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 UPS00831717Doubler · crackedINSPECTION TYPE:C123, RIGHT WING L/E INTERNAL DOUBLER WAS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER IAW DWG 6769600 AND SRM 51-1-21, 51-1-20D.Jan 26, 2000 · N707UP · Doug DC871FSDR UPS00831683Angle · crackedINSPECTION TYPE:C123 RIGHT WING L/E RIB ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753294, AND SRM 51-1-20D.Jan 26, 2000 · N707UP · Doug DC871FSDR UPS00831578Doubler · crackedINSPECTION TYPE:C123 RIGHT WING L/E INTERNAL DOUBLER IS CRACKED AT XW 257. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21, 51-1-21A.Jan 26, 2000 · N707UP · Doug DC871FSDR UPS00831528Doubler · crackedINSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-21, 51-1-20D.Jan 26, 2000 · N707UP · Doug DC871FSDR UPS00831523Doubler · crackedINSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER WAS CRACKED AT XFS297.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D, 51-1-21.Jan 26, 2000 · N707UP · Doug DC871FSDR UPS00831519Doubler · crackedINSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-21, 51-1-20D.Jan 26, 2000 · N707UP · Doug DC871FSDR 00FDEA00036Fastener · corrodedSNRM #N00581 - RIGHT WING LWR SKIN SURFACE DOUBLER STRAP AT BS XOR & 264 & INNER REAR SPAR APPROX. HAS A CORRODED SHEARED FASTENER. ** S/D ** REMOVED FASTENER, EDDY CURRENTED SURFACE INSP WAS COMPLIED WITH. INSTALL & TORQUED BOLT PER DPS 3.67-60 & MM 20-5Jan 26, 2000 · N391FE · Doug DC1010FSDR UPS00831674Angle · crackedINSPECTION TYPE:C123 LEFT WING L/E RIB EXTENSION ANGLE IS CRACKED AT XW 223. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5769859, AND SRM .51 -1-20DJan 25, 2000 · N707UP · Doug DC871FSDR UPS00831522Doubler · crackedINSPECTION TYPE:C123, LEFT WING CENTER L/E INTERNAL DOUBLER CRACKED AT XFS 335.25. REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER IAW DWG 5769589, SRM 51-1-21.Jan 25, 2000 · N707UP · Doug DC871FSDR QXEA0000459Bracket · crackedPDX - RIGHT-HAND WING LOWER SUPPORT BRACKET AT STATION 1700 WAS CRACKED PAST RIVET BELOW PANEL 92L. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-01.Jan 25, 2000 · N477AU · Fokker F28MK4000SDR AALA2000370Casting · corrodedTUL - RIGHT WING AFT BOTTLE BOTL CASTING HAS SEVERAL DEEP PITS IN AFT BUSHING AREA AT CASTING. BORED RIGHT AFT CASTING TO REMOVED CORROSION PER ESO 11697 DATED 1/20/200. INSTALLED BUSHING WITH SLEEVE. (M)Jan 25, 2000 · N892AA · Boeing 727223SDR UPS00831610Stiffner · crackedINSPECTION TYPE:C123 RIGHT WING L/E AT STA XS246.313 FRONT VERTICLE STIFFENER ANGLE IS CRACKED. REPAIRED IAW SRM 57-6-2 FIG 2.Jan 24, 2000 · N707UP · Doug DC871FSDR UPS00831605Stiffner · crackedINSPECTION TYPE:C123 RIGHT WING T/E AT FLAP HINGE STA 97 INBD VERTICLE STIFFENER IS CRACKED. REMOVED AND REPLACED STIFFENER IAW DWG 3643319, AND SRM 51-1-20D.Jan 24, 2000 · N707UP · Doug DC871FSDR ABXA000086Support · crackedRIGHT WING INBOARD SPOILER OUTBOARD SPOILER SUPPORT CRACKED. REPLACED SUPPORT FITTING IAW DC9 SRM 51-30-1.Jan 21, 2000 · N964AX · Doug DC941SDR 2000ZZZX565Weight Assy · corrodedFOUND EXTENSIVE CORROSION ON BOTH STEEL PARTS OF THIS ASSEMBLY DURING 100-HOUR INSPECTION.Jan 21, 2000 · N9436C · Piper PA28R201SDR RRXA000086Tube · failedDURING A MAINTENANCE VISIT FOUND TUBING CRUSHED, RIGHT WING, L/E I/B SECTION ELEC CONDUIT TUBING RUN KWD AT STA XFS 193. