JASC 5720
Service difficulty reports · 13,638
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 CALA2022081202051Shear Tie · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00099. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 U301243, 08/09/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R IAW B737-800 SRM 51-40-02 AND BAC DWG 1SDR CALA2022081202050Shear Tie · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00099. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 U301243, 08/09/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R IAW B737-800 SRM 51-40-02 AND BAC DWG 1SDR CALA2022081202049Shear Tie · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 40.87 IS CRACKED. SUPPORT TASK NSA EMX N/R 00100. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 40.87 U301243, 08/09/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00100 IAW B737-800 SRM 51-40-02 AND BACSDR CALA2022081202048Shear Tie · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 54.60 IS CRACKED. SUPPORT TASK NSA EMX N/R 00101. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL ENTERED BY UAL INSPECTION U301243, 08/09/2022. DATA WAS 54.60 IAW B737-800 SRM 51-40-02 AND BAC DWG 111ASDR CALA2022081202047Shear Tie · crackedB737-57-4-1262 SHEAR FITTING STA 540 AND LBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00093. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 32.40 U301243, DATE 08/10/2022. DATA WAS TRANSCRIBED FROM NSA EMX IAW B737-800 SRM 51-40-02 AND BAC DWG 111SDR CALA2022081202046Shear Tie · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 6.14 IS CRACKED. SUPPORT TASK NSA EMX N/R 00096. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 U301243, DATE 08/10/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R IAW B737-800 SRM 51-40-02 AND BAC DWSDR CALA2022081202045Shear Tie · crackedB737-57-4-1262 SHEAR FITTING STA 540 AND LBL 40.87 IS CRACKED. SUPPORT TASK NSA EMX N/R 00094. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 40.87 U301243, DATE 08/10/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R IAW B737-800 SRM 51-40-02 AND BAC DWGSDR CALA2022081202044Shear Tie · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00092. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 15.04 UAL INSPECTION U301243, DATE 08/10/2022. DATA WAS TRANSCRIBED IAW B737-800 SRM 51-40-02 AND BAC DWSDR FDEA202208111961Plate · crackedR. WING T/E WIGGLE PLATE IS CRACKED, O/B OF THE I/B FLAP, BELOW # 8 SPOILER REMOVE AND REPLACED WIGGLE PLATE PER BAD DWG 113N1630 REV CSDR SWAA2022080839317Angle · crackedRIGHT WING UPPER I/B ACCESS PANEL FWD SUPPORT ANGLE (Z BRACKET) IS CRACKED. / [01] REMOVED AND REPLACED RIGHT WING UPPER I/B ACCESS PANEL FWD SUPPORT ANGLE (?Z? BRACKET) IAW SRM 51-40-02;[02] C/WSDR SWAA2022080839181Bracket · brokenLT MLG AREA; LANDING GEAR ELECTRICAL BUNDLE GUIDE; LOWER BRACKET BROKEN LT MLG AREA LANDING GEAR ELECTRICAL BUNDLE GUIDE LOWER BRACKET BROKEN / [01] REMOVED AND REPLACED BRACKET PER. SRM REF. 51-40-02.SDR IPXA2022081685328Doubler · crackedINSPECTION TYPE:1CRH WING L/E FORMER STRAP DOUBLER CRACK JUST O/B OF #10 SLAT TRACK.REMOVED,FABRICATED AND INSTALLED CRACKED STRAP DOUBLER IAW DWG ARB3954 AND SRM 51-33-01 (MINOR).SDR SWAA2022081638543Access Panel · delaminatedDELAMINATED ACCESS PANEL 621QB AT