# Service difficulty reports: N543EA

A list on [N543EA](https://openairdocs.org/aircraft/N543EA.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 2 · 71 reports

- [SDR VNAA2025021011102](https://openairdocs.org/sdr/VNAA2025021011102.md): Dcu · unserviceable · Feb 6, 2025 · N543EA · Cndair CL6002C10 · Central Computers
  > ON DESCENT BURNING SMELL CBP2 Q2 POPPED. DCU AURAL INOP STATUS MESSAGE. THERE WAS NO MEDICAL ATTENTION REPORTED / INSPECTED FOR SMOKE ODOR ON FLIGHT DECK IAW FIM 21-21-00-810-806-A01. SUSPECT DCU 2 AND DCU CONTROL PANEL AS CAUSE OF ODOR. REMOVED AND REPLACED D
- [SDR WRXR20241115003](https://openairdocs.org/sdr/WRXR20241115003.md): Floor Support · corroded · Nov 15, 2024 · N543EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > 3 AREAS OF PITTING CORROSION IN 2.5" X 1.5" AREA AT LBL 27/ FS 1031. PERFORMED FLOOR BEAM SPLICE REPAIR FOR SECTION FS 1031 TO FS 1060 LBL27 IAW CRJ700 SRM 53-00-41-201-001-A01 COMPLIED WITH REO 670-53-61-2389 DEVIATION TO SRM FLOOR BEAM SPLICE REPAIR (TASK 53
- [SDR WRXR20241115002](https://openairdocs.org/sdr/WRXR20241115002.md): Skin · dented · Nov 15, 2024 · N543EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > WO DENTS FOUND AT F.S. 985 AT BOTTOM CENTERLINE. FWD DENT 1 1/4" X 1 9/16" X.041 DEEP, AFT DENT 1 3/16" X 1 1/2" X.085" DEEP. CUT DAMAGE 2 PLACE BETWEEN FS 969.00 - FS 985.00 STGR 2. FABRICATED TOP AND BOTTOM DOUBLERS (2EA) FROM 2024-T3.063 LOT # 459396B8,
- [SDR WRXR202411150001](https://openairdocs.org/sdr/WRXR202411150001.md): Skin · dented · Nov 15, 2024 · N543EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > MULTIPLE DENTS LOCATED ON THE LOWER SKIN PANEL AT FS 1015 TO FS 1031 BETWEEN STR22R TO STR24R. COMPLETED REPAIR OF ALL AREAS IAW REO 670-53-61-2400 REV --.
- [SDR WRXR20241103001](https://openairdocs.org/sdr/WRXR20241103001.md): Door · damaged · Nov 3, 2024 · N543EA · Cndair CL6002C10 · Landing Gear Doors
  > PERM REPAIR BEFORE 29,283.37 FH - LH NLG SURROUND DOUBLER. REMOVED AND REPLACED DOUBLER IAW BOMBARDIER DRAWING CC670-32010 REV F, SECTION III - PERMANENT REPAIR OF OLIVER WYMAN EA 22-C7-53-1311 REV. A.
- [SDR WRXR20241018001](https://openairdocs.org/sdr/WRXR20241018001.md): Beam · mechanic error · Oct 18, 2024 · N543EA · Cndair CL6002C10 · Fuselage Main, Structure
  > QTY (1) BLENDED AREA OF MISDRILLED DAMAGE TO RBL 36.00 PRESSURE SILL BEAM WEB (DWG SH670-36180, AL ALY 2024-T3511, S8347AA EXTRUSION, 0.090" NOM. THK, REF) BETWEEN FS785.00 AND FS797.00. COMPLETED LPI (FLUORESCENT) PER NDTM 51-20-008 OR EDDY CURRENT INSPECT PE
- [SDR WRXR20241017001](https://openairdocs.org/sdr/WRXR20241017001.md): Fitting · gouged · Oct 17, 2024 · N543EA · Cndair CL6002C10 · Main Landing Gear
  > GOUGES ON RH MLG SIDE-STAY FITTING PN:CC670-10608 BETWEEN RBL 22.5 AND RBL 45.0 INBD. GOUGE (A)MEASURES ROUGHLY.3" X.1" AND THE O/B GOUGE (B) MEASURES.2" X.1". BLENDED DAMAGED AREA IAW PSA EA A1-670-32-00008 STEPS 1-4. ROTO-PEEN REWORKED ARA IAW CRJ700 SRM
- [SDR WRXR20241016001](https://openairdocs.org/sdr/WRXR20241016001.md): Frame · corroded · Oct 16, 2024 · N543EA · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME F.S 310.00 IN BETWEEN L/H STRGR #22 TO R/H STRGR #22. REMOVED AND REPLACED FRAME SECTION FS310.00 AT AND BETWEEN 25L AND 25R IAW CRJ700 SRM 53-00-06-201-006-A01.
