N926EV

Part: STRAP — CORRODED (BS 559) · airframe 33,864 hrs · 33,289 cycles

PRESSURE FLOOR STRAP AT FS 559.000 FROM RBL 27 TO PRESSURE FLOOR SILL IS CORRODED. C-CHECK RO 11/11/2020. REMOVED DAMAGED FLOOR STRAP AND INSTALLED A NEW PRESSURE FLOOR STRAP, IAW CRJ 200 SRM.

Part: FLOORBEAM — CORRODED (BS 513) · airframe 33,864 hrs · 33,289 cycles

AT RBL 9 FS 513.00 INBOARD FLANGE OF FLOOR BEAM CORRODED. C-CHECK RO 11/11/2020. REPAIR WAS ACCOMPLISHED, IAW MHIRJ REO. NO WEIGHT AND BALANCE CHANGE REQUIRED. M-337 AND TASK CARD ATTACHED.

Part: PLATE — CORRODED (PAX DOOR) · airframe 33,864 hrs · 33,289 cycles

PLATE FOR PASSENGER DOOR FWD ANCHOR FITTING IS CORRODED. C-CHECK RO 11/11/2020. RECEIVED NEW PLATE VERIFIED TO BE P/N 600-38061-11 CRJ 200 AIPC, REF JOB 9784381 OP 139 MX TRANS NR 21619598 FOR PLATE INSTALLATION.

Part: SKIN — LOOSE (RT WING TE FLAP) · airframe 33,864 hrs · 33,289 cycles

RT OUTBOARD FLAP UPPER SKIN HAS LOOSE & SMOKING RIVETS ON THE AFT SPAR BETWEEEN F/STA 234 & 245 AND ON F/STA 245 BETWEEN AFT SPAR & TE. C-CHECK RO 11/11/2020. REPAIRED RT OUTBOARD FLAP UPPER SKIN, IAW REO. NO WEIGHT OR BALANCE CHANGE. M-337 AND TASK CARD ATTACHED.

Part: FORMER — CORRODED (PAX DOOR) · airframe 33,864 hrs · 33,289 cycles

FOUND PAX DOOR FORMER 601R318078-3 TO BE CORRODED. C-CHECK RO 11/11/2020. INSTALLED PAX DOOR FORMER AT FS 329.75, IAW CRJ 200 AMM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION FOR WORK PERFORMED.

Part: NUT — CORRODED (LT FLAP HINGE) · airframe 33,864 hrs · 33,289 cycles

LT FLAP HINGE BOX AT WS 264.00 NUT CORRODED ON AFT INBOARD AND OUTBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVED AND REPLACED LT HINGE BOX INBOARD & OUTBOARD NUTS (P/N MS17825-7) AT WS 264.00, IAW CRJ 200 AMM. TORQUE WRENCH WVACT 10147, CAL DUE 30 SEPT 21.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 33,864 hrs · 33,289 cycles

PAX DOOR SURROUND STRUCTURE ANGLE CORRODED BETWEEN FS 310 AND FS 319.70 BETWEEN STGR 17L AND STGR18L. C-CHECK RO 11/11/2020. REMOVED DAMAGED PAX DOOR SURROUND STRUCTURE ANGLE AND INSTALLED A NEW ANGLE, IAW CRJ 200 SRM. COMPLETED TASK CARD FORM M-337 ATTACHED. NO CHANGE TO WEIGHT AND BALANCE.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 33,864 hrs · 33,289 cycles

FOUND PAX DOOR INTERCOSTAL DD4 TO BE CORRODED IN MULTIPLE LOCATIONS. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR INTERCOSTAL DD4, IAW CRJ 200 SRM. COMPETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NUT — CORRODED (LT FLAP HINGE) · airframe 33,864 hrs · 33,289 cycles

LT FLAP HINGE BOX AT WS 220.00 NUT CORRODED ON AFT OUTBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVE AND REPLACED NUT P/N MS17825-7 ON LT HINGE BOX AT WS 220.00 OUTBOARD SIDE, IAW CRJ 200 AMM. REMOVED AND REPLACED NUT P/N MS17828-7 ON LT HINGE BOX AT WS 220.00 OUTBOARD SIDE, IAW CRJ 200 AMM. TORQUE WRECH WVACT 10147, CAL DATE 30 SEPT 21.

Part: NUT — CORRODED (RT FLAP HINGE) · airframe 33,864 hrs · 33,289 cycles

RT FLAP HINGE BOX AT WS 264.00 NUT CORRODED ON AFT INBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVE AND REPLACE NUT ON RT FLAP HINGE BOX AT WS 264.00 ON AFT INBOARD SIDE OF BRACKET, IAW CRJ 200 AMM. TORQUE WRENCH WVACT 10147, CAL DUE 30 SEPT 21.

Part: NUT — CORRODED (RT FLAP HINGE) · airframe 33,864 hrs · 33,289 cycles

RT FLAP HINGE BOX AT WS 220.00 NUT CORRODED ON AFT INBOARD AND OUTBOARD SIDE OF BRACKET AND FWD BRACKET. C-CHECK RO 11/11/2020. REMOVED AND REPLACED RT HINGE BOX AT WS 220.00, THE NUTS ON INBOARD AND OUTBOARD SIDE OF BRACKET AND THE FWD BRACKET, IAW CRJ 200 AMM. TORQUE WRENCH WVACT 10147, CAL DUE 30 SEPT 21.

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 33,864 hrs · 33,289 cycles

WINDSHIELD CENTER POST LOWER FITTING IS CRACKED FROM THE LOWER VERTICAL EDGE TO THE FIRST LOWER FASTENER HOLE ON THE RT & LT SIDES. FAIL DETAILED VISUAL INSPECTION. C-CHECK RO 11/11/2020. REMOVED AND REPLACED WINDSHIELD CENTER POST RT AND LT LOWER FITTING FROM THE LOWER VERTICAL EDGE, IAW SRM NO WEIGHT AND BALANCE CHANGE, M-337 AND TASK CARD ATTACHED.

Part: BRACKET — CORRODED (PAX DOORFRAME) · airframe 33,864 hrs · 33,289 cycles

PAX DOOR SURROUND STRUCTURE BRACKET CONNECTORS FWD AND AFT CORRODED BETWEEN FS 319.70 ND FS 333 AND BETWEEN STGR 17L AND STGR 18L. C-CHECK RO 11/11/2020. REMOVED FWD AND AFT CONNECTOR BRACKETS, IAW CRJ-200 SRM 51-42-06. LOCATED, DRILLED, AND INSTALLED NEW FWD AND AFT CONNECTOR BRACKETS PN: 601R31771-1, IAW CRJ-200 SRM.

Part: FLOOR SKIN — CORRODED (BS 518-522) · airframe 33,864 hrs · 33,289 cycles

LT PRESSURE FLOOR SILL SKIN AT FS 518.00 AND FS 522.00 IS CORRODED. C-CHECK RO 11/11/2020. REPAIRED LT PRESSURE FLOOR SILL SKIN AT FS 518.00 AND FS 522.00 CORROSION, IAW BOMBARDIER REO. REFERANCE CONTINUATION FOR WORK PERFORMED.

Part: BRACKET — CORRODED (RT FLAP HINGE) · airframe 33,864 hrs · 33,289 cycles

RT FLAP HINGE BOX AT WS 178.00 NUT CORRODED ON AFT OUTBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVE AND REPLACE RT FLAP HINGE BOX AT WS 178.00 THE NUT ON THE AFT OUTBOARD SIDE OF THE BRACKET, IAW CRJ 200 AMM. TORQUE WRENCH WVACT 10147, CAL DUE 30 SEPT 21.

Part: FORMER — CORRODED (PAX DOOR) · airframe 33,864 hrs · 33,289 cycles

FOUND PAX DOOR AFT FORMER TO BE CORRODED IN MULTIPLE LOCATIONS. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR AFT FORMER, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FOR 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 473-513) · airframe 33,864 hrs · 33,289 cycles

LT PRESSURE FLOOR SILL IS CORRODED AT (5) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 473.15 AND FS 513.00. C-CHECK RO 11/11/2020. REPAIRED LT PRESSURE FLOOR SILL AT (5) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 473.15 AND FS 513.00, IAW BOMBARDIER REO WEIGHT AND BALANCE NOT AFFECTED. M-337 AND SKYCARD ATTACHED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 33,864 hrs · 33,289 cycles

FOUND PAX DOOR INTERCOSTAL DD1 TO BE CORRODED ON AFT SIDE. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR INTERCOSTAL DD1, IAW CRJ 200 SRM. COMPETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 529-544) · airframe 33,864 hrs · 33,289 cycles

RT PRESSURE FLOOR SILL HAS (3) AREAS OF CORROSION ON THE SILL SKIN BETWEEN FS 529.00 AND FS 544.00. C-CHECK RO 11/11/2020. REPAIR WAS ACCOMPLISHED IAW BOMBARDIER REO. NO WEIGHT AND BALANCE CHANGE, M-337 AND TASK CARD ATTACHED.

Part: ANGLE — CRACKED (PAX DOOR LATCH) · airframe 33,864 hrs · 33,289 cycles

FOUND PAX DOOR LATCH BOX INBOARD ANGLE TO BE CRACKED. C-CHECK RO 11/11/2020. REMOVED AND REPLACED PAX DOOR LATCH LOCK BOX INBOARD ANGLE, IAW CRJ 200 SRM.

Part: FLOOR SUPPORT — CORRODED (BS 544-559) · airframe 33,864 hrs · 33,289 cycles

RT CABIN PRESSURE FLOOR SILL HAS (1) AREA OF CORROSION ON THE SILL SKIN, (1) AREA OF CORROSION ON THE SILL DOUBLER AND (1) AREA OF CORROSION ON THE FLOOR STRAP THAT SPANS RBL 27.00 AND THE PRESSURE FLOOR SILL. DAMAGE IS BETWEEN FS 544.00 AND FS 559.00. C-CHECK RO 11/11/2020. REMOVED CORROSION FROM PRESSURE FLOOR SKIN, IAW BOMBARDIER REO AND PRESSURE FLOOR ANGLE IAW BOMBARDIER REO AS DOCUMENTED ON ATTACHED CONTINUATION CARD WITH NO WEIGHT AND BALANCE CHANGE. M-337 AND TASK CARD ATTACHED. FLOOR STRAP REPAIR DOCUMENTED ON CAMP 21689741.

Part: FLOOR SUPPORT — CORRODED (BS 409-424) · airframe 33,864 hrs · 33,289 cycles

LT PRESSURE FLOOR SILL IS CORRODED AT (2) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 409.00 AND FS 424.00. C-CHECK RO 11/11/2020. REMOVED LT PRESSURE FLOOR SILL CORROSION AT (2) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 409.00 AND FS 424.00, IAW BOMBARDIER REO. WEIGHT AND BALANCE NOT AFFECTED, M-337 AND TASK CARD ATTACHED.

