LAX93LA199

NTSB accident investigation · Canadair F-86E MK.6 · Santa Ana, CA · May 2, 1993

Accident · FatalLimited investigationFinal report
Date
May 2, 1993, 13:43 local (20:43 UTC)
Place
Santa Ana, CA
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N3842JCanadair F-86E MK.6
Weather
Visual (VMC) · Day
Status
Completed · report August 31, 1994
Report
Approved by Office Director
FAA report
19930502011339A
Case key
28372

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 inadequate planning/decision concerning performance of an aerobatic maneuver, and his failure to maintain adequate altitude/clearance above the runway during recovery from the maneuver. A factor related to the accident was: the pilot's lower tolerance to 'g's' (physiological condition) by not wearing a 'g' suit (miscellaneous equipment).

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.

In flight collision with terrain/waterManeuvering
Aerobatics - performedPilot in command
In-flight planning/decision - inadequatePilot in commandCause
Altitude - inadequatePilot in commandCause
Miscellaneous equipment - not usedPilot in commandFactor
Physiological conditionPilot in commandFactor

Analysis

A preplanned routine involving an F-86 and a MIG-15 had been scheduled for the airshow. When the MIG-15 pilot was unable to participate, the F-86 pilot elected to conduct a solo aerobatic routine that had not been practiced for the show. After takeoff, he began a loop with an aileron roll at the top of the maneuver. During descent from the top of the loop, the airplane developed a high rate of descent and contacted the runway in a near nose and wing level attitude. The pilot was not wearing a 'g' suit, and the calculated 'g's' sustained during the pull-out (before impact) were 6.4 g's. no spectators were injured.

Factual narrative

History of flight

On May 2, 1993, about 1343 hours Pacific daylight time, a Canadair F- 86E Mark 6, N3842J, crashed during an aerial demonstration at the El Toro Marine Corps Air Station, Santa Ana, California. The airplane was being operated as part of an annual air show when the accident occurred. The airplane, operated by the pilot in partnership with National Airshows Inc., was destroyed by impact and post-impact fire. The certificated commercial pilot, the sole occupant, received fatal injuries. Visual meteorological conditions prevailed. The flight originated from El Toro at 1341 hours.

An Operations Inspector, Federal Aviation Administration, Long Beach Flight Standards District Office, was present at the airshow. He reported that the pilot was to participate in a mock dog-fighting routine with the pilot's partner/operator flying another aircraft as a portion of the normally planned demonstration. The pilot of the second airplane did not feel well and canceled his participation in the demonstration. The pilot of the accident aircraft then planned to perform a solo aerobatic routine. The routine that the pilot began was not one that had been practiced.

At 1318 hours, Air Traffic Control personnel cleared the accident airplane to taxi to the runway in preparation for the aerial show. Ground personnel working with the pilot reported that as the airplane taxied out from parking, the pilot's shoulder harness was observed lying back behind the seat back and unsecured. At 1324 hours, while waiting for takeoff, the pilot made a radio request for assistance with the airplane's canopy from his ground crew. A witness reported observing the pilot leaning far forward in the seat of the airplane on the right side of the airplane. At 1325 hours, the pilot canceled any assistance from his ground crew. At 1341 hours, the pilot was cleared for takeoff on runway 34L.

After departure, the pilot performed a right 90 degree climbing turn, followed by a left 270 degree descending turn. This positioned the airplane over runway 16R at about 75 feet above ground level (AGL). The pilot then began a loop with an aileron roll at the top of the maneuver. Following the descent at the bottom portion of the loop maneuver, the airplane descended in a near nose and wing level attitude until striking runway 16R about mid-field. An intense explosion occurred. Wreckage was scattered along the runway for about 1/4 mile. No spectators were injured.

The operator reported that the loop maneuver in the accident airplane required a minimum of 275 knots at the entry point, and a minimum altitude of 4,000 feet above ground level (AGL) at 125 knots at the top of the maneuver. The operator indicated to FAA personnel that he observed the accident airplane's maneuver. He reported that it appeared to him that the accident airplane did not have the minimum entry speed. The operator estimated that the maximum altitude gained at the top of the maneuver was about 2,500 feet and the airplane appeared to experience an accelerated stall at 100 to 200 feet AGL just prior to impact. Additionally, the operator indicated that it was normal for the pilot to wear a "G" suit during his aerobatic routine.

Crew information

The pilot held a commercial pilot certificate with airplane single engine land and sea, airplane multiengine land (limited to VFR only), and instrument-airplane ratings. The most recent second class medical certificate was issued to the pilot on April 9, 1993, and contained no limitations. The pilot's airman records, maintained in the FAA's Airman and Records Center located in Oklahoma City, were reviewed by Safety Board investigators. The review noted that pilot was first issued a student pilot certificate on May 18, 1976, followed by a private pilot certificate on May 25, 1976. The pilot then received a commercial pilot certificate on July 21, 1976. The pilot held a letter of authorization (LOA) to act as pilot-in-command of North American F-86 Sabre Jets (All Models).