RT WING 2022-368522 / [01] TOOL USED CALIPER PN: 500-197-30; SN: 15120589; D/D: 28/NOV/22.;[02] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18196127; D/D: 16/JAN/23;[03] TOOL USED SCALE PN: 91847; SN: AE-409322; D/D: 06/JAN/23.;SDR FDEA202208041873Beam · corrodedL.WING I/B FIXED L/E NOSE BEAM IS CORRODED REPLACED NOSE BEAM ASSY. PER BAC DWG 114N1606 AND FEDEX EA F-5720-T0369810 TITLE WING - SECONDARY WING STRCT - LH WING, FIXED LEADING EDGE, ISS 106-168, NOSE BEAM, ALTERNATE NDT PROCESS AND ALTERNATE FINISH.SDR IPXA2022081385191Doubler · crackedINSPECTION TYPE:3CLH WING L/E BEADED DOUBLER CRACK BETWEEN STA.XOS=629.62 AND XOS=633.49.REPAIRED LH WING L/E CRACKED BEADED DOUBLER BETWEEN STA.XOS=629.62 AND XOS=633.49 IAW SRM 57-40-02 REPAIR 15,FIG 205,REV 69 (MAJOR).SDR DALA2022081005456Wing · damagedSHIP 6807 LEFT WING TIP 0.3" X 0.9" METAL MISSING DUE TO LIGHTNING STRIKE. CORRECTIVE ACTION: PERFORMED SECTION 1 TIME LIMITED REPAIR PER ERA 601212-14 REV ORIGINAL. (9206323)SDR YENA2022080200738Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION LOCATED ON RIB 11 PLUS 3 INCH TOP SKIN LOWER SURFACE OVERHANG TRAILING EDGE LH WING. REFER TO THE MPD TASK 572178-01; REWORKED AFFECTED AREA LOC. ON RIB 11 PLUS 3IN AT TOP SKIN LOWER SURFACE OVERHANG TRAILING EDGE AT LH WINSDR YENA2022080200732Skin Panel · corrodedDURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL #2 / TE OVERHANG LOWER SURFACE BETWEEN RIB 9 AND 11 - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2022080200731Skin Panel · corrodedDURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL #2 / TE OVERHANG LOWER SURFACE BETWEEN RIB 13 AND 15 - TIME-LIMITED REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR SWAA2022080136487Angle · crackedL/H WING PANEL 511AT PANEL SUPPORT FWD ATTACH 'Z' ANGLE IS CRACKED / [01] R&R L/H WING PANEL 511AT PANEL SUPPORT FWD ATTACH 'Z' ANGLE IN REF TO SRM 51-40-02. NO FURTHER DEFECTS NOTED.SDR SWAA2022082936325Bracket · crackedRIGHT WING TO BODY FAIRING 191AR SUPPORT CRACKED AT WING L/E ATTACH POINT.(51-003) / [01] REMOVED RIGHT WING TO BODY FAIRING 191AR SUPPORT BRACKET AT WING L/E ATTACH POINT PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED 1;[03] REMOVED PANEL #195AR AND PANEL #191SDR FDEA202207291811Stiffener · crackedRIGHT WING Ï¿½ FIXED LEADING EDGE LOWER STIFFENER FOUND CRACK AT STATION XOS 542. RIGHT WING FIXED LEADING EDGE LOWER CRACKED STIFFENER AT STATION XOS 542 REMOVED AND REPLACED AS PER SRM 51-31-01-OG. STIFFENER FABRICATED AS PER DOUGLAS DRAWING ARB2918 REVSDR ABXA2023050880Skin Panel · corrodedDURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), MAINTENANCE REPORTED CORROSION ON THE RIGHT WING TOP SKIN PANEL NO. 2 (112T3302-4) UPPER SURFACE AT THE FWD SPAR FASTENER LINE. FOUR LOCATIONS OF CORROSION REPORTED OUT OF LIMITS PER 767-300 SRM 57-20-01. LOCASDR IXXA2022728200011Support Beam · corrodedLEFT WING UPPER SURFACE T/E PANEL EXTRUSION ATTACHMENT ANGLE FROM WHEEL TO INBD FLAP HINGE HAS NUMEROUS AREAS OF CORROSION UNDER NUTPLATES.SDR SWAA2022090635281Support Angle · corrodedCORROSION FUEL BOOST PUMP SUPPORT ANGLE LOCATED IRSS145 WBL94.24 AND WL183 AT RT WING 2022-410127 / [01] REPLACED FUEL BOOST PUMP SUPPORT ANGLE LOCATED IRSS145 WBL94.24 AND WL183 AT RT WING IAW B737-700 AMM 28-22-41-400-802 AND