JASC 5720

Service difficulty reports · 13,631

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 SWAA2025032605766Support · wornLEFT WING I/B FIXED TRAILING EDGE SUPPORT BEAM WORN AT THE DEFLECTION CONTROL RIB SERRATED PLATES.<[01] LEFT WING I/B FIXED TRAILING EDGE SUPPORT BEAM WORN AT FASTENER HOLES MEASURES 0.043?; MATERIAL THICKNESS IS 0.100?. WEAR LIMITS IS OUT OF LIMITS PER SRM 57Mar 14, 2025 · N8689C · Boeing 7378H4SDR WRXR20250314001Strap · corrodedCORROSION UNDER PANEL 621AB IN FORWARD INBOARD AND FORWARD OUTBOARD CORNERS AROUND FASTENER HOLES. WS49 AND WS28. REMOVED CORROSION AT R/H WS28 AND WS49 ON AREA OF WING UNDER PANEL 621AB IN FORWARD INBOARD AND FORWARD OUTBOARD CORNERS AROUND FASTENER HOLES ANDMar 14, 2025 · N638NN · Cndair CL6002D24SDR SWI2025F00483Angle · corrodedFOUND CORROSION ON ANGLE P/N 601R10203-34, AT RH BATT RIB, WS53.60. (C-CHECK RO 04/17/2025)ANGLE P/N 601R10203-34. FOUND OUT OF LIMITS IAW CRJ 200 SRM 57-21-12. REMOVED AND INSTALLED NEW ANGLE P/N 601R10203-34, REF.DWG 601R10203, REV -G, CRJ200 SRM 51-42-06 Mar 13, 2025 · N693BR · Cndair CL6002B19SDR SWAA2025032404822Angle · crackedLEFT WING I/B FIXED TRAILING EDGE UPPER PANEL TO DEFLECTION RIB INTERCOSTAL IS CRACKED<[01] DRILLED NEW INTERCOSTAL (ANGLE) PER SRM 51-40-05.;[02] C/W INSPECTION DRILLED NEW INTERCOSTAL (ANGLE) PER SRM 51-40-05.;[03] REMOVED AND REPLACED LEFT WING I/B FIXED TRMar 13, 2025 · N8689C · Boeing 7378H4SDR WRXR20250313002Strap · corrodedCORROSION FOUND AT WS29.00 ON STRUCTURE SIDE WHERE PANEL 521AT MEETS STRUCTURE. REMOVED CORROSION AT L/H WS 29.00 WHERE ACCESS PANEL 521AT ATTACHES TO THE WING IAW CRJ 900 SRM 51-21-06-001-001-A01. BLENDED CORROSION DAMAGE ON L/H WING UPPER FIXED LEADING EDGE Mar 13, 2025 · N638NN · Cndair CL6002D24SDR WRXR20250313001Strap · corrodedCORROSION FOUND AT WS29.00 ON STRUCTURE SIDE WHERE PANEL 521AT MEETS STRUCTURE. REMOVED CORROSION AT L/H WS 29.00 WHERE ACCESS PANEL 521AT ATTACHES TO THE WING IAW CRJ 900 SRM 51-21-06-001-001-A01. BLENDED CORROSION DAMAGE ON L/H WING UPPER FIXED LEADING EDGE Mar 13, 2025 · N638NN · Cndair CL6002D24SDR SWI2025F01176Support Fitting · damagedDURING AUDIT OF 6YR TASK CARD 57-540-504(DETAILED INSPECTION OF THE LEFT WING INBOARD FLAP HINGE BOX SUPPORT FITTING) FOUND IMPACT DAMAGE ON THE OUTBOARD SIDE OF THE AFT FITTING AT WS54.55. REWORKED LUGS AT LEFT INBOARD FLAP HINGE BOX SUPPORT FITTING. FOUND Mar 12, 2025 · N614SK · Cndair CL6002C10SDR NACA2025031200002Nut Plate · damagedFOUND NUTPLATE DAMAGE AT ZONE 500 PNL NO.551UB 1EA.Mar 12, 2025 · N321CM · Boeing 767323SDR JJBA20250324031Angle · crackedCF3 ON WING STUB SPAR 2 LH AFT ANGLE FOUND CRACKED BTW FR 46-47. CF3 ON WING STUB SPAR 2 LH AFT ANGLE BTW FR 46-47 REMOVED AND REPLACEDMar 12, 2025 · N24128 · Emb EMB145XRSDR FDEA202503120380Beam · crackedFABRICATE BEAM USING DWGS AND SAMPLE PART (AT LEFT WS 1032) FABRICATED BEAM USING DWG 113T1913 & SAMPLE PART. INSTALLED ON NR 208 WO 89695. THIS IS A MAJOR REPAIRMar 12, 2025 · N148FE · Boeing 7673S2FSDR SWAA2025041404184Stiffener · crackedR WING FIXED UPPER TRAILING EDGE PANEL SUPPORT STIFFENER AT WBL 198.6 HAS CRACK.