N712EV

Part: NONE — DAMAGED · airframe 37,344 hrs · 26,739 cycles

LH AILERON CENTER, OB HINGE LUG DAMAGED. (C-CHECK RO 1/13/2022) PERFORMED REPAIR ON LEFT HAND AILERON OUTBD HINGE LUG PER MHIRJ REO 670-57-61-379 REV. -- DATED:2021-12-08. NO FURTHER ACTION REQUIRED AT THIS TIME. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTIONS.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

DURING THE REMOVAL OF RIGHT HAND SIDE INTERCOASTAL AT STRINGER STR24R FOR CORROSION AT FUSELAGE STATION FS409 THRU FS421 AIRCRAFT SKIN SUFUR DAMAGED. (C-CHECK RO 1/13/2022) PERFORMED SKIN REPAIR AT STGR24R FROM FS394- FS409, IN ACCORDANCE WITH REPAIR ENGINEERING ORDER (REO) MHIRJ 670-53-21-2184 REV.-- DATED:2021-12-02. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION. / NOTES: / 1. PLEASE REFERENCE CAMP # 23531501 CONTINUATION SHEET ITEM 23 FOR PRESSURIZATION CHECK. / 2.ANALYSIS TO DETERMINE ADDITIONAL REQUIREMENT WILL BE COMPLETED WITHIN 12 MONTH OF ISSUE DATE OF THIS REPAIR. / THE AIRCRAFT MUST NOT BE OPERATED BEYOND 12 MONTHS FROM THE ISSUE DATE OF REPAIR. ISSUE DATE: 02-DEC-2021.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

FS409 THRU FS421 RIGHT SIDE OF FUSELAGE CORROSION ON INTERCOASTAL AT STRINGER STR24R. (C-CHECK RO 1/13/2022) REMOVED CORRODED SECTION OF STRINGER 24R AT FS 409.00 TO FS 421.00 AND REPLACED WITH NEW SECTION. REF. CRJ700 SRM 53-00-03. REFERENCE CONTINUATION CARD FOR REPAIR DISPOSITIONS AND CORRECTIVE ACTIONS.

Part: NONE — DENTED · airframe 37,344 hrs · 26,739 cycles

DENT FOUND ON LEFT HAND OUTER SKIN FROM FS 235 TO FS 250, AT BUT JOIN STGR16L. (C-CHECK RO 1/13/2022) PERFORMED REPAIR ON SKIN AT FS235 TO FS250, STGR16L PER MHIRJ REO 670-53-11-1754 REV. -- DATED: 2021-11-24. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION.NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

CORROSION FOUND ON AFT SIDE OF FRAME FS863, STR27. REQUIRES TO BE REPLACED. (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED LOWER FRAME FS863 FROM SGTR17L TO SGTR17R PER CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — DENTED · airframe 37,344 hrs · 26,739 cycles

DENT FOUND ON LEFT HAND OUTER SKIN FROM FS 533 TO FS 549, BETWEEN STGR 16L AND STGR 17L. (C-CHECK RO 1/13/2022) REPAIRED DENTED AREA AT FUSELAGE STATION FS 533.00 STGR 16L TO STGR 17L PER REO 670-53-31-749 REV -- DATED 2021-12-03. PLEASE REFERENCE CONTINUATION CARD FOR REPAIR DISPOSITIONS AND CORRECTIVE ACTIONS. NO OTHER DEFECTS NOTED.

Part: NONE — DAMAGED · airframe 37,344 hrs · 26,739 cycles

CREASE IN FUSELAGE SKIN UNDER SERVICE DOOR AT FS 333.00 BETWEEN STGR21R AND STRGR22R . NEEDS TO BE EVALUATED . (C-CHECK RO 1/13/2022) PERFORMED REPAIR ON FUSELAGE SKIN CREASE UNDER SERVICE DOOR AT FUSELAGE STATION FS 333.00 BETWEEN STRINGER STGR21R AND STGR 22R PER REPAIR ENGINEERING ORDER (REO) 670-53-21-2176 REV-- DATED 2021-11-10. PLEASE REFER TO CONTINUATION CARD FOR REPAIR DISPOSITIONS AND CORRECTIVE ACTIONS. NO FURTHER ACTION REQUIRED.

Part: NONE — DENTED · airframe 37,344 hrs · 26,739 cycles

SEVERAL DENTS & SKIN DISTORTED AT L/H SKIN SIDE P/N SH670-31151-9 BETWEEN FS 364 & FS 394 & STR 17LH STR 18LH IN AFT SILL ATTACHING ZONE (C-CHECK RO 1/13/2022) PERFORMED A REPAIR ON LEFT HAND OUTER SKIN AT FUSELAGE STATION FS364 UP TO FS394 BETWEEN STRINGER STGR17L AND STGR18L PER MHIRJ REO 670-53-21-2170 REV. -- DATED:2021-11-01 NO DISCREPANCIES OR DEFECTS NOTED. / PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION. / NOTE: PLEASE REFENCE CAMP # 23531501 ITEM 14 FOR PRESSURIZATION CHECK. NO FUTHER ACTION REQUIRED.

Part: NONE — GOUGED · airframe 37,344 hrs · 26,739 cycles

AIRCRAFT RUDDER MIDDLE HINGE FITTING , HINGE LUG AT STATION 92.94 HAS 2 GOUGES , AS MARKED . (C-CHECK RO 1/13/2022) PERFORMED REPAIR ON RUDDER MIDDLE HINGE FITTING AT STA. 92.94 PER REO 670-55-41-093 REV-- DATED 2021-10-14. REFERENCE CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTIONS.

Part: NONE — DAMAGED · airframe 37,344 hrs · 26,739 cycles

FRAME @ FS 517.00 BETWEEN STR 18L & STR 19L BLISTERED PAINT /DEBRIS BUILD-UP. CLEAN & RE-INSPECT. (C-CHECK RO 1/13/2022) REMOVED, FABRICATED AND INSTALLED STUB FRAME AT FS517 FROM STGR18L AND SGTR19L. REF CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. PLEASE REFER TO CONTINUATIONN CARD FOR DISPOSITION AND CORRECTIVE ACTION. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — DAMAGED · airframe 37,344 hrs · 26,739 cycles

REMOVE AND REPLACE FLOOR SUPPORT BEAM AT LBL 9, FROM FS 858.00 - 939.00 (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED LONGITUDINAL FLOOR BEAM WITH A NEW SUPPORT AT LBL9 FROM FS858.00 TO FS939.00 PER CRJ700 SRM 53-00-41-201-001-A01. PAGE 207 PART 5 SECTION B ITEMS 10 THRU 19 AND PART 6 ITEMS A ONLY, / PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTIONS. NO FURTHER ACTION REQUIRED AT THIS TIME. / NOTE: PLEASE REFERENCE CAMPS 23085615 AND 23085616 FOR CORROSION PREVENTION TAPE AND SEALANTS INSTALLATION.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

REPLACE CORRODED FLOOR SUPPORT BEAM AT RBL9 FROM FS858 TO FS939. (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED FLOOR BEAM SUPPORT AT RBL9 FROM FS858 TO FS939 PER CRJ700 SRM 53-00-41-201-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTIONS. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

REPLACE CORRODED LONGITUDINAL FLOOR SUPPORT BEAM FROM FS565.00 TO FS661.00, LBL 9 (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED LONGITUDINAL FLOOR BEAM WITH A NEW SUPPORT AT LBL9 FROM FS565 TO FS661 PER CRJ700 SRM 53-00-41-201-001-A01. PAGE 207 PART 5 SECTION B ITEMS 10 THRU 19 AND PART 6 ITEMS A ONLY, AND REPAIR ENGINEERING ORDER- / (REO) 670-53-31-718 REVISON-- DATED 2021-10-01. / PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTIONS. NO FURTHER ACTION REQUIRED AT THIS TIME. / NOTE: PLEASE REFERENCE CAMPS 23085615 AND 23085616 FOR CORROSION PREVENTION TAPE AND SEALANTS INSTALLATION.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

LEFT SIDE FRAME AT FS565 AND STRINGER 18L IS CORRODED. (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED LEFT SIDE FRAME FS565 FROM SGTR18L TO SGTR7L PER CRJ700 SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CRACKED · airframe 37,344 hrs · 26,739 cycles

WINDSHIELD SUPPORT POST BETWEEN CO- PILOTS LEFT SIDE WINDSHIELD AND FORWARD CO- PILOTS WINDSHIELD IS CRACKED AT TOP NUTPLATE HOLE. (C-CHECK RO 1/13/2022) REMOVED CRACKED CO-PILOT WINDSHIELD SUPPORT POST AND REPLACED WITH NEW WINDSHIELD SUPPORT POST PER CRJ700 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND AMM 56-10-000-801-A01 AND 56-10-05-400-801-A01. REFER TO CONTINUATION CARD FOR REPAIR DISPOSITION AND CORRECTIVE ACTIONS. REFER TO CAMP # 23513606 FOR PRESSURIZATION AND LEAK CHECK COMPLIANCE.

Part: NONE — CRACKED · airframe 37,344 hrs · 26,739 cycles

WINDSHIELD SUPPORT POST BETWEEN PILOTS LEFT SIDE WINDSHIELD AND FORWARD PILOTS WINDSHIELD IS CRACKED AT TOP NUTPLATE HOLE. (C-CHECK RO 1/13/2022) COMPLETED STRUCTURAL MAJOR REPAIR (**RII**) TASK CARD 51-900-1002-SKY MTCM REV: REV DATE:06 OCT 20 . / REMOVED AND REPLACED PILOT SIDE WINDSHIELD SIDE POST P/N 601R33223-1 PER CRJ700 56-10-05-000-801-A01, 56-10-05-400-801-A01, 51-42-21-001-001-A01, 51-42-11-001-001-A01 AND 51-42-06-001-001-A01. REFERENCE CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION. REFER TO CAMP #23513689 FOR PRESSURIZATION AND LEAK CHECK COMPLIANCE.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

LEFT HAND FRAME AT FS549, STR18L CORRODED BEYOND ALLOWABLE DAMAGE. (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED FRAME AT FS549, FROM STR18L TO STR7L PER CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. PRIMED EXPOSED FASTENERS REF CRJ 700 SRM 51-25-06-001-001-A01. REFERENCE CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION. NO FURTHER ACTION REQUUIRED AT THIS TIME.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

FS 319 BTW STR 24 RH TO 26LH, CORROSION FOUND. (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED FRAME AT FS319 FROM STR23R TO STR26L PER CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

ON TOP OF FRAME STATION 310 BTW STR 24 RH TO 24 LH, CORROSION FOUND. (C-CHECK RO 1/13/2022) PERFORMED FRAME REPAIR AT FS310 BETWEEN STR24R TO STR24L PER CRJ700 SRM 53-00-06-201-006-A01. REFERENCE CONTINUATION CARD FOR DISPOSITION AND ALL CORRECTIVE ACTIONS. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

SURFACE CORROSION ON STR26L FROM FS1015 TO FS1047. (C-CHECK RO 1/13/2022) REPAIRED STRINGER STGR26L FROM FS1015 TO FS1047 WITH EXTRUSIONS,SPLICES AND FILLER PER CRJ700 SRM TASK 53-00-03-201-001-A0 PLEASE REFERENCE TO CONTINUATION CARDS FOR DISPOSITION AND CORRECTIVE ACTION. NO DISCREPANCIES NOTED. / NOTE: PLEASE REFERENCE CAMP#23531501 CONTINUATION CARD STEP 15 FOR PRESSURIZATION CHECK .

