Service difficulty report · Sensor · Boeing 737724

Difficulty date
October 31, 2024
Submitted
November 4, 2024
Operation
Air carrier
Aircraft
N24715
Make and model
Boeing 737724
Aircraft serial
28786
Aircraft time
81,392 hours, 29,734 cycles
Part
Sensor
Condition
Faulty
Location
Nr 1 Engine
Part time
20,826 hours, 16,922 cycles
Stage of operation
CL
How discovered
O
Nature of condition
J
Precautionary procedure
A

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

L ENG BLEED PRESSURE LOST THEN FLUCUATED ABNORMALY WITH THRUST C HANGES R&R L ENG BLEED AIR OVERTEMP SENSOR, REF AMM 36-11-05 PARTS USED: 29-3611-9-9001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1392663 SN OFF 6451 SENSOR, BLEED A OFF 29-3611-9-9001 6451 ON 29-3611-9-9001 6820 R&R ENG BLEED AIR REGULATOR REF AMM 36-11-03 PARTS USED: 29-3611-9-0005,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1392518 SN OFF 0876 REGULATOR, BLEE OFF 29-3611-9-0005 0876 ON 29-3611-9-0005 5494 R&R L ENG HI STAGE RWGULATOR REF AMM 36-11-07 PARTS USED: 29-3611-9-0006,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1334877 SN OFF 5849 REGULATOR, HI S OFF 29-3611-9-0006 5849 ON 29-3611-9-0006 4775 R&R L ENG HIGH STAGE VALVE REF AMM 36-11-06 PARTS USED: 29-3611-9-0002,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1335230 SN OFF 1444 VALVE, HIGH STA OFF 29-3611-9-0002 1444 ON 29-3611-9-0002 4920 COMPLETED A BLEED AIR HEALTH CHECK REFERENCE: 36-11-00/501. SYS TEM PASSED TESTING - AFTER REVIEW OF CREW WRITEUP BEFORE RUNNING TO CONFIRM ELECTED TO REPLACE THE OVERTEMP SENSOR 450 AND BAR C OMPLETED ENGINE RUN AND VERIFIED PRESSURE SPLIT AT IDLE LEFT ENG INE WELL BELOW NORMAL LIMITS. BUMPED ENGINE UP TO CHANGE OVER S ETTING AND BLEEDS MATCHED UP. SHUT THE ENGINE BACK DOWN REPLACE D THE HS VALVE AND HS REGULATOR RAN ENG AGAIN THIS TIME AT IDLE BLEEDS MATCHED UP AND WAS WITHIN THE AMM PARAMETERS - THIS ITEM CLOSED.