- Registered owner
- Daly Arthur P
- Location
- El Paso, TX
- Owner type
- Individual
- Serial number
- 21061879
- Year built
- 1977
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- April 12, 1977
- Certificate issued
- April 6, 2020
- Expires
- April 30, 2027
- Mode S code
- A9D4A9
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental TSIO-520 model are included below.
On this page
Airworthiness directives that may apply · 97
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1969 | 2 |
|---|---|
| 1970 | 1 |
| 1971 | 1 |
| 1972 | 1 |
| 1974 | 1 |
| 1975 | 1 |
| 1976 | 1 |
| 1977 | 2 |
| 1978 | 2 |
| 1979 | 8 |
| 1980 | 5 |
| 1981 | 2 |
| 1982 | 2 |
| 1985 | 2 |
| 1986 | 2 |
| 1987 | 3 |
| 1988 | 8 |
| 1989 | 1 |
| 1990 | 3 |
| 1991 | 1 |
| 1993 | 4 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 1 |
| 1998 | 3 |
| 1999 | 1 |
| 2000 | 3 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2007 | 2 |
| 2008 | 2 |
| 2009 | 3 |
| 2010 | 2 |
| 2011 | 3 |
| 2012 | 4 |
| 2014 | 1 |
| 2016 | 1 |
| 2020 | 2 |
| 2022 | 3 |
| 2023 | 6 |
| 2024 | 1 |
See all 108 ADs
Information bulletins that may apply · 20
Advisory, not mandatory.
See all 20 bulletins
NTSB investigations · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB CEN09CA123Accident · No injuriesData collectionFinal reportFort Collins, COA total loss of engine power due to fuel starvation as a result of the pilot's failure to select the fullest tank before landing.NTSB CHI94LA125Accident · No injuriesLimited investigationFinal reportPomona, MOThe seperation of the landing gear door actuator, resulting in total loss of hydraulic fluid.
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 20081231852919AApproach · Fort Collins/L, COAircraft landed on highway about 1 mile south of fnl (ft Collins-Loveland municipal airport co.) pilot stated engine problems. Aircraft struck 3 highway signs with left wing, one prop blade and left side door frame.Accident 19940331007289AFcd/Prec Ldg From Cruise · West Plains, MOExtending gear door acuator piston separated loosing hydraulic fluid. Landing r main folded. Cyl snap ring came out
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2014FA0000046Lifter · spalledTWO SPALLED EXHUAST LIFTERS WHICH DAMAGE CAM.SDR 2011FA0000797Housing · wornCOPILOT SEAT ROLLER HOUSING TANG LENGTH WORN BELOW LIMIT OF AD 2011-10-09.SDR 2011FA0000437Contactor · inoperativeBATTERY CONTACTOR FAILED TO OPEN WHEN DEENERGIZED BY MASTER SWITCH.SDR 2007FA0000817Alternator · failedOVERHAULED DOFF10300B ALTERNATOR FAILED AFTER 458 HOURS IN 35 MONTHS OF USE.SDR 2005FA0000024Bolt · loose3 OF THE 4 BOLTS THAT ATTACH THE METAL PLATE THAT THE ACTUATOR IS MOUNTED ON TO THE WASTEGATE BODY WERE MISSING. FOURTH BOLT WAS BACKED OUT ABOUT HALF WAY. ALL THREE BOLTS FOUND LOOSE IN ENGINE COMPARTMENT. WASTEGATE ASSEMBLY ONLY 287 FROM OVERHAUL BY MAIN SDR 2005FA0001298Alternator · failedOVERHAULED ALTERNATOR FAILED IN FLIGHT AFTER 351 HOURS IN SERVICE.SDR 2004FA0000807Exhaust Valve · burnedEXHAUST VALVE LEAKAGE ON COMPRESSION CHECK. BURNED VALVE VERIFIED BORESCOPE INSPECTION. VALVE STEM AND GUIDE WORN BEYOND SERVICE LIMITS.SDR 2004FA0000021Vernatherm · failedVERNATHERM FAILED TO BYPASS OIL COOLER WHEN OIL TEMPS LOW.SDR 2003FA0001119Exhaust Valve · wornCYLINDER FAILED COMPRESSION CHECK DUE TO EXHAUST VALVE LEAKAGE. VISUAL INSPECTION REVEALED BURNED EXHAUST VALVE WITH NO SIGNS OF OVER TEMP OR CARBON BUILD UP. VALVE STEM AND GUIDE WORN BEYOND SERVICE LIMITS. EXHAUST VALVES IN CYLINDERS 4 AND 5 EXPERIENCE IDSDR 2002FA0000508Switch · failedGEAR FAILED TO INDICATE UP AND LOCKED ON RETRACTION.SDR 99ZZZX2954Hose · separatedHOSE CLOSE TO GEAR DOOR DOUBLE-ACTING HYDRAULIC ACTUATOR SEPARATED AT SOCKET DURING LANDING GEAR LOWERING CYCLE. HOSE WAS FIVE YEARS OLD.
STCs that may be installed · 479
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna T210M
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA2598NMInstallation of an air to air intercooler in the engine induction system downstream of the turbocharger. (See specific serial numbers) H S/N T210-308 THRU T210-0392)STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.