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

CORROSION ON AFT DOOR LOWER SILL FLANGE (C-CHECK RO 1/13/2022) REMOVED CORRODED AFT CARGO DOOR LOWER SILL AND REPLACED WITH NEW LOWER SILL AT FUSELAGE STATION FS985.00 UP TO FS1051.30 / PER CRJ700 SRM TASKS 53-61-23-001-001-A01, 53-61-23-101-001-A01, 53-61-23-201-001-A01,51-42-06-001-001-A01 AND 51-42-21-001-001-A01. PLEASE REFERENCE CONTINUATION CARD FOR REPAIR DISPOSITION AND CORRECTIVE ACTIONS. NO DEFECTED NOTICED. / NOTE: PLEASE REFERENCE CAMP# 23531501 FOR PRESSURIZATION LEAK CHECKS,PLEASE REFERENCE CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

CORROSION ON STR26R FROM FS1015 TO FS1047 (C-CHECK RO 1/13/2022) REMOVED CORRODED SECTION OF STGR 26R AT FS 1015.00 TO FS 1047.00 AND REPLACED WITH NEW STRINGER SECTION PER CRJ700 SRM53-00-03-201-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REFERENCE CONTINUATION CARD FOR REPAIR DISPOSITIONS AND CORRECTIVE ACTIONS.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

AFT DRAIN MAST INNER CHANNEL AT FS1030 TO FS1047 CORRODED. (C-CHECK RO 1/13/2022) REMOVED THE AFT DRAIN MAST AT FS 1030.00 TO FS 1047.00 STGR 27 TO FACILITATE THE REMOVAL OF CORRODED MAST CHANNEL PER AMMTASK 38-32-12-000-801 (CONFIG A01). / REMOVED CORRODED AFT DRAIN MAST CHANNEL AT FUSELAGE STATION FS 1030.00 TO FS 1047.00 ON STRINGER STGR 27 AND REPLACED WITH NEW CHANNEL PER CRJ700 SRM 53-61-04-001-003-A01 AND 51-42-06-001-001-A01. / PLEASE REFERENCE CONTINUATION CARD FOR REPAIR DISPOSITION AND CORRECTIVE ACTIONS.NO DEFECTS NOTED / NOTE: PLEASE REFERENCE CAMP # 23752490 FOR THE DRAIN MAST INSTALLATION DISPOSITION AND CORRECTIVE ACTIONS. AND CAMP # 23531501 FOR PRESSURERIZATION CHECKS.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

BACK UP SILL AT FS 319.00 STRG 21L HAS CORROSION (C-CHECK RO 1/13/2022) REMOVED CORRODED BACK UP SILL AT FS 319.00 STGR 21L AND REPLACED WITH NEW BACK UP SILL PER CRJ700 SRM 51-42-06-001-001-A01. PRESSURIZATION CHECK WILL BE PERFORM UNDER CAMP.23531501, NO FURTHER ACTION REQUIRED.

Part: NONE — CORRODED · airframe 37,344 hrs · 26,739 cycles

ABOVE FWD CARGO DOOR AT FS549 & STR18LH CORROTION FOUND ON FRAME (C-CHECK RO 1/13/2022) REMOVED CORROSION, ORIGINAL MATERIAL .050, .025" MATERIAL LOSS, REMAINING MATERIAL .025" FOUND TO BE OUT OF LIMITS PER CRJ700 SRM 51-21-06-001-001-A01 AND 53-31-06-002-A01. REFER TO CAMP#23503408 FOR REPAIR OF FRAME ON FS549 AT STR18L.

Part: NONE — CRACKED · airframe 37,344 hrs · 26,739 cycles

CAPTAIN WINDSHIELD IS CRACKED LOCATION OUTBOARD UPPER LEFT HAND CONNER, (C-CHECK RO 1/13/2022) REMOVED AND REPLACED BAY ONE SERVICEABLE WINDSHIELD TASK CARD I.A.W 56-220-1000 SKY REMOVED AMM 56-11-01-000-801 INSTALLATION AMM TASK CARD 56-220-1000 SKY AMM56-11-01-400-801 WINDOW HEAT PER AMM30-41-06-710-801 LEACK CHECK PER AMM 56-11-01-400-801 LEACK OK TORQUE WRENCH USED STS 3818 DUE 16 APR 22

Part: NONE — DENTED · airframe 37,344 hrs · 26,739 cycles

LH OUTBOARD FLAP LOWER SKIN AT FLS 210 HAS DENT (C-CHECK RO 1/13/2022) DENT ON LEFT OUTBOARD FLAP LOWER SKIN AT FLS 210 MEASURED L=10.0",W=4.20", D=.025", FOUND TO BE OUT OF LIMITS PER CRJ700 SRM 57-53-01-101-001-A01. FLAP REPAIRED PER CRJ700 SRM 57-53-01-201-001-A01, REV JUL 25/2019 STEPS 1-4, & 5C(1) -(4) TYPE III. PLEASE REFER TO CONTIUATION CARD FOR DISPOSITION AND CORRECTIVE ACTIONS. NO FURTHER ACTION REQUIRED AT THIS TIME. / DEPTH GAUGE: STS-0283 CAL DUE DATE: 11 MAR 22

Part: NONE — DENTED · airframe 37,344 hrs · 26,739 cycles

FS 608 STR 15R EXTERNAL SKIN HAS DENT/CREASE ON STRINGER (C-CHECK RO 1/13/2022) COMPLETED STRUCTURAL MAJOR REPAIR (**RII**) CARD 51-900-1002-SKY MTCM REV: REV DATE: 06 OCT 20. IN ACCORDANCE WITH REPAIR ENGINEERING ORDER (REO) 670-53-31-716 REVISION-- DATED 2021-09-29. FOR THE EXTERNAL SKIN DENT / CREASE ON FUSELAGE STATION FS608 STRINGER STRG 15R. PLEASE REFERENCE CONTUNIATION CARD FOR DISPOSTION AND CORRECTED ACTIONS. NO DISCREPANCIES NOTED,

Part: NONE — CRACKED · airframe 37,344 hrs · 26,739 cycles

FRAME AT FS333, STGR 1R IS CRACKED AS MARKED. (C-CHECK RO 1/13/2022) REMOVE AND REPLACED FS333 FRAME SECTION FROM STGR -0- TO 9R. IAW DWG # SH670-31950 AND CRJ700 SRM 51-23-00-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. SEE CAMP#23531501 FOR PRESSURAZATION CHECK.

Part: LIGHT — INOPERATIVE (EXIT SIGN)

RIC FLIGHT 5529 DURING SCHEDULED MAINTENANCE INSPECTION THE EMERGENCY EXIT SIGN AT ROW 15 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN BULB WITH OPERATIONAL CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 35,551 hrs · 25,301 cycles

AFT LAVATORY SMOKE WARNING MESSAGE AS AIRCRAFT DESCENDED THRU 9000 FT. THE SYSTEM SELF RESET. THE MESSAGE NO LONGER ACTIVE IAW MCC. NO FURTHER ACTION REQUIRED.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,382 hrs · 24,439 cycles

FS 202.75 FWD SIDE OF BULKHEAD AT RBL 30 & LBL 30 STIFFENERS HAVE AN INDICATION OF 0..25 IN THE UPPER EDGE FLANGE. REPAIRED RBL 30 & LBL 30 STIFFENER IAW SRM 53-11-10-201-005-A01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,382 hrs · 24,439 cycles

FS 220 RT FRAME HAS AN INDICATION OF .5" LONG ON THE FWD FACE 1" BELOW STR 14 JUST ABOVE FASTENER HOLE. FAILED NDT INSPECTION. LOCATED, DRILLED UP AND INSTALLED A NEW SERVICEABLE FS 220 FRAME SECTOR IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 34,382 hrs · 24,439 cycles

WHILE PERFORMING SERVICE BULLETIN 670BA-53-044 FOUND 11 HOLES GOING THROUGH SKIN AND CAP ANGLE TO BE DIAMETER .191" DIAMETER OF HOLE SHOULD BE .160" TO .164" PER SERVICE BULLETIN. COMPLIED WITH REO 670-53-11-1284 DATED 6-01-2017.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 20,410 hrs · 14,072 cycles

DURING C CHECK, FOUND INTERNAL JACKING FITTING, LT INTERCOSTAL CORRODED. REMOVED AND REPLACED THE INTERCOSTAL, DUCT SPLICE & INTERCOSTAL ANGLE IAW EA 30-2017-004 REV .

Part: FRAME — CORRODED (BS 349) · airframe 20,410 hrs · 14,072 cycles

DURING C CHECK, FOUND FRAME BS 349 CORRODED BETWEEN STRINGER 26L & 26R. BLENDED CORROSION AND RESTORED FINISH IAW REO 670-53-21-1308 & EC/TC EO 700-53-10-00002.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND MAIN AVIONICS BAY DOOR CUT OUT INTERNAL SKIN CORRODED. BLENDED CORROSION AND INSTALLED SACRIFICIAL STRIPS IAW REO 670-53-21-242, & EC/TC REO 670-53-21-242

Part: FORMER — CORRODED (FUSELAGE) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND RT FLOOR PAX DOOR FORMER NEAR UPPER END CORRODED. BLENDED CORROSION AND RESTORED FINISH IAW EA 25-2016-334 & EC/TC EA 25-2016-334.

Part: HINGE — GOUGED (PAX DOOR) · airframe 20,410 hrs · 14,072 cycles

DURING C CHECK, FOUND PAX DOOR HINGE GOUGED FROM ANTI-ROTATION PIN (MIGRATED). REMOVED AND REPLACED HINGE IAW SRM 53-21-23-201-001-A01, & 53-21-201-007-A01.

Part: LANDING — CORRODED (FUSELAGE) · airframe 33,748 hrs · 23,937 cycles

DURING COMPLIANCE OF MODSUM IS67053210097, 13EA FASTENER HOLES WERE OVERSIZED INADVERTENTLY ON AVIONICS DOOR LAND, LT SIDE. OPENED UP HOLES AND INSTALLED DOUBLE FLUSH SHALLOW HEAD RIVETS PER EC/TC REO 670-53-21-1375.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,748 hrs · 23,937 cycles

INTERNAL FUSELAGE SKIN CORRODED AT FS 397 BETWEEN STRINGERS 25L-26L. BLENDED CORROSION AND RESTORED FINISH IAW EA 30-2016-373 AND EC/TC EA 30-2016-373.

Part: STRINGER — CORRODED (BS 517-533) · airframe 33,748 hrs · 23,937 cycles

FWD CARGO BAY STRINGER 24L CORRODED BETWEEN BS 517-533. REMOVED CORROSION, AND FOUND OUT OF LIMITS. REPAIRED IAW EA 25-2016-337 & EC/TC EA 25-2016-337.

Part: SEAT TRACK — CORRODED (BS 683-836) · airframe 33,748 hrs · 23,937 cycles

CABIN SEAT TRACK SEGEMENT CORRODED BS 683.5-836.5 LBL9. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801-A03, 53-00-49-400-801-A03, EC/TC REO 670-53-00-343, AND GREO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 683-836) · airframe 33,748 hrs · 23,937 cycles

CABIN SEAT TRACK SEGEMENT CORRODED BS 683.5-836.5, RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, 53-00-49-400-801-A03, EC/TC REO 670-53-00-343, AND GREO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,748 hrs · 23,937 cycles

LT SIDE WALL SEAT RAIL SEGMENT CORRODED AT FS 483.00-572.00 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED LT SIDE WALL SEAT RAIL SEGMENT AT 483.00-572.00 IAW AMM 53-00-49-000-801-A03, EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV M AS WRITTEN.

Part: STRAP — CORRODED (BS 280) · airframe 33,748 hrs · 23,937 cycles

CIRCUMFERENTIAL JOINT STRAP HAS CORRODED AT BS 280 STRINGER 26L-26R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION IAW NDT INSPECTION PROCEEDURE 4.3. PERFORMED EDDY CURRENT INSPECTION IAW NDTM PT 1 51-20-006-250-A01. COMPLIED WITH EC/TC EA 30-2016-371.

Part: FLOOR SUPPORT — CORRODED (BS 476-571) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND LBL 9 SIDE FLOOR SUPPORT SEGMENT FROM BS 476 TO 571.5 CORRODED IN SEVERAL AREAS. REMOVED THE CORROSION. PERFORMED UT THICKNESS INSPECTION. PERFORMED EDDY CURRENT INSPECTION. NO INDICATIONS NOTED. REPAIRED THE FLOOR SUPPORT & COMPLIED WITH REO 670-53-31-397.

