N753EV

Part: ROLLER — FAILED INSP (LT SLAT TRACK) · airframe 44,147 hrs · 32,508 cycles

LH ROLLER ON SLATS 3-2 FWD 1B FAILED INSPECTION (C-CHECK RO 12/24/2024) (FILED CLOSED)OK, TO INSTALL. PA. 911290REMOVED AND REPLACED LH ROLLER ON SLAT 3-2 FWD IB IAW CRJ 700 AMM 27-81-44.

Part: ROLLER — FAILED INSP (ZONE 500) · airframe 44,122 hrs · 32,490 cycles

LH ROLLER ON SLATS 3-2 FWD 1B FAILED INSPECTION (C-CHECK RO 12/24/2024) (FILED OPEN)OK, TO INSTALL. PA. 911290REMOVED AND REPLACED LH ROLLER ON SLAT 3-2 FWD IB IAW CRJ 700 AMM 27-81-44.

Part: ROLLER — OUT OF LIMITS (RT SLAT TRACK) · airframe 44,147 hrs · 32,508 cycles

RH SLAT TRACK ROLLER 1-2 AFT OUTBD FLAT SPOT OUT OF LIMITS (C-CHECK RO 12/24/2024) (FILED CLOSED) OK TO INSTALL PA911290 REMOVED AND REPLACED RH SLAT TRACK ROLLER 1-2 AFT OUTBD IAW AMM 27-81-44.

Part: SLAT TRACK — OUT OF LIMITS (ZONE 600) · airframe 44,122 hrs · 32,490 cycles

RH SLAT TRACK ROLLER 1-2 AFT OUTBD FLAT SPOT OUT OF LIMITS (C-CHECK RO 12/24/2024) (FILED OPEN) OK TO INSTALL PA911290 REMOVED AND REPLACED RH SLAT TRACK ROLLER 1-2 AFT OUTBD IAW AMM 27-81-44.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 44,202 hrs · 32,554 cycles

RBL 12 COCKPIT FLOORBEAM CRACKED, OTBD SIDE, AT 280 BEAM. (C-CHECK RO 12/24/2024) (FILED CLOSED)PERFORMED REPAIR ON RBL 12 COCKPIT FLOOR BEAM OTBD SIDE AT 280 BEAM PER REO 670-53-11-896. REV. AMM 20-70-00.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 44,122 hrs · 32,490 cycles

RBL 12 COCKPIT FLOOR BEAM CRACKED, OTBD SIDE, AT 280 BEAM. (C-CHECK RO 12/24/2024) (FILED OPEN)PERFORMED REPAIR ON RBL 12 COCKPIT FLOOR BEAM OTBD SIDE AT 280 BEAM PER BOMBARDIER REO 670-53-11-896. REV. --. DATE: 2015-03-17. CRJ-700 AMM 20-70-00. NDT PERFORMED BY BARON NDT,LLC FAA CRS# 5NDR545D. REPORT # S121324-13. P.O. NUMBER: 174847. DATE OF INSPECTION: 13-DEC-2024. TOOL USE: COUNTING SCALE AV-4800. CAL DUE: DEC-2024.

Part: ATTACH BRACKET — CRACKED (RT FLAP FAIRING) · airframe 36,982 hrs · 26,855 cycles

RT WING FLAP STUB FAIRING ATTACH BRACKET CRACKED. C-CHECK RO 10/22/2020. ORDERED AND RECEIVED A NEW RT STUB FAIRING ATTACH BRACKET. LOCATED AND DRILLED THE NEW BRACKET AND INSTALLED, REF CRJ 700 SRM.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON SUPPORT BRACKET P/N SH670-41524-1 AT STGR 21R BETWEEN FS 349 AND FS 364. C-CHECK RO 10/22/2020. REMOVED AND REPLACED THE SUPPORT BRACKET AT STGR 21R BETWEEN FS 349 AND FS 364 WITH NEW, REF CRJ 700 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR WORK DETAILS.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON STGR 21R BETWEEN FS 349-FS 364. C-CHECK RO 10/22/2020. REMOVED CORRODED STR 21R BETWEEN FS 349-364 AND REPLACED WITH NEW, REFERENCING DWG AND CRJ 700. LEAK TEST GOOD. COMPLIED WITH TASK CARD.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 36,982 hrs · 26,855 cycles

LT INBOARD FLAP DENTED JUST INBOARD OF WS 54.55, MARKED. C-CHECK RO 10/22/2020. REPAIRED LT INBOARD FLAP LOWER SKIN DAMAGE, IAW CRJ700 SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

MAIN CABIN CROSSBEAM AT FS 549.00 FOUND CORROSION UNDER FLOORBEAM AT LBL 9. C-CHECK RO 10/22/2020. BLENDED CORROSION, WITHIN LIMITS, REF REO. ALL STEPS ACCOMPLISHED. SEE CONTINUE CARD FOR DETAILS.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

FS 280 RT CROSS BEAM HAS CORROSION. C-CHECK RO 10/22/2020. REMOVED CORRODED RT FS 280 CROSSBEAM AND REPLACED WITH NEW, REFERENCING DWG CRJ 700 SRM. COMPLIED WITH TASK CARD.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION AT APPROX FS 549 LBL 9 INBOARD ON FLOORBEAM. C-CHECK RO 10/22/2020. REPAIRED DAMAGED FLOORBEAM AT FS 549 LBL 9, REF CRJ700 SRM.

Part: MOUNT — CORRODED (FLOOR) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON FLOOR MOUNT FITTING AT NUTPLATE LOCATION, BETWEEN LBL 9 TO LBL 27 FS 310.00. C-CHECK RO 10/22/2020. CORROSION 100% THROUGH FLOOR MOUNTING FITTING, REMOVED CORRODED FITTING FROM FS 310.00 FLOOR SUPPORT POST, REF CRJ700 SRM. INSTALLED REPLACEMENT FITTING TO FS 310.00 FLOOR SUPPORT POST, REF CRJ700 SRM. RESTORED FINISH, APPLIED CORROSION INHIBITING COMPOUND TO INSTALLED FITTING.

Part: MOUNT — CORRODED (FLOOR) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON FLOOR MOUNT FITTING AT NUTPLATE LOCATION, BETWEEN LBL 9 TO LBL 27, FS 280.00 TO FS 295.00. C-CHECK RO 10/22/2020. CORROSION 100% THROUGH FLOOR MOUNTING FITTING, REMOVED CORRODED FITTING FROM INTERCOSTALS BETWEEN FS 280.00-FS 295.00 LBL 9-LBL 27, REF CRJ700 SRM. INSTALLED REPLACEMENT FITTING TO INTERCOSTALS BETWEEN FS 280.00-FS 295.00 LBL 9-LBL 27, REF CRJ700 SRM. RESTORED FINISH, APPLIED CORROSION INHIBITING COMPOUND TO INSTALLED FITTING.

Part: STRINGER SPLICE — CORRODED (E/E BAY) · airframe 36,982 hrs · 26,855 cycles

MAIN AVIONICS BAY STR 25R JOINT SPLICE AT FS 333.00 CORRODED. C-CHECK RO 10/22/2020. NO ALLOWABLE DAMAGE ON JOINT SPLICE. REMOVED AND INSTALLED NEW MAIN AVIONICS BAY STR 25R SPLICE AT FS 333.00, REF CRJ700 SRM AND DWG. NO LEAKS NOTED. COMPLIED WITH TASK CARD.

Part: MOUNT — CORRODED (FLOOR) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON FLOOR MOUNT FITTING AT NUTPLATE LOCATION, BETWEEN LBL 27 TO LBL 36, FS 280.00 TO FS 295.00. C-CHECK RO 10/22/2020. CORROSION 100% THROUGH FLOOR MOUNTING FITTING, REMOVED CORRODED FITTING FROM INTERCOSTAL BETWEEN FS 280.00-FS 295.00 LBL 27-LBL 36, REF CRJ700 SRM. INSTALLED REPLACEMENT FITTING TO INTERCOSTAL BETWEEN FS 280.00-FS 295.00 LBL 27-LBL 36, REF CRJ700 SRM. RESTORED FINISH, APPLIED CORROSION INHIBITING COMPOUND TO INSTALLED FITTING.

Part: MOUNT — CORRODED (FLOOR) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON FLOOR MOUNT FITTING AT NUTPLATE LOCATION, BETWEEN RBL 9 TO RBL 27, FS 280.00 TO FS 295.00. C-CHECK RO 10/22/2020. CORROSION 100% THROUGH FLOOR MOUNTING FITTING, REMOVED CORRODED FITTING FROM INTERCOSTALS BETWEEN FS 280.00-FS 295.00 APPROXIMATELY RBL 14-16, REF CRJ700 SRM. INSTALLED REPLACEMENT FITTING TO INTERCOSTALS BETWEEN FS 280.00-FS 295.00 APPROXIMATELY RBL 14-16, REF CRJ700 SRM. RESTORED FINISH, APPLIED CORROSION INHIBITING COMPOUND TO INSTALLED FITTING.

Part: FRAME — CORRODED (E/E BAY) · airframe 36,982 hrs · 26,855 cycles

MAIN AVIONICS BAY FS 319.70 LOWER FRAME CORRODED BETWEEN STR 27 AND STR 26R. C-CHECK RO 10/22/2020. REMOVED CORRODED FS 319.70 FRAME BETWEEN STR 27 AND STR 26R AND REPLACED WITH NEW, REFERENCING CRJ 700 SRM. LEAK TEST GOOD. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWEST FORM M-337.

Part: DOUBLER — CORRODED (TCAS ANTENNA) · airframe 36,982 hrs · 26,855 cycles

MAIN AVIONICS BAY TCAS ANTENNA DOUBLER CORRODED BETWEEN FS 295.00 AND FS 310.00. C-CHECK RO 10/22/2020. REMOVED CORRODED TCAS ANTENNA DOUBLER BETWEEN FS 295 TO FS 310 AND INSTALLED NEW, REF CRJ700 SRM AND DWG. NO LEAKS NOTED. COMPLIED WITH TASK CARD. COMPLETED SKYWEST FORM M-337.

Part: DOUBLER — CORRODED (GALLEY) · airframe 36,982 hrs · 26,855 cycles

THE GALLEY NR 1 HAS A CORRODED DOUBLER BEHIND THE FLOOR MOUNT FITTING (FOOT) AT THE INBOARD/AFT CORNER. C-CHECK RO 10/22/2020. REMOVED THE GALLEY NR 1 CORRODED DOUBLER BEHIND THE FLOOR MOUNT FITTING (FOOT) AT THE INBOARD/AFT CORNER REFERENCING ZODIAC AEROSPACE CMM DISASSEMBLY SECTION. INSTALLED A SERVICEABLE DOUBLER (P/N=933507-1) REFERENCING CMM.

Part: CHANNEL — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON LT FUSELAGE SIDE SEAT RAIL RETAINER (U CHANNEL) AT FS 752.00. C-CHECK RO 10/22/2020. REPLACED SEAT RAIL RETAINER WITH NEW (PN SH670-37557-3), REF CRJ700 AMM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RT FUSELAGE SIDE SEAT RAIL RETAINER (U CHANNEL) AT FS 581.00 TO FS 669.00. C-CHECK RO 10/22/2020. RECEIVED NEWLY FABRICATED RT FUSELAGE SIDE SEAT RAIL RETAINER (U CHANNEL) FROM FS 581.00 TO FS 669.00. DRILLED AND LOCATED, REF CRJ700 SRM. INSTALLED ON CAMP 21537949. SEE CONTINUE CARD.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RT FUSELAGE SIDE SEAT RAIL FROM FS 675.00 TO FS 713.00. C-CHECK RO 10/22/2020. REMOVED AND REPLACED WITH NEW THE RT SEAT TRACK AT FS 675-713 CRJ 700 AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RT FUSELAGE SIDE SEAT RAIL FROM FS 785.00 TO FS 855.00. C-CHECK RO 10/22/2020. REPLACED RT FUSELAGE SIDE SEAT RAIL FROM FS 785.00 TO FS 855, REF CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RT FUSELAGE SIDE SEAT RAIL AT FS 581.00 TO FS 669.00. C-CHECK RO 10/22/2020. REPLACED RT FUSELAGE SIDE SEAT RAIL AT FS 581-FS 669, REF CRJ700 AMM. SEE CONTINUE CARD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON JOINT STRAP AT FS 333.00 STGR 21R. C-CHECK RO 10/22/2020. REMOVED CORROSION ON JOINT STRAP AT FS 333.00 STGR 21R, REF CRJ 700 SRM. ORIGINAL MATERIAL IS .063, MATERIAL REMOVED IS .027, MATERIAL REMAINING .036, OUT OF LIMITS. PERFORMED REPAIR, REF REO. NO LEAKS NOTED.

