N748EV

Part: NONE — CRACKED · airframe 40,677 hrs · 29,706 cycles

CAPTAINS LEFT WINDSHIELD CRACKED INFLIGHT FOLLOWED IMMEDIATELY BY L WSHLD CAUTION MESSAGE. QRH COMPLETED. (FLIGHT 6248 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24711696 WITH THE FOLLOWING CORRECTIVE ACTION: "VERIFIED COMPLETION OF TASK CARD 56-220-1000-SKY FOR CAPTAIN'S WINDSHIELD REPLACEMENT. REFERENCE CHILD CAMP ITEMS FOR OTHER WORK PERFORMED."

Part: NONE — CRACKED · airframe 40,493 hrs · 29,570 cycles

DURING A4 INSPECTION OF THE LH ENGINE INLET, FOUND 2 DENTS WITH CRACKS AT THE 3 AND 5 O' CLOCK POSITIONS, BOTH ARE OUT OF LIMITS. (FILED - CLOSED) REMOVED AND REPLACED LH ENGINE INLET IN REFERENCE TO AMM 71-61-01

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

COMPLY WITH SERVICE BULLETIN TO INCORPORATE PERMANENT REPAIR OF STR3L AT FS 280. (C-CHECK) RO 6/24/2020 SERVICE BULLETIN, FUSELAGE CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00. INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR. VERIFIED ALL STEPS OF REO ARE COMPLIED WITH, WORKED IN CONJUNCTION WITH 20993956. SEE 21143000 FOR MAJOR REPAIR COMPLIANCE. NO FURTHER DEFECTS NOTED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

REINFORCEMENT ANGLE SH670-33119-1 IS CORRODED. (C-CHECK) RO 6/24/2020 REPLACED REINFORCMENT ANGLE WITH NEW REF SRM AND DWG. COMPLIED WITH TASK CARD AND FORM M-337.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

FRAME FS364.00 IS CORRODED AT STR 27. (C-CHECK) RO 6/24/2020 REPAIRED LOWER FRAME SECTOR, FS364 PER REO. SEE CONTINAUATION CARD FOR DETAILS, COMPLIED WITH TASK CARD.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

FOUND CORROSION ON STRINGER SPLICE STR25L AT FS333.00. (C-CHECK) RO 6/24/2020 REPLACED SPLICE AT STR 25L REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

FOUND CORROSION ON CLEAT AT FS349.00 STR20R. (C-CHECK) RO 6/24/2020 INSTALLED NEW CLEAT AT FS349.00 STR 20R IAW DWG, SRM. COMPLIED WITH TASK CARD AND FORM M-337.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

CORROSION FOUND ON CLEAT AT FS333.00 STR20R. (C-CHECK) RO 6/24/2020 INSTALLED NEW CLEAT AT FS333 STR 20R IAW DWG SH670-32014 REV NC, SRM. COMPLIED WITH TASK CARD AND FORM M-337.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

ANGLE FOUND CRACKED ON LOWER SIDE OF RT FS280 CROSSBEAM. (C-CHECK) RO 6/24/2020 INSTALLED NEW ANGLE TO LOWER SIDE OF RT FS280 CROSSBEAM REF SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

FOUND STIFFENER CRACKED AT FWD SIDE OF FS280 BULKHEAD AT LBL26 AT LOWER FASTENER HOLE. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED DAMAGED STIFFENER WITH NEW PN CC670-34117-5. REF SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

ANGLE ATTACHMENT BRACKET CORRODED ON INTERCOSTAL AT FS 349.00 STR 26L. (C-CHECK) RO 6/24/2020 REMOVED CORROSION FROM ANGLE AT FORWARD SIDE OF INTERCOSTAL AT FS349, STR 26L AND FOUND REWORKED AREA TO BE OUT OF LIMITS. REPLACED ANGLE REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

SUSPECTED CORROSION ON FS280 CROSSBEAM UNDER CENTER SPLICE TOP STRAP. (C-CHECK) RO 6/24/2020 REMOVED CORROSION ON FS280 CROSSBEAM. FOUND TO BE OUT OF LIMITS. REPLACED FS280 CROSSBEAM REF SRM, DWG.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

FS 1015 STR 22L CORNER GUSSET CORRODED ON BOTH THE LOWER FWD SIDE AND THE INBD SIDE. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 22L FS 1015 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-003 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

FS 1015 STR 23L CORNER GUSSET CORRODED ON LWR FWD SIDE. (C-CHECK) RO 6/24/2020 INSTALLED NEW GUSSET CLIP PN MM670-36482-003 AT FS 1015 STR 23L REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

FS 1015 STR 24L CORNER GUSSET CORRODED ON LWR FWD SIDE. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 24L FS 1015 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-003 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

COCKPIT FLOOR STRUCTURE LT FLOORBEAM AT LBL 12.00, SUSPECT CRACK AT APPROX FS280. (C-CHECK) RO 6/24/2020 CUT AWAY DAMAGED SECTION OF FLOORBEAM AND INSTALLED REPAIR PER SRM. COMPLIED WITH TASK CARD.

Part: HOUSING — CRACKED (LE SLAT) · airframe 37,144 hrs · 27,106 cycles

SLAT TRACK HOUSING CRACKED IN FUEL TANK OF RIGHT WING UNDER PANEL LOCATION 651BB. (C-CHECK) RO 6/24/2020 REPAIRED CRACK AT THE SLAT TRACK HOUSING ON THE RT WING UNDER PANEL 651BB REF REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

RT SIDE SEAT MARKED WITH RED GREASE PEN RAIL AT APPROX 669+40 TO FS740 2ND FWD OF EMER EXIT HAS MULTI AREAS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED RT SIDE SEAT TRACK AT FS 675 TO FS 713 REF AMM. FABRICATED NEW SEAT TRACK FROM P/N N126-2075 PO T-52211 REF SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

COCKPIT FLOOR STRUCTURE RT FLOORBEAM AT RBL 12.00, SUSPECT CRACK AT APPROX FS280 (C-CHECK) RO 6/24/2020 CUT AWAY DAMAGED SECTION OF FLOORBEAM AND INSTALLED NEW FLOORBEAM SECTION AND REPAIR PARTS PER SRM. COMPLIED WITH TASK CARD.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 37,144 hrs · 27,106 cycles

CABIN FLOORBOARD 271GLF CRACKED. (PN: SH670-32593-11) (C-CHECK) RO 6/24/2020 ORDERED/RECEIVED NEW CABIN FLOOR PANEL 271GLF PN SH670-32593-13. SEE TRANS 20927305 FOR INSTALLATION.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

AVIONICS BAY DOOR SURROUND INTERCOSTAL TO THE RIGHT SIDE OF STR 27 BETWEEN FS349 AND FS364 HAS CORROSION. (C-CHECK) RO 6/24/2020 REPLACED RT INTERCOSTAL AT AVIONICS BAY DOOR CUTOUT PER SRM & DRAWING. SEE CONTINUATION CARD FOR SETAILS. COMPLIED WITH TASK CARD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 21L FS 1031 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 21L FS 1031 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-007 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 26R FS 1031 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 26R FS 1031 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN. MM670-36482-008 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: POST — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

FS280 BULKHEAD DOOR POST RIGHT SIDE HAS CORROSION AT FLOOR LEVEL. (C-CHECK) RO 6/24/2020 CUT AWAY DAMAGE AND INSTALLED 2 EA REPAIR ANGLES PER SRM COMPLIED WITH TASK CARD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 19L FS 1051 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 REPLACED STR 19L FS1051 STRINGER CLEAT WITH NEW REF REO.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 20L FS 1047 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 REPLACED ST 20L FS1047 STRINGER CLEAT WITH NEW REF REO. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

LT SIDE SEAT RAIL JUST FWD OF EMER EXIT HAS MULT AREAS OF CORROSION. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED LT SIDE SEAT RAIL FORWARD OF EMER EXIT REF AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

THE SEAT TRACK AT RBL9.00 FROM FS485.00 TO FS581.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED SEAT TRACK AT RBL 9 BETWEEN FS 485.00 TO FS 581.00 REF AMM. FABRICATED SEAT TRACK FROM P/N N126-2075 PO T-52211 REF SRM.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 22L FS 1000 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 22L FS 1000 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-003 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

THE SEAT TRACK AT LBL9.00 FROM FS485.00 TO FS581.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED SEAT TRACK AT RBL 9 FROM FS 485 TO FS 581 REF AMM. FABRICATED SEAT FROM P/N N126-2075 PO T-52211 REF SRM.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 24L FS 1000 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 24L FS 1000 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-003 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 21L FS 1015 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 21L FS 1015 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-003 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 26L FS 989 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 26L FS 989 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-004 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

LT SIDE SEAT RAIL AT APROX FS 865 TO FS 953 (2ND-FWD. OF CARGO DOOR) HAS AREAS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED LT SIDE SEAT RAIL FROM FS 865 TO FS 953 REF AMM. FABRICATED SEAT TRACK FROM P/N N126-2075 PO T-52211 REF SRM.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 20L FS 1031 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 20L FS 1031 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-005 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

RBL9 SEAT TRACK FROM FS 280 TO FS 477 CORRODED AT APROX FS 409 -FS 421. (C-CHECK) RO 6/24/2020 REPLACED SEAT TRACK AT RBL 9 FROM FS 350 TO FS 485 REF AMM. FABRICATED SEAT TRACK FROM P/N N126-2075 PO T52211 REF SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

RT SIDE SEAT RAIL AT APROX FS740 TO 773 (1ST FWD OF EMER EXIT) HAS CORROSION. (C-CHECK) RO 6/24/2020 REPLACED RT SIDE SEAT RAIL FROM FS 740 TO FS 773 REF AMM. FABRICATED SEAT TRACK WITH P/N N126-2075 PO R52211 REF SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

THE FRAME AT FS549.00 HAS CORROSION AT APPROX STRINGER 18L. (C-CHECK) RO 6/24/2020 CUT, REMOVED AND SPLICED IN REPAIR FRAME AT FS 549.00 AT STR 18L REF REO AND SRM'S. COMPLIED WITH TASK CARD. NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

LT SIDE SEAT RAIL AT APPROX FS 669+40 TO FS 740 ( 2ND FWD OF EMER EXIT) HAS MULT AREAS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED LT SIDE SEAT RAIL AT FS 675 TO FS 713 REF AMM. FABRICATED NEW SEAT TRACK FROM P/N N126-2075 PO T-52211 REF SRM.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 22 FS 1031 CORNER BRACKET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 22L FS 1031 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-007 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

RT SIDE WALL SEAT RAIL FROM APROX FS 575 -FS 674, CORRODED AT APROX FS 581 AND GOUGED AT APROX FS 665. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED RT SEAT RAIL FROM APPROX FS 575 TO FS 674, REF AMM.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 23L FS 1031 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 23L FS 1031 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-007 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

PASSENGER DOOR SURROUND STRUCTURE LINTEL, STR 3L: SUSPECT CRACK AT THE FS280-FS282 CIRCUMFERENTIAL JOINT. (C-CHECK) RO 6/24/2020 CUT AWAY DAMAGE AND INSTALLED TEMPORARY REPAIR OF STR 3L AT FS 280 PER SRM AND SB, REFER TO 21142347 FOR COMPLETE SB INCORPORATION, AND PERMANENT REPAIR OF STR 3L. COMPLIED WITH TASK CARD. NO DEFECTS NOTED.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

THE RT PRESSURE FLOOR SILL HAS CORROSION AT FS797.00. (C-CHECK) RO 6/24/2020 REPAIRED DAMAGED AREA REF REO AND COMPLIED WITH ALL STEPS. COMPLIED WITH TASK CARD AND FORM M-337.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

THE SEAT TRACK SECTION AT LBL9.00 FROM FS581.00 TO APPROX FS693.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED SEAT TRACK AT LBL 9 BETWEEN FS 581.00 TO FS 693.00 REF AMM. FABRICATED NEW SEAT FROM P/N N126-2075 PO T-52211 REF SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

THE FRAME AT FS565.00 HAS CORROSION AT APPROX STRINGER 18L. (C-CHECK) RO 6/24/2020 COMPLIED WITH FRAME SPLICE REPAIR REF REO AND SRM. COMPLIED WITH TASK CARD AND FORM M-337.

