N459SW

Part: SEAT TRACK — GOUGED (BS 559) · airframe 39,236 hrs · 36,323 cycles

SEAT TRACK AT LBL 9, BS 559+ 4 - 559+86 HAD MULTIPLE SCRATCHES, GOUGES, & CORROSION RUNNING LENGTHWISE ALONG LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53--01-11-400-802, STEP B.

Part: SEAT TRACK — DAMAGED (BS 559) · airframe 39,236 hrs · 36,323 cycles

SEAT TRACK, RBL 9, BS 559+ 4 - 559+86 HADS MULTIPLE SCRATCHES, GOUGES, & CORROSION RUNNING LENGTHWISE ALONG LENGTH OF THE TRACK. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, & 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 39,236 hrs · 36,323 cycles

LEFT SEAT TRACK HAD MULTIPLE AREAS CORRODED & GOUGED, BS 409 - 409+128. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485 REV-D.

Part: SEAT TRACK — CORRODED (BS 559 RBL 9) · airframe 39,236 hrs · 36,323 cycles

SEAT TRACK AT RBL 9.0 BETWEEN APPROX. FS 559 + 96 AND FS 559 + 116 CORRODED. REMOVED AND REPLACED FLOOR SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: STRAP — CORRODED (BS 559) · airframe 39,236 hrs · 36,323 cycles

FLOOR SUPPORT STRAP AT BS 559 BETWEEN APPROX. RBL 27 & 42 WAS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT STRAP IAW SRM 51-42-06.

Part: STRAP — CORRODED (BS 559) · airframe 39,236 hrs · 36,323 cycles

FLOOR SUPPORT STRAP AT BS 559 BETWEEN LBL 27 & 42 WAS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-43-00 AND SRM 53-41-43-01. LOCATED, DRILLED, AND TRIMMED A NEW STRAP IAW SRM 51-40-11. INSTALLED THE NEW STRAP IAW SRM 51-42-06. COMPLIED WITH DWG 601R31025 REV. N.

Part: SEAT TRACK — CORRODED (BS 559-621 LBL27) · airframe 39,236 hrs · 36,323 cycles

SEAT TRACK, LBL 27, FS 559+80 - 621 HAD MULTIPLE SHORT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-51-49, SRM 53-61-49, AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: FLOORBEAM — CRACKED (BS 280 RBL 7) · airframe 39,236 hrs · 36,323 cycles

FS 280 FWD FLOORBEAM HAD A VERTICAL CRACK AT APPROX RBL 7. REMOVED AND REPLACED THE FWD FLOORBEAM IAW SRM 51-42-06, AND DWG 600-34017 REV AD. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 409) · airframe 39,236 hrs · 36,323 cycles

RIGHT SEAT TRACK HAD MULTI AREAS OF CORRODED & GOUGED, BS 409 - 409+128. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: FLOORBEAM — CRACKED (BS 280 LBL 8) · airframe 39,236 hrs · 36,323 cycles

BS 280 FLOORBEAM HAD A SUSPECT CRACK LBL 8. REPAIRED THE FLOORBEAM IAW REO 601R-53-11-3817 REV- AND REO 601R-53-11-926 REV-B.

Part: SEAT TRACK — DAMAGED (BS 409-559 LBL9) · airframe 39,236 hrs · 36,323 cycles

SEAT TRACK, LBL 9, BS 409+126 - 559+4 HAD MULTIPLE SCRATCHES & GOUGES RUNNING LENGTHWISE ALONG LENGTH OF TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: SUPPORT BRACKET — CRACKED (BS 484 LBL27-36) · airframe 39,236 hrs · 36,323 cycles

FLIGHT CONTROL CABLE FAIRLEAD SUPPORT BRACKET AT BS 484 BETWEEN LBL 27 & 36 WAS CRACKED. REPAIRED THE SUPPORT BRACKET IAW REO 601R-53-41-3114 REV-.

Part: SEAT TRACK — CORRODED (BS 559 LBL 9) · airframe 39,236 hrs · 36,323 cycles

SEAT TRACK AT LBL 9.0 BETWEEN APPROX. BS 559 + 96 AND 559.00 + 116 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — GOUGED (BS 409-559 RBL9) · airframe 39,236 hrs · 36,323 cycles

SEAT TRACK, RBL 9, BS 409+126 - 559+4 HAD MULTIPLE SCRATCHES & GOUGES RUNNING LENGTHWISE ALONG LENGTH OF TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 & AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559-621 RBL27) · airframe 39,236 hrs · 36,323 cycles

SEAT TRACKS, RBL 27, BS 559+80 & 621 HAD MULTIPLE SHORT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW AMM AMM 53-01-11-400-802.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 39,236 hrs · 36,323 cycles

PAX DOOR PIANO HINGE FUSELAGE SIDE THE HINGE PIN HAS FLAT SPOTS AND THE HOLES ON THE HINGE ARE WORN/OBLONG. REMOVED AND INSTALLED NEW PAX DOOR HINGE IAW SRM 53-21-23, AND REO-601R-53-21-656 REV-A

Part: BULKHEAD — GOUGED (LAVATORY) · airframe 39,236 hrs · 36,323 cycles

EVALUATE AND REPAIR GOUGES ON AFT SIDE OF 9G CENTER BULKHEAD SKIN. BLENDED GOUGES AND REPAIRD AFT SIDE OF 9G CENTER BULKHEAD SKIN,& COMPLIED WITH EO CL-600-2B19-53-L07293.

