N662SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,617 hrs · 68,489 cycles

R1 DOOR EMERGENCY EXIT LIGHT NEXT TO GALLEY INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 84,401 hrs · 68,324 cycles

PANEL 3577L LOWER AFT CORNER CRACKED. REPAIRED PANEL IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,401 hrs · 68,324 cycles

FS SKIN CRACKED AT BS 259.5, BETWEEN STRINGER 19L + 3" & STRINGER 24L - 4". REPAIRED SKIN IAW AAR EA & SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,401 hrs · 68,323 cycles

FS SKIN CRACKED AT BS 259.5, BETWEEN STRINGER 19L+3 & STRINGER 24L-4. R&R SKIN IAW EA.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 84,263 hrs · 68,218 cycles

LAST ROW IN CABIN FLIGHT ATTENDANT SMELLED A SWEET SMOKEY ODOR DISSIPATED WHEN GASPER FAN TURNED OFF. R&R GASPER FAN IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,023 hrs · 68,038 cycles

FUSELAGE SKIN CRACKED AT BS 400 + 16, STR 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,449 hrs · 67,615 cycles

AFT CARGO DOOR CUTOUT UPPER AFT CORNER SKIN CRACKED. REPAIRED SKIN PER EA.

Part: LUG — BROKEN (SPOILER) · airframe 83,449 hrs · 67,615 cycles

RT WING GROUND SPOILER INBOARD LUG BROKEN. REMOVED AND REPLACED SPOILER PER M/M.

Part: SLAT — GOUGED (LT WING) · airframe 83,363 hrs · 67,551 cycles

NR 2 SLAT O/B MAIN RACK SLAT CAN GOUGED IN WELD AND ADJACENT AREA. REMOVED AND REPLACED SLAT CAN PER EA.

Part: SLAT — GOUGED (RT WING) · airframe 83,363 hrs · 67,551 cycles

NR 5 SLAT I/B MAIN TRACK SLAT CAN GOUGED IN WELD AND ADJACENT AREA. REMOVED AND REPLACED SLAT CAN PER EA.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 83,089 hrs · 67,356 cycles

NR 7 FLAP CARRIAGE SPINDLE HAS EVIDENCE OF CORROSION & FLAKED OUT OF THEMAL COATING. REMOVED AND REPLACED NR 7 FLAP CARRIAGE PER MT 327-51-08 NR 7 P/N OFF:65C34483-6SWA, S/N OFF:B6576 PN ON:65-46481-154WN, S/N ON:B5561.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON TIE CLIP LOCATED BS 480 STR 15L PAX CABIN. REPLACED TIE CLIP LOCATED BS 480 STR 15L PAX CABIN IAW B737-300 SRM 51-40-02 AND 51-10-02 ITEM 8 DRAWING 65-46532.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON TIE CLIP LOCATED AT BS 277 AT LEVEL STR 26L NLG INTERNAL AREA. REPLACED TIE CLIP AND FASTENERS LOCATED AT BS 277 AT LEVEL STR 26L NLG INTERNAL AREA IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM B737-300 51-40-02 AND DRAWING 65-45805.

Part: PLATE — DAMAGED (R2 DOOR) · airframe 83,086 hrs · 67,355 cycles

DAMAGE PLATE ASSY ADAPTER AND HARDWARE OF GIRT BART FITTING AT AFT ENTRY DOOR AND AFT SERVICE DOOR. REPLACED PLATE ASSY ADAPTER AND HARDWARE OF GIRT BAR FITTING AT AFT ENTRY DOOR AND AFT SERVICE DOOR IAW AMM 25-61-51.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK AROUND HOLE LOCATED ON STRINGER SPLICE AT LEVEL OF STR 2L BS 887+15". REPLACED STRINGER SPLICE AND FASTENERS LOC AT LEVEL STR 2L, BS 907 IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02 AND DRAWING 65-45772.

Part: REVEAL — BROKEN (CABIN) · airframe 83,086 hrs · 67,355 cycles

BROKEN REVEAL ON LEFT OVERWING EMERGENCY EXIT DOOR. REMOVED AND REPLACED REVEAL ON LEFT EMERGENCY EXIT DOOR IAW AMM 25-21-12.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK AROUND HOLE LOCATED ON STRINGER SPLICE AT LEVEL OF STR 4L BS 907. REPLACED STRINGER SPLICE AT LEVEL STR 4L BS 907 IAW SRM B737-300 51-10-02 ITEM 8 SRM B737-300 51-40-02 AND DWG 65-45772.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON EXTERNAL FUSELAGE SKIN BS 360+7" STR 17L. REPAIRED EXTERNAL FUSELAGE SKIN LOCATED BETWEEN STR 16L TO STR 18L AND BETWEEN BS 360 TO BS 380 IAW EO AEM-HC53-010/13 R0 AND EA 1-353-21521 REV 0 FOR INSPECTION REQUIREMENT SEE TLD T031018

Part: SEAL DEPRESSOR — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON DEPRESSOR-SEAL CORNER LOCATED BS 350 FWD AIR STAIR DOOR. REPLACED DEPRRESOR-SEAL CORNER AND FASTENERS LOCATED BS 350 FWD STAIR DOOR IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM B737-300 51-40-02 AND DRAWING 65-45800.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON FRAME LOCATED BS 360 3" ABOVE STR 16L PAX CABIN. REPAIRED SHEAR TIE OF FRAME LOCATED BS 360 AND 3" ABOVE STR 16L PAX CABIN IAW B737-300 SRM 51-10-02 AND 51-40-02 ITEM 8 53-00-07 REPAIR 7.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON SHEAR TIE OF FRAME LOCATED BS 360 2 INCHES BELOW STR 14L PAX CABIN. REPLACED SHEAR TIE OF FRAME LOCATED BS 360+2 INCHES BELOW STR 14L PAX CABIN IAW B737-300 SRM 51-10-02 ITEM 8 AND 51-40-02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON INTERNAL STRAP LOC AFT OF BS 908 3.6" BELOW STR 3L. REPLACED INTERNAL STRAP LOC AFT OF BS 908 3.6" BELOW STR 3L (4R TO 4L) INTERNAL AREA IAW B737- 300 SRM 51-10-02 ITEM 8 AND DRAWING 66-45772 AND 65-46880.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 83,086 hrs · 67,355 cycles

CRACK ON FLOOR PANEL 1325X FWD CARGO COMPARTMENT. REPLACED FLOOR PANEL 1325X LOC ON FWD CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND DRAWING 65-18621.

Part: WEB — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON WEB LOCATED BS 420 TO BS 440 AT STR 16R FWD PAX CABIN. REPLACED WEB LOCATED BS 420 TO BS 440 AT STR 16R FWD PAX CABIN IAW B737-300 SRM 51-10-02, ITEM 8, B737-300 SRM 51-40-02 AND DRAWING 65-20725.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK (2EA) ON S-17L BETWEEN BS 440+5" TO BS 440+9" FWD PAX CABIN. REPAIRED CREASE BEAM ON STR 17L OUTER CHORD REPAIR BETWEEN BS 439 AND BS 455 FWD PAX CABIN IAW EO AEM -HC53-003/13 R0 AND EA 1-353-21562 R0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON FRAME LOCATED AT BS 480 2 INCHES ABOVE S-15L FWD PAX CABIN. REPAIRED FRAME LOCATED AT BS 480 2 INCHES BETWEEN STR 15L TO STR 14L IAW B737-300 SRM 53-00-07-2R-7 AND SRM 51-40 -02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON FRAME LOCATED AT BS 500 4"ABOVE S-15L FWD PAX CABIN. REPAIRED FRAME LOCATED AT BS 500 BETWEEN STR 15L TO STR 14L PAX CABIN IAW B737-300 SRM 53-00-07-2R-7.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON FRAME LOCATED AT BS 500 2" BELOW S-15L FWD PAX CABIN. REPAIRED FRAME LOCATED BS 500 BETWEEN STR 15L TO STR 16L PAX CABIN IAW B737-300 SRM 53-00-07-2R-7.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON S-15L LOCATED AT BS 460+11" FWD PAX CABIN. REPAIRED S-15L LOCATED BETWEEN BS 462 TO BS 478 FWD PAX CABIN IAW B737-300 SRM 53-00-03-2R-1 DETAIL VII FIG 201 SHEET 8 AND SRM B737-300 51-40-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON SHEAR TIE LOCATED ON BS 440 BETWEEN STRINGER 16L AND STRINGER 17L, AT PAX CABIN. REPLACED SHEAR TIE LOCATED ON BS 440 BETWEEN STRINGER 16L AND STR17L AT PAX CABIN IAW DWG 69-36636 AND B737-300 SRM 51-40-02 ITEM 8 AND DWG 65-46529.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

