# Service difficulty reports: N8672A

A list on [N8672A](https://openairdocs.org/aircraft/N8672A.md).

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

- [SDR REXA2014071500701](https://openairdocs.org/sdr/REXA2014071500701.md): First Aid Kit · unserviceable · Jul 15, 2014 · N8672A · Cndair CL6002B19 · Emergency Equipment
  > FIRST AID KIT IS MISSING ITS SEAL. R & R FIRST AID KIT IAW AMM 25-61-06.
- [SDR REXA2014032800336](https://openairdocs.org/sdr/REXA2014032800336.md): Wire · broken · Mar 28, 2014 · N8672A · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY FLOOR PATH LIGHTING FWD SECTION INOPERATIVE. FOUND WIRE BROKE AT TRANSITION CABLE, REPAIRED SPLICE CONNECTOR IAW EXPM 20-17-31.
- [SDR REXA2014022300235](https://openairdocs.org/sdr/REXA2014022300235.md): Life Vest · unserviceable · Feb 23, 2014 · N8672A · Cndair CL6002B19 · Life Jacket
  > FIRST OFFICER`S LIFE VEST BAG TORN. R & R FIRST OFFICER`S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2014022000227](https://openairdocs.org/sdr/REXA2014022000227.md): Landing Gear · obstructed · Feb 20, 2014 · N8672A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > RIGHT MAIN GEAR DID NOT COME UP AFTER TAKEOFF. QRH PROCEDURE WORKED. PERFORMED FUNCTIONAL CHECK OF LG IAW AMM 32-30-00, ALL CHECKED NORMAL. INSPECTED LG FOR DAMAGE OR CONTAMINATION, NOTHING FOUND, ALL CHECKED GOOD. SEE NON-ROUTINE CARDS FOR WORK DETAILS.
- [SDR REXA2013120602289](https://openairdocs.org/sdr/REXA2013120602289.md): Flashlight · inoperative · Dec 6, 2013 · N8672A · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN`S FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-61-04.
- [SDR REXA2013090801137](https://openairdocs.org/sdr/REXA2013090801137.md): Floor Support · corroded · Sep 4, 2013 · N8672A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT PRESSURE FLOOR SUPPORT HAS CORROSION ALONG THE ENTIRE LENGTH FROM FS 409+129 TO 559 WITH A MAX MATERIAL LOSS OF 0.015" DEEP. REPAIRED IAW REO 601R-53-41-666.
- [SDR REXA2013083101135](https://openairdocs.org/sdr/REXA2013083101135.md): Pressure Panel · damaged · Aug 29, 2013 · N8672A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PRESSURE PANEL 131AL HOLE 12 AND HOLE 31 HAVE BROKEN FREEZE PLUGS. REPAIRED IAW REO 601R-53-11-162.
- [SDR REXA2013083001134](https://openairdocs.org/sdr/REXA2013083001134.md): Access Panel · corroded · Aug 28, 2013 · N8672A · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING PLANK ACCESS HOLE FOR PANEL 540BB AT WS54.897 HAS PITTING AND CORROSION ON FAYING SURFACE. REPAIRED IAW REO 601R-57-21-030 AND 601R-57-21-1991.
- [SDR REXA2013083001133](https://openairdocs.org/sdr/REXA2013083001133.md): Access Panel · corroded · Aug 28, 2013 · N8672A · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING PLANK ACCESS HOLE FOR PANEL 510AB AT WS12.245 HAS PITTING AND CORROSION ON FAYING SURFACE. REPAIRED IAW REO 601R-57-21-030 AND 601R-57-21-1991.
- [SDR REXA2013082901132](https://openairdocs.org/sdr/REXA2013082901132.md): Access Panel · damaged · Aug 27, 2013 · N8672A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT FORWARD FUSELAGE ACCESS PANEL 131AL, HOLE LOCATION NR 31, PREVIOUS FREEZE PLUG IS LOOSE. REPAIRED IAW REO 601R-53-11-162.
