N78DA1976 Beechcraft B100
Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply5 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Name not published by the FAA
- Certificate issued
- Aug 27, 2025
- Expires
- Aug 31, 2032
- Airworthiness
- Standard · Normal
- Airworthiness date
- Jun 21, 1976
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Beechcraft
- Model
- B100
- Year
- 1976
- Serial number
- BE-11
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 11
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- AA8E79
Engine
- Make and model
- Airesearch Tpe331-5&6ser
- Type
- Turbo-prop
- Power
- 776 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2025 – nowName not published by the FAAcurrent
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (4)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2004-22-28 | Raytheon Aircraft Company Model B100 Airplanes | Dec 27, 2004 | Airframe (B100)Certain serial numbers: B100 BE-1–BE-136 |
| 2004-17-02 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes | Oct 4, 2004 | Airframe (B100)Certain serial numbers: 65-A90, B90, C90, C90A LJ-76; 65-A90, B90, C90, C90A LJ-114–LJ-1691; E90 LW-1–LW-347; F90 LA-2–LA-236; 99, 99A, A99A, B99, C99 U-1–U-239; 100, A100 B-1–B-94; … |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (B100) |
| 97-23-17 | Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as… | Dec 29, 1997 | Airframe (B100)Certain serial numbers: C90 LJ-683–LJ-1463; C90A LJ-683–LJ-1463; E90 LW-177–LW-347; F90 LA-1–LA-236; H90 LL-1–LL-61; A100 B-228–B-247; … |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (5)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Stabilizers · hinge · crackedMay 28, 2002
DURING 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 REPAIR VISIBLE CRACKING.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Ice and rain protection · tube · damagedMay 28, 2002
WHILE 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 SAFTIED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bracket · crackedMay 28, 2002
WHILE 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.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Wings · rib · crackedMay 28, 2002
DURING 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. INSPECTORS SHOULD INSPECT AREA AT FLAP…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Air conditioning and pressurization · duct · failedJun 22, 2001
WHILE 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.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026