Part: POST — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

FS280 BULKHEAD DOOR POST LEFT SIDE HAS CORROSION AT FLOOR LEVEL. (C-CHECK) RO 6/24/2020 CUT AWAY DAMAGE AND INSTALLED 2 EA REPAIR ANGLES PER SRM. C/W WITH TASK CARD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 20L FS 1015 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 20L FS 1015 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-003 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 19L FS 1047 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 REPLACED STR 19L FS1047 STRINGER CLEAT WITH NEW REF REO. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

LT SIDE SEAT RAIL AT APROX FS 785.15 TO FS 865 HAS AREAS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED LT SIDE SEAT RAIL BETWEEN FS 785.15 TO FS 865.00 REF AMM. FABRICATED FROM N126-2075 PO T52211 REF SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

THE PRESSURE FLOOR IS CRACKED BETWEEN BL0 AND RBL9.00 BETWEEN FS736.00 AND FS752.50. (C-CHECK) RO 6/24/2020 REPAIRED PRESSURE FLOOR CRACK BETWEEN BL 0 AND RBL 9.00 BETWEEN FS 736.00 AND FS 752.50 AS PER REO. COMPLIED WITH TASK CARD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 19R FS 1051 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED CLIP CORROSION BEYOND 30% OUT OF LIMITS PER SRM AT STR 19R FS1051.30. INSTALLED NEW CLIP PN SH670-36482-16 AND HARDWARE WET WITH SEALANT. REF REO AND ENG DWG. COMPLIED WITH SKYWEST TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

THE SEAT TRACK SECTION AT LBL27.00 FROM FS485.00 TO APPROX FS501.00 HAS CORROSION. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED SEAT TRACK SECTION AT LBL 27 FROM FS 485 TO APPROX FS501, REF AMM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

CLIP AT STR 27 ON THE FORWARD SIDE OF THE FS265.00 FRAME IS CORRODED. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED CLIP AT STR 27 FORWARD SIDE OF FS265.00 REFERENCING APPLICABLE STEPS OF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 24L FS 1031 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 24L FS 1031 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-007 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 25L FS 1000 CORNER GUSSET CORRODED, CHECK AREAS IMMEDIATELY ADJACENT. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 25L FS 1000 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-003 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: PLATE — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

THE FWD CARGO PLATE BETWEEN FS581.00 AND FS597.00 AND STRINGER 23L AND 22L HAS CORROSION. (C-CHECK) RO 6/24/2020 REMOVED CORROSION ON FWD CARGO PLATE BETWEEN FS581.00 AND FS597.00 BETWEEN STR 23L AND STR 22L REF REO. COMPLIED WITH ALL STEPS.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 25L FS 1031 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 25L FS 1031 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-008 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STR 23L FS 1000 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 23L FS 1000 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-003 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

THE SEAT TRACK SECTION AT RBL9.00 FROM FS581.00 TO APPROX FS693.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED SEAT TRACK AT RBL 9 BETWEEN FS 581 TO FS 693 REF AMM. FABRICATED SEAT TRACK FROM P/N N126-2075 PO T-52211 REF SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

CLIP FOR INTERCOSTAL STR 20R, APPROX FS319, HAS CORROSION. (C-CHECK) RO 6/24/2020 CLIP FOR INTERCOSTAL STR 20R, APPROX FS319 P/N SH670-32046-3 IS OUT OF LIMITS OF SRM, REPLACED IAW SRM & DWG C/W TASK CARD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STRINGER, STR 21R, BETWEEN FS349 AND FS379 IS CORRODED. (C-CHECK) RO 6/24/2020 REPLACED STRINGER 21R, FS333-379 PER SRM & DRAWING. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

INBOARD TRACK MOUNTS FOR GALLEY 2 ARE CORRODED (2EA). (C-CHECK) RO 6/24/2020 REPLACED 2EA INBOARD TRACK MOUNTS SEAT TRACK, FITTING ASSY P/N CP0748364 FOR GALLEY 2 AT RBL 9.07 BETWEEN FS354 AND FS375 REF AMM FOR COMPLETE DETAILS OF WORK PERFORMED SEE ATTACHED CONTINUATION CARD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STRINGER, STR 26L, BETWEEN FS280 AND FS333 SPLICE CORRODED. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED WITH NEW STRINGER 26L FROM FS280-FS333 REF SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

COCKPIT FLOOR SUPPORT ANGLE AT APPROX FS280 HAS CORROSION. (C-CHECK) RO 6/24/2020 REMOVED CORROSION ON COCKPIT FLOOR SUPPORT ANGLE AT APPROX FS280. REF SRM DAMAGE IS OUT OF LIMITS. INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE. REF SRM, DWG. SEE CONTINUATION FOR DETAILS. COMPLIED WITH CARD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

PAX DOOR SURROUND BACK-UP SILL AT STR 21L, BETWEEN FS333 AND FS349 HAS CORROSION. (C-CHECK) RO 6/24/2020 REPLACED PAX DOOR SURROUND BACK-UP SILL PER SRM, DRAWING. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

AVIONICS BAY DOOR SURROUND INTERCOSTAL STR 26L, BETWEEN FS349 AND FS364 HAS CORROSION. (C-CHECK) RO 6/24/2020 REMOVED CORROSION AND FOUND REWORKED AREA TO BE OUT OF LIMITS. REPLACED INTERCOSTAL AT STR 26L, FS349 - FS364 REF SRM, DWG. COMPLIED WITH TASK CARD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

INTERCOSTAL, STR 20R, BETWEEN FS310 AND FS319 HAS CORROSION. (C-CHECK) RO 6/24/2020 REPLACED INTERCOSTAL STR 20R BETWEEN FS310 AND FS319 WITH NEW PART REF SRM AND DRAWING.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

PAX DOOR SURROUND BACK-UP SILL AT STR 21L, BETWEEN FS310 AND FS319 HAS CORROSION. (C-CHECK) RO 6/24/2020 REPLACED PAX DOOR BACK-UP SILL PER SRM, DRAWING SH670-31810 REV Y, DRAWING. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD AND FORM M-337.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STRINGER, STR 25L, BETWEEN FS295 AND FS333 SPLICE: CORRODED. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED WITH NEW STRINGER 25L FROM FS280-FS333 REF SRM DRAWING. RESTORED FINISH. PRESSURE CHECK GOOD.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

FLOORBEAM BRACKET AT RT SILL, FS319, HAS CORROSION. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED FLOORBEAM BRACKET (P/N SH670-31990-1) AT RT SILL FS319 WITH NEW HARDWARE. REF DWG AND SRM. COMPLIED WITH TASK CARD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

INTERCOSTAL, STR 20R, BETWEEN FS319 AND FS333 HAS CORROSION. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED INTERCOSTAL P/N SH670-32004-1. REF SRM AND DRAWING. COMPLIED WITH ALL STEPS OF TASK CARD.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

AVIONICS BAY DOOR SURROUND LONGERON STR 25R: CORRODED BETWEEN FS333 AND FS349. (C-CHECK) RO 6/24/2020 REPLACED AVIONICS BAY DOOR LONGERON AT STRINGER 25R PER SRM & DRAWING. COMPLIED WITH TASK CARD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

AVIONICS BAY DOOR SURROUND INTERCOSTAL STR 26R, BETWEEN FS349 AND FS364 HAS CORROSION. (C-CHECK) RO 6/24/2020 REMOVED CORROSION FROM STR 26R, FS349 - FS364 AND FOUND REWORKED AREA TO BE OUT OF LIMITS. REPLACED INTERCOSTAL REF SRM AND DWG. COMPLIED WITH TASK CARD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STRINGER, STR 24R, BETWEEN FS333 AND FS349 HAS CORROSION. (C-CHECK) RO 6/24/2020 CUT AWAY DAMAGED SECTION OF STRINGER AT FS333.00 STR 24R BETWEEN FS349.00 AND FS364.00 AND INSTALLED NEW SECTION OF STRINGER. REF SRM. COMPLIED WITH ALL STEPS OF TASK CARD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

FRAME, FS349, HAS CORROSION BETWEEN STR 25L AND STR 26R. (C-CHECK) RO 6/24/2020 REPLACED FRAME SECTOR AT FS349 PER SRM & DRAWING. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD AND FORM M-337.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STRINGER, STR 25R, BETWEEN FS295 AND FS333 SPLICE: CORRODED. (C-CHECK) RO 6/24/2020 REPLACED STRINGER 25R PER SRM, DRAWING. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

AVIONICS BAY DOOR SURROUND LONGERON STR 25L: CORROSION ON AND AROUND FASTENERS BETWEEN FS333 AND FS349. (C-CHECK) RO 6/24/2020 INSTALLED NEW LONGRON AT STR 25L BETWEEN FS 333.00 TO 364.00 REF SRM AND DRAWING. PRESSURE CHECKS GOOD.

