N612NN
Registered owner: AMERICAN AIRLINES INC, TX (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.
9 reports on file, 2023-09-09 – 2026-08-07.
Part: RELAY — UNSERVICEABLE (100) · airframe 14,801 hrs · 12,610 cycles
L ENG DEGRADED CAUTION IN FLIGHT. REPLACED K19, K21 IAW CRJ 900 AMM 24̉‰06̉‰07̉‰000̉‰801. FAULT DID NOT REOCCUR. OPS CHECK GOOD
Part: CONTROL UNIT — FAULTED · airframe 13,578 hrs · 11,681 cycles
RUDDER LIMITER, PITCH FEEL, SLATS FAIL, STALL FAIL, FLAPS FAIL CAUTION MSGS AFTER TAKEOFF. REMOVED AND REPLACED SFECU 1 IAW AMM 27-51-05-000/400-801. OPS CHECK GOOD AT THIS TIME. NO FURTHER DEFECTS NOTED AT THIS TIME. SELF TEST PASSED.
Part: UNKNOWN — ODOR (CABIN) · airframe 13,533 hrs · 11,641 cycles
STRONG ODOR OF EXHAUST FUMES IN THE AIRCRAFT DURING FLIGHT, FOLLOWED FIM 79-30-00-810-821. DUE TO MAINTENANCE PERFORMED LAST NIGHT, SUSPECT POSSIBLE CAUSE NR 3. PERFORMED HIGH POWER DRY OUT PER AMM 72-00-00-100-803-A01-PSA NO SMELLS OR FAULTS NOTED.
Part: SKIN — DENTED (ZONE 100) · airframe 12,841 hrs · 11,112 cycles
DENT DAMAGE FOUND ON FUSELAGE AT FS 949.00, BETWEEN STRINGERS 20R AND 21R. THE DENT IS SMOOTH AND FOUND CRACK FREE BY VISUAL INSPECTION. DIMESION ARE 0.067 X 1.57 X 0.118 INCH. VERIFIED WORK PERFORMED AT RHS FUSELAGE FS942.00-FS897.00 STR 19R-22R IAW REO 690-53-51-528. THIS C/W PERM REPAIR IAW EA 53-2025-1234.
Part: NONE — NO DISCREPANCY · airframe 12,480 hrs · 10,828 cycles
DURING TAKEOFF, WHILE STILL ON THE GROUND, BUT ABOVE 80KTS, THE PLANE NOTICEABLY JERKED. THIS FELT DISTINCTLY DIFFERENT THAN THE VIBRATION THAT IS FELT DUE TO THE LACK OF STRAPS. PERFORMED GENERAL VISUAL INSPECTION OF BOTH MLG AND THE NLG IAW AMM 32-10-00-210-801-PSA AND 32-20-00-210-801-A01. NO DEFECTS NOTED.
Part: ACM — SMOKE (ZONE 100) · airframe 11,472 hrs · 10,037 cycles
FA REPORTED SMOKE IN CABIN AFT TOUCHDOWN, SMOKE CONTINUED TO INCREASE, PARKING BRAKE SET. PAX DOORS AND OVERWING EXITS ARE USED FOR EVACUATION. GRAYISH SMOKE DISSIPATED AFTER A/C SHUTDOWN. NO MEDICAL ATTENTION WAS NOTED AT THIS TIME. / REMOVED AND REPLACED ACM IAW AMM 21-51-08-000/400-801-A01. OPS CHECK GOOD AT THIS TIME. LEAK CHECK GOOD AT THIS TIME.
Part: UNKNOWN — UNKNOWN (ZONE 100) · airframe 7,922 hrs · 6,267 cycles
AFTER BLIND BOLTS REMOVAL, ELONGATED HOLE AND NICK NEXT TO THE HOLE LOCATION WAS FOUND AT FS 780.00 BTW LBL 36 TO LBL 45. (SM). ELONGATED HOLE AND NICK NEXT TO HOLE LOCATION AT FS780.00 BTW LBL36 TO LBL45 WAS REPAIRED PER REO 690-53-41-428 REV. - -
Part: SKIN PANEL — NICKED (ZONE 600) · airframe 7,922 hrs · 6,267 cycles
SEVERAL NICKS ALONG RH INBOARD FLAP PANEL LOWER FACE. NICKS OF RH INBOARD FLAP WAS REMOVED PER CRJ900 SRM 51-12-00-001-001-A01 AND WAS EVALUATED AS FOLLOWS: BTW FLS 45 TO FLS 65 WAS FOUND WITHIN LIMITS AND BTW FLS 15 TO FLS 45 WAS FOUND OUT OF LIMITS PER CRJ900 SRM 57-52-01-101-001-A01 AND WAS REPAIRED PER SRM 57-52-01-201-005-A01.
Part: FLAP — NICKED (UNKNOWN) · airframe 7,922 hrs · 6,267 cycles
SEVERAL NICKS ALONG LH INBOARD FLAP PANEL LOWER FACE. NICKS OF LH INBOARD FLAP WAS REMOVED PER CRJ900 SRM 51-12-00-001-001-A01 AND WAS EVALUATED AS FOLLOWS: BTW FLS 45 TO FLS 65 WAS FOUND WITHIN LIMITS AND BTW FLS 15 TO FLS 45 WAS FOUND OUT OF LIMITS PER CRJ900 SRM 57-52-01-101-001-A01 AND WAS REPAIRED PER SRM 57-52-01-201-005-A01