N218AG
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.
49 reports on file, 2011-10-28 – 2015-10-09.
Part: INTERCOSTAL — DAMAGED (BS 349-364) · airframe 31,476 hrs · 19,985 cycles
INTERCOSTAL BETWEEN BS 349 AND 364, LEFT OF STRINGER 27. R & R THE INTERCOSTAL IAW SRM.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 31,476 hrs · 19,985 cycles
R & R INTERCOSTAL BETWEEN BS 349 AND 364, LEFT OF STRINGER 27. R & R THE INTERCOSTAL IAW SRM.
Part: STRINGER — CORRODED (BS 333-349) · airframe 31,476 hrs · 19,985 cycles
STRINGER 23L, BS 333 AND 349 CORRODED. REPAIRED THE STRINGER IAW SRM.
Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 31,476 hrs · 19,985 cycles
SPLICE ANGLE ON STRINGER 23L AT BS 333 HAS CORROSION. R & R THE STRINGER SPLICE IAW SRM.
Part: FRAME — DAMAGED (BS 333) · airframe 31,476 hrs · 19,985 cycles
FRAME AT FS 333 FOUND TO BE DAMAGED BEYOND LIMITS. REPAIRED IAW REO.
Part: STRINGER — CORRODED (BS 333-349) · airframe 31,476 hrs · 19,985 cycles
STRINGER 25R BETWEEN BS 333 AND 349 CORRODED. R & R THE STRINGER IAW SRM.
Part: SKIN — DENTED (PAX DOOR) · airframe 31,476 hrs · 19,985 cycles
MAIN CABIN DOOR CANNING. REPAIRED IAW EA.
Part: STRINGER — DAMAGED (BS 333-349) · airframe 31,476 hrs · 19,985 cycles
STRINGER 26R BETWEEN BS 333 & 349 DAMAGED. R & R THE STRINGER IAW SRM.
Part: STRINGER — DAMAGED (BS 295-333) · airframe 31,476 hrs · 19,985 cycles
STRINGER 25R BETWEEN BS 295 & 333. R & R THE STRINGER IAW SRM.
Part: FRAME — CORRODED (BS 295) · airframe 31,476 hrs · 19,985 cycles
FORWARD AVIONICS BAY FRAME AT BS 295 CORRODED. REPAIRED FRAME SECTION AT FS 295.00 IAW REO.
Part: STRINGER — DAMAGED (BS 280-333) · airframe 31,476 hrs · 19,985 cycles
STRINGER 26R BETWEEN BS 280 & 333 DAMAGED. R & R THE STRINGER IAW SRM.
Part: ANGLE — DAMAGED (BS 333) · airframe 31,476 hrs · 19,985 cycles
R & R SPLICE ANGLE AT BS 333, STR 26R. R & R SPLICE ANGLE AT FS 333 STR 26R IAW SRM.
Part: ANGLE — DAMAGED (BS 333) · airframe 31,476 hrs · 19,985 cycles
R & R SPLICE ANGLE AT FS 333, STR 25R. R & R SPLICE ANGLE AT FS 333 FOR STR 25R IAW SRM.
Part: FLOOR SUPPORT — CRACKED (E/E BAY) · airframe 31,476 hrs · 19,985 cycles
LEFT FWD EQUIPMENT COMPARTMENT DOOR LANDING HAS A CRACK ON AFT SECTION. R & R L FWD EQUIPMENT COMPARTMENT DOOR LANDING, IAW SRM.
Part: STRUCTURE — CRACKED (E/E BAY) · airframe 31,476 hrs · 19,985 cycles
RIGHT FWD EQUIPMENT COMPARTMENT DOOR LANDING HAS A CRACK ON AFT SECTION. R & R RT FWD EQUIPMENT COMPARTMENT DOOR LANDING IAW SRM.
