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|
Attributes | |
ACN | 410107 |
Time | |
Date | 199808 |
Day | Wed |
Local Time Of Day | 0001 To 0600 |
Place | |
Locale Reference | airport : zzz |
State Reference | US |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Light | Night |
Aircraft 1 | |
Controlling Facilities | tower : mke |
Operator | common carrier : air carrier |
Make Model Name | B737-300 |
Operating Under FAR Part | Part 121 |
Navigation In Use | Other Other |
Flight Phase | ground other : taxi other |
Flight Plan | None |
Person 1 | |
Affiliation | company : air carrier |
Function | other personnel other |
Qualification | other other : other |
ASRS Report | 410107 |
Person 2 | |
Affiliation | company : air carrier |
Function | other personnel other |
Qualification | other other : other |
ASRS Report | 410303 |
Events | |
Anomaly | other anomaly other anomaly other other anomaly other |
Independent Detector | other other : unspecified |
Resolutory Action | none taken : unable |
Consequence | Other |
Supplementary | |
Air Traffic Incident | other |
Narrative:
I was assigned right seat duty for an engine high power run following a variable stator vane rig adjustment. The high power procedure involves a turbine case clearance deactivation procedure which involves a short 3 second acceleration to 92% N2 followed by return to idle power setting. On taxi-out the #1 engine was throttled up, #2 engine at idle. As the left engine approached 80% N1, the airplane nose gear skidded to the right of taxiway centerline. Brakes were applied but control was not recovered. The nose gear left the taxiway and onto the grass. After aircraft recovery, nose tires were changed, nose gear was washed, lubed and gear swing accomplished. Inspection found no damage. Contributing factors were the aircraft's light fuel load and the forward momentum already established during taxi-out. In retrospect, the aircraft should have been stopped with parking brake set. A heavier fuel load would also help in holding the aircraft under full braking. Supplemental information from acn 410303: at about 80% N1, the airplane swerved to the right. Brake pedals were fully depressed, nose landing gear steering was full left. Power was brought back to idle. Within 3 seconds the airplane had left the taxiway centerline and the nose landing gear had stopped 15 ft into the grass. I should have fully stopped airplane before starting the takeoff power run. I've been taxiing B737's since 1989 and thought the brakes were stronger than the engines. More weight would have kept the wheels from skidding with the brakes locked. A 2 engine power run, both to takeoff power requires 20000 pounds of fuel. We had less than 7000 pounds, so I knew better than to have 2 engines at high power. I taxi everything air carrier has at ZZZ overnight, sure learned a lot from my 3 second ride. Maybe doing the run A320 style, with 75% power on the 'non-tested' engine and 95% on the 'testing' engine would have kept me on a straight slide down the taxiway. I didn't have enough weight to feel good about doing that.
Original NASA ASRS Text
Title: A B737-300 ON TAXI OUT FOR MAINT ENG RUN EXITED THE TXWY DUE TO HIGH PWR APPLIED TO THE #1 ENG WITH THE #2 ENG AT IDLE.
Narrative: I WAS ASSIGNED R SEAT DUTY FOR AN ENG HIGH PWR RUN FOLLOWING A VARIABLE STATOR VANE RIG ADJUSTMENT. THE HIGH PWR PROC INVOLVES A TURBINE CASE CLRNC DEACTIVATION PROC WHICH INVOLVES A SHORT 3 SECOND ACCELERATION TO 92% N2 FOLLOWED BY RETURN TO IDLE PWR SETTING. ON TAXI-OUT THE #1 ENG WAS THROTTLED UP, #2 ENG AT IDLE. AS THE L ENG APCHED 80% N1, THE AIRPLANE NOSE GEAR SKIDDED TO THE R OF TXWY CTRLINE. BRAKES WERE APPLIED BUT CTL WAS NOT RECOVERED. THE NOSE GEAR LEFT THE TXWY AND ONTO THE GRASS. AFTER ACFT RECOVERY, NOSE TIRES WERE CHANGED, NOSE GEAR WAS WASHED, LUBED AND GEAR SWING ACCOMPLISHED. INSPECTION FOUND NO DAMAGE. CONTRIBUTING FACTORS WERE THE ACFT'S LIGHT FUEL LOAD AND THE FORWARD MOMENTUM ALREADY ESTABLISHED DURING TAXI-OUT. IN RETROSPECT, THE ACFT SHOULD HAVE BEEN STOPPED WITH PARKING BRAKE SET. A HEAVIER FUEL LOAD WOULD ALSO HELP IN HOLDING THE ACFT UNDER FULL BRAKING. SUPPLEMENTAL INFO FROM ACN 410303: AT ABOUT 80% N1, THE AIRPLANE SWERVED TO THE R. BRAKE PEDALS WERE FULLY DEPRESSED, NOSE LNDG GEAR STEERING WAS FULL L. PWR WAS BROUGHT BACK TO IDLE. WITHIN 3 SECONDS THE AIRPLANE HAD LEFT THE TXWY CTRLINE AND THE NOSE LNDG GEAR HAD STOPPED 15 FT INTO THE GRASS. I SHOULD HAVE FULLY STOPPED AIRPLANE BEFORE STARTING THE TKOF PWR RUN. I'VE BEEN TAXIING B737'S SINCE 1989 AND THOUGHT THE BRAKES WERE STRONGER THAN THE ENGS. MORE WT WOULD HAVE KEPT THE WHEELS FROM SKIDDING WITH THE BRAKES LOCKED. A 2 ENG PWR RUN, BOTH TO TKOF PWR REQUIRES 20000 LBS OF FUEL. WE HAD LESS THAN 7000 LBS, SO I KNEW BETTER THAN TO HAVE 2 ENGS AT HIGH PWR. I TAXI EVERYTHING ACR HAS AT ZZZ OVERNIGHT, SURE LEARNED A LOT FROM MY 3 SECOND RIDE. MAYBE DOING THE RUN A320 STYLE, WITH 75% PWR ON THE 'NON-TESTED' ENG AND 95% ON THE 'TESTING' ENG WOULD HAVE KEPT ME ON A STRAIGHT SLIDE DOWN THE TXWY. I DIDN'T HAVE ENOUGH WT TO FEEL GOOD ABOUT DOING THAT.
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.