N962CC

Cancelled 2014

Deregistered aircraft · 1986 Cessna 210R · Continental IO-520 series

Cancelled
January 10, 2014
Exported to
Brazil
Status when cancelled
Valid registration
Serial number
21064986
Year built
1986
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
April 29, 1986
Certificate issued
March 21, 2013
Last registry action
March 21, 2013
Mode S code
AD63C9
Owner when cancelled
Souther Field Aviation Inc
Location
Americus, GA
Owner type
Corporation

From the FAA registry file of October 27, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N962CC and the event date: up to this one’s cancellation.

Service difficulty reports · 8

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

SDR 99ZZZX3168Cylinder · wornDURING A ROUTINE 100-HOUR COMPRESSION TEST, EXCESSIVE LEAKAGE WAS NOTED GOING PAST THE EXHAUST VALVE. THE EXHAUST VALVE, EXHAUST VALVE GUIDE FOUND TO BE WORN OUT. THERE WAS NO CHOKE LEFT IN THE CYLINDER BORE. THIS IS A FACTORY RE-MANUFACTURED ENGINE.Aug 10, 1999 · N962CC · Cessna 210R · Reciprocating Engine Cylinder SectionSDR 99ZZZX2722Cylinder · wornDURING A ROUTINE 50-HOUR OIL CHANGE COMPRESSION CHECK, EXCESSIVE LEAKAGE WAS FOUND LEAKING PAST THE INTAKE AND EXHAUST VALVE ON THE NR 1 CYLINDER. THE CYLINDER WAS REMOVED AND FOUND TO HAVE A WORN OUT EXHAUST VALVE AND GUIDE. IT ALSO HAD A BROKEN OUTER SPRINGMay 20, 1999 · N962CC · Cessna 210R · Reciprocating Engine Cylinder SectionSDR 98ZZZX4520Starter Adapter · wornTHE ENGINE WOULD NOT CRANK OVER. INVESTIGATION REVEALED THE STARTER MOTOR WAS TURNING. INSPECTION OF THE STARTER ADAPTER, INTERNALLY, INDICATES EXCESSIVE CLEARANCES. REPLACEMENT OF THE UNIT RESOLVES PROBLEM. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE Apr 16, 1998 · N962CC · Cessna 210R · Reciprocating Engine Rear SectionSDR 98ZZZX4519Fcu · wornFUEL PRESSURES ARE UNSTABLE AND FLUCTUATING. THE ENGINE DRIVEN FUEL PUMP AND FUEL CONTROLLER ARE REPLACED AND THE PROBLEM SOLVED. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PARTS OR ASSEMBLY PROCESS OF THE PUMP AND FUEL CONTROLLER AT RE-MANUFACTURE OF TFeb 16, 1998 · N962CC · Cessna 210R · Fuel Control/Reciprocating EnginesSDR 98ZZZX4518Pump · wornFUEL PRESSURES ARE UNSTABLE AND FLUCTUATING. THE ENGINE DRIVEN FUEL PUMP AND FUEL CONTROLLER ARE REPLACED AND THE PROBLEM SOLVED. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PARTS OR ASSEMBLY PROCESS OF THE PUMP AND FUEL CONTROLLER AT RE-MANUFACTURE OF TFeb 16, 1998 · N962CC · Cessna 210R · Engine Fuel PumpSDR 97ZZZX1233Cylinder · crackedWHILE PERFORMING TCM SB 96-12, CONTINUED AIRWORTHINESS INSTRUCTIONS FOR TCM CYLINDERS, BUBBLES WERE FOUND ACCUMULATING AROUND THE NR 2 CYLINDER UPPER SPARK PLUG HOLE. INSPECTION REVEALED A CRACK AT THE SPARK PLUG HOLE. THE CRACK ORIGINATED AT THE 3 O'CLOCK PMar 6, 1997 · N962CC · Cessna 210R · Reciprocating Engine Cylinder SectionSDR 97ZZZX1232Cylinder · crackedNR 3 CYLINDER WAS REMOVED DUE TO LOW COMPRESSION. THE CYLINDER WAS SENT FOR INSPECTION. THE CYLINDER INSPECTION REVEALED A CRACK WHICH BEGAN AT THE SPARK PLUG HOLE AND TERMINATED AT THE INTAKE VALVE SEAT.Mar 6, 1997 · N962CC · Cessna 210R · Reciprocating Engine Cylinder SectionSDR 98ZZZX4459Valve Guide · crackedA ROUTINE COMPRESSION CHECK INDICATES LEAKAGE ON THE NR 2 CYLINDER. FURTHER INVESTIGATION REVEALS A CRACK ON THE CYLINDER HEAD THAT EXTENDS FROM THE FUEL INJECTOR HOLE TO THE SPARK PLUG HOLE. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE CYLINDER HEAD INSTFeb 17, 1997 · N962CC · Cessna 210R · Reciprocating Engine Cylinder Section