N750EV

Part: GUIDE FITTING — GOUGED (ZONE 500) · airframe 44,403 hrs · 32,862 cycles

LEFT OUTBOARD FLAP, INBOARD GUIDE FITTING GOUGED. (C-CHECK RO 2/25/2025) PERFORMED REPAIR AREA ON LH OB FLAP IB GUIDE FITTING IAW REO 670-57-51-587 REV-- DATE 2025-01-17, CRJ700 SRM 51-24-11, 53-00-00, 51-12-00.

Part: HOUSING — CRACKED (WING) · airframe 44,403 hrs · 32,862 cycles

CRACK IN SLAT TRACK HOUSING INSIDE FUEL PANEL 551AB (C-CHECK RO 2/25/2025) REPAIRED DAMAGED SLAT TRACK HOUSING INSIDE FUEL PANEL 551AB IAW REO 670-57-42-577 REV-- DATE 2016-12-02 AND CRJ700 AMM 20-70-00, 28-11-00.

Part: HOUSING — CRACKED (ZONE 600) · airframe 44,403 hrs · 32,862 cycles

SLAT TRACK HOUSING HAS CRACK INSIDE FUEL PANEL 651AB (C-CHECK RO 2/25/2025) REPAIRED DAMAGED SLAT TRACK HOUSING INSIDE FUEL PANEL 651AB IAW REO 670-57-42-577 REV-- DATE 2016-12-02 AND CRJ700 SRM 51-21-11, 51-25-06, AMM 20-70-00, 27-81-41, 27-81-39, 28-11-00. INSTALLATION OF RH SLAT DISCONNECT SENSOR AT WS178.00 AND RH SLAT TRACK 1-3 TO BE ACCOMPLISHED ON AVMAX WC: 6102 CP# 29363030. TOOL USED: DIGITAL SCALE AV-8473 CAL DUE: AUG2025

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 44,403 hrs · 32,862 cycles

LBL12 COCKPIT FLOOR BEAM CRACKED AT BOTTOM WHERE IT ATTACHES TO 280 BEAM (C-CHECK RO 2/25/2025) PERFORMED REPAIR AREA ON LBL12 COCKPIT FLOOR BEAM TO 280 BEAM IAW REO 670-53-11-896 REV-- DATE: 2015-03-17, CRJ700 AMM 20-70-00, CRJ700 SRM 51-42-06, 51-42-10, 51-42-21, 51-40-11, 51-21-11, 51-25-06, PERFORMED NDT INSPECTION BY BARON LLC, FAA CRS# 5NDR545D, REPORT #S011025-1 P.O NUMBER: 175153 DATE: 10-JAN-2025, SEE REPORT FOR DETAILS. CAL TOOL: DIGITAL SCALE ID: AV-8473 CAL DUE: AUG-2025.

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 44,403 hrs · 32,862 cycles

LH REAR FUSELAGE TO VERTICAL FWD AND AFT DRAG ANGLES CRACKED (C-CHECK RO 2/25/2025) PERFORMED REPAIR ON LH REAR FUSELAGE TO VERTICAL STABILIZER AT FWD AND AFT DRAG ANGLES IAW BOMBARDIER REO 670-55-31-018 REV-A DATE: 2016-11-10 AND IAW CRJ 700 SRM 51-25-01PERFORMED NDT ET INSPECTION BY BARON NDT,LLC, FAA CRS# 5NDR545D, REPORT# S122324-15, P.O# 175037 DATE OF INSPECTION: 23-DEC-2024 NO DEFECTS NOTED AT TIME OF INSPECTION CAL TOOL USED DIGITAL SCALE: AV-8473 CAL DUE: AUG-2025FINAL PAPERWORK VERIFICATION LE 2742C

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 44,403 hrs · 32,862 cycles

RH REAR FUSELAGE TO VERTICAL DRAG ANGLE CRACKED (C-CHECK RO 2/25/2025) REPAIRED DAMAGED DRAG ANGLE AND FILLER ON RH REAR FUSELAGE IAW REO 670-55-31-018 REV-A DATE 2016-11-10. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S121824-2, P.O# 174848, DATE OF INSPECTION 18DEC2024.

Part: SKIN — DENTED (ZONE 300) · airframe 44,403 hrs · 32,862 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA78985-670-55-41-107 750EV MXCODEID62683-PR - DENT ON THE RIGHT SIDE RUDDER SKIN AT (RHS DWG: CC670-22031, POCKET THICKNESS AT SUBJECT LOCATION 0.25" +/- 0.004",REF) BETWEEN RS 102.520-RS 108.250. DENT MEASURES 0.383" L X 0.144" W X 0.44" DEEP. COMPLIED WITH TEMPORARY REPAIR PER REO 670-55-41-107. PERMANENT REPAIR DUE WITHIN 5000 FLT HRS BY 45638.3 TAT, PART NUMBER: - , SERIAL NUMBER: 10161, POSITION: (C-CHECK RO 2/25/2025) REPAIRED DENT ON RUDDER RH SIDE IAW CRJ700 SRM 55-41-01, 51-42-06, 51-40-11, 51-21-11, 51-25-06,51-25-16 AND 51-42-13. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S010625-4, P.O# 175153, DATE OF INSPECTION 01JAN2025. SEE REPORT FOR DETAILS. TOOL USED: DIGITAL SCALE AV-8473 CAL DUE: AUG2025

Part: DUCT — WARNING MESSAGE (ANTI-ICE SYS) · airframe 43,220 hrs · 31,868 cycles

DURING DECENT WE TURNED ON WINGS AND COWLS ANTI-ICE. WE RECEIVED ANTI ICE DUCT CAUTION MESSAGE FOLLOWED BY ANTI ICE DUCT WARNING AND L/R DUCT FAIL. WE RAN THE QRH FOR BOTH WARNING AND CAUTION. WE DECLARED AN EMERGENCY AND DESCENDED IMMEDIATELY. ONCE WE LEVELED OFF WE THEN GOT THE STALL HORN. LANDED WITH NO INCIDENT. (FLIGHT 4877 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27722345 WITH THE FOLLOWING CORRECTIVE ACTION: "PLEASE REF. CAMP TRANS ID#27725841, 27725799 FOR CORRECTIVE ACTIONS. "

Part: DUCT — WARNING MESSAGE (ANTI-ICE) · airframe 43,220 hrs · 31,868 cycles

DURING DECENT WE TURNED ON WINGS AND COWLS ANTI-ICE. WE RECEIVED ANTI ICE DUCT CAUTION MESSAGE FOLLOWED BY ANTI ICE DUCT WARNING AND L/R DUCT FAIL. WE RAN THE QRH FOR BOTH WARNING AND CAUTION. WE DECLARED AN EMERGENCY AND DESCENDED IMMEDIATELY. ONCE WE LEVELED OFF WE THEN GOT THE STALL HORN. LANDED WITH NO INCIDENT. (FLIGHT 4877 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS.

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 42,898 hrs · 31,614 cycles

WING OVHT WARNING MESSAGE ON CLIMB OUT, AROUND 600 FT. NOT IN ICING CONDITIONS, WING ANTI/ICE OFF. THEN MESSAGE CLEARED. RAN QRH. MESSAGE DID NOT RETURN. (FLIGHT 4944 FILED CLOSED)PERFORMED OPS CHECK OF WING A/I PER CRJ700 AMM 30-12-00, OPS CHECK GOOD

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 42,402 hrs · 31,178 cycles

THE I/B SEAT TRACK AT SEATS 3C, 4C & 15C ARE DAMAGED. (FILED CLOSED)REMOVED AND REPLACED THE I/B SEAT TRACK AT SEATS 3C, 4C & 15C IN REF TO AMM 25-21-01.

Part: WINDOW — DELAMINATED (RT COCKPIT) · airframe 38,819 hrs · 28,346 cycles

RIGHT SIDE WINDOW SHOWING DELAMINATION REQUIRES REPLACEMENT. (FILED CLOSED) REMOVED FO SIDE WINDOW IN REFERENCE TO AMM 56-12-01.SEE CP 23112089-1 FOR INSTALLATION.

Part: SEAL — OUT OF POSITION (PAX DOOR) · airframe 37,636 hrs · 27,487 cycles

LOUD NOISE HAPPENED WHILE CLIMBING THROUGH FL200. NO PRESSURIZATION ISSUES IDENTIFIED. NO CAUTION NO WARNING NO STATUS MESSAGES ON EICAS ALERTING US OF AN ISSUE. CREW REPORTED THE LANDING WEIGHT WAS 65K AND VSI WAS LESS THAN 360FPM. PERFORMED INSPECTION REFERENCE AMM TASK FOUND A PORTION OF THE MCD SEAL OUT OF THE TRACK, CLEANED SEAL AND RE-INSTALLED INTO RETAINER. PRESSURIZED AC REFERENCE AMM TASK, NO DEFECTS NOTED. OK FOR CONTINUED SERVICE.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION FOUND ON STRINGER JOINT PIECE AT FS 333.00 COMMON TO STGR 23R. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STRINGER JOINT PIECE AT FS 333.00 COMMON TO STGR 23R, REF CRJ 700 SRM AND DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION FOUND ON STRINGER JOINT PIECE STGR 24R AT FS 333.00. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STRINGER JOINT PIECE STGR 24R AT FS 333.00, REF. CRJ 700 SRM AND DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

ATTACHMENT ANGLE LOCATED ON STGR 26L BETWEEN FS 349-FS 364 HAS SEVERE CORROSION ON AFT CORNER, MARKED. C-CHECK RO 12/14/2020. INSTALLED NEW ATTACHMENT ANGLE LOCATED AT STGR 26L BETWEEN FS 349-FS 364, PER CRJ 700 SRM.

Part: DOOR SILL — DAMAGED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

SEVERAL ELONGATED HOLES IN PAX DOOR FLOOR SILL STRUCTURE, MARKED. C-CHECK RO 12/14/2020. UPSIZED HOLES AND INSTALLED NEW FASTENERS, REF MHIRJ REO FOR REPAIR TO ELONGATED HOLES IN PAX DOOR FLOOR SILL STRUCTURE.

Part: SKIN — DENTED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

EXTERNAL SKIN HAS DENT LOCATED APPROXIMATELY AT FS 1015.00 TO FS 1031 BETWEEN STRINGER 23L AND STGR 24L. C-CHECK RO 12/14/2020. CUT DAMAGE OUT AND INSTALLED DOUBLER AT EXTERNAL SKIN AT FS 1015.00 TO FS 1031 BETWEEN STRINGER 23L AND STGR 24L, REF CRJ 700 SRM. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD.

Part: DIAPHRAGM — CORRODED (WASTE DOOR) · airframe 37,567 hrs · 27,436 cycles

WHILE REMOVING FRAME SECTOR AT FS 379.00 FOUND CORROSION ON WATER WASTE SERVICE DOOR LOWER DIAPHRAGM P/N SH670-32284-3. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW SERVICABLE DIAPHRAGM ON LOWER FWD WATER WASTE DOOR SURROUND STRUCTURE, REF DWG AND CRJ 700 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON BACK-UP SILL AT STGR 21L BETWEEN FS 333.00 AND FS 349.00. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW BACK-UP SILL AT STGR 21L BETWEEN FS 333.00 AND FS 349.00, REF CRJ 700 SRM DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON INTERCOSTAL AT 21L FROM FS 310.00 TO FS 333.00. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW INTERCOSTAL AT 21 L FROM FS 310.00 TO 333.00, REF CRJ 700 SRM DWG. COMPLIED WITH TASK CARD. PRESSURE CHECKS GOOD.

