- Registered owner
- Teton Leasing LLC
- Location
- Pocatello, ID
- Owner type
- LLC
- Serial number
- 560-0358
- Year built
- 1996
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 12, 1996
- Certificate issued
- December 18, 2018
- Expires
- December 31, 2028
- Mode S code
- A1AFCF
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada JT15D 5 model are included below.
On this page
Airworthiness directives that may apply · 30
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 |
|---|---|
| 1990 | 1 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 2 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 2 |
| 1998 | 3 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2003 | 1 |
| 2005 | 1 |
| 2006 | 4 |
| 2007 | 2 |
| 2008 | 1 |
| 2009 | 2 |
| 2010 | 1 |
| 2013 | 1 |
| 2014 | 1 |
| 2015 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2025 | 1 |
| 2026 | 1 |
See all 35 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
Airframe · Cessna 560
SAIB AIR-21-15R1Navigation SystemSAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB NM-14-08Fuselage: Aerodynamic FairingsSAIB CE-10-49R1Equipment/Furnishings Drain Mast HeaterSAIB NM-10-13Navigation: Flight Management SystemEngine · Pratt & Whitney Canada JT15D 5 series
SAIB NE-07-03Dual-engine flameoutsHistorical bulletins · 2
NTSB investigations
No NTSB investigations matched to N208AVMatched 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 560 aircraft
FAA incident reports
No FAA accident or incident reports matched to N208AVMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 560 aircraft
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2024FA0000991Control Cable · wornRUDDER LEFT FORWARD CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH FAIRLEAD LOCATED IN CONTROL LOCK SYSTEM. THIS CABLE AVERAGES ROUGHLY 1200 HOURS BEFORE REPLACEMENT IS NECESSARY. PROPER CONTROL LOCK RIGGING AND FLIGSDR 2024FA0000990Control Cable · wornRUDDER RIGHT CENTER CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH A FAIRLEAD LOCATED ROUGHLY AT FS 415. THE MANUFACTURER HAS NO APPROVED REPAIR OR ALTERATION ASIDE FROM CABLE REPLACEMENT. THIS CABLE HAS BEEN REPLACESDR GAYA2024123000986Control Cable · wornELEVATOR LEFT MIDDLE CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CONTROL CABLE PASSES THROUGH A FAIRLEAD LOCATED ROUGHLY AT FS 415. PROPER FLIGHT CONTROL RIGGING HAS BEEN VERIFIED SEVERAL TIMES. CONTACT WITH THE MANUFACTURER HAS BEEN SDR 2025F00003Control Cable · wornELEVATOR RIGHT FORWARD CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH FAIRLEAD LOCATED IN CONTROL LOCK SYSTEM. THIS CABLE AVERAGES ROUGHLY 1200 HOURS BEFORE REPLACEMENT IS NECESSARY. PROPER CONTROL LOCK RIGGING AND FSDR 2025F00002Control Cable · wornELEVATOR LEFT FORWARD CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH FAIRLEAD LOCATED IN CONTROL LOCK SYSTEM. THIS CABLE AVERAGES ROUGHLY 1200 HOURS BEFORE REPLACEMENT IS NECESSARY. PROPER CONTROL LOCK RIGGING AND FLSDR 2025F00001Control Cable · wornAILERON RIGHT FORWARD CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH FAIRLEAD LOCATED IN CONTROL LOCK SYSTEM. THIS CABLE AVERAGES ROUGHLY 1200 HOURS BEFORE REPLACEMENT IS NECESSARY. PROPER CONTROL LOCK RIGGING AND FLSDR 2025F00000Control Cable · wornAILERON LEFT FORWARD CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH FAIRLEAD LOCATED IN CONTROL LOCK SYSTEM. THIS CABLE AVERAGES ROUGHLY 1200 HOURS BEFORE REPLACEMENT IS NECESSARY. PROPER CONTROL LOCK RIGGING AND FLISDR 2024FA0000992Control Cable · wornRUDDER RIGHT FORWARD CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH FAIRLEAD LOCATED IN CONTROL LOCK SYSTEM. THIS CABLE AVERAGES ROUGHLY 1200 HOURS BEFORE REPLACEMENT IS NECESSARY. PROPER CONTROL LOCK RIGGING AND FLISDR 2024FA0000989Control Cable · wornRIGHT WING UPPER INBOARD AILERON CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH A FAIRLEAD LOCATED AT WS 111.62. THE MANUFACTURER HAS NO APPROVED REPAIR OR ALTERATION FOR THIS ISSUE OTHER THAN REPLACING THE CABLE. THSDR 2024FA0000988Control Cable · wornLEFT WING UPPER INBOARD AILERON WING CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH A FAIRLEAD LOCATED AT WS 111.62. PROPER FLIGHT CONTROL RIGGING HAS BEEN VERIFIED MULTIPLE TIMES. THE MANUFACTURER HAS NO APPROVED RESDR 2024F00326Control Cable · wornRIGHT MIDDLE ELEVATOR CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH A FAIRLEAD LOCATED ROUGHLY AT FS 415. PROPER FLIGHT CONTROL RIGGING HAS BEEN VERIFIED SEVERAL TIMES. CONTACT WITH THE MANUFACTURER HAS BEEN MADE WITH NO AP
STCs that may be installed · 259
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 560
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST01823WIInstallation of Garmin GTS Traffic Sensor with Garmin GTX 3000 Mode S Transponders with ADS-B Out.