# N911KB: 1999 Eurocopter Deutschland EC135P1

- Status: Valid registration
- Airframe: Eurocopter Deutschland EC135P1 (registry code 8680990, TCDS H88EU (OpenAirDocs match))
- Engine: Pratt & Whitney Canada PW206A (registry code 52151, TCDS E42NE (OpenAirDocs match))
- Serial number: 0095
- Year built: 1999
- Type: Rotorcraft
- Airworthiness: Standard, normal
- Airworthiness date: January 12, 2000
- Certificate issued: February 21, 2006
- Expires: December 31, 2029
- Mode S code: AC9B45
- Registered owner: Metro Aviation Inc
- Location: Shreveport, LA
- Owner's area on the map: 32.5252° N, 93.7502° W: Placed by OpenAirDocs: center of Shreveport, LA, within about 6 miles (OpenAirDocs)
- Page: https://openairdocs.org/aircraft/N911KB

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 (Eurocopter Deutschland EC135P1) (OpenAirDocs)

- [AD 2026-20-06](https://openairdocs.org/ad/2026-20-06): Main rotor gearbox · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 6 more. Effective Oct 13, 2026
- [AD 2026-17-05](https://openairdocs.org/ad/2026-17-05): Cabin Equipment/Furnishings · Airbus Helicopters H160-B, EC225LP, AS 365 N3 and 18 more. Effective Oct 2, 2026
- [AD 2026-08-10](https://openairdocs.org/ad/2026-08-10): Passenger compartment equipment · B/E Aerospace Fischer Medical Seat 230/305, EC135P1, EC135T1 and 19 more. Effective May 11, 2026
- [AD 2026-02-01](https://openairdocs.org/ad/2026-02-01): Tail Rotor Drive Shaft · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 6 more. Effective Feb 26, 2026
- [AD 2026-03-02](https://openairdocs.org/ad/2026-03-02): Rotorcraft Tail Boom · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 6 more. Effective Feb 17, 2026
- [AD 2025-18-04](https://openairdocs.org/ad/2025-18-04): Cabin Equipment/Furnishings · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 9 more. Effective Oct 21, 2025
- [AD 2025-13-06](https://openairdocs.org/ad/2025-13-06): Tail Rotor Control System · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 6 more. Effective Jul 18, 2025
- [AD 2025-04-10](https://openairdocs.org/ad/2025-04-10): Emergency equipment · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 10 more. Effective Mar 24, 2025
- [AD 2024-20-07](https://openairdocs.org/ad/2024-20-07): Emergency Equipment; Emergency Flotation Section · Apical Emergency Float Kit, P/N 20498 (STC SR00780LA or 12 others). Effective Dec 5, 2024
- [AD 2024-17-01](https://openairdocs.org/ad/2024-17-01): Main Rotor Control · Airbus EC135P1, EC135P2, EC135P2+ and 6 more. Effective Nov 4, 2024
- [AD 2024-04-01](https://openairdocs.org/ad/2024-04-01): Cabin Equipment/Furnishings · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 8 more. Effective Apr 19, 2024
- [AD 2024-04-10](https://openairdocs.org/ad/2024-04-10): Tail Rotor Blades · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 6 more. Effective Mar 19, 2024
- [AD 2022-17-01](https://openairdocs.org/ad/2022-17-01): Air Conditioning System · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 5 more. Effective Sep 27, 2022
- [AD 2022-10-51](https://openairdocs.org/ad/2022-10-51): Flight Control System · Airbus Helicopters AS350B, AS350B1, AS350B2 and 22 more. Effective Jun 7, 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 2022-02-19](https://openairdocs.org/ad/2022-02-19): Flight Compartment Equipment · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 5 more. Effective Mar 17, 2022
- [AD 2022-01-03](https://openairdocs.org/ad/2022-01-03): Fire Bottle, Portable · Airbus Helicopters AS332C, AS332C1, AS332L and 35 more. Effective Mar 7, 2022
- [AD 2021-24-17](https://openairdocs.org/ad/2021-24-17): Tail rotor blades · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 5 more. Effective Jan 18, 2022
- [AD 2021-21-01](https://openairdocs.org/ad/2021-21-01): Cabin Equipment/Furnishings · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 5 more. Effective Dec 10, 2021
- [AD 2021-17-17](https://openairdocs.org/ad/2021-17-17): Cabin Equipment/Furnishings · Airbus Helicopters EC135P3, EC135T3, MBB-BK 117 C-2 and 32 more. Effective Nov 22, 2021
- [AD 2021-22-07](https://openairdocs.org/ad/2021-22-07): Fire Bottle, Portable · Airbus A319-111, A319-112, A319-113 and 127 more. Effective Nov 18, 2021
- [AD 2021-16-10](https://openairdocs.org/ad/2021-16-10): Tail Rotor Blades · Airbus Helicopters Deutschland EC135P3, EC135T3, EC135P1 and 5 more. Effective Oct 13, 2021
- [AD 2021-13-05](https://openairdocs.org/ad/2021-13-05): Tail Rotor Control System · Airbus Helicopters Deutschland EC135P3, EC135T3, EC135P1 and 5 more. Effective Aug 11, 2021
- [AD 2021-07-12](https://openairdocs.org/ad/2021-07-12): Rotorcraft Flight Control · Airbus Helicopters Deutschland EC135P3, EC135T3, EC135P1 and 5 more. Effective May 11, 2021
- [AD 2021-09-07](https://openairdocs.org/ad/2021-09-07): Rotorcraft Flight Control · Airbus Helicopters Deutschland EC135P3, EC135T3, EC135P1 and 5 more. Effective May 10, 2021