Part: STRINGER — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION FOUND ON STRINGER 27 BETWEEN FS 333.00 AND FS 349.00. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STRINGER 27 BETWEEN FS 333.00 AND FS 349.00, REF CRJ 700 SRM & DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON FLOOR SEAT TRACK BETWEEN FS 428.00-485.00 LBL 27, MUTIPLE AREAS MARKED. C-CHECK RO 12/14/2020. REMOVED AND REPLACED NEW SEAT TRACK AT LBL 27 BETWEEN FS 428 TO FS 485, PER CRJ 700 AMM TOOL USED TUC8834 CAL:01-JUN-20 DUE:30-JUN-21.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION FOUND ON RT LATCH PIN INTERCOSTAL LOCATED BETWEEN FS 349.00-FS 364.00 AND BETWEEN STGR 27-STGR 26R. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW RT LATCH PIN INTERCOSTAL LOCATED BETWEEN FS 349.00-FS 364.00 AND BETWEEN STGR 27-STGR 26R, REF CRJ 700 SRM DWG. COMPLIED WITH TASK CARD. PRESSURE CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

INTERCOSTAL ON STRG 20R BETWEEN FS 319.70 AND FS 349.00 IS CORRODED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW INTERCOSTAL ON STRG 20R BETWEEN FS 319.70 AND FS 349.00, REF CRJ 700 SRM DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

INTERCOSTAL ON STRG 20R BETWEEN FS 310 & FS 319.70 IS CORRODED. C-CHECK RO 12/14/2020. REPLACED INTERCOSTAL ON STRG 20R BETWEEN FS 310 & FS 319.70 PN: SH670-32047-1, IAW DWG, CRJ700 SRM, AND COMPLIED WITH SKYCARD.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION FOUND ON STRINGER JOINT PIECE FS 333.00 COMMON TO STGR 25L. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STRINGER JOINT PIECE FS 333.00 COMMON TO STGR 25L, REF CRJ 700 SRM DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON LT SIDE SEAT TRACK BETWEEN FS 364.00-485.00. C-CHECK RO 12/14/2020. INSTALLED NEW REPLACEMENT LT SIDE SEAT TRACK AT FS 378.00-FS 483.00, REF CRJ700 AMM. TOOL NR TUC7824 CAL: 01-JUN-20 DUE: 30-JUN-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON RT SIDE SEAT TRACK BETWEEN FS 485.00-572.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED RT SIDE SEAT TRACK FROM FS 483.00 TO FS 573, P/N SH670-32234-951 PER CRJ700 AMM USING CALIBRATED TOOL TUC5658 DUE: 31-JUL-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON FLOOR SEAT TRACK BETWEEN FS 349.00-428.00 LBL 27, MULTIPLE AREAS MARKED. C-CHECK RO 12/14/2020. REMOVED AND REPLACED SEAT TRACK AT LBL 27 FROM FS 349 TO FS 428, PER CRJ 700 AMM TOOLS USED TUC8834 CAL: 01-JUN-20 DUE:30-JUN-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON LT SIDE SEAT TRACK BETWEEN FS 572.00-669.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED LT SIDE SEAT TRACK FROM FS 573.00 TO FS 675.00, P/N SH670-33558-3 PER CRJ700 AMMS 53-00-49-000-801-A17 AND USING CALIBRATED TOOL TUC5658 DUE: 31-JUL-21.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON RT FLOOR SILL FS 280-FS 319.70. C-CHECK RO 12/14/2020. REMOVED CORROSION ON RT FLOOR SILL AT FS 280-FS 319.70 FOUND 100% MATERIAL LOSS CRJ700 SRM. INSTALLED NEW FLOOR SILL AT RT FS 280-319.70, REF DRW AND CRJ700 SRM. PERFORMED PRESSURE CHECK OF REPAIRED AREA, REF CRJ 700 AMM, CHECK GOOD. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON LT SIDE SEAT TRACK BETWEEN FS 485.00-572.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED LT SIDE SEAT TRACK FROM FS 483.00 TO FS 573.00, P/N SH670-32234-951 PER CRJ700 AMM USING CALIBRATED TOOL TUC5658 DUE: 31-JUL-21.

Part: BRACKET — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

FS 1031 STGR 22L CORNER BRACKET CORRODED, AS MARKED. C-CHECK RO 12/14/2020. REMOVED AND REPLACED CORNER STRINGER CLIP WITH NEW AT FS 1031.00 STR 22L, REF CRJ700 SRM & DWG, FIT CHECK GOOD. RESTORED FINISH. COMPLIED WITH SKYWEST TASK CARD.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

DRAIN MAST DOUBLER BETWEEN STGRS 27/26R AND FS 1031/1047 CORRODED, AS MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW DRAIN MAST DOUBLER BETWEEN STGRS 27/26R AND FS 1031/1047, REF CRJ 700 SRM DWG. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD.

Part: CLAMP — BROKEN (DOOR FRAME) · airframe 37,567 hrs · 27,436 cycles

SERVICE DOOR FWD FRAME FS 319.70 HAS BROKEN TEFLON CLAMP AT APPROXIMATELY STGR 15 HINGE AREA, MARKED. C-CHECK RO 12/14/2020. REPLACED BROKEN TEFLON CLAMP WITH 1 EA NEW TEFLON CLAMP, REF CRJ 700 AMM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON RT SIDE SEAT TRACK BETWEEN FS 364.00-485.00. C-CHECK RO 12/14/2020. INSTALLED NEW REPLACEMENT LT SIDE SEAT TRACK AT FS 378.00-FS 483.00, REF CRJ700 AMM. TOOL NR TUC7824 CAL: 01-JUN-20 DUE: 30-JUN-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON RT SIDE SEAT TRACK BETWEEN FS 572.00-669.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED RT SIDE SEAT TRACK FROM FS 573.00 TO FS 675.00, P/N SH670-33558-3, PER CRJ700 AMM USING CALIBRATED TOOL TUC5658 DUE: 31-JUL-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

SEAT TRACKS CORRODED RBL 9 FROM FS 349.00 THRU FS 485.00. C-CHECK RO 12/14/2020. REPLACED CORRODED SEAT TRACK RBL 9 FROM FS 349.00 THRU FS485.00, IAW CRJ 700 AMM CONFIG A03. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

SEAT TRACK CORRODED RBL 9 FROM 485.00 TO FS 581.00. C-CHECK RO 12/14/2020. INSTALLED NEWLY FABRICATED SEAT TRACK FROM RBL 9 FS 485.00 THRU FS 581.00, IAW CRJ 700 AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: FRAME — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

FRAME FS 319.00 HAS CORROSION ON THE LOWER FRAME, STGR 25L-STGR 26R, MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW FRAME SECTOR AND REPAIR SPLICE AT FS 319.00 BETWEEN STGR 23R & 25R, REF CRJ 700 SRM. TASK CARD COMPLIED WITH, CHECK GOOD.

Part: FRAME — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON FRAME FS 379.00 BETWEEN STGR 22R-24R. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW FRAME SECTOR AT FS 379.00 BETWEEN STGR 20R & 25R, REF DWG CRJ 700 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON ATTACHING ANGLE TO STGR 19L AND FRAME FS 295.00, MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED "NEW" STRINGER CLEAT LOCATED ON STGR 19L AT FS 295, AS REQUIRED REF CRJ700 SRM AND DWG. SEE CONTINUE CARD FOR DETAILS.

Part: FRAME — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

FRAME, FS 364.00, CORRODED AROUND FASTENER STGR 26, MARKED. C-CHECK RO 12/14/2020. REPAIRED FRAME AT FS 364.00, STGR 26, REF CRJ 700 SRM REPAIR POCEDURE. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

SEAT TRACK CORRODED LBL 9 FROM FS 349.00 THRU FS 485.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED NEW SEAT TRACK AT LBL 9 FROM FS 349 TO FS 485, PER CRJ 700 AMM.

Part: FRAME — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

FRAME FS 310.00 HAS CORROSION ON THE LOWER FLANGE FORWARD AND AFT WEB, STGR 25L-STGR 27, MARKED. C-CHECK RO 12/14/2020. REPAIRED FRAME FS 310.00 LOWER FLANGE FORWARD AND AFT WEB, STGR 25L-STGR 27, REF CRJ 700 SRM REPAIR PROCEDURE. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: FRAME — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

FRAME FS 295.00 HAS CORROSION ON THE LOWER FLANGE AND FORWARD WEB, STGR 25L-STGR 23R, MARKED. C-CHECK RO 12/14/2020. REPAIRED FRAME FS 295.00 LOWER FLANGE FORWARD AND AFT WEB, STGR 25L-STGR 23R, REF CRJ 700 SRM REPAIR PROCEDURE. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: STRINGER — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON STGR 21R BETWEEN FS 349.00-379.00, MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STGR 21R BETWEEN FS 349.00-379.00, REF DWG, CRJ 700 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECKS GOOD.

Part: STRINGER — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

STGR 26L HAS CORROSION AROUND FASTENERS, FS 280.00-FS 333.00, MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STGR 26L, FS 280.00-FS 333.00, REF CRJ 700 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD. PRESSURE CHECKS GOOD.

Part: STRINGER — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON STGR 23R BETWEEN FS 319.00-333.00, MARKED. C-CHECK RO 12/14/2020. STGR 23R LOCATED BETWEEN FS 280-FS 333 OUT OF LIMITS. REMOVED AND REPLACED WITH NEW AND RESTORED FINISH, REF CRJ 700 SRM AND DRAWING. TASK CARD COMPLIED WITH. CHECK GOOD SEE CONTINUE CARD FOR WORK PERFORMED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

SEAT TRACK CORRODED LBL 9 FROM 485.00 TO FS 581.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED NEW SEAT TRACK AT LBL 9 FROM FS 485 TO FS 581, PER CRJ 700 AMM.

Part: STRINGER — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

STGR 24R HAS CORROSION AROUND FASTENERS FS 333.00-FS 349.00, MARKED. C-CHECK RO 12/14/2020. REPLACED STRINGER 24R FROM FACTORY SPLICE AT FS 333 TO REPAIR SPLICE AT FS 379.00-394.00, REF CRJ700 SRM. TO INCORPORATE REMOVAL OF CORRODED STRINGER. COMPLIED WITH SKYWEST TASK CARD, LEAK CHECK GOOD.

Part: STRINGER — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON STGR 21R BETWEEN FS 319.00-333.00, MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW AT STGR 21R BETWEEN FS 319.00-333.00, REF CRJ 700 SRM DWG. COMPLIED WITH TASK CARD. PRESURE CHECK GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

SEAT TRACK CORRODED LBL 9 FROM FS 581.00 TO FS 708.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED NEW SEAT TRACK AT LBL 9 FROM FS 581 TO FS 708, PER CRJ 700 AMM. TOOLS USED TUC8834 CAL: 01-JUN-20 DUE: 30-JUN-21.

Part: STRAP — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

UNDERFLOOR CORROSION ON FUSELAGE STRAP AT FS 280.00 BETWEEN STGR 26L-25R, AREAS MARKED. C-CHECK RO 12/14/2020. REMOVED COROSION TO ACCEPTABLE LIMITS AT UNDERFLOOR FUSELAGE STRAP AT FS 280.00 BETWEEN STGR 26L-25R, REF REO AND CRJ700 SRM. VERIFIED ALL CONDITIONS OF REO WERE MET. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: STRINGER — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

STGR 26R HAS CORROSION AROUND FASTENERS FS 319.00-FS 333.00, MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STRINGER 26R BETWEEN FS 280-FS 333, REF MHIRJ REO, DWG, CRJ 700 SRM. TASK CARD COMPLIED WITH, CHECK GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

RT FLOOR SEAT RAIL CORRODED BETWEEN FS 847.00-985.00 RBL 9, MULTIPLE AREAS MARKED. C-CHECK RO 12/14/2020. REMOVED AND REPLACED CORRODED SEAT TRACK WITH NEW SEAT TRACK, REF CRJ 700 AMM AND CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS USING CALIBRATED TOOL TUC5658 DUE: 31-JUL-21.

Part: STRINGER — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON STGR 22R BETWEEN FS 319.00-349.00, MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STGR 22R BETWEEN FS 319.00-349.00, REF CRJ 700 SRM, SNIEO AND DWG. DRAWING COMPLIED WITH TASK CARD. PRESURE CHECK GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

SEAT TRACK CORRODED LBL 9 FROM FS 708.00 THRU FS 847.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED CORRODED SEAT TRACK WITH NEW SEAT TRACK, REF CRJ 700 AMM AND CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

CORROSION ON STRINGER SPLICE ON STGR 22R AT APPROXIMATELY FS 333.00, MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STRINGER SPLICE ON STGR 22R AT APPROXIMATELY FS 333.00, REF CRJ 700 SRM AND DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,567 hrs · 27,436 cycles

SEAT TRACK CORRODED RBL 9 FROM FS 581.00 TO FS 708.00. C-CHECK RO 12/14/2020. INSTALLED 2 EA NEW REPLACEMENT SEAT TRACKS AT RBL 9.00 FROM FS 581.00-FS 683.50 AND FS 683.50-FS 837.00, REF CRJ700 AMM. TOOL NR TUC7824 CAL: 01-JUN-20 DUE: 30-JUN-21.

