# N407FJ: 2000 Dornier 328-300

- Status: Valid registration
- Airframe: [Dornier 328-300](https://openairdocs.org/model/dornier-328-300) (registry code 2990220, 34 seats)
- Engine: [Pratt & Whitney PW300 series](https://openairdocs.org/engine/pratt-whitney-pw300-series) (registry code 52128)
- Data sheets: [TCDS A55NM](https://openairdocs.org/tcds/A55NM) (Deutsche Aircraft GmbH) (OpenAirDocs)
- Serial number: 3157
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 27, 2000
- Certificate issued: May 18, 2006
- Expires: April 30, 2027
- Mode S code: A4C728
- Registered owner: [Ultimate Leasing LLC](https://openairdocs.org/faa-owner/ULTIMATE%20LEASING%20LLC)
- Location: [North Canton, OH](https://openairdocs.org/faa-place/OH/North%20Canton)
- Owner type: LLC
- Owner's area on the map: 40.9034° N, 81.4333° W: Placed by OpenAirDocs at the center of ZIP code 44720, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=407FJ
- Page: https://openairdocs.org/aircraft/N407FJ

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. The registry lists only the engine series, so ADs for every Pratt & Whitney PW300 model are included.

## ADs that may apply (OpenAirDocs): 47 in force

### Matched by airframe (Dornier 328-300)

- [AD 2025-15-05](https://openairdocs.org/ad/2025-15-05): Fuel · Deutsche 328-100 and 328-300. Effective Sep 3, 2025
- [AD 2025-06-08](https://openairdocs.org/ad/2025-06-08): Landing gear · Deutsche 328-100 and 328-300. Effective May 8, 2025
- [AD 2024-19-16](https://openairdocs.org/ad/2024-19-16): Equipment/furnishings · Deutsche 328-100 and 328-300. Effective Nov 26, 2024
- [AD 2023-23-07](https://openairdocs.org/ad/2023-23-07): Flight Controls · Deutsche 328-100 and 328-300. Effective Jan 16, 2024
- [AD 2022-21-07](https://openairdocs.org/ad/2022-21-07): Placards and markings, Equipment/furnishings · Deutsche 328-100 and 328-300. Effective Dec 15, 2022
- [AD 2020-09-13](https://openairdocs.org/ad/2020-09-13): Time Limits/Maintenance Checks · 328 Support Services 328-300. Effective Jun 22, 2020
- [AD 2018-19-13](https://openairdocs.org/ad/2018-19-13): Stabilizers · 328 Support Services 328-100 and 328-300. Effective Oct 31, 2018
- [AD 2018-03-02](https://openairdocs.org/ad/2018-03-02): Fuselage · 328 Support Services 328-300. Effective Feb 23, 2018
- [AD 2017-21-06](https://openairdocs.org/ad/2017-21-06): Fuel · 328 Support Services 328-100 and 328-300. Effective Dec 20, 2017
- [AD 2014-03-15](https://openairdocs.org/ad/2014-03-15): Placards and Markings; and Doors. · 328 Support Services 328-100 and 328-300. Effective Apr 9, 2014
- [AD 2012-07-03](https://openairdocs.org/ad/2012-07-03): Equipment/Furnishings · 328 Support Services 328-100 and 328-300. Effective May 10, 2012
- [AD 2012-01-08](https://openairdocs.org/ad/2012-01-08): Flight Controls · 328 Support Services 328-100 and 328-300. Effective Feb 29, 2012
- [AD 2011-18-13](https://openairdocs.org/ad/2011-18-13): Wings · 328 Support Services 328-100 and 328-300. Effective Oct 25, 2011
- [AD 2011-15-07](https://openairdocs.org/ad/2011-15-07): Stabilizers · 328 Support Services 328-100 and 328-300. Effective Aug 22, 2011
- [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2009-01-06 R1](https://openairdocs.org/ad/2009-01-06-R1): Auxiliary fuel system · 328 Support Services 328-300. Effective Nov 23, 2009
- [AD 2009-18-14](https://openairdocs.org/ad/2009-18-14): Flight controls · 328 Support Services 328-100 and 328-300. Effective Oct 14, 2009
- [AD 2009-10-03](https://openairdocs.org/ad/2009-10-03): Flight controls · 328 Support Services 328-100 and 328-300. Effective May 26, 2009
- [AD 2005-13-04](https://openairdocs.org/ad/2005-13-04): Fuselage drain line · 328 Support Services 328-100 and 328-300. Effective Jul 26, 2005
- [AD 2005-13-03](https://openairdocs.org/ad/2005-13-03): Flight control systems · 328 Support Services 328-100 and 328-300. Effective Jul 26, 2005
