N6875D

Service difficulty reports · 25

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 = 'N6875D' 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 HYIA20231031001Throttle Body · backed outPILOT REPORTED LEFT THROTTLE STUCK AT APPROXIMATELY 34 INCHES MP WHEN REDUCING FROM TAKE OFF POWER TO CLIMB POWER. MAINTENANCE INSPECTED AND FOUND THE LEFT THROTTLE BODY LEVER PIN HAD BACKED OUT AND WAS CONTACTING THE IDLE STOP. THE PIN WAS REPLACED AND NO FUROct 29, 2023 · N6875D · Cessna 402C · Engine Fuel and ControlSDR HYIA20220329001Fitting · crackedWHILE PERFORMING A RECURRENT NDT INSPECTION (HFEC) TO SATISFY THE REQUIREMENTS OF TEXTRON 57-10-16, A CRACK WAS FOUND ON THE RIGHT HAND INBOARD NACELLE FITTING. THIS CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING AND MEASURES .150 IN LENGTH. THIS CRACK Mar 28, 2022 · N6875D · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20210827001Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE RIGHT HAND INBOARD NACELLE FITTING. (P/N: 5292029-22) THIS CRACK MEASURES APPROXIMATELY .123 INCHES LONG ON THE OUTBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACKSAug 27, 2021 · N6875D · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20200521001Adapter · brokenDURING INITIAL CLIMB APPROXIMATELY 3 MINUTES AFTER TAKEOFF THE CREW REPORTED A LT YAW MOVEMENT AND RECOGNIZED LT ENGINE MAP INDICATION DROPPING FOLLOWED BY A RAPIDLY DECREASING LT ENGINE OIL PRESSURE INDICATION. THE CREW ALSO REPORTED WHITE SMOKE STREAMING FRMay 20, 2020 · N6875D · Cessna 402C · Reciprocating Engine Oil SystemSDR HYIA12062016002Fitting · crackedDURING A ROUTINE INSPECTION, CRACKS WERE IDENTIFIED AT RT OB NACELLE FITTING P/N 5292029-10. JUST FWD OF LWR FWD WING SPAR STRAP (REFERENCE MEB02-5 CURRENTLY AT REVISION 2 AND SERVICE KIT SK402-47A/B). THE MAJORITY OF THIS NACELLE FITTING IS NOT ACCESSIBLE FODec 5, 2016 · N6875D · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA12062016001Fitting · brokenDURING A ROUTINE INSPECTION, A CRACK WAS IDENTIFIED AT RT IB ENGINE BEAM ASSEMBLY P/N 5654109-7 AND THE BEAM WAS REMOVED. AT REMOVAL, THE RT NACELLE IB FITTING P/N 5292029-12 WAS FOUND TO BE BROKEN IN HALF JUST FWD OF LWR FWD WING SPAR STRAP (REFERENCE MEB02-5Dec 5, 2016 · N6875D · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20160818076Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Aug 16, 2016 · N6875D · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160818077Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Aug 16, 2016 · N6875D · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160104005Windshield · defectivePILOT REPORTED WINDSHIELD HEAT WIRE CONNECTOR SMOKING AT WINDSHIELD. INSPECTED WINDSHIELD FOR RESISTANCE, FOUND TO BE OPEN. INSPECTED WINDSHIELD INVERTER, FOUND WATER PRESENT IN BAY, BUT NOT EXCESSIVE. VERIFIED NO POWER AT INVERTER AFTER CB PULLED. WINDSHIDec 31, 2015 · N6875D · Cessna 402C · Flight Compartment WindowsSDR HYIA20160104004Grounding Strap · defectivePILOT REPORTED WINDSHIELD HEAT ARCING INFLIGHT. R & R 3 WINDSHIELD GROUNDING STRAPS & OPERATIONALLY CHECKED GOOD.Dec 27, 2015 · N6875D · Cessna 402C · Windshield/Door Rain/Ice RemovalSDR HYIA20150420001Ignition Unit · faultyPILOT REPORTED HEATER, NO HEAT BURNING SMELL IN FLIGHT. R & R THE