N714CK

BOEING 747-200FM Fatal injury Part 121 — KALITTA FLYING SERVICE INC

Operated by KALITTA FLYING SERVICE INC (per NTSB report)

Boeing 747-200B No injuries Part 121 — KALITTA FLYING SERVICE INC

Operated by KALITTA FLYING SERVICE INC (per NTSB report)

ATA 5100

Part: NONE — NONE (NONE)

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)]

ATA 5210

Part: ACCESS DOOR — MISRIGGED (COCKPIT) · airframe 90,031 hrs · 21,883 cycles

CREW UPPER DECK ACCESS DOOR WILL NOT SHUT PROPERLY.

ATA 5210

Part: DOOR FRAME — CORRODED (L3 DOOR) · airframe 89,593 hrs · 21,795 cycles

L-3 DOOR HAS CORROSION ON VERTICAL CHORD FWD CORNER INSIDE DOOR 4 INCHES FROM BOTTOM.

ATA 5230

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 89,593 hrs · 21,795 cycles

STA 2000 BULKPIT DOOR LOWER FWD EDGE HAS SKIN DAMAGE.

ATA 5310

Part: DOOR FRAME — CRACKED (BS 445)

NR 1R MAIN ENTRY DOOR LOWER HORIZ FRAME CRACKED AT FWD CORNER.

ATA 5320

Part: WEB — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

NR 3R MAIN ENTRY DOOR BOTTOM WEB TOP SURFACE CORRODED, BS 1280.

ATA 5340

Part: BRACKET — CRACKED (BS 1780) · airframe 89,593 hrs · 21,795 cycles

FOUND STA-1780 LBL-69 FRAME TO SIDE RAIL BRACKET IS CRACKED .25 INCH.

ATA 5511

Part: STRINGER — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

HORIZ STAB CENTER SECTION LOWER STR-14 CORRODED AT RBL-14.

ATA 5340

Part: STRINGER CLIP — CORRODED (BS 1680 S44L) · airframe 89,593 hrs · 21,795 cycles

STRINGER CLIP S44L IS CORRODED AT STA-1680.

ATA 5511

Part: STRINGER — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

HORIZ STAB CENTER SECTION LOWER STR-7 CORRODED AT RBL-15.

ATA 5511

Part: STRINGER — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

HORIZ STAB LOWER STR-8 CORRODED AT RBL-14.

ATA 5321

Part: FLOOR SKIN — CRACKED (BS 1860-1880) · airframe 89,593 hrs · 21,795 cycles

AFT BILGE FLOOR WEB IS CRACKED BETWEEN STA 1860 TO 1880, LBL 24.

ATA 5311

Part: FRAME — DENTED (BS 1780) · airframe 89,593 hrs · 21,795 cycles

AFT BILGE FUSELAGE FRAME UPPER CHORD IS DENTED AT STA 1780, RBL 51.

ATA 5330

Part: SKIN — DAMAGED (BS 590 S41L) · airframe 89,593 hrs · 21,795 cycles

FOUND EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 590, STR 41L.

ATA 5413

Part: STRINGER — CRACKED (NR 4 NACELLE) · airframe 89,593 hrs · 21,795 cycles

NR 4 PYLON INBOARD STRINGER IS CRACKED AT NAC STA 295 TO 300, BELOW MIDSPAR AREA.

ATA 5730

Part: SKIN — CORRODED (RWS 679) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

FOUND CORROSION ON RT WING LOWER SKIN INBOARD BOOST PUMP ACCESS PANEL CUTOUT FLANGE AT WS 679.50.

ATA 5412

Part: FIREWALL — CHAFED (NR 4 NACELLE) · airframe 89,593 hrs · 21,795 cycles

NR 4 PYLON FIREWALL CHAFED FROM FROM NAC-STA-180 TO NAC-STA-240 INBOARD SIDE.

ATA 5330

Part: SKIN — DAMAGED (BS 362 S43-44R) · airframe 89,593 hrs · 21,795 cycles

FOUND STA-362 SKIN DAMAGED BETWEEN STR-43R AND STR-44R.

ATA 5330

Part: SKIN — DAMAGED (BS 362 S42-43R) · airframe 89,593 hrs · 21,795 cycles

FOUND STA-362 SKIN DAMAGED BETWEEN STR-42R AND STR-43R.

ATA 5330

Part: SKIN — DAMAGED (BS 370 S43-44R) · airframe 89,593 hrs · 21,795 cycles

FOUND STA 370 SKIN DAMAGED BETWEEN STR-43R AND STR-44R.