STRINGER CRACKED AT BS 727D+14, STR 2R. REPAIRED STRINGER IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON SHEAR TIE LOCATED ON BS 400 AND BETWEEN STR 16R TO STR 17R FWD CABIN. REPLACED SHEAR TIE LOCATED ON BS 400 AND BETWEEN STR 16R TO STR 17R FWD CABIN IAW B737-300 SRM 51-10-02 ITEM 8 DRAWING #65-46526 AND 65-45768.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

STRINGER CRACKED AT BS 400+4, STR 16R. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON STRINGER 15R LOCATED BETWEEN BS 380 TO BS 400. REPAIRED STRINGER 15R LOCATED BETWEEN BS 360 TO BS 420 FWD PAX CABIN IAW B737-300 SRM 51-10-01, ITEM 8, B737-300 SRM 51-40-02, B737-300 SRM 53-00-03-2R-1 REPAIR 1.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CORROSION ON STRINGER 22R LOCATED BETWEEN BS 277 TO BS 291.5. REPAIRED STRINGER 22R LOCATED BETWEEN BS 259.5 TO BS 296.5 IAW B737-300 SRM 53-00-03-2R-1 DETAIL VII.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

FUSELAGE SKIN CRACKED AT BS 727C+14, STR 2L. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK WERE FOUND ON LOWER STUB FRAME BS 294.5 AND STR 16R TO STR 17R. REPLACED STUB FRAME LOCATED BS 294.5 AND BETWEEN STR 15R TO STR 17R IAW SRM B737-300 51-10-02 ITEM 8 AND FASTENERS INSTALLED IAW SRM B737-300 51-40-02 AND DRAWING 65-45807.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 83,086 hrs · 67,355 cycles

INOPERATIVE FLASHING RED LED BATTERY CONDITION MONITOR LAMP ON AFT LEFT WINDSCREEN. REPLACED FLASHLIGHT ON AFT LEFT WINDSCREEN IAW CMM 25-60-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON TIE CLIP LOCATED BS 277 AND STR 15L IN FWD CABIN. REPLACED TIE CLIP LOCATED BS 277 AND STR 15L IN FWD CABIN IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DWG 65-45805.

Part: FRAME — CORRODED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

FRAME CORRODED AT BS 277, STR 26L. REPAIRED FRAME IAW EO.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON TIE CLIP LOCATED BS 277 AND STR 14L IN FWD CABIN. REPLACED TIE CLIP LOCATED BS 277 AND STR 14L IN FWD CABIN IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DWG 65-45805.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 908, BETWEEN STR 6R AND STR 7R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 500B+13.25, STR 18R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 500B+15, STR 15R. REPAIRED SKIN IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 500+4.5, STR 16R. REPAIRED SKIN IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 380+15.5, STR 16R. REPAIRED SKIN IAW EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CORROSION ON FRAME WEB LOCATED BS 285.62, AFT LEVEL S-27L, NLG AREA. REPLACED FRAME WEB LOC BS 285.62 AT LEVEL STR 23L TO STR 27L NLG AREA IAW B737-300 SRM 51-10-02 ITEM 8 AND DRAWING 65-45806.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 500D+15, STR 8R. REPAIRED SKIN IAW EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

INTERNAL LOWER ANGLE OF FLOORBEAM CRACKED AT BS 312, WL 202.5. REPAIRED WEB IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED ON CHEM-MILL STEP BS 500D +2.5" ABOVE S-18L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 328+5, STR 25R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 294.5+12, STR 18R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 380+16, STR 16L. REPAIRED SKIN IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 500+4, STR 26L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 400+12, STR 16L. REPAIRED SKIN IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 380+14.5, STR 16L. REPAIRED SKIN IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 727D+2.5, STR 2R. REPAIRED SKIN IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 380+13, STR 15L. REPAIRED SKIN IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 380+13, STR 16L. REPAIRED SKIN IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 727B+16.5, STR 2R. REPAIRED SKIN IAW EO.

Part: ANGLE — CORRODED (NLG WW) · airframe 83,086 hrs · 67,355 cycles

CORROSION ON ANGLE LOCATED AT STA 251. 625 ON BAY NLG. REPLACED ANGLE LOCATED BETWEEN BS 227.8 TO BS 294.5 ON BAY NOSE LANDING GEAR LEFT SIDE IAW SRK B737-300 51-10-02 AND DRAWING 65-45819.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON ANGLE LOCATED BS 328+4" AND BETWEEN STR 17R AND STR 15R IN FWD PAX CABIN. REPLACED ANGLE LOCATED BETWEEN STR 7R AND STR 17R BS 328+4" FWD PAX CABIN IAW SRM B737-300 51-10-02 ITEM 8, SRM B737-300 51-40-02 AND DWG 65-55788.

Part: STRAP — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

STRAP CRACKED BETWEEN BS 312 TO 360, LBL 45.6. REPLACED STRAP IAW SRM AND BOEING DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 908, BETWEEN STR 3L TO STR 4L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 706+3.5, STR 10L. REPAIRED SKIN IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 360, BETWEEN STR 2L TO STR 3L. REPAIRED SKIN IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON SHEAR TIE LOCATED AT BS 767 BETWEEN STR 19L AND STR 20L AFT CARGO COMPARTMENT. REPLACED SHEAR TIE AND FASTENERS LOC BS 767 BETWEEN STR 19L TO STR 20L AFT CARGO COMPARTMENT IAW SRM B737-300 51-40-02 AND DRAWING 65-46549.

Part: WEB — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON WEB LOCATED BETWEEN BS 277 AND BS 294.5 AND STR 14R IN FWD PAX CABIN. REPLACED WEB LOCATED BETWEEN BS 277 AND BS 294.5 AND STR 14R IN FWD PAX CABIN IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DWG

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON UPPER STUB FRAME LOCATED BS 947.5+7" AND BETWEEN STR 9R AND STR 10R IN AFT CABIN. REPLACED UPPER STUB FRAME LOCATED BS 947.5+7" AND BETWEEN STR 9R AND STR 10R IAW B737-300 SRM 51-10-02 ITEM 8 AND 51-42-02 DRAWING 65-46561.

