N714CK
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| KALITTA FLYING SERVICE INC | Operator | 2008-07-07 – 2008-07-07 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AT ABOUT 2:52 A.M. EDT ON JULY 7, THE CARGO AIRCRAFT (N714CK), CRASHED SHORTLY AFTER TAKEOFF FROM EL DORADO INTERNATIONAL AIRPORT, BOGOTA, COLOMBIA. (A) [THIS IS AN ACCIDENT(AP)]
CREW UPPER DECK ACCESS DOOR WILL NOT SHUT PROPERLY.
NR 1R MAIN ENTRY DOOR LOWER HORIZ FRAME CRACKED AT FWD CORNER.
STA 2000 BULKPIT DOOR LOWER FWD EDGE HAS SKIN DAMAGE.
L-3 DOOR HAS CORROSION ON VERTICAL CHORD FWD CORNER INSIDE DOOR 4 INCHES FROM BOTTOM.
NR 3R MAIN ENTRY DOOR BOTTOM WEB TOP SURFACE CORRODED, BS 1280.
STRINGER CLIP S44L IS CORRODED AT STA-1680.
HORIZ STAB CENTER SECTION LOWER STR-14 CORRODED AT RBL-14.
FOUND STA-1780 LBL-69 FRAME TO SIDE RAIL BRACKET IS CRACKED .25 INCH.
HORIZ STAB LOWER STR-8 CORRODED AT RBL-14.
HORIZ STAB CENTER SECTION LOWER STR-7 CORRODED AT RBL-15.
FOUND CORROSION ON RT WING LOWER SKIN INBOARD BOOST PUMP ACCESS PANEL CUTOUT FLANGE AT WS 679.50.
AFT BILGE FLOOR WEB IS CRACKED BETWEEN STA 1860 TO 1880, LBL 24.
FOUND EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 590, STR 41L.
NR 4 PYLON INBOARD STRINGER IS CRACKED AT NAC STA 295 TO 300, BELOW MIDSPAR AREA.
AFT BILGE FUSELAGE FRAME UPPER CHORD IS DENTED AT STA 1780, RBL 51.
AFT BILGE SEATRACK IS WORN UNDERNEATH AFT STOP AT RBL-25 AT STA-1908.
FOUND FUSELAGE FRAME WEB IS CORRODED AT STA-1680 AT LBL-50.
FOUND STA-362 SKIN DAMAGED BETWEEN STR-42R AND STR-43R.
FOUND STA-375 SKIN DAMAGED BETWEEN STR-41R AND STR-42R.
FOUND STA-372 SKIN DAMAGED AT STR-41R.
FOUND STA 370 SKIN DAMAGED BETWEEN STR-43R AND STR-44R.
FOUND STA 364 SKIN DAMAGED BETWEEN STR-43R AND STR-44R.
FOUND STA-362 SKIN DAMAGED BETWEEN STR-43R AND STR-44R.
FOUND STA-354 SKIN DAMAGED BETWEEN STR-42R AND STR-43R.
FOUND SKIN DAMAGED AT STA-346 BETWEEN STR-42R AND STR-43R.
NR 4 PYLON FIREWALL CHAFED FROM FROM NAC-STA-180 TO NAC-STA-240 INBOARD SIDE.
FUSELAGE FRAME INTERCOSTAL HAS .25 INCH CRACK BETWEEN STA 2725 & 2733, BL 0, WL 364.5.
ONE FASTENER HOLE CRACKED IN FUSELAGE SKIN AT BS 800, STR 17R.
FUSELAGE SKIN CORRODED AT BS 1684, STR 42L.
HORZ STAB CENTER SECTION LOWER STR 9 CORRODED AT RBL 14.5.
CORROSION ON BOTTOM OF L-1 MAIN ENTRY DOOR THRESHOLD WEB AT BS 461.
AFT PIT FLOORBEAM UPPER T-CHORD DENTED AT BS 1780, RBL 51.
AFT PIT SEAT TRACK CRACKED AT BS 1839, RBL 46.
FWD PIT FUSELAGE CIRCUMFERENTIAL FRAME UPPER CHORD CRACKED AT BS 840 ABOVE STR 40L.
FRAME CRACKED 1 INCH AT STA 2690.85 LBL 36 WL 305.
PYLON NR 1 OUTER SKIN CHAFED WING L/E STA 1124 NAC STA 263.
CORROSION ON TOP OF HORZ STIFFENER WEB ON AFT SIDE OF BS 1480 BULKHEAD BETWEEN RBL 33 AND RBL 69.
C-1 DOOR AFT LOWER CORNER, SKIN DAMAGED ALONG EDGE.
RIGHT FRAME AT STA 2674.85 APROX WL 304 FASTENERS HAVE ELONGATED HOLES ON FRAME STIFFENER.
AFT PIT FLOORBEAM UPPER CHORD DENTED AT BS 1720, RBL 20.
CAPTAIN'S I/B, AFT SEAT TRACK CRACKED ON WEB AT AFT END AT BS 540, LBL 20.
FUSELAGE SKIN DENTED AT BS 1787 BETWEEN STR 31R AND STR 32R.
BS 2100 RBL 12 SEAT TRACK FLANGE BROKEN.
INTERNAL FUSELAGE SKIN CORRODED AT BS 1484 ABOVE STR 7L.
MAIN ENTRY DOOR L1 FWD LOWER CORNER VERTICAL FRAME CRACKED.
STR 40L CORRODED AT BS 1698.