Part: STRINGER — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

STGR 26R HAS CORROSION AROUND FASTENERS FS 333.00-FS 364.00, MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STGR 26R FS 333.00-FS 364.00, REF CRJ 700 SRM & BOMBARDIER DWG. COMPLIED WITH TASK CARD. PRESSURE CHECKS GOOD.

Part: STRINGER — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

STGR 25L HAS CORROSION AROUND FASTENERS FS 280.00-FS 333.00. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STRINGER 25L LOCATED BETWEEN FS 280-FS 333, REF DRWG, CRJ 700 SRM. TASK CARD COMPLIED WITH, CHECK GOOD.

Part: FRAME — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

FRAME AT FS 333 CORRODED BETWEEN STGRS 24L AND 25L, AS MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW FRAME AT FS 333 BETWEEN STGRS 24L AND 25L, REF CRJ 700 SRM AND DWG. COMPLIED WITH TASK CARD. PRESURE CHECK GOOD.

Part: SUPPORT — CORRODED · airframe 37,567 hrs · 27,436 cycles

LT PRESS BOX SILL CORRODED 2 PL, AS MARKED FORE AND AFT OF FS 797. C-CHECK RO 12/14/2020. REPAIRED LT PRESS BOX SILL FORE AND AFT OF FS 797 TO ACCEPTABLE LIMITS, REF REO. COMPLIED WITH TASK CARD. PRESURE CHECK GOOD.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 37,567 hrs · 27,436 cycles

LT PRESS BOX SILL FS 773 INBOARD EDGE NEXT TO FLOORBOARD CORRODED, AS MARKED. C-CHECK RO 12/14/2020. REPAIRED LT PRESS BOX SILL FS 773 INBOARD EDGE TO ACCEPTABLE LIMITS, REF REO. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,567 hrs · 27,436 cycles

INTERCOSTAL CORRODED FS 349.00-FS 364.00 BETWEEN STGR 27 & STGR 26L, MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW LT SIDE INTERCOSTAL LOCATED BETWEEN FS 349-364, REF DWG CRJ 700 AMM & CRJ 700 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

INTERCOSTAL LOWER FLANGE CORRODED FS 394.00-FS 421.00, BETWEEN STGR 27 & STGR 26R, MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW INTERCOSTAL AT FS 394.00-FS 421.00, BETWEEN STGR 27 & STGR 26R, REF CRJ 700 SRM DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: FRAME — CORRODED (ZONE 100) · airframe 37,567 hrs · 27,436 cycles

FRAME CORRODED ON THE AFT WEB & LOWER FLANGE AND FORWARD WEB FS 349.00 STGR 26L-STGR 25R, MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW LOWER FRAME SECTOR AT FS 349.00 BETWEEN STGR 24R AND STGR 23L, REF DWG CRJ 700 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: BEARING — CORRODED (PAX DOOR LATCH) · airframe 37,567 hrs · 27,436 cycles

PAX DOOR LATCH MECHANISM VARIOUS ROD END JAM NUTS, BOLTS, CASTLELLATED NUTS HAVE EVIDENCE OF RUST CORROSION, MARKED IN RED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW SERVICEABLE BEARING ROD WITH NEW SERVICEABLE HARDWARE ON PAX DOOR SPRING ROD ASSEMBLY, REF CRJ700 AMM. OPERATIONAL TEST GOOD.

Part: BOLT — CORRODED (LT SPOILER) · airframe 37,567 hrs · 27,436 cycles

LT OUTBOARD GROUND SPOILER, FWD OF GROUND SPOILER HINGE ASSEMBLY, CABLE GUIDE HARDWARE CORRODED. C-CHECK RO 12/14/2020. REMOVED CORRODED HARDWARE AT CABLE GUIDE UNDER LT OUTBOARD GROUND SPOILER, FWD OF HINGE ASSEMBLY AND INSTALLED 2 EA NEW BOLTS AND WASHERS, REF CRJ700 SRM AND CRJ700 AMM. TUC5659 CAL DUE 31-JAN-21.

Part: BEARING — CORRODED (FLAP ACT TORQ TB) · airframe 37,567 hrs · 27,436 cycles

LT INBOARD GROUND SPOILER, FLAP ACTUATOR TORGUE TUBE BEARING BETWEEN BOTH INBOARD GROUND SPOILERS, ATTACHMENT HARDWARE CORRODED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW LT INBOARD GROUND SPOILER FLAP ACTUATOR TORGUE TUBE BEARING ATTACHMENT HARDWARE, REF CRJ-700 AMM. TOOL USED: TUC8612, CAL DUE: 31-OCT-21.

Part: CLAMP — CORRODED (LT SPOILER) · airframe 37,567 hrs · 27,436 cycles

LT INBOARD GROUND SPOILER, 3 YELLOW CLAMPS HOLDING CONDUIT OF AFT AUXILIARY SPAR ATTACHMENT HARDWARE CORRODED. C-CHECK RO 12/14/2020. REMOVED AND REPLACED HARDWARE ON LT INBOARD GROUND SPOILER ON 3 EA AFT AUXILARY CONDUITS CLAPS, REF CRJ700 SRM.

Part: SUPPORT — CRACKED (WNG-BDY FAIRING) · airframe 37,567 hrs · 27,436 cycles

THE AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURES DIAPHRAGM AFT OF FS 909 AT LBL 17.63 IS CRACKED ON ITS LOWER EDGE. C-CHECK RO 12/14/2020. COMPLIED WITH ALL STEPS OF REO FOR AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE DIAPHRAGM AT FS 909 AT LBL 17.63.

Part: SUPPORT — CORRODED (WNG-BODY FAIRING) · airframe 37,567 hrs · 27,436 cycles

THE AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURES LT ANGLE AND RT ANGLE AT FS 939 HAVE MULTIPLE SPOTS OF CORROSION. C-CHECK RO 12/14/2020. REMOVED AND REPLACED WITH NEW LT & RT ANGLES ON THE AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURES AT FS 939, REF CRJ-700 SRM.

Part: SUPPORT — CORRODED (WNG-BODY FAIRING) · airframe 37,567 hrs · 27,436 cycles

THE AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURES LT FRAME AND RT FRAME AT FS 939 HAVE MULTIPLE SPOTS OF CORROSION AROUND BL 0.0. C-CHECK RO 12/14/2020. REMOVED CORROSION ON AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE LT AND RT FRAME AT FS 939, REF CRJ 700 SRM. LT FRAME (WEB) FOUND TO BE WITHIN LIMITS AND RT FRAME (WEB) FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RT AFT WING TO BODY FAIRING SUPPORT STRUCTURE FRAME (WEB) AT FS 939.00, REF CRJ-700 SRM.

Part: SUPPORT BRACKET — CORRODED (LT MLG WW) · airframe 37,567 hrs · 27,436 cycles

IN THE LT MLG BAY THE SUPPORT BRACKET THAT IS MOUNTED TO THE FS 797 AFT WING FRAME, FOR THE LT MLGS HYDRAULIC AND ELECTRICAL HARNESS, IS CORRODED ON ITS UPPER AND LOWER SURFACES, MARKED WITH ORANGE FLAG TAPE. C-CHECK RO 12/14/2020. INSTALLED NEW SUPPORT BRACKET IN MLG BAY MOUNTED AT FS 797 AFT WING FRAME, INSTALLED 6 EA NEW HI-LITE FASTENERS AND INSTALLED 1 EA BOLT FASTENING 1 EA WIRE BUNDLE CLAMP, REF CRJ700 SRM.

Part: SUPPORT BRACKET — CORRODED (RT MLG WW) · airframe 37,567 hrs · 27,436 cycles

IN THE RT MLG BAY THE SUPPORT BRACKET THAT IS MOUNTED TO THE FS 797 AFT WING FRAME, FOR THE RT MLG HYDRAULIC AND ELECTRICAL HARNESS, IS CORRODED ON ITS UPPER AND LOWER SURFACES, MARKED WITH ORANGE FLAG TAPE. C-CHECK RO 12/14/2020. INSTALLED NEW SUPPORT BRACKET IN MLG BAY MOUNTED AT FS 797 AFT WING FRAME, INSTALLED 6 EA NEW HI-LITE FASTENERS AND INSTALLED 1 EA BOLT FASTENING 1 EA WIRE BUNDLE CLAMP, REF CRJ700 SRM.

Part: SUPPORT ANGLE — CORRODED (WNG-BODY FAIRING) · airframe 37,567 hrs · 27,436 cycles

THE AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURES MID ANGLE AT FS 847 HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 12/14/2020. REMOVED AND REPLACED WITH NEW PART THE AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURES MID ANGLE AT FS 847, REF CRJ700 SRM BOMBARDIER DRAWING.

Part: SKIN — CHAFED (FUSELAGE) · airframe 37,567 hrs · 27,436 cycles

THE FUSELAGE LOWER SKIN PANEL EXTERNAL REPAIR DOUBLER/TRIPLER BETWEEN FS 969 AND FS 985 AT STRINGER 27 IS CHAFED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW REPAIR PARTS AT THE FUSELAGE LOWER SKIN PANEL BETWEEN FS 969 AND FS 985 AT STRINGER 27, REF REO AND CRJ700 SRM. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD.

Part: SUPPORT — CORRODED (WNG-BODY FAIRING) · airframe 37,567 hrs · 27,436 cycles

THE AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE'S LT AND RT STRAPS AT FS 879 HAVE MULTIPLE SPOTS OF CORROSION. C-CHECK RO 12/14/2020. INSTALLED NEW LT AND RT AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE STRAPS, REF CRJ700 SRM.

Part: SUPPORT ANGLE — CORRODED (WNG-BODY FAIRING) · airframe 37,567 hrs · 27,436 cycles

THE AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURES CENTER ANGLE AT FS 939 IS CORRODED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW CENTER ANGLE AT THE AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURES CENTER ANGLE AT FS 939.00, REF CRJ-700 SRM.

Part: PCU — LEAKING (LT AILERON) · airframe 37,567 hrs · 27,436 cycles

LT AILERON NR 1 PCU (INBOARD) HAS OUT OF LIMITS LEAK ORIGINATING FROM ROD END SEAL. C-CHECK RO 12/14/2020. REMOVED LEAKING AND INSTALLED NEW SERVICEABLE LT AILERON NR 1 PCU, REF CRJ700 AMM, CHECKS GOOD. COMPLIED WITH SKYWEST TASKCARD.

Part: SLAT TRACK — DAMAGED (RT WING) · airframe 37,567 hrs · 27,436 cycles

RT WING SLAT TRACK 3-3 HAS WEAR GROVES ON BOTTOM TRACK FACE, MARKED. C-CHECK RO 12/14/2020. REMOVED WEAR GROVES ON RT WING SLAT TRACK 3-3 BOTTOM TRACK FACE TO ACCEPTABLE LIMITS, REF REO. COMPLIED WITH TASK CARD, OPERATIONS CHECKS GOOD.

Part: SLAT TRACK — DAMAGED (LT WING) · airframe 37,567 hrs · 27,436 cycles

LT WING SLAT TRACK 1-1 HAS WEAR GROVES ON BOTTOM TRACK FACE, MARKED. C-CHECK RO 12/14/2020. REMOVED LT WING SLAT TRACK 1-1 WEAR GROVES ON BOTTOM TRACK FACE TO ACCEPTABLE LIMITS, REF REO. COMPLIED WITHTASK CARD, OPERATIONS CHECKS GOOD.

Part: SPRING — CORRODED (LT WING TE FLAP) · airframe 37,567 hrs · 27,436 cycles

LT WING OUTBOARD FLAP MOST INBOARD HINGE BOX SPRING HAS CORROSION. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW LT WING OUTBOARD FLAP MOST INBOARD HINGE BOX SPRING, REF CRJ700 AMM.

Part: SLAT TRACK — DAMAGED (LT WING) · airframe 37,567 hrs · 27,436 cycles

LT WING SLAT TRACK 3-3 HAS WEAR GROVES ON BOTTOM TRACK FACE, MARKED. C-CHECK RO 12/14/2020. REMOVED LT WING SLAT TRACK 3-3 WEAR GROVES ON BOTTOM AND TOP OF TRACK FACE TO ACCEPTABLE LIMITS, REF REO. COMPLIED WITH TASK CARD, OPERATIONS CHECKS GOOD.

