# Service difficulty reports: N8623A

A list on [N8623A](https://openairdocs.org/aircraft/N8623A.md).

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

- [SDR REXA2014062300629](https://openairdocs.org/sdr/REXA2014062300629.md): Sign · damaged · Jun 23, 2014 · N8623A · Cndair CL6002B19 · Emergency Lighting
  > WARDROBE EMER EXIT SIGN DAMAGED. REPLACED WARDROBE EMER EXIT SIGN IAW AMM 33-51-10.
- [SDR REXA2014050700429](https://openairdocs.org/sdr/REXA2014050700429.md): Light · inoperative · May 7, 2014 · N8623A · Cndair CL6002B19 · Emergency Lighting
  > MAIN CABIN DOOR EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. R & R EMERGENCY LIGHT BULB IAW AMM 33-51-21. OK FOR SERVICE.
- [SDR REXA2014022800249](https://openairdocs.org/sdr/REXA2014022800249.md): Light · unsecure · Feb 28, 2014 · N8623A · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT ATTENDANT REPORTS EMERGENCY LIGHTING ON FLOOR BY SEAT 1C NEEDS TO BE SECURED. SECURED FLOOR LIGHTING BY SEAT 1C AS REQUIRED.
- [SDR REXA2014012100127](https://openairdocs.org/sdr/REXA2014012100127.md): Life Vest · unserviceable · Jan 21, 2014 · N8623A · Cndair CL6002B19 · Life Jacket
  > CAPTAIN`S LIFE VEST HAS HOLE. R & R CAPTAIN`S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013092201742](https://openairdocs.org/sdr/REXA2013092201742.md): Flap System · malfunctioned · Sep 22, 2013 · N8623A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS DEGREADED STATUS MESSAGE, RESET AND PERFORMED ADJUSTMENT AND TEST OF FLAP SYS IAW AMM 27-54-00, NO DEFECTS NOTED.
- [SDR REXA2013072101099](https://openairdocs.org/sdr/REXA2013072101099.md): Skin · chafed · Jul 19, 2013 · N8623A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING INBD FORWARD ACCESS PANEL AT WS 54.897 LANDING CHAFED IN THE NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2013072101098](https://openairdocs.org/sdr/REXA2013072101098.md): Frame · corroded · Jul 19, 2013 · N8623A · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT BS 394 BETWEEN S23-24R CORRODED 100 PERCENT THROUGH. REPAIRED IAW REO 601R-53-21-2451.
- [SDR REXA2013052000897](https://openairdocs.org/sdr/REXA2013052000897.md): Ecu · failed · May 20, 2013 · N8623A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL ON GROUND SETTING FLAPS 20 FOR TAKEOFF LEFT FLAP INDICATING 0 DEGREES RIGHT FLAP INDICATING 2 DEGREES PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD 2009-06-12 PARAGRAPH H.6.I, AMOC DATED DECEMBER 07,2012 AND PA AD27-052L. REMOVED AND RE
- [SDR REXA2013012000157](https://openairdocs.org/sdr/REXA2013012000157.md): Actuator · failed · Jan 20, 2013 · N8623A · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 4006 RECEIVED FLAP FAIL MESSAGE WHEN FLAPS SELECTED 20-30 DEGREES ON APPROACH INTO MSP. FLAP 20 DEGREES LANDING QRH COMPLETED MAX BRAKE TEMP 03 GREEN. PERFORMED TROUBLESHOOT PER BOMBARDIER FIM REV 44 IAW AD 2009-06-12 PARA (L) (6) (I), AMOC DATED DEC
- [SDR REXA2012112801717](https://openairdocs.org/sdr/REXA2012112801717.md): Flap · failed · Nov 28, 2012 · N8623A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > IN FLIGHT ON FLIGHT 3613 (DTW - GRB), RECEIVED FLAPS FAILED AT 30 DEGREES WHEN SELECTING FLAPS FROM 30 DEGREES TO 45 DEGRESS AT 165 KTS APPROXIMATELY 55 MINUTES INTO THE FLIGHT. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 43 IAW AD2009-06-12, PARAGRAPH (
- [SDR REXA2012091101333](https://openairdocs.org/sdr/REXA2012091101333.md): Heat Shield · cracked · Sep 11, 2012 · N8623A · Cndair CL6002B19 · APU Exhaust System
  > APU EXHAUST HEAT SHIELD IS CRACKED. REMOVED AND REPLACED APU EXHAUST HEAT SHIELD IAW AMM 49-81-01.
