# N332PH: 2006 Eurocopter Deutschland EC 135 P2+

- Status: Valid registration
- Airframe: [Eurocopter Deutschland EC 135 P2+](https://openairdocs.org/model/eurocopter-deutschland-ec-135-p2-plus) (registry code 5620030, 7 seats)
- Engine: [Pratt & Whitney Canada PW206B](https://openairdocs.org/engine/pratt-whitney-canada-pw206b) (registry code 52204)
- Data sheets: [TCDS H88EU](https://openairdocs.org/tcds/H88EU) (Airbus Helicopters Deutschland GmbH (AHD)), [TCDS E42NE](https://openairdocs.org/tcds/E42NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 0519
- Year built: 2006
- Type: Rotorcraft
- Engine type: Turbo-shaft
- Airworthiness: Standard, normal
- Airworthiness date: March 23, 2007
- Certificate issued: March 20, 2017
- Expires: March 31, 2030
- Mode S code: A39E8A
- Registered owner: [Phi Health LLC](https://openairdocs.org/faa-owner/PHI%20HEALTH%20LLC)
- Location: [Tempe, AZ](https://openairdocs.org/faa-place/AZ/Tempe)
- Owner type: LLC
- Owner's area on the map: 33.4148° N, 111.9093° W: Placed by OpenAirDocs: center of Tempe, AZ, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=332PH
- Page: https://openairdocs.org/aircraft/N332PH

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): 51 in force

### Matched by airframe (Eurocopter Deutschland EC 135 P2+)

- [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 2021-24-05](https://openairdocs.org/ad/2021-24-05): Cargo Compartments · Airbus Helicopters Deutschland EC135P2+, EC135P3, EC135T2+/EC635T2+ and 1 more. Effective Jan 14, 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 2014-01-02](https://openairdocs.org/ad/2014-01-02): Air conditioning system · Airbus Helicopters Deutschland EC135P2+ and EC135T2+/EC635T2+. Effective Mar 3, 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 2012-11-02](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 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

### Matched by engine (Pratt & Whitney Canada PW206B)

- [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

### Historical (superseded or no longer in force)

- [AD 2021-11-22](https://openairdocs.org/ad/2021-11-22) (historical): Tail Rotor System · Airbus Helicopters Deutschland EC135P3, EC135T3, EC135P1 and 5 more. Effective Jul 16, 2021
- [AD 2021-11-17](https://openairdocs.org/ad/2021-11-17) (historical): Main Rotor Control · Airbus Helicopters Deutschland EC135P3, EC135T3, EC135P1 and 5 more. Effective Jul 16, 2021
- [AD 2019-17-02](https://openairdocs.org/ad/2019-17-02) (historical): Rotorcraft Flight Control · Airbus Helicopters Deutschland EC135 P1, EC135 P2, EC135 P2+ and 5 more. Effective Sep 25, 2019
- [AD 2019-05-06](https://openairdocs.org/ad/2019-05-06) (historical): Cabin Equipment/Furnishings · Airbus Helicopters Deutschland EC135 P1, EC135 P2, EC135 P2+ and 5 more. Effective Apr 17, 2019
- [AD 2014-05-06 R1](https://openairdocs.org/ad/2014-05-06-R1) (historical): Main Rotor Control · Airbus Helicopters Deutschland EC135 P1, EC135 P2, EC135 P2+ and 4 more. Effective Jan 22, 2019
- [AD 2016-11-21](https://openairdocs.org/ad/2016-11-21) (historical): Swashplate Ring, Cardan Ring, Bolt, Mixing Lever Gear Unit (flight controls) · Airbus Helicopters Deutschland EC135 P1, EC135 P2, EC135 P2+ and 3 more. Effective Jul 11, 2016
- [AD 2015-12-09](https://openairdocs.org/ad/2015-12-09) (historical): Flight Controller · Airbus Helicopters Deutschland EC135 P1, EC135 P2, EC135 P2+ and 4 more. Effective Jul 23, 2015
- [AD 2014-13-09](https://openairdocs.org/ad/2014-13-09) (historical): Tail Rotor · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 3 more. Effective Jul 30, 2014
- [AD 2014-05-06](https://openairdocs.org/ad/2014-05-06) (historical): Main Rotor Control · Airbus Helicopters Deutschland EC135 P1, EC135 P2, EC135 P2+ and 4 more. Effective Apr 14, 2014
- [AD 2013-21-05](https://openairdocs.org/ad/2013-21-05) (historical): Tail Rotor Control System · Airbus Helicopters Deutschland EC135 P1, EC135 P2, EC135 P2+ and 3 more. Effective Dec 5, 2013
- [AD 2013-16-14](https://openairdocs.org/ad/2013-16-14) (historical): Main Rotor Gearbox · Airbus Helicopters Deutschland EC135 P1, EC135 P2, EC135 P2+ and 3 more. Effective Oct 9, 2013
- [AD 2012-10-53](https://openairdocs.org/ad/2012-10-53) (historical): Main Rotor Head · Airbus Helicopters Deutschland EC135 P1, EC135 P2, EC135 P2+ and 3 more. Effective Dec 5, 2012
- [AD 2012-10-51](https://openairdocs.org/ad/2012-10-51) (historical): Main Rotor Head · Airbus Helicopters Deutschland EC135 P1, EC135 P2, EC135 P2+ and 3 more
- [AD 2008-22-51](https://openairdocs.org/ad/2008-22-51) (historical): Ring frame that connects the tail rotor fenestron housing to the rear structure tube (tailboom) · Eurocopter Deutschland EC135 P1, EC135 P2, EC135 P2+ and 3 more
- [AD 2007-26-51](https://openairdocs.org/ad/2007-26-51) (historical): Tail rotor control rod (control rod) · Airbus Helicopters Deutschland EC135 P1, EC135 P2, EC135 P2+ and 3 more. Effective Feb 19, 2008

