N572NN

Part: UNKNOWN — ODOR (CABIN) · airframe 24,245 hrs · 21,362 cycles

FLIGHT ATTENDANTS ADVISED US OF A STRONG SMOKE ODOR IN THE CABIN AROUND ROWS 15 AND 16 PRIOR TO LANDING. C/W FIM 21-22-00-810-806-A01. COULD NOT DUPLICATE.

Part: SELECTOR VALVE — FAULTED (NLG STEERING) · airframe 24,212 hrs · 21,337 cycles

STEERING INOP CAUTION AFTER ROTATION. / REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ-900 FIM 32-51-50-810-801 AND AMM 32-32-10-000/400-801. OPS TEST GOOD AND LEAK TEST GOOD

Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 24,190 hrs · 21,322 cycles

STEERING INOPERATIVE CAUTION MSG 200 FT AFTER T/O. PERFORMED MIPM RESET FAULT EXTINGUISHED.

Part: WINDSHIELD — FAILED (ZONE 200) · airframe 22,610 hrs · 20,088 cycles

FO WINDSHIELD SHATTERED AT 25000FT. / REMOVED AND REPLACED THE RH WINDSHIELD IAW CRJ900 AMM 56-11-01-000/400-801-A01-PSA. OPS TEST GOOD. PRESSURIZATION TEST GOOD.

Part: BUSHING — CORRODED (LH WING) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON BORES OF LUGS (2EAS) AT HINGE NO.4 WAS FOUND AT LH WING TRAILING EDGE. BORES OF LUGS (2EAS) AT HINGE NO.4 WAS FOUND AT LH WING TRAILING EDGE WERE REPAIRED PER PER REO 690-57-51-345 REV. - -

Part: FLOOR SUPPORT — CORRODED (BS 280-295) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON FLOOR SUPPORTS (2EAS) LOCATED BTW FS=280 TO FS=295 AND LBL19'' AND LBL 37'' AT FUSELAGE FLOOR STRUCTURE. FLOOR SUPPORTS (2EAS) LOCATED BTW FS=280 TO FS=295 AND LBL19'' AND LBL 37'' AT FUSELAGE FLOOR STRUCTURE ARE OUT OFF LIMITS PER CRJ-900 SRM 53-21-43-101-001-A03 THEREFORE WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01

Part: FLOOR SUPPORT — CORRODED (BS 280-295) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON FLOOR SUPPORTS (4EAS) LOCATED BTW FS=280 TO FS=295 AND RBL17'' AND RBL 38'', FS=295 AND RBL 4'', FS=319 AND RBL 4'' AT FUSELAGE FLOOR STRUCTURE. FLOOR SUPPORTS (4EAS) LOCATED BTW FS=280 TO FS=295 AND RBL17'' AND RBL 38'', FS=295 AND RBL 4'', FS=319 AND RBL 4'' AT FUSELAGE FLOOR STRUCTURE ARE OUT OFF LIMITS PER CRJ-900 SRM 53-21-43-101-001-A03 THEREFORE WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01

Part: ANGLE — DENTED (FUSELAGE) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON ANGLE LOWER SILL OF GALLEY SERVICE DOOR (FWD) SURROUND STRUCTURE . ANGLE LOWER SILL OF GALLEY SERVICE DOOR (FWD) SURROUND STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01

Part: HINGE FITTING — EXCESS PLAY (VERTICAL STAB) · airframe 20,221 hrs · 18,038 cycles

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

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON RH SIDE SEAT RAILS BTW FS379.00 TO FS581.00 (2EA), FS661+16 TO FS720.85 (2EA), FS744.15 TO FS761.85 (1EA) AND FS785.15 TO FS897.70 (3EA). IDE SEAT RAILS BTW FS379.00 TO FS581.00 (2EA), FS661+16 TO FS720.85 (2EA), FS744.15 TO FS761.85 (1EA) AND FS785.15 TO FS897.70 (3EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-A02, CRJ900 SRM 53-31-49-101-001-A02, CRJ-900 SRM 53-41-49-101-001-A02 AND PER SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49

Part: CANISTER — CRACKED (LT WING) · airframe 20,221 hrs · 18,038 cycles

CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. - -

Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON FLOOR SEAT RAILS, LOCATED BTW FS=661+32 TO FS=693 AND LBL 9'' AND RBL 9''. FLOOR SEAT RAILS, LOCATED BTW FS=661+32 TO FS=693 AND LBL 9'' AND RBL 9'' WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-001-A02 AND SRM 53-41-49-101-001-001-A02 WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12)