Part: SEAT TRACK — CORRODED (BS 517-540) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND SEAT TRACK SEGMENT LBL 9 CORRODED AT BS 517.00 AND 540.00. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A03, REO 670-53-00-343 AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 785-861) · airframe 33,748 hrs · 23,937 cycles

RIGHT SIDE SEAT TRACK CORRODED BS 785 - 861. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-000-801, EC/TC REO 670-53-00-343, GREO 670-53-00-343 REV M AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581-683) · airframe 33,748 hrs · 23,937 cycles

CABIN SEAT TRACK CORRODED BS 581-683.5 LBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343.

Part: STRINGER — CORRODED (BS 335-353) · airframe 33,748 hrs · 23,937 cycles

STRINGER 27R CORRODED FROM BS 335-353.5. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03-101-006-A01. COMPLIED WITH EC/TC REO 670-53-21-1368.

Part: FLOORBEAM — CORRODED (BS 549) · airframe 33,748 hrs · 23,937 cycles

FLOORBEAM CORRODED BS 549, RBL 7.5. BLENDED CORROSION. PERFORMED UT THICKNESS INSPECTION, PERFORMED EDDY CURRENT INSPECTION IAW NDTM PT1 51-20-006-250-A01. NO INDICATIONS NOTED. COMPLIED WITH REO 670-53-13-31-396 AND EC/TC REO 670-53-13-31-396.

Part: SEAT TRACK — CORRODED (BS 581-683) · airframe 33,748 hrs · 23,937 cycles

CABIN SEAT TRACK SEGMENT CORRODED BS 581 - 683.5, RBL 9. THE SEAT TRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-41-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, EC/TC REO 670-53-00-343, GREO 670-53-00-343 REV M AND AMM 53-00-49-400-801-A03.

Part: POST — CORRODED (BS 280) · airframe 33,748 hrs · 23,937 cycles

RIGHT COCKPIT DOOR POST CORRODED BS 280. REMOVED AND REPLACED THE DOOR POST IAW EA 32-2016-275, AND EC/TC EA 32-2016-275.

Part: FLOOR SUPPORT — CORRODED (BS 571-583) · airframe 33,748 hrs · 23,937 cycles

RBL9 SIDE FLOOR SUPPORT SEGMENT CORRODED BETWEEN BS 571.5-583. REMOVED CORROSION , PERFORMED UT THICKNESS INSPECTION. PERFORMED EDDY CURRENT INSPECTION, NO INDICATIONS NOTED. REPAIRED THE FLOOR SUPPORT AND COMPLIED WITH REO670-53-31-393 AND REO 670-53-00-029.

Part: POST — CORRODED (COCKPIT DOOR) · airframe 33,748 hrs · 23,937 cycles

LEFT COCKPIT DOOR POST CORRODED AT BS 280. REMOVED. REPAIRED AND REPLACED THE DOOR POST IAW EA 32-2016-275 AND EC/TC EA 32-2016-275.

Part: FLOOR SUPPORT — CORRODED (BS 476-571) · airframe 33,748 hrs · 23,937 cycles

RBL 9 SIDE FLOOR SUPPORT SEGMENT CORRODED IN SEVERAL AREAS. REMOVED CORROSION, REPAIRED AND INSTALLED THE FLOOR SUPPORT IAW REO670-53-31-393 AND REO 670-53-00-029.

Part: STRINGER — CORRODED (BS 333-349) · airframe 33,748 hrs · 23,937 cycles

STRINGER 26R CORRODED BETWEEN BS 333 - 349. DAMAGE MEASURED OUT OF LIMITS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 990-1005) · airframe 33,748 hrs · 23,937 cycles

SEAT TRACK IS CORRODED AT BS 990 - 1005 RBL 9. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.

Part: FRAME — CORRODED (BS 661) · airframe 33,748 hrs · 23,937 cycles

LOWER FUSELAGE FRAME FWD WING TO FUSELAGE SUPPORT STRUCTURE FRAME IS CORRODED ALONG BOTTOM AROUND SCREW HOLES AT BS 661. BLENDED CORROSION, PERFORMED UT THICKNESS CHECK. COMPLIED WITH EA 30-2016-382.

Part: SEAT TRACK — CORRODED (BS 990-1005) · airframe 33,748 hrs · 23,937 cycles

SEAT TRACK IS CORRODED AT BS 990 - 1005 LBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.

Part: FRAME — CORRODED (BS 629) · airframe 33,748 hrs · 23,937 cycles

LOWER FUSELAGE FRAME FWD WING TO FUSELAGE SUPPORT STRUCTURE FRAME IS CORRODED ALONG BOTTOM AROUND SCREW HOLES AT BS 629. BLENDED CORROSION, PERFORMED UT THICKNESS CHECK, COMPLIED WITH EA 30-2016-383.

Part: FLOOR SUPPORT — CORRODED (BS 394-409) · airframe 33,748 hrs · 23,937 cycles

CORRODED FLOOR SUPPORT BETWEEN BS 394-409 RBL 26. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001, 51-40-11-001-001, AND 53-21-23-001-003-A01.

Part: FLOOR SUPPORT — CORRODED (BS 394-409) · airframe 33,748 hrs · 23,937 cycles

CORRODED FLOOR SUPPORT BETWEEN BS 394 - 409, LBL 26. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001, 51-40-11-001-001, AND 53-21-23-001-003-A01.

Part: FLOOR SUPPORT — CORRODED (BS) · airframe 33,748 hrs · 23,937 cycles

FLOOR SUPPORT CORRODED AT BS 1015 - 1051.30, RBL 9. CUT OUT DAMAGED SECTION AND SPLICED NEW SECTION IAW REO 670-53-61-1312, EC/TC REO 670-53-61-1312, REO 670-53-00-029 AND EC/TC EO 700-53-0388.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,748 hrs · 23,937 cycles

FRAME AT FS613 CORRODED ON BOTH SIDES OF STR 27. BLENDED CORROSION, COMPLIED WITH NDT REQUIREMENTS AND RESTORED FINISH IAW STS EA 432016-109 AND EC/TC EA 43-2016-109.

Part: SEAT TRACK — CORRODED (BS 990-1005) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED AT BS 990-1005, RBL 27. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 & EC/TC REO 670-53-00-343. REMOVED THE SEAT TRACK AND INSTALLED FABRICATED SEAT TRACK IAW AMM 53-00-49-00/400-801-A03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,748 hrs · 23,937 cycles

FLOOR SEAT TRACK IS CORRODED AT FS990-1005 RBL27. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343 AND EC/TC REO 670-53-00-343. REMOVED CORRODED SEAT TRACK AND INSTALL NEW FABRICATED SET TRACK IAW AMM 53-00-49-000/400-801-A03.

Part: BRACKET — BROKEN (BS 847) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND AFT LOWER FUSELAGE FAIRING SUPPORT STRUT LOWER ANGLE BROKEN AT BS 847. REMOVED AND REPLACED AFT LOWER ANGLE FAIRING SUPPORT IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND RT SIDEWALL SEAT TRACK SEGMENT BS 675-713 CORRODED SEVERAL AREAS. REMOVED AND REPLACED IAW AMM 53-00-49-000-801-A03, AND AMM 53-00-49-400-801-A17.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND CARGO FLOO BEAM CORRODED AT LBL 9, BS 1031. REPAIRED THE FLOORBEAM SECTION BY COMPLYING WITH REO 670-53-00-029.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND LT SIDEWALL SEAT TRACK CORRODED AT BS 708 TO 761. REMOVED AND REPLACED THE SEAT IAW AMM 53-00-49-00-810-A03, AND AMM53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 483-572) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND RT SIDEWALL SEAT TRACK SEGMENT FROM BS 483 TO 572 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-00-810-A03, AND AMM53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND LH SIDEWALL SEAT TRACK SEGMENT AT BS 675 TO 713 CORRODED IN SEVERAL PLACES. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-00-810-A03, AND AMM53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 363-483) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND THE LT SIDEWALL SEAT TRACK SEGMENT FROM BS 363 TO 483 CORRODED IN SEVERAL AREAS. REMOVED LT SIDEWALL SEAT RAIL SEGMENT IAW AMM 53-00-49-00-810-A03, COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M, AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND RT SEAT TRACK CORRODED AT BS 708 TO FS761.00. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-00-810-A03, AND AMM53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 572-675) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND LT SIDEWALL SEAT TRACK SEGMENT AT BS 572 TO 675 CORRODED IN SEVERAL PLACES. REMOVED THE SEAT TRACK IAW AMM 53-00-49-00-810-A03, COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M, AND INSTALLED NEW SEAT TRACK IAW AMM53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 832-977) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK FOUND SEAT TRACK CORRODED AT RBL 9, BS 832 TO 977 CORRODED IN SEVERAL PLACES. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-00-810-A03, AND AMM53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 861-969) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND LT SEAT TRACK CORRODED AT BS 861 TO 969. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 572-675) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND RT SIDEWALL SEAT TRACK SEGMENT FROM BS 572 TO 675 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-00-810-A03, AND AMM53-00-49-400-801.DURING C CHECK, FOUND RT SIDEWALL SEAT TRACK SEGMENT FROM BS 572 TO 675 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-00-810-A03, AND AMM53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 832-977) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND FLOOR SEAT TRACK CORRODED AT LBL 9, BS 832 TO 987. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-00-810-A03, AND AMM53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-861) · airframe 33,748 hrs · 23,937 cycles

DURING C CHECK, FOUND RT SEAT TRACK CORRODED AT BS 785 TO 861. REMOVED AND REPLACED THE SEAT RAIL IAW AMM 53-00-49-00-810-A03, AND AMM53-00-49-400-801.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,748 hrs · 23,937 cycles

FWD CARGO COMPARTMENT CORRODED AT BTW FS 517-533 AT STR 23L. BLENDED CORRODED AREA TO A SMOOTH FINISH AND RESTORED FINISH PER EC/TC 26-2016-331.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,748 hrs · 23,937 cycles

FWD CARGO COMPARTMENT CORRODED AT FRAME 661 FWD & AFT SIDES BTW STR 26L-26R. CUT AWAY DAMAGED AREA, SPLICED IN LOCALLY FABBED COMPONENTS PER EC/TC REO 670-53-31-395.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 33,748 hrs · 23,937 cycles

SEAT TRACK SEGMENT CORRODED FROM FS 485-581 ON RBL9. -MTC- CORROSION ON SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,748 hrs · 23,937 cycles

RT SIDE SEAT RAIL CORRODED AT FS 861-969. REMOVED, FABBED AND INSTALLED SEAT RAIL PER EC/TC REO 670-53-00-343.

Part: SKIN — CORRODED (PAX DOOR) · airframe 20,410 hrs · 14,072 cycles

DURING C CHECK, FOUND PAX DOOR INNER SKIN CORRODED AT ACCESS PORT LANDS. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW EA 32-2016-270 P1, AND EC/TC EA 32-2016-270. MAJOR REPAIR.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 32,874 hrs · 23,227 cycles

RIGHT AFT EXTERIOR EMERGENCY LIGHT LENS BROKEN. WORK COMPLETED IAW N/R-00012.

Part: LENS — BROKEN (CABIN) · airframe 32,875 hrs · 23,228 cycles

RIGHT SIDE AFT EMERGENCY EXIT LIGHT LENS BROKEN. LIGHT LENS COVERS, INCLUDING EMERGENCY LIGHT. R & R RT AFT EMERGENCY LIGHT LENS IAW AMM 33-51-15, OPS CHECK GOOD.

Part: GROUND WIRE — LOOSE (EMERGENCY LIGHT) · airframe 31,369 hrs · 22,051 cycles

EMERGENCY SIGN OVER SERVICE DOOR WILL NOT ILLUMINATE. SCREWED LOOSE GROUND TO LIGHT IAW MM 33-51-00, OPS CHECK GOOD.

