N758EV

Part: STRIKER — GOUGED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

PAX DOOR CUT OUT LOWER SEAL STRIKER SECTION HAS GOUGE IN SEVERAL AREAS ON LIP. REMOVED AND INSTALLED NEW PAX DOOR LOWER SEAL STRIKER SRM 51-42-21-001-001-A01 AND DWG SH670-31886 REV A. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD.

Part: HINGE — GOUGED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

THE PAX DOOR SIDE HINGE LUGS 24 AND 26 ARE GOUGED AND BETWEEN 25 AND 26, AND 26 AND 27 LANDS ARE CHAFED. BLENDED GOUGE DAMAGE ON LUGS NR 24 AND 26 AND LUG LANDS BETWEEN 25 AND 26, 26 AND 27 REF REO 670-52-11-511 REV -E DATE 2017-08-02 DISPOSITION TYPE 1 AND TYPE 4 STEP 1 HINGE FOUND TO BE WITHIN LIMITS, NO DEFECTS FOUND. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: DOUBLER — MISINSTALLED (ZONE 100) · airframe 39,285 hrs · 28,696 cycles

DURING AUDIT OF RA 44067, FUSELAGE SKIN DOUBLER BTWN BS 349 AND 364, S19 - 23L IAW REO 670-53-21-504, REV. A. FOUND THAT ONE EXTRA FASTENER INSTALLED IN THE REPAIR AS DEPICTED IN THE REO DRAWING. RECEIVED MHI REO 670-53-21-504 REV -B, UPDATES THE REPAIR PERFORMED ON FUSELAGE SKIN DOUBLER BETWEEN BS 349 & 364 S19 - 23L SHOWN IN REO 670-53-21-504, REV -A , INCORPORATING THE ADDITIONAL FASTENER FOUND IN STEP 2 OF THIS CONTINUATION FORM AND MEET ALL THE REO REV -B REQUIREMENT. NO FURTHER ACTION IS REQUIRED; REPETITIVE INSPECTIONS REQUIREMENTS ARE NO CHANGED COMPLIED WITH TC 51-900-1002-SKY.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

AFTER REMOVAL OF PAX DOOR INNER SKIN FOUND INTERCOSTAL DD2 (MID) CORRODED. REMOVED AND REPLACED WITH NEW, PAX DOOR MID INTERCOSTAL DD2 REF SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702 REV-N COMPLIED WITH TASK CARD 51-900-1002-SKY LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

AFTER REMOVAL OF PAX DOOR INNER SKIN FOUND INTERCOSTAL DD1 (MID) CORRODED. REMOVED MODERATE CORROSION FROM PAX DOOR INNER STRUCTURE MIDDLE INTERCOSTAL DD1 UPPER FLANGE AND WEB OUTSIDE & INSIDE SURFACES REF. SRM TASK 51-21-06-001-001-A01,INSTALLED NEW MIDDLE INTERCOSTAL DD1 PER SRM TASK 51-40-06-001-001-A01 , SRM TASK 51-42-06-001-001-A01 & SRM TASK 51-42-21-001-001-A01 REF. DWG. 601R31702 REV. -N ,FIT CHECK GOOD,LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

AFTER REMOVAL OF PAX DOOR INNER SKIN FOUND INTERCOSTAL DD2 (AFT) CORRODED. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD2 (AFT) REF SRM 51-42-06-001-001-A01 COMPLIED WITH TASK CARD 51-900-1002-SKY LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

AFTER REMOVAL OF PAX DOOR INNER SKIN FOUND INTERCOSTAL DD3 (MID) CORRODED. WET INSTALLED NEW REPLACEMENT MIDDLE INTERCOSTAL DD3 AT PAX DOOR INNER STRUCTURE PER SRM TASK 51-42-06-001-001-A01 & SRM TASK 51-42-21-001-001-A01 REF. DWG. 601R31702 REV -N . LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

AFTER REMOVAL OF PAX DOOR INNER SKIN FOUND INTERCOSTAL DD2 (FWD) CORRODED. REMOVED AND REPLACED WITH NEW PAX DOOR INNER SKIN FORWARD INTERCOSTAL DD2 IAW SRM 51-42-06-001-001-A01, LEAK CHECKED GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: HINGE — DAMAGED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

PAX DOOR FUSELAGE SIDE PIANO HINGE SEVERAL LUGS FAILED GO-NO-GO GAUGE. REMOVED AND INSTALLED NEW PAX DOOR HINGE TO FUSELAGE SIDE WITH DRIVE IN PLUGS AND LUBE FITTINGS PER SRM 53-21-23-201-007-A01 STEPS 4. J-T AND DWG SH670-31810 REV AE. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: FRAME — CORRODED (ZONE 100) · airframe 39,285 hrs · 28,696 cycles

FRAME AT FS 661.00 APPROX. STGR 27 CORRODED ON WEB (AFT SIDE). REPAIRED PER REO 670-53-31-1139 REV - AND SRM 51-41-02-001-001-A01. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

PASSENGER DOOR INTERNAL STRUCTURE, CORROSION WITHIN DOOR VENT AREA, REMOVED AND REPLACED PASSENGER DOOR MIDDLE INTERCOSTAL DD4 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-00-00-A01, AND DWG 601R31702, REV N. LEAK CHECKED GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

PASSENGER DOOR INTERNAL STRUCTURE, CORROSION UNDER PANEL 832DL, INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD3 REF DWG 601R31702 REV -N, SRM 51-42-06-001-001-A01. LEAK CHECKED GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: PLATE — CORRODED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

FOUND FWD CARGO DOOR SURROUND STRUCTURE JOINT PLATE AT BS 533 TO HAVE MULTIPLE SPOTS OF CORROSION. REPAIRED FWD CARGO DOOR SURROUND STRUCTURE JOINT PLATE IAW REO 670-53-31-1141, REV -. COMPLIED WITH ALL APPLICABLE STEPS SEE CONTINUE FOR WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: PLATE — CORRODED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

FOUND FWD CARGO DOOR SURROUND STRUCTURE JOINT PLATE AT BS 581 TO HAVE MULTIPLE SPOTS OF CORROSION. REPAIRED FWD CARGO DOOR SURROUND STRUCTURE JOINT PLATE IAW REO 670-53-31-1141, REV-. NO DEFECTS NOTED, ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · airframe 39,285 hrs · 28,696 cycles

CORROSION ON ATTACHMENT ANGLE BTWN BS 349 - 364, S26R. REMOVED AND REPLACED WITH NEW ATTACH ANGLE AT STGR 26R BETWEEN BS 349 - 364 IAW SRM 51-42-21-001-001-A01, AND DWG SH670-32050, REV J, COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: STAND OFF — CRACKED (ZONE 400) · airframe 39,285 hrs · 28,696 cycles

RIGHT LOWER TRANSCOWL INBD -A- BRACKET STANDOFF IS CRACKED. INSTALLED A NEW RT STAND OFF IAW REO 670-54-21-971, REV B. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: STIFFENER — DAMAGED (ZONE 400) · airframe 39,285 hrs · 28,696 cycles

RIGHT UPPER TRANSCOWL ZEE STIFFENER RIVETS ARE SHEARED. CRACKS FOUND IN INNER SKIN UNDER ZEE STIFFENER, REPAIRED INNER SKIN ON RT UPPER TRANSCOWL IAW REO 670-54-21-1787, REV -. COMPLIED WITH SKY CARD 51-900-1002-SKY.

Part: STIFFENER — DAMAGED (ZONE 400) · airframe 39,285 hrs · 28,696 cycles

LEFT UPPER TRANSCOWL ZEE STIFFENER RIVETS ARE SHEARED. LT UPPER TRANSCOWL ZEE STIFFENER REPAIRED IAW REO 670-54-21-1789, REV -. REFER TO CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.

Part: SKIN — GOUGED (ZONE 100) · airframe 39,285 hrs · 28,696 cycles

FOUND GOUGING & CORROSION ON FWD CARGO SURROUND STRUCTURE INNER CLOSING SKIN EDGE BETWEEN BS 533 AND 581. REPAIRED FWD CARGO SURROUND STRUCTURE INNER CLOSING SKIN IAW REO 670-53-31-1141 REV-. COMPLIED WITH ALL STEPS OF REO 670-53-31-1141 REV-. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: DOOR SILL — GOUGED (ZONE 200) · airframe 39,285 hrs · 28,696 cycles

FOUND GOUGED & CORRODED ON FWD CARGO SURROUND STRUCTURE S25L BETWEEN BS 533 - 581. REMOVED DAMAGE ON S25L (DOOR SILL) APPROX. BS 533 AND 581 IAW SRM 51-12-00-001-001-A01, COMPLIED WITH REO 670-53-31-1141 REV -. STEPS 1-3 AND, STEPS 8-10, STEPS 4-7. NOT APPLICABLE TO REPAIR AREA DONE ON THIS NRI. COMPLIED WITH 51-900-1002-SKY. ALL CHECKS GOOD.

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 39,285 hrs · 28,696 cycles

RIGHT TRU DOOR LOWER SILL HAS POSSIBLE CRACKS AT FWD AND AFT LATCH CUTOUTS. RT TRU DOOR LOWER SILL REPLACED AND INSTALLED IAW REO 670-53-11-2233 REV -A DATED 2025-12-22. ALL STEPS COMPLIED WITH ON THE REO, COMPLIED WITH 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: SPLICE PLATE — CRACKED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

AFT BAGGAGE BAY DOOR INTERNAL STRUCTURE, UPPER FORWARD SPLICE PLATE HAD A CRACK. REMOVED AND REPLACED CRACKED UPPER FORWARD SPLICE PLATE IN AFT BAGGAGE BAY DOOR INTERNAL STRUCTURE IAW SRM 51-42-06-001-001-A01, AND DWG CC670-38702, REV F. COMPLIED WITH SKYWEST CARD 51-900-1002-SKY.

Part: LINTEL — CRACKED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

PAX DOOR LINTEL HAS POSSIBLE CRACK AT THE FS.280.00 BULKHEAD. REPAIRED THE PAX DOOR LINTEL, APPROX BS 280 BULKHEAD IAW REO 670-53-21-493, REV D. AND SB 670BA-53-040, PART B, REV C. COMPLIED WITH ALL STEPS OF REO 670-53-21-493, REV D. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS.SERVICE BULLETIN 670BA-53-040, REVISION C. CENTER FUSELAGE, PRIMARY STRUCTURE BS 280 TO 295, INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR, PART B, INCORPORATED.

Part: DOOR FRAME — CHAFED (ZONE 200) · airframe 39,285 hrs · 28,696 cycles

RIGHT OVERWING EMERGENCY EXIT SURROUND STRUCTURE, FWD AND AFT UPPER AREA IS CHAFED. BLENDED THE CHAFING ON FWD & AFT UPPER AREA OF RIGHT OVERWING EMERGENCY EXIT SURROUND STRUCTURE. IAW SRM 51-12-00-001-001-A01, AND PERFORMED REPAIRS PER REO 670-53-41-785 REV -. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: DOOR FRAME — CHAFED (ZONE 200) · airframe 39,285 hrs · 28,696 cycles

LEFT OVERWING EMERGENCY EXIT SURROUND STRUCTURE, AFT UPPER CORNER IS CHAFED. REPAIRED CHAFE ON LT OVERWING EMERGENCY EXIT SURROUND STRUCTURE, AFT UPPER CORNER IAW REO 670-53-41-788, REV -. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: STRINGER — CORRODED (ZONE 100) · airframe 39,285 hrs · 28,696 cycles

CORROSION AT APPROX. BS 365 OTBD SIDE OF S26R. REMOVED AND INSTALLED A NEW STRINGER 26R SECTION BETWEEN BS 333 - 364 IAW SRM 51-42-06-001-001-A01, AND DWG SH670-31350, REV A. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKED GOOD.

Part: DOOR FRAME — DAMAGED (ZONE 200) · airframe 39,285 hrs · 28,696 cycles

FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE, FWD AND AFT LOWER HINGES ARE MARRED, BLENDED OUT DAMAGE ON FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE, FWD & AFT LOWER HINGES IAW SRM 51-12-00-001-001-A01 AND PERFORMED REPAIRS IAW REO 670-53-31-1141 REV-. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: SHAFT — DAMAGED (ZOEN 500 FLAP) · airframe 39,285 hrs · 28,696 cycles

LEFT WING INBOARD FLAP THE MOST OUTBOARD FLAP VANE ACTUATOR SHAFT HAS DAMAGE & GROOVED ON THE LOWER SURFACE. COMPLIED WITH GREO 670-57-52-257 REV -B FOR REPAIR OF LEFT WING INBOARD FLAPVANE ACTUATOR SHAFT, ALL CHECKS GOOD AT THIS TIME. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: SHAFT — DAMAGED (ZONE 500 FLAP) · airframe 39,285 hrs · 28,696 cycles

LEFT WING INBD FLAP THE MOST INBOARD FLAP VANE ACTUATOR SHAFT HAD DAMAGE & GROOVED ON THE LOWER SURFACE. BLENDED LT WING INBD FLAP AT MOST INBD FLAP VANE ACTUATOR SHAFT ON THE LOWER SURFACE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH REO 670-57-52-257 REV -B. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · airframe 39,285 hrs · 28,696 cycles

LEFT MLG WHEEL WELL, TIRE BURST PANEL, THE FWD ATTACH ANGLE, ON THE AFT WING SPAR IS CORRODED ON THE TOP AND BOTTOM. REMOVED AND INSTALLED NEW LT MLG WHEEL WELL TIRE BURST PANEL, THE FWD ATTACH ANGLE. IAW DWG CC670-10320, REV F SRM 51-42-21-001-001-A01, REV 38. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: SHAFT — GROOVED (ZONE 600 FLAP) · airframe 39,285 hrs · 28,696 cycles

RIGHT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR SHAFT HAS DAMAGED & GROOVED ON THE LOWER SURFACE. REMOVED DAMAGE ON RIGHT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR SHAFT LOWER FACE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH REO 670-57-52-257 REV B. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: SHAFT — DAMAGED (ZONE 600 FLAP) · airframe 39,285 hrs · 28,696 cycles

RIGHT WING INBD FLAP, SECOND FROM INBD END FLAP VANE ACTUATOR SHAFT HAS DAMAGE & GROOVED ON THE LOWER SURFACE. REMOVED DAMAGE ON RT WING INBD FLAP SECOND FROM INBD END FLAP VANE ACTUATOR SHAFT LOWER SURFACE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH REO 670-57-52-257 REV -B. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: SLAT TRACK — GROOVED (ZONE 600) · airframe 39,285 hrs · 28,696 cycles

RIGHT WING SLAT TRACK 3-1 HAS LIGHT GROOVING. REPAIRED GROOVING ON RT WING SLAT TRACK 3-1 IAW SRM 51-12-00-001-001-A01. COMPLIED WITH REO 670-57-42-2289 REV-. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: SLAT TRACK — GROOVED (ZONE 600) · airframe 39,285 hrs · 28,696 cycles

RIGHT WING SLAT TRACK 2-3 HAS LIGHT GROOVING, AREAS. REPAIRED THE RT WING SLAT TRACK 2-3 IAW REO 670-57-42-2288 REV-. COMPLIED WITH ALL STEPS OF REO 670-57-42-2288 REV-. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: SLAT TRACK — GROOVED (ZONE) · airframe 39,285 hrs · 28,696 cycles

RIGHT WING SLAT TRACK 1-1 HAS LIGHT GROOVING, AREAS MARKED IN RED. REPAIRED RT WING SLAT TRACK 1-1 IAW REO 670-57-42-2296 REV -. COMPLIED WITH ALL STEPS OF REO 670-57-42-2296 REV --. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: SLAT TRACK — GROOVED (ZONE 600) · airframe 39,285 hrs · 28,696 cycles

RIGHT WING SLAT TRACK 3-3 HAS LIGHT GROOVING, AREAS MARKED IN RED. REPAIRED GROOVING ON RIGHT WING SLAT TRACK 3-3. IAW SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-57-42-2290 REV-. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: SLAT TRACK — DAMAGED (ZONE 200) · airframe 39,285 hrs · 28,696 cycles

LEFT WING SLAT TRACK 1-3 HAS LIGHT GROOVING. REPAIRED THE LT WING SLAT TRACK 1-3 IAW REO 670-57-42-2295, REV -. COMPLIED WITH ALL STEPS OF REO 670-57-42-2295 REV -. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: ROLLER — DAMAGED (ZONE 600 SLAT) · airframe 39,285 hrs · 28,696 cycles

RIGHT FWD INBD & AFT OTBD SLAT TRACK 3-2 ROLLERS HAS A FLAT SPOT. (2 EA). REMOVED AND INSTALLED 1 EA NEW RT FWD INBD. AND AFT OTBD SLAT TRACK 3-2 SIDE ROLLERS REF. AMM 27-81-44-400-803-A01. GAPS CHECKED GOOD AT THIS TIME.

