N468CA

Part: WARNING MESSAGE — ILLUMINATED (LT A/C PACK)

LEFT PACK HI PRESS AFTER TAKEOFF WHEN SWAPPING BLEEDS. FILED CLOSED RO 9/26/2020. DEFERRED LT PACK, PER MEL, DUE TO RT PACK BEING ALREADY DEFERRED. MAINT ACTION COMPLIED WITH. PLACARD INSTALLED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

UPON REMOVAL FOR FOM FOUND CRACK IN ANGLE - FS280.00 STGR3L. (C-CHECK) RO 3/26/2020 REMOVED AND INSTALLED NEW ANGLE AT FS 280.00 STGR 3L REF. BOMBARDIER DWG. CRJ 200 SRM & COMPLIED WITH TASK CARD.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

FS280.00 AT STGR 3L, OUTBOARD STRINGER SPLICE ANGLE IS CRACKED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS280 STR3L OTBD SPLICE ANGLE REF CRJ200 SRM, BOMBARDIER DRAWING. COMPLIED WITH ST, LEAK CHECKS GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

FS280 BEAM/FLOOR SUPPORT BEAM CLIP CRACKED, I/B RBL9. (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED FS 280 FLOOR BEAM CLIP AT INBD AT RBL9 WITH NEW CLIP REF REO. SEE CONTINUE CARD FOR FUTHER DTAILS COMPLIED WITH.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

FS280 BEAM/FLOOR SUPPORT BEAM CLIP CRACKED, O/B RBL9. (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED FS 280 FLOOR BEAM CLIP AT OTBD AT RBL9 WITH NEW CLIP REF REO. SEE CONTINUE CARD FOR FUTHER DTAILS COMPLIED WITH.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

FS280 BEAM/FLOOR SUPPORT BEAM CLIP CRACKED, O/B LBL9. (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED FS 280 FLOOR BEAM CLIP AT OTBD AT LBL9 WITH NEW CLIP REF REO 601R-53-11-926 REV -B DATED 2006-05-10. SEE CONTINUE CARD FOR FUTHER DTAILS. COMPLIED WITH 51-900-1003-SKY.

Part: POST — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

FS409+128 LBL27 VERTICAL POST CRACKED AT THE INBOARD AFT LOWER RIVET. (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS409+128 LBL27 VERTICAL POST REF BOMBARDIER REO. COMPLIED WITH ST, LEAK CHECKS GOOD.

Part: POST — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

FS409+128 LBL18 VERTICAL POST CRACKED AT THE OUTBOARD AFT LOWER RIVET (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS409+128 LBL18 VERITCAL POST REF BOMBARDIER REO. COMPLIED WITH ST, LEAK CHECKS GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

FS280 BEAM/FLOOR SUPPORT BEAM CLIP CRACKED, I/B LBL9.REMOVED AND REPLACED FS 280 FLOOR BEAM CLIP AT INBD AT LBL9 WITH NEW CLIP REF REO 601R-53-11-926 REV -B DATED 2006-05-10. SEE CONTINUE CARD FOR FUTHER DTAILS COMPLIED WITH 51-900-1003-SKY.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

FS280.00 AT STGR 3L, INBOARD STRINGER SPLICE ANGLE IS CRACKED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS280 STR3L INBD SPLICE ANGLE REF CRJ200 SRM, BOMBARDIER DRAWING. COMPLIED WITH ST, LEAK CHECKS GOOD.

Part: POST — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

FS409+128 RBL27 VERTICAL POST CRACKED AT THE INBOARD AFT LOWER RIVET. (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS409+128 RBL27 VERTICAL POST REF BOMBARDIER REO. COMPLIED WITH ST, LEAK CHECKS AND OP CHECKS GOOD.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

PRESSURE BILKHEAD AFT OF F/S 621.0 STIFFENER P/N 601R36008-51 IS CRACK (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS621 STIFFENER REF BOMBARDIER DRAWING. COMPLIED WITH ST. LEAK CHECKS GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

FLOOR SEAT RAIL RBL9 FS399-FS409+128 HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED FLOOR SEAT RAIL FS399 - FS409+128 RBL9 REF CRJ200 AMM

Part: FLOORBEAM — OUT OF LIMITS (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

INBOARD FLANGE OF RBL9 FLOOR BEAM CAP AT FS409+71 FOUND TO BE OUT OF LIMITS ON JOB 2764961 OP 298 CAMP# 20550130, AND REQUIRES REPAIR.REPAIRED INBOARD FLANGE OF RBL9 FLOOR BEAM CAP AT FS409+71 REF. CRJ 200 SRM. TASK CARD COMPLIED WITH.