Part: LANDING — SCRATCHED (RT WING) · airframe 39,236 hrs · 36,323 cycles

SCRATCHES NOTED ON LOWER RT WING ACCESS PANEL LANDING. BLENDED OUT DAMAGE IAW REO 601R-57-21-030 REV L BLEND IS WITHIN LIMITS IAW REO 601R-57-21-030 REV -L.

Part: BULKHEAD — GOUGED (LAVATORY) · airframe 39,236 hrs · 36,323 cycles

EVALUATE AND REPAIR GOUGES ON AFT SIDE OF 9G LAV BULKHEAD SKIN. BLENDED GOUGES AND REPAIRED AFT SIDE OF 9G LAV BULKHEAD SKIN, COMPLIED WITH EO CL-600-2B19-L07294A.

Part: SKIN — DENTED (BS 682) · airframe 39,236 hrs · 36,323 cycles

RIGHT FUSELAGE SKIN AT AEB DOOR CUTOUT NEAR BS 682 HAD A PROTRUDING DENT. REPAIRED THE SKIN IAW SRM 53-00-31, REPAIR 3, STEPS 4.A. (1)-(12) , ADDITIONAL 7EA DENTS IDENTIFIED NEAR BS 688 REWORKED AND FOUND TO BE WITHIN LIMITS IAW REO 601R-53-61-7935 REV -. MAJOR REPAIR.

Part: BULKHEAD — GOUGED (LAVATORY) · airframe 39,236 hrs · 36,323 cycles

EVALUATE AND REPAIR GOUGES ON AFT SIDE OF 9G LOUVER BULKHEAD SKIN. BLENDED GOUGES AND REPAIRED AFT SIDE OF 9G LOUVER BULKHEAD SKIN, IAW EO 600-2B19-53-L07292A.

Part: PRESSURE DECK — CRACKED (BS 461 BL0-RBL9) · airframe 39,236 hrs · 36,323 cycles

PRESSURE DECK WAS CRACKED AT BS 461 BETWEEN BL 0 & RBL 9. REPAIRED PRESSURE DECK IAW REO 601R-53-41-2598 REV -. LEAK CHECKS GOOD.

Part: BEAM — DAMAGED (BS 409 BL 0) · airframe 39,236 hrs · 36,323 cycles

F.S 409+128 BL 0.00 LH FWD VERTICAL BEAM DEFECT NOTED AT TOP FASTENER HOLE. REMOVED AND REPLACED VERTICAL BEAM IAW SRM 51-42-06, REV 39, SRM 51-42-22, REV 39, AND REO 601R-53-41-889 REV-C.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 39,236 hrs · 36,323 cycles

LEFT INBD FLAP VANE L/E SKIN CHAFED NEAR CENTER. REMOVED AND REPLACED LT INBD FLAP VANE L/E SKIN IAW DWG 601R14302 REV E AND SRM 51-42-13.

Part: STRIKER — DENTED (PAX DOOR SEAL) · airframe 39,236 hrs · 36,323 cycles

* PASSENGER DOOR AFT SEAL STRIKER DENTED NEAR UPPER END. REPAIED PASSENGER DOOR AFT SEAL STRIKER NEAR UPPER END IAW REO 601R-53-22-033, REV -D,

Part: BULKHEAD — DAMAGED (BS 621) · airframe 39,236 hrs · 36,323 cycles

MULTIPLE SCREW MARKS NOTED ON FWD FACE OF THE BS 621 BULKHEAD AT APPROX. 30IN ABOVE FLOOR. REPAIRED THE BS 621 BULKHEAD TOP DOUBLERS IAW REO 601R-53-61-7933 REV-.

Part: NONE — CRACKED · airframe 39,142 hrs · 36,205 cycles

FOUND BOTTOM HALF OF PAX DOOR TOP FOLDING STEP CRACKED UNDER LOGO PLATE (FILED CLOSED) REMOVED AND REPLACED BOTTOM HALF OF PAX DOOR TOP FOLDING STEP IN REF TO CRJ 200 AMM 52-11-04. OPS CHECK GOOD AT THIS TIME

Part: LANDING GEAR — MALFUNCTIONED · airframe 36,953 hrs · 33,515 cycles

GEAR DISAGREE ON INITIAL APPROACH. GO AROUND, RAN QRH, ALL GEAR CAME DOWN, LANDED AND TAXIED BACK TO GATE WITH NO FURTHER ISSUES. FLIGHT 4260 - FILED OPEN. THIS IS CURRENTLY A WORK IN PROGRESS.