- [SDR WRXR20241011002](https://openairdocs.org/sdr/WRXR20241011002.md): Skin · gouged · Oct 11, 2024 · N543EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > MULTIPLE GOUGES ON THE LOWER SKIN PANEL AT FS 1000 TO FS 1031 BETWEEN STR25R TO STR27. BLENDED AREAS A-G TO A 20:1 RATIO ON THE LOWER SKIN PANEL AT FS 1000 TO FS 1031 BETWEEN STR25R TO STR27 IAW REO 670-53-61-2384 REV--.
- [SDR WRXR20241011001](https://openairdocs.org/sdr/WRXR20241011001.md): Bulkhead · gouged · Oct 11, 2024 · N543EA · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > THERE ARE THREE GOUGES IN THE FS 169.00 BULKHEAD WHERE THE ATTACHMENT HARDWARE OF THE NOSE RADOME SEEN IN VIEW F PER CRJ 700 IPC 53-81-80 HAVE CONTACTED EACH OTHER. AT THE NINE-O CLOCK POSITION THE GOUGE DEPTH IS 0.023", AT THE SIX-O CLOCK POSITION THE GOUGE D
- [SDR WRXR20241008002](https://openairdocs.org/sdr/WRXR20241008002.md): Drain Line · corroded · Oct 8, 2024 · N543EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD DRAIN VALVE TUBE ASSY ON PASSENGER DOOR SILL IS CORRODED THROUGH. REMOVED & REPLACED DRAIN TUBE ASSY SH670-31904-5 IAW CRJ700 SRM 51-42-06-001-001-A01.
- [SDR WRXR20241008001](https://openairdocs.org/sdr/WRXR20241008001.md): Drain Line · corroded · Oct 8, 2024 · N543EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT DRAIN VALVE TUBE ASSY ON PASSENGER DOOR SILL IS CORRODED THROUGH. REMOVED & REPLACED DRAIN TUBE ASSY SH670-31904-5.IAW CRJ700 SRM SRM 51-42-06-001-001-A01.
