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Attributes | |
ACN | 495770 |
Time | |
Date | 200012 |
Day | Sat |
Local Time Of Day | 1801 To 2400 |
Place | |
Locale Reference | airport : orf.airport |
State Reference | VA |
Altitude | agl single value : 0 msl bound upper : 3000 |
Environment | |
Flight Conditions | IMC |
Weather Elements | Fog |
Light | Night |
Aircraft 1 | |
Controlling Facilities | tracon : orf.tracon tower : orf.tower |
Operator | common carrier : air carrier |
Make Model Name | Fokker 100 |
Operating Under FAR Part | Part 121 |
Navigation In Use | ils localizer & glide slope : 05 other |
Flight Phase | descent : approach |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : flight engineer pilot : instrument pilot : multi engine pilot : atp pilot : cfi pilot : commercial |
Experience | flight time last 90 days : 120 flight time total : 13100 flight time type : 2000 |
ASRS Report | 495778 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : commercial pilot : multi engine pilot : instrument |
Events | |
Anomaly | aircraft equipment problem : critical other anomaly other |
Independent Detector | other flight crewa |
Resolutory Action | none taken : anomaly accepted other |
Consequence | other |
Supplementary | |
Problem Areas | Aircraft Flight Crew Human Performance |
Primary Problem | Aircraft |
Narrative:
During the CAT I ILS runway 5 approach, the autoplt failed to capture the GS at the intercept altitude. I immediately disconnected the autoplt and manually recaptured the GS and continued the CAT I approach utilizing the flight director. Due to variable tailwinds in this non normal situation, the vertical speed momentarily exceeded 1000 FPM descent while correcting. Aircraft configured, on speed, and GS bracketed. First officer reported loss of his GS indicator. Since my GS, localizer, and all other indicators were normal, and I had the required approach lights and runway environment in sight to continue the CAT I approach, and the RVR more than 6000 ft, I continued the approach to a normal landing. Maintenance notified. One of the flight control computers had faulted.
Original NASA ASRS Text
Title: FLT CTL COMPUTER PROB RESULTS IN HAND FLOWN CAT I ILS RWY 5 APCH AT ORF, VA.
Narrative: DURING THE CAT I ILS RWY 5 APCH, THE AUTOPLT FAILED TO CAPTURE THE GS AT THE INTERCEPT ALT. I IMMEDIATELY DISCONNECTED THE AUTOPLT AND MANUALLY RECAPTURED THE GS AND CONTINUED THE CAT I APCH UTILIZING THE FLT DIRECTOR. DUE TO VARIABLE TAILWINDS IN THIS NON NORMAL SIT, THE VERT SPD MOMENTARILY EXCEEDED 1000 FPM DSCNT WHILE CORRECTING. ACFT CONFIGURED, ON SPD, AND GS BRACKETED. FO RPTED LOSS OF HIS GS INDICATOR. SINCE MY GS, LOC, AND ALL OTHER INDICATORS WERE NORMAL, AND I HAD THE REQUIRED APCH LIGHTS AND RWY ENVIRONMENT IN SIGHT TO CONTINUE THE CAT I APCH, AND THE RVR MORE THAN 6000 FT, I CONTINUED THE APCH TO A NORMAL LNDG. MAINT NOTIFIED. ONE OF THE FLT CTL COMPUTERS HAD FAULTED.
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.