Part: PRESSURE DECK — CRACKED (BS 449-473) · airframe 35,722 hrs · 31,936 cycles

PRESSURE FLOOR SKIN CRACKED AT LBL 9.00 BETWEEN FS449.85 AND FS473.15. (C-CHECK) RO 12/3/2019 ACCOMPLISHED REPAIR TO PRESSURE DECK AT LBL 9 AT FS449.85 AND FS473.15 IAW REO. REF CAMP #19682965 FOR ADDITIONAL WORK PERFORMED AND ALSO FOR CRACK, TRIM AND NDT PERFORMED.

Part: PRESSURE DECK — CRACKED (BS 449-473) · airframe 35,722 hrs · 31,936 cycles

PRESSURE FLOOR SKIN CRACK AT LBL 9.00 AFT OF 1ST CRACK, BETWEEN FS 449.85 AND FS473.15. ALSO SEE CAMP #19674937 . (C-CHECK) RO 12/3/2019 ACCOMPLISHED REPAIR IAW REO STRUCTURAL MAJOR REPAIR AND SRM -- ALSO REF TO CAMP #19674937 FOR WORKED PERFORMED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 33,710 hrs · 29,687 cycles

IDG1 CAUTION MESSAGE IN FLIGHT. RUN QRH, RETURN TO DTW. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. (FLT 4282) FO:07/27/2018 CLOSED DEFERRED IAW AMM.

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 32,246 hrs · 28,053 cycles

LEFT LOWER OUTBD WINDSHIELD ANGLE IS CRACKED. REMOVED AND REPLACED THE LT WINDSHIELD POST FITTING IAW SRM.

Part: SKIN — DENTED (BS 677) · airframe 32,246 hrs · 28,053 cycles

FUSELAGE SKIN, BS 677 BETWEEN STRINGERS 24R AND 25R DENTED. REPAIRED THE SKIN IAW REO.

Part: SPAR — CORRODED (LT WING) · airframe 32,246 hrs · 28,053 cycles

LEFT WING AUXILIARY SPAR ASSEMBLY HAS CORROSION AROUND MLG CONNECTORS. INSTALLED A NEW AUXILIARY SPAR IAW SRM.

Part: RETAINER — CORRODED (E/E BAY DOOR) · airframe 32,246 hrs · 28,053 cycles

MAIN AVIONICS DOOR SEAL RETAINER HAS CORROSION. REMOVED AND REPLACED ALL FOUR SEAL RETAINERS ON THE AVIONICS DOOR IAW SRM. OPS CHECKED GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 29,567 hrs · 25,079 cycles

RETURNED TO FIELD WITH SMOKE REPORTED IN CABIN BY F/A. CREW AND PAX REPORTED SMOKE COMING FROM LOWER AND UPPER AIR VENTS. RAN PACKS FOR AN EXTENDED PERIOD USING ENGINES AND APU AS A BLEED SOURCE. NO DEFECTS NOTED. SUSPECT DE-ICE FLUID CONTAMINATION.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 29,208 hrs · 24,690 cycles

GEAR DISAGREE. MAINS WOULD NOT COME DOWN. AFTER CYCLING GEAR HANDLE GEAR FINALLY EXTENDED. R & R MLG SELECTOR VALVE IAW AMM. OPS CHECK GOOD AT THIS TIME. PERFORMED SEVERAL GEAR SWINGS WITH NO FAULTS NOTED AT THIS TIME, GEAR EXTENDED AND RETRACTED NORMALLY IAW AMM. NO LEAKS NOTED AT THIS TIME. ACFT UPGRADED TO CAT II STATUS.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 29,087 hrs · 24,570 cycles

RT INBD FLAP VANE, OTBD, LE SKIN IS CHAFED. R & R RT INBD FLAP VANE OTBD L/E VANE CAP IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 29,087 hrs · 24,570 cycles

RT INBD FLAP VANE, MID OTBD L/E SKIN, DUE TO CHAFING. REMOVED, FABRICATED AND INSTALLED NEW RT INBD. FLAP VANE L/E CENTER SKIN SECTION IAW SRM.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 29,087 hrs · 24,570 cycles

RIGHT INBD FLAP CHAFED AT TOP CENTER ON UPPER SIDE. BLENDED CHAFE ON RT INBD FLAP AT TOP CENTER ON UPPER SIDE IAW SRM AND STS EA.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 29,087 hrs · 24,570 cycles

