- Registered owner
- Traven Ricardo Siro
- Location
- Georgetown, SC
- Owner type
- Individual
- Serial number
- P21000677
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- March 31, 1981
- Certificate issued
- March 18, 2024
- Expires
- March 31, 2031
- Mode S code
- A8F701
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 32
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1978 | 1 |
|---|---|
| 1979 | 4 |
| 1980 | 1 |
| 1981 | 2 |
| 1982 | 2 |
| 1985 | 2 |
| 1986 | 1 |
| 1987 | 1 |
| 1988 | 2 |
| 1990 | 1 |
| 1994 | 1 |
| 1997 | 1 |
| 1998 | 3 |
| 2000 | 2 |
| 2002 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2022 | 1 |
| 2023 | 3 |
See all 34 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Cessna P210N
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-17-16Main Landing Gear Actuator InspectionSAIB CE-13-16Hydraulic Power Pack/Landing Gear SystemSAIB CE-12-41Flight Controls Loose Glide ScrewSAIB CE-12-14Three Alternative Methods of Compliance for AD 2011-10-09SAIB CE-10-40R1Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanesSAIB CE-09-10Availability of Secondary Seat Stops for Pilot and Copilot SeatsSAIB CE-05-27R1StabilizersNTSB investigations
No NTSB investigations matched to N677PCMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna P210N aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 98ZZZX1337Spark Plug · delaminatedTHE SIDE MOUNTED GROUND ELECTRODE SHOWS SIGNS OF DELAMINATION OR END SPLITS. PREVIOUS MDR SUBMITTED AND WRITTEN IN ALERT 230 SEPT 1997.SDR 98ZZZX460Downlock Shell · deformedON APPROACH WHEN GEAR EXTENDED, LT MAIN GREEN FAILED TO LIGHT. EMERGENCY GEAR EXTENSION USED TO LOCK GEAR DOWN. INSPECTION REVEALED INTERIOR OF DOWNLOCK SHELL LT SIDE PEELED BACK AND FOLDED OVER PREVENTING FULL TRAVEL OF LEG AND STOPPING OVER CENTER LOCK FROSDR 97ZZZX977Cylinder · wornDURING 100 HOUR INSPECTION, COMPRESSION CHECK REVEALED ALL SIX CYLINDERS LOW AS FOLLOWS: 35/57/50/51/49/51. CUSTOMER REPORTED USING 1 QUART PER HOUR PRIOR TO INSPECTION. REGULAR SOAP AT 50-HOUR OIL CHANGE REVEALED NO MAJOR PROBLEMS. TOTAL TIME 793.8 HOURS SDR 96ZZZX1246Bracket · crackedDURING ROUTINE INSPECTION, LT HORIZONTAL STABILIZER ATTACH BRACKET REINFORCEMENT WAS FOUND CRACKED .50 INCH IN THE LOWER LT RADIUS. CESSNA SERVICE INFORMATION LETTER SE84-17R1 CALLS FOR A REPETITIVE 100-HOUR INSPECTION OF THIS AREA, BUT IT DOES NOT LIST THE '
STCs that may be installed · 308
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 308 STCs