- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 099
- Year built
- 1988
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, transport
- Airworthiness date
- September 3, 2010
- Certificate issued
- November 2, 2020
- Expires
- November 30, 2027
- Mode S code
- ADD2B7
Dehavilland DHC-8-103TCDS A13NMAirframe · Dehavilland DHC-8-103TCDS E20NEEngine · Pratt & Whitney Canada PW121
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 168
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1986 | 2 |
|---|---|
| 1987 | 2 |
| 1988 | 3 |
| 1989 | 7 |
| 1990 | 8 |
| 1991 | 5 |
| 1992 | 1 |
| 1993 | 8 |
| 1994 | 10 |
| 1995 | 5 |
| 1996 | 8 |
| 1997 | 4 |
| 1998 | 8 |
| 1999 | 7 |
| 2000 | 5 |
| 2001 | 9 |
| 2002 | 6 |
| 2003 | 4 |
| 2004 | 11 |
| 2005 | 6 |
| 2006 | 5 |
| 2007 | 6 |
| 2008 | 2 |
| 2009 | 4 |
| 2010 | 3 |
| 2011 | 4 |
| 2012 | 5 |
| 2013 | 5 |
| 2014 | 6 |
| 2015 | 4 |
| 2016 | 2 |
| 2017 | 3 |
| 2018 | 1 |
| 2019 | 2 |
| 2021 | 1 |
| 2026 | 2 |
Airframe · Dehavilland DHC-8-103
AD 2026-11-06Hardware; Standard practices/structuresAD 2026-13-02NavigationAD 2021-19-11Flight controlsInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N990AVMatched 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 Dehavilland DHC-8-103 aircraft
FAA incident reports
No FAA accident or incident reports matched to N990AVMatched 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 Dehavilland DHC-8-103 aircraft
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 39LA2013120224Skin · dentedFUSELAGE STATION X 280.0 APPROXIMATELY INBD OF STRINGER 31L SKIN HAS DENT. REPAIRED DENT IAW RD8-53-13398.SDR 39LA2013120223Hinge · gougedNOSE LANDING GEAR LT DOOR AFT HINGE AIRCRAFT SIDE IS GOUGED. REPAIRED NLG LT FWD DOOR AFT HINGE IAW RD8-53-13389.SDR 39LA2013120222Skin · dentedFS X 255.0 APPROXIMATELY INBD OF STRINGER 31L SKIN HAS 2 DENTS. REPAIRED DENTS IAW RD8-53-13410.SDR 39LA2013120221Skin Panel · crackedNR 2 ENGINE PANEL 422AT SKIN CRACKED AT OTBD AFT LATCH. REPAIRED NR 2 ENGINE PANEL 422AT IAW RD8-71-317.SDR 39LA2013120220Skin · dentedFS STATION X 771.803 BETWEEN FRAME NR 6 & NR 7 ABOVE STRINGER 22R HAS CREASE APPROXIMATELY 6 INCHES LONG ABOVE EXISTING REPAIR DOUBLER. REPAIRED FS X 771.803 BETWEEN FRAME NR 6 & NR 7 IAW RD8-55-2625.SDR 39LA2013120219Skin · dentedFS X 285.0 APPROXIMATELY INBD OF STRINGER 29R SKIN HAS DENT. REPAIRED DENT IAW RD8-53-13409.SDR 39LA2013120218Plate · wornNR 2 LOWER COWL FWD INBD LATCH PLATE WORN. REPAIRED LATCH PLATE IAW RD8-71-018.SDR 39LA2013120217Skin · dentedRIGHT HAND CENTER EMERGENCY DOOR SKIN DENTED. FABRICATED & INSTALLED A REPAIR DOUBLER IAW RD8-52-1344.SDR 39LA2013050600004Inverter · burnedPRIMARY INVERTER LIGHT WILL NOT EXTINGUISH AND ACCOMPANIED BY BAD ODOR. PERFORMED T/S OF PRI INVERTER SYS, FOUND PRIMARY INVERTER SHORTED/BURNED, R & R PRI INVERTER ASSY PN OFF DH-1030-24-600-CSIIB, SN OFF AB3130-S8, PN ON DH-1030-24-600-CSIIB, SN ON AB3023-SSDR 39LA2013030500004Relay · inoperativeON APPROACH, DESCENDING THROUGH 12,000 FT. MASTER CAUTION ILLUMINATED FOR LANDING GEAR INOPERATIVE. PERFORMED A GO AROUND. COMPLETED QRH PROCEDURES FOR THE CAUTION LIGHT. COMPLETED MANUAL GEAR EXTENSION AND GEAR CAME DOWN WITH THREE GREEN AND LOCKED POSITISDR 3PRA2012020200001Wire · damagedON APPROACH, LANDING GEAR EXTENDED AND CREW RECEIVED A NOSE GEAR UNSAFE INDICATION. APPROACH WAS ABORTED, CREW PERFORMED THE CHECKLIST. ATTEMPTED ALTERNATE GEAR EXTENSION PROCEDURE, BUT STILL DID NOT GET A NOSE GEAR DOWN AND LOCKED INDICATION. DECISION WAS M
STCs that may be installed · 150
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 150 STCs