N219AG
Registered owner: KREBS CALEB, OH (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.
46 reports on file, 2011-09-12 – 2016-05-31.
Part: UNKNOWN — SMOKE (COCKPIT) · airframe 31,320 hrs · 19,696 cycles
SMOKE IN COCKPIT COMING OUT OF F/O'S SIDE VENT. F/O CLOSED, RAN A/C PACKS THROUGH ALL BLEED CONFIGURATIONS COULD NOT DUPLICATE. OPS CHECK GOOD.
Part: FLOOR SUPPORT — CORRODED (BS 579-583) · airframe 30,200 hrs · 19,046 cycles
FLOOR SUPPORT AT BS 579 - 583 CORRODED. COMPLIED WITH PERMANENT REPAIR IAW EA.
Part: INTERCOSTAL — DAMAGED (BS 349-364) · airframe 30,200 hrs · 19,046 cycles
STRINGER 26R INTERCOSTAL LOCATED BETWEEN FS 349 AND FS 364 CORRODED OUT OF LIMITS. REMOVED, LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL AT STR 26R AT FS 349 TO FS 364 IAW SRM.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 30,200 hrs · 19,046 cycles
MAIN AVIONICS BAY, FLOORBOARD MOUNT BRACKET LOCATED AT FS 280 BETWEEN RBL 8.5 AND LBL 8.5. REQUIRES REPLACEMENT DUE TO CORROSION. REMOVED, LOCATED, DRILLED AND INSTALLED CRAWLWAY FLOOR SUPPORT ANGLE AT FS 280 BETWEEN LBL 8.5 AND RBL 8.5 IAW SRM.
Part: DOUBLER — CORRODED (BS 295-310) · airframe 30,200 hrs · 19,046 cycles
MAIN AVIONICS BAY TCAS OMNI-DIRECTIONAL ANTENNA DOUBLER HAS CORROSION BETWEEN FS 295 AND FS 310. REMOVED DAMAGED TCAS ANTENNA DOUBLER IAW SRM AND INSTALLED NEW TCAS ANTENNA DOUBLER, PN: SH670-32364-5 IAW SRM. PERFORMED PRESSURIZATION CHECK IAW AMM PRESSURE CHECK GOOD NO LEAKS DETECTED.
Earlier reports · 2011–2014 · 41 reports
2014
Part: LINE — FAILED (HYD SYSTEM) · airframe 26,291 hrs · 16,890 cycles
DURING CRUISE LOST NR 1 HYD FLUID - DROPPED TO 5 PERCENT EDP. RAN WITH 0 PSI FOR APPROX 5 MIN. R & R NR 1 EDP PRESSURE LINE AND NR 1 EDP IAW AMM,
Part: SEAT TRACK — CORRODED (BS 675-711) · airframe 25,210 hrs · 16,331 cycles
RIGHT SIDE SEAT TRACK HAS CORROSION FROM BS 675 - 711. R & R SEAT TRACK IAW AMM AND SRM.
Part: SEAT TRACK — CORRODED (BS 485-574) · airframe 25,210 hrs · 16,331 cycles
LEFT SIDE SEAT TRACK HAS CORROSION FROM BS 485 - 574. BLENDED CORRODED AREAS IAW REO.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 25,210 hrs · 16,331 cycles
RIGHT SIDE SEAT TRACK HAS CORROSION FROM BS 785 - 863. R & R SEAT TRACK IAW AMM AND SRM.
Part: SEAT TRACK — CORRODED (BS 674-709) · airframe 25,210 hrs · 16,331 cycles
LEFT SIDE SEAT TRACK HAS CORROSION FROM BS 674 - 709. BLENDED CORRODED AREAS IAW REO.
Part: SEAT TRACK — CORRODED (BS 578-683) · airframe 25,210 hrs · 16,331 cycles
LT SEAT TRACK HAS CORROSION FROM BS 578 - 683. BLENDED CORRODED AREAS IAW REO.
Part: ANGLE — CRACKED (ZONE 200) · airframe 25,210 hrs · 16,331 cycles
LEFT OTBD ANGLE FOUND TO BE CRACKED. REPLACED ANGLE IAW REO.
