N336CK
Registered owner: KALITTA CHARTERS II LLC, MI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
REJECTED 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 AMM 05-51-07, OPS CHECK GOOD NO DEFECTS NOTED
LANDING 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.
ON 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 WORK PACKAGE # CRS OMJR606K FOR WORK PERFORMED. R&R 1 AFT FLAP PUSH ROD, R&R THREE FLAP TRACKS FOR WEAR INDICATIONS AND NUMEROUS BEARINGS
LANDING GEAR LEVER STOPPED IN OFF POSITION WHEN TRYING TO GET GEAR UP AFTER TAKE OFF
ABORTED TAKEOFF DUE TO TAKEOFF WARNING SOUNDED DURING TAKEOFF
APU FIRE LIGHT ILLUMINATED ON START, THE FIRE T HANDLE WAS PULLED AND DISCHARGED.
NR 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.
PROBLEM 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 73-11-01, R&R #1 ENGINE MEC IAW B737 AMM 73-21-01, PERFORMED BORESCOPE OF HPC STG 1, 3 AND 8 BLADES WITH NO DEFECTS FOUND, PERFORMED LEAK & OPS CHECK OF FUEL PUMP & MEC IAW B737 AMM 71-00-00 TEST 6 NO DEFECTS NOTED AT THIS TIME. REF KALITTA MX W/O 933600709 FOR WORK PERFORMED AND SIGNATURES, DETAILS AND TAGS
ABOVE 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 34-11-00, NO FAULTS FOUND.
FRAME AT STA 360 STR 20R HAS A CRACK IN THE WEB AROUND INSULATION STUD HOLE ON FWD SIDE
FWD CARGO DOOR FRAME STA 492 DTR-24R IS CRACKED AT UPPER INBD HOLE. ENDS OF CRACK ARE MARKED.
CABIN 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 NO DEFECTS NOTED OPS CHECK GOOD