# Service difficulty reports: N4652N, cancelled Apr 17, 2021

A list on [N4652N, cancelled Apr 17, 2021](https://openairdocs.org/deregistered/N4652N-2021-04-17.md).

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

- [SDR HYIA20171226001](https://openairdocs.org/sdr/HYIA20171226001.md): Cylinder · failed · Dec 22, 2017 · N4652N · Cessna 402C · Reciprocating Engine Cylinder Section
  > PILOT REPORTED RIGHT ENGINE RUNNING ROUGH. UPON INSPECTION FOUND THE RIGHT ENGINE NR 3 CYLINDER TO HAVE LOW COMPRESSION AND THE CYLINDER EXHAUST VALVE TO HAVE EVIDENCE OF A BURNING. THE CYLINDER WAS REPLACED.
- [SDR HYIA20171213001](https://openairdocs.org/sdr/HYIA20171213001.md): Fitting · cracked · Dec 12, 2017 · N4652N · Cessna 402C · Nacelle/Pylon, Main Frame
  > THE RT OB NACELLE FITTING PART NUMBER 5292029-24 WAS FOUND TO BE CRACKED DURING BORESCOPE INSPECTION PRESCRIBED BY TEXTRON MULTI-ENGINE SERVICE LETTER MEL-54-02R2 DATED MARCH 29, 2017 AS CONTINUING ACTION REQUIRED BY AD2017-10-09. THE CRACK IS FAINT BUT V
- [SDR HYIA20161108194](https://openairdocs.org/sdr/HYIA20161108194.md): Exhaust Valve · damaged · Oct 30, 2016 · N4652N · Cessna 402C · Reciprocating Engine Cylinder Section
  > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
- [SDR HYIA20161108193](https://openairdocs.org/sdr/HYIA20161108193.md): Exhaust Valve · damaged · Oct 30, 2016 · N4652N · Cessna 402C · Reciprocating Engine Cylinder Section
  > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
- [SDR HYIA20161018001](https://openairdocs.org/sdr/HYIA20161018001.md): Exhaust Pipe · cracked · Oct 16, 2016 · N4652N · Cessna 402C · Engine Collector/Tailpipe/Nozzle
  > PILOT REPORTED ON PREFLIGHT: RIGHT ENGINE MAIN EXHAUST STACK LOOSE. UPON INSPECTION MAINTENANCE FOUND THE RIGHT OVERBOARD EXHAUST PIPE CRACKED. REPLACED OVERBOARD EXHAUST PIPE.
- [SDR HYIA20160825091](https://openairdocs.org/sdr/HYIA20160825091.md): Exhaust Valve · damaged · Aug 22, 2016 · N4652N · Cessna 402C · Reciprocating Engine Cylinder Section
  > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
- [SDR HYIA20160825090](https://openairdocs.org/sdr/HYIA20160825090.md): Exhaust Valve · damaged · Aug 22, 2016 · N4652N · Cessna 402C · Reciprocating Engine Cylinder Section
  > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
- [SDR HYIA20160825089](https://openairdocs.org/sdr/HYIA20160825089.md): Exhaust Valve · damaged · Aug 22, 2016 · N4652N · Cessna 402C · Reciprocating Engine Cylinder Section
  > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
- [SDR HYIA20160511001](https://openairdocs.org/sdr/HYIA20160511001.md): Unknown · odor · May 5, 2016 · N4652N · Cessna 402C · Air Distribution System
  > PILOT DETECTED SMELL OF BURNING RUBBER IN FIRST OFFICERS FLOORBOARD AREA. PERFORMED A DETAILED VISUAL INSPECTION ON THE FOLLOWING ACFT AREAS & COMPONENTS, MLG BRAKES, MLG WHEELS ASSEMBLY, LT & RT WW, NLG WHEEL ASSEMBLY & WW, COCKPIT AREA, CONTROL PEDESTAL, BO
- [SDR HYIA20141212001](https://openairdocs.org/sdr/HYIA20141212001.md): Sealant · faulty · Dec 10, 2014 · N4652N · Cessna 402C · Fuel Storage
  > PILOT REPORTED SMELL OF FUEL IS CONSTANT WITHIN CABIN. MX IS IN PROCESS OF RESEALING FAULTY SEALANT IN THE WING TANKS.
- [SDR HYIA20140624002](https://openairdocs.org/sdr/HYIA20140624002.md): Web · cracked · Jun 23, 2014 · N4652N · Cessna 402C · Fuselage Miscellaneous Structure
  > DURING SCHEDULED INSPECTION, MULTIPLE WEB FLANGE CRACKS WERE FOUND AT AFT FUSELAGE CARRY THROUGH SPAR ASSEMBLY PN 5211173-2 AT CTR UPPER SECTION FWD & AFT WEBS. THIS DAMAGE AREA DIRECTLY CORRESPONDS TO CTR CABIN FLOORBOARD AREA & IS PRONE TO DAMAGE AS PAXS &