Part: SEAT TRACK — CORRODED (BS 486-508) · airframe 25,210 hrs · 16,331 cycles
RIGHT SEAT TRACK HAS CORROSION FROM BS 486 - 508. BLENDED IAW REO.
Part: SEAT TRACK — CORRODED (BS 712-761) · airframe 25,210 hrs · 16,331 cycles
RIGHT SIDE SEAT TRACK HAS CORROSION FROM BS 712 - 761. R & R SEAT TRACK IAW AMM AND SRM.
Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 25,210 hrs · 16,331 cycles
RT SEAT TRACK HAS CORROSION FROM BS 349 - 485. BLENDED IAW REO.
Part: SEAT TRACK — CORRODED (BS 575-672) · airframe 25,210 hrs · 16,331 cycles
LT SIDE SEAT TRACK HAS CORROSION FROM BS 575 - 672., C-CHECK. REPLACED SEAT TRACK IAW REO.
Part: SEAT TRACK — CORRODED (BS 710-761) · airframe 25,210 hrs · 16,331 cycles
LEFT SIDE SEAT TRACK HAS CORROSION FROM BS 710 - 761. BLENDED CORRODED AREAS IAW REO.
Part: SEAT TRACK — CORRODED (BS 483-575) · airframe 25,210 hrs · 16,331 cycles
RT SIDE SEAT TRACK HAS CORROSION FROM BS 483 - 575. BLENDED SEAT TRACK IAW REO.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 25,210 hrs · 16,331 cycles
LEFT SIDE SEAT TRACK HAS CORROSION FROM BS 785 - 863. BLENDED CORRODED AREAS IAW REO.
Part: SEAT TRACK — CORRODED (BS 379-484) · airframe 25,210 hrs · 16,331 cycles
LEFT SIDE SEAT TRACK HAS CORROSION FROM BS 379 - 484. REPLACED SEAT TRACK IAW REO.
Part: DOUBLER — CRACKED (BS 193) · airframe 25,210 hrs · 16,331 cycles
CRACK BS 193, RT SIDE, JUST OTBD OF ADG PUMP. C-CHECK, R & R THE CRACKED DOUBLER IAW REO.
Part: STRUCTURE — CRACKED (BS 193) · airframe 25,210 hrs · 16,331 cycles
BS 193 FWD EQUIPTMENT BAY HAS CRACK. LT SIDE. REPAIRED IAW REO.
Part: SKIN — DENTED (BS 280) · airframe 25,210 hrs · 16,331 cycles
DENT AT LOWER FUSELAGE AFT OF BS 280 BETWEEN STRINGERS 25-26L. REPAIRED IAW EA.
Part: LIGHT — BURNED OUT (EMERGENCY LIGHT) · airframe 24,598 hrs · 16,012 cycles
EMERGENCY OVERHEAD LIGHT IS BURNED OUT. REPLACED LAMP.
2013
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 22,029 hrs · 14,723 cycles
FLT 3475, EMERGENCY LIGHTS DO NOT ILLUMINATE. POSITIONED EMERGENCY LIGHT SWITCH INTO ARM POSITION & CHANGED BATTERY PACKS. OPS CHECKED GOOD.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,446 hrs · 14,421 cycles
RIGHT SIDE SEAT TRACK IS CORRODED AT FS 400. (C-CHECK) ADDRESSED CORROSION AT RIGHT SIDE SEAT TRACK AT FS 400 IAW REO.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 21,446 hrs · 14,421 cycles
RIGHT SIDE SEAT TRACK IS GOUGED AT FS 708. (C-CHECK) ADDRESSED GOUGE AT FS 708 IAW REO.
Part: AXLE — CORRODED (RT MLG) · airframe 21,446 hrs · 14,421 cycles
CORROSION FOUND ON RIGHT MLG AXLE NR 4 ON ROOT RADIUS. (C-CHECK) COMPLIED WITH THE REPAIR ON THE RIGHT MLG AXLE (4) ROOT RADIUS IAW REO.
