N740EV

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 41,425 hrs · 30,098 cycles

PAX DOOR INTERCOSTAL DD5 AFT IS CORRODED, HN00134302 (C-CHECK RO 3/10/2024) INSTALLED NEW PAX DOOR AFT INTERCOSTAL DD5 IRT DWG 601R31702 REV -N, CRJ700 SRM 51-42-06-001-001-A01. RESTORED FINISH ALL FASTENERS AND APPLIED C.I.C AT REPAIRED LOCATION IAW CRJ 700 SRM 51-25-16-001-001-A01 AND CRJ 700 SRM 51-21-11-001-001-A01. APPLIED FILLET SEAL AROUND NEW PAX DOOR INTERCOSTAL IAW CRJ 700 SRM 51-23-00-001-001-A01.PRESSURIZATION LEAK TEST PASSED - REF CRJ700 AMM 21-31-00-910-801 A01. NO LEAKS NOTED. COMPLIED WITH 51-900-1002-SKY.

Part: WINDOW FRAME — CRACKED (RT WINDSHIELD) · airframe 41,425 hrs · 30,098 cycles

RH WINDSHIELD POST IS CRACKED. (C-CHECK RO 3/10/2024) REMOVED AND INSTALLED NEW R/H WINDSHIELD SIDE POST CRJ 700 SRM 51-42-21-001-001-A01 AND DWG CC670-33055 REV. -F. LEAK CHECK GOOD. COMPLIED WITH TASK 51-900-1002-SKY.

Part: FRAME ANGLE — CORRODED (BS 379 S23R) · airframe 41,425 hrs · 30,098 cycles

RH FS379.00 FRAME REINFORCING ANGLE (PN: SH670-32119-1) CORRODED AT STR 23R. (C-CHECK RO 3/10/2024) REMOVED AND REPLACED UNSERVICABLE RH FS379.00 FRAME REINFORCING ANGLE (PN: SH670-32119-1) WITH NEW REF. DRWG SH670-32050 REV. J AND CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY AND SKYWEST FORM M-337.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 41,425 hrs · 30,098 cycles

POSSIBLE CRACK ON PAX DOOR AFT DD7 INTERCOSTAL JOB # HN00134589 (C-CHECK RO 3/10/2024) REMOVED AND INSTALLED NEW PAX DOOR AFT INTERCOSTAL DD7 IRT DWG 601R31702 REV -N, CRJ700 SRM 51-42-06-001-001-A01, LEAK CHECK GOOD. COMPLIED WITH TASK 51-900-1002-SKY

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 41,425 hrs · 30,098 cycles

PAX DOOR MID DD1 INTERCOSTAL IS CORRODED JOB # HN00134604 (C-CHECK RO 3/10/2024) REMOVED CORRODED AND INSTALLED NEW PAX DOOR MID DD1 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR. LEAK CHECK PASSED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 41,425 hrs · 30,098 cycles

PAX DOOR INTERCOSTAL DD1A BETWEEN FS338.963 & FS347.250 IS CORRODED, HN00134669 (C-CHECK RO 3/10/2024) REMOVED CORRODED AND INSTALLED NEW PAX DOOR AFT INTERCOSTAL DD1A BETWEEN FS338.963 & FS347.250 - REF IRT DWG 601R31702 REV -N & CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR. LEAK CHECK PASSED.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 41,425 hrs · 30,098 cycles

POSSIBLE CRACK ON PAX DOOR FWD DD1 INTERCOSTAL JOB # (C-CHECK RO 3/10/2024) REMOVED CRACKED AND INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD1 IRT DWG 601R31702 REV -N, CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR. LEAK CHECK GOOD.

Part: FORMER — CRACKED (PAX DOOR) · airframe 41,425 hrs · 30,098 cycles

POSSIBLE CRACK FOUND ON PAX DOOR AFT FORMER JOB # HN00134599 (C-CHECK RO 3/10/2024) REMOVED CRACKED AND INSTALLED NEW PAX DOOR AFT FORMER IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 AND IAW DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR. LEAK CHECK PASSED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 41,425 hrs · 30,098 cycles

PAX DOOR INTERCOSTAL DD7A BETWEEN FS320.163 & FS327.763 IS CORRODED, HN00134622 (C-CHECK RO 3/10/2024) REMOVED CORRODED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD7A BETWEEN FS320.163 & FS327.763 - REF IRT DWG 601R31702 REV -N AND CRJ700 SRM 51-42-06-001-001-A01 COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR. LEAK CHECK PASSED.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 41,425 hrs · 30,098 cycles

POSSIBLE CRACK ON PAX DOOR FWD DD1 INTERCOSTAL JOB # (C-CHECK RO 3/10/2024) REMOVED CRACKED AND INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD1 IRT DWG 601R31702 REV -N, CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR. LEAK CHECK GOOD.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 41,425 hrs · 30,098 cycles

POSSIBLE CRACK ON PAX DOOR FWD DD7 INTERCOSTAL JOB # HN00134589 (C-CHECK RO 3/10/2024) REMOVED CRACKED AND INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD7 - REF IRT DWG 601R31702 REV -N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR. LEAK CHECK PASSED.

Part: DOOR FRAME — CORRODED (WASTE DOOR) · airframe 41,425 hrs · 30,098 cycles

FORWARD WATER-WASTE DOOR SURROUND STRUCTURE LOWER DIAPHRAGM PN: SH670-32284-3 CORRODED. (C-CHECK RO 3/10/2024) INSTALLED NEW FORWARD WATER-WASTE DOOR SURROUND STRUCTURE LOWER DIAPHRAGM REF. DRWG SH670-32280 REV. H AND CRJ 700 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW FORWARD WATER-WASTE DOOR SURROUND STRUCTURE LOWER DIAPHRAGM REF. CRJ 700 SRM 51-42-06-001-001-A0. PERFORMED PRESSURIZATION LEAK CHECK OF FORWARD WATER-WASTE DOOR SURROUND STRUCTURE LOWER DIAPHRAGM. PRESSURIZATION LEAK TEST PASSED - REF CRJ700 AMM 21-31-00-910-801 A01. TASK CARD 51-900-1002-SKY COMPLIED WITH NO LEAKS NOTED.

Part: STRINGER — CORRODED (BS 364-379 S23R) · airframe 41,425 hrs · 30,098 cycles

MAIN AVIONICS BAY STR 23R CORRODED BETWEEN FS364.00 AND FS379.00. (C-CHECK RO 3/10/2024) REMOVED AND INSTALLED NEW STR 23R FROM FS356.00 TO FS379.00 REF. DRWG SH690-31350 REV. M AND CRJ 700 SRM 51-42-06-001-001-A01,CRJ 700 SRM 53-00-03-201-001-A01 REV. 38 DATED JUL 25/2020, LEAK CHECK GOOD.COMPLIED WITH TASK 51-900-1002-SKY

Part: FRAME — CORRODED (BS 379 S21-23R) · airframe 41,425 hrs · 30,098 cycles

CORROSION ON FRAME FS 379.00 BETWEEN STGR 21R - 23R, ACCESSED ON THE EXTERIOR OF AIRCRAFT THROUGH FWD WASTE WATER DOOR (HN00133395) (C-CHECK RO 3/10/2024) REMOVED AND INSTALLED NEW FS379.00 FRAME FROM STR 20R TO STR 25R REF. CRJ-700 DRWG SH670-32280 REV. H, DRWG SH670-32050 REV. J AND CRJ 700 SRM 51-42-06-001-001-A01, LEAK CHECK GOOD.COMPLIED WITH TASK 51-900-1002-SKY

Part: ATTACH BRACKET — CRACKED (LT SLAT TRACK) · airframe 41,425 hrs · 30,098 cycles

LEFT WING SLAT TRACK CANISTER ATTACHING BRACKET FOR 1-3 IS CRACKED. (FLAGGED & MARKED) (C-CHECK RO 3/10/2024) REPAIRED LH SLAT TRACK CANISTER ATTACHING BRACKET FOR 1-3 PER REO 670-57-42-577 REV -- DATED 2016-12-02 LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY';]

Part: ATTACH BRACKET — CRACKED (RT SLAT TRACK) · airframe 41,425 hrs · 30,098 cycles

RIGHT WING SLAT TRACK CANISTER ATTACHING BRACKET FOR 1-3 IS CRACKED. (FLAGGED & MARKED) (C-CHECK RO 3/10/2024) REPAIRED RH SLAT TRACK CANISTER ATTACHING BRACKET FOR 1-3 PER REO 670-57-42-577 REV -- DATED 2016-12-02 LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: HINGE — GOUGED (PAX DOOR) · airframe 41,425 hrs · 30,098 cycles

PASSENGER DOOR PIANO HINGE (FUSELAGE SIDE) LAND #27 IS GOUGED. (C-CHECK RO 3/10/2024) REPAIRED GOUGE ON PASSENGER DOOR PIANO HINGE (FUSELAGE SIDE) LAND #27 IRT REO 670-53-21-582 REV -F DATED 2017-08-02 TYPE IV:, COMPLIED WITH 51-900-1002-SKY

Part: HINGE — GOUGED (PAX DOOR) · airframe 41,425 hrs · 30,098 cycles

PASSENGER DOOR PIANO HINGE (DOOR SIDE) LUG #24 IS GOUGED. (MARKED) (C-CHECK RO 3/10/2024) REMOVED AND INSTALLED NEW PAX DOOR PIANO HINGE (DOOR SIDE) IAW CRJ 700 SRM 52-11-01-201-002-A01 STEP 4R, 4T AND DWG 601R31702 REV. N. APPLIED FILLET SEAL AROUND NEW PAX DOOR PIANO HINGE AND RESTORED FINISH TO ALL FASTENERS IAW CRJ 700 SRM 51-23-00-001-001-A01-A01 AND CRJ 700 SRM 51-25-16-001-001-A01. PRESSURIZATION LEAK TEST PASSED - REF CRJ700 AMM 21-31-00-910-801 A01. NO LEAKS NOTED.COMPLIED WITH TASK 51-900-1002-SKY

Part: STAND OFF — CRACKED (RT TRANSCOWL) · airframe 41,425 hrs · 30,098 cycles

R/H UPPER TRANSCOWL INBD A BRACKET IS CRACKED (C-CHECK RO 3/10/2024) R/H UPPER TRANSCOWL I/B "A" BRACKET HAS BEEN REMOVED AND REPLACED REF REO# 670-54-21-971, REV B, DATED 11/28/23. REFER TO CONTINUATION SHEET FOR DETAILS. COMPLIED W/SKYCARD 51-900-1002 SKY.

Part: TRANSCOWL — CHAFED (RT NACELLE) · airframe 41,425 hrs · 30,098 cycles

R/H UPPER TRANSCOWL INBD SLIDER IS WORN/CHAFED (C-CHECK RO 3/10/2024) COMPLIED WITH ALL STEPS OF REO 670-54-21-1610 REV €“ DATED: 2024-01-26, DISPOSITION FOR BLENDED CHAFE DAMAGE TO THE RH UPPER TRANSCOWL UPPER INBOARD SLIDER. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY.

Part: STAND OFF — CRACKED (LT TRANSCOWL) · airframe 41,425 hrs · 30,098 cycles

L/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED. (C-CHECK RO 3/10/2024) INSTALLED 1 EA. NEW STAND-OFF P/N CN624-2082-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28

Part: WEB — DAMAGED (FWD CARGO) · airframe 41,425 hrs · 30,098 cycles

DRILL START NOTED ON FWD CARGO DOOR WEB SILL AT APPROX.FS566 AND STRG26L (MARKED) (C-CHECK RO 3/10/2024) FWD CARGO DOOR WEB SILL AT APPROX.FS566 AND STRG26L REPAIRED PER MHIRJ REO 670-53-31-850 REV -- DATE 2024-02-08, COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 41,425 hrs · 30,098 cycles

CRACK NOTED ON VERTICAL STAB L/H FWD DRAG ANGLE (MARKED) (C-CHECK RO 3/10/2024) REPAIRED VERTICAL STAB LH FWD DRAG ANGLE REF CRJ700SRM 55-31-00-201-001-A01.COMPLETED SKYWEST TASK CARD 51-900-1002-SKY.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 41,425 hrs · 30,098 cycles

CRACK NOTED ON L/H AFT VERTICAL STAB DRAG ANGLE (MARKED) (C-CHECK RO 3/10/2024) REPAIRED VERTICAL STAB LH AFT DRAG ANGLE REF CRJ700SRM 55-31-00-201-001-A01.COMPLETED SKYWEST TASK CARD 51-900-1002-SKY.

Part: SKIN — DENTED (LT WING) · airframe 41,425 hrs · 30,098 cycles

L/H LOWER EXTERNAL SKIN IS SCRATCHED AND DENTED BETWEEN. WS350-WS370 AND 2" FROM L/E (MARKED) (C-CHECK RO 3/10/2024) REPAIRED SCRATCH AND DENT ON L/H LOWER EXTERNAL SKIN IS BETWEEN. WS350-WS370 AND 2" FROM L/E BY COMPLYING WITH REO 670-57-21-968 REV -- DATED 2024-01-19. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: SLAT TRACK — GROOVED (LT NR 1) · airframe 41,425 hrs · 30,098 cycles

LEFT WING SLAT TRACK 1-1 HAS GROOVE IN INBOARD TRACK AS MARKED (C-CHECK RO 3/10/2024) COMPLIED WITH ALL STEPS OF REO 670-57-42-1479 REV -A DATED: 2024-02-27, DISPOSITION FOR BLENDED GOUGE DAMAGE TO SLAT TRACK 1-1, LHS. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. OPS CHECK GOD AT THIS TIME.

