N8891A

Service difficulty reports · 75

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 = 'N8891A' 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 REXA2013053000681Skin · damagedDURING ROUTINE LINE MX AT MX FOUND LIGHTNING DAMAGE TO THE FUSELAGE SKIN IN THE AREA OF THE SKIN JOINT ON THE AFT SIDE OF FS755 BETWEEN S-25R AND S-26R. REPAIRED IAW EA CRJ253-01628 AND ASSOCIATED 8110-3.May 29, 2013 · N8891A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA2013042100754Light · unsecureFORWARD MOST PART OF EMERGENCY FLOOR LIGHTING IS PEELED FROM FLOOR IN THE MAIN CABIN (ORANGE SECTION). REMOVED AND REPAIRED FORWARD MOST SECTION OF FLOOR TRACK LIGHTING IAW AMM 33-51-01. OPERATIONS CHECK GOOD.Apr 21, 2013 · N8891A · Cndair CL6002B19 · Emergency LightingSDR REXA2013030500441Battery · dischargedCREW REPORTS FLIGHT ATTENDANT'S EMERGENCY FLASHLIGHT INOPERABLE. REPLACED FLASHLIGHT BATTERY & RE-SECURED. OPERATIONS CHECK GOOD.Mar 5, 2013 · N8891A · Cndair CL6002B19 · Emergency EquipmentSDR REXA2012102601425Light · inoperativeSERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXTERIOR LIGHT IAW AMM 33-51-21, OP CHECK GOOD.Oct 25, 2012 · N8891A · Cndair CL6002B19 · Emergency LightingSDR REXA2012080601237A/C Pack · out of adjustLEFT HIGH PRESSURE ON TAKEOFF ON FLIGHT 3884. COMPLIED WITH QRH BUT COULD NOT RESET. ISOLATION VALVE WOULD NOT OPEN. DECLARED EMERGENCY AND PERFORMED AIR RETURN TO DEPARTURE. PERFORMED ADJUSTMENT TEST OF LEFT PACK IAW AMM 21-51-00. OPS CHECKED NORMAL, VERAug 6, 2012 · N8891A · Cndair CL6002B19 · Cabin Cooling SystemSDR REXA2012070701052Light · inoperativeNR 3 AISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 3 AISLE OVERHEAD EMERGENCY LIGHT IAW AMM 33-51-16.Jul 7, 2012 · N8891A · Cndair CL6002B19 · Emergency LightingSDR REXA2012061901002Door · lack of lubeMAIN CABIN DOOR HANDLE IS HARD TO OPEN. LUBED MAIN PASSENGER DOOR IAW AMM 52-11-21. OPS CHECKS GOOD.Jun 19, 2012 · N8891A · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA2012032300408Trim Panel · malfunctionedRUDDER TRIM WILL NOT TRIM RIGHT. RUDDER CURRENTLY OUT OF TRIM LEFT. REMOVED AND REPLACED RUDDER/ ALI TRIM CONTROL PANEL IAW AMM 27-12-10. OPS CK RUDDER/ AILERON TRIM CONTROL PANLE NORMAL. OK FOR SERVICE.Mar 23, 2012 · N8891A · Cndair CL6002B19 · Aileron Control SystemSDR REXA2012021900241Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED AT FS 621 AT LEFT LINTEL FITTING. REPAIRED IAW REO 601R-53-61-1230.Feb 13, 2012 · N8891A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2012021300193Bulkhead · crackedFS 202.75 BULKHEAD FOUND CRACKED AT PARKING BRAKE CABLE CUTOUT VIA EDDY CURRENT. REPAIRED IAW BOMBARDIER REO 601R-53-11-563.Feb 12, 2012 · N8891A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201200131Controller · defectiveRETURN LANDING. WILL NOT PRESSURIZE CORRECTLY. 15,000 THRU 20,000 FT CAB ALT 6700 FT WITH RATE 1,000 - 3,000 ^P 4.8 AT IDLE LOSE PRESSURIZATION. REMOVED AND REPLACED NR 1 CABIN PRESSURE CONTROLLER IAW AMM 21-31-16. OP/C F/C GOOD. REMOVED SECONDARY OUTFLOW VJan 22, 2012 · N8891A · Cndair CL6002B19 · Cabin Pressure ControllerSDR REXA201100949Riser · corrodedRT PYLON PRODUCTION RISER HAS AREAS OF FRETTING ON FORWARD SIDE FROM 10 O’CLOCK TO 6 O’CLOCK POSITION APPROX .004 DEEP. REPAIRED IAW BOMBARDIER REO 601R-54-50-036.Dec 28, 2011 · N8891A · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR REXA201100839Battery · dischargedCO-PILOT EMER FLASHLIGHT INOP. REPLACED