RT INBD FLAP CHAFED AT TOP INBD ON UPPER SIDE. BLENDED CHAFE ON RT INBD FLAP AT TOP INBD ON UPPER SIDE IAW SRM AND STS EA.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 29,087 hrs · 24,570 cycles

SEAT TRACK SECTION RBL9 BS 399 TO 409+126 HAS CORROSION ON MULTIPLE SPOTS. R & R SEAT TRACK SECTION IAW AMM.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 29,087 hrs · 24,570 cycles

SEAT TRACK SECTION RBL9, FS 364 TO FS 399 HAS MULTIPLE SPOTS OF CORROSION. R & R SEAT TRACK SECTION FROM FS364 TO FS399, RBL9 IAW AMM.

Part: SKIN — DENTED (RT WING) · airframe 28,270 hrs · 23,733 cycles

RT WING HAS TWO DENTS. REPAIRED IAW SRM.

Part: SKIN — CRACKED (NOSE) · airframe 27,250 hrs · 22,714 cycles

RIGHT NOSE SKIN CRACKED. R & R RT NOSE SKIN IAW SRM. R & R RADOME ASSY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,933 hrs · 22,394 cycles

EXTERIOR EMERGENCY LIGHT NR 2 INOPERATIVE. R & R LIGHT IAW AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 26,735 hrs · 22,166 cycles

OVERHEAD EXIT SIGN THE F/A INDICATOR PANEL IS MISSING THE RED LENS, REPLACED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 26,135 hrs · 21,553 cycles

FS 349.00 FRAME HAS AREAS OF CORROSION ON AFT SIDE OF FRAME BETWEEN STRINGER 264 & STRINGER 26L. C-CHECK INSTALLED A NEW FRAME SECTION IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 26,135 hrs · 21,553 cycles

FOUND FS 409:00+128, VERTICAL POST AT RBL 18.0 INBD SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS APPROXIMATELY .2 INCHES IN LENGTH 50% FSH. C-CHECK INSTALLED NEW VERTICAL POST IAW SRM & REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,961 hrs · 21,387 cycles

FS 202.75 PRESSURE BULKHEAD IS CRACKED AT THE PARKING BRAKE CABLE CUT-OUT. C-CHECK REPAIRED FS 202.75 PRESSURE BULKHEAD AT THE PARKING BRAKE CUT-OUT IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,190 hrs · 21,603 cycles

REAR PRESS BULKHEAD WEB HAS INDICATION NOTED AT LBL 18.0 WL 99 APPROXIMATELY 1.0 INCHES LONG 50% FSH. C-CHECK PERFORMED REPAIR IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,961 hrs · 21,387 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL0.0 BETWEEN WL 127 & WL135 8.0 INCH AREA. C-CHECK REPAIRED THE REAR PRESSURE BULKHEAD WEB AT BL0.0 BETWEEN WL 127 & 2L135 IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,163 hrs · 21,579 cycles

REAR PRESS BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0 0 BETWEEN WL127 & WL 135, 8.0 INCH AREA 80% FSH. C-CHECK REPAIRED IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,163 hrs · 21,579 cycles

REAR PRESS BULKHEAD WEB HAS INDICATION NOTED AT LBL 9 & WL111, APPROXIMATELY 1.0 INCHES LONG 50% FSH. C-CHECK REPAIRED IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,190 hrs · 21,603 cycles

REAR PRESS BULKHEAD WEB HAS INDICATION AT LBL 9 APPROXIMATELY WL 93, 2.0 INCHES LONG 90% FSH. C-CHECK PERFORMED REPAIR IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,961 hrs · 21,387 cycles

REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 9 WL111 APPROXIMATELY 1.0 INCHES LONG. C-CHECK REPAIRED REAR PRESSURE BULKHEAD WEB AT LBL9 WL111 IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,961 hrs · 21,387 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 18.0 WL99 APPROXIMATELY 1.0 INCHES LONG 50% FSH. C-CHECK PERFORMED REPAIR TO REAR PRESSURE BULKHEAD WEB AT LBL 18.0 WL 99 IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,794 hrs · 21,227 cycles

FWD MOST EMERGENCY POD LIGHT BURNED OUT. FLT 4850 RELAMPED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,729 hrs · 21,158 cycles

LT OVERWING FWD EXTERNAL EMERGENCY LIGHT IS BURNED OUT. FLT#4787 RELAMPED.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 25,992 hrs · 21,414 cycles

SUPPORT FITTING CRACKED IN RADIUS APPROXIMATELY 1 INCH LONG AT FS 460.00 AT LBL 10 UNDER THE FLOOR. C-CHECK REPLACED THE CRACKED SUPPORT FITTING FROM FS 460.00 AT LBL 10 IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,992 hrs · 21,414 cycles

