# Service difficulty reports: N8940E

A list on [N8940E](https://openairdocs.org/aircraft/N8940E.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 · 62 reports

- [SDR REXA2017102801134](https://openairdocs.org/sdr/REXA2017102801134.md): Cable · damaged · Oct 28, 2017 · N8940E · Cndair CL6002B19 · Light System Wiring
  > AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED THE REAR STRIP AND CABLE IAW AMM 33-51-01. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR REXA2017100201061](https://openairdocs.org/sdr/REXA2017100201061.md): Apu · malfunctioned · Oct 2, 2017 · N8940E · Cndair CL6002B19 · APU Core Engine
  > APU SHUTDOWN. PERFORMED A RESTART AND IT SHUTDOWN AGAIN. APU BLEW FLAMES AND SMOKE. CHECKED APU FOR FIRE XTINGUISHING BOTTLE DISCHARGE FOUND NO DISCHARGE & APU BOTTLE ALSO GOOD. REMOVED AND REPLACED THE APU IAW 200-49-10-00. OPS CHECKED GOOD, NO LEAKS.
- [SDR REXA2017081600886](https://openairdocs.org/sdr/REXA2017081600886.md): Cover · broken · Aug 16, 2017 · N8940E · Cndair CL6002B19 · Emergency Lighting
  > FLOOR TRACK LIGHT COVER BROKEN AT ROW 1. REPLACED THE SECTION OF COVER IAW 33-51-01. OPS CHECKED GOOD.
- [SDR REXA2016062401190](https://openairdocs.org/sdr/REXA2016062401190.md): Door · binding · Jun 24, 2016 · N8940E · Cndair CL6002B19 · Passenger/Crew Doors
  > FA REPORTS MAIN CABIN DOOR LEVER HARD TO OPEN AND CLOSE. THE GREEN WITNESS MARK DO ALIGN CORRECTLY. PERFORMED VISUAL INSPECT OF DOOR LINKAGES, SHOOT BOLTS, DOOR FRAME, BEARING RODS, AND CABLES. NO DEFECTS NOTED. COMPLETED MULTIPLE OPS CHECKS OF DOOR OPENING
- [SDR REXA2016011900044](https://openairdocs.org/sdr/REXA2016011900044.md): Cover · loose · Jan 19, 2016 · N8940E · Cndair CL6002B19 · Emergency Lighting
  > PLASTIC COVER OVER EMERGENCY LIGHT, ADJACENT TO AISLE 12DC IS LOOSE. REPLACED LIGHT COVER IAW AMM 33-51-01.
- [SDR REXA2015122401246](https://openairdocs.org/sdr/REXA2015122401246.md): Light · cracked · Dec 24, 2015 · N8940E · Cndair CL6002B19 · Emergency Lighting
  > FLOOR TRACK EMER LIGHTING CRACKED & MISSING END CAPS. R & R FLOOR TRACK EMER LIGHTING COVER IAW AMM 33-51-01-400-801 3A 1 -3 & 33-51-01-400-801 3A 5 - 7. INSTALLED END CAPS IAW AMM 33-51-01-400-808 3A 12.
- [SDR REXA2015121701232](https://openairdocs.org/sdr/REXA2015121701232.md): Attach Fitting · cracked · Dec 17, 2015 · N8940E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AEB TWO EACH ATTACH CLIPS CRACKED COMMON TO THE FS 621.0 BULKHEAD HORIZONTAL INTERCOSTALS & ACFT SKIN AT STRINGER 14L & 15L. R & R TWO EACH ATTACH CLIPS COMMON TO THE APB & THE SKIN AT STRINGER 14L & 5L IAW SRM 51-40-06.
- [SDR REXA2015121601236](https://openairdocs.org/sdr/REXA2015121601236.md): Attach Fitting · cracked · Dec 16, 2015 · N8940E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 202.00, RBL 8 NLG BAY INTERCOSTAL ATTACH CLIP CRACKED. R & R FS 202.00, RBL 8 NLG BAY INTERCOSTAL ATTACH CLIP IAW SRM 51-42-06.
- [SDR REXA2015121601235](https://openairdocs.org/sdr/REXA2015121601235.md): Torque Box · cracked · Dec 16, 2015 · N8940E · Cndair CL6002B19 · Engine Thrust Reverser
  > NUMBER 1 ENG THRUST REVERSER TORQUE BOX TE IS CRACKED AT THE 5:30 POSITION. REPAIRED CRACK TO NR 1 ENG THRUST REVERSER TORQUE BOX AT THE 5:30 POSITION IAW REO 601R-78-30-2616.