Part: ROLLER — DAMAGED (ZONE 500 SLAT) · airframe 39,285 hrs · 28,696 cycles

FLAT SPOTS FOUND ON LT SLAT TRACK 2-2 ROLLERS (1EA) FWD INBD. REMOVED AND INSTALLED NEW LT SLAT TRACK 2-2 ROLLERS FWD INBD REF AMM 27-81-44-400-802-A01, TORQUE WRENCH ID TUC6225 CAL 31-DEC-25 &DIGITAL CALIPERS TUC10067 CAL DUE 31-MAY-26. GAP CHECK FAILED BETWEEN SLAT NO1. AND SLAT NO.2, SEE HN00290601 TRANS#31579416 FOR CORRECTIVE ACTION.

Part: ROLLER — DAMAGED (ZONE 500 SLAT) · airframe 39,285 hrs · 28,696 cycles

FLAT SPOTS FOUND ON LH SLAT TRACK 3-2 ROLLERS (2EA) FWD INBD AND FWD OTBD (C-CHECK RO 02/12/2026)REMOVED AND REPLACED LH SLAT TRACK 3-2 ROLLERS FWD INBD AND FWD OTBD WITH NEW SERVICABLE ROLLERS REF CRJ700 AMM 27-81-44-400-803-A01. GAPS CHECK GOOD AT THIS TIME.

Part: ROLLER — DAMAGED (ZONE 600 SLAT) · airframe 39,285 hrs · 28,696 cycles

RIGHT FWD OTBD SLAT TRACK 2-2 ROLLER HAS A FLAT SPOT. REMOVED AND INSTALLED 1EA NEW RT FWD OTBD SLAT TRACK 2-2 SIDE ROLLER IAW AMM 27-81-44-400-802-A01. GAP CHECKED GOOD.

Part: HOUSING — GOUGED (ZONE 800) · airframe 39,285 hrs · 28,696 cycles

AFT BAGGAGE BAY DOOR, EXTERNAL HANDLE HOUSING GOUGED. INSTALLED NEW AFT CARGO DOOR HANDLE HOUSING IAW SRM 51-42-21-001-001-A01, & DWG 601R35027, REV AY. LEAK & OPS TESTED GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 39,285 hrs · 28,696 cycles

RIGHT VERTICAL STAB TO FUSELAGE, AFT DRAG ANGLE HAS POSSIBLE CRACK AT THE AFT END. REPAIRED THE CRACKED DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. NO DEFECTS NOTED.

Part: STRAP — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

PRESSURE FLOOR TENSION STRAP LOCATED AT FS 724 COMMON TO RBL 9 & BL 0 FLOOR BEAMS IS CORRODED. C-CHECK RO 1/17/2021. BLENDED OUT CORROSION ON PRESSURE FLOOR TENSION STRAP AT FS 724 COMMON TO RBL 9 & BL 0 FLOOR BEAMS, REF CRJ 700 SRM 51-21-06-001-001-A01. ORIGINAL THICKNESS 0.050". REMAINING THICKNESS IS 0.035". NO DAMAGE ALLOWED IN THIS AREA. PART IS OUT OF LIMITS, REF CRJ700 SRM 53-41-44-001-001-A01 AND 53-41-44-101-001-A01. REMOVED FABRICATED AND INSTALLED NEW TENSION STRAP AT FS 724 COMMON TO RBL 9 & BL 0, REF DWG SH670-35869 REV NC, DWG SH670-35820 REV NC, AND CRJ700 SRM 51-42-06-001-001-A01. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (RII).

Part: BRACKET — BENT (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

ELECTRICAL MOUNTING BRACKET LOCATED AT FS 333.00 IS BENT. C-CHECK RO 1/17/2021. REPLACED WITH FABRICATED ELECTRICAL MOUNTING BRACKET LOCATED AT FS 333.00, REF CRJ-700 SRM 51-42-21-001-001-A01 AND DRAWING SH670-41538 REV C. COMPLIED WITH 51-900-1002-SKY. RESTORED FINISH.

Part: SPLICE — BROKEN (PAX DOOR) · airframe 36,124 hrs · 26,338 cycles

NUMEROUS PAX DOOR SPLICES BROKEN. C-CHECK RO 1/17/2021. REPLACED 8 EA SPLICES ON PAX DOOR IAW CRJ700 ESPM 20-16-00 AND CRJ700 ESPM 20-44-00. OPERATIONAL TEST OF THE PAX DOOR WARNING SYSTEM PERFORMED, IAW CRJ700 AMM 52-70-00-801-A01. OPERATIONS TEST GOOD. OPERATIONAL TEST OF THE STAIR LIGHTS PERFORMED, IAW CRJ700 AMM 33-45-00-710-802-A01. OPERATIONS TEST GOOD.

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

STRINGER CLEAT STR 19R ON FS 364 IS CRACK. C-CHECK RO 1/17/2021. FABRICATED LOCATED AND DRILLED STRINGER CLEAT STR 19R AT FS 364 FROM S6144-13 PO NR T000056955, REF DWG SH670-35625 REV NC AND REMOVED AND INSTALLED REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-31550 REV G. WEIGHT OF PART REMOVED IS .02 LB, WEIGHT OF PART INSTALLED IS .02 LB, NO WEIGHT CHANGE TOOL USED TUC 1755 DUE 30-SEP-21. COMPLIED WITH TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (RII).

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACK AT RBL 9 BETWEEN FS 835 AND FS 976 HAS DAMAGE, CORROSION, AND CORRODED HARDWARE. C-CHECK RO 1/17/2021. CABIN SEAT TRACK AT RBL 9 BETWEEN FS 835 AND FS 979 P/N SH670-37411-3 REPLACED, PER CRJ700 AMM 53-00-49-400-801-A03. HARDWARE REPLACED PER CRJ700 SRM 51-41-00-001-001-A01. SCREWS TORQUED PER CRJ 700 AMM 20-21-00-910-801-A01. TORQUE SCREWDRIVER TUC9564. S/N 1120400958. CALIBRATION DUE 30/11/2021.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACK AT RBL 9 BETWEEN FS 684 AND FS 835 HAS DAMAGE, CORROSION, AND CORRODED HARDWARE. C-CHECK RO 1/17/2021. REPLACED CORRODED OUT OF LIMITS SEAT TRACK WITH NEW REPLACEMENT SEAT TRACK AND HARDWARE AT RBL 9.00 BETWEEN FS 684.00-FS 835.00, REF CRJ700 AMM 53-00-49-000-801-A03. TOOL TUC9564 CAL: 16-NOV-20 DUE: 30-NOV-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,124 hrs · 26,338 cycles

MULTIPLE SPOTS OF CORROSION FOUND AFTER SEAT TRACK REMOVAL AT RBL 9.00 FROM APPROXIMATELY FS 693-FS 851. C-CHECK RO 1/17/2021. REMOVED CORROSION, OUT OF LIMITS, IAW CRJ 700 SRM 51-21-06-001-001-A01. REPLACED THE BEAM AT RBL 9.0 FROM APPROXIMATELY FS 693-FS 851, PART SH670-35823-3, IAW CRJ 700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01, CRJ 700 SRM 51-41-02-001-001-A01 DWG SH670-35820 REV R & MHIRJ REO 670-53-41-503 REV- DATE 2021-01-07. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD.

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

STRINGER CLEAT STR 19R AT FS 379 IS CRACK. C-CHECK RO 1/17/2021. FABRICATED LOCATED AND DRILLED STRINGER CLEAT STR 19R AT FS 379 FROM S6144-13 PO T000056955, REF DWG SH670-35625 REV NC AND REMOVED AND INSTALLED REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-31550 REV G WEIGHT OF PART REMOVED IS .02 LB, WEIGHT OF PART INSTALLED IS .02 LB, NO WEIGHT CHANGE. TOOL USED TUC 1755 DUE 30-SEP-21 COMPLIED WITH TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (RII).

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

WHILE PERFORMING REPLACEMENT OF STR 20R, FOUND FACTORY SPLICE AT STR 21R, BETWEEN FS 469 TO FS 485 TO BE CORRODED. C-CHECK RO 1/17/2021. INSTALLED NEW STRINGER SPLICE, IAW CRJ700 SRM 51-42-06-001-001-A01, AND DWG SH670-30006 REV A. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYCARD 51-900-1002. LEAK CHECK GOOD.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

WHILE PERFORMING REMOVAL AND REPLACEMENT OF STRINGER, FOUND STR 20R FACTORY SPLICE TO BE CORRODED BETWEEN FS 469 AND FS 485. C-CHECK RO 1/17/2021. REMOVED AND INSTALLED NEW STGR 20R BET FS 469.00 AND FS 485.00, REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG NR SH670-30006 REV A. COMPLIED WITH SKYWEST TASKCARD 51-900-1002-SKY. LEAK CHECK GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

LBL 9.00 FLOOR TRACK FS 683.50-836.50 HAS DAMAGE, CORROSION AND CORRODED HARDWARE AS MARKED. C-CHECK RO 1/17/2021. INSTALLED NEW FLOOR TRACK AT LBL 9.00 BETWEEN FS 683.50 AND FS 836.50, IAW CRJ700 SRM 53-00-49-400-801-A03. TOOL USED TUC8571 CAL DUE DATE 30-JUNE-21. SEAT TRACK FABRICATED ON JOB: 71021085, OP: 165, MX TRANS 21975273.

Part: STIFFENER — CORRODED (PAX DOOR) · airframe 36,124 hrs · 26,338 cycles

5 EACH CORRODED STIFFENERS ON PAX DOOR TOP PANEL. C-CHECK RO 1/17/2021. INTERGRANULAR CORROSION AT NUTPLATES LOCATION ON 5 EACH STIFFENERS. ORDERED AND RECEIVED 5 EACH NEW STIFFENERS P/N 601R317725-1. DRILLED AND LOCATED 5 EACH STIFFENERS ON TOP STEP PANEL, REF CRJ700 SRM 51-40-11-001-001-A01. INSTALLED 5 EACH STIFFENERS, REF CRJ700 SRM 51-42-06-001-001-A01.

Part: FRAME — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

CORROSION ON FS 379.00 FRAME BETWEEN STGR 21R AND STGR 20R. C-CHECK RO 1/17/2021. REMOVED AND INSTALLED 1 EA STRINGER CLEAR AT FS 379.00 STGR 22, REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, DWG. SH670-32050 REV J. COMPLIED WITH SKY CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: DEFLECTOR — CRACKED (PAX DOOR) · airframe 36,124 hrs · 26,338 cycles

CRACKED PASSENGER DOOR FWD AND AFT DEFLECTORS P/N 601R31902-375 AND P/N 601R31902-376. C-CHECK RO 1/17/2021. LOCATED AND DRILLED NEW FWD AND AFT DEFLECTORS P/N 601R31902-375 AND P/N 601R31902-376, REF CRJ700 SRM 51-40-11-001-001-A01. INSTALLED NEW DEFLECTORS, REF CRJ700 SRM 51-42-13-001-001-A01.

Part: GUSSET — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

CORROSION ON GUSSET (P/N#SH670-32000-1) FS 333.00, STGR-20R. C-CHECK RO 1/17/2021. REMOVED AND REPLACED CORRODED GUSSET (P/N SH670-32000-1) AT FS 333.00 AND STGR 20R WITH NEW FABRICATED GUSSET, REF BOMBARDIER DWG SH670-32000 REV NC AND CRJ700 SRM 51-42-06-001-001 A01. SEE CONTINUATION CARD FOR FURTHER DETAILS.

Part: ATTACH ANGLE — CORRODED (BODY FAIRING) · airframe 36,124 hrs · 26,338 cycles

CORROSION ALONG THE FWD FUSELAGE BODY FAIRING (191BB & 192BB) ATTACH STRAP AND ATTACH ANGLE MATING SURFACE APPROXIMATELY FS 613-FS 661, STR 20R-STR 20L. C-CHECK RO 1/17/2021. REMOVED CORROSION ON TEE ATTACH ANGLE AT BL 0 BETWEEN FS 629-661, REF CRJ700 SRM 51-21-06-001-001-A01. MECHANICALLY MEASURED REMAINING MATERIAL AND FOUND TO BE OUT OF LIMITS, REF CRJ700 SRM 53-82-55-101-001-A01 AND DWG SH670-39063 REV A. REMOVED AND REPLACED TEE ANGLE WITH NEW TEE ANGLE P/N SH670-39063-3. REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-39050 REV H. REMOVED CORROSION ON WING FAIRING STRUCTURE STRAP AT FS 629 LT & RT, REF CRJ700 SRM 51-21-06-001-001-A01. BLENDS ARE WITHIN LIMITS FOR STRAP, REF CRJ700 SRM 53-82-55-101-001-A01. RESTORED FINISH AND RE-APPLIED SELF CONTOURING PAD TO WING FAIRING STRAP STRUCTURE, REF CRJ700 SRM 51-21-16-001-001-A01 TEMP REVISION 51-0068 AND SRM 51-23-00-001-001-A01. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: GUSSET — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

CORROSION ON GUSSET (P/N SH670-31998-1) FS 349.00, STGR 20R. C-CHECK RO 1/17/2021. REMOVED CORRODED GUSSET AND REPLACED WITH NEW FABRICATED GUSSET (P/N SH670-31998-1) AT FS 349.00 AND STGR 20R, REF BOMBARDIER DWG SH670-31950 REV Y AND CRJ700 SRM 51-42-06-001-001 A01. COMPLIED WITHTASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR FURTHER DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CORROSION ON FLOOR BEAM LOCATED AT RBL 9.0 FS 571-FS 677. C-CHECK RO 1/17/2021. REMOVED CORROSION FROM FLOORBEAM RBL 9 FS 571-FS 677, "OUT OF LIMITS", REF CRJ700 SRM 51-21-06-001-001-A01, DRAWING SH670-33459 REV NC. REMOVED AND REPLACED FLOORBEAM RBL 9 FS 571-FS 677, REF CRJ200 SRM 53-00-41-201-001-A01. COMPLIED WITH ST 51-900-1002-SKY. OPERATIONS CHECKS GOOD.

Part: FRAME — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

CORROSION INBOARD FLANGE ON STUD FRAME FS 333.00 BETWEEN STGR 18R AND STGR 20R. C-CHECK RO 1/17/2021. COMPLIED WITH ALL STEPS OF REO 670-53-21-1903 REV- DATED 2020-12-13. ENSURED BLEND OUT OF CORROSION WAS DONE, IAW CRJ 700 SRM 51-21-06-001-001-AO1. NDT PERFORMED, AREAS ARE CRACK FREE. RESTORED FINISH. APPLIED CIC. COMPLIED WITH 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS. LEAK CHECK OK.

