# Service difficulty reports: N36911

A list on [N36911](https://openairdocs.org/aircraft/N36911.md).

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

- [SDR HYIA20220405001](https://openairdocs.org/sdr/HYIA20220405001.md): Rib · cracked · May 5, 2022 · N36911 · Cessna 402C · Wing Structure
  > WHILE PERFORMING THE SID 57-10-25 INSPECTION, THREE CRACKS WHERE IDENTIFIED IN THE RIGHT CLOSE-OUT RIB (P/N 5122155-56.) THESE CRACKS WERE FOUND ON THE FORWARD ROW OF AT THE REAR TRUNNION PLATE ATTACH POINT. THERE ARE 6 HI-LOK HOLES ALIGNED VERTICALLY IN TH
- [SDR HYIA20210625001](https://openairdocs.org/sdr/HYIA20210625001.md): Fitting · cracked · Jun 25, 2021 · N36911 · Cessna 402C · Nacelle/Pylon, Attach Fittings
  > DURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE RIGHT SIDE OF THE RIGHT HAND OUTBOARD NACELLE FITTING. THIS CRACK MEASURES APPROXIMATELY.097 LONG AND IS CONSISTENT WITH OTHER CRACKS FOUND USING THE LIGHTED BORESCOPE INSPECTION TE
- [SDR HYIA20181130001](https://openairdocs.org/sdr/HYIA20181130001.md): Crankshaft · fractured · Nov 28, 2018 · N36911 · Cessna 402C · Reciprocating Engine Power Section
  > PILOT REPORTED DURING CLIMB/CRUISE FLIGHT THE RIGHT HYDRAULIC FLOW LIGHT CAME ON AND RIGHT ENGINE LOST POWER. UPON INITIAL INSPECTION, THE ENGINE WAS FOUND TO BE SEIZED. PISTONS AT CYLINDERS 1-4 WERE FOUND TO BE IN THE TOP DEAD CENTER POSITION. CYLINDER #3 W
- [SDR HYIA20170828002](https://openairdocs.org/sdr/HYIA20170828002.md): Fitting · cracked · Mar 8, 2017 · N36911 · Cessna 402C · Nacelle/Pylon, Main Frame
  > DURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT INBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK IS APPROXIMATELY 1.208 INCHES IN LENGTH. OPEN
- [SDR HYIA20170828001](https://openairdocs.org/sdr/HYIA20170828001.md): Fitting · cracked · Mar 8, 2017 · N36911 · Cessna 402C · Nacelle/Pylon, Attach Fittings
  > WHILE CONDUCTING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT INBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING JUST FORWARD OF THE SPAR STRAP. THE CRACK WAS APPROXIMATELY 1.208 INCHES IN LENGTH.
- [SDR HYIA201611081840](https://openairdocs.org/sdr/HYIA201611081840.md): Exhaust Valve · damaged · Oct 21, 2016 · N36911 · Cessna 402C · Reciprocating Engine Cylinder Section
  > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
- [SDR HYIA20161108183](https://openairdocs.org/sdr/HYIA20161108183.md): Exhaust Valve · damaged · Oct 21, 2016 · N36911 · Cessna 402C · Reciprocating Engine Cylinder Section
  > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
- [SDR HYIA20160104001](https://openairdocs.org/sdr/HYIA20160104001.md): O-Ring · worn · Dec 27, 2015 · N36911 · Cessna 402C · Master Cylinder/Brake Valve
  > PILOT REPORTED NO RT BRAKE. INSPECTED & FOUND THE RT MASTER CYLINDER INTERNAL O RING WORN. REPLACED O RING IAW MM CH 32-40-01. OPERATIONALLY CHECKED GOOD.
- [SDR HYIA20140624003](https://openairdocs.org/sdr/HYIA20140624003.md): Dimmer · malfunctioned · Jun 22, 2014 · N36911 · Cessna 402C · Flight Compartment Lighting
  > SMOKE APPEARED FROM INSTRUMENT PANEL LIGHT, DIMMER ASSEMBLY. R & R DIMMER ASSEMBLY PN 5118424-1.
- [SDR HYIA2012043002](https://openairdocs.org/sdr/HYIA2012043002.md): Spar Cap · fractured · Apr 30, 2012 · N36911 · Cessna 402C · Wing Spar
  > DURING ROUTINE MX, A FRACTURE WAS FOUND IN 1 OF OUR ACFT LOCATED AT THE, RT WING AFT LOWER SPAR CAP, INBD FLAP WELL, AND ADJACENT TO LWR BELL CRANK SUPPORT AT WING STA 113.69.
- [SDR HYIA36911KG102311](https://openairdocs.org/sdr/HYIA36911KG102311.md): Gyro · shorted · Mar 16, 2011 · N36911 · Cessna 402C · Directional Gyro and Indicating System
