N720EV

Part: LUG — DAMAGED (ZONE 500) · airframe 42,665 hrs · 31,418 cycles

L/H I/B FLAP- I/B WING LUG FITTING- CENTER INBOARD LUG IS DAMAGED (ROLLED METAL) (C-CHECK RO 10/28/2024) (FILED OPEN)EVALUATED AND REPAIRED DAMAGE ON LH INBD FLAP-INBD WING LUG FITTING-CENTER INBD LUG IAW CRJ700 SRM 57-21-27, 51-12-00. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S090924-2, P.O# 173559, DATE OF INSPECTION 09SEP2024. SEE REPORT FOR DETAILS. FOUND TO BE STRUCTURALLY ACCEPTABLE IAW REO 670-57-21-993 REV-- DATE 2024-09-09. ROTO PEENED REWORKED AREA IAW REO 670-57-21-993 REV-- DATE 2024-09-09. APPLIED ALODINE PRIMER AND TOPCOAT IAW REO 670-57-21-993 REV-- DATE 2024-09-09. TOOLS USED ROTO PEEN KIT TOOL ID FSA0045 CAL. DUE:JAN.2025 DIGITAL CALIPER TOOL ID: AV-7806 CAL. DUE: AUG.2025 DEPTH GAUGE TOOL ID: AJ-1511 CAL. DUE: FEB.2025

Part: FITTING — DAMAGED (ZONE 600 FLAP) · airframe 42,733 hrs · 31,466 cycles

R/H I/B FLAP- IB WING LUG FITTING- CENTER OUTBOARD FITTING IS DAMAGED (ROLLED OVER METAL ON EDGE) (C-CHECK RO 10/28/2024) (FILED CLOSED)PERFORMED REPAIR ON R/H IB FLAP IB WING LUG FITTING CENTER OB FITTING PER MHIRJ REO 670-57-21-992. REV.--. DATE: 2024-09-16 AND CRJ-700 SRM 57-21-27, 51-12-00. NDT PERFORMED BY BARON NDT,LLC FAA CRS# 5NDR545D. REPORT # S091624-2. P.O. NUMBER: 173559. DATE OF INSPECTION: 16-SEP-2024. TOOL USE: DEPTH GAUGE AV-7277. CAL DUE: AUG-2025FLAPPER PEEN FSA0045-A CAL DUE: JAN 2025

Part: FITTING — DAMAGED (ZONE 500 FLAP) · airframe 42,733 hrs · 31,466 cycles

L/H I/B FLAP- I/B WING LUG FITTING- CENTER OUTBOARD LUG IS DAMAGED-(ROLLED METAL) (C-CHECK RO 10/28/2024) (FILED CLOSED)REPAIRED DAMAGE ON LH IB FLAP, IB WING LUG FITTING, CENTER OTBD LUG IAW CRJ700 SRM 51-21-27, SRM 51-12-00, AND REO 670-57-21-993 REV-- DATE 2024-09-09. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S090924-1, P.O. # 173559 DATE OF INSPECTION 09SEP2024, SEE REPORT FOR DETAILS. CAL TOOLS-ROTOPEEN KIT-FSA0045 DUE-JAN2025, DIGITAL CALIPER-AV-7806 DUE-AUG2025, DEPTH GAUGE- AJ-1511 DUE-FEB2025

Part: FITTING — DAMAGED (ZONE 500 FLAP) · airframe 42,733 hrs · 31,466 cycles

L/H I/B FLAP- I/B WING LUG FITTING- CENTER INBOARD LUG IS DAMAGED (ROLLED METAL) (C-CHECK RO 10/28/2024) (FILED CLOSED)EVALUATED AND REPAIRED DAMAGE ON LH INBD FLAP-INBD WING LUG FITTING-CENTER INBD LUG IAW CRJ700 SRM 57-21-27, 51-12-00. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S090924-2, P.O# 173559, DATE OF INSPECTION 09SEP2024. SEE REPORT FOR DETAILS. FOUND TO BE STRUCTURALLY ACCEPTABLE IAW REO 670-57-21-993 REV-- DATE 2024-09-09. ROTO PEENED REWORKED AREA IAW REO 670-57-21-993 REV-- DATE 2024-09-09. APPLIED ALODINE PRIMER AND TOPCOAT IAW REO 670-57-21-993 REV-- DATE 2024-09-09. TOOLS USED ROTO PEEN KIT TOOL ID FSA0045 CAL. DUE:JAN.2025 DIGITAL CALIPER TOOL ID: AV-7806 CAL. DUE: AUG.2025 DEPTH GAUGE TOOL ID: AJ-1511 CAL. DUE: FEB.2025

Part: LUG — DAMAGED (ZONE 600) · airframe 42,665 hrs · 31,418 cycles

R/H I/B FLAP- IB WING LUG FITTING- CENTER OUTBOARD FITTING IS DAMAGED (ROLLED OVER METAL ON EDGE) (C-CHECK RO 10/28/2024) (FILED OPEN)PERFORMED REPAIR ON R/H IB FLAP IB WING LUG FITTING CENTER OB FITTING PER MHIRJ REO 670-57-21-992. REV.--. DATE: 2024-09-16 AND CRJ-700 SRM 57-21-27, 51-12-00. NDT PERFORMED BY BARON NDT,LLC FAA CRS# 5NDR545D. REPORT # S091624-2. P.O. NUMBER: 173559. DATE OF INSPECTION: 16-SEP-2024. TOOL USE: DEPTH GAUGE AV-7277. CAL DUE: AUG-2025FLAPPER PEEN FSA0045-A CAL DUE: JAN 2025

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 42,665 hrs · 31,418 cycles

RH PRESSURE SILL AT FS773.50 HAS SIGNS OF CORROSION ON THE FLOOR ANGLE (C-CHECK RO 10/28/2024) (FILED OPEN)REMOVED CORROSION AND EVALUATED AREA ON RH PRESSURE SILL AT FS773.50 THE FLOOR ANGLE, NOMINAL THICKNEES 0.125", MATERIAL REMAINING 0.124", FOUND WITHIN LIMITS IAW REO 670-53-41-683 REV-- DATE: 2024-09-06, CRJ700 SRM 53-41-44, 51-42-21, AMM 25-82-05, 25-26-02, 21-31-00, NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S082624-3 PO#173559 DATE INSPECTION:26-AUG-2024, SEE REPORT FOR DETAILS.AND IAW CRJ 700 SRM 51-21-06

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 42,733 hrs · 31,466 cycles

RH PRESSURE SILL AT FS773.50 HAS SIGNS OF CORROSION ON THE FLOOR ANGLE (C-CHECK RO 10/28/2024) (FILED CLOSED)REMOVED CORROSION AND EVALUATED AREA ON RH PRESSURE SILL AT FS773.50 THE FLOOR ANGLE, NOMINAL THICKNEES 0.125", MATERIAL REMAINING 0.124", FOUND WITHIN LIMITS IAW REO 670-53-41-683 REV-- DATE: 2024-09-06, CRJ700 SRM 53-41-44, 51-42-21, AMM 25-82-05, 25-26-02, 21-31-00, NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S082624-3 PO#173559 DATE INSPECTION:26-AUG-2024, SEE REPORT FOR DETAILS.AND IAW CRJ 700 SRM 51-21-06

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 42,665 hrs · 31,418 cycles

RIGHT HAND FORWARD DRAG ANGLE AT THE BOTTOM OF THE VERTICAL STABILIZER RH SIDE IS CRACKED (C-CHECK RO 10/28/2024) (FILED OPEN)PERFORMED REPAIR ON RIGHT HAND FORWARD DRAG ANGLE AT THE BOTTOM OF VERTICAL STABILIZER RH SIDE PER BOMBARDIER REO 670-55-31-018. REV.-A. DATE: 2016-11-10. MHIRJ REO 670-55-31-178. REV. --. DATE: 2024-08-22. CRJ-700 SRM 51-26-01. SRM 51-21-11, SRM 51-25-06, SRM 51-25-16. NDT PERFORMED BY BARON NDT,LLC FAA CRS# 5NDR545D. REPORT # S082924-5. P.O. NUMBER: 173559. DATE OF INSPECTION: 04-SEP-2024. TOOL USE: DIGITAL COUTING SCALE AV-4800. CAL DUE: DEC-2024.

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 42,733 hrs · 31,466 cycles

RIGHT HAND FORWARD DRAG ANGLE AT THE BOTTOM OF THE VERTICAL STABILIZER RH SIDE IS CRACKED (C-CHECK RO 10/28/2024) (FILED CLOSED)PERFORMED REPAIR ON RIGHT HAND FORWARD DRAG ANGLE AT THE BOTTOM OF VERTICAL STABILIZER RH SIDE PER BOMBARDIER REO 670-55-31-018. REV.-A. DATE: 2016-11-10. MHIRJ REO 670-55-31-178. REV. --. DATE: 2024-08-22. CRJ-700 SRM 51-26-01. SRM 51-21-11, SRM 51-25-06, SRM 51-25-16. NDT PERFORMED BY BARON NDT,LLC FAA CRS# 5NDR545D. REPORT # S082924-5. P.O. NUMBER: 173559. DATE OF INSPECTION: 04-SEP-2024. TOOL USE: DIGITAL COUTING SCALE AV-4800. CAL DUE: DEC-2024.

Part: NONE — CRACKED · airframe 38,756 hrs · 28,059 cycles

FO SIDE OUTER WINDSHIELD CRACKED AT CRUISE. (FLIGHT 3130 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24684700 WITH THE FOLLOWING CORRECTIVE ACTION: "REPLACED FO 'S WINDSHIELD IN REFERENCE TO CRJ700 AMM 56-11-01 AND COMPLIED WITH TASK CARD 56-220-1000-SKY."

Part: NONE — CRACKED · airframe 37,916 hrs · 27,419 cycles

R WINDOW HEAT CAUTION MESSAGE. FOLLOWED QRH. ABOUT 10 MINUTES LATER THE RIGHT WINDOW HAD A CRACK IN IT. FOLLOWED THE QRH FOR CRACKED WINDOW. (FLIGHT 3074 - FILED CLOSED) REMOVED AND REPLACED RH SIDE WINDOW WITH SERVICEABLE UNIT PER AMM 56-11-01 AND SKYWEST TASK CARD NO 56-220-1000-SKY. PERFORMED LEAK CHECK PER AMM 56-11-01 AND OPS CHECK OF WINDOW TEMPERATURE CONTROLLER PER AMM 30-41-06. BOTH CHECKS GOOD AT THIS TIME. AIRCRAFT OK FOR RETURN TO SERVICE.

Part: BUSS BAR — FAILED (CBP2) · airframe 37,209 hrs · 26,902 cycles

CLIMBING, GOING TO 12,000 FT, RECEIVED A DUAL HYD SYS FAILURE OF SYSTEMS 1 & 3. PRESS ON BOTH SYS WAS 0, BOTH BRAKE READINGS WERE AT 0, FLUID QTY ON TAXI CHECK WAS 80/70/75 ON ALL 3 SYSTEMS. HYD TEMPS NORMAL. RAN QRH FOR COMBINED FAILURE HYD 1 LO PRESS & HYD 3 LO PRESS. COULD NOT REGAIN SYSTEM 1. PUMP 1A & 1B BOTH NOT PROVIDING PRESS, 3A & 3B NOT PROVIDING PRESS. ABOUT 10 MINS OF CYCLING PUMP SWITCHES & TS, GAINED USE OF PUMP 3B & ABLE TO GET PRESS IN SYS 3, HELD AT 2800 PSI. IB & OB BRAKE PRESS REMAINED AT 0 THROUGHOUT LANDING. DECLARED AN EMER & DIVERTED TO OAK. ALL FAILURES WERE THE RESULT OF THE FAILED CBP 2 BUSSBAR & ON REPLACEMENT, NO FURTHUR EICAS MESSAGES WERE PRESENT. ALL STATED SYSTEMS OPS CKD GOOD.