Part: LANDING — CRACKED (TRU BAY) · airframe 41,425 hrs · 30,098 cycles

* R/H TRU BAY DOOR BOTTOM LANDING IS CRACKED AT THE AFT LATCH CUTOUT, MARKED. (C-CHECK RO 3/10/2024) REMOVED AND REPLACED LANDING AT R/H TRU BAY DOOR BOTTOM REF DRWG CC670-33040 REV. G, REO 670-53-11-1916 REV. -- DATED 2024-01-15 AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY AND FORM M-337

Part: SKIN — DENTED (LT TE FLAP) · airframe 41,425 hrs · 30,098 cycles

*DENT NOTED AT R/H INBD FLAP LOWER EXTERNAL SKIN AT APPROX. FLS29 AND 4" FROM T/E (MARKED) (C-CHECK RO 3/10/2024) INSTALLED -1 REPAIR DOUBLER AND -2 REPAIR FILLER ON R/H INBOARD FLAP LOWER SKIN REF CRJ 700 SRM 57-52-01-201-001-A01 TYPE IV REPAIR. COMPLIED WITH SKY WEST TASK CARD 51-900-1002-SKY (CL600-2C10)

Part: SKIN — CHAFED (BS 974) · airframe 41,425 hrs · 30,098 cycles

CHAFFING ON LOWER FUSELAGE SKIN AT FS974 (MARKED, CHAFFING FROM SUPPORT STRAP ON PANEL 196DR). (C-CHECK RO 3/10/2024) REPAIRED CHAFING ON LOWER FUSELAGE SKIN AT FS974 IAW ALL STEPS OF REO 670-53-00-718 REV -- DATED 2024-01-26 AND REO 670-53-00-290 REV-F, DATED 2019-04-26, LEAK CHECK GOOD. COMPLIED WITH TASK 51-900-1002-SKY.

Part: NONE — SMOKE · airframe 41,172 hrs · 29,878 cycles

DURING CLIMB OUT OF DFW ABOUT 2800 FEET FAS CALLED WITH THE SMELL OF SMOKE AND ACTUAL SMOKE IN CABIN COMING FROM GALLEY AREA. / WE DECLARED AN EMERGENCY AND RETURNED TO DFW. SMOKE DISSIPATED IN FLIGHT AND LANDING WAS ROUTINE. WE DID LAND SLIGHTLY OVER WEIGHT AND DECENT RATE AT TOUCHDOWN WAS 500 FT PER MIN. AFTER RETURNING TO GATE FOUND GALLEY HEATER CIRCUIT BREAKER POPPED. (FLIGHT #3234 FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25393252 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH FIM 21-22-00 AND SERVICE LETTER 21-028 SMOKE AND/OR ABNORMAL SMELL IN PASSENGER CABIN AND/OR COCKPIT. SMOKE SOURCE WAS TRACED TO THE GALLEY HEATER, WHICH POPPED ITS CIRCUIT BREAKER AND SMELLED HORRIBLE ONCE REMOVED. SEE 25393253 FOR REPLACEMENT OF THE GALLEY HEATER DETAILS. THE NEW GALLEY HEATER OPERATES NORMALLY. THE NEW GALLEY HEATER DOES NOT POP ITS CIRCUIT BREAKER. NO SMELL OR VISIBLE SMOKE IS PRESENT. / NO OTHER ABNORMALITY WAS UNCOVERED DURING THE INSPECTION. "

Part: NONE — ODOR · airframe 41,045 hrs · 29,775 cycles

AT APPROX FLT LEVEL 300FL FA REPORTED TO THE FLT DECK A BURNING ELECTRICAL SMELL. CAPT VERIFIED BURNING SMELL AROUND THE FLT DECK AND FWD FA JP SEAT AREA. NO SIGNS OF SMOKE OR FIRE. NO OTHER OBSERVED FAULTS OR ABNORMAL INDICATIONS. PACKS WERE NORMAL, ENGINES WERE THE BLEED SOURCE (FLIGHT #4930 FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

Part: NONE — CRACKED · airframe 40,388 hrs · 29,245 cycles

APPROXIMATELY 10 INCH HAIRLINE CRACK IN CAPTAINS SIDE WINDOW. (FLIGHT 3137 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24629586 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED L/H SIDE COCKPIT WINDOW ASSEMBLY IAW TASK CARD# 56-220-1000-SKY. OPS CHECKS GOOD AT THIS TIME, NO LEAKS NOTED AT THIS TIME. / TORQUE WRENCH / SN: 0420502862 DUE 5/2022 / SN: 0914804475 DUE 10/2022"

Part: NONE — INOPERATIVE · airframe 40,086 hrs · 29,014 cycles

STEERING INOP CAUTION MESSAGE WHEN EXTENDING LANDING GEAR. QRH UNHELPFUL. NOSE GEAR WOULD NOT RETRACT FULLY AFTERWARDS, BUT IT DID FULLY EXTEND AGAIN. (FLIGHT 3050 - FILED CLOSED) UPON INVESTIGATION OF NOSE LANDING GEAR FOUND STRUT TO BE IN NEED OF SERVICING. SERVICED NOSE LANDING GEAR SHOCK STRUT PER CRJ 700 AMM 12-12-32. AFTER SERVICING PREFORMED EXTENSION/RETRACTION OF NOSE LANDING GEAR SYSTEM PER CRJ 700 AMM 32-30-00 AND OPS CHECK OF NOSEWHEEL STEERING PER CRJ 700 AMM 32-51-00. OPS CHECK GOOD AT THIS TIME NO DEFECTS NOTED A/C GOOD FOR SERVICE.

Part: FLOOR SUPPORT — DAMAGED (NOT REPORTED) · airframe 37,125 hrs · 26,887 cycles

PERFORM RBL9 FLOOR BEAM FLANGE REPAIR REF. REO 670-53-41-463. PERFORMED RBL9 FLOOR BEAM FLANGE REPAIR REF REO. ALL STEPS COMPLETED AT THIS TIME.

Part: SPLICE — CORRODED (BS 572) · airframe 37,125 hrs · 26,887 cycles

CORROSION FOUND ON I/B TOP SPLICE FOR RBL9 AT FS572.00. REPLACED IB TOP SPLICE ON RBL9 FLOORBEAM AT FS572.00 PER SRM, AND DWGS.

Part: FLOORBEAM — DAMAGED (NOT REPORTED) · airframe 37,125 hrs · 26,887 cycles

FLOORBEAM FLANGE DAMAGED. PERFORMED RBL9 FLOOR BEAM FLANGE REPAIR REF REO. ALL STEPS COMPLETED AT THIS TIME. ST CARD COMPLETE.

Part: SPLICE — CORRODED (BS 572) · airframe 37,125 hrs · 26,887 cycles

CORROSION FOUND ON OB TOP SPLICE FOR RBL9 AT FS572.00. REPLACED OB TOP SPLICE FOR RBL9 FS572.00 IAW SRM, AND DWGS.

Part: SPLICE — CORRODED (BS 686) · airframe 37,125 hrs · 26,887 cycles

CORROSION ON RBL9 SPLICE AT FS 686 IB AND OB TOP SPLICE. REPLACED IB & OB TOP SPLICE AT RBL9 FLOORBEAM, FS686 PER SRM, BOMBARDIER DWG AND BOMBARDIER DWG. COMPLIED WITH SKYWEST TASKCARD

Part: STRINGER — CORRODED (BS 333-349) · airframe 37,125 hrs · 26,887 cycles

STRINGER 22R FS333-FS349 HAD CORROSION. REMOVED AND INSTALLED NEW STRINGER 22R FROM FS 319.00 TO FS 349.00 REF. CRJ 700 SRM. AND DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: FRAME ANGLE — CRACKED (BS 333) · airframe 37,125 hrs · 26,887 cycles

CLIP CRACKED COMMON TO FS333 FRAME AND WATER DRAIN MAST CHANNEL STGR 25R-24R. REMOVED CRACKED AND INSTALLED NEW CLIP REF. DWG AND SRM.

Part: STRINGER — CORRODED (BS 319-333) · airframe 37,125 hrs · 26,887 cycles

STGR 22R BETWEEN F.S. 319 AND F.S. 333 HAS EVIDENCE OF CORROSION (C-CHECK) RO 8/10/2020 REMOVED AND INSTALLED NEW STRINGER AT STGR 22R AT FS 315 TO 349 REF. CRJ 700 SRM AND DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: STRINGER — CORRODED (BS 349-364) · airframe 37,125 hrs · 26,887 cycles

STRINGER 21R BETWEEN FS349 AND FS364 HAS CORROSION. (C-CHECK) RO 8/10/2020 REMOVED AND REPLACED STRINGER 21R BETWEEN FS333.00 AND 379.00. REF BOMBARDIER DWG AND CRJ700 SRM. LEAK CHECK GOOD. COMPLIED WITH TASK CARD.

Part: BOLT — CORRODED (RT WING TE FLAP) · airframe 37,125 hrs · 26,887 cycles

THE FWD 2 MOUNT BOLTS OF THE RH OB FLAP'S OB HINGE BOX ARE CORRODED. REPLACED THE FWD 2EA MOUNT BOLTS OF THE RH OB FLAPS HINGE BOX. REF AMM. OPS TEST GOOD. COMPLIED WITH TASK CARD.

Part: NUT — CORRODED (RT WING TE FLAP) · airframe 37,125 hrs · 26,887 cycles

RH OB FLAPS HINGE ARM SUB ASSY AT W.S. 264.0 HAS A CORRODED NUT ON THE LWR ATTACH BOLT. REMOVED AND REPLACED RH OB FLAPS HINGE ARM SUB ASSY AT W.S. 264.00 LWR ATTACH BOLT NUT AND WASHER P/N MS17826-8 AND P/N NAS1149D0863K REF AMM TASK

Part: CLAMP — CORRODED (RT WING TE FLAP) · airframe 37,125 hrs · 26,887 cycles

RH OB FLAPS MOST OB SKEW DETECTOR HARNESS HAS CORRODED CLAMP HARDWARE. REMOVED AND REPLACED RH OB FLAPS MOST OB SKEW DETECTOR HARNESS CLAMP HARDWARE (SCREW P/N NAS1801-3-7 AND WASHER P/N NAS1149D0332J ) REF CRJ 700 AMM TASK.

Part: BOLT — CORRODED (LT WING TE FLAP) · airframe 37,125 hrs · 26,887 cycles

THE FWD 2 MOUNT BOLTS OF THE LH OB FLAP'S OB HINGE BOX ARE CORRODED. REPLACED THE 2EA FWD MOUNT BOLTS OF THE LH OB FLAPS OB HINGE BOX. REF CRJ700 AMM. OPS TEST GOOD. COMPLIED WITH TASK CARD.

Part: FLOOR SUPPORT — CORRODED (BS 572-686) · airframe 37,125 hrs · 26,887 cycles

FLOOR BEAM TOP SURFACE AT RBL9 BETWEEN FS.572.00 AND FS.686.00 HAS CORROSION AND GOUGING. (C-CHECK) RO 8/10/2020 CORROSION AND DAMAGE REMOVAL NOT ALLOWED FS477 TO FS685 FLOOR SUPPORT STRUCTURE, REFERENCE CRJ700 SRM. REMOVED AND REPLACED RBL9 FLOOR BEAM WITH FABRICATED SECTION, PN SH670-33461-3, FROM PRODUCTION SPLICE AT FS572 TO PRODUCTION SPLICE AT FS685, REFERENCING CRJ700 SRM, BOMBARDIER DRAWING, MHIRJ REO. COMPLIED WITH TASK CARD.

Part: FLOOR SUPPORT — CORRODED (BS 693-797) · airframe 37,125 hrs · 26,887 cycles

RH FLOOR BEAM RBL9 FS693.00 - FS797.00 CORRODED IN SEVERAL AREAS ON TOP. REPAIRED CORRODED FLOOR BEAM RBL 9 AT F.S. 693.00-F.S. 797.00, REF REO

Part: FLOOR SUPPORT — CORRODED (BS 572-686) · airframe 37,125 hrs · 26,887 cycles

FLOOR BEAM TOP SURFACE AT LBL9 BETWEEN FS.572.00 AND FS.686.00 HAS CORROSION AND GOUGING (C-CHECK) RO 8/10/2020 BLENDED CORROSION AND GOUGING FROM FLOOR BEAM TOP CAP AT LBL 9 BETWEEN FS572 - FS686 REF CRJ 700 SRM. EVALUATED AND FOUND NO DAMAGE IS ALLOWED REF CRJ 700 SRM. REPAIRED BEAM TO MHIRJ REO. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD STRUCTURAL MAJOR REPAIR AND FORM M-337.

Part: SEAT TRACK — CORRODED (BS 693) · airframe 37,125 hrs · 26,887 cycles

RH SEAT TRACK AT BS 693 WAS CORRODED. REMOVED AND REPLACED SEAT TRACK RBL9 FS687-FS833 IAW AMM.

Part: FLOORBEAM — CORRODED (BS 693) · airframe 37,125 hrs · 26,887 cycles

* RH FLOORBEAM AT FS693.00 IS CORRODED. FLAGGED. REPAIRED LBL 9 FLOORBEAM AT BS 693, REF REO.

