# Service difficulty reports: N8903A, cancelled Dec 23, 2024

A list on [N8903A, cancelled Dec 23, 2024](https://openairdocs.org/deregistered/N8903A-2024-12-23.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 · 63 reports

- [SDR REXA2022081601867](https://openairdocs.org/sdr/REXA2022081601867.md): Inverter · inoperative · Aug 6, 2022 · N8903A · Cndair CL6002B19 · Emergency Lighting
  > LH INTERIOR EMERGENCY DOOR BOTTON SIGN INOP. R/R INVERTER @ LOCATION FS 424L IAW CRJ 200 AMM 31-5-07. OPS CHECK GOOD. PN ON/OFF 5925-7.
- [SDR SWIA2020022748868](https://openairdocs.org/sdr/SWIA2020022748868.md): Warning Message · multiple fail · Feb 27, 2020 · N8903A · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER TAKE WE GOT STEERING INOP CAUTION MESSAGE. FOLLOW BY A WOW IMPUT CAUTION AND A WOW OUTPUT FAIL STATUS MESSAGE C/W QRH AND RETURN TO FIELD WITH NO OVER WEIGHT LANDING FLIGHT 3610 - FILED CLOSED THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 20547984 WI
- [SDR SWIA20190405731](https://openairdocs.org/sdr/SWIA20190405731.md): Uplock · failed · Apr 4, 2019 · N8903A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON APPROACH RIGHT GEAR DISAGREE WARNING MESSAGE. CYCLED GEAR, ALL THREE GREEN INDICATION. LANDED WITHOUT INCIDENT. (FLT#7427) REMOVED AND REPLACED RT MLG UPLOCK ASSY IAW AMM. OPS AND LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA2018060444750](https://openairdocs.org/sdr/SWIA2018060444750.md): Strap · corroded · May 20, 2018 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CABIN FLOORBEAM STRAP CORRODED AT BS 559, LBL 35. REMOVE AND REPLACED THE STRAP IAW SRM.
- [SDR SWIA2018060444749](https://openairdocs.org/sdr/SWIA2018060444749.md): Floorbeam · corroded · May 12, 2018 · N8903A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM FITTING AT BS 615, LBL 27 HAD CORROSION ON THE OTBD FLANGE. PERFORMED A REPAIR TO THE FLOORBEAM IAW REO.
- [SDR SWIA2018060444748](https://openairdocs.org/sdr/SWIA2018060444748.md): Floor Support · corroded · May 11, 2018 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 27 FLOOR SUPPORT UPPER CAP INBOARD AND OUTBOARD FLANGES CORRODED BETWEEN BS 569 AND 610. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.
- [SDR SWIA2018060444747](https://openairdocs.org/sdr/SWIA2018060444747.md): Floor Support · corroded · May 11, 2018 · N8903A · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT FLOOR SUPPORT CORRODED AT NUTPLATE LOCATIONS BETWEEN BS 574 AND 621 AND ONE SHEARED RIVET AT BS 589. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.
- [SDR SWIA2018060444746](https://openairdocs.org/sdr/SWIA2018060444746.md): Skin · chafed · May 8, 2018 · N8903A · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE LEADING EDGE SKIN CHAFED NEAR OTBD END. REPLACED THE FLAP VANE LEADING EDGE SKIN IAW SRM.
- [SDR SWIA2018060444745](https://openairdocs.org/sdr/SWIA2018060444745.md): Skin · chafed · May 8, 2018 · N8903A · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE LEADING EDGE SKIN CHAFED NEAR INBD END. REMOVED AND REPLACED FLAP VANE IAW SRM.
- [SDR SWIA2018060444744](https://openairdocs.org/sdr/SWIA2018060444744.md): Vane · chafed · May 8, 2018 · N8903A · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE TRAILING EDGE UPPER SURFACE CHAFED NEAR THE INBD END OF VANE. BLENDED THE DAMAGE IAW SRM AND REO.