Part: RETAINER — CRACKED (SPOILER) · airframe 83,086 hrs · 67,355 cycles

CRACK ON RETAINER SEAL LOCATED LOWER SURFACE OF THE SPOILER NR 2 LEFT WING. REPLACED SEAL RETAINER LOCATED LOWER SURFACE OF THE SPOILER NR 2 LEFT WING IAW SRM B737-300 51-40-02 AND DRAWING 65-46451 SRM B737-300 51-10-02 ITEM 8.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CORROSION ON STRINGER LOCATED BETWEEN BS 767 AND BS 787 AND STR 23L IN AFT CARGO COMPARTMENT. REPAIRED STRINGER SECTION LOCATED BS 747+10" TO BS 807+10" SRM 53-00-03 REPAIR 1 STR 23

Part: ANGLE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON ANGLE LOCATED ON BS 344+3 INCHES AT LEVEL OF STR 15L FWD CABIN. REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 957.25+4, STR 5R. REPAIRED SKIN IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON STIFFENER LOCATED ON FLOOR STRUCTURE BS 328 AND AT LEVEL RBL 34 FWD CABIN. REPLACED STIFFENER LOCATED ON FLOOR STRUCTURE BS 328 AND AT RBL 34 FWD CABIN IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DRAWING 65-45812.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

STIFFENER CRACKED BETWEEN BS 312 TO 328, RBL 34. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 827+14.0, STR 16L. REPAIRED SKIN IAW EA.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON GUSSET IN THE FWD CARGO COMPARTMENT AT BS 500D, STR 19L. REPLACED GUSSET (STRINGER TIE) IN THE FWD CARGO COMPARTMENT AT BS 500D STR 19L, IAW B737-300 SRM 51-40-02 AND SRM 51-10-02 ITEM 8 AND DRAWING

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON TIE CLIP LOCATED BS 947.5 AND STR 26L IN AFT CARGO COMPARTMENT. REPLACED TIE CLIP AND FASTENERS LOCATED BS 947.5 AND STR 26L IN AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02 AND DRAWING

Part: ANGLE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON ANGLE LOCATED ON BS 294.5 AND STR 13L. REPLACED ANGLE LOCATED ON BS 294.5 AND STR 23L IAW SRM B737-300 51-10-02 ITEM 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK INDICATION WAS FOUND IN THE FUSELAGE SKIN LOCATED AT THE BS 827+3.5" ABOVE STR 16L CRACK LENGHT=1.00". REPAIRED FUSELAGE EXTERNAL SKIN LOCATED BETWEEN BS 818 TO BS 850 STR 14L TO STR 17L IAW EA 1-353-21451 REV 0 AND EO NO AEM-HC53-592

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON WEB OF FRAME LOCATED BS 277 AND STR 16L IN FWD CABIN. REPAIRED WEB OF FRAME LOCATED BS 277 AND S-15L AND S-17L IN FWD CABIN IAW EO AEM-HC53-583-12 R0 EA 1-353-21461 R0. FOR REQUIREMENT INSPECTION SEE TLD: T031015

Part: ANGLE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON ANGLE LOCATED BETWEEN 294.5 TO BS 303.9 AT LEVEL OF STR 23L. REPLACED ANGLE LOCATED BETWEEN BS 294.5 TO BS 303.9 AT LEVEL STR 13L IAW SRM B737-300 51-10-02 AND DRAWING 65-17684.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

FRAME WEB CRACKED AT BS 294.5, STR 16L. REPAIRED WEB EO.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON STRINGER SPLICE LOCATED BETWEEN BS 353 TO BS 367 AND STR 1 IN FWD CABIN. REPLACED STRINGER LOCATED BETWEEN BS 353 TO BS 367 AND STR 1 IN FWD CABIN IAW B737-300 ITEM 8 SRM 51-10-02 AND DWG 65-45800.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 827+15.5, STR 15L. REPAIRED SKIN IAW EA.

Part: PANEL — CRACKED (RT WING) · airframe 83,086 hrs · 67,355 cycles

CRACK ON INBOARD FIXED LEADING EDGE LOCATED L/E STA 208 RIGHT WING. REPAIRED PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON FRAME LOCATED AT BS 500D, BETWEEN STR 20R AND STR 21R IN FWD CARGO COMPARTMENT. REPAIRED FRAME LOCATED AT BS 500D BETWEEN STR 20R AND STR 21R IN FWD CARGO COMPARTMENT IAW SRM B737- 300 53-00-07-2R-7 DETAIL REPAIR 7.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON FRAME LOCATED AT BS 500D, BETWEEN STR 23R AND STR 24R IN FWD CARGO COMPARTMENT. REPAIRED FRAME LOCATED AT BS 500D, BETWEEN STR 23R AND STR 24R IN FWD CARGO COMPARTMENT IAW SRM B737- 300 51-40-02,53-00-07-2R REPAIR 7.

Part: BRACKET — CRACKED (LT WING) · airframe 83,086 hrs · 67,355 cycles

CRACK ON BRACKET LOCATED AT LEVEL OF RSS 215.97 IN LEFT WING TRAILING EDGE CAVITY. REPLACED BRACKET LOCATED AT LEVEL OF RSS 215.97 IN LEFT WING TRAILING EDGE CAVITY IAW B737-300 SRM 51-10-02 ITEM 8 DRAWING 65-50820.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON TIE CLIP LOCATED BS 360 AND STR 1, IN FWD CABIN. REPLACED TIE CLIP LOCATED BS 360 AND STR 1 IN FWD CABIN IAW B737-300 SRM 51-10-02.

Part: WEB — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON WEB LOCATED BETWEEN BS 294.5 TO BS 303.9 AND STR 7L IN FWD CABIN. REPLACED WEB AND FASTENERS LOCATED BETWEEN BS 294.5 TO BS 303.9 AND STR 7L IN FWD CABIN IAW B737-300 SRM 51-40-02 AND SRM 51-10-02 ITEM 8 AND DRAWING

Part: FITTING — CRACKED (CARGO BAY) · airframe 83,086 hrs · 67,355 cycles

TRACK TIE AT CARGO COMPARTMENT FLOOR STRUCTURE CRACKED AT BS 460, RBL 13.80. REPLACED FITTING IAW SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON BRACKET LOCATED BS 1016 AND RBL 6 AT LEVEL S-5 AFT PAX CABIN. REPLACED BRACKET LOCATED BS 1016 AND RBL 6 AT LEVEL STR 5 AFT PAX CABIN IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DWG

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON TIE CLIP LOC BS 727A AND STR 19L IN AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOC BS 727A AND STR 19L IN AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DWG 65-46595 (NEW ONE).

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 727E+6, STR 20L. REPAIRED SKIN IAW EO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CORROSION ON SHEAR TIE LOC BS 927 AND BETWEEN STR 25L AND STR 24L IN AFT CARGO COMPARTMENT. REPLACED SHEAR TIE AND FASTENERS LOCATED BS 927 AND BETWEEN STR 25L AND STR 24L IN AFT CARGO COMPARTMENT IAW B737-300 SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON TIE CLIP LOCATED BS 277 AND STR 11R IN FWD CABIN. REPLACED TIE CLIP LOC BS 277 AND STR 11R IN FWD CABIN IAW B737-300 SRM 51-10-02.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CORROSION ON STRINGER SPLICE LOC BS 907 AND STR 24L IN AFT CARGO COMPARTMENT. REPLACED STRINGER SPLICE PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON TIE CLIP LOCATED BS 277 AND STR 10R IN FWD CABIN. REPLACED TIE CLIP LOC BS 277 AND STR 10R IN FWD CABIN IAW B737-300 SRM 51-10-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON FRAME LOCATED BS 947.5 AT LEVEL STR 19R IN AFT CARGO COMPARTMENT. REPLACED FRAME LOCATED BS 947.5 BETWEEN STR 17R TO STR 23R IN AFT CARGO COMPARTMENT IAW B737-300 SRM 51-40-02, B737-300 SRM 51-10-02 ITEM 8 AND DRAWING 365-46560.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON ANGLE LOCATED BS 1016 AND LBL 5 AFT PAX CABIN. REPLACED ANGLE PER SRM.

