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 RRXA10754Former · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO T/E FORMER AT STA. XFS 227.335, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0.SDR RRXA10753Bracket · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BRACKET AT STA. XFS248, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8 SRM 51-SDR DHL2001367515Stiffener · damagedC-CHECK- CENTER TANK IMPACT DAMAGE ON TOP FLANGE OF LATERAL STIFFENER FWD OF TANK OVERFLOW VALVE FR 45R. DAMAGE BLENDED OUT, 0.006 INCH ALL AREAS REPROTECTED IAW SRM 51-40-12.SDR DHL2001367514Stiffener · damagedC-CHECK- CENTER TANK: IMPACT DAMAGE ON UPPER LATERAL STIFFENER AT FR 46 FWD OF LT ACCESS NR 80972. BLENDED OUT DAMAGE IAW SRM 51-40-01, DAMAGED ASSESSED AT 0.006 INCH AREA REPROTECTED IAW SRM 51-40-12.SDR C2XA01IA202Support · crackedSJK - DURING C-CHECK INSPECTION, TWO WING SKIN SUPPORTS ON RIB 19, AND ONE SKIN SUPPORT ON RIB 20 OF THE LEFT WING WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORTS IN ACCORDANCE WITH EMB-120 SRM 57-20-07, AND THE AIRCRAFT SDR DHL2001712508Angle · crackedC-CHECK - RT WING WINGLET FAIRING LWR PART SUPPORT ANGLES CRACKED 1.0 INCH. REMOVED SUPPORT ANGLES IAW SRM 51-30-2, PAGE 13. FABRICATED ANGLES (SUPPORT ANGLE) NEW WITH ALCLAD 2024, T3, 0.05 INCH IAW SRM 57-20-3, PAGE 1-3. TREATED AND PRIMED IAW SRM 51-10-2,SDR GAIA01082STAngle · crackedDURING A LTC INSPECTION AT FLIGHT STAR, IT WAS DISCOVERED A PREVIOUS REPAIR CRACKED AT RIGHT WING T/E STATION 120 AT INBOARD GROUND SPOILER ACTUATOR SUPPORT. ACCOMPLISHED FABRICATION AND INSTALLATION OF T/E ANGLE IAW B727 SRM 51-40-3 FIG 1 AND 51-30-2. (M)SDR TWAA0102413Bracket · corrodedDURING CHECK-C MAINT ON RT WING THE AFT RT END OF KEEL BEAM BOX HAD CORROSION ON DUCT BRACKET. REMOVED AND REPLACED ANGLE PER SPM 6-70-01 USING DRAWING 5936395 CALLING FOR USE OF PART NUMBER 5936395-7 ANGLE. INSTALLED ANGLE USING HI-LOKS. INSTALLED HI-LOKS SDR EISA20010022Angle · crackedDURING ROUTINE C-CHECK INSPECTION FOUND ANGLE CRACKED AT STATION 92L WING ROOT. FABRICATED REPAIR ANGLE, ALODINED, PRIMED, AND INSTALLED REPAIR ANGLE IAW SRM 51-30-2, 51-10-2, 51-40-3 FIG 1.SDR DHL2001712510Support Bracket · brokenC-CHECK, NR 4 GROUND SPOILER AFT ACTUATOR HYDRAULIC TUBING ATTACH SUPPORT BROKEN. REMOVED BROKEN SUPPORT IAW SRM 51-30-2, PAGE 1-2. FABRICATED SUPPORT T-ANGLE (EXTRUDED 7075, T6) IAW SRM 51-20-2, FIG 6. CLEANED, TREATED, AND PRIMED IAW SRM 51-10-2, PAGE 1-2SDR RRXA10756Former · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT. SIDE T/E FORMER AT STA. ZFS 175, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0.SDR RRXA10755Former · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT. SIDE T/E FORMER AT STA. ZFS 117, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0.SDR AU010117Fitting · failed(AUS) LT WING FRONT LOWER INTERPLANE STRUT ATTACHMENT FITTING BROKEN AWAY DUE TO WOOD ROT.SDR MWEA010123Fitting · corrodedRIGHT WING STATION 13 HAS 2 AREAS OF LITE CORROSION AT STATION 91 AND 94. FABRICATED AND INSTALLED ANGLE DOUBLER AND FILLER.SDR MWEA010133Fitting · corrodedRIGHT WING STRINGER 20 HAS .5 INCH BY .5 INCH OF LITE CORROSION ON FORWARD BOTTOM FLANGE, STATION 79. FABRICATED AND INSTALLED BUSHINGS AND REPAIR STRAPS.SDR MWEA010132Fitting · corrodedLEFT WING AT STATION 69 HAS LIGHT CORROSION ON A FITTING AT STRINGER 