N818SY
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.
101 reports on file, 2013-05-13 – 2017-12-18.
Part: SKIN — DENTED (NR 12 SPOILER) · airframe 35,794 hrs · 14,632 cycles
RIGHT OUTBOARD GROUND SPOILER HAS A DEEP DENT. REPLACED THE NR 12 SPOILER.
Part: PANEL — DAMAGED (LEFT) · airframe 35,794 hrs · 14,632 cycles
LEFT INBOARD TRAILING EDGE PANEL HAS A HOLE RIGHT ABOVE LEFT MAIN LANDING GEAR STRUT DOOR. REPAIRED THE TRAILING EDGE PANEL.
Part: ACCESS PANEL — DAMAGED (WING) · airframe 35,794 hrs · 14,632 cycles
CENTER AREA OF ACCESS PANEL NR 193AR HAS DAMAGED HONEYCOMB CORE. REMOVED & REPAIRED THE DAMAGE & PAINTED.
Part: TRACK — WORN (RT WING TE FLAP) · airframe 35,794 hrs · 14,632 cycles
ROLLER GUIDE TRACK OF RIGHT INBOARD TRAILING EDGE FLAP IS CONSIDERABLY WORN, PLEASE CHECK AND VERIFY. EVALUATED, FOUND OUT OF LIMITS. REMOVED DRILLED AND INSTALLED REPLACEMENT.
Part: SKIN — DENTED (NR 12 SPOILER) · airframe 35,794 hrs · 14,632 cycles
DENT ON THE NR 12 SPOILER PANEL APPROXIMATELY 5 INCHES AFT OF OTBD HINGE OF L3 FOOR REMOVED, REPLACED, AND OPS CHECKED.
Part: CONTROL CABLE — CORRODED (LEFT AILERONS) · airframe 35,794 hrs · 14,632 cycles
LEFT MLG WW LT AILERON CABLES HAS RUST COLORING INSIDE OF DUEL SET OF PULLIES. REMOVED & REPLACED & OPS CHECKED THE LT AILERON CONTROL CABLES.
Part: FRAME — DENTED (BS 500F) · airframe 35,794 hrs · 14,632 cycles
FWD CARGO BAY FRAME BS 500F FREE FLANGE IS DENTED BETWEEN STRINGERS 24 - 25L. REMOVED THE DENTED AREA FROM FRAME & REPAIRED.
Part: CONTROL CABLE — CORRODED (RT AILERONS) · airframe 35,794 hrs · 14,632 cycles
RT MLG WW RT AILERON CABLES CORRODED. REMOVED, REPLACED & OP CHECKED.
Part: SKIN — DAMAGED (PAX DOOR) · airframe 35,794 hrs · 14,632 cycles
FWD ENTRY DOOR EXTERNAL SKIN DAMAGED BELOW LOWER HINGE ARM. CUT AND REMOVED DAMAGE BELOW LOWER HINGE ARM ON FWD ENTRY DOOR EXTERNAL SKIN. PRIMED, & PAINTED AREA.
Part: PANEL — DAMAGED (RT WING) · airframe 35,794 hrs · 14,632 cycles
RIGHT WING TRAILING EDGE PANEL 651GB SUPPORT ROD ATTACH POINT WORN. REMOVED, RECEIVED VERIFIED PN#. LOCATED. DRILLED. INSTALLED.
Part: RIB — CRACKED (RT WING) · airframe 35,794 hrs · 14,632 cycles
RIGHT WING TRAILING EDGE, 12 INCHES INBD OF DEFLECTOR RIB ANGLE CRACKED ON FWD SIDE OF SEAL BRACKET. REMOVED AND REPLACED THE RIB ANGLE.
Part: STRUCTURE — DAMAGED (LT WING TE FLAP) · airframe 35,794 hrs · 14,632 cycles
LEFT WING, OUTBOARD TRAILING EDGE FLAP, OUTBOARD TRAILING EDGE TIP HAS A DAMAGED AREA. REPAIRED THE FLAP TIP.
