# N261PA: 1998 Raytheon HAWKER 1000

- Status: Valid registration
- Airframe: [Raytheon HAWKER 1000](https://openairdocs.org/model/raytheon-hawker-1000) (registry code 1500290, 13 seats)
- Engine: [Pratt & Whitney PW300 series](https://openairdocs.org/engine/pratt-whitney-pw300-series) (registry code 52128)
- Data sheets: [TCDS A3EU](https://openairdocs.org/tcds/A3EU) (Textron Aviation Inc.) (OpenAirDocs)
- Serial number: 259003
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 17, 1998
- Certificate issued: October 18, 2005
- Expires: July 31, 2028
- Mode S code: A283FA
- Registered owner: [Calla Airways LLC](https://openairdocs.org/faa-owner/CALLA%20AIRWAYS%20LLC)
- Location: [Cohasset, MA](https://openairdocs.org/faa-place/MA/Cohasset)
- Owner type: LLC
- Owner's area on the map: 42.2364° N, 70.8143° W: Placed by OpenAirDocs at the center of ZIP code 02025, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=261PA
- Page: https://openairdocs.org/aircraft/N261PA

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): 30 in force

### Matched by airframe (Raytheon HAWKER 1000)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2016-13-13](https://openairdocs.org/ad/2016-13-13): Engine Exhaust · Textron BAe.125 Series 1000A, BAe.125 Series 1000B and Hawker 1000. Effective Aug 12, 2016
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 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 2009-08-01](https://openairdocs.org/ad/2009-08-01): Honeywell FMSs · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R), CL-600-2B16 (CL-604) and 11 more. Effective May 14, 2009
- [AD 2006-19-04](https://openairdocs.org/ad/2006-19-04): Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 more. Effective Oct 17, 2006
- [AD 2006-12-20](https://openairdocs.org/ad/2006-12-20): Current limiters for the PE, PS1, and PS2 busses · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 9 more. Effective Jul 3, 2006
- [AD 2006-01-04](https://openairdocs.org/ad/2006-01-04): Fan venturi motor casing · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 42 more. Effective Feb 22, 2006
- [AD 2003-04-20](https://openairdocs.org/ad/2003-04-20): Cylinder Head Lugs of Main Landing Gear (MLG) Actuator · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 43 more. Effective Apr 4, 2003
- [AD 94-09-11 R1](https://openairdocs.org/ad/94-09-11-R1): Thrust Reverser System · BAe.125 Series 1000A and Hawker 1000. Effective Sep 3, 2002
- [AD 2001-13-05](https://openairdocs.org/ad/2001-13-05): Turbine Air Discharge Duct and Water Separator Outlet Duct · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 6 more. Effective Aug 1, 2001
- [AD 2000-22-03](https://openairdocs.org/ad/2000-22-03): Pitot/Static and Stall Vent Drain Valves · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 43 more. Effective Dec 4, 2000
- [AD 2000-02-35](https://openairdocs.org/ad/2000-02-35): Oxygen System Plumbing · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 36 more. Effective Mar 13, 2000
- [AD 2000-01-02](https://openairdocs.org/ad/2000-01-02): Turbine Air Discharge Duct in the Air Conditioning System · Textron BAe.125 Series 1000A, BAe.125 Series 1000B and Hawker 1000. Effective Feb 15, 2000
- [AD 99-25-01](https://openairdocs.org/ad/99-25-01): P1 Pitot Pipes · Textron BAe.125 Series 1000A, BAe.125 Series 1000B and Hawker 1000. Effective Jan 4, 2000
- [AD 99-23-10](https://openairdocs.org/ad/99-23-10): PS Wire Bundle · Textron Hawker 1000. Effective Dec 17, 1999
- [AD 97-26-10](https://openairdocs.org/ad/97-26-10): Aft Core Cowl Nozzles Of Engine Nacelles · Textron Hawker 1000. Effective Jan 23, 1998
- [AD 97-09-05](https://openairdocs.org/ad/97-09-05): Venting Of Cabin Pressure · Textron BAe.125 Series 1000A and Hawker 1000. Effective May 30, 1997
- [AD 97-03-07](https://openairdocs.org/ad/97-03-07): Main Landing Gear Sidestay Assemblies · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 42 more. Effective Mar 11, 1997
- [AD 96-22-03](https://openairdocs.org/ad/96-22-03): Thrust Reverser · Textron BAe.125 Series 1000A and Hawker 1000. Effective Dec 11, 1996
- [AD 96-18-09](https://openairdocs.org/ad/96-18-09): TKS Metering Pump · Textron BAe.125 Series 1000A, BAe.125 Series 800A, Hawker 1000 and 1 more. Effective Oct 9, 1996
- [AD 96-17-13](https://openairdocs.org/ad/96-17-13): Elevator Pulley Assembly · Textron BAe.125 Series 1000A and Hawker 1000. Effective Sep 30, 1996
- [AD 96-17-09](https://openairdocs.org/ad/96-17-09): Fuel Hose Assembly on Auxiliary Power Unit (APU) · Textron BAe.125 Series 1000A and Hawker 1000. Effective Sep 24, 1996
- [AD 96-12-17](https://openairdocs.org/ad/96-12-17): Engine Starting Circuits Diode Soldered Connections · Textron BAe.125 Series 1000A, BAe.125 Series 800A, Hawker 1000 and 1 more. Effective Jul 15, 1996
- [AD 96-11-17](https://openairdocs.org/ad/96-11-17): Flap, Turnbuckle, Airbrakes, And Flight Control Cables · Textron BAe.125 Series 1000A and Hawker 1000. Effective Jul 9, 1996
- [AD 96-07-11](https://openairdocs.org/ad/96-07-11): Hydraulic Pipes Inspection · Textron BAe.125 Series 1000A and Hawker 1000. Effective May 6, 1996
- [AD 95-21-17](https://openairdocs.org/ad/95-21-17): Electrical Cable Loom · Textron BAe.125 Series 1000A and Hawker 1000. Effective Nov 17, 1995
- [AD 94-24-08](https://openairdocs.org/ad/94-24-08): Install Modification 253627A & 253661B · Textron BAe.125 Series 1000A and Hawker 1000. Effective Jan 4, 1995
- [AD 94-15-15](https://openairdocs.org/ad/94-15-15): Electrical And Hydraulic Cables, Pipes, And Looms · Textron BAe.125 Series 1000A and Hawker 1000. Effective Aug 15, 1994

