N216AG
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.
35 reports on file, 2011-09-13 – 2018-04-27.
Part: ANGLE — CORRODED (DOOR SILL) · airframe 42,073 hrs · 27,760 cycles
SERVICE DOOR LOWER SILL ANGLE HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED THE DOOR LOWER SILL ANGLE IAW SRM.
Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 42,073 hrs · 27,760 cycles
GALLEY SERVICE DOOR SURROUND STRUCTURE, LOWER SILL HAS CORROSION BEHIND FWD AND AFT FITTINGS. INSTALLED A NEW DOOR SILL IAW SRM.
Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 42,073 hrs · 27,760 cycles
INTERNAL STRUCTURE OF THE FLIGHT CONTROL COMPARTMENT CANOPY RIGHT SIDE HAS A FRAME CRACKED. REMOVED AND REPLACED THE FRAME ON THE WINDSHIELD SUPPORT CANOPY STRUCTURE IAW SRM.
Part: FRAME — CORRODED (BS 319) · airframe 42,073 hrs · 27,760 cycles
CORROSION FOUND ON THE FRAME AT BS 319.7, BETWEEN STRINGERS 26L AND 26R. REPLACED THE FRAME SECTION IAW REO.
Part: STRINGER — CORRODED (BS 295-310) · airframe 42,073 hrs · 27,760 cycles
CORROSION FOUND ON STRINGER 26L BETWEEN BS 295 - 310 AROUND THE STAND OFF. REPLACED THE STRINGER.
Part: CHANNEL — CORRODED (BS 295-310) · airframe 42,073 hrs · 27,760 cycles
CORROSION FOUND ON TCAS OMNIDIRECTIONAL ANTENNA CHANNEL BETWEEN BS 295 - 310, STRINGER 27. REMOVED AND REPLACED THE CHANNEL IAW SRM.
Part: STRINGER — CORRODED (BS 319-333) · airframe 42,073 hrs · 27,760 cycles
CORROSION FOUND ON STRINGER 27 BETWEEN BS 319.7 AND 333. REMOVED AND REPLACED THE STRINGER SECTION IAW SRM.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 42,073 hrs · 27,760 cycles
CORROSION FOUND ON THE INTERCOSTAL BETWEEN BS 349 - 364 STRINGER 27R. REPLACED THE INTERCOSTAL IAW SRM.
Earlier reports · 2011–2015 · 27 reports
2015
Part: BRACKET — CRACKED (LT WING) · airframe 37,206 hrs · 24,910 cycles
WELDED ANGLE BRACKET IN LT FUEL TANK AT SLAT 1-3 ROLLER BOX IS CRACKED AT TOP AND BOTTOM OF BRACKET, MARKED. C-CHECK, ANGLE BRACKET IN LT FUEL TANK AT SLAT 1-3, ROLLER BOX REPAIRED REF STS EA. COMPLIED WITH VISUAL CHECK OF THE LT WING FUEL TANK SLAT 1-3 ROLLER BOX. NO LEAKS NOTED.
Part: FLOOR SUPPORT — CORRODED (BS 777) · airframe 37,206 hrs · 24,910 cycles
RIGHT FLOOR SILL IS CORRODED AT FS 777. C-CHECK, RO 3/13/15, REMOVED CORROSION ON RT FLOOR SILL AT FS 777.00, REF SRM. REMAINING MATERIAL THICKESS IS .126" IAW NDT. NO MATERIAL LOST. RESTORED FINISH TO A023 REF SRM BECAUSE THIS WAS IN A NO DAMAGE AREA IAW SRM , SUBMITTED AND RECEIVED EA. COMPLETED ALL WORK AS DESCRIBED IN STEPS 1-7 SECTION 1 FOR PERMANENT REPAIR. NO DEFECTS WERE NOTED FROM THE VISUAL INSPECTION OR FROM THE NDT INSPECTIONS.
Part: FLOOR SUPPORT — CORRODED (BS 769) · airframe 37,206 hrs · 24,910 cycles
RIGHT FLOOR SILL IS CORRODED AT FS 769. C-CHECK, REMOVED CORROSION ON RT FLOOR SILL AT FS 769.00, REF SRM. REMAINING MATERIAL THICKESS IS .126" IAW NDT. NO MATERIAL LOST. RESTORED FINISH TO A023, REF SRM. BECAUSE THIS WAS IN A NO DAMAGE AREA IAW SRM. SUBMITTED AND RECEIVED EA, COMPLETED ALL WORK AS DESCRIBED IN STEPS 1-7 SECTION I FOR PERMANENT REPAIR. NO DEFECTS WERE NOTED FROM THE VISUAL INSPECTION OR FROM THE NDT INSPECTIONS. REPORTS ARE ATTACHED AS REQUIRED.