Part: BLOCKER DOOR — DAMAGED (THRUST REVERSER) · airframe 35,794 hrs · 14,632 cycles
NR 2 ENGINE OTBD THRUST REVERSER NR 5 BLOCKER DOOR HAS DAMAGE AT THE DRAG LINK ATTACH CUTOUT. REMOVED AND REPLACED THE THRUST REVERSER BLOCKER DOOR. CHECKED GOOD.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 35,534 hrs · 14,521 cycles
EMERGENCY LIGHT LENS UNDER OVERHEAD BIN AT SEAT ROW 15 ABC. FOUND MISSING. REPLACED THE LENS. OK FOR SERVICE.
Part: ANGLE — CORRODED (BS 500H-500I) · airframe 34,823 hrs · 14,250 cycles
FWD CARGO BAY RT SIDE ZEE ANGLE BETWEEN BS 500H AND 500I, HAS MULTIPLE AREAS OF CORROSION. THE ANGLE WAS REPAIRED.
Part: BULKHEAD — CRACKED (BS 540) · airframe 34,823 hrs · 14,250 cycles
BS 540 BULKHEAD WEB, HFEC FOUND A CRACK INDICATION IN AFT ROW, SECOND HOLE BELOW STRINGER 22R. REPAIRED THE BULKHEAD WEB.
Part: FLOORBEAM — CORRODED (BS 987) · airframe 34,823 hrs · 14,250 cycles
FLOORBEAM CORRODED, BS 987, LBL 45. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOORBEAM SURFACE FROM LBL 54 - LBL 9.5.
Part: ANGLE — WORN (LT WING TE FLAP) · airframe 34,823 hrs · 14,250 cycles
LEFT INBD AFT FLAP PROGRAMMING ANGLE HAS SIGNS OF WEAR. REMOVED AND REPLACED THE ANGLE.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
FWD WET AREA FLOORBOARD 141A5810-449 HAS CORRODED INSERTS. REPLACED THE INSERTS.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
FWD WET AREA FLOORBOARD 141A5810-266 HAS A CORRODED INSERT. REPLACED THE INSERTS.
Part: ANGLE — CORRODED (NOT REPORTED) · airframe 34,823 hrs · 14,250 cycles
AFT CARGO BAY RT FWD ZEE ANGLE HAS SEVERAL AREAS OF CORROSION . REPLACED THE ANGLE.
Part: ANGLE — CORRODED (BS 767-787) · airframe 34,823 hrs · 14,250 cycles
AFT CARGO BAY RT ZEE ANGLE, BS 767 - 787, HAD CORROSION AT EVERY FASTENER HOLE, LOWER SURFACE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED THE ANGLE
Part: FITTING — CORRODED (GIRT BAR) · airframe 34,823 hrs · 14,250 cycles
L1 DOOR AFT GIRT BAR TIE DOWN FITTING CORRODED. REMOVED THE GIRT BAR TIE DOWN.
Part: FLOOR SUPPORT — CORRODED (BS 312-328) · airframe 34,823 hrs · 14,250 cycles
FLOOR SUPPORT CORRODED BETWEEN BS 312 - 328, RBL 11. REMOVED AND REPLACED THE FLOOR SUPPORT.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
FWD WET AREA FLOORBOARD 141A5810-56 HAS CORRODED INSERTS. REPLACED THE INSERTS.
Part: ANGLE — CORRODED (BS 847-867) · airframe 34,823 hrs · 14,250 cycles
AFT CARGO BAY, RT ZEE ANGLE, BS 847 - 867 CORRODED AT FASTENER HOLES, UPPER SURFACE. REPLACED THE ANGLE.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
FWD WET AREA FLOORBOARD 141A5810-121 HAS CORRODED INSERTS. REPLACED THE INSERTS.
