N717CK
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.
33 reports on file, 2004-10-24 – 2008-09-20.
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 81,132 hrs · 22,774 cycles
RT BODY GEAR ACTUATOR ATTACH FITTING OTBD LUG IS CRACKED 2 INCHES AT STA 1480.
Part: STOP FITTING — CRACKED (R3 DOOR) · airframe 81,132 hrs · 22,774 cycles
R3 DOOR NR 3 STOP FITTING HAS A 3 INCH CRACK AT STA 1264, WL225.
Part: FRAME — CORRODED (FUSELAGE) · airframe 81,132 hrs · 22,774 cycles
CHORD CORRODED AT STA 1241, RBL 95, WL 160. NEXT TO TOOTH FITTING STIFFENER.
Part: LIGHT — INOPERATIVE (CABIN)
MAIN DECK STA 2290 OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. (K)
Part: LIGHT — INOPERATIVE (CABIN)
L-5 DOOR SILL EMERGENCY EXIT LIGHTS INOPERATIVE. (K)
Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,895 hrs · 22,720 cycles
SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 680, RBL-5.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,895 hrs · 22,720 cycles
SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 787, LBL-2.
Part: SKIN — DAMAGED (BS 788) · airframe 80,895 hrs · 22,720 cycles
SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 788, LBL-2.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,895 hrs · 22,720 cycles
SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 644, RBL-2.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,895 hrs · 22,720 cycles
SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 647, RBL-2
Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,895 hrs · 22,720 cycles
SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 610, LBL-2.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,895 hrs · 22,720 cycles
SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 792, BL-0.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 80,895 hrs · 22,720 cycles
FORWARD BILGE FUSELAGE FRAME UPPER CAP IS DAMAGED AT STA 760, RBL 80.
Part: TORQUE BOX — PUNCTURED (FUSELAGE) · airframe 80,895 hrs · 22,720 cycles
FORWARD BILGE TORQUE BOX WEB HAS A PUNCTURED HOLE AT STA 660 TO 680, RBL 70.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 80,895 hrs · 22,720 cycles
FORWARD BILGE FUSELAGE FRAME UPPER CAP IS DAMAGED AT STA 700, RBL 80.
Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 80,895 hrs · 22,720 cycles
AFT CARGO DOOR SKIN EDGE DAMAGED AT BS 1830, STR 42R.
Part: BULKHEAD — CHAFED (NR 1 PYLON) · airframe 80,895 hrs · 22,720 cycles
NR 1 PYLON BULKHEAD HAS A CHAFED AREA AT NAC STA 221.90.
Part: BULKHEAD — GOUGED (NR 3 PYLON) · airframe 80,895 hrs · 22,720 cycles
NR 3 PYLON FORWARD ENGINE MOUNT BULKHEAD CHORD INBOARD AND OUTBOARD LOWER ENDS ARE GOUGED / WORN AT NAC STA 128.95.
Part: PRESSURE PANEL — LEAKING (FUSELAGE) · airframe 80,748 hrs · 22,690 cycles
UNABLE TO MAINTAIN CABIN ABOVE FL 260. COMPLETED ALL CHECK LISTS BUT STILL UNABLE TO MAINTAIN ALT. FOUND 8 INCH DIAMETER HOLE IN PRESSURE PAN ASSY. INSTALLED NEW PRESSURE PANEL ASSY PER SRM 51-30-02, 51-10-01 AND 51-10-06. PRESSURIZATION LEAK CHECK GOOD PER MM 21-31-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 80,323 hrs · 22,606 cycles
FWD PIT SEAT TRACK DAMAGED AT BS 560, RBL 48.
Earlier reports · 2004–2007 · 13 reports
2007
Part: SEAT TRACK — DAMAGED (BS 570-590) · airframe 80,096 hrs · 22,566 cycles
FORWARD BILGE SEAT TRACK IS DAMAGED AT STA 570 TO 590, LBL 45.
Part: FRAME — DAMAGED (BS 1810) · airframe 79,293 hrs · 22,414 cycles
AFT PIT FUSELAGE FRAME WEB DAMAGED AT BS 1810 BETWEEN STR 39R AND STR 40R.
Part: SKIN — CORRODED · corrosion level 2 · airframe 79,293 hrs · 22,414 cycles
STA 990 ABOVE NR 2 RAM AIR INLET DUCT, LOWER SIDE OF CENTER WING TANK HAS AREA OF CORROSION AT LBL 82.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,293 hrs · 22,414 cycles
FUSELAGE SKIN HAS CORROSION AT STA 2235, BETWEEN STR 29R & 30R.
Part: RIVET — PULLED (RT WING) · airframe 79,293 hrs · 22,414 cycles
RIVETS PULLING THROUGH SKIN AFT OF AFT SPAR TOPSIDE OF WING AT WS-411.
Part: ENGINE — FLAMED OUT (NR 1) · airframe 79,291 hrs · 22,413 cycles
AT FLIGHT LEVEL 370, NR 1 & 4 ENG FLAMEOUT, RAPID RESTARTED ENGINES, NR 1 RELIGHT AT 31.0, NR 4 AT 28.0. BOTH ENGINES STABILIZED WITH NORMAL PARAMETERS & OPERATED NORMAL FOR REST OF FLIGHT.
Part: BULKHEAD — CHAFED (NR 1 PYLON) · airframe 79,026 hrs · 22,357 cycles
NR 1 PYLON HYDRAULIC PRESSURE LINE AT NAC STA 221.9 BULKHEAD IS CHAFING.
2006
Part: BULKHEAD — CHAFED (NR 3 NACELLE) · airframe 77,618 hrs · 22,042 cycles
NR 3 PYLON ENGINE MOUNT BULKHEAD HYDRAULIC FITTING CHAFED INTO REPAIR DOUBLER AT NAC STA 221.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 77,007 hrs · 21,925 cycles
AT STATION 540 INOP. FAILED TEST DURING A-CHECK. REPLACED LIGHT ASSEMBLY.
Part: FUSE — BLOWN (POWER SUPPLY) · airframe 77,007 hrs · 21,925 cycles
EMERGENCY EXIT SLIDE LIGHTS INOP. FAILED TEST DURING A-CHECK. REPLACED 2 FUSES IN THE EXIT LIGHT POWER SUPPLY MODULE.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 77,007 hrs · 21,925 cycles
EMERGENCY EXIT LIGHT AT STATION 460 INOP. FAILED TEST DURING A-CHECK. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY.
2005
Part: FIRE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 74,939 hrs · 21,477 cycles
LOWER AFT CARGO COMPARTMENT FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED (WITH CARGO HEAT ON). INSPECTED LOWER AFT CARGO COMPT FOR SIGNS OF FIRE. NO INDICATION OF FIRE FOUND. CANNOT DUPLICATE ON GROUND. INSPECTED THE CARGO HEATING SYSTEM. NO DEFECTS FOUND.
2004
Part: ENGINE — FAILED (NR 4) · airframe 73,740 hrs · 21,243 cycles
ON T/O FROM HNL, NR 4 ENGINE LOSS AT 200 FT WITH LOUD BANG AND BRIGHT FLASH. EGT WENT TO 1100 DEGREES, ENGINE OIL PRESSURE APPROX 10 PSI FOR 5 MIN, THEN WENT TO 5PSI. RETURNED TO HNL. BOROSCOPED NR 4 ENGINE LP AND HP COMP SECTIONS AND FOUND EVIDENCE OF BIRD STRIKE.