Part: SEAL — LEAKING (PAX DOOR) · airframe 36,803 hrs · 26,624 cycles

MAIN CABIN DOOR AT ALT WAS MAKING A VERY LOUD SOUND CAUSING A RETURN TO FIELD. (FLIGHT 2953 - FILED CLOSED) FOUND LOWER FRWD. CORNER ON PAX DOOR SEAL TORN AND NOT SECURED TO DOOR SEAL TRACK. REMOVED AND REPLACED PAX DOOR SEAL WITH SERVICEABLE UNIT. PRESSURIZED A/C WITH NO ABNORMAL SOUND. A/C PRESSURIZED NORMALLY. REF. AMM.21-31-00, 52-11-07

Part: SKIN — GOUGED (BS 1098-1126) · 26,601 cycles

GOUGE ON EXTERIOR FUSELAGE SKIN BETWEEN STRINGER 2R & 4R AND FS1098 & FS1126 (C-CHECK RO 5/22/2021) GOUGE ON EXTERIOR FUSELAGE SKIN BETWEEN STRINGER 2R AND 4R AND FS1098.00 AND FS1126.00 WAS BLENDED, CHEMICAL CONVERSION COATING APLLIED AND PROTECTIVE FINISH RESTORED IAW REO670-53-61-1897 REV.-- DATE: 2021-05-16. ALL STEPS COMPLIED WITH. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH SKYCARD 51-900-1002-SKY.

Part: FLOOR SUPPORT — CORRODED (CABIN) · 26,601 cycles

PAX DOOR FLOOR SUPPORT ANGLE HAS EVIDENCE OF CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT ANGLE REF CRJ 700 SRM 51-42-06-001-001-A01

Part: D-RING — CORRODED (FWD CARGO BAY) · 26,601 cycles

FORWARD CARGO D RING MOUNT BRACKET AT FS 533 / STRINGRER 26-27L HAS CORROSION ON TOP (C-CHECK RO 5/22/2021) REMOVED AND REPLACED 1EA NEW FORWARD CARGO D RING MOUNT BRACKET P/N SH670-33389-1 AT FS 533/STRINGERS 26-27LH. REF CRJ-700 SRM 51-42-21-001-001-A01, CRJ-700 SRM 51-45-00-001-001-A01, CRJ-700 SRM 51-42-15-001-001-A01, CRJ-700 SRM 51-42-22-001-001-A01, BOMBARDIER ENG. DWG. SH670-33389 REV NC.

Part: ANGLE — CORRODED (PAX DOOR) · 26,601 cycles

PAX DOOR F/S 321.0 CLIP HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR CLIP AT F.S. 321.0, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: STRINGER — CORRODED (ZONE 100) · 26,601 cycles

STGR27 HAS EVIDENCE OF CORROSION ON FUSELAGE SKIN FLANGE BETWEEN FS349 - FS333 (C-CHECK RO 5/22/2021) CORROSION REMOVED FROM STGR27, MATERIAL LOSS FOUND TO BE OUT OF LIMITS, STGR27 REPLACED FROM FS333-FS364 REF CRJ700 SRM 51-42-06-001-001-A01, COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR, ALL CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 26,601 cycles

PAX DOOR MID DD6 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR MID DD6 INTERCOSTAL, REF CRJ 700 SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 26,601 cycles

PAX DOOR AFT DD2 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR AFT DD2 INTERCOSTAL, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: ANGLE — CORRODED (PAX DOOR) · 26,601 cycles

PAX DOOR F/S 320.0 CLIP HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR CLIP AT F.S. 320.0, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESS LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 26,601 cycles

PAX DOOR MID DD4 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR DD4 INTERCOSTAL, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 26,601 cycles

PAX DOOR MID DD2 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) INSTALLED NEW PAX DOOR MID DD2 INTERCOSTAL REF. CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N / COMPLIED WITH TASK CARD 51-900-1002-SKY / SEE CONTINUATION FOR DETAILS

Part: INTERCOSTAL — DENTED (PAX DOOR) · 26,601 cycles

PAX DOOR AFT DD7 INTERCOSTAL HAS DEEP DENT ON UPPER FLANGE RADIUS (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR AFT DD7 INTERCOSTAL, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 26,601 cycles

PAX DOOR AFT DD5 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR AFT DD5 INTERCOSTAL REF. CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N / COMPLIED WITH TASK CARD 51-900-1002-SKY / SEE CONTINUATION FOR DETAILS

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 26,601 cycles

PAX DOOR FWD DD3 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR DD3 INTERCOSTAL, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: CLEAT — CORRODED (PAX DOOR) · 26,601 cycles

PAX DOOR CLEAT HAS CORROSION COMOM TO AFT DD6 INTERCOSTAL (C-CHECK RO 5/22/2021) REMOVED AND INSTALLED NEW PAX DOOR CLEAT COMMON TO AFT DD6 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N AND RESTORED FINISH ALL FASTENERS AND APPLIED C.I.C AT REPAIRED LOCATION IAW CRJ 700 SRM 51-25-16-001-001-A01 ABD CRJ 700 SRM 51-21-11-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: INTERCOSTAL — DENTED (PAX DOOR) · 26,601 cycles

PAX DOOR FWD DD1 INTERCOSTAL HAS DEEP DENT ON UPPER FLANGE RADIUS (C-CHECK RO 5/22/2021) INSTALLED NEW PAX DOOR DD1 INTERCOSTAL REF. CRJ700 SRM 51-40-11-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N / COMPLIED WITH TASK CARD 51-900-1002-SKY / SEE CONTINUATION FOR DETAILS

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 26,601 cycles

PAX DOOR AFT DD4 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR DD3 INTERCOSTAL, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: INTERCOSTAL — DENTED (PAX DOOR) · 26,601 cycles

PAX DOOR AFT DD1 INTERCOSTAL HAS DEEP DENT ON UPPER FLANGE RADIUS (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR AFT DD1 INTERCOSTAL, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: FORMER — CRACKED (PAX DOOR) · 26,601 cycles

PAX DOOR AFT FORMER IS CRACK (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR AFT FORMER, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: INTERCOSTAL — CORRODED (ZONE 200) · 26,601 cycles

PAX DOOR FRAME F/S 313..56 BETWEEN DD4 AND DD5 INTERCOSTAL IS CORRODED (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR FRAME F.S. 313.56, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: STRINGER — CORRODED (ZONE 100) · 26,601 cycles

*STINGER 27 HAS EVIDENCE OF CORROSION ON FUSELAGE SKIN FLANGE BETWEEN FRAMES FS 310 AND FS 319. (C-CHECK RO 5/22/2021) CORROSION REMOVED AT STGR27, MATERIAL LOSS FOUND TO BE OUT OF LIMITS, STGR27 REPLACED BETWEEN FS310-FS333 REF DWG SH670-31635 REV NC AND CRJ700 SRM 51-42-06-001-001-A01, C/W TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR, ALL CHECKS GOOD

Part: SLAT TRACK — WORN (LT WING) · 26,601 cycles

*LEFT WING #2 LEADING EDGE SLAT €“ 2-3 DRIVEN SLAT TRACK HAS WEAR DAMAGE 4 AREAS. (MARKED) (C-CHECK RO 5/22/2021) REMOVED DAMAGE FROM LH SLAT TRACK 2-3.REWORKED AREA FOUND TO BE WITHIN LIMITS REF REO 670-57-42-1049 REV-- DATED 2021-04-08. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: SLAT TRACK — WORN (LT WING) · 26,601 cycles

*LEFT WING #3 LEADING EDGE SLAT €“ 3-1 DRIVEN SLAT TRACK HAS WEAR DAMAGE 4 AREAS. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR DAMAGE ON LH SLAT TRACK 3-1. REF CRJ700 SRM 51-12-00-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1050 REV-- DATED 2021-04-08. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: SUPPORT — CORRODED (PAX DOOR) · 26,601 cycles

PAX DOOR AFT FORMER SUPPORT ANGLE IS CORRODED (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR AFT FORMER SUPPORT ANGLE, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV -N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: TENSION TIE — CORRODED (PAX DOOR) · 26,601 cycles

PAX DOOR LOWER TENSION TIE HAS CORRODED HARDWARE (C-CHECK RO 5/22/2021) REMOVED AND REPLACED CORRODED HARDWARE PAX DOOR LOWER TENSION TIE IAW CRJ 700 AMM 52-11-19-400-801 A01. OPS TEST PREFORMED IN JOB: 71011585 OP: 130 CAMP: 22522934 / TUC 4964 S/N 25237 DUE 31/MAY/2021

Part: TENSION TIE — CORRODED (PAX DOOR) · 26,601 cycles

PAX DOOR UPPER TENSION TIE HAS CORRODED HARDWARE (C-CHECK RO 5/22/2021) REMOVED AND REPLACED CORRODED HARDWARE PAX DOOR UPPER TENSION TIE IAW CRJ 700 AMM 52-11-19-400-801-A01. OPS TEST PREFORMED IN JOB: 71011585 OP: 130 CAMP: 22522934 / TUC 4964 S/N 25237 DUE 31/MAY/2021

Part: CROSSBEAM — CORRODED (BS 549) · 26,601 cycles

CORROSION AT THREE LOCATIONS ON FS549.00 CROSSBEAM BETWEEN RBL9.0 AND LBL9.0 (C-CHECK RO 5/22/2021) REMOVED CORROSION. REF CRJ700 SRM 51-21-06-001-001. NDT DEFECT FREE. EVAL OUT OF LIMITS AS NO DAMAGE ALLOWED AT LOCATION. RECEIVED AND REPAIRED DAMAGE ON FS549.00 CROSSBEAM BETWEEN RBL9.0 AND LBL9.0 IAW REO 670-53-31-639 REV -- DATE 2021-05-03 COMPLIED WITH 51-900-1002-SKY

Part: FLOOR SUPPORT — CORRODED (BS 661-693) · 26,601 cycles

* CORROSION ON RH FLOOR SILL AROUND ALL SCREW HOLES AND AFT END FS661.00 TO FS693.00 (MARKED WITH ORANGE STREAMER) (C-CHECK RO 5/22/2021) REMOVED OLD DAMAGED FLOOR SILL AT FS 661-693 AND INSTALLED A NEW SILL IAWDWG SH670-32170 REV V AND CRJ-700 SRM 51-42-22-001-001-A01 / COMPLIED WITH TASK CARD 51-900-1002-SKY+

Part: SEAT TRACK — CORRODED (BS 477-693) · 26,601 cycles

MULTIPLE SPOTS OF CORROSION ON SEAT RAIL AT LBL 27 FROM FS477.40-FS693.00 (C-CHECK RO 5/22/2021) 2EA SEAT RAILS P/N SH670-33426-1 AND SH670-33463-1 WERE REMOVED AND REPLACED BY NEW ONES P/N SH670-33426-1 AND SH670-33463-1 IAW CRJ700 AMM 53-00-49-400-801-A03.