- [AD 2005-10-06](https://openairdocs.org/ad/2005-10-06): Left- and right-hand elevator horns · 328 Support Services 328-300. Effective Jun 16, 2005
- [AD 2005-10-02](https://openairdocs.org/ad/2005-10-02): Wing leading edge · 328 Support Services 328-300. Effective Jun 15, 2005
- [AD 2005-05-11](https://openairdocs.org/ad/2005-05-11): Main landing gear (MLG) · 328 Support Services 328-300. Effective Apr 18, 2005
- [AD 2004-22-06](https://openairdocs.org/ad/2004-22-06): Metal oxide varistor (MOV) modules · 328 Support Services 328-100 and 328-300. Effective Dec 2, 2004
- [AD 2004-09-38](https://openairdocs.org/ad/2004-09-38): Ground spoiler assemblies · 328 Support Services 328-300. Effective Jun 15, 2004
- [AD 2004-09-22](https://openairdocs.org/ad/2004-09-22): Ground cooling fan · 328 Support Services 328-300. Effective Jun 15, 2004
- [AD 2004-09-17](https://openairdocs.org/ad/2004-09-17): Rudder spirng tab · 328 Support Services 328-100 and 328-300. Effective Jun 9, 2004
- [AD 2004-09-12](https://openairdocs.org/ad/2004-09-12): Passenger seats · 328 Support Services 328-100 and 328-300. Effective Jun 9, 2004
- [AD 2004-08-18](https://openairdocs.org/ad/2004-08-18): Motive Flow Check Valves · 328 Support Services 328-300. Effective Jun 1, 2004
- [AD 2004-03-16](https://openairdocs.org/ad/2004-03-16): Fire extinguisher control panels · 328 Support Services 328-300. Effective Mar 17, 2004
- [AD 2003-20-02](https://openairdocs.org/ad/2003-20-02): Anti-ice tubing · 328 Support Services 328-300. Effective Nov 4, 2003
- [AD 2003-19-03](https://openairdocs.org/ad/2003-19-03): Nose landing gear (NLG) · 328 Support Services 328-100 and 328-300. Effective Oct 27, 2003
- [AD 2003-05-08](https://openairdocs.org/ad/2003-05-08): Flight Data Recorder (FDR) and Cockpit Voice Recorder (CVR) Impact Switches · 328 Support Services 328-100 and 328-300. Effective Apr 18, 2003
- [AD 2003-03-17](https://openairdocs.org/ad/2003-03-17): Aileron, Elevator, Rudder Trim Tabs, and Rudder Spring Tab Screws · 328 Support Services 328-100 and 328-300. Effective Mar 12, 2003
- [AD 2002-26-21](https://openairdocs.org/ad/2002-26-21): Electrical wire harness · 328 Support Services 328-100 and 328-300. Effective Feb 12, 2003
- [AD 2002-26-06](https://openairdocs.org/ad/2002-26-06): Airplane Flight Manual (AFM) · 328 Support Services 328-300. Effective Jan 17, 2003
- [AD 2002-16-16](https://openairdocs.org/ad/2002-16-16): Actuating cartridge on the auxiliary power unit (APU) · 328 Support Services 328-100 and 328-300. Effective Sep 23, 2002
- [AD 2002-16-13](https://openairdocs.org/ad/2002-16-13): Rudder spring tab · 328 Support Services 328-100 and 328-300. Effective Sep 20, 2002
- [AD 2002-03-15](https://openairdocs.org/ad/2002-03-15): Left- and Right-Hand Potentiometer Levers of the Aileron Flight Control System · 328 Support Services 328-100 and 328-300. Effective Mar 27, 2002
- [AD 2001-26-18](https://openairdocs.org/ad/2001-26-18): Forward Engine Mount Vibration Isolators · 328 Support Services 328-300. Effective Feb 8, 2002
- [AD 2001-13-08](https://openairdocs.org/ad/2001-13-08): Brake Assemblies · 328 Support Services 328-300. Effective Aug 1, 2001
- [AD 2001-12-04](https://openairdocs.org/ad/2001-12-04): Hydraulic Line · 328 Support Services 328-300. Effective Jul 18, 2001
- [AD 2000-26-13](https://openairdocs.org/ad/2000-26-13): Hydraulic Accumulators · 328 Support Services 328-300. Effective Jan 17, 2001
- [AD 2000-21-13](https://openairdocs.org/ad/2000-21-13): Parking Brake · 328 Support Services 328-300. Effective Nov 29, 2000
- [AD 2000-04-23](https://openairdocs.org/ad/2000-04-23): Rudder Spring Tab · 328 Support Services 328-100 and 328-300. Effective Mar 22, 2000
- [AD 98-24-27](https://openairdocs.org/ad/98-24-27): Fire Extinguisher · 328 Support Services 328-100, 328-300, A320-111 and 42 more. Effective Jan 29, 1999
- [AD 94-19-06](https://openairdocs.org/ad/94-19-06): Crew Oxygen Masks · 328 Support Services 328-100, 328-300, 500 and 17 more. Effective Oct 6, 1994

