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|
Attributes | |
ACN | 328588 |
Time | |
Date | 199602 |
Day | Mon |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | airport : phx |
State Reference | AZ |
Altitude | msl bound lower : 2000 msl bound upper : 2000 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tower : phx tower : cvg |
Operator | common carrier : air carrier |
Make Model Name | B737-300 |
Operating Under FAR Part | Part 121 |
Navigation In Use | Other Other |
Flight Phase | descent : approach landing : go around landing : missed approach |
Flight Plan | IFR |
Aircraft 2 | |
Operator | general aviation : personal |
Make Model Name | Experimental |
Operating Under FAR Part | Part 91 |
Flight Phase | other |
Flight Plan | None |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : atp |
Experience | flight time last 90 days : 210 flight time total : 4500 flight time type : 2500 |
ASRS Report | 328588 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : atp |
Events | |
Anomaly | aircraft equipment problem : critical conflict : airborne less severe other anomaly other |
Independent Detector | other controllera |
Resolutory Action | flight crew : declared emergency flight crew : overcame equipment problem other other |
Consequence | faa : reviewed incident with flight crew Other |
Miss Distance | unspecified : 1000 |
Supplementary | |
Primary Problem | Aircraft |
Air Traffic Incident | Pilot Deviation |
Narrative:
Lax-phx. Approximately 10 mi out on final runway 8R at phx, a B737- 300 asymmetrical stuck trailing edge flaps at approximately 18 degrees and 23 degrees. While slowly getting dirty, on a 25-30 mi final for runway 8R at phx, the trailing edge flap got stuck. Approximately 15 seconds after discovery of the split flap condition, a decision was made to go around. At go around the aircraft was approximately 5 mi out on final. A level off at approximately 2000 ft and soon after a slow climb as directed to 3000 ft took place. Missed approach, the gears were raised and the flaps were left in position due to the stuck asymmetry. The gear/flap horn sounded very loudly upon gear-up. After approximately 10 seconds with the gear/flap horn sounding very loudly, it was realized that the gear should be lowered. There was plenty of fuel to handle the increased fuel burn with gear down flight. The tower had been informed of the go around right away. Approximately overhead the upwind numbers I (copilot), on my own instinct, turned downwind. Instinct told me to keep the airport/runway in sight at all times until I was sure of the result of our flap problem. A turn was made downwind while the captain was on the PA to the passenger. The captain returned to the #1 radio and declared an emergency to tower. After approximately 145 degrees of turn downwind, the crew was informed by tower of a traffic conflict with an 'experimental aircraft.' a no TCASII small aircraft. We were given a frequency change and a climb by either tower or departure control, climb to 6000 ft and directed to continue our turn to 250 degrees. We were then subsequently vectored around by departure while working the checklist. The flaps, per checklist, were raised and made symmetrical to flaps 15 degrees. It was decided no further troubleshooting would occur and a flaps 15 degree landing would be made. 15 degree reference speed on a long, dry, runway 8R. An uneventful dirty confign approach and landing resulted. On the ground ATC asked us to call on the phone. It was discovered that a traffic conflict (had or almost had?) occurred with the 'experimental aircraft.' the instinct or gut desire for the copilot to keep the airfield in sight with a shallow right turn downwind without clearance caused the problem. Cause, instinct. Solution? Perhaps one solution, a spare tower controller standing by at all times solely to assist when an emergency takes place.
Original NASA ASRS Text
Title: FO OF AN MLG FAILED TO FOLLOW ATC MISSED APCH INSTRUCTIONS AND TURNED DOWNWIND TO KEEP ARPT IN SIGHT BECAUSE OF A SPLIT FLAP PROB AND CAUSED A CONFLICT WITH ANOTHER ACFT ALREADY IN THE TFC PATTERN.
Narrative: LAX-PHX. APPROX 10 MI OUT ON FINAL RWY 8R AT PHX, A B737- 300 ASYMMETRICAL STUCK TRAILING EDGE FLAPS AT APPROX 18 DEGS AND 23 DEGS. WHILE SLOWLY GETTING DIRTY, ON A 25-30 MI FINAL FOR RWY 8R AT PHX, THE TRAILING EDGE FLAP GOT STUCK. APPROX 15 SECONDS AFTER DISCOVERY OF THE SPLIT FLAP CONDITION, A DECISION WAS MADE TO GAR. AT GAR THE ACFT WAS APPROX 5 MI OUT ON FINAL. A LEVEL OFF AT APPROX 2000 FT AND SOON AFTER A SLOW CLB AS DIRECTED TO 3000 FT TOOK PLACE. MISSED APCH, THE GEARS WERE RAISED AND THE FLAPS WERE LEFT IN POS DUE TO THE STUCK ASYMMETRY. THE GEAR/FLAP HORN SOUNDED VERY LOUDLY UPON GEAR-UP. AFTER APPROX 10 SECONDS WITH THE GEAR/FLAP HORN SOUNDING VERY LOUDLY, IT WAS REALIZED THAT THE GEAR SHOULD BE LOWERED. THERE WAS PLENTY OF FUEL TO HANDLE THE INCREASED FUEL BURN WITH GEAR DOWN FLT. THE TWR HAD BEEN INFORMED OF THE GAR RIGHT AWAY. APPROX OVERHEAD THE UPWIND NUMBERS I (COPLT), ON MY OWN INSTINCT, TURNED DOWNWIND. INSTINCT TOLD ME TO KEEP THE ARPT/RWY IN SIGHT AT ALL TIMES UNTIL I WAS SURE OF THE RESULT OF OUR FLAP PROB. A TURN WAS MADE DOWNWIND WHILE THE CAPT WAS ON THE PA TO THE PAX. THE CAPT RETURNED TO THE #1 RADIO AND DECLARED AN EMER TO TWR. AFTER APPROX 145 DEGS OF TURN DOWNWIND, THE CREW WAS INFORMED BY TWR OF A TFC CONFLICT WITH AN 'EXPERIMENTAL ACFT.' A NO TCASII SMALL ACFT. WE WERE GIVEN A FREQ CHANGE AND A CLB BY EITHER TWR OR DEP CTL, CLB TO 6000 FT AND DIRECTED TO CONTINUE OUR TURN TO 250 DEGS. WE WERE THEN SUBSEQUENTLY VECTORED AROUND BY DEP WHILE WORKING THE CHKLIST. THE FLAPS, PER CHKLIST, WERE RAISED AND MADE SYMMETRICAL TO FLAPS 15 DEGS. IT WAS DECIDED NO FURTHER TROUBLESHOOTING WOULD OCCUR AND A FLAPS 15 DEG LNDG WOULD BE MADE. 15 DEG REF SPD ON A LONG, DRY, RWY 8R. AN UNEVENTFUL DIRTY CONFIGN APCH AND LNDG RESULTED. ON THE GND ATC ASKED US TO CALL ON THE PHONE. IT WAS DISCOVERED THAT A TFC CONFLICT (HAD OR ALMOST HAD?) OCCURRED WITH THE 'EXPERIMENTAL ACFT.' THE INSTINCT OR GUT DESIRE FOR THE COPLT TO KEEP THE AIRFIELD IN SIGHT WITH A SHALLOW R TURN DOWNWIND WITHOUT CLRNC CAUSED THE PROB. CAUSE, INSTINCT. SOLUTION? PERHAPS ONE SOLUTION, A SPARE TWR CTLR STANDING BY AT ALL TIMES SOLELY TO ASSIST WHEN AN EMER TAKES PLACE.
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.