Part: CANISTER — CRACKED (RT WING) · airframe 20,221 hrs · 18,038 cycles

CRACK IN CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK. CRACK IN CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. - -

Part: SKIN — NICKED (INBD FLAP) · airframe 20,221 hrs · 18,038 cycles

INITIAL INSPECTION: SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT LH WING. SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT LH WING WERE BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01, EVALUATED, BTW INBOARD FLAP FLS 36.00 TO FLS 65.50 AT LH WING THEREFORE IS WHITHIN OF LIMITS AND BTW LH INBOARD FLAP FLS 15.00 TO FLS 36.00 AT LH WING, THEREFORE IT IS OUT OF LIMITS PER CRJ-900 SRM 57-52-01-101-001-A01 AND REPAIRED PER CRJ-900 SRM 57-52-01-201-005-A01.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON RH SIDE SEAT RAILS BTW FS379.00 TO FS581.00 (2EA), FS661+16 TO FS720.85 (2EA), FS744.15 TO FS761.85 (1EA) AND FS 785.15 TO FS 879.70(3EAS) . SIDE SEAT RAILS BTW FS379.00 TO FS581.00 (2EA), FS661+16 TO FS720.85 (2EA), FS744.15 TO FS761.85 (1EA) AND FS785.15 TO FS897.70 (3EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A02, CRJ900 SRM 53-31-49-101-001-A02, CRJ-900 SRM 53-41-49-101-001-A02 AND PER SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49.

Part: ANGLE — CORRODED (PASSENGER DOOR) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE. FOR EXCESSIVE DAMAGE , ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE IT IS OUT OF LIMITS PER CRJ/900 SRM 53-00-00-101-001-A01 THEREFORE WAS REPLACED PER PER CRJ 900 SRM 51-41-02-001-001-A01

Part: BRACKET — CORRODED (BS 517-661) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON BRACKETS, MACHINED (4EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS-MACHINED (2EAS) FS 517 AND FS 661 BTW STGR 27 TO 26 LH OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND NOT CORROSION FOUND AND BRACKETS, MACHINED (2EAS) FS 565 AND FS 629 BTW STGR 27 TO 26 LH OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE REPLACED PER CRJ-900 SRM 51-42-22-001-001-A01, SRM 51-42-21-001-001-A01 AND AND SRM 51-42-10-001-001-A01.

Part: FLOORBEAM — CRACKED (BS 280 LBL12) · airframe 20,221 hrs · 18,038 cycles

CRACKED CENTER COCKPIT FLOORBEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOORBEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1711 REV

Part: INTERCOSTAL — CORRODED (BS 333-349 S20R) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON INTERCOSTAL AT STGR 20RH BTW FS333.00 TO FS 349.00. INTERCOSTAL AT STGR 20RH BTW FS333.00 TO FS 349.00 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-10-001-001-A01.

Part: FLOORBEAM — CRACKED (BS 280 RBL 12) · airframe 20,221 hrs · 18,038 cycles

CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1712 REV---

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON ANGLE KICKPLATE AT PASSENGER DOOR SURROUND . REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: SKIN — WORN (WING) · airframe 20,221 hrs · 18,038 cycles

WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN. CORRECTIVE ACTION: AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-457 REV - -

Part: SKIN — WORN (WING) · airframe 20,221 hrs · 18,038 cycles

WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-458 REV - -.

Part: SKIN — DAMAGED (BS 1000-1051) · airframe 20,221 hrs · 18,038 cycles

SEVERAL NICKS ON REAR FUSELAGE, BTW FS1000.00 TO FS1051.30 BTW STGR 27 TO STGR 24RH. SEVERAL NICKS ON REAR FUSELAGE, BTW FS1000.00 TO FS1051.30 BTW STGR 27 TO STGR 24RH WAS BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND EVALUATED,BTW 1000.00 TO FS1051.00 & STRG 25RH TO 26RH AND BTW FS1015.00 TO FS1031 & STGR 26RH STGR 27, THEREFORE IT IS WITHIN LIMITS AND AREAS NO DAMAGE ALLOWED BTW FS 1000 TO FS 1047 & STGR24RH TO STGR 25RH AND BTW FS1031 TO FS1047 & STGR 26RH TO STGR 27,THEREFORE IT IS OUT LIMITS PER CRJ-900 SRM 53-61-01-101-003-A02 AND REPAIRED PER REO 690-53-61-1369 REV

Part: DRAG ANGLE — CRACKED (EMPANAGE) · airframe 20,221 hrs · 18,038 cycles

CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). (SM) . LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01.

