N807SK
Registered owner: SKYWEST AIRLINES INC, UT (owner ≠ operator)
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.
116 reports on file, 2007-05-30 – 2018-05-31.
Part: STRINGER — CORRODED (BS 333-364) · airframe 30,574 hrs · 19,169 cycles
CORROSION FOUND ON STRINGER 27 BETWEEN BS 333, AND 364. REMOVED AND REPLACED THE STRINGER SECTION IAW SRM.
Part: STRINGER — CORRODED (BS 333-364) · airframe 30,574 hrs · 19,169 cycles
CORROSION FOUND ON STRINGER 26R BETWEEN BS 333 - 364. REMOVED AND REPLACED THE STRINGER IAW SRM.
Part: STRINGER — CORRODED (BS 319.7-333) · airframe 30,574 hrs · 19,169 cycles
CORROSION FOUND ON STRINGER 26L BETWEEN BS 319.7 AND 333. REMOVED AND REPLACED THE STRINGER IAW SRM.
Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 30,574 hrs · 19,169 cycles
CORROSION FOUND ON THE STRINGER SPLICE 26L, BS 333 COMMON. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM.
Part: STRINGER — CORRODED (BS 295-310) · airframe 30,574 hrs · 19,169 cycles
CORROSION FOUND ON STRINGER 26R BETWEEN BS 295, AND 310. REMOVED AND REPLACED THE STRINGER IAW SRM.
Part: STRINGER — CORRODED (BS 319.7-333) · airframe 30,574 hrs · 19,169 cycles
CORROSION FOUND ON STRINGER 27, BETWEEN BS 319.7 AND 333. REMOVED AND REPLACED THE STRINGER IAW SRM.
Part: STRINGER — CORRODED (BS 333-364) · airframe 30,574 hrs · 19,169 cycles
CORROSION FOUND ON STRINGER 26L BETWEEN BS 333 - 364. REMOVED AND REPLACED THE STRINGER IAW REO.
Part: ATTACH ANGLE — CORRODED (BS 349-364) · airframe 30,574 hrs · 19,169 cycles
CORROSION FOUND ON THE LT ATTACHMENT ANGLE COMMON TO STRINGER 26L, BETWEEN BS 349 - 364. REMOVED AND REPLACED THE ATTACHMENT ANGLE IAW SRM.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 30,574 hrs · 19,169 cycles
CORROSION FOUND ON THE LT INTERCOSTAL BETWEEN BS 349 - 364 AND, STRINGERS 27 - 26L. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.
Part: FRAME — CORRODED (BS 319) · airframe 30,574 hrs · 19,169 cycles
CORROSION FOUND ON FRAME AT BS 319 BETWEEN STRINGERS 26L AND 26R. REMOVED AND REPLACED THE FRAME SECTION IAW REO. LEAK CHECKED GOOD.
Part: FRAME — CORRODED (BS 310) · airframe 30,574 hrs · 19,169 cycles
CORROSION FOUND ON FRAME AT BS 310 BETWEEN STRINGERS 26L AND 26R. REMOVED AND REPLACED THE FRAME SECTION IAW REO, LEAK CHECKED GOOD.
Part: FRAME — CORRODED (BS 295) · airframe 30,574 hrs · 19,169 cycles
CORROSION ON THE FRAME AT BS 295, BETWEEN STRINGERS 26 AND 27R. REMOVED & REPLACED THE FRAME SECTION IAW REO. LEAK CHECKED GOOD.
Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 30,574 hrs · 19,169 cycles
AFT CARGO BAY DOOR SILL HAS AN AREA OF CORROSION. REMOVED AND INSTALLED A NEW AFT CARGO LOWER DOOR SILL IAW SRM.
Earlier reports · 2007–2016 · 103 reports
2016
Part: UNKNOWN — FAILED (MLG) · airframe 27,400 hrs · 17,127 cycles
RETURNED TO DEPARTURE, FOR GEAR DISAGREE MESSAGE. LEFT MAIN GEAR FAULT. REMOVED AND REPLACED THE PSEU AND GEAR HANDLE IAW AMM. R & R THE LANDING GEAR CONTROL PANEL IAW AMM. SWUNG SEVERAL TIMES, OPS CHECKED GOOD.
Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 27,104 hrs · 16,956 cycles
GEAR DISAGREE ON APPROACH WAS FORCED TO GO AROUND AFTER GEAR WAS SELECTED BACK UP RECEIVED GEAR DISAGREE, MADE 3 ATTEMPTS TO RETRACT GEAR, CREW REPORTED A GRINDING NOISE ON THE ATTEMPTS TO RETRACT GEAR. REMOVED AND REPLACED PSEU AND CYCLED GEAR MULTIPLE TIMES. OPS CHECK GOOD. PSEU AND LANDING GEAR EXTENSION/RETRACTION OPS CHECK GOOD IAW AMM.
2015
Part: FORMER — CORRODED (PAX DOOR) · airframe 25,013 hrs · 15,590 cycles
FOUND CORROSION ON THE FWD FORMER OF THE PAX DOOR. R & R THE FORMER IAW SRM. PRESSURE LEAK CHECKED GOOD.
Part: CHANNEL — CORRODED (PAX DOOR) · airframe 25,013 hrs · 15,590 cycles
LOWER CHANNEL ON PAX DOOR HAS CORROSION. R & R THE CHANNEL IAW SRM. PRESSURE LEAK CHECK GOOD.
Part: STRINGER — CORRODED (BS 333-349) · airframe 25,013 hrs · 15,590 cycles
STRINGER 25R BETWEEN BS 333 - 349 HAS CORROSION. R & R STRINGER IAW SRM. PRESSURE LEAK CHECK GOOD.
Part: STRINGER — CORRODED (BS 333-349) · airframe 25,013 hrs · 15,590 cycles
LONGERON COMMON TO STR 25L BETWEEN BS 333 - 349 HAS CORROSION. R & R STRINGER IAW SRM. CHECKED GOOD.
Part: FRAME — CORRODED (BS 295) · airframe 25,013 hrs · 15,590 cycles
FS 295, FRAME HAS CORROSION BETWEEN STR 26L AND STR 26R. REPAIRED FS 295.00 FRAME IAW REO. PRESSURE LEAK CHECK GOOD.
Part: STRINGER — CORRODED (BS 295-310) · airframe 25,013 hrs · 15,590 cycles
STRINGER 26L HAS CORROSION BETWEEN BS 295 - 310. R & R THE STRINGER IAW SRM AND STS EA. PRESSURE LEAK CHECK GOOD.
Part: SKIN — CORRODED (BS 294-310) · airframe 25,013 hrs · 15,590 cycles
CORRODED OUTER SKIN UNDER TCAS OMNI DIRECTIONAL ANTENNA, FS 310 TO FS 294 BETWEEN STR 26L AND STR 26R. REPAIRED BLENDED AREA IAW REO. PRESSURE LEAK CHECK GOOD.
Part: STRINGER — CORRODED (BS 295-310) · airframe 25,013 hrs · 15,590 cycles
STRINGER 24L HAS CORROSION BETWEEN BS 295 AND 310. R & R THE STRINGER IAW SRM. PRESSURE LEAK CHECK GOOD.
Part: FRAME — CORRODED (BS 333) · airframe 25,013 hrs · 15,590 cycles
FS 333 FRAME IS CORRODED ON AFT SIDE BETWEEN STR 26L AND STR 27. REPAIRED FS 333, FRAME BETWEEN STR 26L AND STR 27 IAW STS EA. PRESSURE LEAK CHECK GOOD.
Part: STRINGER — DAMAGED (BS 1162) · airframe 24,653 hrs · 15,355 cycles
COMPLY WITH MAJOR REPAIR OF STR 7L, JUST FORWARD OF FS 1162. HAS WEAR DAMAGE FROM WATER LINE. COMPLIED WITH MAJOR REPAIR OF STR 7L JUST FORWARD OF FS 1162. HAD WEAR DAMAGE FROM WATER LINE.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 23,619 hrs · 14,664 cycles
CARGO FLOOR PANEL 282FRF HAS DAMAGE TO TOP PLY AND CORE. REPAIRED IAW REO.
