20060323013409I

Incident

FAA incident report · Boeing 737-522 · Philadelphia, PA · March 23, 2006

Date
March 23, 2006 · 17:27 local
Place
Philadelphia, PA
Airport
Philadelphia International
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
Air carrier (Part 121)
Operator
UALA
Aircraft
N927UA
Reported as
Boeing 737522
Reported engine
CFMINT CFM563C1
People aboard
69
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) At 1727 eastern standard time, flight 563, returned to Philadelphia International Airport (phl) and landed on runway 27L after reporting smoke in the cabin. During this incident the crew reported smoke in the cabin after take-off. Both lav smoke detectors sounded and smoke was visible in the aft galley area. Flight attendants reported a burning rubber or oily smell in the cabin. The fire department responded, no fire or injuries were reported and the aircraft taxied to the ramp without incident. United phl maintenance conducted troubleshooting procedures and isolated the cause to the #2 engine bleed air system. The #2 engine primary regulator shut-off valve (prsov) was deactivated per MEL 36030, amm 36-11-15-201 in preparation for ferry flight to denver for #2 engine change. Aircraft landed overweight and post inspection was completed with no findings. This inspector notified the pmi and he stated the certificate management office (cmo) will review the engine teardown report. Operator notified the cmo iaw 14 CFR 121.703(a)(5).

As the FAA filed it

(-23) AT 1727 EASTERN STANDARD TIME, FLIGHT 563, RETURNED TO PHILADELPHIA INTERNATIONAL AIRPORT (PHL) AND LANDED ON RUNWAY 27L AFTER REPORTING SMOKE IN THE CABIN. DURING THIS INCIDENT THE CREW REPORTED SMOKE IN THE CABIN AFTER TAKE-OFF. BOTH LAV SMOKE DETECTORS SOUNDED AND SMOKE WAS VISIBLE IN THE AFT GALLEY AREA. FLIGHT ATTENDANTS REPORTED A BURNING RUBBER OR OILY SMELL IN THE CABIN. THE FIRE DEPARTMENT RESPONDED, NO FIRE OR INJURIES WERE REPORTED AND THE AIRCRAFT TAXIED TO THE RAMP WITHOUT INCIDENT. UNITED PHL MAINTENANCE CONDUCTED TROUBLESHOOTING PROCEDURES AND ISOLATED THE CAUSE TO THE #2 ENGINE BLEED AIR SYSTEM. THE #2 ENGINE PRIMARY REGULATOR SHUT-OFF VALVE (PRSOV) WAS DEACTIVATED PER MEL 36030, AMM 36-11-15-201 IN PREPARATION FOR FERRY FLIGHT TO DENVER FOR #2 ENGINE CHANGE. AIRCRAFT LANDED OVERWEIGHT AND POST INSPECTION WAS COMPLETED WITH NO FINDINGS. THIS INSPECTOR NOTIFIED THE PMI AND HE STATED THE CERTIFICATE MANAGEMENT OFFICE (CMO) WILL REVIEW THE ENGINE TEARDOWN REPORT. OPERATOR NOTIFIED THE CMO IAW 14 CFR 121.703(A)(5).