OpenAirDocs.org

N612NN

Open the Markdown

2019 Bombardier CL-600-2D24 · GE CF34-8C5

Open in FAA registry

© OpenStreetMap
Registered owner
American Airlines Inc
Location
Fort Worth, TX
Owner type
Corporation
Serial number
15477
Year built
2019
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
December 5, 2019
Certificate issued
December 5, 2019
Expires
December 31, 2029
Mode S code
A7F765
Bombardier CL-600-2D24Airframe model · 95 seats · 2 engines · 314 registeredTCDS A21EA-1Airframe · Bombardier CL-600-2D24TCDS E00063ENEngine · GE CF34-8C5

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 130

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2003In forceSuperseded2026
See all 155 ADs

Information bulletins that may apply · 4

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N612NNMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Bombardier CL-600-2D24 aircraft

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Incident 20230123002019ITaxi · Portland, MEOn January 23, 2023, [privacy data omitted] departed philadelphia international airport (phl) for Portland International Jetport (pwm). 11:49- Portland approach control told 5280 to expect the ILS RW11 approach into pwm. Approach added that the last arriving…Jan 23, 2023 · Minor damage

Service difficulty reports · 10

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR VNAA2026092225202Control Unit · unserviceableBRAKE OVHT WARNING MSG DURING CRUISE, NR 3 SENSOR, LT INBD CHANNEL ALSO FAILED ON LANDING WITH RT INBD ON MEL. REF. H78AQ. SUSPECT FAULTY ASCU. REMOVED AND REPLACED ASCU IAW AMM 32-44-06-000/400-801. OPS CHECKS GOOD. THIS CLEARS MEL. SYSTEM REACTIVATED.Sep 18, 2026 · N612NN · Cndair CL6002D24 · Brake Anti-Skid SectionSDR VNAA2026081022401Relay · unserviceableL ENG DEGRADED CAUTION IN FLIGHT. REPLACED K19, K21 IAW CRJ 900 AMM 24€“06€“07€“000€“801. FAULT DID NOT REOCCUR. OPS CHECK GOODAug 7, 2026 · N612NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR VNAA2026021612301Control Unit · faultedRUDDER 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.Feb 15, 2026 · N612NN · Cndair CL6002D24 · Flight Control SystemSDR VNAA2026021012001Unknown · odorSTRONG 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.Feb 8, 2026 · N612NN · Cndair CL6002D24 · Air Distribution SystemSDR VNAA2025102211101Skin · dentedDENT 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 690-5Oct 22, 2025 · N612NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA2025082711101None · no discrepancyDURING 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 32-10-00-21Aug 24, 2025 · N612NN · Cndair CL6002D24 · Standard Practices/StructuresSDR VNAA2025040311101Acm · smokeFA 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 ACApr 1, 2025 · N612NN · Cndair CL6002D24 · Cabin Cooling SystemSDR VNAA202310070002Unknown · unknownAFTER 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. - -Sep 13, 2023 · N612NN · Cndair CL6002D24 · Fuselage Structure (General)SDR VNAA202310070003Flap · nickedSEVERAL 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 CRJ9Sep 9, 2023 · N612NN · Cndair CL6002D24 · Trailing Edge FlapsSDR VNAA202310070001Skin Panel · nickedSEVERAL 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 CRJ9Sep 9, 2023 · N612NN · Cndair CL6002D24 · Trailing Edge Flaps

STCs that may be installed · 139

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 139 STCs