- [SDR REXA2013082801131](https://openairdocs.org/sdr/REXA2013082801131.md): Access Panel · corroded · Aug 27, 2013 · N8672A · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING PLANK ACCESS HOLES FOR 540FB AND 540EB HAVE MINOR PITTING AND CORROSION IN NON-CRITICAL REGIONS. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2013082701128](https://openairdocs.org/sdr/REXA2013082701128.md): Floorbeam · corroded · Aug 26, 2013 · N8672A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > MX FOUND THE UPPER FLANGE OF THE FLOORBEAM AT FS 349 TO BE CORRODED BETWEEN RBL 32.75 AND 36 AND A 0.6" CRACK AT THE OTBD END OF THE FLOORBEAM UPPER FLANGE. REPAIRED IAW EA CRJ253-01874.
- [SDR REXA2013082601124](https://openairdocs.org/sdr/REXA2013082601124.md): Floorbeam · corroded · Aug 25, 2013 · N8672A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FLOORBEAM BETWEEN RBL 9 AND LBL 9 CORRODED ON FORWARD AND AFT ANGLES. REPAIRED IAW REO 601R-53-11-926.
- [SDR REXA2013082601123](https://openairdocs.org/sdr/REXA2013082601123.md): Floorbeam · damaged · Aug 25, 2013 · N8672A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM FS 280 AT LBL 9 INBD ANGLE CRACKED AT UPPER END DAMAGED. REPAIRED IAW REO 601R-53-11-926.
- [SDR REXA2013082601122](https://openairdocs.org/sdr/REXA2013082601122.md): Floorbeam · cracked · Aug 25, 2013 · N8672A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 AT RBL 9 INBD ANGLE CRACKED AT UPPER END. REPAIRED IAW REO 601R-53-11-926.
- [SDR REXA2013082601121](https://openairdocs.org/sdr/REXA2013082601121.md): Floorbeam · cracked · Aug 25, 2013 · N8672A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 AT RBL 9 OTBD ANGLE CRACKED AT UPPER END. REPAIRED IAW REO 601R-53-11-926.
- [SDR REXA2013082701127](https://openairdocs.org/sdr/REXA2013082701127.md): Bulkhead · damaged · Aug 24, 2013 · N8672A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 FORWARD SIDE OF BULKHEAD HAS 12 SCREW MARKS. REPAIRED IAW REO 601R-53-61-2155.
- [SDR REXA2013062101212](https://openairdocs.org/sdr/REXA2013062101212.md): Steering Sys · malfunctioned · Jun 21, 2013 · N8672A · Cndair CL6002B19 · Steering Unit
  > STEERING INOPERATIVE MESSAGE & LOSS OF STEERING CONTROL ON TOUCHDOWN. STOPPED ACFT ON RUNWAY AND RECYCLED NOSEWHEEL STEERING THREE TIMES BEFORE IT WOULD ENGAGE. PERFORMED OPS TEST OF NOSE WHEEL STEERING SYSTEM IAW 32-51-00. NO DEFECTS NOTED AT THIS TIME.
- [SDR REXA2013062001204](https://openairdocs.org/sdr/REXA2013062001204.md): Selector Valve · failed · Jun 20, 2013 · N8672A · Cndair CL6002B19 · Landing Gear Steering System
  > STEERING INOPERATIVE CAUTION ON LANDING, LOST NOSEWHEEL STEERING. NWS ECU FLAGGED, SOLENOID SELECTOR VALVE FAILED. REPLACED SOLENOID SELECTOR VALVE IAW AMM 32-51-25. ALL CHECKS GOOD.
- [SDR REXA2013060801072](https://openairdocs.org/sdr/REXA2013060801072.md): Warning Message · false activation · Jun 8, 2013 · N8672A · Cndair CL6002B19 · Drag Control System
  > SPOILERONS FAULT WHITE STATUS MESSAGE ON FLIGHT CONTROL PAGE. LEFT SPOILERON WAS WHITE DID RESET, FAILED. FOLLOWED MOC RESET PASSED. BOTH TIMES FAILED WHEN CONTROL CHECK DONE, ROLLING YOKE TO THE LEFT. IAW MOC, CYCLED CIRCUIT BREAKERS IAW FIM MESSAGE. CLEA
- [SDR REXA2013032300586](https://openairdocs.org/sdr/REXA2013032300586.md): Light · inoperative · Mar 23, 2013 · N8672A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTING STRIP SECTION, AISLE 6 AND 7 INOPERABLE. REMOVED AND REPLACED LIGHT STRIP SECTION IAW AMM 33-50-01. OPERATIONS CHECK GOOD.
