JASC 5720
Service difficulty reports · 13,629
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 SWAA2025081292843Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING IAW SRM 51-40-02 AND DRAWING 115A2001, SHEET 30, REV A.SDR SWAA2025081292846Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT LT WING. REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE IRSS 217 AT LH WING IAW SRM 51-40-02 AND DWG 115A2001, SHEET 30, REV A. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM 57-51-02. CRACK LENGTH: 0SDR SWAA2025081292845Angle · crackedCRACK ON ANGLE LOCATED ORSS 271 TRAILING EDGE AT LT WING. REPLACED ANGLE LOCATED ORSS 271 TRAILING EDGE AT LT WING IAW SRM 51-40-02, SRM SRM 51-10-02, ITEM 9, AND DRAWING 115A2930, SHEET 7, REV -.SDR SWAA2025081292841Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT RT WING 2025-452361<[01] REPLACED CORRUGATED PLATE AND FASTENERS TRAILING EDGE LOCATED ORSS 241 AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9 AND DWG 115A2001 SHEET 30 REV-A. MEASURE SDR SWAA2025081292837Support Angle · brokenBROKEN SUPPORT ANGLE LOCATED IRSS 212 TRAILING EDGE AT RT WING, REPLACED SUPPORT ANGLE LOCATED IRSS 212 TRAILING EDGE AT RT WING IAW SRM 51-10-02; SRM 51-40-02 AND DWG 115A2001; SHEET 24 AND REV A.SDR SWAA2025081292838Plate · corrodedCORROSION SUPPORT PLATE LOCATED ORSS 376 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING. REPLACED SUPPORT PLATE LOCATED ORSS 376 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING IAW SRM 51-040-20-G-0. AND PERFORMED VISUAL INSPECTION ON ADJACENT AREASSDR SWAA2025081292839Web · crackedCRACK ON WEB TRAILING EDGE LOCATED ORSS 276 AT RT WING. REPLACED WEB TRAILING EDGE LOCATED ORSS 276 AT RT WING IAW SRM 51-40-02 AND DWG 115A2512 SHEET 5 REV. B . DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM 57-51-02. CRACK LENGTH: 0.500.SDR SWAA2025081292840Support Angle · crackedCRACK ON SUPPORT ANGLE INTERNAL CAVITY LOCATED ORSS 271 TRAILING EDGE AT RT WING. REPLACED SUPPORT ANGLE INTERNAL CAVITY LOCATED ORSS 271 TRAILING EDGE AT RT WING IAW SRM 51-40-02 AND DWG 115A2930 SHEET 6 REV - . DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM 57-51SDR SWAA2025072192496Bracket · crackedVERTICAL BRACKET CRACKED UNDER FWD INBD CORNER OF PANEL 551AT. REMOVED & REPLACED VERTICAL BRACKET UNDER FWD INBD CORNER OF PANEL 551AT. I.A.W. SRM 51-40-02.SDR SWAA2025081491965Panel · elongatedELONGATED HOLES ON ACCESS PANEL 561BB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WIN IAW SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2025081491720Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 RT WING. REPLACED ANGLE TRAILING EDGE ORSS 271, RT WING IAW SRM 51-10-02-0G-0 ITEM 9, SRM 51-40-02-0G-0, AND DWG 115A2930, SHEET 8, REV -.SDR SWAA2025081491722Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING. REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING IAW SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 115A2930, SHEET 6 REV -. MEASUREMENT OF CRACK IS L: 0.225.SDR UIEA2025071300942Web · crackedLEFT WING L/E FIXED INTERNAL AT