# Service difficulty reports: N981EV

A list on [N981EV](https://openairdocs.org/aircraft/N981EV.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 3 · 145 reports

- [SDR REXA2021111501013](https://openairdocs.org/sdr/REXA2021111501013.md): Longeron · cracked · Nov 13, 2021 · N981EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > "DURING COMPLIANCE OF TASK CARD CRJ200 53-160-615 (DETAILED INSPECTION OF THE LONGERON AT FS424, A CRACK WAS FOUND ON THE IB FLANGE OF THE RH LONGERON, 4"" FWD OF FS424.0. THE CRACK EXTENDS FROM THE TOP FASTENER USED FOR ATTACHING THE REINFORCING ANGLE (ITEM
- [SDR REXA2021111000942](https://openairdocs.org/sdr/REXA2021111000942.md): None · none · Nov 1, 2021 · N981EV · Cndair CL6002B19 · Cabin Pressure Control System
  > DURING DECENT INTO CRW APPROX. FL220, CREW STATED HEARING LOUD AIR NOISE FROM THE CABIN AREA. FLIGHT ATTENDANT ALSO REPORTED NOISE TO FLIGHT CREW. CREW PERFORMED EMERGENCY DECENT AND MANUALLY DEPLOYED CABIN O2 MASKS. CABIN ALTITUDE NEVER EXCEEDED 6000FT. EMERG
- [SDR REXA2020040100418](https://openairdocs.org/sdr/REXA2020040100418.md): Light · inoperative · Mar 29, 2020 · N981EV · Cndair CL6002B19 · Emergency Lighting
  > RH OVERWING EMERGENCY EXIT LIGHT AT FLOOR LEVEL INOP REPLACED RH OVERWING EMERGENCY EXIT LIGHT PN 6020-5 AT FLOOR LEVEL IAW CRJ-200 AMM 33-51-10. EMERGENCY LIGHTS OPS CHECKS GOOD IAW CRJ-200 AMM 33-51-10.
- [SDR REXA2020021030187](https://openairdocs.org/sdr/REXA2020021030187.md): Battery Pack · inoperative · Feb 3, 2020 · N981EV · Cndair CL6002B19 · Emergency Lighting
  > DURING MORNING WAKE UP FOUND EMERGENCY EXIT SIGN IN MID CABIN FACING FORWARD INOP R&R EMRGENCY LIGH BATTERY PACK #2 IAW AMM 33-51-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR REXA201906274981](https://openairdocs.org/sdr/REXA201906274981.md): Bulkhead Web · dented · Jun 24, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 REAR PRESSURE BULKHEAD WEB FWD FACE HAS 2 TOOLING MARKS.1"" ROUND BY.002 DEEP AT LBL 42 AND RBL 42 WL76. REPAIRED AREA IAW REO 601R-53-61-7003 AND GREO 601R-53-61-2155.
- [SDR REXA2019062720985](https://openairdocs.org/sdr/REXA2019062720985.md): Wire · broken · Jun 22, 2019 · N981EV · Cndair CL6002B19 · Light System Wiring
  > WIRE BROKEN FOR WARDROBE EMERGENCY LIGHT. INSTALLED SERVICEABLE CONTACT ON WARDROBE EMERGENCY LIGHT AND INSTALLED CONTACT IN SPLICE CONNECTOR IAW CRJ 200 ESPM 20-17-10 OPS CHECK GOOD IAW CRJ 200 AMM 33-51-00-710-801.
- [SDR REXA2019062720960](https://openairdocs.org/sdr/REXA2019062720960.md): Floor Support · corroded · Jun 22, 2019 · N981EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MULTIPLE CORR BETWEEN FS 513 TO FS 544 OB FLOOR BOARD FLABGE RBL9. REPAIRED CORROSION DAMAGE ON RBL 9 BETWEEN FS 513 AND FS 544 IAW BOMBARDIER REO 601R-53-41-2495 REV IR DATED 2019-06-19 OB FLOOR BOARD FLANGE.
