N915CK
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.
153 reports on file, 2005-03-03 – 2019-07-09.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,539 hrs · 76,280 cycles
EMERGENCY EXIT LIGHTS INOP.
Part: UNKNOWN — MALFUNCTIONED (AILERON SYS) · airframe 64,537 hrs · 76,279 cycles
AFTER TAKEOFF FLIGHT CONTROLS REQUIRED ABNORMAL AND EXCESSIVE AMOUNT OF RIGHT AILERON INPUT "UP" POSITION TO CONTROL AIRCRAFT.
Part: UNKNOWN — MALFUNCTIONED (AILERON SYS) · airframe 64,537 hrs · 76,279 cycles
IMMEDIATELY FOLLOWING TAKEOFF, I NOTICED THAT PILOT WAS USING GREATER THAN NORMAL AILERON INPUT TO CONTROL AIRCRAFT. HE APPEARED TO BE FIGHTING THE PLANE. I ASKED HIM "IS THE PLANE FLYING OKAY"? HE RESPONDED "SHE'S FLYING FUNNY". THE DEPARTURE CLEARANCE WAS RUNWAY HEADING TO 3,000'. IT WAS FAIRLY SMOOTH AND WE WERE STRAIGHT OUT AT THIS POINT GOING THROUGH 800' AGL. I ASKED HIM TO TRANSFER THE CONTROLS TO ME, SO THAT I COULD FEEL THE PLANE. THE AILERON MOVEMENT WAS GREATER THAN WHAT SHOULD HAVE BEEN REQUIRED TO FLIGHT STRAIGHT AHEAD FOR THE CONDITIONS. AS WE ACCELERATED, THE AIRCRAFT HANDLING CHARACTERISTICS IMPROVED, BUT TO NORMAL EXPECTATIONS. WE WERE THROUGH 2500' AGL AT THIS POINT. I STARTED TO COMPLETE THE AFTER TAKEOFF TAKEOFF ITEMS. DURING THE "UPLATCH" CHECK, THE GEAR DOOR OPEN LIGHT ILLUMINATED, FOLLOWED BY AERODYNAMIC NOISE FROM THE GEAR AND AN ASSOCIATED LEFT GEAR UNSAFE LIGHT. I IMMEDIATELY TURNED THE HYDRAULIC PUMPS ON-HIGH-HIGH-ON AND PUT THE GEAR SELECTOR IN THE UP POSITION. THE LIGHTS EXTINGUISHED AND THE ASSOCIATED AERODYNAMIC NOISE CEASED. THE AILERON INPUTS NEEDED WERE STILL GROSSLY ABOVE NORMAL FOR THE FLIGHT REGIME, SPEED, AND CONDITIONS. I INFORMED PILOT THAT WERE GOING TO GO BACK AND LAND AND TO MAINTAIN VFR 4,500' MSL AND THAT WE WOULD BE RETURNING TO GYH WHICH WAS DIRECTLY UNDER OUR LEFT WING (AIRCRAFT POSITION - 3 MILE DOWNWIND). I INFORMED DEPARTURE THAT WE WOULD BE RETURNING TO GYH, THAT WE HAD AN INDICATION ISSUE. WHEN ASKED ABOUT DECLARING AN EMERGENCY, I STATED "NO, THAT IS NOT NECESSARY AND THAT THIS WAS A PRECAUTIONARY LANDING". WE WERE CLEARED TO 3,000. I STATED THAT WE HAD THE FIELD IN SIGHT. WE WERE CLEARED FOR THE VISUAL TO RUNWAY 23. WE WERE HANDED OFF TO TOWER, AND CLEARED TO LAND. ON FINAL PILOT WAS STILL FIGHTING THE AIRPLANE. I INFORMED PILOT TO NOT GET BELOW THE APPROACH "TARGET SPEED" AND TO CARRY A LITTLE EXTRA SPEED TO ENSURE THAT THERE WAS ENOUGH AIRFLOW OVER THE SURFACES TO CONTROL THE AIRCRAFT. WHEN THE GEAR PLACED IN THE EXTEND POSITION, IT EXTENDED NORMALLY WITH NO ABNORMAL INDICATIONS. FLIGHT 305736 LANDED WITHOUT INCIDENT. DISPATCH WAS CALLED AFTER SHUTDOWN, AS WELL AS MAINTENANCE CONTROL. THE DISCREPANCIES WERE DISCUSSED. THE SAFETY OFFICER AND CHIEF PILOT WERE NOTIFIED VIA PHONE. AFTER LANDING DURING CREW DISCUSSION, PILOT STATED THAT AILERON LIGHT WAS ILLUMINATING DURING THE NEAR "FULL" CONTROL DEFLECTION(S).