Part: FITTING — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

CLIP FOR INTERCOSTAL STR 20R, APPROX FS333, HAS CORROSION. (C-CHECK) RO 6/24/2020 CLIP FOR INTERCOSTAL STR 20R, APPROX FS333 OUT OF LIMITS OF SRM, REPLACED WITH NEW CLIP P/N SH670-32014-2 IAW DWG, & SRM C/W TASK CARD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

STRINGER, STR 26R BETWEEN FS333 SPLICE AND FS364 FRAME HAS CORROSION. (C-CHECK) RO 6/24/2020 REPLACED STRINGER 26R FS333-364 REF SRM, AND DWG. COMPLIED WITH TASK CARD. NO LEAKS NOTED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

AVIONICS BAY DOOR SURROUND INTERCOSTAL TO THE LEFT SIDE OF STR 27 BETWEEN FS349 AND FS364 HAS CORROSION. (C-CHECK) RO 6/24/2020 REPLACED LT INTERCOSTAL AT LT AVIONICS BAY DOOR CUTOUT PER SRM & DRAWING. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

FUSELAGE LOWER SKIN, IN THE AREA OF THE AFT WASTE WATER SERVICING PANEL: THERE IS CORROSION ON AND AROUND MULTIPLE RIVETS. (C-CHECK) RO 6/24/2020 REPAIRED LOWER SKIN PANEL AT APPROXIMATELY FS939.00 TO FS969.00, STRINGER 23R-25R, PER REO. ALL STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

FUSELAGE LOWER SKIN, IN THE AREA OF THE AFT POTABLE WATER SERVICING PANEL: THERE IS CORROSION ON AND AROUND MULTIPLE RIVETS. (C-CHECK) RO 6/24/2020 REPAIRED CORROSION AT LOWER FUSELAGE SKIN, FS939.00 - FS969.00 STRINGER 23L-24L PER REO. ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

RT FORWARD EQUIPMENT COMPARTMENT (TRU BAY) DOUBLER UNDER ADG STOW PUMP CRACKED AT APPROXIMATELY FS 193. (C-CHECK) RO 6/24/2020 COMPLIED WITH REPAIR OF RH TRU BAY DOUBLER UNDER ADG STOW PUMP AS PER REO TASK CARD COMPLIED WITH.

Part: FAIRING — CRACKED (PAX DOOR) · airframe 37,144 hrs · 27,106 cycles

PAX DOOR HINGE FAIRING 141AL IS CRACKED. (C-CHECK) RO 6/24/2020 ORDERED, RECEIVED AND LOCATED/DRILLED NEW PAX DOOR HINGE FAIRING 141AL REF SRM. SEE JOB 710158105 & 20979966 FOR FAIRING INSTALLATION.

Part: MOUNT BOLT — CORRODED (TE FLAP VANE) · airframe 37,144 hrs · 27,106 cycles

RIGHT WING INBOARD FLAP, INBOARD FLAP VANE UPPER MOUNT BOLTS ARE CORRODED. (C-CHECK) RO 6/24/2020 REMOVED AND INSTALLED WITH NEW FROM STOCK 2EA BOLTS PN THE RT WING INBOARD FLAP INBOARD FLAP VANE UPPER MOUNT REF AMM.

Part: HINGE — GOUGED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

PASSENGED DOOR PIANO HINGE ON FUSELAGE SIDE HAS A GOUGE ON THE AFT LUG LAND (27TH LUG), (C-CHECK) RO 6/24/2020 REPLACED PASSENGER DOOR PIANO HINGE(FUSELAGE SID) REF SRM DWG. COMPLIED WITH TASK CARD AND FORM M-337.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,144 hrs · 27,106 cycles

CORROSION FOUND ON PAX DOOR INTERCOSTAL DD4 AT APPROX FS320.163. (C-CHECK) RO 6/24/2020 BLENDED OUT DAMAGE AND RESTORED FINISH TO INTERCOSTAL DD4. REF SRM AND INSTALLED 2 EA FASTENERS IN REPAIR AREA PER REO. COMPLIED WITH TASK CARD AND M-337.

Part: BEAM — GOUGED (CARGO DOOR) · airframe 37,144 hrs · 27,106 cycles

AFT BAGGAGE BAY DOOR LOWER BEAM GOUGED. (C-CHECK) RO 6/24/2020 REPLACED AFT CARGO LOWER BEAM PER SRM & DRAWING. COMPLIED WITH TASK CARD.

Part: FASTENER — CORRODED (PAX DOOR) · airframe 37,144 hrs · 27,106 cycles

PASSENGER DOOR LATCH MECHANISM HAS MULTIPLE (7 EACH) CORRODED HARDWARE ON MULTIPLE COMPONENTS. (C-CHECK) RO 6/24/2020 REMOVED AND INSTALLED NEW HARDWARE ON MULTIPLE COMPONENTS AT PASSENGER DOOR LATCH MECHANISM REFERENCE AMM.

Part: BEARING — WORN (RT ELEVATOR) · airframe 37,144 hrs · 27,106 cycles

RT ELEVATOR REMOVED (CANN), FOUND NR 4 HINGE ASSEMBLY COMPONENTS BUSHINGS, BEARINGS, HARDWARE WORN BEYOND SERVICEABLE LIMITS. FAILED BACKLASH TESTS. (C-CHECK) RO 6/24/2020 REPLACED THE RT ELEVATOR NR 4 HINGE BEARINGS AS PER AMM. ORDERED AND RECEIVED NEW BUSHINGS. REPLACEMENT OF BUSHINGS AND HARDWARE ACCOMPLISHED ON ELEVATOR INSTALLATION 20970094.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 37,144 hrs · 27,106 cycles

RT ELEVATOR REMOVED (CANN), FOUND NR 3 HINGE ASSEMBLY COMPONENTS BUSHINGS, BEARINGS, HARDWARE. WORN BEYOND SERVICEABLE LIMITS. FAILED BACKLASH. (C-CHECK) RO 6/24/2020 REPLACED NR 3 HINGE ASSY BEARINGS AS PER SRM. ORDERED AND RECEIVED NEW BUSHINGS. REPLACEMENT OF BUSHINGS AND HARDWARE ACCOMPLISHED ON ELEVATOR INSTALLATION 20970094.

Part: BEARING — WORN (RT ELEVATOR) · airframe 37,144 hrs · 27,106 cycles

RT ELEVATOR REMOVED (CANN ), FOUND NR 2 HINGE ASSEMBLY COMPONENTS BUSHINGS, BEARINGS, HARDWARE. WORN BEYOND SERVICEABLE LIMITS. FAILED BACKLASH. (C-CHECK) RO 6/24/2020 REPLACED RT ELEVATOR NR 2 HINGE BEARINGS REF AMM. ORDERED AND RECEIVED NEW BUSHINGS. REPLACEMENT OF BUSHINGS AND HARDWARE ACCOMPLISHED ON ELEVATOR INSTALLATION 20970094.

Part: BEARING — WORN (RT ELEVATOR) · airframe 37,144 hrs · 27,106 cycles

RT ELEVATOR REMOVED FOR CANN. PKG 60 BORESCOPE INSPECTION REF TASK CARD, FOUND INBOARD HINGE NR 1 WORN BEYOND LIMITS BUSHINGS, BEARINGS, HARDWARE FAILED BACK LASH CHECKS. (C-CHECK) RO 6/24/2020 RT ELEVATOR HINGE NR 1 BEARINGS REPLACED AS PER AMM. ORDERED AND RECEIVED NEW BUSHINGS. REPLACEMENT OF BUSHINGS AND HARDWARE ACCOMPLISHED ON ELEVATOR INSTALLATION 20970094.

Part: RETAINER — CHAFED (CARGO DOOR) · airframe 37,144 hrs · 27,106 cycles

FWD BAG BAY DOOR SEAL RETAINER IS BENT AND CHAFED ON LWR FWD AND AFT CORNERS. (C-CHECK) RO 6/24/2020 REPLACED FWD BAGGAGE BAY DOOR SEAL RETAINER PER SRM. SEE MX TRANS 21131934 FOR CORRECTION TO LEAK CHECK FAILURE DURING PRESSURIZATION.

Part: SKIN — DENTED (TE FLAP) · airframe 37,144 hrs · 27,106 cycles

EVALUATE 2 DENTS ON RIGHT INBD FLAP, MIDDLE TOP SIDE. (C-CHECK) RO 6/24/2020 COMPLIED WTIH RT INBD FLAP DENT REPAIRS ON MIDDLE TOP SIDE AS PER REO. COMPLIED WITH M-337 AND TASK CARD.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

EVALUATE SEVERAL DENTS OUTLINED AFT AND BELOW THE GROUND AIR SERVICE DOOR. (C-CHECK) RO 6/24/2020 REPAIRED DENTED AREA ON AFT FUSELAGE LOWER SKIN NEAR/AROUND GROUND AIR SERVICE DOOR PER REO. COMPLIED WITH TASK CARD.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

EVALUATE DENT BETWEEN FS 280-295 AND STRINGER 25-26R. (C-CHECK) RO 6/24/2020 PERFORMED ALL STEPS OF REO PRESSURE CHECK GOOD. RESTORED FINISH.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 37,144 hrs · 27,106 cycles

POSSIBLE CRACK AT ATTACHING ANGLE WHERE THE VERTICAL STAB AND FUSELAGE MEET APPROXIMATELY 67.5 SPAR DATUM AREA. (MARKED, OUT OF SCOPE) (C-CHECK) RO 6/24/2020 REPAIRED CRACK AT ATTACHING ANGLE WHERE THE VERTICAL STAB AND FUSELAGE MEET. APPROX 67.5 SPAR DATUM AS PER SRM. TASK CARD COMPLIED WITH.

Part: SKIN — DENTED (TE FLAP) · airframe 37,144 hrs · 27,106 cycles

EVALUATE 2 DENTS ON THE LEFT INBD FLAP, INBD BOTTOM SIDE. ( TIRE PLANE OF ROTATION) (C-CHECK) RO 6/24/2020 REPAIRED 2 DENTS ON THE LEFT INBD FLAP, INBD BOTTOM SIDE AS PER REO. OPS CHECK GOOD REF AMM. M-337 AND TASK CARD COMPLIED WITH.

Part: SKIN — DENTED (TE FLAP) · airframe 37,144 hrs · 27,106 cycles

EVALUATE SEVERAL DENTS ON RIGHT INBD FLAP, BOTTOM INBD SIDE (TIRE PLANE OF ROTATION). (C-CHECK) RO 6/24/2020 REPAIRED DENTS ON THE RT I/B FLAP REF SRM. OPS CHECK GOOD REF AMM.

Part: SEAL REST — BENT (PAX DOORWAY) · 24,438 cycles

THE PASSENGER DOOR SEAL LANDING WAS BENT. REPAIRED THE SEAL LANDING IAW REO 0-53-21-1569.

Part: SKIN — DENTED (LT NACELLE) · 24,438 cycles

LEFT ENGINE LOWER FAN COWL WAS DENTED. REPAIRED THE SKIN IAW REO 670-54-14-1012.

Part: STRUCTURE — DENTED (BS 517-520) · 24,438 cycles

DENTS FOUND APPROXIMATELY BS 517 - 520, STRINGER 14L. REPAIRED.

Part: SKIN — DAMAGED (BS 1126) · 24,438 cycles

SKIN DAMAGED AT BS 1126. REPAIRED THE SKIN IAW REO 670-51-00-085.

Part: SKIN — DAMAGED (PAX DOOR) · 24,438 cycles

PAX DOOR OUTTER SKIN TOP PORTION WAS DAMAGED. REPAIRED PAX DOOR SKIN IAW REO 670-52-11-1044.