Part: WEB — CRACKED (NLG WW) · airframe 83,086 hrs · 67,355 cycles

NLG W/W WEB CRACKED AT BS 243.7+3.5" AND WL 169.1 RIGHT SIDE. REPAIRED WEB IAW SRM.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 83,086 hrs · 67,355 cycles

CRACK ON VERTICAL ANGLE AFT POS LOCATED STRUT TORQUE BOX ACCESS PANEL 5757L ENGINE NR 1. REPLACED VERTICAL ANGLE LOC AFT POSITION STRUT TORQUE BOX ACCESS PANEL 5757L ENGINE 1 IAW SRM B737-300 51-10-02 ITEM 8 SRM 51-40-02 AND DRAWING 313A1380.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CORROSION ON STRINGER LOCATED BETWEEN BS 807 AND BS 827 AND STR 25L IN AFT CARGO COMPARTMENT. REPAIRED STRINGER LOCATED STR 25L BETWEEN BS 787+11" TO BS 807+11" AFT CARGO COMPARTMENT IAW B737-300 SRM 53 -00-03-2R-1.

Part: RUB STRIP — CRACKED (NR 1 NACELLE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON RUBSTRIP LOCATED NACELLE STRUT ACCESS PANEL 57700L ENGINE NR 1 (2EA). REPLACED RUBSTRIP LOCATED NACELLE STRUT ACCESS PANEL 57700L ENGINE NR 1 (2EA) IAW B737-300 51-10-02 ITEM 8 51-40-02 AND DWG 65C26720.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON SUPPORT ANGLE LOC BS 947.5 AT LEVEL OF STR 25R IN AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS 947.5 AT LEVEL OF STR 25R IN AFT CARGO COMPARTMENT IAW B737-300 SRM.

Part: WEB — CRACKED (NR 1 PYLON) · airframe 83,086 hrs · 67,355 cycles

CRACK ON WEB LOCATED INTERNAL AREA AFT STRUT FAIRING 5743L ENGINE NR 1. REPLACED WEB (CHANNEL) LOCATED INTERNAL AREA AFT STRUT FAIRING 5743L ENGINE NR 1 IAW DWG 313A1355 AND SRM B737-300 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 767+2, STR 18L. REPAIRED SKIN IAW EO.

Part: WEB — CRACKED (NLG WW) · airframe 83,086 hrs · 67,355 cycles

NLG W/W WEB CRACKED AT BS 243.7+3.5, WL 169.1 LEFT SIDE. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 83,086 hrs · 67,355 cycles

NLG W/W WEB CRACKED AT BS 243.7+3.5, WL 169.1 LEFT SIDE. REPAIRED WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

FRAME CORRODED AT BS 747, BETWEEN STR 27L TO 27R. REPAIRED FRAME IAW SRM AND DWG.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 83,086 hrs · 67,355 cycles

CRACK ON EXISTING REPAIR TRACK TIE DOWN LOCATED BS 747 AND RBBL 13.80 IN AFT CARGO COMPARTMENT. REPAIRED TRACK TIE DOWN LOC BETWEEN BS 727 TO BS BS 767 AND RBBL 13.80 IN AFT CARGO COMPARTMENT IAW SRM B737 -300 53-00-53 REPAIR 2 FIG 201.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CORROSION ON TIE CLIP LOCATED BS 787+6" AND STR 26R IN AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED BS 787+6" AND STR 26R IN AFT CARGO COMPARTMENT IAW B737-300 SRM

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

CRACK ON SUPPORT ZEE ANGLE LOC BETWEEN BS 847 AND BS 867 AT LEVEL OF STR 25L IN AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE AND FASTENERS LOC BETWEEN BS 807 TO BS 907 AT LEVEL OF STR 25L IN AFT CARGO COMPARTMENT IAW B737-300 SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 781.5, STR 18L. REPAIRED SKIN IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,086 hrs · 67,355 cycles

SKIN CRACKED AT BS 520+4, STR 1. REPAIRED SKIN IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 82,876 hrs · 67,206 cycles

LEFT OVERWING EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED LEFT OVERWING EMERGENCY EXIT LENS AS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,807 hrs · 67,156 cycles

FUSELAGE SKIN CRACKED AT BS 900, STR 2R. REPAIRED SKIN IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,457 hrs · 66,896 cycles

R1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,402 hrs · 66,851 cycles

FUSELAGE SKIN CRACKED AT BS 437, STR 21L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 82,402 hrs · 66,851 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M & MT.

Part: POWER UNIT — FAULTY (E&E BAY) · airframe 81,236 hrs · 65,937 cycles

DECLARED EMERGENCY -- NO FLAP EXTENSION WHEN FLAP HANDLE MOVED TO FLAPS 5. FOLLOWING QRH WHEN ALT FLAP SWITCH WAS MOVED TO DOWN POS THE "ALT T/E FLAP DRIVE AC" CIRCUIT BREAKER POPPED. REMOVED AND REPLACED FLAP MOTOR HYD POWER UNIT PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,942 hrs · 65,702 cycles

STRINGER CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER SECTION IAW SRM AND BOEING DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,942 hrs · 65,702 cycles

SKIN CRACKED AT BS 360, STR 5R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,942 hrs · 65,702 cycles

SKIN CRACKED AT BS 362, STR 4L. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 80,906 hrs · 65,669 cycles

L2 DOOR SIDEWALL EMERGENCY EXIT SIGN BULBS INOP. REMOVED AND REPLACED BULBS IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 80,906 hrs · 65,669 cycles

R2 DOOR SIDEWALL EMERGENCY EXIT SIGN BULB INOP. REMOVED AND REPLACED BULB IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,906 hrs · 65,669 cycles

FUSELAGE SKIN IS CRACKED BETWEEN BS 394 TO BS 396, STR 2L. REPAIRED SKIN PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 80,904 hrs · 65,668 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 80,904 hrs · 65,668 cycles

FUSELAGE SKIN IS CRACKED BETWEEN BS 394 TO BS 396, STR 2L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,748 hrs · 65,558 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,748 hrs · 65,558 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT SIDEWALL LIGHT BULB INOP. RELAMPED LIGHT IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SIGN CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: BATTERY — BROKEN (CABIN) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY CHARGER AT POSITION M1133 MOUNTING PLATES BROKEN. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 867+5, STR 1. REPAIRED SKIN PER ER AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 500D, STR 26R. REPAIRED FRAME IAW ER AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 500, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND BEAR STRAP SKIN CRACKED AT BS 349, STR 21L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND BEAR STRAP SKIN CRACKED AT BS 305, STR 7R. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT SIDEWALL LIGHT BULB INOP. RELAMPED LIGHT IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 663, BETWEEN STR 2L TO STR 2R. REPAIRED FRAME PER SRM AND ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM T-CHORD CORRODED AT BS 986, BETWEEN RBL 26 TO RBL 40. REPAIRED BEAM PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, RBL 6. REPAIRED SHEAR TIE PER ER AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER EA.