Part: CHECK VALVE — STUCK (FUEL CELL) · airframe 64,493 hrs · 76,248 cycles
IN FLIGHT THE CENTER TANK GAINS FUEL FROM THE LEFT TANK. REMOVED AND REPLACED CENTER TANK PUMP DISCHARGE CHECK VALVE IAW DC9 AMM 28-20-11, LEAK AND OPS CHECK GOOD IAW AMM 28-20-00 NO DEFECTS NOTED
Earlier reports · 2005–2017 · 149 reports
2017
Part: WARNING LIGHT — MULTIPLE IND · airframe 64,181 hrs · 76,080 cycles
SPOILER DEPLOYED ANNUNCIATOR LIGHT CAME ON, SPOILERS WERE DEPLOYED. CABIN PRESSURIZATION INOPERATIVE. WINDSHEAR FAIL ANNUNCIATOR LIGHT CAME ON. FLIGHT CONTROLS, SPOILER MALFUNCTION, SECURED AIRCRAFT FOR LANDING IAW COM AND A/C CHECKLIST. RETURNED TO DEPARTURE WITHOUT INCIDENT. DID NOT DECLARE EMERGENCY.
Part: BUTTON — OUT OF ADJUST (LANDING GEAR) · airframe 64,189 hrs · 76,087 cycles
LANDING GEAR HANDLE DID NOT GO UP INTO THE UP POSITION AFTER TAKEOFF. ADJUSTED ANTIRETRACTION BUTTON IAW DC-9 AMM 32-31-1, OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.
Part: FRAME — CORRODED (BS 786) · corrosion level 2 · airframe 64,041 hrs · 75,990 cycles
FRAME BS 786, RBL 0 - 30 CORRODED.
Part: SKIN — CORRODED (BS 642) · corrosion level 2 · airframe 64,041 hrs · 75,990 cycles
AFT CARGO BAY SKIN CORRODED AT BS 642, RBL 14
2016
Part: CABLE — OUT OF ADJUST (ZONE 700) · airframe 63,809 hrs · 75,852 cycles
ON TAKEOFF, LANDING GEAR WOULD NOT RETRACT, FOLLOWED COM PROCEDURE, CHAPTER 32, PAGE 8.
Part: WINDOW FRAME — CRACKED (BS 83) · airframe 63,789 hrs · 75,837 cycles
COCKPIT ENCLOSURE WINDOW SILL INTERNAL FRAME HAS A CRACK 1.3 INCHES AT BS 83 LBL 12
Part: FRAME — CRACKED (FUSELAGE) · airframe 63,789 hrs · 75,837 cycles
L/W WINDOW SILL INTERNAL FRAME CRACKED (INTERNAL FRAME) LT END CRACK LENGTH 2.0, RT END CRACK LENGTH 1.375.
Part: PRESSURE PANEL — CORRODED (RT MLG WW) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
RT WW PRESSURE WEB CORROSION.
Part: FRAME — CRACKED (FUSELAGE) · airframe 63,789 hrs · 75,837 cycles
FRAME CRACK.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
CUSP WEB CORROSION.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
FWD PIT FLOORBEAM CORROSION.
Part: VANE — CORRODED (TE FLAP) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
RT I/B FLAP VANE HAS CORROSION.
