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 ASOA201101800Fairing · damagedLT WING TIP FAIRING REMOVED DUE TO DAMAGE. R & R LT WING TIP FAIRING IAW AMM 57-30-01. REMOVED LT WING TIP FAIRING IAW AMM 57-30-01. REPLACED LT WING TIP FAIRING IAW AMM 57-30-01.SDR UALA2011090204738Fastener · damagedDAMAGED RIVET ON PANEL 29" OUTBOARD OF LT ENG PYLON SAILTAIL AREA, LEADING EDGE OF PANEL. REPLACED FASTENER.SDR COEA2011082929816Bracket · corrodedHEAVY CK COE / LEVEL 2 CORROSION: RT WING INBOARD AND CENTER SPRING BRACKET FOR PANEL 631BB HAS LEVEL 2 CORROSION ON SURFACE. (LENGTH 5.5", WIDTH 3.5", DEPTH .009") REMOVED AND REPLACED SPRING BRACKET.SDR COEA2011082928816Bracket · corrodedHEAVY CK COE / LEVEL 2 CORROSION: RT WING SPRING BRACKETS FOR PANEL 631AB HAS LEVEL 2 CORROSION ON SURFACE. (LENGTH 2.5", WIDTH 3.5", DEPTH .009") REMOVED AND REPLACED SPRING BRACKET.SDR IPXA1M69081Stiffener · crackedINSPECTION TYPE:3C, LT WING L/E COMPT, OTBD OF SLAT TRACK NR 10 L/E STIFFENER FOUND CRACKED. REPAIRED STIFFENER (STRINGER) IN LT WING L/E COMPT AT STA XOS667 IAW SRM 57-40-03, REPAIR 2 & DWG ARB2932.SDR CA110824001Angle · cracked(CAN) WHILE CARRYING OUT AN INSPECTION OF THE WING FUEL TANKS FOR TASK RJ2-57-510-502 AND RJ2-57-610-502, THE AME NOTICED CRACKS ON THE LOWER CAP ANGLES FWD OF RIB AT APPROX WS29.42 IN THE CENTER AND RT FUEL TANKS. CAP ANGLES PN 601R-10011-13A AND 601R10011-14SDR A6WA201140844Fairing · chafedCHAFING DAMAGE ON OTBD ENDS OF FAIRING 193AB ON LOWER SKIN UNDER FAIRING MATING SURFACES. REPAIRED DAMAGE IAW REO 601R-57-21-880, REV C, ZONE A.SDR EIAA2011183Support Beam · crackedRT WING REAR SPAR CAVITY SPOILER SUPPORT BEAM UPPER CHORD AT WBL 235.2 FOUND CRACKED. CRACKED CHORD TRIMMED. HFEC INSP TO VERIFY CHORD IS CRACK FREE. FABRICATED REPAIR ANGLES AND CHORD SEGMENT AND INSTALLED PER BOEING DRAWING 65B07738-58 AND EN 049-11.SDR COMA2011082250059Structure · damagedLT WING FUEL DRAIN AFT HOLE AT WS 88.50 IS MISDRILLED. COMPLIED WITH REO 601R-57-21-1485 ON WS 88.50 LT BY REAMING AND INSTALLING FREEZE PLUG.SDR COMA2011082250058Structure · damagedRIGHT WING FUEL DRAIN AFT HOLE AT WS 48.00 IS MISDRILLED. COMPLIED WITH REO R01R-57-21-1485 ON WS 48.00 RT BY REAMING AND INSTALLING A FREEZE PLUG.SDR ABXA2011081898Web · crackedLT WING L/E WEB AT WS 475 AT NR 5 SLAT AREA HAS CRACKED INBD UPPER CORNER. REMOVED L/E WEB. REPAIRED IAW SRM CH 51-70-11 AND INSTALLED IAW SRM CH 51-40-2 AWG.SDR IPXA11668875Stiffener · crackedINSPECTION TYPE:C, WING CENTER TANK FRONT SPAR VERTICAL STIFFENER TOP AREA FOUND CRACK JUST AT STA 785.9 RBL 10.94 STIFFENER REPAIRED IAW SRM 57-10-10-2R2, REPAIR 2, FIG 201, REV 50 AT STA 785.9 RBL 10.94 ORG MATERIAL BAC1518-912-2024T3511 CRACK LENGTH 1.2" CUSDR IPXA11668874Stiffener · crackedINSPECTION TYPE:C WING CENTER TANK FRONT SPAR VERTICAL STIFFENER TOP AREA FOUND CRACK JUST AT STA 785.9 LBL 10.94 WNG CTR TANK FRONT SPAR VERT STIFFENER REPAIRED PER SRM 57-10-10-2R2 REPAIR 2 FIG 201 REV 50 JUST AT STA 785.9 LBL 10.94 ORG MAT'L BAC1518-91SDR UIEA2011102100623Support · corrodedLT WING ACCESS PANEL SUPPORT AT WBL 289.45 HAS CORROSION. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. TREATED AND PRIME.SDR KPVA20110816001Strap · crackedLT WING STRINGER 14 AT STA YW 196 STRAP PN 85711248 CRACKED.SDR KPVA 201108Strap · crackedLT WING STRINGER 14 AT STATION YW 196 STRAP PN 85711250 IS CRACKED.SDR QXEA2011081800683Channel · corrodedWHILE ATTEMPTING TO CLOSE FUEL PANEL 522BT FOUND CORRODED NUTPLATE SHELL. REMOVED GANG CHANNEL AND REPLACED NUTPLATE WITH NEW IAW SRM 51-42-75-01-02. INSTALLED GANG CHANNEL IAW Q400 SRM 51-42-75-02-01.SDR FDEA201108163298Panel · chafedNR 1, PYLON HYD LINE UNIONS AT AFT FAIRING DISCONNECT POINT FRETTING IN WING REAR SPAR FITTING. REWORK ACCOMPLISHED ON EA 6-5720-150921.SDR FDEA201108163297Panel · chafedLT PYLON HYD LINE UNIONS AT AFT FAIRING DISCONNECT POINT FRETTING IN WING REAR SPAR FITTING. REWORKED ACCOMPLISHED ON EA 6-5720-150921.SDR FDEA201108163296Panel · chafedRT PYLON HYD LINE UNIONS AT AFT FAIRING DISCONNECT POINT FRETTING IN WING REAR SPAR FITTING REWORKED, ACCOMPLISHED ON EA 6-5720-150920.SDR PCSA2011083002Support · corrodedLEFT WING UPPER AFT COVE PANEL SUPPORT OUTBOARD FLANGE CORRODED. REPLACED CORRODED SUPPORT.SDR PCSA2011083001Support Bracket · corrodedRIGHT WING ROOT UPPER SURFACE FAIRING SUPPORT BRACKET CORRODED. REPLACED CORRODED BRACKET.SDR SWAA115769Stiffener · crackedDURING SCHEDULED 24Y CHECK, FOUND RT WING STIFFENER 8 LOWER FLANGE CRACKED AT WBL 453. REPAIRED STIFFENER IAW EA AND EO.SDR SWAA115768Stiffener · crackedDURING SCHEDULED 24Y CHECK, FOUND RT WING STIFFENER 7 AND 8 LOWER FLANGE CRACKED AT WBL 355. REPAIRED STIFFENER IAW EA AND EO.SDR IPXA11568752Stiffener · corrodedINSPECTION TYPE:C-CHECK, RT WING DEFUELING VALVE BONDING WIRE MOUNT POINT HAS CORROSION ON VERTICAL STIFFENER. REPAIRED RT WING DEFUELING VALVE BONDING WIRE MOUNT POINT STIFFENER IAW EA 111018.SDR FDEA201107303041Angle · gougedRT WING FIXED T/E STRUCTURE, RIB LOWER ANGLE GOUGED ABOVE INBD FLAP OTBD GUIDE ROLLER. R & R BOTTOM ANGLE ON RT OUTER SHROUD BOX AT INNER FLAPS OUTER ROLLER GUIDE IAW SRM 51-72-10, SRM 51-40-21.SDR K11A2011083072201Stiffener · corrodedL/W FRONT SPAR STIFFENER CORROSION, 1X4 INCHES.SDR IPXA1M68466Strap · crackedINSPECTION TYPE:3C, RT OTBD WING LOWER FIXED L/E STRAP CRACKED OTBD OF SLAT ACTUATING MECHANISM. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT STRAP IN RT WING L/E IAW ARB1180, SRM 51-21-01, SRM 51-35-01.SDR DALA1145213738Vapor Barrier · crackedRT WHEEL WELL VAPOR BARRIER PANEL WAS CRACKED AND REPAIRED PER SRM 57-10-10.SDR KCSA111168Support · corrodedLEFT WING LEADING EDGE UPPER SUPPORT ON BULLNOSE CORRODED FROM FSSI 562 TO 620.SDR FDEA201107172767Support Bracket · crackedLT WING T/E LOWER PANEL SUPPORT BRACKET AT INBD FLAP OTBD HINGE FAIRING OTBD FOUND CRACKED. REMOVED IAW SRM 51-33-01, REV 47. NEW SUPPORT BRACKET FABRICATED IAW DWG ARC0361. NEW SUPPORT BRACKET HOLES PICKED UP IAW SRM 51-31-01, REV 47 AND INSTALLED IAW SRM SDR FDEA201107122662Support · corrodedCORROSION TO RIGHT WING SUPPORT DOUBLER LOWER SURFACE OTBD OF RIB 8 AT FRONT SPAR ATTACHMENT.SDR IPXA1M67976Strap · crackedINSPECTION TYPE:2C, RT WING FIXED L/E COMPT SPLICE STRAP CRACKED AT XOS669 REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERNAL SPLICE STRAP IN RT WING L/E AT STA XOS669 IAW DWG ARB3954 AND SRM 51-33-01.SDR TSAA1154007Fairing · damagedAFT LT PYLON FAIRING ASSY-WING TO NACELLE STRUCTURE DAMAGED. REPLACED NR1 ENGINE TO WING AFT FAIRING IAW AMM 54-51-32. NO MAJOR REPAIR REQUIRED. THE ACFT WAS RETURNED TO SERVICE.SDR ASAA1149941Attach