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|
Attributes | |
ACN | 439769 |
Time | |
Date | 199906 |
Day | Thu |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : phl.airport |
State Reference | PA |
Altitude | msl bound lower : 3000 msl bound upper : 3600 |
Environment | |
Flight Conditions | IMC |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tracon : phl.tracon |
Operator | common carrier : air carrier |
Make Model Name | A319 |
Operating Under FAR Part | Part 121 |
Navigation In Use | ils localizer & glide slope : 09r other |
Flight Phase | descent : approach |
Route In Use | approach : instrument precision arrival : on vectors |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : atp |
Experience | flight time last 90 days : 45 flight time total : 10300 flight time type : 45 |
ASRS Report | 439769 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : atp |
Events | |
Anomaly | altitude deviation : excursion from assigned altitude non adherence : published procedure |
Independent Detector | other flight crewa other flight crewb |
Resolutory Action | flight crew : overrode automation |
Supplementary | |
Problem Areas | Flight Crew Human Performance |
Primary Problem | Flight Crew Human Performance |
Air Traffic Incident | Pilot Deviation |
Narrative:
The aircraft was being flown by the captain and was on vectors for the runway 9R localizer at phl. The aircraft was level at 3000 ft MSL, in IMC, 190 KTS, flaps 1 degree. All FMGS automation was in use: autoplt #1 engaged, autothrottle active, flight director #1 and #2 on, localizer armed, heading selected for the vector to the localizer. Just as the aircraft captured the localizer, ATC issued the ILS runway 9R approach clearance, at which time the captain pushed the approach button and selected autoplt #2 per company procedure (ie, autoplt #1 controling, autoplt #2 armed). All FMA annunciations were correct. Immediately upon pushing the approach and autoplt #2 buttons (the buttons were pushed within 1-2 seconds of each other), the aircraft pitched up abruptly and the autothrottle system commanded a significant increase in thrust, but did not go to toga. The captain disconnected the autoplt and recaptured the altitude and localizer course. The aircraft had climbed to 3600 ft. Autothrottle remained engaged throughout the excursion. Thrust was reduced by the autothrottle system as the captain began a descent to the assigned altitude. During the uncommanded climb, the FMA continued to show altitude green, localizer green and GS blue. Autothrottle continued to annunciate speed green. The captain re-engaged the autoplt and the landing was completed without further anomalies. On the ground in phl, an airbus technical representative examined the available stored system reports and found no discrepancies in the aircraft system. He attributed the fault to the captain's 'procedures.' it is my observation that the captain's procedures were timely and correct and consistent with published company procedures. Although 3 changes occurred almost simultaneously with the uncommanded climb (localizer capture, autoplt #2 armed and approach engaged) I believe the climb began as autoplt #2 was armed. For whatever reason, I believe autoplt #2 was commanding open cl, even though the FMA did not indicate this, nor was the FCU set to a higher altitude than 3000 ft MSL. The autothrottle system responded as if open cl had been commanded and increased thrust during the climb, then decreased thrust as the captain descended to 3000 ft.
Original NASA ASRS Text
Title: AN A320 IN AUTOFLT ATTEMPTED AN AUTOPLT COUPLED APCH. UPON SELECTING THE APCH MODE SINCE THE ACFT INCREASE THRUST AND CLBED RATHER THAN FLY THE APCH.
Narrative: THE ACFT WAS BEING FLOWN BY THE CAPT AND WAS ON VECTORS FOR THE RWY 9R LOC AT PHL. THE ACFT WAS LEVEL AT 3000 FT MSL, IN IMC, 190 KTS, FLAPS 1 DEG. ALL FMGS AUTOMATION WAS IN USE: AUTOPLT #1 ENGAGED, AUTOTHROTTLE ACTIVE, FLT DIRECTOR #1 AND #2 ON, LOC ARMED, HDG SELECTED FOR THE VECTOR TO THE LOC. JUST AS THE ACFT CAPTURED THE LOC, ATC ISSUED THE ILS RWY 9R APCH CLRNC, AT WHICH TIME THE CAPT PUSHED THE APCH BUTTON AND SELECTED AUTOPLT #2 PER COMPANY PROC (IE, AUTOPLT #1 CTLING, AUTOPLT #2 ARMED). ALL FMA ANNUNCIATIONS WERE CORRECT. IMMEDIATELY UPON PUSHING THE APCH AND AUTOPLT #2 BUTTONS (THE BUTTONS WERE PUSHED WITHIN 1-2 SECONDS OF EACH OTHER), THE ACFT PITCHED UP ABRUPTLY AND THE AUTOTHROTTLE SYS COMMANDED A SIGNIFICANT INCREASE IN THRUST, BUT DID NOT GO TO TOGA. THE CAPT DISCONNECTED THE AUTOPLT AND RECAPTURED THE ALT AND LOC COURSE. THE ACFT HAD CLBED TO 3600 FT. AUTOTHROTTLE REMAINED ENGAGED THROUGHOUT THE EXCURSION. THRUST WAS REDUCED BY THE AUTOTHROTTLE SYS AS THE CAPT BEGAN A DSCNT TO THE ASSIGNED ALT. DURING THE UNCOMMANDED CLB, THE FMA CONTINUED TO SHOW ALT GREEN, LOC GREEN AND GS BLUE. AUTOTHROTTLE CONTINUED TO ANNUNCIATE SPD GREEN. THE CAPT RE-ENGAGED THE AUTOPLT AND THE LNDG WAS COMPLETED WITHOUT FURTHER ANOMALIES. ON THE GND IN PHL, AN AIRBUS TECHNICAL REPRESENTATIVE EXAMINED THE AVAILABLE STORED SYS RPTS AND FOUND NO DISCREPANCIES IN THE ACFT SYS. HE ATTRIBUTED THE FAULT TO THE CAPT'S 'PROCS.' IT IS MY OBSERVATION THAT THE CAPT'S PROCS WERE TIMELY AND CORRECT AND CONSISTENT WITH PUBLISHED COMPANY PROCS. ALTHOUGH 3 CHANGES OCCURRED ALMOST SIMULTANEOUSLY WITH THE UNCOMMANDED CLB (LOC CAPTURE, AUTOPLT #2 ARMED AND APCH ENGAGED) I BELIEVE THE CLB BEGAN AS AUTOPLT #2 WAS ARMED. FOR WHATEVER REASON, I BELIEVE AUTOPLT #2 WAS COMMANDING OPEN CL, EVEN THOUGH THE FMA DID NOT INDICATE THIS, NOR WAS THE FCU SET TO A HIGHER ALT THAN 3000 FT MSL. THE AUTOTHROTTLE SYS RESPONDED AS IF OPEN CL HAD BEEN COMMANDED AND INCREASED THRUST DURING THE CLB, THEN DECREASED THRUST AS THE CAPT DSNDED TO 3000 FT.
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.