N409BK

Service difficulty reports · 16

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 = 'N409BK' 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 HYIA20231006001Rib · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE RIGHT HAND CLOSEOUT RIB (P/N: 5122115-56) AT R.W.S. 106.79. THIS CRACK ORIGINATES FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE AND TRAVELS FORWARD AN APPSep 22, 2023 · N409BK · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20200921001Packing · leakingTHE PILOT REPORTED A FUEL SMELL IN COCKPIT. MAINTENANCE INSPECTED AND FOUND THE CABIN HEATER FUEL FILTER BOWL LEAKING. REMOVED AND REPLACED THE BOWL SEAL WITH NO FURTHER DEFECTS NOTED.Sep 18, 2020 · N409BK · Cessna 402C · Aircraft Fuel Distribution SystemSDR HYIA20200519001Spar Cap · corrodedDURING MAINTENANCE TWO SPOTS OF CORROSION WERE VISUALLY IDENTIFIED ON THE AFT LEFT HAND VERTICAL SPAR CAP (P/N: 5131007-5) OF THE  VERTICAL STABILIZER. THESE SPOTS EXIST AT APPROXIMATE W.L 156.52 AND W.L. 167.52, AND HAVE A MAXIMUM DEPTH OF .033 INCHES. THIS DMay 19, 2020 · N409BK · Cessna 402C · Vertical Stabilizer, Spar/RibSDR HYIA20180104002Spar Cap · crackedA CRACK WAS IDENTIFIED AT THE LT SIDE OF LWR FWD CARRYTHROUGH SPAR CAP, IB MOST AFT FASTENER HOLE WHILE PERFORMING NDT PROCEDURE AS AMOC FOR AD2018-03-03R1. THE CRACK WAS CONFIRMED WITH BOLT HOLE EDDY CURRENT AFTER THE FASTENER WAS REMOVED. WE BELIEVE THIS SJan 3, 2019 · N409BK · Cessna 402C · Wing SparSDR HYIA20181031001Attach Fitting · corrodedDURING MAINTENANCE CORROSION WAS DISCOVERED ON THE RIGHT HAND UPPER AFT WING FITTING (P/N: 0822550-46) IN THE WHEEL WELL. THIS FITTING WILL BE REMOVED AND REPLACED WITH A NEW PART. A PICTURE HAS BEEN ATTACHED TO THIS SDR FOR FURTHER DETAILS AND CLARITY.Oct 31, 2018 · N409BK · Cessna 402C · Wing, Attach FittingsSDR HYIA20181023002Gasket · tornPILOT REPORTED A FUEL SMELL WHEN TURNING ON CABIN HEAT. MAINTENANCE INSPECTED AND FOUND THE HEATER FUEL FILTER GASKET IN NEED OF REPLACEMENT, THE GASKET WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Oct 20, 2018 · N409BK · Cessna 402C · Heating SystemSDR HYIA20161028001Spark Plug · failedPILOT REPORTED THE LEFT ENGINE WOULD NOT DEVELOP FULL POWER, STOPPED AT 26 INCHES MAP AND VIBRATION. INSPECTION OF THE LEFT ENGINE REVEALED A PREIGNITION EVENT IN THE NR 3 CYLINDER WHICH CAUSED SIGNIFICANT DAMAGE TO THE PISTON HEAD. THE CYLINDER IS IN THE PROOct 26, 2016 · N409BK · Cessna 402C · Spark Plug/IgniterSDR HYIA201608002011Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Jun 23, 2016 · N409BK · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20150529001Transistor · failedPILOT REPORTED SMOKE COMING FROM PANEL LIGHT RESISTOR. R & R THE DIMMER ASSEMBLY FOR INSTRUMENT LIGHTS. REPLACED Q7 TRANSISTOR FOR DIMMER SWITCH IAW MM 33-10-105 & WDM 33-10-00.May 25, 2015 · N409BK · Cessna 402C · Flight Compartment LightingSDR HYIA20131219001Engine · failedOPERATING FLIGHT 1821 ALB TO MSS RETURNED TO ALB IMMEDIATELY AFTER TAKEOFF & LANDED SAFELY WITH 3 PAX ON BOARD. PILOT NOTED DECREASING LT ENG OIL PRESS & HEARD A LOUD BANG FROM LT ENG AFTER ROTATION. LT ENG MAGNETO SEPARATED FROM ACCESSORY DRIVE & CONNECTINGDec 19, 2013 · N409BK · Cessna 402C · Engine (Reciprocating)SDR HYIA20120118002Governor · inoperativePILOT REPORTED THAT WHEN REDUCING POWER WHILE TRANSITIONING FROM CLIMB TO CRUISE, THE LT ENGINE PROPELLER RPM STAYED AT FULL RPM AND WOULD NOT REDUCE. THE PILOT ELECTED TO RETURN TO THE DEPARTURE AIRPORT. AFTER MX INSPECTION, THE DISCREPANCY WAS UNABLE TO BE Jan 16, 2013 · N409BK · Cessna 402C · Propeller GovernorSDR HYIA20121210002Latch · out of adjustPILOT REPORTED THAT AFTER TAKEOFF, DURING CLIMB, EMERGENCY EXIT DOOR LOCATED ON THE RT SIDE OF THE AFT, OPENED UNCOMMANDED. SAFELY RETURNED TO THE DEPARTURE. DURING INSPECTION, DOOR LATCHES WERE FOUND TO BE OUT OF ADJUSTMENT. LATCHES WERE ADJUSTED IAW MM.Dec 7, 2012 · N409BK · Cessna 402C · Emergency ExitsSDR HYIA20121023001Doubler · crackedDURING A ROUTINE SCHEDULED MX EVENT, A CRACK WAS DISCOVERED IN THE RT FORWARD NLG TUNNEL WEB 00DOUBLER AT FS 44.00 IN THE AREA OF THE RT NLG TRUNNION BEARING BLOCK FORWARD MOUNT HOLE LOCATIONS. DETERMINED TO BE A REMOVAL AND REPLACEMENT OF OWNER PRODUCED WEB Oct 23, 2012 · N409BK · Cessna 402C · Fuselage Miscellaneous StructureSDR HYIA20140415060Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE May 27, 2011 · N409BK · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414002Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & AApr 14, 2011 · N409BK · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA409BKCBNHTSwitch · shortedCREW REPORTED, ON DESCENT, NOTICED AN ODOR AND SAW SMOKE COMING FROM CABIN HEAT SWITCH. EMERGENCY WAS DECLARED, DEACTIVATED ALL ELECTRICAL SYS AND SMOKE STOPPED. TURNED ON SELECTIVE ELECTRICAL EQUIPMENT ON TO FINISH APPROACH, LANDING WAS UNEVENTFUL. MX FOUNDDec 1, 2010 · N409BK · Cessna 402C · Heating System
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