Part: HOUSING — CORRODED (PAX DOOR) · airframe 36,124 hrs · 26,338 cycles

CORRODED PAX DOOR BUSHING HOUSING P/N 600-31320-79 AT FWD PULL-IN LEVER. C-CHECK RO 1/17/2021. ORDERED AND RECEIVED NEW FWD PULL-IN LEVER BUSHING HOUSING P/N 600-31320-79. LOCATED AND DRILLED, REF CRJ700 SRM 51-40-11-001-001-A01.

Part: ATTACH ANGLE — CRACKED (FAIRING) · airframe 36,124 hrs · 26,338 cycles

FUSELAGE FAIRING 194AB HAS CRACKED RT ATTACHING ANGEL (MEMBER SEAL) P/N CC670-39202-2 AND DAMAGED NUTPLATE ATTACHMENT POINT. C-CHECK RO 1/17/2021. REMOVED, REPLACED AND INSTALLED NEW ATTACHING ANGLE P/N CC670-39202-2 FOR FUSELAGE FAIRING 194AB, REF CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-13-001-001-A01.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 36,124 hrs · 26,338 cycles

CORRODED CLEAT P/N 600-31902-269 ON PAX DOOR COMMON TO INTERCOSTAL DD6 AND FORMER FRAME FS 329. C-CHECK RO 1/17/2021. REMOVED AND REPLACED CORRODED, 100% EXFOLIATED CLEAT P/N 600-31902-269 ON PAX DOOR COMMON TO INTERCOSTAL DD6 AND FORMER/FRAME FS 329, REF CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 AND DWG 601R31702 REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: CLEAT — CRACKED (PAX DOOR) · airframe 36,124 hrs · 26,338 cycles

CRACKED CLEAT P/N 600-31902-269 COMMON TO PAX DOOR FORMER FS 338 AND DD6 INTERCOSTAL. C-CHECK RO 1/17/2021. ORDERED AND RECEIVED NEW CLEAT P/N 600-31902-269. REMOVED AND REPLACE CRACKED CLEAT WITH A NEW CLEAT COMMON TO THE PAX DOOR FORMER FS 338 AND INTERCOSTAL DD6, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV-N. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACKS STGR 15R HAVE DAMAGE, CORROSION, AND CORRODED HARDWARE, AS MARKED FS 869/961. C-CHECK RO 1/17/2021. REMOVED AND REPLACED THE SEAT TRACK AT STR 15R FS 869-FS 961 WITH A FABRICATED PART, REF CRJ700 AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACKS STGR 15L HAVE DAMAGE, CORROSION, AND CORRODED HARDWARE, AS MARKED FS 961/988. C-CHECK RO 1/17/2021. MULTIPLE AREAS OF CORROSION AND DAMAGE FOUND ACROSS SINGLE CROSS SECTION. OUT OF LIMITS, REF CRJ700 SRM 53-51-49-101-001-A01. REMOVED AND INSTALLED NEW SEAT TRACK LT FS 961-988, REF CRJ700 AMM 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACKS STGR 15R HAVE DAMAGE, CORROSION, AND CORRODED HARDWARE, AS MARKED FS 961/988. C-CHECK RO 1/17/2021. MULTIPLE AREAS OF CORROSION AND DAMAGE FOUND ACROSS SINGLE CROSS SECTION. OUT OF LIMITS, REF CRJ700 SRM 53-51-49-101-001-A01. REMOVED AND INSTALLED NEW SIDE SEAT TRACK RETAINER FS 961-988, REF CRJ700 AMM 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACKS STGR 15L HAVE DAMAGE, CORROSION, AND CORRODED HARDWARE, AS MARKED FS 869/961. C-CHECK RO 1/17/2021. REMOVED CORROSION ON THE STR 15L FS 869-961 SEAT TRACK, "OUT OF LIMITS". REMOVED AND REPLACED SEAT TRACK AT STR 15L FS 869-961, REF CRJ700 SRM 51-41-02-001-001-A01, AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACKS STGR 15R HAVE DAMAGE, CORROSION, AND CORRODED HARDWARE, AS MARKED FS 783/852. C-CHECK RO 1/17/2021. REMOVED AND REPLACED THE CABIN SEAT TRACK STR 15R FS 783-FS 852 WITH A FABRICATED PART, REF CRJ700 AMM 53-00-49-400-801-A17. REINSTALLED SEAT TRACK RETAINER AND REPLACED HARDWARE.

Part: SEAT TRACK — CORRODED (ZOEN 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACKS STGR 15R HAVE DAMAGE, CORROSION, AND CORRODED HARDWARE, AS MARKED FS 852/869. C-CHECK RO 1/17/2021. BLENDED CORROSION ON RT SIDE SEAT TRACK "OUT OF LIMITS", REF CRJ700 SRM 53-51-49-101-001-A01. REMOVED AND REPLACED RT SIDE SEAT TRACK AT 15R FS 852-FS 869, REF CRJ700 AMM 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACKS STGR 15L HAVE DAMAGE, CORROSION, AND CORRODED HARDWARE, AS MARKED FS 852/869. C-CHECK RO 1/17/2021. REMOVED AND REPLACED SEAT TRACK STR 15L FS 852-FS 869 WITH A FABRICATED PART, REF CRJ700 AMM 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACKS STGR 15L HAVE DAMAGE, CORROSION, AND CORRODED HARDWARE, AS MARKED FS 703/763. C-CHECK RO 1/17/2021. DAMAGE IS OF MULTIPLE TYPES ACROSS MULTIPLE SURFACES. OUT OF LIMITS CRJ 700 SRM 53-41-49-101-001-A01. REMOVED AND INSTALLED NEW SEAT TRACK LT FS 703-763, REF CRJ700 AMM 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACKS STGR 15R HAVE DAMAGE, CORROSION, AND CORRODED HARDWARE, AS MARKED FS 675/703. C-CHECK RO 1/17/2021. REMOVED AND REPLACED RT SIDE SEAT TRACK WITH NEW HARDWARE AT STGR 15R, FS 675.00-FS 713.00, PER CRJ700 AMM 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACKS STGR 15L HAVE DAMAGE, CORROSION, AND CORRODED HARDWARE, AS MARKED FS 675/703. C-CHECK RO 1/17/2021. DAMAGE IS OF MULTIPLE TYPES ACROSS MULTIPLE SURFACES. OUT OF LIMITS, CRJ 700 SRM 53-41-49-101-001-A01. REMOVED AND INSTALLED NEW SEAT TRACK LT FS 675-703, REF CRJ700 AMM 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACKS STGR 15R HAVE DAMAGE, CORROSION, AND CORRODED HARDWARE, AS MARKED FS 703/763. C-CHECK RO 1/17/2021. MULTIPLE AREAS OF CORROSION AND DAMAGE FOUND ACROSS SINGLE CROSS SECTION. OUT OF LIMITS, REF CRJ700 SRM 53-41-49-101-001-A01. REMOVED AND INSTALLED NEW SIDE SEAT TRACK RETAINER FS 703-763, REF CRJ700 AMM 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN SEAT TRACKS STGR 15L HAVE DAMAGE, CORROSION, AND CORRODED HARDWARE, AS MARKED FS 783/852. C-CHECK RO 1/17/2021. CORROSION ON SEAT TRACK FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEWLY FABRICATED SEAT TRACK, REF CRJ700 AMM 53-00-49-400-801-A17. SEE MX 21975959 FOR TRACK FABRICATION.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 36,124 hrs · 26,338 cycles

CORROSION FOUND ON PAX DOOR BOTTOM ANGLE P/N 601R317726-3. C-CHECK RO 1/17/2021. REMOVED CORROSION ON PAX DOOR BOTTOM ANGLE, REF CRJ700 SRM 51-21-06-001-001-A01. EVALUATED PAX DOORBOTTOM ANGLE P/N 601R317726-3, 100% MATERIAL LOSS ARROUND FASTENER HOLES REPLACE PART INSTALLED NEW BOTTOM ANGLE TO PAX DOOR REF CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-13-001-001-A01.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,124 hrs · 26,338 cycles

FOUND CORROSION ON PAX DOOR AFT SIDE INTERCOSTAL P/N 601R31902-317. C-CHECK RO 1/17/2021. REMOVED CORROSION ON THE PAX DOOR AFT INTERCOSTAL "OUT OF LIMITS", REF CRJ700 SRM 51-21-06-001-001-A01. REMOVED AND REPLACED INTERCOSTAL P/N 601R31902-317, REF SRM 51-42-06-001-001-A01 AND DWG 601R31902 REV BE. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 36,124 hrs · 26,338 cycles

PAX DOOR SURROUND STRUCTURE, FRAME AT FS 319.00 LT CORRODED. C-CHECK RO 1/17/2021. REMOVED CORRODED FRAME AT FS 319.00 BETWEEN STGR 18L AND 21L, REF CRJ700 SRM 51-42-06-001-001 A01. INSTALLED NEW FRAME (P/N SH670-31891-3) AT FS 319.70 USING NEW FASTENERS, REF BOMBARDIER DWG SH670-31810 REV AE AND CRJ700 SRM'S 51-42-06-001-001 A01 AND 51-42-21-001-001 A01. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK FAILED. SEE CAMP 22136478.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN, RT SIDE SEAT RAIL RETAINERS FS 669 TO 989 RETAINERS HAVE MULTIPLE AREAS OF CORROSION, GOUGES INTO BASE METAL, AND CORRODED OR MISSING NUTCLIPS. C-CHECK RO 1/17/2021. REPAIRED WITHIN LIMITS AND REPLACED OUT OF LIMITS CORRODED. CABIN, RT SIDE SEAT RAIL RETAINERS FS 669 TO 989, REF CRJ700 SRM 53-00-00-001-001-A01 AND CRJ700 AMM 53-00-49-400-801-A017. INSTALLED NEW REPLACEMENT HARDWARE, REF CRJ700 AMM 53-00-49-400-801-A017. TOOL TUC9564 CAL: 16-NOV-20 DUE: 30-NOV-21.

Part: FORMER — CORRODED (PAX DOOR) · airframe 36,124 hrs · 26,338 cycles

PAX DOOR FORWARD FORMER IS CORRODED AT ACCESS PANEL 832FL AREA. C-CHECK RO 1/17/2021. REMOVED AND REPLACED CORRODED OUT OF LIMITS PAX DOOR FORWARD FORMER WITH A NEW FORMER AND FASTENERS, REF MHI RJ DWG 601R31702 REV-N, CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-13-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. COMPLIED WITH SKY CARD 51-900-1002-SKY. LEAK CHECK GOOD.

Part: FORMER — CORRODED (PAX DOOR) · airframe 36,124 hrs · 26,338 cycles

PAX DOOR CENTER INTERNAL FORMER/FRAME AT APPROXIMATELY FS 329 HAS CORROSION. C-CHECK RO 1/17/2021. REMOVED AND REPLACED THE PAX DOOR CENTER INTERNAL FORMER FRAME FS 329, REF DRAWING 601R31702 REV -N, AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH ST 51-900-1002-SKY. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,124 hrs · 26,338 cycles

PAX DOOR INTERCOSTAL AT DD6 IS CORRODED. C-CHECK RO 1/17/2021. REMOVED AND REPLACED THE PAX DOOR INTERCOSTAL DD6, REF DWG 601R31702 REV-N, CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01. COMPLIED WITH ST 51-900-1002-SKY. LEAK CHECK GOOD.

Part: PLATE — CHAFED (PAX DOOR) · airframe 36,124 hrs · 26,338 cycles

PAX DOOR FORWRAD STRIKE PLATE IS CHAFED. C-CHECK RO 1/17/2021. REMOVED AND REPLACE DAMAGED PAX DOOR STRIKE PLATE WITH A NEW ONE AND FASTENERS, REF CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. SEE CONTINUATION CARD FOR DETAILS.

Part: BEAM — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

CORROSION ON LONG BEAM FS 517 TO FS 575 LBL 9. C-CHECK RO 1/17/2021. REMOVED CORROSION ON LONG BEAM LBL 9 FS 517.00, REF CRJ700 SRM 51-21-06-001-001-A01. DAMAGE OUT OF LIMITS AS NO DAMAGE ALLOWED, REF CRJ700 SRM 53-31-43-101-001-A02. REMOVED AND REPLACED LONG BEAM LBL 9 FROM FS 517 TO FS 575, REF CRJ700 SRM 53-00-41-201-001-A01, SNIEO SH670-33440 DATED DEC 30, 2020 AND REO 670-53-31-592 REV- DATED JAN 01, 2021. ALL CHECKS GOOD AT THIS TIME. COMPLIED WITH 51-900-1002-SKY.

Part: CLEAT — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

FS 1000-STGR 20R CORNER CLEAT CORRODED, AS MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION ON CLEAT AT STR 20R FS 1000, PER CRJ 700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. INSTALLED NEW CLEAT AT FS 1000-STRG 20R, IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01.

Part: CLEAT — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

FS 1015 STGR 25R CORNER CLEAT CORRODED, AS MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION ON CLEAT, REF CRJ700 SRM 51-21-06-001-001-A01. MECHANICALLY MEASURED REMAINING THICKNESS. CLEAT IS OUT OF LIMITS, PER CRJ700 SRM 53-61-03-001-003-A01. REMOVED AND REPLACED CORNER CLEAT AT FS 1015 STGR 25R, REF MM670-36062, REV NC AND CRJ700 SRM 51-42-06-001-001-A01. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

RBL 9 SEAT TRACK FROM FS 280 TO 485 CORRODED. C-CHECK RO 1/17/2021. INSTALLED NEW REPLACEMENT SEAT TRACK AND HARDWARE FOR SEAT TRACK, P/N: SH670-32159-1 AT RBL 9.00 FROM FS 349.00-FS 485.00, REF CRJ700 AMM 53-00-49-400-801-A03.

Part: SKIN — DENTED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

2 EA DENTS IN EXTERNAL FUSELAGE STGR 27 JUST AFT OF FS 969, AS MARKED. C-CHECK RO 1/17/2021. THE BLENDS ON THE EXTERNAL SKIN AT STRG 27 JUST AFT OF FS 969 IS STRUCTURALLY ACCEPTABLE, REF MHIRJ REO 670-53-00-644 REV- DATE 2020-12-02. THE 2 EA DENTS IN EXTERNAL FUSELAGE AT STRG 27 JUST AFT OF FS 969, THE TWO LOCATION JUST AFT OF FS 969 ARE BLENDS THAT COINCIDE WITH PREVIOUS REPAIR REO 670-53-51-120 REV - DATED 2017-10-27. SUBMITTED AND RECEIVED REVISED REO 670-53-00-644 REV -A DATED 2020-12-15, ALL STEPS COMPLIED WITH. COMPLIED WITH ST 51-900-1002-SKY.

Part: SKIN — DENTED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

EXTERNAL SKIN DENT AND GOUGE AT STGR 27 JUST FWD OF FS 985, AS MARKED. C-CHECK RO 1/17/2021. BLENDED GOUGE TO SMOOTH CONTOUR, REF CRJ700 SRM 51-12-00-001-001-A01. DAMAGE IS OUT OF LIMITS, REF CRJ700 SRM 53-61-01-101-003-A01. FABRICATED AND INSTALLED REPAIR, PER REO 670-53-00-290 REV F DATED 2019/04/26, REO 670-53-00-645 REV- DATED 2020-12-12, AND REO 670-53-00-644 REV A DATED 2020-12-15. LEAK CHECKS GOOD AT THIS TIME. ALL STEPS OF THE REO'S COMPLIED WITH. COMPLIED WITH 51-900-1002-SKY.

