N747CK
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
55 reports on file, 2007-05-27 – 2011-10-04.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 119,268 hrs · 26,959 cycles
CORROSION ON ANGLE BOTTOM OF KEEL BEAM BOX TOP WEB AT BS 1264, LBL 10 TO RBL 10.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 119,268 hrs · 26,959 cycles
CORROSION ON FUSELAGE SKIN AT BS 2385, STR 35R.
Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 119,268 hrs · 26,959 cycles
STIFFENER ANGLE CORRODED IN RT WLG W/W AT STA 1255 RBL 130 BWL 175.
Part: DOUBLER — CORRODED (LT WING) · corrosion level 2 · airframe 119,268 hrs · 26,959 cycles
LEFT WING L/E CAVITY INTERIOR , FSSO 1530: LWR WING SKIN INTERIOR DOUBLER HAS SUSPECT CORROSION NEXT TO 1 FASTENER.
Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 118,655 hrs · 26,825 cycles
NR 4 ENGINE FIRE WARNING LIGHT AND BELL LIGHT ILLUMINATED - EXTINGUISHED WHEN ENGINE SHUT DOWN. NO BOTTLE DISCHARGED. ENGINE WINDMILLED 53 MINUTES, 33 MINUTES AT 12 PSI, 20 MINUTES AT 4 PSI. COMPLIED WITH WINDMILLING PROCEDURE. FOUND BLEED AIR LEAK AT NR 4 ENGINE PRESSURE RELIEF VALVE CLAMP. RE-SECURED AS PER MM REF 36-11-03. LEAK CHECK OK. PERFORMED ENGINE WINDMILL INSPECTION PER MM REF 72-00-00. NO DISCREPANCY NOTED IAW AMM REF 36-11-00/501.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,418 hrs · 26,748 cycles
CORROSION ON INTERNAL FUSELAGE SKIN FORWARD SIDE OF STA 1241 BETWEEN STR 14R & 15R.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,418 hrs · 26,748 cycles
STA 1241, CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STR. 14L & 15L FORWARD SIDE.
Earlier reports · 2007–2010 · 48 reports
2010
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 117,956 hrs · 26,612 cycles
UPPER DECK EMERGENCY DOOR AISLE LIGHT INOPERATIVE.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 115,554 hrs · 26,104 cycles
UPPER DECK EMERGENCY LIGHT ABOVE SLIDE INOP.
Part: CHANNEL — CORRODED (RT MLG WW) · corrosion level 2 · airframe 115,192 hrs · 26,037 cycles
CORROSION ON U-CHANNEL ON BOTTOM OF RT WING MLG WHEEL WELL PRESSURE DECK AT BS 1335 FUSELAGE FRAME.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 115,192 hrs · 26,037 cycles
CORROSION ON AFT LOWER SIDE OF BS 1335 FUSELAGE FRAME JUST ABOVE OVERWING LONGERON.
Part: STIFFENER — CRACKED (NR 2 PYLON) · airframe 115,192 hrs · 26,037 cycles
NR 2 PYLON STIFFENER CRACKED .5 INCH AT STA 221 LOWER WEB.
Part: STIFFENER — DAMAGED (NR 1 PYLON) · airframe 115,192 hrs · 26,037 cycles
PYLON NR 1 STIFFENER DAMAGED AT LOWER SPAR WEB STA 221.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 115,192 hrs · 26,037 cycles
FUSELAGE STRINGER CLIP IS CRACKED AT STA 1820, STR 11R.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 115,192 hrs · 26,037 cycles
STA 760 LBL 99 SEAT TRACK CORRODED.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 115,192 hrs · 26,037 cycles
FUSELAGE STRINGER CLIP IS CRACKED AT STA 1820, STR 12R.
