- Registered owner
- Dodson International Parts Inc
- Location
- Rantoul, KS
- Owner type
- Corporation
- Serial number
- 043
- Year built
- 1994
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 16, 1998
- Certificate issued
- November 2, 2017
- Expires
- November 30, 2027
- Mode S code
- A52201
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada 305 model are included below.
On this page
Airworthiness directives that may apply · 19
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1993 | 1 |
|---|---|
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 1 |
| 1998 | 1 |
| 1999 | 2 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 1 |
| 2005 | 1 |
| 2010 | 1 |
| 2012 | 1 |
| 2013 | 1 |
| 2014 | 1 |
| 2017 | 2 |
| 2018 | 1 |
| 2019 | 1 |
| 2020 | 1 |
| 2022 | 1 |
See all 23 ADs
Information bulletins that may apply · 2
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N43NRMatched 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 Learjet 60 aircraft
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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2017FA0000310Armature · shortedSTARTER GEN WOULD NOT START ENGINE. ON TEAR DOWN EXAMINATION, IT WAS DISCOVERED THE ARMATURE WAS SHORTED INTERNALLY, EXHIBITING HIGH HEAT AND THE BRUSH HOLDER ASSEMBLY SHOWED SIGNS OF EXTREME HEAT. ANTI-DRIVE BEARING DID NOT SHOW DAMAGE.SDR U5QA201510020071Skin · damagedBIRD STRIKE PRIOR TO LANDING. DAMAGE TO RT LE & FLAP, BEING INSPECTED & MAPPED FOR DAMAGE AT THIS TIME.SDR U5QA2015830069Skin · damagedBIRD STRIKE ON LANDING, DAMAGE TO RT WING LE. COMPLIED WITH TEMP REPAIR IAW ENGINEERING LETTER 60043-27780 DATED 8 31 15, REPAIR OPTION 2. FERRIED ACFT UNDER JS SFP VIA D084 FOR PERMANENT REPAIR. LE IS BEING REPLACED AT THIS TIME. EXPECT RTS MID-NEXT WEEK,SDR U5QA06021Computer · intermittentFLIGHT HAD NR 1 "AHRS FAIL" INDICATION DURING DECENT. CREW MADE REVERSION SOURCE CORRECTION AND DISCUSSED POSSABILITY OF DIVERT DUE TO LIMITED OR UNKNOWN MX CAPABILITIES. DURING DISCUSSIONS, "AHRS FAIL" CORRECTED ITSELF AND SYS FUNCTIONED NORMAL. CREW MADE SESDR AJC2007F00000Sensor · shortedWHILE ON 10 MILE FINAL, THE ENGINE FIRE LIGHT ILLUMINATED FOR APPROXIMATELY 10 SECONDS. AFTER FOLLOWING THE CHECK LIST, THE FIRE LIGHT EXTINGUSHED. WHILE PERFORMING POST FLIGHT, THE FIRE DETECTION SYSTEM DID NOT PASS. NR 1 ENGINE SPECIFIC PART CAUSING PROBLESDR AJCA200600004Landing Gear · lack of lubeDEC. 04, 2006 DURING CLIMB OUT, RETRACTED LANDING GEAR AND THE UNSAFE NOSE LANDING GEAR RED LIGHT ILLUMINATED. RECYCLED THE GEAR TWICE AND EACH TIME THE NLG LIGHT REMAINED ILLUMINATED. RETURNED AND LANDED SAFELY. INVESTIGATED AND FOUND THE GEAR NEEDED LUBRICASDR AJC2005F00013Starter Gen · failedPASSING THROUGH FL 250, CREW EXPERIENCED AN IRREGULAR AIRFRAME VIBRATION AND A YAW MOTION LT TO RT. AFTER INCREASING AND DECREASING THE POWER, THE CREW FELT THE SAME IRREGULAR YAW. AFTER LANDING, CREW ISOLATED THE VIBRATION TO THE LT ENGINE. MAINTENANCE BOR
STCs that may be installed · 157
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Learjet 60
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 SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)