N608NN
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, 2020-03-31 – 2026-08-14.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
CORROSION ON SEAT RAIL LBL=10 BTW FS=598 TO FS=669.40 AT CPAX. CORROSION ON SEAT RAIL LBL=10 BTW FS=598 TO FS=669.40 AT CPAX. WAS EVALUATED OUT OF LIMITS PER SRM 53-31-49-101-001-A02 REPLACED PER AMM 53-00-49.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
CORROSION ON LT SIDE RAIL BTW FS=881 TO FS=785 AT CPAX. CORROSION ON LH SIDE RAIL BTW FS=881 TO FS=785 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-A02 REPLACED PER AMM 53-00-49.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
CORROSION ON LT SIDE RAIL BTW FS=700 TO FS=379 AT CPAX. CORROSION ON LH SIDE RAIL BTW FS=700 TO FS=379 AT CPAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 REPLACED PER AMM 53-00-49.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
WEAR RH SEAT RAIL FS 847.00 +16.00 TO 977.00 AT PAX CABIN. RT SEAT RAIL FS 847.00 +16.00 TO 977.00 AT PAX CABIN. WAS EVALUATED OUT OF LIMITS PER SRM 53-51-49-101-001-A02 AND REPLACED PER AMM 53-00-49.
Part: CANISTER — CRACKED (ZONE 500) · airframe 15,433 hrs · 13,161 cycles
CRACK ON CANISTER WELDED NO.3 IN STA WS=148 AT INTERNAL LH MAIN FUEL TANK. CRACK ON CANISTER WELDED NO.3 IN STA WS=148 AT INTERNAL LT MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV -.
Part: BEARING — WORN (RUDDER HINGE) · airframe 15,433 hrs · 13,161 cycles
FREE PLAY ON BEARINGS OF RUDDER HINGES NR 2 AND 3 AT REAR SPAR OF VERTICAL STABILIZER. BEARINGS OF RUDDER HINGES NR 2 AND 3 AT REAR SPAR OF VERTICAL STABILIZER WERE REPLACED PER RIL #1213 REV. NC.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 15,433 hrs · 13,161 cycles
CRACK ON FLOOR SUPPORT RBL 12, BTW BS 221.73 - 229, (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50) AT FWD FUSELAGE INTERNAL STRUCTURE. FLOOR SUPORT RBL 12.0 BTW BS 221.73 - 229 (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50) AT FWD FUSELAGE INTERNAL STRUCTURE WAS REPAIRED PER REO. 690-53-11-2235 REV -.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
CORRODED FLOOR FITTING IN AFT ACCESS 107 OUTSIDE (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 107 OUTSIDE (1EA) ON GALLEY WAS FABRICATED AND INSTALLED PER EA NO:2531-2026-0889 REV: - - SECTION III PERMANENT REPAIR.
Part: FITTING — CORRODED (ZONE 500 AILERON) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
CORROSION ON CENTER FITTING OF LH AILERON L5 LUG BORE. REPAIRED PER REO 670-57-61-237
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
CORROSION ON SEAT RAIL LBL=26 BTW FS=486 TO FS=597 AT CPAX. CORROSION ON SEAT RAIL LBL=26 BTW FS=486 TO FS=597 AT CPAX. WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
CORROSION ON RH SIDE RAIL BTW FS=421 TO 485 , FS=501 TO FS=570 , FS=610 TO FS=720 AT CPAX. RIGHT SIDE RAIL BTW FS=421 TO 485 , FS=501 TO FS=570 , FS=610 TO FS=720 AT CPAX WERE REPLACED PER CRJ900 AMM 53-00-49"
Part: DOOR — CRACKED (ZONE 800) · airframe 15,433 hrs · 13,161 cycles
DOOR WASTE ASSEMBLY WAS REPAIRED PER EA NO: 2542-2026-0913 REV. -
Part: TAIL CONE — DENTED (ZONE 100) · airframe 15,433 hrs · 13,161 cycles
DENT IN TAILCONE WAS REPAIRED IAW REO 690-53-84-062 REV -.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 15,433 hrs · 13,161 cycles
CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2234 REV -.
Part: RIB — CRACKED (ZONE 500) · airframe 15,433 hrs · 13,161 cycles
CRACK ON RIB LEADING EDGE SS 57.16 AT LH WING. RIB LEADING EDGE SS 57.16 AT LH WING WAS REPAIRED PER REO 690-57-41-240 REV -.
