N452SW

Part: RVDT — INOPERATIVE (NLG STEERING) · airframe 37,633 hrs · 33,572 cycles

STEERING INOP CAUTION MSG IN FLIGHT COMPLIED WITH QRH DID NOT FIX ISSUE. FLIGHT 4449 FILED CLOSEDREMOVED AND REPLACED THE LEFT FEEDBACK RVDT IN REF TO CRJ200 AMM. OPS CHECK GOOD.

Part: SKIN — CHAFED (RT WING) · airframe 36,414 hrs · 32,153 cycles

R/H LWR WING PLANK AND TRAILING EDGE IS CHAFED AT RBL45. (C-CHECK) RO: 06/12/2019 REMOVED CHAFING FROM R/H LWR WING PLANK AND TRAILING EDGE, RBL45 IAW REO AND SRM. PERFORMED PRESSURIZATION CHECK IAW AMM. NO LEAK NOTED

Part: FRAME — CORRODED (BS 310) · airframe 36,414 hrs · 32,153 cycles

FS 310 FRAME FWD/AFT SIDE CORRODED FROM STRG25L TO 26R. (C-CHECK) RO: 06/12/2019 REMOVED AND REPLACED FRAME AT FS310 BETWEEN STR23L TO STR23R IAW SRM. / COMPLETED PRESSURE LEAK CHECK IAW AMM. NO LEAKS NOTED.

Part: STRINGER — CORRODED (BS 319-349) · airframe 36,414 hrs · 32,153 cycles

FS STRG 26L CORRODED FROM FS 319.70 TO FS 349.0. (C-CHECK) RO: 06/12/2019 INSTALLED NEW SPLICE SECTION OF STR 26L FROM FS364 TO FS314 PN: 601R31022-23 AND 2 EACH REPAIR SPLICE CHANNELS PN: N126-7001, AND N126-7606 IAW SRM. COMPLETED PRESSURE LEAK CHECK IAW AMM. NO LEAKS NOTED.

Part: FRAME — CORRODED (BS 333) · airframe 36,414 hrs · 32,153 cycles

FS 333.0 FRAME CORRODED FWD/AFT SIDE FROM STRG 25L TO 26R. (C-CHECK) RO: 06/12/2019 REMOVED AND REPLACED FS333 FRAME ASSY. BETWEEN STR 23L AND STR 23R IAW SRM. / COMPLETED PRESSURE LEAK CHECK IAW AMM. NO LEAKS NOTED.

Part: FRAME — CORRODED (BS 319) · airframe 36,414 hrs · 32,153 cycles

FS 319.70 FRAME CORRODED FWD/AFT SIDE FROM STRG25L TO STRG 26R. (C-CHECK) RO: 06/12/2019 REMOVED AND INSTALLED NEW FS319.70 LOWER FRAME SECTION FROM STR 23L TO STR 23R IAW SRM. COMPLETED PRESSURE LEAK CHECK IAW AMM. NO LEAKS NOTED.

Part: STRAP — CORRODED (BS 559) · airframe 36,414 hrs · 32,153 cycles

RH FLOOR SUPPORT STRAP IS CORRODED AT FS559.00. (C-CHECK) RO: 06/12/2019 REMOVED AND REPLACED WITH NEW FLOOR SUPPORT STRAP P/N 601R31025-29 IAW SRM AND REO. COMPLETED PRESSURE LEAK CHECK IAW AMM. NO LEAKS NOTED.

Part: SEAT TRACK — CORRODED (BS 559-621) · airframe 36,414 hrs · 32,153 cycles

LH SEAT RAIL BEAMS FS559.00+112 TO FS621.00 HAS CORROSION AROUND SCREW HOLES. (C-CHECK) RO: 06/12/2019 REMOVED AND.INSTALLED NEW L/H FLOOR BEAM CAP AT FS 559.00+112 TO FS 621.00 LBL 27 IAW SRM.

Part: SUPPORT — CORRODED (BS 559) · airframe 36,414 hrs · 32,153 cycles

RH SILL AT FS559.00+116 CORRODED. (C-CHECK) RO: 06/12/2019 INSTALLED NEW SILL FROM 559 TO 559+80 IAW SRM.