Part: AXLE — CORRODED (LT MLG) · airframe 21,446 hrs · 14,421 cycles
CORROSION FOUND ON LEFT MLG AXLE NR 1 ROOT RADIUS. (C-CHECK) COMPLIED WITH THE REPAIR ON THE LEFT MLG AXLE (1) ROOT RADIUS IAW REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,446 hrs · 14,421 cycles
LEFT FS 714-FS 764 SIDE SEAT RAIL HAS CORROSION AT 2 EACH SCREW HOLES. (C-CHECK) ADDRESSED CORROSION ON LEFT FS 714-764 SIDE SEAT RAIL IAW REO.
Part: LEVER — CHAFED (CABIN DOOR) · airframe 21,446 hrs · 14,421 cycles
MAIN CABIN DOOR FORWARD PULL IN LEVER IS CHAFED. (C-CHECK) REMOVED DAMAGE TO A DEPTH OF .040 AND RESTORED FINISH TO PASSENGER DOOR FWD PULL IN LEVER IAW REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,446 hrs · 14,421 cycles
RIGHT FS 785-FS 863 SIDE SEAT RAIL HAS CORROSION AT 1 EACH SCREW HOLE. (C-CHECK) ADDRESSED CORROSION AT RIGHT FS 785-863 SIDE SEAT RAIL IAW REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,446 hrs · 14,421 cycles
LEFT FS 369-FS 574 SIDE SEAT RAIL HAS CORROSION AT 3 EACH SCREW HOLES. (C-CHECK) ADDRESSED CORROSION AT LEFT FS 369-574 SIDE SEAT RAIL IAW REO.
Part: AXLE — CORRODED (LT MLG) · airframe 21,446 hrs · 14,421 cycles
CORROSION FOUND ON LEFT MLG AXLE NR 2 ROOT RADIUS. (C-CHECK) COMPLIED WITH THE REPAIR ON THE LEFT MLG AXLE (2) ROOT RADIUS IAW REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,446 hrs · 14,421 cycles
LEFT FS 785-FS 863 SIDE SEAT RAIL HAS CORROSION AT 1 EACH SCREW HOLE. (C-CHECK) ADDRESSED CORROSION AT LEFT SIDE SEAT RAIL FS 785-863 IAW REO.
Part: AXLE — CORRODED (RT MLG) · airframe 21,446 hrs · 14,421 cycles
CORROSION FOUND ON THE RIGHT MLG AXLE NR 3 ROOT RADIUS. (C-CHECK) COMPLIED WITH THE REPAIR ON THE RIGHT MLG AXLE (3) ROOT RADIUS IAW REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,446 hrs · 14,421 cycles
LEFT FS 616-FS 714 SIDE SEAT RAIL HAS CORROSION AT 3 EACH SCREW HOLES. (C-CHECK) REMOVED CORROSION FROM LEFT FS 616-714 SIDE SEAT RAIL AT 3 EACH SCREW HOLES IAW REO.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 20,780 hrs · 14,087 cycles
EMERGENCY EXIT SIGN AT 13 A IS PARTIALLY BURNED OUT. (FLT 3451) RELAMPED EMERGENCY EXIT SIGN.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,471 hrs · 13,423 cycles
SECOND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 3461) RELAMPED EMERGENCY LIGHT.
Part: DOOR — LACK OF LUBE (CABIN) · airframe 18,302 hrs · 12,824 cycles
MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. (FLT 3490) ADJUSTED DOOR CLOSURE GAP AND LUBED DOOR.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,114 hrs · 12,727 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 9 IS OUT. (FLT 3453) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,898 hrs · 12,616 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 16 IS OUT. (FLT 3461) RELAMPED EMERGENCY LIGHT.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 19,183 hrs · 13,272 cycles
FS 280 FLOORBEAM CRACKED. (C-CHECK) REPAIR CRACK AT FS 280.
Part: SKIN — CRACKED (PAX DOOR) · airframe 19,183 hrs · 13,272 cycles
PAX DOOR LOWER INNER SKIN IS CRACKED AT FS 340.0 LOWER INTERCOSTAL. (C-CHECK) REPAIRED PER MODSUM.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,774 hrs · 12,013 cycles
SECOND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 3451) RELAMPED EMERGENCY LIGHT.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 16,147 hrs · 11,673 cycles
EMERGENCY LIGHTS ARE NOT WORKING. (FLT 3486) REPLACED NR 1 EMERGENCY LIGHT BATTERY PACK. P/N OFF 2013-1A, S/N OFF 62910.