Part: SKIN — DENTED (FUSELAGE) · airframe 20,221 hrs · 18,038 cycles

DENT ON CANOPY SKIN BTW FS 241.60/FS 247.30 AND BL 0.00/ LBL 5.50. REF ( BTW STGR 2RH /STGR 2LH). NT ON CANOPY SKIN BTW FS 241.60/FS 247.30 AND BL 0.00/ LBL 5.50. REF ( BTW STGR 2RH /STGR 2LH) WAS REPAIRED PER REO 690-53-11-1721 REV -- AND REO 670-51-00-085 REV -A.

Part: SKIN — DENTED (BS 169-202) · airframe 20,221 hrs · 18,038 cycles

DENT ON TOP PANEL SKIN BTW FS 169.00/ FS202.75 AND BL0.00/LBL5.50. REPAIRED PER REO 690-53-11-1720 REV -- AND REO 670-51-00-085 REV - -

Part: BUSHING — CORRODED (RT AILERON) · airframe 20,221 hrs · 18,038 cycles

WEAR ON BORES OF CENTER FITTING LUGS R1 AND R2 WAS FOUND AT RH AILERON. BORES OF CENTER FITTING LUGS R1 AND R2 WAS FOUND AT RH AILERON WERE REPAIRED PER PER REO 670-57-61-237 REV - - NOTES F

Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON FLOOR SEAT RAILS LBL9 AND RBL9 BTW FS 847.00 TO FS 977.00 AT PASSENGER CABIN. FLOOR SEAT RAILS LBL9 AND RBL9 BTW FS 847.00 TO FS 977.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)

Part: SEAT TRACK — CORRODED (BS 349-477) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON SEAT RAIL BTW FS349.00 TO FS477,40 ON RBL9 (1EA) AND SEAT RAIL BTW FS379.00 TO FS485.00 ON LBL9 (1EA).. SEAT RAIL BTW FS349.00 TO FS477,40 ON RBL9 (1EA) AND SEAT RAIL BTW FS379.00 TO FS485.00 ON LBL9 (1EA). WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-001-A01 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 20,221 hrs · 18,038 cycles

CORROSION ON FLOOR SEAT TRACK LOCATED BTW FS=485 TO FS=581 AND LBL 9'' AND RBL 9''. FLOOR SEAT RAILS, WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 20,221 hrs · 18,038 cycles

DISCREPANCY: CORROSION ON FLOOR SEAT RAILS, LOCATED BTW FS=581 TO FS=661+32 AND LBL 9'' AND RBL 9''.

Part: SKIN — PUNCTURED (UNKNOWN) · airframe 18,956 hrs · 16,909 cycles

TUG IMPACT DAMAGE TO R/H SIDE OF NOSE SKIN FS 250 TO FS 265. REPAIRED IAW MHIRJ REO 690-53-11-1587 REV. – DATED 2023-08-16 AND MHIRJ REO 690-53-11-1591 REV. -- DATED 2023-08-25.

Part: STRINGER — DAMAGED (UNKNOWN) · airframe 18,956 hrs · 16,909 cycles

UPON REMOVAL OF PREVIOUS REPAIRS, FOUND STGR13R JUST FWD OF FS265 TO HAVE 1EA ELONGATED HOLE. REPAIRED IAW CRJ 900 SRM 53-00-03-201-001-A02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 18,776 hrs · 16,748 cycles

SMOKE SMELL MID CABIN AND AFT. OPS CHECKS PRODUCED NO NOTICEABLE SMELLS IAW CRJ900 FIM M21-22-00-810-806-A01 CYCLED LEFT AND RIGHT PACK THROUGH VARIOUS TEMPS AND BLEED SOURCES ALL SYSTEMS NORMAL

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 18,375 hrs · 16,421 cycles

STEERING INOP MSG IN FLIGHT WHEN MLG IN TRANSIT. PERFORMED REPACK OF NLG STRUT IAW AMM 32-21-20-000/400-801 USING ALTERNATE TORQUE PROCEDURE AMM 05-51-30-420-801 AT 110 INCH POUNDS. OPS AND LEAK CHECK GOOD. PERFORMED SUCCESSFUL OPS CHECK OF NOSEWHEEL STEERING IAW AMM 32-51-00-710-801