Part: FLOOR SUPPORT — CORRODED (BS 711) · airframe 37,206 hrs · 24,910 cycles
RIGHT FLOOR SILL IS CORRODED AT FS 711.00. C-CHECK, REMOVED CORROSION ON RT FLOOR SILL REF SRM. REMAINING MATERIAL THICKESS IS .129" IAW NDT. NO MATERIAL LOST. RESTORED FINISH TO A023 REF SRM. BECAUSE THIS WAS IN A NO DAMAGE AREA IAW SRM, SUBMITTED TO STS ENGINEERING SOLUTIONS AND RECEIVED EA. COMPLETED ALL WORK AS DESCRIBED IN STEPS 1-7 SECTION ONE FOR PERMANENT REPAIR. NO DEFECTS WERE NOTED FROM THE VISUAL INSPECTION OR FROM THE NDT INSPECTIONS. REPORTS ARE ATTACHED AS REQUIRED.
2014
Part: FRAME — CRACKED (BS 235) · airframe 36,626 hrs · 24,606 cycles
FRAME BS 235 CRACKED. REPAIRED IAW SRM.
Part: FRAME — CRACKED (BS 235) · airframe 36,626 hrs · 24,606 cycles
BS 235 FRAME CRACKED. REPAIRED IAW SRM.
Part: FRAME — CRACKED (BS 220) · airframe 36,626 hrs · 24,606 cycles
FRAME BS 220 CRACKED. REPAIRED IAW SRM.
Part: FRAME — CRACKED (BS 235) · airframe 36,598 hrs · 24,593 cycles
FOUND BS 235 FRAME TO BE CRACKED. REPAIRED THE FRAME IAW SRM.
Part: FRAME — CRACKED (BS 220) · airframe 36,598 hrs · 24,593 cycles
BS 220 FRAME FOUND CRACKED. REPAIRED IAW SRM.
Part: FRAME — CRACKED (BS 235) · airframe 36,598 hrs · 24,593 cycles
BS 235 FRAME CRACKED. REPAIRED IAW SRM.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 36,017 hrs · 24,288 cycles
NR 3 ELBP DOESN'T HOLD A CHARGE. R & R NR 3 BATTERY PACK IAW AMM. OPS CHECKED GOOD.
Part: CONNECTOR — FAILED (EMERGENCY LIGHT) · airframe 35,111 hrs · 23,831 cycles
EMERGENCY LIGHT POD NR 5 IS INOPERATIVE. RESECURED EMERGENCY LIGHT ELECTRICAL CONNECTOR.
2013
Part: CHANNEL — CORRODED (WING) · airframe 33,221 hrs · 22,922 cycles
TE PANEL 581AB MOUNTING GANG CHANNEL IS CORRODED & BROKEN. C-CHECK R & R GANG CHANNEL PN B0204044-3-12-6M PO NR T000024490 FOR TE PANEL 581AB IAW SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,221 hrs · 22,922 cycles
REPLACE RT SIDE SEAT TRACK FS457-00 TO 483.00, SEAT TRACK CORRODED. C-CHECK REPLACED RT SIDE SEAT TRACK AT FS457.00 TO FS 483.00 IAW SRM & REO.
Part: HINGE — CHAFED (PAX DOOR) · airframe 33,221 hrs · 22,922 cycles
PAX DOOR PIANO HINGE DOOR CHAFED. C-CHECK BLENDED CHAFE ON PAX DOOR PIANO HINGE DOOR SIDE IAW REO.
Part: HINGE — CHAFED (PAX DOOR) · airframe 33,221 hrs · 22,922 cycles
PAX DOOR PIANO HINGE FS CHAFED. C-CHECK BLENDED CHAFE ON PAX DOOR LUGS FS SIDE IAW REO.
Part: FITTING — CHAFED (RT MLG DOOR) · airframe 33,221 hrs · 22,922 cycles
RT MLG DOOR CHAFED. C-CHECK REPLACED RT MLG DOOR FITTING IAW REO & SRM.
Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 33,221 hrs · 22,922 cycles
FS280.00 CROSSBEAM CRACKED AT LBL 11. C-CHECK REPAIR TO BE ACCOMPLISHED IAW SERVICE BULLETIN.
Part: FITTING — CHAFED (LT MLG DOOR) · airframe 33,221 hrs · 22,922 cycles
LT MLG DOOR CHAFED. C-CHECK REPLACED LT MLG DOOR FITTING IAW REO & SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,506 hrs · 22,048 cycles
NR 4 REAR EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 3454) RELAMPED EMERGENCY LIGHT.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,661 hrs · 21,624 cycles
ROW 7 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 3471) RELAMPED EMERGENCY LIGHT.
Part: WIRE — DISCONNECTED (CABIN) · airframe 28,595 hrs · 20,574 cycles
EXIT SIGN OVER SERVICE DOOR DOES NOT ILLUMINATE WHEN TESTING EMERGENCY LIGHTS. (FLT 3459) CONNECTED WIRE AT SPLICE IN REFERENCE TO AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,324 hrs · 20,437 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,365 hrs · 19,918 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 3451) RELAMPED EMERGENCY LIGHT.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 26,937 hrs · 19,682 cycles
SERVICE DOOR EMERGENCY EXIT LIGHT IS OUT. (FLT 3477) RECONNECTED SERVICE DOOR EMERGENCY LIGHT CONNECTOR.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,550 hrs · 19,468 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 3471) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,501 hrs · 19,443 cycles
OVERHEAD EMERGENCY LIGHT OVER ROW 16 BURNED OUT. (FLT 3482) RELAMPED EMERGENCY LIGHT.