Premium research interface

The modern interface for aviation safety intelligence.

Search investigations, review source evidence, monitor watched reports, and trace long-term patterns from one calm, data-first workspace.

63k+
Reports indexed
1940-2026
Coverage
Recent
Last data refresh
Featured Report

Loading…

Loading featured report…

Loading…
Open Report

Safety trends by operating rule

Track fatal and non-fatal accident patterns across Part 91, Part 135, and Part 121 operations.

Loading trend charts…

Browse the aviation graph

Move quickly by aircraft, airport, operator, and time with indexes built for research, not wandering.

Last Data Update

By Decade

By Month

Aircraft Manufacturer

More manufacturers

Airports

More airports

Operators

More operators

About

Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

The goal is practical safety education: make it faster to find relevant investigations, compare similar events, review factual records, and understand the evidence behind probable-cause and preliminary reports.

The investigative work and source records belong to the National Transportation Safety Board and the published investigation record. This site is not affiliated with or endorsed by the NTSB.

FAQs

NTSB Report

January 23, 1998 · Cessna 340A · N41NR

Groveland, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
January 23, 1998
Injury Outcomes
No injuries (2 uninjured)
Location
Groveland, CA
Aircraft
Cessna 340A
Tail Number
N41NR
Operator
Louis E Fricke
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX98LA081

The pilot stated that after touchdown the left brake failed. Examination of the aircraft revealed that flexible duct tubing was in close proximity to the aluminum brake line. The brake line showed evidence of corrosion, and the flexible duct tubing showed evidence of cracking. Further examination revealed that there would have been an insufficient amount of fluid in the left main landing gear brake system due to a leak, which would have restricted the operation of the left brake. The pilot reported that per the aircraft logbook, the brake lines had never been replaced. Documents from the manufacturer state that the pressurization system must be inspected every 200 hours or every year for plumbing condition, security, and loose connections. The brake system, per the manufacturer, must also be inspected every 200 hours or every year for leaks, hoses for bulges, and deterioration. The last annual maintenance performed included an inspection of the brake lines without removal of the structural sheet metal that overlies the pressurization system.

NTSB Probable Cause

Failure of the brake line as a result of inadequate maintenance.

Full Narrative

On January 22, 1998, at 1730 hours Pacific standard time, a Cessna 340A, N41NR, veered off runway 27 after landing, collapsed the nose gear, and struck a ditch at the Groveland, California, airport. The aircraft sustained substantial damage. The private pilot/owner, and passenger were not injured. Visual meteorological conditions existed for the personal flight that departed the Whiteman, California, airport at 1630. The flight was operated under 14 CFR Part 91, and no flight plan was filed. The pilot reported that on touchdown the left brake failed. He was unable to stop the aircraft on the runway, and it departed to the right. The nose wheel landing gear collapsed when the aircraft struck a soft shallow ditch. The pilot reported in an interview that the left brake line under the floor at the master cylinder ruptured where it was worn by adjacent pressurization system duct tubing. According to the pilot, and as per the aircraft logbook, the brake lines had never been replaced, and the aircraft had never been out of annual since 1978. The aircraft was examined on-scene by a Federal Aviation Administration (FAA) airworthiness inspector from the Fresno, California, Flight Standards District Office. According to the inspector, in the area beneath the floorboards where the brake line assembly in question is housed, a flexible duct tubing overlays the aluminum brake line. The examination revealed that the brake line showed evidence of corrosion. He reported that there would have been an insufficient amount of fluid in the left main landing gear brake system due to the leak, and would have restricted the operation of the left brake. A mechanic hired by the owner to repair the brake line reported that both brake lines showed evidence of corrosion. The duct tubing, a rubberized cloth, had been touching the lines and pitting approximately 1 inch of the aluminum brake line (picture appended to this file). There was also evidence of cracking in the duct tubing (picture appended to this file). The mechanic stated the corrective action taken was to replace the brake lines and rerouted the duct tubing so that it did not come into contact with the brake lines. Documents from the manufacturer state that the pressurization system needs to be inspected every 200 hours or every year for plumbing condition, security, and loose connections. The brake system, per the manufacturer, should also be inspected every 200 hours or every year for leaks, hoses for bulges, and deterioration. The mechanic who performed the last annual stated that he had complied with all of the Airworthiness Directives and no discrepancies were noted. He further reported that the brake lines were checked without moving any structural sheet metal, but that he did not note any anomalies. The mechanic stated that the aircraft was flown to Whiteman airport the day after the annual was completed with no malfunctions noted. The accident was reported to the Safety Board on January 29, 1998, following confirmation of substantial damage to the aircraft.

Flight

Event TypeAccident
Event Time17:30 PST
Nearest AirportPine Mountain Lake (0nm)
Runway27
Runway Length3625 ft
Runway Width50 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 340A
Tail NumberN41NR
Aircraft CategoryAir
DamageSubstantial
OperatorLouis E Fricke
Operating RulePart 91
Engines2
Engine TypeReciprocating
Engine DetailsContinental · TSIO-520-NB · Reciprocating · 325
Seats6

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 64 · Second Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data