# Service difficulty reports: N8933B

A list on [N8933B](https://openairdocs.org/aircraft/N8933B.md).

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

- [SDR REXA2021122301184](https://openairdocs.org/sdr/REXA2021122301184.md): Post · cracked · Dec 23, 2021 · N8933B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > "DUIRNG COMPLIANCE OF TC 53-160-604(NDTM PART 9 53-41-116) NOTED VERT P OST RBL 27.00 CRACKED @ FS409.0+128. CRACK ON I/B LWR FLANGE FROM EDGE EXTENDING UP BETWEEN 1ST AND 2ND FASTENERS " COMPLIED WITH REO 601R-53-056
- [SDR REXA2021122301183](https://openairdocs.org/sdr/REXA2021122301183.md): Post · cracked · Dec 23, 2021 · N8933B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > "DURING COMPLIANCE OF TC 53-160-604(NDTM PART 9 53-41-116) NOTED VERTIC AL POST LBL 27.00 @ FS409.0+128 IS CRACKED. CRACK ON I/B LWR FLANGE EX TENDING UP TO AND PAST 1ST RIVET ENDING BETWEEN 1ST AND 2ND RIVETS " COMPLIED WITH REO 601R-53-41-056
- [SDR SWIA2019050845869](https://openairdocs.org/sdr/SWIA2019050845869.md): Sensor · faulty · May 7, 2019 · N8933B · Cndair CL6002B19 · Power Indicating System
  > ON CLIMB OUT LT ENGINE N1 WAS FLUCTUATING/SURGING. (FLT#7434) FO: 05/08/2019 CLOSED REMOVED AND REPLACED LT T2 SENSOR AND LT ENGINE CONTROL AMPLIFIER IAW AMM. OPS CHECK GOOD.
- [SDR SWIA2017120543968](https://openairdocs.org/sdr/SWIA2017120543968.md): Warning System · activated · Nov 10, 2017 · N8933B · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT ENGINE THRUST REVERSER UNLOCK CAUTION INFLIGHT. PER QRH SHUT DOWN LEFT ENGINE. DECLARED EMERGENCY. (FLT 4776) DEFERRED LT T/R IAW MEL.
- [SDR SWIA2017103143933](https://openairdocs.org/sdr/SWIA2017103143933.md): Shim · worn · Oct 24, 2017 · N8933B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL PLATE SHIM IS WORN. (C-CHECK) REMOVED AND REPLACED WITH NEW SERVICE DOOR SILL PLATE SHIM PN: 601R38695-19.
- [SDR SWIA2017103143936](https://openairdocs.org/sdr/SWIA2017103143936.md): Floorbeam · corroded · Oct 13, 2017 · N8933B · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED. (C-CHECK) REMOVED AND REPLACED CARGO FLOORBEAM IAW SRM.
- [SDR SWIA2017103143935](https://openairdocs.org/sdr/SWIA2017103143935.md): Intercostal · corroded · Oct 13, 2017 · N8933B · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL CORRODED. (C-CHECK) REMOVED AND REPLACED INTERCOSTAL IAW SRM.
- [SDR SWIA2017103143934](https://openairdocs.org/sdr/SWIA2017103143934.md): Skin · dented · Oct 7, 2017 · N8933B · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > BELOW RT 3RD PAX WINDOW, ONE SMALL DENT. (C-CHECK) REPAIRED DENT IAW SRM.
- [SDR SWIA201642800](https://openairdocs.org/sdr/SWIA201642800.md): Sensor · malfunctioned · Nov 6, 2016 · N8933B · Cndair CL6002B19 · Pneumatic Distribution System
  > RIGHT ENGINE BLEED AIR DUCT WARNING MESSAGE AT 4000 FEET AND AGAIN AT 7500 FEET. RAN QRH. REMOVED AND REPLACED BLEED LEAK SENSING ELEMENT A46WK FOR RT ENGINE IAW AMM.
- [SDR SWIA201541542](https://openairdocs.org/sdr/SWIA201541542.md): Web · corroded · Nov 6, 2015 · N8933B · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT STAIR WEB CORRODED ON INTERNAL SIDE ABOVE ACCESS PANEL 832HR. R & R AFT WEB PANEL IAW SRM.
