N582NN

Part: WINDSHIELD — FIRE (ZONE 200) · airframe 21,035 hrs · 18,770 cycles

FRONT RIGHT WINDSHIELD SEALANT CAUGHT FIRE AT THE GATE, WINDSHIELD SHATTERED AS A RESULT. [WINDSHIELD HEAT HAD BEEN LEFT IN LOW POSITION FOR THE REPO FROM HANGAR]. NO MEDICAL ATTENTION WAS REPORTED. / PERFORMED INSTALLATION OF THE R/H WINDSHIELD AS REQUIRED IN ACCORDANCE WITH AMM 56-11-01-400-801-A01-PSA. OPS AND LEAK CHECKS GOOD AT THIS TIME.

Part: SENSOR — ABNORMAL (WING OVHT WARNIN) · airframe 20,577 hrs · 18,344 cycles

WING OVHT WARNING MSG INTERMITTENT IN FLIGHT. / INSP RH INBD TEMP SENSOR AND FOUND 1 PIN NOT SECURE. INSTALLED PIN IAW AMM 30ˆ’12ˆ’06ˆ’400ˆ’801 OPS CHECK GOOD.

Part: PRESSURE SYSTEM — UNSERVICEABLE (200) · airframe 20,455 hrs · 18,235 cycles

CABIN ALTITUDE WARNING MESSAGE AT 24000FT / REMOVED AND REPLACED BOTH CABIN PRESSURE CONTROLLERS IAW CRJ 900 AMM 21-31-04-000/400-801. REMOVED AND REPLACED CABIN PRESSURE CONTROL PANEL IAW CRJ 900 AMM 21-33-01-000/401-801. OPS TEST GOOD. PERFORMED OPS TEST OF OUTFLOW VALVE IAW CRJ 900 AMM 21-32-01-720-801, VALVE OPENED AND CLOSED .OPS CHECK GOOD. PERFORMED OPS TEST OF SAFETY VALVE IAW CRJ 900 AMM 21-32-03-720-801 , VALVE OPENED AND CLOSED OPS CHECK GOOD REMOVED AND REPLACED JB10 PCB 1 IAW CRJ 900 AMM 24ˆ’05ˆ’03ˆ’000/400ˆ’801. PERFORMED OPS CHECKS IAW CRJ 900 AMM 24ˆ’05ˆ’03ˆ’710ˆ’801-A04 EXCEPT FOR 4A5 AND 4A15. REMOVED AND INSTALLED JB11 PCB 2 IAW CRJ 900 AMM 24ˆ’06ˆ’05ˆ’000/400ˆ’801. PERFORMED OPS CHECKS OF JB10 PCB 1 AND JB11 PCB2 IAW AMM 24-06-05-710-801 AND AMM 24-05-03-710-801. OPS CHECK GOOD.

Part: FRAME — CORRODED (BS 349 S25-26L) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON FRAME FS= 349 BETWEEN STRG 26LH TO 25RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS= 349 BETWEEN STRG 26LH TO 25RH AT MAIN AVIONICS COMPARTMENT.

Part: FITTING — CORRODED (GALLEY 1 PAX CAB) · airframe 19,187 hrs · 17,145 cycles

MANUFACTURING PART. IN REFERENCE NRC 00169: FABRICATE PN: A661091-1 (FLOOR FITTING ) 1EA IN ACCORDANCE WITH EA NO: A1-690-25-00209. FITTING (1 EA) WAS MANUFATURED PN: A661091-1 PER EA Nº: A1-690-25-00209 REV. ORIGINAL

Part: STRAP — CORRODED (PAX DOOR FRAME) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON STRAP, INNER FS 349.00 AND STGR 17LH AT PASSENGER DOOR SURROUND STRUCTURE. FITTING WAS FOUND OUT OFF LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01

Part: SKIN — CORRODED (FUSELAGE) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON DOOR CUT-OUT INNER SKIN AT E/E MAIN COMPARTMENT. CORROSION ON DOOR CUT-OUT INNER SKIN AT E/E MAIN COMPARTMENT WAS REMOVED AND WAS EVALUATED WITHIN LIMITS PER REO 690-53-21-032 REV. --

