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 SWAA2013090619937Attach Angle · crackedTE UPPER SHELF PANEL AFT OF NR 2 STRUT FAIRING ATTACH ANGLE CRACKED. R&R ANGLE IAW SRM.SDR SWAA2013102221349Angle · crackedRT WING INTERNAL AREA TE ANGLE CRACKED AT RSS 238+7. R & R ANGLE IAW SRM & DRAWING.SDR FDEA201308272041Stiffener · chafedLEFT L/E FRONT SPAR VERTICAL STIFFENER, FOUND CHAFED. REMOVED AND REPLACED IAW DWG 112N2038 SHT 1, REV -, AND DWG 112N2002 SHT 6, REV D.SDR SWAA2013091020033Angle · crackedRT WING TE ANGLE CRACKED AT WBL 184.40. R&R ANGLE IAW SRM & DRAWING.SDR SWAA2013082919682Bracket · crackedRT WING REAR SPAR SHELF PLATE BULB SEAL BRACKET CRACKED. R&R BRACKET IAW SRM.SDR ASOA2013091208992Angle · crackedLT WING HAS A CRACKED ANGLE JUST FWD & INBD OF MLG. REMOVED 601R10213-11, ANGLE TO REPLACE WITH NEW ANGLE IAW SRM . INSTALLED ANGLE, PN 601R10213-11 IAW SRM 51-42-06, COUNTERSUNK & ALODINED SRM 51-21-00 & 51-40-11.SDR SWIA201334386Structure · dentedDENT IN THE LT WING. DENT OUT OF LIMITS IAW FLT#4694 REPAIRED DENT IAW SRM.SDR FDEA201308232009Shim · migratedLEFT WING BETWEEN OTBD NAC FITTING AND LOWER WING SKIN, FOUND WITH SHIMS MIGRATION AT WS 303.5. REPAIRED IAW EA F-5450-167521 PT.1. CATAGORY B MAJOR.SDR CALA2013082690707Structure · damagedLW FUEL TANK LANDING 540KB HAS FOUR OVER SIZED FASTENER HOLES. REPAIRED LT WING FUEL TANK LANDING 540KB IAW REO-L01412 & EC-RA 5720-02442. THIS REPAIR HAD BEEN APPROVED AS CAT 'B' VIA RDAS 70581393-003- 2013 ISSUE A.SDR SWIA201334657Fitting · crackedRT WING UPPER CLIP CRACKED 2ND FROM FWD AT RIB 20. C-CHECK REPLACED UPPER WING CLIP AT RT WING 2ND FROM FWD AT RIB 20, IAW SRM.SDR SWIA201334656Fitting · crackedRT WING LOWER SMALL CLIP CRACKED AT RIB 15 2ND FROM FWD. C-CHECK REPLACED RT WING LOWER SMALL CLIP AT RIB 15, 2ND FROM FWD IAW SRM.SDR IPXA3M80159Web · crackedDURING 2C, LT WING FUEL TANK WEB LIGHTNING HOLE OTBD DOUBLER CRACKED AT STA XORS 345, BETWEEN STRINGERA 44 AND 45. REPAIRED LT WING FUEL TANK LIGHTNING HOLE OTBD DOUBLER AT STA XORS 345 BETWEEN STGR. 44 AND 45 REF STASA EA 011-5710-01-A4882 REV I/R, UPS EO SDR SWAA2013082719619Bracket · crackedRT WING BULB SEAL BRACKET CRACKED ABOVE PANEL 651GB. R&R BRACKET IAW SRM.SDR SWAA2013082819657Bracket · crackedRT WING INBD FIXED TE BRACKET CRACKED AT WBL 114. R&R BRACKET IAW SRM & DRAWING.SDR SWIA201334658Support Fitting · crackedLT OTBD WING HAS ONE CRACKED UPPER SKIN SUPPORT CLIP AT STATION 20A. C-CHECK REPLACED LT OTBD WING ONE CRACKED UPPER SKIN SUPPORT CLIP AT WING STATION 20A IAW SRM.SDR SWAA2013082619535Angle · crackedLT WING NR 3 INBD LOWER SIDE INTERNAL AREA ANGLE CRACKED. R&R ANGLE IAW SRM & DRAWING.SDR SWAA2013090419841Strap · crackedRT WING BONDING STRIP CRACKED AT LOWER SIDE WING TO BODY. R&R STRAP IAW & DRAWING.SDR ABXA20130818508Channel · splitT/E PANEL, 661NB LOWER AFT ATTACH CHANNEL AND BRACKET FROM REAR SPAR TO T/E AT WS 1055 SPLIT. R & R AFT LOWER ATTACH BRACKET AND CHANNEL IAW SRM 51-40-02.SDR ABXA20130817545Web · corrodedLEADING EDGE WEB AT LES 441-456 FOUND TO BE EXFOLIATED. REMOVED & REPLACED L/E WEB IAW SRM 51-40-02. NOSE BEAM CORRODED, RT WING LES 454 - 456. AIRCRAFT WAS GROUNDED.SDR SWAA2013082819667Attach