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Aircraft record

N61GB2002 Beechcraft 400A

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 198218 ADs may apply6 service difficulty reports

Registration
Valid
expires Feb 28, 2030
Based in
Grand Island, NE
owner city / state
Owners
1
since 2023
NTSB events
None
since 1982
ADs may apply
18
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Kilo Papa LLC
Owner type
LLC
City, state
Grand Island, NE
Certificate issued
Feb 4, 2023
Expires
Feb 28, 2030
Airworthiness
Standard · Transport
Airworthiness date
Jul 23, 2002

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Beechcraft
Model
400A
Year
2002
Serial number
RK-341
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
10
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A7ECFD

Engine

Make and model
P&W Canada Jt15d 5 Ser
Type
Turbo-fan
Power
2,900 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2023 – nowKilo Papa LLCGrand Island, NE · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (18)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2014-21-06Flight ControlsNov 28, 2014Airframe (400A)Certain serial numbers: 400 RJ-1–RJ-65; 400A RK-1–RK-604; 400T TT-1–TT-180; 400T TX-1–TX-13; MU-300 A003SA–A093SA
2014-15-15StabilizersSep 5, 2014Airframe (400A)Certain serial numbers: MU-300 A003SA–A093SA; 400 RJ-1–RJ-65; 400A RK-1–RK-604; 400T TT-1–TT-180; 400T TX-1–TX-13
2013-03-07Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft…Mar 19, 2013Airframe (400A)Certain serial numbers: 400A RK-45; 400A RK-49–RK-353; 400A RK-354–RK-594
2011-03-12Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft…Mar 14, 2011Airframe (400A)Certain serial numbers: 400A RK-337–RK-484; 400A RK-486–RK-570; 400A RK-572; 400A RK-573; 400A RK-575–RK-577; 400T TX-13
2009-07-02Hawker Beechcraft Corporation Model MU-300-10 Airplanes and Model 400 and 400A Series…Apr 30, 2009Airframe (400A)Certain serial numbers: 400 RJ-1–RJ-65; 400A RK-1–RK-93; MU-300-10 A1001SA–A1011SA; MU-300 A003SA–A091SA
Show all 18 ADs
ADSubjectEffectiveApplies to
2008-24-10Pratt & Whitney Canada Corp. JT15D-5; -5B; -5F; and -5R Turbofan EnginesJan 2, 2009Engine (JT15D 5 SER)Certain serial numbers: JT15D-5 …–PCE-100411; JT15D-5 …–PCE-JA0818; JT15D-5R …–PCE-JG0104. Only with: Compressor air to HMU delivery tube P/N 3119150-01 installed; all JT15D-5B and -5F engines and all JT15D-5 engines converted to JT15D-5R per P&WC SB No. 7605 are included.
2006-21-02Raytheon (Beech) Model 400, 400A, and 400T Series Airplanes; and Raytheon (Mitsubishi)…Oct 25, 2006Airframe (400A)
2006-15-16Raytheon (Beech) Model 400 and 400A Series AirplanesSep 5, 2006Airframe (400A)Certain serial numbers: 400 RJ-1–RJ-65; 400A RK-1–RK-23. Only with: Kit P/N 128-3004-1 P or 128-3004-3 P (Lucas Aerospace/Goodrich DC Starter Generator) has been incorporated.
2004-03-35Raytheon Model Beech 400A and 400T Series AirplanesMar 24, 2004Airframe (400A)Certain serial numbers: 400A RK-45; 400A RK-49–RK-322; 400T TT-1–TT-180; 400T TX-1–TX-12
2003-10-13Raytheon Model Beech 400A and 400T Series AirplanesJul 1, 2003Airframe (400A)Certain serial numbers: 400A RK-232–RK-265; 400T TX-10
2002-01-23Raytheon Model Beech 400, 400A, and 400T Series Airplanes; Model Beech MU-300-10…Feb 14, 2002Airframe (400A)Certain serial numbers: 400 RJ-1–RJ-65; 400A RK-1–on; 400T TT-1–TT-180; 400T-1 TX-1–TX-11; MU-300-10 A1001SA–A1011SA; MU-300 A003SA–A091SA
2001-24-11Raytheon Model Beech 400, 400A, and 400T Series Airplanes, Model Mitsubishi MU-300…Dec 11, 2001Airframe (400A)
2001-20-07Raytheon Model Beech 400A Series AirplanesNov 15, 2001Airframe (400A)Certain serial numbers: 400A RK-78; 400A RK-87–RK-207
2000-09-12Raytheon (Beech) Model 400A and 400T Series AirplanesJun 16, 2000Airframe (400A)Certain serial numbers: 400A RK-01–RK-188; 400T TT-01–TT-180; 400T TX-01–TX-09
99-21-26Raytheon (Beech) Model 400, 400A, 400T, and MU-300-10 AirplanesNov 22, 1999Airframe (400A)Certain serial numbers: 400A RK-1–RK-107
99-21-08Raytheon (Beech) Model 400A AirplanesNov 12, 1999Airframe (400A)Certain serial numbers: 400A RK-1–RK-92
98-06-30Raytheon (Beech) Model 400, 400A, 400T, MU-300, and MU-300-10 AirplanesApr 24, 1998Airframe (400A)Serial numbers per AlliedSignal Aerospace Service Bulletin 103570-21-4012, Revision 1. Only with: Equipped with AlliedSignal outflow/safety valves identified in AlliedSignal Aerospace Service Bulletin 103570-21-4012, Revision 1.
96-25-03Raytheon (Beech) Model 400A, 400T (Military T-1A), and 400T (Military TX) Series AirplanesJan 24, 1997Airframe (400A)Serial numbers per Beech Service Bulletin No. 2522, dated January 1994, and Raytheon Service Bulletin No. 2522, Revision 1, dated May 1996

