# Service difficulty reports: N8709A

A list on [N8709A](https://openairdocs.org/aircraft/N8709A.md).

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

- [SDR REXA2013120102285](https://openairdocs.org/sdr/REXA2013120102285.md): Flashlight · inoperative · Dec 1, 2013 · N8709A · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDANT'S FLASHLIGHT NOT FLASHING. R & R FLIGHT ATTENDANT'S FLASHLIGHT IAW AMM 25-61-02.
- [SDR REXA2013103101784](https://openairdocs.org/sdr/REXA2013103101784.md): Light · damaged · Oct 31, 2013 · N8709A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT MISSING AND DAMAGED. R & R DAMAGED EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.
- [SDR REXA2013092301747](https://openairdocs.org/sdr/REXA2013092301747.md): Unknown · odor · Sep 23, 2013 · N8709A · Cndair CL6002B19 · Air Distribution System
  > BURNING ODOR COMING FROM F/A GALLEY FAN. OPS CHECKED GALLEY FAN IAW AMM 21-23-07-710-001. OPS CHECKED NORMAL, OPS CHECKED GALLEY HEATER IAW AMM 21-23-05-710-801, OPS CHECKED NORMAL, COULD NOT DUPLICATE.
- [SDR REXA2013072401105](https://openairdocs.org/sdr/REXA2013072401105.md): Structure · cracked · Jul 24, 2013 · N8709A · Cndair CL6002B19 · Wing Main, Frame Structure
  > A FASTENER HOLE WAS FOUND CRACKED AROUND THE RT FUEL BOOST PUMP MEASURING 0.05" LONG. REPAIRED IAW REO 601R-57-21-169.
- [SDR REXA2013051400889](https://openairdocs.org/sdr/REXA2013051400889.md): Flashlight · inoperative · May 14, 2013 · N8709A · Cndair CL6002B19 · Emergency Equipment
  > FIRST OFFICER'S FLASHLIGHT INOPERABLE.
- [SDR REXA2013042300761](https://openairdocs.org/sdr/REXA2013042300761.md): Light · inoperative · Apr 23, 2013 · N8709A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR LIGHT AFT OF ROW 12 IS INOPERABLE.
- [SDR REXA2012111301518](https://openairdocs.org/sdr/REXA2012111301518.md): Angle · cracked · Nov 13, 2012 · N8709A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK FOUND IN CAP ANGLES AT RBL 18 AND LBL 18 OF FS 559 SEMI-PRESSURE BULKHEAD. REPAIRED IAW PA53-025 AND BOMBARDIER REO 601R-53-41-260/601R-53-41-609.
- [SDR REXA2012111201675](https://openairdocs.org/sdr/REXA2012111201675.md): Battery · discharged · Nov 12, 2012 · N8709A · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDANT FLASHLIGHT NOT SHOWING FLASHING CHARGE LIGHT. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-61-02 DM 74772 CLEARED.
- [SDR REXA2012110401145](https://openairdocs.org/sdr/REXA2012110401145.md): Skin · damaged · Nov 2, 2012 · N8709A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THE DAMAGE CONSISTS OF A BLENDOUT IN THE SKIN MEASURING 2.5 X 1.2 X 0.022 DEEP LOCATED 0.4 BELOW THE LOWER FASTENER ROW COMMON TO S-18L AND 1.1 FORWARD OF THE FORWARD FASTENER ROW COMMON TO FS 621. REPAIRED IAW EA CRJ253-00987A.
- [SDR REXA2012101401400](https://openairdocs.org/sdr/REXA2012101401400.md): Light · loose · Oct 14, 2012 · N8709A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR LIGHT CAME LOOSE BY ROW ONE. REPLACED FLOOR TRACK COVER AND FLEX LAMP IAW CRJ-200 AMM 33-51-01.
- [SDR REXA2012091701344](https://openairdocs.org/sdr/REXA2012091701344.md): Life Vest · unserviceable · Sep 17, 2012 · N8709A · Cndair CL6002B19 · Life Jacket
  > F/O'S LIFE VEST BAG TORN. REMOVED AND REPLACED F/O LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012070601051](https://openairdocs.org/sdr/REXA2012070601051.md): Pcu · out of adjust · Jul 6, 2012 · N8709A · Cndair CL6002B19 · Aileron Control System
  > RIGHT AILERON OUT OF CENTER BY APPROXIMATELY 1/2 INCH FROM WING AND TRAILING EDGE OF OUTBOARD FLAP. RIGGED RIGHT INBOARD AND OUTBOARD AILERON PCU'S PER AMM 27-11-00. OPS CHECKED NORMAL, AIRCRAFT OK FOR SERVICE.
