N792CK
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.
36 reports on file, 2010-12-22 – 2013-09-30.
Part: FRAME — CHAFED (NR 4 NACELLE) · airframe 81,826 hrs · 15,350 cycles
NR 4 PYLON FRAME HAS CHAFING DAMAGE AT MAIN PNEUMATIC DUCT RT MOUNT.
Part: FIRESHIELD — CHAFED (NR 4 NACELLE) · airframe 81,826 hrs · 15,350 cycles
NR 4 PYLON OTBD FIRESHIELD NAC. STA. 233.0 TO 236.0 HAS CHAFING UNDER FLIPPER DOOR.
Part: SKIN — CHAFED (NR 4 NACELLE) · airframe 81,826 hrs · 15,350 cycles
NR 4 PYLON OTBD SKIN BETWEEN REPAIR DOUBLER AND FIRESHIELD CHAFED AT NAC. STA. 235.0 TO 236.0.
Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 81,826 hrs · 15,350 cycles
NR 2 PYLON HAS A CRACKED DOUBLER ON THE RT SKIN AT NAC STA 222 NEAR BOTTOM OF PYLON.
Part: SKIN — CRACKED (NR 3 NACELLE) · airframe 81,826 hrs · 15,350 cycles
NR 3 PYLON INBD SKIN HAS A CRACK MIGRATING UNDER AND PAST EXISTING DOUBLER ON LOWER EDGE OF ACESS PANEL, NAC STA 249.
Part: SPAR — CRACKED (NR 4 NACELLE) · airframe 81,826 hrs · 15,350 cycles
NR 4 PYLON LOWER SPAR WEB CRACKED AT APPROX. NAC STA 216.
Part: FIRESHIELD — CHAFED (NR 4 NACELLE) · airframe 81,826 hrs · 15,350 cycles
NR 4 PYLON INBF FIRESHIELD NAC STA 268.0 TO 265.0 CHAFED.
Part: SEAT TRACK — CORRODED (BS 500) · corrosion level 2 · airframe 81,826 hrs · 15,350 cycles
BS 500 LBL 11, SEAT TRACK FLANGE HAS AREA OF CORROSION.
Part: SKIN — CHAFED (NR 4 PYLON) · airframe 81,826 hrs · 15,350 cycles
NR 4 PYLON LT SIDE SKIN HAS CHAFING DAMAGE UNDER FIRESHIELD AT NAC STA 203.
Part: FIRESHIELD — CHAFED (ZONE 400) · airframe 81,826 hrs · 15,350 cycles
NR 4 PYLON HAS CHAFING DAMAGE ON RT SIDE FIRESHIELD FROM NAC STA 200 TO 238.
Part: FIRESHIELD — CHAFED (ZONE 400) · airframe 81,826 hrs · 15,350 cycles
NR 4 PYLON HAS CHAFING DAMAGE ON LT SIDE FIRESHIELD FROM NAC STA 200 TO 238.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,826 hrs · 15,350 cycles
L1 DOOR SILL EMERGENCY LIGHT INOPERATIVE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,826 hrs · 15,350 cycles
EMERGENCY LIGHT ON MAIN DECK CEILING AT APPROXIMATELY BS 500 INOPERATIVE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,826 hrs · 15,350 cycles
UPPER DECK EMERGENCY SLIDE LIGHT INOPERATIVE.
Part: FRAME — CRACKED (NR 2 PYLON) · airframe 81,358 hrs · 15,184 cycles
NR 2 PYLON HAS CRACK ON AFT FRAME RIGHT SIDE AT NAC STA 221.9 BULKHEAD.
Part: FIRESHIELD — DAMAGED (NR 3 PYLON) · airframe 81,358 hrs · 15,184 cycles
NR 3 PYLON FIRE SHIELD DAMAGED AT NAC STA 185 ON LT SIDE.
Part: FRAME — CRACKED (NR 2 PYLON) · airframe 81,358 hrs · 15,184 cycles
NR 2 PYLON NAC STA 221 BULKHEAD FRAME HAS A CRACK ON AFT SIDE.
Part: STIFFENER — CRACKED (NR 4 PYLON) · airframe 81,358 hrs · 15,184 cycles
NR 4 PYLON HAS CRACKED STIFFENER ON MID SPAR WEB AT NAC STA 187.
Part: SKIN — CRACKED (NR 3 PYLON) · airframe 81,358 hrs · 15,184 cycles
NR 3 PYLON CAP SKIN HAS A 1 INCH CRACK AT NAC STA 221 COMING FROM A FASTENER HOLE.
Part: FRAME — CRACKED (NR 2 PYLON) · airframe 81,358 hrs · 15,184 cycles
NR 2 PYLON NAC STA 221 BULKHEAD FRAME CRACKED ON FWD RIGHT SIDE.