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

None in force.

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

- [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 2001-17-26 R1](https://openairdocs.org/ad/2001-17-26-R1) (historical): Actuator Cylinder Head Lugs · Raytheon BAe.125 Series (all), BH.125 Series (all), DH.125 Series (all) and 5 more. Effective Oct 3, 2001
- [AD 2001-17-26](https://openairdocs.org/ad/2001-17-26) (historical): Main Landing Gear Actuator · Raytheon BAe.125 Series (all), BH.125 Series (all), DH.125 Series (all) and 5 more. Effective Oct 3, 2001
- [AD 94-11-03](https://openairdocs.org/ad/94-11-03) (historical): Fan Casing Clearance · Raytheon BAe.125 Series (all), BH.125 Series (all), DH.125 Series (all) and 5 more. Effective Jun 10, 1994
- [AD 94-09-11](https://openairdocs.org/ad/94-09-11) (historical): Thrust Reverser System · Hawker Beechcraft BAe.125 Series 1000A and Hawker 1000. Effective May 16, 1994

## Information bulletins (advisory) (4 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB NM-15-24](https://openairdocs.org/saib/NM-15-24): Landing Gear. Issued Sep 29, 2015
- [SAIB NM-14-05](https://openairdocs.org/saib/NM-14-05): Wing: Ailerons. Issued Nov 27, 2013
- [SAIB NM-11-60](https://openairdocs.org/saib/NM-11-60): Landing Gear. Issued Sep 29, 2011
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N261PA.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20220805014149I](https://openairdocs.org/incident/20220805014149I), Aug 5, 2022: Raytheon HAWKER 1000 (N261PA), Plymouth, MA, Minor damage. After landing and decelerating to less than 80 knots a deer suddenly appeared in the pilots field of view from the left. The deer crossed left to right in…

