- Registered owner
- Jet Pros LLC
- Location
- Scottsdale, AZ
- Owner type
- LLC
- Serial number
- CE-1541
- Year built
- 1990
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, utility
- Airworthiness date
- December 6, 1990
- Certificate issued
- July 12, 2021
- Expires
- July 31, 2028
- Mode S code
- AB2621
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental IO-520 model are included below.
On this page
Airworthiness directives that may apply · 75
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 3 |
|---|---|
| 1973 | 2 |
| 1974 | 3 |
| 1975 | 1 |
| 1977 | 2 |
| 1978 | 1 |
| 1979 | 2 |
| 1980 | 2 |
| 1981 | 2 |
| 1984 | 1 |
| 1986 | 1 |
| 1987 | 2 |
| 1988 | 6 |
| 1991 | 4 |
| 1993 | 4 |
| 1994 | 2 |
| 1995 | 3 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 3 |
| 1999 | 2 |
| 2000 | 3 |
| 2001 | 4 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2007 | 2 |
| 2008 | 1 |
| 2009 | 2 |
| 2010 | 2 |
| 2012 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2019 | 2 |
| 2022 | 3 |
| 2023 | 6 |
| 2024 | 1 |
See all 89 ADs
Information bulletins that may apply · 16
Advisory, not mandatory.
See all 16 bulletins
NTSB investigations
No NTSB investigations matched to N8173CMatched 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 F33A aircraft
Investigations on N8173C not matched to an aircraft · 1
They name N8173C, but no registry record covers the date, the aircraft registered then was built later, or the investigation describes another 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.
Reports on N8173C not matched to an aircraft · 2
They name N8173C, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Incident 19811130085589IPiper PA28RT201T · Wichita Falls, TXLanded on wet grass runway on a severe crosswind. Slid off side of runway. Crosswind component exceeded.Incident 19810829069979IPiper PA28RT201T · Wichita Falls, TXSimulated power off landing. Pilot forgot to extend landing gear. Checked, gear operation ok.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR VJ3S2016FA0000017Circuit Breaker · failedPILOT REPORTED THAT THE ALTERNATOR WAS INOPERATIVE. THE TECH TROUBLESHOT THE SYSTEM AND DISCOVERED THE ALTERNATOR CIRCUIT BREAKER SWITCH WAS AT FAULT. THE TECH REPLACED THE CIRCUIT BREAKER SWITCH. NO CAUSE OR RECOMMENDATION AT THIS TIME.SDR 2014FA0000616Circuit Breaker · failedPILOTS REPORTED THAT THE STROBE LIGHTS WERE NOT WORKING. FOUND STROBE LIGHT CIRCUIT BREAKER FAULTY. REPLACED THE CIRCUIT BREAKER.SDR VJ3R2013FA0000263Light · failedTHE LANDING LIGHT WOOD NOT TURN OFF WITH OUT TURNING OFF THE MASTER SWITCH.SDR 2012FA0000781Switch · failedPILOT REPORTED THAT THE STROB LIGHTS WERE INOP. DURING TROUBLESHOOTING IT WAS FOUND THAT THE STROB BREAKER SWITCH WAS TO BE AT FAULT. REMOVED AND REPLACED THE SWITCH AND OPS CHECK WAS NORMAL. EXISTING SWTICH WAS INSTALLED 06/11/10 AT 19849.1, AC HOURS WITH 213SDR 2011FA0000783Circuit Breaker · failedPILOT REPORTED NAV LIGHTS INOPERATIVE. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER TO BE AT FAULT AD 2008-13-17 HAD BEEN COMPLETED.SDR 2011FA0000655Circuit Breaker · failedPILOT REPORTED LANDING LIGHT INOP. ON TROUBLESHOOTING THE TECH FOUND THE CIRCUIT BREAKER AT FAULT. INSTALLED NEW CIRCUIT BREAKER. OPS CHECKED OK.SDR 2010FA0000339Circuit Breaker · failed(VJ3S) NO POWER THROUGHT THE C/B SWITCH. INTERNAL FIALURE.SDR 2010FA0000064Switch · shortedDURING THE USE OF THE NAVIGATION LIGHTS, THE NAVIGATION LIGHT CIRCUIT BREAKER SWITCH WOULD POP AND NOT RESET. TROUBLESHOT SYS AND FOUND FAULT TO BE WITH CIRCUIT BREAKER SWITCH. REMOVED AND REPLACED SWITCH WITH SAME PN 35-380132-101. THESE SWITCHES ARE SUPPOSDR 2003FA0000733Transducer · intermittentPILOT REPORTED GAUGE FLUCTUATED FOR A SHORT TIME THEN WENT TO (0) FOR 15 MINUTES. AFTER THAT GAUGE INDICATED NORMAL FUEL FLOW, DUE TO HIGH TIME PART.SDR 2003FA0000539Pump · wornDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHTER RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NOT WORKING PROPERLY. BELIEVE DRY AIR PUMP VANSDR VJ32003F00019Pump · failedDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHTER RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERLY. BELIEVE DRY AIR PUMP VANESDR VJ32002F00004Distributor Blk · damagedMAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. CARBON BRUSH WEAR ON THE SIDE OF DISTRIBUTOR BLOCK ASSEMBLY, SHAFT SENT TO MFG FOR INSPECTION. NEW DISTRIBUTOR BLOCK ASSEMBLY INSTALLESDR 97ZZZX545Carry Thru Spar · crackedINSP FOUND CRACKS IN CARRY THRU STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER. THIS IS THE 15TH AIRCRAFT REPORTED.
STCs that may be installed · 531
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech F33A
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller
Earlier aircraft with this N-number · 1
This aircraft carried N8173C before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.