# Service difficulty reports: N8800G

A list on [N8800G](https://openairdocs.org/aircraft/N8800G.md).

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

- [SDR REXA2014070300666](https://openairdocs.org/sdr/REXA2014070300666.md): Light · disconnected · Jul 3, 2014 · N8800G · Cndair CL6002B19 · Emergency Lighting
  > FLOOR ILLUMINATION EMER LIGHTS PULLED UP. CONNECTED FLOOR EMER LIGHTS. OPERATIONS CHECKED IAW AMM 33-51-01 GOOD, OK FOR SERVICE.
- [SDR REXA2014040300342](https://openairdocs.org/sdr/REXA2014040300342.md): Priority Valve · failed · Apr 3, 2014 · N8800G · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > WHEN SELECTING GEAR DOWN GOT GEAR DISAGREE & NOSE DOOR OPEN WARNING MSG. MSG CAME ON 3 - 5 SEC AFTER GEAR SELECTION, WE RAN THE QRH & AFTER CYCLING THE GEAR WITH ALL PUMPS ON, THE GEAR CAME DOWN & LOCKED NORMALLY. TROUBLE SHOT LG SYS IAW PA 05-018 REV K SCEN
- [SDR REXA2014021800214](https://openairdocs.org/sdr/REXA2014021800214.md): Light · unknown · Feb 18, 2014 · N8800G · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT PBA NEEDS NEW BULBS. RELAMPED IAW AMM 31-11-00, LAMP TESTED GOOD.
- [SDR REXA2014013000146](https://openairdocs.org/sdr/REXA2014013000146.md): Light · inoperative · Jan 30, 2014 · N8800G · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. RELAMPED IAW AMM 33-51-16, OPERATIONS CHECKED GOOD.
- [SDR REXA2013082001119](https://openairdocs.org/sdr/REXA2013082001119.md): Bulkhead · cracked · Aug 18, 2013 · N8800G · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > THE AFT PRESSURE BULKHEAD AT FS 621 WAS FOUND TO HAVE A CRACK NEAR THE CARGO DOOR LINTEL. REPAIRED IAW REO 601R-53-61-1230.
- [SDR REXA2013080301551](https://openairdocs.org/sdr/REXA2013080301551.md): Computer · malfunctioned · Aug 3, 2013 · N8800G · Cndair CL6002B19 · Autopilot System
  > DURING CLIMB THRU 16000 FT, ACFT JERKED ABRUPTLY LATERALLY DISPLACING ABOUT 10-20 DEGREES. ISSUE CONTINUED TO GET MORE VIOLENT AND VERY ABRUPT. DISCONNECTED THE YAW DAMPER AND ASSUMED MANUAL CONTROL. RUDDER TRIM SEEMED TO INITALLY WORK NORMAL BUT AS THE PRO
- [SDR REXA2013052800924](https://openairdocs.org/sdr/REXA2013052800924.md): Life Vest · unserviceable · May 28, 2013 · N8800G · Cndair CL6002B19 · Life Jacket
  > INFANT LIFE VEST BAG TORN. R & R INFANT LIFE VEST IAW PA 25-096A.
- [SDR REXA2013052100902](https://openairdocs.org/sdr/REXA2013052100902.md): Smoke Goggles · missing · May 21, 2013 · N8800G · Cndair CL6002B19 · Emergency Equipment
  > OBSERVERS SEAT MISSING SMOKE GOGGLES.
- [SDR REXA2012121201738](https://openairdocs.org/sdr/REXA2012121201738.md): Mount · cracked · Dec 11, 2012 · N8800G · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE RUBBER MOUNTS ON FS 621 BULKHEAD AT RBL 7 AND LBL 7 ARE CRACKED. REMOVED AND REPLACED IAW SRM 51-42-06/51-40-11.
- [SDR REXA2012121101735](https://openairdocs.org/sdr/REXA2012121101735.md): Link · chafed · Dec 10, 2012 · N8800G · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON OUTBOARD PCU LINK AND AILERON LUG ARE CHAFED ON LOWER SIDE. REPAIRED IAW BOMBARDIER REO 601R-57-61-324.