Part: LENS — CRACKED (CABIN) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: ATTACH FITTING — CRACKED (L1 DOOR) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR ATTACH POINT CRACKED. REPAIRED ATTACH POINT IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 967, BETWEEN STR 19L TO STR 20L. REMOVED AND REPLACED FRAME PER SRM AND ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 663 TO BS 668, RBL 24.8. REMOVED AND REPLACED CHORD PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 947, STR 21L. REPAIRED FRAME IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 500A+4, STR 26L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 500, STR 26L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 481, STR 26L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 500B+2, STR 26L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 500C, STR 26L. REPAIRED STRINGER PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK FOUND, STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK FOUND, SHEAR TIE CORRODED AT BS 500D, STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOOR WEB CORRODED BETWEEN BS 986 TO BS 992, RBL 41. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 24L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 21L. REMOVED AND REPLACED CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 460, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: FLOORBEAM — LOOSE (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD LOOSE BETWEEN BS 727A+1735 TO BS 727A+18.5, RBL 23. REMOVED AND REPLACED CHORD PER DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 867, BETWEEN STR 22L TO STR 23L. REPAIRED FRAME PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,993 hrs · 64,984 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 500C+18, BETWEEN STR 26R TO STR 27R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,594 hrs · 64,668 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 500A, STR 1R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,594 hrs · 64,668 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 414, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,594 hrs · 64,668 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 500B, STR 2L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,594 hrs · 64,668 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 706, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,590 hrs · 64,667 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 500B, STR 2L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,590 hrs · 64,667 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 717, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,590 hrs · 64,667 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 717, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,590 hrs · 64,667 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 500A, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,590 hrs · 64,667 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 500B, STR 2L. REPAIRED SKIN PER SRM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 78,995 hrs · 64,222 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT OVERHEAD CENTER EMERGENCY EXIT LIGHT ASSY INOP. CONNECTED CONNECTOR PER WDM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR FWD LOWER CORNER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2R. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 497, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 7R. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 3L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, LBL 3. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD LOWER CONER CUTOUT. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,298 hrs · 63,709 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,787 hrs · 63,320 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 440, STR 16R. REPAIRED SKIN PER ER AND EA.

Part: FAN — FAULTY (AC BAY) · airframe 77,837 hrs · 63,354 cycles

CREW REPORTED BURN SMELL. REMOVED AND REPLACED ALTERNATE EQUIPMENT COOLING BLOWER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,789 hrs · 63,321 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 434, STR 16R. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,789 hrs · 63,321 cycles

DURING SCHEDULED OTS CHECK, FOUND STUB FRAME CRACKED AT R1 DOOR. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 77,787 hrs · 63,320 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 4 SLAT O/B LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,685 hrs · 63,238 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 472, STR 17L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,685 hrs · 63,238 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 311, STR 19R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,685 hrs · 63,238 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 476, STR 17L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,685 hrs · 63,238 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 386, STR 15R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,685 hrs · 63,238 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 331.5, STR 19R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,704 hrs · 63,252 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 472, STR 17L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,704 hrs · 63,252 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 476, STR 17L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,704 hrs · 63,252 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 311, STR 19R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,704 hrs · 63,252 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 386, STR 15R. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,685 hrs · 63,238 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CRACKED AT BS 500B, BETWEEN STR 15L TO STR 16L. REPAIRED SHEAR TIE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,685 hrs · 63,238 cycles

DURING SCHEDULED OTS CHECK, FOUND RT EEPLS INOP AT ROW 2. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,685 hrs · 63,238 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 764 TO BS 809, STR 18L. REPAIRED SKIN PER ER AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,685 hrs · 63,238 cycles

DURING SCHEDULED OTS CHECK, FOUND RT AFT EEPLS INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 77,084 hrs · 62,760 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (R2 DOOR) · airframe 76,279 hrs · 62,144 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR CRACKED THROUGH RIVET ON AFT LOWER CORNER OF OUTER SKIN. REPAIRED DOOR PER SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 76,279 hrs · 62,144 cycles

DURING SCHEDULED HC1 CHECK, FOUND FLOORBEAM SUPPORT STRAP CRACKED AT BS 312, LBL 15. REPAIRED STRAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,279 hrs · 62,144 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED AT R2 DOOR UPPER LATCH ROLLER TORQUE TUBE CENTER BEARING SUPPORT RIB. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 75,736 hrs · 61,739 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,594 hrs · 61,629 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 685, STR 9R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,594 hrs · 61,629 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 695, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,594 hrs · 61,629 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 711, STR 10R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 74,834 hrs · 61,076 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,834 hrs · 61,076 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 947, STR 23R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,834 hrs · 61,076 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 703, STR 10R. REPAIRED SKIN PER EA.

Part: LENS — CRACKED (CABIN) · airframe 74,834 hrs · 61,076 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 74,369 hrs · 60,729 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,335 hrs · 60,695 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 500, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,290 hrs · 60,657 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 500 TO BS 513A, STR 16L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,290 hrs · 60,657 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 446, STR 16L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,290 hrs · 60,657 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 516B, STR 16L. REPAIRED SKIN PER EA.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 74,103 hrs · 60,516 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE FROM BUSTLE. REMOVED AND REPLACED SLIDE PER MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,447 hrs · 6,026 cycles

AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT AT BS 291, WL 261. REPAIRED SKIN PER AAR EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 400, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 639, BETWEEN STR 16R TO STR 17R. REPAIRED FRAME PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT BETWEEN BS 291 TO BS 304, BETWEEN WL 233 TO WL 238. REPAIRED SKIN PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 670, BBL 0, WL 207. REPAIRED BEAM PER SI.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 360, STR 16L. REPAIRED STRINGER PER ACO.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED LIGHT PER SRM.

Part: LENS — MISSING (CABIN) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE BEARSTRAP SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BETWEEN BS 303 TO BS 304, BETWEEN BS WL 256 TO WL 258. REPAIRED SKIN PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, LBL 24. REPAIRED BEAM PER AAR EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 639, STR 17R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CRACKED AT BS 663, LBL 24. REPAIRED BEAM PER AAR EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT CREASE BEAM WEB CRACKED BETWEEN BS 639 TO BS 664. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND RADIO ALTIMETER BELLY SKIN CUTOUT CRACKED AT BS 410. REPAIRED SKIN PER BOEING SB AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 663 TO BS 669, BBL 0. REPAIRED BEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 359, STR 16L. REPAIRED STRINGER PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 886, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 540, STR 27R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT E&E EQUIPT COMPT EXHAUST CUTOUT, BETWEEN BS 360 TO BS 380. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED AT BS 709, RBL 24. REPAIRED BEAM PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CHORD CRACKED AT BS 616, RBL 65. REPAIRED CHORD PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 708, RBL 24. REPAIRED WEB PER AAR EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 27R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 787, STR 25L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 747 TO BS 767. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SLAT O/B EDGE DELAMINATED. REPAIRED SLAT PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,041 hrs · 59,736 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 827, STR 27R. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,969 hrs · 59,685 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 480, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,969 hrs · 59,685 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 420, STR 22L. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 71,792 hrs · 58,851 cycles

DURING SCHEDULED HC2 CHECK, FOUND KEEL BEAM CORRODED AT BS 500C + 10. REMOVED AND REPLACED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,726 hrs · 58,803 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR CUTOUT AFT UPPER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 581 S10R) · airframe 71,726 hrs · 58,803 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 581, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 773 S20L) · airframe 71,726 hrs · 58,803 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 20L. REPAIRED SKIN PER SRM.

Part: FAN — FAULTY (E&E BAY) · airframe 71,346 hrs · 58,514 cycles

DECLARED EMERGENCY. ON DESCENT INTO ELP CREW REPORTED STRONG BURNING SMELL. GASPER AND RECIRC FANS TURNED OFF SMELL DISSIPATED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 70,363 hrs · 57,804 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,160 hrs · 57,642 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 405, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,160 hrs · 57,642 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 427, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,160 hrs · 57,642 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,264 hrs · 56,959 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (BS 980 S21L) · airframe 69,138 hrs · 51,260 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 513 S16L) · airframe 68,759 hrs · 56,557 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 750 S18L) · airframe 68,759 hrs · 56,557 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 68,498 hrs · 56,348 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,108 hrs · 42,810 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM.

Part: PRESSURE PANEL — CORRODED (NLG W/W) · airframe 68,483 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT NLG W/W PRESSURE WEB CORRODED AT BS 251.6. REPAIRED WEB PER EA AND SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,433 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 360, LBL 2. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 68,483 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 16 ABC. INSTALLED STRIP PER MM.

Part: BOLT — WORN (RT ELEVATOR TAB) · airframe 68,483 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BOLT AND BUSHING PER MM.

