20010602014079I

Incident

FAA incident report · Boeing 727-22C · Rochester, NY · June 2, 2001

Date
June 2, 2001 · 07:30 local
Place
Rochester, NY
Airport
Greater Rochester Internationa
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
Air carrier (Part 121)
Operator
DHLA
Aircraft
N705DH
Reported as
Boeing 72722C
People aboard
3
Fatal injuries
0

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.

(-23) On Saturday, June 2, 2001, just after take-off from the Rochester international airport (roc), the number three engine of a dhl airlines, inc. aircraft, N705DH, began to vibrate severely and the engine instruments all rolled back to minimal indications. Capt robert walker, certificate number 381643876, decided that there had been an engine failure and returned to roc, landed unevently and taxied to the ramp. Ground examination showed failure of the last two rotor/stator stages in the turbine. The tailpipe was punctured in three places by exiting/tumbling debris. There was no evidence of liberated debris in the plane of rotation nor any sign of bulging in the engine exhaust case. At the time, the decision from maintenance control was to send a crew to change the engine. This incident is considered closed.

As the FAA filed it

(-23) ON SATURDAY, JUNE 2, 2001, JUST AFTER TAKE-OFF FROM THE ROCHESTER INTERNATIONAL AIRPORT (ROC), THE NUMBER THREE ENGINE OF A DHL AIRLINES, INC. AIRCRAFT, N705DH, BEGAN TO VIBRATE SEVERELY AND THE ENGINE INSTRUMENTS ALL ROLLED BACK TO MINIMAL INDICATIONS. CAPT ROBERT WALKER, CERTIFICATE NUMBER 381643876, DECIDED THAT THERE HAD BEEN AN ENGINE FAILURE AND RETURNED TO ROC, LANDED UNEVENTLY AND TAXIED TO THE RAMP. GROUND EXAMINATION SHOWED FAILURE OF THE LAST TWO ROTOR/STATOR STAGES IN THE TURBINE. THE TAILPIPE WAS PUNCTURED IN THREE PLACES BY EXITING/TUMBLING DEBRIS. THERE WAS NO EVIDENCE OF LIBERATED DEBRIS IN THE PLANE OF ROTATION NOR ANY SIGN OF BULGING IN THE ENGINE EXHAUST CASE. AT THE TIME, THE DECISION FROM MAINTENANCE CONTROL WAS TO SEND A CREW TO CHANGE THE ENGINE. THIS INCIDENT IS CONSIDERED CLOSED.