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 SWAA2024100930268Angle · crackedCRACK ANGLE LOCATED TRAILING EDGE ORSS269 APPROX. DEFLECTION CONTROL RIB AREA AT LT WING 2024-528458<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 269 APPROX DEFLECTION CONTROL RIB AREA AT LT WING. IAW B737-700 SRM 51-40-02 AND DWG # 115A2930 SHEET 7 AND RSDR SWAA2024092330257Angle · crackedCRACK ON ANGLE LOCATED ORSS278 TRAILING EDGE AT RT WING 2024-525810<[01] REPLACED ANGLE LOCATED ON ORSS278 TRAILING EDGE AT RT WING IAW B737 800 SRM 51-40-02-0G AND DWG 115A6200 SHEET 24 REV A.;[02] REPLACED ANGLE LOCATED ON ORSS278 TRAILING EDGE AT RT WING IASDR SWAA2024092330258Web · crackedCRACK ON WEB LOCATED BTW ORSS261 TO ORSS277 TRAILING EDGE AT RT WING 2024-525811<[01] REPLACED WEB LOCATED ON BTW ORSS261 TO ORSS277 TRAILING EDGE AT RT WING IAW B737 800 SRM 51-40-02-0G AND DWG 115A2512 SHEET 16 REV -.;[02] REPLACED WEB LOCATED ON BTW ORSS261SDR SWAA2024092030413Plate · elongatedCHECK R/W DEFLECTOR RIB TO DEFLECTOR PANEL ATTACH SERRATED PLATES FOR CONDITION AND ELONGATED HOLES<[01] FOUND NO DAMAGE TO SERRATED PLATES I/B AND O/B SIDE PER SRM 51-10-02 INSPECTION FOR DAMAGE.;[02] STEP 1 ENTERED IN ERROR.;[03] REMOVED AND REPLACED SERRATESDR SWAA2024092029635Angle · corrodedCORROSION INBOARD TRAILING EDGE BONDING JUMPER SUPPORT ANGLE OF AFT BOOST PUMP TANK 2 AT RT WING (2 EA) 2024-512553<[01] REPLACED INBOARD TRAILING EDGE BONDING JUMPER SUPPORT ANGLE OF AFT BOOST PUMP TANK 2 AT RT WING (2 EA) IAW B737-800 AMM 28-22-41-400-801. SSDR SWAA2024091129619Angle · crackedLT WING UPPER T/E FIX PANEL BETWEEN #5 AND #6 SPOILERS; SUPPORT BEAM ATTACHMENT ANGLE TO DEFLECTION CONTROL RIB CRACK.<[01] REMOVED; REPLACED; AND INSTALLED A NEW SUPPORT BEAM ATTACHMENT ANGLE TO DEFECTION CONTROL RIB AT LT WING UPPER T/E PANEL BETWEEN #5 AND SDR SWAA2024082729589Angle · crackedSIGNIFICANT DAMAGE TO PRIMARY STRUCTURE KRAS 150 (PN 116A4005) AND KRAS 166 (PN 116A4004). CRACK FOUND IN BULB SEAL Z ANGLE (NOSE BEAM PN 116A4610) AT THE BOTTOM OF THE LEADING EDGE. SEE ATTACHED PHOTOS OF DAMAGE<[01] ACCOMPLISHED EA 24-157-02319.SDR SWAA2024092429452Support Angle · crackedCRACK SUPPORT ANGLE FIXED TRAILING EDGE ORSS 297 LT WING 2024-512538<[01] REPLACED SUPPORT ANGLE LOCATED FIXED TRAILING EDGE ORSS 297 LT WING IAW B737-800 SRM 51-40-02 AND DWG 115A3700 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ANGLE LOCATED FSDR SWAA2024092428584Nut Plate · corrodedCORROSION O/B FIXED LEADING EDGE RAIL NUTPLATE OFSS 449 AT LT WING 2024-512523<[01] REPLACED O/B FIXED LEADING EDGE RAIL NUTPLATE OFSS 449 AT LT WING IAW B737-800 SRM 51-40-02 AND DWG: 112A4402; SHEET: 40; REV: A.;[02] REPLACED O/B FIXED LEADING EDGE RAIL NUTPSDR DALA2025070204956Tape · peelingLH WINGLET TIP LEADING EDGE EROSION TAPE FOUND PEELED UP. REQUIRES REPAIR. INSPECTED LH WINGLET TIP L E WHERE EROSION TAPE WAS DAMAGED & FOUND NO UNDERLYING DAMAGE. TRIMMED OFF EXCESS EROSION BOOT MATERIAL TO MEET AERODYNAMIC SMOOTHNESS IAW ASRP 55-32-01-01AAASDR SWAA2024092427971Web · crackedCRACK WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING 2024-512484<[01] REPLACED WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2512 SHEET 16 REV-. <BR><BR>MEASURE OF CRACSDR SWAA2024092427972Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 277 DEFLECTION CONTROL RIB AREA LT WING 2024-512485<[01] REPLACED ANGLE TRAILING EDGE ORSS 277 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A2512 SHEET 16 REV-.