Part: FLOORBEAM — CORRODED (BS 693) · airframe 37,125 hrs · 26,887 cycles

LH FLOOR BEAM LBL9 CORRODED FS693.00 (MARKED) (C-CHECK) RO 8/10/2020 REPAIRED LH LBL9 FLOOR BEAM AT F.S. 693.00, REF MHIRJ REO COMPLIED WITH SKYWEST TASK CARD STRUCTURAL MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 693) · airframe 37,125 hrs · 26,887 cycles

LH FLOOR SEAT TRACK LBL9 SEGMENT CORRODED FS693.00 AFT. REMOVED, FABRICATED NEW SEAT TRACK AND REPLACED SEAT TRACK AT LBL9 FROM FS684.00 - FS835.40 REF. CRJ-700 AMM AND CRJ-700 SRM.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 37,125 hrs · 26,887 cycles

INTERCOSTAL BETWEEN FS364 TO FS349 AT STR 26R CORRODED AT FS364 REMOVED CORROSION FROM INTERCOSTAL AT STR26R BETWEEN FS364.00 TO FS349.00 REF: CRJ700 SRM AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL REF: CRJ700 SRM. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. PRESSURE CHECK GOOD. / COMPLIED WITH TASK CARD

Part: STRINGER — CORRODED (BS 333) · airframe 37,125 hrs · 26,887 cycles

STRINGER JOINT PIECE AT BS 333, STRINGER 25R CORRODED. REMOVED CORROSION ON STRINGER JOINT PIECE AT FS333, STR 25R IAW SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS, IAW SRM AND DWG. REMOVED CORRODED STRINGER SPLICE JOINT AND INSTALLED NEW STRINGER SPLICE JOINT IAW SRM AND DWG.

Part: STOP FITTING — WORN (CARGO DOOR) · airframe 37,125 hrs · 26,887 cycles

THE FORWARD UPPER, FORWARD LOWER, AND AFT LOWER STOPS FOR THE AFT BAGGAGE BAY DOOR ARE WORN/CRACKED AND THE SPRING DETENT FOR THE FORWARD UPPER STOP IS BROKEN. (C-CHECK) RO 8/10/2020 REMOVED AND REPLACED THE FWD UPPER, FWD LOWER, AND AFT LOWER TRACK STOPS AND THE SPRING DETENT FOR THE FWD UPPER STOP FOR THE AFT BAGGAGE BAY DOOR REF. CRJ-700 AMM. PERFORMED OPERATIONAL TEST OF THE AFT BAGGAGE BAY DOOR REF. CRJ-700 AMM. OPS CHECKED GOOD

Part: DIAPHRAGM — CORRODED (DRAIN MAST) · airframe 37,125 hrs · 26,887 cycles

FWD DRAIN MAST DIAPHRAGM IN THE A BAY BETWEEN F.S. 333 AND 347 COMMON TO STGR 25R IS CORRODED OUT OF LIMITS. REMOVED AND INSTALLED A NEW FWD DRAIN MAST DIAPHRAGM IAW SRM AND DWG.

Part: GUARD — CORRODED (PAX DOOR CABLE) · airframe 37,125 hrs · 26,887 cycles

*PAX DOOR ASSIST CABLE NYLON GUARD ON THE DOOR SURROUND FS349.00, ATTACHING NUT PLATES ARE CORRODED AND GUARD IS BROKEN. REMOVED AND REPLACED PAX DOOR ASSIST CABLE NYLON GUARD ASSY. ON THE DOOR SURROUND FS349.00 P/N 601A40053-13 REF CRJ 700 SRM. TOOL USED TUC8619 CAL DUE 31-OCT-20.

Part: FLOOR SUPPORT — CORRODED (BS 923-939) · airframe 37,125 hrs · 26,887 cycles

BS 939 - 923, LBL 9 FLOOR SUPPORT WAS CORRODED ON THE TOP. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: FITTING — CORRODED (BS 314) · airframe 37,125 hrs · 26,887 cycles

*PAX DOOR SURROUND CLOSING FITTING FS314.00 STGR 18LH IS CORRODED AROUND THE FASTENER HOLES (MARKED) (C-CHECK) RO 8/10/2020 REMOVED CORROSION ON FITTING. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW FITTING IAW CRJ 700 SRM AND DWG. COMPLIED WITH SKYWEST TASK CARD AND SWA M-337.

Part: SEAT TRACK — CORRODED (BS 394-485) · airframe 37,125 hrs · 26,887 cycles

FWD OF FS485.00 €“ FS394.00 FLOOR SEAT TRACK AT LBL 27 HAS UPPER SURFACE CORROSION PITTING0. REMOVED, FABRICATED NEW SEAT TRACK AND REPLACED SEAT TRACK AT LBL27 FROM FS364.00 - FS485.00 REF CRJ-700 AMM AND SRM

Part: SUPPORT — CORRODED (BS 310-319) · airframe 37,125 hrs · 26,887 cycles

BS 310 - 319.7 SILL BACKUP CORRODED AT STRINGER 21L. REMOVED AND REPLACED THE SILL BACKUP IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 565) · airframe 37,125 hrs · 26,887 cycles

FS565.00 FWD OF FS533.00 FLOOR SEAT TRACK RBL 9 CORRODED IN SEVERAL AREAS REMOVED, FABRICATED NEW SEAT TRACK AND REPLACED SEAT TRACK AT RBL9 FROM FS565.00 - FS501.00 REF. CRJ-700 AMM AND CRJ-700 SRM.

Part: INTERCOSTAL — CORRODED (BS 310-319) · airframe 37,125 hrs · 26,887 cycles

BS 319.70 - 310, STRINGER 20R INTERCOSTAL WAS CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM AND BOMBARDIER DWG . BOMDING CHECK GOOD. MAJOR REPAIR.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 37,125 hrs · 26,887 cycles

SERVICE DOOR BOTTOM SEAL STRIKER, ON SURROUND, HAD CORROSION AROUND THE FASTENER HOLES ON THE INSIDE. REMOVED CORROSION FROM THE SERVICE DOOR SEAL STRIKER IAW SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED THE SEAL STRIKER IAW DWG AND SRM . PRESSURE LEAK CHECKED GOOD.

Part: SUPPORT — CORRODED (BS 333-349) · airframe 37,125 hrs · 26,887 cycles

BS 333 - 349 SILL BACKUP CORRODED AT STRINGER 21L. REMOVED AND INSTALLED A NEW BACKUP SILL IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 581) · airframe 37,125 hrs · 26,887 cycles

FS581.00 €“ AFT OF FS677.00 FLOOR SEAT TRACK RBL 9, WHOLE SEGMENT HAS CORROSION ALL OVER. REMOVED AND REPLACED SEAT TRACK AT RBL9 FROM FS581.00 - FS677.00 REF. CRJ-700 AMM AND CRJ-700 SRM.

Part: SEAT TRACK — CORRODED (BS 565) · airframe 37,125 hrs · 26,887 cycles

FS565.00 FWD OF FS533.00 FLOOR SEAT TRACK LBL 9 CORRODED IN SEVERAL AREAS. REMOVED, FABRICATED NEW SEAT TRACK AND REPLACED SEAT TRACK AT LBL9 FROM FS501.00 - FS565.00 REF. CRJ-700 AMM AND CRJ-700 SRM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 37,125 hrs · 26,887 cycles

BS 581 AFT OF 677.00 FLOOR SEAT TRACK LBL 9, WHOLE SEGMENT HAS CORROSION ALL OVER. REMOVED, FABRICATED NEW SEAT TRACK AND REPLACED SEAT TRACK AT LBL9 FROM FS581.00 - FS677.00 REF. CRJ-700 AMM AND CRJ-700 SRM.

Part: SEAT TRACK — CORRODED (BS 847-969) · airframe 37,125 hrs · 26,887 cycles

FLOOR SEAT TRACK AFT OF FS969.00 €“ FWD OF FS847.00 RBL 9, ENTIRE SEGMENT CORRODED ALL OVER. FLOOR SEAT TRACK AFT OF BS 969 FWD OF FS847.00 RBL 9 FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED SEAT TRACK BETWEEN FS847 TO FS969 RBL9 IAW AMM.

Part: STRINGER — CORRODED (BS 319-333) · airframe 37,125 hrs · 26,887 cycles

A BAY - BETWEEN FS'S 319 / 333 - STGR 25R CORRODED. REMOVED AND INSTALLED NEW STRINGER AT BS 319 TO 333 IAW SRM AND DWG . COMPLIED WITH TASK CARD. PRESSURE CHECKED GOOD.

Part: STRINGER — CORRODED (BS 333-349) · airframe 37,125 hrs · 26,887 cycles

A BAY - BETWEEN BS 333 - 349 - STRINGER 26R WAS CORRODED. REMOVED AND REPLACED THE SECTION OF THE STRINGER IAW SRM. MAJOR REPAIR.

Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 37,125 hrs · 26,887 cycles

CORROSION DETECTED ON THE AFT CARGO DOOR SILL AT SEVERAL LOCATIONS, AROUND AND ADJACEINT TO FLOOR PANEL NUT PLATES. REMOVED AND INSTALLED A NEW CARGO DOOR SILL IAW SRM AND MHIRJ.

Part: STRINGER — CORRODED (BS 1088) · airframe 37,125 hrs · 26,887 cycles

CORROSION DETECTED ON STRINGER 26R, IMEDIATELY AFT OF BS 1088.2, AROUND FASTENER BUCKTAILS. REMOVED CORROSION FROM THE STRINGER IAW SRM, MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW REO.

Part: BOLT — CORRODED (FWD CARGO BAY) · airframe 37,125 hrs · 26,887 cycles

FWD CARGO BAY LINER MAIN MODULE AFT - HARDWARE CORRODED ON SEVERAL FLOOR ROLLER ASSY. REMOVED CORRODED HARDWARE FROM ROLLER ASSEMBLIES OF FWD BAGGAGE-BAY CARGO RETRIEVAL SYSTEM, AFT MAIN MODULE AND REPLACED WITH NEW HARDWARE BOLTS, WASHERS. AND SELF LOCKING NUTS IAW SRM.

Part: SEAT TRACK — CORRODED (BS 785-797) · airframe 37,125 hrs · 26,887 cycles

*RH SIDE SEAT RAIL RETAINER CHANNEL HAS A CORRODED NUTPLATE AND FASTENER HOLE BETWEEN FS785.15 FS797.00 REMOVED AND REPLACED THE R/H SIDE SEAT RAIL RETAINER CHANNEL LOCATED BETWEEN FS785.00 AND FS797.00. REF SRM.

Part: RIB — CHAFED (RT AILERON) · airframe 37,125 hrs · 26,887 cycles

DEEP CHAFE DAMAGE ALONG INBOARD EDGE OF INBOARD CLOSING RIB, RT AILERON . REMOVED THE CHAFE ALONG INBD EDGE OF RT AILERON, CRACK NOTED DURING NDT. REPLACED THE RT AILERON INBOARD CLOSING RIB WITH NEW PART IAW DWG, AND SRM.

Part: PRESSURE SWITCH — FAILED (NLG STEERING) · airframe 34,555 hrs · 24,820 cycles

STEERING INOP CAUTION MESSAGE IN FLIGHT. (FLT#2963) CLOSED REMOVED AND REPLACED NOSE WHEEL STEERING MANIFOLD PRESSURE SWITCH IAW AMM. OPS CHECKS GOOD AT THIS TIME.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 31,995 hrs · 22,818 cycles

THE FLOOR LEVEL EMERGENCY EXIT SIGN WAS FOUND HANGING OUT OF ITS COVER. MX REMOVED AND REPLACED THE EXIT SIGN ASSY AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (PAX DOOR) · airframe 31,245 hrs · 22,261 cycles

PAX DOOR INNER SKIN CORRODED IN MULTIPLE AREAS AROUND SERVICE/ACCESS HOLES. BLENDED CORROSION ON PAX DOOR INNER SKIN AT ACCESS HOLES, PERFORMED NDT, UT THICKNESS INSPECTION, MATERIAL REMOVED WAS .004", UPON FURTHER EVAL. FOUND MORE CORROSION AND CRACK ON FWD RISER PANELS EXCEEDING ALLOWABLE LIMITS. REMOVED AND REPLACED PAX DOOR INNER SKIN IAW SRM 51-42-06-001-001-A01 AND 51-21-13-001-001-A01 AND DRAWING 601R318029.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

RBL 9 FLOORBEAM CORRODED AT FS 1031. REMOVED AND REPLACED FLOORBEAM AT RBL 9 FROM FS 1031 IAW SRM 53-00-41-201-001-A01, 51-80-00-910-804-A01 AND EC/TC EO 700-53-10-00044.