Earlier reports · 2011–2014 · 34 reports
2014
Part: LINKAGE — OUT OF ADJUST (SERVICE DOOR) · airframe 27,243 hrs · 17,742 cycles
SERVICE DOOR CAUTION IN FLIGHT. F/A REPORTED ALIGNMENT MARKINGS ARE NOT ALIGNED. RETURNED TO FIELD. ADJUSTED GALLEY SERVICE DOOR LINKAGE IAW AMM. ALIGNMENT MARKS ARE NOW ALIGNED AND SERVICE DOOR INDICATION NORMAL. OPS CHECK GOOD AT THIS TIME.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,213 hrs · 17,727 cycles
CEILING EMERGENCY EXIT LIGHT FWD SIDE INOPERATIVE AT OVERWING EXITS. C-CHECK, REPLACED THE LAMP.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,213 hrs · 17,727 cycles
RIGHT WING EMERGENCY EXIT DOOR LOWER EXIT LIGHT HAS BURNED OUT BULB. C-CHECK, REPLACED BULB.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,213 hrs · 17,727 cycles
EMERGENCY LIGHT INOPERATIVE IMMEDIATELY AFT OF LT OVERWING EXIT. C-CHECK, REMOVED/INSTALLED NEW EMERGENCY LIGHT BATTERIES NR 2 AND NR 3 IAW AMM.
Part: LIGHT — DELAMINATED (CABIN) · airframe 27,213 hrs · 17,727 cycles
DELAMINATED EMERGENCY PATH STRIP. INSTALLED EMERGENCY LIGHT.
Part: SEAT TRACK — CORRODED (BS 485-570) · airframe 27,213 hrs · 17,727 cycles
LEFT SEAT TRACK BS 485-570 CORRODED. C-CHECK, R & R SEAT TRACK IAW AMM.
Part: SEAT TRACK — CORRODED (BS 570-677) · airframe 27,213 hrs · 17,727 cycles
LEFT SEAT TRACK BS 570 - 677 CORRODED. C-CHECK, R & R SEAT TRACK IAW AMM.
Part: SEAT TRACK — CORRODED (BS 720-761) · airframe 27,213 hrs · 17,727 cycles
RIGHT SEAT TRACK BS 720-761.85 CORRODED. C-CHECK, REMOVED AND REPLACED THE SEAT TRACK IAW AMM AND SRM.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 27,213 hrs · 17,727 cycles
RIGHT SEAT TRACK BS 785.15-863 CORRODED. C-CHECK, R & R SEAT TRACK IAW AMM.
Part: SEAT TRACK — CORRODED (BS 397-485) · airframe 27,213 hrs · 17,727 cycles
RT SEAT TRACK BS 397-485 CORRODED. C-CHECK, REMOVED AND REPLACED THE SEAT TRACK IAW AND SRM.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 27,213 hrs · 17,727 cycles
RIGHT SEAT TRACK BS 485-581 CORRODED. C-CHECK, R & R SEAT TRACK IAW SRM.
Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 27,213 hrs · 17,727 cycles
CORROSION ON LT SEAT TRACK FROM BS 708-761.85. C-CHECK, REPAIRED LT SIDE SEAT TRACK IAW REO.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 27,213 hrs · 17,727 cycles
CORROSION INSIDE LT SEAT TRACK BETWEEN BS 785.15- 863. C-CHECK, REPAIRED SEAT TRACK IAW REO.
Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 27,213 hrs · 17,727 cycles
RT WING FLAP PANEL 684EB HAS CHAFE ON TOP SIDE OF PANEL. C-CHECK, INSTALLED NEW PANEL IAW SRM.
Part: SKIN — CRACKED (BS 193) · airframe 27,213 hrs · 17,727 cycles
CRACK AT FS 193, NEAR FRAME ON RT SIDE OF THE FORWARD EQUIPMENT COMPARTMENT. C-CHECK, CRACK REPAIRED IAW EA.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,213 hrs · 17,727 cycles
SERVICE DOOR SILL CORRODED AROUND FITTINGS. C-CHECK, R & R DOOR SILL IAW SRM.
Part: SKIN — CRACKED (BS 193) · airframe 27,213 hrs · 17,727 cycles
CRACK AT FS 193, NEAR FRAME ON LT SIDE OF THE FORWARD EQUIPMENT BAY. C-CHECK, REMOVED CRACK AND INSTALLED REINFORCEMENT DOUBLER IAW REO.
Part: SUPPORT ARM — CHAFED (CARGO DOOR) · airframe 27,213 hrs · 17,727 cycles
FWD CARGO BAY DOOR FWD INBD SUPPORT ARM CHAFED ON TOP SIDE OF ARM. C-CHECK, BLENDED CHAFED AREA ON TOP SIDE OF SUPPORT ARM IAW STS EA.