The operator reported that the pilot's formal aerobatic training was unknown. The pilot had owned and flown aerobatic aircraft in aerobatic flight in the past. The pilot received a checkout in the accident airplane on January 10, 1992, and the pilot completed all approved maneuvers by January 15, 1992. During 1992, the pilot did not fly any aerial demonstrations; however, he did practice the F-86 solo routine several times, down to ground level. In 1993, the pilot prepared for solo and dual air show routines by practicing in a Pitts S-2 and the accident airplane. The operator indicated that practice sessions exceeded 25 sequences.

The operator reported that the pilot portrayed himself as an ex-naval aviator and A-4 pilot. U.S. Naval Investigative Service (NIS) personnel assisted Safety Board investigators in an inquiry of the pilot's military experience. According to the NIS, the pilot was terminated from the U.S. Navy advanced jet training curriculum, Pensacola, Florida, on May 19, 1976.

Review of pilot logbook entries submitted by the operator revealed that the pilot's total aeronautical experience consisted of about 5,596.4 hours, of which 47 were accrued in the accident airplane. In the preceding 90 and 30 days prior to the accident, the logbook lists a total of 26.8 and 24.5 hours, respectively, flown in the accident airplane. On the last application for medical certificate, dated April 9, 1993, the pilot listed a total time of 6,200 hours, with 150 hours accrued in the preceding 6 months. The application did not have any entry for military experience.

Pilots participating in aerial demonstrations are required to demonstrate to the FAA their competency. The FAA utilizes air show professionals as Airshow Certification Evaluators (ACE) to evaluate other air show performers for the purpose of recommending a performer for aerobatic flight. The ACE program is administered by the International Council of Air Shows Inc. (ICAS). Evaluations and recommendations are forwarded to the FAA for review. The FAA is has the final authority to issue a Certificate of Acrobatic Competency, Form 8710-7. An FAA statement of acrobatic competency is valid for 1 year. An ACE has evaluation authority through ICAS Inc. that is valid for 2 years.

Safety Board investigators examined the evaluation records of the pilot and those of his last evaluator that are maintained by ICAS Inc. The pilot received an initial evaluation of acrobatic competency on September 19, 1991, by an ACE. The FAA issued a Form 8710-7 for solo and formation maneuvers in Pitts S-2 aircraft, with a level 2 (250 feet) altitude limitation to the pilot, with an expiration date of September 30, 1992. The evaluator indicated that the pilot's initial qualification at level 2 was based on the pilot's prior military low level and air-to-ground experience.

On October 19, 1992, the pilot applied for a statement of acrobatic competency with a level 1 (no restriction) altitude. The pilot was evaluated again by the same evaluator on January 4, January 18, and January 19, 1993, in a Pitts S-2 airplane. Additionally, the evaluator observed the pilot in formation flight in the F-86 with a MIG-15 on February 9, 1993. A review of the pilot's logbook indicated that the pilot logged flights in the Pitts on January 12 and January 18, 1993.

On February 24, 1993, the pilot was given an ACE acrobatic competency recommendation to the FAA with the following limitations: Maneuver limitations - solo/formation; Altitude limitations - Level 1, surface; Authorized aircraft - Pitts S-2, F-86 Sabre. A Level 1 authorization means that a performer may conduct aerobatic maneuvers down to the surface, not having any other altitude restriction for termination of a maneuver. On February 26, 1993, the FAA issued a statement of acrobatic competency (FAA Form 8710-7) to the pilot.

The pilot's evaluator submitted an applicatio

Aircraft

Registration
N3842J
Reported as
Canadair F-86E MK.6
Category
Airplane
Serial number
1480
Airframe hours
1,667
Engine
Orenda 10, 6,000 lbs thrust, turbo jet
Damage
Destroyed
Fire
On-Ground
Flight
Part 91
Operator
James A. Gregory
Registered owner
National Airshows Inc.
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · February 3, 1993 · 25 hours before
Departed
NZJ
Destination
NZJ
Airport
NZJ · Mcas El Toro, runway 16R, 6,311 × 250 ft, concrete

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
40
Certificate
Commercial
Airplane ratings
Single-engine land, Single-engine sea, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Center
Toxicology
Performed
Flight hours
5,596 total · 47 in this make and model · 27 in the last 90 days · 25 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
150° at 3 knots
Visibility
30 statute miles
Lowest ceiling
None
Temperature
77 °F, dew point 55 °F
Altimeter
29.00 inHg
Observed at
NZJ

FAA reports on this event · 1

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