- Registered owner
- Helfrick Edward W Jr
- Location
- Elysburg, PA
- Owner type
- Individual
- Serial number
- 31T-8104052
- Year built
- 1981
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- December 9, 1981
- Certificate issued
- January 9, 2020
- Expires
- January 31, 2030
- Mode S code
- AB3FEB
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 34
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1979 | 5 |
|---|---|
| 1980 | 4 |
| 1981 | 3 |
| 1982 | 1 |
| 1983 | 1 |
| 1985 | 1 |
| 1993 | 1 |
| 1994 | 1 |
| 1996 | 5 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 2 |
| 2004 | 1 |
| 2005 | 4 |
| 2009 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2017 | 1 |
See all 38 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Piper PA-31T1
SAIB CE-17-05Electrical Power/Electrical Power System WiringSAIB CE-08-11Landing GearNTSB investigations
No NTSB investigations matched to N824CBMatched 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 Piper PA-31T1 aircraft
Investigations on N824CB not matched to an aircraft · 2
They name N824CB, but no registry record covers the date, the aircraft registered then was built later, or the investigation describes another aircraft.
NTSB SEA85FA190Accident · 2 fatalField investigationFinal reportBeachner Quick Silver · Vancouver, WAPlt was observed working on engine distributor prior to departure for weekend demo at airshow for design sales promotion. Witnesses noted engine sound on takeoff seemed less than normal. Acft lifted off, gear were retracted and acft climbed to about 200 ft…NTSB LAX82FUJ26Accident · Minor injuriesFinal reportBeachner Quick Silver · Kingman, AZAfter climbing up to pattern altitude the engine lost power. The pilot made a turn back towards the airport while trying to restart the engine but had to land in an old B-17 parking area. The aircraft struck a fence and ditch during rollout and nosed over.…
FAA incident reports
No FAA accident or incident reports matched to N824CBMatched 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 Piper PA-31T1 aircraft
Reports on N824CB not matched to an aircraft · 2
They name N824CB, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Accident 19850807040489AAmtr Quicksilver · Vancouver, WADuring attempted turn back to airport, nose fell through. Impacted ground, fuselage was totally consumed by fire.Accident 19820119001299AAmtr Quicksilver · Kingman, AZEngine quit after takeoff. Landed in parking lot, overturned. Particles engine cleaning beads blocked oil holes. .
Service difficulty reports
No reports matched to N824CBGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Piper PA-31T1 aircraft
Reports on N824CB not matched to an aircraft · 6
They name N824CB, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR ZESA20110714001Starter Gen · failedRIGHT GENERATOR FAILED, WARNING LIGHT ILLUMINATED, VOLTAGE DROPPED TO ZERO AND A SLIGHT VIBRATION OCCURED THAT HAD DIRECT RELATIONSHIP TO THROTTLE POSITION. PILOT ELECTED TO RETURN TO DEPARTED AIRPORT. NO FURTHER DEFECTS WERE NOTED WITH UNEVENTFUL LANDING.SDR ZESA2008007Check Valve · chatteringVIBRATION EVIDENT WITH CHANGES IN AIRSPEED, PRESSURIZATION AND GEAR RETRACTION. TROUBLESHOT SYS WITH TECH REP AND FOUND BRAKE RESERVOIR PRESSURIZATION CHECK VALVE VIBRATING DURING OPERATION. CHANGED CHECK VALVE AND RELIEF VALVE THEN PRESSURIZED CABIN. NO FASDR ZESA2008011Pitot Line · obstructedCREW IDENTIFIED AN INDICATED AIRSPEED MISCOMPARE ON TAKEOFF 15-20 KNOTS DIFFERENCE. THEY ABORTED THE TAKEOFF. MAINT REMOVED BOTH PITOT LINES FROM BOTH ADC'S AND BLEW OUT THE LINES. RECONNECTED AND TESTED ALL SYSTEMS.
STCs that may be installed · 194
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Piper PA-31T1
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 N824CB before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.