N720CK
Registered owner: KALITTA CHARTERS II LLC, MI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| KALITTA CHARTERS II LLC (K11A) | Operator | 2019-01-28 – 2019-01-28 | Operator named in NTSB report |
| Kalitta Charters Ii Llc | Operator | 2019-01-28 – 2019-01-28 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
NOSE GEAR DID NOT EXTEND ON LANDING. REPLACED NOSE LANDING GEAR, INSTALLED REPAIRS TO FUSELAGE IAW BOEING MSG KAE-KAE-19-0005-15C, PERFORMED TERM SERVICE AND INSTALLED GEAR PINS FERRY AIRCRAFT TO KYIP, REF NTO MSG KAE-KAE-19-0005-22B, AIRCRAFT BEING EVALUATED FOR FURTHER REPAIRS AT KOSC
AFT CARGO DOOR LOWER CHORD CORRODED
RIGHT SIDE INNER NOSE W/W STA 312-328 T CHORD CORROSION
FWD CARGO PIT DOOR CORRODED AT AFT LOWER LIGHTNING HOLE... REMOVED & REPLACED DOOR
ON THROTTLE UP FOR TAKEOFF, THE NR 1 ENGINE HAD A COMPRESSOR STALL, RETURNED TO BLOCKS. OPEN
FUSELAGE SKIN AT STA. 188-200 BETWEEN STRINGER 24L TO 24R.
NOSE LANDING GEAR WOULD NOT EXTEND, HAD TO CYCLED HANDLE FOR NOSE GEAR TO EXTEND AND LOCK
NR 3 BLEED TRIP LIGHT CAME ON DURING CRUISE.
DURING CLIMB OUT, NR 3 FUEL CROSS FEED VALVE WAS STUCK CLOSED.
FUEL LEAKING FROM NR 3 ENGINE FUEL PUMP, INSPECTED AND FOUND O-RING WAS BAD, REPLACED O-RING WITH NEW, LEAK AND OP'S CHECK GOOD. NO OTHER DEFECTS NOTED.
FUSELAGE SKIN CORROSION BS 950E + 12 ABOVE STR 28R.
FRAME SHEAR TIE CORROSION BS 970, STR 27L-28L.
STRINGER 27L DIRECTLY UNDER FRAME CORRODED UNDER FASTENER HEAD BS 970 UNDER STR 27L.
FUSELAGE SKIN ATTACH BRACKET AT BULKHEAD SHELF POINT HAS CORROSION BS 950, RBL 70.
CRACKED FASTENER HOLE.
CORRODED ANGLE.
EVIDENCE OF CORROSION ON AFT WEB SIDE.
FLOOR SUPPORT CORRODED (BOTTOM SIDE) 1X3 INCHES.
TEN INCHES OF CORROSION, SEAT TRACK CORRODED.
TIE STRAP LOOSE AND CRACKED.
FIVE INCHES OF CORROSION SEAT TRACK CORRODED.
SHEAR TIE CORROSION.
R3 WINDOW LOWER SILL HAS EVIDENCE OF CORROSION, 6 INCHES.
SKIN BULGE AT LAP SEAM, 7 INCHES OF CORROSION.
L3 WINDOW LOWER SILL HAS EVIDENCE OF CORROSION.
SEAT TRACK CORRODED 4 INCHES.
STA 600 FWD LOWER CARGO LOWER LEG OF SHEAR TIE CORRODED.
SKIN DENTED CREASED 4 INCHES BELOW VERT STAB LT SIDE.
FWD LWR CARGO DOOR INSIDE DOOR SILL 6 INCHES OF CORROSION.
STRINGER CORROSION, 15 INCHES.
EIGHT INCHES OF SKIN CORROSION.
CORROSION UNDER DOOR SILL PLATE, 8 INCHES.
STRINGER SUPPORT CORROSION, 20 INCHES.
CORROSION ON S-29L.
CORROSION ON S-28L.
CORROSION UNDER SILL S-26R STA 970-990.
CRACK ON FLANGE.
REAR SPAR HAS CRACK, LT ELE STA 66.5.
REAR SPAR HAS CRACK, LT ELE STA 68.
SEAT TRACK CORROSION.
FLOORBEAM LOWER CHORD REPAIR CORRODED ON FORWARD SIDE.
FLOORBEAM LOWER CHORD REPAIR CORRODED ON FORWARD SIDE.
DURING CLIMBOUT CABIN ALT BEGAN TO CLIMB AT 1500 FT/MIN RT AC PACK WAS FOUND TO BE INOPERATIVE, LT PACK WORKING BUT WOULD NOT MAINTAIN CABIN PRESS. REMOVED AND REPLACED RIGHT AC PACK FLOW CONTROL MODULATING AND SHUTOFF VALVE.
RT ELEVATOR REAR SPAR CRACKED FWD OF THE NR 4 TRIM TAB HINGE, ELEVATOR STA 99.79.
