N8800G

Service difficulty reports · 37

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR REXA2014070300666Light · disconnectedFLOOR ILLUMINATION EMER LIGHTS PULLED UP. CONNECTED FLOOR EMER LIGHTS. OPERATIONS CHECKED IAW AMM 33-51-01 GOOD, OK FOR SERVICE.Jul 3, 2014 · N8800G · Cndair CL6002B19 · Emergency LightingSDR REXA2014040300342Priority Valve · failedWHEN 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 SCENApr 3, 2014 · N8800G · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA2014021800214Light · unknownEMERGENCY LIGHT PBA NEEDS NEW BULBS. RELAMPED IAW AMM 31-11-00, LAMP TESTED GOOD.Feb 18, 2014 · N8800G · Cndair CL6002B19 · Emergency LightingSDR REXA2014013000146Light · inoperativeEMERGENCY LIGHTS INOPERATIVE. RELAMPED IAW AMM 33-51-16, OPERATIONS CHECKED GOOD.Jan 30, 2014 · N8800G · Cndair CL6002B19 · Emergency LightingSDR REXA2013082001119Bulkhead · crackedTHE AFT PRESSURE BULKHEAD AT FS 621 WAS FOUND TO HAVE A CRACK NEAR THE CARGO DOOR LINTEL. REPAIRED IAW REO 601R-53-61-1230.Aug 18, 2013 · N8800G · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2013080301551Computer · malfunctionedDURING 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 PROAug 3, 2013 · N8800G · Cndair CL6002B19 · Autopilot SystemSDR REXA2013052800924Life Vest · unserviceableINFANT LIFE VEST BAG TORN. R & R INFANT LIFE VEST IAW PA 25-096A.May 28, 2013 · N8800G · Cndair CL6002B19 · Life JacketSDR REXA2013052100902Smoke Goggles · missingOBSERVERS SEAT MISSING SMOKE GOGGLES.May 21, 2013 · N8800G · Cndair CL6002B19 · Emergency EquipmentSDR REXA2012121201738Mount · crackedTHE 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.Dec 11, 2012 · N8800G · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2012121101735Link · chafedRIGHT AILERON OUTBOARD PCU LINK AND AILERON LUG ARE CHAFED ON LOWER SIDE. REPAIRED IAW BOMBARDIER REO 601R-57-61-324.Dec 10, 2012 · N8800G · Cndair CL6002B19 · AileronsSDR REXA2012112601701Unknown · smokeEXPERIENCED 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 Nov 26, 2012 · N8800G · Cndair CL6002B19 · Air Distribution SystemSDR REXA2012091901355Unknown · odorON 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 SQUESep 19, 2012 · N8800G · Cndair CL6002B19 · APU Core EngineSDR REXA2012062801028Bulb · inoperativeNR 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.Jun 28, 2012 · N8800G · Cndair CL6002B19 · Emergency LightingSDR REXA2012062701029Container · tornCAPTAIN’S LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN LIFE VEST IAW AMM 25-61-03.Jun 27, 2012 · N8800G · Cndair CL6002B19 · Life JacketSDR REXA2012052400772Clamp · unsecureSMOKE 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 AMMMay 24, 2012 · N8800G · Cndair CL6002B19 · Air Distribution SystemSDR REXA2012052400773Container · tornCAPTAINS LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAINS LIFE VEST IAW AMM 25-61-03.May 24, 2012 · N8800G · Cndair CL6002B19 · Life JacketSDR REXA2012041700525Structure · dentedFOUND 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.Apr 17, 2012 · N8800G · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2012040900481Sign · brokenEMERGENCY 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.Apr 9, 2012 · N8800G · Cndair CL6002B19 · Emergency LightingSDR REXA201200135Bpsu · out of rigA/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, N3Jan 21, 2012 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201200028Flex Drive · dirtyEMERGENCY 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 2Jan 2, 2012 · N8800G · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR REXA201100989Inverter · inoperativeFWD EMERGENCY LIGHT STRIP AND SIDE WALL EMERGENCY LIGHTING INOP. REMOVED AND REPLACED NR 2 INVERTER IAW AMM 33-51-07.Dec 18, 2011 · N8800G · Cndair CL6002B19 · Emergency LightingSDR REXA201100958Ecu · defectiveFLAPS 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 27-51-0Dec 10, 2011 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100847Ecu · defectiveFLAPS 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 Nov 17, 2011 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100663Angle · crackedFS 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.Oct 14, 2011 · N8800G · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100431Window · crackedCAPT 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.Jun 27, 2011 · N8800G · Cndair CL6002B19 · Flight Compartment WindowsSDR REXA201100283Brake · malfunctionedTOOK 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.May 10, 2011 · N8800G · Cndair CL6002B19 · BrakeSDR REXA201100258Coalescer Bag · dirtyFUMES 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.May 3, 2011 · N8800G · Cndair CL6002B19 · Humidity Control SystemSDR REXA201100104Shaft · dirtyCREW 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 3Feb 10, 2011 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100103Bpsu · inoperativeCREW 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 Feb 8, 2011 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100019Shaft · lack of lubeFLAPS 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. Jan 7, 2011 · N8800G · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201000268Skin · dentedLEFT 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.Nov 19, 2010 · N8800G · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA201000267Skin · dentedTHE 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.Nov 19, 2010 · N8800G · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201000266Floorbeam · corrodedOUTBOARD 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 ENov 19, 2010 · N8800G · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR REXA201000265Beam · crackedFS 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 DEVIATINov 19, 2010 · N8800G · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201000264Plate · corrodedSERVICE DOOR STEP PLATE CORRODED. REPLACED STEP PLATE IAW CRJ200 SRM 51-42-06.Nov 19, 2010 · N8800G · Cndair CL6002B19 · Service DoorsSDR REXA200900140Pdu · failedFLAPS 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.Dec 16, 2009 · N8800G · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR 05106Warning Light · illuminatedAFTER 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 EMERGAug 20, 2005 · N8800G · Cndair CL6002B19 · Engine Thrust Reverser
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