Part: SKIN — GOUGED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

EXTERNAL SKIN 1.5" GOUGE AT STGR 27 JUST AFT OF FS 985. C-CHECK RO 1/17/2021. BLENDED GOUGE AT STRG 27 JUST FWD OF FS 985, REF CRJ 700 SRM 51-12-00-001-001-A01. THE BLEND ON THE EXTERNAL SKIN AT STRG 27 JUST FWD OF FS 985 IS STRUCTURALLY ACCEPTABLE, REF MHIRJ REO 670-53-00-644 REV- DATE 2020-12-02. SUBMITTED AND RECEIVED REVISED MHIRJ REO 670-53-00-644 REV -A DATED 2020-12-15, ALL STEPS COMPLIED WITH. COMPLIED WITH ST 51-900-1002-SKY.

Part: SKIN — CORRODED (EXTERIOR) · airframe 36,124 hrs · 26,338 cycles

EXTERNAL SKIN APPROXIMATELY 6 EA RIVETS SHOW SIGNS OF CORROSION STGR 25R BETWEEN FS 939/969, AS MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION FROM LOWER EXTERNAL SKIN, IAW CRJ700 SRM 51-21-06-001-001-A01. REMOVED AND REPLACED RIVETS, IAW CRJ700 SRM 51-42-06-001-001-A01. SEE CONTINUATION CARD FOR DETAILS.

Part: CARGO TRACK — CORRODED (FWD CARGO BAY) · airframe 36,124 hrs · 26,338 cycles

MULTIPLE FWD CARGO RETRIEVAL SYSTEM FLOOR TRACKS HAVE SPOTS OF CORROSION. C-CHECK RO 1/17/2021. BLENDED AND EVALUATED CORRROSION ON FWD CARGO SEAT TRACKS. FOUND TO BE OUT OF LIMITS. FABRICATED NEW TRACKS ON JOB 71021085 OP 221. SEE MX 21779803 FOR INSTALL.

Part: SUPPORT — CRACKED (BODY FAIRING) · airframe 36,124 hrs · 26,338 cycles

LEFT SIDE FUSELAGE BODY FAIRING SUPPORT STRUCTURE JUST AFT OF FS 909.0 STRAP HAS CRACK. C-CHECK RO 1/17/2021. REPAIRED THE LT SIDE FUSELAGE BODY SUPPORT FAIRING STRUCTURE AFT OF FS909 BY CUTTING AWAY DAMAGED AREA AND INSTALLING A REPAIR DOUBLER REF REO 670-53-82-478 REV -A DATED 2014/11/12. COMPLIED WITH ST 51-900-1002-SKY.

Part: TRACK — DAMAGED (AFT CARGO DOOR) · airframe 36,124 hrs · 26,338 cycles

AFT CARGO AFT DOOR TRACK UP SURFACE HAS IMPACT DAMAGE AT APPROXIMATELY 6" (AT BEGINNING OF RADIUS) FROM LOWER END. C-CHECK RO 1/17/2021. BLENED 2 EA AREA ON AFT CARGO, AFT DOOR TRACK , 1 EA ON UPPER FLANGE AND 1 EA ON LOWER FLANGE OF TRACK PER CRJ 700 SRM 51-12-00-001-001-A01 BLENDS FOUND TO BE OUT OF LIMITS. INSTALLED NEW REPLACEMENT TRACK P/N: CC670-38798-5 AND SEGMENT OF OLD TRACK, PER BOMBARDIER REO 670-53-62-102 REV -A DATED 2016-10-12 ALL STEPS COMPLIED WITH.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

CABIN RT FLOOR SILL FS 517/533 DECOMPRESSION PANEL AND HARDWARE CORRODED. C-CHECK RO 1/17/2021. REMOVED AND REPLACED RT FLOOR SILL FS 517/533 DECOMPRESSION PANEL AND HARDWARE, IAW CRJ 700 AMM 21-35-01-000-801-A01 AND 21-35-01-400-801-A01.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 36,124 hrs · 26,338 cycles

CABIN, FS 549 FLOOR CROSS BEAM BETWEEN RBL 9 AND RBL 27 CORRODED, AS MARKED. C-CHECK RO 1/17/2021. COMPLIED WITH ALL STEPS OF REO 670-53-31-579 REV - DATED 2020-12-03 FOR CORROSION ON FLOOR CROSS BEAM AT FS 549 BETWEEN RBL 9 AND RBL 27.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,124 hrs · 26,338 cycles

PAX DOOR SURROUND STRUCTURE, MIDDLE CAP ANGLE IS CORRODED, MARKED. C-CHECK RO 1/17/2021. PAX DOOR SURROUND STRUCTURE, MIDDLE CAP ANGLE CORROSION IS EXFOLIATED THROUGH PART THICKNESS, 100% MATERIAL LOSS. REMOVED AND REPLACED CAP ANGLE WITH NEW PART PER CRJ700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN LBL 9-FS 477/693 SEAT RAIL CORRODED MANY PLACES ON BOTH SIDES OF SEAT TRACK, AS MARKED. C-CHECK RO 1/17/2021. INSTALLED 2 EA NEW REPLACEMENT SEAT TRACKS AND HARDWARE AT LBL 9.00 FROM FS 485.00-FS 581.00 AND FS 581.00-FS 683.50, REF CRJ700 AMM 53-00-49-400-801-A17. TOOL NR TUC9564 CAL: 16-NOV-20 DUE: 30-NOV-21. SEAT TRACK P/N'S: SH670-33426-1 AND SH670-33425-3.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

RIGHT SIDE FLOOR SILL BETWEEN FS 280 AND FS 319 HAS CORROSION, SCRATCHES, AND A CRACK, MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION ON THE RT FLOOR SILL FS 280-FS 319, "OUT OF LIMITS." REMOVED AND REPLACED THE RT FLOOR SILL BETWEEN FS 280-FS 319, REF DRAWING SH670-32170 REV V, CRJ700 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01. COMPLIED WITH ST 51-900-1002-SKY, RESTORED FINISH. LEAK CHECKS GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

RT SIDE SEAT TRACK FS 573-663 HAS CORROSION, AS MARKED. C-CHECK RO 1/17/2021. REMOVED AND REPLACED RT SIDE SEAT TRACK FS 573.00-FS 663.00, PER CRJ700 AMM 53-00-49-400-801-A17.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

STRINGER, STGR 21R, HAS CORROSION BETWEEN APPROXIMATELY FS 349 TO FS 364, MARKED. C-CHECK RO 1/17/2021. INSTALLED 1 EA STGR CLEAT ONTO STGR 21R AT FS 364.00, REF CRJ700 SRM 51-42-06-001-001 A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-31350 REV A. SEE CONTINUATION CARD FOR DETAILS. LEAK CHECK GOOD COMPLIED WIRH SKYCARD 51-900-1002-SKY.

Part: DOOR SILL — CORRODED (AFT CARGO BAY) · airframe 36,124 hrs · 26,338 cycles

AFT BAGGAGE BAY DOOR SILL HAS AREAS OF CORROSION, FRETTING, A DENT, AND SOME GOUGES, MARKED. C-CHECK RO 1/17/2021. BLENDED DAMAGE ON THE AFT BAGGAGE BAY DOOR SILL "OUT OF LIMITS", REF CRJ700 SRM 51-21-06-001-001-A01, SRM 53-61-23-001-001-A01. REMOVED AND REPLACED THE AFT BAGGAE BAY DOOR SILL, REF DRAWING MM670-35085 REV L, CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01, SRM 51-42-21-001-001-A01. RESTORED FINISH. COMPLIED WITH ST 51-900-1002-SKY.

Part: FITTING — CORRODED (FUSELAGE) · airframe 36,124 hrs · 26,338 cycles

PAX DOOR SURROUND STRUCTURE, THE FORWARD CLOSING FITTING IS CORRODED, MARKED. C-CHECK RO 1/17/2021. BLENDED CORROSION ON THE PAX DOOR FWD CLOSING FITTING "OUT OF LIMITS", REF CRJ700 SRM 51-21-06-001-001-A01, SRM 53-21-23-101-001-A01. ORIGINAL: .080, REMAINING: .060, LOSS: .020. REMOVED AND REPLACED THE PAX DOOR FWD CLOSING FITTING, REF CRJ700 SRM 51-40-11-001-001-A01, SRM 51-42-02-001-001-A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

STRINGER, STGR 27, IS CORRODED BETWEEN FS 310 TO FS 319, MARKED. C-CHECK RO 1/17/2021. BLENDED CORROSION ON STRINGER 27 AT FS 310-FS 319 "OUT OF LIMITS", REF CRJ700 SRM 53-21-03-101-002-A01. REMOVED AND REPLACED THE STRINGER 27 AT FS 310 - FS 319, REF DRAWING SH670-31630 REV G, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. COMPLIED WITH ST 51-900-1002-SKY. LEAK CHECKS GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN RBL 9 SEATRAIL AT FS 565 CORRODED AT NUTPLATE, AS MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION ON RBL 9.0 FS 476.0 TO FS 571.0, REF CRJ 700 SRM 51-21-06-001-001-A01, OUT OF LIMITS. REPAIRED THE FLOOR BEAM BETWEEN FS 476.0 TO FS 571.0 RBL 9.0, REF CRJ700 SRM 53-00-41-201-001-A01 REPAIR-001-A01 AND MHIRJ REO 670-53-31-592 REV DATED 2021-01-01. 51-900-1002-SKY COMPLIED WITH.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

LT SIDE SEAT TRACKS TRIM RETAINERS FS 349-669 HAS CORROSION, AS MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION ON LT SIDE SEAT TRACK TRIM RETAINER FS 349 TO FS 477, REF CRJ 700 SRM 51-21-06-001-001-A01, ORIGINAL THICKNESS IS .040", REF CRJ 700 SRM 53-21-49-001-001-A01. REMOVED .007" REMAINING THICKNESS IS .033" OUT OF LIMITS, REF CRJ 700 SRM 53-21-51-101-001-A01. REMOVED AND INSTALLED NEW SIDE SEAT TRACK RETAINER FS 573-669, REF CRJ700 AMM 53-00-49-400-801-A17.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

STRINGER, STGR 26R, IS CORRODED BETWEEN FS 295 TO FS 319, MARKED. C-CHECK RO 1/17/2021 BLENDED CORROSION ON STRINGER AT 26R FS 295-FS 319 "OUT OF LIMITS", REF CRJ700 STM 53-21-03-101-002-A01, SRM 51-21-06-001-001-A01. REMOVED AND REPLACED STRINGER 26R AT FS 295-FS 319, REF CRJ700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, DWG SH670-31630 REV K, AND REO 670-53-21-799 REV A DATED 2016-11-27. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

LT SIDE SEAT TRACK FS 378-483 HAS CORROSION, AS MARKED. C-CHECK RO 1/17/2021. REMOVED AND INSTALLED FABRICATED SEAT SIDE TRACK LT FS 378-FS 483, REF CRJ700 AMM 53-00-49-400-801-A17.

Part: SUPPORT ANGLE — CORRODED (E/E BAY) · airframe 36,124 hrs · 26,338 cycles

AVIONICS COMPARTMENT CRAWLWAY SUPPORT ANGLE AT FS 280 HAS CORROSION, MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION FROM AVIONICS COMPARTMENT CRAWLWAY SUPPORT ANGLE AT FS 280 REF CRJ 700 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS .050" MATERIAL REMOVED .004". MATERIAL REMAINING .046", NDT NOTED. FOUND TO BE WITH IN LIMITS, REF CRJ700 SRM 53-11-10-001-003-A01.

Part: ANGLE — CORRODED (DOOR FRAME) · airframe 36,124 hrs · 26,338 cycles

PAX DOOR SURROUND STRUCTURE, LOWER KICKPLATE ANGLE IS CORRODED AROUND THE NUTPLATE ON THE INBOARD SIDE, MARKED. C-CHECK RO 1/17/2021. FOUND PAX DOOR SURROUND KICKPLATE TO BE 100% EXFOLIATED "OUT OF LIMITS." REMOVED AND REPLACED THE PAX DOOR SURROUND STRUCTURE KICKPLATE, REF CRJ700 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, DRAWING 670-31810 REV Y. COMPLIED WITH ST 51-900-1002-SKY. LEAK CHECKS AND OPERATIONS CHECKS GOOD.

Part: MOUNT — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

FWD INBOARD ENTRANCE STORAGE MOUNT ON THE FLOOR STRUCTURE HAS CORROSION AROUND AND IN THE BOLT HOLE, MARKED. C-CHECK RO 1/17/2021. REMOVED AND REPLACED THE 100% CORRODED FWD INBOARD ENTRANCE STORAGE MOUNT, REF CRJ700 SRM 51-42-21-001-001-A01. RESTORED FINISH.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

STRINGER, STGR 20R, HAS CORROSION BETWEEN APPROXIMATELY FS 364 TO FS 394 AND FS 421 TO FS 437, MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION ON STRINGER 20R FS 364 - 394 "OUT OF LIMITS", REF CRJ700 SRM 51-21-06-001-001-A01, SRM 51-21-03-101-007-A01. REMOVED AND REPLACED STRINGER 20R FS 349-FS 485, REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, DRAWING SH670-31401 REV A. COMPLIED WITH ST 51-900-1002-SKY. LEAK CHECKS GOOD.

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 36,124 hrs · 26,338 cycles

PAX DOOR SURROUND STRUCTURE, BACK-UP SILL AT STGR 21L IS CORRODED BETWEEN FS 310 TO FS 333. C-CHECK RO 1/17/2021. REMOVED AND REPLACED CORRODED BACK UP SILL WITH NEW PART (P/N SH670-31822-1) ON STGR 21L BETWEEN FS 310.00 AND FS 333.00 USING ALL NEW FASTENERS, REF BOMBARDIER DWG SH670-31810 REV AE AND CRJ700 SRM'S 51-42-06-001-001 A01 AND 51-42-21-001-001 A01. COMPLIED WITH SKYCARD 51-900-1002-SKY. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

INTERCOSTAL STGR 20R BETWEEN FS 319 TO FS 333 IS CORRODED, MARKED. C-CHECK RO 1/17/2021. REMOVED AND INSTALLED NEW INTERCOSTAL P/N SH670-32004-3, REF CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 AND DRAWING SH670-31950 REV Y. COMPLIED WITH SKY CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS. LEAK CHECK GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

RT SIDE SEAT TRACK FS 378-483 HAS CORROSION, AS MARKED. C-CHECK RO 1/17/2021. INSTALLED NEW RT SIDE SEAT TRACK FS 378-483, REF CRJ700 AMM 53-00-49-400-801. CONFIG A17.

Part: DOUBLER — CORRODED (TCAS ANTENNA) · airframe 36,124 hrs · 26,338 cycles

TCAS OMNIDIRECTIONAL ANTENNA DOUBLER IS CORRODED AROUND THE CONNECTOR PENETRATION, LOCATED AT STGR 27, BETWEEN FS 295 TO FS 310. C-CHECK RO 1/17/2021. REMOVED CORROSION FROM THE TCAS ANTENNA DOUBLER "OUT OF LIMITS". REMOVED AND REPLACED THE TCAS ANTENNA AT STR 27 FS 295-FS 310, REF DRAWING SH670-30023 REV G, CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. COMPLIED WITH ST 51-900-1002-SKY. RESTORED FINISH, LEAK CHECKS GOOD.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

CABIN FS 549 FLOOR CROSSBEAM BETWEEN LBL 9 AND RBL 9 CORRODED, AS MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION ON FS 549 FLOOR CROSSBEAM BETWEEN LBL 9 AND RBL 9, REF CRJ 700 SRM 51-21-06-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-53-31-579 REV- DATED 2020-12-03.

