N284DBHawker Siddeley DH.125-400A
This N-number isn't registered right now. Below is its last known registration, canceled Mar 26, 2008.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched2 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- 284 Db INC
- Owner type
- Corporation
- City, state
- Wilmington, DE
- Certificate issued
- Oct 10, 1997
- Canceled
- Mar 26, 2008
- Airworthiness
- Standard · Transport
- Airworthiness date
- Apr 4, 1969
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
- Hawker Siddeley
- Model
- DH.125-400A
- Serial number
- NA715
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 10
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A2DD24
Engine
- Make and model
- Rolls-Royc Viper Mk522
- Type
- Turbo-jet
- Power
- 333 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 1997 – 2008284 Db INCWilmington, DE
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (0)
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.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (2)
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.
- Wings · structure · failedJan 13, 2003
LT FLAP FAILURE 41 INCHES OUTBOARD OF INBOARD END. FLAP WAS IAW SB. WHICH STRENGTHENS FLAP FOR LANDING IN HEAVY WATER/ SLUSH CONDITIONS. AIRCRAFT ARRIVED WITH HEAVY PRECIP PRIOR TO LANDING.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · structure · failedJan 13, 2003
LEFT FLAP FAILURE 41 INCHES OUTBOARD OF INBOARD END. FLAP WAS IAW HS 125 MSB 27-112-2426, MOD 252426 WHICH STRENGTHENS FLAP FOR LANDING IN HEAVY WATER/ SLUSH CONDITIONS. AIRCRAFT ARRIVED 1/1/2003 WITH HEAVY PRECIP PRIOR TO LANDING.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026