N862AS

Part: SKIN — DENTED (BS 605-625) · airframe 40,651 hrs · 36,227 cycles

REF: CO# 7476718 JOB# 7747675 OP# 62: FUSELAGE SKIN REPAIR REQUIRED BELOW CARGO DOOR BETWEEN FS 605.0 TO FS 625.0 AND STR 18L TO 22L. C/A: PERFORMED PERMANENT REPAIR I.A.W. EXPRESSSJET ECTC REO 601R-53-61-6789.

Part: SKIN — CORRODED (RT WING) · airframe 40,651 hrs

REF: CO# 7476718 JOB# 7747675 OP# 57 LOWER WING PLANK CUTOUT FOR RH BOOST PUMP HAS MULTIPLE INDICATIONS NOTED AROUND ENTIRE CIRCUMFERENCE ON HORZ AND VERTICAL SURFACE 50% FSH. FAILED NDT INSP. C/A: PERFORMED MAJOR REPAIR CARD NO: REO 601R-57-21-2908 BLENDED TO REMOVE DAMAGE.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 40,651 hrs · 36,227 cycles

REF: CO# 7476718 JOB# 7747671 OP# 105: CORROSION FOUND ON PRESSURE FLOOR SILLS F.S. 409.00+128 TO F.S. 559.00 BETWEEN LBL 36-45 AND RBL 36-45. C/A: PERFORMED A MAJOR REPAIR ON FLOOR SILLS FS 409-128 TO 559 BETWEEN LBL 36-45 AND RBL 36-45 I.A.W. EXPRESSJET WO 561189 ECTC REO 601R-53-41-2396 REV. 2018-11-20, ECTC REO 601R-53-41-2397 REV. 2018-11-26 AND BOMBARDIER REO 601R-53-41-2396 REV. --, ECTC REO 601R-53-41-2397 REV. -- AND REO 601R-53-41-666 01 REV. C.

Part: SKIN — DENTED (BS 589-605) · airframe 40,651 hrs · 36,227 cycles

REF: CO# 7476718 OP# 62 FUSELAGE SKIN HAS 1 EA DENT BETWEEN FS605 AND FS589 FROM STR 24L TO 25L. C/A PERFORMED PERMANENT REPAIR IAW EXPRESSJET ECTC EA 32-2018-239

Part: SKIN — CRACKED (RT WING) · airframe 40,651 hrs · 36,227 cycles

REF: CO#7476718 JOB# 7747675 OP#43 R/H LOWER WING PLANK AND STRAP JOINT CRACKED AT RWS 148.00. C/A REPAIRED DAMAGE IAW EXPRESSJET ECTC REO 601R-57-21-130 01.

Part: ANGLE — CRACKED (BS 484) · airframe 35,484 hrs · 33,270 cycles

REF: CO# 7476718 JOB# 7747671 OP# 83: F.S.484, RBL 36.00 INBD AND OUTBD CLIPS ARE CRACKED. C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER REO 601R-53-41-2393 REV.A, DATED 2018-11-18, EXPRESSJET EC/TC REO 601R-53-41-2393 REV.0, DATED 2018-11-19, BOMBARDIER REO 601R-53-41-059 REV.B, DATED 2009-09-16 AND EXPRESSJET EC/TC REO 601R-53-41-059 REV.D, DATED 2015-06-16.

Part: OIL SYSTEM — LOW PRESSURE (RT ENGINE) · airframe 40,198 hrs · 35,695 cycles

RIGHT ENGINE FAILED IN FLIGHT, THE RIGHT ENG OIL PRESSURE MASTER WARNING, PRESSURE SHOWED ZERO. REMOVED AND REPLACED THE RT ENGINE ASSY IAW AMM. OPS AND LEAK CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 39,772 hrs · 35,170 cycles

AFTER TAKE OFF ON RETRACTION GEAR DISAGREE NLG DOOR OPEN CAUTION. (FLT 3198) 01/24/2018 WORK IN PROGRESS.

