N8674A

Service difficulty reports · 30

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 = 'N8674A' 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 REXA2014071300697Light · inoperativeSERVICE DOOR INTERIOR WHITE EMER LIGHTS, 2 OF 5 INOPERATIVE. R & R EMER EXIT LIGHT BULBS IAW 33-51-13. OPERATIONS CHECKED GOOD.Jul 13, 2014 · N8674A · Cndair CL6002B19 · Emergency LightingSDR REXA2014031200031Stiffener · chafedISOLATION VLV IN AEB IS CHAFING ON VERTICAL STIFFENER ON REAR FS 621. REPAIRED IAW REO 601R-53-61-1523.Mar 8, 2014 · N8674A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2014031100030Frame · corrodedMAINTENANCE FOUND THE FRAME AT FS 349 TO BE CORRODED IN THE WEB & LOWER FLANGE AT STRINGER 25L. THE FRAME WAS SPLICED IAW EA CRJ253-02345 & ASSOCIATED 8110-3.Mar 8, 2014 · N8674A · Cndair CL6002B19 · Fuselage Main, FrameSDR REXA2014031100029Floorbeam · corrodedMAINTENANCE FOUND THE UPPER FLANGE OF THE FLOOR BEAM AT FS 349 TO BE CORRODED FROM RBL 33.20 TO RBL 42.50. THE CORROSION MEASURES 4.25 INCHES X 1.00 INCH X .034 INCH DEEP. REPAIRED IAW EA CRJ253-02335 & ASSOCIATED 8110-3.Mar 8, 2014 · N8674A · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR REXA2014031100028Floorbeam · corrodedMAINTENANCE FOUND THE UPPER FLANGE OF THE FLOOR BEAM AT FS 349 TO BE CORRODED SURROUNDING TWO NUTPLATE FASTENER HOLES BETWEEN RBL 9.00 & LBL 45.00. REPAIRED IAW EA CRJ253-02333 & ASSOCIATED 8110-3.Mar 8, 2014 · N8674A · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR REXA2014030500024Skin · wornRIGHT FUEL ACCESS HOLE FOR PANEL 640BB AT WS 54.897 IS WORN AROUND ENTIRE CIRCUMFERENCE 0.003 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.Mar 4, 2014 · N8674A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2014030300021Fitting · crackedINBOARD & OTBD CLIPS ON FLOOR SUPPORT BEAM CRACKED AT FS 280, RBL9. REPAIRED IAW SRM 51-11-20, 51-42-21, 51-31-59, 51-24-36, 51-21-11, 51-25-16 & 51-41-02.Feb 28, 2014 · N8674A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2014030300020Fitting · crackedOUTBOARD CLIP CRACKED ON FLOOR SUPPORT BEAM AT FS 280, LBL 9. REPAIRED IAW SRM 51-11-20, 51-42-21, 51-31-59, 51-24-36, 51-21-11, 51-25-16 & 51-41-02.Feb 28, 2014 · N8674A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2014020600184Mechanism · obstructedBOARDING DOOR HANDLE IS VERY DIFFICULT TO MOVE TO OPEN DOOR. CLEARED ICE FROM DOOR LATCH MECHANISM. OPERATIONS CHECKED DOOR IAW AMM 52-11-00, HANDLE MOVES OK.Feb 6, 2014 · N8674A · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA2013021900356Structure · contaminatedON FLIGHT 4096 (DTW TO TYS) STRONG ODOR OF FUEL EACH TIME TRANSFER PACKS TO APU BOTH WHILE ON THE GROUND AND AIRBORNE. FOUND RESIDUAL FUEL IN APU COMPARTMENT. CLEANED COMPARTMENT. LEAK CHECKED APU-NO LEAKS NOTED. RUN LEFT & RIGHT PACKS FROM ENGINES AND APUFeb 19, 2013 · N8674A · Cndair CL6002B19 · APU Cowling/ContainmentSDR REXA2012111101514Bulkhead · damagedFORWARD SIDE OF FS 621 BULKHEAD HAS 4 EACH SCREW MARKS IN A LINE APPROX 30 INCHES ABOVE THE FLOOR. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Nov 7, 2012 · N8674A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2012083101306Drain Line · disconnectedLEFT PACK IS BLOWING HEAVY CONDENSATION OBSCURING COCKPIT SIDE WINDOWS. FOG ALSO OBSCURING FLOOR PATH IN CABIN, UNABLE TO SEE FLOOR OR EGRESS PATH LIGHTS. FOUND DRAIN LINE ON WATER SEPARATOR DISCONNECTED, RECONNECTED IAW AMM 21-50-00. OPS CHECKS GOOD.Aug 31, 2012 · N8674A · Cndair CL6002B19 · Humidity Control SystemSDR REXA2012071601163Battery Pack · dischargedEMERGENCY LIGHTS ON FLOOR ARE INOPERATIVE. ALLOWED SYSTEM TO CHARGE. OPS SYSTEM NORMAL. OK FOR SERVICE PER FIM.Jul 16, 2012 · N8674A · Cndair CL6002B19 · Emergency LightingSDR REXA2012041600521Manifold · crackedFOUND CRACK MANIFOLD MAINFEED UNDER CARGO FLOOR. C/W REO 601R-21-22-003 IAW WORK INSTRUCTION PROVIDED BY ENGINEERING, A/C OK FOR SERVICE.Apr 16, 2012 · N8674A · Cndair CL6002B19 · Air Distribution SystemSDR REXA2012040900419Intercostal · crackedINTERCOSTAL AT BS 621 TO 625 S14L CRACKED. REPAIRED IAW REO 601R-53-61-100.Apr 6, 2012 · N8674A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2012040300418Floor Support · corrodedLBL 27 FLOOR SUPPORT CORRODED AROUND NUT PLATES BETWEEN FS 574 AND FS 589. REPAIRED IAW REO 601R-53-00-005 AND REO 601R-53-61-3778.Apr 2, 2012 · N8674A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2012040300417Floorbeam · corrodedLBL 9 FLOORBEAM TEE CAP CORRODED AROUND NUT PLATES AT FS 615 WITH 0.004" REMOVED. REPAIRED IAW REO 601R-53-00-005.Apr 2, 2012 · N8674A · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR REXA2012040300416Vane · wornLEFT INBOARD FLAP VANE SLIDING BEAM HAS WEAR DAMAGE 0.4" X 0.08" X 0.002" DEEP AND 0.003" DEEP AT WS 59.5. REPAIRED IAW BOMBARDIER REO 601R-57-52-1891.Apr 2, 2012 · N8674A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA201100063Tape · missingTHE CREW REPORTED A SMOKE TOILET MESSAGE ON APPROACH. MAINTENANCE COMPLIED WITH PINNACLE AIRLINES MINIMUM WORK SCOPE FOR SMOKE VISUAL OR INDICATION. MAINTENANCE FOUND SPEED TAPE FOR LAV VENT MISSING, RE-APPLIED TAPE IAW PA 21-009. MAINTENANCE PERFORMED MAX Jan 27, 2011 · N8674A · Cndair CL6002B19 · Smoke DetectionSDR REXA201000191Landing Gear · malfunctionedGEAR DISAGREE IN FLIGHT NOSE GEAR DID NOT COME UP WHEN SELECTED. RAN QRH GEAR CAME UP WITH PUMPS ON, GEAR CAME DOWN NORMALLY. FLT--3677 STA--MBS EMP--1 C/W PA 05-018A. FOUND NO DEFECT. FOUND PSEU CODES S22 DOWN FAR, S30 DOWN FAR, S31 DOWN FAR, S32 DOWN FAR,Oct 4, 2010 · N8674A · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA201000184Warning System · malfunctionedOPERATING UNDER AN MEL FOR THE MAIN LANDING GEAR BAY OVERHEAT SYSTEM BEING DEFERRED. THIS MEL REQUIRED THE GEAR TO REMAIN DOWN FOR 10 MINUTES AFTER TAKEOFF. AFTER 10 MINUTES OF FLIGHT, RETRACTED THE GEAR AND THE NOSE GEAR FLAGGED RED DURING TRANSIT AND THE TOct 4, 2010 · N8674A · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA201000028Priority Valve · malfunctionedGEAR DISAGREE WARNING ON GEAR DOWN, NOSE GEAR INDICATED AMBER. DISCONTINUED APPROACH. RAN QRH. THREE GREEN, DOWN AND LOCKED INDICATION. NOTIFIED F/A, PAX, ATC, SOC/MOC. LANDED WITHOUT INCIDENT. NOSE GEAR PRIORITY VALVE MALFUNCTION, COMPUTER POSTED A NOSEFeb 27, 2010 · N8674A · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA201000014Compressor · damagedON CLIMBOUT OF KDTW, THE RIGHT ENGINE WOULD NOT REACH TARGET POWER SETTING WITHOUT OVER TEMPING. THE FLIGHT CREW ELECTED TO RETURN TO KDTW. CENTER WAS NOTIFIED AND THE AIRCRAFT WAS VECTORED FOR A RETURN APPROACH. ON THE APPROACH THE RIGHT ENGINE WAS MAKING Jan 26, 2010 · N8674A · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR REXA200700057Connector · damagedFOUND FORWARD FLOOR EMERGENCY LIGHTS INOP. REPLACED CONNECTOR OF EMERGENCY LIGHT STRIP.Jul 16, 2007 · N8674A · Cndair CL6002B19 · Light System WiringSDR REXA200700040Flap System · unknownFLAPS FAIL, SECOND OCCURRENCE WITHIN 72 HOURS.Feb 4, 2007 · N8674A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200700028Flap System · unknownFLAPS FAIL AT 20 DEGREES. RESET PER AD 2006-12-21.Feb 3, 2007 · N8674A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA05002Bpsu · failedFLAPS FAILED AT ZERO AT FLIGHT LEVEL 310. QRH FOLLOWED, DECLARED EMERGENCY, UNEVENTFUL ZERO FLAPS LANDING MADE. SYSTEM WOULD NOT RESET. REPLACED RT BPSU (BRAKE POSITION SENSING UNIT) IAW AMM. OPERATIONALLY TESTED GOOD. (K)Jan 1, 2005 · N8674A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA04041Control Unit · failedFLAPS FAILED AT ZERO WHEN SELECTED TO 20 ON APPROACH. QRH FOLLOWED, DECLARED EMERGENCY WITH UNEVENTFUL LANDING. RESET SYSTEM AND PLACED FLAPS ON 72 HOUR MONITORING IAW AD98-20-01.Dec 4, 2004 · N8674A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA04037Control System · failedFLAPS FAILED ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01.Nov 24, 2004 · N8674A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA04030Flap · malfunctionedFLAPS FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. (NE02200500600)Nov 9, 2004 · N8674A · Cndair CL6002B19 · Trailing Edge Flap Control System
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