Part: SLAT TRACK — DAMAGED (RT WING) · airframe 37,567 hrs · 27,436 cycles

RT WING SLAT TRACK 1-1 HAS WEAR GROVES ON BOTTOM TRACK FACE, MARKED. C-CHECK RO 12/14/2020. REMOVED RT WING SLAT TRACK 1-1 WEAR GROVES ON BOTTOM TRACK FACE TO ACCEPTABLE LIMITS, REF REO. COMPLIED WITH TASK CARD, OPERATIONS CHECKS GOOD.

Part: BOLT — CORRODED (LT SPOILERS) · airframe 37,567 hrs · 27,436 cycles

LEFT WING MULTI-FUNCTION SPOILERS HAVE CORRODED HARDWARE ON THE BONDING WIRES. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW HARDWARE AND BONDING JUMPERS ON THE LT WING INBOARD AND OUTBOARD MULTI FUNCTION SPOILERS, REF CRJ700 AMM. BONDING CHECK GOOD.

Part: BONDING WIRE — CORRODED (LT AILERON) · airframe 37,567 hrs · 27,436 cycles

LEFT AILERON BONDING WIRES, (4) EACH, HARDWARE IS CORRODED. C-CHECK RO 12/14/2020. REPLACED (2 EA) BONDING JUMPERS AND MOUNTING HARDWARE WITH (2 EA) NEW BONDING JUMPERS AND MOUNTING HARDWARE TO THE LH AILERON HINGE TAB, IN REF TO CRJ700AMM. REPLACED (2 EA) BONDING JUMPERS AND MOUNTING HARDWARE WITH (2 EA) NEW BONDING JUMPERS AND MOUNTING HARDWARE TO THE LT AILERON, IN REF TO CRJ700AMM. ELECTRICAL BONDING TEST GOOD.

Part: BONDING JUMPER — CORRODED (LT WING TE FLAP) · airframe 37,567 hrs · 27,436 cycles

LEFT OUTBOARD FLAP MIDDLE HINGE FAIRING BONDING JUMPER HARDWARE IS CORRODED, FLAGGED. C-CHECK RO 12/14/2020. REPLACED HARDWARE AND BONDING JUMPER ON LEFT OUTBOARD FLAP MIDDLE HINGE FAIRING, REF CRJ 700 AMM. BONDING CHECK GOOD.

Part: BONDING WIRE — CORRODED (RT WING SPOILER) · airframe 37,567 hrs · 27,436 cycles

RIGHT WING BOTH MULTI-FUNCTION SPOILER ACTUATOR BONDING WIRES AND HARDWARE ARE CORRODED. C-CHECK RO 12/14/2020. REMOVED AND REPLACED RT WING MULTI-FUNCTION SPOILER INBOARD AND OUTBOARD ACTUATOR BONDING WIRES AND HARDWARE, REF CRJ700 AMM. BONDING CHECK GOOD.

Part: FITTING — CORRODED (LT WING TE FLAP) · airframe 37,567 hrs · 27,436 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE BOX FORWARD MOUNT FITTING HAS CORRODED HARDWARE, FLAGGED. C-CHECK RO 12/14/2020. LEFT WING OUTBOARD FLAP OUTBOARD HINGE BOX FORWARD MOUNT FITTING HAS BEEN REPLACED, REF CRJ700 AMM.

Part: BONDING WIRE — CORRODED (LT WING SPOILERS) · airframe 37,567 hrs · 27,436 cycles

LEFT WING BOTH MULTI-FUNCTION SPOILER ACTUATOR BONDING WIRES AND HARDWARE ARE CORRODED. C-CHECK RO 12/14/2020. REPLACED (2 EA) LEFT WING MFS ACTUATOR BONDING JUMPERS WITH NEW BONDING JUMPERS (P/N: M83413/8-A005BB) AND ASSOCIATED HARDWARE, IN REF TO CRJ700AMM. ELECTRICAL BONDING TEST GOOD, IN REF TO CRJ700AMM. HUMISEAL APPLIED TO (2 EA) NEW BONDING JUMPERS, IN REF TO CRJ700AMM. CALIBRATED TOOLING USED: ELECTRICAL BONDING METER: TUC4608, CAL DUE DATE: 28-FEB-2021-TORQUE WRENCH: TUC5658, CAL DUE DATE: 31-JUL-2021.

Part: BONDING WIRE — CORRODED (LT WING SPOILER) · airframe 37,567 hrs · 27,436 cycles

RIGHT WING MULTI-FUNCTION SPOILERS HAVE CORRODED HARDWARE ON THE BONDING WIRES. C-CHECK RO 12/14/2020. REMOVED AND REPLACED RIGHT WING OUTBOARD SPOILER BONDING WIRES AND HARDWARE, REF CRJ 700 AMM NO DEFECTS NOTED.

Part: HANDLE — DAMAGED (CARGO DOOR) · airframe 37,567 hrs · 27,436 cycles

CARGO DOOR OUTER HANDLE HOUSING IS DAMAGED IN TWO PLACES, MARKED. CARGO DOOR OUTER HANDLE HOUSING DAMAGE OUT OF LIMITS. REMOVED AND INSTALLED NEW CARGO DOOR HANDLE AND HOUSING ASSEMBLY, REF CRJ 700 SRM AND DWG. TASK CARD COMPLIED WITH. SEE CONTINUE CARD FOR WORK PERFORMED, CHECKS GOOD.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 37,567 hrs · 27,436 cycles

ACCESS PANEL 598BB HAS ELONGATED AND OVERSIZE FASTENER HOLE. C-CHECK RO 12/14/2020. REPLACED ACCESS PANEL 598BB AND REPAIRED ELONGATED AND OVERSIZE FASTENER HOLE COMMON WITH WING TRAILING EDGE, REF REO AND DWG. COMPLIED WITH SKYWEST TASKCARD. SEE CONTINUATION CARD FOR DETAILS.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 37,567 hrs · 27,436 cycles

THE PASSENGER DOOR HINGE HALF (FUSELAGE SIDE) HAS SCRATCHES AND CHAFES ON ALL 27 LUG LANDS, THE AFT LUG LAND IS ALSO GOUGED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW PAX DOOR HINGE HALF FUSELAGE SIDE, REF CRJ 700 SRM & DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: ANGLE — CHAFED (PAX DOOR FRAME) · airframe 37,567 hrs · 27,436 cycles

THE PASSENGER DOOR SURROUND STRUCTURES KICKPLATE ANGLE HAS MULTIPLE SPOTS OF CORROSION AND CHAFES. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW SERVICEABLE PAX DOOR SURROUND STRUCTURE KICKPLATE, REF CRJ700 SRM AND DWG. OPERATIONAL TEST GOOD.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 37,567 hrs · 27,436 cycles

THE PASSENGER DOOR HINGE HALF (DOOR SIDE) HAS SCRATCHES AND CHAFES ON ALL 27 LUGS, EXTENDING FROM THE BASE OF THE LUG TO THE TOP, AND THE AFT LUG HAS A MIGRATED SLOTTED SPRING PIN. C-CHECK RO 12/14/2020. BLENDED THE SCRATCHES AND CHAFES ON ALL 27 LUGS, EXTENDING FROM THE BASE OF THE LUG TO THE TOP ON THE PAX DOOR HINGE HALF (DOOR SIDE), REF CRJ700 SRM. PAX DOOR HINGE HALF (DOOR SIDE) IS WITHIN LIMITS, REF CRJ700 SRM. WALL THICKNESS NEEDS TO BE .100" OR GREATER. COMPLIED WITH SKYWEST TASK CARD. REMOVED MIGRATED SLOTTED SPRING PIN ON PAX DOOR, REF CRJ700 AMM. INSTALLED NEW SLOTTED SPRING PIN ON PAX DOOR, REF CRJ700 AMM.

Part: HANDLE — CHAFED (GALLEY DOOR) · airframe 37,567 hrs · 27,436 cycles

THE GALLEY SERVICE DOORS OUTER HANDLE HOUSING IS CHAFED. C-CHECK RO 12/14/2020. INSTALLED NEW OUTER HANDLE HOUSING (P/N 133107-3) WITH NEW FASTENERS, REF DWG AND CRJ 700 SRM. COMPLIED WITH TASK CARD. PERFORMED PRESSURE CHECK OF REPAIRED AREA, REF CRJ 700 AMM, CHECK GOOD.

Part: YOKE — CHAFED (DOOR ASSIST CABL) · airframe 37,567 hrs · 27,436 cycles

THE PASSENGER DOOR POWER ASSIST MOTOR CABLES YOKE ASSEMBLY IS CHAFED. C-CHECK RO 12/14/2020. REMOVED AND REPLACED THE PAX DOOR YOKE ASSEMBLY, AS PER REF CRJ 700 AMM.

Part: STRUCTURE — DAMAGED (PAX DOOR) · airframe 37,636 hrs · 27,487 cycles

THERE IS DAMAGE TO THE PAX DOOR TOP EDGE IN PRIMER THAT NEEDS EVALUATED/REPAIRED. PLOT, MAP, AND EVALUATED DAMAGE. IF THE DAMAGE IS FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICES/PROCEDURES. C-CHECK RO 12/14/2020. REMOVED DAMAGE TO PAX DOOR FWD TOP EDGE, REF CRJ700 SRM. REMOVED/REINSTALLED THE PAX DOOR FWD TOP CORNER CAP TO FOM. COMPLIED WITH MHIRJ REO. NO NDT DEFECTS NOTED.

Part: BUSHING — CORRODED (LT AILERON) · airframe 37,567 hrs · 27,436 cycles

REMOVE & REINSTALL LT AILERON TO FOM, PER AMM. USE NEW BOLTS WHEN REINSTALLING AILERON. C/W TASK CARD. C-CHECK RO 12/14/2020. REMOVED AND RE-INSTALLED THE LT AILERON WITH NEW ATTACHING HARDWARE, REF CRJ700 AMM. COMPLIED WITH SKYWEST TASK CARD. ALL CHECKS GOOD. SEE CONTINUE CRAD FOR DETAILS OF WORK PERFORMED.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE DUCT) · airframe 35,959 hrs · 26,186 cycles

ANTI ICE DUCT WARNING MESSAGE ON APPROACH IN ORD FOLLOWED BY AN ANTI ICE DUCT CAUTION MESSAGE. RAN QRH, TRIED TURNING WING ANTI ICE BACK ON PER QRH AND SYSTEM SEEMED TO OPERATE NORMAL. (FLT#3059) CLOSED COULD NOT DUPLICATE. PERFORMED AILC SELF TEST TESTS GOOD. PERFORMED WING ANTI-ICE OPS CHECK, ALL INDICATIONS CORRECT AND LEADING EDGE TEMPS NORMAL IAW AMM.

Part: FASTENER — DEFECTIVE (NLG STEERING) · airframe 34,642 hrs · 25,057 cycles

STEERING INOP CAUTION MESSAGE IN FLIGHT. DIDN€™T REENGAGE ON GROUND. (FLT#3166) CLOSED INSTALLED NEW HARDWARE ON NWS ARM SWITCH GROUND TERMINALS -GS1247 & GS1249 IAW ESPM. NWS NOW FUNCTIONS NORMALLY IAW AMM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 24,674 cycles

PAX DOOR CENTER INTERCOSTAL DD3 FOUND CORRODED. (C-CHECK) 12/10/2018 REPLACED INTERCOSTAL IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 24,674 cycles

PAX DOOR FWD INTERCOSTAL DD7A AND ATTACH AFT CLIP FOUND CORRODED. (C-CHECK) 12/10/2018 REPLACED INTERCOSTAL AND CLIP IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 24,674 cycles

PAX DOOR FWD INTERCOSTAL DD3 FOUND CORRODED. (C-CHECK) 12/10/2018 REPLACED INTERCOSTAL IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 24,674 cycles

PAX DOOR CENTER INTERCOSTAL DD1 FOUND CORRODED. (C-CHECK) 12/10/2018 REPLACED INTERCOSTAL IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · 24,674 cycles

PAX DOOR AFT INTERCOSTAL DD7 FOUND CRACKED. (C-CHECK) 12/10/2018 REPLACED PAX DOOR AFT INTERCOSTAL DD7 IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 24,674 cycles

PASSENGER DOOR. INTERCOSTAL DD2 CORRODED. (C-CHECK) 12/10/2018 REPLACED INTERCOSTAL IAW SRM. LEAK CHECK GOOD

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 24,674 cycles

PASSENGER DOOR. INTERCOSTAL DD4 CORRODED. (C-CHECK) 12/10/2018 REPLACED INTERCOSTAL IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 24,674 cycles

PASSENGER DOOR. INTERCOSTAL DD6 CORRODED. (C-CHECK) 12/10/2018 REPLACED INTERCOSTAL IAW SRM. LEAK CHECK GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 31,139 hrs · 22,323 cycles

RT FLOOR SILL CORRODED, FS280 - FS319.370. REMOVED CORRODED RT FLOOR SILL FS280 - FS319.70 IAW SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01, AND 51-42-13-001-001-A01. PREPPED AND INSTALLED NEW FLOOR SILL IAW SRM 51-42-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND DWG SH670-32172. ALL DEFECTS CORRECTED.