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 20, 2000 · N792FT · Doug DC873FSDR RRXA000085Cap · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LWR AFT CAP CRACKED XRS 358 NR 1 MAIN TANK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM.. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 20, 2000 · N792FT · Doug DC873FSDR ABXA000085Bracket · crackedRIGHT WING OUTBOARD SPOILER OUTBOARD SUPPORT CRACKED. REPLACED OUTBOARD SPOILER SUPPORT BRACKET IAW 51-30-2 AND 51-30-5.Jan 20, 2000 · N964AX · Doug DC941SDR RRXA000044Angle · crackedDURING A MAINTENANCE VISIT, FOUND CRACK, RIGHT WING, I/B FLAP INSIDE HINGE CUTOUT (WEDGE) ATTACH ANGLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 18, 2000 · N792FT · Doug DC873FSDR RRXA000042Rivet · missingDURING A MAINTENANCE VISIT, FOUND RIVET MISSING, TOP CENTER SECTION, RIGHT WING, L/E AT STA XFS 315.600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 18, 2000 · N792FT · Doug DC873FSDR DHL200080307CSupport Bracket · crackedAT C-CHECK, RT WING L/E DUCT SUPPORT SHOWS 2 CRACKS OF 1 INCH AND 1.5 INCH LENGTH AT WS 622.500. INSTALLED DOUBLER REPAIR PER SRM 53-20 PAGE 9 AND 10.Jan 18, 2000 · N803DH · Doug DC873FSDR RRXA000040Fitting · gougedDURING A MAINTENANCE VISIT FOUND GOUGE, RIGHT WING, RT O/B NR 3 FLAP CANOE FITTING GOUGED AND CHAFFED ON BOTH SIDES (EO).. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 17, 2000 · N792FT · Doug DC873FSDR DHL200071771DStiffener · crackedAT D-CK, WING CENTER SECTION INTERIOR FRONT SPAR, CRACK INDICATIONS ON VERT STIFFENER TIE CLIPS TO UPPER SPAR CHORD AT RBL 25.0 AND RBL 45.61. REMOVED AND REPLACED VERTICAL STIFFENER AT STA 740 RBL 25, PER B727 SRM 51-30-2 AND TIE CLIP AT BS 740 RBL 25 AND RBJan 16, 2000 · N717DH · Boeing 72723SDR DHL200071788DStiffener · crackedAT D CK, LW PANEL STIFFENER CRACKED AT LOWER REAR SPAR CHORD AREA WS. 247. REMOVED AND REPLACED STIFFENER PER B727 SRM 51-30-2. REF: N/R 1672.Jan 15, 2000 · N717DH · Boeing 72723SDR TWAA0001607Rivet · corrodedTHE LEFT WING HAD 48 RIVETS WITH CORROSION REMOVED PER SRM 57-20-01 FIG 101. ONE RIVET REMOVED AND REPLACED AT STRINGER 4 WBL 326, ONE RIVET REMOVED AND REPLACED AT S-5 WBL 333. ONE RIVET REMOVED AND REPLACED AT S-5 WBL 328 PER SRM 51-40-02, PAGE 9. CHECK-CJan 14, 2000 · N701TW · Boeing 7572Q8SDR DHL200071776DWeb · crackedAT D CK, NR 4 SLAT OUTBOARD HOOK CAVITY IN WING IS CRACKED AT AFT OUTBOARD CORNER. STOP DRILLED CRACK AT NR 4 SLAT OUTBOARD HOOK CAVITY PER B727 SRM 51-10-1, VISUALLY INSPECTED, NO FURTHER CRACK NOTED. INSTALLED REPAIR AT NR 4 SLAT OUTBOARD HOOK CAVITY PER BJan 14, 2000 · N717DH · Boeing 72723SDR DHL2000717110Angle · crackedAT D CHECK, LEFT WING NR 4 SPOILER ACTUATOR MOUNT CASTING I/B VERTICAL SUPPORT ANGLE CRACKED AT LOWER MOUNT BOLT. REMOVED SPOILER ACTUATOR, AND