## Information bulletins (advisory) (3 in force)

- [SAIB SW-12-45](https://openairdocs.org/saib/SW-12-45): Garmin Model 400W/500W Series GPS-WAAS Navigation System. Issued Oct 3, 2012
- [SAIB SW-09-26](https://openairdocs.org/saib/SW-09-26): Operation with Emergency Flotation System ARMED. Issued May 7, 2009
- [SAIB SW-08-42](https://openairdocs.org/saib/SW-08-42): Emergency Float with Liferaft Kits (kits). Issued Aug 27, 2008

## NTSB investigations

None matched to N332PH.

## FAA accident and incident reports

None matched to N332PH.

## Reports on N332PH not matched to an aircraft (2)

They name N332PH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19960303008329I](https://openairdocs.org/incident/19960303008329I), Mar 3, 1996: Dorner DO328100 (N332PH), Eugene, OR. Narrative: on Sunday March 3, 1996, horizon flight #2569, aircraft N332PH, a dornier D0-328 experienced smoke in the cockpit enroute from pdx to acv at 0040Z.…
- [Incident 19960220012479I](https://openairdocs.org/incident/19960220012479I), Feb 20, 1996: Dorner DO328100 (N332PH), Medford, OR. Narrative: aircraft lost electrical power due to static discharge, possible lightning strike, and diverted to eugene, Oregon. Aircraft landed without further…