Part: PANEL — CORRODED (PAX DOOR) · airframe 31,139 hrs · 22,323 cycles

PAX DOOR GUARD PLATE HAS CORROSION. REMOVED AND REPLACED GUARD PLATE PANEL P/N 601R317075-3 AND STIFFENER P/N 601R317725-1 IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, AND DRAWING 601R31707.

Part: SKIN — CORRODED (FUSELAGE) · airframe 31,139 hrs · 22,323 cycles

AVIONICS DOOR SKIN CUTOUT HAS CORROSION IN SEVERAL AREAS. REMOVED CORROSION, REPAIRED CUTOUT SKIN IAW EC/TC IS67053210097, EC/TC REO 670-53-21-242, MODSUM IS67053210097 AND REO 670-53-21-242.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 31,139 hrs · 22,323 cycles

PASSENGER DOOR AFT SIDE PANEL STIFFENER FOUND CRACKED. REMOVED AND REPLACED STIFFENER P/N 601R317745-7 IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND DRAWING 601R317745.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,139 hrs · 22,323 cycles

STR 26R SPLICE HAS CORROSION FS 295-310. REMOVED AND REPLACED SPLICE PN SH 670-31634-2 IAW SRM 53-00-03-201-001-001-A01 STEP 5A-6A.

Part: SKIN — CORRODED (PAX DOOR) · airframe 31,139 hrs · 22,323 cycles

PAX DOOR SKIN HAS CORROSION UNDER PANEL 832 AL. COMPLIED WITH EC/TC EA 43-2017-050 AND EA 43-2017-050. FOR REPAIR OF PAX DOOR SKIN.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,139 hrs · 22,323 cycles

LT SIDE SEAT RAIL FS 863-953 HAS CORROSION. COMPLIED WITH ECTC & REO 670-53-00-343 AND GENERIC REO 670-53-00-43 REV M.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,139 hrs · 22,323 cycles

LT SIDE SEAT RAIL FS 761.55-847 HAS CORROSION. COMPLIED WITH ECTC & REO 670-53-00-343 AND GENERIC REO 670-53-00-43 REV M.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,139 hrs · 22,323 cycles

RBL9 FLOOR SEAT RAIL SEGMENT FS 349-477 HAS CORROSION. COMPLIED WITH ECTC & REO 670-53-00-343 AND GENERIC REO 670-53-00-43 REV M.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 31,139 hrs · 22,323 cycles

ANTENNA DOUBLER HAS CORROSION FS 295-310 STR 27. REMOVED AND REPLACED ANTENNA DOUBLER PN SH670-32364-7 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. DRAWING SH670-32364.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 31,139 hrs · 22,323 cycles

CRAWL WAY FLOOR SUPPORT HAS CORROSION BS 280. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-00-001-A01, 51-42-21-001-001-A01, AND DRAWING SH670-34010.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,139 hrs · 22,323 cycles

RT SIDE SEAT RAIL FS 677-724.08 HAS CORROSION. COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343.AND INSTALLED PER AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,139 hrs · 22,323 cycles

LT SIDE SEAT RAIL FS 677-708 HAS CORROSION. COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343.AND INSTALLED PER AMM 53-00-49-400-801.

Part: HINGE — CORRODED (PAX DOOR) · airframe 31,139 hrs · 22,323 cycles

PAX DOOR FOLDING STEP HINGE LUG CRACKED. REMOVED AND REPLACED PAX DOOR FOLDING STEP HINGE PER SRM 51-42-06-001-001-A01.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 31,139 hrs · 22,323 cycles

CROSSBEAM PACKER CORRODED ,FS 333,LBL 9. REMOVED AND REPLACED CROSSBEAM PACKER FS 333.00 LBL 9 IAW SRM 51-42-06-00-001-A01 & 51-42-21-001-001-A01. P/N-SH670-32167-3 DRAWING SH670-32167.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,139 hrs · 22,323 cycles

RIGHT I/B INTERCOSTAL FS 333-364 CORRODED. REMOVED AND REPLACED CORRODED INTERCOSTAL FS 333-364 STR 26R IAW SRM 51-42-06-00-001-A01 & 51-42-21-001-001-A01. P/N-SH670-32075-4 DRAWING SH670-32075.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 34,325 hrs · 24,488 cycles

CROSSBEAM PACKER CORRODED AT FS 349 AND RBL 9. UPON REMOVAL OF CORRODED PACKER, FOUND CORROSION ON CROSSBEAM. REPAIRED CROSSBEAM AND PACKER PER REO 670-53-21-1415, REV A AND EC/TC REO 670-53-21-1415.

Part: RISER — CORRODED (PAX DOOR) · airframe 34,325 hrs · 24,488 cycles

PAX DOOR FWD RISER HAS CORROSION AT BOTTOM STEP ATTACH ANGLE. DETERMINED THAT RISER HAS SEVERE CORROSION AND IS OUT OF LIMITS. REMOVED AND REPLACED FWD RISER PANEL PER SRM 51-42-06-001-001-A01, 51-41-13-001-001-A01 AND DWG 601R31707 AND 601R317071. THIS IS A MAJOR REPAIR.

Part: RETAINER — BENT (CARGO DOOR SEAL) · airframe 29,060 hrs · 20,679 cycles

FWD CARGO BAY DOOR OUTER SEAL RETAINER BENT AT AFT LOWER CORNER. COMPLIED WITH EC/TC REO 670-52-35-127 01. PERMANENT REPAIR, FWD CARGO DOOR, PN- KLE670-39502-2, SN-076. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 28,976 hrs · 20,616 cycles

FWD F/A FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 28,566 hrs · 20,276 cycles

AISLE OVERHEAD EMERGENCY EXIT SIGN FOR MAIN AND SERVICE DOORS INOPERATIVE. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,566 hrs · 20,276 cycles

AISLE EMERGENCY OVERHEAD LIGHT INOPERATIVE AT ROW 1. R & R NR 1 EMERGENCY BATTERY IAW AMM 33-51-17, IPC 33-51-17, FIG 1, ITEM 6A, OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1031) · airframe 28,556 hrs · 20,269 cycles

FLOOR SUPPORT LBL 27 CORRODED BETWEEN FS 1000 -1031. FOUND CORRODED OUT OF LIMITS NO DAMAGE ALLOWED REF SRM 53-61-43-101-001-A01. NEW FLOOR SUPPORT SECTION FABRICATED IAW GREO 670-53-00-029, REV A. AND INSTALLED REF GREO 670-53-00-029. REPAIRED IAW GREO 670-53-00-029.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 28,556 hrs · 20,269 cycles

CARGO DOOR SILL CORRODED. REMOVED LOWER CARGO DOOR SILL ASSY REF SRM TASKS 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. INSTALLED NEW LOWER CARGO DOOR SILL ASSY, PN MM670-35655-003 REF DWG MM670-35085, REV L 2010/3/23 AND SRM TASK 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED & DRILLED NEW LOWER CARGO DOOR SILL, PN MM670-35655-003, REF SRM TASK 51-40-11-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 977-1051) · corrosion level 2 · airframe 28,556 hrs · 20,269 cycles

FLOOR SUPPORT LBL 9 CORRODED BETWEEN BS 1015 - 1051. FOUND OUT OF LIMITS IAW SRM 53-61-43-A01. SECTION FABRICATED IAW GREO 670-53-00-029, REV A. BEAM SECTION FABRICATED IAW GREO 670-53-00-029, REV A 2010/08/31. DURING LOCATE & DRILL OF BEAM SECTION FURTHER CORROSION FOUND OUT OF LIMITS IAW SRM 53-61-43-A01. EXTENDED REPAIR TO BS 977 TO 1035 IAW GREO 670-53-00-029, REV A. INSTALLED REPAIR IAW GREO 670-53-029, REV A.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 28,062 hrs · 19,879 cycles

12 CD LOWER EXIT SIGN HAVE 1 BULB BURNED OUT. R & R THE BULB IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 28,062 hrs · 19,879 cycles

MAIN ENTRANCE LOWER EXIT SIGN HAD ONE BULB BURNED OUT. R & R THE BULB IAW 33-51-05. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,062 hrs · 19,879 cycles

MAIN ENTRANCE EXIT SIGN BELOW FLASHLIGHT HAD ONE BULB BURNED OUT. R & R THE BULB IAW 33-51-05. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,529 hrs · 19,458 cycles

GALLEY SERVICE DOOR ENTRANCE AFT LOWER EXIT SIGN HAD ONE LIGHT BULB BURNED OUT. REPLACED THE BULB IAW GMM 3-8. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 27,529 hrs · 19,458 cycles

12 CD SIDEWALL LOWER EXIT SIGN HS 1 LIGHT BULB BURNED OUT. REPLACED THE BULB IAW GMM 3-8. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,529 hrs · 19,458 cycles

MAIN ENTRANCE LOWER EXIT SIGN HAS ONE LIGHT BULB BURNED OUT. REPLACED THE BULB IAW GMM 3-8. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 25,704 hrs · 18,012 cycles

RT FLOOR SUPPORT AT 349, CORRODED JUST AFT OF SERVICE DOOR. REPAIRED IAW REO 670-53-00-390 AND REO 670-53-00-390.

Part: STRUCTURE — GOUGED (BS 985) · airframe 25,704 hrs · 18,012 cycles

DAMAGE AT BS 985 . REPAIRED IAW EC/TC REO 670-53-61-892.

Part: CUP — CORRODED (HAND RAIL) · airframe 25,704 hrs · 18,012 cycles

PASSENGER DOOR FWD HAND RAIL SUPPORT ROD CUP CORRODED BS 31 IN DOOR SILL ANGLE. REMOVED FWD CAP ANGLE IAW SRM 51-42-06-001-001-A01, LOCATED AND DRILLED ANGLE IAW DWG SH67031-810, REV Y. INSTALLED NEW FWD CAP ANGLE IAW DWG SH670-31810, REV Y AND SRM 51-42-06-001-001-A01, 51-42-15-001-001-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,704 hrs · 18,012 cycles

BS 280 BULKHEAD WEB FOUND CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRED IAW REO 670-53-11-594 AND REO 670-53-11-594, REV A.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,704 hrs · 18,012 cycles

BS 280 BULKHEAD WEB FOUND CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRD IAW REO 670-53-11-594 & REO 670-53-11-594.

Part: CUP — CORRODED (HAND RAIL) · airframe 25,704 hrs · 18,012 cycles

PASSENGER DOOR SILL ANGLE CORRODED BY THE HAND RAIL, FWD SUPPORT ROD CUP AT FS 310. REMOVED CORROISON IAW SRM 51-21-06-001-001-A01 AND 51-42-15-001-001-A01. DAMAGE EXCEEDS ALLOWABLE LIMITS IAW SRM 53-21-23-101-001-A01. REPLACED FWD SUPPORT ROD CUP IAW DWG SH670-31810, REV Y. REMOVED FWD SUPPORT ROD CUP IAW SRM 51-42-06-001-001-A01 LOCATED AND DRILLED NEW CUP IAW DWG SH670-31810, REV Y. INSTALLED NEW FUEL SUPPORT ROD CUP IAW DWG SH670-31810, REV Y AND SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 319) · airframe 25,704 hrs · 18,012 cycles

FLOORBEAM CORRODED BS 319.7 RBL 9. REPAIRED IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001.