Part: RETAINER — CORRODED (PAX DOOR SEAL) · 26,601 cycles

PAX DOOR AFT SEAL RETAINER HAS CORROSION AT FASTENERS (C-CHECK RO 5/22/2021) REPLACED CORRODED FASTENERS ON PAX DOOR AFT SEAL RETAINER IAW CRJ 700 SRM 51-42-06-001-001-A01

Part: RETAINER — CORRODED (PAX DOOR SEAL) · 26,601 cycles

PAX DOOR FWD SEAL RETAINER HAS CORROSION AT FASTENERS (C-CHECK RO 5/22/2021) REPLACED CORRODED FASTENERS ON PAX DOOR FWD SEAL RETAINER IAW CRJ 700 SRM 51-42-06-001-001-A01

Part: RETAINER — CORRODED (PAX DOOR SEAL) · 26,601 cycles

PAX DOOR UPPER SEAL RETAINER HAS CORROSION AT FASTENERS (C-CHECK RO 5/22/2021) REPLACED CORRODED FASTENERS ON PAX DOOR UPPER SEAL RETAINER IAW CRJ 700 SRM 51-42-06-001-001-A01

Part: SEAT TRACK — CORRODED (BS 379-669) · 26,601 cycles

*MULTIPLE SPOTS OF CORROSION ON R/H SIDE SEAT TRACK FROM FS379.00-FS669.00 (C-CHECK RO 5/22/2021) 3 EA. RH SIDE SEAT TRACKS P/N SH670-32234-951, SH670-33558-3 AND SH670-32233-3 FROM FS379.00-FS669.00 WERE REMOVED AND REPLACED BY NEW ONES P/N SH670-32234-951, SH670-33558-3 AND SH670-32233-3 IAW CRJ700 AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 349-477) · 26,601 cycles

**CORROSION NOTED ON SEAT TRACK RAILS AT LBL 9 FROM FS349.00-FS477.00 (C-CHECK RO 5/22/2021) REPLACED AND INSTALLED NEW SEAT TRACK RAIL P/N SH670-32249-3 AT FS349.00 - FS477.00 REF CRJ700 AMM 53-00-49-400-801-A03

Part: INTERCOSTAL — CORRODED (ZONE 100) · 26,601 cycles

*STRINGER 20R INTERCOSTAL BETWEEN FS 349 AND FS 364 HAS EVIDENCE OF CORROSION. (C-CHECK RO 5/22/2021) REMOVED AND REPLACED STGR20R INTERCOSTAL BETWEEN F.S.349 AND F.S.364 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-31994 REV.NC, COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR, ALL CHECKS GOOD.

Part: SEAT TRACK — CORRODED (BS 349-477) · 26,601 cycles

*CORROSION NOTED ON SEAT TRACK RAILS AT RBL 9 FROM FS349.00-FS477.00 (C-CHECK RO 5/22/2021) INSTALLED NEW SEAT TRACK RAIL. P/N SH670-32159-1 REF. CRJ 700 AMM 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 379-669) · 26,601 cycles

MULTIPLE SPOTS OF CORROSION ON L/H SIDE SEAT TRACK FROM FS379.00-FS669.00 (C-CHECK RO 5/22/2021) 3 EA. LH SIDE SEAT TRACKS P/N SH670-322-3, SH32234-951 AND SH670-33558-3 FROM FS379.00-FS669.00 WERE REMOVED AND REPLACED BY NEW ONES P/N SH670-322-3, SH32234-951 AND SH670-33558-3 FROM FS379.00-FS669.00 IAW CRJ700 AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 477-693) · 26,601 cycles

*MULTIPLE SPOTS OF CORROSION ON SEAT RAIL AT RBL 9 FROM FS477.40-FS693.00 (C-CHECK RO 5/22/2021) REMOVED AND REPLACED WITH NEW SEAT TRACK RAIL AT RBL9 FROM FS477.40 TO FS693.00 REF CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ 700 AMM 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 349-477) · 26,601 cycles

*CORROSION NOTED ON SEAT TRACK RAILS AT LBL 27 FROM FS349.00-FS477.00 (C-CHECK RO 5/22/2021) SEAT TRACK RAIL P/N SH690-32127-3 OF 27LBL AT FS349.00-FS477.00 WAS REMOVED AND REPLACED BY A NEW ONE P/N SH690-32127-3 IAW CRJ700 AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 669-989) · 26,601 cycles

*MULTIPLE SPOTS OF CORROSION ON L/H SIDE SEAT RAILS FROM FS669.40-989.00 (C-CHECK RO 5/22/2021) REMOVED AND REPLACED SIDE SEAT TRACKS ON L/H FS669.40-989.00 REF CRJ700 AMM 53-00-49-000-801-A17 & 53-00-49-400-801-A17. SEE CONTINUE CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (CABIN) · 26,601 cycles

*PAX DOOR SILL UPPER FLOOR SUPPORT ANGLE HAS EVIDENCE OF CORROSION ON OUTBOARD EDGE AND AT FASTENER HOLES ALONG ENTIRE LENGTH. (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR SILL UPPER FLOOR SUPPORT ANGLE REF CRJ 700 SRM 51-41-02-001-001-A01

Part: SEAT TRACK — CORRODED (BS 669-989) · 26,601 cycles

*MULTIPLE SPOTS OF CORROSION ON R/H SIDE SEAT RAILS FROM FS669.40-FS989.00 (C-CHECK RO 5/22/2021) 6 EA CORRODED R/H SIDE SEAT RAILS FROM FS669.40 TO FS989.00 WERE REMOVED AND REPLACED BY NEW ONES IAW CRJ700 AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 477-693) · 26,601 cycles

MULTIPLE SPOTS OF CORROSION ON SEAT RAIL AT LBL 9 FROM FS477.40-FS693.00 (C-CHECK RO 5/22/2021) REMOVED AND REPLACED SEAT TRACK RAIL AT LBL 9 FROM FS477.40 TO FS693.00 REF CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ 700 AMM 53-00-49-400-801-A17

Part: SLAT TRACK — WORN (LT WING) · 26,601 cycles

*LEFT WING #3 LEADING EDGE SLAT NON-DRIVEN SLAT TRACK HAS 2 AREAS WITH WEAR AND PITTING DAMAGE. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR AND PITTING DAMAGE ON LH SLAT TRACK 3-2. REF CRJ700 SRM 51-12-00-001-001-A01 AND 51-21-06-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH REO 670-57-42-1051 REV-- DATED 2021-04-08. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: MOUNT BRACKET — CORRODED (FWD CARGO) · 26,601 cycles

*FWD CARGO "D" RING MOUNT BRACKET AT FS 581 / STRINGER 26L - 27 HAS EVIDENCE OF CORROSION ON TOP. (C-CHECK RO 5/22/2021) REPLACED AND INSTALLED NEW MOUNT BRACKET P/N SH670-33389-2 AT FS581 STGR26L - 27 REF DWG NO. SH670-33600 REV Y. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (RII).

Part: SLAT TRACK — WORN (RT WING) · 26,601 cycles

* RIGHT WING #3 LEADING EDGE SLAT NON-DRIVEN SLAT TRACK HAS 1 AREA WITH WEAR AND PITTING DAMAGE. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR DAMAGE AND PITTING FROM RH SLAT TRACK 3-2. REF CRJ700 SRM 51-12-00-001-001-A01 AND 51-21-06-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1042 REV-- DATED 2021-04-05. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: SLAT TRACK — DAMAGED (RT WING) · 26,601 cycles

* RIGHT WING #2 LEADING EDGE SLAT NON-DRIVEN SLAT TRACK HAS 3 AREAS WITH WEAR/PITTING/CORROSION DAMAGE. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR DAMAGE/PITTING/CORROSION FROM RH SLAT TRACK 2-2. REF CRJ700 SRM 51-12-00-001-001-A01 AND 51-21-06-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH REO 670-57-42-1039 REV-- DATED 2021-04-05. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: SLAT TRACK — CORRODED (LT WING) · 26,601 cycles

*LEFT WING #2 LEADING EDGE SLAT NON-DRIVEN SLAT TRACK HAS 2 AREAS WITH WEAR/ PITTING DAMAGE AND 1 AREA WITH CORROSION. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR AND PITTING FROM LH SLAT TRACK 2-2. REF CRJ700 SRM 51-12-00-001-001-A01 AND 51-21-06-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1048 REV-- DATED 2021-04-08. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: SLAT TRACK — DAMAGED (RT WING SLAT) · 26,601 cycles

*RIGHT WING #1 LEADING EDGE SLAT €“ 1-1 DRIVEN SLAT TRACK HAS WEAR DAMAGE 5 AREAS. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR MARKS ON RH SLAT TRACK 1-1. REF CRJ700 SRM 51-12-00-001-001-A01. EVAL NO DAMAGE ALLOWED IN REPAIR LOCATION. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1035 REV-- DATED 2021-04-05. ALL CHECKS GOOD AT THIS TIME. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: SLAT TRACK — WORN (LT WING) · 26,601 cycles

*LEFT WING #2 LEADING EDGE SLAT €“ 2-1 DRIVEN SLAT TRACK HAS WEAR 2 AREAS AND WEAR AND PITTING DAMAGE 2 AREAS. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR DAMAGE AND PITTING ON LH SLAT TRACK 2-1. REF CRJ700 SRM 51-12-00-001-001-A01 AND 51-21-06-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1047 REV-- DATED 2021-04-08. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: SLAT TRACK — DAMAGED (RT WING) · 26,601 cycles

* RIGHT WING #1 LEADING EDGE SLAT €“ 1-3 DRIVEN SLAT TRACK HAS WEAR DAMAGE 6 AREAS. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR DAMAGE ON RH SLAT TRACK 1-3. REF CRJ700 SRM 51-12-00-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1037 REV-- DATED 2021-04-08. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH SKYCARD 51-900-1002-SKY.

Part: SLAT TRACK — DAMAGED (RT WING) · 26,601 cycles

* RIGHT WING #3 LEADING EDGE SLAT €“ 3-3 DRIVEN SLAT TRACK HAS WEAR DAMAGE 2 AREAS. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR DAMAGE ON RH SLAT TRACL 3-3. REF CRJ700 SRM 51-12-00-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1043 REV-- DATED 2021-04-05. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: SLAT TRACK — DAMAGED (RT WING) · 26,601 cycles

* RIGHT WING #2 LEADING EDGE SLAT €“ 2-3 DRIVEN SLAT TRACK HAS WEAR DAMAGE 2 AREAS. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR DAMAGE ON RH SLAT TRACK 2-3. REF CRJ700 SRM 51-12-00-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1040 REV-- DATED 2021-04-05. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR

Part: STRINGER — CORRODED (ZONE 100) · 26,601 cycles

*STRINGER 26R HAS EVIDENCE OF CORROSION ON SKIN FLANGE BETWEEN FS 333 AND FS 349. (C-CHECK RO 5/22/2021) REMOVED AND REPLACED STGR26R BETWEEN FS333 AND FS349 REF. CRJ 700 SRM 51-42-06-001-001-A01 DWG =# SH690-31350 REV. NC, COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR, ALL CHECKS GOOD

Part: SLAT TRACK — DAMAGED (RT WING) · 26,601 cycles

*RIGHT WING #2 LEADING EDGE SLAT €“ 2-1 DRIVEN SLAT TRACK HAS WEAR DAMAGE 4 AREAS. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR DAMAGE ON RH LEADING EDGE SLAT 2-1. REF CRJ700 SRM 51-12-00-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1038 REV-A DATED 2021-04-12. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS FO WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR

Part: SKIN — DAMAGED (RT WING LE) · 26,601 cycles

* RIGHT WING #1 LEADING EDGE SLAT NON-DRIVEN SLAT TRACK HAS 3 AREAS WITH WEAR/PITTING/CORROSION DAMAGE. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR DAMAGE/PITTING/CORROSION FROM RH SLAT TRACK 1-2. REF CRJ700 SRM 51-12-00-001-001-A01 AND 51-21-06-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1036 REV-- DATED 2021-04-05. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: SLAT TRACK — WORN (RT WING) · 26,601 cycles

*LEFT WING #1 LEADING EDGE SLAT €“ 1-3 DRIVEN SLAT TRACK HAS WEAR AND PITTING DAMAGE, 4 AREAS. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR AND PITTING DAMAGE FROM LH SLAT TRACK 1-3. REF CRJ700 SRM 51-12-00-001-001-A01 AND 51-21-06-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1046 REV-- DATED 2021-04-08. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: SLAT TRACK — WORN (LT WING) · 26,601 cycles

*LEFT WING #1 LEADING EDGE SLAT €“ 1-2 NON-DRIVEN SLAT TRACK HAS WEAR AND PITTING DAMAGE, 2 AREAS. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR DAMAGE AND PITTING FROM LH SLAT TRACK 1-2. REF CRJ700 SRM 51-12-00-001-001-A01 AND 51-21-06-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1045 REV-- DATED 2021-04-08. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: SLAT TRACK — DAMAGED (RT WING) · 26,601 cycles