Part: BRACKET — CORRODED (FLOOR) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON MACHINED BRACKET (FLOOR MOUNT PLATE) AT APPROXIMATELY FS 533 STGR 27. C-CHECK RO 10/22/2020. REMOVED CORROSION ON MACHINED BRACKET (FLOOR MOUNT PLATE) AT APPROXIMATELY FS 533 STGR 27, REF CRJ700 SRM. ORIGINAL MATERIAL THICKNESS IS 0.240,? REF DRW. REMAINING MATERIAL THICKNESS PER NDT IS 0.195? (LOOKING AT NUMBERS WRITTEN ON PART IN GRIDDED AREA). MATERIAL LOSS IS 0.045?. DAMAGE IS IN A NO DAMAGE ALLOWED AREA AND IS OUT OF LIMITS, REF CRJ700 SRM. DRILLED AND LOCATED NEW BRACKET PN SH670-33389-1, REF CRJ700 SRM. INSTALLED MACHINED BRACKET (FLOOR MOUNT PLATE) AT APPROXIMATELY FS 533 STGR 27, REF CRJ700 SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION FOUND ON STRINGER JOINT PIECE AT STGR 21R FS 333.00. C-CHECK RO 10/22/2020. REMOVED CORROSION ON STRINGER JOINT PIECE AT STGR 21R FS 333.00, REF CRJ 700 SRM. MATERIAL REMOVED IS .016, MATERIAL REMAINING .047, ORIGINAL MATERIAL IS .063, OUT OF LIMTS. REMOVED AND INSTALLED NEW STRINGER JOINT PIECE AT STGR 21R FS 333.00, REF CRJ 700 SRM AND DWG. NO LEAKS NOTED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON STRINGER JOINT PIECE AT STGR 22R FS 333.00. C-CHECK RO 10/22/2020. REMOVED AND REPLACED STRINGER JOINT PIECE AT STGR 22R FS 333.00, REF CRJ700 SRM AND DW. NO LEAKS NOTED.

Part: PLATE — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON GROUND PLATES AT FS 319.00 STGR 21R. C-CHECK RO 10/22/2020. REMOVED AND REPLACED GROUND PLATES AT FS 319.00 STGR 21R, REF CRJ700 SRM AND DWG. COMPLETED FORM M-337. SEE CONTINUATION CARD FOR DETAILS.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON CLIP AT FS 310.00 STGR 20R. C-CHECK RO 10/22/2020. CLIP AT FS 310 STGR 20R CORRODED BEYOND LIMIT. REMOVED AND REPLACED, REF CRJ700 SRM AND DWG. COMPLIED WITH SKYWEST TASK CARD "STRUCTURAL MAJOR REPAIR" (RII).

Part: SKIN — CHAFED (EXTERIOR) · airframe 36,982 hrs · 26,855 cycles

AFT FUSELAGE EXTERNAL SKIN AT APPROXIMATEY FS 985.0 STGR 27 HAS 3 CHAFED AREAS, MARKED. C-CHECK RO 10/22/2020. BLENDED 3 CHAFED AREAS AFT FUSELAGE EXTERNAL SKIN AT APPROXIMATELY FS 985.0 STGR 27, REF REO. AREAS NR 1 & NR 2 ORIGINAL THICKNESS .118, NR 1 MATERIAL REMOVED .016, REMAINING .102. NR 2 MATERIAL REMOVED .025 REMAINING .083, WITHIN LIMITS. NR 3 ORIGINAL THICKNESS .110, REMOVED .046 REMAINING .064 OUT OF LIMITS. PERFORMED REPAIR, REF REO AND CRJ 700 SRM. NO LEAKS NOTED.

Part: FITTING — CORRODED (PAX DOOR SILL) · airframe 36,982 hrs · 26,855 cycles

PAX DOOR SILL FWD CLOSING FITTING HAS EVIDENCE OF CORROSION. C-CHECK RO 10/22/2020. PAX DOOR SILL FWD CLOSING FITTING HAS 100% MATERIAL LOSS DUE TO PITTING CORROSION. REMOVED AND INSTALLED NEW PAX DOOR SILL FWD CLOSING FITTING, REF CRJ 700. COMPLETED FORM M-337. SEE CONTINUATION CARD FOR DETAILS.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON STGR 21R BETWEEN FS 319.00-FS 333.00. C-CHECK RO 10/22/2020. REMOVED AND INSTALLED NEW STRINGER JOINT AND ANGLE AT STR 21R FS 333, REF CRJ 700 SRM AND DWG. REMOVED AND INSTALLED NEW STRINGER 21R BETWEEN FS 280-FS 333, REF REO. NO LEAKS NOTED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON ANGLE BETWEEN FS 533.00 TO FS 517.00 STGR 27 TO 26L. C-CHECK RO 10/22/2020. REMOVED CORRODED ANGLE AT FS 333-FS 517 STR 27-26L AND REPLACED WITH NEW REFERENCING CRJ 700 SRM. OPERATIONAL, BONDING, AND LEAK TESTS GOOD.

Part: FRAME — CORRODED (ZONE 100) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON FRAME FS 310.00 BETWEEN STGR 26R-STGR 24L, AREAS MARKED ON FRONT AND AFT SIDES. C-CHECK RO 10/22/2020. REMOVED CORROSION ON FRAME FS 310.00 BETWEEN STGR 26R-STGR 24L, REF CRJ 700 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS. REMOVED CORRODED LOWER FRAME SECTION AT FS 310 FROM STR 23L TO STR 25R AND INSTALLED NEW LOWER FRAME SECTION, REF CRJ 700 SRM AND DWG. PRESSURE LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS. .

Part: FRAME — CORRODED (ZONE 100) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON FRAME FS 295.00 BETWEEN STGR 26R-20L ON MULTIPLE AREAS, FRONT AND AFT SIDES, AREAS MARKED. C-CHECK RO 10/22/2020. REMOVED AND INSTALLED NEW FRAME SECTION REINFORCING ANGLE FROM STR 20L TO STR 25R, REF REO DWG, CRJ 700 SRM. NO LEAKS NOTED.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON STGR 20R ATTACHED INTERCOSTAL BETWEEN FS 310.00 TO FS 349.00. C-CHECK RO 10/22/2020. REPLACED INTERCOSTAL BETWEEN FS 310-FS 349 ON STRINGER 20R, REF DRAWING AND CRJ700 SRM. SEE CONTINUE CARD FOR DETAILS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON FRAME FS 549.00 BETWEEN STGR 27 AT STGR 26L FWD SIDE. C-CHECK RO 10/22/2020. COMPLIED WITH MHI RJ REO-ALL STEPS ACCOMPLISHED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON STRG 27 AT APPROXIMATELY FS 283.00, MARKED. C-CHECK RO 10/22/2020. REMOVED CORROSION ON STR 27 AT FS 283.00, REF CRJ700 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW STR 27 FROM FS 280 TO FS 298, REF CRJ700 SRM AND DWG. NO LEAKS NOTED. COMPLIED WITH TASK CARD.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON SGTR 21L ATTACHED INTERCOSTAL BETWEEN FS 349.00-FS 333.00. C-CHECK RO 10/22/2020. INSTALLED NEW INTERCOSTAL BETWEEN FS 333.00 AND FS 349.00 AT STR 21L, REF DWG AND CRJ700 SRM. RESTORED FINISH, REF CRJ700 SRM 51. APPLIED FILLET SEALENT, REF CRJ700 SRM. COMPLIED WITH TASK CARD.

Part: SLAT TRACK — WORN (RT WING) · airframe 36,982 hrs · 26,855 cycles

RT SLAT TRACK 3-3 HAS MULTIPLE WEAR MARKS ON ITS UPPER AND LOWER ROLLING SURFACES. C-CHECK RO 10/22/2020. REPAIRED RT SLAT TRACK 3-3, REFERENCING REO CRJ 700 SRM CRJ 700 AMM AND DWG. OPERATIONAL TEST GOOD. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWEST FORM M-337.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON STGR 25 BETWEEN FS 319.00-FS 333.00, MARKED. C-CHECK RO 10/22/2020. REMOVED CORRODED STR 25R BETWEEN FS 280 AND FS 333 AND REPLACED WITH NEW REFERENCING DWG CRJ 700 SRM. LEAK TEST GOOD. COMPLIED WITH TASK CARD.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON STGR 20R BETWEEN FS 295.00 TO FS 310.00. C-CHECK RO 10/22/2020. REPAIRED STR 20R BETWEEN FS 295-FS 310, REFERENCING CRJ 700 SRM DWG. LEAK TEST GOOD. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWEST FORM M-337.

Part: BRACKET — CORRODED · airframe 36,982 hrs · 26,855 cycles

CORROSION ON MACHINED BRACKET (FLOOR MOUNT PLATE) BETWEEN FS 549.00 TO FS 565.00, STGR 25R TO STGR 24R. C-CHECK RO 10/22/2020. REMOVED CORRODED MACHINED BRACKET BETWEEN FS 549-565 STR 25R-STR 24R AND REPLACED WITH NEW REFERENCING CRJ 700 SRM. LEAK TEST GOOD.

Part: STRINGER CLIP — CORRODED (ZONE 100) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON ATTACHING CLIP FOR STGR 19L FS 295.00. C-CHECK RO 10/22/2020. REMOVED CORRODED STR19L CLIP AT FS 295 AND REPLACED WITH NEW REFERENCING DWG AND CRJ 700 SRM. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWEST FORM M-337.

Part: SLAT TRACK — WORN (LT WING) · airframe 36,982 hrs · 26,855 cycles

LT WING SLAT TRACK 3-3 HAS MULTIPLE WEAR MARKS ON UPPER AND LOWER ROLLER CONTACT SURFACES. C-CHECK RO 10/22/2020. REPAIRED LT WING SLAT TRACK 3-3 WEAR MARKS, IAW REO CRJ700 SRM CRJ700 AMM. OPERATIONS CHECK GOOD AT THIS TIME.

Part: FLOORBEAM — CORRODED (BS 333) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON FLOOR BEAM AT FS 333.00, BETWEEN RBL 9-RBL 36. C-CHECK RO 10/22/2020. REPAIRED FS 333.00 FLOOR CROSS BEAM BETWEEN RBL 9-RBL 36, REFERENCING REO. ALL STEPS COMPLIED WITH. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWEST FORM M-337.

Part: BRACKET — CORRODED (THRESHOLD) · airframe 36,982 hrs · 26,855 cycles

SERVICE DOOR SILL THRESHOLD BRACKETS AT APPROXIMATELY FS 321 AND FS 338 HAVE EVIDENCE OF CORROSION. C-CHECK RO 10/22/2020. INSTALLED 4 EA BRACKETS AND 4 EA ANGLES, REF CRJ 700 SRM AND DWG. COMPLIED WITH SKY CARD.

Part: FLOORBEAM — CORRODED (BS 549) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON LT SIDE FLOOR SUPPORT BEAM LBL 9-LBL 27, AT FS 549.00. C-CHECK RO 10/22/2020. REPAIRED LT SIDE FLOOR SUPPORT BEAM LBL 9-LBL 27 ST FS 549, REF REO ALL STEPS COMPLETED OF PERMANENT REPAIR, COMPLIED WITH. SEE CONTINUE CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RBL 9 FLOORBEAM INBOARD FLANGE BETWEEN FS 830.40-FS 847.00. C-CHECK RO 10/22/2020. REPAIRED FLOOR BEAM, IAW MHI RJ REO, COMPLETED FORM M-337. SEE CONTINUATION CARD FOR DETAILS.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON STGR 21L BETWEEN FS 1015.00-FS 1031.00. C-CHECK RO 10/22/2020. REPAIRED STR 21L BETWEEN FS 1015-FS 1031, REFERENCING REO. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWEST FORM M-337. LEAK CHECK GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON AFT FACE OF FRAME AT FS 879.00, BETWEEN STGR 26L-25R. C-CHECK RO 10/22/2020. REMOVED AND REPLACED FRAME SECTOR AT FS 879.00 BETWEEN STR 26L-25R, REF CRJ 700 SRM AND REO. NO LEAKS NOTED.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON STRG 20L ATTACH CLIP AT FS 1015.00. C-CHECK RO 10/22/2020. REMOVED CORRODED CLIP FROM STR 20L AT FS 1015 AND REPLACED WITH NEW REFERENCING DWG AND CRJ 700 SRM. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWEST FORM M-337.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON LT SEAT TRACK FROM FS 597.00 TO 613.00 LBL 9 ON MULTIPLE AREAS. C-CHECK RO 10/22/2020. REMOVED AND INSTALLED NEWLY FABRICATED SEAT TRACK AT FS 597-613 LBL 9, REF CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 36,982 hrs · 26,855 cycles

BL 2 LT INTERCOSTAL BETWEEN FRAMES 349 AND 364 HAS EVIDENCE OF CORROSION ON FUSELAGE SKIN FLANGE. C-CHECK RO 10/22/2020 REMOVED CORROSION ON ATTACH FLANGE OF INTERCOSTAL AT BL 2 LT BETWEEN FRAMES AT FS 349 AND FS 364, REF CRJ700 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW BL 2 LT INTERCOSTAL BETWEEN FRAMES FS 349 AND FS 364, REF CRJ700 SRM AND DWG. NO LEAKS NOTED. COMPLIED WITH TASK CARD.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 36,982 hrs · 26,855 cycles

PAX DOOR SILL UPPER FLOOR SUPPORT ANGLE HAS EVIDENCE OF CORROSION ALONG ENTIRE LENGTH. C-CHECK RO 10/22/2020. PAX DOOR SILL UPPER FLOOR SUPPORT ANLGE FOUND TO BE OUT OF LIMITS, REF CRJ-700 SRM. REMOVED AND INSTALLED NEW PAX DOOR SILL UPPER FLOOR SUPPORT ANGLE, REF CRJ-700 SRM AND DWG.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RT FUSELAGE SIDE SEAT RAIL RETAINER (U CHANNEL) AT FS 752.00. C-CHECK RO 10/22/2020. RT SEAT RAIL U CHANNEL AT FS 752.00 REPLACED WITH NEW FROM FABRICATION. LOCATED AND DRILLED, REF CRJ700 SRM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RT SEAT TRACK FROM FS 349.00 TO FS 379.00 RBL9 ON MULTIPLE AREAS. C-CHECK RO 10/22/2020. REMOVED AND INSTALLED NEWLY FABRICATED SEAT TRACK AT FS 349-379 RBL 9, REF CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS.

Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 36,982 hrs · 26,855 cycles

AFT CARGO DOOR LOWER SILL CORRODED FROM FS 1000.00 TO FS 1047.00. C-CHECK RO 10/22/2020. COMPLIED WITH REO. STEP NR 1 BLENDED DAMAGE, IAW CRJ700 SRM. STEP NR 2 REPLACED BLENDED OVER FASTENERS AS REQUIRED, IAW CRJ700 SRM. STEP NR 3 NDT COMPLIED WITH. STEP NR 4 RESTORED FINISH, IAW CRJ700 SRM. STEP NR 5 RE-IDENTIFIED PART AS 670-53-61-913-1. STEP NR 6 APPLIED CORROSION INHIBITING COMPOUND, IAW CRJ700 SRM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON LT FUSELAGE SIDE SEAT RAIL BETWEEN FS 533.00 TO FS 549.00. C-CHECK RO 10/22/2020. INSTALLED NEW SEAT RAIL AT FS 533-549, IAW CRJ700 AMM. SEE CONTINUATION FOR DETAILS.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON LT FUSELAGE SIDE SEAT RAIL ON MULTIPLE AREAS BETWEEN FS 677.00 TO FS 708.00. C-CHECK RO 10/22/2020. REMOVED AND REPLACED SEAT RAIL AT FS 677-708, IAW CRJ700 AMM. SEE CONTINUATION FOR DETAILS.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RT SEAT TRACK FROM FS 581.00 TO FS 684.00 RBL 9 ON MULTIPLE AREAS. C-CHECK RO 10/22/2020. REMOVED AND INSTALLED NEWLY FABRICATED SEAT TRACK AT FS 581-684 RBL 9, REF CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RT SEAT TRACK FROM FS 684.00 TO FS 830.00 RBL 9 ON MULTIPLE AREAS. C-CHECK RO 10/22/2020. REMOVED AND INSTALLED NEWLY FABRICATED SEAT TRACK AT FS 677-830 RBL 9, REF CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS.

Part: DOOR SILL — CORRODED · airframe 36,982 hrs · 26,855 cycles

SERVICE DOOR SILL LOWER FLOOR SUPPORT ANGLE HAS EVIDENCE OF CORROSION ALONG ENTIRE LENGTH. C-CHECK RO 10/22/2020. REPLACED SERVICE DOOR SILL LOWER FLOOR SUPPORT ANGLE, REF DRAWING CRJ700 SRM. SEE CONTINUE CARD FOR DETAILS.

Part: BULKHEAD — CORRODED (BS 280) · airframe 36,982 hrs · 26,855 cycles

FS 280.00 RT BULKHEAD AFT SIDE LOWER OUTBOARD CORNER, FLOOR LEVEL, WEB IS CORRODED, MARKED. C-CHECK RO 10/22/2020. REMOVED CORRODED FS 280 RT WEB AND REPLACED WITH NEW REFERENCING DWG CRJ 700 SRM. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWEST FORM M-337.

Part: INTERCOSTAL — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

BL 2 RT INTERCOSTAL BETWEEN FRAMES 349 AND 364 HAS EVIDENCE OF CORROSION ON FUSELAGE SKIN FLANGE. C-CHECK RO 10/22/2020. REMOVED CORROSION ON ATTACH FLANGE OF INTERCOSTAL AT BL 2 RT BETWEEN FRAMES AT FS 349 AND FS 364, REF CRJ700 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW BL 2 RT INTERCOSTAL BETWEEN FRAMES FS 349 AND FS 364, REF CRJ700 SRM AND DWG. NO LEAKS NOTED. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON LT FUSELAGE SIDE SEAT RAIL ON MULTIPLE AREAS BETWEEN FS 613.00 TO FS 581.00. C-CHECK RO 10/22/2020. REMOVED AND REPLACED SIDE SEAT RAIL, IAW CRJ700 AMM. SEE CONTINUATION FOR DETAILS.

Part: STRAP — CORRODED (BS 319 FRAME) · airframe 36,982 hrs · 26,855 cycles

FS 319 FRAME STRAP AT FLOOR LEVEL WL 72.50 FWD OF SERVICE DOOR HAS EVIDENCE OF CORROSION. C-CHECK RO 10/22/2020. BLENDED CORROSION, IAW CRJ700 SRM. ORIGINAL THICKNESS OF UPPER OUTER STRAP 0.100, MATERIAL REMOVED 0.030, REMAINING MATERIAL 0.070. ORIGINAL THICKNESS OF MID SECTION 0.160, MATERIAL REMOVED 0.080, REMAINING MATERIAL 0.080 (REF DWG) FOUND TO BE OUT OF LIMITS OF 10% MAX MAT LOSS, IAW CRJ700 SRM. INSTALLED NEW FRAME BRACKET PN SH670-31990-1 AT FS 319 AT FLOOR LEVEL WL 72.50 FWD OF SERVICE DOOR, REF BOMBARDIER DWG AND CRJ700 SRM. DRILLED AND LOCATED NEW BRACK PN SH670-31990-1, REF BOMBARDIER DWG AND CRJ700 SRM. SEE CONTINUATION CARD FOR DETAILED WORK PERFORMED. COMPLETED FORM M-337.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RT SEAT TRACK FROM FS 985.00 TO FS 1000.00 RBL 9. C-CHECK RO 10/22/2020. REPLACED RT SEAT TRACK FROM FS 985 TO FS 1000 RBL 9, REF CRJ700 AMM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON LT FUSELAGE SIDE SEAT RAIL BETWEEN FS 453.00 TO FS 485.00. C-CHECK RO 10/22/2020. REMOVED AND REPLACED LT FUSELAGE RAIL FROM 453-485, IAW AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: DOOR SILL — CORRODED · airframe 36,982 hrs · 26,855 cycles

PAX DOOR SILL LOWER FLOOR SUPPORT ANGLE HAS EVIDENCE OF CORROSION IN RADIUS AT SEVERAL LOCATIONS, MARKED. C-CHECK RO 10/22/2020. REMOVED CORRODED FLOOR SUPPORT ANGLE AND INSTALLED NEW PAX DOOR LOWER SUPPORT ANGLE, IAW CRJ700 SRM & DWG. OPERATIONAL TESTS CHECKED GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: CHANNEL — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON LT FUSELAGE SIDE SEAT RAIL RETAINER (U CHANNEL) ON MULTIPLE AREAS BETWEEN FS 785.00 TO FS 830.00. C-CHECK RO 10/22/2020. REPLACED LT FUSELAGE SIDE SEAT RAIL RETAINER (U CHANNEL) BETWEEN FS 785 TO FS 830, REF CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RT FUSELAGE SIDE SEAT RAIL RETAINER (U CHANNEL) ON MULTIPLE AREAS BETWEEN FS 677.00 TO FS 724.00. C-CHECK RO 10/22/2020. REMOVED AND REPLACED RT FUSELAGE SIDE SEAT RAIL RETAINER (U CHANNEL) BETWEEN FS 677.00 TO FS 724.00, IAW CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS.

Part: POST — CORRODED (BS 280) · airframe 36,982 hrs · 26,855 cycles

FS 280.00 RT DOOR POST BOTTOM ISLE SIDE, CORROSION AROUND FASTENER, MARKED. C-CHECK RO 10/22/2020. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PART ON RT BOTTOM DOOR POST AT FS 280.00, REF CRJ700 SRM. COMPLIED WITH SKYWEST TASK CARD STRUCTURAL MAJOR REPAIR (RII).

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RT SEAT TRACK FROM FS 485.00 TO FS 581.00 RBL 9 ON MULTIPLE AREAS. C-CHECK RO 10/22/2020. REMOVED AND INSTALLED NEWLY FABRICATED SEAT TRACK AT FS 485-581 RBL 9, REF CRJ700 AMM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON LT FUSELAGE SIDE SEAT RAIL RETAINER (U CHANNEL) ON MULTIPLE AREAS BETWEEN FS 565.00 TO FS 581.00. C-CHECK RO 10/22/2020. INSTALLED NEW SEAT RAIL RETAINER, IAW CRJ700 AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RT FUSELAGE SIDE SEAT RAIL AT FS 736.00. C-CHECK RO 10/22/2020. REPLACED RT FUSELAGE SIDE SEAT RAIL AT FS 736, REF CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON LT SEAT TRACK FROM FS 501.00 TO 581.00 LBL 9 ON MULTIPLE AREAS. C-CHECK RO 10/22/2020. REPLACED LT SEAT TRACK FROM FS 501.00 TO FS 581.00 LBL 9, REF CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON LT SEAT TRACK FROM FS 985.00 TO 1000.00 LBL 9 ON MULTIPLE AREAS. C-CHECK RO 10/22/2020. REPLACED LT SEAT TRACK FROM FS 985 TO FS 1000 LBL 9, REF CRJ700 AMM.

Part: FLOOR SUPPORT — CORRODED (BS 830) · airframe 36,982 hrs · 26,855 cycles

CORROSION ON RT SIDE FLOOR SUPPORT AT FS 830.00, RBL 10. C-CHECK RO 10/22/2020. REPAIRED FLOOR SUPPORT, IAW MHI RJ REO. COMPLETED FORM M-337.

Part: ACTUATOR — CORRODED (BUTTE DOOR) · airframe 36,982 hrs · 26,855 cycles

LEFT HAND OUTBOARD FLAP BUTE DOOR ACTUATOR ON THE CENTER HINGE BOX ATTACH POINT HAS A CORRODED BUSHING, FLAGGED. C-CHECK RO 10/22/2020. LEFT OUTBOARD FLAP BUTE DOOR ACTUATOR LEVER, OUTBOARD SPACER REMOVED AND REPLACED WITH NEW, REF CRJ 700 AMM.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 36,982 hrs · 26,855 cycles

RT OUTBOARD FLAP INBOARD HINGE BOX FWD FITTING 3 EA BOLTS CORRODED. C-CHECK RO 10/22/2020. REMOVED AND REINSTALLED THE RT FLAP HINGE BOX AT WS 178 WITH NEW BOLTS, BUSHINGS, NUTS AND WASHERS, REF CRJ700 AMM. ALL OPERATIONS AND LEAK CHECKS CHECKED GOOD. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD.

Part: HINGE FITTING — CHAFED (RT WING TE FLAP) · airframe 36,982 hrs · 26,855 cycles

RT OUTBOARD FLAP MID HINGE ARM LUG HAS CHAFE. C-CHECK RO 10/22/2020. COMPLIED WITH REPAIR TO CHAFE ON THE RT OUTBOARD FLAP MID HINGE ARM REFERENCING REO, REWORK IS WITHIN LIMITS, SEE CONTINUATION CARD FOR ADDITIONAL DETAILS OF WORK PERFORMED. COMPLIED WITH TASK CARD COMPLETED FORM M-337.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 36,982 hrs · 26,855 cycles

RT OUTBOARD FLAP OUTBOARD HINGE BOX FWD FITTING 2 EA BOLTS CORRODED. C-CHECK RO 10/22/2020. REMOVED 2 EA CORRODED BOLTS FROM RT OUTBOARD FLAP OUTBOARD HINGE BOX FWD FITTING AND REPLACED WITH NEW, REFERENCING CRJ 700 AMM. OPERATIONAL AND LEAK TESTS GOOD.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 36,982 hrs · 26,855 cycles

VERTICAL STABILIZER TO FUSELAGE LT DRAG ANGLE HAS SUSPECT CRACK, MARKED. C-CHECK RO 10/22/2020. REPAIRED DRAG ANGLE, REF CRJ 700 SRM. COMPLIED WITH SKY CARD.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 36,982 hrs · 26,855 cycles

VERTICAL STABILIZER TO FUSELAGE RT DRAG ANGLE HAS SUSPECT CRACK, MARKED. C-CHECK RO 10/22/2020. REPAIRED DRAG ANGLE, REF CRJ 700 SRM. COMPLIED WITH SKY CARD.

