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 2026FA0000103Stiffener · crackedFOUND RIGHT WING LOWER, INBOARD, FORWARD SKIN, FORWARD STIFFENER CRACKED. REPLACED STIFFENERSDR 2026FA0000102Stiffener · crackedFOUND RIGHT WING LOWER, INBOARD, FORWARD SKIN, FORWARD STIFFENER CRACKED. REPLACED STIFFENERSDR SWAA2025092907114Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED TRAILING EDGE INTERNAL CAVITY UPPER POSITION ORSS 472, RT WING. REPLACED RAIL NUT-PLATE IAW SRM 51-40-02.SDR SWAA2025092907115Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE, TRAILING EDGE INTERNAL CAVITY UPPER POSITION ORSS 438, RT WING. REPLACED RAIL NUT-PLATE AND FASTENERS IAW SRM 51-40-02, AND DWG 115A3500, SHEET 31, REV A.SDR SWAA2025092907117Support Angle · corrodedCORROSION SUPPORT ANGLE LOCATED TRAILING EDGE INTERNAL CAVITY ORSS 404 AT RT WING. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED TRAILING EDGE INTERNAL CAVITY BTW ORSS 326.00 TO ORSS 432.50 AT RT WING IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A3700; SHSDR SWAA2025092906899Support Angle · corrodedCORROSION ON SUPPORT ANGLE LOCATED TRAILING EDGE INTERNAL CAVITY ORSS 472 AT LT WING. REPLACED SUPPORT ANGLE LOCATED ON TRAILING EDGE INTERNAL CAVITY ORSS 472 AT LT WING. IAW B737-800 SRM 51-40-02 AND DWG# 115A3710; SHEET 5 AND REV -.SDR SWAA2025092906888Support Angle · corrodedCORROSION SUPPORT ANGLE LOCATED TRAILING EDGE INTERNAL CAVITY ORSS 415 AT LT WING. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED TRAILING EDGE INTERNAL CAVITY ORSS 415AT LT WING IAW BOEING 737-800 SRM 51-40-02 AND DWG 115A3700 SHEET 75 REV A.SDR SWAA2025092906889Support Angle · corrodedCORROSION SUPPORT ANGLE LOCATED TRAILING EDGE INTERNAL CAVITY ORSS 454 AT RT WING. REPLACED SUPPORT ANGLE LOCATED TRAILING EDGE INTERNAL CAVITY ORSS 454 AT RT WING IAW B737-800 SRM 51-40-02-0G; SRM-51-10-02-0G-0 ITEM 9 AND DWG:115A3758 SHEET:8 REV:-.SDR SWAA2025092907111Support Angle · corrodedCORROSION SUPPORT ANGLE LOCATED TRAILING EDGE INTERNAL CAVITY ORSS 297 AT RT WING 2025-506944<[01] REPLACED SUPPORT ANGLE LOCATED TRAILING EDGE INTERNAL CAVITY ORSS 297 AT RT WING IAW B737-800 SRM 51-10-02 ITEM 9 AND DWG 115A3712 SHEET 7 REV: A..<BR>SEE INDIVISDR SWAA2025092606897Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE INTERNAL CAVITY IRSS 216 AT LT WING 2025-506927<[01] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED TRAILING EDGE INTERNAL CAVITY IRSS 216 AT LT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9<BR>LENSDR JR2R20250820029Bracket · corrodedIDG GROUND BRACKET IN LH WING IS CORRODED. REPAIRED.SDR JR2R20250820030Bracket · corrodedIDG GROUND BRACKET IN RH WING IS CORRODED. REPAIRED.SDR SWAA2025091506237Plate · crackedLEFT WING TRAILING EDGE WAFFLE PLATE JUST OTBD OF PANEL 551DB FOUND CRACKED. REMOVED AND REPLACED THE LT WING TRAILING EDGE WAFFLE PLATE JUST OTBD OF PANEL 551DB IAW SRM 51-40-02-0G-0, AND DWG 115A2713.SDR SCNA20251001391Angle · crackedCRACKED ANGLE ON INTERNAL FIXED LEADING EDGE WS 228 AT RT WING. ANGLE AT INTERNAL FIXED LEADING EDGE WS 228 AT RT WING WAS REPLACED IAW SRM 51-40-02-0G-0.SDR REXA2025091500858Fitting · wornWEAR ON FLAP FITTING OF FLAP STUB FAIRING 171DL AT LH WING TRAILING EDGE (ROOT WING). FLAP FITTING OF FLAP STUB FAIRING 171DL AT LH WING TRAILING EDGE (ROOT WING). WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42-21-001-001-A01SDR REXA2025091500857Support · wornWEAR ON PLATE SUPPORT OF FLAP STUB FAIRING 171DL AT LH WING TRAILING EDGE (ROOT WING). PLATE SUPPORT OF FLAP STUB FAIRING 171DL AT LH WING TRAILING EDGE (ROOT