Part: STEP — CRACKED · airframe 18,119 hrs · 16,177 cycles

PAX DOOR TOP STEP PANEL HAS 1EA CRACK ON THE AFT SIDE : REPAIRED DAMAGE IAW CRJ-900 SRM 52-11-04-201-006-A01

Part: DRAG ANGLE — CRACKED · airframe 18,119 hrs · 16,177 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED : : REACOMPLISHED DRAG ANGLE REPAIR IAW CRJ-900 SRM 52-11-04-201

Part: SKIN — DENTED (ZONE 200) · airframe 18,119 hrs · 16,177 cycles

L/H EXTERNAL FUSELAGE SKIN HAS MULTIPLE DENTS BETWEEN FS 193.00 AND FS 202.75 AFT OF TRU BAY DOOR. REMOVED AND REPLACED THE LH EXTERNAL FUSELAGE SKIN BETWEEN FS 193.00 AND FS 202.75 AFT OF TRU BAY DOOR IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, AND PERFORMED AERODYNAMIC CONTOUR MEASUREMENTS IAW CRJ 900 AMM 51-10-00-220-801-A01

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 15,528 hrs · 13,940 cycles

DURING THE FLIGHT THE CREW RECEIVED A CABIN PRESSURE WARNING MESSAGE AND SHORTLY AFTER THE FAS REPORTED THE SMELL OF SMOKE IN THE MAIN CABIN. THE FLIGHT DIVERTED TO IAD AND STILL HAD A STRONG SMOKE SMELL IN THE COCKPIT AND MAIN CABIN AFTER LANDING. THE PAX WERE EVACUATED VIA THE MAIN CABIN DOOR ONTO THE TAXIWAY WHERE THEY WERE TRANSPORTED TO THE TERMINAL. NO INJURIES WERE REPORTED. INFLT EMERGENCY DIVERT-IAD-PRESSURATION ISSUE-SMOKE EVENT-L ENG FIRE BOTTLE DISCHARGED. ALL O2 MASKS DEPLOYED. REPACKED O2 MASKS IAW AMM 35-21-09-860-801, 35-21-13-860-804, 35-21-17-860-803. OPS CHECK GOOD. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER #1 IAW CRJ 900 AMM 21-31-04-000/400-801 OPS CHECK GOOD REMOVED AND REPLACED CABIN PRESSURE CONTROL PANEL IAW CRJ 900 AMM 21-33-01-400-801 AND R&R'D OUTFLOW VALVE IAW CRJ 900 AMM 21-32-01-720-801 OPS CHECK GOOD PRESSURIZED AIRCRAFT WITH APU, LH ENGINE AND RH ENGINE IAW CRJ 900 AMM 21-31-00-910-801 ALL OPS CHECKED GOOD ALL TASKS DONE IAW FIM 21-33-00-810-801

Part: A/C PACK — SMOKE (200) · airframe 15,284 hrs · 13,747 cycles

L PACK AUTOFAIL CAUTION MSG ACCOMPANIED BY L PACK FAULT STATUS MSG AND SMOKE IN CABIN. FOUND LH PACK TO SMOKE DEFERRED COCKPIT TEMP CONTROL SYS. REMOVED AND REPLACED LH ACM IAW CRJ 900 AMM 21-51-08-000/400-801. OPS CHECK GOOD. LEAK CHECK GOOD

Part: SKIN — DENTED (ZONE 100) · airframe 13,404 hrs · 12,166 cycles

DURING ROUTINE OVERNIGHT MAINTENANCE IN PENSACOLA, FL (PNS), MAINTENANCE NOTED THAT THERE IS A DENT COMMON TO THE FUSELAGE SKIN BETWEEN FS 245, AND BETWEEN STRINGERS 22L AND 23L. THE DENT MEASURES .780Ï¿½ LONG X .330Ï¿½ WIDE X .035Ï¿½ DEEP. ITÏ¿½S WIDTH TO DEPTH RATIO (W/D) IS 9.42, AND IT IS 1.14Ï¿½ FROM THE CLOSEST FASTENER LINE. PERFORMED EA 21-C9-53-055 SECTION I, ITEMS 1-3, 5-6 DVI OF DENT IN FUSELAGE.PERFORMED EA 21-C9-53-055 SECTION I, ITEM 4 EDDY CURRENT INSPECTION IN ACCORDANCE WITH NDTM 51-20-006. NO CRACKS FOUND. COMPLETED FAA FORM 337.

