N332CK
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
FLOOR SUPPORT IN FWD PIT AT STA 485 LBL 18.2 CORRODED
FLOORBEAM LOWER CHORD AT STA 767 APPROX RBL 34 HAS CORROSION.
FLOORBEAM LOWER TEE AT BS 747 AT APPROX RBL 24 TO RBL 45 IS CORRODED.
EVIDENCE OF CORROSION ON STRINGER 21R AT STA 890.
EVIDENCE OF CORROSION ON STRINGER 22R AT STA 880.
#1 PYLON PANEL 5724L OPENING ON I/B SIDE OF #1 PYLON HAS EVIDENCE OF POSSIBLE CRACK EXTENDING PAST STOP DRILL ON PYLON SKIN AND DOUBLER.
EVIDENCE OF CORROSION ON BOTTOM SECTION OF VERTICAL STIFFENER ON FWD SIDE OF STA 227 BULKHEAD BL0
EVIDENCE OF CORROSION ON STIFFENER IN FWD ACCESSORY COMPARTMENT STA 219 - 227 BL-0.
EVIDENCE OF CORROSION ON STRINGER 26L AT STA 907
STIFFENER AT STATION 352 BETWEEN STRINGER 27R AND 26R HAS EVIDENCE OF CORROSION
FRAME IN FWD PIT STA 520 BETWEEN STR 26R-27R HAS EVIDENCE OF CORROSION ON LWR LEG.
STATION 226 RBL 7 TO LBL 2 EVIDENCE OF CORROSION UNDER LEVELING COMPOUND ON A/C SKIN.
KEEL BEAM FOUND TO HAVE EVIDENCE OF CORROSION IN FWD PIT AT APPROX STA 500D STR-28R.
INTERCOSTAL ASSY HAS EVIDENCE OF CORROSION ON AFT SIDE OF FWD GALLEY DOOR SURROUND STRUCTURE AT APPROX STA 332-344 STR 16R
INTERCOSTAL ASSY HAS EVIDENCE OF CORROSION ON AFT SIDE OF FWD GALLEY DOOR SURROUND STRUCTURE AT APPROX STA 332-344 ABOVE STR 13R
WEB HAS EVIDENCE OF CORROSION ON AFT SIDE OF FWD GALLEY DOOR SURROUND STRUCTURE AT APPROX STA 332 - 344 STR 7.
DAMAGED ANGLE ON FWD SIDE OF STA 1016 BBL 0.00 FLOOR BEAM AT AFT CARGO COMPARTMENT
L/H AFT CARGO FLOOR SUPPORT AT LBL 12 HAS CORROSION UNDER NUTPLATE APPROX 6 INCHES AFT OF STA 727D.
#3 SLAT HAS EVIDENCE OF CORROSION ON UPPER SURFACE
EVIDENCE OF CORROSION ON STRINGER S25L STA 927 AT AFT CARGO COMPARTMENT.
EVIDENCE OF CORROSION ON FUSELAGE SKIN NEAR STA 520 STR 0
FLOOR BEAM IN AFT PIT CEILING AT STATION 727B HAS CORROSION AROUND FASTENER HOLES FROM LBL 4 TO LBL 58
AUTO PILOT CMD IN A AND B WILL NOT ENGAGE. PERFORMED DFCS BITE CHECK IAW B737 AMM 22-11-34. OPS CHECK GOOD NO FAULTS STORED. COULD NOT DUPLICATE ON GROUND, THIS CLEARS DMI 33200051 PLACARDS REMOVED.
CABIN ALTITUDE WARNING HORN AND LIGHT CAME ON DURING FLIGHT @ FL 360. LEFT BLEED WAS SHOWING 12 PSI AND RIGHT BLEED WAS SHOWING 38 PSI.
CABIN ALTITUDE WARNING HORN AND LIGHT CAME ON DURING FLIGHT @ FL 360. LEFT BLEED WAS SHOWING 12 PSI AND RIGHT BLEED WAS SHOWING 38 PSI. REMOVED AND REPLACED CONNECTOR D1208 IAW SWPM 20-61-11. PERFORMED ENGINE RUN IAW AMM 71-00-00. EGT SYSTEM OPS CHECKS GOOD IAW AMM 77-21-00. NO DEFECTS NOTED.
WHILE ON DESCENT LOST CABIN PRESSURE AT 33,000 FEET MADE EMERGENCY DECENT BOTH PACKS OPERATED NORMAL NO PACK TRIP. CORRECTIVE ACTION: REMOVED AND REPLACED CABIN PRESSURE CONTROLLER OPS CHECK GOOD.
WHILE ON DECENT LOST CABIN PRESSURE AT 33,000 FEET MADE EMERGENCY DECENT BOTH PACKS OPERATIONAL NORMAL NO PACK TRIP.