- [SDR REXA2012062001003](https://openairdocs.org/sdr/REXA2012062001003.md): Light · weak · Jun 20, 2012 · N8709A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS FAINT. FADED IN AND OUT BUT STAYED ON. HARD TO SEE. ADJUSTED AND TESTED EMERGENCY LIGHTS. CHECKED NORMAL IAW AMM 33-51-00.
- [SDR REXA2012050200597](https://openairdocs.org/sdr/REXA2012050200597.md): Light · inoperative · May 2, 2012 · N8709A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT IN CEILING @ ROW 8 IS BURNT OUT. RELAMPED ROW 8 EMERGENCY LIGHT PER AMM 33-51-10.OK FOR SVC. OPS GOOD.
- [SDR REXA2012042200549](https://openairdocs.org/sdr/REXA2012042200549.md): Light · inoperative · Apr 22, 2012 · N8709A · Cndair CL6002B19 · Emergency Lighting
  > VERY BACK AFT CABIN CEILING EMERGENCY LIGHT NOT WORKING. REMOVED AND REPLACED 1 CEILING EMER EXIT LIGHT.
- [SDR REXA2012022700284](https://openairdocs.org/sdr/REXA2012022700284.md): Pump · malfunctioned · Feb 27, 2012 · N8709A · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > HYD PUMP 3A CAUTION ILLUMINATED. RESET HYD PUMP 3A IAW AMM 29-10-10.
- [SDR REXA201200145](https://openairdocs.org/sdr/REXA201200145.md): Sensing Element · defective · Jan 25, 2012 · N8709A · Cndair CL6002B19 · Pneumatic Indicating System
  > AIR RETURN FOR WING ANTI-DUCT MASTER WARNING ON CLIMBOUT. REMOVED AND REPLACED 14TH STG LT DUCT SENSING ELEMENT (A39WK) IAW AMM 36-21-01. OPC GOOD. OK FOR SVC.
- [SDR REXA201100974](https://openairdocs.org/sdr/REXA201100974.md): Loop · defective · Dec 15, 2011 · N8709A · Cndair CL6002B19 · Pneumatic Indicating System
  > ANTI ICE DUCT WARN MESSAGE ON TAKEOFF. REMOVED AND REPLACED SHORTED LOOP A18WK & OP CHECK GOOD IAW AMM 36-21-04. OK FOR SERVICE.
- [SDR REXA201100890](https://openairdocs.org/sdr/REXA201100890.md): Warning System · false activation · Nov 29, 2011 · N8709A · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > RT ANTI ICE DUCT WARNING MESSAGE. PERFORMED VISUAL AND OPS CHECK OF RT ANTI ICE DUCT SYSTEM IAW AMM 30-10-00. NO DEFECTS NOTED. OPS CHECK GOOD.
- [SDR REXA201100835](https://openairdocs.org/sdr/REXA201100835.md): Computer · malfunctioned · Nov 11, 2011 · N8709A · Cndair CL6002B19 · Fuel Indicating System
  > INFLIGHT L FUEL TANK QTY READOUT SHOWED, AND GOT AUTO XFLOW INHIB STATUS MSG FOR APPROX 60SEC. RE-RACKED FUEL CONTROL COMPUTER IAW AMM 28-40-00. NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR REXA201100780](https://openairdocs.org/sdr/REXA201100780.md): Warning System · false activation · Oct 25, 2011 · N8709A · Cndair CL6002B19 · Pneumatic Indicating System
  > DURING CLIMB - ANTI ICE DUCT WARNING MESSAGE CAME ON JUST AS THE WING ANTI ICE WAS TURNED OFF. STILL HAD COWL ANTI ICE ON. A/ICE SYNOPTIC PAGE SHOWED RED LINE THROUGH LEFT FUSELAGE ONLY. PERFORMED OPC OF BLEED AIR INDICATION SYSTEM IAW AMM 36-20-00. UNABLE
- [SDR REXA201100771](https://openairdocs.org/sdr/REXA201100771.md): Warning System · false activation · Oct 23, 2011 · N8709A · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > WING ANTI DUCT WARNING MSG IN FLIGHT. QRH COMPLETE. MSG EXTINGUISH IN 3 MINUTES. PERFORMED TEST OF WAI SYS IAW AMM30-10-00. NO DEFECT NOTED.