- [AD 2021-03-04](https://openairdocs.org/ad/2021-03-04): Fasteners, Tail Rotor Drive Shaft · Airbus Helicopters Deutschland EC135P3, EC135T3, EC135P1 and 5 more. Effective Mar 29, 2021
- [AD 2020-26-03](https://openairdocs.org/ad/2020-26-03): Rotorcraft Flight Control · Airbus Helicopters Deutschland EC135P3, EC135T3, EC135P1 and 5 more. Effective Jan 22, 2021
- [AD 2020-22-04](https://openairdocs.org/ad/2020-22-04): Tail Rotor Drive · Airbus Helicopters Deutschland EC135P3, EC135T3, EC135P1 and 5 more. Effective Nov 18, 2020
- [AD 2014-05-06 R2](https://openairdocs.org/ad/2014-05-06-R2): Main Rotor Control · Airbus Helicopters Deutschland MBB-BK 117 C-2, EC135P1, EC135P2 and 4 more. Effective Feb 19, 2019
- [AD 2013-21-05 R1](https://openairdocs.org/ad/2013-21-05-R1): Tail Rotor Control System · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 3 more. Effective Dec 21, 2018
- [AD 2018-07-01](https://openairdocs.org/ad/2018-07-01): Main Rotor Gearbox · Airbus Helicopters Deutschland EC135P3, EC135T3, EC135P1 and 5 more. Effective May 3, 2018
- [AD 2017-03-01](https://openairdocs.org/ad/2017-03-01): Main Rotor Control · Airbus Helicopters Deutschland MBB-BK 117 C-2, EC135P1, EC135P2 and 4 more. Effective Mar 31, 2017
- [AD 2015-12-09 R1](https://openairdocs.org/ad/2015-12-09-R1): Flight Controller · Airbus Helicopters Deutschland MBB-BK 117 C-2, EC135P1, EC135P2 and 4 more. Effective Feb 25, 2016
- [AD 2014-16-24](https://openairdocs.org/ad/2014-16-24): Main Rotor Head · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 3 more. Effective Sep 25, 2014
- [AD 2014-05-01](https://openairdocs.org/ad/2014-05-01): Main Rotor Gearbox · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 3 more. Effective Apr 14, 2014
- [AD 2013-21-06](https://openairdocs.org/ad/2013-21-06): Fuselage, Equipment Attach Fittings · Airbus Helicopters Deutschland MBB-BK 117 C-2, EC135P1, EC135P2 and 4 more. Effective Jan 31, 2014
- [AD 2013-18-05](https://openairdocs.org/ad/2013-18-05): Extinguishing System · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 3 more. Effective Oct 18, 2013
- [AD 2013-11-15](https://openairdocs.org/ad/2013-11-15): Main Rotor Control · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-1 and 14 more. Effective Jul 26, 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 2013-10-01](https://openairdocs.org/ad/2013-10-01): Exterior lighting · Agusta AB139, AW139, MBB-BK 117 C-2 and 7 more. Effective Jun 20, 2013
- [AD 2012-23-07](https://openairdocs.org/ad/2012-23-07): Main Rotor Mast/Swashplate · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135T1 and 1 more. Effective Jan 11, 2013
- [AD 2012-11-02](https://openairdocs.org/ad/2012-11-02): Crack · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 3 more. Effective Jul 10, 2012
- [AD 2012-03-01](https://openairdocs.org/ad/2012-03-01): Engine Controls · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 3 more. Effective Mar 21, 2012
- [AD 2011-25-01](https://openairdocs.org/ad/2011-25-01): Liferafts · Agusta AB412, AB412 EP, 206A and 23 more. Effective Jan 17, 2012
- [AD 2009-11-10](https://openairdocs.org/ad/2009-11-10): Main rotor drive · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 3 more. Effective Jun 12, 2009
- [AD 2008-04-05](https://openairdocs.org/ad/2008-04-05): Wiring harness · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 3 more. Effective Mar 6, 2008
- [AD 2004-22-11](https://openairdocs.org/ad/2004-22-11): Rotorcraft Flight Manual (RFM) · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135T1 and 1 more. Effective Dec 7, 2004
- [AD 2002-14-17](https://openairdocs.org/ad/2002-14-17): Main rotor hub shaft · Airbus Helicopters Deutschland EC135T1 and EC135P1. Effective Jul 26, 2002
- [AD 2001-26-52](https://openairdocs.org/ad/2001-26-52): Rotorcraft Flight Manual - Smart Multifunction Display (SMD45H) · Airbus Helicopters Deutschland EC135P1 and EC135T1. Effective Feb 6, 2002
- [AD 2000-26-12](https://openairdocs.org/ad/2000-26-12): Hydraulic Line Shielding Hose · Airbus Helicopters Deutschland EC135P1 and EC135T1. Effective Feb 6, 2001
- [AD 2000-26-02](https://openairdocs.org/ad/2000-26-02): Fenestron Tail Rotor · Airbus Helicopters Deutschland EC135P1 and EC135T1. Effective Jan 26, 2001
- [AD 2000-13-08](https://openairdocs.org/ad/2000-13-08): Tail Rotor Drive Shaft · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 3 more. Effective Aug 9, 2000
- [AD 2000-10-07](https://openairdocs.org/ad/2000-10-07): Oil Cooler Fan Splined Drive Shaft · Airbus Helicopters Deutschland EC135P1 and EC135T1. Effective Jun 21, 2000
- [AD 2000-01-19](https://openairdocs.org/ad/2000-01-19): Main Rotor Blade Expansion Bolt · Airbus Helicopters Deutschland EC135P1 and EC135T1. Effective Feb 4, 2000
- [AD 99-22-01](https://openairdocs.org/ad/99-22-01): Tail Boom Frame Flange Inspection · Airbus Helicopters Deutschland EC135P1 and EC135T1. Effective Dec 17, 1999