- [SDR REXA2015121601234](https://openairdocs.org/sdr/REXA2015121601234.md): Torque Box · cracked · Dec 16, 2015 · N8940E · Cndair CL6002B19 · Engine Thrust Reverser
  > NUMBER 1 ENG THRUST REVERSER TORQUE BOX TE IS CRACKED AT 6:30 POSITION. REPAIRED CRACK TO NR 1 ENG THRUST REVERSER TORQUE BOX AT THE 6:30 POSITION IAW REO 601R-78-30-2616.
- [SDR REXA2015121601233](https://openairdocs.org/sdr/REXA2015121601233.md): Bracket · cracked · Dec 16, 2015 · N8940E · Cndair CL6002B19 · Engine Cowling System
  > NUMBER 1 ENG NOSE COWL OTBD COWL BRACKET IS CRACKED. R & R NR 1 ENG COWL OTBD COWL BRACKET IAW AMM 71-61-01.
- [SDR REXA2015121501242](https://openairdocs.org/sdr/REXA2015121501242.md): Fitting · cracked · Dec 15, 2015 · N8940E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PILOT`S SIDE POST LOWER OTBD FITTING IS CRACKED. R & R WINDOW POST FITTING IAW SRM 51-42-21.
- [SDR REXA2015121501241](https://openairdocs.org/sdr/REXA2015121501241.md): Frame · corroded · Dec 15, 2015 · N8940E · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 605.00 FRAME HAS CORROSION AT STRINGER 27. REPAIRED CORROSION DAMAGE ON FRAME AT STRINGER 27 IAW EA 253-03844.
- [SDR REXA2015121501240](https://openairdocs.org/sdr/REXA2015121501240.md): Attach Bracket · cracked · Dec 15, 2015 · N8940E · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > ATTACH BRACKET WAS FOUND CRACKED UPON REMOVAL OF RT ACM SUPPORT AT FS 710. R & R RT ACM SUPPORT AT FS 710 IAW SRM 51-42-20.
- [SDR REXA2015121501239](https://openairdocs.org/sdr/REXA2015121501239.md): Seat Track · damaged · Dec 15, 2015 · N8940E · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FLOOR SEAT TRACK CHAFED & CORRODED IN SEVERAL PLACE FROM FS 409-409+112. R & R SEAT TRACK FROM FS 409-409+112, RBL 9 IAW AMM 53-01-11.
- [SDR REXA2015121501238](https://openairdocs.org/sdr/REXA2015121501238.md): Seat Track · corroded · Dec 15, 2015 · N8940E · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK CORRODED FROM FS 409+128 - 559. R & R SEAT TRACK FROM FS 409+128 - 559 IAW AMM 53-01-11.
- [SDR REXA2015121501237](https://openairdocs.org/sdr/REXA2015121501237.md): Seat Track · corroded · Dec 15, 2015 · N8940E · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK IS CORRODED & HAS CORRODED ATTACHING HARDWARE FROM FS 364 - 400, LBL 9. R & R SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2015121501231](https://openairdocs.org/sdr/REXA2015121501231.md): Hinge · corroded · Dec 15, 2015 · N8940E · Cndair CL6002B19 · Service Doors
  > LAVATORY SERVICE DOOR BOTH HINGES CORRODED. R & R BOTH LAVATORY SERVICE DOOR HINGES IAW SRM 51-42-21.
- [SDR REXA2015121201243](https://openairdocs.org/sdr/REXA2015121201243.md): Support · cracked · Dec 12, 2015 · N8940E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE COMPARTMENT RT ACM SUPPORT HAS A CRACKED ANGLE AT FS 710. INSTALLED NEW RT ACM SUPPORT AT FS 710 IAW CRJ 200 SRM 51-42-20
- [SDR REXA2015100400915](https://openairdocs.org/sdr/REXA2015100400915.md): Light · inoperative · Oct 4, 2015 · N8940E · Cndair CL6002B19 · Emergency Lighting
  > FLOOR TRACK EMER EXIT LIGHTS INOPERATIVE. REPLACED EMER LIGHT STRIP IAW AMM 33-51-01. OPERATIONS CHECKED GOOD. OK FOR SERVICE.
