N619NN
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.
35 reports on file, 2023-02-01 – 2023-04-24.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON STGR 26R BTW FS=364.00/349.0 AT MAIN AVIONICS COMPARTMENT. (E/E)
Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON FRAME FS= 364.00 BETWEEN STRG 26RH TO 26RH AT MAIN AVIONICS COMPARTMENT
Part: SUPPORT — CORRODED (MLG AREA) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON LH/RH MLG SIDE STAY SUPPORT.
Part: SKIN — DENTED (ZONE 600) · airframe 6,217 hrs · 6,577 cycles
SEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FROM FLS 15.00 TO FLS 65.50
Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON SUPPORTS (2EA) AT LH WHEEL WELL AREA BTW FS=797 TO FS=830 AND LBL / RBL 45".
Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON INTERNAL PRODUCTION DOUBLER AND ANCHORE NUT IN STA. FS=310 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT
Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON LEADING EDGE (LIP SKIN) OF RH ENGINE INLET COWL.
Part: ACOUSTIC LINER — DENTED (ZONE 400) · airframe 6,217 hrs · 6,577 cycles
DENT AT 7:00 O'CLOCK POSITION CLOSE TO THE LEADING EDGE ON METAL PERFORATE ACOUSTIC LINER OF RIGHT FORWARD CORE COWL
Part: LUG — CORRODED (ZONE 600) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON BORE LUGS AT HINGE FITTING #2 (I/B AND O/B) & HINGE FITTING#3 (O/B), RH AILERON
Part: HINGE FITTING — WORN (ZONE 200) · airframe 6,217 hrs · 6,577 cycles
AFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO.2 AND NO. 3 AT VERYTICAL STABILIZER REAR SPAR MIDDLE SECTION.
Part: COUPLING — CORRODED (ZONE 200) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON COUPLINGS OF FUEL OVERWING VENT TUBING, LOCATED IN WHEEL WELL AREA BTW FS=797.00 TO FS= 813 AND RBL 39".
Part: HINGE FITTING — CORRODED (ZONE 300) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON LOWER RUDDER HINGE AT REAR SPAR OF VERTICAL STABILIZER
Part: CAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON MID CAP AT LOWER SILL, FUSELAGE PASSENGER DOOR FRAME
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION AT SEAT RAIL LBL 9.0 BETWEEN FS364.00-FS485.00
Part: SKIN — DENTED (ZONE 100) · airframe 6,217 hrs · 6,577 cycles
DENTS ON EXTERNAL FUSELAGE SKIN, REAR FUSELAGE SKIN COVERED BY RH VENTRAL FIN FAIRING
Part: SKIN — DENTED (ZONE 100) · airframe 6,217 hrs · 6,577 cycles
DENTS ON EXTERNAL FUSELAGE SKIN, REAR FUSELAGE SKIN COVERED BY LH VENTRAL FIN FAIRING.
Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON KICK PLATE ANGLE AT LOWER SILL, FUSELAGE PASSENGER DOOR FRAME
Part: SUPPORT — CORRODED (ZONE 300) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON LH/RH CONNECTORS SUPPORT PX10J1, PX01J1 AND PX09J1.
Part: RIB — CORRODED (ZONE 600) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON RIB #1 AT RH WING.
Part: BLOCK — CORRODED (ZONE 700) · corrosion level 2
CORROSION ON LH/RH MLG HYDRAULICS LINES BLOCKS AND THEIR SUPPORTS
Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON FRAME FS= 310 BETWEEN STRG 24LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E)
Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON HYD LINE SUPPORTS (4 EAS) AT LH / RH WHEEL WELL AREA BTW FS=797 TO FS= 830 AND LBL 40" AND 35" / RBL 40" AND 35"
Part: SKIN — CORRODED (ZONE 700) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON LH MLG DOOR ON INTERNAL AND EXTERNAL SKIN
Part: PRESSURE DECK — CORRODED (ZONE 500) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON DOUBLER OF WING STUD LOWER SKIN AT LH WHEELWELL AREA BTW FS 797 TO FS=830 AND LBL 38".
Part: ACCESS PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON SETTLEMENT AREA OF ACCESS PANELS 542AZ, 542BZ, 642BZ AND 642AZ
Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON FRAME FS=333 BETWEEN STRG 25LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E)
Part: DOOR — CORRODED (ZONE 700) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON RH MLG DOOR ON INTERNAL AND EXTERNAL SKIN
Part: RETAINER — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON SEAL RETAINER OF LH/RH WING TO FUSELAGE FAIRING AT WHEEL WELL AREA.
Part: VALVE — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON FLOATATION VALVE OF AFT ACCESSORIES COMPARTMENT BULKHEAD FS 1098
Part: RETAINER — CORRODED (ZONE 500) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON RETAINER SEALS AT ACCESS PANEL 583AB, 583BB, 683AB, 683BB
Part: CYLINDER — CORRODED (ZONE 700) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION IN LOWER SURFACE OF NLG OUTER CYLINDER
Part: FRAME — CORRODED (ZONE 800) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON FWD HANDLE FRAME AT FWD / CENTER BAGGAGE BAY DOOR INTERNAL STRUCTURE.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION WAS FOUND IN DRAIN OF THE LOWER TAILCONE FS1181.00.
Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
IN TAILCONE AND THE DRAG ANGLE ADJACENT TO BELOW RUDDER WAS FOUND CORROSION
Part: DOUBLER — CORRODED (ZONE 300) · corrosion level 2 · airframe 6,217 hrs · 6,577 cycles
CORROSION ON LIGHTNING PROTECTION STRIP ON RH/LH HORIZONTAL STABILIZER TIP EXTERNAL STRUCTURE (ACCESS PANEL 343BR AND 333BL)