Part: FLOOR SUPPORT — CORRODED (BS 449-473) · airframe 33,864 hrs · 33,289 cycles

LT PRESSURE FLOOR SILL IS CORRODED AT (1) LOCATION ON THE FLOOR SKIN BETWEEN FS 449.85 AND FS 473.15. C-CHECK RO 11/11/2020. REMOVED LT PRESSURE FLOOR SILL CORROSION AT (1) LOCATION ON THE FLOOR SKIN BETWEEN FS 449.85 AND FS 473.15, IAW BOMBARDIER REO. WEIGHT AND BALANCE NOT AFFECTED. M-337 AND TASK CARD ATTACHED.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 33,864 hrs · 33,289 cycles

LT PRESSURE FLOOR SILL IS CORRODED AT (4) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 513.00 AND FS 544.00. C-CHECK RO 11/11/2020. REPAIRED LT PRESSURE FLOOR SILL CORROSION AT (4) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 513.00 AND FS 544.00. REFERENCE CONTINUATION FOR WORK PERFORMED.

Part: A/C PACK — CORRODED (PAX DOOR) · airframe 33,864 hrs · 33,289 cycles

FOUND PAX DOOR LOWER AFT INTERCOSTAL TO BE CORRODED. C-CHECK RO 11/11/2020. INSTALLED SERVIEABLE PAX DOOR LOWER AFT INTERCOSTAL, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 33,864 hrs · 33,289 cycles

FOUND PAX DOOR INTERCOSTAL DD3 TO BE CORRODED. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR INTERCOSTAL DD3, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTIUATION CARD FOR WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 424-439) · airframe 33,864 hrs · 33,289 cycles

RT PRESSURE FLOOR SILL HAS (3) AREAS OF CORROSION ON THE SILL SKIN BETWEEN FS 424.00 AND FS 439.00. C-CHECK RO 11/11/2020. REPAIR TO RT PRESSURE FLOOR SILL WAS COMPLETED, IAW BOMBARDIER REO, AS DOCUMENTED ON ATTACHED CONTINUATION CARD. M-337 AND TASK CARD ATTACHED. NO CHANGE TO WEIGHT AND BALANCE.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 33,864 hrs · 33,289 cycles

LT PRESSURE FLOOR SILL SKIN PANEL AT FS 473.15 LBL 36 IS CORRODED. C-CHECK RO 11/11/2020. COMPLIED WITH BOMBARDIER REO AND MHIRJ REO. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION FOR WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 544-559) · airframe 33,864 hrs · 33,289 cycles

LT PRESSURE FLOOR SILL IS CORRODED AT (2) LOCATIONS ON THE FLOOR SKIN, (1) LOCATION ON THE FLOOR DOUBLER AND THE FLOOR STRAP SPANNING LBL 27.00 AND FLOOR SILL IS CORRODED IN NUMEROUS LOCATIONS. DAMAGE IS BETWEEN FS 544.00 AND FS 559.00. C-CHECK RO 11/11/2020. REMOVED CORROSION FROM PRESSURE FLOOR SKIN, IAW BOMBARDIER REO AND PRESSURE FLOOR ANGLE IAW BOMBARDIER REO 601RAS. DOCUMENTED ON ATTACHED CONTINUATION CARD WITH NO WEIGHT AND BALANCE CHANGE. M-337 AND TASK CARD ATTACHED. FLOOR STRAP REPAIR DOCUMENTED ON CAMP 21689664.

Part: DOOR FRAME — DAMAGED (PAX DOORWAY) · airframe 33,864 hrs · 33,289 cycles

FOUND PAX DOOR FRAME ON FWD SIDE TO HAVE MULTIPLE OVERSIZED HOLES. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR FWD FRAME, IAW CRK 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: A/C PACK — CORRODED (PAX DOOR) · airframe 33,864 hrs · 33,289 cycles

FOUND PAX DOOR INTERCOSTAL TO BE CORRODED ON AFT SIDE. C-CHECK RO 11/11/2020. INSTALLED SEVICABLE PAX DOOR INTERCOSTAL, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTIUATION CARD FOR WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 424-449) · airframe 33,864 hrs · 33,289 cycles

LT PRESSURE FLOOR SIL IS CORRODED AT (3) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 424.00 AND FS 449.85. C-CHECK RO 11/11/2020. REMOVED LT PRESSURE FLOOR SILL CORROSION AT (3) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 424.00 AND FS 449.85, IAW BOMBARDIER REO. WEIGHT AND BALANCE NOT AFFECTED, M-337 AND TASK CARD ATTACHED.

Part: FLOOR SUPPORT — CORRODED (BS 461) · airframe 33,864 hrs · 33,289 cycles

RT PRESSURE FLOOR SILL HAS (1) AREA OF CORROSION ON THE SILL SKIN AT FS 461.00. C-CHECK RO 11/11/2020. RT PRESSURE FLOOR SILL CORROSION WAS REMOVED AND TREATED, IAW BOMBARDIER REO, AS DOCUMENTED ON ATTACHED CONTINUATION CARD. NO WEIGHT AND BALANCE CHANGE, M-337 AND TASK CARD ATTACHED.

Part: FLOOR SUPPORT — CORRODED (BS 513-529) · airframe 33,864 hrs · 33,289 cycles

RT CABIN PRESSURE FLOOR SILL HAS (2) AREAS OF CORROSION ON THE SILL SKIN BEWTEEN FS 513.00 AND FS 529.00. C-CHECK RO 11/11/2020. REMOVED CORROSION AND TREATED AREA, IAW BOMBARDIER REO. NO WEIGHT AND BALANCE CHANGE. M-337 AND TASK CARD ATTACHED.

Part: FLOOR SUPPORT — CORRODED (BS 484-513) · airframe 33,864 hrs · 33,289 cycles

RT CABIN PRESSURE FLOOR SILL HAS (4) AREAS OF CORROSION ON THE SILL SKIN BETWEEN FS 484.00 AND FS 513.00. C-CHECK RO 11/11/2020. REPAIRED RT CABIN PRESSURE FLOOR SILL (4) AREAS OF CORROSION ON THE SILL SKIN BETWEEN FS 484.00 AND FS 513.00. REMOVED CORROSION BY BLENDING, IAW BOMBARDIER REO. REFERENCE CONTINUATION FOR WORK PERFORMED. COMPLETED TASK CARD AND ATTACHED COMPLETED SKYWEST FORM NR 337. NO WEIGHT CHANGE.

Part: FRAME — CORRODED (BS 409) · airframe 33,864 hrs · 33,289 cycles

FS 409.00 IS CORRODED ON THE FORWARD SIDE ON THE FRAME DOUBLER BETWEEN STR 26 AND STR 27 AND ON THE AFT SIDE ON THE FRAME DOUBLER. C-CHECK RO 11/11/2020. REMOVED UNSERVICEABLE FS 409.00 FRAME DOUBLER BETWEEN STR 26 AND STR 27 AND AFT SIDE ANGLE ON THE FRAME DOUBLER AND INSTALLED SERVICEABLE FS 409.00 FRAME DOUBLER BETWEEN STR 26 AND STR 27 AND AFT SIDE ANGLE ON THE FRAME DOUBLER, IAW CRJ-200 SRM. PRESSURIZATION LEAK CHECKS GOOD, REFERENCE CONTINUATION FOR WORK PERFORMED. COMPLETED SKYWEST TASK CARD AND ATTACHED COMPLETED SKYWEST FORM 337. NO WEIGHT CHANGE.

Part: HINGE — GOUGED (PAX DOOR) · airframe 33,864 hrs · 33,289 cycles

FUSELAGE SIDE OF PASSENGER DOOR HINGE, MOST AFT LANDING HAS A DEEP GOUGE AT A PREVIOUS REPAIR. C-CHECK RO 11/11/2020. REPAIRED FUSELAGE SIDE OF PASSENGER DOOR HINGE, IAW CRJ-200 AMM SRM, BOMBARDIER REO, AND MHIRJ REO. REFERENCE CONTINUATION CARD FOR WORK PERFORMED. COMPLETED SKYWEST TASK CARD AND ATTACHED COMPLETED SKYWEST FORM 337. NO WEIGHT CHANGE.

Part: LINK — CORRODED (LT SPOILER) · airframe 33,864 hrs · 33,289 cycles

LT INBOARD GROUND SPOILER PCU LINK HAS CORRODED HARDWARE. C-CHECK RO 11/11/2020. REPLACED INBOARD GROUND SPOILER PCU LINK HARDWARE PART NUMBERS NAS-6305U-19D AND NAS6205-12D, REF CRJ200 AMM. TW SN 08158140 CAL DATE 16 MAR 20 CAL DUE 31 MAR 20.

Part: CUP — CORRODED (DOOR HAND RAIL) · airframe 33,864 hrs · 33,289 cycles

PAX DOOR HAND RAIL STOW CUPS ARE CORRODED. C-CHECK RO 11/11/2020. LOCATED, DRILLED, AND INSTALLED NEW FWD AND AFT STOW CUP ASSEMBLY'S, IAW CRJ-200 SRM.

Part: BOLT — CORRODED (SPOILER HINGE) · airframe 33,864 hrs · 33,289 cycles

RT OUTBOARD GROUND SPOILER HAS CORRODED HINGE HARDWARE. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE RIGHT OUTBOARD GROUND SPOILER HINGE HARDWARE, IAW CRJ-200 AMM TASK. TORQUE WRENCH PN: WVACT204356, CALIBRATED DATE: 09-14-2020.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 33,864 hrs · 33,289 cycles

RT CABIN FLOOR BEAM ON RBL 9.00 HAS A HOLE CORRODED THROUGH IT AND NUMEROUS OTHER LOCATIONS WITH HEAVY CORROSION BETWEEN FS 409.00 TO FS 409.00+128. C-CHECK RO 11/11/2020. REPAIRED RT CABIN FLOOR BEAM AT RBL 9.00, HOLE CORRODED THROUGH IT AND NUMEROUS OTHER LOCATIONS WITH HEAVY CORROSION BETWEEN FS 409.00 TO FS 409.00+128, IAW MHIRJ REO. COMPLETED SKYWEST TASK CARD AND ATTACHED COMPLETED SKYWEST FORM 337. NO WEIGHT CHANGE. REFERENCE CONTINUATION FOR WORK PERFORMED.

Part: BOLT — CORRODED (SPOILER PCU) · airframe 33,864 hrs · 33,289 cycles

RT INBOARD GROUND SPOILER PCU LINK HAS CORRODED HARDWARE. C-CHECK RO 11/11/2020. REMOVED AND REPLACED CORRODED HARDWARE ON INBOARD GROUND SPOILER PCU LINK WITH SERVICABLE P/N; NAS6305U19D, IAW CRJ-200 AMM TASK. CALIBRATED TOOL REQUIRED, TORQUE WRENCH WVACT 0083 CAL. 9-14-20 DUE 9-30-21.

Part: BOLT — CORRODED (SPOILER PCU) · airframe 33,864 hrs · 33,289 cycles

RT OUTBOARD GROUND SPOILER PCU LINK HARDWARE IS CORRODED. C-CHECK RO 11/11/2020. REMOVED AND REPLACED RT WING OUTBOARD GROUND SPOILER PCU LINK HARDWARE, IAW CRJ-200 AMM TASK.

