N197AN

MINR
None

BOEING 757-223S/N: NT975

Accident Details

Date
Monday, September 22, 2008
NTSB Number
CHI08IA292
Location
Chicago, IL
Event ID
20081007X03940
Coordinates
41.978610, -87.904724
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
192
Total Aboard
192

Probable Cause and Findings

The failure of an electrical relay due to eroded contacts and the flight crew's decision to continue a flight that was operating on battery power.

Aircraft Information

Registration
Make
BOEING
Serial Number
NT975
Engine Type
Turbo-fan
Year Built
2001
Model / ICAO
757-223B752
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
178
FAA Model
757-223

Registered Owner (Current)

Name
AERSALE INC
Address
9850 NW 41ST ST STE 400
City
DORAL
State / Zip Code
FL 33178-2992
Country
United States

Analysis

HISTORY OF FLIGHT

On September 22, 2008, at 1342 central daylight time, a Boeing 757-223, N197AN, operated by American Airlines as flight 268, overran the side of Runway 22R (7,500 feet by 150 feet), while landing at the O’Hare International Airport (ORD), Chicago, Illinois. There were no injuries to the 2 flight crewmembers, 5 flight attendants, and 185 passengers. The airplane received minor damage to the landing gear. The scheduled domestic passenger flight was being operated under the provisions of Title 14 Code of Federal Regulations Part 121. Visual meteorological conditions prevailed and the flight was operating on an instrument flight rules flight plan. The flight originated from the Seattle-Tacoma International Airport (SEA), Seattle, Washington, at 0801 pacific daylight time, with an intended destination of the John F. Kennedy International Airport (JFK), New York, New York. (All times are central daylight unless noted.)

The captain reported that prior to takeoff from SEA, he noticed that the standby horizon had tumbled with the flags in view and that it was unpowered. He turned the Standby Power Selector Off and On followed by turning the Battery Switch Off and On. The standby horizon righted itself and the flags disappeared. He noticed five status messages displayed on the lower engine indicating and crew alert system (EICAS) screen; however, he could not recall what the messages were. He then called maintenance to report the messages. A mechanic came into the cockpit, cleared the messages, and stated that they were “good to go.” No logbook entries were made regarding this event.

The flight crew reported that just prior to leveling off at flight level (FL) 370, some cockpit lights flickered, multiple EICAS messages appeared including an AIR/GRD SYS caution message, and the Standby Power OFF light illuminated. In addition, the autopilot disconnect warning sounded and the autothrottles disconnected and the captain reported the autopilot began to act “squirrely”. According to the flight data recorder (FDR), electrical system anomalies began at 10:25:35, when the battery voltage spiked to approximately 31 volts direct current (VDC).

The first officer referred to the quick reference handbook (QRH) regarding the AIR/GND SYS message. The flight crew then followed the procedure for STANDBY BUS OFF as referenced in the QRH, turning the Standby Power selector to the BAT position. The second step did not apply to their situation, so they stopped the checklist with the Standby Power selector in the BAT position. This QRH procedure also stated, “The battery will provide bus power for approximately 30 minutes.” The DISCHARGE light remained illuminated. The captain reported that he looked at the list of items on the page that may be inoperative with the standby bus unpowered. At 10:30:55, according to the FDR, the main battery discharge indicated “discharge” and the main battery voltage began to decrease.

The first officer then performed the QRH Main Battery Charger checklist, which tests the main battery charger. The crew determined that this QRH procedure did not apply to the situation and they did not complete the checklist. The procedure stated that the battery discharge light should not be illuminated, but it was. The captain reported the airplane appeared to be stabilized with the Standby Power Selector in the BAT position.

The captain contacted American Airlines maintenance technical support (Tulsa Tech) twice and subsequently elected to continue the flight on battery power. Conversation regarding the electrical anomalies between the captain and first officer continued throughout the flight.

At 12:54:38, a sound similar to the master caution warning was heard on the cockpit voice recorder (CVR). The FDR indicated that this was around the time that battery power was depleted; approximately 2 hours 24 minutes after the flight crew switched the Standby Power selector to the BAT position.

The first officer stated the first indication of a problem was that the auto-throttle light illuminated, the auto-throttles disconnected, and the autopilot became “squirrelly.” According to the captain, numerous cockpit systems then began to fail. At 12:57:35, the captain stated, “…I’ve lost my whole side here.” The captain then told the first officer, “…everything’s working on your side so you got the airplane the rest of the leg.”

