- Registered owner
- Kalitta Charters II LLC
- Location
- Ypsilanti, MI
- Owner type
- LLC
- Serial number
- 26072
- Year built
- 1992
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 27, 2021
- Certificate issued
- August 2, 2021
- Expires
- August 31, 2028
- Mode S code
- A3A89E
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-3C model are included below.
On this page
Airworthiness directives that may apply · 19
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1990 | 1 |
|---|---|
| 1991 | 1 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 5 |
| 1999 | 1 |
| 2000 | 3 |
| 2001 | 1 |
| 2002 | 1 |
| 2007 | 1 |
| 2009 | 1 |
| 2013 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2022 | 1 |
Engine · CFM International CFM56-3C series
AD 2022-02-03Turbine Engine Accessory DriveAD 2017-14-08Turbine Engine Compressor SectionAD 2016-14-10High-pressure turbine (HPT) disksInformation bulletins that may apply · 1
Advisory, not mandatory.
Engine · CFM International CFM56-3C series
SAIB NE-08-17R3Turbine Section - Propulsion Technology LLC Unapproved RepairNTSB investigations
No NTSB investigations matched to N335CKMatched 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 Boeing 737-3Y0 aircraft
FAA incident reports
No FAA accident or incident reports matched to N335CKMatched 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 Boeing 737-3Y0 aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR K11A2025112500360Warning Light · false activationLEADING EDGE FLAPS TRANSIT LIGHT WOULD NOT EXTINGUISH IN FLIGHT. PERFORMED OPS CHECK OF LEADING EDGE FLAP AND SLAT POSITION INDICATING SYSTEM IAW AMM 27-88-00-215-013. OPS CHECK GOOD AT THIS TIME. FAULT CLEARED AIRCRAFT OK FOR SERVICE.SDR K11A2025071900327Fire Warning · false activationAPU FIRE INDICATION IN FLIGHT, FOLLOWED QRH PROCEDURE BLEW FIRE BOTTLE, FIRE LIGHT EXTINGUISHED PER QRH CHECK LIGHT CONTINUED TO AIRPORT. PERFORMED APU COMPARTMENT COMPONENT AND STRUCTURE INSPECTION IAW B737-300 AMM 05-41-07, NO DAMAGE, NO FIRE INDICATION NOTSDR K11A2024102500291Power Supply · inoperativeEMERGENCY LIGHTING INOP. REMOVED AND REPLACED L/H & R/H EMERGENCY LIGHTING POWER SUPPLIES IAW B737 AMM 33-51-51, OPS CHECK GOOD NO DEFECTS NOTEDSDR K11A2023053100209Unknown · unknownFRD ENTRY DOOR LIGHT ON TAKEOFF ROLL 10KTS REJECTED TAKEOFF AND RESCUED DOOR.SDR K11A2022090500157None · crackedPROBLEM DESCRIPTION: FIRST OFFICERS WINDSHIELD CRACKED IN FLIGHT. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: R&R R1 WINDOW IAW B737 AMM 56-11-11 OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIMESDR K11A2022021500112None · nonePROBLEM DESCRIPTION: GEN BUS SEEMS NOT TO BE POWERED. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: FOUND #1 DC BUS C/B POPPED RESET #1 DC BUS C/B, OPS CHECK GOOD IAW B737 AMM 20-60-05 AND 24-31-00, 21-21-00SDR K11A2021102200082Battery Pack · failedPROBLEM DESCRIPTION: DURING BRIDGING INSPECTION FOUND L/H EMERGENCY LIGHT INOP, CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: REMOVED AND INSTALLED SERVICEABLE L/H EMERGENCY BATTERY PACK IAW B737 AMM 33-51-51 OPS CHECK PAS NO DEFECTS NOTED
STCs that may be installed · 5
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · CFM International CFM56-3C series
STC SE00032ENInstallation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Fan/Booster Module.STC SE00033ENInstallation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Compressor ModuleSTC SE00034ENInstallation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Turbine ModuleSTC SE00035ENInstallation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Low Pressure Turbine ModuleSTC SE00822CHInstall AeroControlex P/N 2604880-001 variable stator feedback control cable and P/N 2604880-002 variable bleed valve feedback control cable on CFM International engines.