- [SDR REXA2012112601701](https://openairdocs.org/sdr/REXA2012112601701.md): Unknown · smoke · Nov 26, 2012 · N8800G · Cndair CL6002B19 · Air Distribution System
  > EXPERIENCED VISIBLE SMOKE/FUME FOLLOWED BY A SMOKE TOILET CAUTION MESSAGE AFTER TRANSFERRING ENGINE BLEEDS TO APU ON APPROACH INTO BWI. RAN ENGINE WITH APU WITH PACKS ON UNABLE TO DUPLICATE PROBLEM AT THIS TIME. INSPECTED LAVATORY SPEED TAPE AND FOUND TO BE
- [SDR REXA2012091901355](https://openairdocs.org/sdr/REXA2012091901355.md): Unknown · odor · Sep 19, 2012 · N8800G · Cndair CL6002B19 · APU Core Engine
  > ON FLIGHT 4317 FROM IND TO RDU APU PRODUCED SMOKE SMELL AND SMOKE TOLIET MESSAGE ON DECENT WHEN PACKS RUN OFF OF APU. SMELL WENT AWAY WHEN SWITCHED BACK TO 10TH STAGE BLEEDS. MAINTENANCE DEFERRED THE APU. COMPLETED APU OPS CHECKS AND BLEED AIR TRANSFER SQUE
- [SDR REXA2012062801028](https://openairdocs.org/sdr/REXA2012062801028.md): Bulb · inoperative · Jun 28, 2012 · N8800G · Cndair CL6002B19 · Emergency Lighting
  > NR 3 CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 3 CEILING EMERGENCY LIGHT BLUB IAW AMM 33-50-00. OPS CHECK GOOD AT THIS TIME.
- [SDR REXA2012062701029](https://openairdocs.org/sdr/REXA2012062701029.md): Container · torn · Jun 27, 2012 · N8800G · Cndair CL6002B19 · Life Jacket
  > CAPTAIN’S LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012052400772](https://openairdocs.org/sdr/REXA2012052400772.md): Clamp · unsecure · May 24, 2012 · N8800G · Cndair CL6002B19 · Air Distribution System
  > SMOKE IN COCKPIT BLACK SMOKE BURNT ODOR, RETURNED TO GATE. QRH PERFORMED, HAPPENED PRIOR TO TAKING RUNWAY, NOTED COMING FROM FIRST OFFICER'S GASPER. SECURED CLAMP, OP CHECKED GOOD WITH NO DEFECTS NOTED IAW AMM
- [SDR REXA2012052400773](https://openairdocs.org/sdr/REXA2012052400773.md): Container · torn · May 24, 2012 · N8800G · Cndair CL6002B19 · Life Jacket
  > CAPTAINS LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAINS LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012041700525](https://openairdocs.org/sdr/REXA2012041700525.md): Structure · dented · Apr 17, 2012 · N8800G · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND DENT AT FS 310, 1/4W X 9/16L BY PAX DOOR. EA NO: CRJ253-00495 DENT REPAIR COMPLIED WITH IAW REO601R-53-21-160. PERMANENT REPAIR NO FURTHER ACTION REQUIRED. OK FOR SVC.
- [SDR REXA2012040900481](https://openairdocs.org/sdr/REXA2012040900481.md): Sign · broken · Apr 9, 2012 · N8800G · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT SIGN BY THE GALLEY SERVICE DOOR IS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT SIGN BY GALLEY SERVICE DOOR IAW AMM 33-50-00, OK FOR SERVICE.
