JASC 5720
Service difficulty reports · 13,637
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 SWAA2023071863428Angle · corrodedL/W #1 TANK FWD BOOST PUMP UPPER BONDING JUMPER ATTACH POINT IS CORRODED ON FRONT SPAR<[01] SRM 57-20-10-1A-3 IS APPLICABLE TO THIS REPAIR.[08] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>CORROSION NOTED WITHIN BLENDED AREA. MARKED AREAS. <BR>EQUIP USED: <BR>-RADSDR SWAA2023061246343Panel · crackedCRACK ACCESS PANEL 661BB AROUND HOLE AT RT WING 2023-311085<[01] TOOL USED: CALIPER: P/N:500-193-30 S/N:0000288 DUE DATE:27-DEC-23;[02] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 18196126 DUE DATE: 26-MAR-24.;[03] TOOL USED: SCALE P/N: CR5200 S/N: 8343110855 DUSDR SWAA2023061246344Panel · crackedCRACK ACCESS PANEL 561BB AROUND HOLE AT LT WING 2023-311087<[01] TOOL USED: CALIPER: P/N:500-193-30 S/N:0000288 DUE DATE:27-DEC-23;[02] TOOL USED HOTBONDER P/N: HCS9000B-AV S/N: 18185761 DUE DATE: 24-SEP-23;[03] TOOL USED: SCALE P/N: CR5200 S/N: 8343110855 DUESDR ABXA20230515100Web · crackedDURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED LH WING L/E BULLNOSE WEB (BEAM) AT APPROX. OSS 679.82 (AT FUEL PANEL) IS CRACKED. THE B767-300 SRM 57-41-13 FIG. 201 REPAIR 3 IS FOR THIS SPECIFIC AREA. THE REFERENCED SRM REPAIR IS FOR THE CSDR SWAA2023061343530Bracket · crackedR/H WING T/E DEFLECTION RIB @ WS 278.50 I/B SIDE ATTACHMENT BRACKET CRACKED. (18-017)<[01] RECEIVED NEW PART PN:115A6260-2}REMOVED AND REPLACED NEW BRACKET [CLIP] AT RH WING TE DEFLECTION RIB @WS 278.50 IB SIDE SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2023052242949Support · crackedLH FWD OVERWING ACCESS PANEL 195AL SUPPORT STRUCTURE CRACK.<[01] REMOVED LH FWD OVERWING ACCESS PANEL 195AL SUPPORT STRUCTURE; LOCATED AND DRILLED NEW FRAME SUPPORT TREATED AND PRIMED HOLES; INSTALLED NEW FRAME SUPPORT. REF B737 SRM 51-40-02-0G-0; SRM 51-40-05SDR SWAA2023050343233Attach Bracket · crackedLEFT WING UPPER ACCESS PANEL INBD FWD SUPPORT ATTACH BRACKET (Z BRACKET) CRACKED.<[01] R&R LEFT WING UPPER ACCESS PANEL INBD FWD SUPPORT ATTACH BRACKET (Z BRACKET) IN REF TO SOPM 20-50-18.SDR SWAA2023052541416Bracket · crackedCRACKED DUCT SUPPORT BRACKET AT STA 546; WL 168.75; RBL 9.5<[01] REMOVED CRACKED DUCT SUPPORT BRACKET AT STA 546; WL 168.75; RBL 9.5 IAW SRM 51-40-02;[02] INSTALLED NEW DUCT SUPPORT BRACKET AT STA 546; WL 168.75; RBL 9.5 P/N 212A1116-1 LOT # 1521877-1 PO# 9111SDR SWAA2023051641882Web · crackedTHE LH UPPER FIXED TE PANEL TRANSVERSE WEB IS CRACKED AT APPROX ORSS 280.<[01] UPDATED MEASUREMENT SECTION; REMOVED CRACKED TRANSVERSE WEB LEFT HAND WING UPPER FIXED TRAILING EDGE PANEL AND INSTALLED NEW TRANSVERSE WEB PART NUMBER 115A2156-7 SAME LOCATION ABOVSDR IXXA2023042601Panel · crackedPANEL 521BB CRACKED.SDR SWAA2023053041356Bracket · crackedCRACK REAR SPAR BRACKET LOC ORSS 273 AFT POSITION AT RT WING 2023-282640<[01] REPLACED BRACKET LOC ORSS 273 AFT POSITION AT RT WING.IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. MEASURES OF CRACK IS: L=0.793? TOOL USED DIGITAL CALIPER P/N :8647A42 S/N B22SDR SWAA2023053041358Bracket · crackedCRACK REAR SPAR