Part: FRAME — CRACKED (FUSELAGE) · airframe 63,789 hrs · 75,837 cycles
FRAME CRACK.
Part: VANE — CORRODED (TE FLAP) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
RT O/B FLAP VANE HAS CORROSION.
Part: VANE — CORRODED (TE FLAP) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
RT CENTER FLAP VANE HAS CORROSION.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
FLOOR WEB CORROSION.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
SEAT TRACK CORROSION.
Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
BULKHEAD BETWEEN 19R & 20R IN AFT CARGO COMPARTMENT CORROSION.
Part: ANGLE — CRACKED (COCKPIT) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
LT WINDSCREEN COCKPIT ENCLOSURE ZEE CORRODED.
Part: SEAT TRACK — CORRODED (BS 323-394) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
SEAT TRACK CORRODED BS 323-394 RBL 45.
Part: CUSP WEB — CORRODED (BS 624-642) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
CUSP WEB CORRODED BS 624 - 642.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
FWD FUSELAGE EXTERIOR BELOW CUSP LINE CORROSION.
Part: FLOORBOARD — CORRODED (CABIN) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
FWD OF RT OVERWING DOOR, FLOORBOARD CORROSION.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
MAIN DECK CUSP WEB CORRODED STA 216, LBL 55.
Part: FRAME — CRACKED (BS 624) · airframe 63,789 hrs · 75,837 cycles
BS 624 FRAME CRACKED LOWER FLANGE.
Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
RT STA 566-642 FLOORBOARD SUPPORT BROKEN.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
RT STA 566-642 FLOORBOARD CORROSION.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
STA 756-762, STR 1, INTERCOSTAL CORROSION.
Part: INTERCOSTAL — CRACKED (BS 604-623) · airframe 63,789 hrs · 75,837 cycles
BS 604 - 623, STRINGER 1 INTERCOSTAL, CRACKED.
Part: GUSSET — CRACKED (BS 332) · airframe 63,789 hrs · 75,837 cycles
FRAME GUSSET CRACKED BS 332, RBL 60.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
NOSE WW CORROSION, STA 69, RBL 12.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
NOSE WW CORROSION, STA 69, LBL 12.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
CORROSION ON AND UNDER SEAT TRACK AT CUSPLINE, STA 642.
Part: WINDSCREEN — CRACKED (ZONE 200) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
CORROSION AND CRACKED WINDSCREEN ENCLOSURE, PN 5912350-68, REF AD 2002-21-09.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 63,789 hrs · 75,837 cycles
COCKPIT WINDOW INTERNAL FRAME 1" CRACK, PN 9911505-5, REF AD 2002-21-09 AND SB 53-290.
Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 63,789 hrs · 75,837 cycles
FLOOR SUPPORTS ARE DAMAGED, STA 300-389 RT, FWD OF RT OVERWING DOOR.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
CORROSION ON CUSP WEB, STA 535-585, RT SIDE.
Part: FITTING — CRACKED (FUSELAGE) · airframe 63,789 hrs · 75,837 cycles
FITTING CRACKED STA 535, RBL 55, PN 3921947-503.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
AFT CARGO COMPARTMENT CEILING STA 661, RBL 60.
Part: THRUST REVERSER — CRACKED (RT ENGINE) · airframe 63,789 hrs · 75,837 cycles
RIGHT ENGINE LOWER THRUST REVERSER HALF OTBD T/E CRACKED.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles
CORROSION ON LT SIDE OF FUSELAGE EXTERIOR, STA 218, BELOW CUSP LINE.
2015
Part: UNKNOWN — UNKNOWN (FUEL SYSTEM) · airframe 63,368 hrs · 75,577 cycles
FUEL MIGRATION.
2014
Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 63,244 hrs · 75,494 cycles
FWD SIDE OF AIRSTAIR DOOR SURROUND CRACK.
Part: DOOR FRAME — CRACKED (BS 817) · airframe 63,244 hrs · 75,494 cycles
LEFT UPPER DOOR SURROUND FRAME IS CRACKED.