FS 349.00 FRAME HAS AREAS OF CORROSION ON AFT SIDE OF FRAME, BETWEEN STRINGER 26R & 26L. C-CHECK INSTALLED A NEW FRAME IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,037 hrs · 19,429 cycles

EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 4663) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,955 hrs · 19,347 cycles

LEFT WING AFT EMERGENCY EXIT LIGHT IS OUT. (FLT 4763) RELAMPED EMERGENCY LIGHT.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 23,521 hrs · 18,933 cycles

RECEIVED NOSE GEAR DOWN AND LOCKED BUT THE TWO MAIN GEAR HAD RED HATCH MARKS. CYCLED GEAR HANDLE 3 TIMES NOSE GEAR CYCLED BUT MAINS REMAIN IN DISAGREE. (FLT 4529) REPLACED MLG SELECTOR VALVE PER AMM. PN: 750005000 SN OFF: 0763

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,439 hrs · 18,851 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4680) RELAMPED EMERGENCY LIGHT.

Part: FITTING — FAILED (MLG) · airframe 23,163 hrs · 18,591 cycles

GEAR DISAGREE ON EXTENSION AND THE MLG DID NOT EXTEND. FOLLOWED THE QRH AND THE GEAR CAME DOWN. (FLT 7757) REPLACED 90° ELBOW ON THE MLG RUNAROUND VALVE.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 23,139 hrs · 18,567 cycles

LEFT PACK CAUSING A BURNING SMELL. (FLT 4542) REPLACED THE TEMPERATURE SWITCH AND AIR CYCLE MACHINE. P/N: 782790-15, S/N OFF: 200209041, PN: AD-750659-17, SN OFF: 779199/73030.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,709 hrs · 18,149 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4725) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,676 hrs · 18,125 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4698) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,581 hrs · 18,038 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4511) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,436 hrs · 17,886 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4570) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,359 hrs · 17,814 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7770) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,330 hrs · 17,788 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7806) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,143 hrs · 17,613 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4579) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,077 hrs · 17,553 cycles

THE 1ST FORWARD CEILING EMERGENCY LIGHT IS OUT. (FLT 4456) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 23,088 hrs · 18,522 cycles

DAMAGE TO LEFT SIDE FS 559.0 PRESSURE BULKHEAD. (C-CHECK) REPAIRED PER REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,088 hrs · 18,522 cycles

CORROSION ON FLOORBEAM OUTBOARD FLANGE AT FS 615.0 LBL 27.0. (C-CHECK) REPAIRED IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,828 hrs · 17,313 cycles

AFT 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,809 hrs · 17,295 cycles

RIGHT REAR OVERWING EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4539) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,662 hrs · 17,164 cycles

NR 7 AND NR 8 EXTERIOR EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,662 hrs · 17,164 cycles

NR 2 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4670) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,662 hrs · 17,164 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,631 hrs · 17,136 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4547) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,598 hrs · 17,104 cycles

RIGHT OVERWING FORWARD EMERGENCY LIGHT IS OUT. (FLT 4629) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,598 hrs · 17,104 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4457) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,570 hrs · 17,078 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4507) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,538 hrs · 17,052 cycles

RIGHT OVERWING EXTERIOR FORWARD AND AFT EMERGENCY LIGHTS ARE OUT. (FLT 4763) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,490 hrs · 17,010 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4514) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,389 hrs · 16,921 cycles

THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4697) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,180 hrs · 16,719 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS NOT ILLUMINATING. (FLT 4604) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,071 hrs · 16,618 cycles

NR 2 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4733) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,777 hrs · 16,365 cycles

NR 3 CEILING EMERGENCY LIGHT IS OUT. (FLT 4449) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,777 hrs · 16,365 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4674) RELAMPED EMERGENCY LIGHT.

Part: ROLLER — OBSTRUCTED (SERVICE DOOR) · airframe 20,437 hrs · 16,072 cycles

SERVICE DOOR HARD TO OPEN. (SERVICE) REMOVED FOD FROM RECEPTACLE SIDE OF FORWARD DOWNLOCK ROLLER.

Part: RIB — CRACKED (HORIZ STAB) · airframe 19,976 hrs · 15,699 cycles

RIGHT HORIZONTAL STAB FORWARD INBOARD RIB CRACKED. (A-CHECK) REPLACED RIGHT HORIZONTAL STAB FORWARD INBOARD RIB PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,347 hrs · 15,154 cycles

THE 2ND EMERGENCY LIGHT AFT INOPERATIVE. (FLT 4490) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,829 hrs · 14,683 cycles

EMERGENCY CEILING LIGHT NR 2 INOP. (FLT 4750) RELAMPED EMERGENCY LIGHT.