### Matched by engine (Pratt & Whitney PW300 series)

None in force.

### Historical (superseded or no longer in force)

- [AD 2024-03-07](https://openairdocs.org/ad/2024-03-07) (historical): Fuel · Deutsche 328-100 and 328-300. Effective Apr 16, 2024
- [AD 2011-01-07](https://openairdocs.org/ad/2011-01-07) (historical): Flight controls · 328 Support Services 328-100 and 328-300. Effective Feb 9, 2011
- [AD 2009-21-06](https://openairdocs.org/ad/2009-21-06) (historical): Equipment/furnishings. · 328 Support Services 328-100 and 328-300. Effective Nov 20, 2009
- [AD 2009-01-06](https://openairdocs.org/ad/2009-01-06) (historical): Electrical wiring of the fuel pumps · 328 Support Services 328-300. Effective Apr 3, 2009
- [AD 2008-14-16](https://openairdocs.org/ad/2008-14-16) (historical): Passenger door · 328 Support Services 328-100 and 328-300. Effective Aug 21, 2008
- [AD 2008-10-51](https://openairdocs.org/ad/2008-10-51) (historical): Rear trailing edge · 328 Support Services 328-100 and 328-300. Effective Jun 3, 2008
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2005-15-16](https://openairdocs.org/ad/2005-15-16) (historical): Electrical wiring of the fuel pumps · 328-300. Effective Sep 6, 2005
- [AD 2004-09-16](https://openairdocs.org/ad/2004-09-16) (historical): Rudder spring tab lever · 328-100 and 328-300. Effective Jun 9, 2004
- [AD 2001-09-04](https://openairdocs.org/ad/2001-09-04) (historical): Motive Flow Check Valve · 328-300. Effective May 15, 2001
- [AD 96-12-13](https://openairdocs.org/ad/96-12-13) (historical): Honeywell GP-300 Guidance And Display Controller · 328-100 and 328-300. Effective Jun 26, 1996

## Information bulletins (advisory) (2 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N407FJ.

## FAA accident and incident reports

None matched to N407FJ.

## Service difficulty reports (7)

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

- [SDR DTHA2008001](https://openairdocs.org/sdr/DTHA2008001), Feb 11, 2008: OUTFLOW VALVE. DIRTY. EN ROUTE DTW TO CLT AT FL310 UNCOMMANDED CABIN ALTITUDE CLIMB TO 9100'. MAINTENANCE DETERMINED PNEUMATIC OUTFLOW VALVE/FILTER ASSY CONTAMINATED. VALVE AND FILTE
- [SDR CMRR200604011](https://openairdocs.org/sdr/CMRR200604011), Apr 26, 2006: POWER SUPPLY. FAILED. THE NR 1 MFD DISPLAY UNIT REFERENCED HERE IN FAILED DURING TAXI OPERATIONS PRIOR TO FLIGHT. THE SUSPECTED SPECIFIC COMPONENT FAILURE IS THE HIGH VOLTAGE POWER S
- [SDR CMRR200604010](https://openairdocs.org/sdr/CMRR200604010), Apr 26, 2006: POWER SUPPLY. FAILED. THE NR 1 PFD DISPLAY UNIT REFERENCED HERE IN FAILED DURING TAXI OPERATIONS PRIOR TO FLIGHT. THE SUSPECTED SPECIFIC COMPONENT FAILURE IS THE HIGH VOLTAGE POWER S
- [SDR 04214407](https://openairdocs.org/sdr/04214407), Aug 1, 2004: SWITCH. MISINSTALLED. LOW SPEED ABORT DUE TO LOW FUEL PRESSURE MESSAGE. FOUND LEFT JET PUMP SWITCH PUSHED.
- [SDR 03283407](https://openairdocs.org/sdr/03283407), Oct 10, 2003: POWER SUPPLY. DISCHARGED. DURING INSPECTION THE EMERGENCY LIGHTS NEAR SEATS 4 AND 5 B AND C WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY.
- [SDR 03031407](https://openairdocs.org/sdr/03031407), Jan 31, 2003: SMOKE. DETECTED. AFTER TAKE OFF, CREW REPORTED HEAVY SMOKE IN COCKPIT. AN EMERGENCY WAS DECLARED WITH ATC AND AIRCRAFT RETURNED TO POINT OF DEPARTURE. AIRCRAFT LANDED WITHOUT AN
- [SDR 02035407](https://openairdocs.org/sdr/02035407), Feb 4, 2002: STARTER GEN. FAILED. DURING CRUISE FROM CHS TO LGA RT ENGINE VIBRATION ICON ILLUMINATED INDICATING VIBRATIONS >.2" UP TO 1.3" PER SECOND. FLIGHT CREW COMPLIED WITH QRH AND DIVERTED 

