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N108MS

Open the Markdown

2002 Boeing 737-7BC · CFM International CFM56 series

Open in FAA registry

© OpenStreetMap
Registered owner
Yona Aviation II LLC
Location
Las Vegas, NV
Owner type
LLC
Serial number
33102
Year built
2002
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
June 11, 2004
Certificate issued
May 1, 2003
Expires
June 30, 2027
Mode S code
A02390
Boeing 737-7BCAirframe model · 149 seats · 2 engines · 9 registeredEngine modelCFM International CFM56 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56 model are included below.

On this page

Airworthiness directives that may apply · 55

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1985In forceSuperseded2026
See all 71 ADs

Information bulletins that may apply · 4

Advisory, not mandatory.

Historical bulletins · 5
SAIB NE-13-33R1Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle VanesIssued Jun 24, 2013SAIB NE-13-33Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle VanesIssued May 13, 2013SAIB NE-08-17R2Turbine Section - Propulsion Technology LLC Unapproved RepairIssued Mar 7, 2011SAIB NE-08-17R1Propulsion Technology LLC Unapproved RepairIssued May 22, 2008SAIB NE-08-17Propulsion Technologies International Unapproved RepairIssued May 14, 2008

NTSB investigations

No NTSB investigations matched to N108MSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 737-7BC aircraft
Investigations on N108MS not matched to an aircraft · 1

They name N108MS, but no registry record covers the date, the aircraft registered then was built later, or the investigation describes another aircraft.

NTSB CHI02LA020Accident · No injuriesLimited investigationFinal reportMaule MX-7 · Middleton, WIthe pilot's improper rotation and failure to maintain directional control during takeoff. Additional factors were the crosswind and the soft terrain.Nov 6, 2001 · Substantial damage

FAA incident reports

No FAA accident or incident reports matched to N108MSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing 737-7BC aircraft
Reports on N108MS not matched to an aircraft · 2

They name N108MS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

Accident 20011106030519AMaule MX7160 · Madison, WI(-23) Pilot stated he was taking off on runway 30 for a local pleasure flight. He stated the wind was 200 degrees at eleven knots. He stated that the aircraft lifted off prematurely, and then started drifting to the right. He stated the aircraft settled back…Nov 6, 2001 · No damageIncident 19951212042889IMaule MX7160 · Vicksburg, MSNarrative: (there are no remarks nor narrative.)Dec 12, 1995 · Minor damage

Service difficulty reports · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR TX22003F00000Starter · failedNPRM STATES TO REMOVE PART NUMBERS AND SERIES NUMBER AND REPLACE THESE ITEMS WITH A SERIES 7 OR GREATER. THE SERIES 7 UNIT WHEN INSTALLED FAILED. WHEN AN APU START WAS ATTEMPTED USING A SERIES 7 START CONVERTER UNIT. THE NEW UNIT EXPERIENCED A COMPLETE ELECApr 15, 2003 · N108MS · Boeing 737100 · APU Start/Ignition System

STCs that may be installed · 7

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

Engine · CFM International CFM56 series

STC SE04840NYInstallation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engineKilroy Aviation LLC · Lists CFM56-7B20STC SE03036CHApplication of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision.Delta Air Lines Inc. · Lists CFM56-7B20STC SE00032ENInstallation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Fan/Booster Module.Pratt & Whitney · Lists CFM56-3STC SE00033ENInstallation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Compressor ModulePratt & Whitney · Lists CFM56-3STC SE00034ENInstallation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Turbine ModulePratt & Whitney · Lists CFM56-3STC SE00035ENInstallation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Low Pressure Turbine ModulePratt & Whitney · Lists CFM56-3STC SE00822CHInstall AeroControlex P/N 2604880-001 variable stator feedback control cable and P/N 2604880-002 variable bleed valve feedback control cable on CFM International engines.AeroControlex Group TransDigm Inc · Lists CFM56-2