INBD ILES 693.5 WEB CRACKED. WEB CRACK AREA REPAIRE AS PER RI-57-41-17749 REV A. NO FURTHER DEFECTS NOTED.SDR IPXA2025080138830Angle · crackedRIGHT WING, KRUEGER BOX AREA, BY RIB 2, ANGLE REINF. IS CRACKED. INSTALLED ANGLE RH WING, KRUEGER BOX AREA, BY RIB 2, IAW A300-600 SRM 51-40-21.SDR IPXA2025080808880Angle · crackedRIGHT WING, KRUEGER BOX AREA, LOWER AREA, 2ND ANGLE BRACKET IS CRACKED. STAMP23. INSTALLED ANGLE RH WING, KRUEGER BOX AREA, BY RIB 2, IAW A300-600 SRM 51-40-21. REVIEWEDSDR IPXA2025080504516Bracket · crackedHYDRAULIC CASE DRAIN LINE SUPPORT BRACKET IS CRACKED, LOCATED AT LT WING INSIDE OF ACCESS PANEL 575AB.SDR SWAA2025071789886Tail Cone · damagedCR VB #3 FLAP FAIRING AFT CONE HAS PULLED FASTENERS<[01] REMOVED AND REPLACED TAILCONE ON #3 FLAP FAIRING IAW B737-800 SRM 51-40-02 AND REF. B737-800 AIPC 27-51-18-01REMOVED AND REPLACED TAILCONE ON #3 FLAP FAIRING IAW B737-800 SRM 51-40-02; B737-800 AMM 20-50SDR SWAA2025081187415Web · crackedCRACK ON WEB LOCATED AT LEVEL ORSS 268 DEFLECTION CONTROL RIB AREA AT LT WING. REPLACED WEB LOCATED AT LEVEL ORSS 268 DEFLECTION CONTROL RIB AREA AT LT WING IAW SRM- 51-40-02-0G-0 AND DWG # 115A2512 SHEET 14 REV A.SDR SWAA2025081187416Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 265 DEFLECTION CONTROL RIB AREA AT LT WING. REPLACED SUPPORT ANGLE LOCATED AT LEVEL ORSS 265 DEFLECTION CONTROL RIB AREA AT LT WING IAW SRM-51-40-02 AND DWG 115A2930 SHEET 7 REV-.SDR SWAA2025081187420Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 264 DEFLECTION CONTROL RIB AREA AT RT WING. REPLACED SUPPORT ANGLE LOCATED AT LEVEL ORSS 264 DEFLECTION CONTROL RIB AREA AT RT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 8 REV -.SDR SWAA2025073087176Angle · crackedCRACK ON ANGLE TRAILING EDGE LOCATED AREA DEFLECTION CONTROL RIB ORSS278 RT WING. REPLACED ANGLE AND FASTENERS TRAILING EDGE LOCATED AREA DEFLECTION CONTROL RIB ORSS278 RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A6200; SHEET 11; REV B.SDR SWAA2025072987175Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS327 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS TRAILING EDGE LOCATED ORSS327 AT RT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9, AND DWG 115A3700 SHEET: 41 REV -.SDR SWAA2025071787165Support Web · crackedRIGHT WING INBD. FIXED UPPER SHELF PANEL SUPPORT WEB JUST INBD. OF DEFLECTION CONTROL RIB IS CRACKED. REMOVED CRACKED SUPPORT WEB PER SRM 51-40-02.SDR CALA2025070906374Bracket · wornR/H AFT FLAP STRUT SENSOR BRACKET PLATE BEARING HAS EXCESSIVE PLAY. REMOVED AND REPLACED DICREPANT R/H AFT FLAP STRUT SENSOR BRACKET IAW A319 SRM 51-42-11-001.SDR SWAA2025073086807Angle · crackedCRACK ANGLE ON TRAILING EDGE LOCATED ON AREA DEFLECTION CONTROL RIB ORSS278 LT WING. REPLACED ANGLE ON TRAILING EDGE LOCATED ON AREA DEFLECTION CONTROL RIB ORSS278 LT WING IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG: 115A6200; SHEET: 11; REV: B. SDR SWAA2025073087039Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED ON TRAILING EDGE IRSS141 LT WING. REPLACED SUPPORT BRACKET LOCATED ON TRAILING EDGE