- [SDR SWIA201541541](https://openairdocs.org/sdr/SWIA201541541.md): Vane · damaged · Nov 6, 2015 · N8933B · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE CHAFED ON L/E NEAR FLAP, BS 105, CENTER. REMOVED CHAFE FROM LT INBD FLAP VANE ON L/E NEAR FLAP 105, CENTER IAW REO. R & R LT INBD FLAP VANE L/E CENTER SECTION CAP WITH NEW FABRICATED CAP IAW SRM.
- [SDR SWIA201541540](https://openairdocs.org/sdr/SWIA201541540.md): Vane · chafed · Nov 6, 2015 · N8933B · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE CHAFED ON L/E NEAR FLAP BS 57, INBOARD. REMOVED CHAFE FROM LT INBD FLAP VANE ON L/E NEAR FLAP BS 57, INBOARD, IAW REO.
- [SDR SWIA201541539](https://openairdocs.org/sdr/SWIA201541539.md): Skin · corroded · Nov 6, 2015 · N8933B · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INNER SKIN CORRODED UNDER EDGE MEMBERS BELOW TOP STEP. R & R PAX DOOR INNER SKIN IAW SRM.
- [SDR REXA2014111700913](https://openairdocs.org/sdr/REXA2014111700913.md): Skin · mechanic error · Nov 14, 2014 · N8933B · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING INSPECTION FOUND A DRILL START ON THE FUSELAGE SKIN AT THE FWD POTABLE WATER DRAIN MAST. THE DAMAGE MEASURES.757 INCHES X.382 INCHES X.061 INCHES DEEP. REPAIRED IAW EA CRJ253-03084.
- [SDR REXA2014110101107](https://openairdocs.org/sdr/REXA2014110101107.md): Motor · malfunctioned · Nov 1, 2014 · N8933B · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN PAX DOOR ASSIST CABLE JAMMED. R & R PAX DOOR POWER ASSIST MOTOR IAW AMM 52-11-08. OPERATIONS CHECKED GOOD. THIS CLEARS MEL MM02 CLEARED PLACARD REMOVED. PN ON OFF 897889-2 SN ON 65037EL SN OFF 0450.
- [SDR REXA2014071200694](https://openairdocs.org/sdr/REXA2014071200694.md): Light · inoperative · Jul 12, 2014 · N8933B · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS IN CABIN ON FLOOR DO NOT LIGHT UP FROM OVERWING EXIT AFT. R & R LUMINESCENT STRIP. PERFORMED OPERATIONAL TEST PASSED AT ROW 8 IAW AMM 33-51-01.
- [SDR REXA2014071100692](https://openairdocs.org/sdr/REXA2014071100692.md): Connector · disconnected · Jul 11, 2014 · N8933B · Cndair CL6002B19 · Light System Wiring
  > EXIT LIGHTS IN CABIN FROM OVERWING EXIT AFT DO NOT LIGHT UP. RECONNECT AFT CONNECTOR & OPERATIONS CHECKED GOOD IAW 33-51-01.
- [SDR REXA2014070800688](https://openairdocs.org/sdr/REXA2014070800688.md): Defibrillator · unserviceable · Jul 8, 2014 · N8933B · Cndair CL6002B19 · Emergency Equipment
  > AED KIT MISSING SECURITY TAPE & FIRST RESPONDER TAB RIPPED. R & R AED IAW AMM 25-60-10.
- [SDR REXA2014070400669](https://openairdocs.org/sdr/REXA2014070400669.md): Battery · discharged · Jul 4, 2014 · N8933B · Cndair CL6002B19 · Emergency Lighting
  > AFT CABIN EMER LIGHTS INOPERATIVE. R & R NR 3 & 4 EMER LIGHT BATTERIES IAW AMM 33-51-04. OPERATIONS CHECKED GOOD OK FOR SERVICE.
- [SDR REXA2014021400208](https://openairdocs.org/sdr/REXA2014021400208.md): Apu · contaminated · Feb 14, 2014 · N8933B · Cndair CL6002B19 · APU Core Engine
  > HALFWAY THROUGH TAKEOFF ROLL, SMOKE STARTED COMING OUT FLIGHT DECK VENTS. AFTER AIRBORNE, CREW DONNED O2 MASKS, GEAR WAS RETRACTED, EMERGENCY WAS DECLARED. ACCOMPLISHED QRH, LANDED 10 MIN AFTER TAKEOFF AT 51000 LBS GROSS WT, 4000 LB ABOVE MAX LANDING WT. RA
- [SDR REXA2014012900147](https://openairdocs.org/sdr/REXA2014012900147.md): Connector · loose · Jan 29, 2014 · N8933B · Cndair CL6002B19 · Landing Gear System Wiring
  > CREW REPORTED GEAR DISAGREE WHILE ON APPROACH TO LAND, BOTH MLG SHOW IN THE UP POSITION. CREW FOLLOWED QRH & ON 2ND ATTEMPT TO GET GEAR DOWN STILL HAD DISAGREE. DID AN EMERGENCY EXTENSION & ALL GEAR & DOORS DOWN & LOCKED. CREW DID NOT DECLARE AN EMERGENCY.