<BR><BR>MEASURE CSDR IXXA2024092002Support Bracket · crackedNUMBER 6 SLAT LOWER LEADING EDGE SUPPORT BRACKET, LOCATED AT THE CENTER AUX TRACK, IS CRACKEDSDR IXXA2024092001Support Bracket · crackedNO. 6 SLAT LOWER LEADING EDGE SUPPORT BRACKET, LOCATED AT THE BASE OF THE OUTBOARD AUX TRACK, IS CRACKEDSDR DALA2024081508189Intercostal · crackedAIRCRAFT 3732, INITIAL INSPECTION: CRACKED INTERCOSTAL ON FIXED L/E FRONT SPAR AREA WS 326.00 APPROX AT LH WING. CORRECTIVE ACTION: INTERCOSTAL AND BRACKET ON FIXED L/E FRONT SPAR AREA WS 326.00 APPROX AT LH WING WERE REPLACED PER B737-800 SRM 51-40-02-0G PAR.SDR 2024FA0000610Stiffener · crackedR/H WING FWD WING WALK SKIN CRACKED AROUND CORRUGATED SKIN. REPLACED WITH NEWSDR 2024FA0000609Stiffener · crackedR/H WING FWD WING WALK SKIN CRACKED AROUND CORRUGATED SKIN. REPLACED WITH NEWSDR 2024FA0000608Stiffener · crackedR/H WING FWD WING WALK SKIN CRACKED AROUND CORRUGATED SKIN. REPLACED WITH NEWSDR 2024FA0000607Stiffener · crackedL/H WING I/B FWD BTM SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR 2024FA0000606Stiffener · crackedL/H WING I/B FWD TOP SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR 2024FA0000605Stiffener · crackedR/H WING I/B FWD TOP SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR 2024FA0000604Stiffener · crackedR/H WING I/B FWD TOP SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR 2024FA0000603Stiffener · crackedR/H WING I/B FWD TOP SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEWSDR HNAA2024091200800Profile · cracked57-2177 LH WING STUB AREA, UPPER PROFILE CRACKED AT BTW STA 16000 AND 16783.5. RAR PROFILE IAW SRM 51-40-02SDR SWAA2024091923855Support · crackedUPPER BULB SEAL RETAINER SUPPORT IS CRACKED AT LOWER FASTENER HOLE AT RIGHT WING FIXED TE PANEL JUST AFT OF THE PYLON. MARKED<[01] REMOVED AND REPLACED UPPER BULB SEAL RETAINER SUPPORT AT RIGHT WING FIXED TE PANEL JUST AFT OF THE PYLON<BR>I.A.W SRM 51-40-02.<BSDR SWAA2024082826890Panel · looseL/H SHELF PANEL LOOSE AT L/H DEFLECTION RIB<[01] REMOVED HARDWARE AND FASTENERS PER SRM 57-51-02-2R-4.;[02] REMOVED DAMAGE FROM UPPER CONTROL RIB TAB PER SRM 57-51-02-2R-4 AND DAMAGE FROM TRAILING EDGE SUPPORT BEAM PER SRM 57-51-02-2R-1.;[03] C/W DAMAGE REMOVASDR SWAA2024092322986Bracket · crackedRH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT O/B BRACKET FWD FACE HAS CRACK.