37000 Feet | Browse and search NASA's Aviation Safety Reporting System |
|
Attributes | |
ACN | 248705 |
Time | |
Date | 199308 |
Day | Tue |
Local Time Of Day | 1801 To 2400 |
Place | |
Locale Reference | airport : hnl |
State Reference | HI |
Altitude | agl bound lower : 0 agl bound upper : 800 |
Environment | |
Flight Conditions | VMC |
Light | Night |
Aircraft 1 | |
Controlling Facilities | tower : hnl tower : sdf |
Operator | common carrier : air taxi |
Make Model Name | Small Transport |
Flight Phase | climbout : initial climbout : takeoff other |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air taxi |
Function | flight crew : single pilot |
Qualification | pilot : instrument pilot : commercial pilot : atp pilot : flight engineer |
Experience | flight time last 90 days : 50 flight time total : 5325 flight time type : 215 |
ASRS Report | 248705 |
Person 2 | |
Affiliation | government : faa |
Function | controller : local |
Events | |
Anomaly | aircraft equipment problem : critical |
Independent Detector | aircraft equipment other aircraft equipment : unspecified other flight crewa |
Resolutory Action | flight crew : overcame equipment problem other |
Consequence | Other |
Supplementary | |
Primary Problem | Aircraft |
Air Traffic Incident | other |
Narrative:
Soon after taking off from hnl as I passed through approximately 250 ft AGL, I noticed my airspeed began to decrease. Both engines were developing full power and at this weight the aircraft would normally be climbing at about 1200 FPM. I also noticed that my rate of climb was also decreasing. As I pushed the nose over to gain airspeed, the airspeed indicator displayed a continuing decrease from approximately 120 KIAS to approximately 80 KIAS. As the airspeed decreased through about 90 KIAS, I began to realize that there was probably a problem with the airspeed indicator. At this point I advised hnl tower that I would need to return for landing. I then made a right hand turn to enter the downwind leg of the traffic pattern to runway 4R in hnl. At this point, I also noticed that my altimeter did not appear to be displaying the proper altitude, as it was only showing approximately 300 ft and I estimated the aircraft's altitude to be approximately 800-900 ft. As I returned for landing, the airspeed indicator showed an increase to approximately 120 KIAS and stayed there until I landed and began my taxi off of the runway. After clearing the runway, it took about 1 min for the airspeed indicator to decrease to '0' KIAS. The apparent cause of the problem was the aircraft's static pressure system drain valve was partially open. In the pressurized cabin this produced erroneous indications to the static system instruments (airspeed indicator, altimeter, rate of climb indicator). This valve is located on the side of the aircraft within about 3 inches of the pilot's left knee while sitting. Since the valve is very easy to move, I believe I may have hit it with my knee as I sat down. To prevent any future occurrence of this, I will always check this valve after I am in my seat to ensure that it is completely shut. I also believe it should be harder to turn it to prevent it from being moved inadvertently. Also possible consideration may need to be given to moving the drain valve to another location on future aircraft.
Original NASA ASRS Text
Title: AN ATX AMB ACFT TOOK OFF WITH ITS STATIC DRAIN LINE PARTIALLY OPEN.
Narrative: SOON AFTER TAKING OFF FROM HNL AS I PASSED THROUGH APPROX 250 FT AGL, I NOTICED MY AIRSPD BEGAN TO DECREASE. BOTH ENGS WERE DEVELOPING FULL PWR AND AT THIS WT THE ACFT WOULD NORMALLY BE CLBING AT ABOUT 1200 FPM. I ALSO NOTICED THAT MY RATE OF CLB WAS ALSO DECREASING. AS I PUSHED THE NOSE OVER TO GAIN AIRSPD, THE AIRSPD INDICATOR DISPLAYED A CONTINUING DECREASE FROM APPROX 120 KIAS TO APPROX 80 KIAS. AS THE AIRSPD DECREASED THROUGH ABOUT 90 KIAS, I BEGAN TO REALIZE THAT THERE WAS PROBABLY A PROB WITH THE AIRSPD INDICATOR. AT THIS POINT I ADVISED HNL TWR THAT I WOULD NEED TO RETURN FOR LNDG. I THEN MADE A R HAND TURN TO ENTER THE DOWNWIND LEG OF THE TFC PATTERN TO RWY 4R IN HNL. AT THIS POINT, I ALSO NOTICED THAT MY ALTIMETER DID NOT APPEAR TO BE DISPLAYING THE PROPER ALT, AS IT WAS ONLY SHOWING APPROX 300 FT AND I ESTIMATED THE ACFT'S ALT TO BE APPROX 800-900 FT. AS I RETURNED FOR LNDG, THE AIRSPD INDICATOR SHOWED AN INCREASE TO APPROX 120 KIAS AND STAYED THERE UNTIL I LANDED AND BEGAN MY TAXI OFF OF THE RWY. AFTER CLRING THE RWY, IT TOOK ABOUT 1 MIN FOR THE AIRSPD INDICATOR TO DECREASE TO '0' KIAS. THE APPARENT CAUSE OF THE PROB WAS THE ACFT'S STATIC PRESSURE SYS DRAIN VALVE WAS PARTIALLY OPEN. IN THE PRESSURIZED CABIN THIS PRODUCED ERRONEOUS INDICATIONS TO THE STATIC SYS INSTS (AIRSPD INDICATOR, ALTIMETER, RATE OF CLB INDICATOR). THIS VALVE IS LOCATED ON THE SIDE OF THE ACFT WITHIN ABOUT 3 INCHES OF THE PLT'S L KNEE WHILE SITTING. SINCE THE VALVE IS VERY EASY TO MOVE, I BELIEVE I MAY HAVE HIT IT WITH MY KNEE AS I SAT DOWN. TO PREVENT ANY FUTURE OCCURRENCE OF THIS, I WILL ALWAYS CHK THIS VALVE AFTER I AM IN MY SEAT TO ENSURE THAT IT IS COMPLETELY SHUT. I ALSO BELIEVE IT SHOULD BE HARDER TO TURN IT TO PREVENT IT FROM BEING MOVED INADVERTENTLY. ALSO POSSIBLE CONSIDERATION MAY NEED TO BE GIVEN TO MOVING THE DRAIN VALVE TO ANOTHER LOCATION ON FUTURE ACFT.
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.