Part: HINGE — CORRODED (RT WING SPOILER) · airframe 33,864 hrs · 33,289 cycles

RT INBOARD GROUND SPOILER HINGE HARDWARE IS CORRODED. C-CHECK RO 11/11/2020. REMOVED CORRODED HARDWARE AT RT INBOARD GROUND SPOILER HINGES AND REPLACED WITH SERVICABLE PARTS, IAW CRJ-200 AMM TASK. CALIBRATED TOOL REQUIRED, TORQUE WRENCH WVACT 0083 CAL 9/14/20 DUE 9/30/20.

Part: BOLT — CORRODED (LT SPOILER PCU) · airframe 33,864 hrs · 33,289 cycles

LT OUTBOARD GROUND SPOILER HINGE HARDWARE IS CORRODED. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE LT WING OUTBOARD SPOILER INBOARD AND CENTER HINGES HARDWARE, IAW CRJ-200 AMM TASK.

Part: LINK — CORRODED (LT SPOILER) · airframe 33,864 hrs · 33,289 cycles

LT OUTBOARD GROUND SPOILER PCU LINK HAS CORRODED HARDWARE. C-CHECK RO 11/11/2020. REPLACED LT OUTBOARD GROUND SPOILER PCU LINK HARDWARE PART NUMBERS NAS-6305U-19D AND NAS6205-12D PER CRJ200 AMM. TW SN 08158140 CAL DATE 16 MAR 20 CAL DUE 31 MAR 21.

Part: HINGE — CORRODED (LT SPOILER) · airframe 33,864 hrs · 33,289 cycles

LT INBOARD GROUND SPOILER HAS CORRODED HINGE HARDWARE. C-CHECK RO 11/11/2020. INSTALLED SERVICABLE LT WING INBOARD SPOILER INBOARD AND CENTER HINGES HARDWARE, IAW CRJ-200 AMM TASK.

Part: SEAT TRACK — CORRODED (BS 574-621) · airframe 33,864 hrs · 33,289 cycles

FLOORBEAM CAP ON LBL 27.00 IS CORRODED AROUND NUTPLATES ON THE INBOARD AND OUTBOARD EDGES BETWEEN FS 574.00 AND FS 621.00. C-CHECK RO 11/11/2020. REMOVED UNSERVICEABLE FLOORBEAM CAP ON LBL 27.00 BETWEEN FS 574.00 AND FS 621.00 AND INSTALLED SERVICEABLE FLOORBEAM CAP ON LBL 27.00 BETWEEN FS 574.00 AND FS 621.00, IAW CRJ200 SRM. NO WEIGHT AND BALANCE CHANGE, M-337 AND TASK CARD ATTACHED.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 33,864 hrs · 33,289 cycles

FLOOR CROSSBEAM CAP IS CORRODED BETWEEN RBL 9.00 AND LBL 9.00 AT FS 559.00+80. C-CHECK RO 11/11/2020. REMOVED CORRODED CROSS BEAM CAP, INSTALLED NEW SERVICEABLE FLOOR CROSSBEAM CAP BETWEEN RBL 9.00 AND LBL 9.00 AT FS 559.00+80, IAW CRJ 200 SRM REFERENCE CONTINUATION CARD FOR ALL WORK PEFORMED.

Part: DOOR SILL — CRACKED (BS 605) · airframe 33,864 hrs · 33,289 cycles

CARGO DOOR FLOOR SILL IS CRACKED AT FS 605.00. C-CHECK RO 11/11/2020. REMOVED DAMAGED CARGO SILL PLATE AND INSTALLED A NEW SILL PLATE, IAW BOMBARDIER REO AND CRJ-200 SRM, AS DOCUMENTED ON ATTACHED CONTINUATION CARD. NO WEIGHT AND BALANCE CHANGE MADE, M-337 AND TASK CARD ATTACHED.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 33,864 hrs · 33,289 cycles

FLOOR BEAM CROSSBEAM CAP IS HEAVILY CORRODED BETWEEN RBL 9.00 AND RBL 27.00 AT FS 559.00+80. C-CHECK RO 11/11/2020. REMOVED UNSERVICEABLE FLOOR BEAM CROSSBEAM CAP BETWEEN RBL 9.00 AND RBL 27.00 AT FS 559.00+80 AND INSTALLED SERVICEABLE FLOOR BEAM CROSSBEAM CAP BETWEEN RBL 9.00 AND RBL 27.00 AT FS 559.00+80. REFERENCE CONTINUATION CARD FOR MAINTENANCE PERFORMED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 33,864 hrs · 33,289 cycles

CARGO FLOOR SEAT TRACK ON LBL 9.00 AND RBL 9.00 BETWEEN FS 574.00 AND FS 559.00+112 ARE CORRODED. C-CHECK RO 11/11/2020. REMOVED DAMAGED PARTS AND INSTALLED NEW SEAT TRACK SECTIONS AT LBL 9 AND RBL 9, IAW CRJ 200 SRM AND CRJ 200 AMM, AS DOCUMENTED ON ATTACHED CONTINUATION CARD.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 33,864 hrs · 33,289 cycles

(3) CARGO FLOOR TRACK CLEATS ON LBL 27.00 BETWEEN FS 574.00 AND FS 559.00+96 AND (1) CLEAT ON LBL 9.00 BETWEEN FS 589.00 AND FS 605.00 ARE CORRODED. C-CHECK RO 11/11/2020. REMOVED 3 CARGO FLOOR TRACK CLEATS AND INSTALLED 3 NEW FLOOR CLEATS, IAW CRJ 200 SRM AS DOCUMENTED ON ATTACHED CONTINUATION CARD.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 33,864 hrs · 33,289 cycles

CABIN FLOORBEAM CAP ON RBL 9.00 IS HEAVILY CORRODED BETWEEN FS 559.00+48 AND FS 559.00+80. C-CHECK RO 11/11/2020. INSTALLED A NEW FLOOR BEAM CAP, IAW REO AS DOCUMENTED ON ATTACHED CONTINUATION CARD. NO WEIGHT AND BALANCE CHANGE, M-337 AND TASK CARD ATTACHED.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 33,864 hrs · 33,289 cycles

FLOORBEAM CAP ON RBL 9.00 HAS ONE SPOT OF CORROSION AROUND NUTPLATE JUST AFT OF FS 559.00. C-CHECK RO 11/11/2020. REMOVED AND REPLACED DAMAGED SECTION OF FLOORBEAM CAP AT RBL 9.00 FS 529.00 TO 559.00+16, IAW MHIRJ REO. REFERENCE CONTINUATION FOR WORK PERFORMED. COMPLETED SKYWEST TASK CARD AND ATTACHED COMPLETED SKYWEST FORM 337. NO WEIGHT CHANGE.

Part: SUPPORT BRACKET — CRACKED (WINDSHIELD) · airframe 33,864 hrs · 33,289 cycles

COPILOT WINDSHIELD SIDEPOST LOWER AFT SUPPORT BRACKET IS CRACKED. C-CHECK RO 11/11/2020. REMOVED AND REPLACED COPILOT WINDSHIELD SIDEPOST LOWER AFT SUPPORT BRACKET, IAW CRJ200 SRM. COMPLIED WITH TASK CARD AND FORM 337. NO WEIGHT CHANGE.

Part: PUCK — CORRODED (CARGO) · airframe 33,864 hrs · 33,289 cycles

ALL (3) CARGO TIE DOWN PADS INBOARD OF CARGO DOOR ARE CORRODED. C-CHECK RO 11/11/2020. UPON FURTHER INVESTIGATION, FOUND ALL 3 CARGO TIE DOWNS TO BE OUT OF LIMITS, IAW CRJ200 SRM. REMOVED UNSERVICEABLE CARGO TIE DOWNS. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE CARGO TIE DOWNS, IAW CRJ200 SRM.

Part: FRAME — CORRODED (BS 559) · airframe 33,864 hrs · 33,289 cycles

FS 559.00+96 IS HEAVILY CORRODED ON THE FORWARD FLANGE AND AFT FACE AT STR 26R. C-CHECK RO 11/11/2020. REPAIRED FS 559.00+96 CORROSION ON THE FORWARD FLANGE AND AFT FACE AT STR 26R BY PERFORMING SPLICE REPAIR, IAW CRJ-200 SRM. COMPLETED SKYWEST TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION FOR WORK PERFORMED.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 33,864 hrs · 33,289 cycles

FLOOR CROSSBEAM CAP BETWEEN LBL 9.00 AND LBL 27.00 AT FS 589.00 IS CORRODED. C-CHECK RO 11/11/2020. REPLACED UNSERVICEABLE FLOOR CROSSBEAM CAP AT FS 589 BETWEEN LBL 9 AND LBL 27, IAW CRJ200 SRM.

Part: SKIN — CHAFED (RT WING) · airframe 33,864 hrs · 33,289 cycles

RT LOWER WING SKIN IS CHAFED FROM CONTACT WITH THE AFT SIDE OF THE FORWARD MLG FAIRING AT BL 45.00. C-CHECK RO 11/11/2020. REPAIRED RT LOWER WING SKIN CHAFE FROM CONTACT WITH THE AFT SIDE OF THE FORWARD MLG FAIRING AT BL 45.00, IAW BOMBARDIER REO. NO WEIGHT AND BALANCE CHANGE M-337 AND TASK CARD ATTACHED.

Part: SKIN — CHAFED (LT WING) · airframe 33,864 hrs · 33,289 cycles

LT LOWER WING SKIN IS CHAFED FROM CONTACT WITH AFT SIDE OF THE FORWARD MLG FAIRING AT BL 45.00. C-CHECK RO 11/11/2020. REPAIRED LT LOWER WING SKIN CHAFE FROM CONTACT WITH AFT SIDE OF THE FORWARD MLG FAIRING AT BL 45.00, IAW BOMBARDIER REO. MAJOR REPAIR TASK AND FORM M337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE, REFER TO CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: DOOR FRAME — DENTED (EMERGENCY EXIT) · airframe 33,864 hrs · 33,289 cycles

LT EMERGENCY EXIT TOP/FWD CORNER OF CASTING DOOR STRUCTURE DENTED AND CRACKED. C-CHECK RO 11/11/2020. REPAIRED LT EMERGENCY EXIT TOP/FWD CORNER, IAW MHIRJ REO. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 33,864 hrs · 33,289 cycles

SIDE SEAT RAIL CORRODED BETWEEN FS 364 TO FS 409+18.02T STRG 15L. C-CHECK RO 11/11/2020. REMOVED UNSERVICEABLE SIDE SEAT RAIL BETWEEN FS 364 TO FS 409+18.02T STRG 15L AND INSTALLED SERVICEABLE SIDE SEAT RAIL BETWEEN FS 364 TO FS 409+18.02T STRG 15L, IAW CRJ-200 AMM.

Part: FLOORBEAM — CORRODED (BS 310) · airframe 33,864 hrs · 33,289 cycles

FLOOR BEAM ANGLE SUPPORT BRACKET CORRODED AT FS 310 AND AT APPROXIMATELY STRG 17L. C-CHECK RO 11/11/2020. FLOOR BEAM ANGLE WAS REPAIRED, IAW REO AND CRJ 200 SRM TO INCLUDE BLENDING. NDT AND FINISH COATS APPLIED, AS DOCUMENTED ON ATTACHED CONTINUATION CARD. NO WEIGHT AND BALANCE CHANGE. M-337 AND TASK CARD 51-900-1003-SKY ATTACHED.

