N719CK

No registry detail on file · not in current registry

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.

47 reports on file, 2007-08-08 – 2008-04-09.

OTHER · 2008-04-09 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CRACKED (BS 360) · airframe 74,527 hrs · 35,279 cycles

UPPER DECK FLOORBEAM UPPER CHORD CRACKED AT BS 360, 18TH HOLE FROM LT SIDE

Source: SDR KCSA081220
OTHER · 2008-04-09 Matched by certificate designator
ATA 5311

Part: FRAME — DAMAGED (BS 1760) · airframe 74,527 hrs · 35,279 cycles

BS 1760 FUSELAGE FRAME LOWER CHORD DAMAGED BETWEEN STR-39R AND STR-40R.

Source: SDR KCSA081221
OTHER · 2008-03-31 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,527 hrs · 35,279 cycles

STR-48R CORRODED AT BS 1480 ON O/B SIDE.

Source: SDR KCSA081218
OTHER · 2008-03-31 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

FLOOR SUPPORT DAMAGED AT STA-2100 RBL-36.

Source: SDR KCSA081219
OTHER · 2008-03-28 Matched by certificate designator
ATA 5311

Part: FRAME — BENT (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

FRAME BENT BETWEEN STA-2200 AND STA-2220 LBL-28.

Source: SDR KCSA081214
OTHER · 2008-03-28 Matched by certificate designator
ATA 5311

Part: FRAME — BENT (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

FRAME BENT BETWEEN STA-2180 AND STA-2200 LBL-28.

Source: SDR KCSA081215
OTHER · 2008-03-28 Matched by certificate designator
ATA 5311

Part: FRAME — BENT (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

FRAME BENT AFT OF BULKHEAD 2160 RBL-32.

Source: SDR KCSA081213
OTHER · 2008-03-28 Matched by certificate designator
ATA 5320

Part: CAP — DENTED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

FWD CARGO STA-920 LBL-12 UPPER CAP DENTED.

Source: SDR KCSA081216
OTHER · 2008-03-28 Matched by certificate designator
ATA 5312

Part: PRESSURE PANEL — CORRODED (WHEEL WELL) · airframe 74,527 hrs · 35,279 cycles

BELOW MAIN DECK FLOOR UPPER WHEEL WELL PRESSURE WEB SURFACE HAS CORROSION AT BS 1460 LBL-69.

Source: SDR KCSA081212
OTHER · 2008-03-26 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,527 hrs · 35,279 cycles

MAIN DECK SEAT TRACK CORRODED AT BS 1800, LBL-99.

Source: SDR KCSA081206
OTHER · 2008-03-26 Matched by certificate designator
ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

STA-1760 STR-38R SKIN DAMAGED.

Source: SDR KCSA081211
OTHER · 2008-03-26 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

FWD PIT FUSELAGE FRAME UPPER CHORD DENTED AT BS 800.

Source: SDR KCSA081207
OTHER · 2008-03-26 Matched by certificate designator
ATA 5320

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

STA-1920 BETWEEN STR-34L AND STR-35L FRAME STIFFENER HAS DAMAGED FLANGE.

Source: SDR KCSA081210
OTHER · 2008-03-26 Matched by certificate designator
ATA 5320

Part: WEB — CRACKED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

FWD PIT BILGE TORQUE BOX UPPER WEB CRACKED AT BS 866, LBL-3.

Source: SDR KCSA081208
OTHER · 2008-03-25 Matched by certificate designator
ATA 5340

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

STRINGER CLIP DAMAGED AT BS 1520, STR-33R.

Source: SDR KCSA081205
OTHER · 2008-03-24 Matched by certificate designator
ATA 5320

Part: TENSION TIE — BROKEN (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

FUSELAGE FRAME TENSION TIE BROKEN BETWEEN BS 1860 AND 1880 ABOVE STR-36L.

Source: SDR KCSA081200
OTHER · 2008-03-24 Matched by certificate designator
ATA 5320

Part: TENSION TIE — BROKEN (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

FUSELAGE FRAME TENSION TIE BROKEN BETWEEN BS 1840 AND 1860 ABOVE STR-36L.

Source: SDR KCSA081201
OTHER · 2008-03-24 Matched by certificate designator
ATA 5320

Part: TENSION TIE — BROKEN (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

FUSELAGE FRAME TENSION TIE BROKEN BETWEEN BS 1880 AND 1900 ABOVE STR-36L.

Source: SDR KCSA081199
OTHER · 2008-03-21 Matched by certificate designator
ATA 5320

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

STA-1580 FRAME VERTICAL STIFFENER DAMAGED AT RBL-18.

