Takeoff aborted because of takeoff warning horn.

Attributes
ACN	163595
Time
Date	199011
Day	Mon
Local Time Of Day	1201 To 1800
Place
Locale Reference	airport : grr
State Reference	MI
Altitude	agl bound lower : 0 agl bound upper : 0
Environment
Flight Conditions	VMC
Light	Daylight
Aircraft 1
Operator	common carrier : air carrier
Make Model Name	Medium Large Transport, Low Wing, 2 Turbojet Eng
Navigation In Use	Other Other
Flight Phase	climbout : takeoff other
Flight Plan	IFR
Person 1
Affiliation	company : air carrier
Function	flight crew : first officer
Qualification	pilot : cfi pilot : atp
Experience	flight time last 90 days : 150 flight time total : 11500 flight time type : 700
ASRS Report	163595
Person 2
Affiliation	company : air carrier
Function	flight crew : captain oversight : pic
Qualification	pilot : atp
Events
Anomaly	aircraft equipment problem : less severe
Independent Detector	aircraft equipment other aircraft equipment : unspecified
Resolutory Action	flight crew : rejected takeoff
Consequence	Other
Supplementary
Primary Problem	Aircraft
Air Traffic Incident	other

Narrative:

The aircraft was configured for a 5 degree flap takeoff with a stabilizer setting of 5.4. The stabilizer setting of 5.4 is close to the aft limit for takeoff. The rejected takeoff feature of the autobrake system was selected. Autothrottles were used for the takeoff which was a reduced thrust takeoff. The takeoff roll was normal until approximately 105 KTS when a takeoff confign warning sounded. The takeoff was rejected. The autobrake feature functioned normally. After we cleared the runway, it was determined that it was a false warning for stabilizer position. It is not unusual to get a stabilizer warning with the stabilizer trim indicators in the green takeoff band.

Original NASA ASRS Text

Title: TKOF ABORTED BECAUSE OF TKOF WARNING HORN.

Narrative: THE ACFT WAS CONFIGURED FOR A 5 DEG FLAP TKOF WITH A STABILIZER SETTING OF 5.4. THE STAB SETTING OF 5.4 IS CLOSE TO THE AFT LIMIT FOR TKOF. THE REJECTED TKOF FEATURE OF THE AUTOBRAKE SYS WAS SELECTED. AUTOTHROTTLES WERE USED FOR THE TKOF WHICH WAS A REDUCED THRUST TKOF. THE TKOF ROLL WAS NORMAL UNTIL APPROX 105 KTS WHEN A TKOF CONFIGN WARNING SOUNDED. THE TKOF WAS REJECTED. THE AUTOBRAKE FEATURE FUNCTIONED NORMALLY. AFTER WE CLRED THE RWY, IT WAS DETERMINED THAT IT WAS A FALSE WARNING FOR STABILIZER POS. IT IS NOT UNUSUAL TO GET A STAB WARNING WITH THE STAB TRIM INDICATORS IN THE GREEN TKOF BAND.

Data retrieved from NASA's ASRS site as of July 2007 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.