Part: JOINT — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

FS 280 CIRCUMFERENTIAL JOINT FROM STR 26L-23R HAS CORROSION. REMOVED CORROSION FROM FS 280 STR 26L-23R IAW SRM 51-21-06-001-001-A01. PERFORMED EDDY CURRENT INSPECTION, MATERIAL REMOVED .002" AND .003'. COMPLIED WITH EA 32-2017-074 AND EC/TC EA 32-2017-074.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

LBL 9 FLOORBEAM CORRODED AT FS 1031. REMOVED AND REPLACED FLOORBEAM AT LBL 9 FROM FS 977-1031 IAW SRM 53-00-41-201-001-A01, 51-80-00-910-804-A01 AND EC/TC EO 700-53-10-00043 REV D.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

LBL 27 FLOORBEAM CORRODED AT FS 1031. REMOVED AND REPLACED FLOORBEAM AT LBL 27 FROM FS 1037-977 IAW SRM 53-00-41-201-001-A01, 51-80-00-910-804-A01 AND EC/TC EO 700-53-10-00045.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

PASSENGER DOOR UPPER SILL ANGLE HAS CORROSION. EVALUATED CORROSION DAMAGE AT PASSENGER DOOR AND FOUND IT TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-21-23-101-001-A01 AND 53-00-00-101-0019, HEAVY CORROSION AT FASTENER HOLES. REMOVED AND REPLACED CORRODED PASSENGER DOOR SILL ANGLE IAW SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 31,245 hrs · 22,261 cycles

ASD INTERCOSTAL FOR DOOR HANDLE IS CRACKED. REMOVED AND REPLACED PAX DOOR HANDLE INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DRAWING 601R318072.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

FS 319 FRAME FWD SIDE BETWEEN STR 25R-24R HAS CORROSION. REMOVED CORROSION, MATERIAL REMOVED WAS .014" PERFORMED EDDY CURRENT INSPECTION, NO INDICATIONS NOTED, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-21-06-101-002-A01. REPAIRED IAW REO 670-53-21-799 AND EC/TC REO 670-53-21-799.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

FS 295 FRAME SIDE BETWEEN STR 26R AND 24R HAS CORROSION. REMOVED CORROSION FROM FS 295 FRAME SIDE AND BETWEEN STR 26R TO 24R IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS CHECK; MATERIAL REMOVED .002", ORIGINAL .050", REMAINING .048" PER CRJ-700 NDTM 51-20-06-250-A01. REPAIRED DAMAGE PER REO 670-53-21-1406 AND EC/TC REO 670-53-21-1406. THIS IS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

CABIN SEAT RAIL SEGMENT LBL9 FS836-978 CORRODED SEVERAL AREAS. REMOVED AND REPLACED WITH FABRICATED SECTION PER ECTC REO 670-53-00-343 AMM 53-00-49-000/400-801-A03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

SEAT TRACK CORRODED RBL9 FS 485.00 - 581.00. REMOVED AND INSTALLED NEW FABRICATED SEAT TRACK AT F/S 485.00-581.00 PER AMM 53-00-49-000-801 A03, 53-00-49-400-801-A03 AND EC/TC REO 670-53-00-343 AND GENERIC REO 670-53-00-343 REV. M.

Part: WEB — CRACKED (BS 909) · airframe 31,245 hrs · 22,261 cycles

DIAPHRAGM CRACKED AT BS 909 AND RBL 17. REPAIRED CRACKED DIAPHRAGM IAW REO 670-53-82-478, REV A AND EC/TC 670-53-82-478. MAJOR REPAIR.

Part: WEB — CRACKED (BS 909) · airframe 31,245 hrs · 22,261 cycles

DIAPHRAGM CRACKED AT BS 909 AND LBL 17. REPAIRED THE DIAPHRAGM IAW REO 670-53-82-478, REV A AND EC/TC 670-53-82-478. MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 31,245 hrs · 22,261 cycles

BS 364 STRINGER 27L INTERCOSTAL CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01, 51-42-20-001-001-A01, AND 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

RBL9 SEAT TRACK CORRODED OUT OF LIMITS FROM FS349-485. REMOVED, FABBED NEW AND INSTALLED PER AMM 53-00-49-000/400-801A03 AND ECTC REO 670-53-00-343.

Part: PLATE — CORRODED (BS 1008) · airframe 31,245 hrs · 22,261 cycles

AFT CARGO RESTRAINT NET FWD ATTACH RING PLATE CORRODED AT BS 1008. REMOVED AND REPLACED THE FWD ATTACH RING PLATE IAW SRM 51-42-06-001-001-A01, AND DWG MM670-353.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 31,245 hrs · 22,261 cycles

INTERCOSTAL CORRODED IN PAX DOOR BELOW AND FWD OF MID PIVOT. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

SEAT TRACK CORRODED RBL9 FS 581.00-682.00. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (803), 53-00-49-400-801 (803) AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

RT SIDE SEAT RAIL AT FS 573-674 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

SEAT TRACK CORRODED LBL 9 FS 581.00-683.00. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND ECTC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

SEAT TRACK CORRODED LBL9 FS 545.00-581-00. REMOVED, FABBED NEW AND INSTALLED PER AMM 53-00-49-000/400-801A03 AND ECTC REO 670-53-00-343.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 31,245 hrs · 22,261 cycles

PAX DOOR INTERNAL PULL IN CAM DOUBLER CRACKED UPPER AFT SIDE. REMOVED AND REPLACED CAM DOUBLER IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 31,245 hrs · 22,261 cycles

BS 280 CRAWLWAY FLOORBEAM ANGLE HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREAS ARE WITHIN ALLOWABLE LIMITS IAW SRM 53-00-00-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 785-861) · airframe 31,245 hrs · 22,261 cycles

LEFT SIDE SEAT TRACK BS 785 - 861 IS CORRODED IN MULTIPLE AREAS. REMOVED THE SEAT TRACK, FABRICATED A NEW SEAT TRACK & INSTALLED IAW AMM 53-00-49-000-801 (A03), 53-00-49-400-801 (A03) AND ECTC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

LT SIDE SEAT RAIL AT FS 674-713 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

RT SIDE SEAT RAIL AT FS 674-713 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND EC/TC REO 670-53-00-343.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

INTERCOSTAL ABOVE LOWER CONTROL ROD PIVET CORRODED. REMOVED AND INSTALLED PER SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

FS 295 FRAME AFT SIDE BETWEEN STR 26L TO 26R HAS CORROSION. REMOVED CORROSION FROM FS 295 FRAME AFT SIDE AND BETWEEN STR 26L TO STR 26R IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS CHECK; MATERIAL REMOVED .003", ORIGINAL .050", REMAINING .047" PER NDTM 51-20-06-250-A01. REPAIRED DAMAGE PER REO 670-53-21-1406 AND EC/TC REO 670-53-21-1406. THIS IS A MINOR REPAIR.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 31,245 hrs · 22,261 cycles

INTERCOSTAL CORRODED IN PAX DOOR BELOW OUTER HANDLE HOUSING (FIG 52-11-06-991-801 ITEM 33). REMOVED AND REPLACED PER SRM 51-42-00-001-001-A01, 51-42-06-001-001-A01, 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

LT SIDE SEAT RAIL AT FS 861-969 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND ECTC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

RT SIDE SEAT RAIL AT FS 481-573 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 379-481) · airframe 31,245 hrs · 22,261 cycles

RT SIDE SEAT TRACK BS 379 - 481 IS CORODED IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-53-00-343, AND GREO 670-53-00-343 REV M. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A17, AND 53-00-48-400-801 A17

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

LT SIDE SEAT RAIL AT FS 481-573 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

LT SIDE SEAT RAIL AT FS 573-674 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

RT SIDE SEAT RAIL AT FS 861-969 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND ECTC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 785-862) · airframe 31,245 hrs · 22,261 cycles

RT SIDE SEAT TRACK, BS 785 - 862 IS CORRODED IN MULTIPLE AREAS. REMOVED THE SEAT TRACK, FABRICATED A NEW SEAT TRACK AND INSTALLED IAW AMM 53-00-49-000-801 (A03), 53-00-49-400-801 (A03) AND ECTC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

RT SIDE SEAT RAIL AT FS 713-761 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND ECTC REO 670-53-00-343.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

INTERCOSTAL CORRODED ABOVE AND AFT OF MID PIVOT (FIG 52-11-06-991-801 ITEM 73). REMOVED AND REPLACED WITH SERVICEABLE ONE PER SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

LT SIDE SEAT RAIL AT FS 713-761 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND ECTC REO 670-53-00-343.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 31,245 hrs · 22,261 cycles

ASD INTERCOSTAL UNDER PRESSURE VENT FLAP IS CORRODED. REMOVED AND REPLACED IAW SRM 51-42-00-001-001-A01.

Part: RISER — CORRODED (PAX DOOR) · airframe 31,245 hrs · 22,261 cycles

PAX DOOR FORWARD RISER IS CORRODED IN MULTIPLE AREAS. BLENDED CORROSION ON FWD RISER AND FOUND TO BE OUT OF LIMITS IAW SRM 52-00-01-101-001-A01. REMOVED AND REPLACED FWD RISER PER SRM 51-42-12-001-001-A01 AND DWG 601R31707. THIS IS A MAJOR REPAIR.

Part: DOUBLER — CORRODED (TCAS) · airframe 31,245 hrs · 22,261 cycles

TCAS ANTENNA DOUBLER HAS CORROSION. REMOVED AND REPLACED THE DOUBLER IAW SRM 57-42-06-001-001-A01.

Part: RISER — CRACKED (PAX DOOR) · airframe 31,245 hrs · 22,261 cycles

PAX DOOR AFT RISER IS CRACKED AT BOTTOM FWD STEP. PAX DOOR REPLACED AFT RISER AND STIFFENER IAW SRM 51-42-06-001-001 A01 AND 51-40-11-001-001 A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

FS 295 FRAME AFT SIDE BETWEEN STR 26L TO 26R HAS CORROSION. REMOVED CORROSION FROM FS 295 FRAME AFT SIDE AND BETWEEN STR 26L TO STR 26R IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS CHECK; MATERIAL REMOVED .003", ORIGINAL .050", REMAINING .047" PER NDTM 51-20-06-250-A01. REPAIRED DAMAGE PER REO 670-53-21-1406 AND EC/TC REO 670-53-21-1406. THIS IS A MINOR REPAIR.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

ROW 12 CD LOWER EXIT SIGN HAD ONE LIGHT BULB BURNED. REPLACED THE BULB IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

LOWER EXIT SIGN BY MAIN ENTRANCE HAD ONE BULB BURNED. REPLACED THE LAMP IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: FIRE DETECTOR — FALSE INDICATION (RT NACELLE) · airframe 29,820 hrs · 21,158 cycles

AT 2000 FT, RECEIVED RT ENGINE FIRE WARNING. COMPLIED WITH IMMEDIATE ACTION CHECKLIST AND QRH PROCEDURES AND RETURNED TO LAND. LANDED AT LESS THAN 100 FPM ON THE 63000 LB CART. ACFT RETURNED TO DEPARTURE, FALSE FIRE WARNING DURING FLIGHT. REMOVED AND REPLACED NR 2 ENGINE. REPAIRED IAW CAE 2016-7-01.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 29,296 hrs · 20,746 cycles

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

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 28,396 hrs · 20,023 cycles

THE EMERGENCY EXIT SIGN FOR THE FORWARD CABIN SERVICE DOOR DS173, FAILED THE OPS TEST. FOUND WIRES TO EMERGENCY EXIT SIGN DS173 FOR THE FORWARD CABIN SERVICE DOOR TO BE DISCONNECTED. CONNECTED WIRE IAW AMM, OPS TEST OF EMERGENCY LIGHTS NOW GOOD. OPS TEST OF EXIT SIGN LIGHT, DS173, GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 25,451 hrs · 17,702 cycles

EMERGENCY LIGHTS FAILED OPS TEST. TROUBLESHOT IAW FIM 33-51-00-810-804 AND FOUND ESPU BATTERY PACK NR 3 & NR 4 TO BE UNSERVICABLE. REPLACED BATTERY PACK IAW 33-51-17-400-801. PERFORMED OPS CHECK TASK 33-51-17-710-801, OPS TESTED GOOD OK TO CLOSE PANEL 273ALC. INSTALLED PANEL 273ALC THAT WAS SERVICEABLE IAW AMM 25-26-05-400-804. PERFORMED OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-802.

Part: RISER — CRACKED (PAX DOOR) · airframe 25,451 hrs · 17,702 cycles

DISCOVERED FWD RISER CRACKED AT BOTTOM PAX DOOR STEP. REPAIRED IAW EA 32-2014-043.

Part: PANEL — DAMAGED (WING) · airframe 25,451 hrs · 17,702 cycles

PANEL 631DZ HAS ONE ELONGATED HOLE. FURTHER INVESTIGATION FOUND THAT UNDERLYING STRUCTURE WAS DRILLED INTO. REMOVED LOWER ANGLE AT SLAT TRACK 2-3 AND SEAL ASSY, INSPECTED SLAT TACK RIB AND FOUND NO DAMAGE BLENDED SMALL DRILL START FROM ANGLE, REPAIRED IAW REO 670-57-42-539 P2.

Part: UNKNOWN — DAMAGED (WING) · airframe 25,451 hrs · 17,702 cycles

WHILE PERFORMING SB 670BA-57-015 01 ON RT SIDE GO-NO-GO GAUGE GOES ALL THE WAY IN TOP AND BOTTOM HOLE LOCATIONS. REPAIRED IAW REO 670-57-21-721.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 25,451 hrs · 17,702 cycles

LT COCKPIT FLOOR SUPPORT IS CRACKED. REMOVED AND RPLACED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 AND DWG CC670-33199. MAJOR REPAIR.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 25,451 hrs · 17,702 cycles

RT COCKPIT FLOOR SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED RT COCKPIT FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, SRM 51-42-06-001-001, AND DWG CC670-33199.

