20170325004529I

Incident · No damage

FAA incident report · Mcdonnell Douglas DC-9-83(MD-83) · Sanford, FL · March 25, 2017

Date
March 25, 2017 · 19:05 local
Place
Sanford, FL
Airport
Orlando Sanford International
Phase of flight
Takeoff: Climb Out
Operating rules
Air carrier (Part 121)
Operator
WX0A
Damage
No damage
Aircraft
N862GA
Reported as
Mcdonnell Douglas DC-9-83(MD-83)
Reported engine
Pratt & Whitney JT8D series
People aboard
159
Fatal injuries
0
Other 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.

Log 757313:

Discrepancy: right eng fire light on ref qrh 72.3

Light out with throttle idle oil temp

Reached 138 degrees

Corrective action: see logpage 757314 for t/s of RH eng,see

Logpages 757315,757316,757321 and 757322 for

Replacement of RH eng aft igv duct ,fuel /air heater

Air shutoff valve and main oil filter. Ops & lk

Checks good of RH eng igv duct ,fuel /air heater air

Shutoff valve and main oil filter. Ok for service.

Log 757314:

Discrepancy: reference log page 757313, right eng

Fire light on, ref qrh 72.3 light out

With throttle idle oil temp reached

138 Degrees

Corrective action: performed trouble shooting of high

Oil temperature, inspected oil tank

Level, found to be normal, fuel

De-icing s/o valve indicator found in

Open position, inspected #4 and #5

Bearing scavenge tube oil temp

Indicator, both windows on

Indicators are yellow. All trouble

Shooting c/w iaw amm 72-00-02-1-0 and

Sb 5944 rev 5, oil temp indicating sys

Ops check good iaw MD80 amm 79-00-00

No defects noted. Oil sample taken ,

And sent out for analysts iaw MD80

Amm 72-00-02-1-0 figure 109 step 12. See

Log page 757315 for other mx.

Log 757315:

Discrepancy: ref log page 757314, corrective

Action for t/shooting of right eng

High oil temperature continuation

Corrective action: found RH engine igv left aft anti-ice

Duct ruptured . Removed and

Replaced RH engine igv left aft

Anti-ice duct iaw MD80 amm 75-10-02-2-1

See log page 757316 for pneumatic

Pressure test and leak

Check. Removed and replaced right

Engine fuel de-icing shutoff valve

Iaw MD80 amm 73-14-02-2-0. Valve

Operates electrically and position

Indication normal iaw MD80 amm

73-14-02-2-0. See log page 757316 for

Leak check and operational check of

Fuel deicing s/o valve

Log 757316:

Discrepancy: reference log page 757315

Corrective action leak check of

Right engine igv left aft anti ice duct

And operational check and leck

Check of fuel deicing valve

Corrective action: performed leak check of right igv

Antiice duct good iaw mm 36-00-00 and

Mm 71-00-00 performed ops and leak

Check of right eng fuel deiicng valve

Op & lk check good iaw mm 73-14-02 and

71-00-00

As the FAA filed it

LOG 757313:

DISCREPANCY: RIGHT ENG FIRE LIGHT ON REF QRH 72.3

LIGHT OUT WITH THROTTLE IDLE OIL TEMP

REACHED 138 DEGREES

CORRECTIVE ACTION: SEE LOGPAGE 757314 FOR T/S OF RH ENG,SEE

LOGPAGES 757315,757316,757321 AND 757322 FOR

REPLACEMENT OF RH ENG AFT IGV DUCT ,FUEL /AIR HEATER

AIR SHUTOFF VALVE AND MAIN OIL FILTER. OPS & LK

CHECKS GOOD OF RH ENG IGV DUCT ,FUEL /AIR HEATER AIR

SHUTOFF VALVE AND MAIN OIL FILTER. OK FOR SERVICE.

LOG 757314:

DISCREPANCY: REFERENCE LOG PAGE 757313, RIGHT ENG

FIRE LIGHT ON, REF QRH 72.3 LIGHT OUT

WITH THROTTLE IDLE OIL TEMP REACHED

138 DEGREES

CORRECTIVE ACTION: PERFORMED TROUBLE SHOOTING OF HIGH

OIL TEMPERATURE, INSPECTED OIL TANK

LEVEL, FOUND TO BE NORMAL, FUEL

DE-ICING S/O VALVE INDICATOR FOUND IN

OPEN POSITION, INSPECTED #4 AND #5

BEARING SCAVENGE TUBE OIL TEMP

INDICATOR, BOTH WINDOWS ON

INDICATORS ARE YELLOW. ALL TROUBLE

SHOOTING C/W IAW AMM 72-00-02-1-0 AND

SB 5944 REV 5, OIL TEMP INDICATING SYS

OPS CHECK GOOD IAW MD80 AMM 79-00-00

NO DEFECTS NOTED.OIL SAMPLE TAKEN ,

AND SENT OUT FOR ANALYSTS IAW MD80

AMM 72-00-02-1-0 FIGURE 109 STEP 12. SEE

LOG PAGE 757315 FOR OTHER MX.

LOG 757315:

DISCREPANCY: REF LOG PAGE 757314, CORRECTIVE

ACTION FOR T/SHOOTING OF RIGHT ENG

HIGH OIL TEMPERATURE CONTINUATION

CORRECTIVE ACTION: FOUND RH ENGINE IGV LEFT AFT ANTI-ICE

DUCT RUPTURED . REMOVED AND

REPLACED RH ENGINE IGV LEFT AFT

ANTI-ICE DUCT IAW MD80 AMM 75-10-02-2-1

SEE LOG PAGE 757316 FOR PNEUMATIC

PRESSURE TEST AND LEAK

CHECK.REMOVED AND REPLACED RIGHT

ENGINE FUEL DE-ICING SHUTOFF VALVE

IAW MD80 AMM 73-14-02-2-0. VALVE

OPERATES ELECTRICALLY AND POSITION

INDICATION NORMAL IAW MD80 AMM

73-14-02-2-0. SEE LOG PAGE 757316 FOR

LEAK CHECK AND OPERATIONAL CHECK OF

FUEL DEICING S/O VALVE

LOG 757316:

DISCREPANCY: REFERENCE LOG PAGE 757315

CORRECTIVE ACTION LEAK CHECK OF

RIGHT ENGINE IGV LEFT AFT ANTI ICE DUCT

AND OPERATIONAL CHECK AND LECK

CHECK OF FUEL DEICING VALVE

CORRECTIVE ACTION: PERFORMED LEAK CHECK OF RIGHT IGV

ANTIICE DUCT GOOD IAW MM 36-00-00 AND

MM 71-00-00 PERFORMED OPS AND LEAK

CHECK OF RIGHT ENG FUEL DEIICNG VALVE

OP & LK CHECK GOOD IAW MM 73-14-02 AND

71-00-00

Other reports on N862GA · 1

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