Dassault DA-900B N523AC
9 October 1999 · Holland, Michigan, United States · Serious injuries
Summary
On 9 October 1999 at about 19:10 local time, a Dassault DA-900B registered N523AC was involved in an accident near Holland, Michigan, United States. 5 people were on board and one was seriously injured. The aircraft was slightly damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.
The record
- Date
- at 19:10
- Classification
- Accident
- Location
- Holland, Michigan, United States
- Coordinates
- 42.7703, -86.1002
- Aircraft
- Dassault DA-900B
- Registration
- N523AC
- Category
- Airplane
- Engines
- 3
- Operator
- Not recorded
- Operating rule
- Part 91: General Aviation
- Purpose of flight
- Executive/Corporate
- Phase of flight
- Not recorded
- Route
- Portland → Grand Rapids
- Aircraft damage
- Minor
- Weather
- VMC
- Light
- Day
- NTSB number
- CHI00FA006
People
1 person was seriously injured.
| On board | Died | Serious | Minor | Uninjured |
|---|---|---|---|---|
| 5 | 0 | 1 | 0 | 4 |
Probable cause
The copilot's improper use of the autopilot system while leveling the flight from descent, resulting in an inadvertent pilot-induced pitch oscillation of the airplane. A factor was the flight attendant not wearing a seat belt at the time of the occurrence.
Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.
Read the full NTSB narrative
The flight experienced a series of pitch oscillations while on descent to an assigned altitude of 11,000 feet mean sea level(msl). The flight attendant was seriously injured. The Captain reported that when he was at about 11,400 feet msl, it appeared the airplane was going to descend below the assigned altitude. The First Officer, who was the flying pilot in the left seat, reported that he pulled back on the airplane's yoke to initiate the level off without disengaging the autopilot. He reported that when he relaxed the back pressure on the yoke, the airplane pitched nose down violently and a series of three to four pitch oscillations occurred before the airplane was brought under control. The aircraft load factors reached magnitudes between +3.3g and -1.2 g. The flight attendant was not wearing a seat belt at the time of the incident. The inspection of the airplane revealed no pre-existing anomalies. Neither the autopilot's pilot manual nor the airplane's flight manual contained a Warning, Caution, or Note that explicitly stated not to manually override the autopilot. On October 18, 1999, Falcon Aviation issued Newsflash 52 that notified operators not to manually apply control yoke forces in an attempt to control the aircraft when the autopilot is engaged.
Quoted verbatim from the NTSB record.
Other accidents in this area
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 20 Mar 1999 | Delong GLASTAR GS-1 | Lapeer, Michigan, United States | - | No injuries | - |
| 22 Jan 1999 | Beechcraft 95-C55 | Pellston, Michigan, United States | - | Fatal | 3 |
| 13 Aug 1999 | Piper PA-28-181 | Paw Paw, Michigan, United States | National Flyers Association | Fatal | 4 |
| 16 Aug 1999 | Cessna 150G | Lambertville, Michigan, United States | - | Minor injuries | - |
| 19 Jan 1999 | Cessna 150F | Hillsdale, Michigan, United States | - | No injuries | - |
| 17 Aug 1999 | Piper PA-28-180 | Harsens Island, Michigan, United States | - | No injuries | - |