N733CK
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
Maintenance disclosures
REJECTED TAKE OFF AT 60 KNOTS, AFT CARGO DOOR LIGHT INDICATED OPEN. RESECURED AFT CARGO DOOR IAW B737-345 AMM 52-31-00, NO DEFECTS NOTED. PERFORMED HIGH ENERGY STOP CONDITIONAL INSPECTION IAW B737-345 AMM 05-51-07, NO DEFECTS NOTED
DURING WALKAROUND FOUND RH FUEL BOOST PUMP DOOR MISSING. TRANSFERRED TO DMI #73300134, CAT D, DUE 7/29/26 IAW B737 KC2 MEL CDL REF 57-30-4, SPECIAL PROCEDURES DCL 57-30-04 COMPLIED WITH PLACARDS INSTALLED. PERFORMED GROUND HANDLING HITS AIRPLANE OR PART DEPARTS AIRPLANE CONDITIONAL INSPECTION IAW B737-400 AMM CH 05-51-59, NO DEFECTS NOTED.
WITH PUMPS ON, FUEL PUMPS TO CENTER TANK LOST OF ELECTRICAL POWER ON CLIMB OUT. PERFORMED AC GENERATION SYSTEM TEST IAW AMM 24-21-00. OPS CHECK PASS WITH NO DEFECTS NOTED. REF BLOCK 2 OF LP 737-004-1877 FOR CENTER TANK FUEL QUANTITY INDICATION ERROR. CENTER TANK FUEL QUANTITY INDICATOR SHOWS INACCURATE READING.
TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL AT 30 KNOTTS. FOUND SPEED BRAKE OUT OF DETENT, PUT SPEED BRAKE INTO DETENT AND PERFORMED AURAL WARNING OPERATION TEST IAW B737 AMM 31-26-00, OPS CHECK GOOD NO DEFECTS NOTED.
THE AIRCRAFT WOULD NOT PRESSURIZE. THE NUMBER ONE BLEED VALVE INDICATED 3 PSI. R&R #1 ENGINE BLEED AIR PRESSURE REGULATOR IAW B737 AMM 36-11-16, OPS CHECK GOOD. BLEED AIR SYSTEM LEAK CHECK GOOD IAW B737 AMM 36-11-05, PERFORMED ENGINE RUN TO IDLE, OPS CHECK GOOD IAW B737 AMM 71-00-00 NO DEFECTS NOTED
FWD PIT STATION APPRX 520 RBL APPRX 8 FRAME SUPPORT CRACKED.
AT STA 344 FRAME FOUND CRACKED BETWEEN S-22L AND S-23L AT 1 INCH HYDRAULIC LINE HOLE
FWD PIT FLOOR SUPPORT HAS CORROSION AT STA 540 RBL 16
FOUND CRACK INDICATION AT L-1 DOOR S-16 DOOR STOP LOWER FASTENER ROW MIDDLE HOLE.
DURING TAKEOFF ROLL ALL AIR DATA INFORMATION ON F/O SIDE NO ANALOG AIRSPEED, DIGITAL AIRSPEED, AC ALTIMETER, NO VSI, AND VAU WOULD NOT ENGAGE. DURING TAKEOFF CLIMB, FWD ENTRY LIGHT ILLUMINATED. CABIN ALT UNCONTROLLABLE IN AUTO MODE. ALL OF THESE RELATE TO THE SAME PROBLEM AND FIXED BY R/R THE CABIN PRESSURE CONTROLLER.
L/H WING GROUND SPOILER INBOARD ACTUATOR MOUNT FITTING CRACKED.
AFT CARGO COMPARTMENT STA 947 RBL 3 FLOOR CHANNEL HAS EVIDENCE OF CORROSION.
AFT CARGO COMPARTMENT STA 947 LBL 3 FLOOR CHANNEL HAS EVIDENCE OF CORROSION.
AFT CARGO COMPARTMENT STA 947 RBL 14 TRACK TIE DOWN HAS EVIDENCE OF CORROSION.
AFT CARGO COMPARTMENT STA 812 RBL 8 FLOOR CHANNEL HAS EVIDENCE OF CORROSION.
FWD GALLEY APPROX STA 312 LBL 11 FLOOR BEAM HAS EVIDENCE OF CORROSION.
FWD GALLEY APPROX STA 300 LBL 11 FLOOR SUPPORT HAS EVIDENCE OF CORROSION.
AFT CARGO PIT STRINGER IS STARTING TO CRACK APPROX STA 727C S-21 EA09.