Part: BRACKET — DAMAGED (NLG WOW) · airframe 39,842 hrs · 35,264 cycles

AFTER TAKE OFF, AND DURING RETRACTION OF THE GEAR, A DISAGREE NLG DOOR OPEN CAUTION MESSAGE. REMOVED AND REPLACED THE NLG NR 2 WOW SENSOR BRACKET IAW AMM. OPS CHECKED GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,583 hrs · 32,592 cycles

EVIDENCE OF CORROSION ON THE CARGO BAY FLOOR SILL AT APPROXIMATELY FS 574.00 AND FS 621.00 AROUND NUT PLATES. CARGO DOOR FLOOR SILL REPLACED IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 37,583 hrs · 32,592 cycles

LEFT INBD FLAP HAS CHAFE ON INBD VANE L/E. REPLACED LT INBD FLAP VANE, INBD WEAR CAP WITH NEW PN K601R14302-15 IAW SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 37,583 hrs · 32,592 cycles

LEFT INBD FLAP HAS CHAFE ON OTBD VANE L/E. REPLACED LT INBD FLAP VANE OTBD WEAR CAP WITH NEW PN K601R14302-7 IAW SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 37,583 hrs · 32,592 cycles

LEFT INBD FLAP HAS CHAFE AT CENTER VANE L/E. REPLACED LT INBD FLAP VANE, CENTER WEAR CAP WITH NEW PN K601R14302-7 IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,583 hrs · 32,592 cycles

AT FS 349.0 FRAME IS CORRODED FROM STR 25 LT TO STR 25 RT. REMOVED AND INSTALLED NEW LOWER FRAME SECTOR AT FS 349.00 IAW REO AND SRM.

Part: SKIN — DENTED (TE FLAP) · airframe 37,583 hrs · 32,592 cycles

DENT ON LT SIDE INBD FLAP BOTTOM SKIN LOCATED WS 67.00. REPAIRED DENT IAW SRM.

Part: BRACKET — BENT (PROXIMITY SWITCH) · airframe 36,527 hrs · 31,705 cycles

NOSE GEAR WOULD NOT RETRACT. RETURNED TO FIELD. FOUND THE NOSE GEAR PROXIMITY SWITCH BRACKET WAS BENT FROM IMPROPER TOW STRAP PLACEMENT. R & R PROXIMITY SWITCH AND BRACKET. OPS CK GOOD.

Part: BYPASS VALVE — FAILED (RT A/C PACK) · airframe 33,663 hrs · 28,892 cycles

RT PACK HIGH TEMP CAUTION. NO CONTROL IN EITHER AUTO OR MANUAL. PACK TEMP INDICATED 110 DEGREES C. R & R RT PACK DUAL BYPASS VALVE IAW AMM. ALL OPS GOOD. NO LEAKS NOTED. PN: 808440-2, SN ON: 9611055, SN OFF: 2000425.

Part: BULKHEAD — CRACKED (BS 202) · airframe 32,667 hrs · 27,895 cycles

CRACK IN BS 202 BULKHEAD WHERE PARKING BRAKE ROD PASSES THROUGH. REPAIRED IAW REO.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 32,667 hrs · 27,895 cycles

DENT AND GOUGE IN TOP SKIN ON RT INBD FLAP 10 INCHES FROM AFT EDGE. REPAIRED FLAP IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,667 hrs · 27,895 cycles

FRETTING ALL THE WAY AROUND AVIONICS BAY DOOR CUTOUT ON INNER SURFACE OF SKIN. C-CHECK, REMOVED FRETTING ALL THE WAY AROUND AVIONICS BAY DOOR INNER SURFACE, IAW REO.

Part: PANEL — CRACKED (UNKNOWN) · airframe 32,667 hrs · 27,895 cycles

PANEL 221BLC IS CRACKED. C-CHECK, REPAIRED CRACKED PANEL 221BLC IAW EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,667 hrs · 27,895 cycles

RIGHT INBD FLAP VANE IS CHAFED NEAR CENTER. C-CHECK, REMOVED CHAFE ON RT INBD FLAP VANE NEAR THE CENTER IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,667 hrs · 27,895 cycles

RT INBD FLAP VANE IS CHAFED NEAR INBD SIDE. C-CHECK, REMOVE CHAFE ON THE RT INBD FLAP VANE NEAR THE INBD SIDE IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 32,667 hrs · 27,895 cycles

LT AILERON TOP L/E IS CHAFED IN TWI AREAS NEAR OTBD SIDE. C-CHECK, REPAIRED LT AILERON UPPER SKIN IAW REO.

