JASC 5720

Service difficulty reports · 13,629

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.

SDR IPXA2026090342747Skin · dentedMAJOR REPAIR. LT WING OTBD MAIN FLAP UPPER SURFACE INBD T/E AREA DENTED. FABRICATED REPAIR PLIES TO INSTALLED AT DAMAGE AREA LOCATED 57" FORM INBD-OTBD AND 11" FROM T/E- FWD, SIZE OF DAMAGE IS 2.5" IN DIAMETER. IAW SRM 57-53-01-2R-1, FIGURE 201, DETAIL IIJul 24, 2026 · N461UP · Boeing 75724APFSDR CALA2026072618012Web · crackedRIGHT WING OTBD L/E AREA BULL NOSE WEB IS CRACKED AT LOWER ATTACH FLANGE APPROX OFSS 620. ACCOMPLISHED ANGLE REPAIR IAW REO-G26003, REV IR AND ECRA 5741-01722.Jul 24, 2026 · N87507 · Boeing 737824SDR IPXA2026091019366Stiffener · crackedMAJOR REPAIR, CWB FR40 -Y450 STIFFENER HAS A CRACK INSTALLED PARTS ON STIFFENER IAW SRM 57-10-21-201, PARAGRAPH 5.2.Q AND SRM 51-40-21-001.Jul 23, 2026 · N136UP · Airbus A300F4622RSDR FDEA202607231009Landing · corrodedLEFT WING- TRAILING EDGE LOWER ACCESS PANEL 541JB CUTOUT FORWARD EDGE SUPPORT CHORD LOWER SURFACE FOUND CORROSION AT STA XW= 335. EVALUATED & FOUND EXFOLIATED OUT OF LIMITS IAW SRM 57-00-00-2R, FIGURE 202, SHEET 3. REPAIRED STA XW= 276.029 - XW= 375.50 OJul 23, 2026 · N615FE · Doug MD11FSDR AALA202608101203Intercostal · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT WING, DEFLECTION PANEL, INTERCOSTAL HAS CRACK AROUND FASTENER HOLE, O/B SIDE I14-007. MAINTENANCE REPLACED LEFT WING, DEFLECTION PANEL, INTERCOSTAL IAW B737 SRM 51-40-02.Jul 22, 2026 · N352PS · Boeing 737823SDR SWAA2026080310149Web · crackedLEFT WING TRAILING EDGE TRANSVERSE WEB ABOVE NR 1 AFT PYLON TIP CRACKED. REMOVED AND REPLACED LT WING TRAILING EDGE TRANSVERSE WEB ABOVE NR 1 AFT PYLON TIP IAW SRM 51-40-02, AND AIPC 57-50-00-36A.Jul 22, 2026 · N8545V · Boeing 7378H4SDR FDEA202607210965Stiffener · crackedRIGHT WING- LEADING EDGE COMPARTMENT STIFFENER AT XOS 541 FOUND CRACK ABOUT 0.5 INCHES. RIGHT WING LEADING EDGE COMPARTMENT CRACKED STIFFENER AT XOS 541 REMOVED AS PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G. FABRICATED STIFFENER AS PER DOUGLAS DRJul 21, 2026 · N615FE · Doug MD11FSDR FDEA202607210963Angle · crackedRIGHT WING- LEADING EDGE COMPARTMENT ANGLE AT XOS 1083 FOUND CRACK ABOUT 0.5 INCHES. RIGHT WING LEADING EDGE COMPARTMENT CRACKED ANGLE AT XOS 1083 REMOVED AS PER MD-11 SRM 51-35-01-0G. FABRICATED ANGLE AS PER DOUGLAS DRAWING ARB2920 REVISION BB. FABRICATEJul 21, 2026 · N615FE · Doug MD11FSDR FDEA202607210962Angle · crackedLEFT WING- LEADING EDGE COMPARTMENT ANGLE AT XOS 1083 FOUND CRACK ABOUT 0.6 INCHES. LEFT HAND WING LEADING EDGE COMPARTMENT CRACKED ANGLE AT XOS 1083 REMOVED AS PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G. FABRICATED ANGLE PER DOUGLAS DRAWING ARB2Jul 21, 2026 · N615FE · Doug MD11FSDR FDEA202607210961Angle · crackedLEFT HAND WING- LEADING EDGE COMPARTMENT ANGLE AT XOS1089 FOUND CRACK ABOUT 0.5 INCHES. LEFT HAND WING LEADING EDGE COMPARTMENT CRACKED ANGLE AT XOS 1089 REMOVED AS PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G. FABRICATED ANGLE AS PER DOUGLAS DRAWIJul 21, 2026 · N615FE · Doug MD11FSDR SWAA2026081754518Bracket · crackedCRACKED INBD TRAILING EDGE BRACKET, IRSS 210 LT WING. REPLACED THE BRACKET IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 115A2001, SHEET 24, REV A.Jul 20, 2026 · N499WN · Boeing 7377H4SDR SWAA2026081786389Angle · crackedCRACKED ANGLE, ORSS 270 ON LT WING T/E. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.Jul 20, 2026 · N499WN · Boeing 7377H4SDR SWAA2026080433329Stiffener · corrodedCORROSION FOUND ON LT L/E STIFFNER COMMON TO NR 4 TAI DUCT TAB AT OFSS 308 SS 73. REMOVED LT L/E STIFFNER COMMON TO NR 4 TAI DUCT TAB AT OFSS 308 SS 73 IAW SRM 51-40-02-0G-0. INSTALLED LT L/E STIFFNER COMMON TO NR 4 TAI DUCT TAB AT OF SS 308 SS 73 IAW SRM 51-4Jul 20, 2026 · N495WN · Boeing 7377H4SDR SWAA2026080486563Stiffener · corrodedCORROSION WAS FOUND ON STIFFNER COMMON TO NR 6 TAI DUCT TAB AT OFSS 421 SS 186 [MARKED] REMOVED AND REPLACED STIFFNER COMMON TO NR 6 TAI DUCT TAB AT OFSS 421 SS 186 IAW SRM 51-40-02-0G-0 AND AIPC 57-40-00-17.Jul 20, 2026 · N495WN · Boeing 7377H4SDR AALA202607302801Web · crackedAIRCRAFT IN BASE MAINTENANCE: WEB ASSEMBLY 115A2982-9 FOUND CRACKED AT L/H WING T/E. MAINTENANCE REPLACED WEB ASSEMBLY AT L/H WING T/E IAW B737 SRM 51-40-02.Jul 19, 2026 · N927AN · Boeing 737823SDR SWAA2026081719303Angle · crackedCRACKED ANGLE, TRAILING EDGE, ORSS 261 + 10 INCHES ON RT WING. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, & SRM 51-10-02-0G-0, ITEM 9, & DWG 115A2930, SHT 8, REV- .Jul 17, 2026 · N499WN · Boeing 7377H4SDR SWAA2026081736720Angle · crackedCRACKED ANGLE, TRAILING EDGE AT ORSS 261 + 18 INCHED, RT WING. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, & SRM 51-40-02-0G-0, & DWG 115A6200, SHEET 11, REV B.Jul 17, 2026 · N499WN · Boeing 7377H4SDR AALA202608143870Support Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SUPPORT ANGLE FIXED PANEL REAR SPAR TRAILING EDGE INBOARDSIDE LOC BTW WS 495.50 TO WS 547.0 RIGHT WING. REPLACED SUPPORT ANGLE LOC AT FIXED PANEL REAR SPAR TRAILING EDGE INBOARD SIDE BTW WS 495.50 TO WS 547.0, RIGHT WING IJul 17, 2026 · N751AN · Boeing 777223SDR CALA2026072017851Seal · wrong partESCAPE DOOR 192 CR HAS WRONG SEAL INSTALLED, IS WORN AND DOUBLE DRILLED AT EACH FASTENER HOLE. NEW CORRECT SEAL IN STOCK AND ORDERED. PARTIALLY INSTALLED NEW SEAL, FINAL INSTALL AWAITING 192DR DOOR LOWER WING CHORD REPAIR REF LP 9615472 REF SRM 51-40-02 INSTALJul 15, 2026 · N14230 · Boeing 7378H4SDR 2026FA0000717Stiffener · crackedRIGHT WING FWD LWR I/B SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWJul 14, 2026 · N755G · Piper PA28181SDR SWAA2026081744521Web · crackedCRACKED WEB, ORSS 275, LT WING T/E. REPLACED THE WEB, IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2512, SHEET 16, REV-.Jul 14, 2026 · N8651A · Boeing 7378H4SDR IPXA2026091125874Web · crackedLH WING, WEB UNDERNEATH SPOILER #5 HAS A CRACK AT I/B SIDE (DOT64-037) INSTALLED NEW INTERCOSTAL WEB P/N 2024-T3.032C B/N 0004481575 TRAVELER# T26/1872446 IAW A300-600PF SRM 51-40-21Jul 12, 2026 · N136UP · Airbus A300F4622RSDR IPXA2026090325692Stiffener · crackedLEFT WING, LEADING EDGE INTERNAL STRUCTURE, STIFFENER CRACKED INSIDE FLAP KRUEGER BAY. INSTALLED NEW STIFFENER AT LT WING, LEADING EDGE INTERNAL STRUCTURE IAW SRM 51-40-21,Jul 