Part: FLOOR SUPPORT — CORRODED (BS 319-349) · airframe 25,704 hrs · 18,012 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 319.7 - 349. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-01-A01, AND DWG SH670-31985.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 25,704 hrs · 18,012 cycles

FLOORBEAM BS 280 IS CORRODED. REPAIRED IAW EC/TC REO 670-53-00-390 AND REO 670-53-00-390 REV.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK BS 379-485 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 25,702 hrs · 18,011 cycles

RT SEAT TRACK LBL 9, BS 485-581 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 469--565) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK BS 469-565 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, A03, STEPS 4.A, 1, A-C AND AMM 53-00-49-000-801-A03 .

Part: SEAT TRACK — CORRODED (BS 677-864) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK LBL 9 BS 677-864 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, A03 AND 53-00-49-400-801-A03.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1051) · airframe 25,704 hrs · 18,012 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 1031-1051. REPAIRED IAW ECTC REO 670-53-00-390 AND REO 670-53-00-390 REV.

Part: SEAT TRACK — CORRODED (BS 677-864) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK RBL 9, BS 677-864 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 25,702 hrs · 18,011 cycles

RT SEAT TRACK RBL 9 BS 349 - 485 IS CORRODED. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-21-49-101-001-A01. R & R THE SEAL TRACK IAW AMM 53-00-49-400-801-A03 AND 53-00-49-000-801-A03.

Part: SKIN — CORRODED (BS 295-310) · airframe 25,702 hrs · 18,011 cycles

CORROSION FOUND BETWEEN BS 295 - 310 STRINGER 27 AROUND BASE OF ANTENNA. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. DOUBLER AT TCAS DETERMINED OUT OF LIMITS IAW SRM 53-21-01-101-002-A01. INSTALLED NEW TCAS LOWER CHANNEL AFTER REMOVING OLD TCAS LOWER DOUBLER IAW DWG-SH670-32364, SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 830-985) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK LBL 9, BS 830-985 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, A03 STEPS 4.C., 1-4.C, 3 AND AMM 53-00-49-400-801, A03, STEPS 4.C.1-4.C. 3.

Part: FLOOR SUPPORT — CORRODED (BS 1047) · airframe 25,704 hrs · 18,012 cycles

CORROSION AROUND SCREW HOLE ON FLOOR SUPPORT BS 1047. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. NO DAMAGE ALLOWED IAW SRM 53-61-43-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 379-581) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK LBL 9, BS 379-581 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK BS 485-581 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, A03, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK BS 677-708 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 830-985) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK RBL 9 BS 830-985 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND 53-00-49-400-801-A03.

Part: INTERCOSTAL — CORRODED (BS 319) · airframe 25,702 hrs · 18,011 cycles

FOUND CORROSION AT BS 349 AND STRINGER 26R INTERCOSTAL. FOUND OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED AND REPLACED THE INTERCOSTAL IAW DWG SH670-32075, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, DWG 670-3205, AND SRM 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK AT BS 708-761 IS CORRODED. FOUND OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-865) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK BS 785-865 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-01-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A03, AND SRM 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 785-865) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK BS 785-865 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK AT BS 565-677 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-49-000-801, A03, STEPS 4 A, 1, A.C, AND AMM 53-00-49-400-801, A03, STEPS 4.A. 1, A-C.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK FS 565 - 677 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-49-000-801, A03, STEPS 4.A 1, A.C AND AMM 53-00-49-400-801, A03 STEPS 4.A.1, A-C.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 25,704 hrs · 18,012 cycles

SEAT TRACK BS 708-761.85 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801 A03.

Part: SKIN — DAMAGED (BS 280-295) · airframe 25,705 hrs · 18,013 cycles

BURNED RIVET ON STR 0 BETWEEN FS 280 & 295. INSTALLED FASTENER ON STR 0 BETWEEN FS 280 & 295 IAW SRM 51-42-06-001-001-A01, SUPP 53-00-00 AND REO 670-53-00-045, PT B 06-OCT 14. REMOVED TEMP FASTENER ON STR O BETWEEN FS 280 & 295 IAW SRM 51-42-10-001-001-A01 & SRM SUPP 53-00-00. INSTALLED PERM FASTENER ON STR O BETWEEN FS 280 & 295 IAW SRM 51-21-16-001-001-A01, SUPP 53-00-00 & REO 670-53-00-045.

Part: SKIN — DAMAGED (BS 813-830) · airframe 25,705 hrs · 18,013 cycles

BURNED RIVET ON STG 1R BETWEEN FS 813.70 & 830.40. INSTALLED PERM FASTENER ON STR 1R BETWEEN FS 813.70 & 830.40 IAW SRM 51-42-06-001-001-A01 SUPP 53-00-00 AND REO 670-53-00-045, PART B. BURNED RIVET ON STGR 1R BETWEEN FS 813.70 & 830.40. REMOVED TEMP FASTENER ON STR 1R BETWEEN FS 813.70 & 830.40 IAW SRM 51-42-10-001-001-A01 & SRM SUPP 53-00-00. INSTALLED PERM FASTENER ON STR 1R BETWEEN FS 813.70 & 830.40 IAW SRM 51-21-16-001-001-A01, SUPP 53-00-00 & REO 670-53-00-045 PART B.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,011 hrs · 17,471 cycles

LT NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-15. OPS CHECKED GOOD.

Part: KNOB — BROKEN (MEGAPHONE) · airframe 24,883 hrs · 17,375 cycles

CABIN MEGAPHONE VOLUME ADJUST KNOB IS BROKEN. INSTALLED SERVICABLE MEGAPHONE IAW AMM 25-61-14, OPS CHECKED GOOD.

Part: LIGHT — UNKNOWN (CABIN) · airframe 21,885 hrs · 15,257 cycles

NR 2 OVERHEAD EMERGENCY LIGHTS OUT. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: ANGLE — CRACKED (FUELAGE) · airframe 20,840 hrs · 14,455 cycles

ANGLE AT RBL 26 FS 280 IS CRACKED. REMOVED ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-11-001-001-A01 AND INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01.

Part: ANGLE — CRACKED (BS 280) · airframe 20,840 hrs · 14,455 cycles

ANGLE AT RBL 38.5 FS 280 IS CRACKED. REMOVED CRACKED ANGLE AND REPLACED WITH NEW SERVICEABLE ANGLE IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,840 hrs · 14,455 cycles

UPON REMOVAL OF TEE BRACKETS AT BS 280 TRANSVERSE BEAM AT LBL 9 & RBL 9, FOUND BOTH TEE BRACKETS CRACKED. LOCATED AND DRILLED FASTENER HOLES IN SERVICEABLE "T" BRACKETS AT FS 280 LBL 9 & RBL 9 FLOORBEAM T TRANSVERSE BEAM IAW SRM 31-40-11-001-001-A01. INSTALLED SERIVCEABLE TEE BRAKCETS AT FS 280 LBL 9 AND RBL 9 FLOORBEAM TO TRANSVERSE BEAM IAW SRM 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 20,840 hrs · 14,455 cycles

AVI BAY FLOORBOARD AFT OF FS 280 FWD NUTPLATE ANGLE CORRODED. REMOVED CORRODED FLOORBOARD SUPPORT ANGLE COMMON TO FS 280 & AVI BAY IAW SRM TASK 51-42-06-001-001-A01 & 51-42-21-001-01. REMOVED NEW SUPPORT ANGLE FROM STORES (PN CC670-34256-3) DRILLED & LOCATED NEW ANGLE IAW SAMPLE & SRM TASK 51-40-06-001-001-A01. INSTALLED NEW SUPPORT ANGLE AT FS 280 AVI BAY IAW SRM 51-42-21-001-001-A01 & 51-42-06-001-00-A01. SDR CLOSED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,840 hrs · 14,455 cycles

PAX DOOR SILL ANGLE HAS AREAS OF MINOR CORROSION. REMOVED FWD CAP ANGLE AND AFT CAP ANGLE FROM THE PAX DOOR SURROUND. LOCATED, DRILLED AND INSTALLED FWD CAP ANGLE AND INSTALLED AFT CAP ANGLE IAW SRM 51-42-06-001-001-A01. REMOVED KICKPLATE ANGLE FROM PAX DOOR SURROUND. LOCATED, DRILLED AND INSTALLED KICK PLATE ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 20,840 hrs · 14,455 cycles

SEAT TRACK CORRODED AT FS 349.00 RBL 9. R & R CORRODED SEAT TRACK AT FS 349.00, RBL 9 WITH NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801 (A03) AND 53-00-49-400-801 (A03).

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 20,840 hrs · 14,455 cycles

PAX DOOR LOWER FWD CORNER CORRODED UNDER CMS532-02. REMOVED PAX DOOR LOWER FWD CORNER IAW SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR LWR FWD CORNER IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,840 hrs · 14,455 cycles

FS 280 FLOORBEAM AND FWD J CHANNEL CORRODED FORM LBL 9 TO RBL 9. REMOVED FLOORBEAM J CHANNEL IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE J CHANNEL IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01.

Part: SHEAR TIE — CORRODED (PAX DOOR) · airframe 20,840 hrs · 14,455 cycles

PAX DOOR LOWER PORTION FWD & AFT FRAME CLIPS ARE CORRODED AT FS 320.00 & FS 338.963. REMOVED FWD & AFT CLIPS FROM FS 320.00 & FS 338.963 OF PAX DOOR LOWER PORTION IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR FWD & AFT CLIP AT FS 320.00 & FS 338.963 OF PAX DOOR LOWER PORTION IAW SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 20,840 hrs · 14,455 cycles

INTERCOSTAL BETWEEN FS 349.00 AND 364.00 STR 27 IS CORRODED. REMOVED INTERCOSTSAL BETWEEN FS 349 & 364 STR 27 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 20,840 hrs · 14,455 cycles

FOUR "L" BRACKETS ON SERVICE DOOR SILL CORRODED. R & R 4 "L" BRACKETS ON SERVICE DOOR SILL IAW SRM 51-42-06-001-001-A01,

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,840 hrs · 14,455 cycles

SERVICE DOOR SILL LOWER ANGLE IS CORRODED. REMOVED ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED & INSTALLED ANGLE IAW SRM 51-42-06-001-001-A01. SDR CLOSED.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 20,840 hrs · 14,455 cycles

FS 280 RT BULKHEAD WEB IS CORRODED AT FLOOR COWL, RBL 34. BLENDED AREA. REMOVED 10 PERCENT OF MATERIAL. CORROSION APPEARS TO BE 30 PERCENT DEEP. FURTHER ACTION IS REQUIRED IAW SRM 53-00-00-101-001-A01. UPON REMOVAL OF 280 TRANSVERSE BEAM (REF MWC 71016158 OP 3) FOUND LT LOWER FS 280 WEB TO BE CORRODED BEYOND LIMITS OF REO 670-53-11-052 REPAIR NR 1. (.007" MATERIAL REMOVED). LT AND RT FS 280 BULKHEAD LOWER WEBS REQUIRE REPLACEMENT. REF REO 670-53-11-052 REPAIR NR 2.

Part: SEAT TRACK — CORRODED (BS 374) · airframe 20,840 hrs · 14,455 cycles

SEAT TRACK CORRODED AT FS 374.00 LBL 9. R & R FLOOR SEAT TRACK AT FS 374.00 LBL 9 IAW AMM 53-00-49-000-801 (CONFIG A03) AND 53-00-49-400-801 (CONFIG A03).

Part: FLOOR SUPPORT — CORRODED (BS 280-319.7) · airframe 20,840 hrs · 14,455 cycles

RT SIDE FLOOR SILL FROM FS 280 TO 319.70 HAS AREAS OF CORROSION AND IS BENT AT FS 319.70. REMOVED SILL PLATE IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILL NEW SERVICEABLE PART IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE FLOOR SILL FROM FS 280.00 -FS 319.70 IAW SRM 51-42-06-001-004-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 20,840 hrs · 14,455 cycles

LT & RT FS 280 BULKHEAD WEBS ARE CORRODED AT LBL AND RBL 9. FOUND CORROSION ON LBL 9 TO BE WITHIN LIMITS IAW SRM 53-00-00-101-001-A01. PAINTED REPAIRED AREA ON LBL 9 IAW SRM 53-11-10-201-003-A01, TASK 51-21-16-001-001 PROCEDURE 3B STEP 7. FOUND CORROSION ON RBL 9 TO BE WITHIN REPAIRABLE LIMITS. WEB REQUIRES REPLACEMENT DUE TO OTHER AREA CORRODED BEYOND LIMITS.