13. REMOVED AND REPLACED NEW CLIP FITTING.SDR MWEA010131Fitting · corrodedRIGHT WING STRINGER 12 HAS .5 INCH BY .5 INCH AREA OF LIGHT CORROSION STATION 101. FABRICATED AND INSTALLED BUSHINGS AND REPAIR STRINGER.SDR UPS01234919Angle · crackedINSPECTION TYPE:IN RT WING LEADING EDGE STA 349.6 WEB O/B UPPER SUPPORT ANGLE CRACKED. STOPPED DRILLED CRACK PER B727 SRM 51-10-1, NDT STOPPED DRILLED INSTALLED ANGLE REPAIR PER B727 SRM 51-40-3.SDR UPS01834798Angle · crackedINSPECTION TYPE:C1&3, RIGHT WING CENTER L/E VERTICAL ATTACH ANGLE AT XS 520 IS CRACKED. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297, AND SRM 51-1-20D.SDR RRXA010624Former · chafedDURING A MAINTENANCE VISIT FOUND THE DE-ICER DUCT CHAFED DEEP INTO FORMER AT STA XFS 416, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0 & 51-1-20D.SDR MWEA010095Splice · damagedCENTER SPLICE 14 FORWARD HAS 9 EACH OUT OF ROUND HOLES. FABRICATED AND INSTALLED NEW CENTER SPLICE.SDR MWEA010094Cap · corrodedLEFT HAND WING STATION XRS 58.500 T-CAP REMOVED DUE TO CORROSION BEYOND SRM LIMITS. FABRICATED AND INSTALLED NEW TEE CAP.SDR MWEA010093Cap · corrodedRIGHT HAND WING T-CAP REMOVED DUE TO CORROSION BEYOND SRM LIMITS. FABRICATED AND INSTALLED NEW TEE CAP.SDR MWEA010048Fitting · damagedLEFT HAND WING STRINGER 21 HAS MECHANICAL DAMAGE AT XRS 70. FABRICATED AND INSTALLED NEW STRINGER SECTION AND SPLICES.SDR SCNA01317Plate · corrodedDURING HEAVY MAINTENANCE CHECK, CORROSION WAS DISCOVERED OUT OF LIMITS ON THE LEFT HAND WING FRONT SPAR LOWER FORWARD CHORD PLATE, WS 360 TO WS 450. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED SECTION IAW B727 SRM 513002. FABRICATED NEW CHORD FROSDR CALA0100027Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING I/B BRACKET AT I/B SIDE PANEL. A NEW BRACKET WAS INSTALLED IAW ECRA 5730-01741.SDR RRXA10780Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H WING T/E AT STA. XRS 19 TO XRS 90 AND UPPER SURFACE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIRS AND INSTALLED SDR 01FDEA00016Angle · crackedRT WING PIE SECTION I/B WEB SUPPORT ANGLE CRACKED AT LOWER END. *S/D* REMOVED, REPLACED AND FAB PER IAW SRM 51-30-2, 51-10-3, AND 51-30-5.SDR UPS01234660Support Fitting · crackedINSPECTION TYPE:C, SUPPORT FITTING ON RT WING REAR SPAR AT WS 620 APPROX CRACKED. REPLACED SUPPORT FITTING WITH PART FABRICATED IAW DRAWING 69-16227.SDR UPS01634590Attach Fitting · crackedINSPECTION TYPE:PFLT LEFT WING, LEFT O/B FLAP, PANEL (WING) ABOVE O/B FITTING HAS AN 18 INCH CRACK THRU AND 24 INCH CRACK THRU THE PANEL. (SEE ITEM 1, PG 534960) MARKED THE UPPER SURFACE. REMOVED PANEL AND ACCOMPLISHED INTERIM REPAIR IAW B767-5750-13691A INSSDR UPS01434923Angle · crackedINSPECTION TYPE:C, RT WING FEAR STRUT DOOR I/B FAIRING SUPPORT ANGLE IS CRACKED. SUPPORT ANGLE REPLACED IAW SRM 51-30-02.SDR UPS01434740Bracket · crackedINSPECTION TYPE:C, RT WING LOWER T/E SUPPORT BEAM CLIP CRACKED AT FWD SIDE OF LDG BEAM AT WS 500. BRACKET REMOVED AND REPLACED IAW SRM 51-30-02.SDR DHL2001801518Structure · crackedRT WING L/E INNER PART CRACKED 2 INCHES AT HOT AIR LINER XFS 716.000. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. FABRICATED DOUBLER PER SRM 57-2-0 FIG 62. INSTALLED DOUBLER PER SRM 572-0 FIG 2.SDR CA010118008Vortex Gen · missing(CAN) - AIRCRAFT OVERNIGHTED AT ALTERNATE AIRPORT DUE TO SNOW & RAIN (ICE). - WAS DEICE NEXT DAY. HOME BASE, AME NOTICED MISSING VORTEX GEN & NEXT INBOARD BENT.