N706CK
Registered owner: KALITTA AIR 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
ON DESCENT NOTICED STRONG ODOR OF OIL ON UPPER DECK AND MAIN DECK CREW REPORTED LOW OIL ON ENG 4, INDICATED 4 QUARTS. PERFORMED CONDITIONAL INSPECTION OF #4 ENG IAW FIM 21-00 TASK 810 NO EXTERNAL LEAKS FOUND. SERVICED ENG OIL IAW AMM 12-13-03.
WHILE WORKING AD 2016-25-05 G2/SB 747-55A2050, FOUND 2EA HOLE CRACKED AT HORIZONTAL STAB CENTER SECTION I/B OF LBL 43.5
STA 2231 AT L5 DOOR STRG 17L FRAME STRAP AND AFT INNER CHORD CRACKED
FLIGHT DECK CREW ESCAPE HATCH GUIDE/RUB STRIP AFT SIDE IS MISSING A FASTENER, STICKER 20-01. FLIGHT DECK CREW ESCAPE HATCH GUIDE/RUB STRIP FORWARD AND AFT SIDES, THEY HAVE BECOME DISBONDED FROM THE LINER. FLIGHT DECK CREW ESCAPE HATCH EXTERIOR HANDLE DRAIN HOLES SEEM TO BE BLOCKED WITH GREASY DIRT.
CONTACT DAMAGE TO LEFT HAND SIDE OF UPPER RUDDER. REPAIRED DAMAGE TO LEFT HAND SIDE OF UPPER RUDDER IAW B747-400 SRM 51-70-07 AND KALITTA AIR EA #9097 REVISION OR.
EMERGENCY LIGHTS WILL NOT EXTINGUISH.
FOUND CRACK AT SHEAR TIE STAND OFF AT RBL 57.50 AND STA 1000
FOUND INTERCOSTAL LUG FITTING CRACKED AT LBL 11.33 AND STA 1000
FLOOR- SUPPORT HOLES (2) FOR NUTCLIPS DAMAGE, AT STA 1120-1140 RBL 110
FLIGHT COMPARTMENT EMERGENCY DECENT DEVICE #1 POSITION P/N 379103D-23 S/N 19972 EVIDENCE OF DEPLOYMENT
EMERGENCY BATTERY CHARGER M5169 AT STA 590 R/H INOP
EVIDENCE OF CORROSION ON SEAT TRACK AT STA. 1000 LBL 33
FOUND CRACK ON SHEAR TIE STAND OFF AT LBL 33.99 AND STA 1000
FOUND CRACK ON SHEAR TIE STAND OFF AT RBL 33.99 AND STA 1000
L5 MAIN DECK DOOR FWD SURROUND SKIN STRUCTURE BETWEEN STR 22 AND 21 HAS POSSIBLE CRACK.
SEAT TRACK DAMAGED BS 1910, RBL 40.
EVIDENCE OF CORROSION ON MAIN DECK SEAT TRACK BS 1040 TO 1060, LBL 100.
TENSION TIE AT BS 800 STR 11R AT RBL 80, 1.5 INCH.
TENSION TIE AT BS 800 STR 11L AT LBL 80 HAS CRACK 1 INCH.
EMERGENCY LIGHT ABOVE UPPER DECK STAIRS IS DIM AND SLOW TO COME ON.
UPPER DECK EMERGENCY CLOSET LIGHT IS INOP.
UPPER DECK RT EMERGENCY EXIT SIGN INOP.
FUMES COMING FROM NR 1 CARGO PALLET AND OR LOWER FWD CARGO AREA. SUSPECT CARGO FLUID LEAK. AFTER IDENTIFICATION OF ALL AFFECTED CARGO WITH THE USE OF THE PROPER MSDS SHEET, IT WAS DETERMINED THAT A GASEOUS LEAK HAD OCCURRED. ALL AFFECTED CARGO HAS BEEN INSPECTED AND REMOVED FROM THE AIRCRAFT. AIRCRAFT HAS BEEN THOROUGHLY VENTED AND ALL PALLET POSITIONS WERE INSPECTED WITH NO LIQUID SPILLS FOUND, AIRCRAFT WAS RETURNED TO SERVICE.