- [SDR REXA201100764](https://openairdocs.org/sdr/REXA201100764.md): Sensing Element · defective · Oct 20, 2011 · N8709A · Cndair CL6002B19 · Pneumatic Indicating System
  > ANTI-ICE DUCT WARNING IN FLIGHT LEFT SIDE OF FUSELAGE RED ON A/ICE SYNOPTIC PAGE. TROUBLE SHOT AND FOUND LEFT FUSELAGE SENSING ELEMENT A47WK TO BE AT FAULT. REMOVED AND REPLACED A47WK SENSING ELEMENT IAW AMM 36-21-04. OPERATIONAL TEST OF THE BLEED AIR LEAK
- [SDR REXA201100738](https://openairdocs.org/sdr/REXA201100738.md): Warning System · false activation · Oct 20, 2011 · N8709A · Cndair CL6002B19 · Pneumatic Indicating System
  > ANTI ICE DUCT WARNING IN FLT LEFT SIDE FUSELAGE RED ON A/ICE SYNOPTIC PAGE. LT LOOP CIRCUIT INSULATION CHECK GOOD FROM BLCU IAW ESPM 20-12-00 RAN WING ANTI ICE SYS. NO LEAKS NOTED OP CHECK GOOD IAW AMM 36-21-00.
- [SDR REXA2011100900701](https://openairdocs.org/sdr/REXA2011100900701.md): Bulb · inoperative · Oct 9, 2011 · N8709A · Cndair CL6002B19 · Emergency Lighting
  > 3 &4 OVERHEAD EMERERGENCY EXIT FLOOD LIGHTS INOPERATIVE. SWAPPED BULBS IAW AMM 33-51-16 AND DEFERRED CEILING FLOOD LIGHTS PER MEL 33-51-11 AUTH 52528 CAT C PER MOC SB PLACARD INSTALLED.
- [SDR REXA201100679](https://openairdocs.org/sdr/REXA201100679.md): Battery · discharged · Oct 5, 2011 · N8709A · Cndair CL6002B19 · Emergency Equipment
  > F/AS FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED BATTERY IAW AMM 25-60-00, OP/C GOOD OK FOR SERVICE. VERIFIED PARTS EFFECTIVITY.
- [SDR REXA201100257](https://openairdocs.org/sdr/REXA201100257.md): Loop · faulty · May 3, 2011 · N8709A · Cndair CL6002B19 · Pneumatic Indicating System
  > WING ANTI ICE WARNING MESSAGE. REMOVED AND REPLACED 14TH STAGE AFT EQUIP BAY BLEED AIR LEAD DETECTION LOOP IAW CRJ AMM 36-21-04, OP CHECK GOOD OK FOR SERVICE. WING ANTI ICE CHECKS GOOD IAW CRJ AMM 30-11-00.
- [SDR REXA201100140](https://openairdocs.org/sdr/REXA201100140.md): Unknown · malfunctioned · Feb 22, 2011 · N8709A · Cndair CL6002B19 · Cabin Pressure Control System
  > AIR RETURN DUE TO CABIN WAS CLIMBING RATE OF 2500FPM RIGHT AFTER TAKEOFF. DURING DESCENT IT WAS AT 700 FPM. PRESSURIZED IAW AMM 21-31-00. OPS CHECK GOOD. A/C IS OK SERVICE NST-310663-2011 NO 91674 91 PRESSURIZATION CONTROL.
- [SDR REXA201100410](https://openairdocs.org/sdr/REXA201100410.md): Unknown · malfunctioned · Feb 22, 2011 · N8709A · Cndair CL6002B19 · Cabin Pressure Control System
  > AIR RETURN DUE TO CABIN WAS CLIMBING AT A RATE OF 2500 FPM RIGHT AFTER TAKE OFF DURING DESCENT IT WAS AT 700 FPM PRESSURIZED A/C IAW AMM 21-31-00. OPS CHECK GOOD. ACFT IS OK FOR SERVICE.
- [SDR REXA201100138](https://openairdocs.org/sdr/REXA201100138.md): Drag Angle · cracked · Feb 22, 2011 · N8709A · Cndair CL6002B19 · Passenger/Crew Doors
  > ASD AFT DRAG ANGLE CRACKED. REMOVED AND REPLACED AFT DRAG ANGLE IAW CRJ200 SRM 51-42-00.
- [SDR 2011F00054](https://openairdocs.org/sdr/2011F00054.md): Drag Angle · cracked · Feb 22, 2011 · N8709A · Cndair CL6002B19 · Passenger/Crew Doors
  > ASD AFT DRAG ANGLE CRACKED. R & R AFT DRAG ANGLE IAW SRM 51-42-00.