## Service difficulty reports (15)

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 ZKFA20240701058](https://openairdocs.org/sdr/ZKFA20240701058), Jul 2, 2024: FILTER HOUSING. PULLED. DURING A MAINTENANCE GROUND RUN, THE RT ENGINE DEVELOPED A MAJOR OIL LEAK AND WAS IMMEDIATELY SHUT DOWN. TECHNICIANS DISCOVERED THE OIL FILTER BOWL HAD BLOWN OF
- [SDR ZKFA2024030600201](https://openairdocs.org/sdr/ZKFA2024030600201), Mar 5, 2024: ELECTRONIC UNIT. OVERHEATED. PILOTS NOTICED SMOKE SMELL IN COCKPIT DURING CRUISE FLIGHT, ON TRIP KHYA-KAPF, FOLLOWED BY OBSERVING SMOKE. CONDUCTED EMERGENCY DESCENT AND LANDING AT KSAV. MAI
- [SDR 2022F00364](https://openairdocs.org/sdr/2022F00364), Aug 5, 2022: NONE. NONE. AIRCRAFT IMPACTED A DEER ON LANDING AT KPYM. RIGHT TRAILING EDGE FLAP WAS DAMAGED BEYOND REPAIR AND WAS REPLACED.
- [SDR 2022F00244](https://openairdocs.org/sdr/2022F00244), May 18, 2022: NONE. NONE. AIRCRAFT WAS ON SHORT FINAL TO KPYM, PLYMOUTH, MA MUNICIPAL AIRPORT, FULLY CONFIGURED FOR LANDING, WHEN PILOTS SAW SMOKE AND HEARD A POPPING SOUND FROM THE COPI
- [SDR 2021FA0000311](https://openairdocs.org/sdr/2021FA0000311), Nov 4, 2021: HINGE. CORRODED. RH AILERON SIGNIFICANT CORROSION FOUND AT CENTER TRIM TAB HINGE, AROUND BONDING STRAP ATTACHMENT HOLE, IN AFT SPAR STRUCTURE. TEXTRON ENGINEERING NOTIFIED AND N
- [SDR ZKFR20130724001](https://openairdocs.org/sdr/ZKFR20130724001), Jul 24, 2013: ATTACH FITTING. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION ON LT SIDE OF VERTICAL TO HORIZONTAL STABILIZER ATTACH FITTING. CORROSION IS INTERGRANULAR, AND IS LOCATED AROUND 1
- [SDR ZKFR20130117002](https://openairdocs.org/sdr/ZKFR20130117002), Jan 10, 2013: O-RING. LEAKING. DURING PREFLIGHT, FLIGHT CREW NOTICED LT OTBD TIRE LOOKED LOW. MX DISCOVERED TIRE ALMOST COMPLETELY DEFLATED BUT NOT BLOWN. WHEEL ASSYS ONLY HAD 9 CYCLES SINCE 
- [SDR ZKFR20130117001](https://openairdocs.org/sdr/ZKFR20130117001), Jan 10, 2013: O-RING. LEAKING. DURING PREFLIGHT, FLIGHT CREW NOTICED LT INBD TIRE LOOKED LOW. MX DISCOVERED TIRE ALMOST COMPLETELY DEFLATED BUT NOT BLOWN. WHEEL ASSYS ONLY HAD 9 CYCLES SINCE 
- [SDR ZKFR20120605001](https://openairdocs.org/sdr/ZKFR20120605001), Jun 5, 2012: CHECK VALVE. LEAKING. OXYGEN SYS NON-RETURN VALVE LEAKING ALLOWING OXYGEN TO FLOW BACKWARDS AND LEAK OUT OF FILLER PORT. THIS WAS A BRAND NEW CHECK VALVE FROM MFG. REMOVED AND REPLAC
- [SDR ZKFR20120530001](https://openairdocs.org/sdr/ZKFR20120530001), May 30, 2012: CHECK VALVE. LEAKING. OXYGEN SYSTEM LEAKING: FOUND OXYGEN SYSTEM NON-RETURN VALVE INOP AND ALLOWING OXYGEN TO FLOW BACKWARDS AND LEAKING OUT OF FILLER PORT. REMOVED AND REPLACED NON-
- [SDR ZKFR2012040900001](https://openairdocs.org/sdr/ZKFR2012040900001), Apr 9, 2012: SKIN. DELAMINATED. DURING ENGINE CHANGE, CORE COWL SEGMENT FOUND DELAMINATED. MFG HAS A REPAIR FOR THIS PROBLEM BUT UNFORTUNATELY THE EXTENT OF DAMAGE TO THIS CORE COWL IS BEYOND 
- [SDR ZKFR201112163233](https://openairdocs.org/sdr/ZKFR201112163233), Dec 16, 2011: CONTROLLER. FAULTY. CABIN TEMPERTURE UNCONTROLLABLE IN AUTO MODE. FOUND CABIN TEMPERTURE CONTROLLER NOT PROVIDING ANY OUTPUT VOLTAGE. CONTROLLLER GIVES MOMENTARY PULSES ONLY VISIBL
- [SDR 2011F00036](https://openairdocs.org/sdr/2011F00036), Mar 23, 2011: STARTER GEN. FAILED. ACFT EXPERIENCED MODERATE VIBRATION IN CRUISE, FLIGHT CREW FELT VIBRATION WAS FROM NR 2 ENGINE, FOLLOWED SHORTLY AFTER WITH GEN 2 FAIL INDICATION, CREW SHUTDOWN
- [SDR 2011F00000](https://openairdocs.org/sdr/2011F00000), Dec 21, 2010: STARTER GEN. DESTROYED. DURING CRUISE FLIGHT, EXPERIENCED VIBRATION, BELIEVED TO BE FROM ENGINE AREA. VIBRATION INCREASED, BUT DID NOT SHOW ON EVM INDICATOR, FOLLOWED BY GEN 1 FAIL IND
- [SDR AJC2004F00002](https://openairdocs.org/sdr/AJC2004F00002), Jun 10, 2004: POSITION SWITCH. DAMAGED. DURING TAKEOFF, ENROUTE, THE LANDING GEAR HORN SOUNDED WHEN GEAR LEVER WAS PLACED IN UP POSITION, BOTH WITH FLAPS IN 15 DEGREE AND 0 DEGREE POSITION. CREW PLACE