At 13:15:48, the captain contacted American Airlines dispatch stating that the electrical problems they were experiencing were getting worse and they needed to divert to ORD. The captain contacted the Chicago Air route Traffic Control Center (ARTCC) stating that they needed to divert to ORD because of electrical problems. The controller cleared the airplane to ORD via radar vectors and cleared the airplane to begin a descent. The airplane was over western Michigan at this time.

It was around this time that the flight attendants discovered the public address (PA) system and the interphone were inoperative. The number one flight attendant wrote a note and slipped it under the cockpit door informing the flight crew of their communication problems. A short time later, the captain opened the cockpit door and told the flight attendants that they were diverting to ORD. One of the flight attendants then walked through the aisle informing the passengers of the unscheduled landing.

At 13:20:39, the ARTCC controller asked the flight crew if they needed any assistance. The captain replied that they were alright. He stated that more than one electrical system had failed and it appeared everything was functioning, but their backups were “going away.” He also informed the controller that they were unable to fly an instrument landing system (ILS) approach. The controller continued to issue radar vectors to the airport and descents.

At 13:22:02, the captain tried to make a PA announcement informing the passengers that they had an “electrical complication” and they were diverting to ORD. He was not aware whether or not the PA system was working.

At 13:32:04, the captain contacted ORD approach control stating they were at 10,000 feet and slowing down. He stated they had “almost no indications in the cockpit” and emergency equipment was not required.

The first officer reported the captain’s instruments were all inoperative and that he was flying the airplane. As the airplane decelerated, the first officer realized the main stabilizer trim and the alternate stabilizer trim were inoperative. He stated he had a “hand full of airplane.”

At 13:39:18, the captain reporting having the airport in sight. The local controller then cleared the airplane for the visual approach to Runway 22R. At 13:39:53, the first officer stated, “we’re close to being an emergency right now. We don’t have trim.”

At 13:40:25, the captain declared an emergency. The controller cleared the airplane to land and stated that emergency crews were on standby.

The captain then assisted the first officer on the flight controls and they continued the landing approach. The captain reported that the systems they needed to slow the airplane on the runway appeared normal, and because of the flight control issues they did not want to perform a go-around and land on a longer runway. The captain reported it was very difficult to maintain pitch control of the airplane, so he stopped the flap extension at 20.

The captain reported they made a good landing, but the nose of the airplane touched down a “little firmer than I cared for.” The first officer selected reverse thrust, but nothing happened. The captain stated the spoilers were armed, but they did not automatically deploy. He reported he manually deployed the spoilers, but still was not sure if they deployed. The first officer reported that he applied the brakes, but they were insufficient and did not feel normal. The captain reported he was concerned about the brake function and accumulator pressure, so he made one smooth application of the brakes, which did not “perform well.” Due to obstructions off the end of the runway, the captain elected to veer the airplane off the left side of the runway into the grass.

Airport personnel and firefighters who witnessed the landing reported the airplane appeared to be fast and it touched down approximately 2,500 feet down the runway, near the intersection of taxiway Papa. They reported the airplane touched down hard, and they heard several loud “pops” when the airplane contacted the runway.

Skid marks from the left main gear began near the point of touchdown, followed 165 feet later by skid marks from the right main gear. These skid marks were visible for the entire length of the runway up until the airplane departed the pavement. The airplane came to rest with all three landing gear off the left side of the pavement. The nose of the airplane came to rest approximately 100 feet prior to the end of the blast pad pavement which extended 397 feet past the departure end of the runway.

After coming to a stop, the flight crew was not able to shut the engines down with either the fuel cutoff valves or by activating the fire handles. Airport firefighting and rescue (ARFF) personnel, and American Airlines maintenance personnel boarded the airplane. The engines were subsequently shutdown by depressing the fire handles and recycling the generator control switch. Once the engines were shut down, the passengers were deplaned through the L1 and R3 doors using portable stairs.

DAMAGE TO AIRCRAFT

Damage to the airplane was confined to the landing gear. Seven of the eight main landing gear tires were either blown out or deflated during the landing.

PERSONNEL INFORMATION

The captain, age 50, held an airline transport pilot certificate with an airplane multi-engine rating and commercial privileges for single-engine land airplanes. He also held type ratings for B-757 and B-767...

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI08IA292