- [SDR SWIA201642205](https://openairdocs.org/sdr/SWIA201642205.md): Vane · chafed · May 20, 2016 · N8903A · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE L/E MIDDLE SECTION CHAFED. R & R LT INBD FLAP VANE L/E MIDDLE SECTION AT APPROXIMATELY LT WS 93 - 130 IAW SRM AND EA.
- [SDR SWIA201642204](https://openairdocs.org/sdr/SWIA201642204.md): Vane · chafed · May 17, 2016 · N8903A · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE LE CHAFED INBD SIDE. THE L/E SECTION WAS REMOVED, NEW OTBD MID SECTION, PN: 601R14303-52, WAS INSTALLED IAW SRM.
- [SDR SWIA201541253](https://openairdocs.org/sdr/SWIA201541253.md): Battery Pack · inoperative · Jun 4, 2015 · N8903A · Cndair CL6002B19 · Emergency Lighting
  > ALL EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED NR 1 AND 2 EMERGENCY BATTERY PACKS IAW AMM. OPS CHECKED GOOD.
- [SDR REXA2014100301015](https://openairdocs.org/sdr/REXA2014100301015.md): Light · inoperative · Oct 3, 2014 · N8903A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY STRIP LIGHT AT 1C INOPERATIVE. R & R EMER FLOOR LIGHT STRIP AT 1C IAW AMM 33-51-01. OPERATIONS CHECKED GOOD, OK FOR SERVICE.
- [SDR REXA2014092701001](https://openairdocs.org/sdr/REXA2014092701001.md): Door Seal · dirty · Sep 27, 2014 · N8903A · Cndair CL6002B19 · Passenger/Crew Doors
  > LOUD SQUEAL FROM MAIN CABIN DOOR DURING DESCENT. PRESSURIZATION WAS NORMAL. INSPECTED DOOR SEAL & CLEANED SEAL IAW 52-11-10. OPERATIONS CHECKED DOOR, NO DEFECT NOTED, OK FOR SERVICE.
- [SDR REXA2014060200546](https://openairdocs.org/sdr/REXA2014060200546.md): B-Nut · loose · Jun 2, 2014 · N8903A · Cndair CL6002B19 · APU Engine Fuel and Control
  > GOT A VERY STRONG SMELL OF FUEL IN FLIGHT CHECK WITH THE FLIGHT ATTENDANT & SHE DID NOT SMELL ANYTHING IN THE CABIN, ALL INDICATIONS NORMAL. WORE O2 MASK TO LANDING AS A PRECAUTION. AFTER LANDING SMELL PERSISTED. TIGHTENED B NUT AT APU FUEL CONTROL UNIT & S
- [SDR REXA2014052800531](https://openairdocs.org/sdr/REXA2014052800531.md): Connector · not seated · May 28, 2014 · N8903A · Cndair CL6002B19 · Light System Wiring
  > FLOOR TRACK EMERGENCY LIGHT STRIP INOPERATIVE ROW 1. RESEATED CONNECTOR FOR AFFECTED STRIP OPERATIONS CHECKED GOOD IAW AMM 33-51-21.
- [SDR REXA2014041800389](https://openairdocs.org/sdr/REXA2014041800389.md): Battery · discharged · Apr 18, 2014 · N8903A · Cndair CL6002B19 · Emergency Equipment
  > ON PREFLIGHT FOUND FIRST OFFICER'S FLASHLIGHT DEAD. REPLACED BATTERY IN FLASHLIGHT IAW STANDARDS PRACTICES CH 20.
- [SDR REXA2014041600067](https://openairdocs.org/sdr/REXA2014041600067.md): Skin · corroded · Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER WING PLANK ACCESS HOLE FOR PANEL 510AB HAS CORROSION MEASURING 10" X 0.185" X 0.007" DEEP. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014041400064](https://openairdocs.org/sdr/REXA2014041400064.md): Skin · corroded · Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK ACCESS HOLE 540DB HAS CORROSION AROUND NON-CRITICAL REGION, MEASURING 4 INCHES X 0.185 INCHES X 0.001 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014041400063](https://openairdocs.org/sdr/REXA2014041400063.md): Skin · gouged · Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER SKIN SURFACE GOUGED ADJACENT TO ACCESS PANEL 650LB APPROX WS 341. REPAIRED IAW SRM 57-21-31.
