# Service difficulty reports: N138EV

A list on [N138EV](https://openairdocs.org/aircraft/N138EV.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 186 reports

- [SDR REXA2026050600495](https://openairdocs.org/sdr/REXA2026050600495.md): Lamp · inoperative · May 5, 2026 · N138EV · Cndair CL6002D24 · Emergency Lighting
  > EXTERIOR SERVICE DOOR EMERGENCY LIGHT OUT. R/R EXTERIOR SERVICE DOOR EMERGENCY LIGHT BULB IN REFERENCE TO AMM 33-51-15. PN ON/OFF: 8GH002473-08
- [SDR REXA2026050700505](https://openairdocs.org/sdr/REXA2026050700505.md): Fairing · cracked · Apr 26, 2026 · N138EV · Cndair CL6002D24 · Engine Thrust Reverser
  > CRACK 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 54-12-01
- [SDR REXA2026050700525](https://openairdocs.org/sdr/REXA2026050700525.md): Landing · cracked · Apr 16, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK 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-A01
- [SDR REXA2026050700524](https://openairdocs.org/sdr/REXA2026050700524.md): Angle · corroded · Apr 10, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 S
- [SDR REXA2026050700523](https://openairdocs.org/sdr/REXA2026050700523.md): Angle · corroded · Apr 10, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 S
- [SDR REXA2026050700521](https://openairdocs.org/sdr/REXA2026050700521.md): Angle · corroded · Apr 10, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 S
- [SDR REXA2026050700520](https://openairdocs.org/sdr/REXA2026050700520.md): Angle · corroded · Apr 10, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 S
- [SDR REXA2026050700518](https://openairdocs.org/sdr/REXA2026050700518.md): Angle · corroded · Apr 10, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 CR
- [SDR REXA2026050700517](https://openairdocs.org/sdr/REXA2026050700517.md): Angle · corroded · Apr 10, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 LIMIT
- [SDR REXA2026050700516](https://openairdocs.org/sdr/REXA2026050700516.md): Plate · bent · Apr 9, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, Structure
  > WEAR 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-A01
- [SDR REXA2026050700515](https://openairdocs.org/sdr/REXA2026050700515.md): Support Angle · cracked · Apr 8, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK 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-A01
- [SDR REXA2026050700514](https://openairdocs.org/sdr/REXA2026050700514.md): Channel · corroded · Apr 7, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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. A
- [SDR REXA2026050700511](https://openairdocs.org/sdr/REXA2026050700511.md): Crossbeam · cracked · Mar 24, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, Structure
  > AFTER 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-
- [SDR REXA2026050700510](https://openairdocs.org/sdr/REXA2026050700510.md): Crossbeam · cracked · Mar 24, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, Structure
  > AFTER 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-
- [SDR REXA2026050700537](https://openairdocs.org/sdr/REXA2026050700537.md): Fitting · corroded · Mar 19, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON ATTACHMENT FITTING OF GALLEY 1 WAS FOUND. FITTING OF GALLEY 1 WAS REPLACED PER CRJ/900 SRM 51-42-21-001-001-A01
- [SDR REXA2026050700503](https://openairdocs.org/sdr/REXA2026050700503.md): Channel · damaged · Mar 19, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > ELONGATED 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-A01
- [SDR REXA2026050700536](https://openairdocs.org/sdr/REXA2026050700536.md): Floorbeam · corroded · Mar 18, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION 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-A01
- [SDR REXA2026050700535](https://openairdocs.org/sdr/REXA2026050700535.md): Fitting · corroded · Mar 18, 2026 · N138EV · Cndair CL6002D24 · Passenger/Crew Doors
  > AFTER 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 P
- [SDR REXA2026050700509](https://openairdocs.org/sdr/REXA2026050700509.md): Bracket · corroded · Mar 18, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER 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-
- [SDR REXA2026050700508](https://openairdocs.org/sdr/REXA2026050700508.md): Bracket · corroded · Mar 18, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER 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-
- [SDR REXA2026050700507](https://openairdocs.org/sdr/REXA2026050700507.md): Web · corroded · Mar 18, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER 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-
- [SDR REXA2026050700502](https://openairdocs.org/sdr/REXA2026050700502.md): Support Bracket · cracked · Mar 17, 2026 · N138EV · Cndair CL6002D24 · Trailing Edge Flaps
  > BROKEN 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.
- [SDR REXA2026050700534](https://openairdocs.org/sdr/REXA2026050700534.md): Seat Track · corroded · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 53-00-49
- [SDR REXA2026050700533](https://openairdocs.org/sdr/REXA2026050700533.md): Door Sill · corroded · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION 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 51-42-21-00
- [SDR REXA2026050700532](https://openairdocs.org/sdr/REXA2026050700532.md): Bracket · corroded · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "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-A
- [SDR REXA2026050700531](https://openairdocs.org/sdr/REXA2026050700531.md): Support · cracked · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK 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 O
