- Registered owner
- Central Iowa Aviation LLC
- Location
- Ankeny, IA
- Owner type
- LLC
- Serial number
- RK-98
- Year built
- 1995
- Type
- Fixed wing multi engine
- Engine
- Turbo-jet
- Airworthiness
- Standard, transport
- Airworthiness date
- May 9, 1996
- Certificate issued
- June 19, 2019
- Expires
- June 30, 2029
- Mode S code
- ADF63A
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 · 47
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1991 | 1 |
|---|---|
| 1992 | 2 |
| 1993 | 7 |
| 1994 | 6 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 2 |
| 2000 | 2 |
| 2001 | 4 |
| 2002 | 2 |
| 2003 | 1 |
| 2004 | 3 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 2 |
| 2011 | 2 |
| 2013 | 1 |
| 2014 | 2 |
| 2023 | 1 |
| 2026 | 1 |
See all 51 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Beech 400A
SAIB CE-18-24Flap Cable InspectionSAIB NM-13-19Airfoil Anti/De-ice SystemSAIB NM-12-25Auto Flight: Altitude ControllerEngine · Pratt & Whitney Canada JT15D 5 series
SAIB NE-07-03Dual-engine flameoutsNTSB investigations
No NTSB investigations matched to N999YBMatched 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 400A aircraft
FAA incident reports
No FAA accident or incident reports matched to N999YBMatched 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 400A aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 1KSA20140312001Warning Light · illuminatedGEAR IN TRANSIT LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION.SDR L7OA201305142002Unknown · unknownDURING TAKE OFF ROLL RT WING DIP DOWN. PILOT VERBALLY REPORTED LOUD THUMP/SUSPECTED TIRE FAILURE. INSPECTED RT LANDING GEAR STRUT, BRAKE AND MAIN WHEEL. FOUND NO DEFECTS, COULD NOT DUPLICATE PROBLEM DONE IAW AMM 32-00-00-201 & 12-00-00-201.SDR L7OA20130513001Lamp · burned outRIGHT MAIN GEAR INDICATOR LAMP OUT.SDR L7OA20130314001Resistor · burnedAFTER TAKEOFF, NOTICED SMOKE IN CABIN. FOUND AFT EVAPORATOR BLOWER RESISTOR BURNED.SDR L7OA20130109001Pressure Valve · defectivePILOT STATED NOTICED CABIN AT 10,000 FT AND CLIMBING. DONNED MASKS AND STARTED AN EMERGENCY DESCENT. CABIN CONTINUED TO CLIMB AT ABOUT 2,200 FPM AND RECEIVED A CABIN ALTITUDE ANNUNCIATOR AND THEN THE PAX MASKS DROPPED AUTOMATICALLY AROUND 14,000 CABIN ALTITUDSDR L7OA201212070001Pitch Control · malfunctionedPITCH TRIM FAILED ON TAKEOFF. REVERTED TO EMERGENCY TRIM THEN BACK TO NORMAL. AUTO PILOT PITCH TRIM OK. PERFORMED A FULL FUNCTIONAL CHECK OF THE PITCH TRIM SYSTEM IAW AMM 27-40-00-201. COULD NOT DUPLICATE PROBLEM.SDR 2012F00030Roll Servo · bindingUPON LANDING YOKE WOULD NOT TURN TO THE RIGHT. HAD NO CONTROL.
STCs that may be installed · 134
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 400A
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 ST01999WIModification to replace the lead-acid battery with a True Blue Power TB40 Nanophosphate Lithium-Ion battery.