20110105000179A

Accident · Destroyed

FAA accident report · Beech 58P · Birmingham, AL · January 5, 2011

Date
January 5, 2011 · 18:45 local
Place
Birmingham, AL
Airport
Birmingham-Shuttlesworth International
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N48TS
NTSB investigation
NTSBERA11FA107
Reported as
Beech 58P
Reported engine
Continental TSIO
People aboard
1
Fatal injuries
1
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
1,500 total0 in this make and model0 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

On January 5, 2011, about 1845 central standard time, a Beech 58P, N48TS, was destroyed when it crashed during approach to Birmingham international airport (bhm), Birmingham, Alabama. The personal flight was conducted under the provisions of 14 code of federal regulations part 91. Nightinstrument meteorological conditions prevailed, and an instrument flight rules (IFR) flight plan was filed. The certificated private pilot was killed. The flight originated from morristown municipal airport (mmu), morristown, new jersey, about 1345. According to preliminary air traffic control data from the federal aviation administration (FAA), the intended destination for the flight was shelby county airport (eet), alabaster, Alabama. Upon nearing eet, and obtaining the local weather at that airport, the pilot elected to divert to bhm. The airplane was in radar and radio contact with bhm terminal radar approach control, and subsequently the bhm control tower. The pilot was cleared for the instrument landing system (ILS) runway 24 approach at bhm, which he acknowledged. The airplane initially intercepted the localizer for the approach, but did not intercept the glide slope. The airplane then proceeded left of course, above glide slope, followed by a continued left deviation and descent below the glide slope. The tower controller then provided heading and altitude instructions in an attempt to guide the pilot onto a missed approach. The pilot acknowledged the heading instruction, but failed to turn to the assigned heading and climb to the assigned altitude. No further communications were received from the accident airplane and radar contact was lost. The wreckage was located in a residential area, resting near a street.

As the FAA filed it

ON JANUARY 5, 2011, ABOUT 1845 CENTRAL STANDARD TIME, A BEECH 58P, N48TS, WAS DESTROYED WHEN IT CRASHED DURING APPROACH TO BIRMINGHAM INTERNATIONAL AIRPORT (BHM), BIRMINGHAM, ALABAMA. THE PERSONAL FLIGHT WAS CONDUCTED UNDER THE PROVISIONS OF 14 CODE OF FEDERAL REGULATIONS PART 91. NIGHTINSTRUMENT METEOROLOGICAL CONDITIONS PREVAILED, AND AN INSTRUMENT FLIGHT RULES (IFR) FLIGHT PLAN WAS FILED. THE CERTIFICATED PRIVATE PILOT WAS KILLED. THE FLIGHT ORIGINATED FROM MORRISTOWN MUNICIPAL AIRPORT (MMU), MORRISTOWN, NEW JERSEY, ABOUT 1345. ACCORDING TO PRELIMINARY AIR TRAFFIC CONTROL DATA FROM THE FEDERAL AVIATION ADMINISTRATION (FAA), THE INTENDED DESTINATION FOR THE FLIGHT WAS SHELBY COUNTY AIRPORT (EET), ALABASTER, ALABAMA. UPON NEARING EET, AND OBTAINING THE LOCAL WEATHER AT THAT AIRPORT, THE PILOT ELECTED TO DIVERT TO BHM. THE AIRPLANE WAS IN RADAR AND RADIO CONTACT WITH BHM TERMINAL RADAR APPROACH CONTROL, AND SUBSEQUENTLY THE BHM CONTROL TOWER. THE PILOT WAS CLEARED FOR THE INSTRUMENT LANDING SYSTEM (ILS) RUNWAY 24 APPROACH AT BHM, WHICH HE ACKNOWLEDGED. THE AIRPLANE INITIALLY INTERCEPTED THE LOCALIZER FOR THE APPROACH, BUT DID NOT INTERCEPT THE GLIDE SLOPE. THE AIRPLANE THEN PROCEEDED LEFT OF COURSE, ABOVE GLIDE SLOPE, FOLLOWED BY A CONTINUED LEFT DEVIATION AND DESCENT BELOW THE GLIDE SLOPE. THE TOWER CONTROLLER THEN PROVIDED HEADING AND ALTITUDE INSTRUCTIONS IN AN ATTEMPT TO GUIDE THE PILOT ONTO A MISSED APPROACH. THE PILOT ACKNOWLEDGED THE HEADING INSTRUCTION, BUT FAILED TO TURN TO THE ASSIGNED HEADING AND CLIMB TO THE ASSIGNED ALTITUDE. NO FURTHER COMMUNICATIONS WERE RECEIVED FROM THE ACCIDENT AIRPLANE AND RADAR CONTACT WAS LOST. THE WRECKAGE WAS LOCATED IN A RESIDENTIAL AREA, RESTING NEAR A STREET.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N48TS · 1

Matched to the same aircraft by N-number and date.