CHI07CA165

NTSB accident investigation · WSK PZL Mielec PZL-M-18 · Manito, IL · June 11, 2007

Accident · Minor injuriesData collectionFinal report
Date
June 11, 2007, 06:50 local (11:50 UTC)
Place
Manito, IL
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N26756WSK PZL Mielec PZL-M-18
Weather
Visual (VMC) · Day
Status
Completed · report August 30, 2007
Report
Approved by Office Director
Parties
Federal Aviation Administration - Springfield FSDO
FAA report
20070611018989A
Case key
66235

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

The pilot's failure to maintain proper airspeed and his decision to attempt flight over maximum gross weight. A factor to the accident was the stall encountered while attempting to avoid obstacles.

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.

Loss of control - in flightTakeoff - initial climb
Aircraft weight and balance - exceededPilot in commandCause
Airspeed - not maintainedPilot in commandCause
Stall - encounteredPilot in commandFactor
Object - residenceFactor
Object - tree(s)Factor
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - open field

Analysis

The agricultural airplane was substantially damaged when it impacted terrain during initial climb from runway 22 (2,784 feet by 40 feet, asphalt). Prior to departure the pilot completed a preflight inspection of the airplane, including loading the airplane with 350 gallons of an aerial application chemical and 125 gallons of avgas, and warming up the engine. The pilot reportedly did not experience any engine problems during the takeoff ground run, but he noted that the tail took longer than normal to come up into a flying position. The airplane became airborne about two-thirds down the runway. After liftoff, the pilot lowered the aircraft nose to gain additional airspeed and increased engine power because the airplane's performance was reportedly "sluggish." After the airplane had cleared some irrigation equipment the pilot lowered the nose again in an attempt to gain additional airspeed, but the airplane was "vibrating and felt rough." The pilot then noted trees and houses ahead of the airplane and began a slight right turn to clear them. The airplane "stalled" and impacted terrain while the pilot attempted to avoid the obstacles. The aircraft's type-certificate data sheet lists the maximum gross weight as being 9,260 lbs. The pilot reported that the airplane's gross weight was 10,500 lbs, but supporting documentation for the gross weight increase was not located. The airplane's weight at departure was reportedly 10,289 lbs.

Factual narrative

The agricultural airplane was substantially damaged when it impacted terrain during initial climb from runway 22 (2,784 feet by 40 feet, asphalt). Prior to departure the pilot completed a preflight inspection of the airplane, including loading the airplane with 350 gallons of an aerial application chemical and 125 gallons of avgas, and warming up the engine. The pilot reportedly did not experience any engine problems during the takeoff ground run, but he noted that the tail took longer than normal to come up into a flying position. The airplane became airborne about two-thirds down the runway. After liftoff, the pilot lowered the aircraft nose to gain additional airspeed and increased engine power because the airplane's performance was reportedly "sluggish." After the airplane had cleared some irrigation equipment the pilot lowered the nose again in an attempt to gain additional airspeed, but the airplane was "vibrating and felt rough." The pilot then noted trees and houses ahead of the airplane and began a slight right turn to clear them. The airplane "stalled" and impacted terrain while the pilot attempted to avoid the obstacles. The aircraft's type-certificate data sheet lists the maximum gross weight as being 9,260 lbs. The pilot reported that the airplane's gross weight was 10,500 lbs, but supporting documentation for the gross weight increase was not located. The airplane's weight at departure was reportedly 10,289 lbs.

Aircraft

Registration
N26756
Reported as
WSK PZL Mielec PZL-M-18
Category
Airplane
Serial number
1Z006-20
Airframe hours
2,624
Engine
WSK PZL Kalisz ASZ-62IR-M18, 967 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial application · Part 137
Operator
Palmer Flying Service Inc
Registered owner
Mitchell Aerial Application Inc
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · October 1, 2006
Departed
C45 · Manito, IL
Airport
C45 · Manito Michell, runway 22, 2,784 × 40 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
51
Injuries
Minor
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, With waivers/limitations
Last flight review
February 1, 2007
Seat
Single
Flight hours
2,167 total · 33 in this make and model · 2,098 as pilot in command · 33 in the last 90 days · 33 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
70° at 4 knots
Visibility
8 statute miles
Lowest ceiling
None
Temperature
64 °F, dew point 57 °F
Altimeter
30.07 inHg
Observed at
PIA, 11 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.