- [SDR VNAA202304181111](https://openairdocs.org/sdr/VNAA202304181111.md): Gcu · unknown · Apr 14, 2023 · N543EA · Cndair CL6002C10 · AC Generation System
  > IDG 2 FAIL INFLIGHT, MULTIPLE STATUS MESSAGES APU BATTERY CHARGER, FLAPS HALFSPEED, SLATS HALFSPEED, DC ESS TIED CLOSED, DC MAIN TIE CLOSED, ICE DET 2 FAIL / REMOVED AND #2 GCU IAW CRJ 900 AMM 24-11-07-000/400-801 AND OPS CHECK GOOD IAW CRJ 900 AMM 24-11-01-71
- [SDR VNAA2022112009915](https://openairdocs.org/sdr/VNAA2022112009915.md): Floor Support · corroded · Nov 20, 2022 · N543EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON RH FLOOR SILL UNDERSIDE FS 310- FS 319. REMOVED CORRODED RH FLOOR SILL PN:SH670-32172-11 IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE RH FLOOR SILL PN: SH670-32172-11
- [SDR VNAA2022112099914](https://openairdocs.org/sdr/VNAA2022112099914.md): Support Bracket · cracked · Nov 20, 2022 · N543EA · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > DURING ACCESS FOUND SUPPORT BRACKET BETWEEN PANELS 195DL AND 196DR TO BE CRACKED TOWARDS THE AFT SECTION OF THE BRACKET. CORRECTIVE ACTION: LOCATED, DRILLED CHANNEL PN# CC670-39251-1 IAW CRJ700 SRM 51-40-11-001-001-A01 AND INSTALLED IAW CRJ700 SRM 51-42-06-
- [SDR VNAA2022112099913](https://openairdocs.org/sdr/VNAA2022112099913.md): Angle · corroded · Nov 20, 2022 · N543EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > REAR FUSELAGE FAIRING SUPPORT FRAME, LOWER SPLICE IS CORRODED AT F.S. 939.00, STRINGER 27. CORRECTIVE ACTION: LOCATED, DRILLED, AND DEBURRED REAR FUSELAGE FAIRING SUPPORT FRAME, LOWER SPLICE AT F.S.939.00, STGR27 IAW CRJ700 SRM 51-40-11-001-001-A01. INSTA
- [SDR VNAA2022112099912](https://openairdocs.org/sdr/VNAA2022112099912.md): Stringer · cracked · Nov 20, 2022 · N543EA · Cndair CL6002C10 · Fuselage Main, Frame
  > FOUND FS280-295 STRINGER 3L HAS INDICATION NOTED 3.950 LONG 100%FSH FROM FWD EDGE OF STRINGER TO THE 4TH HOLE FAILED NDT INSPECTION CORRECTIVE ACTION: REPAIRED F.S. 280 TO F.S. 295 STRINGER 3L CRACK IAW BOMBARDIER REO 670-53-21-493, REV -B, DATED 2011-11-18
- [SDR VNAA2022112099911](https://openairdocs.org/sdr/VNAA2022112099911.md): Actuator · corroded · Nov 20, 2022 · N543EA · Cndair CL6002C10 · Leading Edge Devices
  > BUTE DOOR ACTUATOR SPRING ON THE RH WING OTBD FLAP MIDDLE HINGE BOX IS CORRODED. CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE BUTE DOOR ACTUATOR SPRING ON RH WING OTBD FLAP MIDDLE HINGE BOX IAW CRJ700 AMM 57-54-02-400-804-A01
- [SDR VNAA202109171111](https://openairdocs.org/sdr/VNAA202109171111.md): Slat System · malfunctioned · Sep 17, 2021 · N543EA · Cndair CL6002C10 · Leading Edge Slat Control System
  > ON THE WAY INTO KILM THE CREW HAD A SLATS FAILURE. ONCE ON THE GROUND MX HAD CLEARED THE FAILURE. FOR THE NEXT LEG TO KPHL THE EXACT SAME FAIRURE HAPPENED AT FL060 THEY THEN DECLARED AN EMERGENCY AND TURNED BACK TO KILM. THEY LANDED SAFELY WITHOUT ANY ISSUE."
- [SDR VNAA202108051111](https://openairdocs.org/sdr/VNAA202108051111.md): Acm · odor · Aug 3, 2021 · N543EA · Cndair CL6002C10 · Cabin Cooling System
  > AT FL050 THE CREW SMELLED SMOKE AND CALLED TO THE FA WHO REPORTED THEY SMELLED IT IN THE CABIN. THE AFT FA SAID THERE WAS VISIBLE SMOKE AS WELL. THE CREW DECLARED AN EMERGENCY, RAN THE QRH AND THE SMOKE AND SMELL BEGAN TO DISSIPATE. THEY CONTINUED ON THE APPRO
- [SDR VNAA202012291111](https://openairdocs.org/sdr/VNAA202012291111.md): Acm · damaged · Dec 27, 2020 · N543EA · Cndair CL6002C10 · Cabin Cooling System
  > CREW REPORTED SMOKE IN COCKPIT (NO FIRE) WHILE AT GATE IN CLT. PASSENGERS WERE DEPLANED THRU MAIN CABIN DOOR WITHOUT INCIDENT AND MAINTENANCE WAS CALLED TO AIRCRAFT. RIGHT AC PACK WAS FOUND TO BE THE CAUSE. 12/27/20: DEFERRED RT PACK, IAW CRJ-900 MEL 21-51-
- [SDR SIMA2020031615003](https://openairdocs.org/sdr/SIMA2020031615003.md): Channel · cracked · Mar 15, 2020 · N543EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT BAGGAGE BAY STRUCTURE CHANNEL FOR BAGGAGE BAY DOOR IS CRACKED.-C/A-REPAIRED IAW ERS-CR-53MR-4070.
