# Service difficulty reports: N1361G, cancelled May 22, 2020

A list on [N1361G, cancelled May 22, 2020](https://openairdocs.org/deregistered/N1361G-2020-05-22.md).

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

- [SDR HYIA20190123001](https://openairdocs.org/sdr/HYIA20190123001.md): Spar Cap · cracked · Jan 23, 2019 · N1361G · Cessna 402C · Wing Spar
  > DURING MAINTENANCE A CRACK WAS VISUALLY DISCOVERED ON THE RIGHT HAND FORWARD UPPER SPAR CAP P/N: 5122031-6. THIS CRACK HAS BEEN CONFIRMED BY SURFACE EDDY CURRENT INSPECTION AND IS LOCATED IN THE FORWARD RADIUS BETWEEN THE VERTICAL AND HORIZONTAL LEGS OF THE CA
- [SDR HYIA20180605001](https://openairdocs.org/sdr/HYIA20180605001.md): Spar Cap · corroded · Jun 1, 2018 · N1361G · Cessna 402C · Wing Spar
  > CORROSION WAS DISCOVERED ON THE LT AFT LOWER OUTBOARD SPAR CAP WS 221.71 ON THE FORWARD SIDE OF THE CAP, INSIDE THE FUEL TANK, NEAR THE RADIUS. THE CORRODED AREA MEASURED.075 TALL,.243 IN WIDTH, AND.063 IN DEPTH. OUT OF LIMITS IAW MEB 95-11, R1, SECTION 3
- [SDR HYIA20171109001](https://openairdocs.org/sdr/HYIA20171109001.md): Fitting · corroded · Nov 2, 2017 · N1361G · Cessna 402C · Wing, Attach Fittings
  > DURING A ROUTINE VISUAL INSPECTION OF THE WING ATTACH FITTINGS, CORROSION WAS DISCOVERED ON THE LEFT OUTBOARD FORWARD, AFT SIDE WING ATTACH FITTING. THE FITTING WAS REMOVED AND REPLACED WITH FACTORY NEW PARTS.
- [SDR HYIA20161109208](https://openairdocs.org/sdr/HYIA20161109208.md): Exhaust Valve · damaged · Nov 7, 2016 · N1361G · Cessna 402C · Reciprocating Engine Cylinder Section
  > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
- [SDR HYIA20160803027](https://openairdocs.org/sdr/HYIA20160803027.md): Exhaust Valve · damaged · Jul 4, 2016 · N1361G · Cessna 402C · Reciprocating Engine Cylinder Section
  > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
- [SDR HYIA03252015002](https://openairdocs.org/sdr/HYIA03252015002.md): Beam · cracked · Mar 21, 2015 · N1361G · Cessna 402C · Nacelle/Pylon Miscellaneous Structure
  > THE LT NACELLE OTBD ENG BEAM WAS FOUND TO BE CRACKED JUST FWD OF AFT ENG MOUNT, TRANSVERSE TO LENGTH OF BEAM, ACROSS UPPER FACE OF BEAM, DURING NDT PRESCRIBED WITHIN MEL-54-01. REMOVE BEAM ASSEMBLY FROM NACELLE, PERFORM DETAILED VISUAL INSPECTION OF SURROUNDI
- [SDR HYIA03252015001](https://openairdocs.org/sdr/HYIA03252015001.md): Beam · cracked · Mar 21, 2015 · N1361G · Cessna 402C · Nacelle/Pylon Miscellaneous Structure
  > THE LT NACELLE INBD ENG BEAM WAS FOUND TO BE CRACKED JUST FWD OF AFT ENG MOUNT, TRANSVERSE TO LENGTH OF BEAM, ACROSS UPPER FACE OF BEAM, DURING NDT PRESCRIBED WITHIN MEL-54-01. REMOVE BEAM ASSEMBLY FROM NACELLE, PERFORM DETAILED VISUAL INSPECTION OF SURROUNDI
- [SDR HYIA20141217002](https://openairdocs.org/sdr/HYIA20141217002.md): Door · unsecure · Dec 16, 2014 · N1361G · Cessna 402C · Emergency Exits
  > RIGHT SIDE EMER DOOR OPENED AT 1000 FT AFTER DEPARTURE. INSPECTED THE EMER EXIT DOOR SYS, SECURED THE EMER EXIT DOOR, SEALED & SEATED PROPERLY IN THE DOOR FRAME. NO FURTHER DEFECTS FOUND.
- [SDR HYIA20130621001](https://openairdocs.org/sdr/HYIA20130621001.md): Beam · cracked · Jun 17, 2013 · N1361G · Cessna 402C · Nacelle/Pylon, Main Frame
  > DURING ROUTINE INSPECTION, DAMAGE WAS NOTED AT LT NACELLE CROSSOVER BEAM INCLUDING A CRACK EXTENDING FROM OTBD EXHAUST HANGAR BRACKET HOLE LOCATIONS.
- [SDR HYIA20130611104](https://openairdocs.org/sdr/HYIA20130611104.md): Bolt · failed · May 27, 2013 · N1361G · Cessna 402C · Engine (Reciprocating)
  > CREW REPORTED LOSING RT ENGINE MAP AT 9000 FEET AND NOTICED OIL LEAKING FROM RT ENGINE COWL. THE RT PROP WAS FEATHERED AND RT ENGINE SHUTDOWN AND THE ACFT RETURNED TO DEPARTURE AIRFIELD. MX INSPECTED AND FOUND THE CRANKSHAFT GEAR WAS SEPARATED FROM THE CRANK