12, 2026 · N136UP · Airbus A300F4622RSDR CALA2026071317733Intercostal · crackedRIGHT WING FIXED UPPER T/E PANEL JUST INBD OF THE DEFLECTION CONTROL RIB SUB-STRUCTURAL INTERCOSTAL IS CRACKED IN THE RADIUS AND THROUGH THE ATTACH FASTENERS REMOVED AND REPLACED R/H WING,FIXED T/E INTERCOSTAL INBD OF THE DEFLECTION CONTROL RIB SUBSTRUCTURE IJul 12, 2026 · N87507 · Boeing 737824SDR CALA2026071217700Web · corrodedRIGHT WING OTBD L/E AREA BULL NOSE WEB IS CORRODED ON THE UPPER ATTACH FLANGE AT APPROX OFSS 580. REMOVED CORROSION AND EVALUATED MATERIAL REMOVED .002, ORIGINAL THICKNESS .050, REMAINING THICKNESS .048 FOUND WITHIN LIMITS IAW SRM 57-41-02. RESTORED SURFACE FJul 11, 2026 · N87507 · Boeing 737824SDR FDEA202607110902Support Beam · crackedCRACK ON UPPER PANEL SUPPORT BEAM, WS 1054 INNER ACCESS PANEL 561QB, LH WING UPPER PANEL SUPPORT BEAM, WS1054 INNER ACCESS PANEL 561QB, LH WING WAS REPLACED AND FASTENERS, SHIM S AND CHORDS WERE INSTALLED I.A.W. E.O. #: H-5720-E0353920 C (P5) RELEASE DATE: Jul 11, 2026 · N298FE · Boeing 767300SDR 2026FA0000732Stiffener · crackedL/H WING FWD LWR I/B SKIN, TOP AFT STIFFENER CRACKED. REPLACED WITH NEWJul 10, 2026 · N164G · Piper PA28181SDR IPXA2026082691602Support Channel · crackedRH WING T/E UPPER FIXED PANEL SUPPORT CHANNEL ABOVE THE NO.4 FLAP TRACK IS CRACKED. INSTALLED NEW SUPPOR TCHANNEL PANEL FROM RT WING T/E ABOVE THE NO.4 FLAP, IAW SRM 51-40-21.Jul 10, 2026 · N136UP · Airbus A300F4622RSDR SWAA2026081794996Nut Plate · crackedCRACKED RAIL NUT PLATE, INTERNAL CAVITY, LEADING EDGE OF SS 570 RT WING. REPLACED RAIL NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 112A4402, SHT 40, REV A. .Jul 10, 2026 · N8651A · Boeing 7378H4SDR SWAA2026081726891Support Angle · crackedCRACKED SUPPORT ANGLE ON ACCESS PANEL 651FB, RT WING. REPLACED SUPPORT ANGLE ON ACCESS PANEL 651FB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02.Jul 10, 2026 · N8651A · Boeing 7378H4SDR SWAA2026081746948Bracket · crackedCRACKED BRACKET ON ACCESS PANEL 551FB, LT WING. EVALUATED AND DID NOT FIND ALLOWABLE DAMAGE IN SRM 57-41-02-1A-2, ALLOWABLE DAMAGE 2, BRACKET MUST BE REPLACED. REPLACED THE BRACKET ON ACCESS PANEL 551FB IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02,Jul 10, 2026 · N8651A · Boeing 7378H4SDR SWAA2026081725572Web · crackedCRACKED WEB, LEADING EDGE INTERNAL CAVITY, SS 308 + 23 INCHES, LT WING. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 116A5440, SHEET 50, REV B.Jul 10, 2026 · N8651A · Boeing 7378H4SDR 2026FA0000716Stiffener · crackedR/H WING FWD LWR I/B SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWJul 9, 2026 · N779G · Piper PA28181SDR SWIA2026070976982Angle · crackedANGLE @ WS 48.30 R/H HAS 2 CRACKS (C-CHECK RO 08/29/2026)REMOVED AND REPLACED NEW CAP (ANGLE) ON THE R/H WS 48.30 IAW CRJ 200 SRM 57-21-12,51-42-20,51-40-11,51-23-00.Jul 9, 2026 · N982SW · Cndair CL6002B19SDR SWIA2026070976978Angle · crackedANGLE @ WS 48.30 L/H HAS A CRACK (C-CHECK RO 08/29/2026)REMOVED AND REPLACED NEW CAP (ANGLE) ON L/H FROM WS 48.30 IAW CRJ200 SRM 51-42-20,51-40-11,57-21-12.Jul 9, 2026 · N982SW · Cndair CL6002B19SDR IPXA2026072966442Stiffener · crackedFAULT-STR-Z500- KRUEGER