Part: FLOORBEAM — CORRODED (BS 344) · airframe 34,823 hrs · 14,250 cycles
FLOORBEAM CORRODED, BS 344, BL 0. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOORBEAM UPPER FLANGE.
Part: ANGLE — CRACKED (BS 767) · airframe 34,823 hrs · 14,250 cycles
AFT CARGO BAY LT ZEE ANGLE, BS 767+7 INCHES, CRACK FOUND VISUALLY IN RADIUS OF CUTOUT. REPLACED THE ANGLE.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
AFT WET AREA FLOORBOARD 147A5810143 HAS CORRODED INSERTS. REPLACED THE INSERTS.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
FWD WET AREA FLOORBOARD 141A5810-31 HAS CORRODED INSERTS. REPLACED THE INSERTS.
Part: TIE DOWN — CORRODED (AFT CARGO NET) · airframe 34,823 hrs · 14,250 cycles
AFT CARGO BAY AFT NET TIE DOWN, HAS CORROSION AROUND FASTENER HOLES. FOUND TO BE OUT OF LIMITS. REPLACED TIE DOWN PLATE.
Part: CREASE BEAM — CORRODED (BS 967-987) · airframe 34,823 hrs · 14,250 cycles
R2 DOOR CREASE BEAM CORRODED, BETWEEN BS 967 - 987. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE CREASE BEAM.
Part: FLOORBEAM — CORRODED (BS 947) · airframe 34,823 hrs · 14,250 cycles
FLOORBEAM CORRODED AT BS 947, RBL 10. REMOVED CORROSION ON THE FLOORBEAM UPPER SURFACE AND FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOORBEAM.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
FWD WET AREA FLOORBOARD 141A5810-159 HAS CORRODED AND MISSING INSERTS. REPLACED THE INSERTS.
Part: FLOOR SUPPORT — CORRODED (BS 312-328) · airframe 34,823 hrs · 14,250 cycles
FLOOR SUPPORT CORRODED, BETWEEN BS 312 - 328, LBL 12. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT.
Part: ANGLE — CORRODED (BS 500G-500H) · airframe 34,823 hrs · 14,250 cycles
FWD CARGO BAY RT SIDE ZEE ANGLE BETWEEN BS 500G AND 500H, HAS MULTIPLE AREAS OF CORROSION. CUT OUT DAMAGED SECTION OF THE ANGLE AND INSTALLED A SPLICE AND NEW SECTION OF ANGLE.
Part: STRAP — CORRODED (BS 787-847) · airframe 34,823 hrs · 14,250 cycles
AFT CARGO BAY DOOR THRESHOLD STRAP CORRODED AT FASTENER HOLES BETWEEN BS 787 - 847, UPPER SURFACE. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED & REPLACED THE STRAP.
Part: SCUFF PLATE — CRACKED (CARGO DOOR) · airframe 34,823 hrs · 14,250 cycles
SCUFF PLATE HAS A CRACK. REPAIRED THE SCUFF PLATE.
Part: FLOORBEAM — CORRODED (BS 987) · airframe 34,823 hrs · 14,250 cycles
FLOORBEAM CORRODED AT BS 987, RBL 30 ON THE UNDERSIDE OF FLOORBOARD HOLE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED AREA.
Part: ANGLE — CRACKED (BS 500H) · airframe 34,823 hrs · 14,250 cycles
FWD CARGO BAY LT SIDE ZEE ANGLE BAFFLE ANGLE FWD OF BS 500H IS CRACKED. REMOVED AND REPLACED THE BAFFLE ANGLE.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
FWD WET AREA FLOORBOARD 141A5810-189 HAS CORRODED INSERTS. REPLACED CORRODED INSERTS.
Part: FLOORBEAM — CORRODED (BS 328) · airframe 34,823 hrs · 14,250 cycles
CABIN FLOORBEAM CORRODED, BS 328, LBL 12. REMOVED THE CORROSION ON THE FLOORBEAM UPPER FLANGE AND FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOORBEAM.