Part: ATTACH ANGLE — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

RIGHT SIDE FLOOR SILL ATTACH ANGLE AT THE FS 319 FRAME HAS CORROSION, MARKED. C-CHECK RO 1/17/2021. REMOVED AND INSTALLED NEW RIGHT SIDE FLOOR SILL ATTACH ANGLE AT THE FS 319 FRAME, REF CRJ 700 SRM 51-42-06-001-001-A01 & CRJ 700 SRM 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

LT SIDE SEAT TRACK FS 483-573 HAS CORROSION, AS MARKED. C-CHECK RO 1/17/2021. LT SIDE SEAT TRACK FS 483 TO FS 573 IS OUT OF LIMITS, REF CRJ 700 SRM 53-31-49-101-001-A01. REMOVED AND INSTALLED NEW SEAT TRACK LT FS 483-573, REF CRJ700 AMM 53-00-49-400-801-A17.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

STRINGER, STGR 19R, HAS CORROSION BETWEEN APPROXIMATELY FS 364 TO FS 374, MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION ON STR 19R FS 364-FS 374 "OUT OF LIMITS" REF CRJ700 SRM 53-21-03-101-007-A01. REMOVED AND REPLACED THE STRINGER AT 19R FS 364-FS 374, REF DRAWING SH670-31070 REV J, SRM 53-00-03-201-001-A01, SRM 51-42-06-001-001-A01. COMPLIED WITH ST 51-900-1002-SKY. LEAK CHECKS GOOD.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

STRINGER, STGR 19L, IS CORRODED BETWEEN FS 319 TO FS 349, MARKED. C-CHECK RO 1/17/2021. REMOVED CORRODED STRINGER 19L BETWEEN FS 310.00 AND 349.00, REF CRJ700 SRM 51-42-06-001-001 A01 AND 51-42-21-001-001 A01. INSTALLED NEW STRINGER (P/N SH670-31936-1) AT 19L BETWEEN FS 310.00 AND 349.00 USING ALL NEW FASTENERS, REF BOMBARDIER DWG SH670-31810 REV AE AND CRJ700 SRM'S 51-42-06-001-001 A01 AND 51-42-21-001-001 A01. COMPLIED WITH SKYCARD 51-900-1002-SKY. LEAK CHECK GOOD.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 36,124 hrs · 26,338 cycles

COCKPIT AFT FLOOR SUPPORT ANGLE ON FWD SIDE OF 280 BEAM LBL 9-RBL 9 IS CORRODED. C-CHECK RO 1/17/2021. BLENDED CORROSION ON THE COCKPIT AFT FLOOR SUPPORT "OUT OF LIMITS", REF CRJ700 SRM 53-00-00-101-001-A01, SRM 51-21-06-001-001-A01 ORIGINAL: .063; REMAINING: .037; LOSS: .026. REMOVED AND REPLACE THE COCKPIT AFT FLOOR SUPPORT ANGLE FS280 LBL9 - RBL9 REF DRAWING CC670-34095 REV--, CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. COMPLIED WITH ST 51-900-1002-SKY

Part: TRACK — BROKEN (CARGO DOOR) · airframe 36,124 hrs · 26,338 cycles

AFT CARGO DOOR, AFT TRACK UPPER STOP IS BROKEN. C-CHECK RO 1/17/2021. REMOVED AFT CARGO DOOR, AFT TRACK UPPER STOP, REF CRJ 700 AMM 52-31-23-000-801 (A01) AND INSTALLED WITH NEW FROM STOCK, REF CRJ 700 AMM 52-31-23-400-801 (A01).

Part: SHAFT — CORRODED (CRGO DOOR HANDLE) · airframe 36,124 hrs · 26,338 cycles

FORWARD CARGO DOOR OUTER HANDLE SHAFT HARDWARE IS CORRODED. C-CHECK RO 1/17/2021. CLEANED FWD CARGO DOOR OUTER HANDLE SHAFT HARDWARE. FOUND NO CORROSION PRESENT, REF CRJ700 SRM 51-26-00-001-001-A01. REPLACED ONE STRIPPED NUT, REF CRJ700 SRM 51-41-02-001-001-A01.

Part: SCREW — BROKEN (RT WING PANEL) · airframe 36,124 hrs · 26,338 cycles

SCREW SHANK STUCKED ON RT WING PANEL 684FB. C-CHECK RO 1/17/2021. REMOVED SCREW SHANK AND COMPLIED WITH NECESSARY REPAIRS, IAW REO 670-57-52-477 REV- DATED 2020-12-17. SEE CONTINUATION CARD FOR DETAILS.

Part: BRACKET — BROKEN (PANEL) · airframe 36,124 hrs · 26,338 cycles

1 EACH BRACKET BROKEN ON PANEL 433BB. C-CHECK RO 1/17/2021. REMOVED AND REPLACED 1 EACH BRACKET BROKEN ON PANEL 433BB, IAW CRJ 700 SRM 51-42-06-001-001-A01.

Part: SKIN — DAMAGED (ZONE 100) · airframe 36,124 hrs · 26,338 cycles

FS 1031.00-FS 1051.00 STRG 23-24RT EXTERIOR SKIN PITTING DAMAGE, MARKED. C-CHECK RO 1/17/2021. REPAIRED AREA ON FUSELAGE SKIN BETWEEN FS 1031.00 TO FS 1051.00 BETWEEN STRINGER 23R TO STRINGER 24R TO COMPLY WITH REO 670-53-61-1778 REV- DATE 2020-12-02. SEE CONTINUATION FOR FUTHER DETAILS.

Part: PANEL — ERODED · airframe 36,124 hrs · 26,338 cycles

LEADING EDGE OF PANEL 331BL ERODED ENTIRE LENGTH. C-CHECK RO 1/17/2021. BLENDED LEADING EDGE PANEL 331BL, IAW CRJ700 SRM 51-12-00-001-001-A01 AND REO 670-55-12-175 REV DATE 2020-12-01.

Part: PANEL — ERODED · airframe 36,124 hrs · 26,338 cycles

LEADING EDGE OF PANEL 341BR ERODED ENTIRE LENGTH. C-CHECK RO 1/17/2021. BLENDED LEADING EDGE PANEL 341BR, IAW CRJ700 SRM 51-12-00-001-001-A01 AND REO 670-55-12-175 REV -- DATE 2020-12-01.

Part: BEARING — DAMAGED (LT AILERON) · airframe 36,124 hrs · 26,338 cycles

ROUTE LT AILERON TO BACK SHOP TO REMOVE AND REPLACE SWEDGED BEARINGS AND BUSHINGS AT HINGE POINTS (INBOARD, MID, OUTBOARD) ON LT AILERON, PER AMM. C-CHECK RO 1/17/2021. REMOVED AND REPLACED WORN BUSHINGS AND BEARINGS, REF CRJ 700 AMM 20-31-00-400-804-A01 FOR BEARINGS AND CRJ 700 AMM 20-31-00-400-802 FOR 2 EA BUSHINGS AND REO 670-57-61-107 REV-B DATED 2019-01-14 FOR 2 EA, OVERSIZED BUSHINGS.

Part: BOLT — BROKEN (WHEEL) · airframe 32,779 hrs · 23,631 cycles

BROKEN TIE BOLTS. (INSP)MSO M2397945 SN DEC10-2409, 2 BOLTS. LAST SHOP VISIT FAT M2382446 TIRE CHANGE, 3RD CYCLE ON BOLTS SINCE OVERHAUL. MS21250-08034 BOLTS USED ON THE WHEELS.

Part: NOT REPORTED — DENTED (FUSELAGE) · airframe 31,935 hrs · 22,934 cycles

DENT AFT OF FS 409.00 BETWEEN STR 16L AND 15L. (C-CHECK) RO: 09/21/2018. REPAIRED DENT AFT OF FS 409.00 BETWWEN STR 16L AND 15L IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,935 hrs · 22,934 cycles

FOUND LT FS220 FRAME HAS CRACK INDICATION FROM FASTENER HOLE TOWARDS LIGHTNING HOLE APPROX 1/8" LONG. (C-CHECK) RO: 09/21/2018. REMOVED AND INSTALLED NEW SERVICEABLE FRAME AT LT FS220 IAW SRM.

Part: STRINGER — CORRODED (BS 333-349) · airframe 30,515 hrs · 21,794 cycles

STRINGER 26R CORRODED BETWEEN BS 333 AND 349. MAINTENANCE REPLACED THE STRINGER.

Part: STRINGER — CORRODED (BS 280-310) · airframe 30,515 hrs · 21,794 cycles

STRINGER 25R HAS CORROSION BETWEEN BS 280 - 295 AND 295 - 310. REMOVED AND REPLACED THE STRINGER AND SPLICE IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-06-001-001-A01, AND DRAWING SH670-31630.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 30,515 hrs · 21,794 cycles

ONE CARGO TRACK PAD CORRODED. REMOVED AND REPLACED THE CARGO TRACK PAD IAW SRM 51-42-21-001-001-A01.

Part: SPLINE — CORRODED (FUSELAGE) · airframe 30,515 hrs · 21,794 cycles

SPLICE ANGLE AT FS939 ON AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE IS CORRODED. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE SPLICE ANGLE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,515 hrs · 21,794 cycles

FLOOR SEAT RAIL SEGMENT RBL9 FS847-969 HAS CORROSION. MAINTENANCE REPLACED FLOOR SEAT RAIL SEGMENT AT RBL9 FS847-969.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 30,515 hrs · 21,794 cycles

PASSENGER DOOR OPENING UPPER MID CAP ANGLE BETWEEN FS 310-349 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED ANGLE

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,515 hrs · 21,794 cycles

FLOOR SEAT RAIL SEGMENT LBL9 FS581-677 HAS CORROSION. MAINTENANCE REPLACED FLOOR SEAT RAIL SEGMENT LBL9 FS581-677.

Part: SEAT TRACK — CORRODED (BS 379-581) · airframe 30,515 hrs · 21,794 cycles

SEAT TRACK LBL 9, BS 379 - 581 CORRODED. MAINTENANCE REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 830-969) · airframe 30,515 hrs · 21,794 cycles

SEAT TRACK BS 830 - 969 HAS CORROSION. MAINTENANCE REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,515 hrs · 21,794 cycles

LEFT SIDEWALL SEAT RAIL SEGMENT FS565-677 HAS CORROSION. MAINTENANCE REPLACED LEFT SIDEWALL SEAT RAIL SEGMENT AT FS565-677.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 30,515 hrs · 21,794 cycles

SEAT TRACK CORRODED AT RBL 9, BS 349 - 485. MAINTENANCE REPLACED THE SEAT TRACK.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 30,515 hrs · 21,794 cycles

LEFT VERTICAL AFT DRAG ANGLE CRACKED, FORWARD END. MAINTENANCE REPLACED THE AFT DRAG ANGLE.

Part: STRUCTURE — CORRODED (BS 533) · airframe 30,515 hrs · 21,794 cycles

LBL 9 PACKER CORRODED AT BS 533. MAINTENANCE REPLACED THE PACKER.

Part: BOLT — DIRTY (EMERGENCY EXIT) · airframe 30,515 hrs · 21,794 cycles

RIGHT OVERWING EMERGENCY EXIT DOOR FAILED FUNCTIONAL CHECK. MAINTENANCE REMOVED SHOOT BOLTS, CLEANED, LUBED, REINSTALLED SHOOT BOLTS IAW SRM 51-26-00-001-001-AO1.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 28,549 hrs · 20,346 cycles

DAMAGE FOUND ON FLOORBEAM AT LBL27. REPAIRED PER EC/TC MM 670-35332S01.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,549 hrs · 20,346 cycles

CORROSION FOUND ON AFT CARGO DOOR LOWER SILL BETWEEN FS1025-1035. PERFORMED BLEND OUT REPAIR IAW REO 670-53-61-913 AND EC/TC REO 670-53-61-913.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,549 hrs · 20,346 cycles

CORROSION FOUND ON RBL9 AT FS1031.00 FLOORBEAM. PERFORMED BEAM SPLICE REPAIR IAW SRM 53-00-44-201-001-A01 AND EC/TC EO 700-53-0372 AND REO 670-53-61-1300.

Part: BEAM — CORRODED (FUSELAGE) · airframe 28,549 hrs · 20,346 cycles

CORROSION FOUND ON LBL27 BETWEEN FS1000-1033.0. PERFORMED BEAM SPLICE REPAIR IAW SRM 53-00-44-201-001-A01 AND EC/TC EO 700-53-0376.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,549 hrs · 20,346 cycles

CORROSION FOUND ON SILL FWD OF SERVICE DOOR. PERFORMED BLEND OUT REPAIR IAW REO 670-53-00-390 AND EC/TC REO 670-53-00-390.

Part: SEAT — UNSERVICEABLE (COCKPIT) · airframe 28,077 hrs · 19,981 cycles

CAPTAINS SEAT WILL NOT MOVE ALL THE WAY BACK, RON. C/W REO 670-53-11-210 PERMANENT REPAIR, INSTALLED RIVETS IAW REO 670-53-11-210. OK FOR SERVICE, MCO CLOSED.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 26,431 hrs · 18,634 cycles

RT WING EMERGENCY EXIT EMERGENCY LIGHT INOPERATIVE. R & R EXTERIOR EMERGENCY LIGHT AFT OF EMERGENCY DOOR IAW AMM 33-51-15 AND AIPC 33-51-15. OPS TEST IAW 33-51-15, GOOD AT THIS TIME.

Part: DOOR — LACK OF LUBE (SERVICE DOOR) · airframe 26,314 hrs · 18,544 cycles

FORWARD GALLEY SERVICE DOOR FAILED FUNCTIONAL CHECK. CLEANED AND LUBED SERVICE DOOR IAW AMM 51-26-00-110-801-S01. REPERFORMED FUNCTIONAL TEST OF THE GALLEY SERVICE DOOR IAW AMM 52-41-00-720-801-A01. FUNCTIONAL TEST GOOD.

Part: SEAT TRACK — CORRODED (BS 847-969) · airframe 26,314 hrs · 18,544 cycles

SEAT TRACK CORRODED IN SEVERAL AREAS FROM BS 847 - 969. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, REO 670-53-00-343, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 26,314 hrs · 18,544 cycles

SEAT TRACK CORRODED IN SEVERAL AREAS FROM BS 677 - 708. FOUND TO BE OUT OF LIMITS IAW 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 785-847) · airframe 26,314 hrs · 18,544 cycles

SIDE SEAT TRACK CORRODED IN SEVERAL AREAS FROM FS 785.15 TO FS 847.00. CORROSION OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. R & R 1 SEAT RAIL AT 785.15 TO 847 RT IAW AMM 53-00-49-000-801-A03, 53-00-49-400-801-A03 AND 53-00-49-400-801-A03. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV M AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 26,314 hrs · 18,544 cycles

SEAT TRACK CORRODED IN SEVERAL PLACES FROM BS 677 - 708. FOUND TO BE OUT OF LIMITS IAW 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 708-761) · airframe 26,314 hrs · 18,544 cycles

SIDE SEAT TRACK CORRODED IN SEVERAL AREAS FROM FS 708.00 TO FS 761.85. DAMAGE FOUND TO BE OUT OF LIMITS SRM 53-41-101-001-A01. REMOVED SIDE SEAT RAIL RT SIDE BETWEEN FS 708-FS 761.85 IAW AMM 53-00-49-000-801, CONFIG A03. INSTALLED NEW SERVICEABLE SIDE SEAT RAIL RT SIDE BEWTEEN FS 708 AND FS 761.85 IAW AMM 53-00-49-4000-801, CONFIG A03. COMPLIED WITH ECTC REO 670-53-00-344 AND GREO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 26,314 hrs · 18,544 cycles

SEAT TRACK CORRODED IN SEVERAL AREAS FROM BS 785.15 - 847. FOUND OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A01 AND AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 26,314 hrs · 18,544 cycles

SEAT TRACK CORRODED IN SEVERAL AREAS FROM BS 708 - 761.85. FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-00-801 A01, AND AMM 53-00-49-400-801-A01.