Angle · brokenLT WING ATTACH ANGLE BETWEEN SHELF PANELS 551DB AND 551EB FWD END ATTACH TO WING BROKEN. R&R ANGLE IAW SRM AND DWG.SDR ASOA2013091709022Mount · corrodedBELLY FAIRING PANEL 193AB HAS CORROSION DAMAGE ALONG THE FWD MOUNTING FLANGE. R & R LT AND RT FWD FLANGES ON PANEL 193AB IAW SRM 51-42-13-001-001-A01.SDR SWIA201334234Support · crackedLT WING INBD NR 2 FUEL PANEL HAS ONE SKIN SUPPORT CRACKED OTBD OF PANEL. C-CHECK REPLACED LT WING SKIN SUPPORT JUST OTBD OF NR 2 FUEL PANEL IAW SRM.SDR SWAA2013081919332Angle · crackedLT WING AILERON MID INBD HINGE ANGLE CRACKED AT FWD INBD SIDE AT APPROXIMATELY RSS 545. R&R ANGLE IAW SRM.SDR DALA13039793217Clamp · corrodedDURING INSPECTION, FOUND CORROSION ON CLAMP RING OF THE ACCESS PANEL 540DB LT WING FUEL TANK SSI 572040. L=0.05", W=0.03", D=0.001 APPROX. REPLACED CLAMP RING THE ACCESS PANEL 540DB LT WING FUEL TANK IAW AMM 57-27-11-000-001-A. THE INSTALLATION IS DOCUMENTEDSDR DALA13039783217Clamp · corrodedDURING INSPECTION, FOUND CORROSION ON CLAMP RING THE ACCESS PANEL 540CB LT WING FUEL TANK SSI 572040. L=0.05" W=0.03" D=0.001" APPROX. REPLACED CLAMP RING THE ACCESS PANEL 540CB LT WING FUEL TANK IAW AMM 57-27-11-000-001-A. THE INSTALLATION IS DOCUMENTED IN SDR WVER20130816001Strap · damagedRT WING STRAP, FOUND 18 DISCREPANT HOLES IN COLD WORKED AND NON COLDWORKED HOLES.SDR FDEA201308151900Horn · crackedRT OTBD FWD BEARING HORN IS CRACKED. CRACK PROPAGATES FROM LOWER INBD CORNER TO INBD SIDE. R & R IAW WC E-8-5750-5000, F5, PT2 SEQ 259.SDR AALA20130815003Support Bracket · corrodedLT WING FORWARD BOOST PUMP THE UPPER BONDING STRAP ATTACHED TO FORWARD SPAR IS CORRODED ON THE SPAR. REMOVED CORROSION & INSTALLED SERVICEABLE UPPER SUPPORT BRACKET IAW SRM 57-20-10-1A-3.SDR SWAA2013081619276Stiffener · crackedRT WING VERTICAL STIFFENER CRACKED FWD OF NR 2 AILERON HINGE. R&R STIFFENER IAW SRM.SDR SWAA2013081519248Bracket · crackedLT WING ANGLE CRACKED AT APPROXIMATELY RSS 545 FWD OF MID INBD AILERON HINGE. R&R BRACKET IAW SRM.SDR ABXA20130813521Support Fitting · crackedRIGHT WING REAR SPAR FITTING AT WS 700, A SUPPORT FITTING FOR THE NR 11 SPOILER AND THE FLAP DRIVE TORQUE TUBE, AFT SUPPORT LEG IS CRACKED IN HALF. R & R NR 11 SPOILER INBD SUPPORT FITTING IAW SRM 51-40-02. PN: 113T1566-26, NSN, FITTING, CRACK 1.5", RIGHT WINSDR SWAA2013081919337Angle · crackedRT WING TE ANGLE CRACKED AT CAVITY RSS 546. R&R ANGLE IAW SRM & DRAWING.SDR SWAA2013082119400Latch · crackedRT WING ACCESS PANEL NR 6540R LATCH CRACKED. R&R LATCH IAW SRM.SDR SWAA2013081519255Access Panel · crackedRT WING ACCESS PANEL PLATE CRACKED ON PANEL NR 6531R. R&R PANEL IAW SRM & DRAWING.SDR SWAA2013081419215Shim · crackedLT WING FIXED TE SUPPORT STRUCTURE ACCESS PANEL 5735L SHIM CRACKED. R&R SHIM IAW SRM & DRAWING.SDR SWAA2013081319163Angle · crackedLT WING INBD TE STRUCTURE ANGLE CRACKED AT WBL 184.63. R&R ANGLE IAW SRM & DRAWING.SDR SWAA2013080818945Bracket · crackedLT WING CRACKED BRACKET AT INBD AFT EDGE OF PYLON PANEL 5735L. R&R BRACKET IAW SRM.SDR SWAA2013081219134Support Angle · crackedUPPER SHELF PANEL INBD OF NR 5 SPOILER, CENTER SUPPORT ANGLE CRACKED. R&R ANGLE IAW SRM.SDR SWAA2013082619589Strap · crackedRT WING FIXED LE