Part: FRAME — CORRODED (BS 349) · airframe 20,840 hrs · 14,455 cycles

FS 349.00 FRAME IS CORRODED AT STR 27. REMOVED FRAME AT FS 349 & STR 27 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE FRAME IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,840 hrs · 14,455 cycles

FWD JACK FITTING SUPPORT CORRODED. REMOVED SUPPORT IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE SUPPORT IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (E/E BAY) · airframe 20,840 hrs · 14,455 cycles

AVIONICS DOOR FWD INTERCOSTAL JUST LT OF CENTER IS CORRODED. REMOVED FWD AVIONICS DOOR INTERCOSTAL ANGLE & REPLACED WITH NEW SERVICEABLE ANGLE IAW SRM 51-42-06-001-001-A01. PAINTED AREA IAW SRM 51-25-01-001-001-A01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,904 hrs · 13,748 cycles

PAX DOOR AFT DRAG BRACE ANGLE IS CRACKED (LENGTH .75"). REMOVED AND REPLACED DAMAGED DRAG ANGLE IAW SRM 51-42-06-001-001-A01.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 19,030 hrs · 13,131 cycles

PHOTOILUMMESCENT STRIP AT EMERGENCY EXIT AB MISSING. REPLACED PATH MARKING AT EMERGENCY EXIT ROW IAW AMM 33-51-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,957 hrs · 12,402 cycles

2ND FROM AFT CABIN CEILING CENTER EMERGENCY LIGHT INOPERATIVE. RELAMPED 2ND FROM AFT CABIN CEILING CENTER EMERGENCY LIGHT AS REQUIRED. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 17,854 hrs · 12,330 cycles

CABIN MEGAPHONE INOPERATIVE. REPLACED BATTERY IAW CMM 25-61-04.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,381 hrs · 11,282 cycles

GALLEY FWD AND SIDE FLOOR LEVEL EMERGENCY FLOOD LIGHTS HAVE SEVERAL INOPERATIVE BULBS. RELAMPED GALLEY FWD AND SIDE FLOOR LEVEL EMERGENCY FLOOD LIGHTS AS REQUIRED. OPS CHECK GOOD. RELAMPED GALLEY FWD AND SIDE FLOOR LEVEL EMERGENCY FLOOD LIGHTS AS REQUIRED. OPS CHECK GOOD. (CLOSED)

Part: STRINGER SPLICE — CORRODED (BS 333 S26R) · airframe 16,194 hrs · 11,154 cycles

FACTORY SPLICE AT STR 26R, STA 333 CORRODED. (OPEN)

Part: INTERCOSTAL — CORRODED (BS 349-364 S27R) · airframe 16,194 hrs · 11,154 cycles

MAIN AVIONICS COMPARTMENT BETWEEN FS 349.00 AND FS364.00, STR27 INTERCOSTAL AND STR 26R ATTACHMENT ANGLE HAS CORROSION ON ATTACHMENT FLANGE AND FACE. (OPEN)

Part: STRINGER — CORRODED (BS 333 S25R) · airframe 16,194 hrs · 11,154 cycles

STR 25R CORRODED AFT OF STA 333 FACTORY STRINGER SPLICE AND FWD OF STR 364. (OPEN)

Part: STRINGER — CORRODED (BS 333-364 S26R) · airframe 16,194 hrs · 11,154 cycles

STR 26R BETWEEN STA 333 AND STA 364 CORRODED. (OPEN)

Part: STRINGER — CORRODED (BS 280 S25R) · airframe 16,194 hrs · 11,154 cycles

STRINGER 25R JUST AFT OF FS 280 HAS CORROSION AROUND FASTENERS. INSTALLED STRINGER IAW SRM 51-42-06-001-001.

Part: STRINGER SPLICE — CORRODED · airframe 16,194 hrs · 11,154 cycles

FACTORY STRINGER SPLICE AT FS 333 CORRODED. REMOVED FACTORY STRINGER SPLICE AT FS 333 AND DRILLED SERVICEABLE STRINGER SPLICE ALL WORK DONE IAW SRM 51-42-06-001-001-A01. INSTALLED STRINGER SPLICE IAW SRM 51-42-06-001-001-A01. FILLET SEALED IAW SRM 51-223-00-001-001 AND PAINTED IAW SRM 51-25-06-001-001. APPLIED CORROSION INHIBITOR IAW SRM 51-21-11-001-001.

Part: BEAM — CORRODED · airframe 16,194 hrs · 11,154 cycles

BEAM HAS CORROSION IN SEVERAL AREAS. INSTALLED CTR SPLICE, SEALED, CLEANED & PAINTED. ALL WORK DONE IAW SRM 54-42-06-001-001-A01 AND 51-42-21.

Part: STIFFENER — CRACKED (BS 280) · airframe 16,194 hrs · 11,154 cycles

FS 280 VERT STIFFENER AT RBL 26 CRACKED. INSTALLED NEW SIFFENER ANGLE AND CLIPPER SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-13-001-001-A01.

Part: POST — CORRODED (BS 280) · airframe 16,194 hrs · 11,154 cycles

COCKPIT DOOR POST LT & RT SIDE AT FS 280 CROSSBEAM CORRODED. REPAIRED IAW REO 670-53-11-536.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 16,194 hrs · 11,154 cycles

COCKPIT DOOR POST LT & RT SIDE AT FS 280 CROSSBEAM CORRODED. BLENDED CORROSION ON CABIN FLOOR SILL PLATE ON RT SIDE JUST AFT OF F/S 280 IAW SRM 57-21-06-001-001-A01. PERFORMED UT THICKNESS INSP OF BLEND AREAS ON CABIN FLOOR SILL IAW MAC NDT INSP PROCEDURE UT-3, MINIMUM MATERIAL REMAINING IS LOCATION NR1 .038", LOCATION NR2 .048". LOCATION NR 1 FOUND TO BE OUT OF LIMITS AND LOCATION NR 2 FOUND TO BE WITHIN LIMITS IAW SRM 53-21-43-101-001-A01. COMPLIED WITH STEPS 1,2,4-8 IAW REO 670-53-21-135. COMPLY WITH STEPS 3,9-15 IAW REO 670-53-21-135. COMPLIED WITH STEP 3 OF REO 670-53-21-139 NO INDICATIONS NOTED.

Part: STRINGER — CORRODED (BS 280 S25R) · airframe 16,194 hrs · 11,154 cycles

STR 25R FS 280 HAS CORROSION AROUND FASTENERS KC161770. REMOVED STRINGER AND DRILLED UP NEW STRINGER IAW SRM 51-40-11-001-001.

Part: STRINGER — CORRODED (BS 280 S26R) · airframe 16,194 hrs · 11,154 cycles

STRINGER 26R, JUST AFT OF FS 280 HAS CORROSION AROUND FASTENERS. DRILLED NEW STRINGER AND FABRICATED SPLICE PIECES DRILLED ALL PARTS TO SIZE ALODINED & PRIMED PARTS REF SRM 53-00-03-991-803. INSTALLED SPLICE REPAIR & SEALED SPLICE, & APPLIED CIC OUTER SKIN ALODINED PRIMED & PAINTED AREA IAW SRM 53-00-03-201-001-A01 & 51-25-01-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,194 hrs · 11,154 cycles

LIGHT CORROSION LT SIDE SIDESEAT RAIL ROW 12 TO 17. R & R WITH SERVICEABLE SEAT TRACK IAW AMM TASK 53-00-49-400-801 AND TASK 53-00-49-000-801. INSTALL SCREWS RETAINED BY NUTS AND WASHERS IAWTASK 53-00-49-400-801. INSTALLED SCREWS WASHERS AND NUTS AS REQUIRED IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 16,194 hrs · 11,154 cycles

SEAT TRACK 9R AT FS 485 TO FS581 SEVERELY CORRODED. SEAT TRACK 9A AT FS 485 TO 581 REMOVED IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 16,194 hrs · 11,154 cycles

SEAT TRACK 9R AT FS 677 TO FS 830 SEVERLY CORRODED. R & R SEAT TRACK AT FS 677 TO FS 830.40 IAW AMM TASK 53-00-49-000-801 AND TASK 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 16,194 hrs · 11,154 cycles

SEAT TRACK 9R AT FS581 TO FS677 SEVERLY CORRODED. R & R SEAT TRACK 9R AT FS 581 TO FS 677 IAW AMM 53-00-49-000/(400)-801.

Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 16,194 hrs · 11,154 cycles

SEAT TRACK 9R AT FS364 TO FS 485 CORRODED OUT OF LIMITS AND NEEDS TO BE REPLACED. SEAT TRACK 9R REMOVED IAW AMM 53-00-49-000-80. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 589-677) · airframe 16,194 hrs · 11,154 cycles

SEAT TRACK 9L AT FS269 AND FS613 AND FS 645 4EA MINOR CORROSION SPOTS. R & R SEAT TRACK 9L AT FS 589 TO FS 677 IAW AMM TASK 53-00-49-000-801 AND TASK 53-00-49-400-801.

Part: SKIN — CORRODED (BS 280 S24-26R) · airframe 16,194 hrs · 11,154 cycles

SKIN SPLICE AT FS 280 BETWEEN STR26R-24R HAS CORROSION. REMOVED FASTENERS AND BLENDED CORROSION IAW SRM CH51-21-06-001-001. PERFORMED UT THICKNESS INSP OF BLEND AREAS ON BUTTSTRAP AT FS 280.00 IAW MAC NDT INSP PROCEDURE UT-3 MINIMUM MATERIAL REMAINING IS .078 " BETWEEN STR27-26R, .077" BETWEEN SRT26R-25R AND .077" BETWEEN DAMAGE SUBMITTED TO FOR REPAIR. AWAITING RESPONSE, RECEIVED REO 670-53-21-589 STEP 1, COMPLIED WITH STEP 2 OF REO 670-53-21-589. NO INDICATIONS NOTED AT THIS TIME. INSTALLED RIVETS IAW SRM 51-42-06-001-001-A01 C/W STEPS 3&4 OF REO 670-53-21-589.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,194 hrs · 11,154 cycles

LIGHT CORROSION RT SIDE SEAT RAIL ROW 12 TO 15. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801. RECEIVED EC/TC REO 670-53-00-074, SEAT TRACK IS COMPLETED IAW REO 670-53-00-074 REV A. SEAT RAIL NEEDS TO BE INSTALLED. INSTALLED SEAT RAIL IAW AMM 53-00-49-400-801. MISSING 4 SCREWS, REQUIRING INSTALLATION. COMPLETED INSTALLATION IAW AMM 53-00-49-400-801. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 16,194 hrs · 11,154 cycles

SEAT TRACK 9L AT FS 364 TO FS 485 CORRODED OUT OF LIMITS. R & R SEAT TRACK 9L AT FS 364 TO FS 485 IAW AMM TASK 53-00-49-000-801 AND TASK 53-00-49-400-801.

Part: FRAME — CRACKED (FUSELAGE) · airframe 16,194 hrs · 11,154 cycles

LEFT AFT BELLY FAIRING 195DL AFT FRAME IS CRACKED AND HAS CHAFING DAMAGE. R & R C-CHANNEL FOR LT AFT BELLY FAIRING 195DL IAW SRM 51-41-02-001-001-A01 (PN CC670-39171-1) COMPLY WITH MODSUM IS670538200021. COMPLIED WITH EC/TC MOD SUM IS670538200021 AND MET ALL THE REQUIREMENTS OF MODSUM IS670538200021 REV B. REFER TO M-212 FOR INSTALLATION.

Part: POST — CORRODED (COCKPIT DOOR) · airframe 16,194 hrs · 11,154 cycles

COCKPIT DOOR POST LT AND RT SIDE AT FS 280 CROSSBEAM HAS CORROSION. REMOVED TEO CLIPS AND BLENDED CORROSION ON COCKPIT DOOR POST LT AND RT AT FS 280 CROSSBEAM IAW SRM 51-21-06-001-001-A01, 51-42-06-001001-A01. CUT AWAY CORRODED SECTION OF DOOR POST AS SHOWN IN THE FIG SHEETS 2 OF REO 670-53-11-536 BOTH LT & RT SIDES. COMPLIED WITH STEP 2 OF REO 670-53-11-536. PERFORMED EDDY CURRENT INSP IAW NDTM 51-20-006-250-A01. NO FURTHER DAMAGE NOTED. APPLIED CONVERSION COATING & PRIMER IAW REO 670-53-11-536. REPAIR PARTS NEED INSTALLED.