NR 3 PYLON INTERIOR HAS A 2 INCH CRACK ON 252 BULKHEAD FRAME LOWER O/B SECTION 2 INCHES ABOVE LOWER HORIZONTAL WEB.
STA 330 FLOORBEAM WEB CRACKED 3.5 INCHES AT LBL 63.
LT TRAILING EDGE INBOARD MID-FLAP HAS CORROSION ON TIE PLATE AT WBL 235.20.
LT SLIDE LIGHT HAS ONE LAMP INOP.
EMERGENCY LIGHT AT STA 460 ABOVE STAIRS IN UPPER DECK INOP.
BS 960 FUSELAGE FRAME CRACKED AT STR 39L
MAIN DECK SEAT TRACK CORRODED AT BS 1035, RBL 98.58.
BS 880 FUSELAGE FRAME CRACKED BETWEEN STR 39R AND STR 40R.
F/O`S FWD O/B SEAT TRACK CRACKED.
C2 DOOR ACCESS PANEL HAS CORROSION ON DOUBLER.
SEAT TRACK CRACKED AT STA 998 ON MAIN DECK LBL75.
NLG SIDEWALL SKIN STRAP CRACKED AT BS 300, LBL33
NR 1 PYLON MID SPAR WEB STIFFENER HAS CHAFF DAMAGE AT NAC. STA-210 R/H TOP.
NR 3 PYLON NAC STA 248 AFT, LOWER, I/B SIDE VERTICAL STIFFENER DAMAGED.
RT WING SPOILER SUPPORT BEAM UPPER CHORD CORRODED AT APPROX W.S. 528.
L1 MAIN ENTRY DOOR LOWER FRAME CRACKED AT FWD EDGE BS 442 TO 450.
AFT CARGO DOOR SKIN INNER DOUBLER CORRODED AT AFT LOWER CORNER BS 1915.
L1 MAIN ENTRY DOOR AFT TOP CORNER FITTING CRACKED.
L-5 DOOR FORWARD LOWER CORNER VERTICAL FRAME CRACKED .5 INCHES. (K)
DENT IN SKIN AT STA-2612 AT STR-51R. (K)
CAPTAINS INBD SEAT TRACK WORN LBL-36, STA-320. (K)
L-5 DOOR FORWARD LOWER CORNER HORIZONTAL BEAM CRACKED .5 INCH. (K)
DENT IN SKIN AT STA-2610 BETWEEN STR-42R AND STR-46R. (K)
DENT IN SKIN AT STA-2595 AT STR-46R. (K)
DENT IN SKIN AT STA-2412 INBD OF JACK PAD AT RBL-65R. (K)
CAPTAINS AFT SEAT TRACK IS CRACKED .250 INCH. (K)
CAPTAINS FORWARD INBD SEAT TRACK, WORN. (K)
SKIN, BS 2715 TOP OF FUSELAGE DENTED. (K)
RT FRAME CRACKED AT STR CUT OUT STA 210 ABOUT 2 INCHES LONG. (K)
CORROSION ON BS 1720 FUSE FRAME REINFORCEMENT CHORD I/B OF STR-42R.
NR 3 PYLON NAC STA 221.9 BULKHEAD LT FWD FRAME WEB CORRODED. (K)
NR PYLON NAC STA 221.9 BULKHEAD RT FWD FRAME WEB CORRODED. (K)
NR 3 PYLON NAC STA 221.9, BULKHEAD RT AFT FRAME WEB CRACKED AT (2) SPOTS. 750 AND .250. (K)
NR 3 PYLON NAC STA 221.9 BULKHEAD LT AFT FRAME WEB CRACKED. (K)
NR 3 PYLON NAC STA 221.9 BULKHEAD FWD FRAME WEB DOUBLERS CORRODED. (K)
FUSELAGE SKIN IS CORRODED AT STA 2362, BETWEEN STR 40L AND 46L. (K)
AFT BILGE FUSELAGE FRAME UPPER CHORD IS CORRODED AT STA 1880, RBL 18. (K)
MAIN DECK SEAT TRACK CORRODED BETWEEN BS 610 AND 620, RBL 46.