- THIS IS OUTBOARD VICINITY OF OUTBOARD FUEL CAP. - NOT ESTABLISHED IF DONE DURING DE-ICING OR DURISDR UPS01234728Structure · crackedINSPECTION TYPE:C CK RIGHT WING L/E CAVITY AT STA 330.6, EXISTING REPAIR ANGLE IS CRACKED. REMOVED AND REPLACED REPAIR ANGLE IN ACCORDANCE WITH SRM 51-30-2.SDR SPAA0000032Carriage · corrodedDURING ACCOMPLISHMENT OF CPCP TASK C57-306-04 PART 2 OF 2, CORROSION WAS FOUND ON THE RT OUTBOARD MIDFLAP, OUTBOARD CARRIAGE SPINDLE. REMOVED AND REPLACED CARRIAGE PER BOEING MM 27-51-81. RIGGED FLAP SYSTEM PER BOEING MM 27-51-12 A/TSDR SPAA0000031Carriage · corrodedDURING ACCOMLISHMENT OF CPCP TASK C57-306-04 PART 2 OF 2, CORROSION WAS FOUND ON THE RIGHT OUTBOARD MIDFLAP, INBOARD CARRIAGE SPINDLE. REMOVED AND REPLACED SPINDLE PER BOEING MM 27-51-81 AND RIGGED SYSTEM PER BOEING MM A/T 27-51-12SDR SPAA0000030Carriage · corrodedDURING ACCOMPLISHMENT OF CPCP TASK C57-306-04 PART 1 OF 2, CORROSIOIN WAS FOUND ON THE LET WING OUTBOARD FLAP, INBOARD FLAP CARRIAGE SPINDLE. REMOVED AND REPLACED FLAP CARRIAGE SPINDLE PER BOEING MM 27-51-81 AND RIGGED SYSTEM PER BOEING MM 27-51-12 A/TSDR AALA20002114Stiffener · corrodedTUL - FOUND VERTICAL STIFFENER CORRODED AT AROUND WIRE TERMINAL. FABRICATED AND INSTALLED DOUBLER PER SRM 57-10-4. (M)SDR CALA0001840Casting · crackedINSPECTION FOUND LT WING TIP LEADING EDGE CASTING CRACKED WITH POPPED RIVETS AND GOUGES. THE CASTING PANEL WAS REMOVED AND A NEW CASTING PANEL WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.SDR QXEA0003296Web · damagedPDX- WEB AND ANGLE BEHIND PANELS 92M AND 92N ON RIGHT HAND WING ROOT HAVE BEEN CHAFED BY PANELS. REPAIRED IAW FOKKER SRM 51-31-01, 51-31-05 AND 53-02-17.SDR QXEA0003295Web · damagedPDX- WEB AND ANGLE BEHIND PANELS 92M AND 92N ON RIGHT HAND WING ROOT HAVE BEEN CHAFED BY PANELS. REPAIRED IAW FOKKER SRM 51-31-01, 51-31-05 AND 53-02-17.SDR 20001120SH047Web · crackedRIGHT WING MID-SPAR BETWEEN MSS 573.08 AND 585.82 HAD A CRACKED WEB. REPAIRED PER ECRA 621-57-0002. (X)SDR P2EA00389Channel · crackedSJO - DURING Q-CHECK, FOUND THE RIGHT WING TRAILING EDGE CAVITY LOWER CHORD CHANNEL AT RSS 180 WITH CRACK. (M)SDR WXOA00015Retainer · damagedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND RIGHT WING INBOARD PANEL NR 2214A TO HAVE DAMAGED RETAINER. REMOVED DAMAGED SECTION OF RETAINER, FABRICATED REPLACEMENT PART FROM 70744 T6 .032, TREATED AND PRIMED COMPONENT AND INSTALLED PERSDR WXOA00014Seal · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND LEFT WING INBOARD FILLET PANEL METAL RUB SEAL DAMAGED. REMOVED DAMAGED RUB SEAL, FABRICATED REPLACEMENT RUB SEAL FROM 2024 T3 .020, TREATED AND PRIMED COMPONENT PER DC-9 SRM 51-10-3 AND INSTASDR L1GA200000371Structure · chafedLOCALIZED CHAFING RT WING BUTTE DOOR AT XRS 145 AND 276. INSTALLED 3 DOUBLERS AND FILLERS.SDR L1GA200000369Support Bracket · gougedTHREE INCH LONG CRACK LEFT WING O/B LEADING EDGE SUPPORT. WELDED REPAIR.SDR P2EA00417Support Bracket · crackedDURING Q CHECK FOUND THE RT WING AUXILIARY SPAR AREA , UPPER FIXED PANEL SUPPORT ANGLE AT RSS 159 CRACKED L/2.00 W/0.005. REPAIRED RT WING AUXILIARY SPAR AREA UPPER FIXED PANEL SUPPORT ANGLE.SDR P2EA00353Angle · crackedSJO - DURING Q-CHECK, FOUND THE RIGHT WING AUXILIARY SPAR AREA UPPER FIXED PANEL SUPPORT ANGLE AT RSS 159 CRACKED. (M)
Back to JASC 5720