Part: FRAME — CORRODED (BS 333) · airframe 33,864 hrs · 33,289 cycles

FRAME AT FS 333 CORRODED BETWEEN STGR 27 AND STGR 25L. C-CHECK RO 11/11/2020. DAMAGED FRAME SECTION WAS REMOVED AND NEW SECTION INSTALLED, IAW CRJ 200 SRM, NO CHANGE TO WEIGHT AND BALANCE. M-337 AND TASK CARD ATTACHED.

Part: INTERCOSTAL — CORRODED (BS 327-338) · airframe 33,864 hrs · 33,289 cycles

PAX DOOR INTERCOSTAL DD6 CORRODED BETWEEN FS 327.763 AND FS 338.963. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR INTERCOSTAL DD6, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION FOR WORK PERFORMED.

Part: SKIN — CORRODED (LT WING) · airframe 33,864 hrs · 33,289 cycles

LT WING, LOWER WING PLANK ACCESS HOLE CUTOUT AT 510AB HAS PITTING CORROSION AT THE INBOARD AND OUTBOARD RADIUS LOCATIONS. C-CHECK RO 11/11/2020. COMPLIED WITH REO. MAJOR REPAIR COMPLETED TASK CARD & ATTTACHED COMPLED FORM M-337. NO WEIGHT CHANGE.REFER TO ATTACHED CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: RIB — CRACKED (RT WING) · airframe 33,864 hrs · 33,289 cycles

RT WING, INBOARD BATTERY RIB IS CRACKED AT THE FORWARD END. C-CHECK RO 11/11/2020. REMOVED AND INSTALLED NEW SERVICEABLE CAP 600-10389-2, IAW CRJ 200 SRM.

Part: RIB — CRACKED (LT WING) · airframe 33,864 hrs · 33,289 cycles

LT WING, INBOARD BATTERY RIB IS CRACKED AT THE AFT END. C-CHECK RO 11/11/2020. REMOVED AND INSTALLED NEW SERVICEABLE CAP 600-10389-1 ON LT WING INBOARD, IAW CRJ 200 SRM.

Part: SKIN — CORRODED (RT WING) · airframe 33,864 hrs · 33,289 cycles

RT WING, LOWER WING PLANK ACCESS HOLE CUTOUT AT 640BB HAS PITTING CORROSION AROUND THE INBOARD AND OUTBOARD RADIUS LOCATIONS. C-CHECK RO 11/11/2020. REPAIR TO 640BB CUTOUT WAS PERFORMED, IAW REO. NO CHANGE TO WEIGHT AND BALANCE, M-337 AND TASK CARD ATTACHED. ORIGINAL THICKNESS MEASURED 0.191" REMAINING THICKNESS 0.181".

Part: SKIN — CORRODED (BS 559) · airframe 33,864 hrs · 33,289 cycles

FUSELAGE SKIN HAS CORROSION AROUND DRAIN HOLES BETWEEN BL 27-26 AT FS 559+14, +46 AND +94. C-CHECK RO 11/11/2020. REPAIR WAS ACCOMPLISHED IAW MHIRJ REO. NO CHANGE TO WEIGHT AND BALANCE, M-337 AND TASK CARD ATTACHED.

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 33,864 hrs · 33,289 cycles

EVALUATE RT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS (REFERENCE RIL 5378), REPAIR IF NEEDED IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 11/11/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE AROUND POTTED INSERTS ON RT 9G BULKHEAD AFT WALL. REPAIR DOUBLER MATERIAL 2024-T3 .040 P/O W58363. NEW P-SEAL P/N 1024, P/O W72038. DEPTH GAGE WVACT 204441 CAL. DUE 28 FEB. 2021. NO WEIGHT REMOVED, TOTAL WEIGHT ADDED 1.726 LBS.

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 33,864 hrs · 33,289 cycles

EVALUATE LT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS (REFERENCE RIL), REPAIR IF NEEDED IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 11/11/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE AROUND POTTED INSERTS ON LT 9G BULKHEAD AFT WALL. REPAIR DOUBLER MATERIAL 2024-T3 .040 P/O W58363. NEW P-SEAL P/N 1024, P/O W72038. DEPTH GAGE WVACT 204441 CAL DUE 28 FEB 2021. NO WEIGHT REMOVED. TOTAL WEIGHT ADDED 1.742 LBS.

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 33,864 hrs · 33,289 cycles

EVALUATE CENTER 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS (REFERENCE RIL 5378), REPAIR IF NEEDED IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 11/11/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE AROUND POTTED INSERTS ON CENTER 9G BULKHEAD AFT WALL. REPAIR DOUBLER MATERIAL 2024-T3 .040 P/O W58363. DEPTH GAGE WVACT 204441 CAL DUE 28 FEB 2021. NO WEIGHT REMOVED, TOTAL WEIGHT ADDED .837 LBS.

Part: BULKHEAD — CRACKED (BS 621) · airframe 33,864 hrs · 33,289 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD-COMPLY WITH AD: (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 TR. (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: 7843, POSITION. C-CHECK RO 11/11/2020. COMPLIED WITH 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 TR. (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 7843.

Part: SCREW — DAMAGED (FUSELAGE) · airframe 33,864 hrs · 33,289 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA-REPAIRED DAMAGED SCREW HOLE 7 O' CLOCK POSITION, 3RD WINDOW AFT OF PAX DR, LT REF REO. SDIR-SPECIAL DETAILED-SEE NOTE (1), METHOD TBD, PART NUMBER: -, SERIAL NUMBER: 7843, POSITION: C-CHECK RO 11/11/2020. COMPLIED WITH RA, REPAIRED DAMAGED SCREW HOLE 7 O' CLOCK POSITION, 3RD WINDOW AFT OF PAX DR, LT REF REO AND MHIRJ REO. MAJOR REPAIR TASK AND FORM M337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE, REFERENCE ATTACHED CONTINUE CARD FOR WORK PERFORMED.

Part: FRAME — WEAK (BS 559) · airframe 33,864 hrs · 33,289 cycles

COMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LOWER CAP ANGLES BL 9.00 & 18.00 LT & RT. C-CHECK RO 11/11/2020. REPAIR AND REINFORCEMENT OF THE LOWER CAP ANGLE BL 9 AND 18 LT AND RT SIDES WERE ACCOMPLISHED, IAW MHIRJ REO AND BOMBARDIER REO. FORM M-337 AND TASK CARD ATTACHED. WEIGHT AND BALANCE CHANGE: +2.8LBS AT ARM 559.00, MOMENT +1,565.2 LB IN.

Part: ACTUATOR — SLOW (RT MLG) · airframe 32,490 hrs · 31,698 cycles

ON APPROACH, THE RIGHT MAIN GEAR STAYED IN TRANSIT FOR SEVERAL SECONDS THEN GAVE THE GEAR DISAGREE WARNING. UPON INITIALIZING THE GO-AROUND THE RIGHT MAIN INDICATED GREEN DOWN AND TOWER VERIFIED ITS POSITION. (FLT#3953) FO: 07/02/2019 CLOSED REMOVED AND REPLACED RT MLG SIDESTAY ACTUATOR, UPLOCK ACTUATOR AND #3A HYDRAULIC PUMP IAW AMM. OPS CHECK GOOD.

Part: ENGINE — VIBRATION (LEFT) · airframe 30,392 hrs · 29,376 cycles

DURING CLIMBOUT, CREW FELT A COUPLE OF ABRUPT VIBRATIONS, THEN NOTICED THE ITT WAS ABOUT 910. CREW DECREASED ENGINE POWER AND FELT MORE VIBRATIONS, LEVELED OUT 13000 FT. FA REPORTED VIBRATIONS ON THE LT SIDE OF THE ACFT, RETURNED TO FIELD. EMERGENCY DECLARED. LT ENGINE ITT WAS HIGHER THAN THE RT DURING FINAL. LANDING WAS UNEVENTFUL TAXIIED TO THE GATE. ENGINE WAS NEVER SHUT DOWN. OPEN.

Part: RIB — DAMAGED (RT WING TE FLAP) · airframe 29,434 hrs · 28,324 cycles

RIGHT INBD RIB ASSY FOUND WITH FIVE ELONGATED CRACKED, DAMAGED HOLES UNDERNEATH THE INBD FLAP SEAL AT TRAILING EDGE. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 29,434 hrs · 28,324 cycles

LH PRESSURE FLOOR SILL IS CORRODED BETWEEN FS 409+128 - 559. REPAIRED LH PRESSURE FLOOR SILL CORROSION BETWEEN FS 409+128 - FS 559 IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 29,434 hrs · 28,324 cycles

BS 349 FLOOR SUPPORT IS CORRODED AT LBL 36. REPAIRED IAW REO.

Part: FRAME — CORRODED (BS 589) · airframe 29,434 hrs · 28,324 cycles

CARGO BAY BS 589 FRAME IS CORRODED BETWEEN STRINGERS 22L AND 24R. REMOVED AND REPLACED THE FRAME IAW SRM.

Part: CROSSBEAM — CRACKED (BS 280) · airframe 29,434 hrs · 28,324 cycles

BS 280 CROSSBEAM LOWER FLANGE CRACKED APPROX 1.5 INCHES LONG AT RBL 9. REMOVED AND REPLACED THE CROSSBEAM IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 29,434 hrs · 28,324 cycles

PASSENGER DOOR HINGE GOUGED. REPLACED THE DOOR HINGE IAW SRM. OPS AND LEAK CHECKED GOOD.

Part: FRAME — CORRODED (BS 605) · airframe 29,434 hrs · 28,324 cycles

CARGO BAY BS 605 FRAME IS CORRODED BETWEEN STRINGERS 22L AND 26R. REMOVED AND REPLACED THE FRAME SECTOR IAW AMM.

Part: SKIN — DENTED (BS 654) · airframe 29,434 hrs · 28,324 cycles

FUSELAGE SKIN DENTED AFT OF BS 654 NEAR STRINGER 15L. REPAIRED IAW REO.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 29,434 hrs · 28,324 cycles

LEFT INBD FLAP HAS ONE SMALL DENT ON UPPER SURFACE, TWO INCHES FORWARD OF TRAILING EDGE AND 21.3 INCHES FROM I/B EDGE. REPAIRED IAW SRM.

Part: FAIRING — DAMAGED (RT HORIZ STAB) · airframe 29,177 hrs · 28,055 cycles

RT HORIZONTAL STABILIZER TIP FAIRING HAS BURN MARKS ON UPPER SURFACE AROUND FASTENER HOLES. COMPLIED WITH DISPOSITION. INSTALLED RT HORIZONTAL STAB TIP, DIMPLE WASHERS AND APPLIED ADHESIVE IAW EA 12-2017-094 REV- BETWEEN BL 102.25-BL 112.00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,934 hrs · 24,464 cycles

EXTERNAL EMERGENCY LIGHT NR 2 INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: FLOOR SUPPORT — CORRODED (BS 449) · airframe 25,653 hrs · 24,167 cycles

CORROSION WAS FOUND ON THE RT SIDE FLOOR STRUCTURE FS 449.85 UNDER THE RT SIDE EMERGENCY EXIT. BLENDED AREA AT RBL 45, FS 449.85 ON PRESSURE FLOOR SILL IAW GREO 601R-53-41-666. C/W EC/TC REO 601R-53-41-666 IAW NDTM PT 1 51-20-06. BLENDED AREA ON RBL 45 FS 449.85 ON FLOOR ANGLE IAW REO 601R-53-41-666.