Part: FLOORBEAM — OUT OF LIMITS (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

INBOARD FLANGE OF RBL9 FLOOR BEAM CAP AT FS409+5-FS409+26 FOUND TO BE OUT OF LIMITS ON JOB 2764961 OP 298 CAMP# 20550130, AND REQUIRES REPAIR. (C-CHECK) RO 3/26/2020 REPAIRED RBL9 FLOOR BEAM CAP AT FS409+5-FS409+26 REF. CRJ 200 SRM REPAIR. TASK CARD COMPLIED WITH.

Part: FLOORBEAM — OUT OF LIMITS (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

INBOARD FLANGE OF RBL9 FLOOR BEAM CAP AT FS409+98-FS409+104 FOUND TO BE OUT OF LIMITS ON JOB 2764961 OP 298 CAMP# 20550130, AND REQUIRES REPAIR. (C-CHECK) RO 3/26/2020 REPAIRED INBOARD FLANGE OF RBL9 FLOOR BEAM CAP AT FS409+98-FS409+104 REF. CRJ 200 SRM. TASK CARD COMPLIED WITH.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

*CORROSION SUPPORT ANGLES CORRODED AT FASTENER LOCATIONS ON INBD SIDE OF FLOORBEAM FROM FS 409.00 - 406.00+96 ST LBL 9 (MARKED)REMOVED AND INSTALLED NEW FLOOR BEAM FROM 409.00 - 409 +96 AT LBL 9 REF, BOMBARDIER DWG. CRJ 200 SRM. COMPLIED WITH TASK CARD

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

*CORROSION SUPPORT ANGLES CORRODED AT FASTENER LOCATIONS ON INBD SIDE OF FLOORBEAM FROM FS 409.00 - 406.00+96 AT RBL 9 (MARKED) (C-CHECK) RO 3/26/2020 CORROSION ON RBL9 FLOOR BEAM INBOARD FLANGE FOUND TO BE OUT OF LIMITS REF. CRJ 200 SRM. REFERENCE THE FOLLOWING CAMP'S FOR REPAIRS ON THE INBOARD FLANGE OF THE RBL 9 FLOOR BEAM CAP AT 3 EA. LOCATIONS: / CAMP# 20587077 - FS409+5-FS409+26 / CAMP# 20587098 - FS409+71 / CAMP# 20587115 - FS409+98-FS409+104 / NO ADDITIONAL DAMAGE ON FLOOR BEAM INBOARD FLANGE FROM FS409+5-FS409+128.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

*FS 333 AT STR 1R FRAME CRACKED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS333 FRAME STR1R REF CRJ200 SRM, SRM, BOMBARDIER DRAWING. COMPLIED WITH ST, LEAK CHECKS GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

*CORROSION AROUND HOLE ON LH FLOOR SUPPORT BEAM AT FS 349.00, BL 20 (MARKED) (C-CHECK) RO 3/26/2020 COMPLIED WITH PERMANENT REPAIR CORROSION AROUND HOLE ON LH FLOOR SUPPORT BEAM AT FS 349.00, BL 20 REF REO, VERIFIED ALL STEPS COMPLIED WITH, COMPLETED TASK CARD , ALL CHECKS OKAY

Part: FORMER — CORRODED (PAX DOOR) · airframe 38,214 hrs · 37,252 cycles

FOUND CORROSION ON PAX DOOR AFT FORMER. (C-CHECK) RO 3/26/2020 --BLENDED CORROSION ON THE PAX DOOR AFT FORMER "OUT OF LIMITS" REF CRJ200 SRM (ORIGINAL: .063) - (REMAINING: .058) - (LOSS: .005). --REMOVED AND REPLACED PAX DOOR AFT FORMER REF CRJ200 SRM, BOMBARDIER DRAWING. COMPLIED WITH ST, LEAK CHECKS GOOD.