- [SDR REXA2012072601188](https://openairdocs.org/sdr/REXA2012072601188.md): Lamp · inoperative · Jul 26, 2012 · N8623A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. RELAMPED EMERGENCY LIGHTS OFF SWITCH LIGHT IAW ESPM 20-24-00. OPS CHECKED GOOD, OK FOR SERVICE.
- [SDR REXA2012071001061](https://openairdocs.org/sdr/REXA2012071001061.md): Landing Gear · malfunctioned · Jul 10, 2012 · N8623A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR UP DISAGREE AND NOSE DOOR STAYED OPEN AFTER TAKEOFF. WARNING MESSAGE ON GEAR LEVER UP SELECTION. COMPLIED WITH PA 05-018REV G SCENARIO 2. FOUND PS14GA IA AMM 32-61-05. OPS CHECKED GOOD.
- [SDR REXA201201000](https://openairdocs.org/sdr/REXA201201000.md): Bulb · inoperative · Jun 19, 2012 · N8623A · Cndair CL6002B19 · Emergency Lighting
  > RIGHT NR 2 EXTERIOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED RIGHT NR 2 EXTERIOR EMERGENCY LIGHT BULB IAW AMM 33-51-21.
- [SDR REXA2012040800470](https://openairdocs.org/sdr/REXA2012040800470.md): Light · inoperative · Apr 8, 2012 · N8623A · Cndair CL6002B19 · Emergency Lighting
  > LEFT WING EMERGENCY EXIT OVERWING LIGHT INOPERATIVE. REMOVED AND REPLACED OVERWING EXIT LIGHT IAW AMM 33-51-21.
- [SDR REXA2012030300323](https://openairdocs.org/sdr/REXA2012030300323.md): Sensing Element · defective · Mar 3, 2012 · N8623A · Cndair CL6002B19 · Pneumatic Indicating System
  > AIR RETURN FOR ANTI-ICE DUCT WARNING MSG INFLIGHT CLIMBOUT OF DTW WITH WING & COWL ANTI ICE ON. QRH COMPLETED MSG WENT OUT AFTER 14TH STAGE BLEEDS TURNED OFF MSG CAME BACK WHEN 14TH STAGE BLEEDS AND WING & COWL ICE TURNED BACK ON COMING BACK TO DTW IN ICING C
- [SDR REXA201101018](https://openairdocs.org/sdr/REXA201101018.md): Valve · malfunctioned · Dec 25, 2011 · N8623A · Cndair CL6002B19 · Fuel Transfer Valve
  > GRAVITY XFLOW WILL NOT TURN OFF WHEN COMMANDED. OPS CHECK OF GRAVITY XFLOW GOOD IAW AMM 28-13-16. SEE NON-ROUTINE CARDS N23501, N23513, N23517, AND N23515 FOR R&R OF GRAVITY XFLOW VALVE. REMOVED AND REPLACED GRAVITY XFLOW VALVE IAW 28-13-16 REFERENCE NON-ROU
- [SDR REXA201100988](https://openairdocs.org/sdr/REXA201100988.md): Sensor · leaking · Dec 18, 2011 · N8623A · Cndair CL6002B19 · APU Engine Fuel and Control
  > APU LEAKING FUEL. REMOVED AND REPLACED APU FUEL SOV IAW AMM 49-31-05. NO FIX. DM 56373 REMAINS OPEN. OK FOR SERVICE. VERIFIED PART EFFECTIVITY. REMOVED AND REPLACED APU P3 SENSOR IAW AMM 49-51-03. THIS CLEARS DM 56373. OPS/CHECK GOOD LEAK CHECK GOOD.
