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 9605409162Splice · corrodedDURING A SPECIAL MAINTENANCE VISIT, FOUND CORROSION IN THE RIGHT WING FORWARD SPAR SPLICE PLATE AND SPLICE ANGLE DOUBLER. REPLACED PLATE (P/N 3912208-1) AND DOUBLER (P/N 4913572-1) PER EA 91-106788.Feb 13, 1996 · N8907E · Doug DC914SDR ABXA9600261Stringer Doubler · gougedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND RIGHT WING TENSION BOLT HOLE AT STRINGER NR 23 GOUGED. REPAIRED IAW ABX REA D957-14318-MR.Feb 12, 1996 · N967AX · Doug DC941SDR ABXA9600260Stringer Doubler · gougedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND RIGHT WING TENSION BOLT HOLE AT STRINGER NR 23 GOUGED. REPAIRED IAW ABX REA D957-14318-MR.Feb 12, 1996 · N967AX · Doug DC941SDR UPS96805706Angle · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON CHORD ANGLE, FS 70, BETWEEN LONGERONS 29R-30R. WILL BE REPAIRED ON TASK CARD 423121.Feb 11, 1996 · N811UP · Doug DC873FSDR CAL960390Support · crackedMIA - INSPECTION FOUND A .75 INCH CRACK IN LT WING TRAILING EDGE X-SUPPORT MEMBER AT UPPER AFT LEG FORWARD OF ATTACH POINT, JUST INBOARD OF NR 1 SPOILER ACTUATOR. THE SUPPORT MEMBER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)Feb 11, 1996 · N14890 · Doug DC982SDR CAL960389Support · crackedMIA - INSPECTION FOUND A 1 INCH CRACK IN LT WING TRAILING EDGE X-SUPPORT MEMBER AT UPPER AFT LEG FORWARD OF ATTACH POINT, JUST OUTBOARD OF NR 1 SPOILER ACTUATOR. THE SUPPORT MEMBER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)Feb 11, 1996 · N14890 · Doug DC982SDR UPS405428Support Tube · puncturedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, HOLE IN SUPPORT TUBE AT I/B LEADING EDGE STATION 788. REPLACED SUPPORT IAW SRM 51-30-05 AND MM 20-10-13.Feb 10, 1996 · N691UP · Boeing 747121SDR UPS96205702Stiffener · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT FRONT SPAR VERTICAL STIFFENER INB OF NR 3 TANK FUELING VALVE HAS CORROSION AT BONDING WIRE. REMOVED DAMAGED STIFFENER, FABRICATED REPLACEMENT STIFFENER IAW SRM 51-10-1 AND INSTALLED IAW SRM 51-30-2.Feb 9, 1996 · N940UP · Boeing 727185CSDR 9605389162Clips · corrodedDURING A SPECIAL MAINTENANCE VISIT, FOUND CORROSION IN THE RIGHT WING REAR SPAR STR 15 - 16 CLIPS AT STA 69. REPLACED CLIPS (P/N 4192009-2, P/N 4911499-520) PER EA 91-104054.Feb 9, 1996 · N8907E · Doug DC914SDR DL72S960282Angle · crackedFOUND ON B-1 LETTER CHECK, TWO L/E SPAR STIFFENERS CRACKED .50 INCH, ONE AT NR 3 SLAT INBD TRACK, THE OTHER AT NR 2 SLAT OUTBD TRACK. REPLACED ANGLES PER MM 57-20-21.Feb 6, 1996 · N484DA · Boeing 727232SDR DL72S960281Stiffener · crackedFOUND ON B1 LETTER CHECK, 2 INCH CRACK IN WING L/E SPAR STIFFENER AT NR 6 SLAT INBD TRACK. REPLACED STIFFENER PER MM 57-20-21.Feb 6, 1996 · N484DA · Boeing 727232SDR COMA9610063Bracket · crackedTHE LEFT AILERON WAS STRUCK BY A GROUND VEHICLE. NO DAMAGE WAS FOUND ON THE AILERON. HOWEVER, THE BRACKET ON THE WING REAR SPAR, THAT THE AILERON