N8847A

Service difficulty reports · 106

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 = 'N8847A' 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 REXA2016081601708Seat Track · corrodedLT NR 1 SEAT TRACK FROM BS 364 - 394 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.Aug 16, 2016 · N8847A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016081501711Seat Track · corrodedNR 4 SEAT TRACK FROM BS 409+112 - 439 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.Aug 15, 2016 · N8847A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016081501709Seat Track · corrodedLT NR 4 SEAT TRACK FROM BS 409+112 - 449.85 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.Aug 15, 2016 · N8847A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016081501707Support Fitting · crackedLEFT WINDSHIELD SIDE POST LT SUPPORT FITTING CRACKED. REMOVED & REPLACED THE SUPPORT FITTING IAW SRM 51-42-21.Aug 15, 2016 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2016081301688Fitting · crackedLEFT FUSELAGE CLIP AT STR 3 LT AND FS 280 IS CRACKED. R & R CLIP IAW SRM 51-42-21 AND SRM 51-42-06.Aug 13, 2016 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2016080601484Light · disconnectedSECTION OF EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. FOUND SECTION OF EMERGENCY FLOOR TRACK LIGHTING TO BE DISCONNECTED. CONNECTED THE LIGHT IAW AMM 20-10-00-910-803. OPS CHECKED IAW AMM 33-51-00, NO OTHER DEFECTES NOTED AT THIS TIME.Aug 6, 2016 · N8847A · Cndair CL6002B19 · Light System WiringSDR REXA2016051000712Light · inoperativeEMERGENCY FLOOR LIGHTS FROM ROW 2 - 6 INOPERATIVE. R & R CABIN EMER FLOOR LIGHT ASSEMBLY 2, NR 2 INVERTER PS2LY IAW AMM 33-51-00 & WM 33-51-00 PG 7. OPERATIONAL CHECKED GOOD.May 10, 2016 · N8847A · Cndair CL6002B19 · Emergency LightingSDR REXA2016050100662Light · inoperativeFLOOR EMER LIGHTS NOT ILLUMINATING ON FWD SECTION. R & R FLOOR TRACK EMER LIGHT FLOOR STRIP, DS13LY, NR 2 IAW AMM 33-51-01. R & R EMER BATTERY PACK NR 2 IAW AMM 33-51-04. PERFORMED OPERATIONS TEST OF EMER LIGHTS IAW AMM 33-51-00. OPERATIONS TESTED GOOD.May 1, 2016 · N8847A · Cndair CL6002B19 · Emergency LightingSDR REXA2016042000639Connector · looseCENTER AISLE EMER LIGHTS INOPERATIVE, FWD SECTION, FOUND LOOSE PLUG AT FLOOR CONNECTOR FOR FWD FLOOR EMER LIGHTS. PROPERLY CONNECTED LIGHTS & REINSTALLED COVERS IAW AMM 33- 51-01. OPERATIONS CHECKED GOOD.Apr 20, 2016 · N8847A · Cndair CL6002B19 · Light System WiringSDR REXA2016032700439Connector · unsecureEMERGENCY FLOOR STRIP LIGHTING 1/2 OUT. SECURED FLOOR EMER LIGHT CONNECTIONS. ALL LIGHTS WORK NORMALLY, DONE IAW AMM 33-51-01 & 33-51-00.Mar 27, 2016 · N8847A · Cndair CL6002B19 · Light System WiringSDR REXA2016032400438Connector · not seatedFLOOR PATH EMER INOPERATIVE ROWS 1- 5. RESEATED CONNECTOR UNDER FLOOR IN AVIONICS BAY. EMER FLOOR PATH LIGHTING, OPERATIONS CHECKED GOOD