Part: FORMER — CRACKED (PAX DOOR) · 24,181 cycles

PAX DOOR AFT FORMER IS CRACKED AT TOP FLANGE POWER ASSIST PULLEY BASE MOUNT ATTACHING POINT. (C-CHECK) RO: 11/26/2018. REPLACED PAX DOOR AFT FORMER REF SRM 51-42-21-001-001-A01.

Part: INTERCOSTAL — DENTED (FUSELAGE) · 24,181 cycles

PAX DOOR FWD LOWER INTERCOSTAL IS DENTED ON TOP FLANGE. (C-CHECK) RO: 11/26/2018. REPLACED PAX DOOR FWD LOWER INTERCOSTAL REF SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 24,181 cycles

PASSENGER DOOR INTERCOSTAL DD2 HAS CORROSION ON WEB AND FLANGES. (C-CHECK) RO: 11/26/2018. REPLACED PAX DOOR INTERCOSTAL DD2 REF SRM 51-42-06-001-001-A01. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 24,181 cycles

PASSENGER DOOR INTERCOSTAL DD6 HAS CORROSION ON WEB AND FLANGES. (C-CHECK) RO: 11/26/2018. REPLACED PAX DOOR INTERCOSTAL DD6. REF SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LEAK AND OPS TEST GOOD.

Part: CHANNEL — CORRODED (PAX DOOR) · 24,181 cycles

PASSENGER DOOR CHANNEL HAS CORROSION ON WEB AND FLANGES. (C-CHECK) RO: 11/26/2018. REPLACED PAX DOOR CHANNEL. REF SRM 51-42-06-001-001-A01. LEAK CHECK GOOD.

Part: FORMER — CORRODED (PAX DOOR) · 24,181 cycles

PAX DOOR FORWARD FORMER HAS CORROSION. (C-CHECK) RO: 11/26/2018. REPLACED PAX DOOR FWD FORMER. REF SRM 51-42-06-001-001-A01. PRESSURE CHECK GOOD.

Part: PANEL — CORRODED (PAX DOOR) · 24,181 cycles

PAX DOOR TOP PANEL HAS CORROSION AROUND NUT PLATES. (C-CHECK) RO: 11/26/2018. REMOVED AND INSTALLED NEW NUT PLATES TO PAX DOOR REF SRM 51-42-06-001-001-A01.

Part: ANGLE — CORRODED (PAX DOOR) · 24,181 cycles

PAX DOOR BOTTOM ANGLE NUT PLATES HOLES HAS CORROSION. (C-CHECK) RO: 11/26/2018. REMOVED AND REPLACED PAX DOOR BOTTOM ANGLE NUT PLATES REF SRM 51-42-06-001-001-A01.

Part: STRUCTURE — DENTED (FUSELAGE) · 24,181 cycles

ONE DENT LOCATED RT SIDE FORWARD FUSELAGE. (C-CHECK) RO: 11/26/2018. REPAIRED DENT LOCATED AT RT SIDE FORWARD FUSELAGE REFERENCING REO 670-53-11-1451.

Part: STRUCTURE — DENTED (FUSELAGE) · 24,181 cycles

5 DENTS LOCATED ON FORWARD FUSELAGE LT SIDE. (C-CHECK) RO: 11/26/2018. REPAIRED 5 DENTS LOCATED ON FORWARD FUSELAGE LEFT-HAND SIDE REF REO 670-53-11-1450.

Part: COWLING — DENTED (LT ENGINE) · 24,181 cycles

LT ENGINE FAN COWL HAS NUMEROUS DENTS. (C-CHECK) RO: 11/26/2018. REPAIRED ALL DENTS IN THE LT ENGINE FAN COWL REF REO 670-54-14-1012.

Part: SKIN — DENTED (FUSELAGE) · 24,181 cycles

GROUND AIR SERVICE DOOR HAS NUMEROUS DENTS IN SURROUNDING AREA. (C-CHECK) RO: 11/26/2018. REPAIRED DENTS, COMPLIED WITH ALL THE STEPS OF REO 670-53-61-1494.

Part: STRUCTURE — DENTED (FUSELAGE) · 24,181 cycles

ONE DENT LOCATED RT SIDE FORWARD FUSELAGE. (C-CHECK) RO: 11/26/2018. REPAIRED DENT ON RT FWD FUSELAGE REF REO 670-21-1574.

Part: ACCESS PANEL — DAMAGED (LT WING) · 24,181 cycles

LEFT WING LEADING EDGE ACCESS PANEL HAS DAMAGED SCREW HOLE. (C-CHECK) RO: 11/26/2018. REPAIRED SCREW HOLE ON LT LE WING PANEL REF REO 670-57-41-396.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,980 hrs · 23,619 cycles

PILOT REPORTED THE BACK OF EXIT SIGN WAS NOT ILLUMINATING ON THE INDICATOR PANEL. MX REMOVED AND REPLACED THE EXIT SIGN BULB AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

RT SUPPORT FOR JACK PAD FITTING FOUND CORRODED BEYOND LIMITS WHILE GAINING ACCESS TO NLG JACK PAD FITTING. REMOVED AND REPLACED NOSE JACK PAD FITTING SUPPORT PER SRM 51-42-06-001-001-A01, 51-42-001-001-A01 AND DRAWING CC670-32050.

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

FS 310.00 FRAME, STG 26L-26R CORRODED FWD & AFT. COMPLIED WITH EC/TC REO 670-53-21-1308 AND REO 670-53-21-1308 FOR REPAIR.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

LOWER FS 280 FRAME FLOOR SUPPORT ANGLE CORRODED. REMOVED AND REPLACED UNSERVICEABLE 280 LOWER FRAME SUPPORT ANGLE WITH NEW SUPPORT ANGLE IAW SRM 51-42-06-001-001 A01 AND DRAWING CC670-34010. RESTORED CIC TO REPAIR AREA. REFERENCE: SRM 51-21-11-001-001 A01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

NOSE JACKING FITTING LT SUPPORT, FS265-FS280, CORRODED. REMOVED AND INSTALLED NEW SUPPORT FOR NOSE JACK PAD FITTING IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND DRAWING NR CC670-32-050

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

STUB FITTING CRACKED BY NOSE JACKPAD FITTING. REMOVED AND INSTALLED NEW STUB ASSY IAW SRM 51-42-13-001-001-A01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

NOSE JACKPAD FITTING CRACKED. REMOVED AND INSTALLED NEW NOSE JACK PAD FITTING IAW SRM 51-42-21-001-001-A01, AMM 51-41-10-960-801-A01, AND DRAWING NR CC670-32050.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

FS 265 FRAME, STR 26L - 26R CORRODED. EVALUATED DAMAGE AND DETERMINED CORROSION TO BE CONTAINED TO STIFFENING ANGLE AT FS 265. DAMAGE IS OUT OF LIMITS. REF SRM 53-00-00-101-001 A01. REMOVED STIFFENING ANGLE REF SRM 51-42-06-001-001 A01. DRILLED UP NEW STIFFENING ANGLE REF SRM 54-40-11-001-001 A01. INSTALLED NEW, SERVICEABLE STIFFENING ANGLE IAW SRM 51-42-06-001-001 A01, 51-23-00-001-001 A01, DWG CC670-33025 & DWG CC670-34-020. RESTORED FINISH AND CIC REF SRM 51-25-16-001-001 A01 & 51-21-11-001-001 A01.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

IN FWD CARGO AREA STRUCTURE AROUND ADF ANTENNA IS CORRODED. REMOVED CORROSION IN SUPPORT CHANNEL IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF REWORK AREA IAW NDTM PT 1, 51-20-004-270-A01 MIN THICKNESS IS .069". NO DAMAGE ALLOWED. PERFORMED EDDY CURRENT INSPECTION OF REWORKED AREA IAW NDTM PT 1, 51-20-006-250-A01. NO CRACK INDICATIONS NOTED AT THIS TIME. COMPLIED WITH EC/TC EA 05-2017-048 IAW EA 05-2017-048 REV--, DATED 06-04-2017.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

IN FWD CARGO AREA STRUCTURE AROUND LOWER BEACON IS CORRODED. REMOVED CORROSION IN SUPPORT CHANNEL IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF REWORK AREA IAW NDTM PT 1, 51-20-004-270-A01 MIN THICKNESS IS .054". NO DAMAGE ALLOWED. PERFORMED EDDY CURRENT INSPECTION OF REWORKED AREA IAW NDTM PT 1, 51-20-006-250-A01. NO CRACK INDICATIONS NOTED AT THIS TIME. COMPLIED WITH EC/TC EA 05-2017-048 IAW STS EA 05-2017-048 REV--, DATED 06-04-2017.

Part: PANEL — CORRODED (PAX DOOR) · airframe 30,864 hrs · 40,056 cycles

PAX DOOR FWD SIDE PANEL CORRODED SEVERAL AREAS. REMOVED AND REPLACED PAX DOOR FWD SIDE PANEL IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.

Part: SKIN — NOT REPORTED (LT WING) · airframe 30,864 hrs · 40,056 cycles

PERMANENT REPAIR REQUIRED ON LT LOWER WING PLANK FWD EDGE (FUR-57-00-00923). COMPLIED WITH PERMANENT REPAIR OF WING PLANK BY COMPLYING WITH EC/TC EA 20-2017-081, STS EA 20-2017-081, AND EC/TC FUR-57-00-00923.

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,864 hrs · 40,056 cycles

FS 364 FRAME STR 26L-25R CORRODED. REPAIRED FRAME BY COMPLYING WITH EC/TC REO 670-53-21-687 AND GREO 670-53-21-687 REVB DATED 06-06-2016.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 30,864 hrs · 40,056 cycles

ATC LOWER ANTENNA INTERNAL DOUBLER, FS 349 - FS 364 STR 26R CORRODED. REMOVED ATC 1 LOWER ANTENNA IAW AMM 34-54-04-000-801 A01. REMOVED ATC ANTENNA DOUBLER IAW SRM 51-42-06-001-001A01. ATC DOUBLER OUT OF LIMIT IAW SRM 53-21-01-101-006 A01. DRILLED NEW ATC ANTENNA DOUBLER IAW SRM 51-40-11-001-001 A01. INSTALLED ATC DOUBLER IAW SRM 51-42-06-001-001 A01.

Part: LANDING — CRACKED (TRU BAY DOOR) · airframe 30,864 hrs · 22,009 cycles

RT TRU DOOR AFT LATCH ANGLE CRACKED ON THE TRU FLOOR. REMOVED AND REPLACED RT AVIONIC DOOR LANDING IAW SRM 51-42-06-001-001-A01, AND 51-42-13-001-001-A01. MAJOR REPAIR.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

FLOOR CROSSBEAM CORRODED AT FS 1051 RBL 27-RBL 40. BLENDED CORROSION IAW EA 38-2017-091 AND EC/TC EA 38-2017-091.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

STR 27 CORRODED AT FS280-300. REMOVED CORRODED STRINGER AND INSTALLED NEW STRINGER IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

INTERCOSTAL FS 349 - FS 364 STR 27 LT CORRODED. LOCATED & DRILLED NEW INTERCOSTAL & INSTALLED IAW SRM 51-40-11-001-001-A01 & SRM 51-42-06-001-001 & DRAWING SH670-32075.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

LT FLOOR SILL CORRODED FROM FS 985-1000. COMPLIED WITH E/C T/C EA 32-2017-140 AND EA 32-2017-140 FOR REPAIR OF FLOOR SILL AT FS 985-1000 LT.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

SPLICE ANGLE, STG 26R, FS333 CORRODED. REMOVED AND REPLACED CORRODED SPLICE ANGLE STG 26R, FS333 IAW SRM 51-42-06-001-001-A01. ALL DEFECTS CORRECTED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

SUPPORT, FS 349- FS 364 STR 26 RT CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40--11-001-001-A01 AND 51-42-06-001-001-A01 THIS IS A MINOR REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

STRINGER 26 RT FS 280 - FS 333 CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE STRINGER 26 RT FS 280- FS 333 PER SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01,51-40-11-001-001-A01 AND DAW SH670-31634. THIS IS A MAJOR REPAIR.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 30,864 hrs · 22,009 cycles

SILL CORRODED AT FS319.70 TO 310.00 AND BETWEEN RBL40-43. REMOVED FLOOR SILL FROM FS280-319, RBL40 IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED HOLES IN NEW FLOOR SILL IAW SRM 51-42-06-001-001-A01, 51-40--11-001-001-A01. ASSEMBLED AND INSTALLED RT FLOOR SILL, FS280-319.7 IAW SRM 51-42-06-001-001-A01 AND DRAWING SH670-32-170. COMPLIED WITH SH670-32170 S28.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 30,864 hrs · 22,009 cycles

HOUSING AROUND CARGO DOOR HANDLE CRACKED (AFT). REMOVED AND INSTALLED NEW AFT CARGO DOOR HANDLE HOUSING IAW SRM 51-42-21-001-001-A01 AND 52-31-03-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 30,865 hrs · 22,009 cycles

LEFT SEAT TRACK CORRODED, BS 785 - 863. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343, & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 30,865 hrs · 22,009 cycles

LEFT SEAT TRACK CORRODED, BS 677 - 708. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 30,865 hrs · 22,009 cycles

CORROSION FOUND ON THE FLOORBEAM ANGLE BS 280 BETWEEN LBL 9 AND RBL 9. R & R THE FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, & 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 30,865 hrs · 22,009 cycles

RIGHT SEAT TRACK CORRODED, BS 485 - 565. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343, & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.