MAIN DECK FLOORBEAM UPPER CHORD CORRODED AT BS 640, LBL 103.
MAIN DECK SEAT TRACK DAMAGED BETWEEN BS 1320 AND 1340, LBL 34.
MAIN DECK SEAT TRACK DAMAGED AT BS 1200, LBL 11.
MAIN DECK SEAT TRACK DAMAGED BETWEEN BS 1140 AND 1240, LBL 34.
MAIN DECK SEAT TRACK CORRODED AT BS 670, RBL 28.
FUSELAGE SKIN HAS CORROSION AROUND FASTENER HEADS AT STA 1960 TO 2180, STR 46R. (K)
SEAT TRACK AT STA-620 AT LBL-70 CORRODED. (K)
STRINGER 46-L CORRODED AT STA-990. (K)
LT BODY GEAR TRUNNION SUPPORT, DRAG ANGLE CORRODED AT BS 1482, STR-42. (K)
LT BODY GEAR TRUNNION SUPPORT, DRAG ANGLE CORRODED AT BS 1482, STR-42R. (K)
STA-264, UPPER DECK FLOOR WEB CRACKED 1 INCH WL-306. (K)
STA-264 UPPER DECK FLOOR WEB CRACKED "1 INCH WL-306. (K)
STA 281, RBL-50, W/L-312 CARGO DOOR FRAME CRACKED. (K)
CORROSION ON CENTER TANK UPPER SURFACE STA-1160 RBL-80.
FRAME WEB GOUGED AT STA-220 BL-O AT WL-177.
STA-1241 LBL-1 TO LBL-14 CENTER TANK UPPER SKIN HAS CORROSION.
EXTERNAL FUSELAGE SKIN IS CHAFFED AT STA 990, STR 39R.
FORWARD BILGE HAS A DENT IN FLOORBEAM WEB AT STA 720, LBL 46, WL 108. (S)
STA 700 STRINGER TIE AT STRINGER 41L IS DENTED. (S)
STA 1000 SKIN CORRODED AT STRINGER 40R. (S)
STRINGER CLIP DENTED AT STA 660 STRINGER 44L. (S)
STRINGER 39L DENTED AT STA 695. (S)
AFT PRESSURE BULKHEAD AT STA 2360 DENTED WL340 LBL 35 AFT SIDE. (S)
STA 540 FLOORBEAM GOUGED ON UPPER CHORD LBL 41. (S)
INTERCOSTAL UPPER FLANGE BENT BETWEEN BS 660 TO BS 680. (S)
DOOR L-1 DOOR FRAME LOWER SILL FWD CORNER CRACK EXTENDS BEYOND STOP DRILL. (S)
FUSELAGE STRINGER IS CORRODED AT STA 990, STR 45R. (S)
MAIN DECK L1 DOOR VERTICAL FRAME IS CRACKED (1.5 INCHES) AT FORWARD LOWER CORNER IN RADIUS AT STA 442, WL 209. (S)
FUSELAGE SKIN HAS A DENT AT STA 182 BETWEEN STR 45R & 47R. (S)
FUSELAGE STRINGER IS DENTED AT STA 690, STR 38L. (S)
NR 2 PYLON AFT ENG MOUNT HAS 9 HOLES ELONGATED AT WL 145, LAL 1 TO RBL 9 FOR AFT ENG MOUNT BULKHEAD WEB FRAMES ATTACH AT NAC STA 221.9. (S)
NR 2 PYLON REAR ENG MOUNT BULKHEAD LT AFT FRAME WEB IS CRACKED (.750 INCHES) AT 221.9, LBL 5, WL 148.5. (S)
NR 2 PYLON REAR ENG MOUNT BULKHEAD LT FORWARD FRAME WEB IS CRACKED (.250 INCHES) AT 221.9, LBL 5, WL 148.5. (S)