Part: SKIN — CRACKED (RT WING) · airframe 38,214 hrs · 37,252 cycles

RH WING PLANK ACCESS HOLE FOR PANEL 650BB IS CRACKED ON INNER EDGE. (C-CHECK) RO 3/26/2020 BLENDED CORROSION AT RH WING PLANK ACCESS HOLE 650BB REF BOMBARDIER REO, REO. ROTO PEENED AND RESTORED FINISH. ALL CHECKS GOOD. COMPLETED TASK CARD, WEIGHT CHANGE NEGLIGIBLE DUE TO REPAIR BEING BLEND ONLY

Part: HINGE ARM — CRACKED (ESCAPE HATCH) · airframe 38,214 hrs · 37,252 cycles

* CREW ESCAPE HATCH HAS SUSPECT CRACK AT HINGE ARM.(MARKED) (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED HINGE ARM REF SRM

Part: HINGE — CHAFED (RUDDER) · airframe 38,214 hrs · 37,252 cycles

*RUDDER UPPER CENTER HINGE CHAFFED ON RUDDER SIDE (C-CHECK) RO 3/26/2020 BLENDED THE CHAFFED AREA OF THE RUDDER UPPER CENTER HINGE, NDT'ED REPAIR, ROTO PEENED THE HINGE AND RESTORE THE FINISH. COMPLIED WITH ALL STEPS OF REO.REF REO.

Part: HINGE FITTING — CHAFED (RUDDER) · airframe 38,214 hrs · 37,252 cycles

*RUDDER UPPER CENTER HINGE ON ACFT SIDE CHAFFED (C-CHECK) RO 3/26/2020 BLENDED CHAFE ON UPPER CENTER RUDDER HINGE FITTING, AIRCRAFT SIDE. STRUCTURALLY ACCEPTABLE. REF. BOMBARDIER REO. RESTORED FINISH, NO DEFECTS NOTED, BLENDED AREA L=.700" X W=.275" X D=.016". COMPLETED TASK CARD, WEIGHT CHANGE NEGLIGIBLE DUE TO REPAIR BEING BLEND ONLY

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

*RH WINDSHIELD SIDE POST BOTTOM SUPPORT AFT SIDE, POSSIBLE CRACK (MARKED) (C-CHECK) RO 3/26/2020 REMOVED DAMAGE SUPPORT FITTING, RECEIVED LOCATED DRILLED AND INSTALLED NEW RH WINDSHIELD SIDE POST BOTTOM SUPPORT AFT SIDE, FITTING.REF CRJ200 SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

*INTERCOSTAL AT FS 310 LH SIDE FWD OF PAX DOOR CORRODED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE LH FS310 INTERCOSTAL FWD OF PAX DOOR REF CRJ200 SRM, BOMBARDIER DRAWING. LEAK CHECKS GOOD. COMPLIED WITH ST.

Part: FASTENER — CORRODED (LT SPOILER) · airframe 38,214 hrs · 37,252 cycles

*LH WING OUTBD GROUND SPOILER INBD AND OUTBD HINGE HARDWARE CORRODED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED R/H WING OTBD GROUND SPOILER OTBD AND INBD HINGE HARDWARE. REF. CRJ 200 AMM. OPERATIONAL TEST GOOD AT THIS TIME, NO DEFECTS NOTED.

Part: FASTENER — CORRODED (LT SPOILER) · airframe 38,214 hrs · 37,252 cycles

*LH WING INBD FLIGHT SPOILER OUTBD HINGE HARDWARE CORRODED (C-CHECK) RO 3/26/2020 INSTALLED 1 EACH NEW SERVICEABLE SHIM ( TEFLON PAD ) AT L/H WING FLIGHT SPOILER, OTBD SIDE. REF. CRJ 200 AMM

Part: FASTENER — CORRODED (LT SPOILER) · airframe 38,214 hrs · 37,252 cycles

*LH WING INBD GROUND SPOILER PCU UPPER LINK HARDWARE CORRODED (C-CHECK) RO 3/26/2020 CLEANED AND INSPECTED LEFT WING INBOARD GROUND SPOILER PCU LINK HARDWARE. NO CORROSION NOTED. CHECKED GOOD. REF CRJ 200 SRM.