IAW AMM 33-51-00.Mar 24, 2016 · N8847A · Cndair CL6002B19 · Light System WiringSDR REXA2015120301169Cover · tornLIFE VEST COVER ON COPILOT SEAT TORN. REPLACED LIFE VEST COVER IAW CMM 25-14-10.Dec 3, 2015 · N8847A · Cndair CL6002B19 · Life JacketSDR REXA2015092500907Roller · dirtyMAIN CABIN DOOR HANDLE HARD TO CLOSE BY FLIGHT ATTENDANT. CLEANED & LUBED MAIN CABIN DOOR, FOUND DIRT & DEBRIS IN INNER HANDLE ROLLER. PERFORMED OPERATIONS CHECK IAW 52-11-00. ALSO INSPECTED DOOR, NO DEFECTS NOTED. OPERATIONS CHECKED GOOD.Sep 25, 2015 · N8847A · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA2015050200459Unknown · malfunctionedBRAKE EFFECTIVENESS WAS NOT NORMAL UPON TOUCHDOWN & LANDING. RT SIDE BRAKES SEEM LIGHT OR LESS EFFECTIVE AT HIGH SPEEDS, TOUCHDOWN & ROLLOUT. RIGHT SIDE BRAKE TEMP, ONLY 1. REST OF BRAKE TEMPS 5 OR HIGHER. OPERATIONS CHECK DONE OF BRAKES IAW AMM 32-43-26.May 2, 2015 · N8847A · Cndair CL6002B19 · Landing Gear Brake SystemSDR REXA2015022300311Apu · malfunctionedBURNING SMELL DURING CLIMB. WIP ON DM 000659 APU AUTO SHUT DOWN. WIP ON WORK SCOPE SMOKE & FUMES IN CABIN & COCKPIT IAW AML 3185062. INSP BLEED DUCT & CHECK VLV OFF APU IAW IPC 36-11-10 FIG ITEM 225A SPECIALLY THE INNER DIAMETER IAW MOTR RD IAW AML 3185065.Feb 23, 2015 · N8847A · Cndair CL6002B19 · APU Core EngineSDR REXA2015022100245Coalescer Bag · contaminatedRECEIVED SMOKE TOILET CAUTION MSG CLIMBING THROUGH 2,000 FEET. WE SMELLED SMOKE IN COCKPIT. FLIGHT ATTENDANT REPORTED SEEING & SMELLING SMOKE IN LAVATORY. IN RESPONSE TO THE SMOKE TOILET CAUTION MSG, LANDED AT 44,300 IBS, NORMAL LANDING AR0UND 200' MIN BTMSFeb 21, 2015 · N8847A · Cndair CL6002B19 · Humidity Control SystemSDR REXA2015020600186Seal · missingFLIGHT ATTENDANT PBE IS MISSING IN SEAL. INSTALLED PBE SECURITY SEAL AS REQUIRED.Feb 6, 2015 · N8847A · Cndair CL6002B19 · Emergency EquipmentSDR REXA2014120300918Flap · dentedLEFT INBD FLAP DENTED AT WS 57, 9 INCHES FWD OF TE. REPAIRED IAW SRM 57-52-00.Dec 2, 2014 · N8847A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2014120800920Vane · chafedLEFT INBD FLAP VANE LE CHAFED IN THREE LOCATIONS MEASURING 0.040 INCHES, 0.033 INCHES, & 0.014 INCHES DEEP. REPAIRED IAW REO 601R-57-52-004.Dec 1, 2014 · N8847A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2014112500915Skin · corrodedDURING INSPECTION, FOUND CORROSION ON THE PANEL LANDING FOR PANELS 640AT, 640BT & 640CT ON THE RT UPPER WING SKIN AT WS 74.15, WS 96.34 & WS 114.27. REPAIRED IAW EA CRJ257-03093.Nov 25, 2014 · N8847A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2014102800903Skin · dentedDURING ROUTINE LINE MAINTENANCE FOUND THE FUSELAGE SKIN TO BE DENTED BETWEEN FS 610 & FS 621 & STRINGER 21L - 22L, MEASURING 6.5 INCHES X 2.35 INCHES X 0.050 INCHES DEEP. REPAIRED IAW EA CRJ253-03030.Oct 28, 2014 · N8847A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA2014091700960Light · inoperativeLEFT NR 3 EXTERIOR EMER LIGHT INOPERATIVE. DEFERRED - REMAINS DEFERRED. MORE INFORMATION TO COME.Sep 17, 2014 · N8847A · Cndair CL6002B19 · Emergency LightingSDR REXA2014072200730Fire Bottle · low pressureLAVATORY FIRE EXTINGUISHER BOTTLE READS IN THE RED. DEFERRED R & R LAVATORY FIRE EXTINGUISHER IAW AMM-26-26-01. THIS CLEARS DM 007206.Jul 22, 2014 · N8847A · Cndair CL6002B19 · Fire Bottle, FixedSDR REXA2014070300664Battery · dischargedFIRST OFFICER`S EMER FLASHLIGHT BATTERY INDICATOR NOT FLASHING. R & R FIRST OFFICER`S EMER FLASHLIGHT BATTERY IAW AMM 25-61-00. OPERATIONS CHECKED GOOD, OK FOR SERVICE.Jul 3, 2014 · N8847A · Cndair CL6002B19 · Emergency EquipmentSDR REXA2014041700382Seal · missingFLIGHT ATTENDANT PBE MISSING SEAL. R & R PBE SEAL IAW AMM 35-30-00, OK FOR SEAL.Apr 17, 2014 · N8847A · Cndair CL6002B19 · Emergency EquipmentSDR REXA2014021200202Accumulator · defectiveAIR RETURNED DTW DUE TO GEAR DISAGREE & ASSOC, HYD 3 LO PRESS, MSG, NON-EMERGENCY. AFTER TAKEOFF WE GOT A HYD 3 LO PRESS CAUTION MESSAGE. SOON THEREAFTER, WE GOT GEAR DISAGREE WARNING MESSAGE WITH ALL THREE BOXES IN RED. AFTER THE HYD 3 MESSAGE WENT AWAY ONFeb 11, 2014 · N8847A · Cndair CL6002B19 · Landing Gear Brake SystemSDR REXA2014020500175Hydraulic System · contaminatedON TAKEOFF WHEN GEAR HANDLE RAISED, RECEIVED HYDRAULIC 3 LOW PRESS, CAUTION MSG, COULD HEAR THAT GEAR WAS IN TRANSIT, BUT TOOK ABOUT 40+ SECONDS TO NOSE GEAR UP. WHEN IT LOCKED UP, WE RECEIVED, MASTER WARNING, GEAR DISAGREE APPROXIMATELY 10 SECONDS LATER. COFeb 5, 2014 · N8847A · Cndair CL6002B19 · Hydraulic System, MainSDR REXA2013102901781Pump · contaminatedGEAR DISAGREE WHEN GEAR RETRACTED. FOUND NR 3 HYD HAD AIR IN PUMP.Oct 29, 2013 · N8847A · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR REXA2013102501777Detector · out of adjustFLAPS FAIL CAUTION MSG WHEN SELECTING FLAPS TO 20 ON THE AFTER START CHECK. ACFT WILL NEED A REPLACEMENT FLAP FAIL EVENT CARD. PERFORMED TROUBLESHOOTING IAW FIM, REV 44 IAW AD 2009-06-12, PARA H6I AMOL DATED DECEMBER 07.2012 AND PA AD 27-052L. FOUND SKEW DEOct 25, 2013 · N8847A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA2012112201696Priority Valve · malfunctionedAFTER TAKEOFF ON FLIGHT 3915 FROM AZO TO DTW IMMEDIATELY AFTER SELECTING GEAR UP RECEIVED THE FOLLOWING MESSAGE: HYD 3 LO PRESS CAUTION - LOW PRESS QTY 100 PERCENT, NOSE GEAR DOOR OPEN WARNING, GEAR DISAGREE WARNING. ALL 3 MESSAGES EXTINGUISHED BEFORE CHECKLINov 22, 2012 · N8847A · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA2012102601424Connector · not seatedON FLIGHT 4291 (ICT TO MSP) HYDRAULIC QUANTITY NR 1 READOUT ERRATIC & INTERMITTENT. ON APPROACH INTO MSP RECEIVED GEAR DISAGREE. TWO MAINS NOT DOWN AND LOCKED. FOLLOWED QRH PULLED GEAR RELEASE HANDLE & GOT 3 DOWN & GREEN INDICATION. HYD SYS NR 1 READOUT TROct 25, 2012 · N8847A · Cndair CL6002B19 · Landing Gear System WiringSDR REXA2012101901413Life Vest · unserviceableOBSERVER LIFE VEST BAG TORN. REMOVED AND REPLACED OBSERVER LIFE VEST IAW AMM 25-61-03.Oct 19, 2012 · N8847A · Cndair CL6002B19 · Life JacketSDR REXA2012091401342Lever · faultyRECEIVED FLAPS FAIL CAUTION ON APPROACH INTO DTW WITH FLAPS AT 8 DEGREES. REMOVED AND REPLACED FLAP LEVER IAW AMM CRJ 200 AMM 27-51-01. OPS CHECK GOOD. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 43. IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED APSep 14, 2012 · N8847A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA2012071901172Power Supply · malfunctionedFLIGHT 3922, RECEIVED A "FLAPS FAIL" AT 0 DEGREES DURING CLIMB-OUT (14000'). EMERGENCY DECLARED. PERFORMED TROUBLESHOOTING PER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I). REMOVED AND REPLACED RIGHT HAND BPSU IAW AMM 27-51-10. OPS CHECKED GOOD.Jul 19, 2012 · N8847A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA2012061600846Light · inoperativeROW 1 CD EMERGENCY LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED ROW 1 CD EMERGENCY LIGHT STRIP IAW AMM 33-51-01. OPS CHECKS GOOD.Jun 16, 2012 · N8847A · Cndair CL6002B19 · Emergency LightingSDR REXA201101026Sensing Element · defectiveABORTED TAKEOFF, ANTI-ICE DUCT WARNING MESSAGE AND DUCT FAIL OVER HEAD LIGHT ILLUMINATED ON T/O ROLL. SYNOPOTIC PAGE SHOWED RED LINE ON RT FUSELAGE MESSAGE REMAINED ON AFTER ENGINES WERE SHUT DOWN. REMOVED AND REPLACED FUSELAGE SENSING ELEMENT A18WK IAW AMM Dec 27, 2011 · N8847A · Cndair CL6002B19 · Pneumatic Indicating SystemSDR REXA201100944Bulkhead · crackedFS 559 SEMI-PRESSURE BULKHEAD FOUND CRACKED. REPAIRS IAW BOMBARDIER REOS 601R-53-41-260 REV E, 601R-53-41-609, AND PINNACLE PA53-025.Dec 16, 2011 · N8847A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100784Warning System · false activationAFTER APU IN FLT AND ABOUT 30 SEC AFTER BLEEDS WERE TRANSFERED TO THE APU, RECEIVED APU OVERTEMP WARNING MSG FOR ABOUT 5 SECS THEN BACK OUT. PERFORMED OP CHECK OF APU IAW AMM 49-10-00. OP CHECK NORMAL. OK FOR SERVICE.Oct 26, 2011 · N8847A · Cndair CL6002B19 · APU Indicating SystemSDR REXA201100178Angle · crackedFS 559 SEMI PRESSURE BULKHEAD CAP ANGLE RADIUS CRACK INDICATION AT LBL 9, .5 INCH LONG, AT LBL 18 1.5 INCH LONG, AT RBL 18.5 INCH LONG. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 REV E AND REO 601R-53-53-41-609 REV B.Mar 17, 2011 · N8847A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100170Bulkhead · chafedFS 621 PRESSURE BULKHEAD FWD SKIN HAS FIVE CHAFES AT WL 103.5 BETWEEN LBL 27 AND RBL 35. REPAIR IAW BOMBARDIER REO 601R-53-61-2155.Mar 14, 2011 · N8847A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100171Support Angle · damagedTHE FRAME SECTOR AFT SUPPORT ANGLE AT FS 682.00 AT STRINGER 27 BETWEEN LBL 2.5 AND RBL 6 IS CRACKED AND BENT. REPAIR IAW BOMBARDIER SERVICE