CASTING SUPPORT. REPLACED VERTICAL ANGLE SUPPORT PER SRM 51-30-2. REINSTALLED REMOVED PARTS PER MM 27-61-81. N/RJan 14, 2000 · N717DH · Boeing 72723SDR DHL200071759DFairing · crackedAT D-CK, NR 5 FLAP TRACK MOVEABLE FAIRING FWD END IS CRACKED. CUTOUT DAMAGED AREA ON NR 5 FLAP TRACK FAIRING PER B727 SRM 51-10-1. INSTALLED REPAIR DOUBLER ON FWD END OF FAIRING PER B727 SRM 51-40-2. REF: N/R 2848.Jan 13, 2000 · N717DH · Boeing 72723SDR DHL200071743DBracket · corrodedAT D-CK, LEFT O/B MID FLAP PULLEY BRACKET FOR FORE FLAP TRACK, CORRODED FLAP STA WBL 317, MID FLAP T/E. REMOVED AND REPLACED PULLEY BRACKET PER B727 SRM 51-30-2. REF: N/R 1680.Jan 13, 2000 · N717DH · Boeing 72723SDR UPS00831632Doubler · crackedINSPECTION TYPE:C1 RIGHT WING L/E AT STA XFS 335.250 INTERNAL DOUBLER IS CRACKED. REMOVED, FABRICATED, AND REPLACED IAW DWG 5718963, AND SRM 51-1-21, 51-1-20D.Jan 11, 2000 · N703UP · Doug DC871FSDR UPS00831663Stiffner · crackedINSPECTION TYPE:C1 RIGHT WING L/E VERTICLE STIFFENER (OTBD END OF SLOT) IS CRACKED AT XS250.089. REMOVED, FABRICATED, AND REPLACED STIFFENER IAW DWG 9753293, AND SRM 51-1-21, 51-1-20D.Jan 9, 2000 · N703UP · Doug DC871FSDR UPS00831443Doubler · corrodedINSPECTION TYPE:C1, INTERNAL DOUBLER CORRODED RIGHT WING L/E AT XFS 372.750. REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER IAW DWG 5641253, AND SRM 51-1-21, 51-1-20D.Jan 9, 2000 · N703UP · Doug DC871FSDR RRXA003371Vane · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT INBD SLOT VANE INBD LWR CORNER AT XILO.7095, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21, 51-3-0,Jan 7, 2000 · N831AL · Doug DC873FSDR UPS00431748Fitting · crackedINSPECTION TYPE:C 44, LEFT HAND WING NR 2 MAIN FUEL TANK WS 586 REAR SPAR FITTING HAD A 2 INCH CRACK APPROX AT UPPER RADIUS. REPAIR PER QUERY NOTE 2/200 0 REPLY. ACCOMPLISHED TEMPORARY REPAIR IAW EO B747-5720-10909 AAENDUM TO UPS SRM. NOTE REPAIR MUST BE REJan 7, 2000 · N674UP · Boeing 747123SDR RRXA000003Fitting · gougedDURING A MAINTENANCE VISIT FOUND GOUGE, FLAP CANOE FITTING ON I/B SIDE FROM ICE BRAKER ROD BOLT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED DAMAGE AREA ORIGINAL THICKNESS .300, AFTER BLEND OUT .227. ACCEPTJan 5, 2000 · N792FT · Doug DC873FSDR UPS00231382Support · crackedINSPECTION TYPE:C LEFT WING FIXED LEADING EDGE CAVITY VERTICLE OUTBOARD SUPPORT IS CRACKED FOR THE NR 2 SLAT INBOARD TRACK, INBOARD SUPPORT RIB. REPLACED LEFT WING FIXED LEADING EDGE CAVITY VERTICAL OUTBOARD SUPPORT AS PER SRM 57-20-03 FIG 2. MATERIAL USED 7Jan 5, 2000 · N906UP · Boeing 72730CSDR QXEA0000120Bracket · crackedPDX - RIGHT-HAND WING FALSE SPAR HAD A BRACKET CRACKED, VIEWED THROUGH 82X DOWN AND AFT AT CENTER STIFFENER FOR APERATURE. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-04.Jan 5, 2000 · N476US · Fokker F28MK4000SDR TWAA0001606Rivet · corrodedTHE RT WING HAD 126 RIVETS WITH CORROSION AT TOP WING SKIN FROM WBL 300 TO WBL 336, FROM FRONT SPAR TO REAR SPAR. REMOVED CORROSION PER SRM 57-20-01, FIG 106. SEVEN FASTENERS REPLACED PER SRM 51-40-02, PAGE 9 AT STRINGER 2, WBL 317, WBL 308, AFT SPAR AFT ROWJan 4, 2000 · N701TW · Boeing 7572Q8SDR TWAA0000614Bracket · missingDURING OP 16 MAINT CHECK, RT WING TE NEED INSTALL RIB ASSEMBLY OTBD OF CENTER FLAP HINGE ASSEMBLY AFTER FLAP BRACKET INSTALLED. INSTALLED RIB ASSEMBLY USING HI-LOCKS PER SRM 51-30-5 AND RIVETS PER SRM 51-30-2.Dec 30, 1999 · N925L · Doug DC932SDR ABXA000175Bolt · brokenLEFT WING LOAD FITTING BOLT BROKEN. (REF: S/B 767-57A064 AND AD 99-19-29). REPLACEDBOLT AND REPAIRED FITTING IAW ABX REA B653-34274MR AND BOEING FAX ABX-ILN-99-00410H.Dec 29, 1999 · N785AX · Boeing 767281SDR TWAA0000612Bolt · corrodedDURING OP 16 MAINT CHECK, FOUND ON RT WING TE, RUST EMITTING FROM TOP INBD BOLT OF CENTER FLAP HINGE CASTING AT REAR SPAR. ACCOM HIGH FREQ EDDY CURRENT OF HOLES AND AREA PER TWA NDT 51-00-03, PART 6, AND 2 EA CRACKS FOUND. INSTALLED 4 EA NEW STUDS AND ONE FLDec 29, 1999 · N925L · Doug DC932SDR TWAA0000610Bracket · damagedDURING OP 16 MAINT CHECK ON LT WING TE NEED INSTALL RIB ASSEMBLY OTBD OF CENTER, FLAP HINGE ASSEMBLY, AFTER FLAP HINGE BRACKET INSTALLED. REINSTALLED HI-LOCKS IN RIB ASSEMBLY PER SRM 51-30-5, PAGE 12 AND 13, PARAGRAPH 7 A AND B. REINSTALLED RIB PER SRM 51-30Dec 29, 1999 · N925L · Doug DC932SDR TWAA0000613Bracket · corrodedDURING OP 16 MAINT CHECK, FOUND ON LT WING TE THE INBD FLAP HINGE SUPPORT BRACKET HAD RUST EMITTING FROM BETWEEN HINGE SUPPORT BRACKET TO ATTACH BOLT. ACCOMP HIGH FREQ EDDY CURRENT OF HOLES IN AREA PER TWA NDT 51-00-03 PART 6. INSTALLED NEW STUDS AND FLAP HIDec 28, 1999 · N925L · Doug DC932SDR TWAA0000611Hinge · corrodedDURING OP 16 MAINT CHECK, FOUND ON LT WING, CENTER FLAP HINGE SUPPORTS HAD RUST EMITTING FROM HINGE TO REAR SPAR ATTACH BOLTS. ACCOMP HIGH FREQ EDDY CURRENT TO HOLES AND AREA PER TWA NDT 51-00-3, PART 6. INSTALLED NEW STUDS AND FLAP HINGE FITTING PER MM 57-4Dec 28, 1999 · N925L · Doug DC932SDR QXEA0000118Aperture · corrodedPDX - 74B APERATURE HAD MINOR CORROSION AT SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH 4B (2B).Dec 23, 1999 · N476US · Fokker F28MK4000SDR QXEA0000117Aperture · corrodedPDX - 74A APERATURE HAD MINOR CORROSION AT SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH 4C (2B).Dec 23, 1999 · N476US · Fokker F28MK4000SDR DL72S992817Stiffener · crackedNR 2 SLAT O/B TRACK I/B SPAR STIFFENER CRACKED. REPLACED STIFFENER PER M/M 57-20-21 PG 813.Dec 22, 1999 · N522DA · Boeing 727232SDR QXEA0000116Plate · gougedPDX - RIGHT-HAND FORWARD CENTER WING TO OUTER WING LOWER TIE PLATE HAD A GOUGE FROM A FAIRING FASTENER STATION 1700 NEAR LEADING EDGE. REPAIRED IAW HORIZON AIR EA 4-57-339.Dec 21, 1999 · N476US · Fokker F28MK4000SDR AT9900909Cap · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON LEFT LOWER WING T-CAP BS 605. REMOVED AND REPLACED LEFT LOWER WING T-CAP AT BS 605 IAW DC9 SB 57-98 REV 8.Dec 20, 1999 · N833AT · Doug DC932SDR AT9900908Cap · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON RIGHT LOWER WING T-CAP BS 605. REMOVED AND REPLACED RIGHT LOWER WING T-CAP AT BS 605 IAW DC9 SB 57-98 REV 8.Dec 20, 1999 · N833AT · Doug DC932
Back to JASC 5720