# N508CF: 2001 Agusta A109E

- Status: Valid registration
- Airframe: Agusta A109E (registry code 0260101, TCDS H7EU (OpenAirDocs match))
- Engine: Pratt & Whitney Canada PW206C (registry code 52160, TCDS E42NE (OpenAirDocs match))
- Serial number: 11103
- Year built: 2001
- Type: Rotorcraft
- Airworthiness: Standard, normal
- Airworthiness date: January 23, 2013
- Certificate issued: June 5, 2024
- Expires: June 30, 2031
- Mode S code: A657E0
- Registered owner: Aerotrust Services Corp Trustee
- Location: Wilmington, DE
- Owner's area on the map: 39.7376° N, 75.6671° W: Placed by OpenAirDocs at the center of ZIP code 19808, within about 2 miles (OpenAirDocs)
- Page: https://openairdocs.org/aircraft/N508CF

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 matched by airframe (Agusta A109E) (OpenAirDocs)

- [AD 2026-17-07](https://openairdocs.org/ad/2026-17-07): Main rotor mast/swashplate · Leonardo A109A, A109A II, A109C and 6 more. Effective Oct 2, 2026
- [AD 2026-09-09](https://openairdocs.org/ad/2026-09-09): Fuselage structure · Leonardo A109E and A109S. Effective Jun 17, 2026
- [AD 2025-18-01](https://openairdocs.org/ad/2025-18-01): Main Rotor Head · Leonardo A109E, A109S, AW109SP and 2 more. Effective Sep 25, 2025
- [AD 2025-09-10](https://openairdocs.org/ad/2025-09-10): Extinguishing System · Leonardo A109E, A109S and AW109SP. Effective Jun 16, 2025
- [AD 2025-07-07](https://openairdocs.org/ad/2025-07-07): Main Rotor Blades · Leonardo A109C, A109E, A109S and 1 more. Effective May 23, 2025
- [AD 2025-03-03](https://openairdocs.org/ad/2025-03-03): Cabin Equipment/Furnishings · Leonardo A109E, A109K2, A109S and 4 more. Effective Feb 19, 2025
- [AD 2024-15-11](https://openairdocs.org/ad/2024-15-11): Tail Rotor System · Leonardo A109C, A109E, A109K2 and 2 more. Effective Oct 21, 2024
- [AD 2023-25-08](https://openairdocs.org/ad/2023-25-08): Main Rotor System · Leonardo A109E, A109S, AW109SP and 2 more. Effective Feb 2, 2024
- [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023
- [AD 2023-01-02](https://openairdocs.org/ad/2023-01-02): Emergency Equipment · Apical Industries, Inc. Emergency Float Kit (STC SR01812LA). Effective Feb 17, 2023
- [AD 2022-07-11](https://openairdocs.org/ad/2022-07-11): Tail Rotor System · Leonardo A109C, A109K2, A109E and 2 more. Effective May 5, 2022
- [AD 2022-05-10](https://openairdocs.org/ad/2022-05-10): Cabin Equipment/Furnishings · Airbus Helicopters AS332L, AS332L1, AS332L2 and 57 more. Effective Apr 20, 2022
- [AD 2021-24-11](https://openairdocs.org/ad/2021-24-11): Main Landing Gear Strut/Axle/Truck · Leonardo A109E, A109S and AW109SP. Effective Jan 14, 2022