- [SDR SIMA202002253005](https://openairdocs.org/sdr/SIMA202002253005.md): Bracket · bent · Feb 23, 2020 · N543EA · Cndair CL6002C10 · Elevator Structure
  > LH ELEVATOR UPPER INPUT ARM BRACKET (VERT. STAB. TO HORZ. STAB. FLANGES ARE BENT. (LEVER ASSY)-C/A-REMOVED AND REPLACED LH ELEVATOR UPPER BELLCRANK LEVER ON HORZ. STAB AFT SPAR IAW CRJ 700 27-31-30-400-805. SEE E776830 FOR OPS CHECK.
- [SDR SIMA202002253004](https://openairdocs.org/sdr/SIMA202002253004.md): Bracket · damaged · Feb 23, 2020 · N543EA · Cndair CL6002C10 · Elevator Structure
  > RH ELEVATOR INPUT ARM BRACKET (VERT. STAB. TO HORZ. STAB.) FLANGES ARE BENT/CRACKED. (LEVER ASSEMBLY.)-C/A-REMOVED AND REPLACED RH ELEVATOR UPPER BELLCRANK LEVER ON HORZ. STAB. AFT SPAR IAW CRJ 700-27-31-30-400-805. SEE E776803 FOR OPS CHECK.
- [SDR SIMA202003021003](https://openairdocs.org/sdr/SIMA202003021003.md): Door Sill · corroded · Feb 21, 2020 · N543EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON SERVICE DOOR SILL-C/A-REMOVED AND REPLACED SERVICE DOOR SILL IAW SRM 51-40-11, SRM 51-42-06, DRGSH670-3195, SRM 51-42-34 AND SRM 51-25-16.
- [SDR SIMA2020030419010](https://openairdocs.org/sdr/SIMA2020030419010.md): Floorbeam · cracked · Feb 19, 2020 · N543EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM FS280.00-C/A-REPAIRED RH CENTER COCKPIT FLOOR BEAM AT BL 12.00 JUST FWD OF THE FLOOR BEAM AT FS 280.00 IAW SRM 53-11-43-201-003.
- [SDR SIMA2020030419009](https://openairdocs.org/sdr/SIMA2020030419009.md): Floorbeam · corroded · Feb 19, 2020 · N543EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH FLOOR BEAM AT FS 280.00 HAS NUMEROUS AREAS OF CORROSION WHERE IT IS SANDWITCHED BETWEEN DRIP TRAY AND L ANGLE OF THE BULKHEAD.-C/A-REPLACED LH SIDE FLOOR BEAM AT FS280. IAW SRM 51-42-06 AND 51-42-13.
- [SDR SIMA2020030419008](https://openairdocs.org/sdr/SIMA2020030419008.md): Floorbeam · corroded · Feb 19, 2020 · N543EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH FLOOR BEAM AT FS 280.00 HAS NUMEROUS AREAS OF CORROSION WHERE IT IS SANDWITCHED BETWEEN DRIP TRAY AND L ANGLE OF THE BULKHEAD.-C/A-REPLACED RH SIDE FLOOR BEAM AT FS280. IAW SRM 51-42-06 AND 51-42-13.
