N396AX
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.
5 reports on file, 2012-04-11 – 2016-10-01.
Part: SENSOR — FAILED · airframe 90,876 hrs · 15,838 cycles
DURING APPROACH, ENGINE SURGED AND WOULD NOT MAINTAIN COMMANDED N1. PERFORMED LANDING W/ LEFT ENGINE AT IDLE. ODOR OF SMOKE DURING SURGES. REPLACED CIT SENSOR IAW AMM 73-21. ENGINE RUN (MPA) IAW AMM 71-00.NO CHANGE IN STATUS. REPLACED MEC IAW 73-21 OPS CK AND LEAK CK GOOD REPLACED IP CHECK VALVE, OPS GOOD IAW AMM 36-11. OPS & LEAK CHECKED.
Part: FRAME — CORRODED (FAN CASE) · corrosion level 2 · airframe 84,041 hrs · 14,393 cycles
CORROSION ON LOWER FAN CASE FRAME FROM 5 TO 7 O`CLOCK POSITION BLENDED AND FOUND TO BE OUT OF LIMITS. R & R FAN CASE.
Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 80,678 hrs · 13,662 cycles
ON LT WING L/E LOWER RIB CORRODED INB OF NR 2 SLAT OTBD TRACK AT WS920. MADE REPAIR PART FABRICATED AND INSTALLED IAW SRM 57-41-00, GI 1 AND SRM 51-40-02. (REF DWG 114T2223) NR 2 SLAT ADJUSTMENT CHECK CARRIED OUT ON ADDITIONAL WC PG 1 OF 1 (CIRCLE STAMP 100) IAW AMM 27-81-02-825-001.
Part: TEE FITTING — CORRODED (BS 808) · corrosion level 2 · airframe 80,678 hrs · 13,662 cycles
CORROSION FOUND ON PANEL 139BL AFT HOLDING BRACKET SEQ140. TEE BRACKET IN KEEL BEAM AREA REPLACED IAW SRM 51-40-02 PARA 4, FIG 3 PANEL INSTALLATION COVERED ON T/C 1025.
Part: FLOORBEAM — CORRODED (BS 808) · corrosion level 2 · airframe 80,678 hrs · 13,662 cycles
CORROSION FOUND ON FLOORBEAM UPPER CHORD AT BS 808 AND LBL 11.00. FLOORBEAM UPPER CHORD REPAIRED AT LBL11, BS 808 IAW SRM 53-50-52 FIG 101, SRM 53-00-51, FIG 201 AND DWG 111T5007 (CIRCLE STAMP 119).