<[01] REMOVED AND REPLACED RH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT O/B BRACKET IAW SRM 51-40-02 AND AIPC 57-42-51-03.;[02] SDR DALA2024120211380Winglet · abnormalLH WINGLET LEADING EDGE EROSION TAPE FOUND PARTIALLY PEELED UP. REQUIRES REPAIR. REPAIRED EROSION TAPE DAMAGE IAW A220 ASRP 57-32-00-00AAA-662A-A. C/W TERMINATING ACTION. OK TO CLOSE LOG. (LP# 6017585)SDR SWAA2024090321312Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 215 AT RT WING 2024-458885<[01] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ON TRAILING EDGE IRSS 215 AT RT WING I.A.W. B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 ;SRM 51-40-02-0G-0 DWG 115A2713 SHEET 4 REV -;[SDR SWAA2024090319959Support Bracket · crackedCRACK TRAILING EDGE SUPPORT BRACKET ORSS 270 AT LT WING 2024-458832<[01] REPLACED SUPPORT BRACKET LOC TRAILING EDGE ORSS 270 AT LT WING IAW B737-700 SRM 51-40-02 AND DRAWING 115A2930 SHEET 6 REV -:;[02] TASK COMPLETEDSDR SWAA2024082020387Angle · crackedCRACK ANGLE LOCATED DEFLECTION CONTROL RIB AREA ORSS279 AT LT WING 2024-453449<[01] REPLACED ANGLE LOCATED DEFLECTION CONTROL RIB AREA ORSS279 AT LT WING IAW B737-800 SRM 51-40-02-0G-0 AND DWG 115A6200; SHEET 29; REV. -. SEE INDIVIDUAL SIGN-OFFS BELLOW.;[02] JSDR SWAA2024082020388Angle · crackedCRACK ANGLE LOCATED DEFLECTION CONTROL RIB AREA ORSS279 AT RT WING 2024-453450<[01] REPLACED ANGLE LOCATED DEFLECTION CONTROL RIB AREA ORSS279 AT RT WING IAW B737-800 SRM 51-40-02-0G-0 AND DWG 115A6200; SHEET 29; REV. -. SEE INDIVIDUAL SIGN-OFFS BELLOW.;[02] RSDR UIEA2024072500745Support Bracket · damagedRH WING LDG BEAM MID AREA T/E UPPER SURFACE SUPPORT ROD BRACKET FOUND ELONGATED(<P>RH WING LDG BEAM MID AREA T/E UPPER SURFACE SUPPORT ROD BRACKET REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 AND 69B11994U2 FITTING ASSY FABRICATED AS PER DWG AND PLSDR CALA2024073002139Plate · crackedREF AMES NR 173733-0500-0036 GEN ITEM 53-5700-1-2107 L/W TE WIGGLE PLAT AT WS330.50 CRACKED/BROKEN REMOVED AND REPLACED 2 EA L/W T/E WIGGLE PLATES AT WS330.5 IAW B 757 SRM 51-40-02 PAR 9 AND B757 AMM 20-11-00-912-001.SDR IPXA2024072468148Angle · crackedFAULT: LH WING, I/B SHROUD BOX LWR T/E, I/B SUPPORT BRACKET IS CRACKED. INSTALLED ANGLE AT LH WING T/E LOWER SKIN WITH MATERIAL P/N: MS20470AD5-11. BTCH: 4222164. IAW A300-600 SRM 51-40-21. AUDIT COMPLETE.SDR SWAA2024082315300Bracket · crackedCRACK ON SUPPORT BRACKET ACCESS PANEL 651FB TRAILING EDGE AT RT WING 2024-443808<[01] REPLACED SUPPORT BRACKET AND FASTENERS ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; 51-40-02 AND DWG 115A2710 REV: - .<BR>MESSURE OF CRASDR SWAA2024090314926Angle · crackedR/H REAR SPAR T/E DEFLECTION CONTROL RIB FIXED PANEL LOWER T/E BULB SEAL RETAINER CRACKED AT FASTENER HEAD MKD DOT<[01] REMOVED AND REPLACED LOWER SEAL RETAINER ANGLE AT RIGHT WING REAR SPAR T/E DEFLECTION CONTROL RIB FIXED PANEL PER B737-700 SRM 51-40-02-0G-0SDR IPXA2024081364749Support Fitting · corroded**SDR FILED OPEN**FAULT - R/H WING STA OLES 1525.45 FRONT SPAR FIXED PNL SUPPORT FITTING ROD CORROSION (AGING A/C INSPECTION). (REPLACE) 1. I.A.W AMM 20-51-01-912-008 REV.111 REPLACED THE ROD.<BR>2. COND CHECK NORMAL.