- [SDR REXA201404140062](https://openairdocs.org/sdr/REXA201404140062.md): Angle · corroded · Apr 11, 2014 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 621 ANGLE BETWEEN LBL 9 & LBL 27 HAS CORROSION AROUND 2 FASTENER HOLES MEASURING 0.007 INCHES DEEP MAX. REPAIRED IAW SRM 53-00-00.
- [SDR REXA2014041400061](https://openairdocs.org/sdr/REXA2014041400061.md): Fitting · cracked · Apr 11, 2014 · N8903A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD LINTEL FITTING CRACKED. REPAIRED IAW REO 601R-53-61-1230.
- [SDR REXA2014041300057](https://openairdocs.org/sdr/REXA2014041300057.md): Skin · corroded · Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER PLANK ACCESS HOLE 650AB HAS CORROSION AT NON-CRITICAL AREAS 2.0 INCHES X 0.185 INCHES X 0.002 INCHES DEEP AT WS 163.00. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014041300056](https://openairdocs.org/sdr/REXA2014041300056.md): Skin · corroded · Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER PLANK ACCESS HOLE 640DB HAS CORROSION AT NON-CRITICAL AREAS 2.0 INCHES X 0.185 INCHES X 0.001 INCHES DEEP AT WS 95.95. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014041300055](https://openairdocs.org/sdr/REXA2014041300055.md): Skin · corroded · Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER PLANK ACCESS HOLE 640BB HAS CORROSION AT NON-CRITICAL AREAS 7.0 INCHES X 0.185 INCHES X 0.002 INCHES DEEP AT WS 54.897. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014041300054](https://openairdocs.org/sdr/REXA2014041300054.md): Skin · corroded · Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER PLANK ACCESS HOLE 610AB HAS CORROSION AT NON-CRITICAL AREAS 3.75 INCHES X 0.185 INCHES X 0.002 INCHES DEEP AT WS 12.245. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014041200053](https://openairdocs.org/sdr/REXA2014041200053.md): Skin · corroded · Apr 10, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER WING PLANK ACCESS HOLE 650FB HAS CORROSION AT NON-CRITICAL AREAS MEASURING 1.0 INCHES X 0.185 INCHES X 0.002 INCHES DEEP AT WS 274.319. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014041200052](https://openairdocs.org/sdr/REXA2014041200052.md): Skin · corroded · Apr 10, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER WING PLANK ACCESS HOLE 650BB HAS CORROSION AT NON-CRITICAL AREAS MEASURING 1.75 INCHES X 0.185 INCHES X 0.001 INCHES DEEP AT WS 188.04. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014040800049](https://openairdocs.org/sdr/REXA2014040800049.md): Bulkhead · dented · Apr 8, 2014 · N8903A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 PRESS BULKHEAD FWD SIDE HAS A DENT APPROXIMATELY 6 INCHES OTBD OF RBL 27 & 8 INCHES UP FROM THE FLOOR MEASURING 3.45 INCHES X 3.4 INCHES X 0.041 INCHES DEEP. REPAIRED IAW REO 601R-53-61-5251.
- [SDR REXA2014041000050](https://openairdocs.org/sdr/REXA2014041000050.md): Bulkhead · chafed · Apr 7, 2014 · N8903A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD FWD SIDE HAS 10 MARKS FROM FASTENERS CHAFE BETWEEN 15 INCHES & 30 INCHES FROM FLOOR & LBL 27 & RBL 27.5 UP TO 0.008 INCHES DEEP. REPAIRED IAW REO 601R-53-61-2155.