- [SDR SIMA202003029005](https://openairdocs.org/sdr/SIMA202003029005.md): Floorbeam · cracked · Feb 19, 2020 · N543EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM FS280.00-C/A-REPAIRED IAW SRM 53-11-43-201-003
- [SDR SIMA2020032706009](https://openairdocs.org/sdr/SIMA2020032706009.md): Cover · cracked · Dec 6, 2019 · N543EA · Cndair CL6002C10 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHT STRIPS: (#1 FWD RHT AND LFT)(#2 RHT)(#3 LFT)(#4 LFT AND RHT)(#6 RHT)(#7 LFT)(#8 RHT AND LFT)(#9 LFT)(#10 EXIT RH FWD)(#12 RHT) ARE CRACKED.-C/A-COMPLETE:REMOVED AND REPLACED MULTIPLE EMERGENCY LIGHT STRIP COVERS IAW AMM 33-51-01.
- [SDR SIMA20190903001](https://openairdocs.org/sdr/SIMA20190903001.md): Actuator · failed · Sep 3, 2019 · N543EA · Cndair CL6002C10 · Stabilizer Actuator
  > PITCH FEEL CAUTION MSG IN FLIGHT. QRH COMPLIED WITH. EMERGENCY DECLARED. C/A-REMOVED AND REPLACED LINEAR PITCH TRIM ACTUATOR IAW AMM 27-31-23 OPS CHECK GOOD.
- [SDR SIMA20190320002](https://openairdocs.org/sdr/SIMA20190320002.md): Flashlight · missing · Mar 20, 2019 · N543EA · Cndair CL6002C10 · Emergency Equipment
  > AFT FLIGHT ATTENDENT FLASHLIGHT MISSING-C/A-DEFERRED AFT FLIGHT ATTENDENT FLASHLIGHT TEMP INSTALLED. COULD NOT LOCATE TEMPORARY FLASHLIGHT. INSTALLED NEW AFT FLASHLIGHT IAW AMM 25-61-02. OPS CHECK GOOD IAW AMM 25-61-00. MEL 25-14 ITEM RESTORED
- [SDR SIMA2018073130002](https://openairdocs.org/sdr/SIMA2018073130002.md): Handle · not seated · Jul 30, 2018 · N543EA · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO CAUTION MSG AFTER TAKE OFF. FOUND CARGO DOOR HANDLE PARTIALLY OPEN. CLOSED CARGO DOOR AND VERIFIED SECURED. NO FURTHER DEFECTS NOTED.
- [SDR SIMA201807081004](https://openairdocs.org/sdr/SIMA201807081004.md): Flashlight · odor · Jul 6, 2018 · N543EA · Cndair CL6002C10 · Emergency Equipment
  > STRONG SULFUR SMELL IN CABIN AND ALSO COCKPIT BURNS THE EYES BOTH ENGINE AND PACK ON. PERFORMED GVI FWD AVIONICS AFT BAY NO FINDINGS INSPECTED CABIN AND FOUND ALL FLASHLIGHTS BURNT SMELL LIKE SULFUR. RAN APU PACKS AND BLEEDS NO SMELL NOTED CREW RAN ENGINES NO
- [SDR SIMA201806185003](https://openairdocs.org/sdr/SIMA201806185003.md): Fan · failed · Jun 15, 2018 · N543EA · Cndair CL6002C10 · Communications System
  > ON ENTERING THE COCKPIT, SMELLED A BURNED ELECTRONIC LIKE ODOR. PERFORMED FIM 21-21-00-810-806. FOUND RTU NR 2 INTERNAL FAN INOPERATIVE MESSAGE ON THE MDC. VERIFIED SOURCE OF THE ODOR TO BE THE RTU. R & R RTU 2 IAW AMM 23-81-01. OPS CHECKED GOOD.
- [SDR SIMA20170821005](https://openairdocs.org/sdr/SIMA20170821005.md): Tire · failed · Aug 21, 2017 · N543EA · Cndair CL6002C10 · Tire
  > NR 2 TIRE DESTROYED WITH THROWN THREAD SEPARATION. REMOVED AND REPLACED THE TIRE & WHEEL ASSEMMBLY IAW W/C 32-008.
