ATL91IA017

NTSB incident investigation · Fokker F28 MK0100 · Atlanta, GA · November 11, 1990

Incident · No injuriesIncident investigationFinal report
Date
November 11, 1990, 18:10 local (23:10 UTC)
Place
Atlanta, GA
Injuries
75 uninjured
Damage
No damage
Phase of flight
Enroute
Aircraft
N850USFokker F28 MK0100
Weather
Visual (VMC) · Dusk
Status
Completed · report May 10, 1993
Report
Approved by Office Director
FAA report
19901111057209I
Case key
8341

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the incident.

On this page

Probable cause

Frozen moisture in the stabilizer actuator hydraulic servo valve which resulted in reduced movement of the servo valve and limited its ability to respond to flight control inputs. The lack of response from the servo valve resulted in the jammed stabilizer message. A factor was the inadequate design of the servo valve which precluded moisture drainage.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionDescent - normal
Flight control,stabilator - jammedCause
Flt control syst,horiz stab drive - frozenCause
Acft/equip,inadequate designManufacturerFactor

Analysis

During descent the afcas stabilizer trim & autopilot disengaged. Both were reset with a 2nd disengagement. Nose down control pressures were encountered & the flt crew attempted to use manual trim, followed by a jammed stabilizer master warning. Afcas stabilizer trim was left off iaw abnormal procedures. FDR data showed the stab then creeped to a full acft nose down position & hyd pres to the stab actuator was automatically removed, per design. Subsequent testing of the horizontal stabilizer control unit assembly showed that, after spraying the servo valve with water and cold soaking, ice would form inside the end cap and a jammed servo valve condition would occur. The end cap and spring exhibited substantial rust corrosion. Crew movement of the manual trim resulted in the jammed stab warning.

Aircraft

Registration
N850US
Reported as
Fokker F28 MK0100
Category
Airplane
Serial number
11276
Airframe hours
2,674
Engine
Rolls-Royce TAY650715, 15,000 lbs thrust, turbo jet
Damage
No damage
Flight
Part 121
Operator
Usair
Airworthiness certificate
Standard, Transport
Last inspection
Continuous airworthiness · October 10, 1990 · 147 hours before
Departed
PHL · Philadelphia, PA
Destination
ATL · Atlanta, GA
Flight plan
IFR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
41
Certificate
Airline transport
Airplane ratings
Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
15,127 total

Weather

Conditions
Visual (VMC) · Dusk
Wind
300° at 4 knots
Visibility
20 statute miles
Lowest ceiling
None
Temperature
61 °F, dew point 39 °F
Altimeter
30.00 inHg
Observed at
ATL

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.