Historical (superseded or no longer in force): AD 2021-11-22, AD 2021-11-17, AD 2019-17-02, AD 2019-05-06, AD 2014-05-06 R1, AD 2016-11-21, AD 2015-12-09, AD 2014-13-09, AD 2014-05-06, AD 2013-21-05, AD 2013-16-14, AD 2012-10-53, AD 2012-10-51, AD 2008-22-51, AD 2007-26-51

## ADs matched by engine (Pratt & Whitney Canada PW206A) (OpenAirDocs)

- [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 2004-17-03](https://openairdocs.org/ad/2004-17-03): Compressor turbine and power turbine blades for blade axial shift · Pratt & Whitney Canada PW206A and PW206E. Effective Sep 24, 2004

Historical (superseded or no longer in force): AD 2003-16-10

## Information bulletins (advisory)

- [SAIB SW-12-45](https://openairdocs.org/saib/SW-12-45): Garmin Model 400W/500W Series GPS-WAAS Navigation System
- [SAIB SW-09-26](https://openairdocs.org/saib/SW-09-26): Operation with Emergency Flotation System ARMED
- [SAIB SW-08-42](https://openairdocs.org/saib/SW-08-42): Emergency Float with Liferaft Kits (kits)

## Earlier aircraft with N911KB

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N911KB before.

- [Cancelled 2014-08-06](https://openairdocs.org/deregistered/N911KB-2014-08-06): Eurocopter Deutschland EC135P1, S/N 0013, built 1997. Owner: Metro Aviation Inc, Shreveport, LA

## Service difficulty reports (4)

- [SDR HDNA200811072008](https://openairdocs.org/sdr/HDNA200811072008), Nov 6, 2008: CONTACTOR. DURING TAKEOFF, THE NR 1 ENGINE FIRE DETECTOR LIGHT ILLUMINATED ON THE WARNING PANEL.  THE AIRCRAFT RETURNED TO THE HELIPAD WITHOUT INCIDENT.  DURING THE INSPEC
- [SDR 2007FA0000788](https://openairdocs.org/sdr/2007FA0000788), Aug 10, 2007: EEC. EEC CAUSED ENGINE TO DROP FROM FULL POWER TO IDLE IN CRUISE FLIGHT WITH AN ENGINE FAILURE AND ENGINE MANUAL HORN AND LIGHT.  (K)
- [SDR HDNA610E](https://openairdocs.org/sdr/HDNA610E), Jun 27, 2001: RING. DURING 100 HUR INSPECTION, FOUND A RETAINING RING MISSING.  THE RING SECURES A BELLCRANK TO THE CYCLIC SHAFT ASSEMBLY.  THIS ALLOWED THE BELLCRANK TO SHIFT UP A
- [SDR 20000919SH016](https://openairdocs.org/sdr/20000919SH016), Aug 29, 2000: WIRE. BRUSH WIRE CONTACTED HOUSING AFTER A BRUSH INSPECTION.  EXTREME CARE SHOULD BE TAKEN DURING RE-ASSEMBLY AFTER INSPECTION.  (X)

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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.