Part: STRAP — CORRODED (BS 320 S17R) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON STRAP, INNER FS 319.70 AND STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE. STRAP, INNER FS 319.70 AND STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE WAS REPAIRED PER REO 690-53-21-1774 REV - -

Part: SEAT TRACK — CORRODED (BS 349-477) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON SEAT RAIL BTW FS 349.00 TO FS 477.40 RBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 349.00 TO FS 477.40 RBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)

Part: FLOORBEAM — CRACKED (FLIGHT COMPARTME) · airframe 19,187 hrs · 17,145 cycles

CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR BEAM RBL 12 AT FS280.00 FLOOR INTERNAL SUPPORT STRUCTURE WAS REPAIRED PER REO 690-53-11-1758 REV. --

Part: SEAT TRACK — CORRODED (BS 364-477) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON SEAT RAIL BTW FS 364 TO FS 477.40 LBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 364 TO FS 477.40 LBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)

Part: SEAT TRACK — CORRODED (BS 744-762) · airframe 19,187 hrs · 17,145 cycles

CORROSION AT SIDE SEAT RAIL OF STRG 15LH/RH BETWEEN FS744.15 - FS 761.85. EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)

Part: SKIN — ERODED (RT NR 3 SLAT) · airframe 19,187 hrs · 17,145 cycles

EROSION ON LEADING EDGE AT SLAT 3 OF THE RH WING. LEADING EDGE AT SLAT 3 OF THE RH WING WAS REPAIRED PER REO 690-57-42-1066 REV. --

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON INTERCOSTALS (2 EAS) BTW STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. INTERCOSTALS (2 EAS) BTW STA. FS= 349 TO FS= 364 NEAR STGR 27 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01

Part: SEAT TRACK — CORRODED (BS 699-721) · airframe 19,187 hrs · 17,145 cycles

CORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS699.40 - FS 720.85. SIDE SEAT RAIL OF STRG 15LH BETWEEN FS699.40 - FS 720.85 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)

Part: FLOORBEAM — CRACKED (FLIGHT COMPARTME) · airframe 19,187 hrs · 17,145 cycles

CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM LBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE WAS REPAIRED PER REO 690-53-11-1758 REV. --

Part: HINGE FITTING — EXCESS PLAY (VERTICAL STAB) · airframe 19,187 hrs · 17,145 cycles

FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL #2103 REV. B.

Part: PLATE — CORRODED (FWD BAG BAY) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON JOINT PLATE FS 519.64 OF FWD BAGGAGE BAY DOOR SURROUND STRUCTURE AT FWD CARGO COMPARTMENT. JOINT PLATE FS 519.64 OF FWD BAGGAGE BAY WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-23-001-001-A02, AND WAS REPLACED PER CRJ900 SRM 51-42-22-001-001-A01

Part: SEAT TRACK — CORRODED (BS 477-669) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON SEAT RAIL BTW FS 477.40 TO FS 669.00 RBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 477.40 TO FS 669.00 RBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)

Part: ARM — GOUGED (FWD CARGO DOOR) · airframe 19,187 hrs · 17,145 cycles

CTR BAGGAGE BAY DOOR FWD INNER ARM WITHIN 1384.3 FHS FROM IR (BEFORE 19,227.08 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. CTR BAGGAGE BAY DOOR FWD INNER ARM WAS REPAIRED PER REO 690-52-35-411 REV. - - IN REFRENCE TO EA 23-C9-52-1419 REV. IR SECTION III PERMANENT REPAIR

Part: ACCESS PANEL — CRACKED (FAIRING) · airframe 19,187 hrs · 17,145 cycles

CRACK IN ACCESS PANEL 171CL. ACCESS PANEL 171CL WAS REPAIRED PER REO 670-53-82-430. REV--

Part: SEAT TRACK — CORRODED (BS 477-581) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON SEAT RAIL BTW FS 477.40 TO FS 581 LBL 9.00 AT CABIN PAX. SEAT RAIL BTW FS 477.40 TO FS 581 LBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)

Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON SEAT RAILS (SEVERAL LOCATIONS) LBL 9 AND RBL 9 BTW FS 874.00 TO FS 977.00 AT PASSENGER CABIN. PER CRJ900 SRM 53-51-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)