- [SDR REXA201100973](https://openairdocs.org/sdr/REXA201100973.md): Bpsu · defective · Dec 15, 2011 · N8623A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MSG IN FLIGHT AFTER T/O. FAILED AT 0 DEGREES. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I) AMOC DATED MARCH 27 2009 TR# 27-012 PER AMOC DATED DECEMBER 18 2009 AND PA AD27-052G. REMOVED AND REPL
- [SDR REXA201100817](https://openairdocs.org/sdr/REXA201100817.md): Spar · damaged · Nov 22, 2011 · N8623A · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL STAB RT SPAR TIP AT BL116 HAS TWO ELONGATED SCREW HOLES FOR THE ATTACHMENT OF THE STAB TIP FAIRING. REPAIRED IAW BOMBARDIER SERVICE CORPORATION EO CL600-2B19-55-L00726 AND ASSOCITATED 8110-3.
- [SDR REXA201100716](https://openairdocs.org/sdr/REXA201100716.md): Bulkhead · dented · Nov 18, 2011 · N8623A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 PRESSURE BULKHEAD FWD FACE HAS A DENT AT RBL 32 APPROX 3 INCHES ABOVE FLOOR 1.2" X 1.1" X 0.040". DENT WITHIN ALLOWABLE LIMITS PER CRJ SRM 53-61-19 AND 53-00-31.
- [SDR REXA201100798](https://openairdocs.org/sdr/REXA201100798.md): Windshield · cracked · Oct 26, 2011 · N8623A · Cndair CL6002B19 · Flight Compartment Windows
  > AT FL 310 F/O SIDE WINDSHIELD CRACKED. EMERGENCY DECLARED. REMOVED AND REPLACED F/O'S WINDSHIELD IAW AMM 56-11-01. PRESSURE CHECK GOOD. OK FOR SERVICE. VERIFIED PART EFFECTIVITY.
- [SDR REXA201100082](https://openairdocs.org/sdr/REXA201100082.md): Retainer · damaged · Feb 3, 2011 · N8623A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TWO PASSENGER DOOR SEAL RETAINERS WERE FOUND DAMAGED. DAMAGE TO THE LOWER SEAL RETAINER (P/N 601R318722-1) CONSISTS OF A 1-1/8 CRACK AND 1-1/2 BEND/DENT. DAMAGE TO THE LOWER FORWARD SEAL RETAINER (P/N 601R318712-2) CONSISTS OF A 1/2 CRACK AND A 1-3/4 BEND/DE
- [SDR REXA201100062](https://openairdocs.org/sdr/REXA201100062.md): Flap · out of rig · Jan 24, 2011 · N8623A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 30 DEG ON FINAL APPROACH WITH IAS 160 TAT 15 DEG C. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H), (6), (I) AMOC DATED MARCH 27 2009 TR 27-012 PER AMOC DATED DECEMBER 18 2009 AND PA AD 27-052G RE-RIGGED FLAP
- [SDR REXA201100050](https://openairdocs.org/sdr/REXA201100050.md): Flap System · failed · Jan 20, 2011 · N8623A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 30 DEG ON FINAL APPROACH WITH IAS 160 TAT 15 DEG C. PERFORMED TROUBLESHOOTING PER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H), (6), (I). RIGGED FLAPS IAW AMM 27-51-10, OP CHECKS GOOD.
- [SDR REXA201000235](https://openairdocs.org/sdr/REXA201000235.md): Engine · shutdown · Oct 31, 2010 · N8623A · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > UPON LANDING AT KORF, THE LT ENGINE SHUTDOWN FOR NO APPARENT REASON. THE FLIGHT CREW REPORTED THAT THE THRUST LEVER WAS ABOVE THE IDLE GATE AT ALL TIMES AND THAT THE OCCURRENCE HAPPENED ALMOST SIMULTANEOUS WITH THE TOUCHDOWN OF THE MAIN WHEELS ONTO THE RUNWAY
- [SDR REXA200900102](https://openairdocs.org/sdr/REXA200900102.md): Warning System · malfunctioned · Aug 15, 2009 · N8623A · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE DURING APPROACH. AFTER GO AROUND AND QRH LANDED WITH 3 GREEN. MTX IN DTW PERFORMED GEARS SWINGS AND FOLLOWED TROUBLESHOOTING PROCEDURES PER FIM AND PA. OPS CHECKS WERE PERFORMED IAW AMM AND NO DEFECTS WERE FOUND.