- [SDR REXA2019062720959](https://openairdocs.org/sdr/REXA2019062720959.md): Floor Support · corroded · Jun 22, 2019 · N981EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MULTIPLE CORROSION BETWEEN FS 529.00 TO 544 BETWEEN 2 PREVIOUS REPAIRS IB FLOOR BOARD FLANGE RBL 9. REPAIRED CORROSION BETWEEN FS 529 TO 544 IAW REO 601R-53-41-2495 REV IR DATED 2019-06-19 AND SRM 53-41-43, 53-00-00 INBD FLOOR BOARD FLANGE CONTINUED ON CO 77
- [SDR REXA2019062720958](https://openairdocs.org/sdr/REXA2019062720958.md): Floor Support · corroded · Jun 22, 2019 · N981EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MULTIPLE CORR BETWEEN FS 449.85 TO 473.15 IB FLOOR BOARD FLANGE RBL 9. FOUND CORROSION OUT OF LIMITS IAW REO 601R-53-00-005. REPAIRED AREA BTW FS 449.85 TO 473.15 IB FLOOR BOARD FLANGE RBL 9 IAW REO 6010R-53-41-2498 REV IR DATED 2019-06-20 MOERSCH, DANIEL 71
- [SDR REXA2019062720949](https://openairdocs.org/sdr/REXA2019062720949.md): Skin · dented · Jun 22, 2019 · N981EV · Cndair CL6002B19 · Trailing Edge Flaps
  > LH OB FLAP BOTTOM SKIN DENTED BETWEEN WS 280.66 AND FS 273 APPROX 6"" WIDE BY 4"" HIGH BY.050 DEEP. REPAIRED LH OB FLAP LOWER SKIN IAW ENDEAVOR EA 257-09206.
- [SDR REXA2019062780967](https://openairdocs.org/sdr/REXA2019062780967.md): Frame · corroded · Jun 18, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 333 IS CORRODED AT STR 22R. REMOVED AND REPLACED FS 333 FRAME SECTOR BETWEEN STR 18 AND 23R IAW CRJ 200 SRM 51-42-06 AND 51-42-21
- [SDR REXA2019062740948](https://openairdocs.org/sdr/REXA2019062740948.md): Frame · corroded · Jun 14, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 574.00 FRAME CORRODED ON FWD SIDE BETWEEN STRINGER 25L AND 25R. REPLACED FS 574 LOWER FRAME SECTION P/N 601R36024-61 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-40-11 TR#51-42
- [SDR REXA2019062740947](https://openairdocs.org/sdr/REXA2019062740947.md): Frame · corroded · Jun 14, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 589 FRAME CORRODED ON FWD AND AFT SIDES BETWEEN STRINGERS 22L AND 23R. REPLACED FS 589 FRAME IAW SRM 51-42-21, 51-42-06,51-40-11 TR 51-42 51-23-00, 51-21-16, 51-25-00, AND 51-21-11
- [SDR REXA2019062710971](https://openairdocs.org/sdr/REXA2019062710971.md): Plate · corroded · Jun 11, 2019 · N981EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WARDROBE AFT INBD AND OB MOUNT BOLT PLATES CORRODED AT FS 310 LBL 18 AND LBL 36. REMOVED AND REPLACED WARDROBE AFT IB AND OB MOUNT BOLT PLATES IAW SRM 51-42, 51-42-06, AND 51-42-13.