Part: LOCK FASTENER — MISSING (SEAT TRACK) · airframe 25,451 hrs · 17,702 cycles

ON REMOVAL OF RT SIDEWALL SEAT TRACK BS 785.15-FS 863.00 FOUND TWO LOCK FASTENERS MISSING. INSTALLED THE LOCK FASTERNERS IAW SRM 51-42-20-001-001-A01. MAJOR REPAIR.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,451 hrs · 17,702 cycles

RT BS 280 BULKHEAD WEB IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. FABRICATED RT LOWER WEB AND RT BUTTSTRAP IAW REO 670-53-11-594. MAJOR REPAIR.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,451 hrs · 17,702 cycles

LT 280 BULKHEAD WEB IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. FABRICATED LT LOWER WEB AND LT BUTTSTRAP IAW REO 670-53-11-594. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 785.15) · airframe 25,451 hrs · 17,702 cycles

LT SIDE SEAT TRACK CORRODED AT APPROX BS 785.15. REMOVED SEAT TRACK FROM BS 784 - 861 IAW AMM 53-00-49-000-801-403. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801, A03.

Part: SEAT TRACK — CORRODED (BS 785.15) · airframe 25,451 hrs · 17,702 cycles

RT SIDE SEAT TRACK CORRODED AT BS 785.15. REMOVED SEAT TRACK FROM BS 785.15 - 863 IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 25,451 hrs · 17,702 cycles

CORROSION FOUND ON FLOOR BRACKET. R & R BRACKET IAW DWG SH670-31996 AND SRM 51-42-06-001-001-A01

Part: FLOORBEAM — CORRODED (BS 333) · airframe 25,451 hrs · 17,702 cycles

CORROSION ON FLOORBEAM AROUND SCREW HOLE BS 333, LBL 16. REPAIRED IAW EC/TC EA 25-2014-237 AND EA 25-2014-237. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 310) · airframe 25,451 hrs · 17,702 cycles

PACKER CORRODED ON BS 310 FLOORBEAM, LBL 4. REMOVED PACKER IAW SRM 51-42-06-001-001-A01. INSTALLED NEW PACKER IAW SRM 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 25,447 hrs · 17,699 cycles

CORROSION FOUND ON RT FLOOR SUPPORT BS 349-364. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 333) · airframe 25,451 hrs · 17,702 cycles

PACKER CORRODED ON FS 333 FLOORBEAM, RBL 8. REMOVED PACKER IAW SRM 51-42-06-001-001-A01. INSTALLED NEW PACKER IAW SRM 51-42-06-001-001.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 25,451 hrs · 17,702 cycles

PAX DOOR LOWER SILL MID CAP ANGLE CORRODED. REMOVED FWD & AFT CAP ANGLES IAW SRM 51-42-06-001-001-A01. FOUND TO BE CORRODED, REPLACE FWD AND AFT CAP ANGLES. INSTALLED FWD & AFT CAP ANGLES, SRM 51-42-06-001-001-A01 PAX DOOR LOWER SILL REF DWG SH 670-31821. REMOVED MID CAP ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED MID CAP ANGLE IAW SRM 51-42-06-001-001-A01 PAX DOOR LOWER SILL REF DWG SH670-31825. MAJOR REPAIR.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 25,451 hrs · 17,702 cycles

PAX DOOR CUTOUT LOWER SILL KICKPLATE ANGLE HAS CORROSION DAMAGE AT FWD END. REMOVED KICKPLATE ANGLE FROM PAX DOOR OBTAINED NEW ANGLE LOCATED DRILL HOLES, DEBURED AS REQUIRED AND INSTALLED NUTPLATES IAW SRM 51-40-11-001-001, 51-45-00-001-001. INSTALLED KICKPLATE ANGLE IAW SRM 51-42-06-001-A01 AND 51-42-21-001-001-A01 AND IAW DWG SH670-31810. MAJOR REPAIR.

Part: DOOR SILL — CORRODED (BS 319-349) · airframe 25,447 hrs · 17,699 cycles

DOOR SILL BS 319-349 IS CORRODED. REMOVED AND REPLACED DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-42-06-001-001-A01, AND DWG SH670-31996.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 25,447 hrs · 17,699 cycles

RT FLOORBEAM BS 280 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND FOUND OUT OF LIMITS. REPAIRED IAW ECTC REO 670-53-21-139.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 25,447 hrs · 17,699 cycles

LT SIDE BS 193, ELECTIRCAL BAY FLOOR PANEL CRACKED. REPAIRED IAW ECTC REO 670-53-11-509 AND GREO 670-53-11-509, REV B.

Part: BRACKET — CORRODED (SERVICE DOORWAY) · airframe 25,447 hrs · 17,699 cycles

FWD LOWER BRACKET AT SERVICE DOOR BS 319.7 IS CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ANGLE IAW SRM 51-42-06-001-001-A01.

Part: SKIN — CHAFED (BS 977) · airframe 25,447 hrs · 17,699 cycles

FUSELAGE SKIN CHAFED JUST AFT OF BS 977 STRINGER 27. BLENDED DAMAGE IAW RM (TR) 51-12-00-001-001-A01, & REO 670-53-00-290, REV C.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 25,447 hrs · 17,699 cycles

BS 280 FLOORBEAM CORRODED. R & R FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34256.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 25,447 hrs · 17,699 cycles

BS 280 FLOORBEAM CORRODED AT MULTIPLE AREAS. FLOORBEAM WAS REPLACED.

Part: RETAINER — BENT (CARGO DOOR SEAL) · airframe 25,447 hrs · 17,699 cycles

FWD CARGO DOOR OUTER SEAL RETAINER IS BENT AT FWD AND AFT LOWER CORNERS. REPAIRED IAW EC/TC REO 670-52-35-127 01 REV STEP 11.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,451 hrs · 17,702 cycles

DENT FOUND ABOVE AND LT OF FWD CARGO DOOR BETWEEN TWO REINFORCING PLATES. REPAIRED IAW EA 12-2014-171.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,135 hrs · 15,321 cycles

AFT CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. R & R LAMP. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 20,642 hrs · 14,204 cycles

FWD FUSELAGE, EMERGENCY LIGHTS INOPERATIVE. R & R TWO FWD LIGHT ASSY BULBS. PERFORMED OPS TEST IAW AMM 33-51-15-710-801. OPS CHECKED GOOD.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 20,642 hrs · 14,204 cycles

PASSENGER DOOR RELEASE HANDLE EXCEEDS MAXIMUM FORCE. ADJUSTED PASSENGER DOOR WITHIN SPECIFIED LIMITS IAW AMM 52-11-04-710-801 A01, 52-11-02-820-801 A01. 52-11-00-710-701-A01.

Part: FRAME — CORRODED (BS 349) · airframe 20,642 hrs · 14,204 cycles

CORROSION ON FS 349 FRAME FROM STRINGERS 24-26 RIGHT.

Part: STRINGER — CORRODED (BS 349-364 S26R) · airframe 20,642 hrs · 14,204 cycles

CORROSION ON STRINGER 26R BETWEEN FS 349-364.

Part: INTERCOSTAL — CORRODED (BS 364 S26-27R) · airframe 20,642 hrs · 14,204 cycles

CORROSION AT FS 364 RT INTERCOSTAL BETWEEN STRINGERS 27 & 26R. INSTALLED INTERCOSTAL AT FS 364 RT INTERCOSTAL IAW SRM 51-42-21-001-001.

Part: INTERCOSTAL — CORRODED (BS 364 S26-27L) · airframe 20,642 hrs · 14,204 cycles

CORROSION AT FS 364 INTERCOSTAL BETWEEN STRINGERS 26 & 27L.

Part: STRINGER SPLICE — CORRODED (BS 333 S26R) · airframe 20,642 hrs · 14,204 cycles

STRINGER SPLICE 26R FS 333, FOUND CORRODED OUT OF LIMITS. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-42-06-001-001.

Part: STRINGER — CORRODED (BS 295-310 S26R) · airframe 20,642 hrs · 14,204 cycles

CORROSION ON STRINGER 26R BETWEEN FS 295 & 310.

Part: STRINGER — CORRODED (BS 333-349 S25R) · airframe 20,642 hrs · 14,204 cycles

CORROSION ON STRINGER 25 RIGHT FROM FS 349 - 333. REMOVED CORROSION ON STRINGER AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED STRINGER 25R IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. LOCATED & DRILLED NEW STRINGER IAW SRM 51-40-11-001-001. INSTALLED IAW SRM 51-42-21-001-001.

Part: STRINGER — CORRODED (BS 364 S26L) · airframe 20,642 hrs · 14,204 cycles

CORROSION AT FS 364 STRINGER 26L. INSTALLED NEW STRINGER 26L IAW SRM 51-42-06-001-001, A01 & DWG SH670-31372.

Part: FRAME — CORRODED (BS 349 S24-26R) · airframe 20,642 hrs · 14,204 cycles

CORROSION ON FS 349 FRAME FROM STRINGERS 24-26 RIGHT. BLENDED CORROSION AND FOUND FRAME TO BE OUT OF LIMITS REF SRM 51-21-06-001-001 & SRM 53-21-06-101-006. REMOVED FRAME IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. LOCATED AND DRILLED NEW FRAME IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED FRAME SPLICE IAW SRM 51-42-06-001-001.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 20,642 hrs · 14,204 cycles

LT AFT CARGO FLOOR SUPPORT UNDER PANEL 281JLF HAS SURFACE CORROSION BETWEEN FS 1015 TO 1045. REMOVED DAMAGE IAW SRM 51-12-00-001-001-A01. MEASURED AREA, ORIGINAL MATERIAL THICKNESS .063" BLEND DIMENSIONS : 5.3"X2.1X.035", .028" REMAINING; 2.7" X 1.4"X .005",.058" REMAINING; 1"X1.1"X.003", .060" REMAINING; 3.6"X1"X.006" .057" REMAINING THICKNESS.

Part: SILL — CRACKED (E/E BAY) · airframe 20,642 hrs · 14,204 cycles

FWD EQUIPMENT COMPARTMENT RT SIDE, SILL UNDER THE ADG HYD PUMP IS CRACKED. REPAIRED IAW GREO 670-53-11-504 AND ECTC REO 670-53-11-509.

Part: INTERCOSTAL — CORRODED (BS 364 S26-27L) · airframe 20,642 hrs · 14,204 cycles

CORROSION AT FS 364 INTERCOSTAL BETWEEN STRINGERS 27 AND 26L. BLENDED CORROSSION AND FOUND OUT OF LIMITS REF SRM 53-21-23-101-003-A01 & SRM 51-21-06-001-001. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001 & SRM 51-42-21-001-001. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-21-001-001.

Part: STRINGER — CORRODED (BS 349-364 S26R) · airframe 20,642 hrs · 14,204 cycles

CORROSION ON STRINGER 26R BETWEEN FS 349 TO 364. CORROSION FOUND OUT OF LIMITS IAW SRM 53-21-03-101-006-A01. REMOVED STRINGER SPLICE AND SECTION OF STRINGER IAW SRM 51-42-06-001-001. DRILLED NEW SECTION OF STRINGER IAW SRM 51-40-11-001-001. INSTALLED STRINGER IAW SRM 51-42-06-001-001.

Part: LIGHT — BROKEN (CABIN) · airframe 20,642 hrs · 14,204 cycles

LIGHT, AISLE WITH ARROW BROKEN AT END OF TRACK. RECEIVED NEW TRACK LIGHTING SEGMENT,

Part: INTERCOSTAL — CORRODED (BS 364 S26-27R) · airframe 20,642 hrs · 14,204 cycles

CORROSION AT FS 364 RT INTERCOSTAL BETWEEM STRG27 AND 26R. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06-001-001-A01.

Part: FRAME — CORRODED (BS 333) · airframe 20,642 hrs · 14,204 cycles

CORROSION AT FS 333 BETWEEN STRINGERS 26 AND 27 LEFT. BLENDED DAMAGE ON FRAME. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MIN MATERIAL REMAINING IS .040" ORIGINAL IS .050" MATERIAL REMOVED IS .010" . REPAIRED IAW REO 670-53-21-867.

Part: FRAME — CORRODED (BS 319 S26L/R) · airframe 20,642 hrs · 14,204 cycles

CORROSION ON FRAME AT FS 319 AND FROM STRINGERS 26L TO 26R. REMOVED CORROSION ON FRAME IAW SRM 53-21-06-101-002-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .042"7, ORIGINAL IS .050" MATERIAL REMOVED IS .008". CORROSION ON FRAME IS OUT OF LIMITS IAW SRM 53-21-06-101-003-A01 IAW NOTE 1. REPAIRED IAW REO 670-53-21-870 RC161761.

Part: STRINGER — CORRODED (BS 364 S26L) · airframe 20,642 hrs · 14,204 cycles

CORROSION AT FS 364 STRINGER 26L. CORROSION OUT OF LIMITS IAW SRM 53-21-03-101-006-A01. REMOVED STRINGER IAW SRM 51-42-06-001-001-A01. DRILLED NEW STRINGER AND INSTALLED IAW SRM 51-42-06-001-001.

Part: SUPPORT — CORRODED (NLG) · airframe 20,642 hrs · 14,204 cycles

CORROSION ON NLG NOSE JACK FITTING SUPPORTS (LT AND RT) BETWEEN FS 265.00 AND FS 280.00. BLEND DAMAGE FROM FITTING SUPPORTS DETERMINE REMAINING MATERIAL & SUBMIT TO THD REF SRM 51-21-06-001-001. STARTED BLENDING LT AND RT SIDE OF NOSE JACK SUPPORT FITTING IAW SRM 700. CONTINUE REMOVING RIVETS AND CORROSION ON LT AND RT NOSE JACK SUPPORT FITTINGS. REMOVED (13) EA RIVETS FROM NLG NOSE JACK FITTING SUPPORTS (LT & RT) BETWEEN FS 265.00 & 280.00 AND REMOVED CORROSION FROM FITTING SUPPORTS (LT & RH) IAW SM 51-42-06-001-001 & 51-21-06-001-001. FABRICATE -1 & -2 NLG FITTING SUPPORT. FABRICATED -1 & -2 NLG FITTING SUPPORTS LT & RT IAW DWG PL CC670-32179 & SRM 51-24-16-001-001-A01. 1 & 2 NLG SUPPORTS REQUIRE FINAL TRIMMING HEAT TREAT. PARTS IN ITEM 3 NOT USED. REQUEST NDT FOR THICKNESS CHECK CM162141. PERFORMED UT THICKNESS INSP OF BLEND AREAS IAW MAC NDT INSP PROCEDURE UT-3 MIN MATERIAL REMAINING IS .062" ORIGINAL IS .063", MATERIAL REMOVED IS .001". RII FOUND TO BE SATSIFACTORY. SDR CLOSED.