Part: SKIN — CHAFED (LT NACELLE) · airframe 27,213 hrs · 17,727 cycles
LT PYLON PANEL 433BB IS CHAFED. C-CHECK, REPLACED PANEL IAW AMM.
Part: SUPPORT — CHAFED (PAX DOOR) · airframe 27,213 hrs · 17,727 cycles
PAX DOOR SUPPORT WHEEL ARM CHAFED ON OTBD EDGE. C-CHECK, BLENDED CHAFE ON PAX DOOR SUPPORT WHEEL ARM OTBD EDGE IAW SRM AND STS EA.
Part: SLIDER — CHAFED (THRUST REVERSER) · airframe 27,213 hrs · 17,727 cycles
LT ENG UPPER TRANSCOWL THRUST REVERSER OTBD SLIDER CHAFED. C-CHECK, BLENDED CHAFE ON SLIDER IAW REO.
Part: LUG — CHAFED (RT WING AILERON) · airframe 27,213 hrs · 17,727 cycles
RT WING ALERON INBD LUG CHAFED. C-CHECK, REPAIRED CHAFE TO RT WING ALERON INBD LUG IAW REO.
Part: SLIDER — CHAFED (THRUST REVERSER) · airframe 27,213 hrs · 17,727 cycles
RT ENGINE LOWER TRANSCOWL THRUST REVERSER OTBD SLIDER CHAFED. C-CHECK, BLENDED CHAFE ON SLIDER IAW REO.
Part: SUPPORT ARM — CHAFED (CARGO DOOR) · airframe 27,213 hrs · 17,727 cycles
FWD CARGO BAY DOOR FWD INBD SUPPORT ARM CHAFED ON FWD FACE OF ARM. C-CHECK, BLENDED CHAFED IAW EA.
Part: LATCH — CHAFED (NACELLE DOOR) · airframe 27,213 hrs · 17,727 cycles
RT ENGINE LOWER TRANSCOWL, LATCHING DOOR RECEPTACLE CHAFED. C-CHECK, BLENDED CHAFE ON LATCHING DOOR RECEPTACLE IAW EA.
Part: SLIDER — CHAFED (THRUST REVERSER) · airframe 27,213 hrs · 17,727 cycles
RT ENGINE LOWER TRANSCOWL THRUST REVERSER INBD SLIDER CHAFED. C-CHECK, BLENDED CHAFE ON SLIDER IAW REO.
2013
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,120 hrs · 16,190 cycles
SECOND FROM AFT OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT#3465 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,724 hrs · 15,986 cycles
AFT EMERGENCY OVERHEAD LIGHT IS BURNED OUT, RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,290 hrs · 15,768 cycles
EMERGENCY OVERHEAD LIGHT AT ROW 4 IS BURNED OUT. (FLT 3490) RELAMPED EMERGENCY LIGHT.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,097 hrs · 15,670 cycles
CORROSION ON THE AFT FLOOR SUPPORT STRUCTURE FOR THE COCKPIT FLOOR PANEL ATTACHED TO THE 280 CROSSBEAM. (C-CHECK) REMOVED AND REPLACED CORRODED FLOOR SUPPORT ANGLE IAW REO.
Part: SKIN — CHAFED (FUSELAGE) · airframe 23,097 hrs · 15,670 cycles
CHAFE ON FUSELAGE SKIN AND ON HEAD OF 6 EA FASTENERS BETWEEN FS 970 - FS 985. (C-CHECK) REMOVED DAMAGE FROM FUSELAGE SKIN APPROXIMATELY AT STR 27 AND FS 970 - FS 985 IAW REO.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,555 hrs · 15,396 cycles
NR 3 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 3454) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,960 hrs · 15,095 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 3465) RELAMPED EMERGENCY LIGHT.
2011
Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 18,965 hrs · 13,528 cycles
TWO CRACKS IN THE UPPER ANGLE OF FLOOR SUPPORT CROSS MEMBER AT FS 280, ONE AT LBL 11 AND ONE AT RBL 13. (C-CHECK) REPLACED FS 280 CROSSBEAM PER REO.