WING). WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42-21-001-001-A01SDR SWAA2025090804964Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 276 AT RT WING. REPLACED ANGLE AND FASTENERS LOCATED TRAILING EDGE ORSS 276 AT RT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 115A6200 SHEET: 11 REV: B; MEASURES OF CRACK IS: L= 0.464.SDR SWAA2025090804963Support Bracket · crackedCRACKED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING 2025-505207<[01] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9. AND DRAWING #115A2930 SHEET 6 REV -.SDR JJBA20250902001Web · crackedRH AFT MLG WEB CRACKED. RH AFT MLG WEB REPLACED.SDR SWAA2025092303058Web · corrodedCORROSION WEB INDICATORS FUEL LOCATED INTERNAL CAVITY LEADING EDGE AT RT WING. PERFORMED PERMANENT REPAIR ON WEB INDICATION OF FUEL SYSTEM PANEL IAW EA 25-157-02404.SDR SWAA2025091603353Bracket · crackedRIGHT WING T/E PANEL 651FB HAS CRACKED L ANGLE AT FWD EDGE 27' FROM O/B END. REMOVED AND REPLACED RIGHT WING T/E PANEL 651FB BRACKET AT FWD EDGE 27' FROM O/B END IAW SRM 51-10-02-0G-0 PAR. 9; C. AND AIPC 57-50-00-38.SDR SWAA2025091600180Support Angle · crackedLEFT WING T/E PANEL 561AB AFT PANEL SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED LEFT-HAND WING T/E PANEL 561AB BEAM ASSY IAW SRM 51-40-02 AND DWG# 115A3712 ID: 0005 REV: -.SDR SWAA2025091699867Web · crackedLEFT WING T/E ORSS 261 UPPER SURFACE PANEL JUST I/B OF #5 SPOILER TRANSVERSE WEB CRACKED AT O/B FASTENER. REMOVED AND REPLACED WEB; IAW SRM 51-40-02 & DWG 115A2512.SDR SCNA20250808306Nonskid · degradedDEGRADED NON-SKID COATING FOR THE EMERGENCY ESCAPE PATH ON RT & LT OVERWING WALKWAY. PAINT WAS RESTORED ON THE EMERGENCY ESCAPE PATH ON RH/LH OVERWING WALKWAY PER B737-800 AMM 51-21-97-370-802 AND AMM 51-21-99-300-801.SDR UIEA2025080701095Web · crackedCRACK- WEB OUTBD FACE OF L/H WING T/E INBD AILERON INBD WEB WBL 445(<P>1. ACCOMPLISHED IAW EI #T2025A57M-1399 REV 1. 2. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR SWAA2025082298619Angle · crackedLH WING ANGLE CRACKED INBOARD OF MIDSPAN DEFLECTION CONTROL RIB<[01] REMOVED L/H WING ANGLE INBOARD OF MID SPAN DEFLECTION CONTROL RIB FOR REPLACEMENT.;[02] LOCATED AND DRILLED FASTENER HOLES IN NEW ANGLE PER SRM 51-40-05.;[03] INSPECTED WORK PERFORMED IN CORRSDR 2026FA0000101Stiffener · crackedFOUND RIGHT WING LOWER, INBOARD, FORWARD SKIN, FORWARD STIFFENER CRACKED. REPLACED STIFFENER.SDR 2026FA0000100Stiffener · crackedFOUND RIGHT WING LOWER, INBOARD, FORWARD SKIN, FORWARD STIFFENER CRACKED. REPLACED STIFFENERSDR 2026FA0000099Stiffener · crackedFOUND RIGHT WING LOWER, INBOARD, FORWARD SKIN, FORWARD STIFFENER CRACKED. REPLACED STIFFENERSDR SWAA2025091098557Angle · crackedCRACKED ANGLE TRAILING EDGE, IRSS 199 PLUS 12 INCHES, RT WING. REPLACED ANGLE TRAILING EDGE, IRSS 199, PLUS 12 INCHES, RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2001, SHEET 50, REV -.SDR CALA2025080807491Support · corrodedRH WING NR 6 TRANSMISSION SUPPORT CORRODED. REPAIRED IAW ECRA 5753-02342, AND EA 757-5753-13-A4035 REV-.SDR JR2R20250803053Sill Drain · corrodedRH MOP SILL, FROM FR88-FR90 IS CORRODED OUT OF LIMITS. REPLACEDSDR IXXA20250803003Web · corrodedCORROSION IN RWW UPPER WEB STA 1108, RBL10SDR VNAA20251015012Channel · corrodedCORROSION ON GANG CHANNEL AT LH/RH WINGS. CORROSION ON GANG CHANNEL AT LH/RH WINGS WAS EVALUATED DUE TO EXCESIVE DAMAGE PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ900 SRM 51-41-02-001-001-A01SDR SWAA2025090397479Angle · crackedCRACK ANGLE TRAILING EDGE SUPPORT BEAM LOCATED IRSS 186 LT WING . REPLACED ANGLE TRAILING EDGE SUPPORT BEAM LOCATED IRSS 186 LT WING IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 115A2510 SHEET 12 REV -.SDR SWAA2025090397478Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED IRSS 140 LT WING, REPLACED ANGLE TRAILING EDGE LOCATED IRSS 140 LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DWG 115A2000 SHEET 21 REV -.SDR SWAA2025090397243Plate · crackedCRACK INBOARD TRAILING EDGE CORRUGATED PLATE IRSS 216 AT RT WING. REPLACED CORRUGATED PLATE LOCATED INBOARD TRAILING EDGE IRSS 216 AT RT WING IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND AND DWG: 115A2713 SHEET: 4 REV -.SDR SWAA2025090397099Nut Plate · crackedCRACK RAIL NUT PLATE O/B FRONT SPAR OFSS 491 AT RT WING. REPLACED RAIL NUT PLATE O/B FRONT SPAR OFSS 491 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 112A4402 SHEET: 14 REV:- MEASURE CRACK IS L:0.200 INCHES.SDR IXXA20250731001Skin · corrodedCORROSION ON LEFT WING SURFACE LEADING EDGE UPPER SKIN.SDR SWAA2025082796671Support Angle · crackedCRACK SUPPORT ANGLE TRAILING EDGE LOCATED BTW ORSS281 TO ORSS327 AT LT WING. REPLACED SUPPORT ANGLE TRAILING EDGE LOCATED BTW ORSS281 TO ORSS327 AT LT WING IAW B737-800 SRM 51-40-02 AND DWG115A3758 SHEET 4 REV-.SDR SWAA2025082796127Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED IRSS 140 LT WING. REPLACED ANGLE TRAILING EDGE LOCATED IRSS 140 LT WING IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG: 115A2000; SHEET: 21; REV- . MEASURE OF CRACK IS L: 0.534.SDR SWAA2025082795599Strap · corrodedCORROSION ON O/B FRONT SPAR LOWER STRAP OFSS 294 AT RT WING. REPAIRED STRAP LOCATED FROM OSS 26.94 TO OSS 109.69 AT RT WING IAW B737-800 SRM 51-40-02 AND B737-800 SRM 57-20-01-2R-3 REPAIR 3 AND EA 25-157-02082-WIP1; EA 25-157-02082-WIP2; EA 25-157-02082-WIP3SDR SWIA2025072575183Helicoil · damagedLEFT WING JACKING POINT HELI-COIL IS DAMAGED. INSTALLED NEW LEFT WING JACK FITTING IAW SRM 51-42-21-001-001-A01, DWG CC670-10126, REV NC, AND DWG CC670-10038, REV NC. .COMPLIED WITH 51-900-1002-SKY.SDR 9WGA2025082354641Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT L/H APPROX STA 1196, XCW 5.0 AT S-19. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT L/H CENTER WING USDR SWAA2025082693633Plate · crackedLEFT WING REAR SPAR, WAFFLE PLATE INBD OF NR 3 FLAP TRACK WAS CRACKED AT FASTNERS. REMOVED AND REPLACED LT WING REAR SPAR WAFFLE PLATE IAW SRM 51-40-02.SDR FDEA202507221290Channel · crackedRIGHT WING FIXED UPPER TRAILING EDGE PANEL, UNDER SIDE "U" CHANNEL STIFFENER ALONG THE TRAILING EDGE OF THE PANEL, AROUND WING STATION 1034, IS CRACKED REMOVED AND REPLACED DAMAGED BEAM REF BOEING DWR: 113T1913 AND B767 SRM 51-40-02SDR SWAA2025081493373Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED IRSS 141 AT RT WING. REPLACED ANGLE TRAILING EDGE LOCATED IRSS 141 AT RT WING IAW SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9. MEASURED OF CRACK IS L: 1.631.SDR SWAA2025082793173Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 279 AT RT WING. REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 279 AT RT WING IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG: 115A6200; SHEET: 9; REV: A. MEASURE OF CRACK IS L: 1.631.SDR SWAA2025081493143Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED IRSS 141 AT LT WING. REPLACED ANGLE TRAILING EDGE LOCATED IRSS 141 AT LT WING IAW SRM 51-40-02, AND SRM 51-10-02, PARAGRAPH 9, AND DWG 115A2000, SHEET 21, REV -. LENGTH OF CRACK IS L: 0.841 INCHES.SDR SWAA2025081493140Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT LT WING IAW SRM 51-40-02; SRM 51-10-02 AND DWG 115A2001, SHEET 30, REV A.
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