Part: ANGLE — CORRODED (BS 727C-803) · airframe 34,823 hrs · 14,250 cycles
AFT CARGO BAY LT FWD ZEE ANGLE HAS SEVERAL AREAS OF CORROSION BS 727C-803. REPAIRED THE ANGLE.
Part: SUPPORT ANGLE — CORRODED (BS 500I) · airframe 34,823 hrs · 14,250 cycles
FWD CARGO BAY AFT SIDEWALL ATTACH ANGLE SUPPORT AT BS 500I BETWEEN STRINGERS 25R AND 26R HAS CORROSION. FOUND TO BE OUT OF LIMITS. THE SUPPORT ANGLE WAS REPLACED.
Part: ATTACH ANGLE — CRACKED (BS 500I) · airframe 34,823 hrs · 14,250 cycles
FWD CARGO SIDEWALL TO FRAME ATTACH ANGLE CRACKED AT BS 500I STRINGER 18R. REMOVED AND REPLACED THE ATTACH ANGLE.
Part: FLOORBEAM — CORRODED (BS 987) · airframe 34,823 hrs · 14,250 cycles
FLOORBEAM CORRODED AT BS 987, RBL 45. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOORBEAM FROM RBL 54 - LBL 9.5.
Part: ANGLE — CORRODED (BS 767) · airframe 34,823 hrs · 14,250 cycles
AFT CARGO BAY LT ZEE ANGLE, BS 767 +3 INCHES, HAD CORROSION NEAR FASTENER HOLE, UPPER SURFACE. REPAIRED THE ANGLE.
Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 34,823 hrs · 14,250 cycles
FLOOR SUPPORT CRACKED, BS 312-328, LBL 45. REMOVED AND REPLACED FLOOR SUPPORT.
Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 34,823 hrs · 14,250 cycles
FLOOR SUPPORT CRACKED BETWEEN BS 344 - 360, BL 0. REMOVED & REPLACED THE FLOOR SUPPORT.
Part: ANGLE — CRACKED (BS 727-767) · airframe 34,823 hrs · 14,250 cycles
AFT CARGO BAY LT ZEE ANGLE CRACKED AT THE TIE STRAP BS 727D, 727I + 6, AND 767 + 6. REPAIRED THE ANGLE.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
AFT WET AREA FLOORBOARD 147A5810-344 HAS CORRODED INSERTS. REPLACED THE INSERTS.
Part: ANGLE — CRACKED (BS 727D-727I) · airframe 34,823 hrs · 14,250 cycles
AFT CARGO BAY RT ZEE ANGLE CRACKED AT THE TIE STRAP AREA BS 727D AND 727I +6. REPLACED THE ANGLE.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
AFT WET AREA FLOORBOARD 147A5810-29 HAS A CORRODED INSERT. REPLACED THE INSERT.
Part: RETAINER — CRACKED (DEFLECTOR SEAL) · airframe 34,823 hrs · 14,250 cycles
LEFT WING OTBD DEFLECTOR RIB SEAL RETAINER IS CRACKED ON FWD SIDE. REMOVED AND REPLACED THE SEAL RETAINER.
Part: FLOORBEAM — CORRODED (BS 328) · airframe 34,823 hrs · 14,250 cycles
FLOORBEAM CORRODED, BS 328, RBL 11. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM UPPER FLANGE.
Part: INSERT — CORRODED (FLOORBOAR) · airframe 34,823 hrs · 14,250 cycles
AFT WET AREA FLOORBOARD HAS CORRODED FLOATING INSERTS. REPLACED THE INSERTS.
Part: INSERT — CORRODED (FLOORBEAM) · airframe 34,823 hrs · 14,250 cycles
AFT WET AREA FLOORBOARD 147A5810-304 HAS CORRODED INSERTS. REPLACED THE INSERTS.
