JASC 5710

Service difficulty reports · 4,458

Reports filed under 5710 · Wing Main, Frame 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 = '5710'
  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.

SDR SWAA2024100136127Winglet · crackedDOT#19 A-043 RH WINGLET LOWER BLADE; DURING INTERNAL BORESCOPE INSPECTION FOUND EVIDENCE OF A CRACK APPROXIMATELY 45.5' FROM UPPER EDGE<[01] REMOVED AND REPLACED RH WINGLET LOWER BLADE IAW B737-8 AMM TASK 57-31-21 <BR><BR>ISSUED TAG: WN 47681;[02] VERIFIED ITESep 10, 2024 · N8725L · Boeing 7378SDR UATA2024092405701Profile · crackedL/H OUTBOARD WING HAS ONE CRACKED PROFILE ON THE FALSE SPAR AT WING STATION 4900. REPLACED CRACKED PROFILE WITH ONE OF LOCAL MANUFACTURE.Sep 10, 2024 · N439RA · Casa C212200SDR UIEA2024091000893Retainer · corrodedCORROSION - RETAINER, INBD SIDE FWD SEAL OF L/H WING INBD T/E CAVITY FWD LOWER FIXED PNL, WBL 129.(<P>1. REMOVE DAMAGE PART IAW SRM 51-40-0G-0, REV=101. 2. INSTALL NEW PART IAW SRM 51-40-02-0G-0, REV=101 AND DWG NO: 65B11631, SH=2 REV=J. 3. JOB COMPLETED AND CSep 10, 2024 · N486MC · Boeing 74745EFSDR IXXA20241003001Support Beam · corrodedRIGHT WING, UPPER TRAILING EDGE PANEL SUPPORT BEAM IS CORRODED. HAECO WO 320008 NON ROUTINE 40687Sep 5, 2024 · N491AZ · Boeing 767323SDR FDEA202409051241Doubler · corrodedRIGHT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN INNER REAR SPAR AND YW 467, BETWEEN XW 212 AND XW 230 FOUND CORROSION AS MARKED. RIGHT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN INNER REAR SPARSep 5, 2024 · N596FE · Doug MD11FSDR SWIA20250106830Fairing · wornRIGHT WING, INBOARD FLAP, INBOARD AND OUTBOARD FAIRINGS HAVE WORN THROUGH THE PAINT OF THE FLAP LOWER SKIN, HN00184284 (C-CHECK RO 12/21/2024) (FILED CLOSED)R/H WING, I/B FLAP LWR SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01, FIG. 57-52-01-9Aug 30, 2024 · N374CA · Cndair CL6002C10SDR SWAA2024092432459Winglet · corrodedCORROSION WINGLET TIP AT LT WING 2024-512594<[01] REPAIRED WINGLET TIP AT LT WING I.A.W B737-800 SRM 57-30-01 REPAIR 6. SEE INDIVIDUAL SIGNS OFF BELOW;[02] REPAIRED WINGLET TIP AT LT WING I.A.W B737-800 SRM 57-30-01 REPAIR 6. SEE INDIVIDUAL SIGNS OFF BELOWAug 30, 2024 · N8324A · Boeing 7378H4SDR SWAA2024092332883Gasket · corrodedTHE METAL GASKET FOR PANEL 633BB HAS AREAS OF CORROSION.<[01] ORDERED NEW METAL GASKET (RING ASSY) FOR PANEL 633BB. RING TO BE INSTALLED ON (TTG8Q00UYGPU) LINE# 814 (J-PANEL TASK CARD) CLOSE-PANEL 633BB. NEW RING IS ATTACHED TO PANEL 633BB FOR REFERENCE.;[02] Aug 30, 2024 · N8723Q · Boeing 7378SDR SWAA2024090332086Plate · pulledL/H WING LWR T/E PANEL I/B OF #1 PYLON WIGGLE PLATE FASTENERS PULLED.<[01] R&R L/H WING LWR T/E PANEL OF #1PYLON WIGGLE PLATE PER SRM 51-40-02;[02] R&R L/H WING LWR T/E PANEL I/B OF #1PYLON WIGGLE PLATE PER SRM 51-40-02Aug 30, 2024 · N454WN · Boeing 7377H4SDR SWAA2024090332087Support Bracket · separatedL/H WING LWR T/E PANEL I/B OF #1 PYLON I/B SUPPORT BRACKET; FWD SUPPORT ROD SEPARATED/DAMAGED.