(MARKED)<[01] REMOVED CRACKED SUPPORT STIFFENER PER SRM 51-40-02.;[02] VERIFIED WORK PERFORMED ON C/A #1;[03] LOCATED;DRILLED AND DEBURRED THE NEW SUPPORT ANGLE PER SRM 51-40-05.;[Mar 11, 2025 · N8683D · Boeing 7378H4SDR SWAA2025041404185Angle · crackedL/H WING UPPER FIXED T/E PANEL ABOVE #1 ENGINE PYLON AFT FAIRING HAS CRACKED ANGLE ON I/B END (MARKED)<[01] REMOVED CRACKED ANGLE.;[02] REMOVED AND REPLACED PER SRM 51-40-02.;[03] 02 - INSPECTED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION ANMar 11, 2025 · N8683D · Boeing 7378H4SDR SWAA2025041404294Support Beam · damagedR WING FIXED UPPER TRAILING EDGE PANEL SUPPORT BEAM AT WBL.198.6 HAS 2EA ELONGATED FASTENER HOLES.(MARKED)<[01] REMOVED DAMAGE FROM UPPER SUPPORT BEAM AND FOUND TO BE OUT-OF-LIMITS PER SRM 57-51-02-2R-1.;[02] VERIFIED WORK ACCOMPLISHED IN C/A #1;[03] REMOVED DMar 11, 2025 · N8683D · Boeing 7378H4SDR UATA2025031915701Stiffener · crackedCRACKED U CHANNEL IN AFT LH CENTER WING SECTION STATION 2380, AS FLAGGED. REPLACED CRACKED STIFFENER WITH NEW. SEE 337 DATED 03/11/2025 FOR FURTHER INFO. FAA FORM 337 STATES: FOUND CRACK IN STIFFENER ON THE LEFT CENTER WING AFT BEAM AT W.S. 2380. CRACKED STIFFMar 11, 2025 · N348CA · Casa C212CCSDR FDEA202503110361Stiffener · crackedLEFT WING UPPER FIXED TRAILING EDGE PANEL, WING STATION 1032, PANEL TRAILING EDGE SPANWISE VERTICAL "U" STIFFENER IS CRACKED ON INBOUND END AS MARKED. REMOVED AND REPLACED LEFT WING FIXED T.E. PANEL, W.S. 1032, PANEL T.E. SPANWISE VERTICAL "U" STIFFENER REMar 11, 2025 · N148FE · Boeing 7673S2FSDR VNAA202504140015Canister · crackedCRACKS 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 REO670-57-42-577. REV.--.Mar 9, 2025 · N597NN · Cndair CL6002D24SDR VNAA202504140013Canister · crackedCRACKS 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 REAPIARED PER REO670-57-42-577. REV.--Mar 9, 2025 · N597NN · Cndair CL6002D24SDR SWAA2025040203457Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED TRAILING EDGE IRSS213 AT LT WING 2025-186156<[01] REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE IRSS213 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG115A2001 SHEET 24 REV A MEASURE OF CRAK IS: 0.609.Mar 8, 2025 · N7821L · Boeing 7377CTSDR SWAA2025040203343Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING 2025-186146<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02. AND DWG 115A2001 SHEET 29 REV -. <BR>MEASURE OF CRACK L:Mar 8, 2025 · N7821L · Boeing 7377CTSDR SWAA2025033115240Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT LT WING 2025-186155<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02. AND DWG 115A2001 SHEET 29 REV -.