ATA 5330

Part: SKIN — DAMAGED (BS 364 S43-44R) · airframe 89,593 hrs · 21,795 cycles

FOUND STA 364 SKIN DAMAGED BETWEEN STR-43R AND STR-44R.

ATA 5330

Part: SKIN — DAMAGED (BS 346 S42-43R) · airframe 89,593 hrs · 21,795 cycles

FOUND SKIN DAMAGED AT STA-346 BETWEEN STR-42R AND STR-43R.

ATA 5330

Part: SKIN — DAMAGED (BS 354 S42-43R) · airframe 89,593 hrs · 21,795 cycles

FOUND STA-354 SKIN DAMAGED BETWEEN STR-42R AND STR-43R.

ATA 5330

Part: SKIN — DAMAGED (BS 375 S41-42R) · airframe 89,593 hrs · 21,795 cycles

FOUND STA-375 SKIN DAMAGED BETWEEN STR-41R AND STR-42R.

ATA 5311

Part: FRAME — CORRODED (BS 1680) · airframe 89,593 hrs · 21,795 cycles

FOUND FUSELAGE FRAME WEB IS CORRODED AT STA-1680 AT LBL-50.

ATA 5347

Part: SEAT TRACK — WORN (BS 1908) · airframe 89,593 hrs · 21,795 cycles

AFT BILGE SEATRACK IS WORN UNDERNEATH AFT STOP AT RBL-25 AT STA-1908.

ATA 5330

Part: SKIN — DAMAGED (BS 372 S41R) · airframe 89,593 hrs · 21,795 cycles

FOUND STA-372 SKIN DAMAGED AT STR-41R.

ATA 5320

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

FUSELAGE FRAME INTERCOSTAL HAS .25 INCH CRACK BETWEEN STA 2725 & 2733, BL 0, WL 364.5.

ATA 5330

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

FUSELAGE SKIN CORRODED AT BS 1684, STR 42L.

ATA 5330

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

ONE FASTENER HOLE CRACKED IN FUSELAGE SKIN AT BS 800, STR 17R.

ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

FWD PIT FUSELAGE CIRCUMFERENTIAL FRAME UPPER CHORD CRACKED AT BS 840 ABOVE STR 40L.

ATA 5320

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

CORROSION ON BOTTOM OF L-1 MAIN ENTRY DOOR THRESHOLD WEB AT BS 461.

ATA 5347

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

AFT PIT SEAT TRACK CRACKED AT BS 1839, RBL 46.

ATA 5315

Part: FLOORBEAM — DENTED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

AFT PIT FLOORBEAM UPPER T-CHORD DENTED AT BS 1780, RBL 51.

ATA 5511

Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

HORZ STAB CENTER SECTION LOWER STR 9 CORRODED AT RBL 14.5.

ATA 5312

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

CORROSION ON TOP OF HORZ STIFFENER WEB ON AFT SIDE OF BS 1480 BULKHEAD BETWEEN RBL 33 AND RBL 69.

ATA 5311

Part: FRAME — DAMAGED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

RIGHT FRAME AT STA 2674.85 APROX WL 304 FASTENERS HAVE ELONGATED HOLES ON FRAME STIFFENER.

ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

FRAME CRACKED 1 INCH AT STA 2690.85 LBL 36 WL 305.

ATA 5414

Part: SKIN — CHAFED (NR 1 PYLON) · airframe 89,593 hrs · 21,795 cycles

PYLON NR 1 OUTER SKIN CHAFED WING L/E STA 1124 NAC STA 263.

ATA 5230

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 89,593 hrs · 21,795 cycles

C-1 DOOR AFT LOWER CORNER, SKIN DAMAGED ALONG EDGE.

ATA 5315

Part: FLOORBEAM — DENTED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

AFT PIT FLOORBEAM UPPER CHORD DENTED AT BS 1720, RBL 20.

ATA 5347

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

CAPTAIN'S I/B, AFT SEAT TRACK CRACKED ON WEB AT AFT END AT BS 540, LBL 20.

ATA 5347

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

BS 2100 RBL 12 SEAT TRACK FLANGE BROKEN.

ATA 5330

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

INTERNAL FUSELAGE SKIN CORRODED AT BS 1484 ABOVE STR 7L.

ATA 5330

Part: SKIN — DENTED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

FUSELAGE SKIN DENTED AT BS 1787 BETWEEN STR 31R AND STR 32R.

ATA 5210

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 89,593 hrs · 21,795 cycles

MAIN ENTRY DOOR L1 FWD LOWER CORNER VERTICAL FRAME CRACKED.

ATA 5313

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

STR 40L CORRODED AT BS 1698.

ATA 5330

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

FUSELAGE SKIN IS CORRODED IN TWO AREAS AT STA 1244 BETWEEN STR 2R & 1L.