RT WING FRONT SPAR VERTICAL STIFFENER CRACKED.
SHEAR TIE CRACKED.
MAIN DECK FLOOR WEB CORRODED AROUND NUT PLATE.
FUSELAGE SKIN CORROSION.
CORROSION AT BULKHEAD FITTING ATTACH BOLTS.
FRAME SHEAR TIE CORRODED.
LT AFT OVERWING ESCAPE HATCH EXTERNAL SKIN CRACKED, 1/4 INCH ABOVE OPENING.
FRAME DENTED.
FRAME HAS EVIDENCE OF CORROSION.
CENTER ENGINE AIR INTAKE DUCT HAS SKIN DAMAGE AT AFT EDGE, 9 OâCLOCK POSITION.
STRINGER 24R CORRODED.
CENTER ENGINE AIR INTAKE DUCT HAS SKIN CRACK, 4 O`CLOCK POSITION.
SKIN HAS CORROSION, AFT PIT.
SKIN CORROSION, AFT PIT.
SKIN HAS CORROSION, AFT PIT.
SHEAR TIE HAS CORROSION.
FLOOR SUPPORT WEB CRACKED.
SKIN HAS CORROSION, C2 DOOR CUTOUT LOWER SILL LOWER WEB.
C1 DOOR CRACK AT PREVIOUS REPAIR.
EXTERNAL SKIN HAS CORROSION AT ACCESS PANEL.
SHEAR TIE HAS CORROSION.
SKIN HAS CORROSION, LOWER FUSELAGE.
SKIN HAS DENT, EXTERNAL FUSELAGE.
VERTICAL STIFFENER CORROSION, RT W/W KEEL BEAM.
VERTICAL STIFFENER CORROSION, LT W/W KEEL BEAM.
RT LEADING EDGE STIFFENER HAS CORROSION.
CORROSION ON FRAME WEB AFT SIDE.
MCD AFT UPPER INNER SKIN DAMAGED, MAIN CARGO DOOR.
MCD FWD LOWER CORNER INNER SKIN DAMAGED.
CORROSION ON BACK SIDE OF VERTICAL STIFFENER, LT W/W STA 915 54 INCHES BELOW W/W CEILING NET TO KEEL BEAM.
CORROSION ON BACK SIDE OF VERTICAL STIFFENER, LT W/W STA 930 54 INCHES BELOW W/W CEILING NEXT TO KEEL BEAM.
SHEAR TIE HAS AREA OF CORROSION.
CORROSION AT SHEAR TIE.
SHEAR TIE HAS AREA OF CORROSION.
FWD PIT CORROSION ON SHEAR TIE.
FWD PIT CORROSION ON SHEAR TIE.
SKIN HAS DENT.
SKIN HAS A DENT EXTERNAL FUSELAGE.
SKIN HAS A GOUGE EXTERNAL SKIN.
SKIN HAS A DENT EXTERNAL FUSELAGE.
SKIN HAS DENT EXTERNAL FUSELAGE.
FUSELAGE SKIN DENTED.
EXTERNAL FUSELAGE SKIN HAS A DENT.
SKIN HAS A DENT.
SKIN HAS A DENT.
SKIN HAS DENT.
SKIN HAS DENT.
SKIN HAS DENT.
SKIN HAS A DENT EXTERNAL FUSELAGE.
SKIN HAS A DENT EXTERNAL SKIN.
SKIN HAS A DENT EXTERNAL FUSELAGE.
AREA OF DAMAGE LOWER RIGHT SIDE JUST AFT OF SOUND ATTENUATING MATERIAL TOP OF DUCT BEHIND INLET (S DUCT).
AREA OF DAMAGE LOWER LEFT SIDE OF SOUND ATTENUATING MATERIAL TOP OF DUCT BEHIND INLET (S DUCT).
CENTER OF DOOR OUTER SKIN DENTED.
FRAME DENTED ON TOP SIDE.
SHEAR TIE HAS CORROSION ON AFT SIDE.
SHEAR TIE HAS CORROSION ON AFT SIDE.
RT HORIZONTAL STAB AFT REAR LOWER SPAR CHORD CORRODED (STAB STA 68.92 TO 78.13).
FLOOR SUPPORT HORIZONTAL STABILIZATION STRAP HAS AREA OF CORROSION UNDER NUT PLATES.
FLOOR SUPPORT STABILIZATION STRAP HAS AREA OF CORROSSION UNDER NUT PLATES.
FLOOR SUPPORT HAS AREA OF CORROSION UNDER NUT PLATES.
FLOOR SUPPORT HAS AREA OF CORROSION AROUND NUT PLATES.
FLOOR SUPPORT L-ANGLE HAS AREA OF CORROSION AROUND NUT PLATES.
FLOOR SUPPORT L-ANGLE HAS AREA OF CORROSION AROUND NUT PLATES.
FLOOR SUPPORT HAS AREA OF CORROSION AROUND NUT PLATES.