Part: BULKHEAD WEB — DAMAGED (AFT) · airframe 32,667 hrs · 27,895 cycles

DEFECTS NOTED ON AFT PRESSURE BULKHEAD WEB FWD FACE C-CHECK, REPAIRED DEFECTS IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 32,667 hrs · 27,895 cycles

RT AILERON TOP L/E IS CHAFED IN TWO AREAS NEAR CENTER. C-CHECK, REPAIRED RT AILERON UPPER SKIN IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,667 hrs · 27,895 cycles

RT INBD FLAP VANE IS CHAFED NEAR OTBD SIDE. C-CHECK, REMOVED CHAFE ON RT INBD FLAP VANE NEAR OTBD SIDE IAW REO.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,890 hrs · 27,089 cycles

AFT FLOOR LEVEL LIGHTS & OVERHEAD EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT 2601 REPLACED NR 4 ELBP IAW AMM, PN ON AD-2013-1A, SN ON 126606, PN OFF 2013-1A & SN OFF 101363.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,556 hrs · 26,754 cycles

EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT 2627 CHARGED UP ELBP'S. OPERATIONS CHECKED GOOD ON EMERGENCY LIGHTS

Part: CHARGER — FAILED (CABIN) · airframe 28,835 hrs · 23,848 cycles

EMERGENCY FLOOR LIGHT 2ND 3RD 4TH STRIP IS NOT LIT. (FLT 2660) REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER.

Part: TRUNNION — CRACKED (MLG) · airframe 28,492 hrs · 23,467 cycles

CRACK INDICATIONS ON 4 HOLES EACH IN LEFT AND RIGHT MLG TRUNNION LOWER PLANK. (C-CHECK) REPAIRED PER REO.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 28,492 hrs · 23,467 cycles

FLOOR SUPPORT BEAM LBL 27 IN BETWEEN FS 589 AND FS 605 BLEND OUT IS OUT OF LIMIT. (C-CHECK) REPLACED FLOOR SUPPORT BEAM LBL 27 IN BETWEEN FS 569 AND FS 621 PER CRJ200 SRM.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 28,492 hrs · 23,467 cycles

FLOOR SUPPORT BEAM LBL 9 IN BETWEEN FS 589 AND FS 605 BLEND OUT IS OUT OF LIMIT. (C-CHECK) REPLACED FLOOR SUPPORT BEAM LBL 9 IN BETWEEN FS 569 AND FS 621 PER CRJ-200 SRM.

Part: SILL — CRACKED (FUSELAGE) · airframe 28,492 hrs · 23,467 cycles

CRACK ON AFT CARGO DOOR SILL AT FS 605. (C-CHECK) REPAIRED DAMAGED AREA OF AFT CARGO DOOR SILL AT FS 605.

Part: POST — CRACKED (FUSELAGE) · airframe 28,492 hrs · 23,467 cycles

CRACK ON LEFT FS 409+128 VERTICLE POST AT LBL 18, OUTBOARD C-CHANNEL IN AFT RADIUS. (C-CHECK) REPLACED LEFT FS 409+128 VERTICLE OUTBOARD POST AT LBL 18 PER REO.

Part: POST — CRACKED (FUSELAGE) · airframe 28,492 hrs · 23,467 cycles

CRACK ON RIGHT FS 409+128 VERTICLE POST AT RBL 18, OUTBOARD C-CHANNEL IN AFT RADIUS. (C-CHECK) REPLACED VERTICLE POST AT RBL 18 IN REFERENCE TO REO.

Part: PANEL — CHAFED · airframe 28,492 hrs · 23,467 cycles

PANEL 326CL HAS CHAFING. (C-CHECK) REPAIRED PANEL 326CL AS PER CRJ 200 SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,492 hrs · 23,467 cycles

CORROSION ON FLOOR SUPPORT BEAMS BETWEEN FS 589.00 AND FS 605.00. (C-CHECK) REPAIRED FLOOR SUPPORT BEAMS BETWEEN FS 589.00 AND FS 605.00 IN REFERENCE TO CRJ200 SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 28,492 hrs · 23,467 cycles

CRACK ON RIGHT FS 409+128 VERTICLE POST AT RBL 18, INBOARD C-CHANNEL IN AFT RADIUS. (C-CHECK) REPLACED VERTICLE POST AT RBL 18 IN REFERENCE TO REO.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,447 hrs · 23,427 cycles

SERVICE DOOR CABIN EMERGENCY LIGHT FIXTURE IS DAMAGED. (SERVICE) REPLACED SERVICE DOOR EMERGENCY LIGHT FIXTURE IN REFERENCE TO MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,310 hrs · 23,302 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 8436055) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,189 hrs · 23,180 cycles

NR 1 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4483) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,950 hrs · 22,970 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4837) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,789 hrs · 22,821 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4502) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,470 hrs · 22,505 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4496) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,433 hrs · 22,470 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4799) RELAMPED EMERGENCY LIGHT.