FUSELAGE SKIN IS CORRODED IN TWO AREAS AT STA 1244 BETWEEN STR 2R & 1L.
R-5 DOOR FWD LOWER CORNER AROUND DOME NUT 2ND FROM CORNER.
RIGHT BS 1480 BULKHEAD SPLICE FITTING, INNER SURFACE AROUND BOLT HOLE NR 7 DAMAGED AT STRINGER 33R.
BS 1480 BULKHEAD SPLICE BOLT HOLE LEFT NR 1 HAS A CRACK INDICATION.
R-5 DOOR HAS A 2 INCH CRACK FWD OF LOWER CORNER VERTICAL FRAME AT RADIUS.
BS 1880 FUSELAGE FRAME CRACKED ACROSS ENTIRE WIDTH, (APPROX 7 INCHES) AT STR 11R.
NR 1 PYLON NAC STA 128.95 LOWER O/B DOUBLER CRACKED AT LOWER END OF RADIUS.
BS 2320 FUSELAGE FRAME GOUGED BETWEEN STR 24L AND 25L.
CORROSION ON BS 480 CIRCUMFERENTIAL FRAME UPPER CHORD AROUND NUT PLATES BETWEEN LBL-36 AND LBL-44.
CORROSION ON UPPER CHORD OF BS 800 CIRCUMFERENTIAL FRAME AT LBL-33 TO LBL-43.
AFT BILGE TORQUE UPPER WEB HAS SEVERAL AREAS OF CORROSION FROM STA-1660 TO STA-1680 LBL-37 TO RBL-56.
L-5 DOOR FWD LWR CORNER AROUND DOME NUTS HAVE CORROSION.
MAIN ENTRY DOOR NR 3R LOWER HINGE CUTOUT UPPER SURFACE OF LOWER WEB IS CORRODED.
MAIN ENTRY DOOR NR 4R FWD FRAME WEB CRACKED AT UPPER O/B FLANGE.
AFT PIT FLOORBEAM UPPER CHORD DENTED AT BS 1740, RBL 20.
UPPER DECK SEAT TRACK CORRODED AT BS 600, LBL 65.
MAIN DECK SEAT TRACK DAMAGED BETWEEN BS 540 AND BS 550, RBL 33.
L-5 DOOR JUST BELOW UPPER HINGE HAS SKIN PILLOWING AROUND FASTENERS.
MAIN DECK SEAT TRACK INBOARD FLANGE IS CORRODED AT STA 420 TO 460, LBL 63.
MAIN DECK FUSELAGE L1 DOOR THRESHOLD WEB IS CORRODED ON BOTTOM SIDE AT STA 461.
MAIN CABIN TOP OF NOSE WHEEL WELL STIFFENER BETWEEN STA 280 TO 300, LBL 10 IS CRACKED IN RADIUS 1 INCH LONG.
MAIN DECK FLOOR SUPPORT IS CRACKED .5 INCH ON OUTBOARD FLANGE AT STA 1480 RBL 77.
NOSE WHEEL WELL TUNNEL STA 260 TO 280, WL 150 HORIZONTAL STIFFENER IS CRACKED IN RADIUS IN 2 AREAS BOTH .5 INCHES LONG.
FUSELAGE SKIN DAMAGED AT SIDE OF FWD CARGO DOOR OPENING AT STA-680 BETWEEN STR-31R AND STR-32R.
SKIN HAS CORROSION AT STA 1000 BETWEEN STR 44R AND STR 45R.
NR 3 PYLON NAC STA 221.0 BULKHEAD WEB CHAFED AROUND HYDRAULIC FITTINGS.
UPPER DECK RIGHT DOOR EMERGENCY EXIT SIGN DOES NOT ILLUMINATE
3 INCH CRACK IN CANTED PRESSURE BULKHEAD COMPOSITE PANEL WEB AT BS 1245, LBL 75, WL 170.
MAIN DECK L1 DOOR INTERNAL HORIZONTAL FRAME WEB IS DAMAGED AT STA 452, WL 234.
L5 DOOR FORWARD EMERGENCY EXIT LIGHT FLICKERS THEN GOES OUT.
EMERGENCY EXIT LIGHT AT STATION 710 FAILED TEST DURING A-CHECK. REPLACED LIGHT BULBS. OPERATIONAL TEST GOOD IAW AMM 33-51-00.
EMERGENCY EXIT LIGHT AT STATION 460 FAILED TEST DURING A-CHECK. REPLACED FUSE IN EMERGENCY LIGHT BATTERY PACK. OPERATIONAL TEST GOOD IAW AMM 33-51-00.
EMERGENCY EXIT LIGHT AT STATION 580 FAILED TEST DURING A-CHECK. REPLACED LIGHT BULBS. OPERATIONAL TEST GOOD IAW AMM 33-51-00.
AFTER INITIATING CLIMB THRUST AT 1,000 FT, NR 3 ENGINE FIRE LIGHT ILLUMINATED WITH ACCOMPANYING FIRE WARNING BELL AND BOTH MASTER WARNING LIGHTS. ENGINE FIRE CHECKLILST, FUEL JETTISON CHECKLIST AND NR 2 GENERATOR INOPERATIVE CHECKLIST ACCOMPLISHED IAW WITH QRH RETURNED TO LAND.
SMOKE IN COCKPIT ORIGINATING FROM BENEATH P-10 PANEL
AFT BULK FIRE "B" LIGHT ON, "A" LIGHT WOULD NOT TEST.