Part: FLOOR SUPPORT — CORRODED (BS 449) · airframe 25,653 hrs · 24,167 cycles

DURING THE REAPPLICATION OF THE AVDEC SEALANT CORROSION WAS FOUND ON THE LT SIDE FLOOR STRUCTURE FS 449.85 AND APPEARS TO RUN UNDER THE POST JUST FWD OF THE LT SIDE EMERGENCY EXIT. BLENDED AREA AT LBL 45, FS 449 ON PRESSURE FLOOR SILL IAW GREO 601R-53-41-666. BLENDED AREA ON LBL 45, FS 449.85 ON FLOOR ANGLE IAW REO 601R-53-41-666.

Part: STRUCTURE — CRACKED (RT ELEVATOR) · airframe 25,659 hrs · 24,173 cycles

ON RT ELEVATOR WHERE PANEL 344CB GOES TAB WITH NUTPLATE IS CRACKED. FABRICATED DOUBLER IAW DWG 600-24054 SNIEO NR S01. INSTALLED DOUBLER IAW SRM 51-42-06.

Part: SKIN — CRACKED (RT WING) · airframe 25,659 hrs · 24,173 cycles

RIGHT WING LOWER AFT PLANK DRAIN HOLE BETWEEN WS 0.00 & 22.50 BY RT BOOST PUMP HAS MULTIPLE INDICATIONS AROUND DRAIN HOLE 50 PERCENT FCH. FAILED NDT. SPOT FACED LOWER WING SKIN AS REQUIRED IAW REO 601R-57-21-2324. RECEIVED REO 601R-57-21-2324 AND COMPLIED WITH REO 601R-57-21-2324.

Part: ACCESS PANEL — CRACKED (WING) · airframe 25,653 hrs · 24,167 cycles

FUEL ACCESS HOLE 550EB HAS INDICATIONS ON THE OTBD SIDE APPROXIMATELY.25W X 9.0L 50 PERCENT FCH. FAILED NDT. THE FUEL PANEL LISTED IN THE DISCREPANCY SHOULD HAVE BEEN 550DB. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.

Part: SKIN — CRACKED (WING) · airframe 25,655 hrs · 24,169 cycles

LOWER WING PLANK LANDING FOR BOOST PUMP ACCESS PANEL 610CB HAS MULTIPLE INDICATIONS NOTED ON HORIZONTAL AND VERTICAL SURFACES GREATER THAN 50 PERCENT AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSP. C/W STS EA 32-2015-191 DATED 05/13/15.

Part: ACCESS PANEL — CRACKED (WING) · airframe 25,653 hrs · 24,167 cycles

FUEL ACCESS HOLE 650GB HAS AN INDICATION ON THE INBD SIDE APPROXIMATELY .25W X 9.0L 50 PERCENT FCH. FAILED NDT. THE FUEL PANEL IN DISCREPANCY BLOCK SHOULD HAVE BEEN 650FB. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,653 hrs · 24,167 cycles

FS 280, LBL 9, TWO CRACKED BRACKETS. R & R LBL 9 INBD FLOORBEAM CLIP, PN 601R31113-57 IAW SRM 51-40-11, 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW BRACKET PT 601R31113-57 AT LBL 9, FS 280 IAW SRM 51-40-11 AND 51-42-21.

Part: BRACKET — CRACKED (BS 280) · airframe 25,653 hrs · 24,167 cycles

FS 280, RBL 9, CRACKED BRACKET. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-06, 51-42-21, & 51-40-11.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 25,653 hrs · 24,167 cycles

CARGO TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-02 AND SRM 51-41-04.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 25,655 hrs · 24,169 cycles

RIGHT SIDE, FLOORBEAM, FS 349 CORRODED. C/W REO 601R-53-21-2619.

Part: ANGLE — CORRODED (BS 319) · airframe 25,653 hrs · 24,167 cycles

FWD CLIP AT BS 319, RT GALLEY SERVICE DOOR SILL CORRODED. REMOVED FWD CLIP IAW SRM 51-42-21. LOCATED & DRILLED NEW CLIP IAW SRM 51-40-11. INSTALLED NEW ANGLE, IAW SRM 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 25,653 hrs · 24,167 cycles

RT FLOOR SUPPORT BS 310 - 319, CORRODED. REMOVED AND REPLACED IAW SRM 51-42-06 AND SRM 51-42-10.

Part: CHANNEL — CORRODED (BS 280) · airframe 25,653 hrs · 24,167 cycles

BS 280, CHANNEL AT BL 0 IS CORRODED. R & R CHANNEL IAW SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-25-06, AND 51-25-01.

Part: DOOR SILL — CORRODED (BS 319-349) · airframe 25,655 hrs · 24,169 cycles

GALLEY SERVICE DOOR SILL CORRODED, LOWER SILL FS 319.00-FS 349.00. RECEIVED SERVICEABLE ANGLE NR 601R38303-253. LOCATED AND DRILLED SERVICEABLE ANGLE 601R38303-253 IAW SRM 51-40-11. INSTALLED NEW LOWER SILL ANGLE, PN:601R-38303-253 IAW SRM 51-42-21 AND 51-42-06.

Part: FLOORBEAM — CRACKED (BS 460) · airframe 25,653 hrs · 24,167 cycles

BS 460, OTBD SIDE OF RBL 9 FLOORBEAM IS CRACKED ON UPPER AFT RADIUS. REMOVED AND REPLACED IAW SRM 51-42-21 AND 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · airframe 25,653 hrs · 24,167 cycles

CARGO BAY FLOOR EDGE MEMBER ON RT SIDE FROM BS 559.80 - 574 HAS CORROSION AROUND FASTENER HOLES. C/W ECTC REO 601R-53-00-526-01 AND GREO 601R-53-00-526.

Part: ANGLE — CRACKED (BS 484) · airframe 25,653 hrs · 24,167 cycles

BS 484 FLOOR ANGLE CRACKED. REPAIRED IAW REO 601R-53-41-1906, SRM 51-42-06 AND 51-42-21.

Part: BRACKET — CRACKED (WINDSHIELD) · airframe 25,653 hrs · 24,167 cycles

PILOT'S WINDSHIELD SIDE POST AFT BRACKET IS CRACKED APPROXIMATELY .5L. R & R THE BRACKET IAW SRM 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 25,653 hrs · 24,167 cycles

RIGHT FLOOR SUPPORT BS 310 - 349, CORRODED. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-00-530, REV A.

Part: ANGLE — CRACKED (BS 484) · airframe 25,653 hrs · 24,167 cycles

BS 484 RBL 27 FLOOR ANGLE IS CRACKED. R & R ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 25,653 hrs · 24,167 cycles

CARGO BAY DOOR SILL HAS CORROSION AROUND FASTENER HOLES. REPAIRED IAW REO 601R-53-00-526 AND GREO 601R-53-00-526, REV.

Part: SEAT TRACK — CORRODED (BS 400-409) · airframe 25,653 hrs · 24,167 cycles

RIGHT SEAT TRACK FROM BS 400-409+128 HAS MULTIPLE AREAS OF CORROSION MOSTLY AROUND SCREWS HOLES. ONE COIN SLAT LANDING HAS LARGE AREA OF CORNER MISSING. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-02 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 400-409) · airframe 25,653 hrs · 24,167 cycles

LEFT SEAT TRACK FROM BS 400 - 409+128 HAS MULTIPLE AREAS OF CORROSION MOSTLY AROUND SCREW HOLES AND 2 AREAS OF MISSING MATERIAL ON CORNERS OF COIN SLOT LANDING. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-02, AMM 53-01-11-400-802.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 25,653 hrs · 24,167 cycles

CARGO DOOR LINTEL CHANNEL AFT LOWER BRACKET IS CRACKED AT FS 621. REMOVED AND INSTALLED NEW 601R35050-109, ANGLE IAW SRM 51-42-21.

Part: BEAM — CHAFED (CARGO BAY) · airframe 25,659 hrs · 24,173 cycles

CARGO MEMBER BEAM WHERE CARGO NET ATTACHES IS CHAFED APPROXIMATELY .010 DEEP ON AFT OTBD END FROM CONTACT WITH AFT CARGO DOOR SPRING BOX CABLE DUE TO A DELAMINATED PULLEY. COMPLIED WITH STS EA 12-2015-159 AND EC/TC REQUIRED FOR EA 12-2015-159. PERMANENT REPAIR.

Part: POST — CRACKED (BS 409) · airframe 25,653 hrs · 24,167 cycles

BS 409+128, LBL 18.0 INBD VERTICAL POST AFT RADIUS HAS AN INDICATION .25" L X 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED POST SECTIONS IAW SRM 51-42-06. LOCATED AND DRILLED NEW POST IAW SRM 51-40-11. INSTALLED NEW POST IAW SRM 51-42-22 AND SRM 51-42-06 AND REO 601R-53-41-889, REV A.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 25,655 hrs · 24,169 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED FWD FACE BL 0.0, WL 112 - WL 118.5 APPROXIMATELY 6.5" IN LENGTH 55 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGED PORTION OF REAR PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1285. COMPLIED WITH REO 601R-53-61-1285, REV D DATED 10/31/2011. COMPLIED WITH EC/TC REO 601R-53-61-1285 07 AND GREO 601R-53-61-1285, REV D DATED 10/31/2011 AS WRITTEN.

Part: STIFFENER — CRACKED (BS 409) · airframe 25,653 hrs · 24,167 cycles

BS 409.0+128, BL 0, RT VERTICAL POST AFT RADIUS HAS AN INDICATION .25" L X 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED BL 0 INBD AND OTBD POST SECTIONS IAW SRM 51-42-06. POST REMOVED FROM 409+128. LOCATED NEW BL 0 INBD AND OTBD POSTS AT FS 409+128 IAW SRM 51-40-11. NEW BL L0 POST ASSY REQ INSTALL AT FS 409+128. INSTALLED NEW POST ASSY AT FS 409+128 BL 0 IAW SRM 51-42-06 AND SRM 51-42-22 AND REO 601R-53-41-889, REV A. ASSEMBLED LT AND RT FS 409+128, BL 0 POST TOGETHER IAW SRM 51-42-06 AND NEW REINFORCING ANGLES IAW SRM 51-42-06. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889, REV A.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 25,653 hrs · 24,167 cycles

ISOLATOR PN SL2337-3, BROKEN ON AFT PRESSURE BULKHEAD MIDWAY UP NEAR CARGO DOOR. REMOVED 10 EA BROKEN ISOLATORS FROM FS 621 BULKHEAD AND INSTALLED NEW IAW SRM 51-42-06.

