20120421008669I

Incident · No damage

FAA incident report · Airbus Industrie A320-232 · Tampa, FL · April 21, 2012

Date
April 21, 2012 · 15:00 local
Place
Tampa, FL
Airport
Tampa International
Phase of flight
Cruise/Level Flight
Operating rules
Air carrier (Part 121)
Operator
CALA
Damage
No damage
Aircraft
N418UA
Reported as
Airbus Industrie A320-232
Reported engine
IAE V2500SERIES
People aboard
6
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
8,430 total714 in this make and model67 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Flight 6866-21 was approximately one hour into test flight when the flight crew noticed that neither autopilots (1 & 2) would stay engaged. When the autopilot would attempt to adjust pitch it would disengage. The crew began to get fault indications on the electronic centralized aircraft monitor (ecam) related to elevator and aileron computor (elac) #1 and elac #2. The flight crew completed the checks that were able to be accomplished in the current condition of the aircraft and noticed that the pitch trim would not allow them to trim nose up. As they lined the aircraft up for final approach they noted that the pitch trim was locked in the 5 degree nose down position. The crew did not declare an emergency and continued the approach to a full stop landing. NTSB was notified by the pilots due to the elac 1 and 2 fault indications. After a review of the incident NTSB released the aircraft to united airlines inc. to allow them to perform an investigation into the incident. It was discovered that a bolt p/n NAS6704-12 had become lodged in the mechanism which controlled the pitch trim of the horizontal stabilizer.

As the FAA filed it

FLIGHT 6866-21 WAS APPROXIMATELY ONE HOUR INTO TEST FLIGHT WHEN THE FLIGHT CREW NOTICED THAT NEITHER AUTOPILOTS (1 & 2) WOULD STAY ENGAGED. WHEN THE AUTOPILOT WOULD ATTEMPT TO ADJUST PITCH IT WOULD DISENGAGE. THE CREW BEGAN TO GET FAULT INDICATIONS ON THE ELECTRONIC CENTRALIZED AIRCRAFT MONITOR (ECAM) RELATED TO ELEVATOR AND AILERON COMPUTOR (ELAC) #1 AND ELAC #2. THE FLIGHT CREW COMPLETED THE CHECKS THAT WERE ABLE TO BE ACCOMPLISHED IN THE CURRENT CONDITION OF THE AIRCRAFT AND NOTICED THAT THE PITCH TRIM WOULD NOT ALLOW THEM TO TRIM NOSE UP. AS THEY LINED THE AIRCRAFT UP FOR FINAL APPROACH THEY NOTED THAT THE PITCH TRIM WAS LOCKED IN THE 5 DEGREE NOSE DOWN POSITION. THE CREW DID NOT DECLARE AN EMERGENCY AND CONTINUED THE APPROACH TO A FULL STOP LANDING. NTSB WAS NOTIFIED BY THE PILOTS DUE TO THE ELAC 1 AND 2 FAULT INDICATIONS. AFTER A REVIEW OF THE INCIDENT NTSB RELEASED THE AIRCRAFT TO UNITED AIRLINES INC. TO ALLOW THEM TO PERFORM AN INVESTIGATION INTO THE INCIDENT. IT WAS DISCOVERED THAT A BOLT P/N NAS6704-12 HAD BECOME LODGED IN THE MECHANISM WHICH CONTROLLED THE PITCH TRIM OF THE HORIZONTAL STABILIZER.

Other reports on N418UA · 1

Matched to the same aircraft by N-number and date.