Part: PROXIMITY SENSOR — ICED (MLG) · airframe 34,555 hrs · 30,080 cycles

NOSE GEAR DISAGREE ON TAKE OFF RETURNED TO FIELD. EMERGENCY WAS DECLARED. PROXIMITY SENSORS WERE COVERED WITH ICE. THAWED ICE FROM GEAR. PERFORMED GEAR SWINGS AND EMERGENCY EXTENSION.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 33,052 hrs · 28,390 cycles

CORROSION ON END FITTING BETWEEN BS 605 TO 621, LBL 9. REPAIRED THE AREA OF THE FLOOR SUPPORT FITTING IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 33,052 hrs · 28,390 cycles

CORROSION ON END FITTING BETWEEN BS 605 TO 621, LBL 27. REPAIRED THE AREA OF THE FLOOR SUPPORT IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 33,052 hrs · 28,390 cycles

AFT CARGO FLOOR SUPPORT AT LBL 27 BS 605 TO 621 HAS CORROSION AT NUTPLATES. REPAIRED THE FLOOR SUPPORT IAW REO.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 33,052 hrs · 28,390 cycles

AFT CARGO DOOR SILL HAS CORROSION AT NUTPLATES. REPAIRED THE DOOR SILL IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 33,052 hrs · 28,390 cycles

AFT CARGO FLOOR SUPPORT AT LBL 9 BETWEEN BS 589 AND 621 HAS CORROSION AT NUTPLATES. REPAIRED THEFLOOR SUPPORT IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 33,052 hrs · 28,390 cycles

PANEL 699BB HAS MULTIPLE CHAFE SPOTS. REPAIRED THE AILERON LOWER SKIN PANEL IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 33,052 hrs · 28,390 cycles

RIGHT AILERON, LOWER SHROUD PANEL 699AB IS CHAFED. REPAIRED THE AILERON LOWER SKIN IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 33,052 hrs · 28,390 cycles

PANEL 699CB HAS CHAFED. REPAIRED THE RT AILERON SHROUD PANEL IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,052 hrs · 28,390 cycles

LEFT INBOARD FLAP VANE, THE OTBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,052 hrs · 28,390 cycles

LEFT INBOARD FLAP VANE, THE MID-CENTER LEADING EDGE IS CHAFED. REPLACED THE FLAP VANE CAP IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 29,326 hrs · 24,501 cycles

RIGHT SIDE WHEEL WELL HAS VOLUMETRIC FUSE SUPPORT BRACKET CRACK. C-CHECK, COMPLIED WITH STS EA. REMOVED DAMAGED RT SIDE VOLUMETRIC FUSE SUPPORT BRACKET AND REPLACED WITH SERVICEABLE BRACKET.

Part: SUPPORT BRACKET — CRACKED (LT MLG WW) · airframe 29,326 hrs · 24,501 cycles

LT SIDE WHEEL WELL HAS VOLUMETRIC FUSE SUPPORT BRACKET CRACK. C-CHECK, RO 4/22/15, REMOVED DAMAGED LT SIDE VOLUMETRIC FUSE SUPPORT BRACKET AND REPLACED WITH SERVICEABLE BRACKET REF STS EA.

Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 29,326 hrs · 24,501 cycles

RT SIDE WHEEL WELL HAS BRAKE APPLICATION PRESSURE TRANSDUCER SUPPORT BRACKET CRACK. C-CHECK, COMPLIED WITH STS EA, REMOVED DAMAGED RT WHEEL WELL BRAKE APPLICATION PRESSURE TRANSDUCER SUPPORT BRACKET AND REPLACED WITH SERVICEABLE BRACKET REF STS EA,

Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 29,326 hrs · 24,501 cycles

RT SIDE WHEEL WELL HAS HYDRAULIC LINES SUPPORT BRACKET CRACK NEXT. BRAKE APPLICATION PRESSURE TRANSDUCER C-CHECK, RO 4/22/15. INSTALLED SERVICEABLE RH WHEEL WELL HYD. LINES SUPPORT BRACKET NEXT TO BRAKE APPLICATION PRESSURE TRANSDUCER REF STS EA.