Part: DOOR FRAME — CRACKED (BS 817) · airframe 63,244 hrs · 75,494 cycles
RT UPPER DOOR FRAME IS CRACKED.
Part: SPAR — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,244 hrs · 75,494 cycles
BS 491, FRONT SPAR RT BEHIND WING ATTACH FITTING CORROSION, 1 X 1.
Part: BEAM — CRACKED (BS 604) · airframe 63,244 hrs · 75,494 cycles
SPAN WISE BEAM FWD LOWER ATTACH FLANGE CRACKED AT FASTENER HOLE.
Part: SEAT TRACK — CORRODED (BS 313-435) · corrosion level 2 · airframe 63,244 hrs · 75,494 cycles
MCD SEAT TRACK CORRODED, BS 313-435, LBL 54.
Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,244 hrs · 75,494 cycles
FRONT SPAR LOWER WING ATTACH FITTING HAS CORROSION BETWEEN LONGERON 22R AND 23R. 1 X 1 AND 2 CRACKS.
Part: FRAME — CRACKED (BS 585) · airframe 63,244 hrs · 75,494 cycles
CRACK ON LOWER AFT OTBD POCKET OF FRAME FITTING, LEFT.
Part: SKIN — CRACKED (THRUST REVERSER) · airframe 63,244 hrs · 75,494 cycles
NR 1 ENGINE THRUST REVERSER OUTER SKIN CRACKED AT INBD SIDE, 3 O'CLOCK POSITION, 8" FROM AFT END.
Part: FRAME — CRACKED (LT MLG WW) · airframe 63,244 hrs · 75,494 cycles
FUSELAGE FRAME LOWER FARING LT W/W LOWER FITTING HAS CRACK AT UPPER END.
Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 63,244 hrs · 75,494 cycles
LEFT INBD FLAP DAMAGED OTBD L/E, 1 X 1.
Part: RETAINER — CRACKED (RT WINDOW) · airframe 63,244 hrs · 75,494 cycles
CRACK INDICATION FOUND DURING X-RAY INSPECTION, RT OUTER LOWER WINDOW RETAINER.
Part: SKIN — CRACKED (LT MLG WW) · airframe 63,244 hrs · 75,494 cycles
LEFT MAIN GEAR WHEEL WELL UPPER LT SKIN HAS A CRACK.
Part: BULKHEAD WEB — CRACKED (LT MLG WW) · airframe 63,244 hrs · 75,494 cycles
LEFT MAIN GEAR WHEEL WELL UPPER LT SKIN HAS A CRACK.
Part: INDICATOR — INACCURATE (ALTIMETER) · airframe 63,181 hrs · 75,455 cycles
ALTIMETER DISCREPANCY WITH ATC ENROUTE FLYING AT 29.92 AT 35,000, ATC SHOWED AIRCRAFT AT 35,300 FT. REPLACED AIU, PERFORMED OP'S CHECK, OP'S CHECKED GOOD. AIRCRAFT IS RVSM COMPLIANT.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,015 hrs · 75,324 cycles
CORROSION ON STRINGER 23L BS 766 - 786.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 63,015 hrs · 75,324 cycles
CRACKED FLOOR SUPPORT AT BS 786, LBL 28.