- [SDR REXA200900070](https://openairdocs.org/sdr/REXA200900070.md): Bulkhead · cracked · Jun 21, 2009 · N8623A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FWD PRESSURE BULKHEAD CRACKED AROUND PARKING BRAKE CUT OUT LT SIDE FS 202.75 AT BL 23.71. REPAIRED PRESSURE BULKHEAD IAW BOMBARDIER AEROSPACE REO 601R-53-11-563.
- [SDR REXA200900033](https://openairdocs.org/sdr/REXA200900033.md): Selector Valve · failed · Mar 15, 2009 · N8623A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON APPROACH WHEN GEAR SELECTED DOWN RECEIVED "GEAR DISAGREE" MESSAGE. MX TROUBLESHOT SYSTEM, FOUND THE NLG SELECTOR VALVE FAILED. REMOVED AND REPLACED SELECTOR VALVE AND PERFORMED GEAR SWINGS IAW AMM. (K)
- [SDR REX2009F00024](https://openairdocs.org/sdr/REX2009F00024.md): Bracket · misaligned · Jan 25, 2009 · N8623A · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR NOSE GEAR DISAGREE MESSAGE ON CLIMB-OUT, RAN QRH AND DECIDED TO CONTINUE TO QRH FOLLOWED WITH UNEVENTFUL LANDING. SYSTEMS INSPECTED AND FOUND NOSE GEAR TORQUE LINK PROXIMITY SENSOR BRACKET TO BE MISALIGNED, DURING PUSHBACK BY CAPTURE STRAP. PROXIMITY SE
- [SDR REX2008F00058](https://openairdocs.org/sdr/REX2008F00058.md): Flap System · out of rig · Nov 18, 2008 · N8623A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH SELECTED FLAPS 20, RECEIVED FLAP FAILURE MSG WITH FLAPS STUCK AT ZERO. QRH FOLLOWED DECLARED EMERGENCY WITH AN UNEVENTFUL LANDING. FOUND FLAPS TO BE OUT OF RIG. RIGGED FLAPS PER AMM PERFORMED OPS CHECK WITH NO DEFECTS.
- [SDR REX2008F00033](https://openairdocs.org/sdr/REX2008F00033.md): Selector Valve · malfunctioned · Aug 8, 2008 · N8623A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON APPROACH GEAR FAILED TO EXTEND. QRH FOLLOWED MANUALLY EXTENDED. DECLARED EMERGENCY WITH UNEVENTFUL LANDING. PERFORMED GEAR SWING PER AMM. FOUND THE MAIN LANDING GEAR SELECTOR VALVE OPERATIONALLY CHECK GOOD PER AMM. (S)
- [SDR REX2008F00026](https://openairdocs.org/sdr/REX2008F00026.md): Strut · discharged · Aug 1, 2008 · N8623A · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > ON APPROACH INTO KMEM, WHEN GEAR WAS LOWERED THE AURAL "GEAR DISAGREE" WARNING WENT OFF WITH A RED NOSE GEAR INDICATION. CREW DECLARED AN EMERGENCY AND A GO AROUND. WHILE PERFORMING THE QRH, THE NOSE GEAR LOCKED DOWN. AN OTHERWISE NORMAL APPROACH AND LANDIN
- [SDR REX2008F00011](https://openairdocs.org/sdr/REX2008F00011.md): Unknown · malfunctioned · Jun 17, 2008 · N8623A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON APPROACH WITH NOSE NOT SHOWING DOWN AND LOCKED, EMERGENCY DECLARED, QRH FOLLOWED WITH UNEVENTFUL LANDING. COMPLIED WITH PINNACLE AIRLINES TROUBLESHOOTING PA (PROJECT AUTHORIZATION) AND PERFORMED GEAR SWINGS PER BOMBARDIER AMM 32-30-00 WITH NO
- [SDR REXA200800008](https://openairdocs.org/sdr/REXA200800008.md): Flap System · malfunctioned · Apr 13, 2008 · N8623A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH, FLAPS FAILED AT ZERO WHEN SELECTED DOWN. QRH FOLLOWED UNEVENTFUL ZERO FLAP LANDING. SYSTEM RESET PER FIM 27-50 AND PLACED ON SEVENTY TWO HOUR WATCH.

## 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 = 'N8623A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8623A/reports

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