Part: CONTROL PANEL — FAILED (ADC) · airframe 31,074 hrs · 21,813 cycles

DURING CLIMBOUT AROUND 34,000 FT, SMOKE FROM FIRST OFFICER`S INSTRUMENT PANEL. DIVERTED. R & R NR 2 AIR DATA REFERENCE PANEL IAW AMM 34-13-02. REFER TO IPC 34-13-04, ITEM 5, PERFORMED OPS CHECK IAW AMM 34-13-04-700-801, OPS CHECK GOOD. PERFORMED GENERAL INSPECTION OF CO-PILOT INSTRUMENT PANEL IAW ENGINEERING SL- 21-028, NO DEFECTS FOUND. ACFT GOOD TO RETURN TO SERVICE.

Part: OVERHEAT LOOP — SHORTED (MLG) · airframe 30,876 hrs · 21,645 cycles

MLG OVERHEAT WARNING AFTER TAKE OFF. DECLARED AN EMERGENCY AND COMPLIED WITH QRH AND LANDED AT 66.7K LBS. ACFT RETURNED TO DEPARTURE AFTER T/O. EMERGENCY DECLARED AS A PRECAUTION. UPON FURTHER INSPECTION, FOUND RT ELEMENT TO HAVE LOW RESISTANCE FROM INNER TO OUTER PORTIONS OF ELEMENT. R & R IAW AMM 26-14-04. ALL CHECKS GOOD AT THIS TIME.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,649 hrs · 21,451 cycles

12 AB LOWER SIDEWALL EXIT SIGN HAS 1 LIGHT BULB BURNED OUT. REPLACED THE BULB IN LOWER SIDEWALL EXIT LIGHT IAW AMM 33-51-11, OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,649 hrs · 21,451 cycles

GALLEY LOWER FWD EXIT SIGN HAD ONE BULB BURNED OUT. REPLACED THE BULB IAW AMM 33-51-11. OPS CHECKED GOOD.

Part: GROUND WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 29,479 hrs · 20,530 cycles

EMERGENCY LIGHTS OVER SERVICE DOOR IN GALLEY INOPERATIVE. WHEN TESTED, CABIN EMERGENCY LIGHTS. SECURED GROUND AT GROUND TERMINAL FOR SERVICE DOOR EXIT LIGHT DS52. IAW AMM 33-51-05 , ALL CHECKS GOOD. PLACARD REMOVED, DEFER CLEARED.

Part: SCREW — MISSING (MEGAPHONE) · airframe 29,224 hrs · 20,339 cycles

MEGAPHONE MISSING SCREWS. R & R MEGAPHONE IAW AMM 25-61-14.

Part: INTERCOSTAL — CHAFED · airframe 29,076 hrs · 20,215 cycles

CHAFING WAS DISCOVERED ON PREVIOUS REPAIR AND ON INTERCOSTAL FWD OF REPAIR & INTERCOSTAL 9L BETWEEN FS 1144 AND FS 1154.48. REMOVED DAMAGED REPAIR. COMPLIED WITH REO 670-53-61-1103, REV-. COMPLIED WITH ECTC REO 670-53-61-1103.

Part: STRINGER — CORRODED (BS 349-364) · airframe 29,076 hrs · 20,215 cycles

STRINGER 24R CORRODED BETWEEN FS 349-364. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03-101-006-A01. REPAIRED IAW SRM 53-00-03-201-001-A01.

Part: ANGLE — DAMAGED · airframe 29,076 hrs · 20,215 cycles

RBL 9 LOWER FLANGE HAS A DOUBLE DRILLED HOLE . FREEZE PLUGGED IAW SNIEO S68 ISB 670-30026.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 29,076 hrs · 20,215 cycles

SEVERE CORROSION FOUND AT FS 349, FLOOR SUPPORT RBL 45. REPAIRED IAW EA 15-2014-214 SECTION I .

Part: PANEL — BUCKLED (PAX DOOR) · airframe 29,076 hrs · 20,215 cycles

PAX DOOR FWD AND AFT SIDEWALL PANELS BUCKLED. REMOVED SUPPORT STRUCTURE ON AFT SIDE PANEL. STIFFENER PN 601R317745-7, CRACKED REPLACE WITH NEW. FASTENERS REMOVED IAW SRM 51-42-06-001-001-A01/51-42-10-001-001-A01/51-42-22-001-001-A01. INSTALLED SUPPORT STRUCTURE FOR AFT SIDE PANEL WITH NEW STIFFENER, PN 601R3171457 IAW SRM 51-42-06-001-001-A01- AND DWG 601R31707. REMOVED FWD SIDE PANEL FROM ASD INNER SKIN SRM 51-42-06-001-A01. INSTALLED NEW AFT SIDE PANEL IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND DWG 601R31707. REMOVED SUPPORT STRUCTURE FROM FWD SIDE PANEL IAW SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED SUPPORT STRUCTURE ON FWD SIDE PANEL IAW SRM 51-42-06-001-01-A01,51-42-13-001-001-A01 AND 51-42-21-001-001-A01 AND DWG 601R31707. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH REO 670-52-11-800 REV--.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 29,076 hrs · 20,215 cycles

FOUND CORROSION ON ASD KICKPLATE ANGLE. REMOVED KICKPLATE ANGLE IAW SRM 51-42-06-001-001-A01. DRILLED NR 21 HOLE AT FS 333 AND TRANSFERRED NR 46 PILOT NOT FROM MIDCAP TO KICKPLATE ANGLE 11EA AND 1EA, 21 TO CLIP FITTING. INSTALLED.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 29,076 hrs · 20,215 cycles

AFTER REMOVING FWD DRAG ANGLE ON PAX DOOR FOUND PREVIOUSLY OVERSIZED HOLE AROUND PANEL 832DL, CUTOUT. REPAIRED IAW REO 670-52-11-800, REV--, REO 670-52-11-806 REV--, AND EC/TC REO 670-52-11-800 .

Part: ANGLE — CORRODED · airframe 29,076 hrs · 20,215 cycles

SERVICE DOOR LOWER MOUNTING ANGLE CORRODED AND IS OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED MOUNTING ANGLE IAW SRM 51-42-21-001-001-A01 AND 51-40-06-001-001-A01. INSTALLED MOUNTING ANGLE IAW SRM 51-42-21-801-001-A01 AND 51-40-06-001-01-A01 AND DWG SH 670-31996.

Part: FRAME — CORRODED (BS 319) · airframe 29,076 hrs · 20,215 cycles

FRAME BS 319 HAS CORROSION BETWEEN STRINGER 25-27R. REMOVED CORROSION IAW SRM 53-21-06-101-002-A01.

Part: STRINGER — CORRODED (BS 310-333) · airframe 29,076 hrs · 20,215 cycles

STRINGER 25R HAS CORROSION BETWEEN 310 TO 333. REMOVED CORROSION AND FOUND DAMAGE 3TO BE BEYOND LIMITS, CORROSION IS THROUGH STR 25R IAW SRM 53-21-03-101-002-A01, 51-24-06-001-001-A01. R & R STRINGER 25R FS280-349 IAW SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 29,076 hrs · 20,215 cycles

LT LOWER BS 280 BULKHEAD WEB CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRED IAW REO 670-53-11-594.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 29,076 hrs · 20,215 cycles

INTERCOSTAL HAS CORROSION AT BS 364. REMOVED CORROSION IAW SRM 5121-06-001-001-A01.

Part: FRAME — CORRODED (BS 295) · airframe 29,076 hrs · 20,215 cycles

FRAME BS 295 HAS CORROSION BETWEEN STRINGERS 25L-25R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND 53-21-06-101-002-A01. COMPLIED WITH GREO 690-53-21-799.

Part: STRAP — CORRODED (BS 280) · airframe 29,076 hrs · 20,215 cycles

BELLY FS 280, STRAP HAS CORROSION BETWEEN STRINGERS 26L-26R. REMOVED CORROSION IAW SRM 57-21-06-001-001-A01.

Part: STRINGER — CORRODED (BS 333-349) · airframe 29,076 hrs · 20,215 cycles

STRINGER 25R HAS CORROSION BETWEEN BS 333 TO 349. REMOVED CORROSION AND FOUND DAMAGE IS BEYOND LIMITS, CORROISON IS COMPLETELY THROUGH DTGR 25T IAW SRM 53-21-03-101-006-A01, 51-21-06-001-001-A01. REPLACED STR 25R SPLICE BETWEEN FS 333-FS349. REMOVED STR25R BETWEEN FS 333 364 IAW SRM 51-42-20-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,076 hrs · 20,215 cycles

AVIONICS BAY FLOORBEAM HAS CORROSION AT BS 280. R & R FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01, 51-40-11-001-0001-A01, 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (BS 333-349) · airframe 29,076 hrs · 20,215 cycles

STRINGER 26R HAS CORROSION BETWEEN FS 333 TO 349. REMOVE CORROISON IAW SRM 53-21-03-101-002-A01. REMOVED CORROSION IAW SRM 53-21-23-101-003-A01 AND SRM 51-1-23-101-003-A01 AND SRM 51-21-06-001-001-A01. BLENDED AREA IS OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED CORROSION FROM STR 26R BETWEEN FS 333-349 IAW SRM 51-21-06-001-001-A01, 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 295-333) · airframe 29,076 hrs · 20,215 cycles

STRINGER 26R HAS CORROSION BETWEEN FRAMES 295 TO 333. REMOVED CORROSION BETWEEN FRAMES 295-333 ON STR 26R IAW SRM 53-21-03-101-002-A01, 51-21-06-001-001-A01. BLENDED AREAS ARE OUT OF ALLOWABLE LIMITS IAW SRM 53-21-06-101-002-A01. INSTALLED STRINGER TO ORGINAL CONFIGURATION IAW SRM 51-42-06-001-001-A01 REF DWG SH670-31634.

Part: TRACK — BENT (CARGO DOOR) · airframe 29,074 hrs · 20,214 cycles

FWD/AFT, AFT CARGO DOOR, DOOR TRACKS HAVE IMPACT DAMAGE, BENT, PREVENTING DOOR FROM OPERATING SMOOTHLY OPEN, AS MARKED. RECEIVED FINAL EA 32-2014-177 AND EA 32-2014-167. RESHAPED AND CONTOURED IAW ENGINEERING REQUEST AND BLENDED GOUGES AND DENTS IAW SRM 51-12-001-001-A01. RECEIVED EA 32-2014-177 AND EA 32-2014-167. COMPLIED WITH STS EA 32-2014-167. COMPLIED WITH STEP 1E OF EA 32-2014-177. PERMANENT REPAIR.

Part: HINGE — GOUGED (PAX DOOR) · airframe 29,076 hrs · 20,215 cycles

FUSELAGE SIDE PAX DOOR HINGE, AFT LUG, QOUGED BY ROLL PIN. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH ECTC GREO 670-53-21-582 AND TYPE I DISPOSIITION REO 670-53-21-582. ECTC COMPLIED WITH REPAIRED PASSENGER DOOR HINGE, FUSELAGE SIDE IAW REO 670-53-21-582, REV B. COMPLIED WITH REO 670-53-21-1141. COMPLIED WITH ECTC REO 670-53-21-1141 AND VERIFIED ALL STEPS OF REO 670-53-21-1141 WERE COMPLETED. MAJOR REPAIR.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 29,076 hrs · 20,215 cycles

RT LOWER BS 280 BULKHEAD WEB CORRODED. FOUND IT TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRED IAW EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594 REV-.

Part: DOUBLER — CORRODED (BS 295-310) · airframe 29,076 hrs · 20,215 cycles

ANTENNA DOUBLER HAS CORROSION IN AVIONICS BAY BETWEEN BS 295 - 310. REPLACED TCAS DOUBLER WITH SERIVCEABLE TCAS DOUBLER IAW SRM 51-4-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW TCAS DOUBLER IAW SRM 51-40-11-001-001-A01.

