JASC 5720
Service difficulty reports · 13,633
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 SWAA2024052080338Intercostal · crackedR/H WING TRAILING EDGE INTERCOSTAL IS CRACKED I/B OF DEFLECTION RIB<[01] FAULT RESOVLED ON N/R TTG8Q00T07NU;[02] VERIFIED ITEM 1.SDR AALA202405021209Landing · brokenAIRCRAFT IN BASE MAINTENANCE: LEFT HAND WING T/E PANEL LANDING BROKEN JUST BELOW NUMBER 3 SPOILER. REMOVED AND INSTALLED NEW LOWER CHORD (AALA202405021209), AND NEW BEAM ASSEMBLY (AALA202405027816). PER B777-200 SRM 51-40-02-0G PARA 7 AND 9.SDR DALA2024042904764Strake · handler error(LOG 5797492) WHILE PULLING INTO THE GATE LEFT LOWER WINGLET STRUCK CATERING TRUCK. R/R LH WINGLET STRAKE ASSY PER B737 CMM 57-31-00 NO DAMAGE TO THE WINGLET NOTED.SDR SWAA2024052079635Support Angle · cracked(A204 DOT 4) LH WING TRAILING EDGE. JUST INBOARD OF DEFLECTION CONTROL RIB. TRAILING EDGE PANEL LATTERAL SUPPORT ANGLE IS CRACKED AT OUTBOARD FASTNER HOLE COMMON TO PANEL<[01] 01 - REMOVED AND REPLACED PER SRM 51-40-02 AND DWG # 115A2156; REV E.;[02] VERIFIED SDR SWAA2024052079633Angle · cracked(A204 DOT 7) RH WING TRAILING EDGE; JUST INBOARD OF DEFLECTION CONTROL RIB. FIXED TRAILING EDGE PANEL; LATTERAL SUPPORT ANGLE IS CRACKED AT OUTBOARD FASTNER HOLE COMMON TO PANEL.<[01] REMOVED AND REPLACED R/WING T/E; FIXED PNL LATTERAL SUPPORT ANGLE IAW 51-40-SDR JR2R20240426537Angle · crackedSTUB ANGLE OF FRAME 52 LH SIDE CRACKEDSDR UATA202406105701Fairing · looseOB FLAP, IB HINGE FWD FAIRING BECAME LOOSE AND CHAFED INTO THE BOTTOM SKIN OF THE RH WING, JUST FORWARD OF THE HINGE. THE DAMAGE SPECIFICATIONS WERE SENT TO AIRBUS ENGINEERING AND THEY PRODUCED REPAIR INSTRUCTIONS ON ENGINEERING AUTHORIZATION (EA) NUMBER 24E3SDR VNAA20240523006Canister · crackedCRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV --SDR IXXA2024042001Intercostal · crackedRW LEADING EDGE INTERCOSTAL CRACKED.SDR SWAA2024051676300Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS273 ON DEFLECTION CONTROL RIB AREA LT WING 2024-259282<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS273 ON DEFLECTION CONTROL RIB AREA LT WING TOOK MEASURE OF CRACK IS 0.835 INCH TOOL USED CALIPER P/N: 500-196-30 S/N: A22SDR SWAA2024051676302Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS217 AT LT WING 2024-259283<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS217 AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; MEASURED CRACK IS L: 0.799 INCH TOOL USED CALIPER P/N: 8647A4SDR NACA2024041600003Support Angle · crackedLH WING T/E UPPER PANEL SUPPORT ANGLE WAS CRACKED , WBL 84.24.SDR NACA2024041600002Support Angle · corrodedLH WING T/E UPPER PANEL SUPPORT ANGLE WAS CORRODED , WBL 185.SDR SWAA2024050275843Bracket · corrodedR/H WING FUELING PANEL BRACKET FOR CENTER FUEL TANK HAS CORROSION.<[01] REPLACED P15 REFUELING PANEL PLATE PER SOPM 20-50-01 AND MM 28-41-61. P15 REFUELING PANEL OPS CHECKED GOOD PER MM 28-21-00-400-801;[02] VERIFIED INSTALLATION OF P15 REFUELING PANEL PLATE PSDR SWAA2024052074713Bracket · crackedLH WING T/E DEFLEECTOR PANEL LOWER BRACKET CRACK<[01] REMOVED AND REPLACED BRACKET AT LH WING T/E DEFLEECTOR PANEL AS PER SRM 51-40-02-0G-0 & DWG 115A2511.;[02] 02 - INSPECTED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAMSDR SWAA2024052074714Bracket · crackedRH WING T/E DEFLEECTOR PANEL LOWER BRACKET CRACK<[01] REMOVED AND REPLACED BRACKET AT RH WING T/E DEFLEECTOR PANEL AS PER SRM 51-40-02-0G-0 & DWG 115A2511.;[02] VERIFIED STEP 1SDR SWAA2024051474772Web · crackedCRACK WEB LOCATED TRAILING EDGE ORSS 270 AT LT WING. REPLACED WEB;AND FASTENERS LOCATED TRAILING EDGE ORSS 270 AT LT WING IAW SRM 51-40-02; SRM 51-10-02 AND DWG 115A2512; SHEET 16; REV.