19921225051609A

Accident · Destroyed

FAA accident report · Gulstm 680FL · Lester, WA · December 25, 1992

Date
December 25, 1992 · 21:37 local
Place
Lester, WA
Phase of flight
Descent
Operating rules
Air taxi and commuter (Part 135)
Operator
HSYA
Damage
Destroyed
Aircraft
N111MN
NTSB investigation
NTSBSEA93FA046
Reported as
Gulstm 680FL
Reported engine
Lycoming IO720B1B
People aboard
1
Fatal injuries
1

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.

After leveling, seen make turns and then a dive. Leveled off prior impact. Left engine at low power. No defects. (.19) no preliminary accident narrative available. (.4) after departure, the airplane intercepted airway V-2, and appeared to climb normally until reaching 8300 ft (9000 assigned) while tracking aprx 110 deg mag. Radar analysis showed the airplane at 128 KIAS when it abruptly turned left 30 deg and then appeared to recover. Voice communication during this event was normal with no change in the pilot's level of anxiety. Immediately thereafter, the heading changed over 90 deg to the left (northbound), and a maximum 6750 fpm rate of descent developed before the heading stabilized and the descent slowed. The airplane's ground impact site was aprx 1 NM sw of the last radar target. Wreckage distribution was roughly parallel to V-2. The airplane impacted the mountainside in a steep nose low, left wing down attitude. The engines, propellers/governors were disassembled and inspected with no evidence of mechanical malfunction. Exam of the left propeller indicated low power on impact. There was no evidence of significant icing/turbulence.

As the FAA filed it

AFTER LEVELING, SEEN MAKE TURNS AND THEN A DIVE. LEVELED OFF PRIOR IMPACT. LEFT ENGINE AT LOW POWER. NO DEFECTS. (.19) NO PRELIMINARY ACCIDENT NARRATIVE AVAILABLE. (.4) AFTER DEPARTURE, THE AIRPLANE INTERCEPTED AIRWAY V-2, AND APPEARED TO CLIMB NORMALLY UNTIL REACHING 8300 FT (9000 ASSIGNED) WHILE TRACKING APRX 110 DEG MAG. RADAR ANALYSIS SHOWED THE AIRPLANE AT 128 KIAS WHEN IT ABRUPTLY TURNED LEFT 30 DEG AND THEN APPEARED TO RECOVER. VOICE COMMUNICATION DURING THIS EVENT WAS NORMAL WITH NO CHANGE IN THE PILOT'S LEVEL OF ANXIETY. IMMEDIATELY THEREAFTER, THE HEADING CHANGED OVER 90 DEG TO THE LEFT (NORTHBOUND), AND A MAXIMUM 6750 FPM RATE OF DESCENT DEVELOPED BEFORE THE HEADING STABILIZED AND THE DESCENT SLOWED. THE AIRPLANE'S GROUND IMPACT SITE WAS APRX 1 NM SW OF THE LAST RADAR TARGET. WRECKAGE DISTRIBUTION WAS ROUGHLY PARALLEL TO V-2. THE AIRPLANE IMPACTED THE MOUNTAINSIDE IN A STEEP NOSE LOW, LEFT WING DOWN ATTITUDE. THE ENGINES, PROPELLERS/GOVERNORS WERE DISASSEMBLED AND INSPECTED WITH NO EVIDENCE OF MECHANICAL MALFUNCTION. EXAM OF THE LEFT PROPELLER INDICATED LOW POWER ON IMPACT. THERE WAS NO EVIDENCE OF SIGNIFICANT ICING/TURBULENCE.

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 N111MN · 1

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