## STCs that may be installed (OpenAirDocs) (60, 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 (Raytheon HAWKER 1000)

- [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 ST03292CH](https://openairdocs.org/stc/ST03292CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development, Inc
- [STC ST00749WI-D](https://openairdocs.org/stc/ST00749WI-D): Installation of AlliedSignal Digital Flight Data Recorder System. KGB Aviation Solutions LLC
- [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 ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST02346AT-D](https://openairdocs.org/stc/ST02346AT-D): Installation of Composite Stang Fairings. Summit Aviation Inc
- [STC ST01070DE](https://openairdocs.org/stc/ST01070DE): Installation of the Curtiss-Wright Fortress Flight Data Recorder (with Cockpit Voice Recorder). Peregrine
- [STC ST01985WI](https://openairdocs.org/stc/ST01985WI): Installation of the Garmin GI-275 I Electronic Standby Instrument (ESI). Peregrine
- [STC ST02004WI](https://openairdocs.org/stc/ST02004WI): Installation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI). Peregrine
- [STC ST04281AT](https://openairdocs.org/stc/ST04281AT): Installation for the Upgrade of the NZ-2000 FMS computer for software version NZ6. Chippewa Aerospace Inc
- [STC ST01086DE](https://openairdocs.org/stc/ST01086DE): Installation of the True Blue Power TS60 Lithium-ion Nanophosphate batteries as an alternate to existing Grimes Emergency Exit Lighting (EEL) Power Supply. Peregrine
- [STC ST04210NY](https://openairdocs.org/stc/ST04210NY): Installation of LAI Windshield Panel A. Lee Aerospace Inc
- [STC ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC d/b/a West Star Aviation
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST10137SC](https://openairdocs.org/stc/ST10137SC): Installation of leather handgrip covers on control yoke. Textron Aviation Inc
- [STC ST04202NY](https://openairdocs.org/stc/ST04202NY): Installation of Lee Aerospace Inc. Window Panel B. Lee Aerospace Inc
- [STC ST03595NY](https://openairdocs.org/stc/ST03595NY): Installation of Honeywell Laseref IV Upgrade. Dassault Aircraft Services (DAS)
- [STC ST04265AT](https://openairdocs.org/stc/ST04265AT): Replacement of the inner aluminum barrel of the engine inlet cowl, with an inlet barrel of carbon graphite sandwich construction. Quiet Technology Aerospace
- [STC ST00934DE](https://openairdocs.org/stc/ST00934DE): Installation of Becker Avionics BXT6553 transponder. Peregrine
- [STC SA00096LA](https://openairdocs.org/stc/SA00096LA): Installation of a Patient Loading and Utility System (PLUS). LifePort LLC
- [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 ST01248CH](https://openairdocs.org/stc/ST01248CH): Installation of an air ambulance conversion. Spectrum Aeromed LLC dba Spectrum Aeromed
- [STC ST02068CH](https://openairdocs.org/stc/ST02068CH): Install air ambulance conversion. Spectrum Aeromed LLC dba Spectrum Aeromed
- [STC ST00790DE](https://openairdocs.org/stc/ST00790DE): Installation of BendixKing CAS 67B Traffic Alert and Collision Avoidance System (TCAS) II Version 7.1. Peregrine
- [STC ST00813DE](https://openairdocs.org/stc/ST00813DE): Replacement of Honeywell (formerly Sperry) ED-800 cathode ray tube (CRT) display, part number 7003110-90 I or 7003110-902, with Esterline CMC Electronics CMA-6800 multi-purpose liquid crystal display (LCD),. Peregrine
- [STC ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC
- [STC ST00135BO](https://openairdocs.org/stc/ST00135BO): Modification of Honeywell TCAS II system installation with R/T 910 and software Version 6.4a to R/T 910 with Change 7.0 software; or TCAS 2000 system with R/T 950, 951 and software Version 6.4a to R/T 950, 951 with Change 7.0 software. Pro Star Aviation, LLC