Part: COVER — MISSING (CABIN) · airframe 17,973 hrs · 13,956 cycles

LIGHT COVER IN GALLEY BY MAIN CABIN DOOR IS MISSING. (FLT 4765) REPLACED LIGHT ASSEMBLY.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,651 hrs · 13,670 cycles

FS 621 BULKHEAD FORWARD FACE CRACKED ABOVE CARGO DOOR FITTING. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,651 hrs · 13,670 cycles

FS 559 PRESSURE BULKHEAD CRACKED. (C-CHECK) REPAIRED PER REO.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 18,112 hrs · 14,062 cycles

FS 621 FORWARD FACE ABOVE DOOR TRACK FITTING CRACKED. (C CHECK) REPAIRED PER REO.

Part: ATTACH FITTING — WORN (MLG) · airframe 18,112 hrs · 14,062 cycles

MLG FORWARD FAIRING ATTACH FITTINGS WORN BEYOND LIMITS. (C CHECK) REPLACED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,112 hrs · 14,062 cycles

FS 559 PRESSURE BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,583 hrs · 13,620 cycles

NR 1 OVERHEAD FLOOD EMERGENCY LIGHT INOP. (FLT 4685) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,486 hrs · 13,540 cycles

NR 3 EMERGENCY LIGHT INOP. (FLT 4846) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,245 hrs · 13,326 cycles

EMERGENCY LIGHT INOP. (FLT 4873) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,441 hrs · 12,676 cycles

FLT 4762 - RIGHT WING CENTER EMERGENCY EXIT LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,120 hrs · 12,428 cycles

FLT 4807 - NR 3 EMERGENCY LIGHT INOP. RELAMPED.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 15,387 hrs · 11,861 cycles

AD INSPECTION, ENGINE SUPPORT BEAM INSPECTION PER AD CONFIRMED CRACKS. REPAIRED PER SB60R-53-065.

Part: BEAM — CRACKED (ENGINE MOUNT) · airframe 14,236 hrs · 10,945 cycles

UPPER FORWARD ENGINE BEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS ON ENGINE BEAM WEB PER REO 601R-53-61-870 REV C AND REO 601R-53-61-2554.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,236 hrs · 10,945 cycles

CRACK FOUND ON UPPER SUPPORT FRAME AT FS280.0 AND RBL9.0, FOUND AT C-CHECK. INSTALLED REPAIR PARTS FOR UPPER SUPPORT FRAME PER REO 601R-53-111-137.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 13,075 hrs · 10,060 cycles

FLT 3757 - CLIMBING-OUT OF 11,000 FEET, CABIN WOULD NOT PRESSURIZE. RETURNED TO SLC. REPLACED CABIN PRESSURE CONTROLLER IAW CRJ 200 MM 21-31-16.

Part: B-NUT — LEAKING (APU FUEL SYSTEM) · airframe 11,476 hrs · 8,836 cycles

AFTER TAKEOFF FROM SLC, THE CABIN SMELLED OF FUEL AFTER THE APU WAS SHUTDOWN. FOUND APU FUEL SOLENOID TO BE LEAKING AT THE B-NUT CONNECTION. TIGHTENED B-NUT ON APU FUEL SOLENOID. NO LEAKS NOTED.

Part: CONNECTOR — CONTAMINATED (CABIN) · airframe 10,272 hrs · 7,973 cycles

EMERGENCY FLOOR PATH LIGHTING AFT OF EXIT ROW IS INOP. CONNECTION AT ROW 12 WET. DRIED CONNECTION. OPERATIONAL CHECKS GOOD.

Part: STRUCTURE — DETACHED (RT PYLON) · airframe 9,322 hrs · 7,258 cycles

RIGHT ENGINE HAS A PIECE OF COWL DETATCHED FROM IT'S FASTENING POINTS AND BENT BACK WHERE THE UNDERSIDE OF THE ENGINE PYLON MEETS THE ENGINE. REPLACED RIGHT ENGINE LOWER "STANG" FAIRING IAW CRJ MM 78-30-01.

Part: ANGLE — CRACKED (RT WING) · airframe 9,563 hrs · 7,447 cycles

RT BATT ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 601R 107091-3 ANGLE AND 601R 10709-14 COVER PLATE PER CRJ200 SRM 51-41-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 9,563 hrs · 7,447 cycles

CRACKED ANGLES (BOTH SIDES) OF INTERCOSTAL AT FS 484 LBL DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE AND NEW CLIP PER REO 601R-53-41-059 REV 'A'.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 9,563 hrs · 7,447 cycles

CRACK FOUND IN RADIUS OF FIFTH STEP PAX DOOR AFT STAIR SUPPORT, DISCOVERED DURING C-CHECK INSPECTION. PARTS INSTALLED IAW CRJ 200 REO 601R-52-11-702.