- [SDR REXA2015072700742](https://openairdocs.org/sdr/REXA2015072700742.md): Mechanism · lack of lube · Jul 27, 2015 · N8940E · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN CABIN DOOR WILL NOT CLOSE. REMOVED COVER PLATES FROM DOOR TO LUBRICATE MECHANISM'S AS REQUIRED IAW 12-20-52. OPERATIONS CHECKED GOOD. REINSTALLED COVER PLATES.
- [SDR REXA2015072100729](https://openairdocs.org/sdr/REXA2015072100729.md): Bpsu · malfunctioned · Jul 21, 2015 · N8940E · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAP FAIL CAUTION MSG UPON PUSH BACK. R & R LT BPSU & FECU. REFER TO NON-ROUTINE N77913 & N77914 FOR DETAILS.
- [SDR REXA2015071900723](https://openairdocs.org/sdr/REXA2015071900723.md): Unknown · malfunctioned · Jul 19, 2015 · N8940E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 20 APPROACH TO RUNWAY, 36C SPEED 180 KNOTS RAN A + H LANDED AT 400 IAW MIN AT ROOF FLAPS AT 0 + 5 STOPPED BRAKE TEMP ALL IN GUCUE. PERFORMED TROUBLESHOOTING IAW FIM CHAPTER 27-50-00 REV 48 IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC LOG 14-105 DATED
- [SDR REXA2015071700719](https://openairdocs.org/sdr/REXA2015071700719.md): Bpsu · malfunctioned · Jul 17, 2015 · N8940E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AFTER PUSH BACK. R & R RT BPSU IAW AMM 27-51-10. SEE NON-ROUTINE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR REXA2015071200677](https://openairdocs.org/sdr/REXA2015071200677.md): Rod · bent · Jul 12, 2015 · N8940E · Cndair CL6002B19 · Passenger/Crew Doors
  > CREW REPORTS MAIN PAX DOOR WILL NOT CLOSE. INSPECTED MAIN PAX DOOR IAW AMM 52-11-25. FOUND ROD ASSEMBLY BENT GOING TO LOWER STAIR. REMOVED ROD ASSEMBLY IAW AMM 52-11-05, PROBLEM PERSIST. R & R SPRING ROD PN 601R31988-1 IAW AMM 52-11. ALL CHECKED GOOD.
- [SDR REXA2015061400601](https://openairdocs.org/sdr/REXA2015061400601.md): Hinge · dirty · Jun 14, 2015 · N8940E · Cndair CL6002B19 · Passenger/Crew Doors
  > THE PASSENGER DOOR HANDLE IS DIFFICULT TO LATCH CLOSE. REMOVED SAND FROM LOWER STAIR HINGE AS REQUIRED & PERFORMED OPERATIONS CHECK IAW AMM 52-11-00. OPERATIONS CHECKED GOOD.
- [SDR REXA2015061000571](https://openairdocs.org/sdr/REXA2015061000571.md): Door Seal · contaminated · Jun 10, 2015 · N8940E · Cndair CL6002B19 · Passenger/Crew Doors
  > CABIN DOOR WILL NOT CLOSE. CLEANED EXCESS STICKY GREASE FROM DOOR SEAL. OPERATIONS CHECKED GOOD IAW AMM 52-70-01.
- [SDR REXA2015050800470](https://openairdocs.org/sdr/REXA2015050800470.md): Door · contaminated · May 8, 2015 · N8940E · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN CABIN DOOR DIFFICULT TO OPEN AFTER HANDLE IS LIFTED UP. TAKES MUCH EFFORT TO PUSH DOOR OPEN. ALSO HANDLE MUST BE RECYCLED. REMOVED SAND CONTAMINATED GREASE FROM MATING & SLIDING INTERFACE POINTS BETWEEN MCD & FUSELAGE. SERVICED WITH CLEAN GREASE. OPE
- [SDR REXA2015041400407](https://openairdocs.org/sdr/REXA2015041400407.md): Fire Bottle · defective · Apr 14, 2015 · N8940E · Cndair CL6002B19 · Fire Bottle, Portable
  > FLIGHT ATTENDANT REPORTS WATER FIRE EXTINGUISHER DIFFICULT TO ROTATE. REPLACED H2O FIRE EXTINGUISHER WITH SERVICEABLE EXTINGUISHER IAW AMM 26-23-01.