## 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.

## Service difficulty reports on N332PH not matched to an aircraft (20)

They name N332PH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR A6WA200100069](https://openairdocs.org/sdr/A6WA200100069), Dec 13, 2001: BOOT. DEFECTIVE. RIGHT ENGINE HAD FLUCTUATING TORQUE INDICATION OF 10 - 25 PERCENT IN FLIGHT. MAINTENANCE FOUND INTAKE DE-ICE BOOT INFLATING AND CHOKING OFF ENGINE AIR INLET SUP
- [SDR A6WA200100044](https://openairdocs.org/sdr/A6WA200100044), Jul 13, 2001: FAN. FAULTY. STRONG BURNING ODOR IN COCKPIT AND CABIN. MAINTENANCE FOUND AVIONICS FAN PREVIOUSLY MEL EMITTING STRONG BURNING ODOR. REMOVED AND REPLACED HX FAN.
- [SDR A6WA200100036](https://openairdocs.org/sdr/A6WA200100036), May 15, 2001: PSEU. FAILED. HYD AUX QTY FAIL AND PROX SYS CAS DURING DESCENT GEAR WILL NOT COME DOWN AND HAD TO BE MANUALLY LOWERED. MAINTENANCE REMOVED AND REPLACED PSEU.
- [SDR A6WA9800008](https://openairdocs.org/sdr/A6WA9800008), Nov 24, 1998: AIR DISTRIBUTION. ODOR. DEN - FLT 7062 - DURING TAXI IN, HAD NUMEROUS ELECTRICAL FAILURES AND SMOKE IN COCKPIT PRIOR TO NR 1 ENGINE SHUT-DOWN. GROUND RAN A/C USING BOTH ENGINES, OPERAT
- [SDR M8XA9700022](https://openairdocs.org/sdr/M8XA9700022), Dec 26, 1997: BRACKET. FAILED. EN ROUTE, THE CREW RECEIVED A DOOR WARNING INDICATION. ACFT RETURNED, LANDED WITHOUT FURTHER INCIDENT. MX DISCOVERED THE PAX DOOR PROXIMITY SENSOR TARGET WAS MI
- [SDR M8XA9700021](https://openairdocs.org/sdr/M8XA9700021), Dec 23, 1997: DOOR. NOT  CLOSED. EN ROUTE, THE CREW WAS ALERTED BY A DOOR WARNING CAS MESSAGE. CREW ELECTED TO RETURN. MX INSPECTED THE DOOR WARNING SYSTEM IAW AMM 52-71-00 WITH NO DISCREPANCIE
- [SDR M8XA9700020](https://openairdocs.org/sdr/M8XA9700020), Dec 18, 1997: HINGE. DEFECTIVE. SHORTLY AFTER THE A/C ARRIVED IN (DIA) MX WAS REQUESTED TO INSPECT THE PAX DOOR AS A RESULT OF DOOR BEING DIFFICULT TO CLOSE FROM TUL. MX INSPECT DOOR AND DISCO
- [SDR M8XA9700012](https://openairdocs.org/sdr/M8XA9700012), Aug 22, 1997: BOOST PUMP. FAILED. DURING THE TAKEOFF ROLL, THE FLT WAS ALERTED BY A ELPMP AUTO FAIL CAS MESSAGE. THE FLT CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. DENVER MX INSPECTED TH
- [SDR QXEA9700154](https://openairdocs.org/sdr/QXEA9700154), Apr 25, 1997: INTAKE DE-ICE. INOPERATIVE. NR 1 ENGINE INTAKE FAIL CAS MESSAGE AFTER TAKEOFF. AIRCRAFT RETURNED TO THE FIELD. REPLACED INTAKE ASSEMBLY, OPERATIONAL CHECKS GOOD.
- [SDR QXEA9700004](https://openairdocs.org/sdr/QXEA9700004), Jan 2, 1997: CONTROL LEVER. MALFUNCTIONED. NOSE GEAR DID NOT INDICATE DOWN AND LOCKED ON GEAR EXTENSION. CYCLED GEAR AND NOSE GEAR AGAIN FAILED TO INDICATE DOWN AND LOCKED. ALTERNATE GEAR EXTENSION PERFO
