- Registered owner
- Kalitta Charters II LLC
- Location
- Ypsilanti, MI
- Owner type
- LLC
- Serial number
- 26070
- Year built
- 1992
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 9, 2022
- Certificate issued
- December 21, 2021
- Expires
- December 31, 2028
- Mode S code
- A3AC55
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 N336CKMatched 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 N336CKMatched 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR K11A2026090700391Door · unsecureTHE CABIN DIDN’T PRESSURIZE IN ALL MODES OF PRESSURIZATION PANEL. PERFORMED PRESSURIZATION WITH APU IAW AMM 21-31-00, OPS CHECK GOOD AT THIS TIME NO DEFECTS NOTED. ON WALKAROUND FOUND L2 DOOR PARTIALLY OPEN, DOOR WILL NOT LATCH PROPERLY. PERFORMED OPERATIONASDR K11A2025123100365Seat · faultedREJECTED TAKEOFF AT 115 KNOTS. THE CAPTAINS SEAT UNLOCKED AND SLAMMED TO THE AFT. ADJUSTED CAPTAINS SEAT IAW B737 AMM 25-11-11, OPS CHECK GOOD NO DEFECTS NOTED. PERFORMED CONDITIONAL INSPECTION FOR HIGH SPEED STOPPAGE ONCE BRAKES COOLED TO TOUCH IAW B737 AMMSDR K11A2025071700235Control Cable · out of adjustLANDING GEAR LEVER WOULD NOT GO UP WHILE ON TAKEOFF DURING RETRACTION. ADJUSTED MAIN GEAR AIR / GROUND CABLE IAW AMM 32-21-11. PERFORMED OPS CHECK IAW AMM 32-21-11. PERFORMED GEAR SWING SYSTEM OPS CHECK NORMAL.SDR K11A2024080600274Pushrod · out of alignmentON APPROACH THE AIRCRAFT EXPERIENCED WAKE TURBULENCE AND PERFORMED A GO AROUND AND LANDED SAFELY. ON POST FLIGHT WALK AROUND FOUND #5 & #6 LEADING EDGE SLATS MISALIGNED. PERFORMED PHASE 1 AND 2 OVERSPEED CONDITIONAL INSPECTION IAW B737 AMM 5-51-41 REF CJI WORSDR K11A2023121800247Unknown · unknownLANDING GEAR LEVER STOPPED IN OFF POSITION WHEN TRYING TO GET GEAR UP AFTER TAKE OFFSDR K11A2023082200227Unknown · unknownABORTED TAKEOFF DUE TO TAKEOFF WARNING SOUNDED DURING TAKEOFFSDR K11A2023062800215Unknown · unknownAPU FIRE LIGHT ILLUMINATED ON START, THE FIRE T HANDLE WAS PULLED AND DISCHARGED.SDR K11A2022092400165Engine · surgesNR 1 ENGINE SURGE DURING TAKEOFF. R&R NR 1 ENGINE IAW AMM 73-21-04
PERFORMED PLA GEN ADJ / TEST IAW AMM 71-00-00, PERFORMED VSV DYNAMIC RIG IAW AMM 75-31-00, PERFORMED TEST 1,3 & 6 IAW AMM 71-00-00 ALL CHECKS GOOD NO DEFECTS NOTED.SDR K11A2022090600159Mec · failed inspPROBLEM DESCRIPTION: #1 ENGINE SURGE ON CLIMB OUT, FF AND N1 INDICATIONS POINTED TO SURGE. #1 THROTTLE PULLED BACK AND SURGE LESSENED. AIRCRAFT NOTICEABLY SHAKING DURING SURGE. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: R&R FUEL PUMP IAW B737 AMM 73-11-SDR K11A2022081200154None · noneABOVE 10,000 FT. THE DIFFERENCE BETWEEN THE CAPTAIN AND FIRST OFFICERS ALTIMETER IS APPROX. 500 FT., CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: PITOT PROBE INSPECTION PASSED IAW B737 AMM 34-11-11, PITOT STATIC HIGH LEVEL LEAK CHECK PASSED IAW B737 AMM 34SDR K11A2022060100129Stringer · crackedFRAME AT STA 360 STR 20R HAS A CRACK IN THE WEB AROUND INSULATION STUD HOLE ON FWD SIDESDR K11A2022060100128Door Frame · crackedFWD CARGO DOOR FRAME STA 492 DTR-24R IS CRACKED AT UPPER INBD HOLE. ENDS OF CRACK ARE MARKED.SDR K11A2022121800174Door · not closedCABIN ALTITUDE UNCONTROLLABLE WITH AUTO, STANDBY OR MANUAL SYSTEMS. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: FOUND AFT ENTRY DOOR NOT CLOSED COMPLETELY CLOSED AFT ENTRY DOOR IAW B737 AMM 52-73-00, PERFORMED PRESSURIZATION OPS TEST IAW B737 AMM 21-31-00
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.