ESN 720189 (03172026).pdf

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Purchase Boeing ONE (1) 737-700 or 737-800 Aircraft with Trade-in of 737-400
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15M30026RA3700011
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This is a CFM56-3 Life Limited Parts List for a jet engine with serial number 720189. The document provides a comprehensive inventory of critical rotating and structural components subject to operational cycle limitations, dated March 17, 2026, and certified by Rob Hankins.

The list identifies 18 life-limited parts across multiple engine sections including the booster spool, fan disk, fan shaft assembly, high-pressure compressor (HPC) components, high-pressure turbine (HPT) components, and low-pressure turbine (LPT) components. Each part is tracked with specific identifiers: part number (P/N), serial number (S/N), time since new (TSN) of 78,593.1 hours, and cycles since new (CSN) of 64,406 cycles. The document establishes individual cycle limits for three operational categories (A, B, and C) for each component, ranging from 15,000 to 30,000 cycles depending on the part and operational category. Remaining service life varies by component and category, with some parts such as the booster spool and fan shaft assembly having 16,863 remaining cycles across all categories, while others such as the HPC rear air seal and HPT front air seal have more restricted remaining cycles. This inventory document serves as a critical maintenance record for tracking component airworthiness and scheduling overhaul or replacement activities to ensure compliance with manufacturer-imposed life limits.

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CFM56-3 Life Limited Parts List

ENGINE S/N: 720189 TSN: 78,593.1 CSN: 64,406

IIN

DESCRIPTION

P/N

S/N

TSN

CSN

OPERATING CYCLES CYCLE LIMITS REMAINING CYCLES REMARKS

A B C A B C A B C

211 BOOSTER SPOOL 335-009-306-0 DD334413 18 766.1 13 137 8 505 3 154 1 478 30 000 30 000 30 000 16 863 16 863 16 863 213 FAN DISK 335-014-511-0 BC658113 18 766.1 13 137 8 505 3 154 1 478 30 000 24 900 20 100 15 489 12 855 10 377

221 FAN SHAFT ASSY 335-006-414-0 DD935471 18 766.1 13 137 8 505 3 154 1 478 30 000 30 000 30 000 16 863 16 863 16 863

312 HPC FRT SHAFT 1275M37P02 GWN0FR66 18 766.1 13 137 8 505 3 154 1 478 20 000 20 000 20 000 6 863 6 863 6 863 313 HPC SPOOL STG 1 - 2 1589M66G02 GWN0FM24 18 766.1 13 137 8 505 3 154 1 478 20 000 20 000 20 000 6 863 6 863 6 863 314 HPC DISK STG 3 1590M59P01 XAEH5410 18 766.1 13 137 8 505 3 154 1 478 20 000 20 000 20 000 6 863 6 863 6 863 315 HPC SPOOL STG 4 - 9 1588M89G03 GWN0FKM9 18 766.1 13 137 8 505 3 154 1 478 20 000 20 000 15 800 6 470 6 470 5 111 316 HPC REAR AIR SEAL 1319M25P02 GFF5DMMK 18 766.1 13 137 8 505 3 154 1 478 20 000 18 000 15 000 6 019 5 417 4 514

521 HPT FRONT SHAFT 1385M90P04 XAEJ3368 18 766.1 13 137 8 505 3 154 1 478 20 000 17 300 17 000 6 109 5 285 5 193 522 HPT FRONT AIR SEAL 1282M72P05 XAEJ5148 18 766.1 13 137 8 505 3 154 1 478 20 000 15 800 15 100 5 544 4 380 4 186 525 HPT ROTOR DISK 1475M29P03 GWN05HE8 18 766.1 13 137 8 505 3 154 1 478 20 000 18 500 16 600 6 304 5 831 5 232 526 HPT REAR SHAFT 1864M91P02 TMT2B478 18 766.1 13 137 8 505 3 154 1 478 20 000 20 000 20 000 6 863 6 863 6 863

542 LPT DISK STG 1 301-331-126-0 BC908657 18 766.1 13 137 8 505 3 154 1 478 25 000 25 000 25 000 11 863 11 863 11 863 543 LPT DISK STG 2 301-331-227-0 BC917091 18 766.1 13 137 8 505 3 154 1 478 25 000 25 000 25 000 11 863 11 863 11 863 544 LPT DISK STG 3 301-331-322-0 BC878743 18 766.1 13 137 8 505 3 154 1 478 25 000 25 000 25 000 11 863 11 863 11 863 545 LPT DISK STG 4 301-331-429-0 DD687065 18 766.1 13 137 8 505 3 154 1 478 25 000 25 000 25 000 11 863 11 863 11 863 546 LPT CONICAL SPT 305-056-116-0 DD686285 18 766.1 13 137 8 505 3 154 1 478 25 000 25 000 25 000 11 863 11 863 11 863

551 LPT SHAFT 301-330-066-0 DD569934 18 766.1 13 137 8 505 3 154 1 478 30 000 30 000 30 000 16 863 16 863 16 863 552 LPT STUB SHAFT 301-330-626-0 DD359841 18 766.1 13 137 8 505 3 154 1 478 25 000 25 000 25 000 11 863 11 863 11 863

REMARKS: NAME: Rob Hankins DATE: March 17, 2026

Electronically produced document therefore valid without signature

2026-03-17T13:55:21-0500
ROB HANKINS

File details come from the government source that posted it. Updated .