- [SDR QXEA9600476](https://openairdocs.org/sdr/QXEA9600476), Nov 30, 1996: WINDSHIELD. CRACKED. PILOTS WINDSHIELD STARTED ARCING AND CRACKING UP THE CENTER OF THE WINDSHIELD. WINDSHIELD HEAT SWITCHED OFF AND AIRCRAFT LANDED IN BTM WITHOUT FURTHER PROBLEMS.
- [SDR QXEA9600398](https://openairdocs.org/sdr/QXEA9600398), Sep 16, 1996: CIRCUIT BREAKER. TRIPPED. FLIGHT ATTENDENT REPORTED SMOKE IN CABIN ON CLIMBOUT. LEFT AIR PACK SWITCHED OFF AND AIRCRAFT RETURNED TO FIELD. AIRCRAFT LANDED WITHOUT FUTHTER PROBLEM. LEFT H
- [SDR QXEA9600271](https://openairdocs.org/sdr/QXEA9600271), Jul 31, 1996: SENSOR. OUT OF ADJUST. BIL - DOOR WARNING LIGHT ILLUMINATED DURING DESCENT THROUGH 20,000 FEET AT 5.1 PSID, SYSTEM PAGE INDICATED EXIT AT 9A. AIRCRAFT LANDED IN BIL WITHOUT FURTHER PR
- [SDR QXEA9600270](https://openairdocs.org/sdr/QXEA9600270), Jul 31, 1996: DOOR. NOT SEATED. GEG - DOOR WARNING LIGHT ILLUMINATED, SYSTEM PAGE INDICATED EXIT AT 9A. CABIN DIFFERENTIAL PRESSURE LOWERED TO 3.45 PSID AND LIGHT WENT OUT. AIRCRAFT LANDED WIT
- [SDR QXEA9600092](https://openairdocs.org/sdr/QXEA9600092), Mar 3, 1996: PANEL. SMOKING. EN ROUTE, SMOKE WITH ASSOCIATED SMELL COMING FROM NOSE UP/ NOSE DOWN THUMB WHEEL ON FGC. AIRCRAFT DIVERTED TO EUG AND LANDED WITHOUT FURTHER PROBLEMS. FGC AND N
- [SDR QXEA9600035](https://openairdocs.org/sdr/QXEA9600035), Jan 29, 1996: CARBON SEAL. CRACKED. NR 1 ENGINE OIL PRESS DROPPED TO 30 PSI, LEFT ENGINE LIGHT ILLUMINATED. NR 1 ENGINE SHUTDOWN IN FLIGHT. AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. NR 1 ENGINE CEN
- [SDR QXEA9500379](https://openairdocs.org/sdr/QXEA9500379), Nov 10, 1995: CONNECTOR. LOOSE. PDX - RIGHT MAIN GEAR INDICATION LIGHT FLICKERS AND PROXIMITY HYD CAS MESSAGE ON GEAR EXTENSION, ONLY RIGHT MAIN GEAR LIGHT FLICKERS. S12 DOWNLOCK SWITCH CANNON
- [SDR QXEA9500366](https://openairdocs.org/sdr/QXEA9500366), Oct 31, 1995: FAN. FAILED. SEA - SMELL OF SMOKE IN AIRCRAFT FOLLOWED BY AVIONIC FAN FAIL CAS MESSAGE. AFT AVIONIC FAN REPLACED I/A/W MAINT. MANUAL. FAN OPS CHECKED GOOD. AIRCRAFT RETURNED
- [SDR QXEA9500078](https://openairdocs.org/sdr/QXEA9500078), Mar 16, 1995: PBE. CONTAMINATED. DURING ROUTINE MAINTENANCE, FOUND COCKPIT PBE CONTAMINATED. REPLACED PBE AND RETURNED AIRCRAFT TO SERVICE.
- [SDR QXEA9500017](https://openairdocs.org/sdr/QXEA9500017), Jan 13, 1995: ENGINE. LOST POWER. RDM - APPROCH INTO RDM, NR 2 ENG TORQUE DROPPED FROM APPROX 40 PERCENT TO 0 PERCENT, FOLLOWED BY YAWING OF A/C. ADVANCED NR 2 POWER LEVER, TORQUE WAS RESTORED. 

