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NTSB Report

February 24, 2003 · Cessna 172RG · N5177R

Sanford, FL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
February 24, 2003
Injury Outcomes
2 injuries (2 minor injuries)
Location
Sanford, FL
Aircraft
Cessna 172RG
Tail Number
N5177R
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
MIA03LA070

Before the flight departed, hydraulic fluid was added to the landing gear hydraulic system. The certified flight instructor (CFI) reported that after takeoff the landing gear retracted without incident. The flight proceeded to the practice area where airwork was performed. The flight continued and when the landing gear was extended prior to performing additional airwork, it failed to extend. The emergency checklist was followed but failed to extend the landing gear. The flight returned to the departure airport and the flight crew contacted dispatch in an attempt to lower the landing gear which was unsuccessful. Additionally, the CFI attempted to manually extend the main landing gear but was unable. The flight returned for landing and with the nose landing gear extended and the main landing gear in trail, the main landing gear collapsed at touchdown. Examination of the airplane by an FAA Airworthiness inspector revealed the hand pump suction line assembly part number 2480001-23, was damaged. Hydraulic fluid covered the area. The line was retained for further examination. The damaged line was examined by the NTSB Materials Laboratory. Examination of the line revealed at least 8 transverse cuts in the tube section of the line adjacent to the end ferrule. A cut directly adjacent to the end ferrule penetrated the wall thickness and was slightly less than .03 inch wide. The sides of that cut were straight into the tube but the bottom of the cut had a curved surface progressing to a sharp bottom. The other cuts did not penetrate the wall thickness, and loss of metal at the cut locations appeared to be primarily from metal flow as opposed to being from grinding or cutting away material. There was no evidence that the edges of the ferrule or B-nut created the cuts in the tubing.

NTSB Probable Cause

The intentional cutting of the hydraulic line by an unknown person resulting in the loss of hydraulic fluid and the inability of the pilot-in-command to extend and lock the main landing gear, and subsequent collapse of the main landing gear after touchdown.

Full Narrative

On February 24, 2003, about 1432 eastern standard time, a Cessna 172RG, N5177R, registered to and operated by Comair Aviation Academy, experienced collapse of the main landing gear during the landing roll at the Orlando Sanford Airport, Sanford, Florida. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR Part 91 instructional flight. The airplane was substantially damaged and the certified flight instructor (CFI) and pilot-rated student sustained minor injuries. The flight originated at 1130 from the Orlando Sanford Airport. Before the flight departed, hydraulic fluid was added to the landing gear hydraulic system. The CFI reported that after takeoff the landing gear retracted without incident. The flight proceeded to the practice area where airwork was performed. The flight continued and when the landing gear was extended prior to performing additional airwork, it failed to extend. The emergency checklist was followed but failed to extend the landing gear. The flight returned to the departure airport and the flight crew contacted dispatch in an attempt to lower the landing gear which was unsuccessful. Additionally, the CFI attempted to manually extend the main landing gear but was unable. The flight returned for landing and with the nose landing gear extended and the main landing gear in trail, the main landing gear collapsed at touchdown. Examination of the airplane by an FAA airworthiness inspector revealed the hand pump suction line assembly part number 2480001-23, was damaged. Hydraulic fluid covered the area. The line was retained for further examination. The damaged line was examined by the NTSB Materials Laboratory located in Washington, D.C. Examination of the line revealed at least eight transverse cuts in the tube section of the line adjacent to the end ferrule. A cut directly adjacent to the end ferrule penetrated the wall thickness and was slightly less than .03 inch wide. The sides of that cut were straight into the tube but the bottom of the cut had a curved surface progressing to a sharp bottom. The other cuts did not penetrate the wall thickness, and loss of metal at the cut locations appeared to be primarily from metal flow as opposed to being from grinding or cutting away material. There was no evidence that the edges of the ferrule or B-nut created the cuts in the tubing. The airplane minus the retained hand pump suction line was released to John McGann of Comair Aviation Academy, on March 10, 2003. The retained line was released to Jose Lema, of the Federal Bureau of Investigation, Maitland, Florida, on March 29, 2004.

Flight

Event TypeAccident
Event Time14:32 EST
Nearest AirportOrlando Sanford (0nm)
Runway9L
Runway Length9600 ft
Runway Width150 ft
Flight Plan FiledCvfr
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 172RG
Tail NumberN5177R
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360-F1A6 · Reciprocating · 180
Seats4

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 24 · First Class · Minor
Crew 2Age 20 · First Class · Minor

Conditions

ConditionsVMC
LightDaylight
Wind110° @ 9 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point54
Altimeter30.19 inHg
Observation Time19:39
Weather SourceWFAC

Appendix: Source Data