Part: ACTUATOR — OUT OF RIG (TE FLAP) · airframe 27,385 hrs · 22,410 cycles

RIGHT ROLLING FORCE UPON EXTENSION OF FLAPS. (FLT 4658) RE-RIGGED FLAP ACTUATOR R-4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,214 hrs · 22,248 cycles

NR 1 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,214 hrs · 22,248 cycles

LAST ROW EMERGENCY CEILING OVERHEAD LIGHT IS INOPERATIVE. (FLT 4517) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,113 hrs · 22,144 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4760) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,068 hrs · 22,097 cycles

LEFT FORWARD EXTERIOR EMERGENCY LIGHT BURNED OUT. (FLT 4565) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,037 hrs · 22,064 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4589) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,952 hrs · 21,979 cycles

AFT OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 4522) RELAMPED EMERGENCY LIGHT.

Part: ALTIMETER — FAILED (COCKPIT) · airframe 26,850 hrs · 21,894 cycles

STANDBY ALTIMETER READS 3-4000FT HIGH AND MAKES CLICKING NOISES. (FLT 4654) REPLACED STANDBY ALTIMETER. P/N WL102AM55, S/N OFF AN897.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,816 hrs · 21,862 cycles

RIGHT EXTERIOR FORWARD EMERGENCY LIGHT IS OUT. (FLT 4491) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,809 hrs · 21,856 cycles

MIDDLE EXTERIOR EMERGENCY LIGHT IS OUT ON RIGHT SIDE OF AIRCRAFT. (FLT 4458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,546 hrs · 21,608 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4453) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,515 hrs · 21,576 cycles

NR 2 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4451) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,243 hrs · 21,333 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4535) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,319 hrs · 20,500 cycles

NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 4625) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,720 hrs · 19,991 cycles

FS 621 BULKHEAD FORWARD SIDE WEB AT LINTEL FITTING CRACKED. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,785 hrs · 20,045 cycles

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

Part: LINK — CORRODED (ENGINE MOUNT) · airframe 24,549 hrs · 19,851 cycles

LEFT FORWARD ENGINE MOUNT LINK ASSEMBLY CORRODED. (ENGINE CHANGE) INSTALLED SERVICEABLE LINK ASSEMBLY.

Part: MOUNT — CORRODED (RT ENGINE) · airframe 24,223 hrs · 19,574 cycles

RIGHT ENGINE FORWARD YOKE MOUNT CORRODED. (ENG CHANGE) REPLACED YOKE MOUNT.

Part: TIRE — BLOWN (LANDING GEAR) · airframe 23,681 hrs · 19,122 cycles

NR 1 AND NR 4 TIRES BLEW OUT. (FLT 4554) ACCOMPLISHED BURST TIRE INSPECTION AND REPLACED ALL TIRES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,565 hrs · 19,024 cycles

ROW 13 EMERGENCY CEILING LIGHT INOP. (FLT 4534) RELAMPED EMERGENCY LIGHT.

Part: SPRING — CORRODED (MAIN DOOR) · airframe 23,501 hrs · 18,966 cycles

MAIN DOOR COULD NOT BE OPENED FROM THE OUTSIDE. (FLT 4663) REPLACED HANDLE SPRING BOOT, SPRING, PLUNGER, AND ROLLER ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,979 hrs · 18,512 cycles

CEILING EMERGENCY LIGHT AT ROW 5 INOP. (FLT 4740) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,428 hrs · 17,276 cycles

FLT 4568 - EMERGENCY CEILING LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,140 hrs · 17,060 cycles

FLT 4551 - CEILING EMERGENCY LIGHT AT ROW 10 INOP. RELAMPED.

Part: LIGHT — NO TEST (CABIN) · airframe 20,525 hrs · 16,609 cycles

FLT 4643 - EMERGENCY LIGHTS WOULD NOT WORK. TURNED ON EMERGENCY LIGHTS. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 20,188 hrs · 16,335 cycles

FLT 3870 - SEVERAL EMERGENCY CABIN LIGHTS INOP. REPLACED NR 1 EMERGENCY LIGHTING BATTERY, PN AD-2013-1A SN ON 60763 SN OFF 43074.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,412 hrs · 16,515 cycles

DURING C-CHECK, FS 280 RBL9 FLOOR SUPPORT AND CLIPS CRACKED. REPAIRED PER REO.