- [SDR REXA2015031700330](https://openairdocs.org/sdr/REXA2015031700330.md): Hinge · not seated · Mar 17, 2015 · N8940E · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT ATTENDANT REPORTS EXCESSIVE RESISTANCE WHEN PUSHING THE TOP OF THE MAIN CABIN DOOR, FOR OPENING. ALSO THE BOTTOM STEP DOES NOT GO DOWN WHEN THE MCD IS OPEN. FOUND PAX DOOR TOP STEP HINGE BACKED OUT ABOUT 2". RESEATED TOP STEP HINGE IAW AMM 52-11-04.
- [SDR REXA2015011000022](https://openairdocs.org/sdr/REXA2015011000022.md): Relay · failed · Jan 10, 2015 · N8940E · Cndair CL6002B19 · Light System Wiring
  > ACCESS BUSS CAUTION ILLUMINATED SEVERAL TIMES DURING FLIGHT. WOULD STAY ON AND EMERGENCY LIGHTS WOULD COME ON BEFORE BEING ABLE TO TRANSFER TO BUSS 2 CAUTION WOULD DISAPPEAR. R & R ACCESS BUSS SENSE RELAY K1XD IAW AMM TASK 24-51-27-000-801 AND 24-51-27-400-8
- [SDR REXA2014091800971](https://openairdocs.org/sdr/REXA2014091800971.md): Door Seal · dirty · Sep 18, 2014 · N8940E · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT ATTENDANT REPORTS MAIN CABIN PX DOOR DIFFICULT TO OPEN SEEMS TO CATCH ON LT SIDE. CLEANED HINGE DOOR SEAL & SURROUND & REMOVED DEBRIS. PERFORMED ADJUSTMENT TEST IAW AMM 52-11-00. OPERATIONS CHECKED GOOD.
- [SDR REXA2014090900887](https://openairdocs.org/sdr/REXA2014090900887.md): Battery Pack · discharged · Sep 9, 2014 · N8940E · Cndair CL6002B19 · Emergency Lighting
  > FORWARD EXT EMER LIGHT INOPERATIVE ON LT SIDE BY PAX DOOR. R & R BATTERY PACK IAW AMM 33-51-04. OPERATIONS CHECKED GOOD.
- [SDR REXA2014071600704](https://openairdocs.org/sdr/REXA2014071600704.md): Light · inoperative · Jul 16, 2014 · N8940E · Cndair CL6002B19 · Emergency Lighting
  > LEFT AFT EMER LIGHT EXTERIOR INOPERATIVE. R & R LT AFT EMER LIGHT IAW AMM 33-51-21. RAMP TESTS GOOD.
- [SDR REXA2014061100583](https://openairdocs.org/sdr/REXA2014061100583.md): Life Vest · unserviceable · Jun 11, 2014 · N8940E · Cndair CL6002B19 · Life Jacket
  > INFANT LIFE VEST BAG IS TORN. COMPLIED WITH PA 25-096A BY INSTALLING INFANT LIFE VESTS.
- [SDR REXA2013121802412](https://openairdocs.org/sdr/REXA2013121802412.md): Life Vest · missing · Dec 18, 2013 · N8940E · Cndair CL6002B19 · Life Jacket
  > INFANT LIFE VEST MISSING. INSTALLED INFANT LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013121102312](https://openairdocs.org/sdr/REXA2013121102312.md): Skin · corroded · Dec 10, 2013 · N8940E · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING FUEL PANEL CUTOUT HOLE LOCATION NR 15, WS 294.048 CORRODED 0.004 INCHES DEEP IN THE NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2013121102311](https://openairdocs.org/sdr/REXA2013121102311.md): Bulkhead · cracked · Dec 9, 2013 · N8940E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > THE FS 621 BULKHEAD COMMON TO THE LINTEL FITTING WAS FOUND TO BE CRACKED. REPAIRED IAW REO 601R-53-61-1230.
- [SDR REXA2013121002308](https://openairdocs.org/sdr/REXA2013121002308.md): Bulkhead · cracked · Dec 9, 2013 · N8940E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 202 BULKHEAD CRACKED IN THE LT FWD AVIONICS BAY WHERE THE BRAKE CABLE PASSES THROUGH. REPAIRED IAW REO 601R-53-11-563.
- [SDR REXA2013121002310](https://openairdocs.org/sdr/REXA2013121002310.md): Bulkhead · gouged · Dec 8, 2013 · N8940E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD HAS A 0.003 INCH GOUGE ON SKIN JUST BELOW ISOLATOR ON LOWER RT CORNER 16 INCHES ABOVE RBL 36. REPAIRED IAW SRM TR53-33 53-00-31.