- [SDR REXA201200135](https://openairdocs.org/sdr/REXA201200135.md): Bpsu · out of rig · Jan 21, 2012 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Control System
  > A/C REQUIRES APPROX HALF LEFT TRIM AND 1/4 LEFT YOLK TO MAINTAIN WINGS LEVEL AT FLAPS 45 DEGREE ON FINAL. RIGGED BPSU IAW 27-54-00, PERFORMED CHECK OF LT/RT FLAP RIG, IAW AMM 27-54-00. FOUND WITHIN LIMITS. REFER TO CONTINUATION CARDS FOR FURTHER DETAILS, N3
- [SDR REXA201200028](https://openairdocs.org/sdr/REXA201200028.md): Flex Drive · dirty · Jan 2, 2012 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > EMERGENCY DECLARED FOR FLAPS FAIL CAUTION MSG IN FLIGHT, PERFORMED T/S PER BOMBARDIER FIM REV 39 IAW AD2009-06-12 PARA (N)(6)(I), AMOC DATED MARCH 27, 2009 TR#27-012 PER AMOC DATED DEC18,2009 AND PA AD 27-052G, WITH NEWEST FIM REV 42 AS T/S AID. SEE DISC NR 2
- [SDR REXA201100989](https://openairdocs.org/sdr/REXA201100989.md): Inverter · inoperative · Dec 18, 2011 · N8800G · Cndair CL6002B19 · Emergency Lighting
  > FWD EMERGENCY LIGHT STRIP AND SIDE WALL EMERGENCY LIGHTING INOP. REMOVED AND REPLACED NR 2 INVERTER IAW AMM 33-51-07.
- [SDR REXA201100958](https://openairdocs.org/sdr/REXA201100958.md): Ecu · defective · Dec 10, 2011 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 0 DEGREES ON APPROACH. 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 REPLACED FECU IAW AMM 27-51-0
- [SDR REXA201100847](https://openairdocs.org/sdr/REXA201100847.md): Ecu · defective · Nov 17, 2011 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL MSG AT 8000 FEET. COMPLETED THE QRH AND DECLARED THE EMERGENCY WITH APPROACH. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED MARCH 27, 2009 AND TR #27-012 PER AMOC DATED DECEMBER 18, 2009 AND
- [SDR REXA201100663](https://openairdocs.org/sdr/REXA201100663.md): Angle · cracked · Oct 14, 2011 · N8800G · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 559 BULKHEAD CAP ANGLE CRACKED AT 4 LOCATIONS LBL 9, LBL 18, RBL 9, RBL 18. WEB CRACKED AT BL 18. REPAIRED IAW PA53-0025 AND BOMBARDIER REOS 601R-53-41-260 E AND 601R-53-41-609 B.
- [SDR REXA201100431](https://openairdocs.org/sdr/REXA201100431.md): Window · cracked · Jun 27, 2011 · N8800G · Cndair CL6002B19 · Flight Compartment Windows
  > CAPT SIDE WINDOW CRACKED AT FL 280. EN ROUTE TO MSP. DIVERTED TO IND FOR PRECAUTIONARY LANDING. MAINT REPLACED LT SIDE WINDOW IAW AMM 56-12-01.
- [SDR REXA201100283](https://openairdocs.org/sdr/REXA201100283.md): Brake · malfunctioned · May 10, 2011 · N8800G · Cndair CL6002B19 · Brake
  > TOOK 61 PERCENT TO TAXI A/C ONCE GOT A/C ROLLING AND DROPPED THRUST IT INSTANTLY STOPPED BRAKE TEMPS ARE FINE NO OTHER INDICATIONS DEPLANING PASSENGERS. REMOVED AND REPLACED RT O/B BRAKE IAW AMM 32-43-26, OPS CHECKS GOOD, OK FOR SERVICE.
- [SDR REXA201100258](https://openairdocs.org/sdr/REXA201100258.md): Coalescer Bag · dirty · May 3, 2011 · N8800G · Cndair CL6002B19 · Humidity Control System
  > FUMES IN CABIN. C/W WORKSCOPE AND REMOVED AND REPLACED LT + RT PACK WATER SEPARATOR SOCKS IAW AMM 21-51-13 OPC GOOD NO FUMES NOTED.
- [SDR REXA201100104](https://openairdocs.org/sdr/REXA201100104.md): Shaft · dirty · Feb 10, 2011 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAP FAIL IN FLIGHT ON EXTENSION. FLAP POSITION WAS 0 DEGREES AIRSPEED 190KTS FLIGHT TIME 1HR 20MIN AT FAILURE TEMP -18C. EMERGENCY WAS NOT DECLARED AND FLIGHT LANDED UNEVENTFULLY. MAINTENANCE PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 3
- [SDR REXA201100103](https://openairdocs.org/sdr/REXA201100103.md): Bpsu · inoperative · Feb 8, 2011 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTS FLAPS FAIL AT 0 DEGREES WHEN SELECTED DOWN. EMERGENCY WAS DECLARED AND THE LANDING WAS UNEVENTFUL. UPON ARRIVAL, MAINTENANCE TROUBLESHOT PER BOMBD FIM REV 39 IAW AD 2009-06-12 PARAGRAPH H6I USING FIM REV 39 PER AMOC DATED MAR 27, 2009 TR 27-012
- [SDR REXA201100019](https://openairdocs.org/sdr/REXA201100019.md): Shaft · lack of lube · Jan 7, 2011 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 0' ON APPROACH (FECU CODES JAM, LEFT BPSU, WIRING LEFT BPSU - 5 1B,5 2B,9 1A,9 2A,17 1A,25BC,17 2A). PERFORMED T/S 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 DEC 18,2009.