Part: FITTING — CRACKED (FUSELAGE) · airframe 9,563 hrs · 7,447 cycles

FS 280 RT OTBD BL9 CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP PN 601R 3113-58 PO NR 62687 RT OUTBD BL9 FS 280 PER CRJ200 SRM 51-42-06 PG 11/18.

Part: FITTING — CRACKED (FUSELAGE) · airframe 9,563 hrs · 7,447 cycles

FS 280 RT INBD BL9 CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP PN 601R 3113-58 PO NR 62687 RT INBD BL9 FS 280 PER CRJ200 SRM 51-42-06 PG 11/18.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 9,563 hrs · 7,447 cycles

CRACK BETWEEN STEPS 5 AND 6 FWD SIDE OF HANDRAIL SUPPORT PAX DOOR, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS 601R-52-11-702-1 DOUBLER AND ANGLE PER CRJ200 RE0 601R 52-11-702.

Part: STEP — CRACKED (PAX DOOR) · airframe 9,563 hrs · 7,447 cycles

STEP 4 PAX DOOR CRACKED ON AFT SIDE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER, SHIM AND ANGLE PER CRJ200 REO 601R 520-11-1060 REV 'A'.

Part: ANGLE — CRACKED (RT WING) · airframe 9,563 hrs · 7,447 cycles

RT BATT ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R 57-61-046.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 9,563 hrs · 7,447 cycles

FS 280 LT SIDE OTBD OF RL9 FLOOR SUPPORT ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIP ON FS 280 2/B LBL 9 PN 601R31113-57.

Part: FITTING — CRACKED (FUSELAGE) · airframe 9,563 hrs · 7,447 cycles

FS 280 LT INBD BL9 CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP PN 601R 3113-58 PO NR 62687 LT INBD CLIP AND SHIM FS 280 PER CRJ200 SRM 51-42-06 PG 11/18.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 9,563 hrs · 7,447 cycles

CRACKED FLOOR SUPPORT AT AFT BULKHEAD FS621 LBL44, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLES AND STRAP TO FLOOR SUPPORT AT AFT BULKHEAD FS 621 LBL 44 PER CRJ200 SRM 51-42-06 PG 11 AND 51-42-21 PG 17.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 9,563 hrs · 7,447 cycles

CRACKED ANGLES (BOTH SIDES) OF INTERCOSTAL AT FS 484 RBL27-36, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE AND NEW CLIP PER REO 601R-53-41-059 REV 'A'.

Part: FITTING — CRACKED (FUSELAGE) · airframe 9,563 hrs · 7,447 cycles

FS 625 LT CLIP AT STRINGER 12 CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED FS 625 LT CLIP WITH NEW CLIP P/N 601-35012-51 PO 64386 PER CRJ200 SRM 51-42-06 PG 8 AND 11; 12; 13.

Part: ADC — FAILED (NR 1) · airframe 9,590 hrs · 7,466 cycles

AT ROTATION, CA SIDE IAS FAILURE AND ALT FAILURE WITH RED FLAGS. REPLACED NR 1 ADC IAW MM 34-13-01 AND PURGED NR 1 AND NR 2 PITOT/STATIC SYSTEM IAW MM 34-11-00. OPERATIONAL CHECKS GOOD.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 9,145 hrs · 7,124 cycles

COMPLETE IAS FAILURE ON CAPTAIN'S SIDE AND CENTER BACKUP IAS. EFIS COMP MON, IAS, AND ALT, FOLLOWED BY PITCH MESSAGES ON CAPTAIN'S PFD. ALTIMETERS WERE +200 OFF FROM FO SIDE, PITCH, CA SIDE +7 DEGREES. PURGED MAIN AND STANDBY SYSTEM IAW CRJ MM 34-11-00. REPLACED STANDBY IAS IAW 34-12-01 AND REPLACED BOTH ADC IAW 34-13-01. LEAK CHECK PER ST 34-406. SYSTEM OPS CHECKS GOOD. ADC PN'S 822-0372-445 SN'S/OFF 2563 AND 64MP.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 8,675 hrs · 6,772 cycles

GND SLR FAULT MSG. SPOILERON FAULT MSG. PINNED AND OHMED WIRES FROM 2AICN/7A-7B (SECU) TO DCU 2A1WA/6G AND H. CHECKED FOR POWER ON PINS 2A/CN/C4, 5, AND 6. CLEANED PINS ON SECU RACK AND DCU RACK REINSTALLED ORIGINAL DCU AND SECU IN ORIGINAL SPOTS. OPERATIONAL CHECK NORMAL IAW CRJ MM 27-61-05, 27-64-00, 27-65-00.