SERVO TAB RODS ARE CONNECTED TO, WAS FOUND CRACKED. THE BRACKET WAS REPAIRED PER AERODESIGN REPORT NR 1783-1 REFeb 6, 1996 · N161CA · Emb EMB120RTSDR AU960279Rib · cracked(AUS) LH AND RH WHEEL WELL LANDING GEAR SUPPORT RIBS PNO 0822175-65 (LH) AND PNO 0822175-65 (RH) CRACKED AND DISTORTED - UNDER SKINDISTORTED IN AREA OF LANDING GEAR DOOR ATTACHMENT - NUMEROUS RIVETS MISSING - AIRCRAFT IS USED FOR SHORT HAUL OPERATIONS AT MAXIFeb 6, 1996 · Cessna 402BSDR SWAA960055Support · crackedDURING SCHEDULED D-CHECK, FOUND LEFT WING L/E RIB LOWER SURFACE PANEL SUPPORT AT STA 571 CRACKED. REPLACED PER BOEING SRM.Feb 5, 1996 · N601WN · Boeing 7373H4SDR AU960325Panel · faulty(AUS) WING CENTRE SECTION TOP HAT SECTIONS FOUND IN ANNEALED (SOFT) CONDITION FOLLOWING HEAT TREATMENT - SUSPECT HEAT TREATMENTINCOMPLETEFeb 4, 1996 · Gulstm G73SDR ABXA9600304Fitting · crackedDURING C-CHECK INSPECTION, FOUND THE RIGHT WING LEADING EDGE FITTING AT STA XOS 334 CRACKED. REPAIRED FITTING IAW ABX REA D957-14255-MR.Feb 2, 1996 · N943AX · Doug DC931SDR AU960168Fitting · corroded(AUS) WING FITTINGS/STIFFENERS CONTAINED EXFOLIATED INTERGRANNULAR CORROSION - DURING FITTING REPLACEMENT EXTENSIVE CORROSION WAS ALSO FOUND IN LOWER WING STRINGERS PARTICULARLY IN AREA UNDER FUEL CELL BAYS - AIRCRAFT PREVIOUSLY OPERATED IN SALT LADENENVIRONMFeb 1, 1996 · Cessna 402ASDR UPS805453Trap Fitting · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT AND RT TRAP FITTINGS CRACKED AT LOWER ENDS. REPLACED FITTINGS PER SRM 57-2-7.Jan 31, 1996 · N748UP · Doug DC871FSDR AU960313Plate · cracked(AUS) WING CENTRE SECTION FORWARD SPAR WEB PLATE LOCATED AT RH UPPER WING ATTACHMENT AREA CRACKEDJan 31, 1996 · Beech 58SDR AU960114Rib · corroded(AUS) RH WING NACELLE SIDE RIB CONTAINED EXFOLIATION CORROSIONJan 31, 1996 · Beech B60SDR C2XA96IA041Beam · chafedIAH - DURING C-CHECK INSPECTION, FOUND LT WING RIB 13 FORWARD INBOARD FLAP HINGE BEAM CHAFED FROM PANEL 552AB. MAINTENANCE REMOVED AND REPLACED THE BEAM ASSEMBLY, AIRCRAFT APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT, 4,819.7 HOURS. CYCLES, 5,199. (X)Jan 30, 1996 · N69901 · Aerosp ATR72212SDR AU960179Strut · corroded(AUS) LH WING AFT WING STRUT AND TWO BRACES CONTAINED LIGHT CORROSION -FOUND DURING X-RAY INSPECTIONJan 30, 1996 · Airpts A9ASDR ABXA9600193Doubler · corrodedDURING C-CHECK INSPECTION, DISCOVERED RIGHT WING LEADING EDGE HAS CORROSION UNDER RETAINER RING INSIDE PANEL 517B. REPAIRED RIGHT WING OUTBOARD LEADING EDGE INTERNAL DOUBLER ACCESS PANEL 517B, AT XFS 845 IAW ABX REA-D857-13486-MR.Jan 30, 1996 · N843AX · Doug DC861SDR C2XAIA036Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 1 SKIN SUPPORT CRACKED AT RIB NR 18. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7. CYCLES, 18,250. (X)Jan 29, 1996 · N34712 · Emb EMB120RTSDR C2XA96IA040Strut · bearings wornIAH - DURING 6C CHECK INSPECTION, FOUND RIGHT WING STRUT ASSEMBLY AT RIB NR 8 FLAP SUPPORT BEAM TO HAVE PLAY AT FORWARD AND AFT BEARINGS. MAINTENANCE REMOVED AND REPLACED THE STRUT ASSEMBLY, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)Jan 29, 1996 · N14828 · Aerosp ATR42320SDR C2XA96IA038Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 3 SKIN SUPPORT CRACKED AT RIB NR 21. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7 HOURS. CYCLES, 18,250. (X)Jan 29, 1996 · N34712 · Emb EMB120RTSDR C2XA96IA037Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 4 SKIN SUPPORT CRACKED AT RIB NR 18. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7. CYCLES, 18,250. (X)Jan 29, 1996 · N34712 · Emb EMB120RTSDR C2XA96IA035Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 2 SKIN SUPPORT CRACKED AT RIB NR 18. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7. CYCLES, 18,250. (X)Jan 29, 1996 · N34712 · Emb EMB120RTSDR C2XA96IA034Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING UPPER NR 2 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7. CYCLES, 18,250. (X)Jan 29, 1996 · N34712 · Emb EMB120RTSDR C2XA96IA033Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING LOWER NR 2 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7. CYCLES, 18,250. (X)Jan 29, 1996 · N34712 · Emb EMB120RTSDR C2XA96IA032Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING LOWER NR 3 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7. CYCLES, 18,250. (X)Jan 29, 1996 · N34712 · Emb EMB120RTSDR AU960707Chord · corroded(AUS) RH WING LEADING EDGE RIB 'T' AT STN 269.298 CORRODED ON THE BOTTOM FLANGE - FURTHER INVESTIGATION FOUND A SECTION OF THE CHORD APPROXIMATELY 152.4MM (6IN) FROM THE WING FRONT SPAR AND APPROXIMATELY 50.8MM (2IN) IN LENGTH COMPLETELY CORRODED AWAYJan 27, 1996 · Boeing 727277SDR C2XA96IA031Support · crackedIAH - DURING 1C CHECK INSPECTION, FOUND RIGHT WING RIB NR 21 UPPER SURFACE SKIN SUPPORT BRACKET NR 2 TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT BRACKET. (M)Jan 25, 1996 · N34712 · Emb EMB120RTSDR C2XA96IA030Support · crackedIAH - DURING 1C CHECK INSPECTION, FOUND RIGHT WING RIB NR 20 UPPER SURFACE SKIN SUPPORT NR 4 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT BRACKET. (M)Jan 25, 1996 · N34712 · Emb EMB120RTSDR P5CA9600080Tip · delaminatedFOUND PANEL DELAMINATED ON RT WING TIP UPPER SURFACE. REPAIRED SAME IAW SRM 51-40-06.Jan 24, 1996 · N855FT · Boeing 747124SDR P5CA9600070Beam · corrodedFOUND LEVEL 1 CORROSION ON UPPER CHORD OF LT WING L/G BEAM STA 1350. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-30-01.Jan 24, 1996 · N855FT · Boeing 747124SDR P5CA9600069Beam · corrodedFOUND LEVEL 1 CORROSION ON LT WING L/G BEAM AFT SIDE STA 1350. CORROSION REMOVED IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.Jan 24, 1996 · N855FT · Boeing 747124SDR P5CA9600068Bracket · crackedFOUND CRACKED BRACKET IN LT WLG DOOR CUTOUT ON LG SUPPORT BEAM. FABRICATED AND INSTALLED NEW BRACKED IAW SRM 51-30-02.Jan 24, 1996 · N855FT · Boeing 747124SDR