Part: STRUCTURE — DENTED (BS 515) · 24,438 cycles

LEFT SIDE OF FUSELAGE, BS 515 WAS DENTED. REPAIRED .

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,587 hrs · 24,180 cycles

OVERHEAD EMERGENCY FLOOD LIGHT AT ROWS 16 AND 18 INOP. RELAMPED OVERHEAD EMERGENCY FLOOD LIGHTS AT ROW 16 AND 18 IAW AMM 33-51-09. OPS CHECK GOOD.

Part: HINGE — GOUGED (PAX DOOR) · airframe 31,045 hrs · 22,160 cycles

PAX DOOR AFT LUG FUSELAGE SIDE GOUGED DUE TO A MIGRATED ROLL PIN. REPAIRED THE LUG LAND IAW EC/TC REO 670-53-21-582, AND REO 675-53-21-582.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,045 hrs · 22,160 cycles

FRAME 319.70 IS CORRODED AT STGR 26R. BLENDED CORROSION AND RESTORED FINISH IAW REO 670-53-21-1308 AND EC/TC EO700-53-10-00035.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,045 hrs · 22,160 cycles

FRAME 310 IS CORRODED AT STGR 26R. BLENDED CORROSION AND RESTORED FINISH IAW REO 670-53-21-1308 AND EC/TC EO700-53-10-00034.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 31,045 hrs · 22,160 cycles

AVIONICS FLOOR PANEL 141 ALF SUPPORT CORRODED ON AFT SIDE OF FS 280.00. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01,51-42-21-001-001-A01,51-42-13-001-001-A01.

Part: SKIN — CORRODED (PAX DOOR) · airframe 31,045 hrs · 22,160 cycles

PAX DOOR INTERNAL SKIN CORRODED AT LOWER SECTION (DOOR OPEN) AND AROUND SEVERAL PANEL ACCESS HOLES ON FWD SIDE OF DOOR. REMOVED AND REPLACED PAX DOOR SKIN IAW SRM 51-42-06-001-001-A01,51-42-13-001-001-A01 AND 51-42-14-001-001-A01. P/N 601R318024-15S. DRAWING 601R318024.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,045 hrs · 22,160 cycles

STRINGER 26R CORRODED AT FS 280-295. REMOVED CORRODED STRINGER AND THREE CORRODED CLEATS. INSTALLED NEW STRINGER AND CLEATS IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-24-001-001-A01. RESTORED FINISH AND CIC IAW SRM 51-25-00-001-001-A01 AND 51-21-11-001-001-A01.

Part: RETAINER — DENTED (CARGO DOOR) · airframe 31,045 hrs · 22,160 cycles

FWD BAGGAGE BAY DOOR BOTH FWD AND AFT CORNERS DENT ON SEAL RETAINERS. COMPLIED WITH EC/TC REO 670-52-35-127 01 AND REO 670-52-35-127 FOR REPAIR OF CARGO DOOR.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 31,045 hrs · 22,160 cycles

CORROSION FOUND ON THE EXTERNAL SKIN UNDER THE TCAS ANTENNA. BLENDED SKIN UNDER LOWER TCAS ANTENNA, NDT FOUND .001' MATERIAL REMOVED, NO DAMAGE ALLOWED IN THIS AREA IAW SRM 53-21-01-101-002 A01. SUBMITTED TO STS ENGINEERING. COMPLIED WITH EA 43-2017-019 AND EC/TC/EA 43-2017-019.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 31,045 hrs · 22,160 cycles

COCKPIT FLOORBEAM, AFT SIDE CORRODED AT BS 280. REMOVED AND REPLACED THE COCKPIT FLOORBEAM ANGLE IAW SRM 51-42-06-001-A01, AND SRM 51-42-20-001-001-A01.

Part: SKIN — DENTED (RUDDER) · airframe 31,045 hrs · 22,160 cycles

DENT ON RT SIDE OF RUDDER APPROX 1 FOOT ABOVE THE CENTER HINGE POINT 8 INCHES AFT OF THE LEADING EDGE. REPAIRED RUDDER SKIN IAW EO 700-55-40-00001 DISCREPANT AREA WAS CUT OUT. PERFORMED NDT TO ENSURE CRACK FREE. FABRICATED THEN INSTALLED DOUBLER. CLASSIFIED AS A MAJOR REPAIR

Part: FITTING — CORRODED (FUSELAGE) · airframe 31,045 hrs · 22,160 cycles

SERVICE DOOR LOWER SEAL STRIKER CORRODED AROUND THRESHOLD FASTENER HOLES. REMOVED AND INSTALLED NEW SERVICEABLE SEAL STRIKER FITTING IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. ALL DEFECTS CORRECTED.

Part: HINGE — GOUGED (PA XDOOR) · airframe 31,045 hrs · 22,160 cycles

PAX DOOR HINGE (DOOR SIDE) HAS GOUGES ON LUGS 1, 2, 3, 24, 25. BLENDED LUGS CHAFFED AREAS IAW REO 670-52-11-511 AND ECTC REO 670-52-11-511.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 31,045 hrs · 22,160 cycles

FOUND LOWER CENTER NUT PLATE CHANNEL CORRODED PANELS 196DR/195DL. REMOVED AND REPLACED STRIPING ASSEMBLY AND INSTALLED 2 EA CHANNELS IAW SRM 51-42-14-001-001- A01,51-40-11-001-001 A01, 51-23-00-001-001 A01, 51-41-02-001-001 A01 AND DWG CC670-39302.

Part: RISER — CORRODED (PAX DOOR) · airframe 31,045 hrs · 22,160 cycles

PAX DOOR FWD RISER PANEL SKIN CORRODED UPPER AND LOWER SECTIONS. REMOVED AND REPLACED THE RISER IAW SRM 52-11-04-101-001 A01, 51-42-06-001-001 A01, 51-42-13-001-001 A01, 51-42-21-001-001 A01, 51-42-15-001-001 A01, ESPM 20-24-00, AND DWG 601R312071.

Part: FLOOR SUPPORT — CORRODED (BS 975-1000) · airframe 31,045 hrs · 22,160 cycles

LEFT FLOOR SUPPORT CORRODED BETWEEN BS 985-1000. BLENDED CORRODED AREA IAW REO 670-53-00-390, AND ECTC REO 670-53-00-390.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,896 hrs · 20,480 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. INSTALLED NEW FLASHLIGHT ON CAPT'S SIDE IAW AMM 25-61-02. OPS CHECK GOOD. ACFT OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1051) · airframe 28,622 hrs · 20,273 cycles

FLOOR SUPPORT LBL 27, BS 1015 - 1051 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43-001-A01. RECEIVED AND COMPLIED WITH EC/TC FOR FLOORBEAM REPAIR AND EO 700-53-0284, REV 0.

Part: FRAME — CRACKED (BS 855) · airframe 28,622 hrs · 20,273 cycles

PERFORM HFEC INSPECTION FOR ALL MACHINED PARTS IN SUPPORT OF SB 670BA-25-094. CRACK CHECK ON SIDE TRACK CUTOUT AT FS 855.5 RT, SIDE TRACK CUTOUT AT FS 859.5 RT, SIDE TRACK CUT-OUT AT FS 961 RT, SIDE TRACK CUTOUT AT FS 855.5 LT, SIDE TRACK CUTOUT AT FS 869.5 LT, SIDE TRACK CUTOUT AT FS 961 LT, TRIMOUT OF INTERCOSTAL AT STR 12R BETWEEN FS 953-969. ET INSP REF NDTM 51-20-006-250-A01. NO DEFECTS NOTED BEYOND CUTLINE.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1051) · airframe 28,622 hrs · 20,273 cycles

FLOOR SUPPORT LBL 9, BS 1031 - 1051 CORRODED. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-61-43-101-001-A01. C/W EC/TC EO 700-53-0285 AND GREO 670-53-00-029, REV A.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,923 hrs · 19,726 cycles

12 AB LOWER EXIT SIGN HAD ONE BULB BURNED OUT. REPLACED THE BULB IAW 33-51-II. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,334 hrs · 19,265 cycles

12 AB LOWER EXIT SIGN HAVE ONE LIGHT BULB BURNED. R & R THE BULB IAW AMM 33-51-05, OPS CHECKED GOOD.

Part: MEGAPHONE — UNKNOWN (CABIN) · airframe 26,836 hrs · 18,883 cycles

CABIN MEGAPHONE REQUIRES REPLACEMENT. R & R CABIN MEGAPHONE IAW AMM 25-61-14 AND AIPC REF 25-61-14, FIG 1C, ITEM 5.

Part: BULB — UNSECURE (EMERGENCY LIGHT) · airframe 25,288 hrs · 17,666 cycles

AFT MOST EMERGENCY LIGHT IN THE CABIN CELING IS INOPERATIVE. RESEATED BULB . OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 25,288 hrs · 17,666 cycles

EMERGENCY LIGHT NR 1 BATTERY HAS TWO WIRES PULLED OUT OF CONNECTOR P535P1 INSTALLED NEW SPLICE AT IAW ESPM 20-44-00. OPS CHECK GOOD IAW AMM 33-51-00-710-801.

Part: COVER — MISINSTALLED (SEAT BACK) · airframe 25,288 hrs · 17,666 cycles

SEATS 11CD AND 5AB RETURNED FROM REFURB WITH SEAT BACK COVER IN WRONG LOCATION SWAPPED SEAT BACK COVERS FM 11CD T 5AB IAW C&D ZODIAC CMM 25-21-69. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: STRUCTURE — LOOSE · airframe 25,297 hrs · 17,677 cycles

WARDROBE HAS TRIM PULLED LOOSE. BONDED LOOSE TRIM ON WARDROBE AS REQUIRED C&D RPM 25-6000-1 AND SRM 51-22-00-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 374-390) · airframe 25,288 hrs · 17,666 cycles

LT SIDE FLOOR SEAT TRACK CORRODED AT BS 374-390. R & R SEAT TRACK AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: FLOORBEAM — CRACKED · airframe 25,288 hrs · 17,666 cycles

COCKPIT FLOORBEAM ANGLE RBL 9 CRACKED. REMOVED ANGLE IAW SRM 51-42-06-001-002. INSTALLED ANGLE IAW SRM 51-42-06-001-001 AND DWG CC670-33052.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 25,288 hrs · 17,666 cycles

COCKPIT FLOOR SUPPORT ANGLE LBL 9 CRACKED. REMOVED THE LT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED DRILLED, TREATED, PRIMED AND RESTORED FINISH TO BE NEW SUPPORT ANGLE IAW SRMS 51-40-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. INSTALLED THE NEW FLOOR SUPORT ANGLE IA DWG CC670-3319 AND SRM DA162274 51-42-06-001-001-A01.