RSM 51-40-02-0G-0;[02] CORRECTEDSDR SWAA2022081933564Support Angle · corrodedCORROSION ** L/W REAR SPAR LOWER T/E SUPPORT ANGLE BELOW SPOILER PANEL NO- 5 MKD DOT / [01] REF TASK CARD: TTG8Q00DRWEU FOR ANGLE REPLACEMENT.;[02] VERIFIED STEP #1SDR SWAA2022081232754Web · crackedWEB LOCATED AND ATTACHED TO INBOARD SIDE LEFT DEFLECTION CONTROL RIB SUPPORT BEAM IS CRACKED / [01] REMOVE L/H DEFLECTION CONTROL RIB SUPPORT BEAM REF SRM 51-40-02;[02] CORRECTION OF STEP 1. REMOVE WEB FROM L/H DEFLECTION CONTROL RIB SUPPORT BEAM REF SRM 51-40SDR SWAA2022081132064Flap · delaminatedRH O/B AFT FLAP HAS DELAM AREA 21 X 10 LOWER SURFACE; INBD CORNER. / [01] REMOVED R/H O/B AFT FLAP;[02] RII INSPECTED AS REQUIRED. OK TO INSTALL NEW FLAP;[03] INSTALLED NEW R/H O/B AFT FLAP PER AMM 27-51-22.;[04] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #3SDR SWAA2022082431409Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED ON BS 540 BTW BL 0 TO LBL 24 AT PASSENGER CABIN 2022-375868 / [01] REPLACED FLOOR STRUCTURE ANGLE LOCATED ON BS 540 BTW BL 0 TO LBL 24 AT PASSENGER CABIN AREA IAW B737-700 SRM 51-40-02 AND 51-10-02. SEE INDIVIDUAL SIGN OFF BSDR AALA202208025081Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR CARRIER ATTACH ANGLE LOCATED AT BS 663, LBL 9. REPAIRED PER SRM 57-10-10-2R PROCEDURE 5.SDR SWAA2022082230218Angle · crackedCRACK ACCESS PANEL 651GB ON SUPPORT ANGLE AT RT WING 2022-365782 / [01] REPLACED ACCESS PANEL 651GB ON SUPPORT ANGLE AT RT WING IAW B737-700 SRM 51-40-02-0G-0;[02] REPLACED ACCESS PANEL 651GB ON SUPPORT ANGLE AT RT WING IAW B737-700 SRM 51-40-02-0G-0SDR SWAA2022081629983Bracket · crackedCRACK SUPPORT BRACKET TRAILINGE EDGE LOCATED ORSS 270 APPROX AT LT WING 2022-368363 / [01] REPLACED SUPPORT BRACKET TRAILINGE EDGE LOCATED ORSS 270 APPROX AT LT WING IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2930 SHEET 7 REV: -;[02] REPLACED SDR SWAA2022082229669Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 280 APPROX LT WING 2022-365604 / [01] REPLACED ANGLE LOCATED TRAILING EDGE ORSS 280 APPROX LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 PART NUMBER USED: 115A6260-1 P.O: 2022 148173;[02] REPLACED ANGLE LOCATESDR SWAA2022082229670Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 270 APPROX LT WING 2022-365605 / [01] REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 270 APPROX LT WING I.A.W B737-700 51-40-02 AND SRM 51-10-02 ITEM:9 AND DWG:115A2930 SHEET:7 REV:-;[02] CORRECTED STEP 1:RSDR SWAA2022081929675Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED BS540 BLEED AIR DUCT LT SIDE AT AIR CONDITIONING BAY 2022-365641 / [01] REPLACED SUPPORT BRACKET LOCATED BS540 BLEED AIR DUCT LT SIDE AT AIR CONDITIONING BAY AREA IAW B737-700 B737-700 SRM 51-10-02; DUE TO NOT FOUND ALLOWABLE DAMASDR SWAA2022081929678Angle · crackedCRACK ANGLE LOCATED BS663 AND LBL43 APPROX AT AIR CONDITIONING BAY 2022-365648 / [01] TOOL USED TEMPERATURE CONTROLLER P/N:P3015GOES00000;S/N:112031023;DUE DATE:01-FEB-23;TEMPERATURE CONTROLLER P/N:P3015GOES00000;S/N:112820025;DUE DATE:01-FEB-23.;[02] REPLACEDSDR SWAA2022081929676Structure · crackedCRACK T CHORD LOCATED BS540 PLUS 9INCH AND RBL 41 AT AIR CONDITIONING BA 2022-365639 / [01] EQUIPMENT P/N PHASEC 3D; S/N CZ1026/09; DUE DATE: 08-SEP-22 WAS USED.;[02] REPAIRED T CHORD