* RIGHT WING #3 LEADING EDGE SLAT €“ 3-1 DRIVEN SLAT TRACK HAS WEAR DAMAGE 3 AREAS. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR DAMAGE FROM RH SLAT TRACK 3-1. REF CRJ700 SRM 51-12-00-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1041 REV-- DATED 2021-04-05. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: SLAT TRACK — WORN (LT WING) · 26,601 cycles

*LEFT WING #1 LEADING EDGE SLAT €“ 1-1 DRIVEN SLAT TRACK HAS WEAR 2 AREAS AND 2 AREAS WEAR AND PITTING DAMAGE. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR DAMAGE AND PITTING FROM LH SLAT TRACK 1-1. REF CRJ700 SRM 51-12-00-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1044 REV-- DATED 2021-04-08. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: FORMER — CORRODED (PAX DOOR) · 26,601 cycles

* PASSENGER DOOR FWD FORMER GOUGED AND CORRODED (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR FWD FORMER, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: STOP FITTING — WORN (GLY DOOR FRAME) · 26,601 cycles

* GALLEY SERVICE DOOR SURROUND, FWD AND AFT STOP FITTINGS WORN/CHAFED (C-CHECK RO 5/22/2021) BLENDED NOTED WEAR DAMAGE SMOOTH REMOVING MINIMAL MATERIAL. REF CRJ700 SRM 51-12-00-001-001-A01. NDT DEFECT FREE. RECEIVED REO 670-53-21-2024 REV-- DATED 2021-04-28. COMPLIED WITH REO 670-53-21-2024 REV-- DATED 2021-04-28 / OPS AND LEAK CHECK GOOD

Part: STRIKER — DENTED (PAX DOOR SEAL) · 26,601 cycles

* PASSENGER DOOR SURROUND, FWD SEAL STRIKER DENTED AT APPROXIMATELY STGR7L (C-CHECK RO 5/22/2021) REPAIRED FWD SEAL STRIKER AT STGR 4L-9L AT FS 310 IAW PREVIOUSLY INCORPERATED REO 670-53-22-001 REV-J 2016-11-10 REPAIR TYPE III, / PREASSURE CHECK GOOD. / COMPLIED WITH TASK CARD 51-900-1002-SKY / COMPLIED WITH FORM 337

Part: SKIN — CHAFED (BS 969 S26L/R) · 26,601 cycles

* REPAIR AT APPROX. FS969 €“ FS985 STGR26L €“ STGR26R IS CHAFED (C-CHECK RO 5/22/2021) FABRICATED AND INSTALLED REPAIR PARTS -17, -18, -19, -20, -21, -22, -23, & -24 IAW REO# 670-53-00-290 REV-F DATE 2019/04/26 INSTALLED AND RESTORED FINISH IAW REO# 670-53-00-290 REV -F DATE; 2019/04/26 SEE CONTINUE CARD FOR DETAILS, COMPLIED WITH REF 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR & MX TRANS#22507972 JOB 71011581 OP167

Part: SKIN — DENTED (LT ENG FAN COWL) · 26,601 cycles

LH ENGINE LOWER FAN COWL HAS DENTS REPAIR ANY EVIDENCE OF DENTS BY WAY OF STANDARD PRACTICE. (C-CHECK RO 5/22/2021) REPAIRED MULTIPLE DENTS ON LH ENGINE LOWER FAN COWL REF CRJ 700 SRM 54-14-00-201-002-A01 AND REO 670-54-14-1012 REV B DATED 2019//03/18 / COMPLIED WITH CARD NO. 51-900-1002-SKY

Part: HINGE — GOUGED (PAX DOOR)

PASSENGER DOOR HINGE LUGS 1,2,3 Q AND 4 FWD END AND LAST LUG AT AFT END IS GOUGED APPROX 0.001 INCH DEEP. REPAIRED PAX DOOR HINGE (DOOR SIDE) IAW REO 670-52-11-511-01 AND 670-52-11-5110REV E.

Part: ANGLE — CRACKED (NACELLE) · airframe 35,299 hrs · 25,360 cycles

RIGHT PYLON TRAILING EDGE AFT INBD ANGLE IS CRACKED UNDER PANEL 423BT. REPLACED THE ANGLE IAW MM 670-37189 S03.

Part: POST — CORRODED (BS 280) · airframe 35,299 hrs · 25,360 cycles

LT COCKPIT DOOR POST CORRODED AT BOTTOM AT BS 280. REPAIRED THE POST IAW EC/TC REO 670-53-11-745 AND REO 670-53-11-745, REV -A.

Part: POST — CORRODED (BS 280) · airframe 35,299 hrs · 25,360 cycles

RIGHT COCKPIT DOOR POST CORRODED AT BOTTOM AT BS 280. REPAIRED THE POST IAW EC/TC REO 670-53-11-745, AND REO 670-53-11-745, REV -A.

Part: FITTING — CORRODED (BS 349) · airframe 35,299 hrs · 25,360 cycles

FLOORBEAM FITTING IS CORRODED AT BS 349 AND STRINGER 18L. REMOVED AND REPLACED THE FLOORBEAM FITTING IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-20-001-001-A01.

Part: FRAME — CORRODED (BS 333) · airframe 35,299 hrs · 25,360 cycles

BS 333 FRAME IS CORRODED AT STRINGER 27R. REPAIRED THE FRAME IAW REO 670-53-21-799.

Part: FRAME — CORRODED (BS 349) · airframe 35,299 hrs · 25,360 cycles

BS 349 FRAME IS CORRODED BETWEEN STRINGERS 25L AND 25R. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-21-16-001-001-A01, AND 51-21-11-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 35,299 hrs · 25,360 cycles

STRINGER 26R INTERCOSTAL IS CORRODED BETWEEN BS 349 AND 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 35,299 hrs · 25,360 cycles

STRINGER 26L INTERCOSTAL WAS FOUND CORRODED BETWEEN BS 349 AND 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 35,299 hrs · 25,360 cycles

CORROSION ON CRAWLWAY FLOORBEAM ANGLE, BS 280. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01.

Part: POST — DAMAGED (BS 202.75) · airframe 34,026 hrs · 24,384 cycles

BS 202.75 POST RBL 7.5 INBD NLG BAY HAS TWO ELONGATED FASTNER HOLES. COMPLIED WITH ECTC REO 670-53-11-1309.

Part: STRINGER — CRACKED (ZONE 200) · airframe 34,026 hrs · 24,384 cycles

WHILE PPERFORMING SB670BA-53-040, FOUND STRINGER 3 TO BE CRACKED. REPAIRED THE STR 3 IAW REO 670-53-21-493, REV D.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 32,497 hrs · 23,232 cycles

SMELL OF ELECTRICAL SMOKE OR BURNING SMELL IN COCKPIT. INSPECTED COCKPIT AND COULD NOT FIND ISSUE. NO FAULT FOUND. ALL WERE DONE IAW FIM 21-22-00. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LENS — MISSING (CABIN) · airframe 31,545 hrs · 22,465 cycles

GALLEY EXIT LIGHT LENS MISSING. FLT 5203, DEL 290 MINS. REPLACED EXIT LIGHT LENS COVER IAW AMM 33-51-05. ACFT OK FOR SERVICE.

Part: SEAT TRACK — CRACKED (BS 855) · airframe 30,567 hrs · 21,712 cycles

PROVIDE NDT SUPPORT FOR SB 67BA-25-094, REV A, DATED AUG 26-2015 IAW DWG KBA670-36100, REV D, DATED 12/3/15. SIDE SEAT TRACK CUTOUT AT FRAME BS 855.5 RT, SIDE SEAT TRACK CUTOUT AT FRAME BS 869.5 RT, SIDE SEAT TRACK CUTOUT AT FRAME BS 961 RT, SIDE SEAT TRACK CUTOUT AT FRAME BS 855.5 LT, SIDE SEAT TRACK CUTOUT AT FRAME BS 869.5 LT, SIDE SEAT TRACK CUTOUT AT FRAME BS 961 LT, TRIM OUT OF INTERCOSTAL AT STR 12 BETWEEN FS 953-969, ET INSP NDTM 51-20-006-250-A01. NO DEFECTS NOTED BEYOND CUT LINE.

Part: FLOOR SUPPORT — CORRODED (BS 1030-1034) · airframe 30,567 hrs · 21,712 cycles

CORROSION FOUND ON LBL 9 FLOOR SUPPORT BETWEEN BS 1030-1034. CORROSION DETERMINED TO BE OUT OF LIMITS IAW SRM 53-61-43-101-001-A01. REPAIRED IAW EC/TC EO 700-53-0287 AND GREO 670-53-00-029, REV A.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1033) · airframe 30,567 hrs · 21,712 cycles

CORROSION FOUND ON LBL 27 FLOOR SUPPORT BETWEEN BS 1015-1033. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43-101-001-A01. REPAIRED IAW EC/TC EO 700-53-0286 AND GENERIC REO 670-53-00-029 REV A.

Part: MEGAPHONE — INTERMITTENT (CABIN) · airframe 29,933 hrs · 21,192 cycles

CABIN MEGAPHONE WORKS INTERMITTENTLY. R & R CABIN MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,875 hrs · 21,145 cycles

GALLEY FWD LOWER EMERGENCY EXIT SIGN HAS 1 LIGHT BULB BURNED OUT. RELAMPED GALLEY FWD LOWER EMERGENCY EXIT SIGN IAW AMM 33-51-05 AND 33-51-00. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,875 hrs · 21,145 cycles

12CD LOWER SIDEWALL EMERGENCY EXIT SIGN HAD TWO LIGHT BULBS BURNED OUT. RELAMPED 12CD LOWER SIDEWALL EMERGENCY EXIT SIGN IAW AMM 33-51-05 AND 33-51-00. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,572 hrs · 20,879 cycles

SEVERAL EMERGENCY LIGHTS ARE INOPERATIVE. DURING TROUBLESHOOTING, FOUND NR 2 EMERGENCY LIGHT BATTERY PACK TO BE UNSERVICABLE. R & R NR 2 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-17-000-801 AND 33-51-17-400-801-A01. OPS TESTED GOOD.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 29,572 hrs · 20,879 cycles

FOUND STRINGER SPLICE AT STR 31R, BS 333 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-06-001-001, SRM 51-40-11-001-001-A01 & DWG SH 670-31197.

Part: FLOORBEAM — CORRODED (BS 782) · airframe 29,572 hrs · 20,879 cycles

RBL 9 FLOORBEAM CORRODED AT BS 782. BLENDED CORROSION IAW SRM TASK 51-21-06-001-001-A01. REPAIRED IAW SRM 53-00-41-201-001-A01, FIG 53-00-41-991-831.

Part: SUPPORT — CORRODED (BS 333) · airframe 29,572 hrs · 20,879 cycles

AVIONICS SUPPORT STRUCTURE AT BS 333, IS SEVERELY CORRODED. REMOVED CORRODED CLEAT AN 3 EA RIVETS FROM FRAME 333 AT STR 21R AND AVIONICS SUPPORT RAIL IAW SRM 51-42-06-001-001 AND SRM 51-42-21-001-001. INSTALLED SERVICEABLE CLEAT & 3 EA RIVETS AT FS 333 & STR 21R & AVIONIC SUPPORT RAIL REF SRM 42-06-001-001- & DWG SH 670-32600 & SH 670-32695. FORMED A ROUGH CUT OF CLEAT SH670-32695-7, REF SRM 51-24-36-001-A01 AND 51-24-21-001-001-A01. FABRICATED PART NOT USED, OBTAINED NEW SERVICABLE CLEAT AND LOCATED FASTENER HOLES IAW SRM 51-40-11-001-001-A01 AND DWG SH670-32695, REV C.

Part: SEAT TRACK — CORRODED (BS 677-712) · airframe 29,572 hrs · 20,879 cycles

LT SIDE SEAT TRACK BS 677 - 712 FOUND CORRODED. REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343 AND INSTALLED IAW AMM 53-00-49-400-801-A03/000-801 A03.

