Lockheed L-1329 N787WB
27 November 1998 · Austin, Texas, United States · No injuries
Summary
On 27 November 1998 at about 20:05 local time, a Lockheed L-1329 registered N787WB was involved in an accident near Austin, Texas, United States. 3 people were on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.
The record
- Date
- at 20:05
- Classification
- Accident
- Location
- Austin, Texas, United States
- Nearest airport
- Robert Mueller Municipal (AUS)
- Coordinates
- 30.2993, -97.6893
- Aircraft
- Lockheed L-1329
- Registration
- N787WB
- Category
- Airplane
- Engines
- 4
- Operator
- Not recorded
- Operating rule
- Part 91: General Aviation
- Purpose of flight
- Business
- Phase of flight
- Not recorded
- Route
- Houston → Unknown
- Aircraft damage
- Substantial
- Weather
- VMC
- Light
- Night/Dark
- NTSB number
- FTW99LA045
People
Nobody was injured.
| On board | Died | Serious | Minor | Uninjured |
|---|---|---|---|---|
| 3 | 0 | 0 | 0 | 3 |
Probable cause
The steering actuator fatigue failure resulting from inadequate procedure documentation for the manufacturing process.
Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.
Read the full NTSB narrative
During the landing roll, the nose gear settled onto the runway, and the aircraft veered hard to the right. Application of the left brake had no effect. The airplane skidded, exited the runway, struck a runway marker, and collapsed the nose landing gear. The steering actuator had failed, the hydraulic fluid was lost from the steering actuator, and the fuselage received structural damage. The steering actuator assembly, p/n 1501-4, had accumulated 5,938.0 hours since new and had not been repaired or overhauled. Examination of the nose gear steering actuator cylinder by the metallurgist revealed that the cylinder fracture was the result of fatigue cracking initiated by an abrupt machining transition from the 45 degree thread ring chamfer to the straight wall of the cylinder. The engineering drawings appear to depict the radius at the fatigue origin as a continuation of the 0.03 inch to 0.06 inch radius adjacent to the fracture. However, the drawing is not clear on the specific intent of the transition between the nearby radius and the internal threads for the nut.
Quoted verbatim from the NTSB record.
Other Lockheed L-1329 accidents
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 22 Jan 1979 | Lockheed L-1329 | Concord, New Hampshire, United States | Bowater Incorp | Minor injuries | - |
Other accidents in this area
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 9 Jan 1998 | Beechcraft V35 | Seguin, Texas, United States | - | Minor injuries | - |
| 14 Jan 1998 | Poling KELEHER LARK KR1B | Georgetown, Texas, United States | - | Fatal | 1 |
| 24 Jan 1998 | Cessna 140A | Justin, Texas, United States | - | No injuries | - |
| 24 Jul 1998 | Bell 206L-3 | Reklaw, Texas, United States | U.s. Forest Service | Minor injuries | - |
| 29 Aug 1998 | Jodel F11-3 | Beeville, Texas, United States | - | Fatal | 2 |
| 29 Aug 1998 | Piper PA-28-235 | Mineola, Texas, United States | - | No injuries | - |