- [AD 2021-22-10](https://openairdocs.org/ad/2021-22-10): Tail Rotor Gearbox · Leonardo A109E. Effective Dec 27, 2021
- [AD 2021-21-03](https://openairdocs.org/ad/2021-21-03): Rotorcraft Flight Control, Rotorcraft Servo System · Leonardo A109A, A109A II, A109C and 6 more. Effective Dec 10, 2021
- [AD 2021-17-10](https://openairdocs.org/ad/2021-17-10): Main Rotor Brake · Leonardo A109A, A109A II, A109C and 4 more. Effective Sep 7, 2021
- [AD 2021-07-05](https://openairdocs.org/ad/2021-07-05): Main Rotor Blades · Leonardo A109C, A109E and A109K2. Effective Apr 8, 2021
- [AD 2020-21-21](https://openairdocs.org/ad/2020-21-21): Main Rotor Head · Leonardo A109E, A109S, A119 and 2 more. Effective Nov 24, 2020
- [AD 2020-20-02](https://openairdocs.org/ad/2020-20-02): Extinguishing System · Leonardo A109E, A109S and AW109SP. Effective Nov 3, 2020
- [AD 2020-15-16](https://openairdocs.org/ad/2020-15-16): Tail Rotor Drive System · Leonardo A109E, A109K2, A109S and 3 more. Effective Aug 27, 2020
- [AD 2018-16-08](https://openairdocs.org/ad/2018-16-08): Rotorcraft Cooling Fan System · Leonardo A109E, A109S and AW109SP. Effective Aug 20, 2018
- [AD 2018-06-51](https://openairdocs.org/ad/2018-06-51): Main Rotor Mast/Swashplate · Agusta A109A, A109A II, A109C and 6 more. Effective Jun 7, 2018
- [AD 2018-07-02](https://openairdocs.org/ad/2018-07-02): Main Rotor Blades · Agusta A109E, A109S, A119 and 2 more. Effective Apr 13, 2018
- [AD 2016-18-18](https://openairdocs.org/ad/2016-18-18): Tail Rotor Drive Shaft · Agusta A109A, A109A II, A109C and 4 more. Effective Oct 20, 2016
- [AD 2015-11-08](https://openairdocs.org/ad/2015-11-08): Tail Rotor System · Agusta A109C, A109E, A109K2 and 2 more. Effective Jun 24, 2015
- [AD 2015-05-52](https://openairdocs.org/ad/2015-05-52): Tail Rotor Controls · Agusta A109, A109A, A109A II and 7 more. Effective Apr 29, 2015
- [AD 2014-23-02](https://openairdocs.org/ad/2014-23-02): Main Rotor Gearbox · Agusta A109E, A109K2, A119 and 1 more. Effective Dec 26, 2014
- [AD 2014-11-07](https://openairdocs.org/ad/2014-11-07): Main Rotor System · Agusta A109A, A109A II, A109C and 6 more. Effective Jun 18, 2014
- [AD 2014-09-01](https://openairdocs.org/ad/2014-09-01): Tail Rotor · Agusta A109C, A109E, A109K2 and 1 more. Effective Jun 5, 2014
- [AD 2013-16-21](https://openairdocs.org/ad/2013-16-21): Tail Rotor Blades · Agusta A109E. Effective Oct 30, 2013
- [AD 2013-20-51](https://openairdocs.org/ad/2013-20-51): Tail rotor system · Agusta A109A, A109A II, A109C and 6 more. Effective Oct 25, 2013
- [AD 2013-06-51](https://openairdocs.org/ad/2013-06-51): Equipment/Furnishings · Agusta A109, A109A, A109A II and 43 more. Effective Jul 15, 2013