CAL960273Beam · corrodedINSPECTION FOUND CORROSION ON LT MLG BEAM LOWER FLANGE AT INBOARD FLAP INBOARD TRACK ATTACH POINT. A REPAIR WAS PERFORMED IAW ECRA 5750-02437 AND SRM 51-10-6 AD SRM 51-10-2. (X)Jan 24, 1996 · N17402 · Boeing 727243SDR AU960720Stiffener · corroded(AUS) LH WING REAR SPAR STIFFENER CRACKED AND CORRODED - STEEL REAR SPAR BRACKET CONTAINED MINOR CORROSION - FOUND DURING INSPECTION IAW AD/PA32/27 AMDT1Jan 23, 1996 · Piper PA32300SDR AU960068Wing · cracked(AUS) LH AND RH WINGS CRACKED IN AREA OF LANDING GEAR ATTACHMENTJan 22, 1996 · Grob G115CSDR 96FDEA00104Angle · corrosionL/LT WW FWD BULKHEAD TOP OF WING CENTER BOX SECTION, REMOVABLE PANEL HAS HEAVY CORROSION, APPROX 10 INCHES O/B OF VERTICAL KEEL BEAM WEB. REMOVED CORRODED ANGLE, CLEANED, TREATED AND PRIMED UPPER WING SURFACE THAT MATES WITH ANGLES REF 51-00 VOL 11 SRM, OK TOJan 18, 1996 · N68051 · Doug DC1010SDR AU960083Eye Bolt · mismodified(AUS) WING LOWER RH FRONT MAIN SPAR EYEBOLT LOCATED AT THE WING STRUT ATTACHMENT POINT HAD A HOME MADE 'T' SECTION ATTACHED TO BOLTHEAD WITH SOLDER - EYEBOLT IS INCIDENCE WIRE ATTACHMENT POINT AT INTERPLANE STRUT POSITION ON LOWER FRONT MAIN SPAR - UNAPPROVEDPJan 15, 1996 · Dhavxx DH82AROBRTSNSDR AU960062Eye Bolt · mismodified(AUS) DURING WIRE REPAIR ALL EYEBOLTS WERE REMOVED FROM THE LOWER STARBOARD FRONT MAIN SPAR AT THE WING STRUT ATTACHMENT POINT - INSPECTION OF THE EYEBOLTS FOUND THAT ONE IS SUSPECTED TO HAVE A HOME MADE 'T' SECTION ATTACHED TO THE HEAD OF THE BOLT WITHSOLDERJan 15, 1996 · Dhavxx DH82AROBRTSNSDR AU960031Strap · cracked(AUS) LH WING AUXILIARY SPAR TO INBOARD RIB DOUBLER CRACKED IN RADIUS -CRACK LENGTH 5MM (0.196IN) - WING TO FUSELAGE STRAP CRACKED -FOUND DURING INSPECTION IAW AD/AC/93Jan 15, 1996 · Gulstm 500SSDR UPS805383Web · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E LOWER SURFACE CRACKED IN WEB BETWEEN STA. XFS 608-614. REPAIRED WEB PER SRM 57-2-0.Jan 14, 1996 · N701UP · Doug DC871FSDR 9606689610Doubler · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE WING CENTER SECTION LOWER DOUBLER AT STR 21, FS 617 AT LBL 10. REPAIRED DOUBLER PER EA 12-5730-9-C0732.Jan 12, 1996 · N610NW · Doug DC932SDR CAL960055Bracket · crackedHOU - INSPECTION FOUND A.75 INCH CRACK IN RIGHT WING LEADING EDGE RIB AFT BRACKET, LOCATED AT FORWARD SPAR UPPER CAP OUTBOARD OF NR 8 SLAT TRACK. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-60-0 AND 51-30-2. (M)Jan 11, 1996 · N14880 · Doug DC981SDR CAL960054Bracket · brokenHOU - INSPECTION FOUND RIGHT WING LEADING EDGE RIB LOWER ATTACH BRACKET BROKEN OUTBOARD OF NR 2 SLAT TRACK. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-60-0 AND 51-30-2. (M)Jan 11, 1996 · N14880 · Doug DC981SDR AU960045Strut · cracked(AUS) WING INTERPLANE STRUT CRACKED ON FORWARD FACE AT TOP END OF STRUT- CRACK EXTENDS APPROXIMATELY 50.8MM (2IN) DOWN LEADING EDGEJan 10, 1996 · Boeing B75N1
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