Part: STRUCTURE — CORRODED (BS 349) · airframe 29,074 hrs · 20,214 cycles

PACKER CORRODED RBL9 APPROXIMATELY FS 349. R & R PACKER IAW DWG SH670-32120, SRM 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED · airframe 29,074 hrs · 20,214 cycles

RBL 45 SILL CORRODED FS 285 AND APP FS 300-319. REMOVED CORROSION ON RT FLOOR SILL STA 285-319 IAW SRM 51-21-06-001-001-A01. CORROSION OUT OF LIMITS BY VISUAL INSP EXFOLIATION THROUGH PART. REMOVED FS 280-FS 477.40 FLOOR SILL STRUCTURE RT AND BEGAN DRILLING UP NEW FLOOR SILL REF SRM 51-42-06-001-001-A01 & 51-40-11-001-001-A01 AND DWG SH 620-32170, REV T. INSTALLED FLOOR SILL REF DWG SH670-32170, REV T AND SRM, SRM 53-21-45-001-001-A01.

Part: STRUCTURE — CORRODED (BS 333) · airframe 29,074 hrs · 20,214 cycles

PACKER CORRODED LBL9 APPROXIMATELY FS 333. R & R PACKER IAW DWG SH670-32120, SRM 51-42-06-001-001-A01. SDR CLOSED.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 29,074 hrs · 20,214 cycles

FLOOR SUPPORT CORRODED RBL45 AT FS 349 AND SMALL AREA AT APPROXIMATELY FS 385. COMPLIED WITH GREO 670-53-00-390. COMPLIED WITH ECTC REO 670-53-00-370 AND REO 670-53-00-390, REV -- DATED 01/22/2014.

Part: DOOR SILL — CORRODED · airframe 29,074 hrs · 20,214 cycles

ASD SILL ANGLE CORRODED. AFTER EVALUATION OF MIDCAP ANGLE DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED MIDCAP ANGLE IAW SRM 51-42-06-001-001-A01. DRILLED 11 PILOT HOLES IN MIDCAP ANGLE WITH NR 40 DRILL BIT IAW SRM 51-40-11-001-001-A01. DRILLED REMAINING HOLES ON SILL ANGLE INSTALLED NUTPLATES ON ANGLE REF DWG SH670-31825 AND SRM 51-45-00-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 349-385) · airframe 29,074 hrs · 20,214 cycles

FS 349-485, RBL9 SEAT TRACK CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03. RECEIVED AND COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV G AS WRITTEN. LOCATED AND DRILLED NEW SEAT RAIL IAW SRM 61-40-11-001-001-A01.

Part: RETAINER — BENT (CARGO DOOR SEAL) · airframe 27,802 hrs · 19,241 cycles

SEAL RETAINER FWD CARGO DOOR BENT. COMPLIED WITH EC/TC REO 670-52-35-127. MAJOR REPAIR IAW GMM 5-3.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,926 hrs · 18,627 cycles

CAPTAIN'S FLASHLIGHT INOPERATIVE. REPAIRED FLASHLIGHT IAW GMM 3-8. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: SEAL — DIRTY (SERVICE DOOR) · airframe 25,421 hrs · 17,537 cycles

SERVICE DOOR DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBED DR SEAL OPS CKED GOOD IAW AMM 52-41-02.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 24,939 hrs · 17,193 cycles

AFT F/A'S FLASHLIGHT INOPERATIVE. R & R BATTERIES IAW AMM 25-61-02. OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: ANGLE — CORRODED (PAX DOOR HINGE) · airframe 24,727 hrs · 17,039 cycles

ANGLES AT HINGE SIDE OF PAX DOOR. R & R IAW SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,727 hrs · 17,039 cycles

COCKPIT FLOORBEAM AT FS 280 IS CORRODED. REMOVED ANGLE IAW SRM 51-42-21. FABRICATED NEW FLOORBEAM BY MATCH DRILLING TO EXISTING FASTENER HOLES IN ACFT AND OLD ANGLE. INSTALLED IAW SRM 51-42-21, 51-42-06 AND 51-42-13.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 24,727 hrs · 17,039 cycles

LEFT SIDE FS 280 LOWER BULKHEAD WEB HAS CORROSION DAMAGE. REPAIRED IAW REO 670-53-11-594.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 24,705 hrs · 17,021 cycles

FWD EQUIPMENT COMPARTMENT FLOOR CRACKED. COMPLIED REO 670-523-11-509.

Part: DOUBLER — CORRODED (BS 295-310) · airframe 24,727 hrs · 17,039 cycles

TCAS DOUBLER CORRODED UNDER FLOOR AT STRINGER 27 BETWEEN FRAMES BS 295 AND 310. REMOVED TCAS DOUBLER IAW SRM 51-42-06 BECAUSE DOUBLER WAS CORRODED OUT OF LIMITS IAW SRM 53-21-01. INSTALLED NEW TCAS DOUBLER BETWEEN FRAME 295 AND 310 IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 310) · airframe 24,727 hrs · 17,039 cycles

FRAME BS 310 CORRODED AT STRINGER 27 FWD & AFT SIDES. BLENDED CORRODED AREA IAW SRM 51-42-06. BLENDED CORRODED AREA IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-21-907.

Part: ATTACH BRACKET — CRACKED (VERTICAL TO FUSE) · airframe 24,727 hrs · 17,039 cycles

VERTICAL STAB TO FUSELAGE LT CHANNEL BRACKET CRACKED ABOVE APU DOOR. REPAIRED IAW REO 670-55-31-062.

Part: FRAME — CORRODED (BS 295) · airframe 24,727 hrs · 17,039 cycles

FRAME BS 295 CORRODED BETWEEN STGR 26R AND STGR26L. BLENDED FRAME IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-21-908.

Part: STRINGER — CORRODED (BS 333-349) · airframe 24,727 hrs · 17,039 cycles

STRINGER 27 CORRODED BETWEEN FRAMES 333 AND 349. COMPLETED REPAIR IAW REO 670-53-21-261.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,705 hrs · 17,021 cycles

FWD FLOORBEAM ANGLE CORRODED. R & R FLOORBEAM ANGLE BS 280 IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 1050-1031) · airframe 24,705 hrs · 17,021 cycles

RT SIDE FLOOR SUPPORT HAS CORROSION DAMAGE AT APPROX FS 1050.00 AROUND NUTPLATE. FOUND THAT THE CORROSION EXTEND FWD TO FS 1031.00. RECEIVED AND COMPLIED WITH REO 670-53-61-921.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 24,705 hrs · 17,021 cycles

RT SIDE FS 280 CROSSBEAM HAS CORROSION DAMAGE. RECEIVED AND COMPLIED WITH EC/TC REO 670-53-11-047 AND REO 670-53-11-047, REV E DATED 8/13/09. REPAIR CLASSIFIED AS MAJOR.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 24,727 hrs · 17,039 cycles

LEFT SIDE FS 280 CROSSBEAM HAS CORROSION DAMAGE. FS 280 CROSSBEAM R & R IAW REO 670-53-11-047.

Part: BULKHEAD — CORRODED · airframe 24,705 hrs · 17,021 cycles

RT SIDE FS 280 LOWER BULKHEAD WEB HAS CORROSION DAMAGE. RECEIVED AND COMPLIED WITH EC/TC REO 670-53-11-594 AND GENERIC REO 670-53-11-594 REV-DATED 04/27/2011.

Part: FLOOR SUPPORT — CORRODED (BS 1051-1061) · airframe 24,705 hrs · 17,021 cycles

RT SIDE FLOOR SUPPORT HAS CORROSION DAMAGE AT FS 1051.30. CORROSION WAS FOUND TO EXTEND AFT FROM FS 1051.3 TO APPROX 1061.00. COMPLIED WITH REO 670-53-61-921.

Part: SKIN — CRACKED (PAX DOOR) · airframe 24,074 hrs · 16,546 cycles

FWD REPAIR ON PAX DOOR, UPPER CORNER, CRACKED. WORK COMPLETED IAW N/R, ITEM: 1. UPON FURTHER INVESTAGATION, FOUND PREVIOUS REPAIR REO 601R-52-11-279. REPAIR DOUBLER CRACKED ONLY. R & R WITH NEW DOUBLER. REF REO 601R-52-11-279.

Part: SKIN — CRACKED (PAX DOOR) · airframe 24,074 hrs · 16,546 cycles

AFT REPAIR ON PAX DOOR, UPPER CORNER, CRACKED. WORK COMPLETED IAW N/R -00004. UPON FURTHER INVESTAGATION FOUND PREVIOUS REPAIR REO 601R-52-11-279 REPAIR DOUBLER CRACKED ONLY. R & R WITH NEW DOUBLER IAW REO 601R-52-11-279.

Part: LANDING GEAR — NONE (RIGHT) · airframe 23,406 hrs · 16,075 cycles

GEAR DISAGREE AFTER SELECTING UP. RT MAIN GEAR SHOWED NOT RETRACTED. ACFT RETURNED TO DEPARTURE AND AN EMERGENCY DECLARED. PERFORMED FUNCTIONAL TEST OF LANDING-GEAR EXTENSION/RETRACTION SYS IAW AMM 32-30-00. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: FLASHLIGHT — UNSERVICEABLE (CABIN) · airframe 23,083 hrs · 15,845 cycles

FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-60-00. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED, ACFT OK FOR SERVICE.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 21,347 hrs · 14,662 cycles

AFT CABIN MEGAPHONE INOPERATIVE AND DENTED. R & R AFT CABIN MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHT) · airframe 19,894 hrs · 13,648 cycles

NR 4 EMERGENCY BATTERY WEAK. REPLACED THE EMERGENCY BATTERY PACK NR 4 AND PERFORMED OPS CHECK GOOD REF AMM TASK 33-51-04-400-801, 33-51-04-000-801 AND 33-51-06-740-801.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 19,894 hrs · 13,648 cycles

3L STRINGER CRACKED AT FS280 AFT OF BULKHEAD. COMPLY WITH STEPS 5-11 OF REO670-53-21-493. COMPLIED WITH STEPS 5-10 OF REO 670-53-21-493. COMPLIED WITH STEP 11 OF REO 670-53-21-493 IAW DEVIATION REO 670-53-21-618.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,894 hrs · 13,648 cycles

CONTINUED FROM MWC 7107425/100, TOP PLATE ON FLOORBEAM AT RBL9.0 FS 485 TO 581 HAS SEVERAL SPOTS OF CORROSION. REPAIRED IAW REO 670-31-184.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,894 hrs · 13,648 cycles

UPON REMOVAL OF RT 280 CROSSBEAM FOUND RT LOWER WEB TO BE CORRODED BEYOND REPAIRABLE LIMITS. REMOVED WEB IAW SRM 51-42-06-001-001-A01. INSTALLED WEB IAW SRM 53-11-10-99-805.