Part: STRAP — CORRODED (FWD BAG BAY) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON STRAP OF FLOOR STRUCTURE FS 581.00 BTW STGR 24RH TO STGR 27 AT FWD CARGO COMPARTMENT. STRAP OF FLOOR STRUCTURE FS 581.00 BTW STGR 24RH TO STGR 27 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01, WAS FABRICATED PER DWG: SH670-33320 REV: B AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 19,187 hrs · 17,145 cycles

CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE WAS REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01

Part: RIB — CRACKED (LH WING) · airframe 19,187 hrs · 17,145 cycles

CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. WING RIB AT FLS 168.07 AT WING TRAILING EDGE OF LH WING WAS REPAIRED PER REO 690-57-51-354 REV. --

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 19,187 hrs · 17,145 cycles

CORROSION AT SIDE SEAT RAIL OF STRG 15LH/RH BETWEEN FS785.15 FS - 847+8.40. CORROSION AT SIDE SEAT RAIL OF STRG 15LH/RH BETWEEN FS785.15 FS - 847+8.40. WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 19,187 hrs · 17,145 cycles

CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE WAS REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01

Part: WEB — CRACKED (FWD EE BAY) · airframe 19,187 hrs · 17,145 cycles

CRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB. UPPER WEB OF ADG COMPARTMENT WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01.

Part: MOUNT — CRACKED (REFUEL DUCT) · airframe 19,187 hrs · 17,145 cycles

AFTER REMOVAL OF LOWER FUSELAGE FAIRINGS, CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM) AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM) WAS REPAIRED PER REO 690-28-25-019 REV.- -

Part: BRACKET — CORRODED (FWD BAGGAGE BAY) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. CORROSION ON BRACKETS, MACHINED (7EAS) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-01; CRJ900 SRM 51-42-20-001-001-A01; CRJ900 SRM 51-42-22-001-001-A01 AND CRJ900 SRM 51-42-13-001-001-A01

Part: PLATE — CORRODED (FWD BAGGAGE BAY) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON PLATES (BL0) (2EAS) PLATE 1 BTW FS 517.00 STGR 27. PLATE 2 BTW FS565.00 STGR 27. AT FWD CARGO COMPARTMENT. STRINGER 27 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE FABRICATED PER (EO) SH670-3337, AND WERE REPLACED PER (EO) SH670-33600 AND CRJ900 SRM 51-42-06-001-001-A01

Part: FLOOR SUPPORT — CORRODED (CABIN PAX) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON FLOOR SUPPORTS (4EAS) LOCATED BTW FS=280 TO FS=295 AND RBL17'' AND RBL 38'', FS=295 AND LBL20'', FS=310 AND LBL37'' AT FUSELAGE FLOOR STRUCTURE. CORROSION ON FLOOR SUPPORTS (4EAS) AT FUSELAGE FLOOR STRUCTURE WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-43-101-001-A03 AND WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01.

Part: HINGE — CORRODED (LH WING) · airframe 19,187 hrs · 17,145 cycles

CORROSION ON HOUSING OF HINGE FITTING 2 (OUTBD AND INBD) FITTING 3 (INBD) AT LH WING REAR SPAR WAS FOUND. HOUSING OF HINGE FITTING 2 (OUTBD AND INBD) FITTING 3 (INBD) AT LH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-357 REV. - - AND ETI-900-24-004 REV. ORIGINAL

Part: HINGE — CORRODED (LT WING AILERON) · airframe 19,187 hrs · 17,145 cycles

CENTER FITTING BORE LUG L1, L2, L5 AND L6 AT LH AILERON. CENTER FITTING BORE LUG L1, L2, L5 AND L6 AT LH AILERON.