CORPORATION EO 601R-53-20849B.Mar 13, 2011 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100172Beam · damagedFS 280 BETWEEN LBL 20.75 AND RBL 20.75 TRANSVERSE BEAM AND UPPER "J" ANGLES ARE CRACKED AND CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-11-426 AND BOMBARDIER SERVICE CORPORATION EO 601R-53-20850, AND SR 601R-53-0110.Mar 12, 2011 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100173Floor Support · crackedCARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 RBL 45 FOUND CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-61-117 REV C AND BOMBARDIER SERVICE CORPORATION EO 601R-53-020873.Mar 11, 2011 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100166Bulkhead · crackedPERFORMED EDDY CURRENT OF THE 202.75 BULKHEAD AT BL 23.75 AND FOUND INDICATIONS NOTED APPROX .5" IN LENGTH AT 90 PERCENT FSH. REPAIR IAW BOMBARIDER REO 601R-53-11-563 AND BOMBARDIER SERVICE CORPORATION STANDARD REPAIR 601R-53-0101A.Mar 9, 2011 · N8847A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100167Skin · dentedTHREE DENTS FOUND ON THE RIGHT SIDE OF THE FUSELAGE. FIRST AT FS 402 MEASURING .8" X .7" X 0.010". SECOND AT FS 424.6 MEASURING 2" X 1.4" X 0.020". THIRD AT FS 427.5 MEASURING 1.5" X 1.1" X 0.011". ALL DENTS LOCATED BETWEEN S-15R AND S-16R. THE DENTS WERMar 8, 2011 · N8847A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201100169Vane · chafedLEFT INBOARD FLAP VANE HAS CHAFE DAMAGE AT THREE AREAS ON LEADING EDGE AT STOP CONTACT AREAS. REMOVED DAMAGE BY BLENDING (MATERIAL REMOVED APPROX 0.010"). REPAIRED IAW BOMBARDIER REO 601R-57-52-004 REV C.Mar 7, 2011 · N8847A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA201100168Vane · chafedRT INBOARD FLAP VANE HAS CHAFE DAMAGE AT THREE AREAS ON LEADING EDGE AT STOP CONTACT AREAS. REMOVED CHAFE DAMAGE BY BLENDING AREAS (MATERIAL REMOVED APPROX .010"). REPAIRED IAW BOMBARDIER REO 601R-57-52-004 REV C.Mar 7, 2011 · N8847A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA201100165Skin · corrodedLT WING PLANK ACCESS HOLE (NR 2) OF PANEL 510AB, WS 12.245 FOUND CORRODED AND PITTED AROUND OPENING, EXTERNAL UNPAINTED AREA. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.Mar 7, 2011 · N8847A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA201100164Skin · corrodedRIGHT WING PLANK ACCESS HOLE (NR 1) 640BB AT WS 54.897 FOUND CORRODED AND PITTED AROUND OPENING, EXTERNAL UNPAINTED AREA. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.Mar 7, 2011 · N8847A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA201100163AVane · chafedLEFT INBOARD FLAP VANE HAS CHAFE DAMAGE AT THREE AREAS ON LEADING EDGE AT STOP CONTACT AREAS. REMOVED DAMAGE BY BLENDING (MATERIAL REMOVED APPROX 0.010"). REPAIRED IAW BOMBARDIER REO 601R-57-52-004 REV C.Mar 7, 2011 · N8847A · Cndair CL6002B19 · Trailing Edge Flaps
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