Part: INTERCOSTAL — CHAFED (BS 1144-1162) · airframe 26,314 hrs · 18,544 cycles

LT INTERCOSTAL CHAFED AT STR 9 BETWEEN FS 1144-1162. REMOVED CHAFE DAMAGE FROM INTERCOSTAL IAW SRM 51-12-00-001-001 A0. DAMAGE IS WITHIN LIMITS OF GREO 670-53-61-292.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 26,314 hrs · 18,544 cycles

FLOOR PACKER CORRODED AT FS 349-RBL9. R & R FLOOR PACKER AT FS 349, RBL 9, REF SRM 51-42-06-001-001 A01.

Part: HINGE FITTING — GOUGED (PAX DOOR) · airframe 26,314 hrs · 18,544 cycles

PAX DOOR HINGE LUG NR 14 GOUGED, PAX DOOR SIDE. UPON FURTHER INVESTIGATION FOUND THAT LUG 14 AND 25 HAD GOUGES. REPAIRED PAX DOOR HINGE, DOOR SIDE IAW EC/TC REO 670-52-11-511-01 AND REO 670-52-11-511, LATEST REVISION.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 26,314 hrs · 18,544 cycles

RT SIDE, SEAT TRACK CORRODED OUT OF LIMITS BETWEEN BS 485 - 581. REMOVED THE SEAT TRACK IAW AMM 53-00-49-000-801, CONFIG A03. INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-400-801, CONFIG A03.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 26,314 hrs · 18,544 cycles

SEAT TRACK CORRODED AROUND 4 SCREW HOLES LBL9 AND BETWEEN BS 485 AND 581. CORROSION DETERMINED OUT OF LIMITS, REF REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-CONFIG A03 AND INSTALLED A NEW SERIVCABLE SEAT TRACK IAW AMM 53-00-49-400-801, CONFIG A03.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 26,314 hrs · 18,544 cycles

SEAT TRACK CORRODED AT 3 SPOTS ON RBL9 AND BETWEEN FS 581 TO FS 677. CORROSION ON SEAT TRACK AT RBL9, FS 581 TO FS 677 DETERMINED OUT OF LIMITS REF REO G70-53-00-013. R & R SEAT TRACK ON RBL 9 AT FS 581-FS 677 IAW AMM 53-00-49-400-801 A03, 53-00-49-000-801 A03. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV. M AS WRITTEN.

Part: ANGLE — CORRODED (BS 549) · airframe 26,314 hrs · 18,544 cycles

FRAME BS 549, ANGLE HAS CORROSION AT STR 25L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: STRAP — DAMAGED (BS 533) · airframe 26,314 hrs · 18,544 cycles

FRAME 533 "I" STRAP DAMAGED. REMOVED LIGHT SURFACE CORROSION AND PAINT AT DAMAGE IAW SRM 51-21-06-001-001-A01, STRAP IS .063" MATERIAL HOLE DAMAGE MEASURED .142". SUBMITTED DAMAGE TO ENGINEERING FOR PERMANENT DISPOSITION. REMOVED "I" STRAP/LOWER JOINT PLATE AND 5 EA ADDITIONAL FASTENERS TO GAIN ACCESS TO DISCREPANT AREA FOR ENGINEERING SUBMITTAL COMPLY WITH DISPOSITION WHEN RECEIVED. RECEIVED REPLACEMENT "I" STRAP JOINT PLATE AND TRANSFERED DRILLED MOUNTING HOLES IAW SRM 51-40-11-001-001-A01. RECEIVED REO 670-53-31-355, REV DATED 2015-10-31. FINISHED COUNTERSINKING AND INSTALLED REMAINING FASTENERS, REF: REO 670-53-31-355, REV AND DWG SH670-33750, REV V SRM 51-42-21-001-001-A01 AND 51-42-22-001-001-A01. RECEIVED AND COMPLIED WITH ECTC REO 670-53-31-355, REV DATED 10-31-15.

Part: HINGE FITTING — GOUGED (PAX DOOR) · airframe 26,314 hrs · 18,544 cycles

PAX DOOR HINGE LUGS 6 AND 14 GOUGED, ON AIRFRAME SIDE. UPON FURTHER INVESTIGATION FOUND THAT LUGS 5, 6 AND 14 WERE GOUGED. COMPLIED WITH GREO 670-53-21-582 AND ECTC REI 670-53-21-582. REPAIRED PASSENGER DOOR HINGE, FUSELAGE SIDE, IAW REO 670-53-21-582, REV B DATED 3/6/13.

Part: SEAT TRACK — CORRODED · airframe 26,314 hrs · 18,544 cycles

SEAT TRACK CORRODED AND OUT OF LIMITS AT RBL9 AND BETWEEN FS 34G TO FS 48S. REMOVED SEAT TRACK AT RBL 9 BETWEEN FS 349-485 IAW AMM 53-00-49-000-801, CONFIG A03. INSTALLED NEW SERVICABLE SEAT RAIL AT RBL 9 BETWEEN FS 349-485 IAW AMM 53-00-49-400-801, CONFIG A03. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV. M AS WRITTEN.

Part: ANGLE — CORRODED (PAX DOORWAY) · airframe 26,314 hrs · 18,544 cycles

PAX DOOR SURROUND STRUCTURE UPPER AND LOWER SILL CAP ANGLES ARE CORRODED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED PAX DOOR MID CAP ANGLE AND BLENDED CORROSION IN RF TO SRM 51-21-06-001-001-A01. BLENDED CORROSION ON PAX DOOR LOWERSILL CAP IN REF TO SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. R & R PAX DOOR UPPER AND LOWER SILL CAP ANGLES IN REF TO SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 26,314 hrs · 18,544 cycles

SEAT TRACK CORRODED RBL9 AND BETWEEN BS 485 - 581. CORROSION DETERMINED OUT OF LIMITS IAW REO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, 53-00-49-400-801 A03.

Part: FRAME — CORRODED (BS 364) · airframe 26,314 hrs · 18,544 cycles

FS 364 AT STR 27 HAS CORROSION FWD LEG BETWEEN INBD INTERCOSTALS. STARTED REMOVING CORROSION IAW SRM TASK 51-21-06-001-001-A01. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FRAME DETERMINED TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 26,314 hrs · 18,544 cycles

LT SIDE, SEAT TRACK CORRODED IN SEVERAL SPOTS BETWEEN BS 485 - 581. CORROSION DETERMINED OUT OF LIMITS, IAW REO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND 53-00-49-40-801 A03.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 26,314 hrs · 18,544 cycles

CRAWLWAY FLOOR PANEL ANGLE AT F/S 280 HAS CORROSION. REMOVED CRAWLWAY FLOOR PANEL ANGLE IAW SRM 51-42-06-001-001 A01. INSTALLED CRAWLWAY FLOOR PANEL ANGLE IAW SRM 51-42-06-001-001 A01 AND SRM 51-42-21-001-001 A01. LOCATED AND DRILLED NEW SERVICABLE ANGLE IAW SRM 51-40-11-001-001 A01.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 26,314 hrs · 18,544 cycles

LT COCKPIT FLOOR SUPPORT ANGLE CRACKED AND HAS CORROSION AT THE AFT SIDE. REMOVED THE LT COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED FASTENER HOLES IN NEW, SERVICEABLE LT COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-40-11-001-001-A01 AND STARTED INSTALLATION OF ANGLE IAW SRM 51-42-06-001-001-A01. COMPLETED INSTALL OF LT COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 26,314 hrs · 18,544 cycles

INTERCOSTAL AT STRINGER 27R, BS 364 HAS CORROSION. LATCH PIN INTERCOSTAL 27R AT FS 364 IS A NO DAMAGE ALLOWED AREA IAW SRM 53-21-23-101-003-A01. REMOVED RIVETS LOWER LEG OF INTERCOSTAL THROUGH SKIN IAW SRM 51-42-06-0001-001-A01 AND FOUND 3 HILIGHTS IAW SRM 51-42-21-001-001-A01. REMOVED, INSTALLED 27R AT FS364 IAW SRM TASK 51-42-06-001-001-A01, 51-42-21-001-001-000-A01. LOCATED AND DRILL, AND INSTALL NEW INTERCOSTAL IAW SRM 51-42-06-001-001-46-874-271.

Part: FRAME — CORRODED (BS 319) · airframe 26,314 hrs · 18,544 cycles

BS 319 FRAME LT OF STR 27 AFT SIDE HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REWORK AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 58-21-06-101-002-A01. REMOVED CLEAT AT STR 27 AND FS 319 FOR ACCESS IAW SRM 51-42-06-001-001-A01. INSTALLED STR CLEAT AT STR 27 AND FS 319 IAW GREO 670-53-21-799 AND ECTC REO 670-53-21-799-02. COMPLIED WITH ECTC REO 670*-53-21-799-02 AS NEEDED FOR FRAME REPAIR. REPAIRED FRAME BS 319.7 IAW REO 670-53-21-799 BY COMPLYING WITH ECTC REO 670-53-21-794.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 26,314 hrs · 18,544 cycles

INTERCOSTAL 27L AT BS 364 HAS CORROSION. INTERCOSTAL 27L IS A NO DAMAGE ALLOWED AREA IAW SRM 53-21-23-101-003 A01 AT FS 364. REMOVED RIVETS AT BOTTOM INTERCOSTAL THROUGH SKIN IAW SRM 51-42-06-001-001 A01 AND FORWARD HIGHLIGHTS IAW SRM 51-42-21-001-001 A01. REMOVED INTERCOSTAL AT 27L AT F/S 364 IAW CRJ 51-42-06-001-001 A01 AND 51-42-21-001-001 A01 SRM TASKS. LOCATED, DRILLED, AND INSTALLED NEW INTERCOSTAL IAW SRM 51-42-00-001-001 A01.

Part: FRAME — CORRODED (BS 295) · airframe 26,314 hrs · 18,544 cycles

F/S 295, FRAME STR 26L-26R FWD AND AFT SIDE HAS CORROSION. REMOVED CLEATS FROM STR 26L, 27, 26R AND FLOOR SUPPORT FROM FRAME 395 TO GAIN ACCESS TO CORROSION IAW SRM 51-42-06-001-001-A01. REMOVED CORROSION IAW 51-21-06-001-001-A01 ON FRAME 295 AT STRS 26L -26R. FRAME 295 AT STR 26L-26R, 100 PERCENT MATERIAL LOSS IAW 53-00-00-101-001-A01, FRAME REPAIR REQUIRED. REPAIRED FRAME BS 295 IAW REO 670-53-21-799 BY COMPLYING WITH EC/TC REO 670-53-21-799.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 26,314 hrs · 18,544 cycles

CORROSION ON RT FLOOR SUPPORT AT SEVERAL LOCATIONS FROM FS 280 TO FS 319. REMOVED CORROSION ON RT FLOOR SUPPORT AT SEVERAL LOCATION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH ECTC REO 670-53-00-390 AND REO 670-53-00-390, REV.

Part: STRINGER — CORRODED (BS 319) · airframe 26,314 hrs · 18,544 cycles

F/S 319, STR 26R HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. OUT OF LIMITS IAW 53-1-03-101-001-A01. REMOVED FS 333, SPLICE AND RIVETS FROM FS 333 TO 310 IAW SRM 51-42-06-001-001-A01. RECEIVED NEW SPLICE LOCATED, DRILLED & INSTALLED NEW SPLICE IAW SRM 51-42-00-001-001-A01. REMOVED, LOCATED AND PARTALLY INSTALLED STR FROM FS 319-FS 295 STR 26R IAW SRM 51-42-06-001-001-A01. CONTINUED INSTALLING STR 26R BETWEEN FS 280 TO FS 295 IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: FRAME — CORRODED (BS 310) · airframe 26,314 hrs · 18,544 cycles

F/S 310, FRAME STR 26L-26R FWD SIDE HAS CORROSION. BLENDED CORROSION ON FS 310 BETWEEN STRINGERS 26L AND 26R, 100 PERCENT MATERIAL LOSS, FRAME IS OUT OF LIMITS IN REF TO SRM 53-21-06-101-002-A01. RECEIVED AND STARTED INSTALLATION OF FRAME AT BS 310 IAW GREO 670-53-21-0799-01. REMOVED FLOOR POST AT STR 24L IAW SRM 51-42-06-001-001-A01. REPAIRED FRAME STR 310 IAW REO 670-53-21-799 BY COMPLYING WITH EC/TC REO 670-53-21-799.

Part: DOUBLER — CORRODED · airframe 26,314 hrs · 18,544 cycles

TCAS DOUBLER HAS CORROSION, EVALAUTED CORROSION ON TCAS ANTENNA FOR ACCESS TOP DOUBLER IN FOUND TO BE OF OF LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED TCAS ANTENNA FOR ACCESS TO DOUBLER IN SAME AREA REF: AMM 34-43-07-000-801-A03. REINSTALLED THE TCAS ANTENNA IAW: AMM 34-43-07-400-801-A03. OPS CHECK GOOD. REMOVED AND REINSTALLED TCAS DOUBLER REF: SRM 51-42-06-001-001-A01, 51-42-21-0001-001-A01, REV A WEB. RESTORED FINISH TO REPAIR AREA AS NEEED REF ARM 51-21-16-001-001-A01 AND APPLIED CIC IAW SRM 51-21-11-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 310-333) · airframe 26,314 hrs · 18,544 cycles

CORROSION ON INTERCOSTAL BETWEEN FS 310 - FS 333, LBL 9. REMOVED CORROSION ON INTERCOSTAL FS 319, LBL 9 IAW SRM 51-21-06-001-001-A01. MAX MATERIAL REMOVED .005. FURTHER EVALUATION FOUND INTERCOSTAL BETWEEN FS 310-FS 333, LBL 9. REMOVED AREAS TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-21-43-101-001-A01 IAW NOTE 1: DAMAGE ONLY ALLOWED IN 1 ELEMENT. R & R INTERCOSTAL IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 DWG SH670-32120.

Part: FRAME — CORRODED (BS 319) · airframe 26,314 hrs · 18,544 cycles

F/S 319, FRAME STR 26L-25R FWD SIDE HAS CORROSION. BLENDED CORROSION ON FS 319 FROM STRINGERS 26L AND 25R REF TO SRM 51-21-06-001-002-A01. BLENDED AREAS ARE OUT OF LIMITS IAW SRM 53-21-06-101-002-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REPAIRED FRAME ST 319.7 IAW REO 670-53-21-799 BY COMPLYING WITH EC/TC REO 670-53-21-799.

Part: DOOR FRAME — CORRODED (COCKPIT) · airframe 26,314 hrs · 18,544 cycles

LEFT COCKPIT DOOR POST CORRODED ON THE LOWER SECTION AT FLOOR LEVEL 280 BULKHEAD. REMOVED LEFT COCKPIT DOOR POST CLIP TO FACILITATE THE REMOVAL OF CORROSION ON DOOR POST IAW SRM 51-42-06-01-001-A01 & 51-42-13-001-001-A01. INSTALLED CLIP IAW SRM 51-42-06-001-001-A01, 51-52-13-001-001-A01. REMOVED CORROSION FROM LT COCKPIT DOOR & CLIP IAW SRM 51-21-06-001-001-A01. MAXIMUM MATERIAL REMOVED FROM CLIP WAS .007" & OUT OF LIMIT. VERIFIED CLIP WAS REPLACED WITH LOCAL FAB OF NEW CLIP CC670-34191 IAW EA 32-2015-394, SECTION 1, STEP 1, F AND G. COMPLIED WITH EA 32-2015-394.