Part: SPLICE — WRONG PART (EMERGENCY LIGHTS) · airframe 25,659 hrs · 24,173 cycles

WARDROBE INBD EMERGENCY EXIT LIGHT HAS 1 EA INCORRECT SPLICE INSTALLED. R & R SPLICE ON WARDROBE FLOOR LEVEL EMERGENCY EXIT SIGN IAW ESPM 20-17-00 AND AMM 33-51-10-400-801. EMERGENCY LIGHT OPS TEST GOOD IAW AMM 33-51-00-710-801.

Part: SIGN — INOPERATIVE (CABIN) · airframe 23,899 hrs · 22,399 cycles

LIGHTED FLOOR LEVEL EXIT SIGN AT GALLEY INOPERATIVE. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: LIGHT — DETERIORATED (CABIN) · airframe 22,422 hrs · 20,868 cycles

LUMINESCENT STRIP AND COVER AT ROW 7C AND 8D COMING OFF FLOOR. R & R LIGHT IAW MM 33-51-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,929 hrs · 20,345 cycles

PAX DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-21. OPS TESTED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,734 hrs · 20,131 cycles

NR 5 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21, OPS CHECKED GOOD.

Part: BULKHEAD — CRACKED (BS 621) · airframe 21,487 hrs · 19,867 cycles

FOUND AN INDICATION ON FS 621.00 REAR PRESSURE BULKHEAD WEB AT BL 0.0, WL 112 TO WL 113 APPROX 1.5" LONG X 70 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1285 REV.D.

Part: BULKHEAD — CRACKED (BS 621) · airframe 21,487 hrs · 19,867 cycles

FOUND AN INDICATION ON FS 621.00 REAR PRESSURE BULKHEAD WEB AT LBL 27.5, WL 130 (AT TOP OF CARGO DOOR TRACK) APPROX .4" LONG X 100% FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541 REV D DATED 10-31-2011.

Part: BULKHEAD — CRACKED (BS 621) · airframe 21,487 hrs · 19,867 cycles

FOUND AN INDICATION ON FS 621.00 REAR PRESSURE BULKHEAD, WEB LBL 46, WL 108 (LINTEL FITTING) APPROX .3 LONG X 70 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW ECTC REO 601R-53-61-1230 AND REO 601R-53-61-1230, EV F.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 21,487 hrs · 19,867 cycles

LT SIDE INTERCOSTAL BETWEEN FS 621 AND FS 625 AT STR 13 IS CRACKED 1.0" IN THE AFT RADIUS. REMOVED AND LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 21,487 hrs · 19,867 cycles

LT SIDE INTERCOSTAL BETWEEN FS 621 AND FS 625 AT STR 14 IS CRACKED 1.0" IN RADIUS AT THE AFT END. REMOVED, LOCATED & DRILLED NEW INTERCOSTAL IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-21.

Part: POST — CRACKED (BS 409) · airframe 21,487 hrs · 19,867 cycles

OTBD VERTICAL POST AT FS 409.00+128, RBL 18 HAS AN INDICATION NOTED AT WL 69.00 .3" LONG X 55 PERCENT FSH. FAILED NDT INSPECTION AFT FLANGE RADIUS. REMOVED INBD & CRACKED OTBD VERTICAL POST AT FS 409+128 RBL 18 IAW SRM 51-42-06. LOCATED FASTENER HOLES IN NEW INBD POST PN: 601R32208-32S & OTBD, POST PN: 601R32208-156 IAW SRM 51-40-11. BENCH ASSEMBLED THE INBD & OTBD FS 409, RBL 18 VERTICAL POSTS. LOCATED & DRILLED 409 POST ASSY & INSTALLED IAW SRM 51-42-22-00 & 51-40-11-00 & 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,487 hrs · 19,867 cycles

UNDERFLOOR FS 484 PULLEY SUPPORT INTERCOSTAL HAS 2 CRACKED ATTACH ANGLES AT THE INBD SIDE OF LBL 36 AND OTBD SIDE OF LBL 27. REPAIRED IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,487 hrs · 19,867 cycles

UNDERFLOOR FS 484 PULLEY SUPPORT INTERCOSTAL HAS A CRACKED ATTACH ANGLE AT THE INBD SIDE OF RBL 36. REPAIR TO THE INTERCOSTAL AT FS 484 BETWEEN BL 27.00 AND BL 36.00 IS COMPLETED IAW REO 601R-53-41-059.

Part: MODULE — FAILED (NLG STEERING) · airframe 21,134 hrs · 19,515 cycles

NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE IN FLIGHT, COMPLIED WITH QRH MESSAGE NO LONGER EXISTS, SEEMS TO FAIL INTERMITTENTLY ANYWHERE FROM EVERY 5 TO 20 MINUTES. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE. R & R ELECTRO-HYDRAULIC MODULE IAW AMM 32-51-15, OPS & LEAK CHECKED GOOD.

Part: PRESSURE SWITCH — UNSERVICEABLE · airframe 21,039 hrs · 19,416 cycles

CLIMBING THRU FL260, RECEIVED OIL PRESSURE WARNING FOR LT ENGINE, SAW PRESSURE AS LOW AS 16 PSI AND HOVERED AROUND 23 PSI, FOLLOWED QRH WHICH DIRECTS ENGINE SHUTDOWN. RECEIVED BOTH LOW PRESSURE INDICATION AND EICAS WARNING AND AURAL. LANDED SINGLE ENGINE. EMERGENCY DECLARED AS A PRECAUTION. FOUND LINE ON PRESSURE SWITCH LOOSE, RESECURED. R & R PRESSURE TRANSDUCER, SERVICED ENGINE OIL 5.5 QTS. OPS CHECKED NO FURTHER DEFECTS NOTED. OPS CHECKED IAW 79-31-05. SDR CLOSED.

Part: PLACARD — MISSING (CABIN) · airframe 19,641 hrs · 17,889 cycles

EXIT PLACARD MISSING FROM INSIDE OF MAIN PASSENGER DOOR. REPLACED EXIT PLACARD ON PAX DOOR IAW AMM 11-30-00. ACFT OK FOR SERVICE.

Part: FITTING — CRACKED (BULKHEAD) · airframe 19,576 hrs · 17,815 cycles

LEFT SIDE FS 625 FITTING CRACKED ON AFT SIDE OF REAR PRESSURE BULKHEAD. REPLACED WITH NEW FITTING IAW SRM 51-42-21.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,289 hrs · 17,496 cycles

CRACK FOUND ON PAX DOOR AFT DRAG ANGLE. REPAIRED AFT DRAG ANGLE IAW REO 601R-52-11-513.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,976 hrs · 16,034 cycles

F/A FLASHLIGHT INOPERATIVE. R & R F/A FLASHLIGHT IAW AMM 25-61-00.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 17,617 hrs · 15,617 cycles

AMBER SMOKE TOILET MESSAGE AT ABOUT 10,000 DURING DESCENT, LASTED LESS THAN A MINUTE THEN WENT AWAY. OBSERVED AN ODOR LIKE MACHINE OIL, BUT NOT SMOKE. F/A HEARD SMOKE ALARM IN LAV BUT DID NOT SEE OR DETECTED SMOKE. OPS CHECK OF SMOKE DETECTION SYS IAW AMM 26-16-00, NO FURTHER DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,139 hrs · 15,064 cycles

EMERGENCY LIGHT NOT FUNCTIONING WHEN SELECTED ON. R & R EMERGENCY LIGHT BATTERY PACK, OPS CK GOOD. AMM 33-51-04-000-801-802.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 16,825 hrs · 14,704 cycles

THE LT FWD OVERWING EMERGENCY LIGHT IS INOP. REPLACED LIGHT BULB FOR LT FWD OVERWING EMERGENCY LIGHT. OPS CHECKED GOOD. WORK DONE IAW AMM CHAPTER 33-51-21.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 16,776 hrs · 14,637 cycles

PASSENGER COMPARTMENT LT AND RT EMERGENCY LIGHT FLUSH TRACK COVERS CRACKED IN NUMEROUS LOCATIONS. REMOVED THE FLOOR TRACK EMERGENCY LIGHT IAW AMM CH 33-51-01-000-801, SO161774 8/26/10. REINSTALLED THE FLOOR TRACK EMERGENCY LIGHT IAW AMM CH 33-51-01-400-801. INSTALLED NEW EMERGENCY TRACK LIGHTING AS REQUIRED SM161739 8/26/10. (CLOSED)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 16,811 hrs · 14,683 cycles

FLOORBEAM HAS MINOR CORROSION AROUND NUTPLATE ON ON INBD ROW OF CARGO FLOOR PANEL 281LLF. DRILLED NEW FLOORBEAM IAW SRM 51-42-21 & 51-42-06. INSTALLED FLOORBEAM CAP REF SRM 51-42-22.

Part: FRAME — CORRODED (BS 349) · airframe 16,776 hrs · 14,636 cycles

CORROSION FWD AND AFT SIDE OF 349 FRAME AND LOWER LEG BTWN STRINGER 26L AND 26R (BELLY) NEW 349, FRAME NEEDS TO BE DRILLED AND INSTALLED. DRILLED NEW FRAME SRM 22 51-40-11. INTERCOSTALS AT STR 25L & 25R, VERTICAL POST AT FS 349L, DRAIN MAST CHANNEL, SUPPORT BRACKET & GANG CLAMP FS 349 24L AND NEW FRAME NEED TO BE INSTALLED. INSTALLED INTERCOSTALS AT STR 25L & 25R, VERTICAL POST AT FS 349L, DRAIN MAST & CHANNEL, SUPPORT BRACKET & GANG CLAMP FS 349 STR 24L, AND NEW FRAME AT FS 349 IAW SRM 51-42-06, 51-42-21, 51-23-00, 51-21-16, AND 51-21-11.

Part: SKIN — CORRODED (BS 319.17 S26L/R) · airframe 16,776 hrs · 14,636 cycles

CONTINUATION OF BELLY CORROSION JUST FWD OF FRAME FS 319.17 BETWEEN 26L & 26R. INSTALLED 6 FASTENERS, RESTORED FINISH, AND APPLIED CIC PER SRM 51-42-06, 51-21-16, AND 51-21-11.

Part: FRAME — CORRODED (BS 333) · airframe 16,776 hrs · 14,636 cycles

CORROSION ON AFT SIDE OF FRAME FS 333 BETWEEN 26L & 26R. REINSTALL REMOVED FASTENERS AND RESTORE FINISH. INSTALLED 3 FASTENER, RESTORED FINISH, AND APPLIED CIC PER SRM 51-42-06, 51-21-16, AND 51-21-11.

Part: BULKHEAD — CRACKED (BS 202.75) · airframe 16,776 hrs · 14,636 cycles

PERFORMED EDDY CURRENT INSP OF FWD PRESSURE BULKHEAD WEB AT FS 202.75 AT BRAKE CABLE ATTACH POINT IAW NDT INSP PROCEDURE ET.2. FWD PRESSURE BULKHEAD WEB IS CONFIRMED CRACKED AT THE 8 O'CLOCK AND 11 O'CLOCK POSITIONS LOOKING AFT AT BULKHEAD. BOTH INDICATIONS ARE MARKED AT THE END OF THE CRACK. PERFORMED EDDY CURRENT INSPECTION OF FWD PRESSURE BULKHEAD WEB AT FS 202.75 AT BRAKE CABLE ATTACH POINT IAW MAC NDT INSPECTION PROCEDURE ET.2. FWD PRESSURE BULKHEAD WEB IS CONFIRMED CRACKED AT THE 8 O'CLOCK AND 11 O'CLOCK POSITIONS LOOKING AFT AT BULKHEAD. BOTH INDICATIONS ARE MARKED AT THE END OF THE CRACK.