Part: SKIN — DAMAGED (RUDDER) · airframe 38,214 hrs · 37,252 cycles

*RUDDER LOWER LEADING EDGE ON RH SIDE DAMAGED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE DAMAGED RH LOWER LE RUDDER SKIN REF CRJ200 SRM, BOMBARDIER DRAWING. RESTORED FINISH. COMPLIED WITH ST

Part: FASTENER — CORRODED (RT SPOILER) · airframe 38,214 hrs · 37,252 cycles

RH WING FLT SPOILER INBD HINGE HARDWARE CORRODED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED R/H WING FLIGHT SPOILER INBOARD HINGE HARDWARE. REF. CRJ 200 AMM. OPERATIONAL TEST GOOD AT THIS TIME, NO DEFECTS NOTED.

Part: FASTENER — CORRODED (RT SPOILER) · airframe 38,214 hrs · 37,252 cycles

*RH WING OUTBD GROUND SPOILER INBD END HINGE HARDWARE CORRODED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE NUT WASHER AND COTTER PIN WITH NEW REF AMM, SYSTEM OPS CHECK GOOD.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

*CARGO DOOR FWD BOTTOM TRACK SUPPORT IS CRACKED (MARKED) (C-CHECK) RO 3/26/2020 REPLACED CARGO DOOR FWD BOTTOM TRACK SUPPORT CHANNEL WITH NEW PN 601R35050-25 PO# T-52593 REF CRJ 200 SRM 51-42-06.

Part: SKIN — CORRODED (PAX DOOR) · airframe 38,214 hrs · 37,252 cycles

*CORROSION ON SKIN AT ALL SMALL ACCESS PANELS SCREW HOLES ON PAX DOOR (C-CHECK) RO 3/26/2020 --BLENDED CORROSION AROUND ACCESS PANEL SCREW HOLES 832AL & 832GL "OUT OF LIMITS" DUE TO COMPLETE MATERIAL LOSS (ORIGINAL: .040) - (REMAINING: .000) - (LOSS: .040) --REMOVED, FABRICATED AND REPLACED THE PAX DOOR INNER SKIN REF BOMBARDIER DRAWING 601R31702 REV N, CRJ200 SRM. APPLIED CIC & RESTORED FINISH.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

ADM #1293. FS 625.25 AND STR 15.75R RIGHT SIDE OF AIRCRAFT BELLOW ENGINE. FOUND TO BE A DENTED SCRATCH MEASURES 2.55 INCHES LONG AND .011 INCHES DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 3/26/2020 CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER TO THE DENTED SCRACH AT FS625.25 STR15.75R REF BOMBARDIER REO. RESTORED FINISH. COMPLIED WITH ST

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,214 hrs · 37,252 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7649, POSITION: (C-CHECK) RO 3/26/2020 COMPLIED WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE. COMPLIED WITH SERIAL NUMBER 7649. COMPLIED WITH ST LEAK CHECKS GOOD.

Part: VERTICAL SUPPORT — CRACKED (BS 409) · airframe 37,811 hrs · 36,800 cycles

DURING NDT INSPECTION AT FS 409.0+128 VERTICAL POST AT BL 0.0 FOUND CRACKS AROUND RIVET ON RH STIFFENER AT FIRST RIVET ON STIFFENING STRAP. FIRST CRACK EXTENDING OUTWARD FROM RIVET VERTICALLY ALONG STIFFENER MEASURING L=0.117IN. SECOND CRACK EXTENDING FROM RIVET INWARD TOWARD BEND RADIUS OF STIFFENER MEASURING L= 0.229IN. (C-CHECK) RO: 11/8/2019 REMOVED RH STIFFENER AT VERTICAL POST ASSY. LOCATED AT FS409.0+128 PRESSURE BULKHEAD AT BL0.0 & INSTALLED "NEW" RH STIFFENER AT VERTICAL POST ASSY. LOCATED AT FS409.0+128 PRESSURE BULKHEAD AT BL0.0 IAW SRM. PRESSURE LEAK CHECK GOOD.