Part: WEB — CORRODED (BS 280) · airframe 19,894 hrs · 13,648 cycles

LEFT 280 WEB CORRODED AT LBL 9-15. BLENDED CORROSION DAMAGE IAW SRM 53-11-10-201-003-A01. AREA WITHIN LIMITS. RESTORED FINISH PER SRM 51-12-00-001-001-A01

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 19,894 hrs · 13,648 cycles

SEAT TRACK HAS CORROSION ON OUTSIDE OF TRACK FROM FS 349 TO 485, RBL 9.00. REMOVED SEAT TRACK, SEAT TRACK OUT OF LIMITS. IAW SRM 53-21-49-101-001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 855-977) · airframe 19,894 hrs · 13,648 cycles

RT CTR FLOOR SEAT TRACK CORRODED AT ROW 15-16. REMOVED SEAT TRACK AT FS 855-977 RBL 27 IAW AMM 53-00-49-000-801, REMOVED CORROSION FROM SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 52-51-49-101-001. INSTALL NEW SEAT TRACK INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 713-763) · airframe 19,894 hrs · 13,648 cycles

SEAT TRACK IS CORRODED ON LT SIDE WALL AT SEAT ATTACH POINT AT FS 713.00 TO FS 763.00. REMOVED SIDE SEAT TRACK IAW AMM 53-00-49-000-801, INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 861-985) · airframe 19,894 hrs · 13,648 cycles

SEAT TRACK IS CORRODED ON RT SIDE WALL AT SEAT ATTACH POINTS AT FS 861.00 TO FS 985.00. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 669-675) · airframe 19,894 hrs · 13,648 cycles

SEAT TRACK IS CORRODED ON LT SIDE WALL AT SEAT ATTACH POINT FROM FS 669.00 TO FS 675.00. REMOVED LEFT SIDEWALL SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT RAIL IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 784-861) · airframe 19,894 hrs · 13,648 cycles

SEAT TRACK IS CORRODED ON RT SIDE WALL AT SEAT ATTACH POINTS AT FS 784.00 TO FS 861.00. REMOVED RIGHT SIDE WALL SEAT TRACK IAW MLM 53-00-49-000-801. INSTALLED NEW SEAT RAIL IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 19,894 hrs · 13,648 cycles

SEAT TRACK IS CORRODED ON LT SIDE WALL FROM FS 675.00 TO FS 713.00. 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 669.4-675) · airframe 19,894 hrs · 13,648 cycles

SEAT TRACK IS CORRODED ON RT SIDE WALL AT SEAT ATTACH POINTS AT FS 669.40 TO FS 675.00. REMOVED RIGHT SIDEWALL SEAT IAW AMM TASK 53-00-49-000-801. INSTALLED SERVICABLE SIDEWALL SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 861-985) · airframe 19,894 hrs · 13,648 cycles

SEAT TRACK IS CORRODED ON LT SIDE WALL SEAT ATTACH POINTS AT FS 861.00 TO FS 985.00. 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 713-763) · airframe 19,894 hrs · 13,648 cycles

SEAT TRACK IS CORRODED ON RT SIDE WALL SEAT ATTACH POINT AT FS 713.00 TO FS 763.00. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801, RP161783 11/4/10. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-41-51-101-001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 784-861) · airframe 19,894 hrs · 13,648 cycles

SEAT TRACK IS CORRODED ON LT SIDE WALL AT SEAT ATTACH POINTS AT FS 784.00 TO FS 861.00. REMOVED LEFT SIDE WALL SEAT TRACK, FOUND PART TO BE OUT OF LIMITS. IAW SRM 53-21-49-991-804. INSTALLED NEW SEAT TRACK. IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 19,894 hrs · 13,648 cycles

SEAT TRACK IS CORRODED ON RT SIDE WALL SEAT ATTACH POINTS AT FS 675.00 TO FS 713.00. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK SECTION IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 19,894 hrs · 13,648 cycles

SEAT TRACK HAS CORROSION ON INSIDE & OUTSIDE OF TRACK FROM FS 379 TO FS 485, LBL 9.00. REMOVED SEAT TRACK AND FOUND OUT OF LIMITS IAW AMM 53-31-49-210-801-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,894 hrs · 13,648 cycles

RT CTR FLOOR SEAT TRACK CORRODED AT SEAT LOCATIONS 3,4, AND 5. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. EVALUATED DAMAGE AND FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REPLACED SEAT TRACK IAW AMM 53-0049-400-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,894 hrs · 13,648 cycles

LEFT CENTER SEAT TRACK CORRODED BETWEEN SEAT LOCATIONS 6 THRU 9 RT. REMOVED SEAT TRACK IAW AMM 3-00-49-000-801. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM-53-31-49-101-001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,894 hrs · 13,648 cycles

RT CTR FLOOR SEAT TRACK CORRODED BETWEEN SEAT LOCATIONS 6 THRU 9 RT. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. SEAT TRACK IS OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: STRINGER — CRACKED (BS 280 S3L) · airframe 19,894 hrs · 13,648 cycles

3L STRINGER CRACKED AT FS 280 AFT OF BULKHEAD. PERFORMED EDDY CURRENT INSPECTION IAW MAC NDT INSPECTION PROCEDURE ET-2. CRACK EXTENDING TO BUT NOT PAST THIRD FASTENER. REMOVED DAMAGED SECTION AND CLEANED EDGES IAW STEPS 1 & 2 OF REO 670-53-21-493. COMPLIED WITH STEP 3 OF REO 670-53-21-493 NO INDICATIONS NOTED.

Part: STRINGER — CORRODED (STR 26) · airframe 19,894 hrs · 13,648 cycles

LOOKING FWD FROM AVIONICS BAY STR 26, RT HAS CORROSION IN SEVERAL PLACES GOING FWD (MARKED) AVIONICS BAY . REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. FABRICATED NEW STRINGER IAW REO 670-53-21-262. REPLACED STRINGER IAW REO 670-53-21-262 AND SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-20-001-001-A01.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 19,894 hrs · 13,648 cycles

FS 280.00 CROSSBEAM CORRODED FWD OF LT AND RT DRIP TRAYS. REMOVED CROSSBEAM IAW SRM 51-42-06-001-001-A01. DRILLED & DEBURRED NEW CROSSBEAM IAW SRM 51-42-06-001-001-A01.

Part: PLACARD — DAMAGED (CABIN) · airframe 19,894 hrs · 13,648 cycles

CREW ESCAPE HATCH EXTERNAL PLACARD "EMERGENCY EXIT HANDLE INSTRUCTIONS" AND OPEN TO CLOSE ARROW MISSING PIECES, AND UNREADABLE. APPLIED "EMERGENCY EXIT HANDLE INSTRUCTIONS" SILKSCREEN PRINT IAW AMM 20-60-11-000-801.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 19,790 hrs · 13,580 cycles

DURING CLIMB, CAPT SIDE WINDSHIELD CRACKED RETURN TO DEPARTURE, ACFT DID NOT EXCEED STRUCTURAL LANDING WEIGHT. (ACFT RETURNED TO DEPARTURE AFTER T/O -- SPARKS OBSERVED) R & R WINDSHIELD IAW AMM 56-11-01. OP'S AND PRESSURIZATION CHECKS STILL NEEDED, NO FURTHER DEFECTS FOUND AT THIS TIME.

Part: FITTING — CRACKED (BULKHEAD) · airframe 18,914 hrs · 12,933 cycles

WHILE PERFORMING THE EDDY CURRENT OF THE RT BULKHEAD BATHTUB FITTING RECEIVED A RELAVANT CRACK INDICATION AROUND THE RETURN LINE OPENING. FINISHED DRILLING AND FINAL SIZED ALL FASTENER HOLES. APPLIED PRIMER & WET INSTALLED NEW FITTING. ABOVE WORK DONE REF SRM 51-42-21 AND REO PL670-53-61-034. REMOVED CRACKED BULKHEAD BATHTUB FITTING REF SRM 51-42-21. COMPLIED WITH EDDY CURRENT INSP OF ORIGINAL CUTLINE ON RT SIDE AFT PRESSURE BULKHEAD AT FS 1098 IAW NDTM 51-20-006, PART 1. NO DEFECTS NOTED AT THIS TIME. TRIMMED NEW FITTING, DRILLED NEW HOLES FOR HYD LINES & STARTED DRILLING NEW FASTENERS HOLES IAW SRM 51-40-00 AND REO 670-53-61-034. WORK DONE REF SRM 51-42-21 AND REO PL670-53-61-034.

Part: ANGLE — CRACKED (BS 1108) · airframe 18,914 hrs · 12,933 cycles

CRACKED ANGLE ON FS 1108 RT (AT LIGHTNING HOLE IN FRAME) REMOVED CRACKED STANDOFF BRACKETT ANGLE PN MM670-75271-001 IAW SRM 51-42-06. NEW PART ON ORDER. INSTALLED NEW BRACKET MM670-75271- IAW SRM 51-42-21. J

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,666 hrs · 12,754 cycles

LEFT EMERGENCY EXIT ROW SMALL EXIT SIGN HAS MULTIPLE LIGHTS OUT. (RESOLVED ON W/O: 154974 TASKCARD: N/R-00007) RELAMPED LT EMERGENCY EXIT ROW SMALL EXIT SIGN IAW SRM 33-51-11. OPS CHK GOOD. ITEM: 1, RELAMPED LT EMERGENCY EXIT ROW SMALL EXIT SIGN IAW SRM 33-51-11. OPS CHK GOOD. (CLOSED)

Part: LAMP — INOPERATIVE (CABIN) · airframe 18,117 hrs · 12,348 cycles

CABIN NR 5 CEILING EMERGENCY LIGHT INOP. RELAMPED CABIN NR 5 CEILING EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD. ITEM: 1 02-06-2010 RELAMPED CABIN NR 5 CEILING EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,969 hrs · 10,736 cycles

EMERGENCY CEILING LIGHT 5TH FROM FRONT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,531 hrs · 10,395 cycles

FOUND EMERGENCY LIGHTS IN AFT CABIN INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,531 hrs · 10,395 cycles

FOUND EMERGENCY LIGHTS IN CABIN NEXT TO EMERGENCY EXIT INOP.

Part: PLACARD — MISSING (CABIN) · airframe 15,030 hrs · 10,029 cycles

FLT 5311 - EXIT PLACARD MISSING ON PAX ENTRY DOOR.

Part: MOUNT BRACKET — CRACKED (AFT EQUIP BAY) · airframe 14,900 hrs · 9,932 cycles

LT HYD SHUT OFF VALVE MOUNTING BRACKET CRACKED (AFT EQUIP BAY).

Part: MOUNT BRACKET — CRACKED (LT ENGINE) · airframe 14,900 hrs · 9,932 cycles

LT ENG SHUT-OFF VALVE MOUNTING BRACKET CLIP CRACKED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 14,900 hrs · 9,932 cycles

MAIN AVIONICS BAY FLOORBEAM ATTACHED TO AFT SIDE OF FS 280 FRAME HAS CORROSION DAMAGE (MARKED). REMOVED AND BLENDED AVIONICS BAY FLOORBEAM. BLENDED OUT OF LIMITS PER SRM 51-21-06. TRANSFERRED HOLES FROM OLD ANGLE TO TEMPLET AND FROM TEMPLET TO NEW SUPPORT ANGLE IAW SRM 51-40-11.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 14,900 hrs · 9,932 cycles

MAIN AVIONICS BAY FLOORBOARD SUPPORT ANGLE ATTACHED TO AFT SIDE OF FS 280 FRAME HAS CORROSION DAMAGE (MARKED). REMOVED AND BLENDED AVIONICS BAY FLOORBEAM ANGLE. BLENDED OUT OF LIMITS PER SRM 51-21-06. TRANSFERRED HOLES FROM OLD ANGLE TO TEMPLET AND FROM TEMPLET TO NEW SUPPORT ANGLE IAW SRM 51-40-11. RIVETED NEW ANGLE IN PLACE USING SOLID RIVETS AND LOCK FASTENERS IAW SRM 51-42-06 AND 51-42-20.

Part: WEB — CORRODED (FUSELAGE) · airframe 14,900 hrs · 9,932 cycles

LT 280 WEB HAS MINOR CORROSION DAMAGE. BLENDED OUT MINOR CORROSION ON LT FS 280 WEB. DAMAGE IS FOUND TO BE WITH IN LIMITS IAW SRM 53-11-00. MAT'L REMOVED .003 IN OUT OF .005 IN MAX ALLOWED. RESTORED A044 FINISH. RESTORED A023 FINISH ON REWORKED AREA IAW SRM 51-21-16. REINSTALLED ALL FASTENERS IN REWORKED AREA AT LT 280 WEB IAW SRM 51-42-06 BM7024222 JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 14,900 hrs · 9,932 cycles

RIGHT WALL SEAT TRACK SECOND SEGMENT FROM FRONT OF AIRCRAFT HAS CORROSION AS MARKED. REMOVED AND REPLACED RIGHT SIDE WALL SEAT TRACK IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 14,900 hrs · 9,932 cycles

ALL CABIN FLOOR SEAT TRACKS HAVE CORROSION AS MARKED. R & R SEAT TRACK AS PER MM 53-00-49. BLENDED AREA FOUND TO BE OUT OF LIMITS PER SRM 53-51-49.