Part: SEAT TRACK — CORRODED (BS 863-953) · airframe 30,865 hrs · 22,009 cycles

LEFT SEAT TRACK CORRODED, BS 863 - 953. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 30,865 hrs · 22,009 cycles

RIGHT SEAT TRACK CORRODED, BS 785 - 863. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343, & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 30,865 hrs · 22,009 cycles

LEFT SEAT TRACK CORRODED, BS 485 - 565. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343, & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 30,865 hrs · 22,009 cycles

RIGHT SEAT TRACK CORRODED BS 349-485. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.

Part: ANGLE — CORRODED (BS 280 THRESHOLD) · airframe 30,865 hrs · 22,009 cycles

CORROSION FOUND ON DOOR THRESHOLD ANGLE AT BS 280, RBL 9. R & R DOOR THRESHOLD ANGLE IAW SRM 51-42-06-001-001-A01, & 51-42-13-001-001-A01.

Part: POST — CORRODED (BS 280) · airframe 30,865 hrs · 22,009 cycles

RIGHT BS 280 COCKPIT DOOR POST CORRODED AT THE LOWER CORNER. R & R THE POST AND REPAIRED ADDITIONAL DAMAGE IAW EA 32-2017-129, & EC/TC EA 32-2017-129. MAJOR REPAIR.

Part: POST — CORRODED (BS 280) · airframe 30,865 hrs · 22,009 cycles

LEFT FS 280 COCKPIT DOOR POST CORRODED AT THE LOWER CORNER. R & R THE POST AND REPAIRED ADDITIONAL DAMAGE IAW EA 32-2017-128, & EC/TC EA 32-2017-128. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 349) · airframe 30,865 hrs · 22,009 cycles

BS 349 FRAME, STRINGERS 27 - 26R CORRODED, AFT SIDE. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS CHECK. FINISHED REPAIR IAW REO 670-53-21-1308 & EC/TC REO 670-53-21-1308.

Part: FRAME — CORRODED (BS 319) · airframe 30,865 hrs · 22,009 cycles

BS 319.7 FRAME, STRINGERS 26L - 26R CORRODED, FWD & AFT SIDE. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS CHECK. FINISHED REPAIR IAW REO 670-53-21-1308 & EC/TC REO 670-53-21-1308.

Part: LIGHT — WORN (CABIN) · airframe 28,008 hrs · 20,168 cycles

EMERGENCY FLOOR LIGHT NEAR CLOSET IS WORN OUT. MAINTENANCE R & R EMERGENCY FLOOR LIGHT STRIP AT FWD CLOSET IAW AMM 33-51-01. AIRCRAFT OK FOR RETURN TO SERVICE.

Part: LIGHT — DETERIORATED (CABIN) · airframe 29,567 hrs · 21,025 cycles

EMERGENCY FLOOR LIGHT NEAR CLOSET IS WORN OUT. R & R EMERGENCY FLOOR LIGHT STRIP AT FRONT CLOSET IAW AMM 33-51-01.

Part: LENS — BROKEN (EMERGENCY LIGHT)

LEFT AFT EXTERIOR EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED THE EXTERIOR EMERGENY LIGHT LENS IAW CMM 33-52-07.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 27,868 hrs · 19,699 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT COVER BROKEN. R & R RT AFT OVERWING EMERGENCY EXIT LIGHT COVER AND PERFORMED OPS CHECK IAW AMM 33-51-15. OPS TEST GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (ROW 9) · airframe 27,726 hrs · 19,598 cycles

ROW 9 CEILING EXIT LIGHT INOPERATIVE. R & R CEILING EXIT LIGHT IAW AMM 33-51-09. OPS CHECK GOOD.

Part: LATCH — OUT OF ADJUST (SERVICE DOOR) · airframe 27,491 hrs · 19,396 cycles

SERVICE DOOR WILL NOT CLOSE, HARD TO OPEN. COMPLIED WITH INSPECTION OF SERVICE DOOR LATCH ASSY FOUND UNLOCK CRANK LOOSE. RECONNECTED UPLOCK CRANK TO PUSH ROD CW, OPS OF DOOR LOCKING MECHANISM CHECK GOOD IAW AMM 52-41-02. OPS IAW 52-41-00, ITEM CLEARED PLACARD REMOVED ACFT OK FOR SERVICE.

Part: MEGAPHONE — INTERMITTENT (CABIN) · airframe 25,278 hrs · 17,705 cycles

MEGAPHONE WORKING INTERMITTENTLY. R & R MEGAPHONE IAW AMM 25-61-14, IPC REF 25-61-14 FIG 1C, ITEM 5. ACFT OK FOR SERVICE.

Part: TAB — CHAFED (HORIZONTAL STAB) · airframe 25,028 hrs · 17,516 cycles

CHAFE DAMAGE ON LT AND RT ANTI-ROTATION TABS OF THE HORIZONTAL STABILIZER. COMPLIED WITH EC/TC SB 670BA-55-012 01,02,03.

Part: SKIN — CRACKED (LT WING) · airframe 25,028 hrs · 17,516 cycles

LT WING LOWER PLANK HAS THREE FASTENER HOLES WITH CRACK INDICATIONS. REPAIRED IAW REO 670-57-21-733 P1. MAJOR REPAIR.

Part: SKIN — CRACKED (RT WING) · airframe 25,028 hrs · 17,516 cycles

RT WING LOWER PLANK HAS 1 EA FASTENER HOLE WITH CRACK INDICATION. REPAIRED IAW REO 670-57-21-733 P1. MAJOR REPAIR.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 24,993 hrs · 17,488 cycles

LEFT AND RIGHT FLIGHT DECK FLOOR SUPPORT ANGLES ARE CRACKED. REMOVED ANGLES LT & RT AND OBTAIN SERVICEABLE LT & RT ANGLES TRANSFERED HOLES & CAMLOCKS TO SERVICEABLE ANGLES IAW SRM 51-42-06-001-001-A01, SRM 51-40-11-001-001-A01, SRM 51-44-06-001-001-A01. INSTALLED LT AND RT COCKPIT FLOOR PANEL SUPPORT ANGLES IAW DWG CC670-33052, SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 842-893) · airframe 24,993 hrs · 17,488 cycles

SEAT TRACK RBL 9, BS 842 - 893 HAS TWO AREAS OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, REO 670-53-00-343, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 533-645) · airframe 24,993 hrs · 17,488 cycles

LEFT SIDE SEAT TRACK BS 533 - 645 HAS TWO AREAS OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM TASK 53-00-49-000-801-A03, REO 670-53-00-343, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 645-669.4) · airframe 24,993 hrs · 17,488 cycles

LEFT SIDE SEAT TRACK BS 645 - 669.4 HAS THREE AREAS OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM TASK 53-00-49-000-801-A03, REO 670-53-00-343 REV F, AND AMM 53-00-49-400-801, CONFIG A03.

Part: SEAT TRACK — CORRODED (BS 708-863) · airframe 24,993 hrs · 17,488 cycles

LEFT SIDE SEAT TRACK BS 708 - 863 HAS TWO AREAS OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, REO 670-53-00-343, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 863-977) · airframe 24,993 hrs · 17,488 cycles

RIGHT SIDE SEAT TRACK FS 863 - 977 HAS ONE AREA OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801, REO 670-53-00-343, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 669-708) · airframe 24,993 hrs · 17,488 cycles

RIGHT SIDE SEAT TRACK BS 669.4 - 708 HAS TWO AREAS OF CORROSION. CORROSION IS OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, REO 670-53-00-343, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 24,993 hrs · 17,488 cycles

RIGHT SIDE SEAT TRACK BS 708-761.85 HAS TWO AREAS OF CORROSION. FOUND OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000, SRM 51-40-11-001-001, REO 670-53-00-343, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 685-842) · airframe 24,993 hrs · 17,488 cycles

SEAT TRACK LBL 9, BS 685 - 842 HAS SIX AREAS OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-800-801-A03, REO 670-53-00-343, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 669-708) · airframe 24,993 hrs · 17,488 cycles

LEFT SIDE SEAT TRACK BS 669.4 - 708 HAS ONE AREA OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, REO 670-53-00-345, GROE 670-53-00-343 REV F, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 24,993 hrs · 17,488 cycles

SEAT TRACK LBL 9, BS 565 - 677 HAS SIX AREAS OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, REO 670-53-00-343, AMM 53-00-49, AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 565-669) · airframe 24,993 hrs · 17,488 cycles

RIGHT SIDE SEAT TRACK BS 565 - 669.40 HAS TWO AREAS OF CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, EC/TC REO 670-53-00-343, GREO 670-53-00-343, REV F, AND AMM 53-00-49-400-801.

Part: ANGLE — CORRODED (PAX DOOR FRAME) · airframe 24,993 hrs · 17,488 cycles

PAX DOOR SURROUND CENTER LOWER ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. R & R PAX DOOR CENTER LOWER ANGLE IAW SRM 51-42-06-001-A01 & 51-42-20-001-001-A01. LOCATED & DRILLED NEW PAX DOOR LOWER ANGLE IAW SRM 51-40-11-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 333) · airframe 25,028 hrs · 17,516 cycles

FLOORBEAM AT BS 333, RBL 16 CORRODED. REPAIRED IAW EA 12-2014-194, REV P1. MAJOR REPAIR.

Part: STRUCTURE — CORRODED (BS 333) · airframe 24,993 hrs · 17,488 cycles

PACKER CORRODED AT BS 333, RB L9, WL 72.5. R & R PACKER IAW SRM 51-42-06-001-001 AND DWG SH670-32120.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,993 hrs · 17,488 cycles

LT BS 280 FLOORBEAM CORRODED. REPAIRED IAW SB670BA-53-041.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,993 hrs · 17,488 cycles

RT BS 280 FLOORBEAM CORRODED. REPAIRED IAW SB670BA-53-041.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,993 hrs · 17,488 cycles

FLOORBEAM ANGLE AFT SIDE BS 280 CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01 FIG 53-00-00-991-802. REMOVED AND REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND 51-42-20-001-001-A01 AND DWG CC670-34010.

Part: STRUCTURE — CORRODED (BS 349) · airframe 24,993 hrs · 17,488 cycles

PACKER CORRODED AT RBL 9, BS 349. R & R PACKER IAW DWG SH670-32120, AND SRM 51-42-06-001-001-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 24,993 hrs · 17,488 cycles

RT SIDE BS 280 BULKHEAD WEB CORRODED. REPAIRED IAW EC/TC REO 670-53-11-594-01 AND GREO IAW SOP 5702.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 24,993 hrs · 17,488 cycles

LT SIDE BS 280 BULKHEAD WEB CORRODED. REPAIRED IAW ECTC REO 670-53-11-594 AND GREO 670-53-11-594. REV. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 25,028 hrs · 17,516 cycles

CORROSION ON FLOOR SUPPORT AT BS 349. BLENDED DAMAGE FOUND TO BE OUT OF LIMITS DUE TO CRACK & TOTAL MATERIAL LOSS IN BLEND AREA IAW SRM 51-21-06-001-001. MAJOR REPAIR.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 25,028 hrs · 17,516 cycles

PASSENGER DOOR SURROUND CENTER CAP ANGLE CORRODED. REMOVED CAP ANGLE IAW SRM 51-41-02-001-001-A01. DRILLED UP NEW CAP ANGLE IAW SRM 51-40-11-001-A01. INSTALLED UPPER CAP ANGLE IAW SRM 51-42-02-001-001. COMPLIED WITH ADJUSTMENT PASSENGER DOOR PROXIMITY SENSOR PX25 IAW AMM 52-70-04-820-802A-02.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 24,993 hrs · 17,488 cycles

CRACK AT FWD END OF FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE ON LT SIDE. REMOVED AFT DRAG ANGLE ON LT SIDE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01. INSTALLED LT SIDE AFT DRAG ANGLE IAW SRM 51-42-13-001-001-A01, 52-42-21-001-001-A01 AND 51-42-22-001-001-A01, AND DWG PL BA670-35002. LOCATED AND DRILLED NEW DRAG ANGLE ON LT SIDE IAW SRM 51-40-11-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 24,993 hrs · 17,488 cycles

CRACK AT FWD END OF FUSELAGE TO VERTICAL STAB DRAG ANGLE ON RT SIDE. REMOVED AFT DRAG ANGLE ON RT SIDE IAW SRM 51-42-13-001-001-A01, 51-42-21-00-001-A0, 51-42-22-001-001-A01. INSTALLED NEW AFT DRAG ANGLE RT SIDE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-21186. LOCATED AND DRILLED UP NEW DRAG ANGLE ON RT SIDE IAW SRM 51-40-11-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 23,217 hrs · 16,178 cycles

CONNECTOR P358 FOR CABIN EMERGENCY LIGHTS BROKEN. R & R ELECTRICAL CONNECTOR IAW ESPM 20-26-00 AND WD 33-50-05. PERFORMED OPS TEST OF THE EMERGENCY LIGHTING SYSTEM IAW AMM 33-51-00-710-802. NO DEFECTS NOTED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,951 hrs · 15,983 cycles

RIGHT AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-15.