Part: SKIN — DAMAGED (ZONE 500 FLAP) · airframe 15,433 hrs · 13,161 cycles
SEVERAL NICKS, EROSION AND WEAR ON LOWER SKIN OF LH INBOARD FLAP FLS 15.5 TO FLS 75.5 WAS REPAIRED PER CRJ900 SRM 57-52-01-201-005-A01
Part: RIB — CRACKED (ZONE 600) · airframe 15,433 hrs · 13,161 cycles
CRACK ON RIB LEADING EDGE SS 57.16 AT RH WING. CRACK ON RIB LEADING EDGE SS 57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV. -.
Part: WEB — CRACKED (ZONE 100) · airframe 15,433 hrs · 13,161 cycles
CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193. ELECTRICAL BAY FLOOR WEB RIGHT SIDE WAS REPAIRED PER SRM 53-11-43-201-001-A01
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
CORROSION ON SEAT TRACK RBL9, BTW BS 349 - 485 AT CPAX. CORROSION ON SEAT TRACK RBL9.00 BTW FS=349 TO FS=485 AT CPAX. WAS EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-001-A02 AND SRM 53-31-49-101-001-A02 REPLACED IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
CORROSION ON SEAT TRACK LBL 9 BTW BS 379 - 485 AT CPAX. CORROSION ON SEAT TRACK LBL 9 BTW BS 379 - 485 AT CPAX. WAS EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A02 AND SRM 53-31-49-101-001-A02 REPLACED IAW AMM 53-00-49.
Part: LUG — CORRODED (ZONE 600 AILERON) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
AFTER RT AILERON BUSHINGS REMOVAL WAS FOUND CORROSION ON LUG BORE R2 AT CENTER FITTING RT AILERON. LUG BORE R2 AT CENTER FITTING, RH AILERON WAS REPAIRED PER REO 670-57-61-237 REV.-- "
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
CORROSION ON SEAT RAIL LBL=26 BTW FS=364 TO FS=485 AT PAX CABIN. CORROSION ON SEAT RAIL LBL=26 BTW FS=364 TO FS=485 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A02. AND SRM 53-31-49-101-001-A02 REPLACED PER AMM 53-00-49.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
CORROSION ON SEAT RAIL RBL9.00 BTW FS=486 TO FS=597, FS=598 TO FS=669.40 AT CPAX. CORROSION ON SEAT RAIL RBL9.00 BTW FS=486 TO FS=597, FS=598 TO FS=669.40 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-31-49-101-001-A02 REPLACED PER AMM 53-00-49.
Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
CORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-21."
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,433 hrs · 13,161 cycles
CORROSION ON RH SIDE RAIL BTW FS=744 TO FS=761 AT CPAX. CORROSION ON RH SIDE RAIL BTW FS=744 TO FS=761 AT CPAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-A02 REPLACED PER AMM 53-00-49.
Earlier reports · 2020–2023 · 10 reports
2023
Part: HINGE — ELONGATED · airframe 7,720 hrs · 6,690 cycles
AFTER HINGE REMOVAL IN REF. NRC 00005, ELONGATED HOLES (3EAS) WAS FOUND. ELONGATED HOLES (3EAS) WERE REPAIRED PER REO 690-53-21-1626 REV.-A
Part: STRINGER — DAMAGED · airframe 7,720 hrs · 6,690 cycles
DENTS 2 (EA´S) ON INBOARD FLAP, LOWER SKIN. AT WS 29.00 TO WS 68.00. 3.5 IN FROM T.E. DENTS (2 EAS) ON INBOARD FLAP, LOWER SKIN AT WS 29.00 TO WS 68.00 WERE EVALUATED AS FOLLOWS: DENT 1 (BTW FLS25.50 AND FLS30.00) WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 57-52-01-101-001-A01 AND DENT 2 (BTW FLS50.00 AND FLS67.00) WAS EVALUATED OUT OF LIMITS AND REPAIRED PER EA 23-C9-57-0564 REV. IR
Part: SKIN — CRACKED · airframe 7,720 hrs · 6,690 cycles
WEAR MARK ON EXTERNAL FUSELAGE SKING BTW FS897-FS913 AND BTW STGR 26L-27. WEAR ON EXTERNAL FUSELAGE SKIN BTW FS897 TO FS913 AND STGR 26L TO STGR 27 WAS REPAIRED PER EA 23-C9-53-0554 REV. IR
Part: SEAT TRACK — WORN · airframe 7,720 hrs · 6,690 cycles
"DISC.- CORROSION ON SEAT RAIL RBL 9 BTW F.S.349.00 TO F.S. 359.00. CA- SEAT RAIL RBL 9 BTW F.S.349.00 TO F.S. 359.00 WAS EVALUATED OUT OF LIMITS PER CRJ/900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ/900 AMM 53-00-49-000-801 ( CONFIG A12 ) AND CRJ-900 AMM 53-00-49-400-801 (CONFIG A12)."
