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DFW08LA097 · Raytheon B200

10 Apr 2008 · Taylor, TX, United States

Raytheon B200 · Accident: cabin safety event while standing

From Taylor Municipal Airport (T74) to an unrecorded destination

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Event

NTSB case
DFW08LA097
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
1 · all aircraft and ground
Ground fatalities
1
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Raytheon B200

Aircraft type
Beechcraft 200
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N300FL
Operator
Unknown
Onboard fatalities
Unknown
Route
From Taylor Municipal Airport (T74), Taylor, TXTo not recorded
Aircraft age
Not recorded
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Standing · engine(s) operating
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Cabin safety event
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Minor

Cause areas

  • Personnel issues › Action/decision

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

While performing a postmaintenance flight, the pilot heard a loud, high-pitched "screaming" sound emanating from behind the instrument panel. The pilot returned to the airport and radioed the mechanic regarding the loud sound. When the pilot brought the airplane to a stop, the sound diminished. With engines idling, the mechanic opened the door of the airplane to troubleshoot the malfunction. Cabin pressure existed when the mechanic attempted to open the entry door and the door "blew" outward. The door struck the mechanic's head. An examination of the airframe revealed that a vacuum line had separated from the vacuum controller at a T-fitting. The T-fitting was located in the area that the mechanic had worked in during installation of the vertical speed indicator. The disconnected line disabled the entire vacuum system and subsequently disabled the airplane's pressurization system outflow valve. Prior to the mechanic opening the door, the pilot reported turning the environmental controls off which stopped the in-flow of cabin pressure. However, because the vacuum system could not drive the safety valve open, the airplane remained pressurized. An examination of the door assembly and differential-pressure-sensitive diaphragm revealed no anomalies. Testing results conducted on the diaphragm were consistent with a new diaphragm. The door system met the certification requirements of 14 Code of Federal Regulations (CFR) Part 23. The Beech 200 has no means of alerting outside personnel that the airplane is still pressurized while on the ground other than resistance against the release-button, nor is it required to by 14 CFR Part 23. The Pilot's Operating Handbook onboard the airplane had not been updated. A current version of the checklist would have directed the pilot to verify a zero pressure differential during the after-landing checklist.

Probable cause

The failure of the pilot and mechanic to ensure that the airplane was depressurized prior to actuating the door. Contributing to the accident was the failure of the vacuum system.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record DFW08LA097
Event ID
20080414X00469
Case number
DFW08LA097
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: c209c7c36782cc82f74be76d4d1286e13e4fce203bfa24bfe4db255ba5d96343; retrieved 2026-09-13T18:00:24.886Z.