N8903A, cancelled Dec 23, 2024

Service difficulty reports · 63

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 = 'N8903A' AND deregistration_id = 'N8903A-2024-12-23'
  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 REXA2022081601867Inverter · inoperativeLH INTERIOR EMERGENCY DOOR BOTTON SIGN INOP. R/R INVERTER @ LOCATION FS 424L IAW CRJ 200 AMM 31-5-07. OPS CHECK GOOD. PN ON/OFF 5925-7.Aug 6, 2022 · N8903A · Cndair CL6002B19 · Emergency LightingSDR SWIA2020022748868Warning Message · multiple failAFTER TAKE WE GOT STEERING INOP CAUTION MESSAGE . FOLLOW BY A WOW IMPUT CAUTION AND A WOW OUTPUT FAIL STATUS MESSAGE C/W QRH AND RETURN TO FIELD WITH NO OVER WEIGHT LANDING FLIGHT 3610 - FILED CLOSED THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 20547984 WIFeb 27, 2020 · N8903A · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA20190405731Uplock · failedON APPROACH RIGHT GEAR DISAGREE WARNING MESSAGE. CYCLED GEAR, ALL THREE GREEN INDICATION. LANDED WITHOUT INCIDENT. (FLT#7427) REMOVED AND REPLACED RT MLG UPLOCK ASSY IAW AMM. OPS AND LEAK CHECK GOOD AT THIS TIME.Apr 4, 2019 · N8903A · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2018060444750Strap · corrodedCABIN FLOORBEAM STRAP CORRODED AT BS 559, LBL 35. REMOVE AND REPLACED THE STRAP IAW SRM.May 20, 2018 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018060444749Floorbeam · corrodedFLOORBEAM FITTING AT BS 615, LBL 27 HAD CORROSION ON THE OTBD FLANGE. PERFORMED A REPAIR TO THE FLOORBEAM IAW REO.May 12, 2018 · N8903A · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2018060444748Floor Support · corrodedLBL 27 FLOOR SUPPORT UPPER CAP INBOARD AND OUTBOARD FLANGES CORRODED BETWEEN BS 569 AND 610. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.May 11, 2018 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018060444747Floor Support · corrodedLEFT FLOOR SUPPORT CORRODED AT NUTPLATE LOCATIONS BETWEEN BS 574 AND 621 AND ONE SHEARED RIVET AT BS 589. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.May 11, 2018 · N8903A · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA2018060444746Skin · chafedLEFT INBD FLAP VANE LEADING EDGE SKIN CHAFED NEAR OTBD END. REPLACED THE FLAP VANE LEADING EDGE SKIN IAW SRM.May 8, 2018 · N8903A · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018060444745Skin · chafedLEFT INBD FLAP VANE LEADING EDGE SKIN CHAFED NEAR INBD END. REMOVED AND REPLACED FLAP VANE IAW SRM.May 8, 2018 · N8903A · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018060444744Vane · chafedRIGHT INBD FLAP VANE TRAILING EDGE UPPER SURFACE CHAFED NEAR THE INBD END OF VANE. BLENDED THE DAMAGE IAW SRM AND REO.May 8, 2018 · N8903A · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642205Vane · chafedLEFT INBD FLAP VANE L/E MIDDLE SECTION CHAFED. R & R LT INBD FLAP VANE L/E MIDDLE SECTION AT APPROXIMATELY LT WS 93 - 130 IAW SRM AND EA.May 20, 2016 · N8903A · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642204Vane · chafedRIGHT INBD FLAP VANE LE CHAFED INBD SIDE. THE L/E SECTION WAS REMOVED, NEW OTBD MID SECTION, PN: 601R14303-52, WAS INSTALLED IAW SRM.May 17, 2016 · N8903A · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201541253Battery Pack · inoperativeALL EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED NR 1 AND 2 EMERGENCY BATTERY PACKS IAW AMM. OPS CHECKED GOOD.Jun 4, 2015 · N8903A · Cndair CL6002B19 · Emergency LightingSDR REXA2014100301015Light · inoperativeEMERGENCY STRIP LIGHT AT 1C INOPERATIVE. R & R EMER FLOOR LIGHT STRIP AT 1C IAW AMM 33-51-01. OPERATIONS CHECKED GOOD, OK FOR SERVICE.Oct 3, 2014 · N8903A · Cndair CL6002B19 · Emergency LightingSDR REXA2014092701001Door Seal · dirtyLOUD SQUEAL FROM MAIN CABIN DOOR DURING DESCENT. PRESSURIZATION WAS NORMAL. INSPECTED DOOR SEAL & CLEANED SEAL IAW 52-11-10. OPERATIONS CHECKED DOOR, NO DEFECT NOTED, OK FOR SERVICE.Sep 27, 2014 · N8903A · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA2014060200546B-Nut · looseGOT A VERY STRONG SMELL OF FUEL IN FLIGHT CHECK WITH THE FLIGHT ATTENDANT & SHE DID NOT SMELL ANYTHING IN THE CABIN, ALL INDICATIONS NORMAL. WORE O2 MASK TO LANDING AS A PRECAUTION. AFTER LANDING SMELL PERSISTED. TIGHTENED B NUT AT APU FUEL CONTROL UNIT & SJun 2, 2014 · N8903A · Cndair CL6002B19 · APU Engine Fuel and ControlSDR REXA2014052800531Connector · not seatedFLOOR TRACK EMERGENCY LIGHT STRIP INOPERATIVE ROW 1. RESEATED CONNECTOR FOR AFFECTED STRIP OPERATIONS CHECKED GOOD IAW AMM 33-51-21.May 28, 2014 · N8903A · Cndair CL6002B19 · Light System WiringSDR REXA2014041800389Battery · dischargedON PREFLIGHT FOUND FIRST OFFICER'S FLASHLIGHT DEAD. REPLACED BATTERY IN FLASHLIGHT IAW STANDARDS PRACTICES CH 20.Apr 18, 2014 · N8903A · Cndair CL6002B19 · Emergency EquipmentSDR REXA2014041600067Skin · corrodedLOWER WING PLANK ACCESS HOLE FOR PANEL 510AB HAS CORROSION MEASURING 10" X 0.185" X 0.007" DEEP. REPAIRED IAW REO 601R-57-21-030.Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2014041400064Skin · corrodedLEFT LOWER WING PLANK ACCESS HOLE 540DB HAS CORROSION AROUND NON-CRITICAL REGION, MEASURING 4 INCHES X 0.185 INCHES X 0.001 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2014041400063Skin · gougedRIGHT WING LOWER SKIN SURFACE GOUGED ADJACENT TO ACCESS PANEL 650LB APPROX WS 341. REPAIRED IAW SRM 57-21-31.Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA201404140062Angle · corrodedFS 621 ANGLE BETWEEN LBL 9 & LBL 27 HAS CORROSION AROUND 2 FASTENER HOLES MEASURING 0.007 INCHES DEEP MAX. REPAIRED IAW SRM 53-00-00.Apr 11, 2014 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2014041400061Fitting · crackedFS 621 BULKHEAD LINTEL FITTING CRACKED. REPAIRED IAW REO 601R-53-61-1230.Apr 11, 2014 · N8903A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2014041300057Skin · corrodedRIGHT WING LOWER PLANK ACCESS HOLE 650AB HAS CORROSION AT NON-CRITICAL AREAS 2.0 INCHES X 0.185 INCHES X 0.002 INCHES DEEP AT WS 163.00. REPAIRED IAW REO 601R-57-21-030.Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2014041300056Skin · corrodedRIGHT WING LOWER PLANK ACCESS HOLE 640DB HAS CORROSION AT NON-CRITICAL AREAS 2.0 INCHES X 0.185 INCHES X 0.001 INCHES DEEP AT WS 95.95. REPAIRED IAW REO 601R-57-21-030.Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2014041300055Skin · corrodedRIGHT WING LOWER PLANK ACCESS HOLE 640BB HAS CORROSION AT NON-CRITICAL AREAS 7.0 INCHES X 0.185 INCHES X 0.002 INCHES DEEP AT WS 54.897. REPAIRED IAW REO 601R-57-21-030.Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2014041300054Skin · corrodedRIGHT WING LOWER PLANK ACCESS HOLE 610AB HAS CORROSION AT NON-CRITICAL AREAS 3.75 INCHES X 0.185 INCHES X 0.002 INCHES DEEP AT WS 12.245. REPAIRED IAW REO 601R-57-21-030.Apr 11, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2014041200053Skin · corrodedRIGHT WING LOWER WING PLANK ACCESS HOLE 650FB HAS CORROSION AT NON-CRITICAL AREAS MEASURING 1.0 INCHES X 0.185 INCHES X 0.002 INCHES DEEP AT WS 274.319. REPAIRED IAW REO 601R-57-21-030.Apr 10, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2014041200052Skin · corrodedRIGHT WING LOWER WING PLANK ACCESS HOLE 650BB HAS CORROSION AT NON-CRITICAL AREAS MEASURING 1.75 INCHES X 0.185 INCHES X 0.001 INCHES DEEP AT WS 188.04. REPAIRED IAW REO 601R-57-21-030.Apr 10, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2014040800049Bulkhead · dentedFS 621 PRESS BULKHEAD FWD SIDE HAS A DENT APPROXIMATELY 6 INCHES OTBD OF RBL 27 & 8 INCHES UP FROM THE FLOOR MEASURING 3.45 INCHES X 3.4 INCHES X 0.041 INCHES DEEP. REPAIRED IAW REO 601R-53-61-5251.Apr 8, 2014 · N8903A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2014041000050Bulkhead · chafedFS 621 BULKHEAD FWD SIDE HAS 10 MARKS FROM FASTENERS CHAFE BETWEEN 15 INCHES & 30 INCHES FROM FLOOR & LBL 27 & RBL 27.5 UP TO 0.008 INCHES DEEP. REPAIRED IAW REO 601R-53-61-2155.Apr 7, 2014 · N8903A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2014040500044Skin · gougedGOUGE IN THE RT LOWER WING SKIN AT WS 330.25. THE AREA AFTER CLEAN UP MEASURES 1.90” X .800” X .003” DEEP. REPAIRED IAW CRJ257-02409.Apr 2, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2014040500046Fitting · crackedFS 280 OTBD CLIP AT RBL 9 CRACKED. REPAIRED IAW REO 601R-53-11-171.Apr 1, 2014 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2014040400042Skin · corrodedRT & LT LOWER WINGS SKINS AT AFT EDGES OF PANEL 193AB FRETTING CORROSION & CHAFFING. RT SIDE 0.025" DEEP. LT SIDE 0.015" DEEP. REPAIRED IAW REO 601R-57-21-880.Apr 1, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2014040300041Skin · gougedRIGHT WING LOWER SKIN SURFACE GOUGED ADJACENT TO ACCESS PANEL 650LB. BLENDED AND IS WITHIN LIMITS IAW SRM 57-21-31.Apr 1, 2014 · N8903A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2014032000308Flap · malfunctionedFLAPS FAIL EICAS, OCCURRED IN FLT ON APPROACH DURING FLAP EXTENSION. FAILED AT FLAP 30 DEG, AIRSPEED 160, TIME INTO FLIGHT 1 HR 10MIN. OAT +5 DEG C TAT. COMPLETED CB RESET OF FLAP SYS. COMPLETED 5 CONSECUTIVE FLAP CYCLES. DEFERRED FLAPS SYS IAW MEL 27-50-Mar 20, 2014 · N8903A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA2014030400252Seal · missingFLIGHT DECK PBE IS MISSING A SEAL. RE SECURED FLIGHT DECK PBE SEAL IAW CRJ AMM 25-63-00.Mar 4, 2014 · N8903A · Cndair CL6002B19 · Emergency EquipmentSDR REXA2013101001769Light · damagedEMERGENCY EXIT FLOODLIGHT ON GALLEY BY SERVICE DOOR DAMAGED. REPLACED EMERGENCY LIGHT IAW AMM 