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · corrosion level 2 · airframe 12,469 hrs · 11,320 cycles

FS 280 J-ANGLE LOCATED AT FLIGHT DECK ENTRANCE IS CORRODED AT 2 PLACES ON UPPER SURFACE. REMOVED FS 280 J-ANGLE AND INSTALLED NEW SERVICEABLE FS 280 J-ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: DRAG ANGLE — CRACKED (VERTICALS TAB) · airframe 12,469 hrs · 11,320 cycles

LEFT VERTICAL STAB AFT DRAG ANGLE APPEARS CRACKED. REMOVED, LOCATED AND DRILLED AND INSTALLED NEW SERVICEABLE L/H V-STAB AFT DRAG ANGLE IAW CRJ900 SRM 51-42-13-001-001-A01

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 12,469 hrs · 11,320 cycles

RIGHT VERTICAL STAB AFT DRAG ANGLE APPEARS CRACKED. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE R/H VERTICAL STAB AFT DRAG ANGLE IAW CRJ900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 11,281 hrs · 10,267 cycles

ALL 4 EMERGENCY BATTERIES NEED REPLACED DUE TO BEING LEFT ON. MAINTENANCE REMOVED AND REPLACED ALL 4 BATTERY PACKS OPS CHECK GOOD. ALL BATTERY P/N THE SAME S/N #2 104602 S/N #3 115010 S/N #4 125185

Part: WINDOW — ARCED (COCKPIT) · airframe 11,281 hrs · 10,267 cycles

CREW REPORTED SMOKE IN THE COCKPIT DURING FLIGHT, DELCARED EMERGENCY AND DIVERTED TO GSP, PASSENGERS DEPLANED VIA MAIN CABIN DOOR ON RUNWAY. CREW USED A FIRE EXTINGUISHER ON THE COCKPIT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS SIDE WINDOW AND OPS CHECKED IT GOOD

Part: UNKNOWN — SMOKE (CABIN) · airframe 10,697 hrs · 9,735 cycles

FLIGHT RETURNED TO THE GATE FOR A RARV FAULT STATUS MESSAGE. SMOKE STARTED FILLING THE CABIN DURING THE RESET ATTEMPT. THE CREW RAN THE QRH PERFORMED OPS CHECK IAW AMM 21-52-04-710-801. OPS CHECKED GOOD.1-3 C"

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 10,384 hrs · 9,450 cycles

MX FOUND LH FWD EXTERNAL EMERGENCY LIGHT INOP. R/R LH FWD EXTERNAL EMERGENCY LIGHT. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,082 hrs · 9,192 cycles

NR 2 POWER SUPPLY BATTERY FAILED OPS CHECK. R & R THE NR 2 BATTERY POWER SUPPLY IAW AMM 33-51-17-000/400-801

Part: WIRE HARNESS — UNSECURE (ANTI-ICE SYSTEM)

CREW RECEIVED WING ANTI-ICE CAUTION MESSAGE. THEY DECLARED AN EMERGENCY AND RETURNED TO CLT. MAINTENANCE RESECURED THE WIRE BUNDLE FOR THE INBOARD WING ANTI-ICE TEMP SENSOR. OPS CHECK GOOD

Part: SPOILER SYS — MALFUNCTIONED · airframe 7,332 hrs · 6,720 cycles

ON ARRIVAL, THE OUTBOARD SPOILERON AND OUTBOARD FLIGHT SPOILERS, LEFT AND RIGHT, FAILED. AN EMERGENCY WAS DECLARED. LANDED SAFELY, TAXIED TO THE GATE AND PERFORMED A SYSTEM RESET WITH MAINTENANCE AND RESOLVED THE ISSUE.

Part: A/C PACK — SMOKE (RIGHT) · airframe 7,178 hrs · 6,568 cycles

WHEN THE AIRCRAFT WAS ENROUTE TO THE DE-ICE PAD, THE AIRCRAFT EXPERIENCED SMOKE IN THE CABIN. PERFORMED AN EMERGENCY EVACUATION ON THE RUNWAY. MAINTENANCE INSPECTED AND FOUND THE RIGHT PACK CAUSING THE SMOKE. OPEN

Part: DISPLAY — FAULTED (MAIN FLIGHT) · airframe 3,665 hrs · 3,321 cycles

MAIN FLIGHT DISPLAY UNIT BLANKED OUT DURING FLIGHT. THE CREW DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, RESET SYSTEM CIRCUIT BREAKERS AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHT) · airframe 1,448 hrs · 1,327 cycles

AFT CENTER AISLE EMERGENCY LIGHT INOPERATIVE. FOUND AN UNSEATED CONNECTOR. SEATED THE CONNECTOR, PERFORMED OPS CHECK OF LIGHTS IAW AMM 33-51-00-710-801 AO1 OPS CHECK GOOD.