Part: WARNING MESSAGE — ILLUMINATED (LT BLEED DUCT) · airframe 22,495 hrs · 15,650 cycles

LEFT BLEED AIR DUCT WARNING MESSAGE, FOLLOWED BY LOSS OF PRESSURIZATION. ACFT RETURNED TO DEPARTURE. EMERGENCY DECLARED. R & R AILERON IAW AMM 30-12-12, SYS CHECKED GOOD. NO DEFECTS NOTED.

Part: PANEL — DAMAGED (PAX DOOR) · airframe 22,483 hrs · 15,639 cycles

PAX DOOR FWD SIDE PANEL BUCKLED AT TOP STEP. REPAIRED IAW REO 670-52-11-722. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3.

Part: PANEL — DAMAGED (PAX DOOR) · airframe 22,483 hrs · 15,639 cycles

PAX DOOR AFT SIDE PANEL BUCKLED AT TOP STEP. REPAIRED IAW REO 670-52-11-722. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3.

Part: ADC — MALFUNCTIONED · airframe 22,084 hrs · 15,353 cycles

AT FL370, RECIEVED INTERMITTENT STALL FAILED CAUTION, COMPLIED WITH QRH. FEW MINUTES LATER, F/O OBSERVED DECREASING AIRSPEED INDICATED ONLY ON PFD 2. EFIS COMPUTER MONITOR CAUTION DISPLAYED, WITH IAS AMBER CAUTION ANNOUNCAITION POSTED ON BOTH PFD1 AND PFD2. COMPLIED WITH QRH FOR EFIS COMPUTER MONITOR AND SELECTED ADC 1 ON SOURCE SELECTOR PANEL. IN DECENT OUT OF RVSM CAPTAINS INDICATED AIRSPEED STARTED TO DECREASE RELATIVE TO STANDBY INDICATOR. DESCENDING WITH NOSE DOWN PITCH ATTITUDE AND FULL POWER SELECTED, STANDBY INDICATOR WAS INDICATING DECREASING AIRSPEED. DURING THIS TIME, FIRST THE LOW SPEED TAPE THEN THE HIGH SPEED TAPE CAME TOGETHER, WITH STICK SHAKER ACTIVATED. DESCENDING THROUGH LOW 200'S OF ALTITUDE THE RED FLAGS FOR IAS, ALT AND VS CLEARED AND USABLE ADC DATA RETURNED TO JUST STANDBY INDICATOR, THEN PFD 1 AND FINALLY PFD 2 R & R STBY ISI IAW AMM 34-12-01 AND AIPC 34-12-01, ITEM 10. R & R NR 1ADC AND NR 2ADC IAW AMM 34-13-01 AND AIPC 34-13-01, ITEM 5.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 21,405 hrs · 14,893 cycles

LEFT AFT EXTERIOR EMERGENCY INOPERATIVE. REPLACED BULB IAW AMM 33-51-15. ACFT OK FOR SERVICE.

Part: STIFFENER — CRACKED (BS 280 BULKHEAD) · airframe 20,282 hrs · 14,065 cycles

ON REMOVAL LEFT LOWER FUSELAGE BS 280 BULKHEAD WEB FOUND STIFFNER ANGLE AT LBL 26 CRACKED. REMOVED DISCREPANT STIFFNER ANGLE AT LBL 26, FS 280 AND INSTALLED NEW SERVICEABLE STIFFNER ANGLE IAW SRM 51-42-06-001-001 & 51-42-06-001-001-A01. MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 333-349 S25R) · airframe 20,282 hrs · 14,065 cycles

STRINGER 25R CORRODED BETWEEN FRAMES 333 AND 349. RECEIVED AND INSTALLED SPLICE PIECE AT FS 533 AND STRINGER 25R REF SRM 51-42-06-001-001. MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 295-310 S25R) · airframe 20,282 hrs · 14,065 cycles

STRINGER 25R CORRODED BETWEEN FRAMES 295.00 & 310.00. PARTS ON HAND. R & R STRINGER 25R FROM FS 280 TO FS 333 REF SRM 51-42-06-001-001 & SRM 51-42-21-001-001. FOUND TO BE SATISFACTORY.

Part: STRIKER — CORRODED (DOOR FRAME) · airframe 20,282 hrs · 14,065 cycles

SERVICE DOOR LOWER SEAL STRIKER CORRODED AT SILL AREA. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01 & 53-21-23-101-002-A01. REMOVED AND INSTALLED SERVICE DOOR LOWER SEAL STRIKER PLATE IAW SRM 51-42-06-001-001-A01. EDGE SEALED, APPLIED FINISH COAT, AND CPC TO SERVICE DOOR SEAL STRIKER IAW SRM 51-21-11-001-001-A01 & 51-25-16-001-001-A01. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 315) · airframe 20,282 hrs · 14,065 cycles

RT FUSELAGE FLOOR SUPPORT IS CORRODED JUST FWD OF SERVICE DOOR APPROX FS 315. AREA JUST FWD OF FS 319.70 BEYOND ALLOWABLE LIMITS OF SRM 53-00-00-101-001. RECEIVED AND COMPLIED WITH REO 670-53-21-876 IAW NDTM PART 1, 51-20-006. FOUND TO BE SATISFACTORY.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 20,282 hrs · 14,065 cycles

SUPPORT ANGLE CORRODED AT HINGE SIDE OF PAX DOOR. REMOVED CORRODED ANGLE IAW SRM 51-42-21-001-001-A01. INSTALLED NEW SUPPORT ANGLE AT HINGE SIDE OF ASD IAW SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 20,282 hrs · 14,065 cycles

CLIP & INTERCOSTAL CORRODED AT HINGE END OF PAX DOOR. REMOVED CLIP AND INTERCOSTAL SRM 51-42-06-001-001. INSTALLED NEW CLIP & INTERCOSTAL AT HINGE END OF ASD IAW SRM 51-42-06-001-001-A01.

Part: HINGE — CORRODED (PAX DOOR) · airframe 20,282 hrs · 14,065 cycles

FOUR CLIPS CORRODED ON PAX DOOR HINGE SIDE. REMOVED CLIPS FROM PAX DOOR HINGE SIDE IAW SRM 51-42-06-001-001 AND 51-42-10-991-804. DRILLED UP AND INSTALLED 4 EA NEW CLIPS ON HINGE SIDE OF PAX DOOR SRM 51-42-06-001-001. SDR CLOSED.

Part: FLOOR SUPPORT — CORRODED (BS 280-285) · airframe 20,282 hrs · 14,065 cycles

RT FUSELAGE FLOOR SUPPORT IS CORRODED AFT OF FS 280 AT FS 285 APROX. BEYOND ALLOWABLE LIMITS OF SRM 53-00-00-101-001. RECEIVED AND COMPLIED WITH REO 670-53-21-876 IAW NDTM PART 1, 51-20-006. FOUND TO BE SATISAFACTORY.

Part: SEAT TRACK — CORRODED (BS 708-785.15) · airframe 20,264 hrs · 14,048 cycles

LT SIDE SEAT RAIL CORRODED FROM FS708-FS785.15 . FOUND TO BE OUT OF LIMITS. REMOVED LT SIDE WALL SEAT TRACK IAW AMM TASK 53-00-49-000-801. INSTALLED NEW LT SIDE WALL SEAT TRACK IAW AMM 53-00-49-400-801. SDR CLOSED.

Part: WEB — CORRODED (BS 280) · airframe 20,282 hrs · 14,065 cycles

RT LOWER WEB AT FS 280 CORRODED INBD SECTION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001. COMPLIED WITH EC/TC REO 670-53-11-594 01 AND GENERIC REO 670-53-11-594. COMPLIED WITH NOTE ON SHEET 4 OF REO 670-53-11-594 NDTM PART 1, 51-20-006.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 20,264 hrs · 14,048 cycles

SEAT TRACK CORRODED FROM FS 485- 581 RT SIDE. REMOVED CORROSION & FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01, SRM 51-21-06-001-001-A01. 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 485-581) · airframe 20,264 hrs · 14,048 cycles

SEAT TRACK CORRODED FROM FS 485 - 581 LT SIDE. REMOVED CORROSION & FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01 & SRM 53-31-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 785.15-893) · airframe 20,282 hrs · 14,065 cycles

RT SIDE SEAT TRACK CORRODED FROM FS 785.15 -893. REMOVED SEAT TRACK IAW AMM TASK 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM TASK 53-00-49-400-801 CONFIG 3. FOUND TO BE SATISFACTORY.

Part: SEAT TRACK — CORRODED (BS 708-785.15) · airframe 20,264 hrs · 14,048 cycles

RT SIDE SEAT TRACK CORRODED FROM FS 708-785.15. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,264 hrs · 14,048 cycles

SERVICE DOOR LOWER SILL PLATE CORRODED IN SEVERAL PLACES. SERVICE DOOR MOUNTING ANGLE FOUND TO BE CORRODED OUT OF LIMITS IAW SRM 53-21-23-101-002 A01. REMOVED MOUNTING ANGLE IAW SRM 51-42-06-001-001. INSTALLED ANGLE IAW SRM 51-42-06-001-001-A01. FOUND TO BE SATISFACTORY. SDR CLOSED.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 20,264 hrs · 14,048 cycles

RT SIDE SEAT TRACK CORRODED FROM FS 677 - 708 . FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK IAW AMM TASK 53-00-49-000-801. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 581-693) · airframe 20,264 hrs · 14,048 cycles

SEAT TRACK CORRODED FROM FS 581- 693 RT SIDE. REMOVED CORROSION & FOUND SEAT TRACK TO BE OUT OF LIMITS, IAW SRM 51-21-06-001-001-A01, SRM 53-31-49-101-001-A01. 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 581-693) · airframe 20,264 hrs · 14,048 cycles

FLOOR SEAT TRACK CORRODED FROM FS 581- 693 LT SIDE. REMOVED CORROSION & FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01, SRM 53-31-49-101-001-A01. R & R SEAT TRACK IAW AMM TASK 53-00-49-100-801 AND 53-00-49-400-801.

Part: STRINGER — CORRODED (BS 333-349 S26R) · airframe 20,264 hrs · 14,048 cycles

STRINGER 26R CORRODED BETWEEN FRAMES 333 & 349. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED STRINGER AND INSTALLED NEW STRINGER IAW SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,264 hrs · 14,048 cycles

COCKPIT FLOOR SUPPORT FOR PANEL 221ALF CORRODED AT FS 280.00 (PB). REMOVED FLOOR SUPPORT ANGLE. FOUND CORROSION BACK SIDE OF ANGLE TO BE OUT OF LIMITS IAW SRM 53-00-00-401-001-A01 LOCATED & DRILLED NEW SERVICEABLE ANGLE IAW SRM 51-40-06-001-001-A01 & 51-42-06-001-001-A01 INSTALLED NEW, SERVICABLE ANGLE IAW SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 295-310 S26R) · airframe 20,264 hrs · 14,048 cycles

STRINGER 26R CORRODED BETWEEN FRAMES 295 & 310. REPAIRED IAW REO 670-53-21-875.

Part: WEB — CORRODED (BS 280) · airframe 20,264 hrs · 14,048 cycles

LEFT LOWER WEB AT FS 280 CORRODED INBD SECTION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001. REPAIRED LT LOWER WEB IAW EC/TC REO 670-53-11-594.

Part: STRUCTURE — CORRODED (BS 278) · airframe 20,264 hrs · 14,048 cycles

FWD JACK FITTING AT FS 278 BL 0 CORRODED AT LOWER SECTIONS. REMOVED RT NOSE JACK SUPPORT INTERCOSTALS. BLENDED CORRODED AREA & INSTALLED REF SRM 51-21-06-001-001 & SRM 51-42-06-001-001. COMPLIED WITH STEP 4 OF REO 670-53-11-733 IAW NDTM PART 1, 51-20-006 NO INDICATIONS NOTED AT THIS TIME. COMPLIED W/STEP 5 OF REO 670-53-11-733. RII FOUND TO BE SATISFACTORY. SDR CLOSED.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 20,264 hrs · 14,048 cycles

FWD EQUIPMENT COMPARTMENT FLOOR PANEL CRACKED LT SIDE. REPAIRED IAW EC/TC REO 670-53-11-509.