Part: BOLT — WORN (LT ELEVATOR TAB) · airframe 68,483 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BOLT AND BUSHING PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 68,483 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM WEB CRACKED AT BS 711, LBL 4. REPAIRED WEB PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,483 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 1 CRACKED AT BS 344. REPAIRED STRINGER PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 68,483 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING INBOARD MID FLAP T/E DELAMINATED. REMOVED AND REPLACED MID FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,483 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739A, STR 2R. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,483 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27R CORRODED AT BETWEEN BS 376 AND BS 380, WL 149. REPAIRED STRINGER PER SRM.

Part: FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 68,483 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (R1 DOOR GIRT BAR) · airframe 68,483 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 68,483 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — LOOSE (R1 DOOR GIRT BAR) · airframe 68,483 hrs · 56,335 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: ENGINE — VIBRATION (RIGHT) · airframe 68,371 hrs · 56,247 cycles

INFLIGHT SHUTDOWN/DIVERSION. NR 2 ENGINE EXPERIENCED COMPRESSOR STALLS AND EXCESSIVE VIBRATION. SHUTDOWN NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: SPOILER — FAULTY (LT WING) · airframe 67,747 hrs · 55,740 cycles

SIGNIFICANT ROLL TO LEFT ON APPROACH WITH FLAPS AT 40. R&R NR 2 SPOILER PER MM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 67,465 hrs · 55,519 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 67,084 hrs · 55,237 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 66,820 hrs · 55,031 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 66,811 hrs · 55,022 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,615 hrs · 54,869 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 792, STR 19L. REPAIRED SKIN PER SRM.

Part: CONNECTOR — FAULTY (NR 1 GENERATOR) · airframe 54,803 hrs · 66,522 cycles

T/R-1 C/B TRIPPED ALONG WITH EQUIP COOLING BLOWER C/B. FOUND NR 1 ENG GEN D5124P & J CONNECTOR BURNED. REMOVED AND REPLACED CONNECTOR & C-CONTROL PIN PER MM.

Part: VALVE — FAULTY (FWD CARGO) · airframe 54,597 hrs · 66,250 cycles

DIVERSION (OKC - MCI) FWD CARGO COMPT FIRE WARNING LIGHT IND BOTTLE DISCHARGED. REMOVED AND REPLACED CARGO FIRE DIVERTER VALVE & FIRE DISCHARGE BOTTLE PER MM.

Part: CHARGER — FAULTY (E/E BAY) · airframe 54,597 hrs · 66,250 cycles

DIVERSION (OKC - MCI) TR-1 C/B TRIPPED, FOLLOWED BY FUMES. BATTERY CHARGER C/B TRIPPED DURING TAXIING. REMOVED AND REPLACED ACFT BATTERY CHARGER, AND TR-1 PER MM.

Part: SKIN — CRACKED (BS 500B S18L) · airframe 66,264 hrs · 54,610 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 65,807 hrs · 54,255 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,783 hrs · 54,230 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,678 hrs · 54,138 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER BOEING DRAWING AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,678 hrs · 54,138 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER CUTOUT BS 427, BL 0. REPAIRED SKIN PER ER.

Part: STRINGER SPLICE — CRACKED (BS 360 S15L) · airframe 65,678 hrs · 54,138 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE IAW SRM.

Part: SKIN — CRACKED (BS 440 S16R) · airframe 65,033 hrs · 53,638 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 16R. REPAIRED SKIN PER SRM.

Part: CASTING — BROKEN (LT WING SPOILER) · airframe 64,352 hrs · 53,137 cycles

DURING SCHEDULED A1 CHECK, FOUND LT WING NR 4 GROUND SPOILER HINGE CASTING BROKEN AT OUTBOARD END. REMOVED AND REPLACED SPOILER PER MM.

Part: ACTUATOR — BROKEN (NR 5 SPOILER) · airframe 64,030 hrs · 52,881 cycles

NR 5 SPOILER ACTUATOR BROKEN AT ATTACH MOUNT. REMOVED AND REPLACED ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,036 hrs · 52,094 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,036 hrs · 52,094 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,036 hrs · 52,094 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 357, STR 15L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — LOOSE (ROW 17 DEF) · airframe 62,192 hrs · 51,430 cycles

EEPLS TRACK LOOSE AT ROW 17 DEF. SECURED TRACK PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,350 hrs · 50,716 cycles

DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: FITTING — CORRODED (HORIZONTAL STABS) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED HORIZONTAL LUG FITTINGS PER SRM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND NR 3 L/E SLAT DELAMINATED. REPAIRED NR 3 L/E SLAT PER SRM.

Part: BEAM — CORRODED (LT MLG) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND LT MLG ATTACH BEAM CORRODED. REPAIRED ATTACH BEAM PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 360 TO BS 371, LBL 64, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION WEB PER SRM.

Part: SPAR — CORRODED (VERTICAL FIN) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL FIN FWD AND AFT SPAR, RT AND LT CLEVIS LUGS, CORRODED. REPAIRED VERTICAL FIN PER ER.

Part: BEAM — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH LONGITUDINAL BEAMS FROM BS 540 TO BS 727, BETWEEN BS RBL 24 TO RBL 45, CORRODED. REPAIRED LONGITUDINAL BEAMS PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 344, FROM LBL 7 TO RBL 9, CORRODED. REPAIRED CHORD PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 638, CRACKED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND GIRT BAR FITTING AT BS 344, LBL 59, CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: FITTING — CORRODED (RT MLG BEAM) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND RT MLG BEAM STABILIZER LINK FITTING, CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STABILIZER LOWER THRUST BRACE LOWER ATTACH FITTING CORRODED. REPAIRED THRUST FITTING PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN AT STATION 127, CRACKED. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 986.5, FROM LBL 50 TO RBL 50, CORRODED. REPAIRED FLOORBEAM CHORD PER ER.

Part: SPAR — CRACKED (RT WING) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING REAR SPAR UPPER CHORD AT STATION 223, CRACKED. REMOVED AND REPLACED REAR SPAR SECTION PER ER AND BAC DRAWING.

Part: BEAM — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EACH CRACKS ON LONGITUDINAL BEAMS FROM BS 540 TO BS 727B, FROM RBL 45 TO LBL 24. REPAIRED BEAMS PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM INNER CHORD ANGLE AT BS 360, LBL 64, CORRODED. REMOVED AND REPLACED CREASE BEAM CHORD ANGLE PER SRM.

Part: SPAR — CRACKED (LT WING) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND LT WING REAR SPAR AT STATION 285, 12 O'CLOCK POSITION, CRACKED. REMOVED AND REPLACED REAR SPAR SECTION PER ER AND BAC DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH FRAMES CRACKED AT BS 480, STRINGER 8R AND STRINGER 8L. REPAIRED FRAME SECTIONS PER SRM.

Part: STRUCTURE — CRACKED (BS 787-847) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND STRUCTURE CRACKED FROM BS 787 TO BS 847, STRINGER 8L. REPAIRED STRUCTURE SECTION PER SRM.

Part: FITTING — CORRODED (RT MLG) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND RT MLG STABILIZER LINK FWD ATTACH FITTING, CORRODED. REMOVED AND REPLACED FWD FITTING PER SRM.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD, CORRODED. REPAIRED CHORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT BS 270, FROM LBL 11 TO RBL 11, CORRODED. REMOVED AND REPLACED CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 380, STRINGER 13L, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 188, RBL 33, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D CHECK, FOUND FRAME FROM BS 827 TO BS 907, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 727C + 5, STRINGER 2R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT FWD SERVICE DOOR LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 927 TO BS 947, LBL 55, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB FROM BS 188 TO BS 196, LBL 32 TO RBL 32, CRACKED. REMOVED AND REPLACED FLOOR WEB PER SRM.