-.SDR IPXA2024052567973Cap · corrodedLEFT WING XORS 345-433 LWR T.E. AREA TEE CHANNEL HAS MULTIPLE CORROSION AND SINGLE CRACKED. LOCATED, DRILLED AND INSTALLED REPAIR ANGLE AT GUSSET IAW SRM 57-50-02-2R-9. INSTALLED 1 EA TEE CHANNEL, SIX PANEL ACCESS, THREE ANGLES, THREE STIFFENERS, THREE REPAISDR SWAA2024051674036Support Bracket · crackedCRACK ON SUPPORT BRACKET ACCESS PANEL 651GB TRAILING EDGE AT RT WING 2024-253383<[01] REPLACED SUPPORT BRACKET ACCESS PANEL 651GB TRAILING EDGE AT RT WING IAW SRM B737-700 51-10-02 ITEM 9;[02] COMPLETEDSDR SWAA2024051674038Angle · crackedCRACK ON ANGLE ACCESS PANEL 551FB TRAILING EDGE AT LT WING 2024-253384<[01] REPLACED ANGLE ACCESS PANEL 551FB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 115A2710 REV -;[02] REPLACEDSDR 2024FA0000305Stiffener · crackedL/H WING I/B FWD TOP SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEWSDR SWAA2024052073060Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS265 AT RT WING 2024-253357<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS265 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A6200 REV -; MEASURE OF CRACK IS: 1.700 IN TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B233531SDR SWAA2024052073059Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS234 AT RT WING 2024-253356<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS234 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2001; SHEET 30; REV: A. MEASURE OF CRACK IS: 0.405? TSDR SWAA2024052073266Tee Angle · crackedCRACK TRAILING EDGE TEE ANGLE IRSS 212 AT LT WING 2024-253361<[01] REPLACED TRAILING EDGE TEE ANGLE IRSS 212 AT LT WING IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG 115A2001 SHEET 24 REV A. MEASURE OF CRACK IS: L: 0.815? TOOL USED DIGITAL CALIPER: P/N: 500-196-3SDR SWAA2024051673061Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS265 AT RT WING 2024-253354<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS265 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2714 REV: A MEASURE OF CRACK IS: 0.500 IN TOOL USED CALIPER P/N:500-752-20SDR SWAA2024051673058Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS255 AT RT WING 2024-253355<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS255 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2714 REV: A MEASURE OF CRACK IS: 0.300 IN TOOL USED CALIPER P/N:500-752-20SDR SWAA2024051673062Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS265 AT LT WING 2024-253360<[01] REPLACED CORRUGATED PLATE AND FASTENERS TRAILING EDGE LOCATED ORSS265 AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.<BR><BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] SDR SWAA2024042672286Counterweight · corrodedON THE RIGHT WING TIP UNDER PANEL 621AAB; ALL OF THE BALLAST WEIGHTS HAVE CORROSION NOTED.<[01] COMPLIED WITH EA M-22-157-00365. SEE BARCODE TTG8Q00SPL74 FOR WORK ACCOMPLISHED.SDR UIEA2024040500236Plate · corrodedCORROSION- PLATE, UPPER FACE OF R/H WING T/E INBD MID FLAP TOP PNL, WBL 375(<P>1. PERFORM PERMANENT REPAIR - CORROSION DAMAGES ON RH WING MID FLAP UPPER SKIN PANEL WBL 375 ~ WBL 408 AREA IAW EGAT EI T2024A57M-751 REV 1 2. CONDITION CHECK IS SATISFACTORY.</P>)SDR DALA2024040804164Support · corrodedSHIP 3139 CORROSION FOUND COMMON TO THE OUTB'D AND INB'D BORES OF PENDULUM SUPPORT ASSY AT FLAP TRACK 4 LEVEL OF OUTB'D FLAP LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 616677. (0278866)SDR IPXA2024052145527Cover Plate · crackedFAULT: MULTIPLE CRACKS FOUND ON F40 L/W LOWER RADIUS HOLE AROUND 9-11 O'CLOCK FACING FOWARD. INSTALLED REPAIR PARTS IAW DRAWING R53810798 REV C AND SRM 51-40-21 AND EO 64579-JIC003 REV 1. RE-INSTALLED RIB AND INTERCOSTAL AT FR 40 L/E IAW SRM 51-40-21 AND EO 64SDR SCNA20240429227Support Bracket · crackedLH WING REAR SPAR AT RSS 207 SUPPORT WITH RACK . REPLACED SUPPORT BRACKET CLIP ASSY P/N 115A5552-1 IAW B737-800 BCF SRM 51-10-02 PARA. 9 AND REFERENCE AIPC 57-50-00-23 SHEET 001SDR JR2R20240404831Angle · crackedLH WING STUB FAIRING ANGLE CRACKED. REPAIREDSDR UIEA2024040500261Bracket · corrodedCORROSION-BRACKET, LH WING T/E CAVITY HYD TUBE BLOCK - CLAMP WBL 178(<P>1. REMOVE DAMAGE PART IAW SRM 51-40-02-OG-0 REV 120 2. INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 120 AND DWG 65B14463 SHEET 5 REV K & SHEET 9 REV J 3. JOB COMPLETED</P>)SDR SWAA2024040470146Web · missingR/H WING UPPER FIXED PANEL WEB MISSING.