JASC 5720
Service difficulty reports · 13,621
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 SWAA2026102122860Panel · crackedRIGHT MLG AFT SHELF PANEL WAS CRACKED. REPLACED FAIRING CAP IAW AMM 57-50-02 & 20-50-11.SDR DALA2026101505671Elevator · ground damageDAMAGE- AIRCRAFT RTB DUE LEFT WING STRUCK THE RIGHT ELEVATOR OF AIR CANADA AIRCRAFT, WHILE TAXIING. THE WINGLET SEVERED AND STUCK IN THE ELEVATOR OF THE OTHER AIRCRAFT. CORRECTIVE ACTION: WINGLET REPLACED. (LP# 8319112, 1852024, 1852021, 8319116, 8319118; AIRCSDR LR7A2026101103992Stiffener · crackedDURING SCHEDULED B-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH OUTER WING REAR SPAR VERTICAL STIFFENER CRACKED AT OWFS90. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001431654.SDR LR7A2026101103989Web · crackedDURING SCHEDULED B-3 CHECK UNDER SP-316, FOUND LH OUTER WING AFT SPAR WEB CRACKED AT OWS54-108L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001429002. / PSE# 57-50-10, AD 2012-06-09SDR JR2R20261004746Support Fitting · crackedRIGHT WHEELWELL AILERON QUADRANT LOWER SUPPORT FITTING IS CRACKED. REPAIRED PER ETD.SDR AALA202610062856Stiffener · crackedAIRCRAFT WAS NOT GROUNDED: LEFT WHEEL WELL, STIFFENER 111A1301-9 CRACKED. ACCOMPLISHED RE-INSPECTION. CRACK HAS PROGRESSED TO 16 1/2 INCHES. REPLACED STIFFENER IAW AARD 51-00-05 REPAIR 1 WITH THE MINOR DEVIATIONS NOTED IN EA379669.SDR WX0A2026100232968Diaphragm · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 5000-0026: 1711-45 L/H WING TRAILING EDGE DIAPHRAGM (RIBLET) AT RIB25 CORRODED. L/H WING TRAILING EDGE DIAPHRAGM (RIBLET) AT RIB25 REPLACED AS PER SRM 51-72-11-911-001 REV.159"SDR HNAA2026100100934Angle · crackedLEFT WING UPPER SKIN LATERAL FAIRING LOWER RETAINING ANGLE NR 1 CRACKED AT FWD AND AFT SIDE. R & R ANGLE IAW SRM 57-20-01SDR AALA202610159846Support Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON LT WING OUTBOARD FUEL TANK INTERNAL FITTING LT U-9 ZEE REINFORCEMENT ANGLE BETWEEN RIB 21 AND RIB 22. ACCOMPLISHED PERMANENT REPAIR IAW EA 379698.SDR AALA202610026682Intercostal · crackedAIRCRAFT IN BASE MAINTENANCE: R/H WING, ABOVE AFT END OF ENGINE PYLON, AFT INTERCOSTAL ON UPPER FIXED TRAILING EDGE PANEL CRACKED AT OTBD RIVET. DRILLED AND INSTALLED NEW INTERCOSTAL IAW AARD 51-00-05-1.SDR CALA2026092819871Beam · wornSTRIKER PLATE FOR FWD RT LATCH ON ECS DOOR 192CR, MISSING. AFTER CLEANING DAMAGE & FINDING IT OUT OF ALLOWABLE DAMAGE LINITS. REMOVED DAMAGE IAW 57-10-13. PERFORMED HFEC IAW NDT PART 6, 51-00-00 PROCEDURE 23, AND NDT PART 6, 51-00-00 PROCEDURE 16. NO DEFCTS NSDR FDEA202609221411Angle · crackedLEFT WING- LEADING EDGE COMPARTMENT ANGLE AT XOS 1083 FOUND CRACK ABOUT 0.4 INCHES. LEFT HAND WING LEADING EDGE COMPARTMENT CRACKED ANGLE AT XOS 1083 REMOVED PER MD-11 SRM 51-35-01-0G. FABRICATED ANGLE PER DOUGLAS DRAWING ARB 2920 REVISION BB. FABRICATESDR SWAA2026101299047Support Bracket · crackedCRACKED LT WING T/E SUPPORT BRACKET, IRSS 199 + 11 INCHES. REPLACED THE SUPPORT BRACKET AND FASTENERS IAW SRM-51-10-02, ITEM (9), & DWG 115A2001, SHEET 24, REV A.SDR IPXA2026100650463Strap · corrodedRIGHT WING FIXED TRAILING EDGE LOWER SURFACE INBD SIDE JUST OUTBD OF RT FLAP HAS SKIN BULDGING WITH INTERNAL CORROSION. REMOVED LOWER SKIN PANEL (1EA) AT R/W FIXED TRAILING EDGE FOR ACCESS IAW SRM 51-40-21. INSTALLED NEW STRAP AND RE-INSTALLED LOWER SKIN PANESDR SWAA2026102158537Support · no discrepancyCORROSION ON THE LT WING OTBD T/E ON RAIL SUPPORT. PERFORMED A DETAILED VISUAL INSPECTION ON THE LT WING OTBD T/E RAIL SUPPORT IAW SRM 51-10-04, & NO FOUND CORROSION ONLY MISSING PROTECTIVE TREATMENT. THE APPLICATION SEE TTG8Q01ERA8A.SDR SWAA2026102119544Support Angle · crackedCRACKED SUPPORT ANGLE FOR RT WING ACCESS PANEL 651FB. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-20-01, & DWG 115A2710, SHT 9, REV A.SDR CALA2026092119630Stiffener · corrodedLEFT WING T/E CAVITY THROUGH ACCESS PANEL 561FB, AT UPPER PANEL AFT MOUNTING BRACKET HAS FOUR AREAS OF EXFOLIATION, REMOVED AND REPLACED THE STIFFENER. ON LT WING UPPER TRAILING EDGE WSTA 735.80 - 775.10 IAW SRM 51-40-02.SDR SWAA2026102158399Plate · damagedELONGATED HOLE ON LT WING CORRUGATED PLATE T/E, IRSS 199 + 15. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02, SRM 51-10-02, DWG 115A171327, SHT 6, REV A, & DWG 115A2001, SHT 78, REV A.SDR SWAA2026102118304Plate · damagedELONGATED HOLE ON THE SUPPORT OF CORRUGATED PLATET RAILING EDGE, ORSS 297 + 25, RT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02, SRM 51-10-02, & DWG 115A3700, SHT 96, REV-.SDR SWAA2026102117802Support Angle · crackedCRACKED RT WING SUPPORT ANGLE FIXED T/E, ORSS 261 + 16. REPLACED THE SUPPORT ANGLE & FASTENERS IAW SRM 51-40-02, & DWG 115A6200, SHT 17, REV A.SDR SWAA2026100759352Support Bracket · crackedCRACKED SUPPORT BRACKET FOR ACCESS PANEL 551FB ON THE LT WING. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.SDR SWAA2026100765174Support Angle · crackedCRACKED SUPPORT ANGLE FOR ACCESS PANEL 551FB, LT WING. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 115A2710, SHEET 6, REV B.SDR SWAA2026100702313Angle · crackedCRACKED ANGLE, TRAILING EDGE ORSS 261 + 10 INCHES ON THE LT WING. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, AND SRM 51-40-02-0G-0.SDR AALA202609251222Angle · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING, AS VIEWED FROM BELOW, LOWER FORWARD CORNER OF PANEL 651AT GREEN "Z" ATTACH BRACKET CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-40-02.SDR IPXA2026091850925Bracket · crackedCRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.96. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO:114T1240 SH 6 REV: - .SDR AALA202610029120Support Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: R/H WING TRAILING EDGE SUPPORT BEAM ASSEMBLY IS CRACKED AT WS 965. PERFORMED PERMANENT REPAIR AT R/H WING T/E SUPPORT BEAM ASSY AT WS 965 IAW AARD 57-51-10-5.SDR AALA202609159473Support Angle · crackedAIRCRAFT IN BASE MAINTENANCE: PANEL SUPPORT ANGLE (115A2156-8), INBOARD OF FLAP MID SPAN DEFLECTION RIB, HAS 3 INCH CRACK IN O/B UPPER RADIUS. REMOVED AND REPLACED SECONDARY SUPPORT ANGLE FROM T/E MIDSPAN PANEL IAW SRM 51-10-02-0G AND SRM 51-40-02-0G.SDR SWAA2026091450744Bracket · crackedNR 1 ENGINE HYDRAULIC SUPPORT BRACKET CRACKED, INBD OF R3 NACELLE SUPPORT FITTING AFT BOLT. REPAIRED ON W/O 2600R1343.SDR SWAA2026101486080Channel · corrodedCORRODED RAIL NUT PLATES INTERNAL CAVITY LT WING L/E OFSS 580 +12 INCHES, REMOVED AND REPLACED GANG CHANNEL IAW SRM 51-10-02-0G-0, ITEM 9, & SRM 51-40-02.SDR KCSA202609091207Web · crackedDURING W/O 713028794 SURFACE HFEC INSPECTION AT RT WBL 432.65 FIXED RIB WB, CRACK FOUND.SDR IPXA2026102136117Gusset · crackedLH WW HAS A CRACKED GUSSET.SDR SWAA2026091478886Angle · crackedCRACK ON ANGLE LOCATED TRAILING EDGE INTERNAL STRUCTURE AREA DEFLECTION RIB LT WING. REPLACED ANGLE LOCATED TRAILING EDGE INTERNAL STRUCTURE AREA DEFLECTION RIB LT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2900, REV E.SDR 2026FA0000724Stiffener · crackedR/H