Part: SPAR — CRACKED (NR 3 PYLON) · airframe 115,192 hrs · 26,037 cycles
NR 3 PYLON LOWER MID SPAR WEB CHORD CRACKED ON I/B END.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 115,192 hrs · 26,037 cycles
FUSELAGE SKIN CORRODED AT BS 2460, STR 21L.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 115,192 hrs · 26,037 cycles
FUSELAGE SKIN CORRODED AT BS 985 BETWEEN STR 42L AND STR 43L.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 115,192 hrs · 26,037 cycles
UPPER DECK EXIT EMERGENCY LIGHT IS INOP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 115,192 hrs · 26,037 cycles
EMERGENCY LIGHT OVER U/D RIGHT SERVICE DOOR INOP.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 115,192 hrs · 26,037 cycles
FUSELAGE STA 860 LT FRAME SHEAR TIE CRACKED IN RADIUS, AFT SIDE OF FRAME BETWEEN STR 9L AND STR 10L.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 115,192 hrs · 26,037 cycles
STA 610 U/D EMERGENCY LIGHT INOP.
Part: BULKHEAD — CANNING (FUSELAGE) · airframe 114,881 hrs · 25,959 cycles
BS 2360 AFT PRESSURE BULKHEAD WEB OIL CANNED AT WL 330 LBL 40.
2008
Part: FRAME — CRACKED (NR 4 PYLON) · airframe 113,108 hrs · 25,623 cycles
NR 4 PYLON NAC STA 221.90 OUTBOARD AFT FRAME IS CRACKED .500" AT SKIN ATTACHMENT. (A)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 112,683 hrs · 25,540 cycles
EMERGENCY LIGHT ON RIGHT UPPER DECK SLIDE HAS ONE BULB BURNED OUT.
Part: STIFFENER — CRACKED (NR 3 PYLON) · airframe 111,799 hrs · 25,374 cycles
NR 3 PYLON LT UPPER STIFFENER CRACKED AT ATTACH POINT OF THE FWD ENG MOUNT BULKHEAD INTERNAL ANGLE.
Part: STIFFENER — CRACKED (NR 3 PYLON) · airframe 111,799 hrs · 25,374 cycles
NR 3 PYLON RT UPPER STIFFENER CRACKED AT ATTACH ANGLE OF THE FWD ENG MOUNT BULKHEAD INTERNAL ANGLE.
2007
Part: FITTING — CRACKED (FUSELAGE) · airframe 109,828 hrs · 24,990 cycles
LEFT SIDE NOSE CARGO DOOR PORTAL C-3 FRAME UPPER CLOSER FITTING FASTENER HOLE IS CRACKED AT STA 285.5, WL 323.
Part: STANCHION — CORRODED (BS 1920) · corrosion level 2 · airframe 109,828 hrs · 24,990 cycles
AFT PIT SIDEWALL STANCHION CORRODED AT BS 1920, RBL 61.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 109,828 hrs · 24,990 cycles
FLOORBEAM WEB DAMAGED AT LBL 109 TO 117 STA 1180 CRACKED 1 INCH.
Part: FITTING — GOUGED (FUSELAGE) · airframe 109,828 hrs · 24,990 cycles
RIGHT BS 1820 FLOORBEAM END FITTING, FWD TWO FASTENERS HOLES GOUGED AND ELONGATED.
Part: FLOORBEAM — CORRODED (BS 440) · corrosion level 2 · airframe 109,828 hrs · 24,990 cycles
MAIN DECK FLOORBEAM CORRODED AT BS 440, LBL 59.
Part: FITTING — CORRODED (BS 2598 S8L) · corrosion level 2 · airframe 109,828 hrs · 24,990 cycles
FUSELAGE STRINGER END FITTING IS CORRODED AT STA 2598, STR 8L.
Part: FRAME — CORRODED (BS 2598) · corrosion level 2 · airframe 109,828 hrs · 24,990 cycles
FUSELAGE FRAME AFT CHORD IS CORRODED AT STA 2598, STR 8L.
Part: FLOORBEAM — CORRODED (BS 1920) · airframe 109,828 hrs · 24,990 cycles
STA 1920 RBL 60 EVIDENCE OF CORROSION ON FUSELAGE DOOR LOCK BEAM WEB.
Part: SEAT TRACK — CORRODED (BS 1770-1815) · airframe 109,828 hrs · 24,990 cycles
MAIN DECK SEAT TRACK IS CORRODED AT LBL 11 FROM STA 1770 TO 1815.