IRSS141 LT WING IAW. B737-700 SRM 51-40-02 AND DWG 115A2000 SHEET 21 REV-; MEASURES CRACK IS 1.434 INCHES.SDR SWAA2025073086242Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED INBOARD AUXILIARY TRACK SLAT 1 AT LT WING. REPLACED SUPPORT ANGLE LOCATED INBOARD AUXILIARY TRACK SLAT 1 AT LT WING IAW. SRM 51-40-02 MEASURES OF CRACK IS 1.124 INCHES.SDR SWAA2025072386272Bracket · crackedCRACK TRAILING EDGE BRACKET LOCATED INTERNAL CAVITY IRSS 199 PLUS 12 INCHES AT LT WING. REPLACED THE BRACKET LOCATED INTERNAL CAVITY IRSS 199 PLUS 12 INCHES AT LT WING IAW SRM 51-40-02. LENGTH OF CRACK: 0.870.SDR SWAA2025072186271Strap · debondedDEBONDED TRAILING EDGE STRAP LOCATED FLAP TRACK 2 AREA WING LOWER SURFACE AT LT WING. BONDED TRAILING EDGE STRAP LOCATED FLAP TRACK 2 AREA WING LOWER SURFACE AT LT WING IAW B737-700 AMM 51-31-00-390-804. BONDED TRAILING EDGE STRAP LOCATED FLAP TRACK 2 AREA WSDR SWAA2025072386269Bracket · crackedCRACK TRAILING EDGE BRACKET LOCATED DEFLECTION RIB AREA ORSS 261 PLUS 7 INCHES AT LT WING. REPLACED TRAILING EDGE BRACKET LOCATED DEFLECTION RIB AREA ORSS 261 PLUS 7 INCHES AT LT WING IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 AND DWG 115A2930; SHEET 8; REV - . MSDR SWAA2025073085852Web · crackedLEFT WING TRAIING EDGE TRANSVERSE WEB OTBD ATTACH ANGLE CRACKED. REMOVED & REPLACED A NEW ATTACH ANGLE AT LT WING T/E TRANSVERSE WEB OTBD SIDE IAW SRM 51-40-02 & DWG 115A6200 SH 11 REV:B.SDR SWAA2025073085415Angle · crackedCRACK ON ANGLE LOCATED DEFLECTION CONTROL RIB AREA AT LEVEL ORSS 261 AT RT WING. REPLACED WEB AND FASTENERS LOCATED DEFLECTION CONTROL RIB AREA AT LEVEL ORSS 261 AT RT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 115A2900, SHEET 1, REV E.SDR SWAA2025071585571Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS275 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS275 AT RT WING IAW SRM B737-700 51-10-02 SRM 51-40-02 AND DRAWING 115A 2001; SHEET 29; REV.-. MEASURE OF CRACK IS: 1.313.SDR JGVR20250625001Angle · corrodedMECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED IN THE RH MLG WHEEL WELL, ON THE AFT SPAR LOWER CLIP INSIDE BAY 720DR, INBOARD AREA PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED CORROSION BLEND PER NETJETS ENGINEERING REQUEST FOR TECHNICAL SERVISDR SWAA2025071784706Intercostal · crackedL/H WING TRAILING EDGE; INTERCOSTAL WEB INBD OF DEFLECTION CONTROL RIB IS CRACKED. REMOVED AND REPLACED INTERCOSTAL WEB PER SRM 51-40-02.SDR SWAA2025071784705Angle · crackedL/H WING TRAILING EDGE; ANGLE INBD OF INTERCOSTAL WEB AT DEFLECTION CONTROL RIB IS CRACKED. REMOVED CRACKED ANGLE INBD OF INTERCOSTAL WEB PER SRM 51-40-02. CRACKED ANGLE INBD OF INTERCOSTAL WEB HAS BEEN REMOVED. LOCATED; DRILLED AND DEBURRED REPLACEMENT ANSDR SWAA2025071585134Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9. LENGTH OF CRACK IS:0.467.SDR SWAA2025070185155Web · crackedRIGHT WING TRAILING EDGE TRANSVERSE WEB ABOVE THE #2 PYLON AFT TIP HAS CRACK. REMOVED AND REPLACED RIGHT WING TRAILING EDGE TRANSVERSE WEB ABOVE THE #2 PYLON IAW SRM 51-40-02 AND AIPC 57-50-00-36A.SDR