- [SDR REXA2012100801392](https://openairdocs.org/sdr/REXA2012100801392.md): Life Vest · unserviceable · Oct 8, 2012 · N8672A · Cndair CL6002B19 · Life Jacket
  > ONE INFANT LIFE VEST HAS A HOLE IN PACKAGE. REMOVED AND REPLACED INFANT LIFE VEST IAW PA 25-096A.
- [SDR REXA2012070701050](https://openairdocs.org/sdr/REXA2012070701050.md): Door · out of adjust · Jul 7, 2012 · N8672A · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN PASSENGER DOOR WOULD NOT CLOSE WITHOUT MAINTENANCE ASSISTANCE. DOOR WOULD NOT OPEN WITHOUT FIRST OFFICER ASSISTANCE ON ARRIVAL. ADJUSTED MAIN PASSENGER DOOR IAW AMM 52-11-00. OPS CHECKED GOOD, OK FOR SERVICE.
- [SDR REXA201201043](https://openairdocs.org/sdr/REXA201201043.md): Door · out of adjust · Jul 4, 2012 · N8672A · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT ATTENDANT HAD DIFFICULTY OPENING MAIN CABIN DOOR, HAD TO CYCLE DOOR HANDLE X3 TO OPEN DOOR. MAINTENANCE ADJUSTED PASSENGER DOOR IAW AMM 52-11-00. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.
- [SDR REXA2012042400562](https://openairdocs.org/sdr/REXA2012042400562.md): Light · inoperative · Apr 24, 2012 · N8672A · Cndair CL6002B19 · Emergency Lighting
  > NR 3 EMERGENCY LIGHT IN CABIN OVERHEAD INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT IAW AMM 33-51-16 OPC GOOD.
- [SDR REXA2012022600277](https://openairdocs.org/sdr/REXA2012022600277.md): Trim System · malfunctioned · Feb 26, 2012 · N8672A · Cndair CL6002B19 · Aileron Tab Control System
  > AIL TRIM TO THE LEFT STOPPED WORKING ALTHOUGH RIGHT DOES. PERFORMED OPS CHECK IAW CRJ AMM 27-12-10. OPS CHECKS GOOD. A/C MAINT HISTORY CONT'D ON AML 2148301.
- [SDR REXA201200181](https://openairdocs.org/sdr/REXA201200181.md): Mechanism · lack of lube · Feb 2, 2012 · N8672A · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HANDLE JAMMED (WILL NOT MOVE TO LOCK DOOR CLOSED). INSPECTED DOOR PINS, LATCHES AND ROLLERS. CLEANED & LUBED ALL PINS, LATCHES & ROLLERS IAW AMM 52-10-00. OPS CKS GOOD. OK FOR SERVICE.
- [SDR REXA2012000152](https://openairdocs.org/sdr/REXA2012000152.md): Rib · cracked · Jan 12, 2012 · N8672A · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RIGHT WING BATTERY RIB CRACKED. REPAIRED IAW BOMBARDIER REO 601R-57-52-046 REV B.
- [SDR REXA2012000151](https://openairdocs.org/sdr/REXA2012000151.md): Rib · cracked · Jan 12, 2012 · N8672A · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LEFT WING BATTERY RIB CRACKED. REPAIRED IAW BOMBARDIER REO 601R-57-52-046 REV B.
- [SDR REXA201100956](https://openairdocs.org/sdr/REXA201100956.md): Light · inoperative · Dec 10, 2011 · N8672A · Cndair CL6002B19 · Emergency Lighting
  > SECTION OF FLOOR TRACK EMERGENCY LIGHTING INOP. REMOVED AND REPLACED FLOOR TRACK EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECK NORMAL. ALSO REMOVED AND REPLACED SECTION OF FLOOR TRACK LIGHT COVER, IAW AMM 33-51-01.
