19960625022959I

Incident · Minor damage

FAA incident report · Boeing 767-332 · New York, NY · June 25, 1996

Date
June 25, 1996 · 19:15 local
Place
New York, NY
Airport
John F Kennedy International
Phase of flight
Climb
Operating rules
Air carrier (Part 121)
Operator
DALA
Damage
Minor damage
Aircraft
N185DN
NTSB investigation
NTSBNYC96IA131
Reported as
Boeing 767332
Reported engine
Pratt & Whitney PW4060
People aboard
224
Fatal injuries
0
Pilot’s flight hours
15,000 total858 in this make and model203 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.

Narrative: while climbing through 3,000 ft the aircraft experienced loss of the right engine generator as well as an uncommanded left roll. The flight crew was able to regain control of the aircraft and returned to jfk without further incident. The aircraft logbook was reviewed and revealed that there was no history of work accomplished on the ata 24 (electrical) and ata 27 (flight control) systems. Interviews with dala maintenance revealed that A2B aileron control cable, located at station 325, above the P32 panel was severed after it chaffed through the insulation of the generator feed cable located at the main equipment center. Interviews were conducted with dala maintenance mgmt. Including the atl-based mechanics who were installing the replacement aileron control cable. FAA has issued a telegraphic AD (AD T96-14-51) and Boeing has issued Boeing alert service bulletin 767-24-A0113R1, dated July 2, 1996 issued to perform a one-time inspection of the aileron control cable and the right generator power feeder cables.

As the FAA filed it

NARRATIVE: WHILE CLIMBING THROUGH 3,000 FT THE AIRCRAFT EXPERIENCED LOSS OF THE RIGHT ENGINE GENERATOR AS WELL AS AN UNCOMMANDED LEFT ROLL. THE FLIGHT CREW WAS ABLE TO REGAIN CONTROL OF THE AIRCRAFT AND RETURNED TO JFK WITHOUT FURTHER INCIDENT. THE AIRCRAFT LOGBOOK WAS REVIEWED AND REVEALED THAT THERE WAS NO HISTORY OF WORK ACCOMPLISHED ON THE ATA 24 (ELECTRICAL) AND ATA 27 (FLIGHT CONTROL) SYSTEMS. INTERVIEWS WITH DALA MAINTENANCE REVEALED THAT A2B AILERON CONTROL CABLE, LOCATED AT STATION 325, ABOVE THE P32 PANEL WAS SEVERED AFTER IT CHAFFED THROUGH THE INSULATION OF THE GENERATOR FEED CABLE LOCATED AT THE MAIN EQUIPMENT CENTER. INTERVIEWS WERE CONDUCTED WITH DALA MAINTENANCE MGMT. INCLUDING THE ATL-BASED MECHANICS WHO WERE INSTALLING THE REPLACEMENT AILERON CONTROL CABLE. FAA HAS ISSUED A TELEGRAPHIC AD (AD T96-14-51) AND BOEING HAS ISSUED BOEING ALERT SERVICE BULLETIN 767-24-A0113R1, DATED JULY 2, 1996 ISSUED TO PERFORM A ONE-TIME INSPECTION OF THE AILERON CONTROL CABLE AND THE RIGHT GENERATOR POWER FEEDER CABLES.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N185DN · 1

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