Part: TRUNNION PIN — CORRODED (RT MLG) · airframe 14,900 hrs · 9,932 cycles

RT MLG SHOCK STRUT UPPER (FWD) ATTACHMENT TRUNNION PIN SHOWS SIGN OF CORROSION. AFTER FURTHER INSPECTION FOUND RESIDUE TO BE DRIED CORROSION INHIBITING COMPOUND. REMOVED BOLT, CLEANED AREA AND REINSTALLED BOLT WITH CORROSION INHIBITING COMPOUND PER AMM 32-00-05. RII SATISFACTORY FOR THE INSTALLATION OF THE FWD TRUNNION PIN ATTACH BOLT PER CRJ 700 AMM 32-11-05 AND SP 607.

Part: FITTING — CRACKED (FUSELAGE) · airframe 14,900 hrs · 9,932 cycles

DURING REMOVAL OF AFT CARGO DOOR COMING, FOUND CRACKED CLIP ON FWD LOWER EDGE, P/N MM670-35699-013.

Part: TRUNNION PIN — CORRODED (LT MLG) · airframe 14,900 hrs · 9,932 cycles

LT MLG SHOCK STRUT UPPER (FWD) ATTACHMENT TRUNNION PIN SHOWS SIGN OF CORROSION. AFTER FURTHER INSPECTION FOUND RESIDUE TO BE DRIED CORROSION INHIBITING COMPOUND. REMOVED BOLT, CLEANED AREA AND REINSTALLED BOLT WITH CORROSION INHIBITING COMPOUND PER AMM 32-00-05. RII SATISFACTORY FOR THE INSTALLATION OF THE FWD TRUNNION PIN ATTACH BOLT PER AMM 32-11-05 AND SP 607.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 14,900 hrs · 9,932 cycles

FLIGHT COMPT FLOORBOARD AFT SUPPORT ANGLE HAS CORROSION DAMAGE. REMOVED AND REPLACED AFT SUPPORT ANGLE AT FLIGHT COMPT FLOORBOARD. STARTED DRILLING UP NEW FWD COCKPIT FLOORBOARD LAND ALL HOLES AT PILOT SIZE DRILL UP NEW FWD FLOOR SUPPORT ANGLE EXCEPT CAM-LOCK FASTENER HOLES. FWD FLOOR SUPPORT ANGLE IS READY TO BE INSTALLED IAW SRM 51-40-11. INSTALLED FWD SUPPORT ANGLE EXCEPT FOR CAM-LOCKS, ALL WORK DONE IAW 51-42-06. INSTALLED GEA CAM-LOCKS AT FWD FLOOR SUPPORT ANGLE IAW SRM-51-42-06.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,900 hrs · 9,932 cycles

RT FS 280 BEAM HAS CORROSION DAMAGE. R&R BEAM PER SRM 51-42-06. REINSTALLED RT DRIP TRAY IAW SRM 51-42-13 SB 670BA-53-026. REINSTALLED INTERCOSTALS IAW SRM 51-42-21. REINSTALLED PITOT STATIC LINE THRU BEAM IAW AMM 34-11-02. REPLACED WITH NEW T-BRACKET. REINSTALLED CABLE GUIDE IAW AMM 20-21-00. REINSTALLED PULLEY BRACKET IAW AM 20-21-00. DRILLED BEAM PER SRM 51-40-11. WORK DONE IAW SRM 51-24-16. PERFORMED EDDY CURRENT INSPECTION OF U-BRACKET AND BEAM CUT LINE IAW REO 670 -53-11-047 PER NDTM 51-20-006. NO DEFECTS NOTED. INSTALLED NEW CROSSBEAM.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 14,900 hrs · 9,932 cycles

RT VERTICAL STAB DRAG ANGLE CRACKED. COMPLIED WITH REO 670-55-31-018. REMOVED FASTENERS AND CUT AWAY DAMAGED AREA IAW REO. RT SIDE FWD DRAG ANGLE, PER REO 670-55-31-018. PERFORMED EDDY CURRENT INSPECTION IAW NDTM 51-20-006. NO DEFECTS NOTED. FABRICATED DOUBLER AND FILLER IAW REO 670-55-31-018. COUNTERSUNK TO MATCH FASTENER IN REO 670-55-31-018 PER SRM 51-40-11. COMPLIED WITH REO 670-55-31-018. PAINTED RT VERTICAL STAB DRAG ANGLE IAW SRM 51-25-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 14,900 hrs · 9,932 cycles

LT FS 280 BEAM HAS CORROSION DAMAGE. REMOVED AND REPLACED. REPLACED WITH NEW T-BRACKET P/N BA 670-30072-15B. PICK UP ALL FASTENER HOLES IN BEAM, EXCEPT INTERCOSTALS T-BRACKET AND FWD COCKPIT BOARD LAND. FABRICATED U-BRACKET. ALL WORK DONE IAW SRM 51-24-16. PERFORMED EDDY CURRENT INSPECTION OF U-BRACKET AND LT BEAM CUT LINE. NO DEFECTS NOTED. INSTALLED NEW FITTING & BRACKET AT PER SB 670BA-53-026. REFER TO W/O 103067 N/R 00346 FOR LEAK CHECK OF LT STBY PITOT STATIC LINE AT FS 280. RESTORED FINISH, APPLY SEALANT AND PROTECTIVE TAPE. INSTALLED NEW U-BRACKET. INSTALLED 5 CLICK BOND STAND (0900) OFFS. PERFORMED CLEAN UP AT LT SIDE FS 280 BELLY. REAPPLIED CORROSION INHIBITING COMPOUND.

Part: PANEL — CRACKED (PAX DOOR) · airframe 14,939 hrs · 9,960 cycles

PAX DOOR TOP STEP VERTICAL PANEL CRACKED AT FWD SIDE (MARKED).

Part: HANDLE — CRACKED (PAX DOOR) · airframe 14,900 hrs · 9,932 cycles

PAX DOOR FWD INNER HANDLE CRACKED AT TORQUE TUBE ATTACH POINT. REMOVED ASD INNER HANDLE PER AMM 52-11-00. DRILLED AND REAMED HANDLE IAW MM 52-11-00. INSTALLED NEW ASD INNER HANDLE IAW SRM 52-11-02. INSTALLED, REMOVED AND REPLACED BETA LIGHT IAW AMM 52-11-02.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 14,434 hrs · 9,581 cycles

AFT DRAG ANGLE IS CRACKED NEAR DOOR ASSIST PULLEY. WORK COMPLETED IAW: REMOVED AND REPLACED 670-52-11-072-1 AFT ANGLE SECTION (PREVIOUSLY REPAIRED) AS PER REO 670-52-11-072. JOB COMPLETE. (S)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,052 hrs · 9,298 cycles

EMERGENCY LIGHT CEILING ROW 17, LIGHT OUT. REMOVED AND REPLACED EMERGENCY LAMP AT ROW 17 OVERHEAD. OPS CK GOOD REF 33-50-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,052 hrs · 9,298 cycles

EMERGCY LIGHT AT GALLEY SERVI CE DOOR, AFT SIDE 2 LIGHTS OUT REMOVED AND REPLACED LAMPS, OPS CK GOOD. REF 33-50-01. (B)

Part: HANDLE — STICKS (PAX DOOR) · airframe 12,693 hrs · 8,366 cycles

FLT 4859 - PAX DOOR HANDLE STICKS. DIFFICULT TO OPEN FROM BOTH INSIDE AND OUTSIDE THE AIRCRAFT. WHEN CLOSING PAX DOOR OUTER HANDLE COMES ON FOR 20 SECONDS.

Part: PLACARD — MISSING (CABIN) · airframe 12,508 hrs · 8,245 cycles

EXIT PLACARD MISSING AT PAX STAIRWAY DOOR.

Part: DOOR — STUCK (MAIN PAX) · airframe 12,079 hrs · 7,955 cycles

FLT ATTENDANT REPORTS FORWARD PASSENGER DOOR REQUIRED EXCESSIVE FORCE TO OPEN. DOOR HUNG UP ABOUT HALF WAY DOWN.

Part: CHARGER — UNKNOWN (EMERGENCY LIGHTS) · airframe 12,018 hrs · 7,909 cycles

NR 2 EMERGENCY LIGHTS BATTERY CHARGER NEEDS TO BE REPLACED.

Part: CHARGER — UNKNOWN (EMERGENCY LIGHTS) · airframe 12,018 hrs · 7,909 cycles

NR 3 EMERGENCY LIGHTS BATTERY CHARGER NEEDS TO BE REPLACED.

Part: CHARGER — UNKNOWN (EMERGENCY LIGHTS) · airframe 12,018 hrs · 7,909 cycles

NR 4 EMERGENCY LIGHTS BATTERY CHARGER NEEDS REPLACED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,011 hrs · 7,903 cycles

NR 4 EMERGENCY LIGHTS BATTERY PACK IS FULLY DISCHARGED. NEEDS TO BE RECHARGED OR REPLACED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 12,011 hrs · 7,903 cycles

EMERGENCY LIGHTS REMAIN ON WHEN IN THE ARMED POSITION.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 12,011 hrs · 7,903 cycles

EMERGENCY LIGHTS REMAIN ON WHEN IN ARMED POSITION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,011 hrs · 7,903 cycles

NR 2 EMERGENCY LIGHTS BATTERY PACK IS FULLY DISCHARGED. NEEDS TO BE RECHARGED OR REPLACED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,011 hrs · 7,903 cycles

NR 3 EMERGENCY LIGHTS BATTERY PACK IS FULLY DISCHARGED. NEEDS TO BE RECHARGED OR REPLACED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 12,002 hrs · 7,898 cycles

EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION.

Part: HANDLE — BINDS (PAX DOOR) · airframe 11,687 hrs · 7,681 cycles

PAX DOOR HANDLE HARD TO OPEN/CLOSE PAX DOOR. FLT 4407 DEL 147 MINS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 11,509 hrs · 7,551 cycles

AFT PRESSURE BULKHEAD RT SIDE BATHTUB FITTING AT THE NR 2 HYD PRESSURE LINE IS CONFIRMED CRACKED.

Part: DOOR — BINDING (PAX DOOR) · airframe 11,505 hrs · 7,547 cycles

MAIN CABIN DOOR HARD TO OPEN AND CLOSE. FLTS 4094, 4467, 4801 CX AND ON 6/22/07 FLT 4813 CX. (PASSENGER DOOR POWER ASSIST SYSTEM)

Part: UNKNOWN — MALFUNCTIONED (PAX DOOR) · airframe 11,505 hrs · 7,547 cycles

PAX DOOR WILL NOT UNLOCK.

Part: GATE — STUCK (PAX DOOR) · airframe 11,400 hrs · 7,483 cycles

MAIN PASSENGER DOOR STUCK IN CLOSED POSSITION. PRESSURE FLAP WILL OPEN BUT DOOR WILL NOT OPEN FROM INSIDE CABIN OR OUTSIDE CABIN.

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 10,905 hrs · 7,135 cycles

ASD INNER HANDLE CRACKED AT SHAFT CONNECTION (LOCATION MARKED). REMOVED AND REPLACED ASD INNER HANDLE IAW AMM 52-11-02.

Part: FRAME — CORRODED (BS 310 S26L/R) · airframe 10,905 hrs · 7,135 cycles

CORROSION ON FRAME LEG AT FS 310 BETWEEN STR 26L TO 26R.

Part: STRINGER — CORRODED (BS 333-349 S27) · airframe 10,905 hrs · 7,135 cycles

CORROSION ON STR 27 FROM FS 333 TO 349. (SUPPLEMENTAL 28 MARCH 07) COMPLIED WITH EC/TC REO 670-53-21-261 NO FURTHER ACTION REQUIRED.