Part: FLOOR SUPPORT — CRACKED (BS 380-400) · airframe 34,823 hrs · 14,250 cycles
FLOOR SUPPORT CRACKED, BS 380 - 400, BL 0. REMOVED & REPLACED THE FLOOR SUPPORT.
Part: FLOOR SUPPORT — CORRODED (BS 967-987) · airframe 34,823 hrs · 14,250 cycles
FLOOR SUPPORT CORRODED BETWEEN BS 967 - 987, RBL 16. BLENDED CORROSION AND FOUND 100% MAT. LOSS. LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT.
Part: SCUFF PLATE — CRACKED (CARGO DOOR) · airframe 34,823 hrs · 14,250 cycles
AFT CARGO DOOR FWD SCUFF PLATE CRACKED. REPAIRED THE SCUFF PLATE.
Part: PANEL — DAMAGED · airframe 34,823 hrs · 14,250 cycles
EXTERNAL FUSELAGE, KEEL BEAM PANEL 193D, IS CHAFED AND GROOVED ON THE UPPER SURFACE. REPAIRED AREA.
Part: SKIN — CRACKED (BS 540) · airframe 34,823 hrs · 14,250 cycles
RIGHT BS 540 BETWEEN STRINGERS 22R AND 23R, SECOND FASTENER HOLE DOWN AFT ROW CRACK INDICATION IN THE SKIN. REPAIRED THE SKIN.
Part: ANGLE — CORRODED (BS 500H) · airframe 34,823 hrs · 14,250 cycles
FWD CARGO BAY RT SIDE ZEE ANGLE BAFFLE FWD OF BS 500H IS CRACKED. REMOVED AND REPLACED THE ANGLE.
Part: FASTENER — LOOSE (NR 2 NACELLE) · airframe 34,823 hrs · 14,250 cycles
NR 2 NACELLE, LOWER PANEL 422AB HAS LOOSE AND SHANKED OUT FASTENERS. INSTALLED NEW FASTENERS.
Part: HINGE FITTING — CRACKED (LT MLG DOOR) · airframe 34,823 hrs · 14,250 cycles
LEFT MLG AFT DOOR HINGE FITTING FOR INNER HINGE DOOR, CRACK INDICATION IN FITTING IN RADIUS ABOVE OUTTER ATTACH HINGE FITTING ATTACH BOLT, IAW TASK CARD INSTRUCTIONS, ACCOMPLISH TASK CARD. REMOVED AND REPLACED THE LEFT MLG INBD GEAR DOOR HINGE FITTING.
Part: THRESHOLD — CORRODED (BS 787-847) · airframe 34,823 hrs · 14,250 cycles
AFT CARGO BAY, DOOR THRESHOLD WEB CORRODED AT FASTENER HOLES FROM BS 787 - 847, UPPER AND LOWER SURFACES. REMOVED CORRODED THRESHOLD WEB AND INSTALLED NEW THRESHOLD WEB.
Part: FAIRING — ERODED (LT FLAP TRACK) · airframe 34,823 hrs · 14,250 cycles
LEFT WING, NR 2 FLAP TRACK FWD FAIRING FASTENER HOLES ERODED. REPAIRED THE FLAP TRACK FAIRING.
Part: ATTACH ANGLE — CORRODED (BS 500I) · airframe 34,823 hrs · 14,250 cycles
FWD CARGO BAY AFT LT SIDEWALL ATTACH ANGLE AT BS 500I, BETWEEN STRINGERS 25L AND 26L CORRODED. FOUND TO BE 100% MATERIAL LOSS. REPAIRED ATTACH ANGLE.
Part: FLOOR SUPPORT — CORRODED (BS 328-344) · airframe 34,823 hrs · 14,250 cycles
FLOOR SUPPORT CORRODED, BS 328 - 344, LBL 12. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED THE FLOOR SUPPORT.
