- Registered owner
- Federal Aviation Administration
- Location
- Oklahoma City, OK
- Owner type
- Government
- Serial number
- FF-4
- Year built
- 1988
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- July 31, 1995
- Certificate issued
- May 26, 1988
- Expires
- April 30, 2030
- Mode S code
- A9285C
From the FAA registry file of October 22, 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 N69Matched 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 Beech 300 aircraft
FAA incident reports
No FAA accident or incident reports matched to N69Matched 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 Beech 300 aircraft
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR RU3A2025102800001Brake · overtempDURING ROLLOUT INSPECTION, CREW RETURNED TO GATE DUE TO AIRCRAFT'S BRAKES BECAME EXCESSIVELY HOT PRODUCING VISIBLE SMOKE. FIRE TRUCKS WERE ROLLED OUT AND SPRAYED THE HOT BRAKES DOWN; AIRCRAFT WAS EVACUATED AND TOWED BACK TO THE GATE. CREW EVACUATED THROUGH THESDR RU3A201912025065Tube · leakingAT 14,000' THE LEFT BLEED AIR FAIL LIGHT ILLUMINATED WHEN SINGLE AND MANUAL ACTIVATION WAS ATTEMPTED. A SINGLE HOLE WAS DISCOVERED IN 3FT SECTION OF EVA TUBING IN LEFT GEAR WHEEL WELL. REPLACEMENT OF TUBING CORRECTED THIS DISCREPANCY.SDR RU3A201910032048Clamp · leakingRIGHT BLEED AIR FAIL LIGHT ILLUMINATED. MAINTENANCE DISCOVERED SEVERAL HOLES RH INBD NAC EVA TUBING. R2 EVA TUBE, FOUND BAD CLAMPS AND SLEEVES (BLEED AIR LEAK) INSTALLED 3 NEW SLEEVES AND ALL NEW CLAMPSSDR RU3A201906130022Skin · crackedFRAME CRACK AND MULTIPLE SKIN CRACKS IN THE LOWER FUSELAGE SKIN AT THE COMMUNICATION ANTENNA WERE DETECTED WHILE IN CHECK. EXTERNAL DOUBLER PART NUMBER 53-0048-401 HAS BEEN INSTALLED PER MAJOR REPAIR ENGINEERING ORDER 19-28-31 "REPAIR OF CRACKS AT FS180 LOWER SDR RU3A20190326010Proximity Switch · out of adjustLEFT PROP PITCH LIGHT ILLUMINATED IN FLIGHT. LASTED APPROX 10 MIN. ISSUE WAS CLEARED FOLLOWING THE CLEANING AND ADJUSTMENT OF PROXIMITY SWITCH.SDR RU3A2018111508048Proximity Switch · out of adjustLEFT PROP PITCH LIGHT ILLUMINATED IN FLIGHT. ISSUE WAS CLEARED BY ADJUSTING THE PROXIMITY SWITCH.SDR RU3A2018F00127Proximity Switch · faultyL PROP PITCH CAUTION LIGHT ILLUMINATED IN FLIGHT (CRUISE, 200 KTS, 5000') CAUSED BY FAULTY PROX SWITCH. INSTALLED NEW PROX SWITCH. OPERATIONAL CHECK SATISFACTORY.SDR RU3A20180924042Line · damagedRIGHT ENG BLEED AIR LIGHT ILLUMINATES IN FLIGHT. FOUND INSULATION MISSING ON BLEED AIR LINE (RT INBD WING) PUTTING A HOLE IN EVA TUBING. CORRECTED BY WRAPPING BLEED AIR LINE WITH ISULATION AND METAL TAPE AND INSTALLING SPLICE IN EVA TUBING. RAN ENGINES, BLEED SDR RU3A20141215044Governor · failedINSIDE OF 100FT, NOTICED THE LT PROP PITCH LIGHT ILLUMINATED. AT 50 FEET THE THROTTLES WERE RETARDED TO IDLE & THE ACFT EXPERIENCED AN ABRUPT SLOW DOWN & PROP NOISE INCREASED. THE AIRSPEED INSTANTLY DROPPED OFF & THE FIRST OFFICER ATTEMPTED TO ARREST THE ENSSDR RU3A20140828028Tube · delaminatedRIGHT INBD LE FUEL BAG LEAKING BEYOND LIMITS 20 MIN AFTER LANDING. FOUND INBD RUBBER TRANSFER TUBE SPLIT & DELAMINATED. R & R FUEL CELL.SDR RU3A1003Servo · malfunctionedDURING CLIMBOUT AFTER 1000 MSL, PILOT WENT TO ENGAGE AUTOPILOT. HDG AND ALT SEL SELECTED FOR PHASE OF FLIGHT. AIRCRAFT MADE IMMEDIATE 30 DEGREE LEFT THEN 30 DEGREE RIGHT ROLL FOLLOWED BY AUTOPILOT DISCONNECT AND ILLUMINATION OF RED WARNING LIGHTS AND TONE OFSDR RU3A 0905Trunnion · crackedRT MAIN LANDING GEAR INBD TRUNNION ATTACH ANGLE HAS A 3 INCH CRACK. SEVERAL AIRCRAFT IN OUR FLEET WITH THE 101-120122-13 THRU -16 ANGLES CRACKING. REPLACED ANGLE.SDR RU3A99011Inverter · burntLOST NR 1 INVERTER AND ASSOCIATED AVIONICS. USED EMERGENCY CHECK LIST AND SWITCHED TO NR 2 INVERTER. REPLACED CURRENT LIMITER AND NR 1 INVERTER. (X)
STCs that may be installed · 333
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 300
STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light ControllerSTC SA02658LAReplacement of the original Pratt and Whitney PT6A-60A engines and propellers with Pratt and Whitney PT6A-67A engines and MT Propeller MTV-27-1-N-C-F-R(P)/CFR260-65b propellers
Earlier aircraft with this N-number · 3
These aircraft carried N69 before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.