Part: SUPPORT BRACKET — CRACKED (LT MLG WW) · airframe 29,326 hrs · 24,501 cycles

LEFT SIDE WHEEL WELL HAS BRAKE APPLICATION PRESSURE TRANSDUCER SUPPORT BRACKET CRACK. C-CHECK RO 4/22/15, REMOVED DAMAGED LT WHEEL WELL BRAKE APPLICATION PRESSURE TRANSDUCER SUPPORT BRACKET AND REPLACED WITH SERVICEABLE BRACKET REF STS EA.

Part: POST — CRACKED (BS 409) · airframe 29,326 hrs · 24,501 cycles

FS409 +128 LBL27 POST HAS POSSIBLE CRACK EVALUATED AT BOTTOM SIDE, MARKED, C-CHECK RO 4/22/15. INSTALLED VERTICAL POST AT FS 409+128, LBL 27, INBD SIDE REF SRM & STS EA.

Part: POST — CRACKED (BS 409) · airframe 29,326 hrs · 24,501 cycles

FS409 +128 RBL27, POST HAS POSSIBLE CRACK EVALUATE AT BOTTOM SIDE, MARKED INBD SIDE. C-CHECK RO 4/22/15, LOCATED, FIT AND DRILLED NEW VERTICAL POST AT FS 409+128, RBL 27 INBD REF SRM INSTALLED NEW VERT POST AT FS 409, RBL 27 INBD SECTION SRM 51 AND STS EA.

Part: POST — CRACKED (BS 409) · airframe 29,326 hrs · 24,501 cycles

FS409 +128, LBL18 POST HAS CRACK AT BOTTOM SIDE, MARKED, C-CHECK, RO 4/22/15, INSTALLED INBD AND OTBD VERTICAL POSTS AT FS 409+128, LBL 18, REF REO.

Part: POST — CRACKED (BS 409) · airframe 29,326 hrs · 24,501 cycles

FS409 +128, RBL18 POST HAS POSSIBLE CRACK EVALUATE AT BOTTOM SIDE, MARKED OTBD SIDE. C-CHECK RO 4/22/15, LOCATED AND DRILLED NEW POST AT FS.409, RBL.18 OTBD SIDE REF AND REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,326 hrs · 24,501 cycles

CRACK AT FS 280.00 BEAM WEB AT RBL 9, C-CHECK RO 4/22/15, COMPLIED REPAIR OF THE FS 280.00 BEAM WEB AT RBL 9, REF REO.

Part: FLOOR PANEL — CRACKED (BS 460) · airframe 29,326 hrs · 24,501 cycles

PRESSURE FLOOR SKIN PANEL CRACK AT FS460.00 BETWEEN BL0.0 AND LBL9.0, C-CHECK, RO 4/22/15. INSTALLED REPAIR DOUBLERS: -3, -5, -7, -9, REF REO.

Part: VANE — FAILED (RT WING TE FLAP) · airframe 29,326 hrs · 24,501 cycles

RT INBD FLAP VANE CENTER L/E SECTION WORN OUT OF LIMITS REPLACE, C-CHECK RO 4/22/15, R & R BAD RT INBD FLAP VANE L/E SECTION WITH NEW PART REF DWG 601R14303, REV J, DATED MAY/13, 1996. RESTORED FINISH REF STS E/A.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 29,326 hrs · 24,501 cycles

RIGHT INBD FLAP VANE L/E CHAFED, OTBD OF CENTER VANE MOUNT. C-CHECK RO 4/22/15, EVALUATED CHAFE MARK RT INBD FLAP VANE CENTER L/E SECTION ORIGINAL MATERIAL THICKNESS IS 0.050 REMAINING MATERIAL 0.000 FLAP VANE CENTER SECTION IS OUT OF REPAIRABLE LIMITS REF REO L/E SECTION REPLACED ON MX TRANS 12055576.