Part: FLOOR SUPPORT — CORRODED (BS 830-847) · airframe 29,558 hrs · 20,866 cycles

RBL 9, FLOOR SUPPORT IS CORRODED BETWEEN BS 830.1- 847. BLENDED CORROSION AND FOUND TO BE IN A NO DAMAGE ALLOWED AREA. REPAIRED IAW SRM 51-21-06-001-001-A01 & 53-41-44-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 369) · airframe 29,549 hrs · 20,861 cycles

LT SIDE SEAT TRACK CORRODED AT BS 396. CORRODED BEYOND LIMITS IAW SRM 53-41-49. REMOVED AND REPLACED THE SEAT TRACK IAW 53-00-49-000-801-A01, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 977-1006) · airframe 29,558 hrs · 20,866 cycles

CORROSION FOUND ON THE SEAT TRACK AT BS 977 - 1006 LBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 & AMM 53-00-49-400-803.

Part: PLATE — CORRODED (BS 1015-1031) · airframe 29,558 hrs · 20,866 cycles

CORROSION FOUND ON SILL PLATE AT BS 1015 -1031, RBL 40. REPAIRED IAW ECTC REO 670-53-00-390 AND REO 670-53-00-390. REV.

Part: SEAT TRACK — CORRODED (BS 977-1000) · airframe 29,558 hrs · 20,866 cycles

CORROSION FOUND ON THE SEAT TRACK AT BS 977 - 1000 RBL 27. DAMAGED BEYOND LIMITS REF 53-51-49-101-001-A01. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 533) · airframe 29,558 hrs · 20,866 cycles

RBL 9, SEAT TRACK WAS CORRODED AT BS 533. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-000-801 A03.

Part: SEAT TRACK — CORRODED (BS 581 & 613) · airframe 29,549 hrs · 20,861 cycles

RT SIDE SEAT TRACK HAS CORROSION AT BS 581 AND 613. FOUND TO BE OUT OF LIMITS. 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 728) · airframe 29,549 hrs · 20,861 cycles

CORROSION ON RBL 9 SEAT TRACK AT BS 728. CORROSION BEYOND LIMITS IAW SRM SUP 53-41-49, REO 670-53-00-13. 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 977-1006) · airframe 29,558 hrs · 20,866 cycles

CORROSION FOUND ON THE SEAT TRACK AT BS 977 - 1006, RBL 9. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND 53-00-49-400-801 A03 AND INSTALLED NEW FITTING IAW SRM 51-41-02-001-A01.

Part: SEAT TRACK — CORRODED (BS 837-987) · airframe 29,558 hrs · 20,866 cycles

SEAT TRACK, LBL 9 CORRODED AT SEVERAL PLACES BS 837-987. CORRODED BEYOND LIMITS IAW SRM 53-51-49/ REO 670-53-00-013. REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 549) · airframe 29,558 hrs · 20,866 cycles

RBL 9 SEAT TRACK HAS CORROSION AT BS 549. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-000-801, A03.

Part: SEAT TRACK — CORRODED (BS 677-712) · airframe 29,549 hrs · 20,861 cycles

RT SIDE SEAT TRACK FROM BS 677 - 712 WAS CORRODED OUT OF LIMITS. CORROSION FOUND BEYOND LIMITS IAW SRM SUP 53-41-49 REO 670-53-00-13. REPLACED IAW AMM 53-00-49-000-801-A03, 53-00-47-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 837-969) · airframe 29,549 hrs · 20,861 cycles

SEAT TRACK RT RBL 9 HAS CORROSION BS 837-969. CORROSION FOUND BEYOND LIMITS IAW SRM SUP 53-41-49, REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 & AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 581) · airframe 29,549 hrs · 20,861 cycles

LT SIDE SEAT TRACK WAS CORRODED AT BS 581. CORROSION FOUND BEYOND LIMITS IAW SRM SUP 53-41-49, REO 670-53-00-13. REMOVED FABRICATED AND INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-000-801-A03, 53-00-49-400-801-A03 AND REO 670-53-00-343.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 29,549 hrs · 20,861 cycles

BS 280, BULKHEAD WEB IS CORRODED. REPAIRED IAW EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594, REV A.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 29,543 hrs · 20,857 cycles

RT SIDE SEAT TRACK BS 785.15- 863 CORRODED. CORRODED BEYOND LIMITS IAW SRM 53-41-49, REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK AT IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.

Part: ANGLE — CORRODED (BS 349) · airframe 29,549 hrs · 20,861 cycles

ANGLE CORRODED AT INTERCOSTAL STRINGER 20R FWD SIDE OF BS 349. BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-21-23-101-002 A01. REMOVED THE ANGLE. INSTALLED A NEW ANGLE IAW SRM 51-40-11-001-001-A01, SRM 51-42-06-001-001-A01, AND DWG SH670-31950.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 29,549 hrs · 20,861 cycles

CENTER CONSOLE CORRODED JUST ABOVE COCKPIT FLOOR PANEL SUPPORT, FLOOR SUPPORT STRUCTURE CORRODED. REMOVED CORROSION FROM CENTER CONSOLE IAW SRM 51-21-06-001-001-A01. RECEIVED AND COMPLIED WITH EA 32-2015-253.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 29,549 hrs · 20,861 cycles

PAX DOOR SILL ANGLE CORRODED. REMOVED AND REPLACED THE DOOR SILL ANGLE IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-A01 & DWG SH670-31810.

Part: SEAT TRACK — CORRODED (BS 712-761) · airframe 29,543 hrs · 20,857 cycles

RT SIDE SEAT TRACK BS 712-761 CORRODED. CORRODED BEYOND LIMITS IAW SRM 53-41-49, REO 670-53-00-13. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACKIAW AMM 53-00-49-000-801-A02, 53-00-49-400-801-A03 AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 29,543 hrs · 20,857 cycles

LT SIDE SEAT TRACK BS 785.15 - 863 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A03, AMM 53-00-49-400-801-A03.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 29,549 hrs · 20,861 cycles

PAX DOOR SILL CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-31810 TREV.

Part: FRAME — CORRODED (BS 310) · airframe 29,543 hrs · 20,857 cycles

FWD SIDE OF FRAME BS 310 HAS CORROSION BETWEEN STRINGERS 26L-26R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 319-333) · airframe 29,549 hrs · 20,861 cycles

INTERCOSTAL AT STR 20R CORRODED BETWEEN BS 319-333. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, DWG SH670-31950, SRM 51-42-21-001-001-A01.

Part: STIFFENER — CRACKED (BS 280) · airframe 29,543 hrs · 20,857 cycles

THE STIFFENER LOCATED AT FS 280.00, BL 26.00 IS CRACKED THE RT SIDE LWR SECTION. RECEIVED AND COMPLIED WITH REO 670-53-11-1072, REV DATED 2015-06-17. RECEIVED AND COMPLIED WITH REO 670-53-11-1072, REV A, FABRICATED -1 ANGLE & -2 FILLER. RECEIVED REO 670-53-11-1072, REV B AND FINISHED LAYOUT. RECEIVED & COMPLIED WITH REO 670-53-11-1072.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 29,543 hrs · 20,857 cycles

COCKPIT FLOOR SUPPORT CORRODED RT SIDE. REMOVED CORROISON FROM RT SIDE COCKPIT FLOOR SUPPORT IAW SRM 51-21-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 29,549 hrs · 20,861 cycles

FLOOR SUPPORT FOUND TO BE CORRODED BS 310 - 319 AND IS OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 358-485) · airframe 29,549 hrs · 20,861 cycles

SEAT TRACK LBL 9, BS 358-485 WAS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49/REO 670-53-00-013. 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 712-761) · airframe 29,543 hrs · 20,857 cycles

LT SIDE SEAT TRACK BS 712 - 761.88 HAS CORROSION IN SEVERAL PLACES. CORRODED BEYOND LIMITS IAW SRM SUP 53-41-49, REO 670-53-00 13. INSTALLED IAW AMM 53-00-49-400-801-A03/000-801-A03.

Part: NOT REPORTED — CORRODED (BS 295) · airframe 29,543 hrs · 20,857 cycles

AFT SIDE BS 295 CORRODED AT STR 25R. REMOVED CORROSION ON FS 295 AT STR 25R IN REF TO SRM 51-21-06-001-001-A01. COMPLIED WITH EC/TC EA 32-2015-255.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,543 hrs · 20,857 cycles

FLOORBEAM AFT SIDE OF FS 280, CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. R & R FLOORBEAM BRACKET IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 & 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 29,549 hrs · 20,861 cycles

COCKPIT FLOOR SUPPORT CORRODED LT SIDE. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 349-385) · airframe 29,549 hrs · 20,861 cycles

SEAT TRACK RBL 9, BS 349-485 FOUND CORRODED. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-000-400-801-A03 .

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 29,549 hrs · 20,861 cycles

BS 280 BULKHEAD WEB IS CORRODED. REPAIRED IAW EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594, REV A.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,433 hrs · 20,770 cycles

EXTERIOR EMERGENCY LIGHT NR 6 INOPERATIVE. REPLACED THE LAMP. OPS CHECKED GOOD IAW AMM 33-51-15.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,325 hrs · 20,674 cycles

MAIN ENTRANCE LOWER EXIT SIGN HAVE 1 LIGHT BULB BURNED. REPLACED BURNED LIGHT IN MAIN ENTRANCE LOWER EXIT SIGN IAW AMM 33-23-01.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,325 hrs · 20,674 cycles

GALLEY FWD EXIT LOWER SIGN HAVE 1 LIGHT BULB BURNED. REPLACED BURNED LIGHT BULB IN GALLEY FWD LOWER SIGN IAW AM 33-51-05.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,325 hrs · 20,674 cycles

12AB LOWER EXIT SIGN HAVE 1 BURNED LIGHT BULB. REPLACED BURNED LIGHT BULB IN EXIT SIGN AT 12AA/B IAW AMM 33-51-05.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,325 hrs · 20,674 cycles

GALLEY AFT LOWER EXIT SIGN HAVE 1 LIGHT BULB BURNED. REPLACED BURNED LIGHT IN GALLEY AFT LOWER EXIT SIGN IAW AMM 33-51-05.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 28,854 hrs · 20,284 cycles

COCKPIT FLASHLIGHTS ARE INOPERTIVE. REPLACED BATTERIES IAW AMM 25-61-00, OPS CHECKED GOOD.

Part: RUB STRIP — DEBONDED (LT AILERON) · airframe 28,345 hrs · 19,914 cycles

LEFT AIRLERON OTBD RUBSTRIP IS DISBONDED. COMPLIED WITH EC/TC REO 670-57-61-006 01, THIS IS A PERMANENT REPAIR.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 27,971 hrs · 19,631 cycles

CABIN MEGAPHONE INOPERATIVE. R & R THE MEGAPHONE IAW AMM 25-61-14,.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 26,082 hrs · 18,214 cycles

NOSE STEERING INOPERATIVE CAUTION. EMERGENCY DECLARED. PERFORMED RESET IAW IAW FIM 32-50-00, PAGE 221 FAULT NO LONGER EXIST IAW ACFT, OK FOR SERVICE.

Part: POWER SUPPLY — DISCONNECTED (EMERGENCY LIGHT) · airframe 24,988 hrs · 17,412 cycles

EMERGENCY EXIT LIGHT (LOWER) AT ROW 12H AND ROW 12 INOPERATIVE. RECONNECTED EPSU IAW AMM 33-51-17-400-801. OPS CHECKED GOOD IAW 33-51-17-710-801.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,988 hrs · 17,412 cycles

EMERGENCY LIGHTS AT CEILING PANEL 263FLC, 273ALC ARE INOPERATIVE. REPLACED LAMP IN THE EMERGENCY LIGHT NR 6 IAW AMM 33-51-09-400-801. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: LINER — DAMAGED (CARGO DOOR) · airframe 24,988 hrs · 17,412 cycles

FWD BAGGAGE BAY FWD CUP HINGE LINER 151ELW DAMAGED. REPAIRED IAW SRM 51-40-11-001-001-A01. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CRACKED (LT WING) · airframe 24,993 hrs · 17,416 cycles

WHILE PERFORMING NDT INSPECTION OF HOLES ON LT WING PLANK HAD CRACK INDICATION IN LOWER WING PLANK AND MLG RETRACT ACTVATOR BEAM. REPAIRED IAW REO 670-57-21-560, REV P2.