Part: SKIN — DENTED · airframe 23,619 hrs · 14,664 cycles
DENT FOUND ON LT FUSELAGE AT THE UPPER FWD EDGE OF THE RVSM AREA, APPROXIMATELY 3.5 INCHES AFT OF THE LT TRU BAY DOOR AND 20 INCHES UP FROM THE BOTTOM OF THE LT TRU BAY DOOR. REPAIRED IAW SRM.
Part: SKIN — DAMAGED (RT WING) · airframe 23,574 hrs · 14,631 cycles
LIGHTNING STRIKE DAMAGE NOTED ON NOSE AND RT WING NEAR AILERON. REPAIRED IAW REO AND SRM.
2014
Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 21,942 hrs · 13,482 cycles
NR 3 AND NR 4 EMERGENCY LIGHT BATTERIES WON'T HOLD CHARGE. R & R NR 3 AND NR 4 EMERGENCY LIGHT BATTERY IAW AMM. OPS CHECK GOOD AT THIS TIME.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,782 hrs · 13,345 cycles
EMERGENCY EXIT SIGN AT ROW 5 INOPERATIVE. CHANGED THE BATTERY PACK.
Part: FITTING — CRACKED (SERVICE DOOR) · airframe 21,644 hrs · 13,249 cycles
GALLEY SERVICE DOOR PX36 SENSOR SLIDE FITTING, PN 601R38959-3, HAS 1 CRACK ON THE LOWER LUG AND A PORTION OF MATERIAL MISSING ON THE UPPER LUG. COMPLIED WITH TEMPORARY REPAIR IAW REO 690-53-22-017. PERMANENT REPAIR DUE IN 100 FLIGHT HOURS DUE BY TAT 21737.4. DO NOT CLOSE UNTIL PERMANENT REPAIR. R & R THE GALLEY SERVICE DOOR PX36 SENSOR AND SENSOR SLIDER FITTING IAW AMM 52-70-06. PERFORMED OPS CHECK OF GALLEY SERVICE DOOR PX36 SENSOR IAW AMM 52-41-00 OPERATES NORMALLY AT THIS TIME DMI CLEARED.
Part: BATTERY PACK — INOPERATIVE (AFT FLASHLIGHT) · airframe 21,404 hrs · 13,094 cycles
AFT F/A FLASHLIGHT INOPERATIVE. R & R AFT F/A FLASHLIGHT BATTERY IAW AMM. OPS CHECKED GOOD.
Part: BUSHING — DAMAGED (PAX DOOR) · airframe 21,291 hrs · 13,032 cycles
F/A REPORTS MAIN CABIN DOOR VERY DIFFICULT TO OPEN. R & R PAX DOOR FWD ANCHOR SWIVEL LEVER ASSY BUSHINGS AND AFT ANCHOR SWIVEL LEVER ASSY.
Part: SEAL — DIRTY (PAX DOOR) · airframe 21,291 hrs · 13,032 cycles
MAIN CABIN DOOR HANDLE GETS JAMMED. CLEANED PAX DOOR SEAL. OPS CHECKED GOOD IAW AMM.
Part: SKIN — DENTED (PAX DOOR) · airframe 21,247 hrs · 13,010 cycles
FOUND A DENT AND CREASE ON PAX DOOR AFT SIDE PANEL INSIDE OF TOP STAIR TREAD. REPAIRED AFT SIDE PANEL ON PAX DOOR IAW REO.
Part: WARNING LIGHT — FALSE INDICATION (SLATS) · airframe 21,159 hrs · 12,957 cycles
SLATS FAILED CAUTION MESSAGE DURING DESCENT. PERFORMED A GO AROUND. MAINTENANCE CLEARED THE INHIBITS, OPS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,833 hrs · 12,735 cycles
CABIN NR 2 CEILING EMERGENCY LIGHT INOPERATIVE. R & R THE NR 2 CABIN CEILING EMERGENCY LIGHT IAW AMM.
Part: ENGINE — FAILED (LEFT) · airframe 20,760 hrs · 12,687 cycles
LEFT ENGINE OVERTEMP, CREW PULLED POWER BACK, THEN PUSHED UP. ENGINE OVERTEMPED AGAIN THEN FLAMED OUT. FOUND LT ENGINE COMPRESSOR DAMAGE, STAGE 4 AFT. REPLACED LEFT ENGINE OIL PRESSURE TRANSMITTER AND LT ENGINE.
Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 20,516 hrs · 12,541 cycles
FLAPS FAIL CAUTION MESSAGE. R & R NR 1 SFECU.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,208 hrs · 12,296 cycles
EMERGENCY OVERHEAD LIGHT AT ROW 17 IS BURNED OUT. FLT 4572 RELAMPED.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 20,093 hrs · 12,207 cycles
CORROSION FOUND ON STRINGER 27 BETWEEN FS 333.00 & FS 349.00 & BETWEEN STRINGER 26LT & STRINGER 26RT. C-CHECK REPLACED CORRODED STRINGER 27 BETWEEN FS 333.00 & FS 349.00 & BETWEEN STRINGER 26LT & 26RT IAW SRM.
Part: LINE — CHAFED (THRUST REVERSER) · airframe 20,093 hrs · 12,207 cycles
RT LOWER THRUST REVERSER DEPLOY LINE IS CHAFING ON AN INTERCOSTAL. C-CHECK REPAIRED IAW REO.
Part: AXLE — CORRODED (LT MLG) · airframe 20,093 hrs · 12,207 cycles
CORROSION FOUND ON LT NR 2 MLG AXLE ROOT RADIUS. C-CHECK REPAIRED LT NR 2 MLG AXLE CORROSION IAW REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,093 hrs · 12,207 cycles
PERFORM REPAIR ON RT FLOOR SEAT RAIL RBL 9.0 AT FS 355. C-CHECK REPAIRED SEAT TRACK AT FS 355 RBL 9.0 IAW REO.
Part: BEAM — CRACKED (FUSELAGE) · airframe 20,093 hrs · 12,207 cycles
RT FS 280.00 BEAM FOUND CRACKED AT RBL 12.5. C-CHECK REPLACED RT FS 280.00 BEAM IAW REO.
Part: SILL — CORRODED (FUSELAGE) · airframe 20,093 hrs · 12,207 cycles
RT FLOOR SILL JUST AFT OF SERVICE DOOR IS CORRODED. C-CHECK REPLACED DAMAGED RT FLOOR SILL IAW STS EA.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,093 hrs · 12,207 cycles
RT SIDE SEAT RAIL HAS CORROSION AT APPROXIMATELY FS 716, STRINGER 15R. C-CHECK REMOVED CORROSION RT SIDE SEAT TRACK AT APPROXIMATELY FS 716, STRINGER 15R IAW REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,093 hrs · 12,207 cycles
RT SIDE SEAT RAIL HAS CORROSION AT APPROXIMATELY FS 785.15, STRINGER 15R. C-CHECK REMOVED CORROSION ON RT SIDE SEAT RAIL AT APPROXIMATELY FS 785.15, STRINGER 15R IAW REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,093 hrs · 12,207 cycles
RT SIDE SEAT RAIL HAS CORROSION AT APPROXIMATELY FS 752.50 STRINGER 15R. C-CHECK REMOVED CORROSION ON RT SIDE SEAT RAIL AT APPROXIMATELY FS 752.50 IAW REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,093 hrs · 12,207 cycles
RT SIDE SEAT RAIL HAS CORROSION AT APPROXIMATELY FS 813.70, STRINGER 15R. C-CHECK REMOVED CORROSION RT SIDE SEAT RAIL AT APPROXIMATELY FS813.70, STRINGER 15R IAW REO.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 20,107 hrs · 12,215 cycles
CORROSION FOUND ON STRINGER 27 BETWEEN FS 319.70 & FS 310.00. C-CHECK REPAIRED IAW REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,107 hrs · 12,215 cycles
LT SIDE SEAT RAIL HAS CORROSION AT APPROXIMATELY FS 745, STRINGER 5L. C-CHECK REMOVED CORROSION ON LT SIDE SEAT RAIL AT FS 745 STRINGER 15L IAW REO C.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,107 hrs · 12,215 cycles
LT SIDE SEAT RAIL HAS CORROSION IN NUMEROUS LOCATIONS BETWEEN FS 785.15 TO FS 813.70, STRINGER 15L. C-CHECK REMOVED CORROSION ON LT SIDE SEAT RAIL AT FS 785.15 TO FS 813.70, STRINGER 15L IAW REO.
