N138EV

Service difficulty reports · 186

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N138EV' AND registry_match = 'registration'
  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 REXA2026050600495Lamp · inoperativeEXTERIOR SERVICE DOOR EMERGENCY LIGHT OUT. R/R EXTERIOR SERVICE DOOR EMERGENCY LIGHT BULB IN REFERENCE TO AMM 33-51-15. PN ON/OFF: 8GH002473-08May 5, 2026 · N138EV · Cndair CL6002D24 · Emergency LightingSDR REXA2026050700505Fairing · crackedCRACK ON LINE LOWER FAIRING BTW LOWER TRANSCOWL AND PYLON AT LH ENGINE LINE LOWER FAIRING BTW LOWER TRANSCOWL AND PYLON AT LH ENGINE WAS FABRICATED AND REPLACED PER EA NO. CRJ954-22055 REV.A AND CRJ-900 AMM 54-12-01Apr 26, 2026 · N138EV · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2026050700525Landing · crackedCRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCES DOOR 212AR. RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCES DOOR 212AR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01Apr 16, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026050700524Angle · corrodedCORROSION ON ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 SApr 10, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700523Angle · corrodedCORROSION ON ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 SApr 10, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700521Angle · corrodedCORROSION ON ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 SApr 10, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700520Angle · corrodedCORROSION ON ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 SApr 10, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700518Angle · corrodedCORROSION ON LOWER SILL ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. CORROSION ON LOWER SILL ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR WAS REMOVED PER SRM 51-21-06-001-001-A01 EVALUATED OUT OF LIMITS PER CRApr 10, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700517Angle · corrodedCORROSION ON LOWER SILL ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. CORROSION ON LOWER SILL ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 EVALUATED OUT OF LIMITApr 10, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700516Plate · bentWEAR AND BENT IN LOWER PLATE AND SEAL RETAINER OF FWD/CTR BAGGAGE-BAY CARGO DOOR LOWER PLATE (2 EA) ON FWD/CTR BAGGAGE-BAY CARGO DOOR WERE REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01Apr 9, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026050700515Support Angle · crackedCRACK ON SUPPORT ANGLE OF COMMUNICATION/SERVICE PANEL BOX AT FWD FUSELAGE SUPPORT ANGLE OF COMMUNICATION/SERVICE PANEL BOX AT FWD FUSELAGE WAS FABRICATED AND INSTALLED PER EA CRJ953-21779 REV. IR AND SRM 51-42-06-001-001-A01Apr 8, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700514Channel · corrodedCORROSION ON INTERNAL CHANNEL AT AREA OF AFT DRAIN MAST (FS1031.00 TO FS 1051.30 BTW STGR 27 TO 26RH) INTERNAL CHANNEL AT AREA OF AFT DRAIN MAST (FS1031.00 TO FS 1051.30 BTW STGR 27 TO 26RH) WAS REPAIRED PER EA NO: CRJ953-21943 REV. AApr 7, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700511Crossbeam · crackedAFTER RH CROSSBEAM REMOVAL, CRACK ON ANGLE RBL26.00 & LBL26.00 FS280.00 WAS FOUND AT FWD FACE OF THE BULKHEAD FS280.00, BELOW FLOOR ANGLE RBL26.00 & LBL26.00 FS280.00 AT FWD FACE OF THE BULKHEAD FS280.00, BELOW FLOOR WERE REPLACED PER CRJ900 SRM 51-42-06-001-Mar 24, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026050700510Crossbeam · crackedAFTER RH CROSSBEAM REMOVAL, CRACK ON ANGLE RBL26.00 & LBL26.00 FS280.00 WAS FOUND AT FWD FACE OF THE BULKHEAD FS280.00, BELOW FLOOR ANGLE RBL26.00 & LBL26.00 FS280.00 AT FWD FACE OF THE BULKHEAD FS280.00, BELOW FLOOR WERE REPLACED PER CRJ900 SRM 51-42-06-001-Mar 24, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026050700537Fitting · corrodedCORROSION ON ATTACHMENT FITTING OF GALLEY 1 WAS FOUND. FITTING OF GALLEY 1 WAS REPLACED PER CRJ/900 SRM 51-42-21-001-001-A01Mar 19, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700503Channel · damagedELONGATED HOLE ON UP CHANNEL AT LH MLG WHEEL WELL UP CHANNEL AT LH MLG WHEEL WELL WAS REPLACED PER CRJ 900 SRM 51-41-21-001-001-A01Mar 19, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700536Floorbeam · corrodedCORROSION ON CROSSBEAM LH AT FS 280.00 CROSSBEAM LH AT FS 280.00 WAS REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01Mar 18, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026050700535Fitting · corrodedAFTER DISCONNECT FWD HANDRAIL ACTUATOR ROD, CORROSION ON FWD FITTING WAS FOUND AT SURROUND STRUCTURE OF PASSENGER DOOR. FWD FITTING AT SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02, FITTING P/N SH670-31905-5 WAS VERIFIED PMar 18, 2026 · N138EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026050700509Bracket · corrodedAFTER LOWER SIL REMOVAL, CORROSION ON PROTECTOR WEB FLOOR 4(EAS) WAS FOUND. PROTECTOR WEB FLOOR 1(EA) WAS CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND 3(EAS) WERE EVALUATED DUE TO EXCESIVE CORROSION, THEREFORE MUST BE REPLACE PER CRJ-900 SRM 53-00-00-101-Mar 18, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700508Bracket · corrodedAFTER LOWER SIL REMOVAL, CORROSION ON PROTECTOR WEB FLOOR 4(EAS) WAS FOUND. PROTECTOR WEB FLOOR 1(EA) WAS CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND 3(EAS) WERE EVALUATED DUE TO EXCESIVE CORROSION, THEREFORE MUST BE REPLACE PER CRJ-900 SRM 53-00-00-101-Mar 18, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700507Web · corrodedAFTER LOWER SIL REMOVAL, CORROSION ON PROTECTOR WEB FLOOR 4(EAS) WAS FOUND. PROTECTOR WEB FLOOR 1(EA) WAS CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND 3(EAS) WERE EVALUATED DUE TO EXCESIVE CORROSION, THEREFORE MUST BE REPLACE PER CRJ-900 SRM 53-00-00-101-Mar 18, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700502Support Bracket · crackedBROKEN SUPPORT BRACKET OF BONDING JUMPER AT FLAP MECHANISM. SUPPORT BRACKET OF BONDING JUMPER AT FLAP MECHANISM WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 & EA CRJ957-22035 REV. IR.Mar 17, 2026 · N138EV · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2026050700534Seat Track · corrodedCORROSION ON RH SEAT TRACK RBL9 BTW FS349 TO FS394 AT PAX CABIN FLOOR STRUCTURE RH SEAT RAIL RBL9 BTW FS349 TO FS394 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER CRJ900 AMM 53-00-49Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026050700533Door Sill · corrodedCORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH. AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-00Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026050700532Bracket · corroded"STUCK PRESS-TO-TEST INDICATOR LIGHT, CORROSION AT SUPPORT & CLIP OF AFT WASTE TANK (BTW STGR 24RH AND STGR 23RH, FS 959.00). (SM)"" AFT LAV WASTE LEVEL INDICATOR AND NEW BRACKET WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ-900 AMM 38-31-08-960-801-AMar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700531Support · crackedCRACK ON BIN SUPPORT MEMBRANES (2E/A) ON LBL34 AND RBL34 AT FWD FACE OF MLG WHEEL WELL. & CRACK ON ANGLE OF FAIRING SUPPORT 194AB ON BL0 AT MMLG WHEEL WELL. (3 EAS TOTAL). BIN SUPPORT MEMBRANES (2E/A) ON LBL34 AND RBL34 AT FWD FACE OF MLG WHEEL WELL. & ANGLE OMar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700530Support · crackedCRACK ON BIN SUPPORT MEMBRANES (2E/A) ON LBL34 AND RBL34 AT FWD FACE OF MLG WHEEL WELL. & CRACK ON ANGLE OF FAIRING SUPPORT 194AB ON BL0 AT MMLG WHEEL WELL. (3 EAS TOTAL). BIN SUPPORT MEMBRANES (2E/A) ON LBL34 AND RBL34 AT FWD FACE OF MLG WHEEL WELL. & ANGLE OMar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700529Angle · crackedCRACK ON BIN SUPPORT MEMBRANES (2E/A) ON LBL34 AND RBL34 AT FWD FACE OF MLG WHEEL WELL. & CRACK ON ANGLE OF FAIRING SUPPORT 194AB ON BL0 AT MMLG WHEEL WELL. (3 EAS TOTAL). BIN SUPPORT MEMBRANES (2E/A) ON LBL34 AND RBL34 AT FWD FACE OF MLG WHEEL WELL. & ANGLE OMar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700527Support · crackedCRACK ON ALL CORNERS ON SUPPORT OF JB6 AT FWD ACCESORY COMPARMENT. SUPPORT OF JB6 AT FWD ACCESORY COMPARMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700526Fitting · corrodedCORROSION AT SPLICE DOUBLER, GALLEY SERVICE DOOR SURROUND STRUCTURE FS319.70 STGR 17. SPLICE DOUBLER ON GALLEY SERVICE DOOR SURROUND STRUCTURE FS319.70 STGR 17 WAS REPLACED PER SRM 51-42-21-001-001-A01.Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050700512Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 RIB LEADING EDGE SS57.16 WAS REPAIRED PER REO 690-57-41-240 REV - -Mar 15, 2026 · N138EV · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026050700506Floorbeam · crackedCRACK RH FS 280.00 BEAM. RH FS 280.00 BEAM WAS REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026050700501Hinge · corrodedCORROSION WAS FOUND ON FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS) WERE REPLACED PER SRM 51-42-21-001-001-A01 & SRM 51-41-04-Mar 15, 2026 · N138EV · Cndair CL6002D24 · Landing Gear DoorsSDR REXA2026050700500Fitting · corrodedCORROSION WAS FOUND ON FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS) WERE REPLACED PER SRM 51-42-21-001-001-A01 & SRM 51-41-04-Mar 15, 2026 · N138EV · Cndair CL6002D24 · Landing Gear DoorsSDR REXA2026050700499Fitting · corrodedCORROSION WAS FOUND ON FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS) WERE REPLACED PER CRJ900 SRM 51-42-Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage, Landing Gear Attach FittingsSDR REXA2026050700498Fitting · corrodedCORROSION WAS FOUND ON FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS) WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 & SRM 5Mar 15, 2026 · N138EV · Cndair CL6002D24 · Landing Gear DoorsSDR REXA2026050700528Protector · crackedCRACK ON HARNESS PROTECTOR AT FWD HINGE ARM OF FWD BAGGAGE BAY CARGO DOOR. FORWARD BAGGAGE-BAY DOOR HARNESS PROTECTOR WAS REPAIRED PER EA: CRJ952-21867 REV:IRMar 13, 2026 · N138EV · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026050700519Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. COMPLETE: LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM WAS REPAIRED PER SRM 55-31-00-201- 001Mar 12, 2026 · N138EV · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026050700504Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201- 001-AMar 12, 2026 · N138EV · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026050700497Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201- 0Mar 12, 2026 · N138EV · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026012100018Bulb · burned outEMERGENCY FLOOD LIGHT AT PAX DOOR HAS BULB BURNT OUT R/R BULB OPC GOOD IAW CRJ900 AMM 33-51-00Jan 17, 2026 · N138EV · Cndair CL6002D24 · Emergency LightingSDR REXA2025042200450Unknown · odorON TAKE OFF, SMOKE/ODOR IN COCKPIT & CABIN, EMERGENCY DECLARED, NO FIRE INDICATIONS, GO AROUND, RETURNED TO RDU. PERFORMED DRYOUT PROCEDURES IAW CRJ-900 AMM 72-00-00. SMELL EVENTUALLY WAS REMOVED FROM AC. NO FURTHER ANOMALIES NOTED.Apr 16, 2025 · N138EV · Cndair CL6002D24 · Air Distribution SystemSDR REXA2025022500223Light · inoperativeLH AFT OVERWING EMERGENCY LIGHT OUT. R & R AT OVERWING EMERGENCY LIGHT HOUSING/BULB IAW AMM 33-51-15 OPS CHEC K GOOD. PNON/OFF:2LA006954-00 SNON:PT318617 SNOFF:GLSB364Feb 19, 2025 · N138EV · Cndair CL6002D24 · Emergency LightingSDR REXA2025010900028Lug · crackedRH AFT EMERGENCY EXIT AFT LUG CRACKED COMPLIED WITH ENDEAVOR EA CRJ952-17961 REV IR 12/23/2024.Dec 10, 2024 · N138EV · Cndair CL6002D24 · Emergency ExitsSDR REXA2025010900027Lug · crackedLH FWD EMERGENCY EXIT AFT LUG CRACKED COMPLIED WITH ENDEAVOR EA CRJ952-17960 REV IR 12/17/2024Dec 10, 2024 · N138EV · Cndair CL6002D24 · Emergency ExitsSDR REXA2025010900026Lug · crackedLH AFT EMERGENCY EXIT AFT LUG CRACKED COMPLIED WITH ENDEAVOR EA CRJ952-17972 REV IR 12/23/24Dec 10, 2024 · N138EV · Cndair CL6002D24 · Emergency ExitsSDR REXA2024122401609Vent Line · corrodedR/H I/B FWD MAIN FUEL VENT TUBE HAS SPOTS OF CORROSION COMPLIED WITH ENDEAVOR AIR EA CRJ928-17903 REV IR DATED 12/14/2024. DTA FOR 6000FH UNTIL PERMANENT REPAIR.Dec 10, 2024 · N138EV · Cndair CL6002D24 · Fuel StorageSDR REXA2022090101998Seat Track · noneSEAT TRACK SCRATCHED AND PITTED FROM APPROX. FS581-693 LBL27 REPLACED.Aug 30, 2022 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022091302058Cover · crackedPAX DOOR AFT CORNER HAS A CRACK@1 EA FASTENER HOLE REPLACED CORNER COVERAug 24, 2022 · N138EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022090102002Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED REPLACED ANGLEAug 24, 2022 · N138EV · Cndair CL6002D24 · Passenger/Crew Doors
Back to N138EV