NR 3 PYLON REAR ENG MOUNT BULKHEAD LT AFT FRAME WEB IS CRACKED (.250 INCHES & .750 INCHES) AT 221.9, LBL 6, WL 148.5. (S)
NR 3 PYLON REAR ENG MOUNT BULKHEAD LT AFT FRAME WEB IS CRACKED (.250 & .250 INCHES) AT 221.9, LBL 5, WL 150. (S)
BS 460 3.00 INCH ABOVE S12L FRAME OUTBOARD FLANGE CRACKED IN RADIUS OF DOUBLER .375 INCH LONG AFT SIDE. CRACK MARKED UPPER DECK. (S)
BS 460 ABOVE S12R APPROX 1 INCH, FRAME OUTBOARD FLANGE CRACKED AT FASTENER HOLE. CRACK .250 INCH LONG. MARKED UPPER DECK. (S)
BILGE TORQUE BOX UPPER WEB DENTED AT BS670, LBL36 AND LBL40, WL118. (S)
FWD PIT BS640 FUSELAGE FRAME DENTED AT LBL26, WL112. (S)
FWD PIT BS640 FUSELAGE FRAME DENTED AT LBL29, WL101. (S)
BS 460 S12L FRAME DOUBLER AFT SIDE, CRACKED .375 INCH AT STRINGER CUTOUT, INBOARD UPPER CORNER. CRACK MARKED UPPER DECK. (S)
BS 440 S10R LT SIDE FRAME AFT SIDE, STRINGER ATTACH ANGLE CRACKED IN RADIUS .250 INCH CRACK MARKED UPPER DECK. (S)
BS 460 S12R FRAME DOUBLER AFT SIDE CRACKED .500 INCH AT STRINGER CUTOUT, INBOARD UPPER CORNER. CRACK MARKED. UPPER DECK. (S)
BS 460 S12L FRAME DOUBLER AFT SIDE CRACKED .375 INCH AT STRINGER CUTOUT, INBOARD UPPER CORNER. CRACK MARKED. UPPER DECK. (S)
BS 460 3.00 INCH ABOVE S12L FRAME OUTBOARD FLANGE CRACKED IN RADIUS OF DOUBLER .375 INCH LONG AFT SIDE. CRACK MARKED. UPPER DECK. (S)
BS 460 S12R FRAME DOUBLER AFT SIDE CRACKED .500 INCH AT STRINGER CUTOUT, INBOARD UPPER CORNER. CRACK MARKED UPPER DECK. (S)
BS 440 S10R FRAME OUTBOARD FLANGE CRACKED IN RADIUS .375 INCH CRACK MARKED UPPER DECK. (S)
BS 460 ABOVE S12R APPROX 1 INCH FRAME OTBD FLANGE CRACKED AT FASTENER HOLE. CRACK .250 INCH LONG. CRACK MARKED. UPPER DECK. (S)
BS 440 S10R LT SIDE FRAME AFT SIDE, STRINGER ATTACH ANGLE CRACKED IN RADIUS .250 INCH CRACK MARKED. UPPER DECK. (S)
BS 440 S10R FRAME CRACKED .500 INCH AT STRINGER CUTOUT. CRACK MARKED UPPER DECK. (S)
BS 440 S10R FRAME OUTBOARD FLANGE CRACKED IN RADIUS .375 INCH. CRACK MARKED. UPPER DECK. (S)
BS 700 FUSELAGE FRAME WEB DENTED ABOVE STR 47R. (S)
RIGHT UPPER DECK DOOR FRAME EMERGENCY LIGHT IS OUT.
RIGHT SIDE UPPER DECK EXTERIOR EMERGENCY SLIDE EXIT LIGHT INOP.
LEFT SIDE UPPER DECK EXTERIOR EMERGENCY SLIDE EXIT LIGHT INOP.