Part: STRINGER — CORRODED (BS 295-310 S26R) · airframe 20,642 hrs · 14,204 cycles

CORROSION ON STRINGER 26R BETWEEN FS 295 AND 310. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS IAW SRM 53-21-03-101-003-A01. REMOVED STRINGER REF SRM 51-42-06-001-001. DRILLED NEW SECTION OF STRINGER 26R REF SRM 51-40-11-001-001. INSTALLED STRINGER IAW SRM 51-42-06-001-001.

Part: CHANNEL — CORRODED (BS 305 S27) · airframe 20,642 hrs · 14,204 cycles

CHANNEL CORRODED AT FS 305 AND S27 ABOVE ANTENNA. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-01-101-002-A01. R & R CHANNEL IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 20,416 hrs · 14,020 cycles

EMERGENCY LIGHTS WILL NOT STAY ON WHEN SELECTED ON. CHARGED THE EMERGENCY LIGHT BATTERIES, OPS CHECKED GOOD IAW AMM 33-51-00, ACFT OK FOR SERVICE.

Part: GLOWSTRIP — MISSING (GALLEY) · airframe 19,937 hrs · 13,688 cycles

PHOTOLUMINESCENT FLOOR STRIP MISSING FROM GALLEY. INSTALLED SERVICEABLE EMERGENCEY FLOOR PATH MARKING AT GALLEY AREA IAW AMM 33-51-01 NO FURTHER DEFECTS NOTED.

Part: PLACARD — MISSING (EMERGENCY EXIT) · airframe 19,937 hrs · 13,688 cycles

EMERGENCY EXIT PLACARD ON PAX DOOR MISSING. INSTALLED PLACARD IAW GMM 3-8.6

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYSTEM) · airframe 19,659 hrs · 13,495 cycles

ON FINAL APPROACH IN MODERATE ICING CONDITIONS, RECEIVED LT WING ANTI ICE CAUTION MESSAGE. FOLLOWED QRH AND MESSAGE DID NOT EXTINGUISH. EMERGENCY DECLARED. PERFORMED RESET OF WING ANTI ICE SYSTEM IAW FIM 30-12-00, COULD NOT DUPLICATE MESSAGE. NO FURTHER ISSUES AT THIS TIME, ACFT OK FOR SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 19,584 hrs · 13,448 cycles

A SECTION OF THE EMERGENCY FLOOR LIGHTING RIPPED UP. R & R EMERGENCY LIGHT IAW AMM 33-51-11. ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,769 hrs · 12,180 cycles

EMERGENCY LIGHT ON CEILING PANEL ROW 15 INOP. R & R LAMP IAW CRJ 700 33-51-09. OPS CHECK GOOD PLACARD REMOVED DEFER CLEARED. (ITEM RESOLVE UNDER MDDR: 639804-2) R & R LAMP IAW CRJ 700 33-51-09. OPS CHECK GOOD PLACARD REMOVED DEFER CLEARED. (CLOSED)

Part: LAMP — INOPERATIVE (ROW 15) · airframe 17,710 hrs · 12,140 cycles

EMERGENCY LIGHT ON CABIN CEILING INOPERATIVE, ROW 15. RELAMPED IAW 33-51-09, OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,968 hrs · 11,628 cycles

RT AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED RT AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-15, OPS CHECK GOOD. RELAMPED RT AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-15, OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,968 hrs · 11,628 cycles

NR 6 AFT MOST CABIN CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED NR6 AFT MOST CABIN CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-09, OPS CHECK GOOD. RELAMPED NR 6 AFT MOST CABIN CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-09, OPS CHECK GOOD.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 16,513 hrs · 11,316 cycles

PHOTOLUMINESCENT TRACK ON LT SIDE JUST AFT OF EXIT ROW 12AB DAMAGED. R & R PHOTOLUMINESCENT TRACKS ON LT SIDE JUST AFT EXIT ROW 12AB IAW AMM 33-51-01.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 16,357 hrs · 11,212 cycles

LT AFT ENTERIOR EMERGENCY LIGHT INOP. R & R BULB IAW AMM 33-51-15, OPS CHECK GOOD IAW AMM 33-51-15. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,289 hrs · 11,165 cycles

FWD EMERGENCY LIGHTS WILL NOT ILLUMINATE. ITEM TRANSFERRED TO ASA DMIL NR 568377-2 IAW CUSTOMER.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,289 hrs · 11,165 cycles

FWD EMERGENCY LIGHTS WILL NOT ILLUMINATE. R & R FWD EXT BATTERY PACK IAW AMM 33-51-04 OPS CK GOOD DEFER CLEARED MCC NOTIFIED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,289 hrs · 11,165 cycles

EMERGENCY LIGHTS INOPERATIVE, R & R FWD EXT BATTERY PACK IAW AMM 33-51-01. OPS CK GOOD. DEFER CLEAR, MCC NOTIFIED.

Part: DOUBLER — CORRODED (BS 280) · airframe 16,257 hrs · 11,145 cycles

SURFACE CORROSION ON UPPER FS 280.00 MODSUM DOUBLER PN BA670-30069-8. BLENDED CORROSION DAMAGE IS GREATER THAN 10 PERCENT OUT OF LIMITS REF SRM 53-00-00. FABRICATED NEW DOUBLER OUT OF 7075T62 .050 PO T000004626 IAW DWG BA670-30069, REV A. PRIMED & APPLIED PROTECTIVE TOP COAT TO BA670-30069-8 MODSUM DOUBLER REF SRM 51-25-01-001-001-A01. (CLOSED)

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,257 hrs · 11,145 cycles

UPPER MODSUM DOUBLER AT LT FS 280 FLOORBEAM CORRODED. BLENDED CORROSION DAMAGE IS GREATER THAN 10 PERCENT OUT OF LIMITS REF SRM 53-00-00. FABRICATED NEW DOUBLER OUT OF 7075T62 .050 P/O T000004626 IAW DWG BA670-30069, REV A. PRIMED & APPLIED PROTECTIVE TOPCOAT TO MODSUM DOUBLER LT REF SRM 51-25-01-001-001-A01.

Part: STIFFENER — CRACKED (BS 280 BULKHEAD) · airframe 16,257 hrs · 11,145 cycles

RT LOWER FS 280 BULKHEAD WEB STIFFENER PN:CC670-34117-6 IS CRACKED AT LOWER FASTENER LOCATION. REMOVED STIFFINER AT RT FS 280.00 LOWER BULKHEAD RBL 26.00 IAW SRM 51-42-06. LOCATED AND DRILLED NEW STIFFENER REF SRM 51-40-11. REMOVED PNL 221BRF IAW AM 53-00-47-000-805. PERFORMED GVI, NO DEFECTS NOTED. INSTALLED PANEL 221BRF REF SRM 51-41-02. INSTALLED NEW STIFFENER REF SRM 51-42-06.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 16,257 hrs · 11,145 cycles

PAX DOOR AFT INTERCOSTAL CRACKED LOWER AFT. REMOVED AFT DOOR CENTERING PLATE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01, PERFORMED GVI, NO DEFECTS NOTED. REMOVED LWR AFT INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. INSTALLED PAX DOOR LWR AFT INTERCOSTAL IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED PAX DOOR AFT CENTERING PLATE IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01. PERFORMED PRESURIZATION LEAK CHECK IAW AMM 52-00-00-790-801, NO DEFECTS NOTED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,257 hrs · 11,145 cycles

FS 280.00, LT FLOORBEAM CRACKED. REMOVED LT FS280 FLOORBEAM IAW SRM 51-42-06 & 51-42-13. DRILLED-UP NEW FOORBEAM REF SRM 51-40-11-001-001-A01. NDT FLOORBEAM LT CUT LINE IAW NDTM 51-20-06. NO DEFECTS NOTED REF ATTACHED NDT REPORT. INSTALLED FLOORBEAM IAW SRM 51-42-13-001-001-A01 AND SRM 51-42-21-001-001-A01. APPLIED SEALANT AND MYLAR TO FS280.00 WEB & TOP OF BEAM REF AMM TASK 53-00-42-390-801.

Part: SEAT TRACK — CORRODED (BS 379-669.4) · airframe 16,257 hrs · 11,145 cycles

SIDE SEAT RAILS FS 379-669.4, HAVE MODERATE TO SEVERE CORROSION.

Part: SILL — CORRODED (FUSELAGE) · airframe 16,257 hrs · 11,145 cycles

AFT CARGO DOOR, FLOOR SUPPORT SILL FOR 281JLF HAS CORROSION. BLENDED CORROSION REF SRM 53-61-23-001-001-A01. UT THICKNESS TEST REF NDTM 51-20-004. MEASUREMENTS RANGED .062-.070" IN BLENDS, ALL READINGS MARKED ON PART, PERFORMED EPT INSP ON AFT CARGO DOOR FLOOR SUPPORT SILL BLEND OUT, IAW NDTM 53-00-000, NO DEFECTS NOTED. FINISH RESTORED IAW SRM 51-21-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUD IAW SRM 51-21-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 581-683.5) · airframe 16,257 hrs · 11,145 cycles

ONE SEAT TRACK AT LBL 9 FS 581.00 TO FS 683.50 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK AT LBL 9, STA 581.00-683.50 IAW AMM TASK 53-00-49-000-801. FIT & DRILLED SEAT TRACK N126-2075 PO T-3525 IAW SRM 51-40-11-001-001-A01. ET INSP REF NDTM 51-20-006 NO DEFECTS NOTED BEYOND CUT-LINES. INSTALLED SEAT TRACK AT FS 581-683.50 LBL 9 REF AMM TASK 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 683.5-836.5) · airframe 16,257 hrs · 11,145 cycles

ONE SEAT TRACK AT RBL 9, FS 683.50 TO 836.50 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK AT LBL 9 FS 683.50 TO FS 836.50 IAW AMM TASK 53-00-49-000-801. LOCATED & DRILLED SEAT TRACK RBL 9.0 FS 683.50 FS 836.50 FROM PN N126-2075 PO T000004999 IAW SRM 51-40-11-001-001-A01. ET INSP REF NDTM 51-20-006 NO DEFECTS NOTED BEYOND CUT-LINES. PREPPED & PAINTED RT SEAT TRACK SRM 51-25-01-001-001-A01. INSTALLED SEAT TRACK AT FS 683.5-836.5, RBL 9, REFAMM TASK 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 573-675) · airframe 16,257 hrs · 11,145 cycles

LEFT SEAT TRACK AT STA 573.00-675.00 IS CORRODED BEYOND LIMITS, (SIDEWALL TRACK). REMOVED LT SIDEWALL SET TRACK IAW AMM 53-00-49-00-801. FIT & DRILLED SEAT TRACK IAW SRM 51-40-11. PERFORMED P/T INSP ON SEAT TRACK CUT LINE IAW NDTM 51-20-008 NO DEFECTS NOTED NDT REPORT ATTACHED. (NDT-6) PREPPED & PAINTED LT SEAT TRACKS REF SRM 51-25-01-001-001-A01, PGS 1-16, STEPS 1-9. INSTALLED LT SIDEWALL SEAT TRACKS REF AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 16,257 hrs · 11,145 cycles

LEFT SIDEWALL SEAT TRACK AT STA 675.00-713.00 IS CORRODED BEYOND LIMITS. REMOVED LT SIDEWALL SEAT TRACK IAW AMM 53-00-49-00-801. FIT & DRILLED LT SIDEWALL SEAT TRACK IAW SRM 51-41-02-001-001-A01. INSTALLED LT SIDEWALL SEAT TRACKS AT REF AMM 53-00-49-400-801-A03 STEP 4A (2) PERFORMED P/T INSP ON SEAT TRACK CUT LINE IAW NDTM 51-20-008 NO DEFECTS NOTED NDT REPORT ATTACHED. PREPPED & PAINTED LT SEAT TRACK REF SRM 51-25-01-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 575-713) · airframe 16,257 hrs · 11,145 cycles

RIGHT SIDEWALL SEAT TRACK AT STA 675.00-713.00 IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW AMM 53-00-49-00-801. INSTALLED NEW SEAT TRACK REF AMM 53-00-49-400-801 (A03). FIT & DRILLED RT SIDEWALL SEAT TRACK IAW SRM 51-41--02-001-001-A01. PERFORMED P/T INSP ON SEAT TRACK CUT LINE IAW NDTM 51-20-008 NO DEFECTS NOTED NDT REPORT ATTACHED. (NDT-2) PREPPED & PAINTED RT SEAT TRACK SRM 51-25-01-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 784-861) · airframe 16,257 hrs · 11,145 cycles

LEFT SIDEWALL SEAT TRACK AT STA 784.00-861.00 IS CORRODED BEYOND LIMITS. REMOVED LT SIDEWALL SEAT TRACK IAW AMM 53-00-49-00-801. FIT & DRILLED SEAT TRACK IAW SRM 51-40-11. PERFORMED P/T INSP ON SEAT TRACK CUT LINE IAW NDTM 51-20-008 NO DEFECTS NOTED NDT REPORT ATTACHED. PREPPED & PAINTED LT SEAT TRACKS REF SRM 51-25-01-001-001-A01. INSTALLED LT SIDEWALL SEAT TRACKS AMM 53-00-49-400-801-A03 STEP 4A(A).