Part: STRUCTURE — CRACKED (BS 625) · airframe 20,412 hrs · 16,515 cycles

DURING C-CHECK, FS 625 LEFT AND RIGHT CLIPS CRACKED. REPLACED PER REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,412 hrs · 16,515 cycles

DURING C-CHECK, FS 280 FORWARD FLOOR SUPPORT AT RBL 9 RADIUS CRACKED. REPLACED PER SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,412 hrs · 16,515 cycles

DURING C-CHECK, FS 280 UPPER FLOOR SUPPORT AT RBL9 CRACKED. REPAIRED PER REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,412 hrs · 16,515 cycles

DURING C-CHECK, FS 280 LBL 9 LOWER FLOOR SUPPORT CRACKED. REPAIRED PER REO.

Part: AILERON — DAMAGED (RT WING) · airframe 18,893 hrs · 15,319 cycles

FLT 3903 - AILERON DAMAGE FOUND ON THE RIGHT SIDE. REPLACED RIGHT AILERON ASSEMBLY IAW CRJ 200 MM 27-15-01, PN: CC670-13000-2, SN OFF: SBRJ364.

Part: SELECTOR VALVE — MALFUNCTIONED (LANDING GEAR) · airframe 18,855 hrs · 15,291 cycles

FLT 3905 - RECEIVED A LANDING GEAR DISAGREE MESSAGE WHEN SELECTED BEFORE LANDING. REPLACED BYPASS VALVE AND SELECTOR VALVE. OPS AND LEAK CHECK GOOD IAW 32-32-10, PN 750004000-003, SN/OFF 719A, PN 750005000, SN/OFF 0734.

Part: FRAME — CRACKED (BS 280) · airframe 15,514 hrs · 12,760 cycles

FS 280 RBL 9 WL 79 INBOARD AND OUTBOARD FRAME CLIPS ARE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 2EA NEW CLIPS P/N 601R31113-58 AT FS 280, RBL 9.0, INBOARD & OUTBOARD SIDES IAW CRJ200 SRM CH 51-42-21 PG 17, SECTION 9.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 15,514 hrs · 12,760 cycles

PASSENGER DOOR OUTER HANDLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PAX DOOR OUTER HANDLE P/N 601R 31763-1 PER CRJ200 AMM 52-11-03/400-802.

Part: FRAME — CRACKED (BS 280) · airframe 15,514 hrs · 12,760 cycles

FS 280 LBL 9 WL 79 INBOARD AND OUTBOARD FRAME CLIPS ARE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 2EA NEW CLIPS AT FS 280, LBL 9.0 INBOARD & OUTBOARD IAW CRJ200 REO 601R-53-11-138.

Part: ANGLE — CRACKED (BS 280) · airframe 15,514 hrs · 12,760 cycles

A .25 INCH CRACK AT STA 280 UPPER ANGLE LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FILLER ANGLE AND SPLICE ANGLES AT STA 280 UPPER LBL 9.0 IAW CRJ200 REO 601R-53-11-138.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 15,514 hrs · 12,760 cycles

PASSENGER DOOR CRACKED BRACKET FWD SIDE OF DOOR INSIDE 2ND OPENING FROM TOP OUTBOARD AFT CORNER. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE BRACKET PER CRJ200 SRM 51-42-21 PG 1, 47, 13, 17.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 13,322 hrs · 11,101 cycles

LEFT SIDE W/S BEGAN ARCING WITH SINGLE CRACK AND SMALL DELAMINATION. REPLACED THE PILOTS DIRECT WINDSHIELD IAW CRJ MM 56-11-01. PN ON NP-139321-13, SN OFF 01208H4227.

Part: CONTROL UNIT — MALFUNCTIONED (STAB MOTOR) · airframe 13,250 hrs · 11,045 cycles

STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REPLACED MOTOR CONTROL UNIT IAW CRJ 200 MM 27-42-05. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 12,799 hrs · 10,706 cycles

"R SPOILERON" CAUTION MESSAGE. REPLACED RT IB SPOILERON PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK OK.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 12,799 hrs · 10,706 cycles

"SPOILERONS FAULT" AND "IB GND SPLR FAULT" STATUS MESSAGES DURING APPROACH TO SLC. REPLACED SECU NR 2 IAW MM 27-61-05. OPERATIONAL CHECK GOOD.