Part: FLOORBEAM — DAMAGED (BS 280) · airframe 25,288 hrs · 17,666 cycles

FOUND BS 280 FLOORBEAM ANGLE TO HAVE OVERSIZED FASTENER HOLES. REMOVED AND REPLACED IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 724-761) · airframe 25,288 hrs · 17,666 cycles

LEFT SIDE SEAT TRACK CORRODED BS 724 - 761.85. REMOVED CORRODED SIDE 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 645-724) · airframe 25,288 hrs · 17,666 cycles

RIGHT SIDE SEAT TRACK CORRODED AT BS 645 - 724.08. REPAIRED IAW GREO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 25,288 hrs · 17,666 cycles

RIGHT SIDE SEAT TRACK CORRODED BS 785.15 - 863. R & R SEAT TRACK IAW AMM 53-00-49 TASK 53-00-49-000-801 & 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 25,288 hrs · 17,666 cycles

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

Part: SEAT TRACK — CORRODED (BS 724-761) · airframe 25,288 hrs · 17,666 cycles

RIGHT SIDE SEAT TRACK CORRODED BS 724.08 - 761.85. R & R SEAT TRACK IAW AMM 53-00-49, TASK 53-00-49-000-801 & 53-00-49-400-8901.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 25,288 hrs · 17,666 cycles

LEFT SIDE SEAT TRACK CORRODED BS 485 - 565. R & R SEAT TRACK LT SIDE FS 485-565 IAW AMM 53-00-49, TASK 53-00-49-000-801 & 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 565-645) · airframe 25,288 hrs · 17,666 cycles

RIGHT SIDE SEAT TRACK CORRODED AT BS 565 - 645. R & R SEAT TRACK IAW AMM 53-00-49, TASK 53-00-49-000-801 & 53-00-49, TASK 53-00-49-000-801 & 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 565-645) · airframe 25,288 hrs · 17,666 cycles

LEFT SIDE SEAT TRACK CORRODED BS 565 - 645. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: DOOR — LACK OF LUBE · airframe 25,288 hrs · 17,666 cycles

FWD GALLEY SERVICE DOOR FAILED HANDLE PULL TEST MAX FORCE 35LBS TEST PULLED 48. LUBED GALLEY SERVICE DOOR AND COMPLIED WITH FUNCTIONAL TEST OF GALLEY SERVICE DOOR IAW AMM 12-20-52-640-801 & 52-41-00-720-801 FUNCTIONAL TEST GOOD.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 25,288 hrs · 17,666 cycles

RIGHT SIDE SEAT TRACK CORRODED AT BS 485 - 565. BLENDED DAMAGE IAW GREO 670-53-00-013 FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW AMM 53-00-49, TASK 53-00-49-000-801, & 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 25,288 hrs · 17,666 cycles

FLOOR SEAT TRACK LT SIDE CORRODED BS 364 - 485. R & R SEAT TRACK AT LEFT FS 364-485 IAW AMM 53-00-49, TASK 53-00-49-000-801 & 53-00-49-400-801.

Part: INTERCOSTAL — CORRODED (BS 319) · airframe 25,288 hrs · 17,666 cycles

INTERCOSTAL AT S20R FWD OF BS 319 CORRODED. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01. INSTALLED NEW SERIVCABLE INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01. MAJOR REPAIR.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,288 hrs · 17,666 cycles

BULKHEAD LOWER WEB AT FS 280 LT SIDE HAS CORROSION AT WATERLINE AREA LBL 9-12. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594, MAJOR REPAIR.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 25,288 hrs · 17,666 cycles

PAX DOOR UPPER FRAME CORRODED AROUND BOLT HOLES. R & R UPPER DOOR FRAME IAW SRM 51-41-02, TASK 51-41-02-001-001-A01 AND DWG SH670-31825.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,288 hrs · 17,666 cycles

BULKHEAD LOWER WEB BS 280 RT SIDE CORRODED AT WATERLINE AREA RBL 9-12. COMPLIED WITH EC/TC REO 670-53-11-594-01 AND GREO 670-53-11-594, REV. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 25,297 hrs · 17,677 cycles

RIGHT FLOOR SUPPORT CORRODED IN MULITPLE SPOTS BETWEEN BS 280 - 319. FOUND TO BE OUT OF LIMITS. REMOVED CORROSION IAW SRM 51-21-06-001-001. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, SRM 51-40-11-001-001-A01 AND DWG SH670-32170. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 349) · airframe 25,288 hrs · 17,666 cycles

CORROSION ON AFT SIDE OF FRAME AT BS 349 S27. DAMAGE FOUND TO BE OUT OF LIMITS. REPAIRED IAW REO 670-53-21-1108.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 25,288 hrs · 17,666 cycles

CORROSION ON INTERCOSTAL S27R, BS 364. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. DAMAMGE FOUND TO BE OUT OF LIMITS. COMPLIED WITH REO 670-53-21-1109.

Part: SKIN — GOUGED (BS 969-985) · airframe 25,288 hrs · 17,666 cycles

AFT FUSELAGE BS 969 - 985 GOUGED APPROXIMATELY 2 INCHES. BLENDED AREA IAW REO 670-53-00-290 COMPLIED WITH BLEND OUTS. WITHIN LIMITS.

Part: BEARING — CRACKED (RT WING) · airframe 25,297 hrs · 17,677 cycles

FOUND RT LOWER SPHERICAL BEARING CRACKED. R & R RT LOWER WING IAW SB670BA-27-016, REV C. R & R RT LOWER WING LINK IAW SB 670BA-57-016.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 25,288 hrs · 17,666 cycles

EMERGENCY LIGHTS FAILED OPS CHECK IAW AMM 33-51-00-710-802. FOUND BROKEN WIRE PZA-L6014-20N. SPLICED WIRE IAW ESPM 20-44-00. OPS CHECK GOOD IAW AMM 33-51-00-710-802.

Part: TRACK — DAMAGED (CARGO DOOR) · airframe 25,288 hrs · 17,666 cycles

AFT CARGO DOOR AFT TRACK GOUGED AND BENT. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. R & R TRACK. INSTALLED BAGGAGE BAY DOOR TRACKS IAW ECTC REO 670-53-62-0102. COMPLIED WITH REO 670-53-62-0102 INCORPORATED REO 670-53-62-0102.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 25,288 hrs · 17,666 cycles

TRACK LIGHTING NOT INSTALLED CORRECTLY AT EMERGENCY EXITS AND FROM SEAT 1AD FORWARD. CORRECTED TRACK LIGHTING SEGMENTS IAW 33-51-01-400-801.

Part: GLOWSTRIP — MISSING (PAX DOOR) · airframe 24,116 hrs · 16,819 cycles

THREE FEET OF THE GLOW STRIP TAPE MISSING FROM SERVICE DOOR. REPLACED MISSING TAPE AS REQUIRED, ACFT OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 24,008 hrs · 16,743 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERIES IAW AMM 25-60-00, NO FURTHER DEFECT NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,932 hrs · 16,683 cycles

AFT RT SIDE EMERGENCY LIGHT EXTERIOR INOPERATIVE. R & R EMERGENCY LIGHT ASSY IAW AMM 33-15-15-400-801, OPS CHECKED GOOD IAW AMM 33-51-15-710-801.

Part: LENS — WRONG PART (EMERGENCY LIGHTS) · airframe 22,972 hrs · 15,987 cycles

LENS COVER BY SERVICE DOOR SHOULD BE AN EMERGENCY EXIT SIGN. REPLACED LENS COVER AT SERVICE DOOR IAW AMM 33-51-05.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,535 hrs · 14,981 cycles

NR 6 EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. LAMPED NR 6 EXTERIOR EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: MEGAPHONE — DAMAGED (CABIN) · airframe 21,070 hrs · 14,622 cycles

MEGAPHONE NUTPLATE BROKEN. R & R MEGAPHONE IAW AMM 25-61-14.

Part: CABLE — BROKEN (PAX DOOR) · airframe 20,835 hrs · 14,439 cycles

MAIN CABIN DOOR WILL NOT OPEN. FOUND ICE BREAKER DOOR CABLE BROKEN. R & R ICE BREAK CABLE IAW AMM 52-11-15. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: ANGLE — CORRODED (BS 364) · airframe 20,415 hrs · 14,112 cycles

ANGLE AT STRINGER 26 RT FWD OF FS 364 CORRODED.

Part: ANGLE — CORRODED (BS 364) · airframe 20,415 hrs · 14,112 cycles

ANGLE AT STRINGER 26 LT FWD OF FS 364 IS CORRODED.

Part: SEAT TRACK — CORRODED (BS 838.7-985) · airframe 20,415 hrs · 14,112 cycles

RIGHT SEAT TRACK LBL 9.0 FS 838.7 - 985 CORRODED. CORROSION FOUND MORE THAN 30 PERCENT OF TRACK OUT OF LIMITS IAW SRM 53-51-49-101-001-A01 LESS THAN 3 INCHES OF SEPARATION. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801(CONFIG A03).

Part: WEB — CORRODED (BS 280) · airframe 20,415 hrs · 14,112 cycles

RT 280 WEB CORRODED. REPAIR IAW SRM 53-11-10-201-003, SRM 53-11-10-201-003

Part: WEB — CORRODED (BS 280) · airframe 20,415 hrs · 14,112 cycles

LEFT 280 WEB CORRODED. REPAIRED IAW SRM 53-11-10-201-003. SRM 53-11-10-201-003

Part: CROSSBEAM — CORRODED · airframe 20,415 hrs · 14,112 cycles

CROSSBEAM CORRODED. REPAIRED IAW EC/TC REO 670-53-11-047.

Part: CROSSBEAM — CORRODED · airframe 20,415 hrs · 14,112 cycles

CROSSBEAM BETWEEN RBL9 TO RBL27 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001. MEASURED BLENDED AREA FOUND TO BE .018" DEEP . COMPLIED WITH STEP 2 OF REO 670-53-21-850 IAW NDTM PART 1, 51-20-006. NO INDICATIONS NOTED. REPAIRED IAW REO 670-53-21-850.

Part: ANGLE — CORRODED · airframe 20,415 hrs · 14,112 cycles

SERVICE DOOR LOWER SILL ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001 AND REPAIRED IAW SRM 53-21-23-101-001.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,415 hrs · 14,112 cycles

COCKPIT FLOORBEAM ANGLE BS 280 CORRODED. REMOVED FLOORBEAM ANGLE, LOCATED & DRILLED SERVICEABLE ANGLE IAW SRM 51-42-21-001-001. INSTALLED IAW SRM 51-42-21-001-001-A01. REPAIR CLASSIFIED AS MINOR.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 20,415 hrs · 14,112 cycles

CRAWLWAY FLOOR SUPPORT AT FS 280, CORRODED. REMOVED CORROSION PER SRM 51-21-06-001-001. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01, SRM 53-21-06-101-002-A01. REPAIRED IAW REO 670-53-11-713.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 20,415 hrs · 14,112 cycles

LOWER INTERNAL DOUBLER CORRODED TCAS. R & R DOUBLER IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 785.15-855) · airframe 20,415 hrs · 14,112 cycles

SEAT TRACK FROM FS 785.15 - 855 CORRODED. BLENDED CORROSION. MATERIAL LOSS AT .040 IN THIS IS ABOVE THE ALLOWABLE LIMIT OF .035 AND IS OUT OF LIMITS IAW SRM. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801-A03. REPAIR CLASSIFIED MINOR.