## STCs that may be installed (OpenAirDocs) (74, first 50)

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 (Eurocopter Deutschland EC 135 P2+)

- [STC SR12474NY](https://openairdocs.org/stc/SR12474NY): Installation of replacement windows. Tech-Tool Plastics, Inc
- [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 SR11844CH](https://openairdocs.org/stc/SR11844CH): Installation of Heli-Preheat Kit, p/n TA3391-1 for 115 volt application. Hartzell Propeller LLC
- [STC SR04464NY](https://openairdocs.org/stc/SR04464NY): Installation of the iPad Mount. Avio Design Group Inc
- [STC SR00521SE](https://openairdocs.org/stc/SR00521SE): Installation of Geneva Aviation Audio System. AEM USA Inc
- [STC SR02301SE](https://openairdocs.org/stc/SR02301SE): Installation of Geneva Aviation 28 - 14 VDC Power Converter. AEM USA Inc
- [STC SR02445SE](https://openairdocs.org/stc/SR02445SE): Installation of P178 Failsafe Audio Mixer. AEM USA Inc
- [STC SR00440DE-D](https://openairdocs.org/stc/SR00440DE-D): Installation of exterior lighting system. Air Methods LLC
- [STC SR12092IB](https://openairdocs.org/stc/SR12092IB): Manufacturing and Installation of Cargo Hold Nets. ICARUS AERO INC
- [STC SR12065DE](https://openairdocs.org/stc/SR12065DE): Installation of Honeywell 5G Bandpass Filter into existing KRA 405B Radar Altimeter Systems. QAI Aviation Inc
- [STC SR04842NY](https://openairdocs.org/stc/SR04842NY): Installation of RMCI Inc. Expandable Rotorcraft Diagnostic System (XRDS). Sterling Helicopter
- [STC SR04711NY](https://openairdocs.org/stc/SR04711NY): Replacement of Luminator LS400 LED searchlight (steerable landing light). Sterling Helicopter
- [STC SR01790SE](https://openairdocs.org/stc/SR01790SE): Installation of Skidtube and Skidtube extension. Dart Aerospace USA Inc
- [STC SR09947AC](https://openairdocs.org/stc/SR09947AC): Replacement of the original N2 tachometer with a corresponding Ahlers tachometer. Ahlers Aerospace Inc
- [STC SR03704NY](https://openairdocs.org/stc/SR03704NY): Installation of Air Ambulance Technology GmbH's P/N 135-25-20-5000-600 Series Air Ambulance Equipment (EMS config) or P/N 135-25-20-5000-900 Series VIP Interior (VIP config). Air Ambulance Technology GmbH
- [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc
- [STC SR00368BO](https://openairdocs.org/stc/SR00368BO): Installation of an Outerlink SATCOM Communications and Flight Data Monitoring System KIT 135-SAT-100. Outerlink Corporation
- [STC SR02217SE](https://openairdocs.org/stc/SR02217SE): Fabrication of Onboard Systems Single-Hook and Double-Hook Cargo Hook Kit. Onboard Systems
- [STC SR09559RC](https://openairdocs.org/stc/SR09559RC): Installation of Night Vision Goggle Compatible Interior Lighting System. REB Technologies Inc
- [STC SR09102RC-D](https://openairdocs.org/stc/SR09102RC-D): Installation of windows in crew, cabin, and cargo doors. Tech-Tool Plastics Inc
- [STC SR09116RC-D](https://openairdocs.org/stc/SR09116RC-D): Installation of a sliding window in the rear sliding door. Tech-Tool Plastics Inc
- [STC SR09105RC-D](https://openairdocs.org/stc/SR09105RC-D): Installation of a Concorde RG-390E or RG-380E/44 Lead Acid Battery. Airbus Helicopters Inc
- [STC SR09919AC](https://openairdocs.org/stc/SR09919AC): Installation of a Luminator search light LS-400, LS-400M, or LS-400T. Luminator Holdings L.P
- [STC SR02138LA](https://openairdocs.org/stc/SR02138LA): Installation of Utility Step Mount. Airfilm Camera Systems
- [STC SR00666DE](https://openairdocs.org/stc/SR00666DE): Installation of Angled Scene Lights. Air Methods Corporation
- [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC
- [STC SR02114NY-D](https://openairdocs.org/stc/SR02114NY-D): Installation of a Honeywell Chadwick Model 15175 VXP System. Diagnostic Solution International LLC
- [STC SR01052DE](https://openairdocs.org/stc/SR01052DE): Installation of Non-Aviation Band FM Radio Systems. Cert Works LLC