- [AD 2013-05-22](https://openairdocs.org/ad/2013-05-22): Tail rotor pitch control link assembly · Agusta A109, A109A, A109A II and 5 more. Effective Apr 30, 2013
- [AD 2012-23-02](https://openairdocs.org/ad/2012-23-02): Powerplant system · Agusta A109E and A109S. Effective Jan 16, 2013
- [AD 2010-20-21](https://openairdocs.org/ad/2010-20-21): Circuit breaker · Agusta A109E. Effective Nov 9, 2010
- [AD 2009-12-07](https://openairdocs.org/ad/2009-12-07): Cargo hook lever · Agusta A109E, A109S, A119 and 1 more. Effective Jul 17, 2009
- [AD 2008-14-05](https://openairdocs.org/ad/2008-14-05): Tail rotor control · Agusta A109E and A119. Effective Aug 21, 2008
- [AD 2008-12-11](https://openairdocs.org/ad/2008-12-11): Emergency door release · Agusta A109E, A109S and A119. Effective Jul 1, 2008
- [AD 2005-12-01](https://openairdocs.org/ad/2005-12-01): Overhead panel assembly · Agusta A109E. Effective Jul 13, 2005
- [AD 2005-09-07](https://openairdocs.org/ad/2005-09-07): Fitting attachment bolt · Agusta A109E. Effective Jun 13, 2005
- [AD 2004-11-06](https://openairdocs.org/ad/2004-11-06): Electrical System of the Windshield Wipers · Agusta A109E. Effective Jul 9, 2004
- [AD 2004-02-03](https://openairdocs.org/ad/2004-02-03): Passenger compartment sliding door · Agusta A109E. Effective Mar 4, 2004
- [AD 2003-26-04](https://openairdocs.org/ad/2003-26-04): Rod-end of Main Rotor Head Damper · Agusta A109E. Effective Jan 15, 2004
- [AD 2002-21-12](https://openairdocs.org/ad/2002-21-12): Main transmission assembly · Agusta A109E. Effective Nov 26, 2002
- [AD 2002-20-05](https://openairdocs.org/ad/2002-20-05): Rescue hoists · Agusta A109, A109A, A109A II and 31 more. Effective Nov 7, 2002
- [AD 2001-20-04](https://openairdocs.org/ad/2001-20-04): Passenger Compartment Sliding Doors · Agusta A109E. Effective Nov 7, 2001
- [AD 2001-17-16](https://openairdocs.org/ad/2001-17-16): Tail Rotor Blade · Agusta A109E. Effective Sep 13, 2001
- [AD 2000-25-09](https://openairdocs.org/ad/2000-25-09): Exhaust Ejector Locking System · Agusta A109E. Effective Feb 2, 2001
- [AD 2000-26-11](https://openairdocs.org/ad/2000-26-11): Tail Rotor Blades · Agusta A109E. Effective Jan 16, 2001
- [AD 2000-20-06](https://openairdocs.org/ad/2000-20-06): Aft Support Fitting · Agusta A109E and A109K2. Effective Oct 17, 2000
- [AD 2000-17-52](https://openairdocs.org/ad/2000-17-52): Main Rotor Rotating Scissors Assembly · Agusta A109E. Effective Oct 10, 2000
- [AD 78-24-02](https://openairdocs.org/ad/78-24-02): Main Transmission · Agusta A109, A109A, A109A II and 3 more. Effective Nov 24, 1978