SWAA2025070185156Web · crackedLEFTWING TRAILING EDGE TRANSVERSE WEB ABOVE THE #1 PYLON AFT TIP CRACKED AT FASTENER. REMOVED AND REPLACED LEFT WING TRAILING EDGE TRANSVERSE WEB ABOVE THE #1 PYLON IAW SRM 51-40-02 AND AIPC 57-50-00-36A.SDR SWAA2025071584092Support Bracket · crackedRIGHT WING T/E PANEL 651FB WIRE BUNDLE SUPPORT BRACKET CRACKED. REMOVED AND REPLACED R/W T/E PANEL 651FB WIRE BUNDLE SUPPORT BRACKET IAW SRM 51-40-02-0G-0 AND SOPM 20-50-02.SDR SWAA2025071583403Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 279 AT LT WING. REPLACED ANGLE LOCATED ON TRAILING EDGE LOCATED ORSS 279 AT LT WING. IAW B737-700 SRM 51-10-02; ITEM 9. SRM 51-40-02 AND DWG 115A6200; SHEET: 10 AND REV: -.SDR SWAA2025071583402Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED FWD POSITION AT LEVEL ORSS 270 AT RT WING. REPLACED ANGLE TRAILING EDGE LOCATED FWD POSITION AT LEVEL ORSS 270 AT RT WING IAW SRM 51-10-02; ITEM 9 AND SRM 51-40-02. MEASURE OF CRACK IS 0.995.SDR SWAA2025072181455Angle · crackedCRACK OUTBOARD SUPPORT ANGLE OF INBOARD AUXILIARY TRACK SLAT 1 AT LT WING. REPLACED ANGLE LOCATED OF INBOARD AUXILIARY TRACK SLAT 1 AT LT WING AND IAW SRM 51-40-02;[03] TOOK MEASURE OF CRACK IS: L= 1.350 LOCATED SUPPORT ANGLE.SDR SWAA2025071681458Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED FRONT SPAR BOOST PUMP IFSS 116 TO IFSS 126 AT RT WING. REPLACED SUPPORT ANGLE LOCATED FRONT SPAR BOOST PUMP IFSS 116 TO IFSS 126 AT RT WING I.A.W.B737-700 SRM 51-10-01 AND SRM 51-40-05 AND DRAWING 116A3939 SHEET 1 REV B.SDR SWAA2025071580589Angle · crackedCRACK ANGLE TRAILING EDGE AT LEVEL ORSS 270 APPROX RT WING. REPLACED ANGLE AND FASTENERS TRAILING EDGE AT LEVEL ORSS 270 APPROX RT WING IAW SRM 51-40-02 AND DRAWING 115A2930 SHEET 8 REV -.LENGTH OF CRACK 1.250.SDR SWAA2025071580590Plate · crackedCRACK SUPPORT CORRUGATED PLATE TRAILING EDGE BTW ORSS297 AND ORSS 290 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE BTW ORSS297 AND ORSS 290 AT RT WING IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG: 115A3700 SHEET 41 REV -.SDR IPXA2025062648679Angle · corrodedFAULT-STR-Z600-RH WING UPPER SURFACE IN THE ROOTWING NUTPLATES BRACKET THAT ATTACH ACCESS PANEL 192CR WITH CORROSION.REMOVED CORROSION ON BRACKETS PNS 149N7210-128 AND 149N7210-190 IAW B757-200 SRM 51-10-02.EMOVED 2 EA. BRACKETS IAW B757-200 SRM 51-40-02.TRESDR VNAA20250714007Canister · crackedCRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK. CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV -SDR SWAA2025070780044Support Angle · pulledFASTENER HEADS FOR I/B SUPPORT ANGLE PULLED THROUGH ON L/W PANEL 551GB. REPAIRED PER SRM 51-70-04-2R-9-A00753, REPAIR 9 - REPAIR OF DAMAGE TO A FASTENER HOLE WITH LAMINATING RESIN AND CHOPPED FIBER.SDR FDEA202506091078Support · crackedLH WING TE CAVITY LOWER FACE OF UPPER FIXED PNL FOUND SUPPORT WEB CRACK NEAR L5 SPLR INBD. TRIMMED OUT AND INSTALLED REPAIR BRACKET REPAIR AT LH WING SKIN SUPPORT ABX144.2 I.A.W FEDEX EA NO : T6-5740-T0383807 P1, SEQ NO : 1013, TITLE : WING-ATTACH FITTINGS
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