- [SDR REXA2013112002269](https://openairdocs.org/sdr/REXA2013112002269.md): Light · inoperative · Nov 20, 2013 · N8940E · Cndair CL6002B19 · Emergency Lighting
  > CEILING EMERGENCY LIGHT ABOVE ROW 5 INOPERATIVE. RELAMPED CEILING EMERGENCY LIGHT AT ROW 5 IAW AMM 33-51-01, CHECKED GOOD OK FOR SERVICE.
- [SDR REXA2013060401066](https://openairdocs.org/sdr/REXA2013060401066.md): A/C Pack · seized · Jun 4, 2013 · N8940E · Cndair CL6002B19 · Cabin Cooling System
  > IN FLIGHT, SMELLED BURNING ODOR, ALSO NOISE AND VIBRATION, ISOLATED IT TO DISPLAY OR FAN. SELECTED FLT ALTN ON BOTH AND BOTH ODOR + NOISE STOPPED. PERFORMED OPS CHECK OF DISPLAY FANS IAW AMM 21-24-19, NO DEFECTS NOTED. PERFORMED OPS CHECK OF FANS IAW AMM 21
- [SDR REXA2013060101067](https://openairdocs.org/sdr/REXA2013060101067.md): Engine · overheated · Jun 1, 2013 · N8940E · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > LEFT ENGINE REACHED 902C ON TAKEOFF ROLL. ITT GAUGE FLASHED RED BUT NO AUDIBLES. ABORTED AT 85 KNOTS. PERFORMED VISUAL INSP LT ENGINE/ECS DUCTING. NO FAULTS NOTED. PERFORMED POWER ASSURANCE GROUND RUN/ENGINE ACCELERATION CHECK. ALL CHECKED GOOD IAW AMM 71
- [SDR REXA2013050900873](https://openairdocs.org/sdr/REXA2013050900873.md): Flashlight · inoperative · May 9, 2013 · N8940E · Cndair CL6002B19 · Emergency Equipment
  > CAPT FLASHLIGHT IS INOPERABLE.
- [SDR REXA2013032500598](https://openairdocs.org/sdr/REXA2013032500598.md): Battery · discharged · Mar 25, 2013 · N8940E · Cndair CL6002B19 · Emergency Lighting
  > EXTERNAL EMERGENCY LIGHTS NR 1 AND NR 2 INOPERABLE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY IAW AMM 33-51-04. OPERATIONS CHECK GOOD.
- [SDR REXA2013020500091](https://openairdocs.org/sdr/REXA2013020500091.md): Structure · damaged · Feb 4, 2013 · N8940E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > GOUGE/PUNCTURE IS AT FS 250.00 AND STRINGER 12A. DAMAGE AREA IS 28" LONG, 11" TALL, 1 1/4" DEEP WITH A 9" CUT. REPAIRED IAW BOMBARDIER REO 601R-53-11-2451.
- [SDR REXA0830201201302](https://openairdocs.org/sdr/REXA0830201201302.md): Windshield · cracked · Aug 30, 2012 · N8940E · Cndair CL6002B19 · Flight Compartment Windows
  > LEFT WINDSHIELD CRACKED DESCENDING THROUGH 6000 FT. REMOVED AND REPLACED WINDSHIELD IAW AMM 56-11-01. OPS CHECKED NORMAL.
- [SDR REXA2012061100850](https://openairdocs.org/sdr/REXA2012061100850.md): Stiffener · chafed · Jun 11, 2012 · N8940E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD AFT VERTICAL STIFFENER AT BL0 CHAFED 0.3 INCH BY 0.1 INCH BY 0.015 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-1523.
- [SDR REXA2012052200770](https://openairdocs.org/sdr/REXA2012052200770.md): Life Vest · unserviceable · May 22, 2012 · N8940E · Cndair CL6002B19 · Life Jacket
  > OBSERVERS LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012063000754](https://openairdocs.org/sdr/REXA2012063000754.md): Life Vest · unserviceable · May 20, 2012 · N8940E · Cndair CL6002B19 · Life Jacket
  > FLIGHT ATTENDANT LIFE VEST BAG TORN. REMOVED AND REPLACED FLIGHT ATTENDANT LIFE VEST IAW AMM 25-61-03.

Next page: https://openairdocs.org/aircraft/N8940E/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 = 'N8940E' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8940E/reports

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