ATL84FA045

NTSB accident investigation · Robinson R22 · Gaithersburg, MD · November 5, 1983

Accident · No injuriesField investigationFinal report
Date
November 5, 1983, 16:10 local (21:10 UTC)
Place
Gaithersburg, MD
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N8414HRobinson R22
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19831105071319A
Case key
6234

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

On this page

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/malfunctionManeuvering
Maneuver - performedPilot in command
Cyclic - improper use ofPilot in commandCause
Rotor drive system,main rotor mast(drive shaft) - overload
Rotor system,main rotor hub yoke(spindle) - overload
Rotor system,main rotor hub - overload
Rotor system,main rotor hub stop(static/dynamic) - overload

Analysis

During his 2nd solo flt in the Robinson R22, the plt performed 2 low 'g' maneuvers. The 1st maneuver was essentially the same as when he practiced it during a check-out flt. However, the 2nd maneuver produced a rapid right roll to aprx 60 deg of bank. The plt recovered in a descending right turn. After recovery, the acft seemed to be operating normally. Before landing, he practiced an autorotative apch to a power on recovery without touching down. Several landing were made, but he stated all touchdowns were normal. A post flt inspection revealed the main rotor spindles had bumped the mast at the teetering stops, resulting in dents up to .045 to .50 inch in the mast. Also, the main rotor spindle arms (horns) had contacted the droop stops, shearing the droop stop retainer bolt & bending the spindle horns. According to the manufacturer, the droop stop/bolt damage could only occur during a hard landing or negative 'g' flt. The flt manual & safety notice #11 warns: recovery from roll due to low 'g' must begin with aft cyclic first to prevent mast bumping.

Aircraft

Registration
N8414H
Reported as
Robinson R22
Category
Helicopter
Serial number
0355
Airframe hours
153
Engine
Lycoming O-320, 124 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Aero Flight Ltd
Airworthiness certificate
Standard, Normal
Last inspection
Annual · September 29, 1983 · 75 hours before
Airport
GAI · Montgomery County

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
44
Certificates
Flight instructor, Airline transport, Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
22,735 total · 5 in this make and model · 22,515 as pilot in command · 153 in the last 90 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 10 knots
Visibility
12 statute miles
Lowest ceiling
2,000 ft broken
Temperature
45 °F, dew point 34 °F
Altimeter
29.00 inHg
Observed at
DCA, 21 nm away

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 N8414H · 2

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