Part: SILL — CORRODED (FUSELAGE) · airframe 20,107 hrs · 12,215 cycles
AFT CARGO COMPARTMENT DOOR LOWER SILL HAS CORROSION AROUND NUTPLATES. C-CHECK CORROSION WAS BLENDED OUT IAW REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,107 hrs · 12,215 cycles
LT SIDE SEAT RAIL HAS CORROSION AT APPROXIMATELY FS 701, STRINGER 5L. C-CHECK REPLACED LT SIDE SEAT RAIL AT FS 677 - FS720, FS 701.00, STRINGER 15L IAW SRM & REO.
Part: SKIN — CHAFED (LT AILERON) · airframe 20,107 hrs · 12,215 cycles
LT AILERON CHAFING UPPER SIDE. C-CHECK REPAIRED IAW REO.
Part: FRAME — CORRODED (FUSELAGE) · airframe 20,107 hrs · 12,215 cycles
CORROSION FOUND ON FRAME BELOW FLOOR BOARD OF AVIONICS BAY BETWEEN STRINGER 26 RT & STRINGER 26 LT AT FS 319.70. C-CHECK R & R FRAME SPLICE AT FS 319.7 AT STRINGER 23RT IAW REO.
Part: FRAME — CORRODED (FUSELAGE) · airframe 20,107 hrs · 12,215 cycles
AVIONICS BAY FRAME BELOW FLOOR BOARD HAS CORROSION BETWEEN STRINGER 26LT & STRINGER 26RT AT FS 310.00. C-CHECK R & R FRAME SECTION AT FS 310.00 IAW REO.
Part: PAN — CRACKED (FUSELAGE) · airframe 20,107 hrs · 12,215 cycles
FLOOR PAN HAS CRACK ON RT SIDE JUST FWD OF 202 BULKHEAD & NEXT TO ADG HAND PUMP. C-CHECK CUT DAMAGE OUT & INSTALLED REPAIR ON RT SIDE OF FLOOR PAN FWD OF 202 BULKHEAD NEXT TO ADG HAND PUMP IAW REO.
2013
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,205 hrs · 11,651 cycles
OVERHEAD LIGHT AT ROW 14 IS BURNED OUT. FLT#4691 RELAMPED.
Part: ACM — FAILED (AC BAY) · airframe 19,107 hrs · 11,589 cycles
LT PACK BLOWING PARTICLES & OR SMOKE. FLT#4098 REPLACED LT PACK ACM. PN GG670-95009-5, SN ON 00850 & SN OFF 00617.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,958 hrs · 11,481 cycles
ONE OVERHEAD EMERGENCY FLOOD LIGHT IS BURNED OUT AT ROW 14. FLT#4742 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,031 hrs · 10,905 cycles
EMERGENCY OVERHEAD LIGHT AT ROW 17 IS BURNED OUT. (FLT 4534) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,670 hrs · 10,671 cycles
NR 4 OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 4747) RELAMPED EMERGENCY LIGHT.
Part: TORQUE SHAFT — CRACKED (RT ENGINE) · airframe 17,565 hrs · 10,605 cycles
UPON STOWING THRUST REVERSER RT ENGINE FLAMEOUT MESSAGE ILLUMINATED AND ITT SPIKED. AFTER CLEARING AND ITT RETURNED TO NORMAL. RT ENGINE REMAINED FLAMED-OUT. (FLT 4605) REPLACED THE RT ENGINE I/B AND O/B VG TORQUE SHAFTS IAW AMM.
2012
Part: LENS — CRACKED (EXTERIOR) · airframe 16,764 hrs · 10,050 cycles
EXTERIOR EMERGENCY LIGHT LENS ABOVE RIGHT WING CRACKED. (FLT 4608) REPLACED LEFT WING AFT EMERGENCY LIGHT LENS.
Part: STRIP — DETACHED (CABIN) · airframe 16,484 hrs · 9,863 cycles
A PIECE OF THE REFLECTIVE FLOOR TRIM CAME OFF IN THE GALLEY. (FLT 4698) RE-INSTALLED FORWARD FLOOR TRACK LIGHT STRIP.