- [SDR REXA2014010300106](https://openairdocs.org/sdr/REXA2014010300106.md): Pbe · defective · Jan 3, 2014 · N8933B · Cndair CL6002B19 · Emergency Equipment
  > AFT PBE APPEARS DEFECTIVE. R & R AFT PBE IAW ESSEX CMM PRM-01. OK FOR SERVICE.
- [SDR REXA2013122902423](https://openairdocs.org/sdr/REXA2013122902423.md): Battery Pack · inoperative · Dec 29, 2013 · N8933B · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT HAS NO FLASHING LIGHT SHOWING CHARGED. REPLACED FLASHLIGHT BATTERY IAW AMM 25-61-00. OPS CHECKED GOOD.
- [SDR REXA2013122302323](https://openairdocs.org/sdr/REXA2013122302323.md): Access Panel · corroded · Dec 20, 2013 · N8933B · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING PLANK FUEL ACCESS PANEL 540BB CUTOUT CORRODED. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2013122302322](https://openairdocs.org/sdr/REXA2013122302322.md): Access Panel · corroded · Dec 20, 2013 · N8933B · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING FUEL ACCESS PANEL 510AB CUTOUT AT WS 12.245 CORRODED. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2013122302321](https://openairdocs.org/sdr/REXA2013122302321.md): Access Panel · corroded · Dec 20, 2013 · N8933B · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING FUEL ACCESS PANEL 510BB CUTOUT AT WS 32.263 CORRODED. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2013122302320](https://openairdocs.org/sdr/REXA2013122302320.md): Skin · corroded · Dec 20, 2013 · N8933B · Cndair CL6002B19 · Wing, Plate/Skin
  > REMOVED LIGHT SURFACE CORROSION AT LANDING FOR PANEL 540BB, LT WS54.897, WITH MAXIMUM MATERIAL LOSS OF 0.001". REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2013122302319](https://openairdocs.org/sdr/REXA2013122302319.md): Skin · corroded · Dec 20, 2013 · N8933B · Cndair CL6002B19 · Wing, Plate/Skin
  > REMOVED LIGHT SURFACE CORROSION AT LT WS 54.681 WITH NO PITTING FOUND AND NO MATERIAL LOSS NOTED. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2013122202318](https://openairdocs.org/sdr/REXA2013122202318.md): Bulkhead · damaged · Dec 18, 2013 · N8933B · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD HAS DAMAGE. REPAIRED IAW REO 601R-53-61-2155.
- [SDR REXA2013012600201](https://openairdocs.org/sdr/REXA2013012600201.md): Engine · vibration · Jan 26, 2013 · N8933B · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ON FLIGHT 3938 (DTW TO ORF) SHORTLY AFTER DEPARTURE CREW LOST THE RIGHT ENGINE. IN FLIGHT SHUTDOWN OCCURRED ON NUMBER 2 ENGINE DUE TO SUSPECTED ENGINE DAMAGE. OCCURRED UPON PASSING 11000 MSL LOUD VIBRATION NOISE AND ITT IN THE RED. CREW DECLARED AN EMERGENC
- [SDR REXA2012121301773](https://openairdocs.org/sdr/REXA2012121301773.md): Switch · contaminated · Dec 13, 2012 · N8933B · Cndair CL6002B19 · Rudder Tab Control System
  > SYR-DTW, DIVERTED TO BUF FOR RUDDER TRIM RUNAWAY. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT, EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE SWITCH WAS CONTAMINATED (APPEARED TO BE COFFEE). CLEANED SWITCH AND RE-ADJUSTED THE KNOB TO WHERE IT IS NOT FLUSH ON T
- [SDR REXA2012052900697](https://openairdocs.org/sdr/REXA2012052900697.md): Bulkhead · chafed · May 27, 2012 · N8933B · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 PRESSURE BULKHEAD WEB CHAFED 14 PLACES ABOVE WL 73.5, 0.001 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
- [SDR REXA2012040600466](https://openairdocs.org/sdr/REXA2012040600466.md): Flashlight · inoperative · Apr 6, 2012 · N8933B · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-61-02. OK CHECKED GOOD.