AIRSPEED INDICATOR F/O SIDE ROSE TO 62 KTS AND STOPPED. FAILED 80 KTS CHECK. CORRECTIVE ACTION: RESECURED FIRST OFFICERS AIR DATA COMPUTER Q.D. SENSE LINE IAW B737 AMM 34-12-11. OPS CHECK GOOD.
DURING CLIMB ENGINE 1 WOULD NOT ACHIEVE COMMAND POWER SETTING AFTER INITIAL THRUST REDUCTION FROM TAKEOFF POWER ENGINE 1N HUNG BELOW 70% WHILE N2 INCREASED TO LIMITS.
PROBLEM DESCRIPTION: RIGHT PACK TRIP UNABLE TO CONTROL CABIN PRESSURE UNTIL 10,000 FEET. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: REMOVED DEBRIS FROM AFT PIT DOOR, PERFORMED CABIN PRESSURIZATION CHECK IAW B737 AMM 21-31-00 OPS CHECK GOOD NO DEFECTS NOTED
INTERMITTENT CONTROL OF PRESSURIZATION. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: R&R CABIN PRESSURE CONTROL PANEL IAW B737 AMM 21-31-21 OPS CHECK GOOD IAW B737 AMM 21-31-00 NO DEFECTS NOTED
DURING FUNCTIONAL FLIGHT FOR FLAP REMOVAL EXPERIENCED HIGH FREQUENCY BUFFET CLIMBING THROUGH FL 240 @ 280 KIAS, CLEAN WING. INSPECTED AND OPS CHECK TRAILING EDGE FLAPS, LEADING EDGE FLAPS AND KRUEGER FLAPS IAW AMM 27-51-00, 27-81-00 NO DEFECTS NOTED. AIRCRAFT PASSED FUNCTIONAL EVAL FLIGHT ON NEXT FLIGHT AND HAS FLOWN 20 HOURS AND 17 CYCLES SINCE THIS CLEARING ACTION
L5 WINDOW CRACKED IN FLIGHT. AIRCRAFT RETURNED TO KSAT. R & R L5 WINDOW, IAW AMM 56-11-31.
SKIN DAMAGED STA 1080 FWD OF APU ACCESS DOOR
AT STA 291.5 STR 14R R1 DOOR LOWER HINGE CUTOUT HAS CRACK INDICATION
LT HORIZONTAL STAB FWD LOWER FITTING CORRODED
AT STATION 277-360 STR 20L OUTER "T" CHORD IS CRACKED
MAIN DECK FLOOR BEAM STA 312 LBL 12 HAS CORROSION AT INTERSECTION
R/H TORQUE BOX STRINGER STA 1088-1156 IS CORRODED
R/H TORQUE BOX STRINGER STA 1088-1130 IS CORRODED
CRACK INDICATION AT STA 500 = 11" STR 14R
L/H WING @ THE MAIN LANDING GEAR SUPPORT BEAM SUPPORT FITTING REAR SPAR STA 224.14 @ UPPER CHORD CRACKED INDICATION
CRACK FOUND ON STIFFNER LBL 6.15 ON THE WING CENTER SECTION REAR SPAR
CRACK FOUND ON STIFFNER RBL 6.15 ON THE WING CENTER SECTION REAR SPAR
RIGHT WING AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM IS CRACKED
LEFT WING AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM IS CRACKED
AT STA 636-663 LBL 60MAIN DECK SEAT TRACK HAS AREAS OF CORROSION
CUSP WEB CRACKED AFT OF BS 616 RBL 64
CUSP WEB CRACKED FWD OF BS 639 LBL 70
BS 639 RBL 45.5 WL 204 FLLORBEAM WEB CRACKED @ 2 LOWER FASTER HOLES
CUSP WEB CRACKED FWD OF BS 639 RBL 70
CUSP WEB CRACKED AFT OF BS 616 LBL 64 & LBL 70
R/H I/B AFT UPPER SIDE OF FRONT SPAR CHORD LUG HAS GOUGED AREAS AROUND WASHER
L/H I/B UPPER SIDE OF FRONT SPAR CHORD LUG HAS GUAGED AREAS AROUND WASHER (HORIZONTAL STAB)
R/H FRAME @ STA 500B HAS A CRACK IN THE INBD SIDE OF POWER CABLE HOLE BETWEEN S-20 & S-21
LEFT WING UPPER SURFACE WBL 72 APPROX S-19C HAS CORROSION
FWD GALLEY SERVICE DOOR FWD UPPER CORNER HAS CRACKS COMING FROM FASTENER HOLE WITH ENDS OF CRACKS MARKED