Part: LATCH — MISALIGNED (EMERGENCY EXIT)

DURING A C-CHECK, THE LT OVERWING EMERGENCY EXIT FAILED THE PULL TEST. MAINT ADJUSTED THE LATCH FITTNGS ON THE LT OVERWING EMERGENCY EXIT. OPS CHECK GOOD. (K)

Part: SUPPORT BEAM — CRACKED (ENGINE)

DURING C-CHECK, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMIST. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO. (K)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT INBOARD FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT INBOARD FS 280 CLIP. (M)

Part: LIGHT — CRACKED (GALLEY)

DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY ABOVE THE SERVICE DOOR. OPS CHECKS GOOD. (M)

Part: LIGHT — CRACKED (FUSELAGE)

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE AND CRACKED. MAINT REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR. OPS CHECK GOOD. (K)

Part: LIGHT — CRACKED (GALLEY)

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE CRACKED AND INOPERATIVE. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSY BY THE SERVICE DOOR. (K)

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING A GROUND INSPECTION, AN EXTERNAL EMERGENCY LIGHT ON THE RT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EXTERNAL EMERGENCY LIGHT LAMP ON THE RT SIDE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM)

DURING CLIMB-OUT, AT APPROXIMATELY 10,000 FEET THE CREW EXPERIENCED A FULL SCALE NOSE LT RUDDER TRIM DEFLECTION. THE CAPTAIN CORRECTED FOR THE TRIM PROBLEM USING RUDDER AND AILERON INPUTS. AN EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT RETURNED TO VPS AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE AILERON/ RUDDER TRIM CONTROL PANEL. MAINTENANCE VERIFIED FULL TRAVEL ON THE AILERON AND RUDDER TRIM SWITCHES ON EICAS AND ON THE FLIGHT CONTROLS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR BRACE WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: HANDLE — OUT OF ADJUST (PAX DOOR)

DURING APPROACH INTO ATL FROM DHN, THE CREW RECEIVED A RED PASSENGER DOOR EICAS MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE FLIGHT ATTENDANT REPORTED HEARING AIR SLOW IN THE DOOR AREA AND THAT THE DOOR HANDLE HAD POPPED OVER THE TOP DEAD CENTER POSITION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE ADJUSTED THE PASSENGER DOOR OUTER HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS)

FLT 4522 - DURING APPROACH FROM ATL-GTR, A FLAPS FAIL MESSAGE WAS RECEIVED AFTER SELECTING THE FLAPS TO THIRTY DEGREES. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. DUE TO A DEFERRED RIGHT THRUST REVERSER AND A SHORTER RUNWAY AT GTR, THE AIRCRAFT DIVERTED TO CMB, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE FLAPS ELECTRONIC CONTROL UNTI (FECU). OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN BTR, THE LEFT REAR OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT REAR OVERWING EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTALS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0111. (M)

Part: PLATE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR LANDING PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING TEH CARGO DOOR FLOOR LANDING PLATE IAW ASA EO 600-53-0117. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE SPIDER DUCT BRACKET IN THE EQUIPMENT BAY IAW AMM 21-52-00. (M)

Part: SUPPORT BEAM — CRACKED (ENGINE)

DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SIDE IAW ASA EO 600-53-0070. (M)

Part: STEP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR BOTTOM STEP. (M)

Part: PANEL — CRACKED (LT NACELLE)

DURING A GROUND INSPECTION IN DFW, THE LT ENGINE COWL ON THE UNDERSIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LOWER LEFT NOSE COWL PANEL ON THE LEFT ENGINE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: COALESCER BAG — CONTAMINATED (CABIN)

FLT 4318 - DURING FINAL APPROACH INTO ATL FROM CAK, THE CREW RECEIVED A SMOKE TOILET CAUTION MESSAGE AFTER STARTING THE AUXILIARY POWER UNIT, ACCOMPANIED BY A FUEL SMELL AND SMOKE IN THE CABIN NEAR THE LAVATORY AREA. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT AND LEFT COALESCER BAGS ON THE WATER SEPARATOR ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FLT 4783 - DURING FLIGHT FROM DFW TO AMA, AT FL370, THE LEFT FRONT WINDSHIELD SHATTERED. AN EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED AND LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT WINDSHIELD ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL VALVE — MALFUNCTIONED (APU)

ON SHORT FINAL APPROACH FROM TLH TO ATL, CAPTAIN RECEIVED APU OVERHEAT MESSAGE. CAPTAIN BLEW THE FIRE BOTTLE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE FIRE BOTTLE, SQUIB AND APU LOAD CONTROL VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)