Source: SDR KCSA081196
OTHER · 2008-03-21 Matched by certificate designator
ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

STA-400 STR-39R TO STR-40R AT BUTT SPLICE AREA SKIN DAMAGED.

Source: SDR KCSA081193
OTHER · 2008-03-21 Matched by certificate designator
ATA 5311

Part: FRAME — DAMAGED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

STA-1780 FRAME WEB DAMAGED AT RBL-17 ABOVE STR-43R.

Source: SDR KCSA081195
OTHER · 2008-03-21 Matched by certificate designator
ATA 5320

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

STA-1760 FRAME STIFFENER DAMAGED AT RBL-65.

Source: SDR KCSA081197
OTHER · 2008-03-21 Matched by certificate designator
ATA 5311

Part: FRAME — DAMAGED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

STA-1760 RBL-16 FRAME WEB DAMAGED AROUND FASTENERS.

Source: SDR KCSA081194
OTHER · 2008-03-20 Matched by certificate designator
ATA 5320

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

STA-1740 FRAME VERTICAL STIFFENER DAMAGED AT RBL-18.

Source: SDR KCSA081186
OTHER · 2008-03-20 Matched by certificate designator
ATA 5320

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

STA-1540 FRAME VERTICAL STIFFENER DAMAGE AT RBL-14.

Source: SDR KCSA081188
OTHER · 2008-03-20 Matched by certificate designator
ATA 5210

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 74,527 hrs · 35,279 cycles

R-2 DOOR FWD LOWER CORNER VERTICAL FRAME CRACKED IN RADIUS APPROX 11 INCHES.

Source: SDR KCSA081189
OTHER · 2008-03-20 Matched by certificate designator
ATA 5311

Part: FRAME — DAMAGED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

STA-1600 FRAME UPPER CHORD DAMAGED AT RBL-15.

Source: SDR KCSA081187
OTHER · 2008-03-20 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

STA-2120 STR-39R TO STR-41R AREAS OF CORROSION AROUND FASTENERS.

Source: SDR KCSA081185
OTHER · 2008-03-19 Matched by certificate designator
ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 530 BETWEEN STR 41L & 42L.

Source: SDR KCSA081183
OTHER · 2008-03-15 Matched by certificate designator
ATA 5311

Part: STRAP — MISSING (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

AFT BILGE FUSELAGE FRAME STABILIZATION STRAP IS MISSING A SECTION AT STA 2160, LBL 6.

Source: SDR KCSA081176
OTHER · 2008-03-15 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

FUSELAGE FRAME INTERCOSTAL IS CRACKED BETWEEN STA 2220 & 2240, RBL 46 STR 43R.

Source: SDR KCSA081178
OTHER · 2008-03-15 Matched by certificate designator
ATA 5311

Part: STRAP — CRACKED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

AFT BILGE FUSELAGE FRAME STABILIZATION STRAP IS CRACKED AT STA 2160, LBL 28.

Source: SDR KCSA081177
OTHER · 2008-03-13 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,527 hrs · 35,279 cycles

L3 WINDOW, AFT LOWER CORNER EXTERIOR FUSELAGE SKIN HAS A CRACK EXTENDING FROM FASTENER HOLE .250 INCH LONG AT STA 338, STR 8L.

Source: SDR KCSA081174
OTHER · 2008-03-11 Matched by certificate designator
ATA 5210

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 74,527 hrs · 35,279 cycles

MAIN ENTRY DOOR 4R LOWER AFT CORNER FRAME CRACKED AT PREVIOUS STOP DRILL.

Source: SDR KCSA081168
OTHER · 2008-03-11 Matched by certificate designator
ATA 5210

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 74,527 hrs · 35,279 cycles

MAIN ENTRY DOOR 4R TOP AFT CORNER FRAME CRACKED BS 1700.

Source: SDR KCSA081167
OTHER · 2008-03-11 Matched by certificate designator
ATA 5210

Part: FITTING — CRACKED (R1 DOOR) · airframe 74,527 hrs · 35,279 cycles

MAIN ENTRY DOOR 1R UPPER AFT CORNER FITTING CRACKED BS 485.

Source: SDR KCSA081170
OTHER · 2008-03-11 Matched by certificate designator
ATA 5210

Part: DOOR FRAME — CRACKED (L2 DOOR) · airframe 74,527 hrs · 35,279 cycles

MAIN ENTRY DOOR 2L FWD LOWER CORNER FRAME CRACKED BS 808.