- [SDR 2011F00053](https://openairdocs.org/sdr/2011F00053.md): Bulkhead · cracked · Feb 22, 2011 · N8709A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 559 BULKHEAD FOUND CRACKED. COMPLIED WITH 559 REPAIR IAW REO 601R-53-41-260, REV E STEP 1-14 AND REO601R-53-41-609, REV B, DEVIATION E.
- [SDR REXA201100137](https://openairdocs.org/sdr/REXA201100137.md): Bulkhead · cracked · Feb 19, 2011 · N8709A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 559 BULKHEAD FOUND CRACKED. COMPLIED WITH 559 REPAIR IAW BOMBARDIER REO 601R-53-41-260 REV E STEP 1-14 AND REO 601R-53-41-609 REV B DEVIATION E.
- [SDR REXA201100033](https://openairdocs.org/sdr/REXA201100033.md): Warning System · activated · Jan 9, 2011 · N8709A · Cndair CL6002B19 · AC Indicating System
  > NR 2 GEN OFF CAUTION MESSAGE, DEFERRED PER MEL 24-11-11.
- [SDR REXA201000262](https://openairdocs.org/sdr/REXA201000262.md): Torque Link · disconnected · Nov 17, 2010 · N8709A · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > NOSE GEAR DISAGREE AFTER TAKEOFF. TORQUE LINKS NEVER CONNECTED BY RAMP PERSONNEL AFTER PUSH BACK.
- [SDR REXA200900084](https://openairdocs.org/sdr/REXA200900084.md): Priority Valve · bypassing · Jul 23, 2009 · N8709A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > THE A/C WAS CONFIGURED AT FLAPS 20 AND ON ABOUT A 7 MILE FINAL, PUT THE GEAR DOWN. THE NOSE GEAR INDICATION DID NOT SHOW GREEN / DOWN AND LOCKED. AFTER A FEW MOMENTS RECEIVED A GEAR DISAGREE WARNING MESSAGE. EXECUTED THE MISSED APPROACH ACCORDING TO PROFILE
- [SDR REXA20060086](https://openairdocs.org/sdr/REXA20060086.md): Flap · malfunctioned · Oct 7, 2006 · N8709A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED FLAP FAILURE CAUTION MESSAGE ON TAXI. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.
- [SDR REXA20060030](https://openairdocs.org/sdr/REXA20060030.md): Flap System · failed · Mar 3, 2006 · N8709A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DURING NORMAL VISUAL APPROACH, CAPTAIN CALLED FOR FLAPS 45. ED1 SHOWED FLAPS 45 GREEN LINE, BUT THE FLAP FAIL CAUTION ILLUMINATED. THE FLIGHT CREW EXECUTED QRH PROCEDURES AND AN OTHERWISE NORMAL LANDING WAS MADE. THE AIRCRAFT WAS CURRENTLY UNDER THE 72 HOUR
- [SDR REXA200600027](https://openairdocs.org/sdr/REXA200600027.md): Seal · deteriorated · Feb 26, 2006 · N8709A · Cndair CL6002B19 · Turbine Engine Oil System
  > DURING CLIMBOUT ON A FERRY FLIGHT FROM DTW TO MEM, THE -SMOKE TOILET- MESSAGE ANNUNCIATED AND THE FLIGHT CREW DETECTED AN OIL SMELL AND VISIBLE SMOKE. THE AIRCRAFT RETURNED TO DTW WHERE THE PROBLEM WAS DETERMINED TO BE AN ENGINE INTERNAL OIL SEAL LEAK. OIL C
- [SDR REXA200600016](https://openairdocs.org/sdr/REXA200600016.md): Smoke Detector · malfunctioned · Feb 14, 2006 · N8709A · Cndair CL6002B19 · Smoke Detection
  > ON CLIMBOUT RECEIVED LAV SMOKE WARNING. QRH FOLLOWED EMERGENCY DECLARED RETURN TO AIRPORT. REMOVED AND REPLACED SMOKE DETECTOR PER BOMBARDIER AMM, OPERATIONAL CHECKS GOOD.
- [SDR REXA04036](https://openairdocs.org/sdr/REXA04036.md): Elt · failed · Nov 5, 2004 · N8709A · Cndair CL6002B19 · Emergency Locator Beacon
  > ELT FAILS G-SWITCH TEST. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207.

## 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 = 'N8709A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8709A/reports

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