- [STC ST03139CH](https://openairdocs.org/stc/ST03139CH): Installation of Aircell Axxess II Iridium Satcom and High Speed Internet with Wireless Local Area Network (WLAN (IEEE 802.11 b, g, and n only)). Nextant Aerospace
- [STC ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc
- [STC ST00304WI](https://openairdocs.org/stc/ST00304WI): Installation of Keddeg Company 21BC113 coaleser assembly. Purolator Facet, Inc
- [STC ST01228WI](https://openairdocs.org/stc/ST01228WI): Replacement of OEM window pane assemblies with Lee Aerospace laminated window assembly and termination of OEM dry air system. Lee Aerospace, Inc
- [STC ST09069SC](https://openairdocs.org/stc/ST09069SC): Installation of King KHF-950 HF Communication Systems. Textron Aviation Inc
- [STC ST09158SC](https://openairdocs.org/stc/ST09158SC): Installation of a Honeywell TCZ-910 TCAS system. Textron Aviation Inc
- [STC ST04367AT](https://openairdocs.org/stc/ST04367AT): Removal of the Existing Honeywell DL-900 or DL-950 Data Loader and Installation of the Honeywell DL-1000 Data Loader. Chippewa Aerospace Inc
- [STC ST04154CH](https://openairdocs.org/stc/ST04154CH): Installation of acoustic insulation kit for Fuselage and Aft Pressure Bulkhead. Damping Technologies Inc
- [STC ST04155CH](https://openairdocs.org/stc/ST04155CH): Installation of acoustic insulation kit for Forward Wing-to-Body Fairing. Damping Technologies Inc
- [STC ST04156CH](https://openairdocs.org/stc/ST04156CH): Installation of acoustic insulation kit for Interior Panels. Damping Technologies Inc
- [STC ST09250AC](https://openairdocs.org/stc/ST09250AC): Logo light installation on lower surface of the horizontal stabilizer. Textron Aviation Inc
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST01560CH](https://openairdocs.org/stc/ST01560CH): Install Aero Medical Products Mfg., Inc. Air Ambulance Stretcher P/N 125 using Installation Kit P/N 805. Paul/ Lanna Egan LLC
- [STC ST02542LA](https://openairdocs.org/stc/ST02542LA): Installation of PPG Aerospace cockpit windshields P/Ns 196600-1 and 196600-2. PPG Aerospace
- [STC ST03185CH-D](https://openairdocs.org/stc/ST03185CH-D): Activation of a TrueNorth Avionics, Inc. Simphone WiFi System. Standard Aero
- [STC ST546CH-D](https://openairdocs.org/stc/ST546CH-D): Installation of an AlliedSignal Avionics, Dual GNS-XLS, Flight Management System with GPS as a primary means of navigation. Standard Aero
- [STC ST01933CH-D](https://openairdocs.org/stc/ST01933CH-D): Installation of Honeywell Runway Awareness and Advisory System (RAAS). Standard Aero
- [STC ST01406WI-D](https://openairdocs.org/stc/ST01406WI-D): Installation of the Honeywell Primus EPIC Control Display System/Retrofit (CDS/R). Duncan Aviation Inc
- [STC ST02146NY](https://openairdocs.org/stc/ST02146NY): Installation of EMS Technologies Ltd. Cabin Network Xcelerator (CNX). EMS Technologies Canada Ltd
- [STC ST01512LA-D](https://openairdocs.org/stc/ST01512LA-D): Installation of -218-218 software with Runway Awareness Advisory System (RAAS) activation option on Honeywell MK V Enhanced Ground Proximity Warning System (EGPWS). Gulfstream Aerospace Corporation

All 60: https://openairdocs.org/aircraft/N261PA/stcs.md

## Related

- Other Raytheon HAWKER 1000 aircraft: https://openairdocs.org/model/raytheon-hawker-1000/aircraft.md
- The Pratt & Whitney PW300 series engine: https://openairdocs.org/engine/pratt-whitney-pw300-series.md

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