<[01] 01 - REMOVED AND REPLACED PER [AMM 20-50-11-201-NG (STANDARD TORQUE VALUES - MAINTENANCE PRACTICES - PERMANENT)]SDR SWAA2024051069686Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS269 DEFLECTION CONTROL RIB AREA AT LT WING. REPLACED ANGLE TRAILING EDGE LOCATED ORSS269 DEFLECTION CONTROL RIB AREA AT LT WING IAW SRM 51-40-02 SRM 51-10-02 AND DWG 115A2930 REV ?-? SHEET 17. REPLACED ANGLE TRAILING ESDR SWAA2024051069687Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS279 DEFLECTION CONTROL RIB AREA LT WING. REPLACED ANGLE TRAILING EDGE LOCATED ORSS279 DEFLECTION CONTROL RIB AREA LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING # 115A6200 REV: A.SDR FDEA202403290442Former · mismanufacturedR/H L/E NOSE FORMER ANGLE MALFORMED AND HAS MORE THAN .037" GAP TO LEADING EDGE SKIN. ENGINEERING CONTACTED PER SEQUENCE 708 AND RECOMMENDS REPLACEMENT.SDR FDEA202403290440Former · misalignedR/H L/E NOSE FORMER ANGLE MALFORMED AND HAS MORE THAN .037" GAP TO LEADING EDGE SKIN. ENGINEERING CONTACTED PER SEQUENCE 708 AND RECOMMENDS REPLACEMENT. REF. SEQ 708 ON SAME WO FOR REPLACEMENT OF FORMER AT OSS 441 IAW FDX E.O.#:H-5720-E0368563C, WING-SECONSDR SWAA2024042668575Angle · crackedCRACK ANGLE LOCATED BS540 AND RBL 6 AT AIR CONDITIONING BAY 2024-217744<[01] REPLACED ANGLE LOCATED BS540 AND RBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9;[02] REPLACED ANGLE LOCATED BS540 AND RBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51SDR SWAA2024041168559Bracket · crackedRIGHT WING PANEL 661AB AFT I/B BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET AT RIGHT WING PANEL 661AB AFT I/B AS PER SRM 51-40-02-0G-0.SDR SWAA2024042668439Angle · crackedCRACK TRAILING EDGE ANGLE LOCATED ON ORSS 267 AT LT WING 2024-217729<[01] REPLACED ANGLE LOCATED TRAILING EDGE ON ORSS 267 AT LT WING IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED ANGLESDR SWAA2024042668441Angle · crackedCRACK TRAILING EDGE ANGLE LOCATED ON ORSS 272 AT LT WING 2024-217730<[01] REPLACED ANGLE LOCATED ON ORSS 272 AT TRAILING EDGE LT WING IAW B737-700 SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0.;[02] REPLACED ANGLE LOCATED ON ORSS 272 AT TRAILING EDGE LT WING IAWSDR SWAA2024042668442Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 290 AT LT WING 2024-217731<[01] REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE LOCATED ON ORSS 290 AT LT WING. IAW B737-700 SRM 51-40-02-0G-0;SRM 51-10-02-0G-0 ITEM 9 AND DWG 115A3700 SHEET 38 REV -. SEE INSDR SWAA2024042668443Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 212 AT LT WING 2024-217732<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 212 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02. SEE INDIVIDUAL SINGOFF BELOW;[02] CORRECTED STEP 1<BR>RESDR SWAA2024042568397Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS214 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS214 AT RT WING I.A.W B737-700 SRM 51-40-02-0G-0 ; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 115A2001 SHEET: 30 REV A. EVALUATED CRACK OF CORRUGASDR SWAA2024042568396Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS242 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS242 AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 TOOK MEASURE OF CRACK IS: L= 0.351.SDR SWAA2024042568395Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING IAW SRM 51-40-02-0G-0 AND DWG 115A2001 SHEET: 32 REV -, & SRM 51-10-02-0G-0 PARAGRAPH 9, TOOK MEASURE OF CRACK IS: L= 0.750.SDR SWAA2024042568398Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS273 RT WING 2024-211791<[01] FAULT RESOLVED ON OTHER FAULT. SEE TTG8Q00SB7UQ;[02] FAULT RESOLVED ON OTHER FAULT. SEE TTG8Q00SB7UQSDR SWAA2024042667915Bracket · crackedCRACK REAR SPAR BRACKET LOCATED BTW RIB 2 AND RIB 3 ON MLG AREA AT LT WING 2024-217712<[01] REPLACED BRACKET LOCATED BTW RIB 2 AND RIB 3 ON MLG AREA AT LT WING IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMED
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