- [SDR REXA201100671](https://openairdocs.org/sdr/REXA201100671.md): Secu · malfunctioned · Oct 3, 2011 · N8672A · Cndair CL6002B19 · Drag Control System
  > FLT SPOILER FAULT STATUS MESSAGE IN FLIGHT. O/B GND SPOILER FAULT STATUS MESSAGE IN FLIGHT. REMOVED AND REPLACED SECU NR 1 IAW AMM 27-61-05 SELF-TEST, FUNCTIONAL, AND OPS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR REXA201100194](https://openairdocs.org/sdr/REXA201100194.md): Skin · damaged · Mar 22, 2011 · N8672A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING ROUTINE LINE MAINTENANCE AT YQB THE SUBJECT AIRCRAFT WAS STRUCK BY GROUND EQUIPMENT CAUSING DAMAGE TO THE FUSELAGE SKIN AT FS 682 JUST ABOVE S-19R AND THE UNDERLYING FRAME CLIP LOCATED BETWEEN S-18R AND S-19R. THE PUNCTURE AND DENT MEASURE 3 X 2 INCHES
- [SDR REXA201100162A](https://openairdocs.org/sdr/REXA201100162A.md): Warning System · activated · Mar 5, 2011 · N8672A · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT T/R UNLOCK MSG. DEFERRED PER MEL 38-30-01 AUTH 38789.
- [SDR REXA201100158](https://openairdocs.org/sdr/REXA201100158.md): Flap · failed · Mar 3, 2011 · N8672A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 30 DEGREES ON APPROACH INTO MEM. FLIGHT LANDED SAFELY. EMERGENCY DECLARED.
- [SDR REXA201000222](https://openairdocs.org/sdr/REXA201000222.md): Unknown · odor · Oct 21, 2010 · N8672A · Cndair CL6002B19 · Air Distribution System
  > ON DESCENT INTO KMEM THE FLIGHT CREW STARTED THE APU AT 10,000 FEET. BOTH FLIGHT CREWMEMBERS SMELLED THE STRONG ODOR OF JET FUEL. THE APU AND BLEED SYSTEMS WERE SHUT DOWN. SINCE THE SMELL DID NOT DISSIPATE QUICKLY, THE FLIGHT CREW DECLARED AN EMERGENCY. AN
- [SDR REXA201000084](https://openairdocs.org/sdr/REXA201000084.md): Uplock Sensor · out of adjust · May 19, 2010 · N8672A · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING (RT MAIN) AFTER TAKEOFF. ADJUSTED RT MLG UPLOCK ASSEMBLY SENSOR-TO-TARGET (PROXIMITY) TO WITHIN LIMITS IAW AMM 32-61-05.
- [SDR REXA201000010](https://openairdocs.org/sdr/REXA201000010.md): Unknown · odor · Jan 21, 2010 · N8672A · Bombdr CL6002D15 · Air Distribution System
  > DURING CRUISE AT FL200 JUST BEFORE DESCENT INTO DTW THE CA AND FO NOTICED A STRANGE ODOR IN THE COCKPIT. THE ODOR SEEMED TO SMELL LIKE SOMETHING BURNING OR A KIND OF BURNT SMELL. FO CALLED BACK TO THE FLIGHT ATTENDANT TO ASK IF SHE SMELLED AN ODOR ALSO. SHE
- [SDR REXA201000008](https://openairdocs.org/sdr/REXA201000008.md): Flap · out of rig · Jan 15, 2010 · N8672A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL DURING FLAPS AT ZERO OVER SPEED CLICKER WITH FLAP INDICATION 310 KNOTS 36 MIN INTO FLIGHT OQT 41 DEG DURING CLIMB. PERFORMED T/S PER BOMBARDIER FIM R 37 IAW AM 2009-06-12PARA H6I PER AMOC DATED MARCH 27 2009 & PA AD 27-052F.CODES 1 5 1A 1 5 2A RIG
- [SDR REXA201000007](https://openairdocs.org/sdr/REXA201000007.md): Sensor · out of adjust · Jan 13, 2010 · N8672A · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE ON TAKEOFF. NOSE GEAR WILL NOT RETRACT. C/W PA 05-018A ADJUSTED NLG CENTERED / EXTEND SENSOR IAW AMM 32-61-05. PERFORMED OPS CHECK AND RETURNED TO SERVICE.