Part: FITTING — CORRODED (LT MLG) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND LT MLG AFT SPAR SUPPORT BEAM STABILIZER FITTING LUG FACES, CORRODED. REMOVED AND REPLACED SUPPORT FITTING PER BAC DRAWING AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 500C, STRINGER 15R, CRACKED. REPAIRED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 360, STRINGER 14L, CRACKED. REPAIRED SKIN PER ER.

Part: SPLICE — CRACKED (BS 400) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 400, STRINGER 14L AND STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 500D, STRINGER 8L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER SPLICES FROM BS 400 TO BS 420, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 380, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 1128, RBL 26, CORRODED. REMOVED AND REPLACED FRAME SECTION PER BAC DRAWING, SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 380, BETWEEN STRINGERS 13L AND 14L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED BETWEEN BS 500 AND BS 500D, FROM STRINGER 26L TO STRINGER 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (LT WING) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND LT MLG STABILIZER BEAM FWD LUG, CORRODED. REMOVED AND REPLACED LT MLG FITTING PER MM.

Part: SPLICE — CRACKED (BS 908) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STRINGER 4R & STRINGER 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FITTING — CORRODED (LT WING) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND LT WING GEAR SPAR FITTING CORRODED. REMOVED AND REPLACED SPAR FITTING PER BAC DRAWING.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 840, LBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 360, STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT BS 360, BL 0, CORRODED. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT BS 294, LBL 11, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 360 TO BS 380, LBL 64, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: SHEAR TIE — CORRODED (BS 727E) · airframe 61,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED BETWEEN BS 727E AND BS 747, FROM LBL 6 TO RBL 6. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT BS 328, FROM LBL 49 TO RBL 55, CORRODED. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, BETWEEN STRINGERS 23L AND 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND BULKHEAD PRESSURE DOME WEB AT BS 1016, 1 O`CLOCK POSITION, CRACKED. REPAIRED WEB PER ER.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 807, STRINGER 25L, CORRODED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 967, FROM LBL 27 TO RBL 27, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 887, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 787, STRINGER 20R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR SHEAR WEB AT BS 1014, LBL 37, CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 60,457 hrs · 49,981 cycles

DURING SCHEDULED D-CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FWD AND AFT SPARS, UPPER ATTACH LUGS AND CLEVIS, CORRODED. REPAIRED HORIZONTAL STAB PER SRM.

Part: GIRT BAR — BROKEN (R2 DOOR) · airframe 59,923 hrs · 49,558 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR BROKEN. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,865 hrs · 49,522 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 767, STRINGER 19R AND BS 927, STRINGER 25R. REPAIRED SKIN SECTIONS PER EA AND SRM.

Part: SIGN — WORN (EMERGENCY LIGHT) · airframe 59,861 hrs · 49,517 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGNCY EXIT SIGN WORN. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,709 hrs · 49,395 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 519, STRINGER 16L, CRACKED. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 58,995 hrs · 48,813 cycles

DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE ATTACH BUSHINGS PER MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 58,340 hrs · 48,296 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AFT ENTRY DOOR LIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,279 hrs · 48,254 cycles

DURING SPV, FOUND RT BULKHEAD FRAME AT BS 178, WL 207, CRACKED. REMOVED AND REPLACED RT FRAME PER ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 58,271 hrs · 48,249 cycles

DURING SPV, FOUND FLOOR STRUCTURE WEB AT BS 180, RBL 24, CRACKED. REMOVED AND REPLACED FLOOR WEB PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 58,145 hrs · 48,152 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR, FORWARD DOOR FRAME CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,976 hrs · 48,007 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500D + 2, STRINGER 15R, CRACKED. REPAIRED SKIN PER SRM.

Part: STIFFENER — CORRODED (BULKHEAD) · airframe 57,976 hrs · 48,007 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BS 1016, STIFFENER AT DRAIN HOLE CORRODED. REPAIRED STIFFENER PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,726 hrs · 47,809 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT LAP SEAM, BS 540, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,365 hrs · 47,518 cycles

DURING SCHEDULED PM CHECK, FOUND SKIN CRACKED AT BS 312, STRINGER 25R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 56,240 hrs · 46,621 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT LOWER SURFACE. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 56,240 hrs · 46,621 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE RELEASE CABLE MISROUTED. REROUTED SLIDE RELEASE CABLE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,091 hrs · 46,162 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT UPPER EMERGENCY FLASHLIGHT STRAP BROKEN AND STATUS LIGHT ON STEADY. REMOVED AND REPLACED STRAP AND BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (ENTRY DOOR) · airframe 55,344 hrs · 45,887 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 54,131 hrs · 44,971 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: FIRE LOOP — MALFUNCTIONED (APU BAY) · airframe 53,488 hrs · 44,458 cycles

AIR TURNBACK, APU FIRE WARNING LIGHT AND BELL WENT OFF AT APPROX 1000 FEET. COMPLIED WITH AIRCRAFT PROCEDURES CHECK LIST, AND DISCHARGED APU FIRE BOTTLE. APU FIRE WARNING LIGHT WOULD NOT EXTINGUISH. COMPLIED WITH APU COMPT AND APU INSP. NO EVIDENCE OF FIRE NOTED.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 53,040 hrs · 44,113 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 34. REPAIRED BEADED WEB PER SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 53,040 hrs · 44,113 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT KEEL BEAM LEG CRACKED AND CORRODED AT STR 27R, BS 727 PLUS 9 AND BS 727 PLUS 15. REPAIRED KEEL BEAM PER SWA EA.

Part: SKIN — BULGED (FUSELAGE) · airframe 53,040 hrs · 44,113 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN BULGED AT BS 727 + 15,STR 27R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 53,040 hrs · 44,113 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT HORIZ STAB UPPER OUTBOARD SURFACE SKIN CORRODED. REPAIRED LT HORIZ STAB PER SWA EA.

Part: PANEL — BULGED (HORIZ STAB) · airframe 53,040 hrs · 44,113 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT HORIZ STAB UPPER OUTBOARD SURFACE PANEL BULGING ON BOTH INBOARD AND OUTBOARD FWD CORNERS. REPAIRED RT HORIZ STAB PER SWA EA'S.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,521 hrs · 42,897 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 19R, BS'S 745, AND 727E PLUS 12 AND PLUS 4. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 51,521 hrs · 42,897 cycles

DURING SCHEDULED BC3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,484 hrs · 42,868 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 213 AT LBL 5.0 AND WL 195 AT RBL 21. REPAIRED WEB PER SRM.

Part: WIRE — LOOSE (CABIN) · airframe 50,928 hrs · 42,428 cycles

WITH ALL ELECT PWR REMOVED FROM A/C, EMERGENCY EXIT LIGHTS REMAINED ILLUMUNATED WITH LIGHT SWITCH IN OFF POS. FOUND WIRE LOOSE. SECURED WIRE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,686 hrs · 42,229 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH LT CABIN DOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM.

Part: LENS — LOOSE (CABIN DOORS) · airframe 50,686 hrs · 42,229 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENSES PER MM.

