MIA95LA132

NTSB accident investigation · Grumman G-164A · Zellwood, FL · May 21, 1995

Accident · No injuriesLimited investigationFinal report
Date
May 21, 1995, 09:50 local (13:50 UTC)
Place
Zellwood, FL
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N35RAGrumman G-164A
Weather
Visual (VMC) · Day
Status
Completed · report August 31, 1995
Report
Approved by Office Director
FAA report
19950521012139A
Case key
37769

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 loss of aircraft climb capability after the banner pickup for an undetermined reason. A factor related to the accident was: soft terrain in the emergency landing area.

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.

Forced landingEmergency landing after takeoff
Reason for occurrence undeterminedCause
Aircraft performance,climb capability - inadequate
Load jettison - performedPilot in command
Nose overLanding
Terrain condition - softFactor

Analysis

The pilot reported that after picking up an aerial advertising banner, the aircraft climbed to 300 feet, then it stopped climbing and the airspeed began decreasing. He increased engine power, but the airspeed continued to decrease and the aircraft began to descend. He lowered the nose and dropped the advertising banner, but the aircraft still would not maintain altitude. The pilot made a forced landing in a soft field; however, while landing, the aircraft nosed over. During a postcrash examination of the engine, engine accessories and propeller, no precrash mechanical failure or malfunction was found.

Factual narrative

On May 21, 1995, about 0950 eastern daylight time, a Grumman G-164A, N35RA, registered to Robert S. Kafka, nosed over while making a forced landing following loss of engine power at Zellwood, Florida, while on a 14 CFR Part 91 aerial advertising flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft sustained substantial damage and the airline transport-rated pilot was not injured. The flight was originating at the time of the accident.

The pilot stated that he performed a preflight inspection of the aircraft and found the fuel tank to be full. He drained the fuel system sump drains. After takeoff from Crakes Farm Strip he returned to the strip and picked up an aerial advertising banner. During climbout from the banner pickup the aircraft reached about 300 feet at which time he noticed it was not climbing. He increased engine power; however, the aircraft would not maintain airspeed or climb. He lowered the aircraft's nose and dropped the banner. While making a forced landing in a soft field planted with celery, the aircraft nosed over.

Postcrash examination of the engine, engine accessories, and propeller was performed by FAA inspectors. No evidence to indicate precrash failure or malfunction of the engine or propeller was noted.

Aircraft

Registration
N35RA
Reported as
Grumman G-164A
Category
Airplane
Serial number
1382
Airframe hours
7,547
Engine
P&W R-985-AN14B, 450 horsepower, reciprocating
Damage
Substantial damage
Flight
Part 91
Operator
Night Hawk Aerial Adv. Inc.
Registered owner
Robert S. Kafka
Airworthiness certificate
Special, Restricted (Special)
Last inspection
100 hour · March 21, 1995 · 87 hours before

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
49
Certificate
Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Front
Flight hours
15,000 total · 500 in this make and model · 14,000 as pilot in command · 20 in the last 90 days · 20 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
50° at 5 knots
Visibility
7 statute miles
Lowest ceiling
2,900 ft broken
Temperature
81 °F, dew point 70 °F
Altimeter
29.00 inHg
Observed at
ORL, 24 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.