DURING CRUISE STRONG ACRID SMELL IN COCKPIT TURNED OFF PILOT FLUORESCENT & SMELL WENT AWAY. FOUND ONE OF THE CAPTAIN`S FLUORESCENT LIGHT BULBS NOT COMPLETELY SEATED IN LIGHT SOCKET. REMOVED AND REPLACED CAPTAIN'S FLUORESCENT LIGHT BULBS IAW B747 MM CHAPT 33-11-11. OPS CHECKED SYSTEM FOR 7 HRS. NO DEFECTS OR ABNORMAL ODORS NOTED. SYSTEM OPS CHECKS GOOD IAW B747 MM CHAPT 33-11-00.
NR 4 PYLON NAC STA 179 VERTICAL BULKHEAD HAS SHEARED FASTENER AND CRACKED (1 INCH) IN WEB.
C-2 DOOR SILL UPPER CHORD IS CORRODED APPROX AT 1860.
MAIN DECK CARGO DOOR SKIN IS DAMAGED AT FORWARD LOWER AREA AT STA 1790, WL 221.
MAIN DECK CARGO DOOR FRAME INTERCOSTAL IS DAMAGED AT STA 1790, WL 219.
NR 3 PYLON NAC STA 221.9 BULKHEAD WEB CHAFED AT HYD FITTINGS.
LEFT UPPER DECK EMERGENCY LIGHT INOP.
UPPER DECK EMERGENCY LIGHT INOP AT BS 640.
EMERGENCY EXIT SIGN INOP AT LT UPPER DECK EXIT DOOR STA 400.
EMERGENCY EXIT LIGHT INOP AT STA 540.
FLOOR FITTING AT BS460, LBL10 BROKEN
MAIN DECK FLOORBEAM UPPER CHORD IS CORRODED AT STA 460, LBL 34 TO LBL 50.
FLOORBEAM UPPER CHORD STA-460 LBL-72 CORRODED.
EMERGENCY EXIT LT IN CEILING AT RT ESCAPE DOOR MOST FWD LIGHT WILL NOT STAY ILLUMINATED.
STA. 2360 BOLT HOLE NR L85 HAS CORROSION IN STRINGER L16 UPPER HOLE FITTING
IMPROPER STRINGER REPAIR ON STRINGER 11R BETWEEN STA 1831 TO 1815
NR 4 PYLON NAC STA 221.9 AFT ENG MOUNT BULKHEAD JUST OB OF UPPER SPAR HAS STOP DRILLED CRACK IN HORSESHOE FRAME
STRINGER CLIP IS DAMAGED AT STA. 1820 ON STRINGER 11R
PYLON NR 4 AT PYLON STA 221.9 AFT ENG MOUNT BULKHEAD JUST IB OF UPPER SPAR HAS CRACKED HORSESHOE FRAME.
CORROSION ON BOTTOM OF MAIN DECK FLOOR WEB BS520 RBL64.
LOOSE FASTENERS ON L/H SIDE OF EMPENNAGE BETWEEN STA 2680 TO 2701 12 TO 40 INCHES ABOVE APU DOOR HINGE.
CAPTAINS LT FWD O/B SEAT TRACK CRACKED.
FE I/B SEAT TRACK CORRODED AT FWD END
CORROSION ON WING CENTER SECTION UPPER SKIN AT STA 1210 AND 1220 RBL 98 UNDER MAIN DECK FLOOR.
RT HORIZ STAB UPPER I/B POWER PACK ELEVATOR HINGE SUPPORT HAS CORROSION.
NR 2 PYLON UPPER SPAR WEB AT NAC STA 221 I/B AFT SIDE OF BULKHEAD LOWER UPPER SPAR WEB SURFACE BULGED.
NR 1 PYLON MID SPAR WEB AREA BUCKLED NAC STA 221 AFT SIDE OF BULKHEAD LOWER I/B SURFACE.
NOSE WHEEL WELL INTERCOSTAL CRACKED AT BS 300 I/B OF LBL 20 ABOVE LT BRAKE SNUBBER.
ATTACH CLIP CRACKED ON NOSE WHEEL WELL VERTICAL BEAM AFT SIDE AT RT BS 300, WL170.
PUNCTURE IN NOSE CARGO DOOR SKIN FWD OF BS 220, I/B OF STR 43L.