Part: CROSSBEAM — MISREPAIRED (BS 280) · airframe 24,988 hrs · 17,412 cycles

LT 280 CROSSBEAM LOWER TITANIUM DOUBLER 7 OFF FASTENER HAVE LOW E/D. REPAIRED IAW SRM 51-40-11-001-001-A01 & REO 670-53-11-836. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: MOUNT — CORRODED (GALLEY) · airframe 24,988 hrs · 17,412 cycles

RT GALLEY FITTING AT RBL 21 FLOOR SUPPORT BETWEEN FS 280 - 295 HAS DEEP CORROSION. R & R GALLEY FITTING IAW SRM 51-42-21-001-001.

Part: SEAT TRACK — CORRODED (BS 724) · airframe 24,983 hrs · 17,408 cycles

SIDE SEAT RAIL ON LT SIDE AT FS 724 HAS 2 SPOTS OF CORROSION. REPAIRED IAW REO 670-53-00-343 & AMM 53-00-49-000-801, 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 24,983 hrs · 17,408 cycles

FS280 FLOOR SUPPORT FOR 221ALF IS CORRODED. REMOVED & DRILLED UP NEW FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001, 51-42-21-001-001, & 51-40-1-001-001. INSTALLED AFT COCKPIT FLOOR SUPPORT ANGLE AT FS280 IAW SRM 51-42-06-001-004-A01. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 24,993 hrs · 17,416 cycles

RT FLOOR SUPPORT CORRODED AT BS 280. REMOVED FLOOR SUPPORT IAW SRM 51-42-06. LOCATED AND DRILLED MOUNTING HOLES TO FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01. INSTALLED THE RT FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-45-00-001-001-A01, DWG SH670-32170, AND AMM 53-21-23-400-801.

Part: WEB — CORRODED (BS 280) · airframe 24,983 hrs · 17,408 cycles

LT BS 280, WEB CORRODED. REPAIRED IAW SRM 53-11-10-201-003-A01 AND REO 670-53-11-594.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,983 hrs · 17,408 cycles

LT BS 280 FLOORBEAM CORRODED. REPAIRED IAW SRM 53-11-41-201-003-A01. REPAIR CLASSIFIED AS MAJOR.

Part: WEB — CORRODED (BS 280) · airframe 24,983 hrs · 17,408 cycles

RT BS 280 WEB CORRODED. REPAIRED IAW SRM 53-11-10-201-003-A01 AND REO 670-53-11-594.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1047) · airframe 24,983 hrs · 17,408 cycles

RT FLOOR SUPPORT CORRODED BETWEEN FS 1031 AND 1047. REPAIRED IAW SRM 51-21-06-001-001-A01 & REO 670-53-61-970.

Part: SEAT TRACK — CORRODED (BS 379) · airframe 24,983 hrs · 17,408 cycles

SEAT TRACK AT FS 379 IS CORRODED. REPAIRED IAW REO 670-53-00-343 & AMM 53-00-49-400-801-A03.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,983 hrs · 17,408 cycles

RT BS 280 FLOORBEAM CORRODED. REPAIRED IAW SRM 53-11-41-201-003-A01. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CORRODED (BS 319.7) · airframe 24,986 hrs · 17,411 cycles

IN THE MAIN AVIONICS COMPARTMENT WHILE PERFORMING AN INTERNAL ZONE INSPECTION, CORROSION WAS FOUND ON THE FWD SIDE OF FRAME 319.7 BETWEEN S26-27L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CORRODED (BS 785.15) · airframe 24,983 hrs · 17,408 cycles

SIDE SEAT RAIL ON LT SIDE AND AT FS 785.15 HAS 2 SPOTS OF CORROSION. REPAIRED IAW REO 670-53-00-343, AMM 53-00-49-000-801, 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · airframe 24,983 hrs · 17,408 cycles

FLOOR SUPPORT AT ASD THRESHOLD IS CORRODED. R & R FLOOR SUPPORT IAW SRM 51-42-06-001-001.

Part: SEAT TRACK — CORRODED (BS 549) · airframe 24,983 hrs · 17,408 cycles

SEAT TRACK ON LT SIDE AND AT FS 549 HAS ONE SPOT OF CORROSION. REPAIRED IAW REO 670-53-00-343, AMM 53-00-49-000-801 & 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 24,983 hrs · 17,408 cycles

AFT CARGO DOOR FLOOR SUPPORT CORRODED. REPAIRED IAW REO 670-53-61-913.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 24,988 hrs · 17,412 cycles

IN THE MAIN AVIONICS COMPARTMENT THE SUPPORT FOR THE CRAWLWAY FLOORBOARD THAT IS ATTACHED TO THE FRAME BS 280 IS CORRODED. REMOVED DAMAGE CRAWLWAY FLOOR SUPPORT AND INSTALLED IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 24,983 hrs · 17,408 cycles

RT FLOOR SEAT TRACK AT FS 349 IS CORRODED. REPAIRED IAW REO 670-53-00-343 & AMM 53-00-49-400-801.

Part: SKIN — CHAFED (BS 980) · airframe 24,983 hrs · 17,408 cycles

AFT FUSELAGE LOWER SKIN CHAFED AT APROX FS 980. REPAIRED IAW REO 670-53-00-290. REPAIR CLASSIFIED AS MAJOR.

Part: COWLING — GOUGED (RT NACELLE) · airframe 24,983 hrs · 17,408 cycles

GOUGE DAMAGE ON THE INTERIOR OF THE RT ENGINE FWD CORE COWL. REPAIRED IAW GREO 670-54-23-959. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (PAX DOOR) · airframe 24,983 hrs · 17,408 cycles

PAX DOOR INNER SKIN CORRODED AT NUTPLATES UNDER PANELS 832FL, EL, DL, CL, BL AND AL. REMOVED CORROSION FROM PAX DOOR INNER SKIN AT NUTPLATES UNDER PANELS 832FL, EL, DL, CL, BL AND AL IAW SRM 51-21-06-001-001-A01. REPAIRED IAW REO 670-53-11-712.

Part: WIRE — DAMAGED · airframe 24,983 hrs · 17,408 cycles

ICG POWER LEAD WIRE G1 T3 (ORANGE WIRE) GOUGED 3" OTBD OF LT PYLON. REPAIRED WIRING IAW REO 670-24-21-001 AND ESPM 20-33-00. REPAIR CLASSIFIED AS MAJOR.

Part: SILL — CRACKED (FUSELAGE) · airframe 24,983 hrs · 17,408 cycles

THERE IS A CRACK IN THE SILL IN THE FWD AVIONICS COMPARTMENT AT THE FRAME AND THE ADG HYD PUMP RT SIDE. COMPLIED WITH EC/TC REO 670-53-11-509 AND GENERIC REO 670-53-11-509, REV. DATED: 7/6/10 AS WRITTEN. REPAIR CLASSIFIED AS MAJOR.

Part: STRUCTURE — CRACKED (E/E BAY) · airframe 24,993 hrs · 17,416 cycles

THERE IS A CRACK IN THE SILL IN THE FWD AVIOICS COMPARTMENT AT THE FRAME LT SIDE. REPAIRED IAW EC/TC REO 670-53-11-509 AND GENERIC REO 670-53-11-509, REV AND REO 670-53-11-835. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DENTED (BS 1036-1051.3) · airframe 24,993 hrs · 17,416 cycles

SKIN HAS SEVERAL DENTS BETWEEN BS 1036 AND 1051.3 AND S25 AND 27. REPAIRED IAW SRM 53-61-01-101-007-A01. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 1031-1051) · airframe 24,992 hrs · 17,415 cycles

FUSELAGE FROM S22-26R, BS 1031-1051 HAS BLENDED AREAS. REPAIRED IAW REO 670-53-61-968. REPAIR CLASSIFIED AS MAJOR.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 23,842 hrs · 16,565 cycles

CLIMB OUT, FL 250, F/O WINDOW ARCED OUTER WINSHIELD PANE CRACKED LOWER RT CORNER, RT WING. ACFT RETURNED EMERGENCY DECLARED. R & R FO'S WINDSHIELD IAW AMM 56-11-01. , OP'S AND LEAK CHECKED. SDR CLOSED.

Part: CIRCUIT BREAKER — TRIPPED (NLG STEERING) · airframe 23,688 hrs · 16,456 cycles

STEERING INOPERATIVE CAUTION MESSAGE ON CLIMB OUT, EMERGENCY DECLARED. RESET SYS IAW FIM, PAGE 40 IAW MCC, NO FURTHER ACTION REQUIRED.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 23,502 hrs · 16,306 cycles

MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,140 hrs · 15,305 cycles

EMERGENCY EXIT FLOOR FLOODLIGHT AT PAX DOOR IS INOPERATIVE. R & R NR 2 BATTERY PACK CHARGER IAW AMM 33-51-17 AND AIPC 33-51-17, ITEM 8. PERFORMED OP TEST OF EMERGENCY LIGHTS IAW AMM 33-51-15-710-801. NO FAULTS FOUND AT THIS TIME.

Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 21,875 hrs · 15,117 cycles

F/A MEGPHONE INOPERATIVE. REPLACED BATTERY IN MEGPHONE IAW AMM 25-61-14.

Part: GLOWSTRIP — DETERIORATED · airframe 21,468 hrs · 14,841 cycles

EMERGENCY FLOOR GLOWSTRIPS DELAMINATED. INSTALLED EMERGENCY GLOWSTRIPS ON FLOOR AND PASSENGER ISLE IAW AMM 25-25-00.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,794 hrs · 14,381 cycles

FLOOR LEVEL EMERGENCY FLOOD LIGHT AT ENTRYWAY IS INOPERATIVE. R & R BATTERY CHARGER NR 1 FOR EMERGENCY LIGHTS IAW AMM 33-51-17. ALL CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,768 hrs · 14,361 cycles

FLOOR LEVEL EMERGENCY FLOOD LIGHT AT ENTRY WAY IS INOPERATIVE. R & R BATTERY CHARGER NR1 FOR EMERGENCY LIGHTS IAW AMM 33-51-17. CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,768 hrs · 14,361 cycles

SEVERAL EMERGENCY EXIT BULBS INOPERATIVE. RELAMPED EMERGENCY EXIT BULBS IAW AMM 33-51-05, OP'S CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,522 hrs · 14,189 cycles

THIRD FROM FRONT, CABIN CEILING EMERGENCY LIGHT INOP. RELAMPED NR 3 CEILING EMERGENCY LIGHT AS REQUIRED. OPS CHECK GOOD IAW AMM 33-51-00. RELAMPED NR 3 CEILING EMERGENCY LIGHT AS REQUIRED. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 20,269 hrs · 14,016 cycles

EMERGENCY EXIT FLOOR LEVEL FLOOD LIGHT AT SEAT 12CD HAS SEVERAL BULBS INOP. RELAMPED EMERGENCY EXIT FLOOR LEVEL FLOOD LIGHTS AT SEATS 12. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 20,269 hrs · 14,016 cycles

EMERGENCY EXIT FLOOR LEVEL FLOOD LIGHT AT SEAT 12AB HAS BULBS INOP. RELAMPED. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: STRINGER — CORRODED (BS 280 S27) · airframe 20,017 hrs · 13,843 cycles

STRINGER 27 AT FS 280.00 IS CORRODED. FABRICATED STR 27 IAW REO 670-53-21-695, STEP 1. TCAS OMNI DIRECTIONAL TEST OF THE TCAS IAW AMM 34-43-00-710-801. INSTALLED TCAS OMNI DIRECTIONAL ANTENNA IAW AMM 34-43-07-400-801. PERFROMED OPS TEST OF THE TCAS IAW AMM 34-43-00-710-801. OPS TESTED GOOD. COMPLETED ALL STEPS OF REO 670-53-21-695, RECEIVED AND COMPLIED WITH REO 670-53-21-695.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 20,009 hrs · 13,838 cycles

LT SIDEWALL SEAT TRACK FROM FS 785-863 CORRODED. RECEIVED AND COMPLIED WITH REO 670-53-00-311, REV A.

