- Registered owner
- Federal Aviation Administration
- Location
- Oklahoma City, OK
- Owner type
- Government
- Serial number
- FF-15
- Year built
- 1988
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- January 7, 2005
- Certificate issued
- October 26, 1988
- Expires
- October 31, 2028
- Mode S code
- AADF83
From the FAA registry file of October 21, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PT6A-6 model are included below.
On this page
Airworthiness directives that may apply · 48
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1968 | 1 |
|---|---|
| 1969 | 1 |
| 1970 | 1 |
| 1975 | 1 |
| 1977 | 1 |
| 1980 | 2 |
| 1987 | 1 |
| 1989 | 2 |
| 1990 | 3 |
| 1991 | 2 |
| 1992 | 3 |
| 1993 | 2 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 7 |
| 1999 | 1 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 3 |
| 2005 | 5 |
| 2008 | 1 |
| 2012 | 1 |
| 2016 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
| 2025 | 1 |
See all 52 ADs
Information bulletins that may apply · 12
Advisory, not mandatory.
Airframe · Beech 300
SAIB CE-15-15Empennage Horizontal & Vertical Stabilizer StructureSAIB CE-12-36Flight Controls: AileronSAIB CE-06-27SAIB CE-03-43R1SAIB CE-02-19SAIB CE-02-11R1SAIB CE-00-16SAIB ACE-96-15Engine · Pratt & Whitney Canada PT6A-6 series
SAIB NE-15-21Fuel Injector NozzleSAIB NE-12-04Turbine/ Turboprop Engine: Reduction GearboxSAIB NE-06-34SAIB CE-03-24Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N80Matched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Beech 300 aircraft
FAA incident reports
No FAA accident or incident reports matched to N80Matched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Beech 300 aircraft
Service difficulty reports · 11
Reports filed since April 29, 1930, when this mark’s previous registration was cancelled.
SDR 2023F00331Motor · burnedSMOKE WAS DETECTED IN THE CABIN FROM SMELL AND VISUALLY. AIRCRAFT DIVERTED TO THE NEAREST ACCEPTABLE AIRFIELD (KSHD). TROUBLESHOOTING LED TO THE FLAP DRIVE MOTOR ASEMBLY AS THE PART CAUSING THE SMOKE.SDR 2022FA0000355Governor · inoperativeDURING ENGINE PRE-TAKEOFF PERFORMANCE RUNS, THE #2 PROP WOULD NOT COME OUT OF FEATHER. MAINTENANCE TEAM INSPECTED THE ENGINE &PERFORMED ENGINE RUNS AND COULD NOT DUPLICATE THE DISCREPANCY. OUT CAUTION, IT WAS DECIDED TO REPLACE THE RH ENGINE PROP GOVERNOR.SDR RU3A20180530024Warning System · activatedDURING LANDING GEAR EXTENSION, RIGHT GENERATOR INOP LIGHT ILLUMINATED.SDR RU3A20160822011Float Valve · leakingCREW REPORTED FUEL ODOR/FUMES. FOUND LEAK COMING FROM FUEL WING FLOAT VALVE ASSEMBLY. IAW COMMUNIQUE 2012-04, REPLACEMENT KIT 101-9081-5, INSTALLED ON ACFT.SDR RU3A20140331011Tube · failedDURING TAKEOFF ROLL AT APPROXIMATELY 1335Z ON RUNWAY 12 AT KLBF, PF NOTED THAT THE LOWER EFIS TUBE FAILED AT APPROXIMATELY 50-60KTS, WELL BELOW V1. BOTH PILOTS ANNOUNCED ABORT & THE TAKEOFF ROLL WAS SAFELY ABORTED. REPLACED LOWER EFIS TUBE, OPERATIONS CHECKESDR RU3A20140324010Flex Hose · looseON TAKEOFF ROLL WITH FULL THROTTLE APPLIED A VERY STRONG BURNING RUBBER SMELL FILLED THE COCKPIT. THE RT ENG OTBD HOT LIP FLEX HOSE SHOWED SIGNS OF EXHAUST LEAKAGE AROUND THE CLAMP WHICH CONNECTS TO THE INLET HEAT TUBE ON THE EXHAUST STACK. IT APPEARED THE SDR RU3A20140319009Unknown · odorON TAKEOFF ROLL WITH MAXIMUM TAKEOFF POWER SET AT 80 KIAS, A BURNING SMELL WAS NOTICED BY ALL CREW MEMBERS. TAKEOFF WAS ABORTED, EXITED THE RUNWAY & BURNING ODOR DISSIPATED, RETURNED TO FBO.SDR RU3A20140131002Warning Light · illuminatedNUMBER 2 RT PROP PITCH LIGHT ILLUMINATED ON APPROACH TO LANDING & REMAINED ON UNTIL SHUTDOWN.SDR RU3A1009Fuel Cap · unsecureFLIGHT CREW MEMBER NOTICED WHAT APPEARED TO BE A CONTRAIL COMING OFF OF LEFT WING. PIC RECOGNIZED CAUSE AS FUEL BEING SUCKED OUT OF LEFT WING. PRECAUTIONARY LANDING MADE. FOUND THAT LEFT WING FUEL CAP WAS FLAT WITH THE WING BUT UPON OPENING IT, NOTED THAT LSDR RU3A98007Governor · failedLEFT PROP FAILED TO COME OUT OF FEATHER WHEN TESTE IAW FLIGHT TEST PROCEDURES FOLLOWING MAINTENANCE. EMERGENCY PROCEDURES COMPLIED WITH AND AIRCRAFT LANDED SINGLE ENGINE SAFELY. RETURNED FOR SERVICE 12-03-98 FOLLOWING PROPELLER, PROP GOVERNOR CHANGE AND RIGGSDR RU3A98008Governor · failedPROP GOVERNOR REPLCED PRIOR TO FLIGHT TO CLEAR PREVIOUS GRIPE. LEFT PROP FAILED TO COMEOUT OF FEATHER WHEN TESTED IAW FLIGHT TEST PROCEDURES. EMERGENCY PROCEDURES COMPLIED WITH AND AIRCRAFT LANDED SINGLE ENGINE SAFELY. RETURNED TO SERVICE 12-03-98 FOLLOWING
Earlier aircraft with this N-number · 1
This aircraft carried N80 before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.