FAIRING PANEL AT MOST INBD AREA INTERIOR STRAY ATTACHED TO BODY FAIRING PANEL FRAME CRACKED AT UP & LOWER ATTACHED AREAS. R&R STRAPS IAW SRM.SDR FDEA201308041763Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT3, WRI: 57101122, POST REMOVAL OF FASTENER "G" IN CTR WING BOX REAR SPAR FR 47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "G" EXISTING DIA= 0.529 IN. FASTENER "G" HOLE REAMED TO REMOVE SCSDR FDEA201308041765Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT3, WRI: 57101122, POST REMOVAL OF FASTENER "Q" IN CTR WING BOX REAR SPAR FR 47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "Q" EXISTING DIA= 0.653 IN. FASTENER "Q" HOLE REAMED TO REMOVESDR FDEA201308041764Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT3, WRI: 57101122, POST REMOVAL OF FASTENER "C" IN CTR WING BOX REAR SPAR, FR 47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "C" EXISTING DIA= 0.529 IN. FASTENER "C" HOLE REAMED TO REMOVE SDR FDEA201308041762Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT3, WRI: 57101122, POST REMOVAL OF FASTENER "F" IN CTR WING BOX REAR SPAR FR 47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "F" EXISTING DIA= 0.529 IN. FASTENER 'F' HOLE REAMED TO REMOVESDR FDEA201308041761Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT3, WRI: 57101122, POST REMOVAL OF FASTENER "E" IN CTR WING BOX, REAR SPAR, FR 47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "E" EXISTING DIA= 0.529 IN. FASTENER "E" HOLE REAMED TO REMOVESDR FDEA201308041760Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT3, WRI: 57101122, POST REMOVAL OF FASTENER "D" IN CTR WING BOX REAR SPAR, FR.47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. "D" HOLE EXISTING DIA= 0.591 IN. FASTENER "D" HOLE REAMED TO REMOVSDR FDEA201308041759Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT3, WRI: 57101122, POST REMOVAL OF FASTENER "A" IN CTR WING BOX REAR SPAR, FR 47, LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. A-HOLE EXISTING DIA= 0.591 IN. FASTENER "A" HOLE REAMED TO REMOVE SDR FDEA201308041758Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT3, WRI: 57101122, POST REMOVAL OF FASTENER "B" IN CTR WING BOX REAR SPAR FR 47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "B" EXISTING DIA= 0.591 IN. REAMED TO REMOVE SCORE AND HOLE NDTSDR FDEA201308041774Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT4, WRI: 57101121, POST REMOVAL OF FASTENER "S" IN CTR WING BOX REAR SPAR FR 47 RT JUNCTION WITH FUSELAGE SCORE DAMAGED FOUND IN WALL OF HOLE. HOLE "S" EXISTING DIA= 0.653 IN. FASTENER "S" HOLE REAMED TO REMOVESDR FDEA201308041773Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT4, WRI: 57101121, POST REMOVAL OF FASTENER "Q" IN CTR WING BOX REAR SPAR FR 47 RT JUNCTION WITH FUSELAGE SCORE DAMAGED. FOUND IN WALL OF HOLE. HOLE "Q" EXISTING DIA= 0.653 IN. FASTENER "Q" HOLE REAMED TO REMSDR FDEA201308041772Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT4, WRI: 57101121, POST REMOVAL OF FASTENER "G" IN CTR WING BOX REAR SPAR FR 47 RT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "G" EXISTING DIA= 0.529 IN. FASTENER "G" HOLE REAMED TO REMOVE
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