- Owner type
- LLC
- Serial number
- BE-11
- Year built
- 1976
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- June 21, 1976
- Certificate issued
- August 27, 2025
- Expires
- August 31, 2032
- Mode S code
- AA8E79
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 36
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1976 | 1 |
|---|---|
| 1977 | 2 |
| 1978 | 2 |
| 1979 | 1 |
| 1980 | 1 |
| 1982 | 1 |
| 1985 | 1 |
| 1986 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 1 |
| 1990 | 2 |
| 1992 | 2 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 4 |
| 2001 | 1 |
| 2003 | 2 |
| 2004 | 3 |
| 2005 | 3 |
| 2006 | 2 |
| 2008 | 1 |
| 2021 | 1 |
| 2023 | 1 |
See all 39 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N78DAMatched 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 B100 aircraft
FAA incident reports
No FAA accident or incident reports matched to N78DAMatched 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 Beech B100 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 R2J2002F00008Rib · crackedDURING PHASE INSPECTION FOUND CRACK IN SHIM UNDER RIGHT INBOARD FLAP IN AREA OF ACTUATOR ATTACH BRACKET. SKIN WAS CRACKED BECAUSE THE FLAP RIB HAD BROKEN. THIS RIB IS WHAT THE FLAP ACTUATOR FOR INSPECTION. THE CRACKED SHIM WAS A RESULT OF RIB FAILURE. INSSDR R2J2002F00007Bracket · crackedWHILE COMPLETING INSPECTION OF CABIN ELEVATOR PULLEY BRACKET PER MFG SB. FOUND BRACKET CRACKED AND STOP DRILLED NOT APPROVED REPAIR SB CALLS FOR NEW HEAVIER BRACKETS INSTALLED PER KIT.SDR R2J2002F00006Tube · damagedWHILE COMPLYING WITH MFG SB, BOTH ENGINE HAD DAMAGE TO ENGINE ANTI-ICE TUBING AT THE FLARES, WHICH REQUIRED REPLACEMENT. ENGINE BLEED AIR FOR ENGINE ANTI-ICE WAS DUMPING INTO COWL INSTEAD OF GOING INTO DEICE MANIFOLDS. CAUSE WAS LOOSE (B) NUTS. NEED TO BE SSDR R2J2002F00005Hinge · crackedDURING PHASE INSPECTION RIBS AT LEFT ELEVATOR OUTBOARD HINGE FOUND CRACKED. NEW PARTS INSTALLED AND ELEVATOR REINSTALLED AND ELEVATOR REINSTALLED. INSPECTORS SHOULD PAY PARTICULAR ATTENTION TO THIS AREA. MORE CRACKING WAS FOUND, AFTER ELEVATOR REMOVAL TO RESDR 2001F00164Duct · failedWHILE TROUBLESHOOTING POOR CABIN PRESSURIZATION, FOUND FAILED HOSE IN LEFT ENGINE AIR SUPPLY LINE TO CABIN. THIS CAUSED PRESSURIZATION TO WORK POORLY, BECAUSE THERE WAS NO INPUT TO CABIN FROM LEFT FLOW PACK. SUSPECT DUCT FAILED DUE TO AGE.
STCs that may be installed · 197
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech B100
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