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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

May 8, 1990 · Beech B-55 · N113EW

Watkins, CO

Overview

Report Status
Probable Cause
Event Type
Accident
Date
May 8, 1990
Injury Outcomes
1 injury (1 minor injury), 2 uninjured
Location
Watkins, CO
Aircraft
Beech B-55
Tail Number
N113EW
Operator
Int L Air Carrier Flt Academy
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
DEN90LA107

THE PURPOSE OF THE FLIGHT WAS MULTIENGINE INSTRUCTION. THE STUDENT WAS EXECUTING A SIMULATED RT. ENGINE OUT ILS APPROACH TO RUNWAY 26. THE WIND WAS REPORTED TO BE FORM 360 DEGREES AT 19 KTS. WITH GUSTS TO 24 KTS. THE STUDENT AND INSTRUCTOR ATTEMPTED TO CORRECT FOR THE RIGHT CROSSWIND WITH FULL LEFT AILERON AND RUDDER DEFLECTION. THE AIRPLANE CONTINUED TO DRIFT OFF CENTERLINE AS IT CROSSED THE MIDDLE MARKER. A GO-AROUND WAS ATTEMPTED WITH FULL POWER (BOTH ENGINES) BUT THE AIRSPEED DECAYED AND THE PILOTS COULD NOT MAINTAIN DIRECTIONAL OR ALTITUDE CONTROL. THE PILOT OPERATING HANDBOOK FOR THE BEECH 55 STATES THE DEMONSTRATED CROSSWIND LIMITATION WITH BOTH ENGINES OPERATING IS 22 KTS.

NTSB Probable Cause

EXECUTING OF A SIMULATED SINGLE ENGINE APPROACH IN WIND CONDITIONS THAT EXCEEDED THE DEMONSTRATED CROSSWIND CAPABILITY OF THE AIRPLANE WITH BOTH ENGINES OPERATING.

Full Narrative

THE PURPOSE OF THE FLIGHT WAS MULTIENGINE INSTRUCTION. THE STUDENT WAS EXECUTING A SIMULATED RT. ENGINE OUT ILS APPROACH TO RUNWAY 26. THE WIND WAS REPORTED TO BE FORM 360 DEGREES AT 19 KTS. WITH GUSTS TO 24 KTS. THE STUDENT AND INSTRUCTOR ATTEMPTED TO CORRECT FOR THE RIGHT CROSSWIND WITH FULL LEFT AILERON AND RUDDER DEFLECTION. THE AIRPLANE CONTINUED TO DRIFT OFF CENTERLINE AS IT CROSSED THE MIDDLE MARKER. A GO-AROUND WAS ATTEMPTED WITH FULL POWER (BOTH ENGINES) BUT THE AIRSPEED DECAYED AND THE PILOTS COULD NOT MAINTAIN DIRECTIONAL OR ALTITUDE CONTROL. THE PILOT OPERATING HANDBOOK FOR THE BEECH 55 STATES THE DEMONSTRATED CROSSWIND LIMITATION WITH BOTH ENGINES OPERATING IS 22 KTS.

Flight

Event TypeAccident
Event Time15:15 MDT
Nearest AirportPront Range Airport (0nm N)
Runway26
Runway Length8000 ft
Runway Width100 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBeech B-55
Tail NumberN113EW
Aircraft CategoryAir
DamageSubstantial
OperatorInt L Air Carrier Flt Academy
Operating RulePart 91
Engines2
Engine TypeReciprocating
Engine DetailsContinental · IO-520-E7B · Reciprocating · 300
Seats4

People & Injuries

Injury Summary1 injury (1 minor injury), 2 uninjured
Fatal0
Serious0
Minor1
Uninjured2
Total3
Crew 1Age 56 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind360° @ 19 kt, gusting 24 kt
Visibility10 sm
CeilingBroken clouds 800 ft
Temperature / Dew Point50 / 43 C
Altimeter29.00 inHg
Weather SourcePILO

Appendix: Source Data