Part: SKIN — WORN (LH WING) · airframe 19,187 hrs · 17,145 cycles

WEAR ON LOWER SKIN OF SETTLEMENT AREA OF ACCESS PANELS 583AB, 586AB, 592AB AND 597AB AT LH WING. LOWER SKIN OF SETTLEMENT AREA OF ACCESS PANELS 583AB, 586AB, 592AB AND 597AB AT LH WING WAS REPAIRED PER REO 690-57-21-471. REV. - -

Part: HINGE — CORRODED (RT WING AILERON) · airframe 19,187 hrs · 17,145 cycles

CENTER FITTING BORE LUG R1, R2, R5 AND R6 AT RH AILERON. CENTER FITTING BORE LUG R1, R2, R5 AND R6 AT RH AILERON WERE REPAIRED PER REO 670-57-61-237 REV--

Part: LUG — SCRATCHED (RH WING) · airframe 19,187 hrs · 17,145 cycles

HOUSING OF HINGE FITTING 1 (OUTBD), FITTING 3 (OUTBD AND INBD) & FITTING 4 (OUTBD AND INBD) AT RH WING REAR SPAR WAS FOUND. HOUSING OF HINGE FITTING 1 (OUTBD), FITTING 3 (OUTBD AND INBD) & FITTING 4 (OUTBD AND INBD) AT RH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-356 REV -- AND ETI-900-24-005 REV. ORIG

Part: SKIN — DAMAGED (BS 295-693) · airframe 19,187 hrs · 17,145 cycles

LIGHTNING STRIKES (14 EAS) ON FUSELAGE SKIN AT FS 295 TO FS 693 BTW STGR 23RH TO STGR 14RH. LIGHTNING STRIKES (14 EAS) ON FUSELAGE SKIN AT FS 295 TO FS 693 BTW STGR 23RH TO STGR 14RH WERE REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03 AND REO 690-53-21-1769 REV --

Part: LUG — CORRODED (RT AILERON) · airframe 19,187 hrs · 17,145 cycles

SCRATCH ON HOUSING OF LUG 1, LUG 2 AND LUG 6 AT RH AILERON WAS FOUND. SCRATCH ON HOUSING OF LUG 1, LUG 2 AND LUG 6 AT RH AILERON WAS FOUND WERE REPAIRED PER REO 670-57-61-237 REV - - NOTES F

Part: LUG — CORRODED (LH WING) · airframe 19,187 hrs · 17,145 cycles

SCRATCH ON HOUSING OF LUG 2 AND LUG 5 AT LH AILERON WAS FOUND. SCRATCH ON HOUSING OF LUG 2 AND LUG 5 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV - - NOTES F

Part: LUG — SCRATCHED (LH WING) · airframe 19,187 hrs · 17,145 cycles

HOUSING OF HINGE FITTING 1 (OUTBD) FITTING 4 (OUTBD AND INBD) AT LH WING REAR SPAR WAS FOUND. HOUSING OF HINGE FITTING 1 (OUTBD) FITTING 4 (OUTBD AND INBD) AT LH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-357 REV. - -

Part: ARM — GOUGED (FWD CARGO DOOR) · airframe 19,187 hrs · 17,145 cycles

CTR BAGGAGE BAY DOOR AFT INNER ARM WITHIN 1384.3 FHS FROM IR (BEFORE 19,227.08 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. CTR BAGGAGE BAY DOOR AFT INNER ARM WAS REPAIRED PER REO 690-52-35-412 REV. - - IN REFRENCE TO EA 23-C9-52-1420 REV. IR SECTION III PERMANENT REPAIR

Part: SENSOR — MALFUNCTIONED (LT BRAKE TEMP) · airframe 17,374 hrs · 15,560 cycles

LHIB BRAKE OVHT WARNING MSG AFTER T/O., BTMS INDICATION WOULD RADOMLY DASHOUT START AFTER GEAR RETRACTION AND CONTINUED WITH GEAR EXTENDED. REMOVED AND REPLACED LHIB MLG BRAKE TEMP SENSOR IAW CRJ 900 AMM 32-46-01-000/400-801-A01-PSA. NO FURTHER DEFECTS NOTED AT THIS. THERMOCOUPLE SELF TEST GOOD. THIS CLEARS MEL.

Part: BRAKE — OVERHEATED · airframe 13,927 hrs · 12,555 cycles

DURING LANDING THE CREW GOT A BREAK TEMP OVER HEAT MESSAGE. A EMERGENCY WAS DECLARED BY THE CREW AND TRUCKS DID ROLL IN BUT NOT NEEDED. THE CREW DID NOT CALLED FOR A BRACE ON LANDING. THE AIRCRAFT WAS ABLE TO TAXI TO A GATE UNDER THEIR OWN POWER. NO FURTHER INFORMATION HAS BEEN GIVEN. BRAKE OVHT MSG ON TAKEOFF OUT OF KMDT AND ON ARRIVAL INTO KCLT. LH OB TEMP ERRATIC / DEFERRED PER MEL 32-46-1(7).