Part: FLOOR SUPPORT — CRACKED (NOT REPORTED) · airframe 26,314 hrs · 18,544 cycles

RT COCKPIT FLOOR SUPPORT ANGLE CRACKED AT AFT LOCATION. REMOVED THE RT COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED FASTENER HOLES IN NEW, SERVICEABLE RT COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-40-11-001-001-A01 AND STARTED INSTALLATION OF ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-06-001-001-A01. COMPLETED INSTALL OF RT COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-10-001-001-A01. RESTORED FINISH TO RT COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-25-00-001-001-A01.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 26,314 hrs · 18,544 cycles

RT FWD EQUIPMENT BAY ADG PUMP DOUBLER CRACKED AT CORNER. RECEIVED REO 670-53-11-1105. COMPLIED WITH ECTC REO 670-53-11-1105.

Part: HANDLE — BINDING (ESCAPE HATCH) · airframe 26,314 hrs · 18,544 cycles

CREW ESCAPE HATCH OUTER HANDLE WILL NOT OPEN. CLEANED CREW ESCAPE HATCH OUTER HANDLE AND LOBED AND PERFORMED OP CHECK IAW AMM 12-20-52-640-804, A01, AND 52-22-02-710-801, A01. OPS CHECKS GOOD AT THIS TIME.

Part: HINGE FITTING — GOUGED (DOOR) · airframe 26,314 hrs · 18,544 cycles

ASD HINGE, FUSELAGE SIDE IS GOUGED ON AFT LUG LANDING. REPAIRED PASSENGER DOOR HINGE, FUSELAGE SIDE IAW REO 670-53-21-582, REV B, DATED 03/06/2013. ENGINEERING DISPOSITION NOT REQUIRED AT THIS TIME BLEND OUT AT AFT LUG LAND FOUND WITHIN LIMITS OF REO 670-53-21-582, REV B DISPSOITION IV.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,044 hrs · 18,335 cycles

CABIN EMERGENCY LIGHTS CEILING LEVEL LIGHTED EXIT SIGN, CURVE SIGN, AFT LIGHTS OUT, RED, WHITE AND BLUE, CABIN EMERGENCY LIGHTS: CEILING LEVEL LIGHTED EXIT SIGNS, CURVED SIGNS, ITEM RESOLVE UNDER MDDR: A529260, RELAMPED CABIN EMERGENCY LIGHTS CEILING LIGHT EXIT SIGNS IAW AMM 20-41-00. OPS CHECKED GOOD, PCB CONTROL IAW AMM 23-31-17 PLAC REMOVED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 25,834 hrs · 18,174 cycles

ROW 9 CEILING EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED BULB IN ROW 9 EMERGENCY EXIT CEILING FLOOD LIGHT IAW AMM 33-51-07. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 25,260 hrs · 17,720 cycles

12CD LOWER EXIT SIGN HAVE 1 LIGHT BULB BURNED. INSTALLED LIGHT BULB IN LOWER EXIT SIGN 12CD IAW AMM 33-51-05, OPS CHECK GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 24,711 hrs · 17,287 cycles

EMERGENCY LIGHT DAMAGED AT SEAT 5AB & 6AB. R & R THE LIGHT IAW AMM 33-51-01.

Part: BULKHEAD — CORRODED (BS 280) · airframe 21,877 hrs · 15,206 cycles

RT LOWER BULKHEAD WEB AT FS 280 IS CORRODED. REMOVED CORROSION ON RT LOWER BULKHEAD IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-11-594.

Part: FRAME — CORRODED (BS 286) · airframe 21,877 hrs · 15,206 cycles

CORROSION ON FRAME, LBL 9 FS 286 UNDER TOP STRAP. REMOVED CORROSION IAW ASRM 51-21-06-001-001-A01. MAJOR REPAIR.

Part: SKIN — CHAFED (BS 977) · airframe 21,951 hrs · 15,262 cycles

SKIN CHAFED AT BS 977, STRINGER 27, REPAIRED IAW EC/TC, REO 670-53-00-290 AND MODSUMIS 670538200021.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,877 hrs · 15,206 cycles

FS 280 FLOORBEAM CORRODED ON RT SIDE AT DRIP TRAYS. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01 AND 53-21-43-101-001-A01. REPLACED FLOORBEAM IAW SB670BA-53-041. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,877 hrs · 15,206 cycles

FS 280 FLOORBEAM CORRODED ON LT SIDE AT DRIP TRAYS. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01 AND 53-21-43-101-001-A01. REPAIRED IAW SB670BA-53-041. MAJOR REPAIR.

Part: LATCH — LACK OF LUBE (PAX DOOR) · airframe 21,877 hrs · 15,206 cycles

DOOR FAILED FUNCTIONAL TEST OF THE PAX DOOR COMPLETE UNLOCK CYCLE, FORCE GAUGE WAS AT 20LB. AT END OF CYCLE. LUBRICATED PAX DOOR LATCH PINS AND LATCH CAMS IAW AMM 12-20-52-640-809. PERFOMED FUNCTIONAL CHECK OF PAX DOOR IAW AMM 52-11-00-720-801, FUNCTIONAL CHECK GOOD.

Part: HANDLE — NO TEST (RT OVERWING DOOR) · airframe 21,877 hrs · 15,206 cycles

RT OVERWING EMERGENCY EXIT FAILED HANDLE PULL TEST. REMOVED SHOOT BOLT TO INSPECT LINK RODS IAW AMM 52-21-02-000-801. CLEANED AND INSPECTED SHOOT BOLTS AND LINK RODS WITH CONTACT CLEANER INSTALLED SAME SERVICEABLE SHOOT BOLTS IAW AMM 52-21-02-400-801 FUNCTIONAL TEST GOOD IAW AMM 52-21-00-720-801.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,456 hrs · 14,881 cycles

NR 5 EXTERIOR EMERGENCY LIGHT IS OUT. RELAMPED NR 5 EXT EMERGENCY LIGHT IAW AMM 33-51-15, OPS CHECKED GOOD.

Part: HINGE — CHAFED (PAX DOOR) · airframe 21,320 hrs · 14,778 cycles

DURING PAX DOOR HINGE INSPECTION, FOUND CHAFING DAMAGE. REPAIRED IAW REO 670-52-11-511. MAJOR REPAIR IAW GMM 5-3.

Part: MEGAPHONE — UNSERVICEABLE · airframe 21,056 hrs · 14,593 cycles

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

Part: ADC — MALFUNCTIONED · airframe 20,754 hrs · 14,376 cycles

EFIS COMPUTER MONITOR, IAS, ALT, HDG ON BOTH SIDES, STBY AIRSPEED ALSO FAILED, STALL FAIL, MACH TRIM CAUTION. R & R BOTH ADC'S IAW AMM 34-13-01-000-801, 400-801. R & R ISI IAW AMM 34-12-01-000-801, 400-801.

Part: DOOR — BINDING (MAIN PAX) · airframe 19,829 hrs · 13,723 cycles

GATE ON ARRIVAL F/A UNABLE TO OPEN DOOR. HANDLE STUCK/DIFFICULT TO MOVE. OPENED AFTER MULTIPLE ATTEMPTS: HANDLE STICK BINDING. OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECK GOOD, NO FURTHER ISSUES AT THIS TIME.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 19,389 hrs · 13,409 cycles

FWD STOP BRACKET ON DOOR SURROUND STRUCTURE IS CRACKED. R & R FWD STOP BRACKET ON DOOR SURROUND STRUCTURE IAW SRM 51-41-20.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,354 hrs · 13,383 cycles

CEILING EMERGENCY LIGHT AT ROW 6 INOPERATIVE. RELAMPED CEILING EMERGENCY LIGHT AT ROW 6 IAW AMM 33-51-09, OPS CHECKED GOOD.

Part: MEGAPHONE — UNSERVICEABLE (CABIN) · airframe 17,520 hrs · 12,035 cycles

MEGAPHONE MISSING HARDWARE. R & R MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,520 hrs · 12,035 cycles

CABIN CEILING EMERGENCY LIGHT NR 5 INOPERATIVE. RELAMPED CABIN CEILING EMERGENCY LIGHT NR 5 AS REQUIRED. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 17,520 hrs · 12,035 cycles

CABIN CEILING EMERGENCY LIGHT NR 1 INOPERATIVE. FOUND NR 1 EMERGENCY CEILING LIGHT ELECTRICAL CONNECTER DISCONNECTED ON THE CEILING PANEL. RECONNECTED CABIN CEILING EMERGENCY CONNECTOR ON THE CEILING PANEL IAW AMM 25-26-05. OPS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (BRAKES) · airframe 17,194 hrs · 11,807 cycles

AFTER GEAR RETRACTION, RECEIVED AN ANTI-SKID OTBD CAUTION MESSAGE AND AN OTBD GROUND SPOILER FAULT STATUS MESSAGE. RAN QRH CHECKLIST. DECLARED EMERGENCY AND LANDED NORMAL. R & R RT OTBD TRANSDUCER IAW AMM 32-44-01.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 16,874 hrs · 11,577 cycles

RT MIDDLE EXTERIOR EMERGENCY LIGHT IS NOT LIGHTING DURING OPS CHECK. REPLACED LIGHT BULB IAW AMM 33-51-15-000-801 & 33-51-15-400-801. OPS CHECKED FAILED. FOUND LOOSE CONNECTION. RECONNECTED IAW ESPM 20-26-00, OPS CHECKED GOOD IAW AMM 33-51-00-710-801-A01.

Part: BATTERY PACK — INTERMITTENT (EMERGENCY LIGHT) · airframe 16,874 hrs · 11,577 cycles

EMERGENCY LIGHTS ILLUMINATE UNCOMMANDED. TROUBLESHOT EMERGENCY LIGHTS & VERIFIED DISCREPANCY TO BATTERY PACK NR 2 DISCONNECTED THEN RECONNECTED. CONNECTOR PL124P1/P2 PERFORMED SUCCESSFUL OPS TEST OF EMERGENCY LIGHTS SYS REF SSM 33-50-00; SCHEM 2 SHEET 3 AND AMM 33-51-00-710-801.

Part: FLOORBOARD — CRACKED · airframe 16,871 hrs · 11,574 cycles

FWD EQUIPMENT COMPARTMENT RT FLOOR CRACKED ADJACENT TO ADG PUMP. REPAIRED IAW REO 670-57-11-509 AND GENERIC REO 670-53-15-509 REV--, DATED 07/06/2010 AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 667-708) · airframe 16,871 hrs · 11,574 cycles

SEAT TRACK IS CORRODED BETWEEN FS 667.00 - 708.00. REPAIRED IAW REO 670-53-00-343 AND REO 670-53-00-343 REV.

Part: STRINGER — CORRODED (BS 333-349) · airframe 16,871 hrs · 11,574 cycles

STRINGER 6RT BETWEEN FRAMES 333-349 CORRODED. REPAIRED IAW REO 670-53-21-744.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 16,871 hrs · 11,574 cycles

INTERCOSTAL AT FS 364 S27R CORRODED. INSTALLED INTERCOSTAL IAW SRM 51-42-21-001-001 & 51-42-06.

Part: STRINGER SPLICE — CORRODED (BS 319.7-333) · airframe 16,871 hrs · 11,574 cycles

STRINGER SPLICE 25R FS 319.70-333.00 CORRODED. REMOVED STRINGER SPLICE IAW SRM 51-42-06-001-001. INSTALLED NEW STRINGER SPLICE IAW SRM 51-42-00-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 364 S27L) · airframe 16,871 hrs · 11,574 cycles

INTERCOSTAL AT FS 364.00 S27L CORRODED. REMOVED CORRODED INTERCOSTAL, DRILLED AND INSTALLED NEW IAW SRM 51-42-06-001-001.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 16,871 hrs · 11,574 cycles

MAIN AVIONICS BAY FLOORBEAM ANGLE WHICH ATTACHES TO FS 280 CRACKED. REMOVED AND INSTALLED A SERVICEABLE FLOORBEAM ANGLE IAW SRM 51-42-06-0014-001-A01 AND 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,871 hrs · 11,574 cycles

BS 280 FLOORBEAM CORRODED. REPAIRED IAW REO 670-53-11-047.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 16,871 hrs · 11,574 cycles

RIGHT SEAT TRACK IS CORRODED BETWEEN FS 379-485. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 16,871 hrs · 11,574 cycles

CABIN RT SIDE SEAT TRACK IS CORRODED BETWEEN FS 485-565. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 16,871 hrs · 11,574 cycles

CABIN LT SIDE SEAT TRACK IS CORRODED BETWEEN FS 708-761. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 863-977) · airframe 16,871 hrs · 11,574 cycles

RIGHT SIDE SEAT TRACK IS CORRODED BETWEEN FS 863-977. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 16,871 hrs · 11,574 cycles

CABIN LT SIDE SEAT TRACK IS CORRODED BETWEEN FS 785-863. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: FRAME — CORRODED (BS 319.7) · airframe 16,871 hrs · 11,574 cycles

FS 319.70 FRAME CORRODED BETWEEN STR 26 AND 27 RT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS .048. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-21-06-101-002-A01. RESTORED SURFACE FINISH SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 16,871 hrs · 11,574 cycles

CABIN SEAT TRACK IS CORRODED AT RBL 9.0 BETWEEN FS 485 - 581. REMOVED SEAT TRACK IAW AMM 53-00-49-000-807. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 16,871 hrs · 11,574 cycles

CABIN RT SIDE SEAT TRACK IS CORRODED BETWEEN FS 708-761. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: FRAME — CORRODED (BS 310) · airframe 16,871 hrs · 11,574 cycles

FRAME CORRODED AT FS 310 AND ON BOTH SIDES OF STR 27. CORROSION REMOVED IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PROCEDURE UT-3. MIN MATERIAL REMAINING IS .047. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-21-06-101-002-A01. RESTORED SURFACE FINISH IAW SRM 51-42-06-001-001-A01, 51-25-06-001-001-A01, AND 51-25-16-001-001-A01.

Part: WEB — CORRODED (BS 280) · airframe 16,871 hrs · 11,574 cycles

RT 280 WEB IS CORRODED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01. REMOVED DAMAGED WEB IAW REO 670-53-11-594. INSTALLED WEB IAW REO 670-570-53-11-594.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,871 hrs · 11,574 cycles

BS 280 CROSSBEAM IS CORRODED. REMOVED AND REPLACED CROSSBEAM IAW SRM CH 51-42-06-001-001, 51-42-21-001-001 & REO 670-53-11-047.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,871 hrs · 11,574 cycles

COCKPIT FLOORBEAM AT FS 280.00 IS CORRODED. REMOVED AND REPLACED FLOORBEAM ANGLE IAW SRM 51-42-06-001-001.

Part: ATTACH ANGLE — CORRODED (BS 280) · airframe 16,871 hrs · 11,574 cycles

ATTACH ANGLE AT FS 280.00 BULKHEAD CORRODED. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND WITH IN LIMITS IAW SRM 53-00-00-101-001. APPLIED PRIMER AND PAINT IAW SRM 51-21-11-001-A01.