<[01] REMOVED AND REPLACED L/H LWR WING T/E #1 PYLON I/B SUPPORT BRACKET ROD I.A.W AMM 57-50-02Aug 30, 2024 · N454WN · Boeing 7377H4SDR CALA2024090302367Blowout Panel · missingTEST FLIGHT, RIGHT WING BLOW OUT PANEL 622AB MISSING.Aug 29, 2024 · N454UA · Airbus A320232SDR CALA2024083000513Blowout Panel · missingPDA 2 UPON RETURN OF TEST FLIGHT 3836 IN LCQ. FOUND PANEL # 622AB MISSING FROM RT WING LEADING EDGE REF LOG PAGE 9081839. IAW GMM 02-30-95. UPDATED TO ATTACH IMAGE. RT WING PANEL 622AB FOUND MISSING AFTER TEST FLIGHT.Aug 29, 2024 · N454UA · Airbus A320232SDR 2024FA0000672Link · corrodedWHILE ACCOMPLISHING 96-MONTH INSPECTION TASK 57-10-00-202, DETAILED INSPECTION OF THE WING-TO-FUSELAGE ATTACHMENT FITTINGS, FOUND EVIDENCE OF CORROSION ON THE AFT R/H WING TO FUSELAGE ATTACHMENT LINK LOWER SPHERICAL BEARING. SUBMITTED SRPSA TO BOMBARDIER FOR DAug 29, 2024 · N2HL · Bombdr BD1001A10SDR JR2R20240829627Fitting · crackedRH AILERON QUADRANT FITTING CRACK IN RH MLG WHEEL WELLAug 29, 2024 · N86309 · Emb ERJ170200LRSDR SWAA2024092030975Panel · corrodedTHE RIGHT WING REFUELING PANEL HAS AREAS OF CORROSION.<[01] REMOVED AND REPLACED REFUELING PANEL PER SRM 51-40-02;[02] VERIFIED WORK; CORROSION WAS LIMITED TO THE PART REPLACEDAug 27, 2024 · N8723Q · Boeing 7378SDR UIEA2024083000866Beam · crackedRHW L/E - ILES 567 D BEAM WEB CRACKED.(<P><SPAN>RHW L/E - ILES 567 D BEAM WEB REPAIRED IAW RI-57-41-17036 REV.A. NO FURTHER DEFECTS NOTED.</SPAN></P>)Aug 27, 2024 · N852GT · Boeing 74787UFSDR UIEA2024083000863Beam · crackedLHW L/E - ILES 567 D-BEAM WEB CRACKED.(<P><SPAN>LHW L/E - ILES 567 D-BEAM WEB REPAIRED IAW RI-57-41-17037 REV.A. NO FURTHER DEFECTS NOTED.</SPAN></P>)Aug 27, 2024 · N852GT · Boeing 74787UFSDR VNAA20240908008Canister · crackedCRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.- -Aug 23, 2024 · N549NN · Bombdr CL6002D15SDR VNAA20240908007Canister · crackedCRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.--Aug 23, 2024 · N549NN · Bombdr CL6002D15SDR SWIA2024110861Structure · damagedRH WING JACK PAD DOES NOT GO INTO THREADS TRANS#28722388 (C-CHECK RO 11-6/2024) REPLACED RH WING JACK PAD WITH A SERVICEABLE UNIT REF CRJ 700 SRM 51-42-21-001-001-A01 REV. 38, DATED JULY 25, 2020, DWG CC670-10004 REV.-F, DWG CC670-10038 REV.NC. LEAK CHEAug 21, 2024 · N755EV · Cndair CL6002C10SDR SWI2024F01161Pad · damagedRH WING JACK PAD DOES NOT GO INTO THREADS TRANS#28722388 (C-CHECK RO 11-6/2024) REPLACED RH WING JACK PAD WITH A SERVICEABLE UNIT REF CRJ 700 SRM 51-42-21-001-001-A01 REV. 38, DATED JULY 25, 2020, DWG CC670-10004 REV.