Part: LANDING GEAR — MALFUNCTIONED (NLG & MLG) · airframe 49,782 hrs · 41,499 cycles

DURING CLIMB WHEN MOVING GEAR HANDLE FROM UP TO OFF, GEAR STARTED TO EXTEND. RECYCLED HANDLE TO UP. ON APPROACH MOVED HANDLE FROM UP TO OFF AND GEAR REMAINED UP. INSPECTED LANDING GEAR SELECTOR VALVE. LANDING GEAR EXTENSION AND RETRACTION SYSTEM CHECKS NORMAL PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,877 hrs · 70,722 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727 + 12 IN, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,820 hrs · 39,822 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 3.75 EXTERNAL FUSELAGE SKIN CRACK AT BS 500D, STR 12L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (ELEVATOR TAB) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED 1/2 D CHECK, FOUND LT ELEVATOR TAB LOWER SKIN CRACKED AROUND NR 3 AND NR 4 HINGE BEARING CUTOUTS. R & R TAB ASSY PER MM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 44,599 hrs · 39,066 cycles

DURING SCHEDULED 1/2 D CHECK, FOUND L-1 AND R-1 COCKPIT WINDOW FRAMES CRACKED ON OUTBOARD CORNER. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED 1/2 D CHECK, FOUND BS 178 BULKHEAD LH SIDE CHORD CRACKED, LBL 26. REPAIRED CHORD SECTION PER SRM.

Part: BULKHEAD — CORRODED (CABIN) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 PRESSURE BULKHEAD CORRODED JUST BELOW CABIN FLOOR LINE, BL 0. REPAIRED BULKHEAD PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 8 LT FWD LEG ANGLE CRACKED, BS 294.5. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (PAX DOOR) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED HALF D CHECK, FOUND FWD ENTRY DOOR AFT FRAME CRACKED AROUND 4TH AND 5TH STOP FITTINGS. REPAIRED FRAME PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED HALF D CHECK, FOUND KEELBEAM LOWER CHORD CORRODED, BS 727+14, STRINGER 27 LT. REPAIRED PER SWA RA 1-353-2250.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED HALF D CHECK, FOUND 2 EACH STRINGER CLIPS CRACKED, BS 663, STRINGERS 9 LT AND 9 RT. R&R CLIPS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED HALF D CHECK, FOUND AFT ENTRY DOOR LOWER FWD FUSELAGE SKIN CUT OUT CRACKED. REPAIRED PER SWA RA 1-353-2251.

Part: GIRT BAR — CORRODED (ESCAPE SLIDE) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED HALF D CHECK, FOUND FWD SERVICE DOOR BOTH EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. R&R BOTH BRACKETS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED HALF D CHECK, FOUND BS 294 FLOOR BEAM UPPER SURFACE CORRODED, LBL11 TO RBL 27. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED HALF D CHECK, FOUND STUB FRAME CRACKED AT FWD SIDE OF FWD SERVICE DOOR CUT OUT, STRINGER 17 RT. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED HALF D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT LOWER END. REPAIRED FRAME PER BAC DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED HALF D CHECK, FOUND BS 312 FLOORBEAM UPPER SURFACE CORRODED. LBL 11 TO RBL 21. REPAIRED FLOORBEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 44,599 hrs · 37,066 cycles

DURING SCHEDULED HALF D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 1. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (BS 747 - 767)

DURING SCHEDULED RON, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 747-767, BETWEEN STRINGERS 19R-20R. REPAIRED SKIN PER SRM.

Part: SEAL — LEAKING (SERVICE DOOR)

DIVERSION VERY LOUD PRESSURIZATION LEAK NOISE IN AFT SERVICE DOOR. (DIVERTED TO PHX). ADJUSTED AFT SERVICE DOOR PER MM.

Part: BATTERY PACK — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT DOOR, EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — DEPLOYED (SERVICE DOOR)

DURING SCHEDULED SPECIAL VISIT, FWD SERVICE DOOR EVACUATION SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP IN AFT END OF CABIN. REMOVED AND REPLACED BATTERY AND CHARGER PER MM.

Part: SLIDE — LOW PRESS (PASSENGER DOOR)

FWD ENTRY DOOR EVACUATION SLIDE PRESS LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER SWA RA NR 1-353-2073.

Part: LENS — BROKEN (RT EMER EXIT)

DURING SCHEDULED BC4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (NR 6 LE SLAT)

DURING SCHEDULED BC4 CHECK, FOUND NR 6 SLAT CRACKED NEXT TO ACTUATOR CUT OUT. REPAIRED SLAT ASSY PER SRM AND SWA RA NR 1-357-0687.

Part: LENS — MISSING (LT EMER EXIT)

DURING SCHEDULED BC4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — DETACHED (SERVICE DOOR)

FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE FELL OUT. REPACKED SLIDE PER MM.

Part: LINE — CHAFED (B-HYD SYST)

LOST ALL B-HYDRAULIC FLUID IN FLIGHT. AIRCRAFT DIVERTED TO PHX. FOUND ELE B PUMP HYDRAULIC LINE CHAFED THROUGH. REMOVED AND REPLACED LINE, B SYSTEM ENG AND ELE PUMPS CASE DRAIN FILTERS PER M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING PREFLIGHT CHECK, FOUND AFT UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER BOEING M/M.

Part: FRAME — CORRODED (BS 747)

DURING SCHEDULED 1/4 D-CHECK, FOUND BELTFRAME CORRODED AT BS 747. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (PAX DOORWAY)

DURING SCHEDULED C2 CHECK, FWD FUSELAGE SKIN CRACKED .25 INCH AT UPPER HINGE CUTOUT OF AFT ENTRY DOOR. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED B/C CHECK, FOUND A .25 INCH CRACK AT AFT ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED PER BOEING SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED A-CHECK, FOUND EMERGENCY LIGHT AT AFT SERVICE DOOR INOP. REPLACED AND OP CHECKED PER BOEING M/M.

Part: SKIN — GOUGED (BS 300-400)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN GOUGED FROM BS 390 TO 400, BETWEEN S19 AND 20R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SHEAR TIE — CORRODED (BS 887)

DURING SCHEDULED TRANSITION CHECK, FOUND SHEAR TIE CORRODED AT BS 887, BETWEEN S27 R AND L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: ANGLE — CORRODED (BS 270)

DURING SCHEDULED TRANSITION CHECK, FOUND TOP CHORD Z-ANGLE CORRODED AT BS 270, RBL 2 LBL 10, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CREASE (BS 767-820/460)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN CREASED AT BS 767 TO 820, AT S24 TO 26L, AND BS 460, FROM S28L TO S28R, AT SHEAR TIE LOCATION. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORRODED AT BS 328 LBL 49 WL 208, BS 294 LBL 10 TO RBL 10 WL 208, BS 986.5 WL 208 RBL 57 TO LBL 57, BS 312 LBL 10 RBL 10 WL 208, AND AT BS 344 RBL 10 TO LBL 40 WL 208. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (NR 5 SLAT)

DURING SCHEDULED TRANSITION CHECK, FOUND NR 5 SLAT SKIN LOWER T/E SKIN CRACKED. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND DRAWING BAC 65C30133.

Part: DOOR FRAME — CRACKED (BS 294)

DURING SCHEDULED TRANSITION CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED FROM LOWER EDGE TO FASTENER HOLE, BS 294, WL 208, RBL 55. REPLACED FRAME PER BOEING STRUCTURAL REPAIR MANUAL.

Part: BLKHD WEB — CRACKED (BS 178)

DURING SCHEDULED TRANSITION CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 178 RBL 5.5 WL 198. REPAIRED PER TRAMCO EWO 95-0337.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 265, BETWEEN S17R AND S18L, BS 282, S15L, BS 827, BETWEEN S9 AND 10R, BS 920, WL 204, S17-18L, BS 342 AND 350, BETWEEN S20 AND 21R, BS 355, BETWEEN S18R AND 19R, AT BS 338, S18R, BS 1064, AT S22R, BS 378, BETWEEN S19 AND 20R, AND BS 920, BETWEEN S17 AND 18L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: STRINGER — DAMAGED (BS 334)

DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER DAMAGED AT BS 334, S10R, AND STRINGER CRACKED AT BS 294, AT S4R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: CLIP — CRACKED (BS 616/663.75)

DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIPS CRACKED AT BS 616, S8L, AND AT BS 663.75 AT S10L AND R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.