Part: SEAT TRACK — CORRODED (BS 861-985) · airframe 16,257 hrs · 11,145 cycles

RIGHT SIDEWALL SEAT TRACK AT STA 861.00-985.00 IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW AMM 53-00-49-00-801 FS 861-985. INSTALLED NEW RT SIDEWALL SEAT TRACK AT STA 861.00-985.00 AMM TASK 53-00-49-400-801 (A03) PO T000003200. FIT & DRILLED SEAT TRACK PN N126-2075 PO T000004999 IAW SRM 51-40-11. PERFORMED P/T INSP ON SEAT TRACK CUT LINE IAW NDTM 51-20-008, NO DEFECTS NOTED NDT REPORT ATTACHED. PREPPED & PAINTED RT SEAT TRACK REF SRM 51-25-01-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 374-485) · airframe 16,257 hrs · 11,145 cycles

SEAT TRACK AT LBL 9 FS 374.00 TP FS485.00 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK AT LBL 9 FS 374.00-485.00 IAW AMM TASK 53-00-49-000-801. FIT & DRILLED SEAT TRACK NR N126-2075 PO T-4999 IAW SRM 51-40-11-001-001-A01. ET INSP REF NDTM 51-20-006 NO DEFECTS NOTED BEYOND CUT-LINES. INSTALLED SEAT TRACK AT LBL 9 FS 374-488 REF AMM TASK 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 483-573) · airframe 16,257 hrs · 11,145 cycles

RIGHT SEAT TRACK AT STA 483.00-573.00 IS CORRODED BEYOND LIMITS, (SIDEWALL TRACK). REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK AMM 53-00-49-400-801-A03. FIT & DRILLED SEAT TRACK IAW SRM 51-41-02-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,257 hrs · 11,145 cycles

FS 280.00 COCKPIT FLOORBEAM CORRODED. REMOVED FS280 COCKPIT FLOORBEAM ANGLE REF SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND SRM 51-42-22-001-001-A01. INSTALLED NEW FS280 COCKPIT FLOORBEAM ANGLE REF SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 573-675) · airframe 16,257 hrs · 11,145 cycles

LEFT SIDEWALL SEAT TRACK AT STA 573.00-675.00 IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW AMM 53-00-49-00-801, FS 573-675. INSTALLED NEW SEAT TRACK AT RT SIDEWALL REF AMM TASK 53-00-49-400-801. FIT & DRILLED SEAT TRACK IAW SRM 51-40-11. PERFORMED P/T INSP ON SEAT TRACK CUT LINE IAW NDTM 51-20-008 NO DEFECTS NOTED NDT REPORT ATTACHED. PREPPED & PAINED RT SEAT TRACK REF SRM 51-25-01-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 280-477) · airframe 16,257 hrs · 11,145 cycles

FLOOR SEAT RAILS FS 280.0 -477.0 HAVE MODERATE TO SEVERE CORROSION. FLOOR SEAT RAILS FS 280.0 -477.0 HAVE MODERATE TO SEVERE CORROSION. FOUND BEYOND LIMITS IAW REO 670-53-00-013 REV -B, DATED 2009-06-18.

Part: SEAT TRACK — CORRODED (BS 379-483) · airframe 16,257 hrs · 11,145 cycles

LEFT SEAT TRACK AT STA 379.00-483.00 IS CORRODED BEYOND LIMITS. REMOVED LT SIDEWALL SEAT TRACK AT STA 379-483 IAW AMM 53-00-49-000-801. FIT & DRILLED SEAT TRACK PN N126-2075 PO T000004999 IAW SRM 51-40-11. INSTALLED LT SIDEWALL SEAT TRACK FROM FS 379 TO FS 483 REF AMM 53-00-49-400-801-A03. PERFORMED P/T INSP ON SEAT TRACK CUT LINES IAW NDTM 51-20-008 NO DEFECTS NOTED NDT REPORT ATTACHED. PREPPED & PAINTED SEAT TRACK LT REF SRM 51-25-01-001-001-A01, PGS 1-16, STEPS 1-9.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 16,257 hrs · 11,145 cycles

SEAT TRACK AT LBL 9 FS 485.00 TO FS 581.00 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK AT LBL 9, FS 485.00-581.00 IAW AMM TASK 53-00-49-000-801. FIT & DRILLED SEAT TRACK NR N126-2075 PO T-4999 IAW SRM 51-40-11-001-001-A01 & REO 670-53-00-074, REV A 2009/03/05. ET INSP REF NDTM 51-20-006 NO DEFECTS NOTED BEYOND CUT-LINES. ECTC 670-53-00-074 IS C/W. INSTALLED SEAT TRACK AT FS 485-581 LBL 9 REF AMM TASK 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 713-763) · airframe 16,257 hrs · 11,145 cycles

LEFT SIDEWALL SEAT TRACK AT STA 713.00-763.00 IS CORRODED BEYOND LIMITS. REMOVED LT SIDEWALL SEAT TRACK IAW AMM 53-00-49-00-801. FIT & DRILLED SEAT TRACK IAW SRM 51-40-11. PERFORMED P/T INSP ON SEAT TRACK CUT LINE IAW NDTM 51-20-008 NO DEFECTS NOTED NDT REPORT ATTACHED. (NDT-6) PREPPED & PAINTED LT SEAT TRACKS IAW SRM 51-25-01-001-001-A01. INSTALLED LT SIDEWALL SEAT TRACK AT FS 713.00-763.00 IAW AMM 53-00-49-400-801-A03 4A (3).

Part: SEAT TRACK — CORRODED (BS 713-763) · airframe 16,257 hrs · 11,145 cycles

RT SIDEWALL SEAT TRACK AT STA 713.00-763.00 IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW AMM 53-00-49-00-801. FIT & DRILLED SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK AT RT SIDEWALL REF AMM TASK 53-00-49-400-801 (A03). INSTALLED AT RT SIDEWALL SEAT TRACK REF AMM TASK 53-00-49-400-801 PERFORMED P/T INSP ON SEAT TRACK CUT LINE IAW NDTM 51-20-008 NO DEFECTS NOTED NDT REPORT ATTACHED. PREPPED & PAINTED RT SEAT TRACK REF SRM 51-25-01-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 16,257 hrs · 11,145 cycles

ONE SEAT TRACK AT RBL 9, FS 485.00 TO 581 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK AT RBL 9, FS 485.00 TO 581.00 IAW AMM TASK 53-00-49-000-801. FIT & DRILLED SEAT TRACK N126-2075 PO T-3525 IAW SRM 51-40-11-001-001-A01. ET INSP REF NDTM 51-20-006. NO DEFECTS NOTED BEYOND CUT-LINES. INSTALLED SEAT TRACK AT FS 485-581, RBL 9 REF AMM TASK 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 836.5-988) · airframe 16,257 hrs · 11,145 cycles

ONE SEAT TRACK AT LBL 9 FS 836.50 TO 988.00 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK AT LBL 9, FS 836.50 TO 988.00 IAW AMM TASK 53-00-49-000-801. FIT & DRILLED SEAT TRACK N126-2075 PO T-4999 IAW SRM 51-40-11-001-001-A01. ET INSP REF NDTM 51-20-006 NO DEFECTS NOTED BEYOND CUT-LINES. INSTALLED SEAT TRACK AT FS 836.5-988, LBL 9 REF AMM TASK 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 683.5-836.5) · airframe 16,257 hrs · 11,145 cycles

ONE SEAT TRACK AT LBL 9 FS 683.50 TO 836.50 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK AT LBL 9, FS 683.50-836.50 IAW AMM TASK 53-00-49-000-801. FIT & DRILLED SEAT TRACK N126-2075 PO T-3525 IAW SRM 51-40-11-001-001-A01. ET INSP REF NDTM 51-20-006 NO DEFECTS NOTED BEYOND CUT-LINES. INSTALLED SEAT TRACK AT FS 683.5-836.5 LBL 9 REF AMM TASK 53-00-49-400-801

Part: SEAT TRACK — CORRODED (BS 669-977) · airframe 16,257 hrs · 11,145 cycles

SIDE SEAT RAILS FS 669.0 - 977.0 HAVE MODERATE TO SEVERE CORROSION.

Part: SEAT TRACK — CORRODED (BS 861-985) · airframe 16,257 hrs · 11,145 cycles

LEFT SIDEWALL SEAT TRACK AT STA 861.00-985.00 IS CORRODED BEYOND LIMITS. REMOVED LT SIDEWALL SEAT TRACK IAW AMM 53-00-49-00-801. FIT & DRILLED SEAT TRACK IAW SRM 51-40-11. PERFORMED P/T INSP ON SEAT TRACK CUT LINE IAW NDTM 51-20-008 NO DEFECTS NOTED NDT REPORT ATTACHED. PREPPED & PAINTED LT SEAT TRACKS SRM 51-25-01-001-001-A01, PGS 1-16, STEPS 1-9. INSTALLED LT SIDEWALL SEAT TRACKS IAW AMM 53-00-49-400-801-A03 STEPS 4A(5).

Part: FLOORBEAM — CORRODED (FS 280) · airframe 16,257 hrs · 11,145 cycles

FS 280.00 RT CROSSBEAM CORRODED. REMOVED RT FS280.00 FLOORBEAM IAW SRM 51-42-06 AND SRM 51-42-13. LOCATED AND DRILLED RT FS280 FLOORBEAM IAW SRM 51-24-36-001-001-A01 & 51-40-11-001-001-A01. INSTALLED RT FS 280.00 FLOORBEAM IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. APPLIED SEALANT AND VAPOR BARRIER TO RT FS280.0 BEAM AND WEB REF AMM 53-00-42-390-801.

Part: SEAT TRACK — CORRODED (BS 477-693) · airframe 16,257 hrs · 11,145 cycles

FLOOR SEAT RAILS FS 477.0 - 693.0 HAVE MODERATE TO SEVERE CORROSION. FLOOR SEAT RAILS FS 477.0 - 693.0 HAVE MODERATE TO SEVERE CORROSION. FOUND BEYOND LIMITS IAW REO 670-53-00-013 REV -B, DATED 2009-06-18 & SRM 53-31-49.

Part: SEAT TRACK — CORRODED (BS 836.5-977) · airframe 16,257 hrs · 11,145 cycles

ONE SEAT TRACKS AT RBL 9, FS 836.50 TO 977.00 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK AT LBL 9 FS 836.50 TO FS 977.00 IAW AMM 53-00-49-000-801. FIT & DRILLED SEAT TRACK N126-2075, PO T-3525 IAW SRM 51-40-11-001-001-A01. ET INSP REF NDTM 51-20-006 NO DEFECTS NOTED BEYOND CUT-LINES. INSTALLED SEAT TRACK AT FS 836.50-977, RBL 9, REF AMM TASK 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581-683.5) · airframe 16,257 hrs · 11,145 cycles

ONE SEAT TRACK AT RBL 9 FS 581.00 TO 683.50 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK AT LBL 9, FS 581.00 TO FS 683.50 IAW AMM TASK 53-00-49-000-801. FIT & DRILLED SEAT TRACK N126-2075 PO T-3525 IAW SRM 51-42-11-001-001-A01. ET INSP REF NDTM 51-20-006 NO DEFECTS NOTED BEYOND CUT-LINES. INSTALLED SEAT TRACK AT FS 581-683.5 RBL 9 REF AMM TASK 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 483-573) · airframe 16,257 hrs · 11,145 cycles

LEFT SEAT TRACK AT STA 483.00-573.00 IS CORRODED BEYOND LIMITS, (SIDEWALL TRACK). REMOVED SEAT TRACK (LT SIDEWALL) IAW AMM 53-00-49-000-801 . FIT & DRILLED SEAT TRACK IAW SRM 51-40-11. INSTALLED LT SEAT TRACK (SIDEWALL) REF AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 350-485) · airframe 16,257 hrs · 11,145 cycles

ONE SEAT TRACK AT RBL 9, FS 350.00 TO 485.00 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK AT LBL 9 FS 350.00 TO FS 485.00 IAW AMM 53-00-49-000-801. FIT & DRILLED SEAT TRACK NR N126-2075 PO T-3525 IAW SRM 51-42-11-001-001-A01. ET INSP REF NDTM 51-20-006, NO DEFECTS NOTED BEYOND CUT-LINES. INSTALLED SEAT TRACK AT FS 350.00-485, RBL 9, REF AMM TASK 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379-483) · airframe 16,257 hrs · 11,145 cycles

RIGHT SEAT TRACK AT STA 379.00-483.00 IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK SIDE WALL REF AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 784-861) · airframe 16,257 hrs · 11,145 cycles

RIGHT SIDEWALL SEAT TRACK AT STA 784.00-861.00 IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW AMM 53-00-49-00-801. INSTALLED NEW RT SIDEWALL SEAT TRACK IAW AMM 53-00-49-400-801 (A03). FIT & DRILLED SEAT TRACK IAW SRM 51-40-11. PERFORMED P/T INSP ON SEAT TRACK CUT LINE IAW NDTM 51-20-008 NO DEFECTS NOTED NDT REPORT ATTACHED. PREPPED & PAINTED RT SEAT TRACK REF SRM 51-25-01-001-001-A01.