BATTERY IN CO-PILOT EMER FLASHLIGHT IAW AMM 25-61-00.Nov 13, 2011 · N8891A · Cndair CL6002B19 · Emergency EquipmentSDR REXA201100417Bulkhead · damagedWHILE PERFORMING REO 601R-53-11-926B (FS 2800 BULKHEAD REPAIR) THE BULKHEAD WAS FOUND TO HAVE 2 ADDITIONAL DOUBLERS AT LBL 11 AND RBL 11, WL 75 TO WL 82.5. REPAIRED IAW BOMBARDIER REOS 601R-53-11-926 REV B AND 601R-53-11-2140.Jun 30, 2011 · N8891A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100416Access Panel · chafedWHILE REMOVING ACCESS PNL 132AL, BIT CAME OFF OF 2 EACH SCREWS AT 6 O'CLOCK POSITION AND LEFT 3 EA CHAFES APPROX 0.050" LONG X 0.050" WIDE X 0.010" DEEP, 0.060" LONG X 0.060" WIDE, X 0.020" DEEP, AND 0.060" LONG X 0.020" WIDE X 0.010" DEEP. REPAIRED IAW EA CRJun 30, 2011 · N8891A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100415Spoiler · dentedLEFT WING OUTBOARD GROUND SPOILER HAS DENT AT WS 137 APPROXIMATELY 0.247" LONG X 0.086" WIDE X 0.010" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-70-016.Jun 30, 2011 · N8891A · Cndair CL6002B19 · SpoilersSDR REXA201100414Structure · corrodedCORROSION FOUND AROUND NUT PLATE HOLES ON LBL 27 BETWEEN FS 589 AND FS 605. REPAIRED IAW BOMBARDIER REO 601R-53-61-3778.Jun 30, 2011 · N8891A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100511Bulkhead · damagedFS 280 BULKHEAD FOUND CORRODED AND CRACKED. REPAIRED IAW BOMBARDIER REO 601R-3-11-926 AND BOMBARDIER SERVICE CORPORATION EO 601R-53-0110.Jun 26, 2011 · N8891A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100398Skin · damagedDURING C-CHECK MAINTENANCE AT WVAC DAMAGE TO THE RIGHT INBOARD FLAP LOWER WING SKIN WAS REPORTED FOR REPAIR TO TERMINATE DI16691 FOR A DENT TO THE LOWER WING SKIN INBOARD END BETWEEN WS 50.498 AND W554.848 BETWEEN THE FRONT AND REAR SPAR. ADDITIONALLY, DAMAGEJun 24, 2011 · N8891A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA201100281Unknown · smokeCREW REPORTED SMOKE IN COCKPIT DURING TAXI TO GATE AFTER LANDING EMERGENCY WAS DECLARED PAX DEBOARDED AT GATE UNDER NORMAL PROCEDURES.May 9, 2011 · N8891A · Cndair CL6002B19 · Air Distribution SystemSDR REXA201000095B-Nut · looseTROUBLESHOT HYDRAULIC LEAK NR 1 SYSTEM FOUND LOOSE B-NUT ON NR 1 HYDRAULIC FILTER MANIFOLD. RE-SECURED PER 29 10 00, RE-SECURED HYDRAULIC LINE PER 29 10 00.Jun 28, 2010 · N8891A · Cndair CL6002B19 · Hydraulic System, MainSDR REXA200900060Bpsu · failedON CLIMB GOING THROUGH 19,000 FLAPS FAILED AT ZERO, RETURNED TO DTW WITH UNEVENTFUL LANDING. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM AND WAS DETERMINED TO BE A FAILURE OF THE RIGHT BRAKE POSITION SENSING UNIT (BPSU). UNIT REPLACED AND FLAPS RIGGED PER BJun 3, 2009 · N8891A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200900059Fcu · failedFLAP FAIL MESSAGE RECEIVED IN CRUISE. MAINTENANCE TROUBLESHOT SYSTEM PER BOMBARDIER FIM AND DETERMINED FAILURE OF THE FLAP ELECTRONIC CONTROL UNIT (FECU). REMOVED AND REPLACED FECU IAW AMM.Jun 2, 2009 · N8891A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00033Windshield · cracked(REF NR: 05-070) CAPTAINS WINDSHIELD CRACKED. REMOVED AND REPLACED CAPTAINS LT FRONT WINDSHIELD IAW AMM. (K)May 27, 2005 · N8891A · Cndair CL6002B19 · Flight Compartment WindowsSDR REXA04043Control System · malfunctionedFLAPS FAILED ON TAXI OUT. SYSTEM RESET, PLACED FLAP ON 72 HOUR WATCH IAW AD98-20-01.Dec 12, 2004 · N8891A · Cndair CL6002B19 · Trailing Edge Flap Control System
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