Miami - Orlando

During landing roll, the airplanes normal braking system failed as a result of hydraulic fluid leak(s). At the pilot's request, deployment of the drag chute and application of the emergency braking system was performed by the first officer. According to the first officer, application of the emergency brakes caused the airplane to yaw. The first officer then pulled up on the emergency brakes handle followed by re-application of braking pressure. This action took place several times during the landing roll. Gates' Learjet Flight Training Manual (Page 105) states, 'In using the emergency brake lever, slow steady downward pressure is required. Each time the lever is allowed to return upward to the normal position, nitrogen is evacuated overboard. Brace your hand so you will not allow the lever to move up and down inadvertently on a bumpy runway.' The airplane overran the end of the runway and collided with the Instrument Landing System back course antennae.

Flight / Schedule

Miami - Orlando

Aircraft

Learjet 24

Registration

N100DL

MSN

24-201

Year of Manufacture

1969

Date

May 23, 1998 at 03:30 AM

Type

CRASH

Flight Type

Ambulance

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Orlando-Intl Florida

Region

North America • United States of America

Coordinates

28.7760°, -81.2412°

Crash Cause

Human factor

Narrative Report

On May 23, 1998 at 03:30 AM, Miami - Orlando experienced a crash involving Learjet 24, operated by Panther Aviation, with the event recorded near Orlando-Intl Florida.

The flight was categorized as ambulance and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.

6 people were known to be on board, 0 fatalities were recorded, 6 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.

Crew on board: 2, crew fatalities: 0, passengers on board: 4, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is human factor. During landing roll, the airplanes normal braking system failed as a result of hydraulic fluid leak(s). At the pilot's request, deployment of the drag chute and application of the emergency braking system was performed by the first officer. According to the first officer, application of the emergency brakes caused the airplane to yaw. The first officer then pulled up on the emergency brakes handle followed by re-application of braking pressure. This action took place several times during the landing roll. Gates' Learjet Flight Training Manual (Page 105) states, 'In using the emergency brake lever, slow steady downward pressure is required. Each time the lever is allowed to return upward to the normal position, nitrogen is evacuated overboard. Brace your hand so you will not allow the lever to move up and down inadvertently on a bumpy runway.' The airplane overran the end of the runway and collided with the Instrument Landing System back course antennae.

Aircraft reference details include registration N100DL, MSN 24-201, year of manufacture 1969.

Geospatial coordinates for this crash are approximately 28.7760°, -81.2412°.

Fatalities

Total

0

Crew

0

Passengers

0

Other

0

Crash Summary

During landing roll, the airplanes normal braking system failed as a result of hydraulic fluid leak(s). At the pilot's request, deployment of the drag chute and application of the emergency braking system was performed by the first officer. According to the first officer, application of the emergency brakes caused the airplane to yaw. The first officer then pulled up on the emergency brakes handle followed by re-application of braking pressure. This action took place several times during the landing roll. Gates' Learjet Flight Training Manual (Page 105) states, 'In using the emergency brake lever, slow steady downward pressure is required. Each time the lever is allowed to return upward to the normal position, nitrogen is evacuated overboard. Brace your hand so you will not allow the lever to move up and down inadvertently on a bumpy runway.' The airplane overran the end of the runway and collided with the Instrument Landing System back course antennae.

Cause: Human factor

Occupants & Outcome

Crew On Board

2

Passengers On Board

4

Estimated Survivors

6

Fatality Rate

0.0%

Known people on board: 6

Operational Details

Schedule / Flight

Miami - Orlando

Flight Type

Ambulance

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Region / Country

North America • United States of America

Aircraft Details

Aircraft

Learjet 24

Registration

N100DL

MSN

24-201

Year of Manufacture

1969