BRACKET LOC ORSS 273 FWD POSITION AT RT WING 2023-282643<[01] REPLACED REAR SPAR BRACKET AND FASTENER LOC ORSS 273 FWD POSITION AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A293 REV:- SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] COMPLETEDSDR EBVR202304250001Winglet · corrodedCORROSION UNDER STATIC WICK BASE ON RH WINGLET TRAILING EDGE CAUSED STATIC WICK BASE TO FALL OFF. CORROSION REMOVAL WAS OUTSIDE OF SRM LIMITS. PERFORMED AN EXTERNAL DOUBLER PATCH AROUND THE TRAILING EDGE (TACO PATCH).SDR SWAA2023050830383Angle · crackedDOT A24-6 LH WING I/B L/E / WTB FAIRING SUPPORT ANGLE FOR PANEL 195AL CRACKED. MARKED<[01] REMOVED L/H WING I/B L/E WTB FAIRING SUPPORT ANGLE FOR PANEL 195AL I/A/W SRM 51-40-02-0G-0;[02] DRILLED UP NEW SUPPORT ANGLE FOR PNL 195AL I/A/W SRM 51-40-02-0G-0 AND BOSDR 2026FA0000388Stiffener · destroyedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKED.SDR AALA202306096518Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGETOP SKIN PANEL LOWER SURFACE SUPPORT BRACKETAT WX 4010.2 AND RIB 7A. REPLACED BRACKET PER SRM 51-42-11.SDR SWAA2023053129365Strap · corrodedCORROSION LOWER STRUCTURE STRAP LOCATED IFSS 160 TO IFSS 165 IB LEADING EDGE AT RT WING 2023-258116<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 130063701; DUE DATE: 16 JUN 23.;[02] TOOL USED ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 221860711; DUE DASDR DALA2023042003118Unknown · unknownSHIP 3302 RH WING TIP, L.E. RIB CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 608038-14 SECTION I. (2727882)SDR U5OA202308230002Flange · corrodedLH AND RH OUTBOARD TRAILING EDGE BOX WING REBATE FLANGES HAVE EXFOLIATION CORROSION, FOUND DURING CMP 575019 / 575020.SDR SWAA2023053127997Bracket · crackedCRACK BRACKET ASSY BS 540 BTW BL0 TO LBL 24.75 AT PASSENGER CABIN 2023-257937<[01] REPLACED BRACKET ASSY BS 540 BTW BL0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02; SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED BRACKET ASSY SDR SWAA2023053127998Bracket · crackedCRACK BRACKET ASSY BS 540 BTW BL0 TO RBL 24.75 AT PASSENGER CABIN 2023-257940<[01] REPLACED BRACKET ASSY BS 540 BTW BL0 TO RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02; SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED BRACKET ASSY SDR SWAA2023052228062Bracket · elongatedLEFT WING L/E ANTI-ICE DUCT SUPPORT BRACKET HAS ELONGATED HOLES JUST UNDER ACCESS PANEL 511AT. (DOT #28-1)<[01] REMOVED AND REPLACED LEFT WING L/E ANTI-ICE DUCT SUPPORT BRACKET JUST UNDER ACCESS PANEL 511AT. IN REF SOPM 20-50-01;[02] VERIFIED STEP 1.SDR SWAA2023052227584Fitting · damagedL/W REAR SPAR FIXED T/E PANEL 551GB INB AFT SUPPORT STRUT LOWER ATTACHED FITTING HAS ELONGATED HOLE MKD DOT<[01] REMOVED AND REPLACED FITTING AT 551-GB. PANEL. USED REF. SRM-51-40-02-0G-0.;[02] VERIFIED FITTING REPLACEMENT.SDR SWAA2023052227583Fitting · elongatedL/W REAR SPAR FIXED T/E PANEL 551GB INB FWD SUPPORT STRUT UPPER ATTACHED FITTING HAS ELONGATED HOLE MKD DOT<[01] REMOVED AND REPLACED SUPPORT STRUT AT PANEL # 551-GB. REF. SRM- 51-40-02-0G-0.;[02] INSPECTED REPLACEMENT OF BEAM FITTING.SDR IXXA2023041401Rib · crackedLW AIR LOAD RIB CRACKED.SDR SWAA2023051526181Plate · crackedCRACK INBOARD TRAILING EDGE CORRUGATED PLATE IRSS 215 AT RT WING 2023-237955<[01] REPLACED CORRUGATED PLATE LOC. IRSS 215 AT RT WING AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 . SEE INDIVIDUAL SIGN OFF BELOW.;[02] COMPLETE TASK CERTIFIEDSDR EE4Y2023041017575Skin · crackedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND AN CRACK UNDER THE EXISTING REINFORCEMENT LOCATED IN THE LH WING
UPPER SKIN AT SPAR II OVER RIB 10.WAS REPAIRED FOLLOWING EMB REPAIR INSTRUCTIONS UNDER ETD2023-190-004421 REV / AND COOPESA EO# COO-EO-2023-17209-RSDR EE4Y2023041017579Skin · crackedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND A CRACK UNDER THE EXISTING REINFORCEMENT LOCATED IN THE RH WING
UPPER SKIN AT SPAR II OVER RIB 10. WAS REPAIRED FOLLOWING EMB REPAIR INSTRUCTIONS UNDER ETD2023-190-004420 REV A AND COOPESA EO# COO-EO-2023-17310-RSDR SWAA2023051524899Support Angle · crackedCRACK TRAILING EDGE DEFLECTION CONTROL SUPPORT ANGLE LOCATED ORSS 261 PLUS 18 INCHES APROX. AT RT WING. REPLACED SUPPORT ANGLE LOCATED TRAILING EDGE DEFLECTION CONTROL; ORSS 261 PLUS 18 INCHES APROX. AT RT WING IAW SRM 51-10-02 ITEM 9 AND DRAWING 115A6200 SHESDR SWAA2023051524897Support Angle · crackedCRACK TRAILING EDGE DEFLECTION SUPPORT ANGLE LOCATED ORSS 261 PLUS 9 INCHES APROX AT RT WING 2023-237732<[01] REPLACED DEFLECTION SUPPORT ANGLE LOCATED ORSS 261 PLUS 9 INCHES APROX AT RT WING I.A.W B737-700 SRM 51-10-02 ITEM 9.;[02] TASK CARD COMPLETEDSDR SWAA2023050428232Panel · crackedRIGHT WING LOWER MID SPAN T/E ACCESS PANEL # 661CB HAS SEVERAL FASTENERS HOLES BULGING/CRACKED<[01] APPLIED REPAIRED AT PANEL # 661CB PER B737 SRM 51-70-04-2R-0 (4.L.6.7). LOCATED AND DRILLED REPAIRED AREAS ON ACCESS PANEL #661CB AS PER B737-700 SRM 51-40-05-0SDR JR2R20230408156Angle · crackedWING SPAR 2 LOWER ANGLE LOCATED FWD OF LH WHEEL WELL FWD SIDE OF BULKHEAD CRACKEDSDR SWAA2023050924359Angle · crackedLEFT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL LOWER O/B ANGLE CRACKED<[01] REMOVED AND REPLACED DAMAGED L/W T/E DEFLECTION CONTROL RIB PANEL LOWER O/B ANGLE IN REF WITH SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1; COMPLETESDR SWAA2023050924361Angle · crackedLEFT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL LOWER CENTER ANGLE O/B EDGE CRACKED<[01] REMOVED AND REPLACED DAMAGED L/W T/E DEFLECTION CONTROL RIB PANEL LOWER CENTER ANGLE IN REF WITH SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1; COMPLETESDR FDEA202304060577Web · crackedR/H WING L/E SUBSTRUCTRE BULLNOSE WEB IS CRACKED IN THE LOWER BEND RADIUS JUST FWD OF THE FUELING SVC PANEL. REPAIRED R/H WING L/E SUBSTRUCTURE BULLNOSE WEB IAW B767 SRM 57-41-13-2R.SDR FDEA202304060574Web · crackedL/H WING L/E BULLNOSE INTERNAL WEB IS CRACKED IN THE LOWER RADIUS JUST FWD OF THE FUELING SVC PANELSDR SWIA20230519037Unknown · dented*LH WING LOWER WING PLANK DENTED WS163.00 €“ WS178.00 FORWARD OF FUEL PANEL 550AB AREA (MARKED) (C-CHECK RO 5/15/2023) DENT ON LH WING LOWER WING PLANK AT WS163 - 178 FOUND ACCEPTABLE TO ENGINEERING REF REO 601R-57-21-3739 