- Registered owner
- Pdii LLC
- Location
- Concord, NC
- Owner type
- LLC
- Serial number
- RK-27
- Year built
- 1991
- Type
- Fixed wing multi engine
- Engine
- Turbo-jet
- Airworthiness
- Standard, transport
- Airworthiness date
- December 21, 1991
- Certificate issued
- December 21, 2021
- Expires
- December 31, 2028
- Mode S code
- AD32EE
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 · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DBCA2011110600006Starter Gen · failedAFTER FUEL STOP IN GRI LEFT ENGINE WOULD NOT SPOOL. CREW CONTACTED MX. MX CONTACTED LOCAL MX TO EVALUATE. LOCAL MX FOUND LEFT STARTER/GENERATOR FAILED. REPLACED STARTER/GENERATOR WITH OVERHAULED UNIT, OPS CHECK GOOD.SDR DBCA201101020001Starter Gen · failedWHEN PREPARING TO DEPART BZN NR 1 ENGINE WOULD NOT SPOOL. TROUBLESHOOTING BY MAINTENANCE FOUND STARTER/GENERATOR HAD FAILED. REPLACED STARTER/GENERATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD.SDR E81RJT22919Wire · broken(E81R) DURING DESCENT "A/C FAIL" ANNUNUNCIATOR LIGHT ILLUMINATED AND EMERGENCY PRESSURIZATION SYS ACTIVATED. DURING TROUBLESHOOTING FOUND WIRE E067-P0108B-22 WIRE BROKEN AT BLEED AIR OVERPRESSURE SWITCH CONNECTOR P0108. REPAIRED WIRING AT CONNECTOR AND REPLACSDR DBCA2010122100030Wire · brokenON DESCENT "AIR CONDITIONING FAIL" ANNUNCIATOR ILLUMINATED & EMERGENCY PRESSURIZATION ACTIVATED. PER ACFT CHECKLIST DESCENDED TO 10,000 FT & CLOSED BLEED AIR SOURCES. LANDING WAS UNEVENTFUL. TROUBLESHOT AND FOUND WIRE BROKEN IN AIR CYCLE TURBINE OVER PRESSUSDR DBCA2009121095GKO-Ring · failedON CLIMBOUT FROM MKE CREW NOTICED RUMBLE FROM NOSE AREA FOLLOWED BY A NOSE GEAR UNSAFE INDICATION. CREW DETERMINED NOSE GEAR HAD RELEASED FROM UPLOCK AND EXTENDED. CREW EXTENDED LANDING GEAR AND RETURNED TO MKE. LANDING WAS UNEVENTFUL. STERLING MAINTENANCESDR DBCA2009040200024Control Box · failedDURING PREFLIGHT CHECKLIST RUDDER BOOST WOULD NOT TEST. CREW RETURNED TO BLOCK. DETERMINED PROBLEM DUE TO DAU NOT RECEIVING THRUST REVERSER STOWED SIGNAL. FOUND THRUST REVERSER CONTROL BOX FAILED. REPLACED THRUST REVERSER CONTROL BOX.SDR 2008FA0000650Bracket · crackedDURING SCHEDULED AIRFRAME INSPECTION FOUND PN 45A33606-5 AND PN 45A33606-6 CABIN UNDER FLOOR REINFORCING BRACKETS AT CABIN DOOR ENTRANCEWAY CRACKED. SEE SRM 53-10-50-001, FIG 1, SHEET 2 OR 3, ITEMS 29 AND 30. SUSPECT CRACKED FROM FATIGUE, ALSO POSSIBLY FROM PSDR 2006FA0001204Release Cable · frayedDURING SCHEDULE (A) AND (B) INSPECTION FOUND LT MLG EMERGENCY UPLOCK RELEASE CABLE ASSY. SEVERLY FRAYED AND CABLE FUNCTION COMPROMISED AT UPLOCK ATTACH CLEVIS END. THIS SB 32-3200. SB 32-3200 IS A RECOMMENDED SB ONLY, COMPLIANCE RECOMMENDED WHEN CABLE ASSY
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.