33-51-19. OPS TESTED OK.Oct 10, 2013 · N8903A · Cndair CL6002B19 · Emergency LightingSDR REXA2013011400144Life Vest · unserviceableONE INFANT LIFE VEST BAG TORN. COMPLIED WITH PA 25-096A BY INSTALLING INFANT LIFE VEST.Jan 14, 2013 · N8903A · Cndair CL6002B19 · Life JacketSDR REXA2083001201301Bracket · crackedLEFT ENGINE THRUST REVERSER STOW SWITCH BRACKET CRACKED. REMOVED AND REPLACED THRUST REVERSER SWITCH MOUNTING PLATE ASSY IAW AMM 78-37-01. OPS CHECKED GOOD.Aug 30, 2012 · N8903A · Cndair CL6002B19 · Engine Thrust ReverserSDR REXA2012082301091Angle · crackedCRACK FOUND IN FS 559 SEMI-PRESSURE BULKHEAD CAP ANGLE AT RBL18 AND LBL18. REPAIRED IAW REO 601R-53-41-260 AND 601R-53-41-609.Aug 22, 2012 · N8903A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2012071301155Light · inoperativeCABIN OVERHEAD EMERGENCY EXIT FLOOD LIGHT AT SEAT 3B INOPERATIVE.Jul 13, 2012 · N8903A · Cndair CL6002B19 · Emergency LightingSDR REXA2012041000493Switch · failedRIGHT THRUST REVERSER WOULD NOT DEPLOY ON LANDING. REMOVED AND REPLACED RT THRUST REVERSER DEPLOY SWITCH IAW AMM 78-37-01. OPS CHECKED GOOD, OK FOR SERVICE.Apr 10, 2012 · N8903A · Cndair CL6002B19 · Engine Thrust ReverserSDR REXA201100726Sensing Element · defectiveRT 14TH DUCT MASTER WARNING ON CLIMBOUT - FORWARD SECTION OF ENGINE BLEED SHOWED RED. REMOVED AND REPLACED RT 14TH STAGE PYLON DUCT HEAT SENSE ELEMENT A 58WK IAW AMM 36-21-04 OPC NORMAL. RT COWL ANTI-ICE OPC NORMAL IAW AMM 30-22-00. PART EFFECTIVITY VERIFIEOct 14, 2011 · N8903A · Cndair CL6002B19 · Pneumatic Indicating SystemSDR REXA201100664Bulkhead · crackedFS 202.75 BULKHEAD HAS A CRACK INDICATION LOCATED AT 9 O’CLOCK POSITION AT THE PASS THROUGH HOLE (REF PA 53-015). REPAIRED IAW BOMBARDIER REO 601R-53-11-563 AND BOMBARDIER SERVICE CORPORATION STANDARD REPAIR 601R-53-0101A.Oct 7, 2011 · N8903A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100549Structure · damagedRUDDER DAMAGE AT RS 131.17 TO RS 133.33 FWD LT SIDE DAMAGE IS APPROX 1.5L X 1.2W. REPAIRED IAW BOMBARDIER REO 601R-55-41-140.Aug 3, 2011 · N8903A · Cndair CL6002B19 · Rudder Miscellaneous StructureSDR REXA201100463Floor Support · crackedFLOOR SUPPORT INTERCOSTAL AT FS 484.0 IS CRACKED AT RBL 36.0. REPAIRED IAW REO 601R-53-41-059 AND BSC S/R 601R-53-00030B.Jul 18, 2011 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100462Intercostal · crackedFLOOR SUPPORT INTERCOSTAL AT FS 484.0 IS CRACKED AT LBL 36.0. REPAIRED IAW REO 601R-53-41-059 AND BSC S/R 601R-53-00030B.Jul 18, 2011 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100464Structure · corrodedMINOR CORROSION AROUND FASTENERS FROM FS 559+16 - FS 559+32 STR 26L TO 26R. REMOVED MINOR CORROSION AROUND FASTENERS FROM FS 559+16 TO FS 559+32 STR 26L TO 26R IAW SRM 51-21-06.Jul 17, 2011 · N8903A · Cndair CL6002B19 · Fuselage Main, StructureSDR REXA201100497Sill · corrodedTWO EACH NUT PLATE HOLES HAVE MINOR CORROSION AT FS 559+96 RBL 45 ON FLOOR SILL. REPAIRED IAW BOMBARDIER SERVICES CORP EO 601R-53-L00118 AND ASSOCIATED 8110-3 DATED 7/8/11.Jul 16, 2011 · N8903A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
Back to N8903A, cancelled Dec 23, 2024