- [SDR REXA2019062780970](https://openairdocs.org/sdr/REXA2019062780970.md): Vertical Beam · cracked · Jun 8, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Structure
  > FS409.00 + 128 VERTICAL BEAM AT LBL27 SHOWS VISUAL SIGNS OF A CRACK OF A CRACK ON INBD BOTTOM SIDE. THIS ENTRY ICLUDES WORK CONTINUATION CARD JOB 87768111 OP312 REPAIRED LBL27 POST AT FS409+128 IAW BOMBARDIER GREO 601R53-41-056. WVAC EMP STAMP 769
- [SDR REXA2019062780957](https://openairdocs.org/sdr/REXA2019062780957.md): Bulkhead Web · cracked · Jun 8, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL0 WL112 4 INCHES LONG 100% FSH FAILED NDT INSPECTION. INCLUDES WORK CONTINUATION CARD JOB 877681115 OP70 REPAIRED BULKHEAD IAW BOMBARDIOER GREO 601R-53-61-1285. WVAC EMP STAMP 769
- [SDR REXA2019062740976](https://openairdocs.org/sdr/REXA2019062740976.md): Floorbeam · cracked · Jun 4, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RH FS460 FLOOR SUPPORT FITTING CRACKED AT OUTBOARD SIDE OF RBL9. REMOVED AND REPLACED FS480 FLOOR FITTING ON OUTBOARD SIDE OF RBL9 IAW SRM 51-42-21.
- [SDR REXA2019062740973](https://openairdocs.org/sdr/REXA2019062740973.md): Support Angle · corroded · Jun 4, 2019 · N981EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL ANGLE SUPPORT ANGLE CORRODED AT FS319. REPLACED ANGLE IAW SRM 51-42-06 AND 51-42-21.
- [SDR REXA2019062710963](https://openairdocs.org/sdr/REXA2019062710963.md): Floor Support · corroded · May 31, 2019 · N981EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MULTIPLE CORR BETWEEN FS 424 TO FS 439 OUTBD FLOOR BOARD FLANGE RBL9. FOUND CORROSION OUT OF LIMITS IAW REO 601R-53-00-005. REPAIRED AREA BETWEEN FS 424 TO FS 439 O/B FLOOR BOARD FLANGE RBL9 IAW REO 601R-53-41-2499 REV -- DATED 2019-06-20.
- [SDR REXA2019062710951](https://openairdocs.org/sdr/REXA2019062710951.md): Floor Support · corroded · May 31, 2019 · N981EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MULTIPLE CORR BETWEEN FS 409+128 TO FS 439 LBL9 INBD FLOOR BOARD FLANGE. FOUND CORROSION OUT OF LIMITS IAW REO 601R-53-00-005. REPAIRED CORROSION IAW REO 601R-53-41-2490 REV--.
- [SDR REXA2019062700952](https://openairdocs.org/sdr/REXA2019062700952.md): Floor Support · corroded · May 30, 2019 · N981EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION AT BS 424 TO 439, LBL9 OUTBD FLOOR SUPPORT. FOUND DAMAGE OUT OF LIMITS IAW REO 601R-53-00-005. REPAIRED AREA IAW REO 601R-53-41-2490 REV--.
- [SDR REXA2019062790978](https://openairdocs.org/sdr/REXA2019062790978.md): Strap · corroded · May 29, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RH F.S. 559 FLOOR SUPPORT STRAP CORRODED BETWEEN RBL27 AND RBL 42. LOCATED AND DRILLED NEW SERVICEABLE STRAP P/N 601R31025-29 IAW SRM 51-40-11, INSTALLED NEW SERVICEABLE STRAP IAW SRM 51-42-06 AND SRM 51-42-13
- [SDR REXA2019052900944](https://openairdocs.org/sdr/REXA2019052900944.md): Cargo Track · corroded · May 29, 2019 · N981EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO COMPARTMENT BAGGAGE RAIL CORRODED BETWEEN FS 605 AND FS 621 LBL 9.0. REMOVED AND REPLACED WITH SERVICEABLE TRACK P/N 601R31032-51 IAW CRJ 200 AMM 53-00-49-400-801 & 53-00-49-000-801. REMOVED TAPE.WVAC 712
- [SDR REXA2019062760977](https://openairdocs.org/sdr/REXA2019062760977.md): Floorbeam · cracked · May 26, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LH FS 484.00 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED AT LBL 27. REMOVED AND REPLACED LH FS 484.00 INTERCOSTAL ANGLE AT LBL 27 IAW CRJ200 SRM 51-42-21. REMOVED TAPE. WVAC 712.
