# Service difficulty reports: N6875D

A list on [N6875D](https://openairdocs.org/aircraft/N6875D.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR HYIA20231031001](https://openairdocs.org/sdr/HYIA20231031001.md): Throttle Body · backed out · Oct 29, 2023 · N6875D · Cessna 402C · Engine Fuel and Control
  > PILOT 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 FUR
- [SDR HYIA20220329001](https://openairdocs.org/sdr/HYIA20220329001.md): Fitting · cracked · Mar 28, 2022 · N6875D · Cessna 402C · Nacelle/Pylon, Attach Fittings
  > WHILE 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
- [SDR HYIA20210827001](https://openairdocs.org/sdr/HYIA20210827001.md): Fitting · cracked · Aug 27, 2021 · N6875D · Cessna 402C · Nacelle/Pylon, Attach Fittings
  > DURING 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 CRACKS
- [SDR HYIA20200521001](https://openairdocs.org/sdr/HYIA20200521001.md): Adapter · broken · May 20, 2020 · N6875D · Cessna 402C · Reciprocating Engine Oil System
  > DURING 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 FR
- [SDR HYIA12062016002](https://openairdocs.org/sdr/HYIA12062016002.md): Fitting · cracked · Dec 5, 2016 · N6875D · Cessna 402C · Nacelle/Pylon, Attach Fittings
  > DURING 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 FO
- [SDR HYIA12062016001](https://openairdocs.org/sdr/HYIA12062016001.md): Fitting · broken · Dec 5, 2016 · N6875D · Cessna 402C · Nacelle/Pylon, Attach Fittings
  > DURING 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 MEB02-5
- [SDR HYIA20160818076](https://openairdocs.org/sdr/HYIA20160818076.md): Exhaust Valve · damaged · Aug 16, 2016 · N6875D · Cessna 402C · Reciprocating Engine Cylinder Section
  > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
- [SDR HYIA20160818077](https://openairdocs.org/sdr/HYIA20160818077.md): Exhaust Valve · damaged · Aug 16, 2016 · N6875D · Cessna 402C · Reciprocating Engine Cylinder Section
  > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
- [SDR HYIA20160104005](https://openairdocs.org/sdr/HYIA20160104005.md): Windshield · defective · Dec 31, 2015 · N6875D · Cessna 402C · Flight Compartment Windows
  > PILOT 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. WINDSHI
- [SDR HYIA20160104004](https://openairdocs.org/sdr/HYIA20160104004.md): Grounding Strap · defective · Dec 27, 2015 · N6875D · Cessna 402C · Windshield/Door Rain/Ice Removal
  > PILOT REPORTED WINDSHIELD HEAT ARCING INFLIGHT. R & R 3 WINDSHIELD GROUNDING STRAPS & OPERATIONALLY CHECKED GOOD.
- [SDR HYIA20150420001](https://openairdocs.org/sdr/HYIA20150420001.md): Ignition Unit · faulty · Apr 16, 2015 · N6875D · Cessna 402C · Heating System
  > PILOT REPORTED HEATER, NO HEAT BURNING SMELL IN FLIGHT. R & R THE HEATER IGNITION ASSEMBLY & OPERATIONS CHECKED WITH NO FURTHER DEFECTS NOTED.
- [SDR HYIA20140414060](https://openairdocs.org/sdr/HYIA20140414060.md): Drag Brace · cracked · Jan 29, 2014 · N6875D · Cessna 402C · Landing Gear Retraction/Extension System
  > AT 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 REPLACEME
- [SDR HYIA20140414017](https://openairdocs.org/sdr/HYIA20140414017.md): Drag Brace · cracked · Jul 25, 2012 · N6875D · Cessna 402C · Landing Gear Retraction/Extension System
  > AT 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 &
- [SDR HYIA20140415074](https://openairdocs.org/sdr/HYIA20140415074.md): Drag Brace · cracked · Nov 17, 2011 · N6875D · Cessna 402C · Landing Gear Retraction/Extension System
  > AT 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 IAW
- [SDR HYIA20140415015](https://openairdocs.org/sdr/HYIA20140415015.md): Drag Brace · cracked · Jan 28, 2011 · N6875D · Cessna 402C · Landing Gear Retraction/Extension System
  > AT 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 O
- [SDR HYIA6875D12/29](https://openairdocs.org/sdr/HYIA6875D12%2F29.md): Distributor Gear · unserviceable · Dec 29, 2009 · N6875D · Cessna 402C · Magneto/Distributor
  > CREW 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. AS
- [SDR HYIA6875DAVMSTR](https://openairdocs.org/sdr/HYIA6875DAVMSTR.md): Circuit Breaker · unserviceable · Sep 1, 2009 · N6875D · Cessna 402C · DC Power Distribution System
  > DURING ROUTINE SCHEDULED INSP, MX FOUND AVIONICS MASTER SWITCH WOULD SHUT OFF IN CTR POSITION. MX R & R CIRCUIT BREAKER SWITCH. SYS CHECKS OK.
- [SDR 1356875020308](https://openairdocs.org/sdr/1356875020308.md): Adapter · failed · Jan 30, 2008 · N6875D · Cessna 402C · Engine Starter
  > ON 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 A
- [SDR 13505276875D](https://openairdocs.org/sdr/13505276875D.md): Circuit Breaker · defective · Jun 3, 2006 · N6875D · Cessna 402C · AC Power Distribution System
  > CREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.
- [SDR 08222005](https://openairdocs.org/sdr/08222005.md): Bolt · sheared · Aug 22, 2005 · N6875D · Cessna 402C · Engine (Reciprocating)
  > PROPELLER FAILED TO TURN ON START. CRANKSHAFT LARGE ATTACH BOLTS SHEARED AND GEAR DISLODGED FROM CRANKSHAFT. ENGINE REMOVED AND REPLACED.
- [SDR HYI2005F00006](https://openairdocs.org/sdr/HYI2005F00006.md): Bolt · sheared · Aug 18, 2005 · N6875D · Cessna 402C · Reciprocating Engine Power Section
  > LT 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)
- [SDR HYI2004F00000](https://openairdocs.org/sdr/HYI2004F00000.md): Spar Cap · corroded · Feb 6, 2004 · N6875D · Cessna 402C · Horizontal Stabilizer, Spar/Rib
  > CORRODED SPAR CAP LOCATION, REAR SPAR ON HORIZONTAL STABILIZER, LOWER CAP. CORRODED AT LEFT, IB HINGE, 12 INCHES OB OF IB HINGE. (NE01200401202)
- [SDR HYI2001F00003](https://openairdocs.org/sdr/HYI2001F00003.md): Master Switch · failed · Oct 11, 2001 · N6875D · Cessna 402C · DC Power Distribution System
  > ON PREFLIGHT INSPECTION, AVIONICS MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE.
- [SDR 98ZZZX989](https://openairdocs.org/sdr/98ZZZX989.md): Valve Spring · broken · Feb 10, 1998 · N6875D · Cessna 402C · Reciprocating Engine Cylinder Section
  > RIGHT ENGINE RUNNING ROUGH. FOUND 8 OF 12 VALVE SPRINGS BROKEN. REMOVED AND REPLACED ALL VALVE SPRINGS.
- [SDR 98ZZZX988](https://openairdocs.org/sdr/98ZZZX988.md): Valve Spring · broken · Feb 10, 1998 · N6875D · Cessna 402C · Reciprocating Engine Cylinder Section
  > RIGHT ENGINE RUNNING ROUGH. FOUND 8 OF 12 VALVE SPRINGS BROKEN. REMOVED AND REPLACED ALL VALVE SPRINGS.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N6875D/reports

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