NYC86LA081

NTSB accident investigation · Dassault DA-10 · Coatsville, PA · February 28, 1986

Accident · Minor injuriesLimited investigationFinal report
Date
February 27, 1986, 22:30 local (Feb 28, 1986, 03:30 UTC)
Place
Coatsville, PA
Injuries
5 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N821LGDassault DA-10
Weather
Visual (VMC) · Night/dark
Status
Completed · report June 27, 1989
Report
Approved by Office Director
FAA report
19860227075739A
Case key
30305

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionCruise
Maintenance - inadequateOther maintenance personnelFactor
Electrical system,generator - wornCause
Electrical system,generator - failure,totalCause
Electrical system,battery - exhaustion
Electrical system - inoperative
Comm/nav equipment - inoperative
Flt control syst,stabilator trim - inoperative
Flight control,flap - inoperative
Landing gear,steering system - inoperative
Landing gear,anti-skid brake system - inoperative
Thrust reverser - inoperative
Loss of control - on ground/waterLanding - roll
Light condition - dark nightFactor
Performed
Precautionary landing - performed
Directional control - not maintainedPilot in commandFactor
Ground loop/swerve - uncontrolled
OverrunLanding - roll
Powerplant controls - improper use ofPilot in commandFactor
On ground/water collision with objectLanding - roll
On ground/water encounter with terrain/waterLanding - roll

Analysis

As the acft was climbing thru 19,000' at ngt, the #2 generator (gen) lgt came on. The flt crew noted there was no outputfm the #2 gen & it would not reset. They then checked the #1 gen voltage & noted it was 14 to 15 volts. The crew reducedthe elec load; however, about 5 min later, the batteries bcm discharged & there was a total loss of elec pwr. Using a flashlight, the crew diverted to the chester county arpt which had a 4600' rwy. The gear was extdd with the emerg sys. The elev trim was inop, so both plts applied back pressure on the yoke to overcome the nose dwn tendency. After lndg about 1/4 of the way dwn the rwy, the crew tried to use the thrust reversers, but the reversers were inop. Subsequently,the acft contd off the side & beyond the end of the rwy, hit a wooden beam & a snowbank, then came to rest in a ditch. An inv revealed a shaft failure of the #2 gen (starter/gen) & worn brushes in the #1 gen. With total elec failure, the flwg were also inop: wing flaps, anti-skid, capt's airspeed ind & altimeter, nosewheel steering, cockpit lighting.

Aircraft

Registration
N821LG
Reported as
Dassault DA-10
Category
Airplane
Serial number
170
Airframe hours
1,447
Engine
Airesearch TFE-731-2-1C, 3,230 lbs thrust, turbo fan
Damage
Substantial damage
Flight
Executive/Corporate · Part 91
Registered owner
Seneca Livestock Co.
Airworthiness certificate
Standard, Normal
Last inspection
Continuous airworthiness · January 10, 1986 · 46 hours before
Departed
JFK · New York, NY
Destination
LEX · Lexington, KY
Flight plan
IFR
Airport
40N · Chester County, runway 29, 4,600 × 100 ft, asphalt

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
39
Certificate
Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
8,260 total · 963 in this make and model · 8,021 as pilot in command · 89 in the last 90 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Night/dark
Wind
Calm
Lowest ceiling
None

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.