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 FDEA201308041771Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT4, WRI: 57101121, POST REMOVAL OF FASTENER "F" IN CTR WING BOX REAR SPAR FR 47 RT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE, HOLE "F" EXISTING DIA= 0.529 IN. HOLE "F" SCORES REMOVED BY REAMING, SDR FDEA201308041770Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT4, WRI: 57101121, POST REMOVAL OF FASTENER "E" IN CTR WING BOX REAR SPAR FR 47, RT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "E" EXISTING DIA= 0.529 IN. FASTENER "E" HOLE REAMED TO REMOVSDR FDEA201308041769Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT4, WRI: 57101121, POST REMOVAL OF FASTENER "D" IN CTR WING BOX REAR SPAR FR 47 RT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "D" EXISTING DIA= 0.639 IN. FASTENER "D" HOLE REAMED TO REMOVESDR FDEA201308041768Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT4, WRI: 57101121, POST REMOVAL OF FASTENER "C" IN CTR WING BOX REAR SPAR FR.47 RT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "C" EXISTING DIA= 0.529 IN. FASTENER "C" HOLE REAMED TO REMOVSDR FDEA201308041767Skin · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT4, WRI: 57101121, POST REMOVAL OF FASTENER "B" IN CTR WING BOX REAR SPAR FR 47 RY JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "B" EXISTING DIA= 0.591". FASTENER HOLE B REAMED TO REMOVE SCSDR FDEA201308041766Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT4, WRI: 57101121, POST REMOVAL OF FASTENER "A" IN CTR WING BOX REAR SPAR FR.47 RT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE AND SCRATCH IN UPPER SURFACE AROUND HOLE. HOLE "A" EXISTING DIA= 0.59SDR SWAA2013080618913Retainer · crackedRT WING TE CURVED SEAL RETAINER ANGLE CRACKED JUST ABOVE NR 2 PYLON TIP. R&R RETAINER IAW SRM.SDR SWAA2013090619928Access Panel · crackedRT WING ACCESS PANEL 5864R CRACKED. REPAIRED PANEL IAW EA.SDR SWAA2013081319147Support Angle · crackedRT WING TE UPPER PANEL SUPPORT ANGLE AT PROGRAM TRACK CRACKED ORSS 281. R&R ANGLE IAW SRM & SOPM.SDR SWAA2013081319146Angle · crackedRT WING TE BULKHEAD WEB SEAL RETAINER ANGLE CRACKED AT ORSS 271. R&R ANGLE IAW SRM & SOPM.SDR SWAA2013080518835Nut Plate · crackedRT WING NUT PLATE STRIP TE CRACKED AT WBL 202. R&R PLATE IAW SRM.SDR SWAA2013080518834Nut Plate · crackedLT WING NUT PLATE STRIP TE CRACKED AT WBL 202. R&R PLATE IAW SRM.SDR AALA20130731025Stiffener · crackedLT VERTICAL STIFFENER OTBD OF PACK EXHAUST DUCT IS CRACKED, LOWER END. REPLACED VERTICAL STIFFENER IAW AARD 51-10-05 R1 & BOEING DRAWINGS 111A1000 & 149A7210.SDR AALA20130731016Casting · crackedLT WING CRACKED IN CASTING RT SIDE OF NR 4 SLAT TRACK. REPLACED CASTING.SDR SWAA2013081219023Retainer · crackedLT WING TE COVE SEAL RETAINER CRACKED ABOVE NR 1 PYLON AFT TIP. R&R RETAINER IAW SOPM.SDR IPXA13M79679Support Bracket · crackedINSPECTION TYPE: 1C, LT WING FIXED L/E SUPPORT BRACKET CRACKED AT AFT END JUST OTBD OF NR 7 SLAT TRACK XOS 559. REMOVED FABRICATED AND INSTALLED REPLACEMENT SUPPORT BRACKET IAW DWG ARB1162, SRM 51-31-01 AND 51-33-01. (MINOR)SDR ASOA2013082108889Strap · mismanufacturedRT SIDE LOWER STRAP FOR SB670BA-57-02001 HAS ONE HOLE MISCOUNTERSUNK. REPAIRED IAW OF REO 670-57-21-576. MAJOR REPAIR.SDR SWIA201334238Cleat · crackedLT WING RIB 16 LOWER SECOND MOST FORWARD SKIN CLEAT CRACKED. C-CHECK REPLACED LT WING RIB 16 LOWER SECOND MOST FORWARD SKIN CLEAT IAW SRM.SDR SWIA201334239Cleat · crackedRT WING UPPER SKIN CLEAT ABOVE THE NR 4 FUEL ACCESS PANEL CRACKED. C-CHECK REPLACED UPPER SKIN CLEAT AT RT WING ABOVE THE NR 4 FUEL ACCESS PANEL IAW SRM.SDR SWAA2013080918988Angle · crackedRT WING TE ANGLE CRACKED AT LEVEL WBL 204.40. R&R ANGLE IAW SRM & DRAWING.SDR SWAA2013080918997Support Angle · crackedLT WING UPPER TE PANEL SUPPORT ANGLE CRACKED AT ORSS 273. R&R ANGLE IAW SRM.SDR A6WA2013073141121Angle · crackedRIGHT WING L/E ANGLE AT WS 148 CRACKED UPPER OUTBD CORNER. R & R IAW SRM 51-24-16 & 51-42-06.SDR ERAA201308010054Support · chafedCHAFE DAMAGE NOTED AT RT MLG KEEL NEAR ACTUATOR HYDRAULIC LINES. REPAIRED IAW FR-CO-100795. OK FOR SERVICE.SDR CALA2013072600516Screw · misinstalledLEFT WING L/E AT WS 406 APPROX L/E SLAT TORQUE TUBE TO ANGLE TRANSFER DRIVE CONNECTION COUPLING SLEEVE, FOUND ONE LOCK SCREW NOT PROPERLY INSTALLED LT WING L/E SLAT TORQUE TUBE COUPLING SLEEVE ATTACH SCREW REPLACED AND LOCKWIRE RESECURED IAW AMM 27-81-38.SDR ABXA20130722496Strut · corrodedNR 2 SLAT ON LT WING OTBD AUX TRACK OTBD LOWER STRUT CORRODED AROUND NUTPLATES. R & R NR 2 SLAT OTBD AUX TRACK AND OTBD LOWER STRUT IAW SRM 51-40-02, PARA 7B AND REA B657-60610, ACFT GROUNDED.SDR SWIA201334217Fitting · crackedRT WING FUEL TANK UPPER CLIP IS CRACKED AT RIB 20. C-CHECK REPLACED RT WING FUEL TANK UPPER CLIP AT RIB 20.SDR SWIA201334216Fitting · crackedLT WING FUEL TANK UPPER CLIP ON RIB 21 IS CRACKED. C-CHECK REPLACED LT WING FUEL TANK UPPER CLIP AT RIB 21.SDR SWIA201334215Fitting · crackedLT WING FUEL TANK UPPER CLIP IS CRACKED. C-CHECK REPLACED LT WING FUEL TANK UPPER CLIP AT RIB 23.SDR REXA2013072001423Panel · chafedPANEL 684EB CHAFED. BLENDED OUT CHAFE IAW SRM 51-21-00, PANEL FOUND TO BE IN LIMITS IAW REO 690-57-52-47.SDR SWAA2013081219096Angle · crackedLT WING TE CURVED SEAL RETAINER ANGLE CRACKED ABOVE NR 1 PYLON TIP. R&R ANGLE IAW SRM.SDR SWAA2013080518838Support Angle · crackedLT WING TE UPPER PANEL SUPPORT ANGLE CRACKED JUST OTBD OF PYLON. R&R ANGLE IAW SRM.SDR SWAA2013080518837Support