- [SDR REXA2014040500044](https://openairdocs.org/sdr/REXA2014040500044.md): Skin · gouged · Apr 2, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/Skin
  > GOUGE IN THE RT LOWER WING SKIN AT WS 330.25. THE AREA AFTER CLEAN UP MEASURES 1.90” X.800” X.003” DEEP. REPAIRED IAW CRJ257-02409.
- [SDR REXA2014040500046](https://openairdocs.org/sdr/REXA2014040500046.md): Fitting · cracked · Apr 1, 2014 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 OTBD CLIP AT RBL 9 CRACKED. REPAIRED IAW REO 601R-53-11-171.
- [SDR REXA2014040400042](https://openairdocs.org/sdr/REXA2014040400042.md): Skin · corroded · Apr 1, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/Skin
  > RT & LT LOWER WINGS SKINS AT AFT EDGES OF PANEL 193AB FRETTING CORROSION & CHAFFING. RT SIDE 0.025" DEEP. LT SIDE 0.015" DEEP. REPAIRED IAW REO 601R-57-21-880.
- [SDR REXA2014040300041](https://openairdocs.org/sdr/REXA2014040300041.md): Skin · gouged · Apr 1, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER SKIN SURFACE GOUGED ADJACENT TO ACCESS PANEL 650LB. BLENDED AND IS WITHIN LIMITS IAW SRM 57-21-31.
- [SDR REXA2014032000308](https://openairdocs.org/sdr/REXA2014032000308.md): Flap · malfunctioned · Mar 20, 2014 · N8903A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL EICAS, OCCURRED IN FLT ON APPROACH DURING FLAP EXTENSION. FAILED AT FLAP 30 DEG, AIRSPEED 160, TIME INTO FLIGHT 1 HR 10MIN. OAT +5 DEG C TAT. COMPLETED CB RESET OF FLAP SYS. COMPLETED 5 CONSECUTIVE FLAP CYCLES. DEFERRED FLAPS SYS IAW MEL 27-50-
- [SDR REXA2014030400252](https://openairdocs.org/sdr/REXA2014030400252.md): Seal · missing · Mar 4, 2014 · N8903A · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT DECK PBE IS MISSING A SEAL. RE SECURED FLIGHT DECK PBE SEAL IAW CRJ AMM 25-63-00.
- [SDR REXA2013101001769](https://openairdocs.org/sdr/REXA2013101001769.md): Light · damaged · Oct 10, 2013 · N8903A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT FLOODLIGHT ON GALLEY BY SERVICE DOOR DAMAGED. REPLACED EMERGENCY LIGHT IAW AMM 33-51-19. OPS TESTED OK.
- [SDR REXA2013011400144](https://openairdocs.org/sdr/REXA2013011400144.md): Life Vest · unserviceable · Jan 14, 2013 · N8903A · Cndair CL6002B19 · Life Jacket
  > ONE INFANT LIFE VEST BAG TORN. COMPLIED WITH PA 25-096A BY INSTALLING INFANT LIFE VEST.
- [SDR REXA2083001201301](https://openairdocs.org/sdr/REXA2083001201301.md): Bracket · cracked · Aug 30, 2012 · N8903A · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT ENGINE THRUST REVERSER STOW SWITCH BRACKET CRACKED. REMOVED AND REPLACED THRUST REVERSER SWITCH MOUNTING PLATE ASSY IAW AMM 78-37-01. OPS CHECKED GOOD.
- [SDR REXA2012082301091](https://openairdocs.org/sdr/REXA2012082301091.md): Angle · cracked · Aug 22, 2012 · N8903A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK FOUND IN FS 559 SEMI-PRESSURE BULKHEAD CAP ANGLE AT RBL18 AND LBL18. REPAIRED IAW REO 601R-53-41-260 AND 601R-53-41-609.
- [SDR REXA2012071301155](https://openairdocs.org/sdr/REXA2012071301155.md): Light · inoperative · Jul 13, 2012 · N8903A · Cndair CL6002B19 · Emergency Lighting
  > CABIN OVERHEAD EMERGENCY EXIT FLOOD LIGHT AT SEAT 3B INOPERATIVE.