BOX, FWD LOWER SIDE, STIFFENER HAS AN ANGLE SUPPORT CRACKED. INSTALLED ANGLE SUPPORT FROM KRUEGER BOX IAW SRM 51-40-21.Jul 8, 2026 · N136UP · Airbus A300F4622RSDR SWAA2026072760605Angle · crackedANGLE ON INBD SIDE OF LT WING DEFLECTION CONTROL RIB CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-0G AND DWG 115A6200 REV -.Jul 8, 2026 · N487WN · Boeing 7377H4SDR SWAA2026072764745Fitting · crackedLEFT WING FIXED T/E SEAL BULKHEAD AFT FITTING CRACKED. REMOVED AND REPLACED LT WING FIXED T/E SEAL BULKHEAD AFT FITTING IAW SRM 51-40-05-0G-0 AND DWG 115A2930 REV -.Jul 8, 2026 · N487WN · Boeing 7377H4SDR 2026FA0000731Stiffener · crackedL/H WING FWD LWR I/B SKIN, TOP AFT STIFFENER CRACKED. REPLACED WITH NEWJul 7, 2026 · N857G · Piper PA28181SDR 2026FA0000725Stiffener · crackedL/H WING FWD LWR I/B SKIN, TOP FWD STIFFENER CRACKED. REPLACED WITH NEWJul 7, 2026 · N857G · Piper PA28181SDR 2026FA0000570Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND THE BE SHEARED OFF AND/OR CRACKEDJul 7, 2026 · N2433S · Cessna 172RSDR IPXA2026081716817Web · crackedLEFT WING T/E, NEXT TO NR 4 SPOILER OTBD HINGE, WEB CRACKED. WEB, LT WING T/E NEXT TO NR 4 SPOILER OTBD HINGE INSTALLED IAW SRM 51-40-21-001.Jul 5, 2026 · N144UP · Airbus A300F4622RSDR SWAA2026081196749Rail · corrodedCORROSION ON RAIL NUT-PLATE, OFSS 340, INTERNAL CAVITY, RT WING L/E. REPLACED THE RAIL NUT-PLATE AND FASTENERS IAW SRM 51-40-02, AND DWG 112A4402, SHEET 14, REV-.Jul 5, 2026 · N7880D · Boeing 7377K5SDR SWAA2026081188172Rail · corrodedCORROSION ON RAIL NUT-PLATE, OFSS 449 INTERNAL CAVITY LT WING L/E. REPLACED THE RAIL IAW SRM 51-40-02-0G-0, AND DWG 112A4402, SHEET 13, REV -.Jul 5, 2026 · N7880D · Boeing 7377K5SDR SWAA2026081127087Rail · crackedCRACKED ON RAIL NUT-PLATE, OFSS 574 INTERNAL CAVITY RT WING L/E. REPLACED RAIL NUT-PLATE IAW SRM 51-40-02-0G-0.Jul 5, 2026 · N7880D · Boeing 7377K5SDR IPXA2026071716472Bracket · chafedLEFT WING, EVIDENCE OF CHAFING IN BRACKET AND RIVETS LOCATED INSIDE FLAP KRUEGER COMPARTMENT (INTERNAL STRUCTURE) INSTALLED WEB AT LT WING AT INTERNAL KRUEGER IAW SRM 51-40-21-001.Jul 5, 2026 · N144UP · Airbus A300F4622RSDR SWAA2026081716333Angle · crackedCRACKED ANGLE, T/E, ORR 282 RT WING. REPLACED ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A6200, SHEET 17, REV A.Jul 4, 2026 · N8651A · Boeing 7378H4SDR SWAA2026081165477Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 574 INTERNAL CAVITY OF LT WING L/E. REPLACED THE RAIL NUT PLATE IAW SRM 51-40-02-0G-0.Jul 4, 2026 · N7880D · Boeing 7377K5SDR IPXA2026082692052Support Bracket · crackedRIGHT WING FIXED LEADING EDGE INBOARD SIDE, INTERNAL STRUCTURE, NEXT TO KRUEGER COMPARTMENT, PANEL SUPPORT BRACKET BROKEN. INSTALLED SUPPORT BRACKET ON RT WING FIXED LEADING EDGE INBD SIDE, INTERNAL STRUCTURE JUST NEXT TO KRUEGER COMPARTMENT IAW SRM 51-40-2Jul 3, 2026 · N144UP · Airbus A300F4622RSDR IPXA2026081792411Web · crackedRIGHT WING TRAILING EDGE BELOW SPOILER NR 3 I/B HINGE, WEB HAS TWO CRACKS. INSTALLED WEB AT RT WING TRAILING EDGE BELOW SPOILER NR 3 INBD IAW SRM 51-40-21.Jul 3, 2026 · N144UP · Airbus A300F4622R
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