Part: BEAM — CRACKED (FUSELAGE) · airframe 19,990 hrs · 13,824 cycles

UPON REMOVAL OF INTERCOSTAL INBD BEAM, PN MM670-35326-003, FOUND CRACKED. R & R BEAM IAW SRM 51-42-06. FABRICATED, INSTALLED, SEALED, TREATED, PRIMED & PAINTED REPAIR PARTS IAW STEPS 3-6 PF STS EA 05-2011-224 AND SRM 51-42-21-001-001 & 51-42-06-001-001.

Part: FRAME — CORRODED (BS 310) · airframe 19,990 hrs · 13,824 cycles

AVIONICS COMPARTMENT AT FS 310.00 BETWEEN STR 26L AND STR 27 HAS A SMALL AREA OF CORROSION. COMPLIED WITH REO 670-53-21-693 STEPS 1-5

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 19,990 hrs · 13,824 cycles

WEB ATTACH ANGLE AT RBL 26 IS CRACKED. FABRICATED ATTACH ANGL IAW DWG CC 670-34117, REV B. SH 88030. DRILLED NEW ANGLE AND INSTALLED IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01. MINOR REPAIR.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 19,990 hrs · 13,824 cycles

FOUND RBL AND LBL 9.0 TEE BRACKET CRACKED. REMOVED AND REPLACED TEE BRACKETS.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,990 hrs · 13,824 cycles

ASD UPPER SILL ANGLE ATTACHED TO FUSELAGE IS CORRODED. REMOVED ASD UPPER SILL ANGLE (MID) CAP) IAW SRM 51-41-02-001-001-A01. RECEIVED AND DRILLED UP NEW UPPER SILL ANGLE COUNTER SUNK AND INSTALLED NUT PLATES REF SRM 51-42-06 AND SRM 51-40-11-001-001. THIS IS A MINOR REPAIR. INSTALL UPPER SILL ANGLE. INSTALLED ASD UPPER SILL ANGLE REF SRM 51-42-06 AND SRM 51-41-02-001-001-A01. THIS IS A MINOR REPAIR. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 669-713) · airframe 19,990 hrs · 13,824 cycles

LT SIDEWALL SEAT TRACK FROM FS 669.00 - 713.00 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, DAMAGE EXCEEDS LIMITS. REMOVED SEAT TRACK IAW SRM 51-41-02-001-001-A01. INSTALLED SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 613) · airframe 19,990 hrs · 13,824 cycles

RIGHT SEAT RAIL CORRODED AT FS 613.00. SEAT TRACK OUT OF LIMITS IAW SRM 53-31-49-991-804. SEAT TRACK REMOVED AND REPLACED IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 713-761) · airframe 19,990 hrs · 13,824 cycles

RT SIDEWALL SEAT TRACK FROM FS 713.00 - FS 761.00 IS CORRODED AND GOUGED. MEASURED GOUGE AND FOUND TO BE OUT OF LIMITS. DAMAGE MEASURED 0.55" DONE IAW 53-41-49-101-001. R & R RT SEAT RAIL AT FS 713-761.00 WITH NEW SEAT RAIL WORK DONE IAW AMM 53-00-49-400-801 (A03) AND 53-00-49-000-801(A03) THIS IS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 517-579) · airframe 19,990 hrs · 13,824 cycles

RIGHT SEAT TRACK FLOOR SEGMENT (TOP AND SIDE) FROM FS 517 TO FS 579 IS CORRODED. REMOVED SEAT TRACK FROM FS485-581 IAW 51-41-02-001-001-A01 AND 51-41-02-001-001-A01. INSTALLED SEAT TRACK FS 485-581 IAW SRM 51-41-00-001-001-A01 AND 51-41-02-001-001-A01. THIS IS A MINOR REPAIR.

Part: STRUCTURE — CORRODED (BS 310 S26-27L) · airframe 19,990 hrs · 13,824 cycles

AVIONICS COMPARTMENT AT FS 310.00 BETWEEN STR 26L AND STR 27 HAS A SMALL AREA OF CORROSION. BLENDED OUT CORROSION IAW SRM 51-21-06-001-001-A01 AND 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 581-669) · airframe 19,990 hrs · 13,824 cycles

RT SEAT TRACK FLOOR SEGMENT FROM FS 581 TO FS 669.40 CORRODED, ESPECIALLY AROUND SCREW HOLES. UPON FURTHER INSPECTION FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED SEAT TRACK FS 581-683.4 IAW SRM 51-41-00-001-001-A01 AND 51-41-02-001-001-A01. INSTALLED NEW SEAT TRACK AT FS 581-683 IAW SRM 51-41-00-001-001-A01 AND 51-41-02-001-001-A01 THIS IS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 669-713) · airframe 19,990 hrs · 13,824 cycles

RT SIDEWALL SEAT TRACK FROM FS 669.00 - 713.00 IS CORRODED. REMOVED CORROSION IAW SRM 51-41-02-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-47-51-101, 53-31-51-101, 53-31-43-101-001-A01. CUT TO LENGTH & DRILLED SCREW HOLES & COUNTER SUNK & INSTALLED NEW SEAT TRACK IAW REO 670-53-00-311 & AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 713-761) · airframe 19,990 hrs · 13,824 cycles

LT SIDEWALL SEAT TRACK FROM FS 713.00 - 761.000 IS CORRODED. MINOR REPAIR. REMOVED CORROSION FROM SEAT TRACK BETWEEN FS.713.00 AND 761.00 MAX MATERIAL REMOVED WAS .052" THIS WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001. R & R SEAT TRACK. R & R SEAT RAIL AT FS 713.00-716.00 WITH NEW SEAT RAIL (LT) IAW AMM 53-00-49-000-801 (A03) AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 19,990 hrs · 13,824 cycles

LEFT SIDEWALL SEAT TRACK FROM FS 785.00 - 863.000 IS CORRODED. FOUND SEAT TRACK BEYOND LIMITS OF SRM 53-41-51. REMOVED SEAT TRACK IAW SRM 51-41-00-001-001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SUPPORT FITTING — CORRODED (S 265-280 S27) · airframe 19,990 hrs · 13,824 cycles

CORROSION ON NOSE JACK FITTING SUPPORTS AT S27 AND FS 265 AND FS 280. REMOVED NOSE JACK FITTING SUPPORTS & DRILLED NEW SUPPORTS IAW SRM 51-42-06-001-001-A01. INSTALLED NOSE JACK FITTING SUPPORTS IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 19,990 hrs · 13,824 cycles

RT SIDEWALL SEAT TRACK FROM FS 785.00-863.00 IS CORRODED. REMOVED SEAT TRACK IAW SRM 51-41-00-001-001-A01. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM. REPLACE SEAT TRACK WITH NEW. INSTALLED IAW SRM 51-41-00-001-001-A01. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 581-669.4) · airframe 19,990 hrs · 13,824 cycles

LEFT SEAT TRACK FLOOR SEGMENT CORRODED FROM FS 581 TO FS 669.40. UPON FUTHER INSP FOUND SEAT TRACK FS 581-669.40 TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED SEAT TRACK IAW 51-41-001-001-A01 AND 51-41-02-001-001-A01. SRM. INSTALLED NEW SEAT TRACK FOR FS 581-669.40 IAW AMM 53-00-49-400-801. THIS IS A MINOR REPAIR.

Part: BULKHEAD — CORRODED (BS 280) · airframe 19,990 hrs · 13,824 cycles

CO-PILOTS BULKHEAD AFT SIDE FS 280.00 JUST ABOVE WL 72.50 WEB CORRODED. REMOVED, DRILLED, AND INSTALLED NEW BULKHEAD IAW SRM 51-42-13-001-001-A01 AND 51-42-06-001-001-A01. MAJOR REPAIR.

Part: STRUCTURE — CORRODED (BS 280) · airframe 19,990 hrs · 13,824 cycles

FS 280.00 CORRODED BETWEEN LBL 36.00 AND RBL 36.00. REMOVED AND INSTALLED NEW FLOORBEAM IAW REO 670-53-11-047.

Part: SEAT TRACK — CORRODED (BS 549) · airframe 19,990 hrs · 13,824 cycles

LEFT SEAT RAIL CORRODED AT FS 549.00. REMOVED CORROSION FROM LT SIDE SEAT RAIL AT FS. 549.00 MAX MATERIAL REMOVED WAS .049", FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED UNSERVICEABLE SEAT RAIL FROM LT SIDE WALL FROM FS.477.4 TO 573. IAW AMM 53-00-49-000-801. INSTALLED NEW SERVICABLE SEAT RAIL IAW AMM 53-00-49-400-801.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 19,990 hrs · 13,824 cycles

SERVICE GALLEY DOOR LOWER SILL ANGLE ATTACHED TO FUSELAGE IS CORRODED. REMOVED CORROSION FROM SILL ANGLE, ORIG MAT .063 REMOVED .015 REMAINING .048. FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED AND INSTALLED SILL ANGLE IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 847-909) · airframe 19,990 hrs · 13,824 cycles

CABIN LEFT SEAT TRACK HAS CORROSION AT APROX FS 847.00 TO FS 909.00. DAMAGE EXCEEDS LIMITS OF SRM 53-51-49. REMOVED SEAT TRACK IAW SRM 51-41-00-001-001-A01 AND INSTALLED CABIN SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 847-909) · airframe 19,990 hrs · 13,824 cycles

CABIN RIGHT SEAT TRACK HAS EVIDENCE OF CORROSION AT APROX FS 847.00 TO FS 909.00. REMOVED SEAT TRACK IAW SRM 51-41-00-001-001-A01 AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 518) · airframe 19,990 hrs · 13,824 cycles

LEFT SEAT RAIL CORRODED AT FS 518.00. REMOVED CORROSION FROM LT SIDE SEAT TRACK AT FS 581.00 MAXIMUM MATERIAL. REMOVED WAS .045", FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED UNSERVICEABLE SEAT RAIL FROM LT SIDE WALL FROM FS.573.00 TO 669.4 IAW AMM 53-00-49-000-801. INSTALLED NEW SERVICABLE SEAT RAIL ON LT SIDE WALL FROM FS 573.00 TO 669.4 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581) · airframe 19,990 hrs · 13,824 cycles

RIGHT SEAT RAIL CORRODED AT FS 581.00. SEAT TRACK OUT OF LIMITS IAW SRM 53+31-49-991-804. REMOVED AND INSTALLED SEAT TRACK IAW AMM 53-00-49-000-801.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 19,990 hrs · 13,824 cycles

AVIONICS COMPARTMENT FLOORBOARD SUPPORT BRACKET AT FS 280.00 IS CORRODED ON THE UPPER AND LOWER SURFACES. REPLACED FLOORBOARD SUPPORT BRACKET. REMOVED FLOORBOARD SUPPORT BRACKET IAW SRM 51-42-06-001-001-A01. DRILLED NEW BRACKET IAW SRM 51-42-06-001-001-A01. THIS IS A MINOR REPAIR. INSTALL FLOORBOARD SUPPORT BRACKET. INSTALLED NEW FLOORBOARD SUPPORT BRACKET IAW SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01, AND 51-42-06-001-001-A01. THIS IS A MINOR REPAIR.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,990 hrs · 13,824 cycles

ASD LOWER SILL ANGLE ATTACHED TO FUSELAGE IS CORRODED. REMOVED ASD LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01 AND 57-42-21-001-001-A01. RECIEVED AND DRILLED UP NEW ANGLE COUNTER SUNK AND INSTALLED NUT PLATES REF SRM 51-42-06-001-001 MINOR REPAIR. INSTALL LOWER SILL ANGLE. OK TO INSTALL LOWER SILL ANGLE MAC1QC INSTALLED LOWER SILL ANGLE REF SRM 51-42-06-001-001 AND SRM 51-42-06-001-001 AND 51-42-21-001-001. THIS IS A MINOR REPAIR. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 863-977) · airframe 19,990 hrs · 13,824 cycles

RT SIDEWALL SEAT TRACK FROM FS 863.00 - FS 977.00 IS CORRODED. STARTED REMOVING CORROSION ON RT SIDEWALL SEAT TRACK AT FS 863.00-977.00 IAW SRM 51-21-06-001-001-A01. SEAT TRACK OUT OF LIMITS IAW SRM 53-31-49-001-804. REMOVED SEAT TRACK IAW AMM 53-0049-000-801 FROM FS 863- FS 977 RT SIDE WALL. INSTALL SERVICEABLE SEAT TRACK. INSTALLED NEW SERVICEABLE SEAT RAIL ON RT SIDEWALL FROM FS 863-00 TO 977.00 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 613) · airframe 19,990 hrs · 13,824 cycles

LEFT SEAT RAIL CORRODED AT FS 613.00. R & R UNSERVICABLE SEAT RAIL ON LT SIDE WALL FROM FS 573.00 TO 669.4 IAW AMM 53-00-49-000-801 AND 53-00-49-400-801. MINOR REPAIR.