Part: BYPASS VALVE — FAILED (NLG) · airframe 37,390 hrs · 36,325 cycles

AFTER TAKE OFF, RECEIVED GEAR DISAGREE WARNING WITH NOSE GEAR NOT UP AND LOCKED. PERFORMED QRH PROCEDURE AND NOSE GEAR CAME DOWN & LOCKED WITH 3 GREEN. LANDED WITHOUT INCIDENT. (FLT#4249) FO: 07/12/2019 CLOSED REMOVED AND REPLACED MANUAL BYPASS NOSE DOOR VALVE IAW AMM. OPS CHECK AND LEAK CHECK GOOD.

Part: UPLOCK — DEFECTIVE (NLG) · airframe 36,742 hrs · 35,587 cycles

RECEIVED GEAR DISAGREE WARNING MESSAGE AND NOSE GEAR WARNING MESSAGE. PERFORMED QRH PROCEDURE AND MESSAGES CLEARED. RETURNED TO FIELD. (FLT#3736) CLOSED REMOVED AND REPLACED UPLOCK PIN AND BRACKET IAW CMM. RIGGED UPLOCK PIN REF IAW AMM, OPS CHECK GOOD. PERFORMED NLG STRUT SERVICING. PERFORMED MULTIPLE GEAR SWINGS, OPS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (CABIN PRESSURE) · airframe 34,950 hrs · 33,576 cycles

CLIMBING THROUGH 25,000 FT, CABIN ALTITUDE CAUTION, THEN WARNING. RAN QRH. ALL MASKED DROPPED AND DONNED, EMERGENCY DESCENT.

Part: CONTROL HANDLE — FAILED (MLG) · airframe 34,902 hrs · 33,530 cycles

RETURNED TO FIELD FOR GEAR NOT RETRACTING AFTER TAKEOFF. ALL GEAR WOULD NOT RETRACT BUT WAS INDICATING GREEN. REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW AMM. PERFORMED NUMEROUS GEAR SWINGS. OPS CHECKED GOOD.

Part: TIRE — FAILED (MLG) · airframe 34,127 hrs · 32,673 cycles

NR 1 MAIN TIRE FAILED DURING TAKEOFF. EMERGENCY DECLARED. REMOVED AND REPLACED THE NR 1 AND 2 MLG WHEEL ASSEMBLIES.

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · airframe 29,247 hrs · 27,159 cycles

LEFT SIDE FUSELAGE, BS 559+96 - 574, FOUND CORROSION ON FLOOR SUPPORT AROUND NUTPLATE HOLES. BLENDED CORROSION IAW REO.

Part: DOOR SILL — CRACKED (CARGO BAY) · airframe 29,247 hrs · 27,159 cycles

CRACK FOUND ON CARGO DOOR SILL AT BS 605 AT AFT CARGO DOOR STOP. R & R CARGO DOOR SILL IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,247 hrs · 27,159 cycles

FOUR INCH CRACK ON BS 280 FLOORBEAM LOWER RADIUS FROM RBL 9 - 13. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 29,247 hrs · 27,159 cycles

RIGHT SIDE FUSELAGE BS 605- 621 FOUND CORROSION ON FLOOR SUPPORT AROUND NUTPLATE HOLES. BLENDED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 589-605) · airframe 29,247 hrs · 27,159 cycles

RIGHT SIDE FUSELAGE BS 589 - 605, FOUND CORROSION ON FLOOR SUPPORT AROUND NUTPLATE HOLES. BLENDED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 29,247 hrs · 27,159 cycles

LEFT SIDE FUSELAGE, BS 559+80 - 559+96 CORRODED ON FLOOR SUPPORT AROUND NUTPLATE HOLES. BLENDED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · airframe 29,247 hrs · 27,159 cycles

RIGHT SIDE FUSELAGE BS 559+80 - 574, FOUND CORROSION ON FLOOR SUPPORT AROUND NUTPLATE HOLES. BLENDED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 574-589) · airframe 29,247 hrs · 27,159 cycles

RIGHT SIDE FUSELAGE, BS 574 - 589, FOUND CORROSION ON FLOOR SUPPORT AROUND NUTPLATE HOLES. BLENDED CORROSION IAW REO.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 29,247 hrs · 27,159 cycles

CARGO DOOR INNER SKIN CRACKED AT UPPER MID NUTPLATE HOLE. C-CHECK, REPAIRED CARGO DOOR INNER SKIN CRACK AT UPPER MID NUTPLATE HOLE IAW STS EA.

