# N341ML: 2013 Polskie Zaklady Lotnicze Spzoo PZL M28 05 - Status: Valid registration - Airframe: [Polskie Zaklady Lotnicze Spzoo PZL M28 05](https://openairdocs.org/model/polskie-zaklady-lotnicze-spzoo-pzl-m28-05) (registry code 7270100, 21 seats) - Engine: [Pratt & Whitney Canada PT6A-65B](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-65b) (registry code 52115) - Data sheets: [TCDS A56CE](https://openairdocs.org/tcds/A56CE) (Polskie Zakłady Lotnicze Sp. z o.o.), [TCDS E4EA](https://openairdocs.org/tcds/E4EA) (Pratt & Whitney Canada Corp.) (OpenAirDocs) - Serial number: AJE00341 - Year built: 2013 - Type: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: January 25, 2014 - Certificate issued: April 7, 2020 - Expires: April 30, 2030 - Mode S code: A3C223 - Registered owner: [Classic Rotors Museum](https://openairdocs.org/faa-owner/CLASSIC%20ROTORS%20MUSEUM) - Location: [Ramona, CA](https://openairdocs.org/faa-place/CA/Ramona) - Owner type: Corporation - Owner's area on the map: 33.0404° N, 116.8301° W: Placed by OpenAirDocs at the center of ZIP code 92065, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=341ML - Page: https://openairdocs.org/aircraft/N341ML From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 5 in force ### Matched by airframe (Polskie Zaklady Lotnicze Spzoo PZL M28 05) - [AD 2025-21-51](https://openairdocs.org/ad/2025-21-51): Rudder Control System · Polskie Zaklady Lotnicze Spolka zo.o. PZL M28 05. Effective Nov 19, 2025 - [AD 2025-18-11](https://openairdocs.org/ad/2025-18-11): Placards and Markings · Polskie Zaklady Lotnicze Spolka zo.o. PZL M28 05. Effective Oct 29, 2025 - [AD 2020-22-12](https://openairdocs.org/ad/2020-22-12): Fuel Tank · Polskie Zaklady Lotnieze Spolka zo.o PZL M28 05. Effective Dec 8, 2020 ### Matched by engine (Pratt & Whitney Canada PT6A-65B) - [AD 2004-25-18](https://openairdocs.org/ad/2004-25-18): Propeller governor assemblies · Pratt & Whitney Canada PT6A-60A and PT6A-65B. Effective Jan 18, 2005 - [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997 ## Information bulletins (advisory) (2 in force) - [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015 - [SAIB CE-03-24](https://openairdocs.org/saib/CE-03-24): . Issued Feb 19, 2003 ## NTSB investigations None matched to N341ML. ## FAA accident and incident reports None matched to N341ML. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## STCs that may be installed (OpenAirDocs) (20) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Polskie Zaklady Lotnicze Spzoo PZL M28 05) - [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH - [STC SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". Genesys Aerosystems Inc - [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS - [STC SA00107MC](https://openairdocs.org/stc/SA00107MC): Installation of ruggedized utility floor system, including liners and seals over the existing floor panels. Sierra Nevada Corporation - [STC SA00109MC](https://openairdocs.org/stc/SA00109MC): Installation of provisions for a paratrooper retrieval system. Sierra Nevada Corporation - [STC SA00053MC](https://openairdocs.org/stc/SA00053MC): Installation of cabin and cockpit lighting features. Sierra Nevada Corporation - [STC SA00040MC](https://openairdocs.org/stc/SA00040MC): Installation of non-required communications equipment in the cabin section and communication control panels and audio management system in the cockpit. Sierra Nevada Corporation - [STC SA00072MC](https://openairdocs.org/stc/SA00072MC): Installation of a cargo loading system. Sierra Nevada Corporation - [STC SA00093MC](https://openairdocs.org/stc/SA00093MC): Installation of Provisions and Safe Carriage of components for a Combat Hazard Aircraft Survivability Equipment System. Sierra Nevada Corporation - [STC SA00096MC](https://openairdocs.org/stc/SA00096MC): Installation of a gravel guard kit. Sierra Nevada Corporation - [STC SA00074MC](https://openairdocs.org/stc/SA00074MC): Installation of a dual mode landing light system in accordance with Master Drawing List, M28 Dual Mode Landing Light, Document Number MDL-02036700, Revision C, dated January 16, 2012, FAA approved February 29, 2012 or later FAA approved revision. Sierra Nevada Corporation - [STC SA00067MC](https://openairdocs.org/stc/SA00067MC): Establishment of a ground minimum control speed operating limitation in accordance with Airplane Flight Manual Supplement Document Number 0223-00-9007, Revision A, dated October 31, 2011, or later FAA approved revision. Sierra Nevada Corporation - [STC SA00050MC](https://openairdocs.org/stc/SA00050MC): Installation of provisions for wingtip mounted infrared sensors. Sierra Nevada Corporation ### Approved for the engine (Pratt & Whitney Canada PT6A-65B) - [STC SE00014EN](https://openairdocs.org/stc/SE00014EN): Installation of the Pratt & Whitney Engine Services, Inc. CrossCheck Engine Monitor Kit P/N HUMS-K-071-1, Rev. A on the specified PT6A engine models and kit P/N HUMS-K-071-2 on the specified A250 engine models. Pratt & Whitney Engine Services Inc - [STC SE00020EN](https://openairdocs.org/stc/SE00020EN): Installation of the Pratt & Whitney Engine Services, Inc. TrendCheck/ TrendCheck Plus Engine Monitor Kit P/N TREND-K-010-1. Pratt & Whitney Engine Services Inc - [STC SE8652SW](https://openairdocs.org/stc/SE8652SW): Installation of a flexible hose from the Propeller Primary Governor to the Fuel Control Unit. Air Tractor Inc - [STC SE615GL](https://openairdocs.org/stc/SE615GL): Incorporation of a fuel flow transducer. Shadin Avionics - [STC SE01805NY](https://openairdocs.org/stc/SE01805NY): Installation of Fuel Nozzle Adapters using studs and nuts. Atlantic Turbines International Inc - [STC SE09257SC](https://openairdocs.org/stc/SE09257SC): Convert P&W Engine Models PT6A-15AG, -27, and -28, into PT6A-34 configuration. Covington Aircraft Engines, Inc - [STC SE659NE](https://openairdocs.org/stc/SE659NE): Installation of oil tank filler neck check valve, P/N TSA-76A. Aviation Components Support ## Related - Other Polskie Zaklady Lotnicze Spzoo PZL M28 05 aircraft: https://openairdocs.org/model/polskie-zaklady-lotnicze-spzoo-pzl-m28-05/aircraft.md - The Pratt & Whitney Canada PT6A-65B engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-65b.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.