Part: ANGLE — CORRODED (BS 265-280) · airframe 20,415 hrs · 14,112 cycles

INTERNAL FWD JACKING FITTING ANGLE AT S26L IS CORRODED BETWEEN FS 265 & 280. REMOVED CORROSION IAW SRM 51-21-06-001-001.

Part: SEAT TRACK — CORRODED (BS 573-670) · airframe 20,415 hrs · 14,112 cycles

SEAT TRACK FROM FS 573 - 670 CORRODED. FOUND OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A03. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801-A03. REPAIR CLASSIFIED AS MINOR

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 20,415 hrs · 14,112 cycles

CRAWL WAY FLOOR SUPPORT AT FS 280 CORRODED. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01. FOUND IT TO BE OUT OF LIMITS IAW SRM 53-22-51-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 785.15-855) · airframe 20,415 hrs · 14,112 cycles

SEAT TRACK FROM FS 785.15 - 855 CORRODED. FOUND OUT OF LIMITS IAW SRM 53-41-101-001-A01. REMOVED SEAT TRACK IAW IAW SRM 53-00-49-000-801-A03. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801-A03. REPAIR CLASSIFIED AS MINOR.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 20,415 hrs · 14,112 cycles

COCKPIT ENTRANCE FLOOR SUPPORT AT FS 280 CORRODED. REMOVED FLOOR SUPPORT, LOCATED AND INSTALLED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 685-838.7) · airframe 20,415 hrs · 14,112 cycles

SEAT TRACK LBL 9.0 FROM FS 685 - 838.7 CORRODED. FOUND SEPARATION TO BE LESS THAN 3" IAW SRM 53-51-49-101-001-A01. REMOVED SEAT TRACK TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801 (CONFIG A03)

Part: SEAT TRACK — CORRODED (BS 716-761.85) · airframe 20,415 hrs · 14,112 cycles

SEAT TRACK FROM FS 716 - 761.85 CORRODED. BLENDED CORROSION, MAXIUM MATERIAL REMOVED AT .025 IN MAX ALLOWED 0.035 IN WITHIN LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-99-000-801-A03. ALODINED BLENDED AREAS. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03. REPAIR CLASSIFIED AS MINOR.

Part: FRAME — CORRODED (BS 319 S25L-25R) · airframe 20,415 hrs · 14,112 cycles

FRAME FS 319 BETWEEN S25L AND S25R CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001 AND SRM 53-21-06-101-002. FOUND WITHIN LIMITS. TREATED, PRIMED AND PAINTED SRM 51-21-11-001-001-A01 AND 51-25-00-001-A01.

Part: SEAT TRACK — CORRODED (BS 685-838.7) · airframe 20,415 hrs · 14,112 cycles

SEAT TRACK LBL 9.0 FROM FS 685 - 838.7 CORRODED.

Part: SEAT TRACK — CORRODED (BS 870-969) · airframe 20,415 hrs · 14,112 cycles

SEAT TRACK FROM FS 870 - 969 CORRODED. CORROSION OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03, INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03. REPAIR CLASSIFIED AS MINOR.

Part: SEAT TRACK — CORRODED (BS 670-716) · airframe 20,415 hrs · 14,112 cycles

SEAT TRACK FROM FS 670 - 716 CORRODED. FOUND OUT OF LIMITS IAW SRM 53-51-44-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-40-49-000-801-A03. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A01. REPAIR CLASSIFIED AS MINOR.

Part: ANGLE — CORRODED (BS 265-280) · airframe 20,415 hrs · 14,112 cycles

INTERNAL FWD JACKING FITTING ANGLE BETWEEN FS 265 & 280 AT S26R IS CORRODED. REMOVED CORROSION PER SRM 51-21-06-001-001.

Part: SEAT TRACK — CORRODED (BS 685-838.7) · airframe 20,415 hrs · 14,112 cycles

SEAT TRACK LBL 9.0 FROM FS 685 - 838.7 CORRODED. BLENDED CORROSION, REMOVE WAS .050" MAX ALLOWED .035", FOUND OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801(A03). INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 838.7-985) · airframe 20,415 hrs · 14,112 cycles

SEAT TRACK LBL 9.0 FROM FS 838.7 - 985 CORRODED. CORROSION FOUND ON MORE THAN 30 PERCENT OF TRACK SURFACE REMOVED UNSERVICEABLE & INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801. (CONFIG A03) & AMM 53-00-48-400-801.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 20,415 hrs · 14,112 cycles

SEAT TRACK LBL 9 FROM FS 349 - 485 CORRODED. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-21-49-001-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-19-400-801-A01 (CONFIG A03).

Part: FRAME — CORRODED (BS 310 S25L-25R) · airframe 20,415 hrs · 14,112 cycles

FRAME FS 310 BETWEEN S25L & S25R CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001. FOUND WITHIN LIMITS. TREATED, PRIMED, AND PAINTED IAW SRM 51-21-11-001-001.

Part: ANGLE — CORRODED (BS 364 S25R) · airframe 20,415 hrs · 14,112 cycles

ANGLE AT S25R FWD OF FS 364.00 IS CORRODED. REMOVED ANGLE IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW ANGLE IAW SRM 51-42-01-001-001-A01, 51-42-21-001-001-A01 AND SWG SH670-32050.

Part: ANGLE — CORRODED (BS 364 S25L) · airframe 20,415 hrs · 14,112 cycles

ANGLE AT S25L FWD OF FS 364.00 IS CORRODED. REMOVED ANGLE IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 20,415 hrs · 14,112 cycles

FWD RIGHT EQUIPMENT BAY FLOOR CRACKED JUST AFT OF AFT DOOR FRAME STRUCTURE. REPAIRED.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 20,415 hrs · 14,112 cycles

FWD LEFT EQUIPMENT BAY FLOOR CRACKED JUST AFT OF AFT DOOR FRAME STRUCTURE. REPAIRED.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 17,923 hrs · 12,363 cycles

AFT MEGAPHONE INOPERATIVE. R & R AFT MEGAPHONE IAW AMM 25-60-00.

Part: COVER — DISLODGED (EMERGENCY LIGHT) · airframe 17,526 hrs · 12,102 cycles

EMERGENCY EXIT LIGHT COVER FELL OFF. REMOVED AND REPLACED EMERGENCY LIGHT FIXTURE IAW AMM 33-51-05. OPS CK GOOD.

Part: SIGN — DISLODGED (EMERGENCY LIGHTS) · airframe 17,478 hrs · 12,067 cycles

EMERGENCY EXIT LIGHT SIGN AT PAX DOOR HAS FALLEN OFF. LIGHT LENS/ COVERS, INCLUDING EMERGENCY LIGHT. R & R EMERGENCY LIGHT FIXTURE IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,717 hrs · 10,821 cycles

SUPPORT ANGLE LT SIDE FOR COCKPIT PANEL 221ALF CRACKED. BEGAN REMOVING FASTENERS ON LT SIDE FLOOR SUPPORT ANGLE FOR COCKPIT PANEL 221ALF. IAW SRM 51-42-06-001-001-A01. R & R LT SIDE COCKPIT FLOOR SUPPORT ANGLE WITH SERVICEABLE PART ALL WORK DONE IAW SRM 51-42-06-001-001-A01. A023 PROTECTIVE COATING NEEDS TO BE APPLIED. COMPLIED WITH APPLICANCE OF PROTECTIVE COATING OF AREAS WORKED ON LT SUPPORT ANGLE OF PANEL 221ALF IAW SRM 51-25-06-001-001-(AO1).

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,717 hrs · 10,821 cycles

BS 280 BEAM REQUIRES REPLACEMENT DUE TO CORROSION, REPAIRED. PRIMED AND PAINTED BARE AREAS AT CTR EATHING, INSTALLED NEW 280 CROSS BEAM IAW SRM 51-42-06, 51-42-20. 5. DRIP TRAYS AND FLOOR PANEL NUTPLATES REQUIRES INSTALLATION AND 280 BEAM NEEDS TO BE SEALED AND PAINTED. INSTALLED LT/RT DRIP TRAYS, AND NUTPLATES IAW SRM 51-42-21-001-001, 51-42-13-001-001, AND 51-42-15-001-001. SEALED PRIMED,PAINTED AND APPLIED CIC TO 280 REPAIR IAW SRM 51-25-00.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 15,717 hrs · 10,821 cycles

ASD THRESHOLD MID CAP ANGLE CORRODED. BLENDED DAMAGED AREA OF MID CAP ANGLE FOUND TO BE OUT OF LIMITS REF SRM 51-21-06-001-001. RECEIVED SERVICEABLE ANGLE AND PICKED UP ALL EXISTING FASTENER HOLES FROM UNSERVICEABLE ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 INSTALLED ANGLE IAW SRM 51-41-02-001-001-A01.

Part: BULKHEAD — CORRODED (BS 280) · airframe 15,717 hrs · 10,821 cycles

FS 280.00 BULKHEAD LT SIDE LOWER WEB HAS CORROSION DAMAGE. REMOVED LT SIDE FS280 BULKHEAD LOWER WEB IAW SRM 51-42-06-001-001-A01. DRILLED ALL HOLES IN LT SIDE 280 LOWER PANEL, FASTENER HOLES DRILLED IAW SRM 51-40-11-001-001-A01. INSTALLED ALL FASTENERS IN LT SIDE 280 WEB IAW SRM 51-42-06-001-001-A01, 51-42-12-001-001-A01.

Part: BULKHEAD — CORRODED (BS 280) · airframe 15,717 hrs · 10,821 cycles

FS 280.00, BULKHEAD RT SIDE LOWER WEB HAS CORROSION DAMAGE. REMOVED BULKHEAD LOWER IAW SRM 51-42-06-001-001-A01. FABRICATED LOWER WEB IAW REO 670-53-11-052. FABRICATED WEB PANEL. PERFORMED LPI, TYPE 1, METHOD C ON RT LOWER WEB IAW SRM 51-12-00-001-001 IAW MAC NDT INSPECTION PROCEDURE PT-1. NO INDICATIONS NOTED AT THIS TIME. TRIMMED AND DRILLED ALL HOLES IN RT SIDE FABRICATED WEB IAW REO 670-53-11-052, INSTALLED FASTENERS IN WEB IAW REO 670-53-11-052. COMPLIED WITH EO 700-53-006201 REPAIR 2, WEB REPLACEMENT.