- [SDR HYIA20140624001](https://openairdocs.org/sdr/HYIA20140624001.md): Beam · cracked · Jun 23, 2014 · N4652N · Cessna 402C · Nacelle/Pylon Miscellaneous Structure
  > DURING VISUAL INSPECTION OF NACELLE STRUCTURE AT TURBOCHARGER REMOVAL FOR OTHER MAINTENANCE, THE RT NACELLE CROSSOVER BEAM WAS FOUND TO BE CRACKED AT TURBOCHARGER MOUNT BRACKET ATTACH HOLE AFT SIDE OF BEAM. CORRECTIVE ACTION WILL BE TO R & R BEAM WITH NEW OEM
- [SDR HYIA20140621001](https://openairdocs.org/sdr/HYIA20140621001.md): Spar Cap · corroded · Jun 20, 2014 · N4652N · Cessna 402C · Wing Spar
  > DURING SCHEDULED INSPECTION, AREAS OF EXFOLIATING CORROSION WERE FOUND AT RT WING LWR SPAR CAP STRAP OEM PN 5292029-2 PREVIOUSLY INSTALLED TO SATISFY REQUIREMENT OF AD2005-12-13 CONCURRENT WITH MEB02-5. THE CORRECTIVE ACTION WILL BE TO PERFORM A DETAILED INSP
- [SDR HYIA20140414053](https://openairdocs.org/sdr/HYIA20140414053.md): Drag Brace · cracked · Aug 9, 2013 · N4652N · 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 HYIA20140414027](https://openairdocs.org/sdr/HYIA20140414027.md): Drag Brace · cracked · Nov 7, 2012 · N4652N · 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 & A
- [SDR HYIA2012052200001](https://openairdocs.org/sdr/HYIA2012052200001.md): Engine · power loss · May 22, 2012 · N4652N · Cessna 402C · Engine (Turbine/Turboprop)
  > RT ENGINE LOST POWER, VIBRATED SUDDENLY. INSPECTED ENGINE, CHECKED PARAMETERS, PERFORMED COMPRESSION CHECK, ADJUSTED IDLE FUEL MIXTURE, CHECKED RT WING TANK SUMP FOR WATER, PERFORMED RUN UP, COULD NOT DUPLICATE, FCF CHECKS GOOD.
- [SDR HYIA20140414008](https://openairdocs.org/sdr/HYIA20140414008.md): Drag Brace · cracked · Aug 11, 2011 · N4652N · 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 & A
- [SDR HYIA20140415008](https://openairdocs.org/sdr/HYIA20140415008.md): Drag Brace · cracked · Jan 21, 2011 · N4652N · 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 HYIA4652NRMLG](https://openairdocs.org/sdr/HYIA4652NRMLG.md): Trunnion · sheared · Aug 31, 2009 · N4652N · Cessna 402C · Fuselage, Landing Gear Attach Fittings
  > CREW REPORTED, RT MLG SHEERED OFF ON LANDING ROLL. MX FOUND RT MLG UPPER BARREL AND TRUNNION ASSY SHEARED JUST BELOW MLG ACTUATOR ATTACH POINT. MX REMOVED AND REPLACED RT MLG ASSY, RT PROPELLER, RT ENG, RT SIDE INBD AND OTBD FLAP PANEL ASSEMBIES, AND RT LAN
- [SDR 13552N122707](https://openairdocs.org/sdr/13552N122707.md): Skin · debonded · Dec 26, 2007 · N4652N · Cessna 402C · Ailerons
  > ON TAXI IN, CREW NOTICED DEBONDING HAD TAKEN PLACE ON RT AILERON UPPER IB SKIN. THE DISPLACEMENT OF SKIN DID NOT AFFECT THE FLIGHT CHARACTERISTICS OF THE AIRCRAFT AS NOTED BY THE CREW. MX REMOVED AND REPLACED AILERON, DISPENSED AILERON FOR REPAIR.
- [SDR 2002FA0000897](https://openairdocs.org/sdr/2002FA0000897.md): Angle · separated · Jul 12, 2002 · N4652N · Cessna 402C · Ailerons
  > COULD NOT MOVE AILERONS. 90 PERCENT ANGLE, USED TO PREVENT OIL CANNING, BONDED INSIDE AILERON, BROKE LOOSE AND WORKED ITS WAY DOWN TRAILING EDGE OF AILERON AND INTO FLAP TRAILING EDGE, PREVENTING AILERONS FROM MOVING. 90 PERCENT ANGLE IS 8 INCHES LONG AND.3
- [SDR 20000907SH039](https://openairdocs.org/sdr/20000907SH039.md): Tire · unserviceable · Aug 14, 2000 · N4652N · Cessna 402C · Tire
  > CREW REPORTED UNUSUAL NOISE ON TAXI. FOUND CHUNK OF AFT TIRE MISSING. MAINTENANCE DISPATCHED TO CHANGE TIRE. FOUND LARGE PORTION OF RECAP HAD SEPARATED FROM CORE TIRE. MAINTENANCE REMOVED AND REPLACED TIRE AND RELEASED AIRCRAFT BACK INTO SERVICE. (X)

## 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 = 'N4652N' AND deregistration_id = 'N4652N-2021-04-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N4652N-2021-04-17/reports

---
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