- [SDR SIMA20170626001](https://openairdocs.org/sdr/SIMA20170626001.md): Pcu · malfunctioned · Jun 26, 2017 · N543EA · Cndair CL6002C10 · Drag Control System
  > ON DESCENT MOVED FLIGHT SPOILER UNF POSITION RECEIVED IB FLT SPOILERS AND IB SPOILERONS CAUTION MESSAGE. INTERROGATED MDC FOUND RT INBD MFS PCU JAM PERFORMED S POST 1 RESET PERFORMED OPS CHECK IAW ETN-CR-27-093 OPS CHECK GOOD.
- [SDR SIMA20170226005](https://openairdocs.org/sdr/SIMA20170226005.md): Panel · cracked · Feb 26, 2017 · N543EA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT STEP PANEL HAS TWO CRACKS IN THE CORNERS. REPAIRED THE PAX DOOR AFT STEP SHELL IAW SRM 52-11-04 AND ETN CR-52-039R2
- [SDR SIMA20161223004](https://openairdocs.org/sdr/SIMA20161223004.md): Acm · smoke · Dec 23, 2016 · N543EA · Cndair CL6002C10 · Cabin Cooling System
  > RIGHT PACK AUTO FAIL SMOKE IN CABIN. R & R THE ACM AND TEMPERATURE CONTROL VALVE IAW AMM 21-51-08 AND AMM 21-51-20. OPS CHECKED GOOD AND NO LEAKS FOUND.
- [SDR SIMA20160530003](https://openairdocs.org/sdr/SIMA20160530003.md): Vane · defective · May 30, 2016 · N543EA · Cndair CL6002C10 · Stall Warning System
  > STALL FAIL CAUTION POSTED JUST AFTER TAKEOFF. STICK SHAKER ACTIVATED CONTINUOUSLY AT & ABOVE FL 220. PULLED LT CHANNEL STALL PROTECTION CB B/C CAPTAINS LOW SPEED TAPE COMPLETELY CLOSED ON HIGH SPEED, FIRST OFFICERS SIDE NORMAL. FOUND LT AOA VANE FROZEN MSG
- [SDR SIMA20150828006](https://openairdocs.org/sdr/SIMA20150828006.md): Mcu · failed · Aug 28, 2015 · N543EA · Cndair CL6002C10 · Stabilizer Actuator
  > PITCH TRIM RUNAWAY NOTED, FOLLOWED BY STAB FAULT STATUS MSG, FOLLOWED BY AUTOPILOT STAB TRIM CAUTION MSG. TRANSFERRED TO NRWC 543-ORD-01276. R & R MCU IAW AMM 27-42-07. OPERATIONS CHECKED GOOD. REFERENCE NRWC 543-ORD-01276 FOR CORRECTIVE ACTION.
- [SDR SIMA20150828007](https://openairdocs.org/sdr/SIMA20150828007.md): Printed Ckt Board · inoperative · Aug 28, 2015 · N543EA · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY LIGHTS CAME ON AFTER LANDING & REMAINED ON UNTIL FLIGHT ATTENDANT TURNED THEM OFF. PSU LIGHTS CAME ON & STAYED ON. INSPECTED ACFT & FOUND PCB AT SEAT 18A INOPERATIVE. REPLACED PCB AT 18A IAW 23-31-17. OPERATIONS CHECKED GOOD IAW 33-51-00TR. ACFT
- [SDR SIMA20150820002](https://openairdocs.org/sdr/SIMA20150820002.md): Warning System · false activation · Aug 20, 2015 · N543EA · Cndair CL6002C10 · Drag Control System
  > INBOARD FLIGHT SPOILERS CAUTION MSG ILLUMINATED DURING INITIAL APPROACH AT APPROX 4000 FT. DECLARED EMER, LANDED SAFELY & TAXIED TO GATE. POWERED UP ACFT, NO MSG POSTED. PERFORMED SELF-TEST OF THE SPOILER & STAB CONTROL UNIT IAW MM 27-61-05. CHECKED GOOD N