- [SDR HYIA20140414040](https://openairdocs.org/sdr/HYIA20140414040.md): Drag Brace · cracked · Dec 19, 2012 · N1361G · 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 HYIA20121203002](https://openairdocs.org/sdr/HYIA20121203002.md): Beam · cracked · Dec 1, 2012 · N1361G · Cessna 402C · Nacelle/Pylon, Main Frame
  > DURING A SCHEDULED MX EVENT, THE RT ENGINE ASSY WAS REMOVED FOR A SCHEDULED TIME CHANGE. UPON REMOVAL, A CRACK WAS DISCOVERED AT THE RT NACELLE CROSSOVER BEAM IN THE AREA OF TURBOCHARGER BRACKET HOLE LOCATIONS. LOCATION OF CRACK RELATIVE TO RT NACELLE CROSSOV
- [SDR HYIA20121126003](https://openairdocs.org/sdr/HYIA20121126003.md): Beam · corroded · Nov 24, 2012 · N1361G · Cessna 402C · Nacelle/Pylon, Main Frame
  > SEVERE CORROSION WAS DISCOVERED BETWEEN RT NACELLE OTBD ENGINE BEAM AND LOWER NACELLE SKIN. RIGHT NACELLE OTBD BEAM HAT CHANNEL WHICH IS SANDWICHED BETWEEN BEAM AND LOWER NACELLE SKIN, IS SEVERELY CORRODED. REMOVED RT NACELLE OTBD ENGINE BEAM, PERFORMED DET
- [SDR HYIA20120910001](https://openairdocs.org/sdr/HYIA20120910001.md): Spar · damaged · Sep 10, 2012 · N1361G · Cessna 402C · Fuselage Main, Structure
  > DURING A REGULARLY SCHEDULED MX, DAMAGE WAS DISCOVERED TO THE AFT CARRY THROUGH SPAR, CENTER SECTION UPPER CAP AND CORRESPONDING WEB FLANGES. THIS DAMAGED APPEARED TO BE CAUSED BY PREVIOUS REPAIR ATTEMPTS INCLUDING MISDRILLS TO SPAR CAP AND CRACKS IN WEB FLAN
- [SDR HYIA20120708002](https://openairdocs.org/sdr/HYIA20120708002.md): Hsi · inoperative · Jul 8, 2012 · N1361G · Cessna 402C · Directional Gyro and Indicating System
  > SHORTLY AFTER TAKEOFF, THE PILOT REPORTED THAT THEIR HSI WAS INOPERATIVE WHICH WAS ACCOMPANIED BY A SMOKE ODOR IN THE COCKPIT AND ELECTED TO RETURN FOR A LANDING. UPON INSPECTION AND CONFIRMATION BY MX, THE HSI WAS SUBSEQUENTLY REPLACED AND THE ACFT WAS RELEA
- [SDR HYIA1361GHSI](https://openairdocs.org/sdr/HYIA1361GHSI.md): Hsi · failed · Aug 15, 2011 · N1361G · Cessna 402C · Navigation System
  > PPILOT REPORTED THAT DURING CLIMB OUT AT ABOUT 500 FEET, HSI FAILED AND FROZE ON THE RUNWAY HEADING. PILOT DECLARED AN EMERGENCY AND RETURNED TO LAND. MX R & R HSI.
- [SDR HYIA20140415006](https://openairdocs.org/sdr/HYIA20140415006.md): Drag Brace · cracked · Jan 21, 2011 · N1361G · 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 HYIA1361G AVMSTR](https://openairdocs.org/sdr/HYIA1361G%20AVMSTR.md): Master Switch · unserviceable · Jan 7, 2010 · N1361G · Cessna 402C · DC Power Distribution System
  > PREFLIGHT, CREW REPORTED AVIONICS MASTER SWITCH INOPERATIVE. MX R & R CIRCUIT BREAKER SWITCH. SYS CHECKS OK. ACFT RELEASED BACK TO SERVICE.
- [SDR HYIA1361G](https://openairdocs.org/sdr/HYIA1361G.md): Master Switch · failed · Mar 24, 2009 · N1361G · Cessna 402C · AC Power Distribution System
  > CREW REPORTED BURNING ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED AVIONICS MASTER SWITCH.
- [SDR 1350603N1361G](https://openairdocs.org/sdr/1350603N1361G.md): Circuit Breaker · defective · Aug 8, 2006 · N1361G · Cessna 402C · Electrical Power System
  > CREW REPORTED AVIONICS MASTER INOP. MX CHANGED CIRCUIT BREAKER SWITCH.
- [SDR 13504421361G](https://openairdocs.org/sdr/13504421361G.md): Circuit Breaker · defective · Mar 23, 2006 · N1361G · Cessna 402C · Electrical Power System
  > CREW REPORTED AVIONICS MASTER SWITCH INOP, MX CHANGED CIRCUIT BREAKER SWITCH MFG DATE CODE 0442.
- [SDR 20001012SH030](https://openairdocs.org/sdr/20001012SH030.md): Tube · rusted · Sep 4, 2000 · N1361G · Cessna 402C · Elevator Control System
  > REMOVED RIGHT ELEVATOR FROM AIRCRAFT TO REPLACE HINGE BEARINGS. CLEANED INSIDE TUBE AND NOTICED 3 RUSTED HOLES THROUGH TUBE. REPLACED TUBE WITH NEW AND LUBED INSIDE TUBE. (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 = 'N1361G' AND deregistration_id = 'N1361G-2020-05-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N1361G-2020-05-22/reports

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