DEN04LA018

NTSB accident investigation · Cessna 182A · Albuquerque, NM · October 31, 2003

Accident · No injuriesLimited investigationFinal report
Date
October 31, 2003, 16:00 local (23:00 UTC)
Place
Albuquerque, NM
Injuries
2 uninjured
Damage
Destroyed
Phase of flight
Approach
Aircraft
N5127DCessna 182A
Weather
Visual (VMC) · Day
Status
Completed · report March 30, 2004
Report
Approved by Office Director
Parties
FAA FSDO
FAA report
20031031035489A
Case key
58282

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 delayed use of carburetor heat and his inadequate flare resulting in a loss of engine power and a hard landing. Also causal was the inadequate supervision of the flight. Carburetor icing conditions was a contributing factor.

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 engine power(total) - nonmechanicalApproach - vfr pattern - final approach
Emergency procedure - simulatedDual student
Weather condition - carburetor icing conditionsFactor
Carburetor heat - delayedDual studentFactor
In-flight planning/decision - improperDual studentCause
Forced landingDescent - emergency
Hard landingEmergency landing
Flare - inadequateDual studentCause

Analysis

In the pattern for runway 22, the instructor pulled the throttle to idle and applied the carburetor heat to simulate an engine failure. The student established an airspeed of 75 mph and turned towards the runway. Approximately 100 feet agl, the airplane encountered "a heavy sink rate." The instructor stated that the stall horn did not sound and the bank angle was shallow. The student added power "rapidly"; however, the engine did not respond. The airplane struck the runway on the main gear. It bounced and struck the runway again, separating the nose gear, sending the airplane skidding on its nose. A postimpact fire ensued, consuming the fuselage.Temperature was 62 degrees Fahrenheit (F) and dew point was 32 degrees F. According to the carburetor icing probability chart, the temperature and dew point were right on the edge of serious icing conditions at glide power.

Factual narrative

On October 31, 2003, at approximately 1600 mountain standard time, a Cessna 182A, N5127D, was destroyed following a hard landing and postimpact fire at Double Eagle II Airport (AEG), Albuquerque, New Mexico. The commercial certificated instructor and student pilot receiving instruction were not injured. Visual meteorological conditions prevailed. The local instructional flight was being conducted under the provisions of Title 14 CFR Part 91. No flight plan had been filed for the flight that originated approximately 1500.

According the report submitted by the flight instructor, they had been practicing soft and short field landings on runway 17. There was no traffic at the airport so they switched to runway 22 for a better crosswind component. At midfield on the right downwind, at an altitude of 6,800 feet msl, the instructor pulled the throttle to idle and applied carburetor heat to simulate an engine failure. The student established an airspeed of 75 mph and turned towards the runway.

Approximately 100 feet agl, the airplane encountered "a heavy sink rate." The instructor stated that the stall horn did not sound and the bank angle was shallow. The student added power "rapidly"; however, the engine did not respond. The airplane struck the runway on the main gear. It bounced and struck the runway again, separating the nose gear. The airplane continued forward with its nose skidding on the runway. A postimpact fire ensued, consuming the fuselage.

According to the METAR (aviation routine weather report) taken at 1610, winds, 170 degrees at 15 knots, gusting 22 knots; visibility, 8 statute miles; sky condition, scattered 9,000 feet agl; temperature, 62 degrees Fahrenheit (F); dew point, 32 degrees F; altimeter setting, 30.02 inches. According to the carburetor icing probability chart, the temperature and dew point were right on the edge of serious icing conditions at glide power.

An examination of the engine revealed no anomalies that would have precluded it from developing power. An examination of the airplane's systems revealed no anomalies.

Aircraft

Registration
N5127D
Reported as
Cessna 182A
Category
Airplane
Serial number
51227
Airframe hours
2,596
Engine
Continental O-470-L, 230 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Instructional · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · October 17, 2003 · 5 hours before
Departed
AEG · Albuquerque, NM
Destination
NM
Airport
AEG · Double Eagle II, runway 22, 7,400 × 100 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 · 2

As NTSB recorded them. NTSB leaves out names.

Role
Flight instructor
Age
55
Injuries
None
Certificates
Flight instructor, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Last flight review
April 5, 2003
Seat
Right
Flight hours
3,238 total · 484 in this make and model · 3,024 as pilot in command · 121 in the last 90 days · 55 in the last 30 days · 1 in the last 24 hours
Role
Student pilot
Age
49
Injuries
None
Certificate
Student
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
136 total · 79 in this make and model · 49 in the last 90 days · 20 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
170° at 15 knots, gusting 22
Visibility
8 statute miles
Temperature
66 °F, dew point 32 °F
Altimeter
30.02 inHg
Observed at
AEG, 1 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.