- [SDR REXA2012041000493](https://openairdocs.org/sdr/REXA2012041000493.md): Switch · failed · Apr 10, 2012 · N8903A · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT THRUST REVERSER WOULD NOT DEPLOY ON LANDING. REMOVED AND REPLACED RT THRUST REVERSER DEPLOY SWITCH IAW AMM 78-37-01. OPS CHECKED GOOD, OK FOR SERVICE.
- [SDR REXA201100726](https://openairdocs.org/sdr/REXA201100726.md): Sensing Element · defective · Oct 14, 2011 · N8903A · Cndair CL6002B19 · Pneumatic Indicating System
  > RT 14TH DUCT MASTER WARNING ON CLIMBOUT - FORWARD SECTION OF ENGINE BLEED SHOWED RED. REMOVED AND REPLACED RT 14TH STAGE PYLON DUCT HEAT SENSE ELEMENT A 58WK IAW AMM 36-21-04 OPC NORMAL. RT COWL ANTI-ICE OPC NORMAL IAW AMM 30-22-00. PART EFFECTIVITY VERIFIE
- [SDR REXA201100664](https://openairdocs.org/sdr/REXA201100664.md): Bulkhead · cracked · Oct 7, 2011 · N8903A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 202.75 BULKHEAD HAS A CRACK INDICATION LOCATED AT 9 O’CLOCK POSITION AT THE PASS THROUGH HOLE (REF PA 53-015). REPAIRED IAW BOMBARDIER REO 601R-53-11-563 AND BOMBARDIER SERVICE CORPORATION STANDARD REPAIR 601R-53-0101A.
- [SDR REXA201100549](https://openairdocs.org/sdr/REXA201100549.md): Structure · damaged · Aug 3, 2011 · N8903A · Cndair CL6002B19 · Rudder Miscellaneous Structure
  > RUDDER DAMAGE AT RS 131.17 TO RS 133.33 FWD LT SIDE DAMAGE IS APPROX 1.5L X 1.2W. REPAIRED IAW BOMBARDIER REO 601R-55-41-140.
- [SDR REXA201100463](https://openairdocs.org/sdr/REXA201100463.md): Floor Support · cracked · Jul 18, 2011 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT INTERCOSTAL AT FS 484.0 IS CRACKED AT RBL 36.0. REPAIRED IAW REO 601R-53-41-059 AND BSC S/R 601R-53-00030B.
- [SDR REXA201100462](https://openairdocs.org/sdr/REXA201100462.md): Intercostal · cracked · Jul 18, 2011 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT INTERCOSTAL AT FS 484.0 IS CRACKED AT LBL 36.0. REPAIRED IAW REO 601R-53-41-059 AND BSC S/R 601R-53-00030B.
- [SDR REXA201100464](https://openairdocs.org/sdr/REXA201100464.md): Structure · corroded · Jul 17, 2011 · N8903A · Cndair CL6002B19 · Fuselage Main, Structure
  > MINOR CORROSION AROUND FASTENERS FROM FS 559+16 - FS 559+32 STR 26L TO 26R. REMOVED MINOR CORROSION AROUND FASTENERS FROM FS 559+16 TO FS 559+32 STR 26L TO 26R IAW SRM 51-21-06.
- [SDR REXA201100497](https://openairdocs.org/sdr/REXA201100497.md): Sill · corroded · Jul 16, 2011 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TWO EACH NUT PLATE HOLES HAVE MINOR CORROSION AT FS 559+96 RBL 45 ON FLOOR SILL. REPAIRED IAW BOMBARDIER SERVICES CORP EO 601R-53-L00118 AND ASSOCIATED 8110-3 DATED 7/8/11.

Next page: https://openairdocs.org/deregistered/N8903A-2024-12-23/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 = 'N8903A' AND deregistration_id = 'N8903A-2024-12-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8903A-2024-12-23/reports

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