2012
Part: CSD — SEIZED (RT ENGINE) · airframe 62,251 hrs · 74,835 cycles
IN CRUISE FLIGHT AUTOPILOT KICKED OFF AND SUBSEQUENTLY NOTICED A RIGHT GENERATOR OFF AND RIGHT CSD OIL PRESS LOW LIGHT ILLUMINATED ON THE OVERHEAD PANEL. PERFORMED CSD OIL LOW PRES CHECKLIST PER COM. INDICATION SHOWED VOLTS ON THE INDICATOR AND A HIGH TEMP READING ON THE CSD GAUGE IT CALLED FOR A CSD DISCONNECT. UPON COMPLETION OF MANEUVER VOLTS AND HIGH TEMP STILL INDICATING, ATTEMPTED DISCONNECT A SECOND TIME PER COM AND RESETTING OF THE CIRCUIT BREAKER AT WHICH TIME IT SEEMED THAT THERE WAS NOT A CLEAN DISCONNECT. WITH INDICATIONS IT WAS NECESSARY TO PERFORM A PRECAUTIONARY ENGINE SHUTDOWN PER THE COM, DOING SO THE CREW HAD TO DECLARE AND EMERGENCY AND DIVERTED TO KSHV. ONCE ON GROUND VERIFIED CSD DISCONNECT PER MAINTENANCE BY RESTARTING ENGINE. CSD OVERHEATED AND SEIZED SHEERING THE SHAFT ON THE GENERATOR. REPLACED BOTH UNITS TO INCLUDE CSD OILER COOLER.
Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 62,091 hrs · 74,727 cycles
DURING SERVICE CHECK FOUND DAMAGE TO MAIN DECK CARGO DOOR APPROX 9 INCHES FROM SILL AND 6 INCHES FORWARD FROM MANUAL AND UNLOCKING MECHANISM.
Part: WARNING LIGHT — INOPERATIVE (COCKPIT) · airframe 61,711 hrs · 74,473 cycles
RIGHT LANDING GEAR (GREEN DOWN AND LOCK) LIGHT WILL NOT ILLUMINATE WHEN LEVER IS IN THE DOWN POSITION. CREW PERFORMED A GO-AROUND AND LANDED ON THE SECOND ATTEMPT. REPLACED LIGHT ASSY IAW SPWM 20-84-00, OPS CHECKED GOOD IAW DC9 AMM 32-60-1.
2011
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
FLOORBOARD CORROSION, 1X2 INCHES.
Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 61,468 hrs · 74,324 cycles
KEEL BEAM EVIDENCE OF CRACK VERTICAL 3 INCHES.
Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 61,468 hrs · 74,324 cycles
KEEL BEAM EVIDENCE OF 2 INCH CRACK.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
CUSP WEB CORROSION, 2X6 INCHES.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
CUSP WEB CORROSION, 2X6 INCHES.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
SEAT TRACK CORROSION, 2X6 INCHES.
Part: FLANGE — CRACKED (NR 2 PYLON) · airframe 61,468 hrs · 74,324 cycles
2 PYLON UPPER SURFACE TOP FLANGE CRACKED IN RADIUS.
Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 61,468 hrs · 74,324 cycles
NR 2 PYLON ANGLE CRACK, 1 INCH.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOORBOARD UPPER SKIN CORROSION, 3X10 INCHES.
Part: WEB — CRACKED (NR 2 PYLON) · airframe 61,468 hrs · 74,324 cycles
NR 2 PYLON AFT MOUNT WEB CRACKED, .5 INCH CRACK.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOORBOARD UPPER SKIN CORROSION, 3X3 INCHES.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MDC FLOORBOARD SKIN CORROSION, 5X5 INCHES.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOORBOARD UPPER SKIN 3X13 INCHES CORRODED.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOORBOARD UPPER SKIN CORROSION, 5X6 INCHES.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOORBOARD UPPER SKIN, 3X5 INCHES.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOORBOARD UPPER SKIN CORROSION, 3X6 INCHES.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOORBOARD UPPER SKIN CORROSION, 5X9 INCHES.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOORBOARD UPPER SKIN CORROSION, 2X8 INCHES.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOORBOARD UPPER SKIN CORROSION, 1X1 INCH.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
FLOORBOARD CORROSION, 1X2 INCHES.
Part: SPAR — UNKNOWN (NACELLE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
NR 2 I/B SPAR AFT MOUNT SPAR WEB, 1X3 INCHES.
Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 61,468 hrs · 74,324 cycles
MID SPAR LOWER I/B ANGLE CRACKED, NR 2 PYLON AT AFT ENGINE MOUNT.