- [STC SR00565DE](https://openairdocs.org/stc/SR00565DE): Installation of Cabin Air Conditioning System. Air Comm Corporation
- [STC SR09583RC](https://openairdocs.org/stc/SR09583RC): Installation of the Sky Connect Forte Iridium Satellite Phone and/or automated position reporting system including the installation of an Iridium Satellite antenna, Transceiver, aircraft GPS interface to obtain position, SOP and/or MMU dialer panels, and optional GPS antenna. Honeywell International Inc
- [STC SR02124SE](https://openairdocs.org/stc/SR02124SE): Installation functionality. of Data Garmin Required: transponders: (1) Garmin GTX Master 345/345R Drawing with List ADS-B (MDL), Out and In 005-00734-A4, functionality;. Garmin International Inc
- [STC SR02677SE](https://openairdocs.org/stc/SR02677SE): Installation of Heavy Duty Wearplates. Dart Aerospace USA Inc
- [STC SR09164RC](https://openairdocs.org/stc/SR09164RC): Installation of an Airborne Emergency Medical Systems. Metro Aviation Inc
- [STC SR09354RC](https://openairdocs.org/stc/SR09354RC): Installation of Metro Aviation optional equipment. Metro Aviation Inc
- [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SR09193RC](https://openairdocs.org/stc/SR09193RC): Installation of a window in the aft clamshell doors. Metro Aviation Inc
- [STC SR00814DE](https://openairdocs.org/stc/SR00814DE): Installation of Garmin Helicopter Terrain Awareness and Warning System (HTAWS). Cert Works LLC
- [STC SA00339BO](https://openairdocs.org/stc/SA00339BO): Installation of Single pilot IFR KIT135M-GTN-150 with Garmin GTN 650-750 WAAS Navigators. Metro Aviation Inc
- [STC SR00821DE](https://openairdocs.org/stc/SR00821DE): Installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out and in functionality using the BendixKing KT74 Transponder and qualified position sensor and ADS-B In Receiver. Peregrine
- [STC SR00828DE](https://openairdocs.org/stc/SR00828DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the Garmin G330ES or G33H ES Transponder and qualified position sensor. Peregrine
- [STC SR04276NY](https://openairdocs.org/stc/SR04276NY): Installation of the Crosstubes. Dart Aerospace Limited
- [STC SR01042SE](https://openairdocs.org/stc/SR01042SE): Fabrication of Dart D135-692-011 Bearpaws. Dart Aerospace USA, Inc
- [STC SR01709SE](https://openairdocs.org/stc/SR01709SE): Installation of Skidtube and Skidtube extension. Dart Aerospace USA Inc
- [STC SR04235NY](https://openairdocs.org/stc/SR04235NY): Installation of Garmin GTS Traffic System. Maxcraft Avionics Ltd
- [STC SR04228NY](https://openairdocs.org/stc/SR04228NY): Installation of Garmin HTAWS (Helicopter Terrain Awareness Warning System). Maxcraft Avionics Ltd
- [STC SR00812DE](https://openairdocs.org/stc/SR00812DE): Installation of Honeywell Sky Connect Tracker III system. Cert Works LLC
- [STC SR09104RC-D](https://openairdocs.org/stc/SR09104RC-D): Installation of pulsed engine and gearbox chip detector system. Airbus Helicopters Inc
- [STC SR03949NY](https://openairdocs.org/stc/SR03949NY): Installation of Removable Pins for Hinged Door. Airbus Helicopters Canada Limited
- [STC SR01855LA](https://openairdocs.org/stc/SR01855LA): Installation of Apical Industries, Inc. Emergency Float Kit. Apical Industries, Inc. dba Dart Aerospace
- [STC SR02487AK](https://openairdocs.org/stc/SR02487AK): Installation of L-3 Communications Avionics Systems ESI-500 Standby Instrument System. ADS-B Technologies, LLC

All 74: https://openairdocs.org/aircraft/N332PH/stcs.md

## Related

- Other Eurocopter Deutschland EC 135 P2+ aircraft: https://openairdocs.org/model/eurocopter-deutschland-ec-135-p2-plus/aircraft.md
- The Pratt & Whitney Canada PW206B engine: https://openairdocs.org/engine/pratt-whitney-canada-pw206b.md

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