<BR><BR>IPC VERIFIED AND SERVICEABLE TAG NOSDR IPXA2024081364774Link · corroded**SDR FILED OPEN**FAULT - R/H WING STA OLES 1483.95 , 1493.45 FRONT SPAR FIXED PNL 2EA SUPPORT FITTING ROD CORROSION (AGING A/C INSPECTION). (REPLACE) 1. I.A.W AMM 20-51-01-912-008 REV.111 REPLACED THE ROD.<BR>2. COND CHECK NORMAL.<BR><BR>IPC VERIFIED AND SERVSDR IPXA2024081259225Stiffener · corrodedFAULT: STR Z600, RH WING - T/E STIFFENER PN: 113N1184-4 EXFOLIATED.REMOVED STIFFENER EXFOLIATED P/N 113N1184-4 FROM RH WING TRAILING EDGE IAW SRM 51-40-02-0G-0.INSTALLED NEW STIFFENER AND ATTACHING PARTS WITH FASTENERS PN: BACB30NY6K11, BT: 0004279074; BACB30NSDR SWAA2024072613314Web · crackedLH WING MIDFLAP DEFLECTION RIB TO WEB CLIP (MPN 115A6260-1) IS CRACKED<[01] LOCATED AND DRILLED FASTENER HOLES IN NEW CLIP PER ARM 51-40-05.;[02] VERIFIED WORK IN CA# 1.........LOCATED AND DRILLED FASTENER HOLES IN NEW CLIP PER ARM 51-40-05;[03] INSTALLED NEW SDR IPXA2024072259225Stiffener · corrodedRH WING - T/E STIFFENER PN: 113N1184-4 EXFOLIATED REF STEP 2. INSPECTED AND VERIFIED REMOVED STIFFENER EXFOLIATED P/N 113N1184-4 FROM RH WING TRAILING EDGE IAW SRM 51-40-02-0G-0.SDR DALA2024071807241Fuel Tank · elongatedSHIP 3138 ELONGATED HOLE CUT OUT FUEL TANK LOWER SURFACE LOC. BTW RIB14/15 (3E/A) ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON HOLES (3 E/A) LOC.ON CUT OUT OF FUEL TANK LOWER SURFACE BTW RIB14/15 ON LH WING AS PER A319 SRM 57-21-11-300-002. SDR DALA2024071807240Fuel Tank · elongatedSHIP 3138 ELONGATED HOLE CUT OUT FUEL TANK LOWER SURFACE LOC. BTW RIB16/17 (1E/A) ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON HOLE (1 E/A) LOC. ON CUT OUT FUEL TANK LOWER SURFACE LOC. BTW RIB16/17 ON LH WING AS PER A319 57-21-11-300-002. (0SDR UIEA2024071400673Support · crackedLHW LWR SURFACE REFUELING ACCESS DOORS FWD FIXED PNL FWD PNL SUPPORT FOUND CRACK. SUPPORT REPAIRED AS PER SRM 57-41-13-2R-3 REPAIR 13 FIG 201 (CATEGORY A). NO FURTHER DEFECTS NOTED.SDR IXXA2024071701Support · crackedRT WING FIXED L/E LOWER SUPPORT CRACKED LES 684SDR FDEA202407161016Angle · corrodedRIGHT WING - TRAILING EDGE OUTBOARD ISLAND INBOARD EDGE LOWER AFT ANGLE FOUND CORROSION AT STATION XORS 855. RIGHT WING TRAILING EDGE OUTBOARD ISLAND INBOARD EDGE LOWER AFT CORRODED ANGLE REMOVED AS PER SRM 51-31-01-0G. FABRICATED ANGLE PER DOUGLAS DRAWINGSDR 2024FA0000497Shim · migrated9V-SWW STARTED “A” CHECK IN HANGAR ON 11/07/2024 AND RETURNING TO SERVICE ON 15/07/2024. DURING THE ACCOMPLISHMENT OF THE ADSI IB777570078, #7 FLAP SUPPORT FITTING SHIMS WERE FOUND MIGRATED.SDR SWAA2024082312186Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 214 AT RT WING 2024-443662<[01] EVALUATED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 214 AT RT WING AND NOT FOUND ALLOWABLE DAMAGE FOR CORRUGATED PLATE. MEASURE CRACK IS: L=0.813? TOOL USED CSDR SWAA2024090312245Support · crackedLH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT O/B RIVET HAS CRACK.<[01] REMOVED AND REPLACED LH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT AND O/B RIVET PER SRM 51-40-02-0G-0 STEP 4
Back to JASC 5720