HEATER IGNITION ASSEMBLY & OPERATIONS CHECKED WITH NO FURTHER DEFECTS NOTED.Apr 16, 2015 · N6875D · Cessna 402C · Heating SystemSDR HYIA20140414060Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEJan 29, 2014 · N6875D · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414017Drag 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 & Jul 25, 2012 · N6875D · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415074Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWNov 17, 2011 · N6875D · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415015Drag 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 OJan 28, 2011 · N6875D · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA6875D12/29Distributor Gear · unserviceableCREW REPORTED LT ENG MAGNETO CHECK GOOD ON RUN-UP PRIOR TO TAKEOFF. ON CLIMB OUT, LT ENG BEGAN RUNNING ROUGH. MX FOUND LT ENG RT MAGNETO INOPERATIVE. FURTHER INSP REVEALED DISTRIBUTOR DRIVE GEAR TEETH STRIPPED. MX REMOVED AND REPLACED AFFECTED MAGNETO. ASDec 29, 2009 · N6875D · Cessna 402C · Magneto/DistributorSDR HYIA6875DAVMSTRCircuit Breaker · unserviceableDURING ROUTINE SCHEDULED INSP, MX FOUND AVIONICS MASTER SWITCH WOULD SHUT OFF IN CTR POSITION. MX R & R CIRCUIT BREAKER SWITCH. SYS CHECKS OK.Sep 1, 2009 · N6875D · Cessna 402C · DC Power Distribution SystemSDR 1356875020308Adapter · failedON SHORT FINAL OF APPROACH PILOT NOTICED RT PROP WANDERING, LOOKED AT GAGES AND SAW RT OIL PRESSURE AT 0. PILOT SHUTDOWN ENGINE AND FEATHERED PROP. AIRCRAFT LANDED WITHOUT INCIDENT. UPON INITIAL INVESTIGATION FOUND OIL ON RT MLG DOOR. MX INSPECTED ENGINE AJan 30, 2008 · N6875D · Cessna 402C · Engine StarterSDR 13505276875DCircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.Jun 3, 2006 · N6875D · Cessna 402C · AC Power Distribution SystemSDR 08222005Bolt · shearedPROPELLER FAILED TO TURN ON START. CRANKSHAFT LARGE ATTACH BOLTS SHEARED AND GEAR DISLODGED FROM CRANKSHAFT. ENGINE REMOVED AND REPLACED.Aug 22, 2005 · N6875D · Cessna 402C · Engine (Reciprocating)SDR HYI2005F00006Bolt · shearedLT PROPELLER FAILED TO TURN ON START, MAINTENANCE FOUND CRANKSHAFT LARGE ATTACH BOLTS SHEARED AND GEAR DISLODGED FROM CRANKSHAFT. MAINTENANCE REMOVED AND REPLACED THE ENGINE AND RETURNED THE AIRCRAFT TO SERVICE. (NE01200505271) (K)Aug 18, 2005 · N6875D · Cessna 402C · Reciprocating Engine Power SectionSDR HYI2004F00000Spar Cap · corrodedCORRODED SPAR CAP LOCATION, REAR SPAR ON HORIZONTAL STABILIZER, LOWER CAP. CORRODED AT LEFT, IB HINGE, 12 INCHES OB OF IB HINGE. (NE01200401202)Feb 6, 2004 · N6875D · Cessna 402C · Horizontal Stabilizer, Spar/RibSDR HYI2001F00003Master Switch · failedON PREFLIGHT INSPECTION, AVIONICS MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE.Oct 11, 2001 · N6875D · Cessna 402C · DC Power Distribution SystemSDR 98ZZZX989Valve Spring · brokenRIGHT ENGINE RUNNING ROUGH. FOUND 8 OF 12 VALVE SPRINGS BROKEN. REMOVED AND REPLACED ALL VALVE SPRINGS.Feb 10, 1998 · N6875D · Cessna 402C · Reciprocating Engine Cylinder SectionSDR 98ZZZX988Valve Spring · brokenRIGHT ENGINE RUNNING ROUGH. FOUND 8 OF 12 VALVE SPRINGS BROKEN. REMOVED AND REPLACED ALL VALVE SPRINGS.Feb 10, 1998 · N6875D · Cessna 402C · Reciprocating Engine Cylinder Section
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