AFT CARGO PIT STRINGER CLIP HAS CRACK STA 727E S-25 EA10
DUAL FMS FAILURE IN FLIGHT
2 BLEED TRIP OFF LIGHT WOULD NOT RESET AS RESULT CABIN ALTITUDE WARNING, THEN EMERGENCY DESCENT
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 727B BETWEEN STRINGERS 8L AND 9L
EXTERNAL FUSELAGE DOUBLER DENTED AT STA 344-360 BETWEEN STR 16R AND 18R
DAMAGED STRINGER TIE MAIN DECK STA 420 STR 9R
DAMAGED STRINGER TIE MAIN DECK STA 400 STR 9R
CRACK FOUND IN FUSELAGE SKIN AT LOWER AFT CORNER OF FWD GALLEY SERVICE DOOR CUTOUT APROXIMATE STATION 323 WL210
FOUND STRINGER CLIP TO BE CRACKED AT STA 727C S4L
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD AND OUTBOARD ATTACH RIVETS AT STA 380 BETWEEN STRINGERS 8R AND 9R
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD AND OUTBOARD ATTACH RIVET AND INBOARD FRAME RADIUS AT STA 400 BETWEEN STRINGERS 8R AND 9R
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 727D BETWEEN STRINGERS 8L AND 9L
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 867 BETWEEN STRINGERS 8L AND 9L
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 747 BETWEEN STRINGERS 8L AND 9L
CRACK INDICATION FOUND AT FUSELAGE FRAME AT SUPPORT BRACKET INBOARD ATTACH RIVET LOCATION AT STA 440 BETWEEEN STRINGERS 8R AND 9R
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 727D BETWEEN STRINGERS 8R AND 9R
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 747 BETWEEN STRINGERS 8R AND 9R
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 907 BETWEEN STRINGERS 8R AND 9R
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 867 BETWEEN STRINGERS 8R AND 9R
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 827 BETWEEN STRINGERS 8L AND 9L
PROBLEM DESCRIPTION: ENCOUNTERED BIRD STRIKE AFTER TAKEOFF RETURNED FOR LANDING AT KCVG, POST INSPECTION FOUND RIGHT AOA VANE BROKEN AND DAMAGE TO RAY DOME FROM BIRD STRIKE.
REJECTED TAKEOFF CONFIGURATION WARNING ON TAKEOFF. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: FOUND SPEED BRAKE HANDLE NOT STOWED, STOWED SPEED BRAKE HANDLE IAW B737 AMM 27-62-22, PERFORMED TAKEOFF WARNING TEST IAW B737 AMM 31-26-00 OPS CHECK GOOD.
PROBLEM DESCRIPTION: ABORTED TAKEOFF DUE TO CARGO DOOR LIGHT ILLUMINATING. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: INSPECTED AND PERFORMED OPERATIONS CHECK OF CARGO DOOR, IAW B737 AEI SUPPLEMENTAL AMM 52-33-02, NO DEFECTS NOTED.
EVIDENCE OF CORROSION, DUE TO SKIN BULGING, BETWEEN RH HORIZONTAL REAR SPAR UPPER CHORD AND UPPER SKIN @ R/H HORIZONTAL STAB STA 270
R/H ELEVATOR TAB LOWER SIDE @ ELE STA 34.25 CRACKED
REJECTED TAKE OFF AT 80 KNOTS FOR AFT CARGO DOOR LIGHT SWITCH. CLEANED CONTACTS AND PERFORMED OP'S CHECK. OP'S CHECK GOOD IAW AMM 52-13-00.
ABORTED TAKEOFF, AFTER MASTER CAUTION RED LIGHT ILLUMINATED FOR 2 SECONDS THEN WENT OFF. PILOT TAXIED OFF, RAN APPROPRIATE CHECKLIST THEN REQUESTED ANOTHER TAKE OFF. AIRCRAFT HAD NO MORE INDICATION PROBLEMS WITH MASTER CAUTION LIGHT FOR THE REST OF THE FLIGHT.
LEFT HAND ELEVATOR LOWER SURFACE PUNCTURED. REPAIRED LEFT ELEVATOR SURFACE PUNCTURE IAW SRM 55-20-01 REPAIR 1.
WEB FORWARD OF R1 HAS CORROSION. REPAIRED FLOOR STRUCTURE WEB AT STA 280 RIGHT HAND IAW SRM 51-70-13 FIG 1.
AFT CARGO COMPARTMENT TIE DOWN CORRODED, REPAIRED IAW SRM 53-00-53 FIG 201 REPAIR 2.
WEB FORWARD OF R1 HAS CORROSION. REPAIRED FLOOR STRUCTURE WEB AT STA 280 RIGHT HAND IAW SRM 51-70-13 FIG 1.
STRINGER SUPPORT STRUCTURE HAS CORROSION. REPAIRED STRINGER SUPPORT WEB AT STA 271R IAW SRM 51-70-13 FIG 1.
NR 7 FLAP TRACK HAS CRACKS IN THE HORIZONTAL FLANGES (IB AND OB). R&R FLAP TRACK WITH OVERHAULED IAW AMM 27-51-47.
PRESSURE WEB FORWARD SIDE CRACK IN WEB. REPAIRED PRESSURE WEB AT STA 178 LBL 15 IAW SRM 53-10-08, FIG 201 REPAIR 9.
LEFT HAND ELEVATOR UPPER SURFACE PUNCTURED. REPAIRED PUNCTURE ON UPPER SURFACE OF LEFT ELEVATOR IAW SRM 51-70-05, REPAIR 3.
EMERGENCY LIGHT FAILED LIGHTS TEST. R&R BATTERY PACK IAW AMM 33-51-51, OP'S CHECK GOOD.
EMERGENCY LIGHT FAILED LIGHTS TEST. R&R BATTERY PACK IAW AMM 33-51-51, OP'S CHECK GOOD.