Part: FLOOR SUPPORT — CORRODED (BS 585-615) · airframe 16,776 hrs · 14,636 cycles

FLOOR SUPPORT HAS MINOR CORROSION AROUND NUTPLATES ON INBD ROW OF CARGO FLOOR PANEL 281LLF. REMOVED NUT PLATES ON FLOOR SUPPORT CAP AT LBL 27 STA 585-615 BLENDED CORRODED AREAS ON LBL 27 FLOOR SUPPORT CAP AT STA 615, 609, 603, 597, 591, 585 REF SEM 51-21-06. PERFORMED UT THICKNESS INSP OF BLENDED AREAS ON FLOORBEAM CAP IAW MAC NDT INSP PROCEDURE UT-3 MINIMUM MATERIAL REMAINING IS FS 615-.060", FS 609-.039", FS 603-.045", FS 597 UNREADABLE, FS 591-.028", FS 585-.026". REMOVED FASTNERS FROM LT SIDE OF FLOOR SUPPORT CAP IAW SRM 51-42-06. BLENDED AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00- FIG 101.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,776 hrs · 14,636 cycles

SEAT TRACK HAS MINOR CORROSION LBL 9.00 AT FS 559 + 80. REMOVED OLD SEAT TRACK AT LBL 9 AT FS 559+80 & INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,776 hrs · 14,636 cycles

SEAT TRACK HAS MINOR CORROSION, RBL 9.00 AT FS 559+80. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 20-21-00-910-004.

Part: FRAME — CORRODED (BS 349) · airframe 16,776 hrs · 14,636 cycles

CORROSION ON FWD AND AFT SIDE OF 349 FRAME AND LOWER LEG BETWEEN STRINGERS 26L TO 26R BELLY. REMOVED FASTENERS THROUGH SKIN, DRILLED OUT FASTENERS THROUGH TOP OF FRAME FROM STR25L TO 25R, REMOVED GUSSETE & TRACK SUPPORT. REMOVED FASTENERS THROUGH TIE STRAP & FRAME IAW SRM 51-42-06. REMOVED INTERCOSTALS, REMOVED VERTICAL POST AT FS 349L, REMOVE DRAIN MAST AND CHANNEL PER SRM 51-42-06 AND AMM 38-32-01-000-801. FINISHED REMOVING FASTNERS FROM FRAME, DISBONDED SEALENT, REMOVED SUPPORT BRACKET & GANG CLAMP FS 349 STR 24L IAW SRM 51-42-21 & 51-42-06. REMOVED FRAME & DRILL UP NEW FRAME AND INSTALLED.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,776 hrs · 14,636 cycles

SEAT TRACK HAS MINOR CORROSION RBL9.00 AT FS 559 + 92. (APPX). REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 20-21-00-910-004.

Part: SKIN — CORRODED (BS 310) · airframe 16,776 hrs · 14,636 cycles

BELLY CORROSION JUST AFT FRAME 310 AT LT SIDE OF 27 NEXT TO WATER DRAIN. REMOVED WATER DRAIN LEFT OF STR 27 REMOVED 5EA FASTNERS FROM LEFT SIDE OF STR 27 IAW SRM 51-42-06 REMOVED CORROSION LEFT OF STR 27 & AFT OF 310 NEXT TO WATER DRAIN IAW SRM 51-21-06. AREA REQUIRES NDT TO DETERMINE AMOUNT OF MATERIAL REMOVED. PERFORMED UT THICKNESS INSPECTIN OF BLEND AREA ON FUSELAGE SKIN AFT OF FS 310.00 AT LEFT SIDE OF STR 27 IAW MAC NDT INSPECTION PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS 057". REFER TO SRM FOR ALLOWABLE DAMAGE OR NOT . DAMAGE IS WITHIN LIMITS PER SRM 53-00-31. RESTORED A023 PROTECTIVE COATING AND APPLIED CIC PER SRM 51-21-11 AND 51-21-16 ALL FASTNERS REMOVED IN STEP 1 WERE INSTALLED PRIOR TO A023 FINISH AND CIC PER SRM 51-42-06.

Part: SKIN — CORRODED (BS 319.17 S26L/R) · airframe 16,776 hrs · 14,636 cycles

BELLY CORROSION JUST FWD OF FRAME 319.17 BETWEEN 26L AND 26R. REMOVED 6 EA FASTENERS FROM 319 FRAME BETWEEN 26L & 26R IAW SRM 51-42-06. REMOVED CORROSION IAW SRM 51-21-06. AREA REQUIRES NDT TO DETERMINE MATERIAL REMOVED. PERFORMED UT THICKNESS INSP OF BLEND AREA ON FRAME AT FS 319.70 BETWEEN STR 26L AND 26R IAW MAC NDT INSP PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS .048". REFER TO SRM FOR ALLOWABLE DAMAGE OR NOT. FOUND BLENDED AREA TO BE WITHIN LIMITS IAW SRM 53-00-00, BLOCK 101-199. BLENDED AREA NEEDS TO BE NDT FOR CRACKS AND REINSTALL REMOVED FASTENERS AND RESTORE FINISH. PERFORMED LPI, TYPE 1 METHOD C ON BLENDED AREA IAW SRM 51-12-00 IAW MAC NDT INSP PROCEDURE PT-1 NO INDICATIONS NOTED AT THIS TIME.

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 16,776 hrs · 14,636 cycles

FLOOR SUPPORT CRACKED IN CARGO COMPARTMENT AT AFT PRESSURE BULKHEAD UNDER PANEL 281LLF. REMOVED LT FS 621 FLOOR SUPPORT ANGLE LT SIDE REF SRM 51-42-06 AND 51-42-21. DRILLED COUNTERSUNK AND TRIMMED NEW FLOOR SUPPORT ANGLE REF SRM 51-40-11. STARTED INSTALLING LT FS 621 FLOOR SUPPORT ANGLE REF SRM 51-42-21. CONTINUE INSTALLING LT FS 621 FLOOR SUPPORT ANGLE. FINISHED INSTALLING FASTNERS ON LT FS 621 FLOOR SUPPORT ANGLE REF SRM 51-42-06.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,613 hrs · 14,441 cycles

NR 1 CABIN CEILING EMERGENCY LIGHT INOP. RELAMPED NR 1 CEILING EMERGENCY LIGHT IAW AMM 33-51-16 OPS CHECK GOOD. RELAMPED NR 1 CEILING EMERGENCY LIGHT IAW AMM 33-51-16 OPS CHECK GOOD.

Part: SEAL — LACK OF LUBE (SERVICE DOOR) · airframe 15,900 hrs · 13,624 cycles

CATERING PERSONEL AND F/A REPORT SERVICE DOOR BEING DIFFICULT TO CLOSE AND OPEN. CLEANED AND LUBRICATED DOOR SEAL AND STRIKER IAW MM 12-20-52. OPS CK GOOD IAW MM 52-41-00.

Part: DOOR — STUCK (SERVICE) · airframe 14,426 hrs · 12,064 cycles

CABIN SVC REPORTS SERVICE DOOR EXTREMELY DIFFICULT TO OPEN AND CLOSE. FLT 5603 DEL 35 MINS.

Part: FLAP — FAILED (WING) · airframe 14,021 hrs · 11,668 cycles

AFTER TAKEOFF FLAPS FAILED AT 8FT, LANDED CVG. NOT AN OVERWEIGHT LANDING. EMERGENCY DECLARED. A/C RETURNED TO CVG AFTER T/O. FLT 4972 DEL 138 MINS.

Part: STEP — BROKEN (PAX DOOR) · airframe 13,131 hrs · 10,848 cycles

PAX DOOR BOTTOM STEP BROKEN.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 12,609 hrs · 10,387 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.0 INCH IN RADIUS. REMOVED AND REPLACED CARGO DOOR SUUPPORT BEAM ANGLE IAW SRM 51-42-21. PRESSURE CHECK DUE. PERFORMED PRESSURE CHECK IAW AMM 21-32-00-863-801. NO DISCREPANCIES NOTED AT THIS TIME. (S)

Part: SKIN — CORRODED (RT WING) · airframe 12,609 hrs · 10,387 cycles

RT WING LOWER PLANK ACCESS HOLE 650BB HAS CORROSION AROUND ENTIRE LANDING IN CRITICAL AND NON-CRITICAL AREAS. FAILED NDT INSPECTION 60% FULL SCREEN HEIGHT. REPAIRED RT WING LOWER PLANK ACCESS HOLE NR10 650BB IAW REO 601R-57-21-030. COMPLIED WITH EC/TC EO 600-57-81. COMPLIED CONTACTED STRUCTURE ENGINEERING AND PROVIDED ALL FORMS. RII COMPLIED WITH. (S)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,609 hrs · 10,387 cycles

FS 484.0, RBL 36.0 INTERCOSTAL CRACKED (NOT PREVIOUSLY REPAIRED). REPAIRED INTERCOSTAL AT FS 484.0 RBL 36.0 IAW REO 601R-53-41-059. COMPLIED WITH REO 601R-53-41-059. PRESSURE CHECK DUE. PERFORMED PRESSURE CHECK IAW AMM 21-32-00-863-801. NO DISCREPANCIES NOTED AT THIS TIME. RII COMPLIED WITH 5300002. (S)

Part: CHANNEL — CRACKED (CARGO DOOR) · airframe 12,609 hrs · 10,387 cycles

CARGO DOOR FWD, LOWER "C" CHANNEL IS CRACKED. REMOVED AND REPLACED CHANNEL IAW SRM 51-42-06. (S)

Part: SILL — CRACKED (BS 280)

JUST OUTBOARD LBL 9, FS 280 UPPER SILL CRACKED APPROX 1 INCH LONG AT MLG EMERGENCY RELEASE CABLE BRACKET. REMOVED MLG EMERGENCY RELEASE CABLE BRACKET IAW SRM 51-41-02. REPAIRED LBL 9 FS 280 UPPER SILL IAW REO 601R-53-11-138-NC AND DEVIATION REO 601R-53-11-1441. RE-INSTALLED MLG EMERGENCY RELEASE CABLE BRACKET IAW SRM 51-41-02. FUNCTIONAL TEST OF EMERGENCY GEAR EXTENSION DUE. PERFORMED FUNCTIONAL TEST OF EMERGENCY GEAR EXTENSION IAW AMM 32-34-00-720-801. FUNCTIONAL TEST OK AT THIS TIME. COMPLIED WITH ASA ECTC REO 601R-53-11-1441 IAW REO 601R-53-11-1441. COMPLIED WITH ASA EC-TC REO 601R-53-11-138. ASA RII COMPLIED WITH. (S)