Part: FRAME — CRACKED (NR 3 PYLON) · airframe 81,358 hrs · 15,184 cycles
NR 3 PYLON NAC STA 221 BULKHEAD FRAME HAS A CRACK ON UPPER AFT SIDE FLANGE.
Part: FRAME — CRACKED (NR 2 PYLON) · airframe 81,358 hrs · 15,184 cycles
NR 2 PYLON NAC STA 221 BULKHEAD FRAME CRACKED ON AFT LEFT SIDE.
Part: FRAME — CRACKED (NR 3 PYLON) · airframe 81,358 hrs · 15,184 cycles
NR 3 PYLON NAC STA 221 BULKHEAD FRAME CRACKED ON FWD RIGHT SIDE.
Part: FRAME — CRACKED (NR 3 PYLON) · airframe 81,358 hrs · 15,184 cycles
NR 3 PYLON RIGHT SIDE NAC STA 221 BULKHEAD FRAME HAS CRACK IN UPPER AFT FLANGE.
Earlier reports · 2010–2012 · 12 reports
2012
Part: SUPPORT BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 80,850 hrs · 15,076 cycles
SUPPORT BRACKET FOR DIAGONAL BRACE AT RIGHT WING LEADING EDGE STA FSSI 450 HAS EVIDENCE OF CORROSION.
Part: SPAR — CRACKED (NR 3 PYLON) · airframe 80,850 hrs · 15,076 cycles
NR 3 PYLON LOWER SPAR WEB CRACKED AT NAC STA 219, NEXT TO I/B CHORD.
Part: SKIN — CHAFED (FUSELAGE) · airframe 80,850 hrs · 15,076 cycles
UPPER FUSELAGE SKIN HAS WEAR DAMAGE AT BS 2628, LBL 20.
Part: FIREWALL — DAMAGED (NR 2 PYLON) · airframe 80,850 hrs · 15,076 cycles
NR 2 PYLON LOWER SIDE OF STRUT, INTERNAL SKIN FIREWALL DAMAGED ON INBOARD SIDE AT NAC STA 215.9.
Part: FIREWALL — DAMAGED (NR 2 PYLON) · airframe 80,850 hrs · 15,076 cycles
NR 2 PYLON LOWER SIDE OF STRUT, INTERNAL SKIN FIREWALL DAMAGE ON OUTBOARD SIDE PYLON AT NAC STA 215.9.
Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 80,547 hrs · 15,001 cycles
PRIOR TO FLIGHT COULD NOT GET THE EMERGENCY LIGHTS TO EXTINGUISH IN THE ARMED POSITION. REMOVED AND REPLACED THE EMERGENCY LIGHT PANEL ON CAPTAIN'S OVERHEAD IAW B747 AMM 33-51-09, OPS CHECK GOOD.
Part: STIFFENER — CRACKED (RT MLG WW) · airframe 79,700 hrs · 14,814 cycles
REAR SPAR STA 1241 RT FWD W/W, SECOND STIFFENER I/B OF BULKHEAD FITTING HAS A 1.5" CRACK AT UPPER END.
Part: FIRESHIELD — CHAFED (NR 1 PYLON) · airframe 79,700 hrs · 14,814 cycles
NR 1 PYLON INBOARD FIRESHIELD IS CHAFED AT NAC STA 220.
2011
Part: FIRESHIELD — DAMAGED (NR 2 PLYON) · airframe 78,620 hrs · 14,563 cycles
NR 2 PYLON I/B FIRESHIELD AND SKIN DAMAGED, NAC STA 235.
Part: FIRESHIELD — DAMAGED (NR 4 PYLON) · airframe 78,620 hrs · 14,563 cycles
NR 4 PYLON - I/B PYLON LWR SKIN FIRESHIELD DAMAGED, NAC STA 202-219.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,620 hrs · 14,563 cycles
EMERGENCY LIGHT ON UPPER DECK CEILING IN ESCAPE HALLWAY INOP.
2010
Part: FIRE LOOP — OUT OF POSITION (NR 1 ENGINE) · airframe 76,554 hrs · 14,151 cycles
FIRE DETECTION AND NACELLE FIRE DETECTION FAULT LIGHT ILLUMINATED. NR 1 ENGINE TEMPERATURE AND "B" IN RED BAND. INSPECTED NR 1 ENGINE FIRE LOOPS. REPOSITIONED ELEMENT ON UPPER "B" LOOP. PERFORMED OPERATIONAL CHECK OF NR 1 ENGINE FIRE DETECTION SYSTEM IN ACCORDANCE WITH B747 MAINTENANCE MANUAL 26-11-00. NO DEFECTS NOTED.