP TRACK NR 3 IS LOCATED. THE STIFFENER WAS REMOVED IAW SRM 51-30-2. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2, AND 51-30-2.Aug 20, 1998 · N14788 · Boeing 727232SDR C2XA98IA317Support · crackedIAH - DURING C-CHEC INSPECTION, THE NR 4 FROM AFT UPPER SKIN SUPPORT ON RIB 15 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. Aug 20, 1998 · N51726 · Emb EMB120RTSDR 99ZZZX2689Stiffener · crackedLEFT WING TOP WING STIFFENER AFT OF REAR SPAR BETWEEN RIBS 8 AND 9 IS CRACKED AT FORWARD ENG. REPAIRED IAW BAE RDO EJR/RJ0630-98. REF: W/C 5035 FOR ALODINE, PRIME AND PAINT.Aug 20, 1998 · N610AW · Bag BAE146200ASDR 99ZZZX2675Angle · crackedLEFT WING T/E, LOWER SHROUD STIFFENER, AND AFT TAG ANGLE CRACKED BETWEEN RIBS 7 AND 8. REPLACED LEFT WING T/R LOWER SHROUD STIFFENER AND AFT TAG ANGLE BETWEEN RIBS 7 AND 8.Aug 20, 1998 · N610AW · Bag BAE146200ASDR 98ZZZX3257Winglet · damagedWINGLET, 0012L, LEFT WING ATTACH HARDWARE. WINGLET WAS BEING REPLACED BECAUSE OF DAMAGE AND THE ATTACH HARDWARE WAS SEVERELY CORRODED. SUSPECT WATER INTRUSION INTO SEALED AREA. INSTALLED NEW WINGLET AND SEALED IAW MFG PROCEDURES. PARTS REPLACED: BOLT P/N Aug 20, 1998 · N308HG · Gulstm G1159ASDR DL72S981705Chord · crackedUPPER CHORD ANGLE OF THE RT WING AT WS 171.5 WAS FOUND WITH TWO CRACKS. THE CRACKS WERE LOCATED AT FASTENER HOLES ON THE HORIZ FLANGE OF THE CHORD ANGLE UNDER STRINGERS 16 AND 19. ALSO, THE S18 TAB WAS CRACKED. REPAIRED PER ERA 332040-14.Aug 19, 1998 · N405DA · Boeing 727232SDR RRXA98386Trap Panel · damagedDURING GROUND SERVICE, FOUND AILERON BUS CABLE CUT THROUGH LEFT SIDE OF TRAPEZOIDAL PANEL, (P/N 5616481), LEFT WHEEL WELL AT STA 865. REMOVED AND REPLACED CABLE SECTION. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH Aug 18, 1998 · N2674U · Doug DC873FSDR QXEA9801180Fairing · dentedDENT IN SKIN PLANE FAIRING WEB RIGHT-HAND LOWER WING APPROXIMATELY STATION 1800. REPAIRED IAW HORIZON AIR EA 4-57-138.Aug 18, 1998 · N498US · Fokker F28MK4000
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