- [SDR REXA2026050700530](https://openairdocs.org/sdr/REXA2026050700530.md): Support · cracked · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK 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 O
- [SDR REXA2026050700529](https://openairdocs.org/sdr/REXA2026050700529.md): Angle · cracked · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK 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 O
- [SDR REXA2026050700527](https://openairdocs.org/sdr/REXA2026050700527.md): Support · cracked · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK 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.
- [SDR REXA2026050700526](https://openairdocs.org/sdr/REXA2026050700526.md): Fitting · corroded · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR REXA2026050700512](https://openairdocs.org/sdr/REXA2026050700512.md): Rib · cracked · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON RIB LEADING EDGE SS57.16 RIB LEADING EDGE SS57.16 WAS REPAIRED PER REO 690-57-41-240 REV - -
- [SDR REXA2026050700506](https://openairdocs.org/sdr/REXA2026050700506.md): Floorbeam · cracked · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACK 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-A01
- [SDR REXA2026050700501](https://openairdocs.org/sdr/REXA2026050700501.md): Hinge · corroded · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Landing Gear Doors
  > CORROSION 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-
- [SDR REXA2026050700500](https://openairdocs.org/sdr/REXA2026050700500.md): Fitting · corroded · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Landing Gear Doors
  > CORROSION 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-
- [SDR REXA2026050700499](https://openairdocs.org/sdr/REXA2026050700499.md): Fitting · corroded · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Fuselage, Landing Gear Attach Fittings
  > CORROSION 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-
- [SDR REXA2026050700498](https://openairdocs.org/sdr/REXA2026050700498.md): Fitting · corroded · Mar 15, 2026 · N138EV · Cndair CL6002D24 · Landing Gear Doors
  > CORROSION 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 5
- [SDR REXA2026050700528](https://openairdocs.org/sdr/REXA2026050700528.md): Protector · cracked · Mar 13, 2026 · N138EV · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACK 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:IR
- [SDR REXA2026050700519](https://openairdocs.org/sdr/REXA2026050700519.md): Drag Angle · cracked · Mar 12, 2026 · N138EV · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK 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- 001
- [SDR REXA2026050700504](https://openairdocs.org/sdr/REXA2026050700504.md): Drag Angle · cracked · Mar 12, 2026 · N138EV · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK 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-A
- [SDR REXA2026050700497](https://openairdocs.org/sdr/REXA2026050700497.md): Drag Angle · cracked · Mar 12, 2026 · N138EV · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK 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- 0
- [SDR REXA2026012100018](https://openairdocs.org/sdr/REXA2026012100018.md): Bulb · burned out · Jan 17, 2026 · N138EV · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY FLOOD LIGHT AT PAX DOOR HAS BULB BURNT OUT R/R BULB OPC GOOD IAW CRJ900 AMM 33-51-00
- [SDR REXA2025042200450](https://openairdocs.org/sdr/REXA2025042200450.md): Unknown · odor · Apr 16, 2025 · N138EV · Cndair CL6002D24 · Air Distribution System
  > ON 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.
- [SDR REXA2025022500223](https://openairdocs.org/sdr/REXA2025022500223.md): Light · inoperative · Feb 19, 2025 · N138EV · Cndair CL6002D24 · Emergency Lighting
  > LH 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:GLSB364
- [SDR REXA2025010900028](https://openairdocs.org/sdr/REXA2025010900028.md): Lug · cracked · Dec 10, 2024 · N138EV · Cndair CL6002D24 · Emergency Exits
  > RH AFT EMERGENCY EXIT AFT LUG CRACKED COMPLIED WITH ENDEAVOR EA CRJ952-17961 REV IR 12/23/2024.
- [SDR REXA2025010900027](https://openairdocs.org/sdr/REXA2025010900027.md): Lug · cracked · Dec 10, 2024 · N138EV · Cndair CL6002D24 · Emergency Exits
  > LH FWD EMERGENCY EXIT AFT LUG CRACKED COMPLIED WITH ENDEAVOR EA CRJ952-17960 REV IR 12/17/2024
- [SDR REXA2025010900026](https://openairdocs.org/sdr/REXA2025010900026.md): Lug · cracked · Dec 10, 2024 · N138EV · Cndair CL6002D24 · Emergency Exits
  > LH AFT EMERGENCY EXIT AFT LUG CRACKED COMPLIED WITH ENDEAVOR EA CRJ952-17972 REV IR 12/23/24
- [SDR REXA2024122401609](https://openairdocs.org/sdr/REXA2024122401609.md): Vent Line · corroded · Dec 10, 2024 · N138EV · Cndair CL6002D24 · Fuel Storage
  > R/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.
- [SDR REXA2022090101998](https://openairdocs.org/sdr/REXA2022090101998.md): Seat Track · none · Aug 30, 2022 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SEAT TRACK SCRATCHED AND PITTED FROM APPROX. FS581-693 LBL27 REPLACED.
- [SDR REXA2022091302058](https://openairdocs.org/sdr/REXA2022091302058.md): Cover · cracked · Aug 24, 2022 · N138EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT CORNER HAS A CRACK@1 EA FASTENER HOLE REPLACED CORNER COVER
- [SDR REXA2022090102002](https://openairdocs.org/sdr/REXA2022090102002.md): Angle · cracked · Aug 24, 2022 · N138EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE IS CRACKED REPLACED ANGLE

Next page: https://openairdocs.org/aircraft/N138EV/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N138EV/reports

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