N608NN

ATA 5347

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).

ATA 5347

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)."

ATA 5313

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

ATA 5330

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

ATA 5330

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

ATA 5344

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

ATA 3240

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."

ATA 5330

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 Ï¿½ 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 .150Ï¿½, CHEM MILLED DOWN TO .078Ï¿½ IN THE DAMAGED AREA. C/W HFEC OF GOUGE ON AC SKIN LOCATED AT FS581-FS597 STGR20L Ï¿½ 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.

ATA 3244

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

ATA 2424

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.