Part: STRUCTURE — CHAFED (RT MLG DOOR) · airframe 29,326 hrs · 24,501 cycles

RT MLG DOOR AFT OTBD EDGE CHAFED. C-CHECK, RO 4/22/15, COMPLIED WITH REPAIR OF RT MLG DOOR OTBD EDGE REF REO.

Part: SKIN — DENTED (BS 605) · airframe 29,326 hrs · 24,501 cycles

DENT BELOW CARGO DOOR JUST AFT OF FRAME FS605 AND JUST ABOVE STRINGER 22L. C-CHECK, RO 4/22/15, INSTALLED REPAIR PARTS TO OUTER SKIN AT FRAME FS 605.0 AND STR 22L, REF STS EA.

Part: SKIN — DENTED (RT WING) · airframe 29,326 hrs · 24,501 cycles

FOUND A DENT ON THE RT UPPER WING SURFACE 5.25" OTBD OF WS 47.61, 11.25" FORWARD OF THE WING T/E AND 2.5" INBD OF THE RT WING INBD GROUND SPOILER. DENT DEPTH IS 0.0255". PERMANENT REPAIR , COMPLETED ON RH UPPER WING SURFACE 5.25" OTBD OF WS 47.61, 11.25" FORWARD OF THE WING T/E AND 2.5" INBD OF THE RT WING INBD GROUND SPOILER REF STS EA.

Part: MOUNT — GALLED (RT ENGINE) · airframe 28,754 hrs · 23,923 cycles

RT ENGINE FORWARD MOUNT LINK ASSY AND CLAMP BUSHING GALLED. R & R RT FWD MOUNT LINK ASSY IAW AMM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 28,128 hrs · 23,334 cycles

EMERGENCY LIGHTS DO NOT COME. R & R ALL FOUR BATTERY PACKS IAW AMM. OPS CHECKED GOOD.

Part: STRIP — ROUGH (TE FLAP) · airframe 27,276 hrs · 22,511 cycles

WHEN SELECTING FLAPS 45, AIRCRAFT HAS PROMINENT RIGHT ROLL CHARACTERISTICS THAT NEEDS ALMOST 1/2 OF THE LT AILERON TRIM TO NEUTRALIZE. FLT 4689 SANDED RT OTBD FLAP TEFLON STRIP LE TO A SMOOTH TRANSITION TO THE ADJACENT PAINT SURFACE IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,452 hrs · 21,703 cycles

1ST EMERGENCY OVERHEAD LIGHT IS OUT. FLT#4830 RELAMPED.

Part: LEVER — CHAFED (CABIN DOOR) · airframe 25,694 hrs · 20,951 cycles

MAIN CABIN DOOR FORWARD PULL-IN LEVER IS CHAFED. (C-CHECK) MAIN CABIN DOOR FORWARD PULL-IN LEVER REPAIRED IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 25,694 hrs · 20,951 cycles

FS 409.0+128 RBL 18.00 INBD AFT RADIUS OF VERT POST CRACK INDICATION NOTED. (C-CHECK) REPLACED CRACKED POST WITH NEW POST AT FS 409+ 128 IAW REO.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 25,419 hrs · 20,664 cycles

NO PRESSURIZATION, SWITCHED TO MANUAL MODE FOR REMAINDER OF THE FLIGHT. (FLT 4713) REPLACED NR 1 PRESSURE CONTROLLER AND CABIN PRESS CONTROL PANEL ASSEMBLY IAW AMM. OPS CHECK NORMAL. P/N: 2119768-8 S/N ON: 61-C1162 S/N OFF: 92-C1480 P/N: 2119764-6 S/N ON: 21-C0361 S/N OFF: 73-C0750

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,358 hrs · 20,606 cycles

RIGHT SIDE NR 3 LOWER EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. (FLT 4719) REPLACED NR 3 EMERGENCY LIGHT INVERTER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,059 hrs · 20,336 cycles

NR 2 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 4754) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 24,916 hrs · 20,208 cycles

EMERGENCY SIGN AT EXIT ROW RT SIDE BURNED OUT. (FLT 4716) RELAMPED EMERGENCY SIGN.