-F, DWG CC670-10038 REV.NC. LEAK CHEAug 21, 2024 · N755EV · Cndair CL6002C10SDR SWAA2024091928583Plate · crackedCRACK CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 218 RT WING 2024-512522<[01] TOOK MEASURE OF CRACK IS : 0.275? ON CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 218 RT WING; TOOL USED :CALIPER P/N: 500-197-30; S/N: A18135108; DUE DATE: 12 -JUL-25. EVALUATED DAMAug 21, 2024 · N8324A · Boeing 7378H4SDR DALA2024082208383Strut · corrodedSHIP 3143 CORROSION INTERCONNECTING STRUT ON LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON LH WING PER AMDS CARD 2750-6010-LT AND AMDS CARD2750 -6020-LT. (0513445)Aug 21, 2024 · N343NB · Airbus A319114SDR DALA2024082208382Strut · corrodedSHIP 3143 CORROSION INTERCONNECTING STRUT ON RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON RH WING, THE INSTALLATION IS TO BE ACCOMPLISHED WITH AMDS CARD 2750-6020-RT AND AMDS2750-6010. (0513439)Aug 21, 2024 · N343NB · Airbus A319114SDR SWI2024F01164Bolt · corrodedRIGHT WING FLIGHT SPOILER, ALL PIVOT HARDWARE AND KEEPER BOLTS CORRODED (C-CHECK RO 11/7/2024) REMOVED AND REPLACED RIGHT WING FLIGHT SPOILER, ALL PIVOT HARDWARE AND KEEPER BOLTS REF CRJ 200 AMM 27-64-05-000-801 AND 27-64-05-400-801Aug 20, 2024 · N932SW · Cndair CL6002B19SDR SWAA2024082628046Winglet · delaminatedRIGHT WINGLET UPPER TIP SHOWS EVIDENCE OF DELAMINATION UPPER WINGLET CAP HAS THREE INCHES IN LENGTH OF CORROSION.<[01] REMOVED R/H WINGLET ASSY. PER AMM 57-21-21;[02] REMOVED AND REPLACED WINGLET PER AMM 57-21-21 AND MMS 57-31-02.;[03] CWAug 20, 2024 · N8313F · Boeing 7378H4SDR SWIA2024080015Hinge · corrodedRIGHT WING FLIGHT SPOILER I/B HINGE HAS CORRODED HARDWARE TO INCLUDE HINGE BOLT (C-CHECK RO 11/7/2024) REMOVED R/H WING FLIGHT SPOILER I/B HINGE BOLT AND ATTACHING HARDWARE REF. CRJ-200 AMM 27-64-05-000-801 STEPS 3B(4)(B), 3B(5), (8), (13), (15). AND INAug 15, 2024 · N932SW · Cndair CL6002B19SDR SWIA202411080014Fastener · corrodedCORRODED HARDWARE NOTED AT ALL HINGE POINTS FOR L/H SPOILERON (C-CHECK RO 11/7/2024) REMOVED AND REPLACED W/ NEW CORRODED HARDWARE NOTED AT ALL HINGE POINTS FOR L/H SPOILERON REF CRJ-200 AMM 27-64-01-400-801, OP TEST GOODAug 14, 2024 · N932SW · Cndair CL6002B19SDR SWAA2024090325702Plate · brokenPANEL 661BB HAS BROKEN WIGGLE PLATE.<[01] REMOVED AND REPLACED PANEL 661BB WIGGLE PLATE IAW B-737 SRM 51-40-02-0G; SRM 51-40-05-0G-0 AND DWG 115A3760.<BR><BR>USED TOOL B/C 176029 <BR>DUE DATE 12-18-24;[02] VERIFIED REPLACED;<BR>C/W AUDIT PER MPM 52.02.02Aug 14, 2024 · N485WN · Boeing 7377H4SDR LR7A2024081103424Brace · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HSP57165, FOUND LH OUTERWING BRACE CRACKED AT OWS56L, FS535. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 436632. / PSE# 57-50-14, AD 2012-06-09Aug 11, 2024 · N403LC · Lkheed 382GSDR LR7A2024081103423Brace · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HSP57165, FOUND LH OUTERWING BRACE CRACKED AT OWS108L, FS535. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 436631. / PSE# 57-50-14, AD 2012-06-09Aug 11, 2024 · N403LC · Lkheed 382GSDR LR7A2024081103422Brace · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HSP57165, FOUND RH OUTERWING #4 MAIN TANK BRACE CRACKED AT OWS248R. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 436630. / PSE# 57-50-14, AD 2012-06-09Aug 11, 2024 · N403LC · Lkheed 382GSDR DALA2024081408128Winglet · damagedSHIP 669 FOUND DAMAGE ON RH WINGLET TIP INBOARD SIDE. POSSIBLE LIGHTENING STRIKE. DAMAGE OUT OF LIMITS PER B757 SRM 57-30-01-1A-1 APB DOCUMENT AP57.2-0602 [57-31-01]. DAMAGE 1.2" FROM TRAILING EDGE, 1.5" FROM FOWARD FASTENER,1.4375 FROM LOWER FASTENER. CORRECTAug 10, 2024 · N669DN · Boeing 757232SDR SWAA2024092322980Support · crackedLH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT O/B RIVET HAS CRACK.<[01] REMOVED AND REPLACED LT WING DEFLECTION CONTROL RIB FIXED UPPER PANEL TRANSVERSE SUPPORT IAW SRM 51-40-02-0G-0Aug 5, 2024 · N267WN · Boeing 7377H4SDR SWAA2024092322984Support Fitting · crackedLH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM ORRS 261+8 AFT END HAS CRACK.<[01] REMOVED AND REPLACED LT WING DEFLECTION CONTROL RIB FIXED UPPER PANEL MID SUPPORT BEAM AFT END FITTING IAW SRM 51-40-02-0G-0Aug 5, 2024 · N267WN · Boeing 7377H4SDR SWAA2024092322981Beam · crackedRH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM ORRS 261+8 AFT END HAS CRACK<[01] REMOVED AND REPLACED RH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM ORRS 261+8 IAW SRM 51-40-02 AND AMM 20-50-11-910-801.;[02] CAL Aug 5, 2024 · N267WN · Boeing 7377H4SDR DALA2024080907924Strut · corrodedSHIP 3149 CORROSION INTERNAL AREA ON LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON LH WING AS PER A320 FAM AMM 27 -51-44-000-001-A AND 27-51-44-400-001-A. (0484143)Aug 4, 2024 · N349NB · Airbus A319114SDR DALA2024080907923Strut · corrodedSHIP 3149 CORROSION INTERNAL AREA ON RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON RH WING AS PER A320 FAM AMM 27 -51-44-000-001-A AND 27-51-44-400-001-A. (0479667)Aug 2, 2024 · N349NB · Airbus A319114SDR SWIA202408190001Fitting · damagedLOWER WING T/E FITTING INBD GROUND SPOILER STA 0.00, RHS. REMOVED AND REPLACED RH WING TRAILING EDGE FITTING AT SPS0.00 IN REF TO CRJ 700 SRM 51-42-21.Aug 1, 2024 · N768SK · Cndair CL6002C10SDR DALA2024080707848Wing · ground damageSHIP 3265 DISC: LT LWR WINGTIP STRUCK AND DAMAGED DURING REPOSITIONING. C/A: REMOVED LT WINGTIP FENCE PER A320 CDL 57-00-01D. C/W REPETITIVE CHECK. AC DUE PRIOR TO DEPARTURE CHECK TO VERIFY SPEED TAPE IS INTACT. HARDWARE PLACED IN MCO POUCH. AC OK FOR SERVICE.Jul 31, 2024 · N365NW · Airbus A320212SDR IXXA202400731003Stiffener · crackedLEFT WING L/E VERTICAL SPAR STIFFENER CRACKED AT TOP SIDE THROUGH FASTENER AT LES 686 JUST O/B OF FUELING PANELJul 31, 2024 · N313AZ · Boeing 767338SDR SWAA2024090319958Support Bracket · crackedCRACK TRAILING EDGE SUPPORT BRACKET ORSS 270 AT RT WING 2024-458830<[01] REPLACED SUPPORT BRACKET LOC TRAILING EDGE ORSS 270 AT RT WING IAW B737-700 SRM 51-40-02 AND DRAWING 115A2930 SHEET 6 REV -:;[02] TASK COMPLETEDJul 30, 2024 · N259WN · Boeing 7377H4SDR SWAA2024090319957Support Angle · crackedCRACK TRAILING EDGE SUPPORT ANGLE ORSS 270 AT RT WING 2024-458831<[01] REPLACED SUPPORT ANGLE ORSS 270 AT RT ON TRAILING EDGE WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2930 SHEET 8 ( REV. -);[02] REPLACED SUPPORT ANGLE ORSS 270 AT RT ON TRAILING EDGE WINJul 30, 2024 · N259WN · Boeing 7377H4SDR DALA2024080107672Winglet · damaged(LOG 6061532) RETURN TO GATE STRUCK LEFT WING SHARK FIN ON OTHER AIRCRAFT DAMAGE APPEARS LIMITED TO THAT AREA. REMOVED LEFT WINGLET PER B737 AMM 57-21. INSTALLED L/H WINGLET THROUGH STEP H(14) PER B737 AMM 57-21 INSTALLED VENTRAL STRAKE PER B737 APB SUPP AMM 5Jul 30, 2024 · N853DN · Boeing 737932ERSDR IPXA2024091269244Static Wick · corrodedFAULT STR Z600 R/WING TIP WINGLET, STATIC WICK BASES (2EA) ARE CORRODED. 72-012 INSTALLED WING TIP WINGLET R/H SIDE(2EA) STATIC WICK BASES. IAW SRM 51-40-21. REVIEWEDJul 29, 2024 · N164UP · Airbus A300F4622RSDR IPXA2024091069202Doubler · corrodedFAULT STR Z600 R/WING TIP, UPPER SURFACE STATIC WICK BASE IS CORRODED. 72-011 INSTALLED FILLER PLATE, DOUBLER AND STATIC WICK BASE AT R/H WING TIP, UPPER SURFACE I.A.W. A300-600 S.R.M. 57-30-11, FIGURE 214 (SHEET 4) AND S.R.M. 51-40-21.Jul 29, 2024 · N164UP · Airbus A300F4622RSDR UIEA2024072400738Beam · crackedLHW L/E ILES #690 D BEAM WEB, UPPER CHORD, LOWER CHORD AND UPPER CHORD ATTACH STRAP FOUND CRACK(<P>LHW L/E ILES #690D BEAM WEB, UPPER CHORD, LOWER CHORD AND UPPER CHORD ATTACH STRAP REPAIRED IAW RI NO : RI-57-41-17003 REV A. NO FURTHER DEFECTS NOTED</P>)Jul 29, 2024 · N498MC · Boeing 74747UFSDR FDEA202407271063Former · crackedDURING HMV1, LFC, LSY4 CHECK AT INDY HVMX WE HAVE FASTENERS LOOSE/DAMAGE ON LS/RS FLE SKIN (MISSING AND COMING OUT), AT LS FLE S OSS 441. FORMER CRACKED AT LS OSS 441, PN 114T2170-5 WITH ANGLE 114T2171-4, FORMER IS ATTACHED TO RIB 114T2241-7. REMOVED (PN 1Jul 27, 2024 · N264FE · Boeing 7673S2FSDR FDEA202407271061Former · crackedDURING HMV1, LFC, LSY4 CHECK AT INDY HVMX WE HAVE FASTENERS LOOSE/DAMAGE ON LS/RS FLE SKIN (MISSING AND COMING OUT), AT RS FLE S OSS 499; ALSO HAVE FORMERS CRACKED. FORMER CRACKED AT RS OSS 499, PN 114T2511-14 WITH ANGLE 114T2511-12, FORMER IS ATTACHED TJul 27, 2024 · N264FE · Boeing 7673S2FSDR IPXA2024072597199Winglet · ground damageA/C STRUCK BY K-LOADER. DAMAGE TO R/H WINGLET TRAILING EDGE INSTALLED NEW WINGLET UP TO AND INCLUDING STEP 18 REFERENCE AMM 57-31-03-002-002. ALL OPS CHECKS GOOD. ACCOMPLISHED AMM 57-31-03-002-002 1F (19 THRU AND 21)Jul 25, 2024 · N344UP · Boeing 76734AF
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