- Registered owner
- Electric Boat Corp
- Location
- Groton, CT
- Owner type
- Corporation
- Serial number
- UE-336
- Year built
- 1998
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, commuter
- Airworthiness date
- October 25, 2000
- Certificate issued
- January 14, 2025
- Expires
- January 31, 2032
- Mode S code
- AB87AB
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PT6A-6 model are included below.
On this page
Airworthiness directives that may apply · 66
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1968 | 1 |
|---|---|
| 1969 | 1 |
| 1970 | 1 |
| 1975 | 1 |
| 1977 | 1 |
| 1980 | 2 |
| 1992 | 1 |
| 1994 | 1 |
| 1995 | 4 |
| 1996 | 5 |
| 1997 | 10 |
| 1998 | 5 |
| 1999 | 8 |
| 2000 | 2 |
| 2001 | 5 |
| 2002 | 2 |
| 2003 | 5 |
| 2004 | 3 |
| 2005 | 3 |
| 2006 | 2 |
| 2008 | 1 |
| 2009 | 2 |
| 2011 | 1 |
| 2012 | 2 |
| 2014 | 2 |
| 2016 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 74 ADs
Information bulletins that may apply · 9
Advisory, not mandatory.
Airframe · Raytheon 1900D
SAIB 2026-02Elevator Tab Control SystemSAIB CE-12-36Flight Controls: AileronSAIB CE-05-83SAIB CE-00-24SAIB CE-00-15Engine · Pratt & Whitney Canada PT6A-6 series
SAIB NE-15-21Fuel Injector NozzleSAIB NE-12-04Turbine/ Turboprop Engine: Reduction GearboxSAIB NE-06-34SAIB CE-03-24NTSB investigations
No NTSB investigations matched to N842EMatched 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 Raytheon 1900D aircraft
FAA incident reports
No FAA accident or incident reports matched to N842EMatched 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 Raytheon 1900D aircraft
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2012FA0000837Support · damagedLEFT SUPPORT, AFT FLANGE RIVETS WERE MISSING. SUPPORT IS LOCATED BELOW THE CABIN FLOOR UNDER THE CENTER PEDESTAL.SDR RMIA2011112200056Bulkhead · crackedLOWER PORTION OF FUSELAGE CANTED BULKHEAD AT FS 570 BUCKLED. THE LT SIDE OF THE BULKHEAD HAS SMALL CRACKS AROUND RIVET HOLES AT STRINGER 8L. EARLIER SN OF THIS MODEL ACFT HAD 0.032" BULKHEADS WITH A KIT TO UPSIZE THE SIDES OF THE BULKHEAD TO 0.050".SDR 2011FA0000297Fuel Sys · contaminatedFLIGHT CREW REPORTED RT FUEL INDICATOR BOUNCES 700-800 LBS IN FLIGHT. NORMAL TROUBLESHOOTING SHOWED SYS NORMAL. REMOVED CONNECTOR PLUGS TO FUEL CONTROL RELAY PANEL, UNDER CTR FLOOR, AND FOUND WATER IN ALL PLUGS. NO INDICATION OF WATER POOLING IN FLOOR AND ALL SDR 2005FA0001140Mount · faultyTRANSISTOR MOUNT, INSTRUMENT PANEL INDIRECT LISHTS OPERATE AT FULL BRIGHT REGARDLESS OF POTENTIATOR POSITION. TROUBLESHOOTING FOUND THAT TRANSISTOR MOUNT WAS INSTALLED BEHIND LOCATION CALLED OUT AS COPILOTS FLIGHT INSTRUMENTS. IDENTIFYING FAULTY TRANSISTOR CSDR 2004FA0000274Drag Brace · corrodedTHE LOWER BOLT WAS SEVERELY CORRODED IN PLACE REQUIRING IT TO BE DRIVEN OUT FOR REPLACEMENT. THIS BOLT, CENTER DRAG BRACE ASSY PIVOT, IS LUBRICATED ON BOTH ENDS VIA THRU BOLT GREASE PROVISIONS. THE CENTER PORTION HAS NO PROVISION FOR GREASE SINCE THIS AREA I
STCs that may be installed · 203
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 203 STCs