Part: HANDLE — BINDING (PAX DOOR) · airframe 16,257 hrs · 11,145 cycles

PAX DOOR UNLATCH HANDLE REQUIRES TOO MUCH FORCE TO BREAK FREE. LUBED PAX DOOR LATCH PINS IAW AMM 12-20-2-640-809-A01. RT GOOD IAW AMM 52-11-00-720-801-A01.

Part: HANDLE — BINDING (EMERGENCY EXIT) · airframe 16,257 hrs · 11,145 cycles

RT OVERWING EMERGENCY EXIT HANDLE REQUIRES TO MUCH FORCE TO OPEN 52 LBS. ADJUSTED OVERWING EXIT DOOR IAW AMM 52-21-00-820-801. SATISFACTORY IAW SP607, IAW AMM 52-21-00-820-801.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 15,821 hrs · 10,815 cycles

CEILING EMERGENCY LIGHT (SQUARE FIXTURE) INOP 4TH FROM FRONT. REPLACED BULB, OPS CKD GOODIAW AMM 33-50-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,436 hrs · 10,524 cycles

EMERGENCY LIGHT HAS BULB INOP. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-11. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 15,436 hrs · 10,524 cycles

RIGHT EMERGENCY LIGHT JUST AFT OF THE EMERGENCY EXIT DOOR IS INOP. REMOVED AND REPLACED RT MIDDLE EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-15. OPS CHECK GOOD.

Part: GLOWSTRIP — WRONG PART (CABIN) · airframe 15,054 hrs · 10,229 cycles

FOUND 3 EACH INCORRECT PHOTOLUMINESCENT STRIPS INSTALLED. R & R 3EA PHOTOLUMINESCENT EMERGENCY FLOOR PATH MARKING IAW AMM 33-51-01 ITEM: 123 MARCH 2010 -- R & R 3EA PHOTOLUMINESCENT EMERGENCY FLOOR PATH MARKING IAW AMM 33-51-01.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 14,541 hrs · 9,847 cycles

FOUND EMERGENCY LIGHT SWITCH AT F/A STA LT ON, SET SW OFF RECHARGED EMERGENCY LIGHT PACKS FOR 30 MINS- OPS CHECK GOOD IAW AMM 33-51-00, DEFER CLEARED PLACARD REMOVED. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,541 hrs · 9,847 cycles

EMERGENCY LIGHTS INOP.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 14,499 hrs · 9,816 cycles

LT OVERWING EMERGENCY LIGHT INOP.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 14,256 hrs · 9,640 cycles

CAPT WINDSHIELD SHATTERED IN ROUTE. (ENROUTE, DIVERTED DUE TO MX, EMERGENCY DECLARED]

Part: BULB — INOPERATIVE (LAV EMER CALL) · airframe 13,956 hrs · 9,411 cycles

REAR LAV AMBER "EMER" CALL LIGHT BULB WILL NOT ILLUMINATE WHEN FA CALL BUTTON INSIDE REAR LAV IS PUSHED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,872 hrs · 8,582 cycles

RT AFT EXTERIOR EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,053 hrs · 7,955 cycles

PASSENGER COMPARTMENT SECOND FROM FRONT CEILING EMERGENCY LIGHT INOP.

Part: DRAG ANGLE — CRACKED (SERVICE DOOR)

ASD AFT SIDEWALL DRAG ANGLE CRACKED. WORK COMPLETED IAW CURT OUT CRACKED DRAG ANGLE IAW REO 670-52-11-072. PERFORMED EDDY CURRENT INSPECTION OF CUT OUT ON AFT DRAG ANGLE ON AIRSTAIR DOOR IAW REO 670-52-11-072 IAW CRJ 700NDTM 51-20-2006. NOT DEFECTS NOTED.

Part: WEB — CORRODED (FUSELAGE) · airframe 11,349 hrs · 7,420 cycles

RT 280 WEB CORRODED. SUP CLOSED 9/15/2008 - BLENDED OUT CORROSION ON RT WEB. TOOK NO MORE THEN 004 OF MATERIAL IAW REPAIR NR 1 OF REO 670-53-11-052. ALODINE PRIME AND PAINT ON BLENDED AREAS IAW REO 670-53-11-052.

Part: WEB — CORRODED (FUSELAGE) · airframe 11,349 hrs · 7,420 cycles

LT 280 WEBB CORRODED. SUP - 9/15/2008 - REMOVED LT WEB IAW REO 670-53-11-052. (K)

Part: FLOORBEAM — CORRODED (BS 280) · airframe 11,349 hrs · 7,420 cycles

LT BS 280 BEAM CORRODED. 9/15/2008 - SUP- (RESOLVED W/O 99610 TASKCARD NR 00181) WORK COMPLETED IAW: INSTALLED DRUO TRAYS IAW SB 670BA-53-026.

Part: BEAM — CORRODED (FUSELAGE) · airframe 11,349 hrs · 7,420 cycles

RT 280 BEAM CORRODED. SUP 9/15/2008. INSTALLED DRIP TRAYS IAW SB670BA-53-026. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 11,349 hrs · 7,420 cycles

280 FWD FLOOR SUPPORT CORRODED. SUP-9/15/200. REMOVED FWD 280 SUPPORT ANGLE ( FOUND TO BE OUT OF LIMITS) ISW CRJ 700 SRM 51-42-06, BAT 7023167, DRILLED NEW FWD ANGLE IAW CRJ 200 SRM 51-40-11. (K)

Part: STRUCTURE — CRACKED (ASD) · airframe 11,349 hrs · 7,420 cycles

ASD AFT SIDEWALL CRACKED AT SECOND STEP RISER.

Part: STRUCTURE — CRACKED (ASD) · airframe 11,349 hrs · 7,420 cycles

ASD FWD SIDEWALL CRACKED AT SECOND STEP RISER.

Part: HANDLE — CRACKED (ASD) · airframe 11,349 hrs · 7,420 cycles

ASD EXTERNAL HANDLE CRACKED.

Part: SKIN — CRACKED (ASD) · airframe 11,349 hrs · 7,420 cycles

ASD INNER SKIN CRACKED AT AFT CORNER UNDER UPPER STEP.

Part: STEP — CRACKED (AIRSTAIR)

ASD AFT SIDEWALL CRACKED AT 2ND STEP RISER. CUT OUT DAMAGED ON AFT SIDE PANEL NR 2 STEP IAW REO 670-52-11-104. PERFORMED EDDY CURRENT INSPECTION OF CUT OUT ON AIRSTAIR DOOR 2ND STEP RISER ON AFT SIDEWALL IAW REO 670-52-11-104 IAW CRJ 700, NDTM 51-20-006. NO DEFECTS NOTED

Part: SKIN — CRACKED (ASD) · airframe 11,349 hrs · 7,420 cycles

ASD INNER SKIN CRACKED AT FWD CORNER UNDER UPPER STEP.

Part: DRAG ANGLE — CRACKED (ASD) · airframe 11,349 hrs · 7,420 cycles

ASD AFT SIDEWALL DRAG ANGLE CRACKED.

Part: SKIN — CRACKED (DOOR)

ALSO INNER SKIN CRACKED AT FWD CORNER UNDER UPPER STEP. CUTOUT DOOR EDGE MEMBER IAW REO 670-52-11-154. PERFORMED ET INSPECTION OF CUTLINE IAW REO 670-52 NDTM 51-20-006. NO DEFECTS NOTED. FN7013735 090708 (K)

Part: SKIN — CRACKED (SERVICE DOOR)

ASD INNER SKIN CRACKED AT AFT CORNER UNDER UPPER STEP. CUTOUT DOOR EDGE MEMBER IAW REO 670-52-11-154. PERFORMED ET INSPECTION OF CUTLINE IAW REO 670-52-11-154 IAW CRJ 700, NDTM 51-20-006. NO DEFECTS NOTED. FN7013735. 090708. (K)

Part: HANDLE — CRACKED (DOOR)

ASD EXTERNAL HANDLE CRACKED. REFER TO W/O 99613 EC/TC SB 670BA-52-030 FOR WORK ACCOMPLISHED FOR THE REMOVAL AND REPLACEMENT OF THE ASD EXTERIOR HANDLE ASSY. (K)

Part: STRUCTURE — CRACKED (AIRSTAIR DOOR)

ASD FWD SIDEWALL CRACKED AT 2ND STEP RISER. REPAIRED STEP RISER IAW 670-52-11-104 WORK COMPLETED. CUT OUT DAMAGED SECTION OF STEP IAW REO 670-52-11-104. PERFORMED ET INSPECTION OF CUTLINE IAW REO 670-52-11-104 IAW CRJ 700 NDTM 51-20-006. NO DEFECT FN7013735. (K)

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 10,936 hrs · 7,124 cycles

PHOTOLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PATH TAPE DAMAGED AT FORWARD LAV ENTRANCE. (CABIN EMERGENCY LIGHTS-PHOTOLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING). REMOVED AND REPLACED EMERGENCY LIGHT STRIP PER AMM 33-51-01. ACFT OK FOR SERVICE. (S)

Part: GLOWSTRIP — MISSING (CABIN) · airframe 10,334 hrs · 6,695 cycles

RT EMERGENCY FLOOR STRIP FWD ARE MISSING/DAMAGED. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRITE CORRECTIVE ACTION. CABIN EMERGENCY LIGHTS - PHOTOLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,660 hrs · 6,256 cycles

RIGHT OVERWING EMERGENCY EXIT FORWARD LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS.

Part: SIGN — MISSING (SERVICE DOOR) · airframe 8,769 hrs · 5,661 cycles

EXIT SIGN AT SERVICE DOOR IS MISSING. FLT 4235 DEL 23 MINS.

Part: COVER — MISSING (CABIN) · airframe 8,435 hrs · 5,415 cycles

EXIT SIGN COVER MISSING FROM F/A GALLEY AREA NEAR FLOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,386 hrs · 5,378 cycles

G2 EMERGENCY LIGHT BY SERVICE DOOR HAS SEVERAL INOP BULBS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,708 hrs · 4,932 cycles

RIGHT FUSELAGE AFT EXT EMERGENCY LIGHT INOP.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 7,473 hrs · 4,778 cycles

NR 3 EMERGENCY LIGHT BATTERY PACK WILL NOT HOLD CHARGE.

Part: WEB — CORRODED (BS 280) · airframe 7,472 hrs · 4,776 cycles

LEFT 280 LWR WEB HAS MINOR CORROSION.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 7,472 hrs · 4,776 cycles

RIGHT FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. REMOVED RT FS 280 CROSSBEAM IAW CRJ 700 SRM 51-42-06 AND 51-42-21. LOCATED NEW SERVICEABLE CROSSBEAM IAW CRJ 700 SRM 51-40-11.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 7,472 hrs · 4,776 cycles

FS 280 FWD CENTER FLOOR SUPPORT ANGLE CORRODED. REMOVED 280 CENTER FLOOR SUPPORT ANGLE IAW CRJ 700, 51-42-06 AND 51-42-21. OK TO INSTALL SERVICE ANGLE.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 7,472 hrs · 4,776 cycles

LEFT FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. STARTED REMOVING FASTENERS FROM LT 280 BEAM IAW CRJ 700 SRM 51-42-21 AND 51-42-06. CONTINUED TO REMOVED FASTENERS FROM 280 CROSSBEAM IAW CRJ 700 SRM 51-42-21 AND 51-42-06. FINISHED REMOVING FS 280

Part: WEB — CORRODED (BS 280) · airframe 7,472 hrs · 4,776 cycles

RIGHT LOWER FS 280 WEB HAS CORROSION. REMOVED RT FS280 WEB IAW CRJ 700 51-42-06 AND 51-42-21. DUPLICATED R/H LWR 280 WEB.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 7,332 hrs · 4,684 cycles

PAX DOOR HANDLE BROKEN.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 6,469 hrs · 4,116 cycles

WHILE EMERGENCY LIGHTS ARMED IN FLIGHT, THE LIGHTS CYCLE ON AND OFF.

Part: STEP — BROKEN (AIRSTAIR) · airframe 5,919 hrs · 3,783 cycles

ASD BOTTOM STEP BROKEN AT ATTACH LINK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,640 hrs · 3,622 cycles

THE EMERGENCY FLUORESCENT STRIP IN FRONT OF FWD LAV BACK TO ROW 2 DOESN’T ILL.

Part: PLACARD — DAMAGED (CABIN)

DURING A GROUND INSPECTION IN SLC, THE PASSENGER DOOR EXIT PLACARD WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EXIT PLACARD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULKHEAD — CORRODED (BS 280)

DURING A C-CHECK IN TUS, THE LOWER LEFT SIDE FS 280 BULKHEAD WEB WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LOWER LEFT SIDE FS 280 BULKHEAD WEB IAW ASA EC EO700-53-0062, REPAIR NR 2. (M)

Part: FLOORBEAM — CRACKED (BS 280)

DURING A C-CHECK IN TUS, THE FS 280 FLOORBEAM WAS FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 280 FLOORBEAM IAW ASA EC EO700-53-0061. (M)

Part: LIGHT — MISSING (GALLEY)

DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTING NEAR THE GALLEY WAS FOUND MISSING. MAINTENANCE INSTALLED THE EMERGENCY FLOOR LIGHT STRIP NEAR THE GALLEY. (K)