- [SDR REXA2019062760975](https://openairdocs.org/sdr/REXA2019062760975.md): Floor Support · cracked · May 26, 2019 · N981EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH FS 484.00 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED AT RBL 27. REMOVED AND REPLACED RH FS 484.00 INTERCOSTAL ANGLE AT RBL 27 SRM 51-42-21.
- [SDR REXA2019062760969](https://openairdocs.org/sdr/REXA2019062760969.md): Stringer · cracked · May 26, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L CRACKED AT F.S. 379. REPAIRED STRINGER 3L IAW EA 253-09203.
- [SDR REXA2019062760968](https://openairdocs.org/sdr/REXA2019062760968.md): Attach Angle · cracked · May 26, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > STRINGER 3L UPPER ATTACH ANGLE CRACKED JUST AFT OF FS 280 BULKHEAD. REMOVED AND REPLACED STRINGER 3L CRACKED ATTACH ANGLE JUST AFT OF FS 280 BULKHEAD WITH NEW SERVICEABLE ATTACH ANGLE PN 600-31057-19 IAW CRJ 200 SRM 51-42-06 AND 51-40-11 TR 51-42
- [SDR REXA2019052760950](https://openairdocs.org/sdr/REXA2019052760950.md): Bracket · corroded · May 26, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CORRODED CLIP ON INTERCOSTAL BETWEEN FS 319-FS333 AT STR 23. INSTALLED A NEW BRACKET IAW SRM 51-42-06 AND SNIEO 601R44010-501.
- [SDR REXA2019062750974](https://openairdocs.org/sdr/REXA2019062750974.md): Floor Support · corroded · May 25, 2019 · N981EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL HAS CORROSION UNDER AFT END OF SILL, FS 319, RBL 42. REMOVED AND REINSTALLED NEW PLATE ASSY#601R31148-79 TO RBL 42-FS 319 IAW SRM 51-42-21 AND SRM 51-42-06.
- [SDR REXA2019062750972](https://openairdocs.org/sdr/REXA2019062750972.md): Frame · corroded · May 25, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Frame
  > CARGO BAY FS605 FRAME CORRODED FROM STRINGER 23R TO STRINGER 21R. REFERENCE CONTINUATION CARD 87768111 OP 304. REMOVED, LOCATED DRILLED AND INSTALLED NEW SERVICEABLE FS 605 LWR FRAME SEGMENT IAW CRJ 200 SRM 51-42-06, 51-42-21,51-40-11,51-12-16,51-25-00 AND 51
- [SDR REXA2019062750966](https://openairdocs.org/sdr/REXA2019062750966.md): Frame · cracked · May 25, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Frame
  > F.S.333 FRAME CRACKED ABOVE PAX DOOR CUT OUT BETWEEN STRINGER 0 AND 1L1.MARKED WITH TAPE.2. REMOVED CRACKED FS 333 FRAME ABOVE PAX DOOR CUT OUT IAW CRJ200 SRM 51-42-06 & 51-42-21.3NOT USED. 4)PAINT, SEALANT,AND CIC REQUIRED5)DISPLACED WIRE BUNDLE FROM JB1 TO F
- [SDR REXA2019062750965](https://openairdocs.org/sdr/REXA2019062750965.md): Floorbeam · cracked · May 25, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FLOOR SUPPORT BEAM PREVIOUS REPAIR CLIPS CRACKED INBD AND OB. LOCATED, DRILLED, AND INSTALLED I/B AND O/B FS 280.00 CLIPS PN 601R3113-57 AT LBL 9.0 IAW CRJ 200 SRM 51-42-21, 51-40-11, TR 51-42 AND RE-MOVED TAPE. WVAC 712
- [SDR REXA2019062750964](https://openairdocs.org/sdr/REXA2019062750964.md): Floorbeam · cracked · May 25, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 280 BEAM UPPER J-ANGLE CRACKED APPROX. 4""LONG OUTBD OF LBL9. REPAIRED FS 280 BEAM UPPER J-ANGLE AT LBL 9 IAW BOMBARDIER REO 601R-5311-138 REV A DATED 2010-11-10.