Part: WEB — CRACKED (NR 2 PYLON) · airframe 61,468 hrs · 74,324 cycles
NR 2 PYLON AFT PYLON WEB CRACK, 2 INCH CRACK.
Part: FRAME SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
LT WW FRAME SPLICE CORROSION, 1X2 INCHES.
Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
FLOOR MEMBRANE CORROSION, FS 623 BELOW O/B SEAT TRACK 3X5 INCHES.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
EVIDENCE OF CORROSION ON STRINGER, 1X1 INCHES.
Part: FRAME SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
FRAME SPLICE PLATE O/B END OF SLICE PLATE SUSPECT CORROSION IN LEFT W/W, 3X5 INCHES.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOOR PANEL SUPPORT CORRODED, 2X4 INCHES.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MCD FLOORBEAM SUPPORT CORROSION, 2X6 INCHES.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOOR PANEL CORRODED AND DAMAGED AROUND SCREW HOLES, 3X3 INCHES.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
FLOORBOARD CORROSION.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOOR PANEL RT SIDE CORRODED, 2X6 INCHES.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOOR PANEL CORRODED IN SEVERAL PLACES, 2X6 INCHES.
Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOOR PANEL STIFFENER CHANNEL DAMAGED ON END, 1X6 AT CUSP LINE.
Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MCD FLOOR PANEL CORROSION, 4X15 INCHES.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MAIN DECK FLOOR PANEL CORRODED, 5X8 INCHES.
Part: SPAR — CRACKED (WING) · airframe 61,468 hrs · 74,324 cycles
UPPER AFT CENTER SPAR CHORD CRACKED, 1X8 INCHES.
Part: SPAR — CORRODED (WING) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
WING REAR SPAR CORROSION, 1X2 INCHES.
Part: ATTACH ANGLE — CORRODED (LT MLG WW) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
LEFT WW PRESSURE WEB ATTACH ANGLE CORRODED, 1X1 INCHES.
Part: SKIN — CANNING (FUSELAGE) · airframe 61,468 hrs · 74,324 cycles
EXTERIOR SKIN OIL CANNING 6X8 INCHES.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
CORROSION ON INTERCOSTAL, 1X4 INCHES.
Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
SHEAR WEB CORRDED, 2X3 INCHES.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
E&E COMPARTMENT CORROSION, FLOOR WEB 4X8 INCHES, 15 INCHES RIGHT FROM CENTER OF FLOOR WEB.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
E&E COMPARTMENT EVIDENCE OF CORROSION, STA 200 2 INCHES RIGHT FROM CENTER FLOOR WEB 3X4 INCHES CORROSION.
Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
FLOOR SHEAR WEB CORROSION, 4X12 INCHES.
Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
FLOOR SHEAR WEB CORROSION, 4X8 INCHES.
Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 61,468 hrs · 74,324 cycles
FLOOR SHEAR WEB CRACK, 1 INCH.
Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
FLOOR SHEAR WEB CORROSION, 4X8 INCHES.
Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
FLOOR SHEAR WEB CORROSION, 1X1 INCHES.
Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
FLOOR SHEAR WEB CORROSION, 1.5X8 INCHES.
Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
MCD FLOORBOARD SKIN CORROSION, 3X5 INCHES.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
SEAT TRACK CORROSION, 1X1 INCHES.
Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
FLOOR SHEAR WEB CORROSION, 3X8 INCHES.
Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
W/W FWD BULKHEAD CORROSION, 3X7 INCHES.
Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,468 hrs · 74,324 cycles
PRESSURE DECK CORROSION, W/W LOWER SIDE 2X2 INCHES.
Part: FITTING — CRACKED (RT MLG WW) · airframe 61,468 hrs · 74,324 cycles
RIGHT WW FITTING 26 INCHES BELOW PRESSURE DECK HAS VERTICAL CRACK.
Part: DOUBLER — LEAKING (LT WING) · airframe 61,468 hrs · 74,324 cycles
L/W LOWER WING MOST I/B ACCESS PANEL PATCH LEAKING.