Part: CONNECTOR — LOOSE (EXIT SIGN) · airframe 24,830 hrs · 20,122 cycles

LOWER EMERGENCY EXIT SIGN AT SEAT 8D IS OUT. (FLT 4517) RE-SECURED LOOSE CONNECTION ON LOWER EMERGENCY EXIT SIGN ON ROW 8D.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,770 hrs · 20,060 cycles

RIGHT SIDE OVERWING EXIT LOWER BLUE LIGHT IS INOPERATIVE. (FLT 4514) REPLACED NR 4 EMERGENCY LIGHTING BATTERY PACK IN REFERENCE TO AMM. P/N: AD-2013-1A S/N OFF: 72169.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,413 hrs · 19,707 cycles

NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,358 hrs · 19,658 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4539) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,121 hrs · 19,437 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4628) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,932 hrs · 19,256 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4606) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,932 hrs · 19,256 cycles

NR 3 AND NR 5 EXTERIOR EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,832 hrs · 19,158 cycles

THE 3RD EMERGENCY OVERHEAD LIGHT INOPERATIVE. (FLT 4583) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,806 hrs · 19,129 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. (FLT 4850) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,400 hrs · 18,720 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4777) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,348 hrs · 18,672 cycles

NR 2 AND 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,209 hrs · 18,544 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4724) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,172 hrs · 18,506 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,835 hrs · 18,187 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4649) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,730 hrs · 18,077 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4442) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,603 hrs · 17,939 cycles

NR 3 CEILING EMERGENCY LIGHT IS OUT. (FLT 4469) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,559 hrs · 17,894 cycles

NR 3 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 4728) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,533 hrs · 17,868 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4523) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,984 hrs · 17,361 cycles

FS 621 BULKHEAD WEB CRACKED NEAR AFT CARGO DOOR TRACK. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,984 hrs · 17,361 cycles

FS 202 BULKHEAD CRACKED AT PARKING BRAKE CABLE HOLE. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,984 hrs · 17,361 cycles

FS 599 PRESSURE BULKHEAD CRACKED NEAR LEFT CAP RADIUS. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,683 hrs · 17,095 cycles

NR 3 CEILING EMERGENCY LIGHT IS OUT. (FLT 4671) RELAMPED EMERGENCY LIGHT.

Part: MECHANISM — OBSTRUCTED (CABIN DOOR) · airframe 21,090 hrs · 16,575 cycles

THE MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. (FLT 4722) REMOVED ICE BUILT UP ON MAIN CABIN DOOR LATCH MECHANISMS AND OPERATED DOOR NUMEROUS TIMES. FOUND TO OPERATE SMOOTHLY WITH NO DEFECTS NOTED.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 19,935 hrs · 15,594 cycles

MCD IS DIFFICULT TO OPEN. (FLT 4625) OPERATIONAL CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,342 hrs · 15,079 cycles

NR 2 OVERHEAD EMERGENCY LIGHT INOP. (FLT 4486) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,584 hrs · 14,476 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 10 AND 13 INOP. (FLT 4722)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,387 hrs · 14,326 cycles

NR 4 CEILING EMERGENCY LIGHT INOP. (FLT 4702) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 17,972 hrs · 13,990 cycles

THE AFT STRIP OF EMERGENCY LIGHTS INOP. (FLT 4530) OPERATIONAL CHECK NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 17,619 hrs · 13,726 cycles

FLOOR LEVEL EMERGENCY LIGHT BROKEN. (SVC CHECK) REPLACED LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,602 hrs · 13,714 cycles

OVERHEAD EMERGENCY LIGHT IN CABIN INOP. (FLT 4625) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,587 hrs · 13,702 cycles

NR 2 CEILING EMERGENCY LIGHT INOP. (FLT 4473) RELAMPED EMERGENCY LIGHT.

Part: TORQUE LINK — DISCONNECTED (NLG) · airframe 17,388 hrs · 13,552 cycles

NOSE DOOR OPEN MESSAGE DISPLAYED. (FLT 4661) RECONNECTED TORQUE LINKS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,730 hrs · 13,812 cycles

FS 280 CLIPS CRACKED. (C CHECK) REPLACED PER SRM.