<BR>MEASURE OF CRACK L: 0.346Mar 8, 2025 · N7821L · Boeing 7377CTSDR SWAA2025033115241Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED TRAILING EDGE IRSS213 AT LT WING 2025-186156<[01] REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE IRSS213 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG115A2001 SHEET 24 REV A MEASURE OF CRAK IS: 0.609 P/N: 500-19Mar 8, 2025 · N7821L · Boeing 7377CTSDR SWAA2025033115239Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING 2025-186146<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02. AND DWG 115A2001 SHEET 29 REV -. <BR>MEASURE OF CRACK L:Mar 8, 2025 · N7821L · Boeing 7377CTSDR SWIA20250418305Channel · crackedRH WING CHANNEL P/N 601R10203-28 IS CRACKED MX# 29743099 (C-CHECK RO 04/17/2025)REPAIRED RH WING BATT RIB WS53.6 PER REO 601R-57-51-046, REV. -B, DATE: 2002-02-28. COMPLIED WITH SKYWEST TAS CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.Mar 5, 2025 · N693BR · Cndair CL6002B19SDR SWAA2025040202339Angle · crackedCRACK ANGLE TRAILING EDGE AREA AT LEVEL ORSS 270 AT RT WING 2025-185961<[01] REPLACED ANGLE AND FASTENERS LOCATED TRAILING EDGE AREA AT LEVEL ORSS 270 AT RT WING IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G-0 AND DWG 115A2982 SHEET 4. REV -;[02] CORRECTED STEMar 5, 2025 · N7821L · Boeing 7377CTSDR SWAA2025033115201Angle · crackedCRACK ANGLE TRAILING EDGE AREA AT LEVEL ORSS 270 AT RT WING 2025-185961<[01] REPLACED ANGLE AND FASTENERS LOCATED TRAILING EDGE AREA AT LEVEL ORSS 270 AT RT WING IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G-0 AND DWG 115A2982 SHEET 4. REV -;[02] CORRECTED STEMar 5, 2025 · N7821L · Boeing 7377CTSDR IPXA2025032569716Channel · corrodedRIGHT WING OUTBOARD LEADING EDGE CAVITY INSIDE, LOWER CHANNEL CORROSION, OLES 1350-1400.REPAIRED DAMAGE AREA I.A.W. UPS EO-93164-REQ1 REV.1Mar 5, 2025 · N579UP · Boeing 74745ESDR SWAA2025040815098Angle · crackedCRACK ANGLE OUTBOARD AUXILIARY TRACK OF SLAT 7 AT TR WING 2025-171985<[01] REPLACED ANGLE LOCATED OUTBOARD AUXILIARY TRACK OF SLAT 7 AT RT WING IAW B737-800 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG 114A5020; SHEET 40; REV A.<BR><BR>SEE INDIVIDUAL SIGN-OFFMar 4, 2025 · N8614M · Boeing 7378H4SDR SWAA2025040702216Angle · crackedCRACK ANGLE OUTBOARD AUXILIARY TRACK OF SLAT 7 AT TR WING 2025-171985<[01] REPLACED ANGLE LOCATED OUTBOARD AUXILIARY TRACK OF SLAT 7 AT RT WING IAW B737-800 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG 114A5020; SHEET 40; REV A.<BR><BR>SEE INDIVIDUAL SIGN-OFFMar 4, 2025 · N8614M · Boeing 7378H4SDR SWAA2025040201734Panel · debondedPANEL 621ZB FWD. CORNER DISBONDED.<[01] PANEL 621ZB WITH FWD CORNER DISBONDED WAS REPAIRED IAW SRM 57-41-01-2R-6.;[02] VERIFIED CORRECTIVE ACTION 1.Mar 4, 2025 · N219WN · Boeing 7377H4SDR SWAA2025033114774Support Beam · wornR WING FIXED TRAILING EDGE PANEL SUPPORT BEAM AT WBL 198.6(ATTACHED TO DEFLECTION CONTROL RIB) HAS WORN FASTENER HOLES.