Part: SILL — CRACKED (FUSELAGE) · airframe 12,609 hrs · 10,387 cycles

JUST OUTBOARD LBL 9, FL 280 UPPER SILL CRACKED APPROX 1 INCH LONG AT MLG EMERGENCY RELEASE CABLE BRACKET. (S)

Part: ANGLE — CRACKED (BS 621)

RT SIDE FUSELAGE STATION 621 OBLIQUE ANGLE CRACKED. REFERENCE MWC JOB 8784311, OP 48 FOR REPLACEMENT OF OBLIQUE ANGLES. REMOVED LT/RT FS 625 OBLIQUE ANGLES IAW SRM 51-42-21. LOCATED HOLES IN NEW SERVICEABLE OBLIQUE ANGLES IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FS 625 OBLIQUE ANGLES IAW SRM 51-42-21. (A)

Part: ANGLE — CRACKED (BS 621)

LT SIDE FUSELAGE STATION 621 OBLIQUE ANGLE CRACKED. REPLACEMENT OF OBLIQUE ANGLES. REMOVED LT/RT FS 625 OBLIQUE ANGLES IAW CRJ 200 SRM 51-42-21. LOCATED HOLES IN NEW SERVICEABLE OBLIQUE ANGLE IAW CRJ 200 SRM 51-40-11. INSTALLED NEW SERVICEABLE FS 625 OBLIQUE ANGLES IAW CRJ 200 SRM 51-42-21. (A)

Part: PIN — NOT SEATED (CABIN)

JOB 8783411 OPERATION 37. RT OVERWING EMERGENCY EXIT (EYE LEVEL) LIGHT DOES NOT WORK FROM BATTERY PACK NR 4. TROUBLESHOT USING CRJ 200 WDM 33-51-00 AND 33-52-00 AND FOUND WIRE LY10D22 CONTACT PIN NOT SEATED IN TB105-3. SECURED WIRE CONTACT INTO TERMINAL MODULE IAW EESPM 20-18-00. RT EMERGENCY EXIT SIGN NOW ILLUMINATES NORMALLY DURING BATTERY PACK 4 OP TEST IAW AMM 33-51-04-710-801. SUPPLEMENTAL SDR CLOSED 7/31/08 (A)

Part: PIN — NOT SEATED (CONNECTOR) · airframe 12,609 hrs · 10,387 cycles

RT OVERWING EMERGENCY EXIT (EYE LEVEL) LIGHT DOES NOT WORK FROM BATTERY PACK NR 4. TROUBLESHOT USING CRJ 200 WDM 33-51-00 AND 33-52-00 AND FOUND WIRE LY10D22 CONTACT PIN NOT SEATED IN TB105-3. SECURED WIRE CONTACT INTO TERMINAL MODULE IAW EESPM 20-18-00. RT EMER EXIT SIGN NOW ILLUMINATES NORMALLY DURING BATTERY PACK 4 OP TEST IAW AMM 33-51-04-710-801. SUPPLEMENTAL SDR CLOSED 7/31/08. (A)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,609 hrs · 10,387 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED IN PREVIOUS REPAIR SPLICE. COMPLIED WITH REO 601R-52-11-513 AND ASA ECTC 601R-52-11-513. SUPPLEMENTAL SDR CLOSED 7/31/08. (A)

Part: ANGLE — CRACKED (BS 625) · airframe 12,609 hrs · 10,387 cycles

LT AND RT FS 625 OBLIQUE ANGLES ARE CRACKED. OPEN. (S)

Part: LIGHT — DAMAGED (CABIN) · airframe 12,106 hrs · 9,958 cycles

FLOOR EMERGENCY FLOODLIGHT DAMAGED.

Part: FLAP — FAILED (WING) · airframe 11,896 hrs · 9,764 cycles

FLAP FAIL AT ZERO WHEN SELECTING 8 AT 200 KTS. EMERGENCY EQUIPMENT REQUESTED TO BE ON STANDBY AS A PRECAUTION. FLT4656 DEL 171 MINS.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 11,735 hrs · 9,625 cycles

FLAPS FAILED AT 0 AFTER TAKEOFF IN ATL RETURNED FOR LANDING IN ATL, EMERGENCY DECLARED. AIRCRAFT RETURNED TO ATL AFTER T/O.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 11,069 hrs · 9,054 cycles

FLAPS FAIL AT 0 DEGREES ON APPROACH WHEN SELECTED TO 8 DEGREES. EMERGENCY EQUIPMENT ON STANDBY.

Part: STEP — BROKEN (DOOR) · airframe 10,804 hrs · 8,813 cycles

ASD LOWER STEP BROKEN.

Part: DOOR — STUCK (SERVICE DOOR) · airframe 10,303 hrs · 8,422 cycles

SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 8,211 hrs · 6,827 cycles

EMERGENCY EXIT SIGN NEXT TO SERVICE DOOR INOP.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 7,963 hrs · 6,643 cycles

RANRC 244, PAX DOOR AFT DRAG ANGLE CRACKED.

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 7,963 hrs · 6,643 cycles

RANRC 207, LT 621 FLOOR SUPPORT ANGLE CRACKED. ACCOMPLISHED ASA EO CARD NO. REO 601R-53-61-117 STEPS 1-7 JP929 09-05-06 OK TO INSTALL REPAIR ANGLE RA313 INSTALLED REPAIR IAW ASA TASK CARD REO 601R-53-61-117. TS1050 090606 RA313 REQ'S TOP COAT. TOP COATED REPAIR IAW ASA E.O. REO 601R-53-61-117 RA313 RII 5000546 (SUPPLEMENTAL-SDR CLOSED 9/14/06)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 7,963 hrs · 6,643 cycles

RANRC 231, RIGHT RBL 27 AT FS 484 INTERCOSTAL CRACKED.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 7,963 hrs · 6,643 cycles

RANRC 211, LEFT FS 484 OUTBOARD OF LBL 36, BRACKET AND INTERCOSTAL CRACKED.REMOVED DAMAGED ANGLE AT O/B SIDE OF LBL 27 & CUT-OUT DAMAGED SECTION OF INTERCOSTAL AT I/B SIDE OF LBL 36 AS REQUIRED IAW REO. HAD LPI OF INTERCOSTAL CUTLINE PERFORMED REFER TO W/C 281. FABRICATED ANGLE & DUPLICATED CLIP. ALL IAW CRJ REO. OK TO INSTALL BOTH CLIP & ANGLE. RA333 INSTALLED CLIP TO O/B SIDE OF LBL27 IAW CRJ REO. INSTALLED -1 ANGLE AT FS 484 LBL 36 IAW ASA TASK CARD REO. PRIMED & TOP COATED. REPAIR FASTENERS IAW CRJ SRMS. REINSTALLED OBD CABLE PULLEY BRACKET AT FS 484 LBL 31 IAW CRJ SRM 51-41-02. (CLOSED)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 7,963 hrs · 6,643 cycles

RANRC 215, LBL 9, FS 280 CLIPS I/B AND O/B CRACKED. REMOVED AND DUPLICATED CLIPS USING 2024-T3, .050, PO 8398-1. PRIMED AND TOPCOATED. ALL WORK DONE IAW CRJ SRM 51-24-26, 51-25-16. (EMP 302) OK TO INSTALL. (INSP RA313) COMPLETED INSTALLATION IAW CRJ SRM 51-24-26, 51-25-16. (EMP 302 - INSP RA313) (SUPPLEMENAL-SDR CLOSED 9/12/06)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 7,963 hrs · 6,643 cycles

RANRC 216, RBL 9, FS 280 O/B CLIP CRACKED. REMOVED AND DUPLICATED CLIPS USING 2024-T3, .050, PO# 8398-1. PRIMED AND TOPCOATED. ALL WORK DONE IAW CRJ SRM 51-24-26, 51-25-16. (EMP 302) OK TO INSTALL. (INSP RA313) COMPLETED INSTALLATION IAW CRJ SRM 51-24-26, 51-25-16. (EMP 302 - INSP RA313) (SUPPLEMENTAL-SDR CLOSED 9/12/06)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 7,763 hrs · 6,489 cycles

EMERGENCY EXIT FLOOR LIGHTING INOP AT SEAT 1CD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 7,117 hrs · 5,969 cycles

EMERG FLOOR LIGHTING FLICKERS INTERMITTENTLY WHEN SWITCH IS IN THE "ON" POSITION, FLT 4897 DEL 38 MINS.

Part: PLACARD — UNSECURE (PAX DOOR) · airframe 6,980 hrs · 5,860 cycles

EXIT PLACARD ON PAX DOOR FADED AND NOT SECURED.

Part: CONTROL PANEL — MALFUNCTIONED (CARGO FIRE)

DURING CLIMB OUT, AT APPROX 5,000 FT THE CREW RECEIVED A CARGO SMOKE WARNING. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. AFTER THE CREW DISCHARGED THE FIRE BOTTLES, THE WARNING WENT OUT. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED SAFELY. AFTER LANDING THE EMERGENCY SERVICES INSPECTED THE AC AND FOUND NO EVIDENCE OF ANY FIRE OR SMOKE AND THE AC PROCEEDED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE CARGO FIRE X PANEL AND ALSO THE NR1 AND NR2 FIRE BOTTLES ASSEMBLIES, THE NR1 AND NR2 FIRE BOTTLE SQUIBS AND BOTH CARGO SMOKE DETECTORS. OPS CHECK GOOD. AC OK FOR SERVICE. (K)

Part: POWER SUPPLY — DISCHARGED (CABIN)

FLT 4500 - DURING A GROUND INSPECTION IN ATL, LEFT EXTERIOR EMERGENCY LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS POWER SUPPLY UNIT AT ROW 8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDSHIELD — BROKEN (COCKPIT)

DURING DESCENT, OUT OF 25,000 FT, THE F/O`S WINDSHIELD SHATTERED. THE QRH WAS COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT LANDED SAFELY.

Part: BPSU — FAILED (TE FLAPS)

DURING TAKEOFF, AT APPROX 1,000 FEET AFTER SELECTING THE FLAPS FROM EIGHT DEGREES TO ZERO DEGREES THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW REQUESTED EMERGENCY EQUIPMENT STANDBY AS A PRECAUTION AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT BRAKE AND POSITION SENSOR UNIT, AND ALSO PREFORMED OPS CHECK OF THE FLAPS SYSTEM FOR APPROX FIFTEEN MINUTES WITH NORMAL RESULTS. AIRCRAFT OK FOR SERVICE. (M)

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS)

DURING CLIMB-OUT, WHEN FLAPS WERE SELECTED TO ZERO DEGREES, THEY STAYED AT EIGHT DEGREES AND THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW LEVELED OFF THE AIRCRAFT AND MAINTAINED A SPEED OF 200 KNOTS WHILE COMPLYING WITH THE QRH. UPON NOTIFYING THE FLIGHT ATTENDANT AND PASSENGERS OF THE INTENT TO RETURN TO DFW, THE FLIGHT ATTENDANT REPORTED A BURNING SMELL IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE FLAPS ELECTRONIC CONTROL UNIT. OPERATIONAL AND GROUND TEST WERE NORMAL. AIRCRAFT OK FOR SERVICE. (M)