N336CK

ATA 2510

Part: SEAT — FAULTED (ZONE 200) · airframe 61,038 hrs · 40,661 cycles

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

ATA 3230

Part: CONTROL CABLE — OUT OF ADJUST (ZONE 700) · airframe 60,818 hrs · 40,407 cycles

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.

ATA 5754

Part: PUSHROD — OUT OF ALIGNMENT (NR 5 & 6) · airframe 60,260 hrs · 39,989 cycles

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

ATA 3234

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 59,961 hrs · 39,821 cycles

LANDING GEAR LEVER STOPPED IN OFF POSITION WHEN TRYING TO GET GEAR UP AFTER TAKE OFF

ATA 3150

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 59,749 hrs · 39,683 cycles

ABORTED TAKEOFF DUE TO TAKEOFF WARNING SOUNDED DURING TAKEOFF

ATA 2610

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 59,663 hrs · 39,626 cycles

APU FIRE LIGHT ILLUMINATED ON START, THE FIRE T HANDLE WAS PULLED AND DISCHARGED.

ATA 7200

Part: ENGINE — SURGES (NR 1) · airframe 59,123 hrs · 39,342 cycles

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.

ATA 7300

Part: MEC — FAILED INSP (ZONE 400) · airframe 59,078 hrs · 39,318 cycles

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

ATA 3416

Part: NONE — NONE · airframe 59,039 hrs · 39,298 cycles

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.

ATA 5300

Part: STRINGER — CRACKED (ZONE 100) · airframe 58,983 hrs · 39,257 cycles

FRAME AT STA 360 STR 20R HAS A CRACK IN THE WEB AROUND INSULATION STUD HOLE ON FWD SIDE

ATA 5310

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 58,983 hrs · 39,257 cycles

FWD CARGO DOOR FRAME STA 492 DTR-24R IS CRACKED AT UPPER INBD HOLE. ENDS OF CRACK ARE MARKED.

ATA 2130

Part: DOOR — NOT CLOSED (ZONE 800) · airframe 59,328 hrs · 39,458 cycles

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