Part: SKIN — CRACKED · airframe 7,720 hrs · 6,690 cycles
SEVERAL NICKS ON LOWER SKIN OF AFT FUSELAGE BTW FS 977.00 TO 1051.3 AND STG 21 RH TO STR 27. NICKS ON LOWER SKIN OF AFT FUSELAGE BTW FS 977.00 TO 1051.3 AND STG 21 RH TO STR 27 WERE REPAIRED PER EA EA 23-C9-53-0562-IR ; EA 23-C9-53-0565-IR ;EA 23-C9-53-0566-IR AND EA 23-C9-53-0567-IR
Part: SEAT TRACK — WORN · airframe 7,720 hrs · 6,690 cycles
CORROSION WAS FOUND BETWEEN THE FOLLOWING STATIONS: FROM FS 785.15 TO FS 797.00 OF THE R/H SIDE SEAT RAIL. CORRECTIVE ACTION: R/H SIDE SEAT RAIL FROM FS 785.15 TO FS 797.00 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ-900 AMM 53-00-49-000-801 (CONFIG A12) AND CRJ-900 AMM 53-00-49-400-801 (CONFIG A12).
2021
Part: SENSOR — FAULTED (BRAKE TEMP) · airframe 4,052 hrs · 3,554 cycles
CREW GOT A BRAKE TEMP OVER HEAT MESSAGE ON TAKE OFF IN CLT. THEY WERE BETWEEN 30-40KTS WHEN THEY REJECTED THEY TAKE OFF AND NOTIFIED ATC OF THE ISSUE. THEY EXITED THE RUNWAY AND PARKED AT A HARD STAND WHERE EMERGENCY VEHICLES WERE ON STANDBY MONITORING THE BRAKES. AFTER THEY GOT THE ALL CLEAR THE FIRE AND RESCUE THE CREW RETURNED TO THE GATE WITHOUT ANY FURTHER ISSUES. NO FURTHER INFORMATION HAS BEEN PROVIDED. L OB BRAKE OVERHEAT ON TAKE OFF. NO STICKING BRAKES. / DEFERRED L OB BRAKE TEMP SENSOR PER MEL 32-46-01 CAT C. OPTION 3. CW M FUNCTION BY REMOVING AND CAPPING HARNESS AND STOWING CONNECTOR TO ITS SELF AND CAPPING THERMOCOUPLE. REPLACED BRAKE TEMPERATURE PROBE SENSOR ON LH OB MLG BRAKE IAW CRJ 900 AMM 32-46-01-000/400-801. SELF TEST PASSED, NO DEFECTS NOTED. THIS CLEARS MEL."
Part: SKIN — GOUGED (BS 581-597) · airframe 2,970 hrs · 2,666 cycles
DURING OVERNIGHT MAINTENANCE, MX REPORTED A GOUGE ON THE AC SKIN GOUGE LOCATED AT FS581-FS597 STGR20L ÿ½ STGR21L THE GOUGE DIMENSIONS ARE AS FOLLOWS .781"L X .375"W X .0085"D. THE AC SKIN (P/N SH690-33202-19) IS FABRICATED FROM 2024-T3 .150ÿ½, CHEM MILLED DOWN TO .078ÿ½ IN THE DAMAGED AREA. C/W HFEC OF GOUGE ON AC SKIN LOCATED AT FS581-FS597 STGR20L ÿ½ STGR21L IAW CRJ 900 NDT MANUAL 51-21-006 NO DEFECTS NOTED.PERFORMED UT INSPECTION PER CRJ 900 NDTM PART 1 51-20-004-270-A01. PERM REPAIR COMPLIED WITH IAW EA_21-C9-53-230 REV B. 337 SUBMITTED DETAILS ON FILE.
Part: TIRE — FAILED (RT MLG) · airframe 2,705 hrs · 2,433 cycles
CREW REPORTED RH OUTBOARD MLG TIRE BLOWN ON LANDING. REMOVED AND REPLACE RH OB WHEEL ASSEMBLY
2020
Part: GCU — MALFUNCTIONED (NR 1) · airframe 1,305 hrs · 1,159 cycles
DURING CRUISE TO MKE THE CAPT REPORTED A IDG 1, GEN 1, AC BUS 1 MAGENTA FAULT. HE DIVERTED TO DAY PER OUR REQUEST. MX HAD TO TROUBLESHOOT, RE-RACKED IDG 1 AND IDG 2 GENERATOR CONTROL UNIT IAW CRJ 900 AMM. OPS TEST GOOD AT THIS TIME.