Part: SEAT TRACK — CORRODED (BS 863-977) · airframe 16,871 hrs · 11,574 cycles

CABIN LT SIDE SEAT TRACK IS CORRODED BETWEEN FS 863-977. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 16,871 hrs · 11,574 cycles

RIGHT SIDE SEAT TRACK IS CORRODED BETWEEN FS 677-708. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 55-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 16,871 hrs · 11,574 cycles

CABIN LT SIDE SEAT TRACK IS CORRODED BETWEEN FS 485-565. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 16,871 hrs · 11,574 cycles

CABIN LT SIDE SEAT TRACK IS CORRODED BETWEEN FS 379-485. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: STRINGER — CORRODED (BS 295-310) · airframe 16,871 hrs · 11,574 cycles

STRINGER 26 RT BETWEEN FRAMES 295.00 AND 310.00 HAS CORROSION AROUND SEVERAL RIVET SHANKS. REMOVED CORROSION IAW 51-42-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING OS .042. DAMAGE IS OUT OF LIMITS IAW SRM CH 53-21-03-101-002. R & R STRINGER IAW SRM CH 51-42-06-001-001.

Part: SEAT TRACK — CORRODED (BS 684-835) · airframe 16,871 hrs · 11,574 cycles

CABIN SEAT TRACK IS CORRODED AT RBL 9.0 BETWEEN FS 684-835. REMOVED SEAT TRACK IAW AMM 53-00-49-000-807. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 16,871 hrs · 11,574 cycles

SEAT TRACK AT 9 LBL BETWEEN FS 379 - 485 IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-807. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581-684) · airframe 16,871 hrs · 11,574 cycles

CABIN SEAT TRACK IS CORRODED AT LBL 9.0 BETWEEN FS 581-684. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 16,871 hrs · 11,574 cycles

CABIN LT SIDE SEAT TRACK IS CORRODED BETWEEN FS 485-565. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349-385) · airframe 16,871 hrs · 11,574 cycles

CABIN SEAT TRACK IS CORRODED AT RBL 9.0 BETWEEN FS 349-485. REMOVED SEAT TRACK IAW AMM 53-00-49-000-807. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 684-835) · airframe 16,871 hrs · 11,574 cycles

CABIN SEAT TRACK IS CORRODED AT LBL 9.0 BETWEEN FS 684-835. REMOVED SEAT TRACK IAW AMM 53-00-49-000-807. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 16,871 hrs · 11,574 cycles

CABIN RT SIDE SEAT TRACK IS CORRODED BETWEEN FS 785-863. REMOVED IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: FRAME — CORRODED (BS 319.7) · airframe 16,871 hrs · 11,574 cycles

FRAME CORRODED AT FS 319.70 AND BETWEEN STR 27 AND 26L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS .046. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-21-06-101-002-A01. RESTORED SURFACE FINISH IAW SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 835-977) · airframe 16,871 hrs · 11,574 cycles

CABIN SEAT TRACK IS CORRODED AT LBL 9.0 BETWEEN FS 835-977. REMOVED AND INSTALLED SEAT TRACK IAW AMM 53-00-49-000-801-A03.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 16,871 hrs · 11,574 cycles

CABIN RT SIDE SEAT TRACK IS CORRODED BETWEEN FS 565-677. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 581-684) · airframe 16,871 hrs · 11,574 cycles

CABIN SEAT TRACK IS CORRODED AT RBL 9.0 BETWEEN FS 581-684. REMOVED SEAT TRACK IAW AMM 53-00-49-000-807. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: STRINGER — CORRODED (BS 333-349) · airframe 16,871 hrs · 11,574 cycles

STRINGER 26 RT BETWEEN FRAMES 333 AND 349 HAS CORROSION AROUND SEVERAL RIVET SHANKS. REMOVED CORROSION IAW SRM 51-42-06-001-001-A01 AND 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS .050 FROM ORIGINAL .063. MATERIAL REMOVED IS .013. REPAIRED IAW REO 670-53-21-744.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 16,871 hrs · 11,574 cycles

LEFT SIDE SEAT TRACK IS CORRODED BETWEEN FS 677-708. REMOVED SEAT TRACK IAW AMM 53-0-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 835-977) · airframe 16,871 hrs · 11,574 cycles

CABIN SEAT TRACK IS CORRODED AT RBL 9.0 BETWEEN FS 835-977. REMOVED SEAT TRACK IAW AMM 53-00-49-000-807. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-803.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 16,871 hrs · 11,574 cycles

CABIN SEAT TRACK IS CORRODED AT LBL 9.0 BETWEEN FS 485 - 581. REMOVED SEAT TRACK IAW AMM 53-00-49-000-807. INSTALLED NEW SEAT TRACK IAW AMM CH 53-00-49-400-801.

Part: FRAME — CORRODED (BS 295) · airframe 16,871 hrs · 11,574 cycles

FS 275 FRAME CORRODED AT S29R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS .048. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-21-06-101-002-A01. RESTORED SURFACE FINISH IAW SRM 51-25-06-001-001-A01, 51-25-16-001-001-A01, AND 51-42-06-001-001-A01.

Part: WEB — CORRODED (BS 280) · airframe 16,871 hrs · 11,574 cycles

LEFT BS 280, WEB CORRODED. FOUND TO BE OUT OF LIMITS. CUT-OUT AREA IAW REO 670-53-11-594. PERFORMED EDDY CURRENT INSPECTION IAW REO 670-53-11-594 & NDTM PART 1, 51-20-006. NO INDICATIONS NOTED. INSTALLED NEW WEB IAW REO670-53-11-594, STEPS 5-7.

Part: STRINGER — CORRODED (BS 319.7-333) · airframe 16,871 hrs · 11,574 cycles

STRINGER 25 RT BETWEEN 319.7-333 HAS CORROSION AT SEVERAL RIVET SHANKS. REMOVED CORROSION IAW SRM 51-42-06-001-001-A01 AND 51-21-06-001-001-A01. .018 MATERIAL REMOVED, NO DAMAGE ALLOWED IN THIS AREA IAW SRM. R & R STRINGER IAW SRM 51-42-06-001-001.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,871 hrs · 11,574 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED IAW SRM 52-11-04-201-002-A01. PERFORMED EDDY CURRENT INSPECTION OF CUTLINE IAW SRM 52-11-04-201-002-A01. NO INDICATIONS NOTED.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 16,871 hrs · 11,574 cycles

PAX DOOR ANGLE CRACKED. R & R ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 16,871 hrs · 11,574 cycles

FWD EQUIPMENT COMPARTMENT RT FLOOR CRACKED ADJACENT TO ADG PUMP. REPAIRED CRACK IAW GREO 670-53-11-509.

Part: STEP — CRACKED (AIR STAIR DOOR) · airframe 16,871 hrs · 11,574 cycles

ASD WEATHER GUARD STEP CRACKED. R & R PAX DOOR LOWER STEP ASSY IAW AMM 52-11-04-000-806 AND 52-11-04-400-806. OPS TESTED, CHECKED GOOD IAW AMM 52-11-04-710-801.

Part: TILLER — FAILED (NLG STEERING) · airframe 16,046 hrs · 11,006 cycles

NOSE STEERING INOP (EMERGENCY DECLARED AS A PRECAUTION). R & R PILOT HAND WHEEL CONTROL IAW AMM 32-51-01. OPS CHECK GOOD AT THIS TIME. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,879 hrs · 10,886 cycles

EMEGENCY LIGHTING INOP. FOUND AFT SWITCH IN "ON" POSITION RECHARGED SYS IAW FIM 33-51-00. OPS CHECK GOOD. FAULT NO LONGER EXISTS. IAW MCC, NO FURTHER ACTION REQUIRED.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 15,732 hrs · 10,780 cycles

EMERGENCY LIGHT SWITCH IN THE ARM POSITION, CABIN EMERGENCY LIGHTS CYCLE ON AND OFF. R & R PCB 5 IN JB11 IAW AMM 24-06-11. R & R BATTERY PACK 1 AND BATTERY PACK 2 IAW AMM 33-51-17. PERFORMED OP TEST OF PCB 5 IN JB11 IAW AMM 24-06-11-710-801 AND 33-51-00-710-801. NO FAULTS FOUND AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,158 hrs · 10,392 cycles

AFT MOST CABIN CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED AFT MOST CABIN CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-09. OPS CHECK GOOD. RELAMPED AFT MOST CABIN CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-09. OPS CHECK GOOD. (CLOSED)

Part: ROLLER — BROKEN (PAX DOOR) · airframe 14,727 hrs · 10,102 cycles

PAX DOOR WILL NOT OPEN FROM OUTSIDE. FOUND FWD GUIDE ROLLER BROKEN REPLACED FWD GUIDE ROLLER IAW AMM 20-21-00. OPS CHECK PAX DOOR IAW AMM 52-11-00. (CLOSED)

Part: CIRCUIT BREAKER — TRIPPED (NLG STEERING) · airframe 14,702 hrs · 10,082 cycles

STEERING INOP CAUTION MSG AFTER TAKEOFF. (EMERGENCY DECLARED) FAULT MSG IAW FIM RESET PROCEDURES. MCC NO FURTHER ACTION IS REQUIRED. (CLOSED)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,767 hrs · 8,673 cycles

CABIN CEILING EMERGENCY 4TH FROM FRONT LIGHT INOP. RELAMPED CABIN CEILING EMERGENCY 4TH FROM FRONT LIGHT IAW AMM 33-51-09. OPS CHECK GOOD.

Part: PLACARD — UNKNOWN (CABIN) · airframe 12,182 hrs · 8,246 cycles

"EXIT" "OPEN" PLACARDS ON MAIN DOOR NEED REPLACING.

Part: BULKHEAD — CRACKED (BS 280) · airframe 11,952 hrs · 8,076 cycles

LEFT FS 280 WEB HAS CRACK AND CORRODED. REMOVED LT FS 280 LOWER BULKHEAD WEB IAW SRM 51-42-06-001-001-A01. DRILLED UP NEW FS 280 LOWER LT WEB IAW SRM 51-40-11-001-001-A01. OK TO INSTALL NEW WEB AS PER SRM 51-42-06 PG 1 - PG 17

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 11,952 hrs · 8,076 cycles

COCKPIT FLOOR SUPPPORT HAS EXFOLIATED CORROSION AT 2 EA NUTPLATE HOLES.

Part: FLOORBEAM — DAMAGED (BS 280) · airframe 11,952 hrs · 8,076 cycles

FS280 EXFOLIATED ON LT AND RT AND CTR OF BEAM. REMOVE LT & RT INTERCOSTALS PER SRM 51-42-21-001-001-A01. COMPLIED WITH GVI ON LT & RT INTERCOSTALSN. INSTALLED LT & RT INTERCOSTALS PER SRM 51-42-21-001-001-A01. REMOVED LBL9.0 & RBL9.0 ANGLES & DIAGONAL BRACKETS IAW SRM 51-42-22-001-001-A01 & 51-42-21-001-001-A01. COMPLIED WITH GVI OF LT & RT LBL & RBL P.0 ANGLES & DIAGONAL BRCAKETS. INSTALLED RBL 9.0 & LBL 9.0 7 ANGLES & DIAGONAL BRACKETS PER REO 670-53-11-047 REV E DATED 2009/08/13. DISCONNECTED LT & RT PULLEY BRACKETS AT FS 280 IAW 51-41-00-001-001-A01. COMPLIED WITH GVI LT & RT PULLEY BRACKETS. RE-CONNECTED (INSTALLED) LT & RT AILERON PULLEY BRACKETS PER SRM 51-42-06-001-001-A01. REMOVED FS 280 FLOORBEAM IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. MATCH DRILLE NEW FS 280 FLOORBEAM AS PER SRM 51-40-11 BEAM. INSTALLED NEW FS 280 RT BEAM PER SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01. REMOVED JB-2 PER AMM 24-01-01-000-801. REMOVED JB-3 PER AMM 24-02-01-000-801. PERFORMED GVI JB-2 NO DEFECTS NOTED. PERFORMED GVI JB-3 NO DEFECTS NOTED. REINSTALLED JB-2 PER AMM 24-01-01-400-801. OPS CHECKS ACCOMPLISHED ON W/O 7121015/91. REINSTALLED JB-3 PER AMM 24-02-01-400-801 OPS CHECKS ACCOMPLISHED W/O 7121015/91. PERFORMED GVI OF MODSUM PARTS NO DEFECTS NOTED. REMOVED MODSUM PARTS FROM LT & RT 280 BEAM PER SRM 51-42-21-001-00

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 11,057 hrs · 7,412 cycles

AFTER TAKE OFF, CLIMBING, 250 KTS IAS HAD ELEVATOR SPLIT CAUTION [EMERGENCY DECLARED - A/C RETURNED TO DAY AFTER T/O]...FLT 4995 CX

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,622 hrs · 7,065 cycles

F/A REPORTS OVERHEAD EMERGENCY EXIT LIGHTS IN GALLEY ARE BURNED OUT. FLT 5030 DEL 70 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,500 hrs · 6,982 cycles

LT OVERWING EMERGENCY EXIT LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS.

Part: LIGHT — NO TEST · airframe 9,710 hrs · 6,392 cycles

FLT 5531 - EMERGENCY EXIT LIGHTS W/N TEST.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 7,204 hrs · 4,648 cycles

FOUND FS 280 FWD FLOORBEAM ANGLE IN CORRODED.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 7,204 hrs · 4,648 cycles

LT VERTICAL STAB TO FUSELAGE ANGLE T/E CRACKED. NEEDS PAINT REMOVED FOR FURTHER EVALUATION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,204 hrs · 4,648 cycles

RT VERTICAL STAB TO FUSELAGE ANGLE T/E CRACKED. NEEDS PAINT REMOVED FOR FURTHER EVALUATION. CRACK CONFIRMED IN RADIUS . CRACK LENGTH MARKED.

Part: HINGE PIN — CORRODED (HORIZONTAL STAB) · airframe 7,204 hrs · 4,648 cycles

HORIZ STAB INNER AND BOTH OUTER HINGE PINS SHOW SIGNS OF CORROSION.

Part: PLACARD — WORN (CABIN) · airframe 7,204 hrs · 4,648 cycles

ASD "EXIT" PLACARD WORN. REMOVED AND REPLACED ASD "EXIT" PLACARD IAW CRJ 700 AMM 11-30-00.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 7,204 hrs · 4,648 cycles

ASD EXTERNAL HANDLE CRACKED. REMOVED AND REPLACED ASD EXTERNAL HANDLE. PERFORMED ASD HANDLE OPS CK IAW CRJ 700 AMM 52-11-03-701-801. NO DEFECTS NOTED.

Part: PLACARD — MISSING (CABIN) · airframe 6,183 hrs · 3,971 cycles

PAX DOOR PLACARD MISSING.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 6,040 hrs · 3,868 cycles

F/A FLASHLIGHT INOP.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 3,405 hrs · 2,180 cycles

EMERGENCY EXIT ALL LIGHT LENS COVER MISSING.

Part: TORQUE LINK — DAMAGED (MLG)

DURING CLIMB FROM ABQ-SLC, THE CREW RECEIVED A WOW INPUT CAUTION MESSAGE, AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO ABS, AND THE EMERGENCY VEHICLES WERE ROLLED. THE AIRCRAFT LANDED SAFELY IN ABS. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR TORQUE LINKS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE (M)

Part: LINE — MALFUNCTIONED (ENG DRIVEN PUMP)

DURING CRUISE, AT APPROX 36,000 FT, THE CREW RECEIVED A LT PACK HIGH TEMPERATURE MESSAGE. CREW COMPLIED WITH QRH TO TURN OFF PACK. ONCE PACK WAS TURNED OFF, A LT HYDRAULIC LOW PRESSURE 1 APPEARED FOLLOWED BY A LOUD NOISE AND HYDRAULIC QUANTITY FLUCTUATION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED. EMERGENCY VEHICLES WERE DISPATCHED WITH THE AIRCRAFT LANDING SAFELY. MAINT REMOVED AND REPLACED THE NR 1 EDP AND PRESSURE LINE. OPS CHECK GOOD. AC OK FOR SERVICE. (K)