- Registered owner
- Kilo Papa LLC
- Location
- Grand Island, NE
- Owner type
- LLC
- Serial number
- RK-341
- Year built
- 2002
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 23, 2002
- Certificate issued
- February 4, 2023
- Expires
- February 28, 2030
- Mode S code
- A7ECFD
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada JT15D 5 model are included below.
On this page
Airworthiness directives that may apply · 47
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1991 | 1 |
|---|---|
| 1992 | 2 |
| 1993 | 7 |
| 1994 | 6 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 2 |
| 2000 | 2 |
| 2001 | 4 |
| 2002 | 2 |
| 2003 | 1 |
| 2004 | 3 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 2 |
| 2011 | 2 |
| 2013 | 1 |
| 2014 | 2 |
| 2023 | 1 |
| 2026 | 1 |
See all 51 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Raytheon 400A
SAIB CE-18-24Flap Cable InspectionSAIB NM-13-19Airfoil Anti/De-ice SystemSAIB NM-12-25Auto Flight: Altitude ControllerEngine · Pratt & Whitney Canada JT15D 5 series
SAIB NE-07-03Dual-engine flameoutsNTSB investigations
No NTSB investigations matched to N61GBMatched 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 400A aircraft
FAA incident reports
No FAA accident or incident reports matched to N61GBMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Raytheon 400A aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 9JLA2023041336301Controller · failedTHE 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 ASDR 9JLA2022042533543None · noneTHE 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 ALSSDR 9JLA2021111733521Mixing Valve · stuckTHE 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 COSDR 9JLA2021080527037Computer · faultedTHE 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 INSTALLESDR 9JLA2021021227023Anti-Ice Valve · defectiveTHE 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 SDR 9JLA2021010827018Skin · damagedDURING 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
STCs that may be installed · 134
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Raytheon 400A
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST01999WIModification to replace the lead-acid battery with a True Blue Power TB40 Nanophosphate Lithium-Ion battery.