FLOOR SUPPORT HAS AREA OF CORROSION AROUND NUT PLATES.
FLOOR SUPPORT HAS AREA OF CORROSION AROUND NUT PLATES.
CORROSION ON BACK SIDE OF VERTICAL STIFENER.
SHEAR TIE HAS AREA OF CORROSION ON FWD SIDE.
SHEAR TIE HAS AREA OF CORROSION ON AFT SIDE.
FRAME DENTED ON UPPER SURFACE IN 2 AREAS.
UPPER L/E DENTED AND BUCKLED, ELEVATOR STA 225.54 TO 136.50.
MAIN DECK FLOORBEAM INTERCOSTAL HAS CRACK AT LIGHTNING HOLE.
CORROSION ON INBD SIDE VERTICAL FLANGE.
CORROSION ON OTBD SIDE VERTICAL FLANGE.
MAIN DECK LOWER WEB HAS CORROSION.
FRAME DENTED ON TOP SIDE.
SHEAR TIE HAS CORROSION ON AFT SIDE.
SHEAR TIE HAS AREA OF CORROSION ON AFT SIDE.
CORROSION ON MAIN DECK FLOOR SUPPORT.
FWD BILGE CORROSION ON STRINGER AT UPPER FLANGE.
FORWARD BILGE FUSELAGE FRAME HAS CORROSION.
SHEAR TIE HAS CORROSION ON AFT SIDE.
SHEAR TIE HAS CORROSION ON AFT SIDE.
AFT PRESSURE BULKHEAD STIFFENER HAS CORROSION.
FORWARD BILGE STRINGER HAS CORROSION ON UPPER FLANGE.
OVERWING ESCAPE HATCH LOWER EDGE FRAME HAS CORROSION (RT AFT OVERWING HATCH).
MAIN DECK FLOOR WEB, LOWER SIDE HAS AREA OF CORROSION.
STRONG SHUDDER IN AIRCRAFT, TRIM THEN RAN AWAY. SHUDDER LASTED FOR APPROX 10-15 SECONDS. TRIM THEN JAMMED BUT WAS MANUALLY OPERATIONAL AFTER PROCEDURES. EMERGENCY LANDING, DIVERTED FROM ROC TO SYR DUE TO WEATHER.
ON APPROACH, WITH FLAPS SELECTED TO 5 DEG, STAB TRIM WHEEL RAN AWAY FROM APPROX 5 UNITS NOSE UP TO 0 DEG AND BUFFETING WAS FELT IN FLT CONTROLS. AC STARTED A 2000 TO 4000 RPM RATE OF DESCENT, PILOTS TRIED TO INPUT UP ELEVATOR TO ARREST SINK RATE, THERE WAS NO EFFECT ON FLIGHT PATH. ELEVATORS HAD LOST THEIR AUTHORITY EVEN THOUGH SPEED WAS WELL ABOVE FLAPS 5 MANEUVERING SPEED. AC WAS ONLY 3000 FT. AGL AT THIS POINT. FULL POWER WAS ADDED ON ALL 3 ENGINES, WHICH WERE FUNCTIONING NORMALLY, EVEN THOUGH PITCH WAS AT APPROX ZERO DEG, IT TOOK A LONG TIME TO ARREST SINK RATE AND ELEVATORS FINALLY BEGAN RESPONDING AT APPROX. 1000 FT.AGL FROM WHICH AC WAS LANDED SAFELY. MAIN REPLACED HORIZ STAB JACKSCREW AND GEARBOX.
AIRCRAFT TOOK OFF FROM KATL TOWARD KYIP. STABILIZER JAMMED IN A VERY NARROW RANGE FROM 2 DEG UP TO 2 DEG DOWN. CREW ELECTED TO RETURN TO KATL.
DURING ACCOMPLISHMENT OF AD 94-07-08 S/B 727-57-127 FOUND CRACK LT WING UPPER AFT STRINGER STA686 (INTERNAL). INSTALLED REPAIR IAW B727 SB 727-57-A159. NON-ROUTINE TASK CARD NUMBER 17132.
DURING ROUTINE CPCP INSPECTION FOUND: MAIN CARGO DOOR HINGE CRACKED AIRCRAFT SIDE AFT LOBE. REMOVED AND REPLACED DAMAGED DOOR HINGE AFT UPPER FROM STA 590 - STA 600 IAW B727 SRM 51-10-01. CORROSION TASK CARD NUMBER C53-100-01 PART 5 OF 6. NON-ROUTINE TASK CARD NUMBER 17118.
DURING ACCOMPLISHMENT OF AD 94-07-08 S/B 727-157-127 FOUND CRACK LT WING UPPER FWD STRINGER AFT EAR STA629 (INTERNAL). INSTALLED REPAIR PARTS IAW BOEING B727 SERVICE BULLETIN 727-57-A159. NON-ROUTINE TASK CARD NUMBER 17131.