Part: ROLLER — DIRTY (CABIN DOOR) · airframe 16,442 hrs · 9,835 cycles
MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 4515) FOUND THE ROLLER SPRING ON THE INNER HANDLE STICKING. CLEANED THE ROLLER AND TRACK ALONG WITH THE SPRING.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,328 hrs · 9,759 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4701) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,235 hrs · 9,686 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4799) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,693 hrs · 9,305 cycles
SECOND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4784) RELAMPED EMERGENCY LIGHT.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 15,611 hrs · 9,244 cycles
(C-CHECK) COCKPIT FLOORBEAM AT LBL 13 AND FS 274.5 HAS A CRACK ON THE BOTTOM SIDE OF BEAM. REPAIRED COCKPIT FLOORBEAM AT LBL 13 AND FS 274.5.
Part: STRUCTURE — DENTED (FUSELAGE) · airframe 15,611 hrs · 9,244 cycles
(C-CHECK) DENT AND SCRATCH DAMAGE AT FS 453.00 AND FS 469.00 AND BETWEEN STRINGERS 20 AND 21 RIGHT SIDE. REPAIRED IAW REO.
Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 15,611 hrs · 9,244 cycles
(C-CHECK) FS 280 CROSSBEAM IS CRACKED AND CORRODED. REPAIRED FS 280 CROSSBEAM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,499 hrs · 9,159 cycles
NR 1 AND NR 7 EMERGENCY LIGHTS ARE OUT. (FLT 4817) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 15,366 hrs · 9,054 cycles
LEFT FORWARD OVERWING EMERGENCY EXIT SIGN LIGHTS ARE OUT. (FLT 4464) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,296 hrs · 8,997 cycles
LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4535) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,256 hrs · 8,968 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,238 hrs · 8,958 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 14 IS OUT. (FLT 4542) RELAMPED EMERGENCY LIGHT.
Part: STRUCTURE — CRACKED (RT WING) · airframe 15,224 hrs · 8,950 cycles
THERE IS A 4 INCH CRACK IN THE RIGHT WING FIXED LEADING EDGE, JUST UNDERNEATH THE OUTBOARD END OF THE NR 1 SLAT. (SERVICE) REPAIRED RIGHT FIXED LEADING EDGE PER REO.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,901 hrs · 8,736 cycles
NR 6 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4585) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,822 hrs · 8,675 cycles
NR 7 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4497) RELAMPED EMERGENCY LIGHT.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,636 hrs · 8,562 cycles
NR 1 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,616 hrs · 8,552 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 17 IS OUT. (FLT 4675) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,469 hrs · 8,456 cycles
THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4580) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,017 hrs · 8,150 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 17 IS OUT. (FLT 4710) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,917 hrs · 8,086 cycles
THE 2ND TO AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4526) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,775 hrs · 7,988 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4616) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,392 hrs · 7,759 cycles
SECOND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4817) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,303 hrs · 7,680 cycles
NR 6 OVERHEAD EMERGENCY LIGHT DOES NOT ILLUMINATE. (FLT 4506) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,175 hrs · 7,596 cycles
OVERHEAD EMERGENCY LIGHT ABOVE ROW 18 IS OUT. (FLT 4777) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,612 hrs · 7,258 cycles
SECOND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4494) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,344 hrs · 7,082 cycles
SECOND TO LAST AFT OVERHEAD EMERGENCY LIGHT IS NOT WORKING. (FLT 4557)RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,252 hrs · 7,029 cycles
FAR AFT EMERGENCY LIGHT STRIP IS OUT. (FLT 4455) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,985 hrs · 6,864 cycles
CEILING EMERGENCY LIGHT FURTHEST AFT INOPERATIVE. (FLT 4766) RELAMPED EMERGENCY LIGHT.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,364 hrs · 6,466 cycles
EMERGENCY LIGHT OUT AT REAR OF CABIN. (FLT 4785) RELAMPED EMERGENCY LIGHT.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,314 hrs · 6,437 cycles
FS 280 FLOORBEAM CORRODED ON RIGHT SIDE. (C-CHECK) REPLACED FS 280 FLOORBEAM PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,124 hrs · 6,313 cycles
FURTHEST AFT CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6655) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,713 hrs · 5,459 cycles
EXIT ROW 12 EMERGENCY LIGHTING ON LEFT SIDE INOP. (FLT 4771) RELAMPED EMERGENCY LIGHT.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,932 hrs · 5,056 cycles
EMERGENCY OVERHEAD LIGHT INOP. (FLT 4519) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,581 hrs · 4,852 cycles
NR 7 EMERGENCY LIGHT INOP. (FLT 4801)RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,402 hrs · 4,760 cycles
SECOND FROM AFT EMERGENCY LIGHT INOP. (FLT 4466) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,295 hrs · 4,702 cycles
REAR OVERHEAD EMERGENCY LIGHT INOP. (FLT 4466) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,795 hrs · 4,442 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 14 INOP. (FLT 4745) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,614 hrs · 4,342 cycles
NR 7 OVERHEAD EMERGENCY EXIT LIGHT INOP. (FLT 4821) RELAMPED EMERGENCY EXIT LIGHT.
