- Registered owner
- Calla Airways LLC
- Location
- Cohasset, MA
- Owner type
- LLC
- Serial number
- 259003
- Year built
- 1998
- Type
- Fixed wing multi engine
- Engine
- Turbo-jet
- Airworthiness
- Standard, transport
- Airworthiness date
- April 17, 1998
- Certificate issued
- October 18, 2005
- Expires
- July 31, 2028
- Mode S code
- A283FA
Raytheon HAWKER 1000TCDS A3EUAirframe · Raytheon HAWKER 1000Engine modelPratt & Whitney PW300 series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PW300 model are included below.
On this page
Airworthiness directives that may apply · 30
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1994 | 3 |
|---|---|
| 1995 | 2 |
| 1996 | 7 |
| 1997 | 2 |
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 4 |
| 2001 | 3 |
| 2002 | 1 |
| 2003 | 1 |
| 2006 | 4 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 1 |
| 2016 | 1 |
| 2023 | 1 |
| 2026 | 1 |
Airframe · Raytheon HAWKER 1000
AD 2026-13-02NavigationAD 2023-10-02Indicating/Recording System, NavigationAD 2016-13-13Engine ExhaustInformation bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Raytheon HAWKER 1000
SAIB AIR-21-15R1Navigation SystemSAIB NM-15-24Landing GearSAIB NM-14-05Wing: AileronsSAIB NM-11-60Landing GearHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N261PAMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Raytheon HAWKER 1000 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ZKFA20240701058Filter Housing · pulledDURING 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 OFF. ONE HOLD DOWN STUD HAD COMPLETELY PULLED ITS THREADS OUT OF THE OIL FILTER HOUSING. A SECOND HOLDSDR ZKFA2024030600201Electronic Unit · overheatedPILOTS NOTICED SMOKE SMELL IN COCKPIT DURING CRUISE FLIGHT, ON TRIP KHYA-KAPF, FOLLOWED BY OBSERVING SMOKE. CONDUCTED EMERGENCY DESCENT AND LANDING AT KSAV. MAINT TECHNICIAN FOUND 2 AC CIRCUIT BREAKERS TRIPPED IN LEFT WINDSCREEN CIRCUIT AND LEFT WINDSCREEN ELESDR 2022F00364None · noneAIRCRAFT IMPACTED A DEER ON LANDING AT KPYM. RIGHT TRAILING EDGE FLAP WAS DAMAGED BEYOND REPAIR AND WAS REPLACED.SDR 2022F00244None · noneAIRCRAFT 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 COPILOTS INSTRUMENT PANEL NEXT TO THE GEAR HANDLE. A FLAME WAS BRIEFLY OBSERVED BY THE COPILOT IN THE SASDR 2021FA0000311Hinge · corrodedRH AILERON SIGNIFICANT CORROSION FOUND AT CENTER TRIM TAB HINGE, AROUND BONDING STRAP ATTACHMENT HOLE, IN AFT SPAR STRUCTURE. TEXTRON ENGINEERING NOTIFIED AND NO REPAIR ALLOWED. NO NEW REPLACEMENT AILERONS AVAILABLE. ACQUIRED AS REMOVED RH AILERON S/N DHB1002 SDR ZKFR20130724001Attach Fitting · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON LT SIDE OF VERTICAL TO HORIZONTAL STABILIZER ATTACH FITTING. CORROSION IS INTERGRANULAR, AND IS LOCATED AROUND 12 FASTENER HEADS.SDR ZKFR20130117002O-Ring · leakingDURING 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 IT WAS O/H. REMOVED AND REPLACED WHEEL/TIRE ASSY. INSPECTED REMOVED WHEEL ASSY AND FOUND AIR LEASDR ZKFR20130117001O-Ring · leakingDURING 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 IT WAS O/H. R & R WHEEL/TIRE ASSY. INSPECTED REMOVED WHEEL ASSY AND FOUND AIR LEAKING FROM RIM NEASDR ZKFR20120605001Check Valve · leakingOXYGEN 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 REPLACED UNIT.SDR ZKFR20120530001Check Valve · leakingOXYGEN 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-RETUEN VALVE AND LEAK CHECKED GOOD. THIS NON RETURN VALVE WAS JUST INSTALLED 9 MONTHS AGO FOR THSDR ZKFR2012040900001Skin · delaminatedDURING 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 ALL LIMITS OF REPAIR. THE REPAIR IS USUALLY FOR A SMALL AMOUNT OF LIFTING AT THE CORNERS OF THE BOSDR ZKFR201112163233Controller · faultyCABIN TEMPERTURE UNCONTROLLABLE IN AUTO MODE. FOUND CABIN TEMPERTURE CONTROLLER NOT PROVIDING ANY OUTPUT VOLTAGE. CONTROLLLER GIVES MOMENTARY PULSES ONLY VISIBLE USING A TEST LAMP WHICH CAUSES TEMP CONTROL VALVE TO "CLICK" BUT NOT ENOUGH TO MOVE VALVE. R & SDR 2011F00036Starter Gen · failedACFT EXPERIENCED MODERATE VIBRATION IN CRUISE, FLIGHT CREW FELT VIBRATION WAS FROM NR 2 ENGINE, FOLLOWED SHORTLY AFTER WITH GEN 2 FAIL INDICATION, CREW SHUTDOWN NR 2 ENGINE, FLIGHT DIVERTED FOR NON-EVENTFUL SINGLE ENGINE LANDING. MX REMOVED NR 2 ENGINE STARTESDR 2011F00000Starter Gen · destroyedDURING CRUISE FLIGHT, EXPERIENCED VIBRATION, BELIEVED TO BE FROM ENGINE AREA. VIBRATION INCREASED, BUT DID NOT SHOW ON EVM INDICATOR, FOLLOWED BY GEN 1 FAIL INDICATION, WITH BUS TIE CLOSED IN FLIGHT. ACFT MADE UNSCHEDULED LANDING. MX FOUND NR1 STARTER GEN FSDR AJC2004F00002Position Switch · damagedDURING 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 PLACED GEAR LEVER IN DOWN POSITION AND HORN SILENCED. CREW CIRCLED AND BURNED OFF FUEL AND RETURNED TO
STCs that may be installed · 60
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.