- [SDR REXA201101022](https://openairdocs.org/sdr/REXA201101022.md): Pbe · unserviceable · Dec 26, 2011 · N8933B · Cndair CL6002B19 · Emergency Equipment
  > FOUND PBE SPONGY RED INDICATOR POP. REMOVED AND REPLACED COCKPIT PBE IAW AMM 35-30-00.
- [SDR REXA201100912](https://openairdocs.org/sdr/REXA201100912.md): Loop · out of position · Dec 6, 2011 · N8933B · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > ANTI ICE DUCT WARNING. REPOSITIONED LOOP FOR 14TH STAGE IN LT WHEEL BIN AREA - GND CHECKS ARE NORMAL PER CRJ AMM 30-11-00.
- [SDR REXA201100821](https://openairdocs.org/sdr/REXA201100821.md): Skin · corroded · Dec 2, 2011 · N8933B · Cndair CL6002B19 · Wing, Plate/Skin
  > FUEL PANEL CUTOUT ON WING LOWER PLANK AT WS 54.897 CORRODED 0.006" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-21-030 REV H.
- [SDR REXA201100820](https://openairdocs.org/sdr/REXA201100820.md): Bulkhead · damaged · Dec 2, 2011 · N8933B · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FORWARD FACE GOUGED AND CHAFED AT MULTIPLE LOCATIONS. REPAIR IAW BOMBARDIER REO 601R-53-61-4306.
- [SDR REXA201100822](https://openairdocs.org/sdr/REXA201100822.md): Support Fitting · cracked · Dec 1, 2011 · N8933B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 LBL 9 I/B SUPPORT CLIP CRACKED. REPAIRED IAW SRM 51-24-21, 51-21-11, 51-25-06, 51-25-16, 51-42-21.
- [SDR REXA201000227](https://openairdocs.org/sdr/REXA201000227.md): Skin · punctured · Oct 28, 2010 · N8933B · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PUNCTURE THROUGH THE SKIN BETWEEN FS 625 AND FS 640 BETWEEN STRINGER 25L AND 26L. THE DAMAGE IS FULLY CONTAINED WITHIN A BAY. THE PUNCTURE IS.4” ROUND. REPAIRED IAW BOMBARDIER REO 601R-53-61-3871.
- [SDR REX2008F00015](https://openairdocs.org/sdr/REX2008F00015.md): Adg · unwanted deploy · Jul 9, 2008 · N8933B · Cndair CL6002B19 · Phase Adapter
  > ON A REPOSITIONING FLIGHT, AT FL310, THE AIR DRIVEN GENERATOR (ADG) DEPLOYED WITHOUT WARNING. THE FLIGHT CREW VERIFIED THAT ALL AIRCRAFT GENERATORS WERE ON LINE AT THE TIME OF DEPLOYMENT. THE FLIGHT CREW NOTIFIED ATC, DECLARED AN EMERGENCY AND REQUESTED THE
- [SDR REXA04013](https://openairdocs.org/sdr/REXA04013.md): Sensor · out of position · Jul 3, 2004 · N8933B · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON DESCENT, RECEIVED GEAR DISAGREE (NOSE DOOR). QRH FOLLOWED HOWEVER, INDICATION REMAINED. GEAR MANUALLY LOWERED, RECEIVED 3 GREEN, UNEVENTFUL LANDING. NOSE GEAR PROXIMITY SENSOR FOUND TO BE OUT OF POSITION. ADJUSTED IAE MM 32-61-05, GEAR SWINGS PERFORMED
- [SDR REX2004F00004](https://openairdocs.org/sdr/REX2004F00004.md): Proximity Sensor · out of position · Jul 3, 2004 · N8933B · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON DESCENT RECEIVED GEAR DISAGREE (NOSE DOOR). QRH FOLLOWED HOWEVER, INDICATION REMAINED. GEAR MANUALLY LOWERED RECEIVED THREE GREEN, UNEVENTFUL LANDING. NOSE GEAR PROXIMITY SENSOR FOUND TO BE OUT OF POSITION. ADJUSTED IAW AMM, GEAR SWINGS PERFORMED AND OP

## 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 = 'N8933B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8933B/reports

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