Angle · crackedLT WING TE AILERON WIPER WEB SUPPORT ANGLE CRACKED AT RSS 545. R&R ANGLE IAW SRM.SDR SWAA2013080118754Fitting · crackedLT WING TE UPPER PANEL MIDDLE SUPPORT ANGLE FORWARD CLIP ON INNER PART OF PYLON INBD SIDE CRACKED. R&R CLIP IAW SRM.SDR AALA20130718003Casting · crackedCASTING CRACKED INBD OF NR 4 SLAT TRACK INBD UPPER SIDE ON LT WING. INSTALLED NEW CASTING IAW AARD 51-00-05-1.SDR SWAA2013073118698Web · crackedRT WING TE SUPPORT WEB JUST INBD OF DEFLECTION CONTROL RIB CRACKED. R&R WEB IAW SRM.SDR REXA2013071701421Panel · chafedPANEL 684GB CHAFED. REPLACED PANEL IAW SRM 51-40-11.SDR ABXA20130717494Strut · corrodedNR 3 SLAT OTBD AUX TRACK INBD LOWER STRUT CORRODED AT FORWARD END. R & R STRUT IAW SRM 51-40-02, ACFT WAS GROUNDED.SDR SWAA2013072918656Support · crackedLT WING TE UPPER PANEL SUPPORT INBD OF INBD RIB IS CRACKED. R&R SUPPORT IAW SRM.SDR SWAA2013072918655Support · crackedRT WING TE UPPER PANEL SUPPORT INBD OF INBD RIB IS CRACKED. R&R SUPPORT IAW SRM.SDR REXA2013072101097Tab · chafedRT MLG SIDE STAY BRACE FITTING ANTI-ROTATION TAB IS CHAFED WITHIN LIMITS OF REO 601R-57-21-1702.SDR SWAA2013071818321Latch · looseLT WING SNAP PANEL OTBD OF LT GEAR 551DB LATCHES LOOSE. R&R LATCHES IAW MM.SDR SWAA2013071818320Plate · crackedLT WING LOWER AFT TE PANEL WIGGLE PLATE INBD OF ENGINE STRUT CRACKED OUT ON TWO RIVETS. R&R PLATE IAW SRM.SDR ABXA20130716495Strut · corrodedNR 2 SLAT INBD AUX TRACK OTBD LOWER STRUT CORRODED AROUND NUTPLATES. R & R INBD AUX TRACK OTBD STRUT ON NR 2 SLAT IAW DWG 114T2222, REV D, ACFT GROUNDED.SDR SWAA2013080518833Nut Plate · crackedLT WING NUT PLATE STRIP UPPER SURFACE CRACKED BETWEEN WBL 181 TO WBL 191. R&R NUT PLATE STRIP IAW SRM & DRAWING.SDR ABXA20130715497Web · crackedNR 1 SLAT WEB ON L/E OF WING AT OTBD AUX TRACK INBD STRUT ATTACH POINT SPLIT FROM CORROSION. REPAIRED NOSE BEAM WEB IAW SRM 57-41-13, FIG 201, REPAIR 1, ACFT WAS GROUNDED.SDR SWAA2013071918354Support Angle · crackedLT WING TE SUPPORT ANGLE CRACKED AT WBL 182. R&R ANGLE IAW SRM & DRAWING.SDR SWAA2013071518214Plate · crackedLT WING TE LOWER PANEL WIGGLE PLASTIC CRACKED AT ONE FASTENER LOCATION. R&R WIGGLE PLATE IAW SRM.SDR FDEA201307111531Skin · crackedEIGHT FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS, FOUND DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATIONS XORS 683.4 AND XORS 713.6. REPAIRED IAW SRM 57-20-02, REPAIR 5 FIG 201, REV 52. SDR SWAA2013071218169Bracket · crackedRT WING AFT SPAR LOWER BULB SEAL BRACKET CRACKED ABOVE PANEL 651GB. REPAIRED BRACKET IAW SRM.SDR SWAA2013071118115Plate · crackedLT WING LOWER SURFACE WIGGLE PLATE CRACKED AFT OF THE NR 1 ENGINE PYLON LOWER TE FIXED PANEL. R&R PLATE IAW SRM.
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