Part: SEAT TRACK — CORRODED (BS 390-402) · airframe 109,828 hrs · 24,990 cycles
MAIN DECK SEAT TRACK IS CORRODED AT O/B FLANGE RBL 83 FROM STA 390 TO 402.
Part: SEAT TRACK — CORRODED (BS 1152) · airframe 109,828 hrs · 24,990 cycles
MAIN DECK SEAT TRACK IS CORRODED AT LBL 74 STA 1152.
Part: STRINGER — BENT (BS 2160-2180) · airframe 109,828 hrs · 24,990 cycles
FUSELAGE STR 50L HAS A BENT FLANGE BETWEEN BS 2160 AND 2180.
Part: STRINGER — DAMAGED (BS 2160-2180) · airframe 109,828 hrs · 24,990 cycles
FUSELAGE STR 21L DAMAGED BETWEEN BS 2160 AND 2180.
Part: STRINGER — BENT (BS 2160-2180) · airframe 109,828 hrs · 24,990 cycles
FUSELAGE STR 49L HAS A BENT FLANGE BETWEEN BS 2160 AND 2180.
Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 109,828 hrs · 24,990 cycles
RIGHT WING FRONT SPAR LOWER CHORD STRAP CORRODED AT FSSO 1520.
Part: STRINGER — BENT (2160-2180) · airframe 109,828 hrs · 24,990 cycles
FUSELAGE STR 48L HAS A BENT FLANGE BETWEEN BS 2160 AND 2180.
Part: SEAT TRACK — CORRODED (BS 1152) · corrosion level 2 · airframe 109,828 hrs · 24,490 cycles
MAIN DECK SEAT TRACK CORRODED AT BS 1152, LBL 74.
Part: STRINGER — BENT (BS 2160-2180) · airframe 109,828 hrs · 24,990 cycles
FUSELAGE STR 47L IS BENT BETWEEN BS 2160 AND 2180.
Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 109,828 hrs · 24,990 cycles
NR 1 PYLON NAC STA-221 O/B ANGLE CRACKED FWD SIDE OF BULKHEAD.
Part: FRAME — CRACKED (BS 434) · airframe 109,828 hrs · 24,990 cycles
STA 434 FRAME CRACKED LBL 49 WL 121 APROX .75 INCH.
Part: CHANNEL — CHAFED (FUSELAGE) · airframe 109,828 hrs · 24,990 cycles
AFT BILGE FUSELAGE FRAME WEB SUPPORT CHANNEL IS CHAFFED AT STA 1680 RBL40.
Part: FLOORBEAM — CORRODED (BS 800) · airframe 109,828 hrs · 24,990 cycles
STA 800 LBL 97.5 FLOORBEAM UPPER CAP FWD FLANGE LOWER SURFACE CORRODED AT FASTENER LOCATION.
Part: SEAT TRACK — CORRODED (BS 390-402) · airframe 109,828 hrs · 24,990 cycles
SEAT TRACK O/B FLANGE HAS CORROSION FROM STA 390 TO 402 RBL 83.
Part: FLOORBEAM — PUNCTURED (BS 460) · airframe 109,828 hrs · 24,990 cycles
UPPER DECK FLOORBEAM WEB IS PUNCTURED AT STA 460 RBL 46 JUST BELOW UPPER CHORD.
Part: STIFFENER — CORRODED (BS 2008) · airframe 109,828 hrs · 24,990 cycles
BULK CARGO DOOR LONGITUDINAL STIFFENER CORROSION STA 2008.
Part: FRAME — CRACKED (BS 1820) · airframe 109,828 hrs · 24,990 cycles
AFT BILGE FUSELAGE FRAME UPPER CHORD IS CRACKED AT STA 1820 AT RBL 48 1 INCH.
Part: FLOORBEAM — CORRODED (BS 1170) · corrosion level 2 · airframe 102,828 hrs · 24,990 cycles
CORROSION ON MAIN DECK FLOORBOARD ATTACHMENT BEAM AT BS 1170, LBL-11 TO RBL-11.