  > CREW REPORTED, WHILE IN CRUISE CONFIGURATION, IFR CONDITIONS, CAPTAINS HEADING INDICATOR FAILED, REMOTE GYRO CIRCUIT BREAKER TRIPPED. EMERGENCY DECLARED, LANDING WAS UNEVENTFUL. MX INSPECTED ACFT, FOUND REMOTE GYRO CONTAMINATED WITH WATER. R & R GYRO, TESTED
- [SDR HYIA36911RHAXLE](https://openairdocs.org/sdr/HYIA36911RHAXLE.md): Axle · cracked · Jun 18, 2010 · N36911 · Cessna 402C · Main Landing Gear Strut/Axle/Truck
  > ON TAXI, CREW REPORTED LOAD "POP" FROM RT GEAR, ACFT BECAME DIFFICULT TO TAXI. MX FOUND RT MAIN GEAR AXLE ASSY CRACKED AT LOWER HALF. R & R AXLE ASSY. RELEASED ACFT BACK TO SERVICE.
- [SDR HYIA36911100709](https://openairdocs.org/sdr/HYIA36911100709.md): Ground Wire · broken · Oct 7, 2009 · N36911 · Cessna 402C · Landing Gear System Wiring
  > ON APPROACH TO PVC FROM BOS, PILOT REPORTED RIGHT MAIN GEAR DOWNLOCK LIGHT DID NOT ILLUMINATE, PERFORMED EMERGENCY GEAR EXTENSION, STILL DID NOT ILLUMINATE.PRESS TO TEST OF LIGHT CHECKED OK. PILOT ELECTED TO DIVERT. DECLARED AN EMERGENCY, LANDED WITHOUT INCID
- [SDR HYIA3691193009](https://openairdocs.org/sdr/HYIA3691193009.md): Torque Tube · cracked · Sep 30, 2009 · N36911 · Cessna 402C · Rudder Control System
  > DURING SCHEDULED MAINTENANCE INSPECTION, MAINTENANCE FOUND PILOTS LEFT RUDDER PEDAL TO TORQUE TUBE LINKAGE CRACKED. MAINTENANCE REMOVED AND REPLACED RUDDER TORQUE TUBE. AIRCRAFT RELEASED TO SERVICE.
- [SDR HYIA36911 625](https://openairdocs.org/sdr/HYIA36911%20625.md): Master Switch · unserviceable · Jun 25, 2009 · N36911 · Cessna 402C · Electrical Power System
  > CREW REPORTED AVIONIC MASTER SWITCH INOPERATIVE. MX REMOVED AND REPLACED SWITCH AND RETURNED ACFT TO SERVICE
- [SDR HYIA36911](https://openairdocs.org/sdr/HYIA36911.md): Gyro · malfunctioned · Jun 23, 2009 · N36911 · Cessna 402C · Directional Gyro and Indicating System
  > CREW REPORTED HORIZONTAL SITUATION INDICATOR INOPERATIVE IN CLIMB-OUT AT 400 FT. CONTACTED LOCAL TOWER, DECLARED AN EMERGENCY, AND RETURNED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, REMOVED AND REPLACED REMOTE GYRO. AIRCRAFT RELEASED BACK TO SERVICE
- [SDR 1356911120307](https://openairdocs.org/sdr/1356911120307.md): Actuator · intermittent · Dec 2, 2007 · N36911 · Cessna 402C · Landing Gear Retraction/Extension System
  > NOSE GEAR DOWN AND LOCKED LIGHT CAME ON AND THEN WENT OFF DURING FINAL APPROACH. BLEW GEAR DOWN TESTED GEAR DOWN INDICATION WITH FLAP HANDLE, LANDED. MAINTENANCE FOUND UPLOCK ACTUATOR TO BE BAD REMOVED AND REPLACED ACTUATOR.
- [SDR 1350603N36911](https://openairdocs.org/sdr/1350603N36911.md): Circuit Breaker · defective · Aug 3, 2006 · N36911 · Cessna 402C · Electrical Power System
  > CREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.
- [SDR YBS2003F00000](https://openairdocs.org/sdr/YBS2003F00000.md): Barrel · sheared · Jul 24, 2003 · N36911 · Cessna 402C · Main Landing Gear Strut/Axle/Truck
  > UPON LANDING, PILOT REPORTED RT MLG COLLAPSED. MECHANIC FOUND RT MLG UPPER BARREL SHEARED ABOVE UPPER TORQUE LINK ATTACH POINT. MECHANIC REMOVED AND REPLACED MLG ASSY, RT PROP, RT ENGINE, C/W MINOR SHEET METAL REPAIRS TO FLAPS, AND REPLACED RT MLG DOOR. INS
- [SDR 95ZZZW150](https://openairdocs.org/sdr/95ZZZW150.md): Le Skin · corroded · Jan 30, 1995 · N36911 · Cessna 402C · Wing, Plate/Skin
  > CORROSION ON LEADING EDGE OF WING AT TOP AND BOTTOM OF FRONT SPAR AT WS 119.29 THROUGH 229.7. CORROSION AT BOTTOM OF WING JUST AFT OF EXHAUST PIPE ON LEFT AND RIGHT WINGS AT WS 119.29. (W)
- [SDR 95ZZZW148](https://openairdocs.org/sdr/95ZZZW148.md): Le Skin · corroded · Jan 30, 1995 · N36911 · Cessna 402C · Wing, Plate/Skin
  > CORROSION LEADING EDGE TO FRONT SPAR RT WING TOP AND BOTTOM AT WS 119.29 THROUGH 229.71. (W)

## 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 = 'N36911' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N36911/reports

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