- [SDR SIMA20150803001](https://openairdocs.org/sdr/SIMA20150803001.md): Handle · out of adjust · Aug 3, 2015 · N543EA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR WARNING AT 500FT ON FINAL. NR 1 FLIGHT ATTENDANT REPORTS RED FLAG UNLOCKED, APPEARED WHILE AIRBORNE. PRIOR LANDING FLIGHT ATTENDANT NR 2 OBSERVED DOOR HANDLE UP THEN DOWN, APPROXIMATELY 2" AFTER LANDING. ADJUSTED LATCH MECHANISM INNER HANDLE
- [SDR SIMA20150517001](https://openairdocs.org/sdr/SIMA20150517001.md): Warning System · false activation · May 17, 2015 · N543EA · Cndair CL6002C10 · Drag Control System
  > ON APPROACH, INBD FLIGHT SPOILERS & INBD SPOILERONS CAUTION MSGS, DECLARED EMER. COMPLIED WITH AOM VOL 1. INTERROGATED MDC, FOUND RIB MFS PCU & PCU JAM MDC MSG. PERFORM SPOST 1 RESET. PERFORMED OPERATIONS CHECK IAW ETN-CR-27-093. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150401004](https://openairdocs.org/sdr/SIMA20150401004.md): Warning System · false activation · Apr 1, 2015 · N543EA · Cndair CL6002C10 · Drag Control System
  > INBOARD FLIGHT SPOILERS & INBD SPOILERONS CAUTION MSG POSTED ON EICAS ON APPROACH AT 4000' WHEN FLIGHT SPOILERS DISPLAYED. CHECKED AML, NO HISTORY. PERFORMED RESET PROCEDURES IAW ETN-CR-27-093. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS NOTED.
- [SDR SIMA20150309005](https://openairdocs.org/sdr/SIMA20150309005.md): Pcu · failed · Mar 9, 2015 · N543EA · Cndair CL6002C10 · Drag Control System
  > OTBD FL & OTBD SPOILERONS CAUTION MSG AT 8,000 FT. TRANSFERRED TO NRWC 543-DFW-01187. LT OTBD MULTI-FUNCTION SPOILER PCU WAS R & R. OPERATIONS CHECKED GOOD WITH NO LEAKS. REFERENCE NRWC 543-DFW-01187 FOR WORK PERFORMED. FOLLOWING TURN OVER WORK PERFORMED,
- [SDR SIMA20150304005](https://openairdocs.org/sdr/SIMA20150304005.md): Warning System · activated · Mar 4, 2015 · N543EA · Cndair CL6002C10 · Drag Control System
  > OUTBOARD SPOILERONS & OTBD FLIGHT SPOILER CAUTION MSGS IN FLIGHT WITH FLIGHT SPOILER HANDLE DEPLOYED. STOWED FLIGHT SPOILERS. MSG DID NOT EXTINGUISH. COMPLIED WITH AOM VOL 1 EMER PROCEDURES. CAUTION MSGS DID NOT EXTINGUISH. PERFORMED RESET IAW ETN-CR-27-0
- [SDR SIMA20150127008](https://openairdocs.org/sdr/SIMA20150127008.md): Angle · cracked · Jan 27, 2015 · N543EA · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
  > RIGHT VERTICAL STABILIZER TO FUSELAGE FWD ANGLE HAS EVIDENCE OF A CRACK ON THE AFT END. REPAIRED RT VERTICAL STAB TO FUSELAGE FWD ANGLE AFT END IAW EO CR-55MR-038 & ERS CR--5500-230.
- [SDR SIMA20150108012](https://openairdocs.org/sdr/SIMA20150108012.md): Drag Angle · cracked · Jan 8, 2015 · N543EA · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
  > LEFT VERTICAL STAB TO FUSELAGE FWD ANGLE HAS EVIDENCE OF A CRACK ON THE AFT END. APPROX 1 INCH LONG. REPAIRED IAW EO CR-55MR-038.

Next page: https://openairdocs.org/aircraft/N543EA/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 = 'N543EA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N543EA/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.