ATA 5312

Part: SPLICE — CRACKED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

BS 1480 BULKHEAD SPLICE BOLT HOLE LEFT NR 1 HAS A CRACK INDICATION.

ATA 5210

Part: STRUCTURE — CORRODED (R5 DOOR) · airframe 89,593 hrs · 21,795 cycles

R-5 DOOR FWD LOWER CORNER AROUND DOME NUT 2ND FROM CORNER.

ATA 5312

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

RIGHT BS 1480 BULKHEAD SPLICE FITTING, INNER SURFACE AROUND BOLT HOLE NR 7 DAMAGED AT STRINGER 33R.

ATA 5210

Part: FRAME — CRACKED (R5 DOOR) · airframe 89,593 hrs · 21,795 cycles

R-5 DOOR HAS A 2 INCH CRACK FWD OF LOWER CORNER VERTICAL FRAME AT RADIUS.

ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

BS 1880 FUSELAGE FRAME CRACKED ACROSS ENTIRE WIDTH, (APPROX 7 INCHES) AT STR 11R.

ATA 5412

Part: DOUBLER — CRACKED (NR 1 PYLON) · airframe 89,593 hrs · 21,795 cycles

NR 1 PYLON NAC STA 128.95 LOWER O/B DOUBLER CRACKED AT LOWER END OF RADIUS.

ATA 5311

Part: FRAME — GOUGED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

BS 2320 FUSELAGE FRAME GOUGED BETWEEN STR 24L AND 25L.

ATA 5210

Part: DOOR — CORRODED (L5) · airframe 89,593 hrs · 21,795 cycles

L-5 DOOR FWD LWR CORNER AROUND DOME NUTS HAVE CORROSION.

ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

CORROSION ON UPPER CHORD OF BS 800 CIRCUMFERENTIAL FRAME AT LBL-33 TO LBL-43.

ATA 5210

Part: WEB — CORRODED (PAX DOOR) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

MAIN ENTRY DOOR NR 3R LOWER HINGE CUTOUT UPPER SURFACE OF LOWER WEB IS CORRODED.

ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

CORROSION ON BS 480 CIRCUMFERENTIAL FRAME UPPER CHORD AROUND NUT PLATES BETWEEN LBL-36 AND LBL-44.

ATA 5320

Part: TORQUE BOX — CORRODED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

AFT BILGE TORQUE UPPER WEB HAS SEVERAL AREAS OF CORROSION FROM STA-1660 TO STA-1680 LBL-37 TO RBL-56.

ATA 5210

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 89,593 hrs · 21,795 cycles

MAIN ENTRY DOOR NR 4R FWD FRAME WEB CRACKED AT UPPER O/B FLANGE.

ATA 5347

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

UPPER DECK SEAT TRACK CORRODED AT BS 600, LBL 65.

ATA 5347

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 89,593 hrs · 21,795 cycles

MAIN DECK SEAT TRACK DAMAGED BETWEEN BS 540 AND BS 550, RBL 33.

ATA 5315

Part: FLOORBEAM — DENTED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

AFT PIT FLOORBEAM UPPER CHORD DENTED AT BS 1740, RBL 20.

ATA 5210

Part: HINGE — CORRODED (L5 DOOR) · airframe 89,593 hrs · 21,795 cycles

L-5 DOOR JUST BELOW UPPER HINGE HAS SKIN PILLOWING AROUND FASTENERS.

ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

MAIN DECK SEAT TRACK INBOARD FLANGE IS CORRODED AT STA 420 TO 460, LBL 63.

ATA 5320

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,593 hrs · 21,795 cycles

MAIN DECK FUSELAGE L1 DOOR THRESHOLD WEB IS CORRODED ON BOTTOM SIDE AT STA 461.

ATA 5320

Part: STIFFENER — CRACKED (NLG WW) · airframe 89,593 hrs · 21,795 cycles

MAIN CABIN TOP OF NOSE WHEEL WELL STIFFENER BETWEEN STA 280 TO 300, LBL 10 IS CRACKED IN RADIUS 1 INCH LONG.

ATA 5320

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 89,593 hrs · 21,795 cycles

MAIN DECK FLOOR SUPPORT IS CRACKED .5 INCH ON OUTBOARD FLANGE AT STA 1480 RBL 77.

ATA 5320

Part: STIFFENER — CRACKED (NLG WW) · airframe 89,593 hrs · 21,795 cycles

NOSE WHEEL WELL TUNNEL STA 260 TO 280, WL 150 HORIZONTAL STIFFENER IS CRACKED IN RADIUS IN 2 AREAS BOTH .5 INCHES LONG.