Historical (superseded or no longer in force): AD 2021-23-04, AD 2021-23-13, AD 2021-17-18, AD 2018-07-08, AD 2014-02-08, AD 2007-26-52, AD 2001-24-07 R1, AD 2002-25-51, AD 2002-17-51, AD 2002-14-51, AD 2001-24-07, AD 2000-25-54, AD 99-03-10, AD 98-19-04

## ADs matched by engine (Pratt & Whitney Canada PW206C) (OpenAirDocs)

- [AD 2013-03-21](https://openairdocs.org/ad/2013-03-21): Power turbine (PT) disks · Pratt & Whitney Canada PW206B, PW206B2, PW206C and 5 more. Effective Mar 26, 2013
- [AD 2009-03-05](https://openairdocs.org/ad/2009-03-05): Compressor turbine (CT) disc bore · Pratt & Whitney Canada PW206A, PW206B, PW206B2 and 5 more. Effective Mar 27, 2009
- [AD 2004-14-22](https://openairdocs.org/ad/2004-14-22): Automatic low-cycle- fatigue (LCF) · Pratt & Whitney Canada PW206B, PW206C, PW206E and 2 more. Effective Aug 3, 2004

## Information bulletins (advisory)

- [SAIB SW-18-13](https://openairdocs.org/saib/SW-18-13): Main Transmission Plate Fitting
- [SAIB SW-12-45](https://openairdocs.org/saib/SW-12-45): Garmin Model 400W/500W Series GPS-WAAS Navigation System
- [SAIB SW-07-34](https://openairdocs.org/saib/SW-07-34): VOR navigation loop antenna
- [SAIB SW-05-18](https://openairdocs.org/saib/SW-05-18): 

## Service difficulty reports (9)

- [SDR QMLA2022071520041](https://openairdocs.org/sdr/QMLA2022071520041), Jul 13, 2022: STARTER GEN. BURNING SMELL WAS NOTED INSIDE AIRCRAFT IN FLIGHT.  TROUBLE SHOOTING LEAD TO #2 STARTER/GENERATOR CAUSING SMOKING ELECTRICAL SMELL.
- [SDR QMLA2020062320029](https://openairdocs.org/sdr/QMLA2020062320029), Mar 27, 2020: STRINGER. STRINGER CRACKED @ FS 5315 BL 145 AND CHAFE HOLE IN DECK COVER @ FS 4820 BL 375. FOUND DURING HEAVY MAINTENANCE, AND AIRCRAFT IS STILL CURRENTLY OUT OF SERVICE.
- [SDR QMLA2020032420015](https://openairdocs.org/sdr/QMLA2020032420015), Mar 24, 2020: ANGLE. CRACKS FOUND IN 5 PIECES OF SUPPORTING STRUCTURE OF # 1 TAILROTOR DRIVESHAFT BEARING MOUNT. AM SERVICE ENGINEERING WORKING WITH AGUSTA ON REPAIR. *** THIS AIRCR
- [SDR QMLA2018123118139](https://openairdocs.org/sdr/QMLA2018123118139), Dec 31, 2018: MOUNT. FOUND SEVERAL CRACKS AT AFT BULKHEAD STA 3525 ON BOTH THE LT AND RT SIDES ALONG WITH THE INNER MAIN GEARBOX TRANSMISSION MOUNT LT CRACKED THAT MOUNTS TO THE AFT
- [SDR QMLA2018072018086](https://openairdocs.org/sdr/QMLA2018072018086), Jul 17, 2018: ACTUATOR. ON TAKE OFF PILOT FELT UNCONTROLLED ROLL. ABORTED TAKE OFF AND RETURNED TO BASE.
- [SDR QMLA2018010618002](https://openairdocs.org/sdr/QMLA2018010618002), Jan 6, 2018: WIRE. THE NUMBER TWO ENGINE FLAMED OUT ON CLIMB-OUT AND SHOWED NO FUEL PRESSURE SHORTLY THEREAFTER. THE FUEL PRESSURE REAPPEARED AND THE ENGINE RESTARTED WITH NO FURT
- [SDR QMLA2017011817011](https://openairdocs.org/sdr/QMLA2017011817011), Jan 18, 2017: WARNING LIGHT. NR 1 ENGINE, OIL CHIP WARNING LIGHT ILLUMINATED IN FLIGHT.
- [SDR QMLA2017010817006](https://openairdocs.org/sdr/QMLA2017010817006), Jan 8, 2017: FIRE LOOP. FIRE DETECTION LIGHT ILLUMINATED DURING FLIGHT, UPON AIRCRAFT LANDING MECHANIC CHECKED PART AND DID TROUBLESHOOTING PROCEDURES TO DETERMINE THAT THE FIRE LOOP I
- [SDR IFJA2014110400001](https://openairdocs.org/sdr/IFJA2014110400001), Nov 2, 2014: CHIP DETECTOR. DURING NORMAL CRUISE FLIGHT,  THE PILOT RECEIVED A MAIN GEAR BOX CHIP LIGHT,  PROCEEDED TO THE NEAREST AIRPORT WITH OUT INCIDENT.  AFTER LANDING, THE MECH FOUND

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.