ATTACH CLIP AND STIFFENER CRACKED ON NOSE WHEEL WELL TOP PANEL AT RBL 20 BETWEEN BS 265 AND 280.
FIVE CORRODED ATTACH CLIPS IN NOSE WHEEL WELL AT LBL 20 AND LBL 30 BETWEEN BS 265 AND 280.
ATTACH CLIP MIS-DRILLED ON NOSE WHELL WELL VERTICAL BEAM FWD SIDE RT, BS 280, WL 170.
NOSE WHEEL WELL TOP PANEL STIFFENER CRACKED AT LBL 20 BETWEEN BS 265 AND 280.
SEVERAL AREAS OF CORROSION ON FWD SIDE OF BS 280 FLOORBEAM WEB, LBL30 TO RBL30.
BS 360 UPPER DECK FLOORBEAM UPPER CHORD FWD FLANGE HAS MISS DRILLED FASTENER HOLES AT RBL 19 TO RBL 40.
NR 1 PYLON, INBD FIRE SEAL DAMAGED ALONG THE ENTIRE LENGTH OF THE SEAL.
BS 340 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE HAS 3 ELONGATED HOLES WITH NO ED AND CRACK INDICATIONS BETWEEN RBL 10 AND RBL 20.
NOSE WHEEL WELL ANGLE CRACKED AT LT BS 360, WL 140, LBL 10.
NOSE WHEEL WELL, BS 370 LT SIDE BETWEEN WL 130 AND 140, LBL 10, 1 VERTICAL STIFFENER CRACKED.
NOSE WHEEL WELL, THREE ATTACH CLIPS CRACKED LT AT BS 340 LBL10 WL140, 150, AND 160.
BS 340 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE HAS MISS DRILLED HOLES BETWEEN RBL 25 AND RBL 35.
BS 360 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE HAS CRACK INDICATION AT LBL 56.
BS 360 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE HAS DOUBLE DRILLED FASTENER HOLE AT LBL 44.
AFT PIT BS 1780 RT PALLET SIDE RAIL ATTACH ANGLE CRACKED.
UPPER DECK FLOORBEAM UPPER CHORD CORRODED AT BS 480, RBL3.
SEAT TRACK IS CORRODED AT STA 540 TO 560 RBL 27.99.
LT HORIZ STAB UPPER SURFACE HAS CORROSION AT STAB STA 165.
STA 900 LEFT TENSION TIE FWD CHANNEL CRACKED AT STEEL U-CHANNEL ATTACH POINT.
STA 1940 TO 1960, LBL 11 SEAT TRACK SPLICE DAMAGED.
FUSELAGE FRAME SHEAR TIE CRACKED AT BS 440 BELOW STR 9R.
CORROSION ON FUSELAGE SKIN AT BS 1000, LBL 55, WL 109, STR 43L.
CORROSION ON FUSELAGE SKIN AT BS 1000, RBL 51, WL 108, STR 43R.
FUSELAGE FRAME SHEAR TIE CRACKED AT BS 440 BELOW STR 8R.
FUSELAGE FRAME SHEAR TIE CRACKED AT BS 440 BELOW STR 9L.
LT NOSE WHEEL WELL SIDEWALL PANEL WEB STIFFENER CRACKED AT BS 265-280 WL 170.
RT EMERGENCY SLIDE LIGHT WILL NOT TEST.
CAPTAIN SEAT LEFT SEAT TRACK CRACKED 1.5 INCH AT STOP MOUNT. REPLACED LT AFT CAPT SEAT TRACK IAW AMM 25-11-01.
REAR ENGINE MOUNT BULKHEAD WEB CHAFED AROUND HYDRAULIC UNION, NAC STA 221.90. REMOVED REPAIR AREA FASTENERS AND DAMAGED MATERIAL IAW B747 SRM 54-14-03. FABRICATED 4 X 9 INCH DOUBLER IAW B747 SRM 54-14-13 FIG 16.
LEFT UPPER DECK EMERGENCY LIGHT INOP.