## STCs that may be installed (OpenAirDocs) (22)

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 (Dornier 328-300)

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST04508NY](https://openairdocs.org/stc/ST04508NY): Installation of ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST03654NY](https://openairdocs.org/stc/ST03654NY): Installation of Control Horn Anti-Icers. SMR Technologies Inc
- [STC ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC
- [STC ST10933SC](https://openairdocs.org/stc/ST10933SC): Installation of an Executive Interior and Reduction in Maximum Zero Fuel Weight form 28,814 to 28,279 pounds. VT DRB Aviation Consultants
- [STC ST10940SC](https://openairdocs.org/stc/ST10940SC): Installation of an Executive Interior and Maximum Zero Fuel Weight limitation reduction from 28,814 pounds (13,070 kg) to 28,279 pounds (12,854 kg). VT DRB Aviation Consultants
- [STC ST01181SE](https://openairdocs.org/stc/ST01181SE): Installation of increased security cockpit door. Cascade Aviation Services Inc
- [STC ST04169AT](https://openairdocs.org/stc/ST04169AT): Installation of EL/M-2022A(V) 3 Multimode Surveillance Radar System (MSRS). TKC Aerospace, Inc
- [STC ST03394CH](https://openairdocs.org/stc/ST03394CH): Installation of a cabin interior alteration. TKC Aerospace, Inc
- [STC ST00664DE](https://openairdocs.org/stc/ST00664DE): Replacement of existing 33-place cabin configuration with 12 passenger executive configeratin. Zenith Aviation Inc
- [STC ST02485LA](https://openairdocs.org/stc/ST02485LA): Installation of FLIR turret, KU-Band antenna, and radome. TKC Aerospace, Inc
- [STC ST02636NY](https://openairdocs.org/stc/ST02636NY): Installation of Self Illuminating Floor Path Marking System. Lufthansa Technik AG
- [STC ST02132LA](https://openairdocs.org/stc/ST02132LA): Installation of Cabin Interior Noise Reduction Kit. Aircraft Technical Development Inc. dba Aerocon Engineering Company
- [STC ST00188BO](https://openairdocs.org/stc/ST00188BO): Installation of Pratt & Whitney Engine Services, Inc. Data Transmission Unit. Pratt & Whitney Engine Services Inc
- [STC SA09496AC](https://openairdocs.org/stc/SA09496AC): Conversion of the lavatory water supply system from a gravity feed to a pressure system by adding a pump, a small hot water tank and control system and by replacing the single lever faucet with an infrared activated faucet with hot and cold capability in accordance with Fairchild Aircraft Drawing SATA380G0010, Water System Mod -- Hot/Cold, Revision B dated November 22, 1999, or later FAA approved revision. AvCraft Aviation LLC
- [STC SA09839SC](https://openairdocs.org/stc/SA09839SC): Installation of Teledyne Telelink Data Link System. Aircraft Systems & Mfg

## Related

- Other Dornier 328-300 aircraft: https://openairdocs.org/model/dornier-328-300/aircraft.md
- The Pratt & Whitney PW300 series engine: https://openairdocs.org/engine/pratt-whitney-pw300-series.md

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