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LAX99FA106 · Cessna 172N

19 Feb 1999 · El Monte, CA, United States

Cessna 172N · Accident: fire en route

From Van Nuys Airport (VNY) to an unrecorded destination

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Event

NTSB case
LAX99FA106
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
0 · all aircraft and ground
Ground fatalities
0
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Cessna 172N

Aircraft type
Cessna 172
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N5174D
Operator
Unknown
Onboard fatalities
Unknown
Route
From Van Nuys Airport (VNY), Van Nuys, CATo not recorded
Aircraft age
Not recorded
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
En route · cruise
First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Fire
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Cause areas

  • Electrical system, electric switch › Arcing
  • Fuel system, line › Penetrated
  • Manufacturer › Acft/equip, inadequate design

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

A factory installed map light and it's switch were mounted midway down the left doorpost. About 1/2-mile from the airport, a passenger grabbed the left forward doorpost with her hand for support and a 'pop' noise was heard. Immediately, flames shot out from both sides of the plastic doorpost cover at the map light's level and black smoke filled the cockpit. The pilot tried to smother the fire, but each time the flames came back and seemed to grow more intense. An emergency downwind landing was made on runway 1 as the flames completely involved the cockpits left side. The cabin was destroyed in the ground fire. It was unclear if AD 80-04-08 was complied with following its issuance on February 16, 1980. The AD was due to instances of fuel leaks and/or in-flight fires resulting from contact between the map light switch terminals and an adjacent fuel line. The AD required a one-time visual inspection of the left doorpost area to ensure that the switch and the fuel line were at least 0.50-inch apart. It also required the installation of an insulator cover over the map switch electrical terminals. Due to a pilot squawk, a mechanic had repaired the map light the day before the accident. He found a loose wire and reconnected it to the switch. In questioning, the mechanic first said that there was nothing between the switch and the fuel line, then stated during a second interview that after review of the AD and parts manual diagrams, he definitely had reinstalled the insulator cover over the switch terminals. Review of the 172's design history revealed that models prior to the 172N had only one fuel supply line from each tank that were routed down the aft doorpost. Map lights installed prior to the 172N were located at the top of the doorpost in an area with more internal clearance. With the 172N model change, a second fuel feed line was added from each tank and routed down the forward doorpost in the channel with the wire bundles and the map light switch, with nylon spacers added to physically separate the wires from the fuel line. Also, the map light and switch were moved to their present locations. The only flammable components in the doorpost are the wire insulation, the nylon spacers, the plastic doorpost covering, and, the fuel in the fuel line (0.75 psi head pressure at the map light level). No evidence of electrical shorts in the doorpost circuits or flammable fluid leaks external to the doorpost, which would account for the ignition and severity of the doorpost fire, were found during the investigation. Three accidents were found in NTSB accident records where fires originated in the left forward doorpost; all three aircraft were Cessna 172N's. The SDR data base had three instances (only 172N's) where electrical arcs from the map light switch had punctured the fuel line in the left forward doorpost and caused an in-flight fuel leak. Other SDR's documented over 12 instances where electrical wires had chaffed into the fuel lines in either the left or right forward doorpost areas. Examination of two exemplar Cessna 172N's revealed that the internal configuration of the doorpost components were not in conformance to original drawing specifications due to interior replacements and repairs over the years.

Probable cause

An in-flight fuel fire in the left forward doorpost due to an electrical arc from an adjacent map light switch puncturing a main fuel feed line. The manufacturer's inadequate design in routing the fuel line in close proximity to electrical arc sources in the doorpost is causal. A factor in the accident is the probable failure of the doorpost internal component configuration to conform to original design specifications due to aircraft aging issues.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record LAX99FA106
Event ID
20001205X00181
Case number
LAX99FA106
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: local date, investigation status. Values present in the bulk record are kept.
  • The date is the local date; the NTSB stores the UTC date 1999-02-20.
  • API snapshot SHA-256: 1d9d7ad03f92336c6311ac06ef148cb157f344c61fa4fe496d0581f3fd3db4d5; retrieved 2026-09-21T20:36:09.801Z.