Part: FRAME — BENT (NOT REPORTED) · airframe 29,247 hrs · 27,159 cycles

PANEL 172BR GROUND AIR CONDITIONING FRAME IS SLIGHTLY BENT. C-CHECK, REPAIRED GROUND AIR DOOR LANDING PLATE IAW EA.

Part: LEVER — CHAFED (NOT REPORTED) · airframe 29,247 hrs · 27,159 cycles

FWD PULL-IN LEVER IS CHAFED. REPAIRED FWD PULL-IN LEVER CHAFE IAW REO.

Part: COVER — CRACKED (APU BAY) · airframe 29,247 hrs · 27,159 cycles

APU ENCLOSURE COVER HAS THREE CRACKS. REPAIRED APU COVER IAW REO.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,643 hrs · 26,490 cycles

SERVICE DOOR CEILING EMERGENCY EXIT SIGN HAS TWO LIGHTS INOPERATIVE. REPLACED THE LAMPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,643 hrs · 26,490 cycles

FWD FACING REAR CEILING EMERGENCY EXIT SIGN HAS SEVERAL LIGHTS INOPERATIVE. REPLACED THE LAMP.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 28,136 hrs · 25,949 cycles

EMERGENCY EXIT LIGHT LENS IN GALLEY MISSING AT MAIN CABIN DOOR. REPLACED LIGHT COVER IAW AMM.

Part: WIRE — UNSECURE (CABIN) · airframe 28,050 hrs · 25,851 cycles

EMERGENCY EXIT LIGHT AT EXIT ROW DOES NOT ILLUMINATE. FLT 2902 SECURED WIRES FOR EMERGENCY EXIT AT ROW 8A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,962 hrs · 25,755 cycles

EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 2901 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,805 hrs · 25,595 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 2930 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,690 hrs · 25,451 cycles

EMERGENCY OVERHEAD LIGHT NR 1 IS BURNED OUT. FLT 2969 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,531 hrs · 25,271 cycles

EMERGENCY LIGHT POD NR 3 BURNED OUT. FLT 2972 RELAMPED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,531 hrs · 25,271 cycles

OVERWING EMERGENCY LIGHTS BURNED OUT. FLT 2972 REPLACED NR 2 POWER SUPPLY BATTERY. PN AD-2013-1A SN ON77246 SN OFF 83448.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,917 hrs · 24,597 cycles

SEVERAL EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT#2941 CHARGED ELBP`S, EMERGENCY LIGHTS ILLUMINATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,519 hrs · 24,139 cycles

SECOND TO LAST EMERGENCY OVERHEAD LIGHT IS BURNED OUT. RELAMPED.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 24,997 hrs · 22,516 cycles

GOUGE ON FS 621 REAR PRESSURE BULKHEAD AT BL 27.50 + 2 WL 120.43 + 12. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — DAMAGED (SWIA201231987) · airframe 24,997 hrs · 22,516 cycles

DAMAGE AREA ON FS 621 REAR PRESSURE BULKHEAD AT WL 120.43 + 10 BL 27.50 + 3. (C-CHECK) REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,997 hrs · 22,516 cycles

RIGHT FS 484 RBL 36 FLOORBEAM INBOARD CLIP IS CRACKED. (C-CHECK) REPLACED RIGHT 484 CLIP PER REO.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 24,997 hrs · 22,516 cycles

CRACK ON FS 202 AT THE PARKING BRAKE CABLE FEED THROUGH. (C-CHECK) REPAIRED PER REO.

Part: POST — CRACKED (FUSELAGE) · airframe 24,997 hrs · 22,516 cycles

CRACK ON FS 409.0+128 VERTICAL POST AT RBL 18.00 WL 69.00 OUTBOARD AFT RADIUS. (C-CHECK) REPLACED POST P/N 601R32208-156 PER REO AND CRJ 200 SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,997 hrs · 22,516 cycles

CRACK ON FS 621 BULKHEAD WEB, FORWARD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING AT LBL 27.5. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,537 hrs · 20,978 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,508 hrs · 20,948 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,179 hrs · 20,640 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6257) RELAMPED EMERGENCY LIGHT.