Angle · crackedLT WING T/E FIXED PANEL ATTACH ANGLE IS CRACKED INBOARD OF NR 3 SPOILER. FABRICATED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51 40 01, 51 40 02, 51 40 05 AND BOEING DRAWING BAC1470 2793.SDR IPXA11667580Stiffener · crackedINSPECTION TYPE:8C, FWD CARGO COMPT WING CENTER TANK FRONT SPAR VERTICAL STIFFENER UPPER AREA FOUND CRACKED JUST AT STA 785.9, LBL 10.94. ORIGINAL MATERIAL IS BAC1518-912-2024T3511, CRACK LENGTH IS 1.25", CUT OFF LENGTH IS 19.5". THIS REPAIR IS CLASSIFIED ASSDR IPXA11667578Stiffener · crackedINSPECTION TYPE:8C, FWD CARGO COMPT WING CENTER TANK FRONT SPAR VERTICAL STIFFENER UPPER AREA FOUND CRACKED JUST AT STA 785.9 LBL 32.94. ORIGINAL MATERIAL IS BAC1518-749-2024T3511, CRACK LENGTH IS 2.25", CUT OFF LENGTH IS 16.5", THIS REPAIR IS CLASSIFIED AS ASDR REXA201100517Structure · chafedCHAFE BETWEEN WING LOWER AFT SKIN PLANK AND MLG FAIRING AT RBL 45 MEASURING 0.030" DEEP IN ZONE "A". REPAIRED IAW BOMBARDIER REO 601R-57-21-880 REV B.SDR REXA201100466Structure · chafedCHAFE BETWEEN WING LOWER AFT SKIN PLANK AND MLG FAIRING AT RBL45 MEASURING 0.030" DEEP IN ZONE "A". REPAIRED IAW BOMBARDIER REO 601R-57-21-880 REV B.SDR EE4Y20110377Strip · wornLT WING, T/E, STA 5512 BETWEEN SPOILER NR 1 AND SPOILER NR 2 FIXED FAIRING LOWER SECTION, STRIP RUBBING WITH WEAR. MAJOR REPAIR .SDR BQVA2011061300010Structure · corrodedDURING COMPLIANCE OF CMP CODES 573013 & 573014 WINGLET ATTACH HARDWARE (LEFT & RIGHT) - INSPECTION, SOME CORROSION WAS FOUND IN THE WINGLET ATTACH BORES ONCE THE BUSHINGS WERE REMOVED.SDR UIEA2011060800284Support Beam · corrodedCORRODED CLIP ISLES 1036, LT WING L/E COMPT LOWER SUPPORT BEAM AREA. REPLACED WITH NEW PART IAW SRM 51-40-02, REV 9.SDR HYIA20110607001Strap · corrodedDURING HEAVY CHECK INSPECTION, CORROSION WAS FOUND ON THE UPPER SURFACE OF THE RT WING STRIP STRAP OF RIB 20 AT WS 7900. THE CORROSION WAS REMOVED IAW SRM 51-21-58 AND EXCEEDED THE LIMITS OF THE SRM. REPAIRED IAW WITH EA 12-2011-014.SDR WX0A070880Doubler · crackedLT WING UPPER BEAVER TAIL DOUBLER ABOVE MLG AREA IS CRACKED FROM FASTENER TO EDGE (O/B SIDE). REPAIRED WO 2003754 N/R 657955 PER MD80 SRM 57-03 FIG 34, PAGE 143.SDR IPXA11567248Channel · chafedINSPECTION TYPE:MOD, LT UNDERWING FAIRING STRUCTURE UPPER FWD CHANNEL ASSY IS WORN AND CHAFED. PN 313N5004-89 R & R CHANNEL IAW SRM 51-40-02.SDR EE4Y20110324Strap · wornLT WING, STA 4862 T/E FIXED UPPER PANEL STRAP WITH WEAR. MAJOR REPAIR.SDR EE4Y20110323Strap · wornRT WING, STA 4862 T/E FIXED UPPER PANEL STRAP WITH WEAR. MAJOR REPAIR.SDR FDEA201105201889Shim · migratedRT WING BETWEEN OTBD NAC FITTING AND LOWER WING SKIN FOUND WITH SHIMS MIGRATION AT WS 303.5. REPAIRED IAW EA F-5740-146463 PART 1.SDR FDEA201105121826Stiffener · crackedRIGHT WING LOWER SKIN SUPPORT JUST IN FRONT OF ACCESS DOOR 675FB FOUND STIFFENER CRACKED. PERFORMED REPAIR PER DRAWING R57340199 ISSUE E AND EA 6-5710- 150321 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201105121824Stiffener · crackedLT WING LOWER SKIN SUPPORT JUST FRONT OF ACCESS DOOR 575FB FOUND STIFFENER CRACKED. LT WING LOWER SKIN SUPPORT JUST IN FRONT OF ACCESS DOOR 575FB FOUND STIFFENER CRACKED, PERFORMED REPAIR PER DRAWING R57340199 ISSUE E AND FEDEX EA 6- 5710-150320 PART 1.
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