Part: ANGLE — CORRODED (BS 364) · airframe 20,264 hrs · 14,048 cycles

SUPPORT ANGLE FWD OF FS 364.00 FWD OF AVIONICS CUTOUT, ON RT SIDE OF STGR 27 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .076" ORIGINAL IS 080", MATERIAL REMOVED IS .004". REPAIRED IAW REO 670-53-21-874.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,264 hrs · 14,048 cycles

FWD FLOORBEAM AT FS 280 CORRODED. R & R FWD FLOORBEAM IAW SRM 51-42-06-001-001, 51-42-21-001-001.

Part: STRINGER — CORRODED (BS 333-349 S25R) · airframe 20,264 hrs · 14,048 cycles

STRINGER 25R CORRODED BETWEEN BS 333 & 349. BLENDED CORROSION ON STRINGER AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03-101-006-A01. REMOVED OLD STRINGER IAW SRM 51-42-00-001-001 & 51-42-21-001-001. DRILLED AND INSTALLED SERVICEABLE LONGERON REF SRM 51-40-11-001-001.

Part: SKIN — CORRODED (BS 295-310) · airframe 20,264 hrs · 14,048 cycles

INTERNAL SKIN PLATE FOR TCAS ANTENNA LOCATED BETWEEN FS 295.00 & 310.00 IS CORRODED. INSTALLED NEW TCAS DOUBLER IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-23-00-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,264 hrs · 14,048 cycles

FS 280 FLOORBEAM CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001. R & R FS 280 FLOORBEAM IAW REO 670-53-11-047.

Part: FRAME — CORRODED (BS 319.7 S26R) · airframe 20,264 hrs · 14,048 cycles

FRAME BS 319.70 CORRODED AT S26R. REPAIRED IAW REO 670-53-21-799.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 20,264 hrs · 14,048 cycles

FWD EQUIPMENT COMPARTMENT FLOOR PANEL CRACKED RT SIDE FS 193.00, WL 79.50. REPLACED IAW EC/TC REO 670-53-11-509.

Part: UNKNOWN — FUMES (GALLEY AREA) · airframe 20,263 hrs · 14,047 cycles

IN FLT, FUMES DETECTED NEAR GALLEY AREA 1ST CLASS. EMERGENCY DECLARED. DURING INSPECTION, FOUND NO NOTICABLE DEFECTS WITH THE ACFT, NO ODOR OF BURNING PLASTIC WAS FOUND IN GALLEY OR 1ST CLASS. ACFT REMAINS OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,761 hrs · 12,959 cycles

CABIN NR 1 CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED NR 1 CEILING EMERGENCY LIGHT IAW AMM 33-51-06, OP'S CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 18,470 hrs · 12,763 cycles

EMERGENCY LIGHTS WILL NOT TEST. RAN APU TO CHARGE EMERGENCY LIGHTS, DISCREPANCY NO LONGER EXISTS.

Part: WARNING LIGHT — ILLUMINATED (BLEED AIR) · airframe 17,878 hrs · 12,361 cycles

ON CLIMB OUT RECIVED BLEED DUCT WARNING. REMAINED FOR 30 SEC ALL BLEEDS CLOSED C/W QRH RETURNED TO BMI. RT ENG INDICATION RED. ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION. PERFORMED A VISUAL INSP OF THE RT ENG AND FOUND NO VISUAL DEFECTS. PERFORMED LEAK TEST OF BOTH ENG MOUNTED BLEED AIR SYS IAW AMM 36-10-00 AND PERFORMED OPS TEST OF BLEED LEAK AND DETECTION SYS IAW AMM 36-21-00. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,857 hrs · 12,344 cycles

EMERGENCY LIGHTS INOP AT LT OVERWING EMERGENCY EXIT, ENTRANCE DOOR FLOODLIGHT, NR 2 CEILING LIGHT AND MID CABIN AFT FACING EXIT LIGHT. R & R EPSU BATTERY PACK IAW AMM 33-51-17-400-801, OPS CKS GOOD IAW AMM 33-51-17-710-801. NO DEFECTS NOTED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,857 hrs · 12,344 cycles

EMERGENCY EXIT LOCATOR SIGN FACING AFT IN MID CABIN IS INOPERATIVE. R & R EPSU BATTERY PACK IAW AMM 33-51-17-400-801, OPS CKS GOOD IAW AMM 33-51-17-710-801.

Part: OVERHEAT LOOP — MALFUNCTIONED (BLEED SYSTEM) · airframe 17,857 hrs · 12,344 cycles

AT 16000 MSL RECEIVED LT BLEED DUCT WARNING, COMPLIED WITH QRH AIR RETURNED LANDED OVER WEIGHT 2000 LBS. (ACFT RETURNED TO PIT AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) R & R BOTH MT137 AND MT138 BLEED LOOPS ON THE HP GROUND DUCT, OPS CHECK GOOD IAW AMM 36-21-01, ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,375 hrs · 12,014 cycles

NR 3 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED NR 3 EXTERIOR EMERGENCY LIGHT AS REQUIRED. OPS CHECK GOOD IAW AMM 33-51-00. RELAMPED NR 3 EXTERIOR EMERGENCY LIGHT AS REQUIRED. OPS CHECK GOOD IAW AMM 33-51-00. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,258 hrs · 11,916 cycles

EMERGENCY LIGHTS BEHIND SEATS 3CD WILL NOT LIGHT UP AND THE OTHER SIDE IN FRONT OF 4CD WILL NOT LIGHT. REPLACED 3 DIODES IN EMERGENCY LIGHT BATTERY PACK FOR FWD CABIN EMERGENCY LIGHTS IAW CMM 33-21-70. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 17,258 hrs · 11,916 cycles

EMERG LIGHT LENSE COVER NEXT TO SERVICE DOOR IS MISSING AND DOES NOT LIGHT UP. INSTALLED LIGHT COVER AND REPLACED ALL 6 BULBS. OPS CKD GOOD IAW AMM 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,108 hrs · 11,802 cycles

MID CABIN INTERIOR EMERGENCY CEILING LIGHTS INOP FOUND DURING LC2 CHECK. R & R NR 2 BATTERY PACK ASSY IAW AMM 33-51-17. OPS CHECK GOOD ON GROUND. NO OTHER DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: BATTERY PACK — INTERMITTENT (EMERGENCY LIGHTS) · airframe 17,066 hrs · 11,770 cycles

MID CABIN OVERHEAD EMERGENCY LIGHTS WILL NOT ILLUMINATE. R & R NR 1 CHARGER AND EMERGENCY POWER LIGHT BATTERY PACK IAW AMM 33-51-17 AND 33-52-01. DID NOT FIX PROBLEM. (CLOSED)

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 17,066 hrs · 11,770 cycles

REFER TO DMIL 613941-1; NR 2 AND NR 3 LT AND RT EXTERIOR EMERGENCY LIGHTS INOP. R & R 2 BLOWN PICO FUSES IN NR 2 AND NR 3 BATTERY PACK CHARGERS IAW CMM 33-21-70. OPS TEST GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 17,066 hrs · 11,770 cycles

MID CABIN INTERIOR EMERGENCY CEILING LIGHT INOP. R & R 2 BLOWN PICO FUSES IN NR 2 AND NR 3 BATTERY PACK CHARGERS IAW CMM 33-21-70. OPS TEST GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 17,066 hrs · 11,770 cycles

NR 2 AND NR 3 LT AND RT EXTERIOR EMERGENCY LIGHTS ARE IN-OP. (EXTERIOR EMERGENCY LIGHTS - ACFT NOT OPERATED AT NIGHT ) R & R 2 BLOWN PICO FUSES IN NR 2 AND NR 3 BATTERY PACK CHARGERS IAW CMM 33-21-70. OPS TEST GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,059 hrs · 11,765 cycles

MID CABIN OVERHEAD EMERGENCY LIGHT WILL ILLUMINATE. R & R NR 4 EMERGENCY POWER SUPPLY IAW AMM33-51-17.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 17,059 hrs · 11,765 cycles

MID CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE. R & R 2 BLOWN FUSES IN NR 2 AND NR 3 BATTERY PACK CHARGERS IAW CMM 33-21-70. OPS TEST GOOD. (CLOSED)

Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 17,019 hrs · 11,736 cycles

F/A'S (CABIN) MEGAPHONE INOP. R & R MEGAPHONE BATTERY IAW AMM 25-61-14. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. (CLOSED)

Part: DOOR — OUT OF ADJUST · airframe 16,770 hrs · 11,572 cycles

GALLERY SERVICE DOOR HARD TO OPEN. PERFORMED ADJUSTMENT OF THE GALLEY SERVICE DOOR IAW CRJ200 AMM 52-41-00. PERFORMED OPERATIONAL TEST OF THE GALLEY SERVICE DOOR. NO DEFECTS NOTED. ACFT OK FOR SERVICE IAW AMM 52-41-00-710-801.

Part: DOOR — OUT OF ADJUST (SERVICE) · airframe 16,748 hrs · 11,554 cycles

FA ADVISED SERVICED DOOR VERY HARD TO OPEN AND CLOSE. FLT 5450. PERFORMED ADJUSTMENT OF THE GALLEY SERVICE DOOR IAW AMM 52-41-00. PERFORMED OPERATIONAL TEST OF THE GALLEY SERVICE DOOR. NO DEFECTS NOTED. ACFT OK FOR SERVICE IAW AMM 52-41-00-710-801.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 16,635 hrs · 11,476 cycles

RIGHT EXTERNAL EMERGENCY LIGHT AFT EMERGENCY EXIT, ABOVE RT WING, IS INOPERATIVE. REPLACED LAMP IAW CMM 33-52-07.

Part: LIGHT — DAMAGED (CABIN) · airframe 16,635 hrs · 11,476 cycles

RIGHT EMERGENCY LIGHT STRIP NR 13 & NR 12 ARE DAMAGED. REMOVED UNSERVICEABLE RT EMERGENCY LIGHT STRIP NR 13 & NR 12. INSTALLED SERVICEABLE RT EMERG LIGHT STRIP NR 13 & NR 12 IAE AMM 33-51-01.

Part: SEAT TRACK — CORRODED (BS 693-847) · airframe 16,635 hrs · 11,476 cycles

SEAT TRACK SEGMENT FROM FS 693.00 TO FS 847.00 IS CORRODED IN SEVERAL PLACES. RT FLOOR SEAT TRACK. REPAIRED SEAT TRACK SEGMENT IAW SRM 53-41-49.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 16,635 hrs · 11,476 cycles

AFT CARGO COMPARTMENT FLOORBEAM UNDER PANEL 282KRF IS CORRODED AROUND 3 SCREW HOLES. REPAIRED IAW REO 670-53-61-692. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 847-969) · airframe 16,635 hrs · 11,476 cycles

RT FLOOR SEAT TRACK SEGMENT FROM FS 847.00 TO FS 969.00 IS CORRODED IN SEVERAL PLACES. R & R SEAT TRACK IAW AMM 53-00-49 & SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 847-969) · airframe 16,635 hrs · 11,476 cycles

LEFT FLOOR SEAT TRACK SEGMENT FROM FS 847.00 TO FS 969.00 IS CORRODED IN SEVERAL PLACES. REPAIRED SEAT TRACK IAW SRM 53-51-49.