Source: SDR KCSA081169
Earlier reports · 2007 · 10 reports

2007

OTHER · 2007-10-11 Matched by certificate designator
ATA 5412

Part: BULKHEAD — CHAFED (NR 4 PYLON) · airframe 74,048 hrs · 35,185 cycles

NR 4 PYLON FWD ENGINE MOUNT BULKHEAD CHORD HAS CHAFING ON FWD OF NAC STA 128.

Source: SDR KCSA071464
OTHER · 2007-10-10 Matched by certificate designator
ATA 5711

Part: STIFFENER — CORRODED (LT WING) · airframe 74,048 hrs · 35,185 cycles

LEFT WING FRONT SPAR VERTICAL STIFFENER HAS CORROSION AT FS 1280.

Source: SDR KCSA071459
OTHER · 2007-10-08 Matched by certificate designator
ATA 5412

Part: BULKHEAD — WORN (NR 3 NACELLE) · airframe 74,048 hrs · 35,185 cycles

NR 3 PYLON ENG PRESSURE LINE AT NAC STA 221.9 WORN INTO BULKHEAD.

Source: SDR KCSA071454
OTHER · 2007-10-08 Matched by certificate designator
ATA 5412

Part: BULKHEAD — WORN (NR 4 NACELLE) · airframe 74,048 hrs · 35,185 cycles

NR 4 PYLON HYD LINE B-NUT WORN INTO NAC STA 221.9 BULKHEAD.

Source: SDR KCSA071455
OTHER · 2007-10-07 Matched by certificate designator
ATA 5320

Part: WEB — DAMAGED (BS 1660-1680) · airframe 74,048 hrs · 35,185 cycles

AFT PIT BILGE TORQUE BOX UPPER WEB DAMAGED AT PREVIOUS REPAIR BETWEEN BS 1660 AND 1680, BL 0.

Source: SDR KCSA071444
OTHER · 2007-09-18 Matched by certificate designator
ATA 5313

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,048 hrs · 35,185 cycles

STR 38L CRACKED BETWEEN BS 480 AND 500.

Source: SDR KCSA071380
NO TEST · 2007-09-08 Matched by certificate designator
ATA 3350

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,215 hrs · 18,173 cycles

MAIN DECK EMERGENCY LIGHT AT STA -390 INOP.

Source: SDR KCSA071334
NO TEST · 2007-09-08 Matched by certificate designator
ATA 3350

Part: SIGN — INOPERATIVE (CABIN) · airframe 69,215 hrs · 18,173 cycles

UPPER DECK RIGHT DOOR EMERGENCY EXIT SIGN INOP.

Source: SDR KCSA071335
SMOKE/FUMES/ODORS/SPARKS · 2007-08-08 Matched by certificate designator
ATA 2120

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 73,898 hrs · 35,156 cycles

AT FL 360 AT 0230Z, SMOKE APPEARED IN THE COCKPIT. THREE SECONDS LATER THE NR 4 EGT WENT TO RED LINE, THE RED EGT LIGHT ILLUMINATED, THE OIL QUANTITY WENT TO ZERO, THE OIL PRESSURE WENT TO ZERO, THE OIL TEMPERATURE WENT TO THE RED LINE, AND N2 WENT TO ZERO. SEVER ENGINE CHECK LIST WAS COMPLETED. N1 GAUGE INDICATED 33 PERCENT, BUT VISUAL OBSERVATION SHOWED NO ROTATION OF THE N1 FAN BLADES. THE COCKPIT SMOKE CEASED AFTER THE IMMEDIATE ACTION ITEMS WERE ACCOMPLISHED.

Source: SDR KSCA07062
SMOKE/FUMES/ODORS/SPARKS; WARNING INDICATION · 2007-08-08 Matched by certificate designator
ATA 7200

Part: ENGINE — MALFUNCTIONED (NR 4) · airframe 73,898 hrs · 35,156 cycles

AT FL 360 AT 0230Z, SMOKE APPEARED IN THE COCKPIT. THREE SECONDS LATER THE NR 4 EGT WENT TO RED LINE, THE RED EGT LIGHT ILLUMINATED, THE OIL QUANTITY WENT TO ZERO, THE OIL PRESSURE WENT TO ZERO, THE OIL TEMPERATURE WENT TO THE RED LINE, AND N2 WENT TO ZERO. SEVER ENGINE CHECK LIST WAS COMPLETED. N1 GAUGE INDICATED 33 PERCENT, BUT VISUAL OBSERVATION SHOWED NO ROTATION OF THE N1 FAN BLADES. THE COCKPIT SMOKE CEASED AFTER THE IMMEDIATE ACTION ITEMS WERE ACCOMPLISHED.

Source: SDR KCSA07062