- [SDR REXA201000005](https://openairdocs.org/sdr/REXA201000005.md): Ecu · failed · Jan 10, 2010 · N8672A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON DATE 01/11/2010 SUBMITTED TWO SEPARATE SDRS WITH THE SAME CONTROL NUMBER. THAT CONTROL NUMBER WAS REXA201000004. THIS SDR CONTROL NUMBER REXA201000005 IS ISSUED FOR FLAP FAIL ISSUE ON AIRCRAFT S/N 7672 DATE 01/10/2010. FLAPS FAIL AT ZERO DURING CRUISE FL
- [SDR REXA201000004](https://openairdocs.org/sdr/REXA201000004.md): Fcu · failed · Jan 10, 2010 · N8672A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT ZERO DURING CRUISE FLIGHT. FLAPS 0-0 M.73 IAS 270 1 THS 424.FL310 SAT -49 DEGREES C.1825-30Z. PERFORMED T/S PER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I) PER AMOC DATED MARCH 27,2009 AND PAAD27-052F. FOUND CODES 1 5 1A,152A PROBABLE CAU
- [SDR REX2008F00048](https://openairdocs.org/sdr/REX2008F00048.md): Flap · malfunctioned · Sep 2, 2008 · N8672A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > WHILE IN CRUISE AT FL300 OVER SPEED CLACKER FOLLOWED BY FLAPS FAIL CAUTION MSG. QRH FOLLOWED DECLARED EMERGENCY WITH UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.
- [SDR REX2008F00029](https://openairdocs.org/sdr/REX2008F00029.md): Selector Valve · malfunctioned · Aug 12, 2008 · N8672A · Cndair CL6002B19 · Landing Gear Selector
  > ON CLIMBOUT RECEIVED GEAR DISAGREE. QRH FOLLOWED, DECLARED EMERGENCY AND RETURNED TO AIRPORT WITH UNEVENTFUL LANDING. MAINTENANCE INSPECTED ACFT AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE. PERFORMED OPERATIONAL CHECKS PER BOMBARDIER AMM. (S)
- [SDR REX2008F00021](https://openairdocs.org/sdr/REX2008F00021.md): Strut · low · Jul 31, 2008 · N8672A · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > ON CLIMBOUT AND GEAR RETRACTION RECEIVED "GEAR DISAGREE" WARNING. QRH FOLLOWED AND RETURNED TO AIRPORT WITH UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE GEAR AND SERVICED THE NOSE LANDING GEAR STRUT NITROGEN/HYDRAULICS, GEAR SWINGS PERFORMED WITH NO DEFECTS
- [SDR REXA200700016](https://openairdocs.org/sdr/REXA200700016.md): Bpsu · failed · Feb 2, 2007 · N8672A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT ZERO DEGRESS AFTER BLOCK OUT. REMOVED AND REPLACED LT BPSU. FLAPS OPERATIONALLY CHECK GOOD.
- [SDR REXA200700011](https://openairdocs.org/sdr/REXA200700011.md): Unknown · unknown · Jan 28, 2007 · N8672A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT ZERO DEGREES. COMPLIED WITH AD2006-12-21. RESET FLAPS AND MONITORING FOR 72 HOURS.
- [SDR REXA200700010](https://openairdocs.org/sdr/REXA200700010.md): Unknown · unknown · Jan 27, 2007 · N8672A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL ON TAXI OUT. COMPLIED WITH AD2006-12-21, RESET FLAPS, AND MONITORING FOR 72 HRS.

## 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 = 'N8672A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8672A/reports

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