2010
Part: VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 61,028 hrs · 74,098 cycles
UNABLE TO PRESSURIZE IN AUTO MODE.
Part: BEAM — CRACKED (SERVICE DOOR) · airframe 60,450 hrs · 73,758 cycles
RT GALLEY SERVICE DOOR AT STA 200, BEAM NR 3 CRACKED ON AFT END. DOOR HAS BEEN REPLACED.
2009
Part: HEATER — SPARKS (WINDSHIELD) · airframe 60,080 hrs · 73,538 cycles
FO'S WINDOW SPARKED AND OUTER GLASS CRACKED, EMERGENCY DESCENT WAS GIVEN TO 10,000 FT. TURNED OFF WINDSHIELD HEAT AND DONNED O2 MASKS RETURNED TO CYEG.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,845 hrs · 73,379 cycles
AFT EXIT PRESSURE DOOR FRAME HAS A CRACKED ANGLE STIFFENER AT 12 O'CLOCK CENTER FRAME.
Part: SKIN — CRACKED (FUSELAGE) · airframe 59,845 hrs · 73,379 cycles
SKIN CRACKED IN AREA OF RT AFT NOSE GEAR DOOR AFT HINGE CRACKED, 1 X 1 INCH.
Part: WEB — CHAFED (NLG WW) · airframe 59,845 hrs · 73,379 cycles
UPLOCK ACTUATOR MOUNT WEB CHAFED 7 INCHES DOWN FROM MAIN DECK FLOOR, 1 X 1 INCH.
Part: WEB — CHAFED (NLG WW) · airframe 59,845 hrs · 73,379 cycles
UPLOCK ACTUATOR MOUNT WEB CHAFED 7 INCHES DOWN FROM MAIN DECK, 1 X 1 INCH.
Part: BULB — BURNED OUT (CABIN) · airframe 59,845 hrs · 73,379 cycles
EMERGENCY LIGHT ASSY INOP AT L1 DOOR. REPLACED BULB, OPS CHECKED GOOD ALL WORK IAW MM 33-53-00.
2008
Part: TERMINAL BLOCK — BROKEN (ELECTRICAL SYS) · airframe 59,767 hrs · 73,330 cycles
TERMINAL BLOCK AT STA FS 146 FLOORBEAM BROKE, AFTER INVESTIGATION FOUND 2 WIRES DAMAGED. REPLACED WIRE FROM TERMINAL NR 1 TO THE T1 POSITION ON THE LEFT APU BUSS RELAY. ALSO REPLACED TERMINAL END ON THE SECOND ATTACHING IN THE NR 1 POSITION OF THE TERMINAL BLOCK.
2007
Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 58,989 hrs · 72,777 cycles
CABIN WILL NOT PRESSURIZE.
Part: WEB — CORRODED (BS 646) · corrosion level 2 · airframe 58,969 hrs · 72,762 cycles
BS 646 APPROX RBL 55 WEB UNDER FLOOR BOARD CORRODED.
Part: DOOR FRAME — BROKEN (BS 180) · airframe 58,969 hrs · 72,762 cycles
GALLEY SERVICE DOOR FRAME BROKE APPROX STA 180 21 INCHES FROM BOTTOM OF DOOR STR 15 RT.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 58,969 hrs · 72,762 cycles
MAIN DECK FLOOR PANEL EDGE LIFTING BETWEEN BS 503 AND 566 AT LBL 21.
Part: STIFFENER — CRACKED (BS 860) · airframe 58,969 hrs · 72,762 cycles
HORIZONTAL STIFFENER CRACKED AT END FASTENER ON UPPER SKIN SURFACE INSIDE ACCESS PANEL 8204 18 INCHES OTBD OF FUSELAGE APPROX STA 860.
Part: DOOR FRAME — CRACKED (BS 180 S13R) · airframe 58,969 hrs · 72,762 cycles
GALLEY SERVICE DOOR INTERIOR HORIZONTAL FRAME CRACKED BEYOND STOP DRILL IN OUTBOARD RADIUS AT FORWARD SIDE OF DOOR APPROX BS 180 STRINGER 13R 1 INCH CRACK.
Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 58,969 hrs · 72,762 cycles
FLOOR SUPPORT CORRODED AT STA 200 LBL 55.
Part: STRUCTURE — CORRODED (BS 620) · corrosion level 2 · airframe 58,969 hrs · 72,762 cycles
W/W CEILING AT STA 620 RBL 40 HAS SIGNS OF CORROSION.
Part: SUPPORT FITTING — CORRODED (BS 623) · corrosion level 2 · airframe 58,969 hrs · 72,762 cycles
WHEEL WELL CEILING HAS EVIDENCE OF CORROSION AROUND SIDE BRACE SUPPORT FITTING APPROX STA 623 LBL 56.
Part: VERTICAL BEAM — CRACKED (CARGO BAY) · airframe 58,969 hrs · 72,762 cycles
FORWARD PIT DOOR UPPER CENTER AFT STOP FITTING VERTICAL BEAM WEB CRACKED AT TOOLING HOLE AT UPPER AREA VERIFIED USING HIGH FREQ EDDY CURRENT.
Part: CROSSBEAM — CRACKED (CARGO DOORWAY) · airframe 58,969 hrs · 72,762 cycles
AFT PIT DOOR FWD STOP FITTING CROSSBEAM CRACKED UNDER RADIOUS FILLER ON OUT FASTENER FOR STOP FITTING VERIFIED USING HFEC.
Part: CROSSBEAM — CRACKED (CARGO DOORWAY) · airframe 58,969 hrs · 72,762 cycles
AFT PIT DOOR 2ND FROM THE BOTTOM STOP FITTING CROSSBEAM CRACKED IN 2 PLACES UNDER RADIUS FILLER ON INNER FASTENER FOR STOP FITTING VERIFIED USING HFEC.
Part: BEAM — CRACKED (CARGO DOOR) · airframe 58,969 hrs · 72,762 cycles
FORWARD CARGO DOOR UPPER CENTER FORWARD STOP FITTING VERTICAL BEAM WEB CRACKED AT TOOLING HOLE AT UPPER AREA VERIFIED BY HFEC.
Part: FLOOR PANEL — CORRODED (BS 370-446) · corrosion level 2 · airframe 58,969 hrs · 72,762 cycles
CORROSION ON TOP OF MAIN DECK FLOOR PANELS BETWEEN BS 370 AND 446, RBL 52.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 58,969 hrs · 72,762 cycles
MAIN DECK FLOOR PANEL EDGE LIFTING BETWEEN BS 503 AND 566 AT RBL 21.
Part: ANGLE — CRACKED (GALLEY DOOR) · airframe 58,969 hrs · 72,762 cycles
GALLEY SERVICE DOOR HAS CRACK ANGLE FWD OF HINGE TORQUE TUBE.
Part: FRAME — BENT (FUSELAGE) · airframe 58,969 hrs · 72,762 cycles
STA 58 FRAME INNER FLANGE BENT LBL 27 10 INCHES UP FROM NOSE GEAR DOOR OPENING.
2006
Part: FRAME — CRACKED (BS 964) · airframe 58,536 hrs · 72,518 cycles
BS 964 FRAME WEB HAS 1.5 CRACK OTBD OF STAIRWELL OPENING ON RT SIDE.
Part: DOOR FRAME — CRACKED (AIRSTAIR) · airframe 58,536 hrs · 72,518 cycles
AFT AIRSTAIRS DOOR CUTOUT FRAME CRACKED AT AFT END RT SIDE, 1 INCH CRACK IN DOOR OPENING FRAME CAP.
2005
Part: DOUBLER — CRACKED (FUSELAGE)
A 1.375 INCH LONG CRACK IN ACCESS DOOR DOUBLER.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,698 hrs · 71,942 cycles
MAIN DECK FLOORBEAM CORRODED AT NUT PLATES.