Part: SIGN — INOPERATIVE (CABIN) · airframe 23,086 hrs · 20,577 cycles

EMERGENCY EXIT SIGN BY GALLEY SERVICE DOOR IS OUT. (FLT 6303) RELAMPED EMERGENCY EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,034 hrs · 20,531 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6456) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,666 hrs · 20,222 cycles

NR 1 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6456) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,564 hrs · 20,146 cycles

NR 1 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6420) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,447 hrs · 20,059 cycles

OVERHEAD EMERGENCY LIGHT NOT WORKING AT ROW 13. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,435 hrs · 20,045 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6275) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,223 hrs · 19,879 cycles

FORWARD CEILING EMERGENCY LIGHT IS OUT. (FLT 6506) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,030 hrs · 19,736 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 2 IS OUT. (FLT 5449) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,851 hrs · 19,582 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6295) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,683 hrs · 19,438 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6306) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,644 hrs · 19,405 cycles

AFT CEILING EMERGENCY LIGHT NOT ILLUMINATING. (FLT 6289) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,540 hrs · 19,327 cycles

ROW 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6352) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,341 hrs · 19,163 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6912) RELAMPED EMERGENCY LIGHT .

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,154 hrs · 19,009 cycles

AFT OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. (FLT 6994)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,107 hrs · 18,979 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6912)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,847 hrs · 18,778 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 2 IS OUT. (FLT 6828) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,816 hrs · 18,750 cycles

THIRD OVERHEAD CABIN EMERGENCY LIGHT IS OUT. (FLT 6862) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,695 hrs · 18,629 cycles

FS 559.0 PRESSURE BULKHEAD CRACKED AT RIGHT SIDE. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,384 hrs · 18,365 cycles

FS 559.0 PRESSURE BULKHEAD CRACKED AT RIGHT SIDE. (C-CHECK) REPAIR PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,848 hrs · 17,917 cycles

NR 2 OVERHEAD EMERGENCY LIGHT OUT. (FLT 6561) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,456 hrs · 16,724 cycles

THE CEILING EMERGENCY FLOOD LIGHT NR 2 INOP. (FLT 6086) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,182 hrs · 16,499 cycles

AFT EMERGENCY FLOOD LIGHT IN CABIN INOP. (FLT 6069) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,586 hrs · 16,023 cycles

NR 3 CEILING EMERGENCY LIGHT INOP. (FLT 6765) RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,532 hrs · 15,973 cycles

AFT CEILING LIGHT INOP. (PAINT VISIT)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,509 hrs · 15,948 cycles

NR 2 EMERGENCY CEILING LIGHT INOP. (FLT 2559) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,367 hrs · 15,809 cycles

CEILING LEVEL EMERGENCY LIGHTS INOP. (FLT 2573) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,348 hrs · 15,791 cycles

OVERHEAD EMERGENCY LIGHT INOP. (FLT 2591) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,264 hrs · 15,701 cycles

CEILING DOME EMERGENCY LIGHT INOP. (FLT 2525) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,075 hrs · 15,495 cycles

CEILING EMERGENCY LIGHT INOP. (FLT 2538) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,040 hrs · 15,453 cycles

NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 2564) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,040 hrs · 15,453 cycles

EMERGENCY CEILING LIGHT INOP. (FLT 2711) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,933 hrs · 15,341 cycles

CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 2754)RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,898 hrs · 15,307 cycles

AFT EMERGENCY CEILING LIGHT INOP. (FLT 2557) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,727 hrs · 15,124 cycles

FLIGHT ATTENDANT INDICATOR/EMERGENCY EXIT SIGN BURNT OUT. (FLT 2522) RELAMPED EMERGENCY EXIT SIGN.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,599 hrs · 14,975 cycles

FLT 2559 - NR 2 CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,470 hrs · 14,845 cycles

FLT 2753 - OVERHEAD EMERGENCY CEILING LIGHT INOP. RELAMPED.