Part: ISOLATOR — CRACKED (FUSELAGE) · airframe 17,730 hrs · 13,812 cycles

AFT PRESSURE BULKHEAD ISOLATOR CRACKED. (C CHECK)REPLACED PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,730 hrs · 13,812 cycles

CLIPS CRACKED FS 325-484. (C CHECK) REPAIRED PER REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 17,336 hrs · 13,515 cycles

FLT 4464 - AFT EMERGENCY LIGHT INOP. RELAMPED.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 16,883 hrs · 13,171 cycles

FLT 4467 - NOSE GEAR DISAGREE MESSAGE DISPLAYED ON EXTENSION. REPLACED NOSE LANDING GEAR SELECTOR VALVE PN 750006000, SN OFF 2110.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 16,740 hrs · 13,061 cycles

FLT 4423 - EXIT LIGHT COVER AT MAIN CABIN DOOR IS MISSING. REPLACED FLOOD LIGHT ASSEMBLY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,231 hrs · 12,666 cycles

FLT 4383 - AFT CEILING LEVEL EMERGENCY LIGHT INOP, RELAMPED.

Part: ANGLE — CRACKED (BS 640) · airframe 16,206 hrs · 12,646 cycles

C-CHECK, RIGHT SIDE REINFORCEMENT ANGLE AT FS 640 CRACKED. REPAIRED PER SB 601R-53-061.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,038 hrs · 12,518 cycles

OVERHEAD EMERGENCY LIGHT, THIRD FROM THE GALLEY, INOP (FLT 3966). RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 14,720 hrs · 11,491 cycles

FLT 3898 - EMERGENCY LIGHTS FROM 9C TO 12C ARE NOT WORKING. RESECURED LIGHT STRIP CONNECTION. OPS CHECK GOOD.

Part: ENGINE — LEAKING (RIGHT) · airframe 13,772 hrs · 10,740 cycles

FLT 3909 - AFTER ROTATION, RECEIVED A "SMOKE TOILET" MESSAGE ALONG WITH SMOKE IN THE CABIN. FOUND ENGINE OIL MIGRATING INTO THE BLEED SYSTEM. REPLACED RIGHT ENGINE WITH SERVICEABLE UNIT IAW CRJ 200 MM 71-00-00. ALL OPS CHECK AND LEAK CHECKS GOOD, PN CF34-3B1, SN/OFF 873574.

Part: WINDOW — FAULTY (COCKPIT) · airframe 13,711 hrs · 10,684 cycles

FLT 3968 - LEFT WINDOW CAUTION MESSAGE ILLUMINATED. REPLACED LEFT COCKPIT WINDOW IAW CRJ AMM 56-11-01, P/N NP139322-11 S/N OFF 06347H9678.

Part: UNKNOWN — SMOKE (CABIN) · airframe 13,668 hrs · 10,645 cycles

FLT 3938 - RETURNED TO FIELD FOR SMOKE IN THE CABIN AND A "SMOKE TOILET" MESSAGE. OPERATED BOTH PACKS FOR 15 MINUTES AND CLEARED RESIDUAL SMOKE ODOR OUT OF PACK SYSTEMS.

Part: LIGHT — BURNED OUT (CABIN) · airframe 12,878 hrs · 10,029 cycles

EMERGENCY LIGHT POD IN CEILING BY LAVATORY IS BURNED OUT, FLIGHT NR 3954. RELAMPED EMERGENCY LIGHT. OPS CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,212 hrs · 10,294 cycles

FS 280 FLOOR SUPPORT BEAM IS CRACKED AT LBL9, FOUND AT C-CHECK. COMPLIED WITH STANDARD REPAIR 601R 53-00-57A TO REPAIR FS280 LBL9 UPPER FLANGE OF FLOOR SUPPORT BEAM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,212 hrs · 10,294 cycles

FS 280 FLOOR SUPPORT BEAM IS CRACKED AT LBL9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS TO FS 280 SUPPORT BEAM AT LBL9 LOWER PER CRJ200 SRM 51-42-06 P11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,212 hrs · 10,294 cycles

FS 280 FLOOR SUPPORT BEAM IS CRACKED AT RBL9, FOUND AT C-CHECK. COMPLIED WITH REO 601R-53-11-171 REVISION "D" TO REPAIR FS 280 RBL9 FLOOR SUPPORT BEAM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 11,611 hrs · 9,074 cycles

CAPT LEFT SIDE WINDOW HAS TWO CRACKS. REPLACED LEFT SIDE WINDOW IAW RII 56-220-1000 AND AMM 56-12-01, PN OFF NP139322-001 SN OFF 02212H2635.

