DEN89LA199

NTSB accident investigation · Cessna T210F · Englewood, CO · August 24, 1989

Accident · Serious injuriesLimited investigationFinal report
Date
August 24, 1989, 12:30 local (18:30 UTC)
Place
Englewood, CO
Injuries
1 serious, 1 minor
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N6121RCessna T210F
Weather
Visual (VMC) · Day
Status
Completed · report February 15, 1991
Report
Approved by Office Director
FAA report
19890824031539A
Case key
17770

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

A failure in the hyrdraulic power unit, which prevented operation of either the normal or emergency gear extension systems. The raised runway lip contributed to aircraft damage and pilot injury.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionApproach
Hydraulic system - failure,totalCause
Landing gear,normal retraction/extension assembly - inoperative
Landing gear,emergency extension assembly - inoperative
Gear not extendedLanding - flare/touchdown
Gear extension - not possible
Wheels up landing
On ground/water encounter with terrain/waterLanding
Airport facilities,runway/landing area condition - runwayFactor

Analysis

The instructor pilot (CFI) & dual student were practicing simulated instrument apchs. Drg an apch, the landing gear failed to extend. The pilots were unable to extend the gear by using either the normal or emergency systems. Subsequently, an apch was made to rwy 17 for a wheels up landing. To minimize the risks of sparks & fire, the CFI elected to land the acft on dirt, short of the threshold, then allow the acft to skid onto the paved rwy. However, he was unaware of a 6 inch lip at the rwy threshold. The CFI rprtd that drg the wheels up landing, the acft struck the raised lip, which resulted in a hard impact. The CFI received a compression fracture of his back. A post-acdnt exam of the hydraulic power unit revealed a 'lee plug' had 'blown out.' With the plug out, no eng driven or emergency pump pressure could have been applied to the gear extension system.

Aircraft

Registration
N6121R
Reported as
Cessna T210F
Category
Airplane
Serial number
T210-0021
Airframe hours
2,292
Engine
Continental TSIO-520-C, 285 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Gordon Vaughn
Airworthiness certificate
Standard, Normal
Last inspection
Annual · March 18, 1989
Departed
APA
Destination
APA
Airport
APA · Centennial, runway 17, 7,000 × 75 ft, asphalt

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
54
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
2,386 total · 2,204 as pilot in command · 62 in the last 90 days · 6 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
210° at 14 knots, gusting 20
Visibility
50 statute miles
Lowest ceiling
None
Temperature
81 °F

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N6121R · 1

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