Part: FLOOR SUPPORT — CORRODED (BS 947-967) · airframe 34,823 hrs · 14,250 cycles
FLOOR SUPPORT BETWEEN BS 947 - 967, LBL 14 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED THE FLOOR SUPPORT.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
FWD WET AREA FLOORBOARD 141A5810-448 HAS CORRODED INSERTS. REPLACED THE INSERTS.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
AFT WET AREA FLOORBOARD HAS CORRODED INSERTS. REPLACED THE INSERTS.
Part: TIE DOWN — CORRODED (AFT CARGO BAY) · airframe 34,823 hrs · 14,250 cycles
AFT CARGO BAY FWD TIE DOWN PLATE HAS CORROSION ON LOWER SURFACE. FOUND TO BE OUT OF LIMITS. REPLACED THE TIE DOWN.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
AFT WET AREA FLOORBOARD 147A5810105 HAS CORRODED AND MISSING INSERTS. REPLACED THE INSERTS.
Part: INSERT — CORRODED (FLOORBOARD) · airframe 34,823 hrs · 14,250 cycles
FWD WET AREA FLOORBOARD 141A5810-122 HAS CORRODED INSERTS. REPLACED THE INSERTS.
Part: SHAFT — CRACKED (RUDDER) · airframe 34,823 hrs · 14,250 cycles
FORWARD NOSE AREA, FO'S SIDE, RUDDER JACK SHAFT, CROSS ROD, UPPER FLANGE CRACKED. REPLACED JACKSHAFT ASSEMBLY. ADJUSTMENT AND FUNCTIONAL TESTED GOOD.
Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 34,823 hrs · 14,250 cycles
FLOOR SUPPORT CRACKED, BS 312 - 328, RBL 30. REMOVED AND REPLACED THE FLOOR SUPPORT.
Earlier reports · 2013–2016 · 23 reports
2016
Part: LENS — MISSING (CABIN) · airframe 33,325 hrs · 13,766 cycles
THE PLASTIC EXIT SIGN LENS IS MISSING FROM THE AFT LAVATORY LEFT SIDE. INSTALLED EMER EXIT CAP LENS AT L-2 LAV ISLE POSITION.
Part: WIRE — LOOSE (CABIN) · airframe 32,866 hrs · 13,597 cycles
LEFT SIDE OVER WING EMERGENCY LIGHT IS INOPERATIVE. REPAIRED WIRING (LOOSE) AND SOCKET. REPLACED BULB AND OPERATIONALLY CHECKED OK AFTER REPAIRS. COVER NEEDS TO BE INSTALLED YET AND NEW SCREWS FOR THAT COVER WERE REQUISITIONED. INSTALLED NEW SCREWS IN EMERGENCY OVERWING LIGHT. OPS CHECK GOOD. OK FOR SERVICE.
Part: SMOKE GOGGLES — CRACKED (COCKPIT) · airframe 30,676 hrs · 12,771 cycles
JUMP SEAT SMOKE GOGGLES CRACKED, OBSERVER SEAT. PLACED OBESERVER SEAT ON MEL. REPLACED OBSERVERS SMOKE GOGGLES, THIS CLEARS MEL. MAINTENANCE NOTIFIED.
2015
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 29,649 hrs · 12,404 cycles
FLASHLIGHT UNDER FORWARD F/A SEAT, 1R, DOESN'T BLIINK. REPLACED BATTERY PACK, IAW MM 25-64-00.
Part: SKIN — NICKED (HORIZONTAL STAB) · airframe 28,339 hrs · 11,755 cycles
LEFT HORIZONTAL STABILIZER L/E HAS A NICK AT FS 89. REMOVED NICK AND FOUND TO BE OUT OF LIMITS. REPAIRED.
Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 28,339 hrs · 11,755 cycles
FOUND THREE DENTS ON L/E LT HORIZONTAL STABILIZER. REPAIRED DENTS.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 28,339 hrs · 11,755 cycles
RIGHT HORIZONTAL STABILIZER RIB AT STAB STA 101.9 IS CRACKED AT FWD EDGE. REPAIRED.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 28,339 hrs · 11,755 cycles
RT WTB FAIRING HEAT EXCHANGER BAY OTBD FRAME HAS A HOLE WORN THROUGH STOP PAN AND FRAME. REPAIRED RT WTB FAIRING HEAT EXCHANGER BAY OTBD FRAME LOWER CHORD.
Part: SEAT TRACK — CRACKED (BS 727B) · airframe 28,339 hrs · 11,755 cycles
SEAT TRACK HAS CRACK INDICATION AT OTBD AFT HOLE FS 727B AND RBL 45.5. REPAIRED SEAT TRACK.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 28,339 hrs · 11,755 cycles
LEFT HORIZONTAL LOWER SKIN CRACKED.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 28,339 hrs · 11,755 cycles
RIGHT HORIZONTAL STABILIZER RIB AT STABILIZER STA 120.3 IS CRACKED ON LWR END OF VERTICAL RIB STIFFENER. REPAIRED RT HORIZONTAL STAB RIB AT 120.3 LWR VERTICAL RIB STIFFENER.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 28,339 hrs · 11,755 cycles
LEFT HORIZONTAL STABILIZER RIB AT STAB STA 129.5 IS CRACKED AT FWD INBD EDGE. REPAIRED CRACK.
Part: SEAT TRACK — CRACKED (BS 727B) · airframe 28,339 hrs · 11,755 cycles
SEAT TRACK HAS CRACK INDICATION AT INBD FWD HOLE AT FS 727B AND RBL 24.75. REPAIRED CRACKED HOLE.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 28,339 hrs · 11,755 cycles
HORIZONTAL STABILIZER LWR SKIN CRACKED. R & R SKIN.
Part: SKIN — CHAFED (L1 DOOR) · airframe 28,339 hrs · 11,755 cycles
L1 DOOR AFT SIDE SKIN UPPER CORNER IS CHAFED AT UPPER STOP FITTING. BLENDED CHAFE L1 DOOR UPPER AFT CORNER FOUND TO BE OUT OF LIMITS. REMOVED CHAFE TO SMOOTH CONTOUR.
Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 28,399 hrs · 11,755 cycles
THREE DENTS IN L/E ON RT HORIZONTAL STABILIZER. REPAIRED DENTS.
Part: SEAT TRACK — CRACKED (BS 727B) · airframe 28,339 hrs · 11,755 cycles
SEAT TRACK HAS CRACK INDICATION AT INBD FWD HOLE FS 727B AND LBL 45.5. REPAIRED SEAT TRACK.
2014
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 26,753 hrs · 11,125 cycles
EMERGENCY EXIT LIGHT BATTERIES FAIL CAPACITY FUNCTION TEST ROW 14D-21D. REPLACED EMERGENCY BATTERY PACK M1671.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 26,753 hrs · 11,125 cycles
CEILING EMERGENCY EXIT BATTERY FAILS CAPACITY FUNCTION TEST AT 13A. REPLACED BATTERY PACK M1695.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 26,753 hrs · 11,125 cycles
EMERGENCY EXIT LIGHT BATTERIES FAIL CAPACITY FUNCTION TEST ROW 13A. REPLACED BATTERY PACK M1694.
Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 26,753 hrs · 11,125 cycles
COVER MISSING FROM AFT LAV WALL. INSTALLED AFT LAV EMERGENCY LIGHT COVER.
2013
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DURING FUNCTIONAL CHECK, FOUND RT SIDE ROW 14-21 ALONG WITH LT SIDE ROW 13-21, EMERGENCY LIGHTS FAILED CHECK. BATTERY PACKS REPLACED. OPS CHECKED GOOD.
Part: SIGN — MISSING (CABIN) · airframe 22,292 hrs · 9,333 cycles
SEAT 13A MISSING EXIT SIGN. REPLACED 13A EMERGENCY EXIT SIGN. OPS CHECK GOOD.