Part: CONTROL UNIT — OUT OF ADJUST (SPOILERS) · airframe 9,591 hrs · 7,565 cycles

SPOILERONS FAULT STATUS MSG ON TAXI OUT. REPLACED NR 2 SECU REF AMM 27-61-05. OPERATIONAL CHECK GOOD.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 9,293 hrs · 7,338 cycles

FOUND FWD SIDE OF PASSENGER DOOR EDGE MEMBER CRACK. PERFORMED REPAIR TO PASSENGER DOOR EDGE MEMBER IAW REO NR 601R-52-11-279.

Part: TRIM PANEL — MALFUNCTIONED (AILERONS) · airframe 8,962 hrs · 7,084 cycles

AILERON TRIM STUCK AT RT WING DOWN. REPLACED AILERON TRIM PANEL. OPERATIONAL CHECK GOOD IAW MM 27-12-10.

Part: TRIM SWITCH — INOPERATIVE (STAB) · airframe 6,562 hrs · 5,169 cycles

CAPTAINS SIDE STAB TRIM SWITCH INOPERATIVE. CAPTAINS SIDE STAB TRIM SWITCH REPLACED IAW AMM TASK 27-41-05-400-801. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 6,309 hrs · 4,962 cycles

FLIGHT SPOILER AND INBOARD GROUND SPOILER MSG (STATUS) WILL NOT CLEAR. REMOVED AND REPLACED NR 2 SECU WITH A SERVICEABLE SECU IAW 27-00-00. OPERATIONAL CHECK GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 4,399 hrs · 3,401 cycles

FS 625 RIGHT ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,399 hrs · 3,401 cycles

CRACKED INTERCOSTAL AT STA 484.00 LBL 36. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV. A.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,385 hrs · 3,390 cycles

FS 280 RIGHT FLOORBEAM RBL 9.0 OUTBOARD ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-13, 51-41-21, 51-42-06, AND 51-23-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,399 hrs · 3,401 cycles

FS 621 RIGHT FLOOR SUPPORT ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV. B.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 4,331 hrs · 3,342 cycles

CARGO SMOKE MESSAGE ON TAXI. REMOVED AND REPLACED FORWARD AND AFT CARGO SMOKE DETECTORS REF AMM 26-15-01. CARGO SMOKE TEST FUNCTIONS GOOD. P/N: 473597-19, S/N OFF: 2086, S/N OFF: 1315.

Part: CONTROL PANEL — INOPERATIVE (AIL/RUDER) · airframe 4,096 hrs · 3,161 cycles

LT WING DOWN AILERON TRIM IS INOPERATIVE. REMOVED AND REPLACED THE AILERON/RUDDER TRIM PANEL ASSEMBLY. BOTH SYSTEMS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (STAB TRIM) · airframe 2,824 hrs · 2,166 cycles

RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES IN FLIGHT. COMPLIED WITH QRH, COULD NOT RE-ENGAGE ANY STAB TRIM SYSTEM. TESTED AND FUNCTIONALLY CHECKED STAB TRIM AND HSTCU SYSTEM IAW MM 27-40-00. NO FAULTS FOUND.

Part: COMPUTER — MALFUNCTIONED (AHRS) · airframe 329 hrs · 247 cycles

IN FLIGHT THE FIRST OFFICER'S AHAR INDICATES +3 DEGREES NOSE UP ON THE ADI. TRANSFERRED BOTH DISPLAYS TO AHAR NR 1 AND RETURNED TO DFW. REMOVED NR 2 AHRS COMPUTER AND REPLACED WITH A SERVICEABLE ONE IAW CL600 MM 34-21-01. OPS CHECKS GOOD.