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (6)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Air conditioning and pressurization · controller · failedMar 10, 2023

    THE FLIGHT CREW REPORTED THAT THE VAPOR CYCLE A/C SYSTEM STOPPED WORKING AND TRIPPED THE CIRCUIT BREAKER. THE SYSTEM WAS PLACED ON MEL 21-50-01 AND FLIGHT OPERATIONS WERE CONTINUED. THE MAINTENANCE TEAM REMOVED AND REPLACED THE AUTO LOAD SHED CONTROLLER WITH A NEW UNIT . OPERATIONAL CHECKS OF THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · none · noneApr 15, 2022

    THE FLIGHT CREW REPORTED WHILE AT FL360 - FL400 NO CABIN TEMPERATURE CONTROL FROM COCKPIT CONTROLLER IN AUTO OR MAN CABIN TEMP RANGED FROM 20C TO -10C OVER 3.7 HOUR FLIGHT. THE MAINTENANCE TEAM DISCOVERED A LOOSE CONNECTION ON CABIN PROPORTIONING VALVE AND ALSO FOUND CABIN AND COCKPIT TEMP CONTROL…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · mixing valve · stuckNov 10, 2021

    THE FLIGHT CREW REPORTED THAT DURING BRAKING THE COPILOTS LEFT BRAKE PEDAL FADED DURING OPERATION. THE MAINTENANCE TEAM TROUBLESHOT THE BAKE SYSTEM AND FOUND THE LEFT MIXING VALVE INTERNAL SPRING STUCK IN THE CLOSED POSITION CAUSING PRESSURE BUILD UP IN THE CO-PILOTS BRAKE SYSTEM WHICH LET TO THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Navigation · computer · faultedJul 12, 2021

    THE FLIGHT CREW REPORTED THE ANGLE OF ATTACK INDICATOR (AOA) WAS INOP. OPERATIONS CONTINUED MEL DEFERRAL. THE MAINTENANCE TEAM TROUBLESHOT AND FOUND A FAULT WITH THE RIGHT STALL WARNING COMPUTER. THE COMPUTER WAS REMOVED AND A SERVICEABLE COMPUTER WAS INSTALLED. OPERATIONS SATISFACTORY AND THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine air · anti-ice valve · defectiveFeb 6, 2021

    THE FLIGHT CREW REPORTED A RIGHT ENGINE TEMP LOW ANNUNCIATOR WHILE IN FLIGHT AND REMAINED ILLUMINATED WITH N2 AT 82%. THEY INDICATED THE ITT DID SHOW A RISE DURING SWITCH OPERATION. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE ENGINE ANTI-ICE VALVE WAS DEFECTIVE. THE DEFECTIVE VALVE WAS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · skin · damagedJan 5, 2021

    DURING PREFLIGHT CHECKS THE MAINTENANCE TEAM DISCOVERED ELEVATOR SKIN DAMAGE NEAR THE MIDDLE HINGE ON THE BOTTOM SIDE. INVESTIGATION DETERMINED THAT THIS DAMAGE WAS CAUSED WHEN A MAINTENANCE VENDOR COMPLETING INSPECTION CHECKS ON THE HORIZONAL STAB, INSTALLED THE ELEVATOR IN A CARELESS MANNER. THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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