- [SDR REXA201000268](https://openairdocs.org/sdr/REXA201000268.md): Skin · dented · Nov 19, 2010 · N8800G · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP OUTER LOWER SKIN HAS TWO DENTS - GOUGE 0.500" X 1.500" X 0.030". PERFORMED A MAJOR REPAIR TO THE LEFT INBOARD FLAP OUTER LOWER SKIN IAW CRJ 200 SRM 57-52-00, INBOARD FLAP AND VANE - REPAIR 3 - NON-FLUSH REPAIR TO INBOARD FLAP SKIN.
- [SDR REXA201000267](https://openairdocs.org/sdr/REXA201000267.md): Skin · dented · Nov 19, 2010 · N8800G · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN HAS A DENT JUST FORWARD OF FS 379 BETWEEN STR 20R - STR 21R MEASURING 3.2" X 2.1" X 0.102" DEEP. PERFORMED A MAJOR REPAIR TO DAMAGED AREA IAW BOMBARDIER SERVICES CORPORATION ENGINEERING ORDER 601R-53-19853.
- [SDR REXA201000266](https://openairdocs.org/sdr/REXA201000266.md): Floorbeam · corroded · Nov 19, 2010 · N8800G · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > OUTBOARD FLANGE OF FLOORBEAM AT LBL 27 IS CORRODED AROUND NUT PLATE TABS/ HOLES FROM FS 600 TO FS 621. FOUND CORROSION BEYOND LIMITS ON P/N 601R35031-263. REMOVED AND REPLACED FLOORBEAM CAP, P/N 601R35031-263, IAW CRJ BOMBARDIER REO 601R-53-61-3778 AND BSC E
- [SDR REXA201000265](https://openairdocs.org/sdr/REXA201000265.md): Beam · cracked · Nov 19, 2010 · N8800G · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 TRANSVERSE BEAM IS CRACKED IN LOWER RADIUS 1.0 INCH ON THE OUTBOARD SIDES OF LBL 9 AND RBL 9 AND THE UPPER FLANGE (COCKPIT THRESHOLD) AND FORWARD J ANGLE ARE CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND IAW BSC SR 601R-53-0110 DEVIATI
- [SDR REXA201000264](https://openairdocs.org/sdr/REXA201000264.md): Plate · corroded · Nov 19, 2010 · N8800G · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR STEP PLATE CORRODED. REPLACED STEP PLATE IAW CRJ200 SRM 51-42-06.
- [SDR REXA200900140](https://openairdocs.org/sdr/REXA200900140.md): Pdu · failed · Dec 16, 2009 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAIL AT O DEGREES IN FLIGHT. NORMAL TOUCH DOWN ON LANDING. REMOVED AND REPLACED FLAP PDU IAW AMM 27-52-01, FLAPS OP CHECK GOOD IAW AMM 27-51-00.
- [SDR 05106](https://openairdocs.org/sdr/05106.md): Warning Light · illuminated · Aug 20, 2005 · N8800G · Cndair CL6002B19 · Engine Thrust Reverser
  > AFTER TAKEOFF AND CLIMBOUT FROM XNA, THE FLIGHT CREW RECEIVED A NUMBER 2 ENGINE THRUST REVERSER UNLOCKED MESSAGE AND THE N1 REV ICON APPEARED. THE FLIGHT CREW REDUCED POWER ON NUMBER TWO ENGINE AND ACCOMPLISHED MEMORY ITEMS. THE FLIGHT CREW DECLARED AN EMERG

## 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 = 'N8800G' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8800G/reports

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