Part: ANGLE — CRACKED (BS 280 BULKHEAD) · airframe 15,717 hrs · 10,821 cycles

UPON REMOVAL OF RT LOWER BULKHEAD WEB FS 280 FOUND ANGLE AT RBL 26 CRACKED AT BOTTOM HOLE. R & R RT LOWER WEB ANGLE IAW SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,717 hrs · 10,821 cycles

BS 280 FLOORBEAM CORRODED. REMOVED FS 280 BEAM, ALL WORK DONE IAW SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. PERFORMED LPI, TYPE1, METHOD C ON CUT LINE ON NEW FS 280.00 BEAM IAW SRM 52-12-00-001-001 IAW NDT INSP PROCEDURE PT-1. NO INDICATIONS NOTED AT THIS TIME.

Part: POST — CORRODED (BS 280) · airframe 15,717 hrs · 10,821 cycles

FLIGHT STA DOOR POST AT FS280 LBL 11.128 HAS SIGNS OF CORROSION AFT LOWER CORNER. COMPLIED WITH EC/TC REO 670-53-11-511 AND REO 670-53-11-511.

Part: PLACARD — CRACKED (PAX DOOR) · airframe 15,717 hrs · 10,821 cycles

PAX DOOR INNER HANDLE "EXIT/PULL" SIGN CRACKED THRU BOTH ATTACH FASTENERS. R & R PAX DOOR INNER HANDLE BETA LIGHT IAW AMM 33-51-13-400-801.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 15,717 hrs · 10,821 cycles

MAIN AVIONICS COMPARTMENT BETWEEN FS 349.00 & FS 364.00 AND BETWEEN S27 & S26R INTERCOSTAL AROUND ATTACH FASTENERS HAS CORROSION. R & R INTERCOSTAL IAW SRM CH 51-42-06-001-001-A01.

Part: DRAG ANGLE — CRACKED · airframe 15,717 hrs · 10,821 cycles

PERFORMED EDDY CURRENT INSP OF RT VERT STAB TO FUSELAGE ATTACH DRAG ANGLE IAW MAC NDT INSP PROCEDURE ET-2. DRAG ANGLE IS CONFRIMED CRACKED AND END OF CRACK IS MARKED. REMOVED RT AFT DRAG ANGLE IAW SRM 51-42-27-001-001-A01, 51-42-21-001-A01 & 51-42-13-001-001-A01. INSTALLED ANGLE AND STARTED INSTALLING FASTENERS IAW SRM 51-42-13 AND 57-42-22-001-001-A01. INSTALL COLLARS ON ALL LOCK FASTERNERS FOR LT SIDE DRAG ANGLE. INSTALLED ALL COLLARS ON ALL FASTENERS FOR LT SIDE DRAG ANGLE AND APPLIED A023 REFLECTIVE COATING ALL WORK DONE IAW SRM 51-42-21-001-001-A01 AND SRM 51-25-01-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 15,717 hrs · 10,821 cycles

CORROSION DAMAGE ON FLOOR SEAT RAIL FS 485.00 TO FS 581.00 AT RBL 9.0. R & R FLOOR SEAT RAIL IAW AMM TSK 53-00-49-400-801.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 15,717 hrs · 10,821 cycles

ASD THRESHOLD FWD DRAIN AREA CORRODED MARKED. CORROSSION FOUND TO BE ON ANGLE AT ASD THRESHOLD AREA. R & R ANGLE REFER TO JOB 1, OP 169 FOR WORK ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 15,717 hrs · 10,821 cycles

CORROSION DAMAGE ON FLOOR SEAT RAIL FS 581.00 TO FS 677.00 AT RBL 9.0. R & R RT SIDE FLOOR SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: PLACARD — DETERIORATED (PAX DOOR) · airframe 15,717 hrs · 10,821 cycles

PAX DOOR LOWER "EXIT" PLACARD DETERIORATED. R & R PAX DOOR LOWER "EXIT" PLACARD IAWAMM 51-22-81-340-802-A01.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 15,717 hrs · 10,821 cycles

CORROSION DAMAGE ON FLOOR SEAT RAIL FS581.00 TO FS677.00 AT LBL 9.0. R & R FLOOR SEAT RAIL IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: DRAG ANGLE — CRACKED · airframe 15,717 hrs · 10,821 cycles

PERFORMED EDDY CURRENT INSP OF LT VERTICAL STAB TO FUSELAGE ATTACH DRAG ANGLE IAW MAC NDT INSP PROCEDURE ET-2, DRAG ANGLE IS CONFIRMED CRACK AND END OF CRACK IS MARKED. REMOVED LT SIDE AFT DRAG ANGLE & LOCATED HOLES IN NEW DRAG ANGLE IAW SRM 51-42-27-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01. INSTALLED FASTENERS IN SERVICEABLE ANGLE AT BASE OF VERTICAL STAB ON LT SIDE IAW SRM 51-42-20-001-001-A01, COLLARS REQUIRE TIGHTENING ABOVE APU INLET DUCT. TIGHTENED 3 COLLARS FWD APPLIED A023 PROTECTIVE COATING ALL WORK DONE IAW SRM 51-42-21-001-001-A01 AND SRM 51-25-01-001-001-A01.

Part: LOCK — OUT OF ADJUST (GALLEY DOOR) · airframe 15,717 hrs · 10,821 cycles

GALLEY SERVICE DOOR FAILED FUNCTIONAL CHECK. FORCE REQUIRED TO COMPLETE THE UNLATCH CYCLE IS 48 LBF MAXIMUM IAW AMM IS 35 LBF. CLEANED AND LUBRICATED GALLEY SERVICE DOOR LOCKING MECHANISM AND CHECKED ADJUSTMENT IAW AMM 51-41-00-820-801. PERFORMED FUNCTIONAL TEST OF THE GALLEY SERVICE DOOR. OPS CHECK GOOD. IAW AMM 52-41-00-720-801.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 15,717 hrs · 10,821 cycles

NR 1 EMERGENCY CEILING FLOOD LIGHT CONNECTOR P355 (STN 409 RT) HAS A BROKEN WIRE. STRIPPED WIRE OF CONNECTOR P355 AND CRIMPED NEW CONTACT PN 350689-7 ON WIRE AND REINSERTED WIRE IN 9355 IAW ESPM CH 20-11-00-AND CH 20-16-00. PERFORM OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. PERFORMED OPS TEST OF THE EMERGENCY LIGHT IAW AMM 33-51-00-710-801-A01. OPS CHECK GOOD AT THIS TIME.

Part: FRAME — NONE (BS 319 S26-27L) · airframe 15,717 hrs · 10,821 cycles

MAIN AVIONICS COMPARTMENT FS 319.70 BETWEEN S26L & S27 FRAME AFT SIDE HAS CORROSION. AFTER FURTHER INVESTIGATION FOUND TO BE MISSING PAINT AND DIRT. CLEANED AREA NO CORROSION FOUND. ALODINED PRIMED AND PAINTED IAW SRM CH 51-25-00-001-001-A01.

Part: STRINGER — CORRODED (BS 319-333) · airframe 15,717 hrs · 10,821 cycles

MAIN AVIONICS COMPARTMENT BETWEEN FS 319.70 & FS 333.00 S26R AROUND ATTACH FASTENERS HAS CORROSION. REMOVED RIVETS IN AREA OF CORROSION ON STR 26R AND BLENDED CORROSION IAW SRM CH 51-42-06-001-001- & 51-21-06-001-001. KC 161720 05/26/10. PERFORMED THICKNESS MEASUREMENT OF BLEND AREA IAW NDT INSP PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS .023". DAMAGE IS OUT OF LIMITS AS NO DAMAGE IS PERMITTED IN THIS AREA. REMOVED STRINGER IAW SRM 51-42-01. DRILLED UP & INSTALLED FASTENERS THROUGH SKIN IN NEW STRINGER SRM 51-42-06-001-001-A01.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 15,717 hrs · 10,821 cycles

ASD THRESHOLD CORRODED AT CTR JUST AFT OF DOOR HARNESS ADEL CLAMP. BLENDED ANGLE AT ASD THRESHOLD FOUND TO BE OUT OF LIMITS REF SRM 51-21-06-001-001, WA161715 6/4/10. RECEIVED & STARTED DRILLING NEW ANGLE AND INSTALLED NUT PLATES ON NEW ANGLE REF SRM 51-42-06-001-001 WA161715 6/4/10. FINISH PICKING UP HOLES & INSTALL NEW ANGLE WA161715 6/4/10 FINISHED DRILLING ANGLE AND INSTALLED WET REF SRM 51-42-06-001-001, WA161715.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 15,717 hrs · 10,821 cycles

PAX DOOR AFT DRAG ANGLE JUST ABOVE ASSIST MOTOR PULLEY MOUNT BRACKET CRACKED APPROX .5" L. COMPLIED WITH REO 670-52-11-072, STEPS 1 & 2 COMPLIED WITH FILLER IN STEP 5 IS CUT TRIMMED & DRILLED . PERFORMED ET INSP OF CUT LINES ON PAX DOOR AFT DRAG ANGLE IAW REO 670-52-11-072 IAW NDTM PART 1, 51-20-006-250-A01. NO INDICATIONS NOTED AT THIS TIME. COMPLIED WITH STEPS 4-13 OF REO670-52-11-072 REV E. AWAITING EC/TC. COMPLIED WITH EC/TC REO670-52-11-072 IAW REO 670-52-11-072, REV C.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,717 hrs · 10,821 cycles

MAIN AVIONICS COMPARTMENT FS 280.00, 241ALF, FLOOR SUPPORT STRUCTURE UPPER SURFACE HAS CORROSION. FLOOR SUPPORT ANGLE WAS R & R FOR ALL WORK ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 15,717 hrs · 10,821 cycles

CORROSION DAMAGE ON FLOOR SEAT RAIL FS485.00 TO FS581.00 AT LBL 9.0. R & R MAIN CABIN FLOOR SEAT RAIL IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: CIRCUIT BREAKER — TRIPPED (NLG STEERING) · airframe 15,609 hrs · 10,734 cycles

STEERING INOP CAUTION MSG IN FLT. QRH RUN. EMERGENCY DECLARED. RESET CIRCUIT BREAKERS ON GROUND IAW MCC. STEERING INOP EXTINGUISHED. (EMERGENCY DECLARED -- EMERGENCY PERSONNEL WERE STANDING BY) PERFORMED OPS TEST OF NWS IAW AMM 32-51-00. NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — SMOKE (LAVATORY) · airframe 13,991 hrs · 9,519 cycles

FLT 5578-SMOKE AFT LAV, AIR RETURN. EMERGENCY DECLARED-ACFT RETURNED TO DEPARTURE AFTER T/O.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 12,800 hrs · 8,629 cycles

RT EXTERIOR AFT OVERWING EMERGENCY EXIT LIGHT INOP.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 11,902 hrs · 7,963 cycles

CABIN MEGAPHONE INOP.