Part: BULKHEAD — CORRODED (BS 280) · airframe 19,990 hrs · 13,824 cycles

PILOT'S BULKHEAD AFT SIDE JUST ABOVE WL 72.50 WEB CORRODED AT FS 280.00. BLENDED CORROSION IAW SRM 53-11-10-201-003-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW NDT INSPECTION PROCEDURE UT-3. MININUM MATERIAL REMAINING IS .038". ORIGINAL MATERIAL THICKNESS IS .040" MATERIAL REMOVED IS .002", WITHIN LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRED IAW REO 670-53-11-598.

Part: SEAT TRACK — CORRODED (BS 570) · airframe 19,990 hrs · 13,824 cycles

RIGHT SEAT TRACK CORRODED AT FS 570.00. FOUND OUT OF LIMITS IAW SRM 53-31-49-991-804. REMOVED SEAT TRACK IAW AMM 53-06-49-000-801. INSTALLED NEW SEAT SIDE RAIL IAW AMM 53-00-49-400-801-A03.

Part: STRINGER — CORRODED (BS 280) · airframe 19,990 hrs · 13,824 cycles

STRINGER 27 AT FS 280.00 IS CORRODED. REMOVED STRINGER IAW SRM 51-42-06-001-001-A01. INSTALLED STRINGER IAW REO 670-53-21-695.

Part: SEAT TRACK — CORRODED (BS 549-579) · airframe 19,990 hrs · 13,824 cycles

LT SEAT TRACK FLOOR SEGMENT CORRODED FROM FS 549 TO FS 579. UPON FUTHER INSP FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED SEAT TRACK FS 485-581 MAR IAW SRM 51-41-02-001-001-A01 AND 51-41-00-001-001-A01. INSTALLED NEW SEAT TRACK AT FS 485-581 IAW AMM 53-00-49-400-801. THIS IS A MINOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 364 S27R) · airframe 19,990 hrs · 13,824 cycles

CORROSION ON INTERCOSTAL AT 27R STRINGER AND FS 364. REMOVED INTERCOSTAL, IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: PLACARD — MISSING (CABIN) · airframe 19,990 hrs · 13,824 cycles

CREW ESCAPE EMGERENCY EXIT EXTERIOR INSTRUCTION PLACARD HARD TO READ, ARROW FADED AND OPEN PLACARD MISSING. REPLACE PLACARDS IAW AMM 20-60-11-400-801.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 19,818 hrs · 13,714 cycles

MEGAPHONE IS INOP AND REQUIRES REPLACING. R & R MEGAPHONE IAW AMM 25-61-14. OPS CHECK GOOD. R & R MEGAPHONE IAW AMM 25-61-14. OPS CHECK GOOD.

Part: LAMP — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 17,927 hrs · 12,371 cycles

EXTERIOR EMERGENCY LIGHT AFT OF LT EMERGENCY EXIT DIM. R & R LAMP IN EMERGENCY LIGHT DS51 IAW AMM 33-51-15. OPS CHECK GOOD.

Part: HANDLE — UNSECURE (PAX DOOR) · airframe 17,174 hrs · 11,795 cycles

PASSENGER DOOR LATCH CAUTION MESSAGE RECEIVED AFTER TAKEOFF ACCOMPANIED BY PROX SYS FAULT 1 MESSAGE AND RED DOOR HANDLE MECHANICAL INDICATING RED AND PAX DOOR WARNING AT TOUCH DOWN. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) WHEN ACFT ARRIVED AT GATE, FOUND PAX DOOR OUTER HANDLE OPEN APPROX 4 INCHES INSPECTED, CYCLED PAX DOOR AND NO DEFECTS WERE NOTED. PERFORMED OPS TEST OF PAX DOOR IAW AMM 52-11-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,060 hrs · 10,188 cycles

FS 280.00 FWD FLOOR SUPPORT FOR FLIGHTDECK FLOORBOARD CORRODED. REMOVED CORRODED FLOOR SUPPORT IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED FLOOR SUPPORT IAW SRM 51-42-06 & 51-42-21.

Part: NUT PLATE — BROKEN (FUSELAGE) · airframe 15,060 hrs · 10,188 cycles

NUT PLATE BROKE AT STA 349 RBL36 ON FLOOR STRUCTURE UNDER GALLEY NR 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,060 hrs · 10,188 cycles

SEQ 213 \ 2000-0088 SEAT TRACK CORRODED BY FWD LAV.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,060 hrs · 10,188 cycles

FS 280.00 FLOOR SUPPORT BEAM HAS CORROSION ON UPPER FLANGE AT LBL 9.00 & RBL 9.00. REMOVED CORRODED SECTION OF FLOOR SUPPORT IAW REO 670-53-11-414. FABRICATED AND INSTALLED UPPER FLANGE REPAIR FILLERS. TREATED & PRIMED REWORKED SECTION.

Part: FADEC — MALFUNCTIONED (LT ENGINE) · airframe 14,812 hrs · 10,000 cycles

ONE MINUTE AFTER T/O DURING CLIMBOUT GOT L FADEC CAUTION. RAN QRH RETURN TO ATL L ENG INDICATIONS WERE NORMAL FOR ENTIRE FLIGHT. L FADEC CAUTION WAS STEADY FOR ENTIRE FLIGHT. EMERGENCY DECLARED. LT 5125 DEL 81 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,608 hrs · 9,825 cycles

EMERGENCY EXIT LIGHT LOWER AFT OF SERVICE DOOR HAS SEVERAL BULBS BURNED OUT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,984 hrs · 9,315 cycles

EMERGENCY EXIT FLOODLIGHT T PAX DOOR INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,115 hrs · 8,219 cycles

CABIN AFT MOST CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED CABIN AFT MOST CEILING EMERGENCY LIGHT BULB. OPS CHECK GOOD.

Part: ENGINE — SURGES (LEFT) · airframe 12,342 hrs · 8,087 cycles

ON TAKEOFF - LT ENGINE SURGING FROM TAKEOFF POWER TO IDLE. FOLLOWED QRH AND PERFORMED LT ENGINE SHUTDOWN AND RETURNED TO MEM. FLT 4230 CX. AIRCRAFT RETURNED TO ATL AFTER T/O. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. EMERGENCY DECLARED.

Part: DOOR — BINDING (PAX DOOR) · airframe 12,321 hrs · 8,071 cycles

PAX ENTRANCE DOOR DIFFICULT TO OPEN. FLT 4188 DEL 31 MINS.

Part: DOOR — STUCK (PAX DOOR) · airframe 12,237 hrs · 8,009 cycles

MAIN PAX DOOR CANNOT BE OPENED FROM THE OUTSIDE.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 10,799 hrs · 7,000 cycles

COCKPIT AFT FLOOR LAND CORRODED.

Part: BEAM — CORRODED (FUSELAGE) · airframe 10,799 hrs · 7,000 cycles

THE 280 TRANSVERSE BEAM HAS MINOR CORROSION ON TOP SIDE BETWEEN LBL 9 AND RBL 9.

Part: WARNING SYSTEM — ACTIVATED (EXTINGUISH SYS) · airframe 9,858 hrs · 6,317 cycles

APU SQUIB AND APU BOTTLE LOW MESSAGES. APU FIRE EXTINGUISHING SYSTEM - APU INOPERATIVE.

Part: LIGHT — WEAK (CABIN) · airframe 9,162 hrs · 5,874 cycles

AFT EMERGENCY LIGHT DIM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,489 hrs · 5,456 cycles

REAR CEILING EMERGENCY LIGHT 1EA INOP.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,726 hrs · 5,005 cycles

PAX DOOR SILL AREA HAS CORROSION. (MARKED)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,726 hrs · 5,005 cycles

RIGHT FLOOR TRACK CORROSION -SEC 1- FS 350 TO 485. TRACK OUT OF LIMITS PER REO 670-53-00-013 REMOVED AND REPLACED RT FLOOR TRACK SEC 1 -FS 350 TO 485 IAW CRJ700 AMM 53-00-49 (CLOSED)

Part: DOOR — FAILED (OVERWING EXIT) · airframe 7,726 hrs · 5,005 cycles

LEFT OVERWING EMERGENCY EXIT WOULDN'T PASS THE FUNCTIONAL TEST (PULL TEST TOO HARD).

Part: SILL — CORRODED (FUSELAGE) · airframe 7,726 hrs · 5,005 cycles

RT SIDE FLOOR SILL, JUST AFT OF FS 280 CORRODED (MARKED). REPAIRED PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 7,726 hrs · 5,004 cycles

LT FS280 WEB CORRODED.

Part: WEB — CORRODED (FUSELAGE) · airframe 7,726 hrs · 5,004 cycles

RT FS280 WEB CORRODED.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 7,726 hrs · 5,004 cycles

FS280 CROSSBEAM CORRODED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,726 hrs · 5,005 cycles

PAX DOOR AFT SIDE PANEL DRAG BRACE ANGLE CRACKED NEAR MOTOR CABLE PULLEY. (MARKED)

Part: HANDLE — CRACKED (PAX DOOR) · airframe 7,726 hrs · 5,004 cycles

PAX DOOR OUTER HANDLE CRACKED (MARKED).

Part: SWIVEL FITTING — DAMAGED (PAX DOOR) · airframe 7,726 hrs · 5,005 cycles

PAX DOOR AFT CABLE ANCHOR SWIVEL ARM HOLE ELONGATED. (MARKED) REFER TO EO700-52-34 C/W ON RIMP W/O.

Part: SUPPORT ANGLE — CRACKED (VERTICAL STAB) · airframe 7,726 hrs · 5,004 cycles

CRACK FOUND VERTICAL STABILIZER SUPPORT ANGLE AT 67.5 PERCENT REAR DATUM AND LT EXTERNAL REAR FUSELAGE.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 7,726 hrs · 5,005 cycles

E/EXIT LIGHT COVER ABOVE SERVICE DOOR CRACKED.

Part: COVER — CRACKED (CABIN) · airframe 7,726 hrs · 5,004 cycles

EMERGENCY EXIT LIGHT COVER ABOVE SERVICE DOOR CRACKED.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 7,411 hrs · 4,810 cycles

NWS STEERING INOP, CAUTION MSG APPEARED ON CLIMBOUT (FL270-GEAR UP). ON ARRIVIAL SLC MX SUGGESTED CYCLING 2 CB"S, CLEARED THE MSG, NORMAL STEERING FOR LANDING AND TAXI. FLT 4434 DEL 36 MINS (TOWER DECLARED AN EMERGENCY).

Part: DOOR — MALFUNCTIONED (PAX DOOR)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO CLOSE AND FELL RAPIDLY AFTER OPENING. MAINTENANCE PERFORMED AN OPERATIONAL CHECK ON THE PASSENGER DOOR. NO DEFECTS NOTED PASSENGER DOOR OPERATED NORMALLY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M)