REV -- DATED 2023-04-27, ALLSDR DALA2023040502629Unknown · unknownSHIP 5815 LIGHTNING STRIKE ON RT WINGLET UPPER TIP TRAILING EDGE, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B757 SRM APB 57-31-01. (2699111)SDR DALA2023040302585Unknown · unknownSHIP 5815 LIGHTNING STRIKE ON RIGHT WINGLET INBOARD SKIN T/E ZONE 6 APPROX STATION 5, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B757 SRM APB 57-31-01. (2699213)SDR DALA2023040302584Unknown · unknownSHIP 5815 LIGHTNING STRIKE ON RIGHT WINGLET OUTBOARD SKIN MIDDLE L/E SKIN PANEL (ITEM 2), T/E. STATION 3, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B757 SRM APB 57-31-01. (2699207)SDR DALA2023040302583Unknown · unknownSHIP 5815 LIGHTNING STRIKE ON RIGHT WINGLET OUTBOARD SKIN INBETWEEN BOTH ZONE 2 & APPROX STATION 3, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B757 SRM APB 57-31-01. (2699200)SDR DALA2023040302582Unknown · unknownSHIP 5815 LIGHTNING STRIKE ON RIGHT WINGLET OUTBOARD SKIN ON RIB 4 IN ZONE 5, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B757 SRM APB 57-31-01. (2699190)SDR DALA2023040302581Unknown · unknownSHIP 5815 LIGHTNING STRIKE ON RIGHT WINGLET OUTBOARD SKIN TRAILING EDGE ZONE 6 ABOVE STATION 4 #2, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B757 SRM APB 57-31-01. (2699183)SDR DALA2023040302580Unknown · unknownSHIP 5815 LIGHTNING STRIKE ON RIGHT WINGLET OUTBOARD SKIN TRAILING EDGE ZONE 6 ABOVE STATION 4 #1. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B757 SRM APB 57-31-01. (2699177)SDR DALA2023040302579Unknown · unknownSHIP 5815 LIGHTNING STRIKE ON RIGHT WINGLET OUTBOARD SKIN TRAILING EDGE ZONE 6 BELOW STATION 4. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B757 SRM APB 57-31-01. (2699117)SDR DALA2023040302578Unknown · unknownSHIP 5815 LIGHTNING STRIKE ON RIGHT WINGLET OUTBOARD SKIN LOWER CENTER OF ZONE 3. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B757 SRM APB 57-31-01. (2699114)SDR SWAA2023050122035Angle · crackedCRACK SUPPORT ANGLE LOCATED BS540 AND FROM BL0 TO LBL24 CENTER SECTION 2023-219688<[01] REPLACED SUPPORT ANGLE LOCATED BS540 AND FROM BL0 TO LBL24 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9;[02] RII JOB COMPLETEDSDR SWAA2023050122036Angle · crackedCRACK SUPPORT ANGLE BS540 AND FROM BL0 TO RBL24 CENTER SECTION 2023-219689<[01] REPLACED SUPPORT ANGLE LOCATED AT BSTA 540 FROM BL0 TO RBL 24 IAW SRM B737-700 51-10-02 AND DWG 143A060 REV A.;[02] CERTIFIED STEP 1 COMPLETE RII <BR>REPLACED SUPPORT ANGLE LOCATEDSDR SWAA2023050122037Angle · crackedCRACK SUPPORT ANGLE LOCATED BS540 AND FROM RBL25 TO RBL45 CENTER SECTION 2023-219695<[01] REPLACED SUPPORT ANGLE LOCATED BS540 AND FROM RBL25 TO RBL45 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFF BELOW;[02] RII JOB COMPLETEDSDR SWAA2023040721849Fitting · looseRIGHT WING NO 8 MOVEABLE SLAT O/B UP STOP FITTING IS LOOSE MKD DOT<[01] REMOVED UP STOP FITTING AT RIGHT WING;#8SLAT O/B AS PER SRM 51-40-02-0G-0.;[02] REMOVED AND RE-INSTALLED RIGHT WING NO 8 MOVEABLE SLAT O/B UP STOP FITTING AS PER SRM 51-40-02-0G-0. NO PLAY
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