Part: WINDOW — CRACKED (COCKPIT) · airframe 8,275 hrs · 6,479 cycles

WHILE DESCENDING INTO CALGARY OUT OF 6000 FT NOTICED CAPT SIDE WINDOW WAS CRACKED. REPLACED PILOT'S SIDE WINDOW IAW CRJ AMM 56-11-01-400-801, P/N: 601R33033-11 S/N OFF: 02347H2947.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 7,886 hrs · 6,193 cycles

FLIGHT SPOILERS FAULT STATUS MESSAGE DISPLAYED. REPLACED RT NR 2 PCU ON RT FLIGHT SPOILER IAW 27-62-01. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 7,207 hrs · 5,688 cycles

NR 2 STAB CHANNEL WILL NOT ENGAGE. REPLACED HSTA AND MOTOR CONTROL IAW AMM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. P/N 8396-3, S/N OFF 969.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 6,787 hrs · 5,375 cycles

SPOILERON FAULT, STATUS MSG APPEARED ON TAXI. REPLACED RIGHT INBOARD SPOILERON PCU. OPERATIONAL CHECK GOOD IAW 27-64-01.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 6,754 hrs · 5,347 cycles

NR 2 STAB TRIM WILL NOT ENGAGE. REPLACED HSTA, AND MCU IAW 27-42-01. OPERATIONAL CHECK GOOD, PN 7062-3, SN/OFF 1067.

Part: TRIM SWITCH — INOPERATIVE (VERTICAL STAB) · airframe 6,725 hrs · 5,327 cycles

STAB NR 2 CHANNEL WILL NOT ENGAGE. REPLACED FOS TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD IAW AMM 27-44-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,519 hrs · 3,559 cycles

FS 621 FLOOR SUPPORT ANGLE RIGHT SIDE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PIECES IAW CRJ REO 601R-53-61-117 REV "B".

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,519 hrs · 3,559 cycles

FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11.

Part: FLOORBEAM — CRACKED (FUSLEAGE) · airframe 4,519 hrs · 3,559 cycles

FS 280 LEFT FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11.

Part: MANIFOLD — MALFUNCTIONED (GROUND SPOILER) · airframe 2,898 hrs · 2,272 cycles

INBOARD AND OUTBOARD GROUND SPOILER FAULT DURING TAKEOFF ROLL. REMOVED AND REPLACED OUTBOARD GROUND SPOILER MANIFOLD PER AMM 27-63-05. OPS AND LEAK CHECK GOOD. S/N OFF 0100T.

Part: COMPUTER — MALFUNCTIONED (FLIGHT CONTROL) · airframe 2,510 hrs · 1,975 cycles

DURING CLIMBOUT YAW DAMPER 2 DISENGAGED AND WOULD RESET FOR 2 TO 5 MINUTES AND THEN DISENGAGE. REMOVED AND REPLACED FCC 2 IAW 22-12-14. OPS CHECK GOOD.

Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 2,257 hrs · 1,789 cycles

ON TAXI OUT, RECEIVED FLAPS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED FLAP PDU IAW MM 27-52-01. OPS CHECK GOOD. P/N 865D100-7, S/N ON 0831, S/N OFF 1036.

Part: BPSU — MALFUNCTIONED (BRAKE POSITION) · airframe 2,009 hrs · 1,599 cycles

AFTER TAKEOFF AT FLAP RETRACTION RECEIVED FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED RIGHT BPSU IAW CRJ AMM 27-51-10, OPS CHECK GOOD.

Part: PCU — MALFUNCTIONED (LT OB SPOILER) · airframe 1,184 hrs · 952 cycles

SPOILERON FAILS DURING TAKEOFF AND LANDING ROLL (STATUS MESSAGE). REMOVED AND REPLACED LEFT OUTBOARD SPOILER PCU IAW 27-62-01. OPS AND LEAK CHECKS GOOD.

Part: TRANSDUCER — MALFUNCTIONED (STALL WARNING) · airframe 1,004 hrs · 803 cycles

STALL FAIL CAUTION ILLUMINATED. REMOVED AND REPLACED STALL COMPUTER AND MACH TRANSDUCER IAW A/C MM 27-35-25. BOTH OPS CHECKS GOOD. P/N: 3995100208, S/N OFF: 162, S/N ON: 149.

Part: CONTROL PANEL — MALFUNCTIONED (AUTOPILOT SYS) · airframe 963 hrs · 772 cycles

ALTITUDE PRESELECT NOT HOLDING ALTITUDE/DEPARTED PRESELECT AND RAN UP AND DOWN UNCONTROLLABLE. PRESELECT KNOB WOULD NOT CONTROL. DISENGAGED AP AND HAND FLEW PLANE. REMOVED AND REPLACED FCP IAW MM 22-10-07. FCP & AP OPS CHECK GOOD IAW MM 22-11-07.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 360 hrs · 284 cycles

MAIN CABIN DOOR EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB. OPS CHECK GOOD. (P/N 1308)