Part: WEB — CORRODED (BS 280) · airframe 16,194 hrs · 11,154 cycles

LT WEB AT FS 280 HAS CORROSION. BLENDED CORROSION ON LT WEB AT FS 280 IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREAS ON LT BULKHEAD WEB AT FS 280.00 IAW MAC NDT INSP PROCEDURE UT-3 MINIMUM MATERIAL REMAINING IS LOCATION NR1.038", LOCATION NR2.038". PERFORMED LPI, TYPE 1, METHOD C ON BLEND AREAS ON LT BULKHEAD WEB AT FS 280.00 IAW MAC NDT INSP PROCEDURE PT-1 NO INDICATIONS NOTED AT THIS TIME. BLENDED AREAS FOUND TO BE WITHIN LIMITS IAW SRM 53-11-10-201-003-A01 FIG 53-11-10-991-804. SURFACE FINISH RESTORED. TREATED, PRIMED & PAINTED BLEND AREAS IAW SRM 51-25-06 & 51-25-16.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,194 hrs · 11,154 cycles

BS 280 FLOORBEAM HAS CORROSION SEVERAL AREAS. REMOVED FS280 FLOORBEAM IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01, 51-42-21-001-001-A01. DRILLED NEW SERVICEABLE FS 280 FLOORBEAM IAW SRM 51-40-11-001-001-A01. TRANSFERED HOLES FROM NEW 280 BEAM INTO NEW DOUBLERS IS670531100026-1,-2,-3,-4 IAW SRM 51-40-11-001-001-A01. COUNTERSINKED AND DEBURRED FS 280 FLOORBEAM AND DOUBLERS IAW SRM 51-40-11-001-001-A01. SHOT IN RIVETS ON RT SIDE 280, MINUS 3 RIVETS IAW SRM 51-42-06-001-001-A01. INSTALLED 3 EACH RIVETS IN 280 BEAM IAW SRM 51-42-06-001-001-A01.

Part: LENS — CRACKED (CABIN) · airframe 16,194 hrs · 11,154 cycles

LEFT FUSELAGE EMERGENCY LIGHT JUST AFT OF EMERGENCY EXIT IS CRACKED. R & R LT FUSELAGE EMERGENCY LIGHT LENS AS REQUIRED IAW AMM 33-51-15-400-801 & 33-51-15-000-801-A01.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 16,194 hrs · 11,154 cycles

AVIONICS BAY FWD FLOOR SUPPORT AT FS 280 HAS CORROSION. REMOVED FLOOR SUPPORT, PICKED UP EXISTING FASTENER HOLES ON NEW SUPPORT DRILLED TO FINAL SIZE AND DEBURRED IAW SRM 51-40-11. READY TO INSTALL NEW SUPPORT. INSTALLED SERVICABLE FLOOR SUPPORT REF SRM 51-42-06-001-001-A01.

Part: WEB — CORRODED (BS 280) · airframe 16,194 hrs · 11,154 cycles

RT WEB AT FS 280 HAS CORROSION. BLENDED CORROSION ON RT WEB AT FS 280 IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSP OF BLEND AREAS ON RT BULKHEAD WEB AT FS 280.00 IAW MAC NDT INSP PROCEDURES. PERFORMED LPI TYPE 1, METHOD C ON BLEND AREAS ON RT BULKHEAD WEB AT FS 280.00 IAW MAC NDT INSP PROCEDURE PT-1. NO INDICATIONS NOTED AT THIS TIME. BLEND AREAS FOUND TO BE WITHIN LIMITS IAW SRM 53-11-10-201-003-A01 FIG 53-11-10-991-804. TREATED, PRIMED & PAINTED BLEND AREAS IAW SRM 51-25-06-& 51-25-16.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 16,194 hrs · 11,154 cycles

FWD FLOOR SUPPORT AT 280 HAS CORROSION. REMOVED FWD FLOOR SUPPORT AT 280 DRILLED NEW ANGLE & INSTALLED CAM LOCK RECEPTICALS AS NEEDED IAW SRM 51-40-11-001-001 & 51-44-06-001-001. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: PLACARD — MISSING (CABIN) · airframe 14,444 hrs · 9,852 cycles

REPLACED MISSING OPEN PLACARD IAW AMM 11-30-01. (CLOSED)

Part: PLACARD — MISSING (PAX DOORWAY) · airframe 14,444 hrs · 9,852 cycles

"OPEN" PLACARD MISSING FROM INSIDE PASSENGER DOOR.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 13,360 hrs · 9,014 cycles

RIGHT NR 2 EXTERIOR EMERGENCY INOP.

Part: LIGHT — DAMAGED (CABIN) · airframe 13,184 hrs · 8,888 cycles

EMERGENCY FLOOR LIGHT SECTION DAMAGED ON RT SIDE JUST FWD OF LAV.

Part: DOOR — BINDING (PAX DOOR) · airframe 11,592 hrs · 7,679 cycles

F/A REPORTS MAIN CABIN DOOR IS DIFFICULT TO OPEN FROM INSIDE. FLT 5245 DEL 43 MINS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 11,324 hrs · 7,478 cycles

RT SIDE OVERWING EXTERIOR EXIT EMERGENCY LIGHT IS INOP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 11,313 hrs · 7,471 cycles

RT SIDE OVERWING EXTERIOR EXIT EMERGENCY LIGHT IS INOP.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 11,299 hrs · 7,460 cycles

PAX DOOR 318 INTERCOSTAL CRACKED. REMOVED CRACKED 318 INTERCOASTAL AND REPLACED WITH NEW 318 INTERCOASTAL IAW CRJ700 SRM 52-11-06 AND SRM 51-42-06.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 11,299 hrs · 7,460 cycles

FUSELAGE STA 280 FWD FLOOR SUPPORT HAS CORROSION. REINSTALLED DRIP TRAY PER FROM M-234 NR - 0125 PAGE 3. REMOVED 280 FWD FLOOR SUPPORT ANGLE PER SRM 51-42-06. LOCATED FASTENER HOLES ON 280 FWD FLOOR ANGLE PN CC670-33292-13 PER CRJ 700 SRM 51-40-11. INSTALLED NEW ANGLE ON 280 FWD IAW SRM 51-42-06 / PN CC670-33292-13. INSTALLED DRIP TRAY ON RT SIDE OF FS 280 IAW SRM 51-42-21-/51-42-13. APPLIED SEALANT & CIC TO FWD ANGLE OF 280. JOB COMPLETE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 11,299 hrs · 7,460 cycles

LBL 9 OF TRANSVERSE BEAM 280 CORRODED ON T/E. REMOVED CORROSION ON FS 280 AT TRANSVERSE BEAM LBL 9 PER CRJ 700 SRM 51-21-06 SUBMIT TO BOMBARDIER FOR DISPOSITION OF REPAIR.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 11,299 hrs · 7,460 cycles

LEFT SIDE VERTICAL STABILIZER HAS A CRACK IN THE FORWARD DRAG ANGLE AS MARKED. PERFORMED EDDY CURRENT INSPECTION ON DRAG ANGLE. END OF CRACK MARKED. CUT AWAY DAMAGE PER REO 670-55-31-018. PERFORMED ET INSPECTION OF CUT LINE. NO DEFECTS NOTED. REPAIRED PER REO 670-55-31-018. PRIMED & PAINTED.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 11,299 hrs · 7,460 cycles

RIGHT SIDE VERTICAL STABILIZER HAS A CRACK IN THE FORWARD DRAG ANGLE AS MARKED. REMOVED EXISTING FASTENERS FROM REPAIR AREA AND CUT AWAY DAMAGE. PERFORMED ET INSPECTION. NO DEFECTS NOTED. FABRICATED FILLERS IAW REO 670-55-31-018. FINAL TRIMMED DOUBLER, PER REO 670-55-31-018. FABRICATED DOUBLER. OK TO INSTALL. INSTALLED DOUBLER AND FILLER PER REO 670-55-31-018. RESTORED AREA FINISH.

Part: DRAG ANGLE — CRACKED (SERVICE DOOR) · airframe 11,299 hrs · 7,460 cycles

ASD AFT DRAG ANGLE IS CRACKED IN THE RADIUS WHERE MARKED. REPAIRED DRAG ANGLE IAW REO 670-52-11-072. PERFORMED ET INSPECTION OF CUT LINES PER REO IAW NDTM 51-20-006. NO DEFECTS NOTED. FABRICATE REPAIR ITEMS. SEAL AND WET INSTALL FASTENERS. INSTALL BLIND FASTENERS. APPLY TOPCOAT. INSTALL SOLID FASTENERS. FILLET SEAL AND INSTALL PLT FASTENERS. COMPLIED WITH STEPS 1-12 ON SHEET TO REO 670-52-11-072. ALL WORK IAW REO 670-52-11-072.

Part: BATTERY — DISCHARGED (MEGAPHONE) · airframe 11,036 hrs · 7,267 cycles

MEGAPHONE INOP. R&R MEGAPHONE BATTERY. OPS CHECK GOOD. IAW CRJ 700 AMM 25-61-14. A/C OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,585 hrs · 6,929 cycles

ENTRYWAY/GALLEY EMERGENCY LIGHTS HAVE SEVERAL INOP BULBS. RELAMPED ENTRYWAY/GALLEY EMERGENCY LIGHTS IAW AMM 33-51-00. (B)

Part: LIGHT — INOPERATIVE (EXTERNAL) · airframe 9,501 hrs · 6,156 cycles

LT AFT MOST EXTERNAL EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,501 hrs · 6,156 cycles

3RD FROM FORWARD CEILING EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,388 hrs · 6,078 cycles

ALL FORWARD EMERGENCY LIGHTS INOP.

Part: WARNING MESSAGE — ILLUMINATED (FIRE BOTTLE) · airframe 7,984 hrs · 5,101 cycles

NR 1 AND 2 ENG FIRE BOTTLE LOW CAUTION MSGS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,724 hrs · 4,924 cycles

CEILING EMERGENCY LIGHT 2ND FROM AFT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,724 hrs · 4,924 cycles

CEILING EMERGENCY LIGHT 2ND FROM INOP.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,421 hrs · 4,723 cycles

CORROSION FOUND ON RIGHT 280 FLOOR SILL RBL 45.

Part: WEB — CORRODED (FUSELAGE) · airframe 7,421 hrs · 4,723 cycles

LEFT STA 280 WEB CORRODED OUT OF LIMITS.

Part: WEB — CORRODED (FUSELAGE) · airframe 7,421 hrs · 4,723 cycles

RIGHT STA 280 WEB CORRODED OUT OF LIMITS.

Part: BEAM — CORRODED (FUSELAGE) · airframe 7,421 hrs · 4,723 cycles

STA 280 BEAM CORRODED OUT OF LIMITS. REMOVED AND REPLACED STA 280 BEAM IAW REO 670-53-11-052. SUPPLEMENTAL - SDR CLOSED 04/27/07.

Part: LIGHT — INOPERATIVE (ROW 12) · airframe 5,864 hrs · 3,747 cycles

ROW 12 EMERGENCY ROW A, B SIDEWALL LIGHT INOP.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 5,381 hrs · 3,441 cycles

ARRIVED AT AIRCRAFT TO DISCOVER THAT THE OUTSIDE HANDLE TO THE MAIN PASSENGER DOOR WAS BROKEN OFF.

Part: PLACARD — WORN (DOOR) · airframe 4,685 hrs · 3,017 cycles

ASD EXIT AND OPEN PLACARD WORN.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A HANGAR INSPECTION IN BTR, THE AFT AND FORWARD CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE AFT AND FORWARD CEILING EMERGENCY LIGHT ASSEMBLIES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

DURING AN A-CHECK IN BTR, THE THIRD FROM THE FRONT EMERGENCY CEILING LIGHT AS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR TO THE THIRD FROM THE FRONT EMERGENCY CEILING LIGHT DISCONNECTED AND RECONNECTED IT TO THE LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)