AIRFRAME:

Production year 1993

Hours Since New: 49,377:14 Total Landings: 48,109

Airplane TCDS: EASA.IM.A.120 / Issue 15 dated 04 March 2024

FAA A16WE / Rev. 75 dated 17 May 2024

ENGINES: Models:      CFM56-3C

Engine(s) TCDS: EASA E.066 / Issue 2 dated 17 March 2023

FAA E2GL / Rev. 13 dated 17 February 2022

APU: GTCP85-129K

Remaining Hours to H.S.I.:  4,701 Hours

LANDING GEAR:

L/H MLG P/N 65-73761-

R/H MLG P/N 65-73761-122

NLG P/N 65-73762-21

Last Overhaul 2019 – Life 21,000 Cycles / 10 years

The current maintenance program is structured with a transition schedule of the landing gear overhaul calendar limit procedures to a CPCP basic task phase-in inspection as per the provisions of Boeing Doc. Ref. D6-38728 (Section 10 – Corrosion Prevention and Control Program).

Ref. Report – Assessment of technical status of Main and Nose Landing Gear assemblies installed on Boeing 737-4H6 aircraft MSN 26444 and transition of overhaul calendar limit to CPCP periodical inspections.

AVIONICS:

Smiths Airdata Computer 501FAD1-1

Smiths Flight Management Computer 2907A

Honeywell Flight Control Computer SP-300

Smiths Auto Throttle Computer 755SUE2-4

Collins VHF Comm (8.33 kHz) VHF-700

Collins VHF Nav Receiver 51RV-4B/5B

Collins HF Transceiver HFS-700

Teledyne ACARS Management Unit 2229385-45

Honeywell Cockpit Voice Recorder 980-6020-001

Honeywell Flight Data Recorder 980-4700-001

Collins DME Transceiver 860-E5

Collins ADF Receiver 51Y-7

Collins Marker/Receiver 51-Z4

Collins WX Radar Transceiver WRT-701X

Honeywell Inertial Reference Unit (IRU) HG1050AD/AE

Honeywell EGPWS Computer 965-0976-060-222-222

Collins ATC Enhanced Mode S Transponder TPR-720  Allied Signal TCAS Processor (version 7) TPA-81A Triple Frequency ELTs – ELTA / Honeywell ADT406AF/AP

MODIFICATIONS/STCs:

STC ST00389SE

Honeywell Enhanced Ground Proximity Warning System (EGPWS) STC ST00389SE (including Runway Awareness and Advisory System – RAAS)

STC ST00899AT

AlliedSignal Trafic Collision Advisory System (TCAS II)

STC ST01308CH

406 MHz Emergency Locator Transmitter (ELT)

STC ST01335LA

Enhanced Security Cockpit Door

STC ST00971SE-D

Cockpit Door 8 Surveillance System (CDSS)

NOTE: Other modifications as per the Service Bulletin Modifications List.

WEIGHTS:

Max. Ramp: 63,049 kg.

Max. Take-Off: 62,822 kg.

Max. Landing: 54,884 kg.

Max. Zero Fuel: 51,255 kg.

INTERIOR:

144 seats mixed interior arrangement 16 Business seats

128 Economy seats

Maintenance Status:

All due maintenance done 2024 – operational reserve life provided for 1,000 flight hours / 1,000 cycles and 12 months.

Maintenance packages performed: periodic checks (A checks, C check), Out-of-Phase inspections, Airworthiness Directives compliance (up to FAA Large Aircraft Biweekly 2024-21), life limited components restoration.

Note: All maintenance requirements as per the Boeing 737-300/400/500 Maintenance Planning Data (MPD) Document D6-38278 – March 2024.