Part: IDG — FAULTED (RIGHT) · airframe 13,410 hrs · 12,116 cycles

CREW HAD AN IDG CAUTION MESSAGE INFLIGHT AND RAN THE QRH. CREW MADE THE DECISION TO DIVERT TO CAK AS IT WAS A MX BASE AND COULD LIKELY DEAL WITH THE ISSUE BETTER THAN AN OUTSTATION. IDG 2 CAUTION MESSAGE IN FLIGHT. QRH RUN IDG 2 DISCONNECT PUSHED. / DEF IDG 2 PER MEL 24-11-01-2 CAT A. REMOVED AND REPLACED R/H ENGINE IDG ASSEMBLY IAW CRJ900 AMM 24-11-01-000/400-801-A01. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME.

Part: IDG — FAULTED (RIGHT) · airframe 13,410 hrs · 12,116 cycles

CREW HAD AN IDG CAUTION MESSAGE INFLIGHT AND RAN THE QRH. CREW MADE THE DECISION TO DIVERT TO CAK AS IT WAS A MX BASE AND COULD LIKELY DEAL WITH THE ISSUE BETTER THAN AN OUTSTATION. IDG 2 CAUTION MESSAGE IN FLIGHT. QRH RUN IDG 2 DISCONNECT PUSHED. / DEF IDG 2 PER MEL 24-11-01-2 CAT A. REMOVED AND REPLACED R/H ENGINE IDG ASSEMBLY IAW CRJ900 AMM 24-11-01-000/400-801-A01. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME.

Part: ANGLE — CORRODED (BS 280) · corrosion level 2 · airframe 11,227 hrs · 10,201 cycles

FS 280.00 FORWARD "J" ANGLE IS CORRODED. INSTALLED NEW SERVICEABLE FS 280 J ANGLE, IAW CRJ 200 900 SRM 51-42-06-001-001-A01 AND 42-21-001-010-A01.

Part: COMPUTER — MALFUNCTIONED (FUEL QTY) · airframe 9,745 hrs · 8,900 cycles

THERE WAS A FUEL SPILL FROM BOTH SIDE OVERFLOWS DURING FUELING. FIRE TRUCKS DID RESPOND. PERFORMED GVI OF FUEL SPILL, AND INSPECTED FOR ACTIVE LEAKS. NO DEFECTS FOUND. DURING ATTEMPT TO REFUEL AGAIN FOUND THAT CENTER TANK DOESNÏ¿½T TAKE FUEL. DEFFERED CENTER TANK REFUEL SHUT OFF VALVE. INTERROGATED MDC. FOUND B1 CODE 006805. T/S PER FIM. FQGC UNSERVICEABLE. NO RELATED CODES STORED IN REFUEL/DEFUEL PANEL. REMOVED AND REPLACED FUEL QUANTITY GAUGING COMPUTER IAW CRJ900 AMM. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 8,175 hrs · 7,466 cycles

DURING CLIMB OUT OF 8000 FEET JUST AFTER TAKE OFF CREW REPORTED THAT THE FIRST OFFICERS WINDSHIELD SHATTERED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED THE RH WINDSHIELD, OPS CHECK GOOD.

Part: CONTROL LEVER — MALFUNCTIONED (MLG) · airframe 6,179 hrs · 5,659 cycles

DURING TAKE OFF, THE CREW RECEIVED A GEAR DISAGREE MESSAGE. DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. MAINTENANCE DEFERRED THE LANDING GEAR RETRACTION SYSTEM. MX REMOVED AND REPLACED LANDING GEAR CONTROL PANEL LEVER. OPS CHECK GOOD THIS CLEARS MEL

Part: ACM — FAULTY · airframe 2,041 hrs · 1,835 cycles

CABIN FILLED WITH HAZE AND BURNING ODOR, FOLLOWED BY RIGHT PACK AUTO FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE AIR CYCLE MACHINE, AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.