- [SDR REXA2019052750946](https://openairdocs.org/sdr/REXA2019052750946.md): Floorbeam · cracked · May 25, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 BEAM UPPER J-ANGLE PREVIOUS REPAIR ANGLE CRACKED OUTBD OF RBL 9. INSTALLED NEW ANGLE P/N 601R-53-137-6 AT FS 280 IAW CRJ 200 SRM 51-42-06.WVAC 769
- [SDR REXA2019062730984](https://openairdocs.org/sdr/REXA2019062730984.md): Fitting · cracked · May 23, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CO-PILOT WINDSHIELD SIDE POST LOWER AFT FITTING CRACKED. REMOVED AND INSTALLED NEW SERVICEABLE COPILOT WINDSHIELD SIDE POST LOWER AFT FITTING IAW SRM 51-40-11 AND 51-42-21.
- [SDR REXA2019062730983](https://openairdocs.org/sdr/REXA2019062730983.md): Bulkhead Web · chafed · May 23, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 REAR PRESSURE BULKHEAD WEB FWD FACE HAS DAMAGE AT LBL9,18,36,AND RBL9,18,36 WL 103. REPAIRED IAW GREO 601R-53-61-2155.
- [SDR REXA201906273982](https://openairdocs.org/sdr/REXA201906273982.md): Fitting · cracked · May 23, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PILOT WINDSHIELD SIDE POST LOWER AFT FITTING CRACKED. DRILLED UP AND INSTALLED NEW SERVICEABLE PILOT WINDSHIELD SIDE POST LOWER AFT FITTING P/N 601R33235-35 IAW TR#51-42-51-40-11-000 AND 51-42-21-100.
- [SDR REXA2019052730945](https://openairdocs.org/sdr/REXA2019052730945.md): Window Post · cracked · May 23, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Structure
  > WINDSHIELD CENTER POST BOTTOM LH AND RH FITTINGS CRACKED. REMOVED AND REPLACED DAMAGED WINDSHIELD CENTER POST FITTINGS IAW SRM 51-40-11 TR 51-42 AND 51-42-21.
- [SDR REXA2019062710980](https://openairdocs.org/sdr/REXA2019062710980.md): Strap · corroded · May 21, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LH FS 559 FLOOR SUPPORT STRAP CORRODED BETWEEN LBL27 AND LBL42. LOCATED AND DRILLED NEW SERVICEABLE STRAP PN 601R31025-291AW IAW SRM 51-40-11, INSTALLED NEW SERVICEABLE STRAP IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-13.
- [SDR REXA2019062710979](https://openairdocs.org/sdr/REXA2019062710979.md): Floorbeam · corroded · May 21, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LH FLOOR SUPPORT ANGLE ATTACHED TO FS 621 PRESSURE BULKHEAD CORRODED BETWEEN LBL27 AND LBL42. REPAIRED IAW BOMBARDIER REO 601R-53-61-7009.
- [SDR REXA2019052710953](https://openairdocs.org/sdr/REXA2019052710953.md): Floorbeam · corroded · May 21, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RT FLOOR BEAM CAP CORRODED AT FS 559 INBD SIDE OF RBL9. REPAIRED AREA IAW REO 601R-53-41-2483.
- [SDR REXA2019062700962](https://openairdocs.org/sdr/REXA2019062700962.md): Stiffener · cracked · May 20, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAPR PRESSURE BULKHEAD Z-MEMBER BL0.0 WL 112 HAS INDICATION NOTED 2 INCHES LONG 60% FSH FAILED NDT INSPECTION. (FROM CONTINUATION CARD OP69) REPAIRED IAW BOMBARDIER GREO 601R-53-61-1285 REV E.
