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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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.SDR 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.SDR 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.SDR 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)SDR 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)SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 RESDR 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 MAXISDR SWAA960055Support · crackedDURING SCHEDULED D-CHECK, FOUND LEFT WING L/E RIB LOWER SURFACE PANEL SUPPORT AT STA 571 CRACKED. REPLACED PER BOEING SRM.SDR AU960325Panel · faulty(AUS) WING CENTRE SECTION TOP HAT SECTIONS FOUND IN ANNEALED (SOFT) CONDITION FOLLOWING HEAT TREATMENT - SUSPECT HEAT TREATMENTINCOMPLETESDR 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.SDR 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 LADENENVIRONMSDR 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.SDR AU960313Plate · cracked(AUS) WING CENTRE SECTION FORWARD SPAR WEB PLATE LOCATED AT RH UPPER WING ATTACHMENT AREA CRACKEDSDR AU960114Rib · corroded(AUS) RH WING NACELLE SIDE RIB CONTAINED EXFOLIATION CORROSIONSDR 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)SDR AU960179Strut · corroded(AUS) LH WING AFT WING STRUT AND TWO BRACES CONTAINED LIGHT CORROSION -FOUND DURING X-RAY INSPECTIONSDR 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.SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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 AWAYSDR 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)SDR 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)SDR P5CA9600080Tip · delaminatedFOUND PANEL DELAMINATED ON RT WING TIP UPPER SURFACE. REPAIRED SAME IAW SRM 51-40-06.SDR 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.SDR 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.SDR P5CA9600068Bracket · crackedFOUND CRACKED BRACKET IN LT WLG DOOR CUTOUT ON LG SUPPORT BEAM. FABRICATED AND INSTALLED NEW BRACKED IAW SRM 51-30-02.SDR 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)SDR 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 AMDT1SDR AU960068Wing · cracked(AUS) LH AND RH WINGS CRACKED IN AREA OF LANDING GEAR ATTACHMENTSDR 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 TOSDR 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 - UNAPPROVEDPSDR 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 WITHSOLDERSDR 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/93SDR 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.SDR 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.SDR 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)SDR 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)SDR AU960045Strut · cracked(AUS) WING INTERPLANE STRUT CRACKED ON FORWARD FACE AT TOP END OF STRUT- CRACK EXTENDS APPROXIMATELY 50.8MM (2IN) DOWN LEADING EDGE
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