LOCATED BS540 PLUS 9INCH AND RBL 41 AT AIR CONDITIONING BAY IAW B737-700 SRMSDR SWAA2022081629756Plate · brokenBROKEN ACCESS PANEL 542BB PLATE AT LT WING 2022-381618 / [01] REPLACED PLATE ON ACCESS PANEL 542BB AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02;[02] REPLACED PLATE ON ACCESS PANEL 542BB AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02SDR SWAA2022082229298Access Panel · crackedCRACK OPEN HOLES ON ACCESS PANEL 661BB AT RT WING 2022-365585 / [01] TOOL USED; CALIPER PN: 500-197-30; SN: 15120589; DUE DATE:;[02] TOOL USED: HOTBONDER: P/N:HCS9200B-AV S/N:18185733 DUE DATE: 16-JAN-23.;[03] TOOL USED: SCALE P/N: 91847 S/N: AE-409322 DUE DATSDR FDEA202207141731Bracket · crackedRIGHT WING INBOARD LEADING EDGE STATION 282 SLAT DRIVE SHAFT GUIDE BRACKET CRACKED REMOVED & REPLACED BRACKET IAW BAC DWG 114T1240, SHEET 6, REV - & B767 SRM 51-40-02SDR FDEA202207141730Bracket · crackedLH WING INBD LEADING EDGE, SLAT DRIVE TORQUE TUBE ALIGNMENT BRACKET IS CRACKED AT APPROX IFSS 280 REMOVED & REPLACED BRACKET IAW BAC DWG 114T1240, SHEET 6, REV - & B767 SRM 51-40-02SDR FDEA202207131714Skin · abnormalDURING HFEC OPEN-HOLE INSPECTION CARRY OUT ON RIGHT HAND WING LOWER SKIN FUEL TANK ACCESS DOOR CUTOUT BETWEEN STATION XORS 683.4 AND STATION XORS 713.6 , FOUND ADDITIONAL 01 EACH REPAIR BUSHING INSTALLED AT FASTENER HOLE #6 WHICH IS NOT CALLED OUT FOR RESDR SWAA2022082228157Support Bracket · elongatedELONGATED HOLE FRONT SPAR SUPPORT BRACKET AT IFSS 86 APPROX AT LT WING 2022-365489 / [01] REPLACED FRONT SPAR SUPPORT BRACKET AT IFSS 86 APPROX AT LT WING IAW SRM 51-40-02-0G-0 AND AMM 36-13-01-400-801 STEP 7.G(8)<BR>VERIFIED CALIBRATION TOOL USED. TORQUE P/N:SDR SWAA2022082228155Bracket · elongatedELONGATED HOLE FRONT SPAR SUPPORT BRACKET AT IFSS 86 APPROX AT RT WING 2022-365491 / [01] REPLACED FRONT SPAR SUPPORT BRACKET AT IFSS 86 APPROX AT RT WING I.A.W B737-700 SRM 51-40-02 AND AMM 36-13-01-400-801.;[[06] REPLACED FRONT SPAR SUPPORT BRACKET AT IFSS 8SDR SWAA2022081628217Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ON DEFLECTION CONTROL AREA AT ORSS 270 AT LT WING 2022-381278 / [01] REPLACED ANGLE TRAILING EDGE LOCATED ON DEFLECTION CONTROL AREA AT ORSS 270 AT LT WIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV-. SEE INDSDR SWAA2022081628218Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ON DEFLECTION CONTROL AT ORSS 270 AT RT WING 2022-381280 / [01] REPLACED ANGLE TRAILING EDGE LOCATED ON DEFLECTION CONTROL AT ORSS 270 AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING # 115A2930; SHEESDR CALA2022071301716Flap · wornB757-06-3-0324 RIGHT WING IB MAIN FLAP LE AREA WORN NUMEROUS SPO TS, TRANSCRIBED FROM HAECO GSO NR 9280660SDR IPXA2022081785353Bracket · corrodedINSPECTION TYPE:SEGROB SUPPORT FITTING POINT BELOW SPOILER 2 AND BEHIND DEFLECTOR PANEL 572LBFABRICATED AND REPLACED SUPPORT FITTING PER EA 300-5751-27-A2971 AND UPS EO A300-5740-84372-ASDR REXA2022090602019None · crackedLH WING STRINGER CLIP AT WS 163.00 STR 15 CRACKED REPLACED CLIPSDR SWAA2022080227372Angle · crackedCRACK REAR SPAR T-ANGLE LOCATED WS204 AT LT WING 2022-373089 / [01] REPLACED T-ANGLE LOCATED WS204 REAR SPAR AT LT WING IAW SRM B737-700 51-40-02 AND 51-10-02 ITEM 9;[02] STEP 1 CERTIFIED
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