- [SDR REXA2019062780955](https://openairdocs.org/sdr/REXA2019062780955.md): Bracket · cracked · May 18, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT NLG WHEEL WELL HYD TRANSDUCER BRACKET CRACKED. REMOVED ADN REPLACED RH TRANSDUCER BRACKET PN 601R75262-157 IAW CRJ 200 SRM 51-40-11 & 51-42-06
- [SDR REXA2019062760961](https://openairdocs.org/sdr/REXA2019062760961.md): Bulkhead Web · cracked · May 16, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT RBL 27.50 WL 99 3 INCHES LONG 60% FSH FAILED NDT INSPECTION. REPAIRED IAW GREO 601R-53-61-1285 REV E.
- [SDR REXA2019051600954](https://openairdocs.org/sdr/REXA2019051600954.md): Handle · cracked · May 16, 2019 · N981EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > FOUND MAIN AVIONICS DOOR HANDLE HOUSING HAS INDICATIONS NOTED AROUND ENTIRE BASE OF SHAFT HOUSING FAILED NDT 100% FSH. REMOVED AND REPLACED MAIN AVIONICS DOOR HANDLE ASSY IAW CRJ 200 SRM 51-42-41.
- [SDR REXA2019062715956](https://openairdocs.org/sdr/REXA2019062715956.md): Bracket · cracked · May 15, 2019 · N981EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT EQUIPMENT COMPARTMENT HYD. SYSTEM #2 PRESSURE AND RETURN FILTER BRACKET IS CRACKED AT THE AFT BOTTOM CORNER. REMOVED AND REPLACED SYSTEM #2 HYD PRERSSURE AND RETURN FILTER BRACKET INTERCOSTAL IAW CRJ 200 SRM 51-42-06, 51-42-21, 51-45-00, 51-40-11. LEAK O
- [SDR REXA2018090400768](https://openairdocs.org/sdr/REXA2018090400768.md): Not Reported · malfunctioned · Aug 28, 2018 · N981EV · Cndair CL6002B19 · Fuel Controlling System
  > DURING ENGINE START OF THE NUMBER 2 ENGINE THERE WAS NO LIGHT OFF. SHORTLY THERE AFTER THE GROUND CREW INFORMED US SMOKE AND A LITTLE BIT OF FLAMES WERE COMING OUT OF THE ENGINE. REMOVED FUEL CONTROL UNIT IAW AMM 73-21-01. BREAKERS PULLED + COLLARED CBP-1 M2,
- [SDR REXA2018052530408](https://openairdocs.org/sdr/REXA2018052530408.md): Sdu · faulted · May 23, 2018 · N981EV · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED CAUTION AT FLAPS 12, FAILED ON RETRACTION IN FLIGHT, FLAP HANDLE AT 8, EICAS AT 12 BETWEEN 150 - 200 KTS, 2-3 MINUTE FLIGHT TIME. PERFORMED A FLAP FAIL RESET, RESET SUCCESSFUL. PERFORMED TROUBLESHOOTING IAW FIM 27-50-00, REV 54 IAW AD 2009-06-1
- [SDR REXA2017122001273](https://openairdocs.org/sdr/REXA2017122001273.md): Bulb · inoperative · Dec 20, 2017 · N981EV · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT ON OVERHEAD PANEL INOPERATIVE. REMOVED AND REPLACE THE BULBS IAW AMM 31-11-00. OPS CHECKED GOOD.
- [SDR REXA2017100201062](https://openairdocs.org/sdr/REXA2017100201062.md): Strut · malfunctioned · Oct 2, 2017 · N981EV · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > NOSE GEAR DID NOT RETRACT AFTER TAKE OFF. MASTER WARNING MESSAGES, GEAR DISAGREE AND NOSE GEAR DOOR RAN QRH AND RETURNED TO DEPARTURE. R & R THE NOSE LANDING GEAR SHOCK STRUT. RIGGED & OPS CHECKED GOOD. GEAR DISAGREE OPS CHECK PERFORMED IAW AMM 32-30-00. O

Next page: https://openairdocs.org/aircraft/N981EV/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 = 'N981EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N981EV/reports

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