3701
2004-OCT-14 · Jefferson City, Missouri, United States

Pinnacle Airlines — Flight 3701

A Pinnacle Airlines CRJ-200 crashed into a residential area after both engines flamed out at the aircraft's service ceiling of 41,000 feet. The repositioning flight, carrying only two pilots, was conducted with extreme and unprofessional maneuvers as the crew attempted to join the informal 410 club by reaching the aircraft's maximum altitude. During the climb, the crew used an improper vertical speed mode that allowed airspeed to decay significantly. Upon reaching 41,000 feet, the aircraft entered an aerodynamic stall; the pilots repeatedly overrode the automatic stick pusher, leading to a dual engine flameout. The engines then suffered a core lock condition, preventing a restart, and the crew failed to glide to several available airports in a timely manner.

Aircraft
Bombardier CRJ-200LR
Registration
N8396A
Phase
Cause
Souls on Board
2
Fatalities
2
Origin → Dest
Little Rock National Airport, Arkansas → Minneapolis-St. Paul International Airport, Minnesota
Report

Investigation Summary

The investigation revealed a total breakdown of professional standards during the Part 91 ferry flight. Shortly after takeoff, the crew performed high-G zoom climbs and rudder swings. At approximately 15,000 feet, the pilots switched seats, with Captain Rhodes moving to the right (First Officer's) seat and First Officer Cesarz moving to the left (Captain's) seat to fly the aircraft. As they approached 41,000 feet, they failed to maintain the required minimum climb speed of 250 knots, allowing it to drop to 163 knots. This placed the aircraft on the back side of the power curve, where the thin air at high altitude provided insufficient thrust to recover speed without losing altitude. When the aircraft stalled, the crew's reflexive attempts to maintain altitude by pulling back on the yoke overrode the stick pusher three times, causing the engines to ingest turbulent air and flame out. During the subsequent descent, the crew failed to maintain the 300-knot airspeed required for a windmill restart. This allowed the engine components to cool and contract at different rates, leading to a core lock where the high-pressure turbines could no longer rotate. The crew also delayed reporting the dual engine failure to Air Traffic Control for 14 minutes, by which time they had glided past several suitable emergency landing sites.

Final Conclusions

The NTSB determined the probable causes were the pilots' unprofessional behavior, deviation from standard operating procedures, and poor airmanship, which resulted in an unrecoverable in-flight emergency. Contributing factors included the pilots' failure to prepare for an emergency landing in a timely manner and improper management of the double engine failure checklist, which allowed the engine cores to stop rotating and resulted in core lock. The NTSB also cited inadequate training in high-altitude stalls and the failure of flight manuals to emphasize minimum airspeeds for engine rotation.

Video Analysis

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Airframe & Maintenance

Airframe Hours
10,168
Cycles
9,613
Engines
General Electric CF34-3B1

Crew Experience

Captain

Total hours
6,900
On type
973

Jesse Rhodes, age 31

First Officer

Total hours
761
On type
222

Peter Cesarz, age 23

Systems & Failure Modes

i

Stick Pusher

An automated system designed to push the control column forward to lower the nose and reduce the angle of attack when a stall is imminent.

i

CF34-3B1 Turbofan Engines

The aircraft's powerplants, which suffered a dual flameout and subsequent core lock after the crew failed to maintain sufficient airspeed for a windmill restart.

i

Flight Data Recorder (FDR)

Recorded the crew's aggressive maneuvers, including zoom climbs and rudder swings, as well as the improper vertical speed mode used during the final climb.

Interesting Facts

  • 01The flight was a non-revenue repositioning flight with no passengers on board.
  • 02The crew attempted to reach 41,000 feet to join the '410 club,' an informal group of pilots who had flown the CRJ-200 to its service ceiling.
  • 03The pilots switched seats during the climb, with the First Officer moving to the Captain's seat.
  • 04Both engines suffered 'core lock,' a condition where internal components seize due to thermal contraction, making a restart impossible.
  • 05The crew overrode the automatic stick pusher three times during the high-altitude stall.

Safety Actions & Advisories

Altitude Restrictions

Pinnacle Airlines restricted all CRJ-200 flights to a maximum altitude of 37,000 feet following the accident.

Training Enhancements

The airline incorporated high-altitude stall recovery and dual engine failure scenarios into simulator training.

Checklist Revisions

Revised dual engine failure checklists were issued to emphasize the 240-knot minimum airspeed for restart and the necessity of pitching down to reach 300 knots.

Safety Monitoring Programs

Pinnacle adopted a traditional Flight Operational Quality Assurance (FOQA) program and instituted an Aviation Safety Action Program (ASAP) into its operations.

Known Controversies & Unanswered Questions

The 410 Club Culture

Reference ↗

The investigation highlighted a subculture at Pinnacle Airlines where pilots on non-revenue ferry flights would attempt to reach the aircraft's service ceiling of 41,000 feet for personal prestige, often involving unprofessional maneuvers.

Darwin Awards Recognition

Reference ↗

The crew was posthumously awarded the 2004 Darwin Awards, a satirical honor for those who die through their own 'idiotic' actions, reflecting the public and industry backlash against the extreme lack of professionalism displayed.

Location

Jefferson City, Missouri, United States · 38.5492, -92.1433

Case File History

  1. CorrectionUpdated investigation summary and event timeline.
  2. CorrectionUpdated investigation summary, safety actions and open questions.

Related Cases

Case ID · pinnacle-3701-2004Last updated · Filed

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