WING FWD LWR I/B SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000721Stiffener · crackedR/H WING FWD LWR I/B SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR CALA2026090719256Support · corrodedLEFT WING LE O/B LOWER PANEL SUPPORT HAS CORROSION AT STA SS 67.53 LH SIDE. REMOVED SUPPORT ON LEFT WING LE O/B LOWER PANEL AT SLAT STA 67.53 LT SIDE, RECEIVED NEW SUPPORT. LOCATED AND DRILLED THE NEW SUPPORT, APPLIED ALODINE ON NEW HOLES, APPLIED PRIMER & ISDR SWAA2026092565083Bracket · crackedACCESS PANEL 651FB HAD A CRACKED BRACKET. REMOVED AND REPLACED THE BRACKET ON THE RT WING ACCESS PANEL 651FB IAW SRM 51-40-02-0G-0.SDR IPXA2026091553994Support Channel · crackedRH MLG WEEL WELL FWD SEAL SUPPORT CRACKED. REMOVED PANELS 198CR AND 198BR FOR ACCESS AND REMOVRD SEAL AND SEAL RETEINER AND SEAL SUPPORT DAMAGED IAW B757-200PF SRM 51-40-02-0G. INSTALLED NEW SEAL AT RH MLG WEEL WELL IAW B757-200PF AMM 32-12-51-404-004.SDR IPXA2026091554044Support Bracket · crackedRIGHT MLG WEEL WELL RH GEAR DOOR CLOSED SWITCH LATERAL SUPPORT CRACKED. REMOVED DAMAGED SUPPORT BRACKET AT RT MLG WEEL WELL R/H GEAR DOOR CLOSED SWITCH LATERAL IAW SRM B757-200PF SRM 51-40-02-0G. INSTALLED NEW ANGLE IAW B757-200PF SRM 51-40-02-0G-0.SDR IPXA2026091554070Support Bracket · crackedRH MLG WEEL WELL FWD SEAL SUPPORT ANGLE CRACKED. REMOVED SEAL SUPPORT ANGLE IS CRACKED AT R/H MLG WEEL WELL FWD IAW SUPPORT ANGLE IAW SRM SRM 51-40-02-0G. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-0.SDR IPXA2026100214982Support Bracket · missingLH WING LEADING EDGE INSIDE OF ACCESS PANEL 512KB CAMLOC SUPPORT BRACKET IS MISSING P/N: 244-16 (QTY 01). INSTALLED NEW RETAINER P/N A5724183600251 AT Z500 / LH WING LEADING EDGE INSIDE OF ACCESS PANEL 512KB: I.A.W. A300-600 SRM 51-40-21-001SDR SWAA2026091481991Support Bracket · elongatedELONGATED HOLE SUPPORT BRACKET ACCESS PANEL 651GB AT RT WING. REPLACED SUPPORT BRACKET OF ACCESS PANEL 651GB AT RT WING IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, AND DWG 115A2714 SHEET 7 REV.SDR HNAA2026092100867Angle · crackedRIGHT WING UPPER SKIN LATERAL FAIRING LOWER RETAINING ANGLE CRACKED. R & R ANGLE IAW SRM 51-40-02.SDR HNAA2026092100866Angle · crackedLEFT WING UPPER SKIN LATERAL FAIRING LOWER RETAINING ANGLE NR 2 CRACKED. R & R ANGLE IAW SRM 51-40-02.SDR HNAA2026092100865Angle · crackedRIGHT WING UPPER SKIN LATERAL FAIRING LWR RETAINING ANGLE CRACKED. R & R THE RETAINING ANGLE IAW SRM 51-40-02.SDR 2026FA0000720Stiffener · crackedR/H WING FWD LWR I/B SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR SWAA2026091438273Bracket · crackedCRACK BRACKET TRAILING EDGE LOCATED IRSS 210 APROX AT RT WING. REPLACED BRACKET IAW SRM 51-40-02, SRM 51-10-02, AND DWG 115A2001, SHEET 24, REV A.SDR SWAA2026092973065Web · crackedCRACKED WEB TRAILING EDGE PANEL, RT WING, ORSS 266. REPLACED THE WEB AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2512, SHEET 16, REV-.SDR SWAA2026092956153Support Angle · crackedCRACKED SUPPORT ANGLE, RT WING, ORSS 261. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2512, SHEET 13, REV- .SDR SWAA2026092933487Support Angle · crackedCRACKED SUPPORT ANGLE, ORSS 271, RT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 115A6200, SHEET 17, REV A.SDR SWAA2026092956067Support Angle · crackedCRACKED SUPPORT ANGLE AT THE FIXED TRAILING EDGE PANEL, ORSS 261, LT WING. REPLACED THE SUPPORT ANGLE IAW RM 51-10-02, PARAGRAPH 9, SRM 51-40-02, DWG 115A2512, SHEET 16, REV-.
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