(MARKED)<[01] WEAR DAMAGE ON RIGHT WING FIXED T/E UPPER SUPPORT BEAM IS OUT OF LIMITS PER SRM 53-51-02-1A-1. CUT AND REMOVED DAMAGE FROM THE Mar 4, 2025 · N8689C · Boeing 7378H4SDR IPXA2025032660374Angle · brokenRH/WING, DEFLECTOR PANEL 672GB, METAL FINGERS BROKEN DOT-010 DD5240. REPLACED ANGLE-CONDUCTOR AT RH WING, DEFLECTOR PANEL 672 GB IAW A300-600F SRM 51-40-21. GIVEN OK TO PERFORM BONDING TEST.Mar 4, 2025 · N121UP · Airbus A300F4622RSDR SWAA2025032602007Support Bracket · crackedR WING FIXED TRAILING EDGE PANEL INBD SUPPORT BRACKET AT WBL 183.4 HAS CRACK.(MARKED)<[01] REMOVED AND REPLACED R WING FIXED TRAILING EDGE PANEL INBD SUPPORT BRACKET (P/N 115A2156-18) AT WBL 183.4 IAW SRM 51-40-02.;[02] C/W INSPECTION<BR>REMOVED AND REPLACED RMar 4, 2025 · N8689C · Boeing 7378H4SDR SWAA2025032408832Plate · wornR WING FIXED TRAILING EDGE PANEL SUPPORT BEAM AT WBL 198.6(ATTACHED TO DEFLECTION CONTROL RIB) HAS WORN FASTENER HOLES.(MARKED)<[01] WEAR DAMAGE ON RIGHT WING FIXED T/E UPPER SUPPORT BEAM IS OUT OF LIMITS PER SRM 53-51-02-1A-1. CUT AND REMOVED DAMAGE FROM THE Mar 4, 2025 · N8689C · Boeing 7378H4SDR REXA2025031300313Support Plate · chafed"WEAR ON PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH WING TRAILING EDGE (ROOT WING). PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH WING TRAILING EDGE (ROOT WING) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42Mar 3, 2025 · N348PQ · Cndair CL6002D24SDR REXA2025031300310Support Plate · chafed"WEAR ON PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH WING TRAILING EDGE (ROOT WING). PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH WING TRAILING EDGE (ROOT WING) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42Mar 3, 2025 · N348PQ · Cndair CL6002D24SDR SWAA2025040815081Angle · crackedCRACK ANGLE ON AUXILIARY TRACK ON SLAT 1 AT LT WING 2025-171909<[01] REPLACED ANGLE LOCATED ON AUXILIARY TRACK ON SLAT 1 AT LT WING IAW B737-800 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG 114A5020; SHEET 40; REV A.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02]Mar 2, 2025 · N8614M · Boeing 7378H4SDR SWAA2025040815082Angle · crackedCRACK ANGLE ON AUXILIARY TRACK SLAT 8 AT RT WING 2025-171911<[01] REPLACED ANGLE LOCATED ON AUXILIARY TRACK SLAT 8 AT RT WING IAW B737-800 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG 114A5020; SHEET 40; REV A.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] JOB CMar 2, 2025 · N8614M · Boeing 7378H4SDR SWAA2025040701379Angle · crackedCRACK ANGLE ON AUXILIARY TRACK ON SLAT 1 AT LT WING 2025-171909<[01] REPLACED ANGLE LOCATED ON AUXILIARY TRACK ON SLAT 1 AT LT WING IAW B737-800 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG 114A5020; SHEET 40; REV A.