Part: HANDLE — FAULTY (MLG) · airframe 16,116 hrs · 14,460 cycles

FLT 2751 - LANDING GEAR DID NOT RETRACT. REPLACED GEAR SELECTOR HANDLE CONTROL BOX.

Part: SELECTOR VALVE — FAULTY (NLG) · airframe 16,133 hrs · 14,481 cycles

FLT 2558 - NOSE GEAR DISAGREE MESSAGE AND NOSE GEAR WOULD NOT RETRACT. REPLACED NLG SELECTOR VALVE, PN 750006000, SN OFF 1916.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,722 hrs · 14,023 cycles

FLT 2665 - REAR EMERGENCY LIGHT ON CEILING INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,707 hrs · 14,008 cycles

FLT 2559 - RIGHT SIDE AFT CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,641 hrs · 13,936 cycles

FLT 2669 - PASSENGER DOOR FLOOR LEVEL EMERGENCY SIGN HAS TWO BULBS OUT. RELAMPED.

Part: FITTING — CORRODED (LT ENGINE) · airframe 15,629 hrs · 13,927 cycles

C-CHECK, LEFT ENGINE THRUST FITTING CORRODED. REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 15,629 hrs · 13,927 cycles

C-CHECK, RIGHT FS 484 INTERCOSTAL ANGLE AT RBL 36 CRACKED IN UPPER RADIUS. REPAIRED PER REO.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 15,629 hrs · 13,927 cycles

C-CHECK, DURING LEFT FS 484 INTERCOSTAL ANGLE AT LBL36 CRACKED IN UPPER RADIUS. REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,629 hrs · 13,927 cycles

C-CHECK, FLOOR SUPPORT CLIP AT FS 280 RBL9 INBOARD CRACKED. REPLACED.

Part: FITTING — CORRODED (RT ENGINE) · airframe 15,629 hrs · 13,927 cycles

C-CHECK, RIGHT ENGINE THRUST FITTING CORRODED. REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,629 hrs · 13,927 cycles

DURING C-CHECK, FLOOR SUPPORT CLIP AT FS 280 LBL9 INBOARD CRACKED. REPLACED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,209 hrs · 13,470 cycles

FLT 2516 - EMERGENCY LIGHTS NEAR FLOOR AT MAIN CABIN DOOR INOP, RELAMPED.

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 12,776 hrs · 11,268 cycles

SERVICE DOOR OUTER HANDLE WILL NOT OPEN. CLEANED AND LUBED OUTER SERVICE DOOR HANDLE IAW AMM 12-20-52.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 8,808 hrs · 7,756 cycles

FLIGHT 5277 - ON APPROACH TO BWI, SELECTED FLAPS FROM 20 TO 30 DEGREES, RECEIVED FLAP FAIL CAUTION MESSAGE. APPLIED QRH AND LANDED AT 20 DEGREE FLAP WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.

Part: WINDOW — CRACKED (COCKPIT) · airframe 10,677 hrs · 9,420 cycles

FLIGHT 5154 - EN ROUTE IND-JFK, THE CAPTAIN'S SIDE WINDOW CRACKED. REPLACED THE CAPTAIN'S SIDE WINDOW.

Part: WIRE HARNESS — MALFUNCTIONED (RT MLG) · airframe 9,195 hrs · 8,074 cycles

FLIGHT 5182 - ANTI-SKID CAUTION DURING TAKEOFF. REPLACED THE RT MLG WHEEL SPEED WIRE HARNESS.

Part: VISOR — BROKEN (COCKPIT) · airframe 8,827 hrs · 7,751 cycles

PILOT SUN VISOR BROKEN. REPLACED SUN VISOR.

Part: OIL COOLER — CRACKED (APU) · airframe 6,624 hrs · 5,800 cycles

FLIGHT 5220 APU OIL PRESSURE CAUTION MESSAGE. REPLACED THE APU OIL COOLER.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 5,682 hrs · 5,004 cycles

FLIGHT 5343 IAPS DEGRADED STATUS MESSAGE DURING T/O. RESET THE NR 2 DCU, SYSTEM TEST SATISFACTORY.