Part: FRAME — CORRODED (BS 333 S27) · airframe 10,905 hrs · 7,135 cycles

FRAME CORRODED AT FS 333 STRINGER 27. REMOVED FASTNERS AND BLENDED CORRISION IAW CRJ 700 SRM 51-42-06. PERFORMED THICKNESS MEASUREMENT OF BLEND AREA AT FS 333, STR 27 IAW CRJ 700 NDTM 51-20-004. MINIMUM THICKNESS IS .047". SUBMITTED AND RECIEVED REO 670-53-21-260 FOR FS 333 AT STR27. BLENDOUT IS WITHIN LIMITS OF REO 670-53-21-260 ITEM 12. PERFORMED EDDY CURRENT INSPECTION OF BLEND AREA AT FS 333, STR. 27 IAW REO 670-53-21-260 PER CRJ 700 NDTM 51-20-006. NO DEFECTS NOTED. INSTALLED NEW FASTENERS WHERE THEY WERE REMOVED FOR CORROSION REMOVAL IAW CRJ 700 SRM 51-42-06. TREATED, PRIMED AND PAINTED SKIN WHERE RIVETS WERE REMOVED IAW CRJ 700 SRM 51-26-01. JOB COMPLETE.

Part: STRINGER — CORRODED (BS 364 S26L/R) · airframe 10,905 hrs · 7,135 cycles

CORROSION ON STR 26L AND 26R AT FS 364.00. (SUPPLEMENTAL 28 MARCH 07) REMOVED FASTNERS AND BLENDED CORRISION IAW CRJ 700 SRM 51-42-06. DAMAGE IS OUT OF LIMITS, REMOVED .025 FROM S26R BETWEEN FS 349 AND FS 364. DAMAGE ON S26L IS WITH IN LIMIT, REMOVED .006 IAW CRJ 700 SRM 53-21-03-101-006-A01. S26R HAS BEEN REMOVED AND REPLACED ATFS 364 FOR ALL WORK ACCOMPLISHED REFER TO W/O 53023 N/R-00161. INSTALLED RIVETS ON S26L AT FS 364 TREATED, PRIMED AND PAINTED REWOKED AREA IAW CRJ 700 SRM 51-42-06.

Part: WEB — CORRODED (BS 280) · airframe 10,905 hrs · 7,135 cycles

SURFACE CORROSION AT COCKPIT AFT RT WEB FS 280.00 AFT FACE BOTTOM SIDE AT APPROX RBL 26. (SUPPLEMENTAL 28 MARCH 07) BLENDED CORROSION ON LEFT AND RIGHT FS 280 WEB TO THE MAX DEPTH OF .004" BLEND OUT WAS FOUND WITHIN LIMITS IAW 670-53-11-052.

Part: FRAME — CORRODED (BS 295 S27) · airframe 10,905 hrs · 7,135 cycles

FRAME CORRODED AT FS 295 STRINGER 27.

Part: SILL — CORRODED (FUSELAGE) · airframe 10,905 hrs · 7,135 cycles

RIGHT FLOOR SILL PLATE CORRODED AT FS 280.0.

Part: FRAME — CORRODED (BS 319 S27) · airframe 10,905 hrs · 7,135 cycles

FRAME CORRODED AT FS 319 STRINGER 27.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 10,905 hrs · 7,135 cycles

CORROSION ON FLOOR SUPPORT ANGLE ON ASD SILL. REMOVED FWD, MID, AFT ANGLE, LOWER ASD ANGLE AND FWD AND AFT STAIR RAIL FITTINGS. DRILLED, COUNTERSANK, DEBURRED AND ALODINED NEW MID CAP ANGLE PER CRJ 700 SRM 51-42-06. DRILLED, DEBURRED AND COUNTERSANK NEW KICKPLATE PER CRJ 700 SRM 51-40-00. FINISHED INSTALLING NEW KICKPLATE, INSTALLED NEW MID CAP ANGLE AND FWD AND AFT STAIR RAIL FITTINGS AND SEALED AND RESTORED FINISH TO REPAIR AREA PER CRJ 700 SRM 51-42-03, 51-23-00 AND 51-25-16.

Part: FRAME — CORRODED (BS 349 S27) · airframe 10,905 hrs · 7,135 cycles

FRAME CORRODED AT FS 349 STRINGER 27.

Part: STRINGER — CORRODED (BS 294-333 S25R) · airframe 10,905 hrs · 7,135 cycles

CORROSION ON S25R BETWEEN FS 294 AND FS 333. DAMAGE IS OUT OF LIMITS, REMOVED .025 FROM STRG 25R BETWEEN FS 294 AND FS 333 IAW CRJ 700 SRM 53-21-03-101-002-A01. RECIEVED REO 670-53-21-260. FABRICATED REPAIR ANGLE AND SHIM IAW REO 670-53-21-260. PERFORMED NDT PER NDTM 51-20-08 IAW REO 670-53-21-260. INSTALLED REPAIR ANGLE AND SHIM IAW REO 670-53-21-260. INSTALLED CLEAT FOR S26R AND APPLIED CORROSION INHIBITOR TO AREA BETWEEN FS 280 AND FS 349 PER CRJ 700 SRM 51-21-01.

Part: STRINGER — CORRODED (BS 294-333 S26R) · airframe 10,905 hrs · 7,135 cycles

CORROSION ON STR 26R BETWEEN FS 294.00 AND FS 333.00. DAMAGE IS OUT OF LIMITS, REMOVED .018 FROM STRG 26R BETWEEN FS 295 AND FS 319.70 IAW CRJ 700 SRM 53-21-03-101-002-A01. CUT STRINGER 26R AT FS 300 THRU FS 312 AND REMOVED DAMAGED SECTION OF STR. 26 R FROM FS 295 TO FS 364 IAW CRJ 700 SRM 53-00-03. FABRICATED NEW SECTION OF STRINGER AND SHIM AND DOUBLER OUT OF EXTRUSION FOR FS 295 THRU 312, IAW CRJ SRM 53-00-03. PERFORMED EDDY CURRENT INSPECTION OF CUT LINES PER MTC REQUEST, IAW CRJ 700 NDTM PART 1. 51-20-006. NO DEFECTS NOTED. FABRICATED BACKSIDE Z ANGLE DOUBLER FOR BOTH CUTLINES OUT OF EXTRUSION, ALL PARTS DEBURED AND PRIMED IAW CRJ 700 SRM 53-00-03. OK TO INSTALL.

Part: STRINGER — CORRODED (BS 333-349 S26L) · airframe 10,905 hrs · 7,135 cycles

CORROSION ON STR 26L BETWEEN FS 333.00 AND FS 349 (MARKED).

Part: STRINGER — CORRODED (BS 333-349 S26R) · airframe 10,905 hrs · 7,135 cycles

CORROSION ON STR 26R BETWEEN FS 333.00 AND FS 349 (MARKED). (SUPPLEMENTAL 28 MARCH 07) C/W EC/TC REO 670-52-21-262 NO FUTHER ACTION REQUIRED AT THIS TIME

Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,905 hrs · 7,135 cycles

CORROSION ON FLOORBOARD SUPPORT ANGLE AT FS 280.00 IN AVIONICS CRAWLWAY.

Part: FLOORBOARD — CORRODED (BS 280) · airframe 10,905 hrs · 7,135 cycles

CORROSION AT COCKPIT FLOORBOARD AFT LAND AT FS 280.00. (SUPPLEMENTAL 28 MARCH 07) REPAIR ON FLOOR BOARD AFT LAND AT FS 280.00 IAW REO 670-53-11-046.

Part: SKIN — CORRODED (BS 295 S26L/R) · airframe 10,905 hrs · 7,135 cycles

CORROSION ON ANTENNA MOUNT PLATE/DOUBLER BETWEEN STG 26L AND 26R BETWEEN FS 295.00 AND FS 310.00 (MARKED). REMOVED AND REPLACED ANTENNA MOUNT PLATE DOUBLER ASSEMBLY IAW CRJ 700 SRM 51-42-06. INSTALLED LOWER TCAS ANTENNA IAW CRJ 700 MM 34-43-07 SYS OPS CK GOOD.

Part: BRACKET — CRACKED (AIRSTAIR DOOR) · airframe 10,905 hrs · 7,135 cycles

ASD AFT TREAD SKIN TO INNER SKIN L-BRACKET CRACKED IN A PREVIOUSLY REPAIRED AREA, LOCATION MARKED.

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 10,905 hrs · 7,135 cycles

ASD OUTER HANDLE CRACKED IN WEB AS MARKED. REMOVED AND REPLACED ASD OUTER HANDLE IAW CRJ 700 SRM 52-11-03. SUPPLEMENTAL - SDR CLOSED 03/15/07.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,306 hrs · 6,152 cycles

OVERHEAD AISLE EMERG LIGHT INOP

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,687 hrs · 5,749 cycles

FOUND RT SIDE EMERGENCY LIGHT INOP.

Part: LAMP — BURNED OUT (FUSELAGE)

DURING A GROUND INSPECTION, THE LT AFT OVER WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LT AFT OVER WING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: ANGLE — CRACKED (PAX DOOR)

DURING A HANGAR INSPECTION, THE PASSENGER DOOR AFT DRAG ANGLE, ABOVE THE ASSIST MOTOR PULLEY, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR AFT DRAG ANGLE, ABOVE THE ASSIST MOTOR PULLEY, IAW REO 670-52-11-072. (K)

Part: LEVER — MALFUNCTIONED (MLG)

DURING CLIMB-OUT FROM SLC-LAX, THE CREW RECEIVED A MASTER CAUTION `PROX SYSTEM` AND A `PROX SYSTEM 2 FAULT` STATUS MESSAGE. THE CREW COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT DIVERTED BACK TO SLC, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER AND THE LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED (EMERGENCY LIGHT)

FLT 4192 - DURING HANGAR MAINTENANCE IN BTR, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE FLOORBOARD SUPPORT BEAM, JUST INBOARD OF THE AIRSTAIR DOOR SILL, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE FLOORBOARD SUPPORT BEAM, INBOARD OF THE AIRSTAIR DOOR SILL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SEAT TRACK — CORRODED (BS 785-797)

DURING A C-CHECK IN MCN, THE LEFT SEAT TRACK, AT S 785 TO FS 797, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LEFT SEAT TRACK, AT FS 785 TO 797. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DURING A C-CHECK, THE FLASHLIGHT AT ROW 19, SEATS A AND B, WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE FLASHLIGHT AT ROW 19, SEATS A AND B. (K)

Part: PSEU — MALFUNCTIONED (MLG)

FLT 4580 - DURING CLIMB-OUT FROM ATL-TOL, AFTER GEAR RETRACTION THE CREW RECEIVED PROXIMITY SYSTEM CAUTION AND PROXIMITY SYSTEM TWO FAULT STATUS MESSAGES. QRH PROCEDURES WERE COMPLIED WITH AND EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT (PSEU). OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PUMP — INOPERATIVE (HYD SYSTEM)

FLT 4836 - DURING CRUISE FROM OAK-SLC, THE CREW RECEIVED A HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE, INBOARD FLIGHT SPOILER CAUTION MESSAGE AND AN INBOARD SPOILERS CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND A FLAPS TWENTY DEGREE LANDING WAS PERFORMED. AN EMERGENCY WAS NOT DECLARED, HOWEVER, THE TRUCKS WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN SLC. MAINTENANCE REMOVED AND REPLACED THE ENGINE DRIVEN PUMP ON THE RIGHT ENGINE AND ALSO THE CASE DRAIN MANIFOLD FILTERS AS A PRECAUTIONARY MEASURE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4199 - DURING A GROUND INSPECTION IN DFW, THE OVERHEAD EMERGENCY CEILING LIGHT AT ROW SEVENTEEN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE OVERHEAD EMERGENCY CEILING LIGHT LAMP AT ROW SEVENTEEN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A HANGAR CHECK IN BTR, THE LT ANTI-ICE DUCT SUPPORT BRACKET AFT THE PRESSURE BULKHEAD AT FS 1098.2 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANTI-ICE DUCT SUPPORT BRACKET AFT THE PRESSURE BULKHEAD AT FS 1098.2 IAW ASA EO 700-36-0003B. (M)