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02]Mar 2, 2025 · N8614M · Boeing 7378H4SDR SWAA2025040701380Angle · crackedCRACK ANGLE ON AUXILIARY TRACK SLAT 8 AT RT WING 2025-171911<[01] REPLACED ANGLE LOCATED ON AUXILIARY TRACK SLAT 8 AT RT WING IAW B737-800 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG 114A5020; SHEET 40; REV A.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] JOB CMar 2, 2025 · N8614M · Boeing 7378H4SDR IPXA2025032321569Support Fitting · crackedCRACK - FITTING, INBD LOWER SIDE OF L/H WING NO.6 SPOILER MID SUPPORT FITTING (REPAIR). .REPAIR DAMAGE AREA I.A.W. SRM 57-51-13-2R-1 REV.62 AND EGAT WORK SHEET NO.50142. ACCOMPLISH THE REPAIR PER 747-400SF SRM 57-51-13-2R-1 REV.62.Mar 2, 2025 · N579UP · Boeing 74745ESDR SWAA2025040700752Web · crackedCRACK WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING 2025-167701<[01] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF Feb 28, 2025 · N287WN · Boeing 7377H4SDR SWAA2025040700751Support Angle · crackedCRACK SUPPORT ANGLE FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING 2025-167645<[01] REPLACED FITTING LOCATED FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEETFeb 28, 2025 · N287WN · Boeing 7377H4SDR SWAA2025040214210Web · crackedCRACK WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING 2025-167701<[01] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF Feb 28, 2025 · N287WN · Boeing 7377H4SDR IPXA2025032593475Support Beam · corrodedCORROSION - BEAM, L/H WING L/E LOWER PNL FWD SUPPORT BEAM INNER FACE, OLES 1425 (REPAIR). .REPAIR DAMAGE AREA I.A.W. UPS EO-93160-REQ1 REV.1. ALL PAPERWORK REVIEWED AND C/WFeb 28, 2025 · N579UP · Boeing 74745ESDR IXXA20250424006Web · gougedRH WING OTBD LE AREA BULL NOSE WEB EXISTING REPAIR IS GOUGED IN THE RADIUS AT APPROX LES 690. REF HAECO WO 320011 NR 34437Feb 27, 2025 · N229AZ · Boeing 767323SDR IXXA20250424004Web · crackedRH WING OTBD LE AREA BULL NOSE WEB EXISTING REPAIR IS CRACKED IN THE RADIUS AT APPROV LES 680. REF HAECO WO 320011 NR 34436Feb 27, 2025 · N229AZ · Boeing 767323SDR SWAA2025040214207Angle · crackedCRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2025-167634<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLFeb 27, 2025 · N287WN · Boeing 7377H4SDR SWAA2025040214206Angle · crackedCRACK ANGLE ON INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING 2025-167631<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OFFeb 27, 2025 · N287WN · Boeing 7377H4SDR AALA202503218630Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INBOARD AFT FLAP ANGLE LOCATED MID TRACK INBOARD SIDE AT RIGHT WING. REPLACED FLAP ANGLE. PER B777-200 SRM 51-40-02-0G AND DWG 113W2710.Feb 24, 2025 · N767AJ · Boeing 777223SDR AALA202503213876Support Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SUPPORT BRACKET AT INBOARD CENTER TRACK FITTING OF INBOARD AFT FLAP LEFT WING. REPLACED SUPPORT BRACKET. PER B777-200 SRM 51-40-02-0G DWG 113W2710.Feb 21, 2025 · N767AJ · Boeing 777223
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