Part: FLOOR SUPPORT — CORRODED (BS 958-1047) · airframe 16,635 hrs · 11,476 cycles

AFT CARGO COMPARTMENT FLOORBEAM NEXT TO CARGO DOOR IS CORRODED AROUND SEVERAL SCREW HOLES FROM FS 985.00 TO FS 1047.00. REPAIRED IAW ASA EC/TC REO 670-53-61-693. CLASSIFIED A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 16,635 hrs · 11,476 cycles

AFT CARGO COMPARTMENT FLOORBEAM UNDER FLOORBOARD 282JRF IS CORRODED AROUND SEVERAL SCREW HOLES. REPAIRED IAW EC/TC REO 670-53-61-692. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 693-847) · airframe 16,635 hrs · 11,476 cycles

SEAT TRACK SEGMENT FROM FS 693.00 TO FS 847.00 IS CORRODED IN SEVERAL PLACES. LT FLOOR SEAT TRACK. REPAIRED SEAT TRACK SEGMENT IAW 53-41-49.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 16,635 hrs · 11,476 cycles

FS 280 BULKHEAD CROSSBEAM IS SEVERELY CORRODED. REPLACED FS 280 BULKHEAD CROSSBEAM IAW SRM 53-11-10, 51-42-06, 51-42- SRM 53-11-10, 51-42-06, 51-42-13 AND 51-42-21.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,635 hrs · 11,476 cycles

AFT DRAG ANGLE CRACKED AT MID DOOR ( PAX) MARKED 12601, PG 13. REPLACED AFT DRAG ANGLE ON PAX DOOR (AFT) IAW SRM 51-42-06, 51-42-13, 51-40-11, 51-42-12, 51-40-11, AND 51-23-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,085 hrs · 11,098 cycles

EMERGENCY LIGHTS INOP. R & R EMERGENCY LIGHT BATTERY PACK IAW CRJ 700 33-51-17, OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,287 hrs · 10,518 cycles

MAIN CABIN NR 2 EMERGENCY LIGHT POWER SUPPLY WILL NOT OPERATE NR 2 CABIN FLOOD LIGHT - LT FWD EXTERNAL O/W LIGHT. R & R NR 2 EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-17-000-805 AND 33-51-17-400-802. PERFORMED OPS TEST OF EMERGENCY POWER SUPPY UNIT IAW AMM 33-51-17-710-80. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 379-549) · airframe 14,997 hrs · 10,291 cycles

RIGHT I/B SEAT TRACK HAS CORROSION FROM STA 379 TO STA 549 IN SEVERAL SPOTS AS MARKED. REMOVED AND REPLACED RT I/B SEAT TRACK IAW SRM 51-41-00. CLEANED AND TREAT CORROSOION OFF THE REMAINING SEAT TRACK IAW SRM 53-21-49.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 14,931 hrs · 10,241 cycles

THE EMERGENCY INDICATOR LIGHT CAP/COVER IN THE OVERHEAD EMERGENCY EXIT INDICATOR IS MISSING. REPLACED MISSING RED LIGHT COVER ON EXIT ROW EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-07. ACFT OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,894 hrs · 10,212 cycles

LT OVER WING EMERGENCY LIGHT INOP. (RESOLVED ON W/O: 157833 TASKCARD: N/R-00002 ), R & R NR 2 EMERGENCY BATTERY CHARGER ASSY IAW AMM 33-51-05 OPS CHECK IS GOOD. (CLOSED)

Part: CHARGER — DEFECTIVE (EMERGENCY LIGHT) · airframe 14,731 hrs · 10,075 cycles

FOUND THE CTR LIGHTED CEILING EXIT SIGN FWD DIRECTION, CABIN EMERGENCY FLOODLIGHT 2, AND THE EXTERIOR EMERGENCY LIGHT 3 ARE ALL INOP. R & R NR 1 EPSU BATTERY CHARGER IAW AMM 33-51-17. OPS CHECK GOOD AT THIS TIME.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 13,717 hrs · 12,225 cycles

R & R NLG PRIORITY VALVE IAW AMM 32-33-15,OPS CK GOOD, NO FURTHER DEFECTS NOTED. ACFT OK FOR FURTHER SERVICE. (CLOSED)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 14,558 hrs · 9,945 cycles

EMERGENCY LIGHTS FAILED FUNCTIONAL TEST. R & R BATTERY SUPPLY UNITS IAW AMM 33-51-07. ALL OPS CHECK GOOD. R & R NR 1, NR 2, NR 3 AND NR 4 BATTERY SUPPLY UNITS IAW AMM 33-51-07. ALL OPS CHECK GOOD.

Part: PLACARD — UNKNOWN (CABIN) · airframe 14,465 hrs · 9,880 cycles

F/A REPORTS MAIN CABIN DOOR EXIT STICKER NEEDS REPLACING. INSTALLED EXIT PLACARD ON PAX DOOR STEP IAW IPC 11-30-02.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,172 hrs · 9,665 cycles

R & R NR 2 BATTERIES POWER SUPPLLY UNIT. ITEM REMIAINS OPEN SEE AFDL 514042-1. IAW AMM 33-51-17. (CLOSED)

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,172 hrs · 9,665 cycles

EMERGENCY SIGN LIGHT ROW 14 IS INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,032 hrs · 9,552 cycles

FWD CEILING OVERRUNING EMERGENCY EXIT EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,823 hrs · 9,400 cycles

EMG LIGHTS INOP. FLT 5146

Part: STEP — CRACKED (PAX DOOR) · airframe 12,040 hrs · 8,033 cycles

BOTTOM STEP ON PAX DOOR CRACKED NEAR ANCHOR FITTING.

Part: ANGLE — CRACKED (BS 280) · airframe 11,819 hrs · 7,863 cycles

280 WEB ANGLE BL 26R PART NR CC670-34117-6 (SRM 53-11-10) CRACKED THROUGH LOWER FASTENER HOLE. REMOVED AND REPLACED 280 WEB ANGLE BL 26R P/N CC670-34117-6 PER SRM 51-42-06. BAT 7023167 2-11-2009.

Part: BULKHEAD — CORRODED (BS 280) · airframe 11,819 hrs · 7,863 cycles

LT 280 WEB CORRODED ON AFT SURFACE. LT 280 WEB REMOVED AND REPLACED PER SRM 51-42-06 AND 51-42-21. REMOVED LT LOWER WEB STRUCTURE AND STRAP IAW SRM 53-11-10 AND 51-42-06. LOCATED HOLES IN AFT FACE OF LOWER WEBS IAW SRM 51-42-06. FINISHED LOCATING HOLES IN LT LOWER WEB PER SRM 51-42-0. OK TO INSTALL. STARTED INSTALLING FASTENERS IN LT LOWER WEB PER SRM 53-11-10 AND 51-42-06. CONTINUED INSTALLING LT FASTENERS IN LT LOWER WEB PER SRM 53-11-10, 51-42-06, AND 51-42-13. FINISHED INSTALLING ALL FASTENERS IN LOWER LT FS 280 WEB PER SRM 53-11-10.

Part: BULKHEAD — CORRODED (BS 280) · airframe 11,819 hrs · 7,863 cycles

RT FS280 BULKHEAD LOWER WEB HAS SURFACE CORROSION. REMOVED AND REPLACED RT FS 280 WEB PER SRM 51-42-06 AND 51-42-21. REMOVED RT FS 280 LOWER WEB. DRILLED RT FS 280 LOWER WEB PER SRM 51-42-06. FINAL SIZED ALL HOLES IN RT 280 WEB PER SRM 51-42-06 AND 51-40-11, 51-42-20. OK TO INSTALL RT LOWER WEB PER SRM 53-11-10. STARTED INSTALLING FASTENERS IN RT LOWER WEB PER SRM 53-11-10, 51-42-06, AND 51-42-13. FINISHED INSTALLING FASTENERS IN RT LWR WEB FS 280 PER SRM 53-11-10.

Part: BULKHEAD — CORRODED (BS 280) · airframe 11,819 hrs · 7,863 cycles

LT FS280 BULKHEAD LOWER WEB HAS SURFACE CORROSION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,818 hrs · 7,863 cycles

FS 280 FLOORBEAM IS CORRODED (RT OF BL 0). REMOVED AND REPLACED FS 280 BEAM (RT OF BL 0). REMOVED RIGHT SIDE BEAM IAW SRM 700 51-42-06 AND 51-42-21. PILOT DRILLED RT FS 280 FLOORBEAM PER CRJ 700 SRM 51-41-00. BEGIN FINAL SIZING HOLES IN AFT FACE RT 280 BEAM CRJ 700 SRM 51-42-06 AND 51-40-11, 51-42-20. FINAL SIZED HOLES IN RT FS 280 FLOORBEAM AND WET INSTALLED TITANIUM DOUBLERS AND U-BRACKET IAW CRJ 700 SRM 51-42-21 AND 51-42-06. OK TO INSTALL RT FLOORBEAM. STARTED INSTALLING FASTENERS IN RT FS 280 FLOORBEAM IAW CRJ 700 SRM 51-42-06 AND 51-42-11 AND 51-42-20. FINISHED INSTALLING FASTENERS IN RT FS 280 BEAM PER CRJ 700 SRM 51-42-06 EXCEPT FASTENERS COMMON TO SB670BA-53-026.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 11,819 hrs · 7,863 cycles

FS 280 FLOORBEAM IS CORRODED (RT OF BL0).

Part: FLOORBEAM — CORRODED (BS 280) · airframe 11,819 hrs · 7,863 cycles

FS 280 FLOORBEAM IS CORRODED (LT OF BL0). LT FS 280 FLOORBEAM (LT OF BL 0). REMOVED AND REPLACED PER SRM 51-42-06 & 51-42-21. REMOVED LEFT BEAM IAW SRM 700 51-42-06 AND 51-42-21. PILOT DRILLED L/S FS 280 FLOORBEAM PER SRM 51-41-00. FINAL SIZED HOLES IN L/S FLOORBEAM AND WET INSTALLED TITANIUM DOUBLES AND U-BRACKET IAW SRM 51-42-21- AND 51-42-06. OK TO INSTALL LT FLOORBEAM. STARTED INSTALLING LT FS 280 FLOORBEAM PER SRM 51-42-06. INSTALLED WET WITH PS870C12. PICKED UP FASTENER HOLES FOR CENTER SPLICE IAW REO 670-53-11-047. OK TO INSTALL CENTER SPLICE. REFER TO W/O 109650 N/R-00217 FOR DISPOSITION. FINISHED INSTALLING FASTENERS IN LT FS 280 BEAM EXCEPT FASTENERS COMMO

Part: SILL — CORRODED (BS 280) · airframe 11,819 hrs · 7,863 cycles

RT FLOOR SILL AT FS 280 FWD CORNER CORRODED AT WL 72.50. REPAIRED RT FLOOR SILL AT FS 280 PER REO 670-53-21-139. REFER TO EC/TC REO 670-53-21-139 FOR WORK ACCOMPLISHED 2-11-09.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,214 hrs · 7,446 cycles

CABIN OVERHEAD EMERGENCY LIGHTS OUT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,266 hrs · 6,745 cycles

EMERGENCY LIGHT IN GALLEY NEAR SERVICE DOOR HAS A COUPLE LIGHTS BURNT OUT. RELAMPED EMERGENCY LIGHT IAW CRJ 700 AMM 33-51-05. (B)

Part: COVER — MISSING (CABIN) · airframe 9,205 hrs · 6,005 cycles

PLASTIC EXIT LIGHT COVER BY FRONT DOOR IS MISSING. FLT 4182 DEL 31 MINS.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 8,291 hrs · 5,413 cycles

L/R EMERGENCY EXIT LIGHTED EXIT SIGNS HAVE LIGHT BULBS OUT.

Part: BATTERY — WEAK (EMERGENCY LIGHTS) · airframe 7,555 hrs · 4,930 cycles

NR 1 EMERGENCY BATTERY IS WEAK.

Part: RAIL — CORRODED (CABIN SEAT) · airframe 7,537 hrs · 4,917 cycles

CORROSION ON LEFT SIDE CABIN SEAT SIDE RAIL FS 677.00 TO 708.00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,537 hrs · 4,917 cycles

CORROSION ON RT SIDE CABIN FLOOR RAIL FS 349.00 TO 485.00.

Part: FRAME — CORRODED (FUSELAGE) · airframe 7,537 hrs · 4,917 cycles

CORROSION AT FS 280 FRAME TO FS 295 FRAME BETWEEN STRINGERS 26L AND 26R BL 0 (MARKED). REMOVED CORROSION FROM FS 295 LOWER FRAME. DAMAGE FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-21-06. REMOVED AND REPLACED FOUR SOLID RIVETS ON FS 295 FRAME ON RT SIDE OF BL 0. RESTORED FINISH TO SURFACE. WORK DONE IAW CRJ 700 SRM 51-00-00. SUPPLEMENTAL - SDR CLOSED 07/10/07.

Part: WEB — CORRODED (FUSELAGE) · airframe 7,537 hrs · 4,917 cycles

LEFT AND RIGHT WEBS AT FS 280 RBL 9 TO OUTBOARD WALL AND LBL 9 TO OUTBOARD WALL CORRODED (PER MTC).

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 7,537 hrs · 4,917 cycles

ASD EXTERIOR HANDLE CRACKED. REMOVED AND REPLACED EXTERIOR HANDLE IAW 700 AMM 52-11-03. SUPPLEMENTAL - SDR CLOSED 07/11/07.

Part: BRACKET — CRACKED (AIRSTAIR DOOR) · airframe 7,537 hrs · 4,917 cycles

ASD LOWER SIDE WALL ANGLE BRACKET CRACKED (MARK). REMOVED FASTENERS, MOTOR PULLEY BRACKET AND DID CUT-OUT IAW BOMBARDIER REO 670-52-11-072. EDDY CURRENT INSPECTED, NO CRACKS NOTED PER NDTM 51-20-06. FABRICATED PARTS AND INSTALLED IAW BOMBARDIER REO 670-52-072. SUPPLEMENTAL - SDR CLOSED 07/10/07.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,480 hrs · 4,213 cycles

THE 2ND FROM AFT CEILING EMERGENCY LIGHT INOP.

Part: DOOR — CRACKED (FUSELAGE)

DURING A C-CHECK, THE PASSENGER DOOR FORWARD AND AFT SIDEWALL, UNDER THE HANDRAIL SUPPORT BRACKET, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR FORWARD AND AFT SIDEWALL, UNDER THE HANDRAIL SUPPORT BRACKET IAW REO. (K)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN ATL, THE NR 2, 3 AND 4 EMERGENCY LIGHT BATTERY PACKS WERE FOUND DEAD. MAINTENANCE REMOVED AND REPLACED THE NR 2, 3 AND 4 EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

FLT 4871 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS BATTERY PACK IN THE AVIONICS COMPARTMENT WAS FOUND DEAD. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IN THE AVIONICS COMPARTMENT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)