Part: MOUNT — CORRODED (RT ENGINE) · airframe 7,129 hrs · 4,056 cycles
RIGHT ENGINE FORWARD MOUNT CORRODED. ENG CHANGE, REPLACED MOUNT.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 6,934 hrs · 3,947 cycles
FLT 4603 - REAR EMERGENCY CEILING LIGHT INOP. RELAMPED.
Part: FLOORBEAM — CORRODED (280) · airframe 7,402 hrs · 4,220 cycles
C-CHECK, FS 280 BEAM CORRODED. REPAIRED PER REO.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 7,402 hrs · 4,220 cycles
C-CHECK, FS 280 BEAM CRACKED AND CORRODED. REPAIRED PER REO.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,345 hrs · 3,569 cycles
FLT 4703 - EMERGENCY LIGHT, THIRD FROM AFT, INOP. RELAMPED.
2008
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 5,556 hrs · 3,153 cycles
FLT 3784 - CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED.
Part: SELECTOR — MALFUNCTIONED (LANDING GEAR) · airframe 4,001 hrs · 2,283 cycles
FLT 3945 - RECEIVED A "GEAR DISAGREE" WARNING MESSAGE. REPLACED VALVE SELECTOR ASSEMBLY WITH SERVICEABLE VALVE SELECTOR ASSEMBLY. OPS AND LEAK CHECK GOOD, PN 53340-7 SN OFF NGL/1394/04.
Part: PUMP — LEAKING (HYD SYSTEM) · airframe 3,778 hrs · 2,159 cycles
FLT 3785 - NR 2 EDP HYD CAUTION MESSAGE IN FLIGHT. QUANTITY AND PRESSURE AT ZERO. REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-11-01. OPS AND LEAK CHECK GOOD, P/N: 66190-05, S/N OFF: K0608.
Part: PUMP — LEAKING (HYD SYSTEM) · airframe 3,728 hrs · 2,134 cycles
THE HYDRAULIC SYSTEM 1 QUANTITY READ "0", FLIGHT NR 4089. REPLACED NR 1 ENGINE DRIVEN PUMP AND INSPECTED NR 1 HYDRAULIC SYSTEM PRESSURE MANIFOLD DELTA P INDICATORS IAW MM 29-11-01. OPS AND LEAK CHECK OK.
2007
Part: UNKNOWN — ODOR (CABIN) · airframe 1,771 hrs · 1,020 cycles
CREW REPORTS STRONG FUEL ODOR FROM FORWARD LAV. PERFORMED FLUSHING PROCEDURES IAW MONOGRAM CMM 38-35-04. SNIFFER INDICATIONS ARE WITHIN LIMITS.
Part: PUMP — LEAKING (HYD SYSTEM) · airframe 1,557 hrs · 895 cycles
ON LANDING RECEIVED AN EDP 1 CAUTION MSG. FOUND LEAK IN THRUST REVERSER ACTUATION SYSTEM. REPLACED LEFT ENGINE EDP IAW 29-11-01. ALSO, REPLACED INBOARD PRESSURE LINE. OPS AND LEAK CHECK GOOD. OPS CHECK GOOD ON THRUST REVERSER, P/N AE711152-04.