Part: LIGHT — MISSING (CABIN) · airframe 11,668 hrs · 7,769 cycles

EMERGENCY FLOOR PATH MARKING MISSING FWD LT STRIP BY GALLEY 3.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,914 hrs · 7,220 cycles

MAIN AVIONICS COMPARTMENT UNDER FLOOR CRAWLWAY, FLOORBEAM ANGLE IS CORRODED AT FS 280 STR 27. BLENDED OUT MINOR CORROSION IAW SRM 51-21-06. MATERAL REMOVED .003 IN OUT OF .006 IN MAX ALLOWED IAW SRM 53-22-55. (B)

Part: DRAG ANGLE — CRACKED (VERTCAL STAB) · airframe 10,914 hrs · 7,220 cycles

RIGHT SIDE VERTICAL TO FUSELAGE DRAG ANGLE IS CRACKED. REFER TO STEPS 2-9 ON M-234 FORM ATTACHED FOR WORK ACCOMPLISHED DK 7022603. REMOVED RT VERTICAL DRAG ANGLE PAINT IAW CRJ 700 SRM 51-26-00. (S)

Part: WEB — CORRODED (BS 280) · airframe 10,914 hrs · 7,220 cycles

LT FS280 WEB CORRODED. (B) REMOVED MINOR CORROSION ON LT 280 WEB, LOWER INBD CORNER (1X.8X.004 REMOVED). BLEND IS WITHIN LIMITS PER SRM 53-11-10. (S)

Part: FLOORBEAM — CORRODED (FS 280) · airframe 10,914 hrs · 7,220 cycles

LT FS 280 FLOORBEAM CORRODED. (B) BLENDED MINOR CORROSION AREAS (3 TOTAL) ON FLOORBEAM IAW REO 670-53-11-046. .004 MATERIAL REMOVED. BLENDED AREAS WITHIN LIMITS. PERFORMED CUTOUT OF DAMAGED AREA FLOORBEAM, AND FABRICATED FILLER PER REO 670-53-11-310. (S)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 10,914 hrs · 7,220 cycles

COCKPIT ENTRANCE PANEL 221ALF AFT ANGLE CORRODED. REMOVED ANGLE IAW SRM 51-42-06. (B)

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 10,914 hrs · 7,220 cycles

SUSPECT CRACK ON LT SIDE VERTICAL STAB TO FUSELAGE DRAG ANGLE. (B) REFER TO STEPS 3-9 ON M-234 FOR WORK ACCOMPLISHED DK 7022603. REFER TO STEP NUMBER THREE ON M-234 FOR WORK ACCOMPLISHED FOR THIS STEP.

Part: STEP — CRACKED (PAX DOOR) · airframe 10,914 hrs · 7,220 cycles

ASD LOWER STEP CRACKED. REMOVED AND REPLACED ASD LOWER STEP IAW AMM 52-11-04. (S)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 10,429 hrs · 6,881 cycles

RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 10,324 hrs · 6,808 cycles

RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP.

Part: DOOR — BINDING (SERVICE DOOR) · airframe 10,248 hrs · 6,758 cycles

SERVICE DOOR HARD TO OPEN. FLT 4484 DEL 36 MINS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 9,791 hrs · 6,458 cycles

RIGHT AFT MOST EXTERNAL EMERGENCY LIGHT INOP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 9,093 hrs · 5,984 cycles

CAPTAIN`S FLASHLIGHT INOP.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 8,752 hrs · 5,727 cycles

PORTABLE MEGAPHONE WILL NOT WORK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 7,917 hrs · 5,152 cycles

F/A FLASHLIGHT INOP.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 7,610 hrs · 4,943 cycles

1ST CEILING LEVEL EMERGENCY FLOODLIGHTS OUT. CABIN EMERGENCY LIGHTS - CEILING LEVEL FLOODLIGHTS) [SUP 05-09-07] REPINNED WIRE AT 1ST CEILING EMERGENCY LIGHT . OPS CKED GOOD

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 7,355 hrs · 4,784 cycles

CO-PILOTS FLASHLIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,235 hrs · 4,701 cycles

REFER TO AFDL 335624 ITEM NR 1 EMERGENCY LIGHT AT ROW 1 OUT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,226 hrs · 4,694 cycles

SIDEWALL LIGHT INOP, CEILING ROW 1. FLT 4685 DEL 23 MINS N/C FLTS 4157, 4914, 4326 CX CABIN EMERGENCY LIGHTS - CEILING LEVEL FLOODLIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 7,150 hrs · 4,648 cycles

EXTERIOR EMERGENCY LIGHT AT ASD INOP.

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 7,150 hrs · 4,648 cycles

ASD OUTER HANDLE CRACKED IN RADIUS (MARKED). REMOVED DOOR HANDLE AND TRANSFERED HARDWARE (NOT SAFTIED). PER AMM 52-11-00PRIMED AND PAINTED NEW OUTER PAX DOOR HANDLE PER CRJ 700 SRM 51-21-16. SAFTIED HARDWARE PER CRJ 700 AMM 20-00-00 OK TO INSTALL OUTER PAX DOOR HANDLE INSTALLD NEW OUTER PAX DOOR HANDLE PER CRJ 700 AMM 52-11-00.

Part: FLOOR SUPPORT — CORRODED (BS 330) · airframe 7,150 hrs · 4,648 cycles

PAX DOOR LOWER SILL, FLOOR SUPPORT LOWER LEG IS CORRODED FS 330. BLEND IS WITHIN LIMITS (MATERIAL THICKNESS .063 , REMOVAL .001 REMAINING 062) :INSTALLED FASTENERS AND RESTORED REWORKED AREA. PER CRJ 700 SMR51-42-06 AND SRM 51-21-23.

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 7,150 hrs · 4,648 cycles

ASD OUTER HANDLE CRACKED IN RADIUS (MARKED). REMOVED DOOR HANDLE AND TRANSFERED HARDWARE (NOT SAFTIED). PER AMM 52-11-00. PRIMED AND PAINTED NEW OUTER PAX DOOR HANDLE PER CRJ 700 SRM 51-21-16. SAFTIED HARDWARE PER CRJ 700 AMM 20-00-00 OK TO INSTALL OUTER PAX DOOR HANDLE INSTALLD NEW OUTER PAX DOOR HANDLE PER CRJ 700 AMM 52-11-00.

Part: STEP — CRACKED (AIRSTAIR DOOR) · airframe 7,150 hrs · 4,648 cycles

ASD LOWER STEP CRACKED. ASD LOWER STEP REMOVED & REPLACED IAW CRJ 700 AMM 52-10-00.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,150 hrs · 4,648 cycles

CORROSION ON ASD SILL ANGLE AROUND NUT PLATES WHERE MARKED. REMOVED AND REPLACED ASD SILL ANGLE IAW CRJ 700 SRM 53-21-23.

Part: PLACARD — WORN (CABIN) · airframe 7,150 hrs · 4,648 cycles

ASD EXIT PLACARD WORN AND PEELING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,150 hrs · 4,648 cycles

ASD LOWER AFT INTERCOSTAL CRACKED INSIDE SHOOT BOLT ACCESS PANEL 832BR. REMOVED AND REPLACED INTERCOSTAL IAW CRJ 700 SRM 51-42-06 OPS CK GOOD IAW CRJ 700 MM 52-11-00.

Part: PLACARD — WORN (EMERGENCY EXIT) · airframe 7,150 hrs · 4,648 cycles

CREW EMERGENCY EXIT EXTERIOR EMERGENCY EXIT PLACARD FADED. REMOVED AND REPLACED CREW EMERGENCY ESCAPE HATCH PLACARD IAW CRJ 700 AMM 11-00. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 7,150 hrs · 4,648 cycles

CENTER FS 280 FLOOR SUPPORT CRACKED AND CORRODED. COMPLIED WITH EO 700-53-0061 AND MODSUM IS67053110026.

Part: SEAT TRACK — CORRODED (BS 379-977) · airframe 7,150 hrs · 4,648 cycles

CORROSION AND CHAFING ON LEFT AND RIGHT SIDE SEAT RAILS AS MARKED FROM FS 379.00 TO FS 977.00.

Part: BULKHEAD — CRACKED (BS 280) · airframe 7,150 hrs · 4,648 cycles

RIGHT & LEFT 280 BULKHEAD WEBS CRACKED. REMOVED AND REPLACED LT AND RT 280 BULKHEAD WEBS IAW IS 670531100026 AND SRM 51-40-11 AND REO 670-53-11-052.

Part: PLACARD — DAMAGED (CABIN) · airframe 7,150 hrs · 4,648 cycles

CREW EMERGENCY EXIT EXTERIOR EMERGENCY EXIT PLACARD FADED. REMOVED AND REPLACED CREW EMERGENCY ESCAPE HATCH PLACARD IAW CRJ 700 AMM 11-00. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: PLACARD — DETERIORATED (PAX DOOR) · airframe 5,785 hrs · 3,806 cycles

PAX DOOR EXIT PLACARD DETERIORATED.

Part: SMOKE DETECTOR — NO TEST (AFT LAVATORY) · airframe 5,552 hrs · 3,664 cycles

AFT LAV SMOKE DET WILL NOT TEST.

Part: SMOKE DETECTOR — NO TEST (AFT LAVATORY) · airframe 5,552 hrs · 3,664 cycles

AFT LAV SMOKE DETECTOR WILL NOT TEST.

Part: LAMP — BURNED OUT (CABIN)

DURING A GROUND INSPECTION, THE CEILING EMERGENCY LIGHT, AT ROW 4, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE CEILING EMERGENCY LIGHT, AT ROW 4. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: PLACARD — WORN (CABIN)

DURING A C-CHECK IN MCN, THE EXIT PLACARD ON THE PASSENGER DOOR WAS FOUND WORN. MAINTENANCE REMOVED AND REPLACED THE EXIT PLACARD ON THE PASSENGER DOOR. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING MAINTENANCE, THE LEFT EXTERIOR EMERGENCY LIGHT NEAREST THE OVERWING EMERGENCY EXIT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: DOOR — STIFF (SERVICE)

DURING A GROUND INSPECTION, THE SERVICE DOOR WAS FOUND HARD TO OPEN AND CLOSE. MAINTENANCE INSPECTED THE SERVICE DOOR WITH NO DEFECTS FOUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM)

DURING CRUISE, JUST PRIOR TO INITIAL DESCENT AT APPROX 37,000 FT, CREW RECEIVED MACH TRIM CAUTION MSG AND A STAB TRIM CAUTION. QRH WAS COMPLIED WITH FOR BOTH MESSAGES WITH NO CORRECTION. SHORTLY THEREAFTER, CREW RECEIVED AUTOPILOT TRIM CAUTION MSG AND COMPLIED WITH QRH WITH NO CORRECTION. CREW DECLARED EMERGENCY AND ELECTED TO PERFORM NO FLAP LANDING DUE TO HEAVY CONTROL FORCES WITH NOSE DOWN. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED HORIZONTAL STAB TRIM MOTOR CONTROL UNIT (MCU). OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)