N369SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,981 hrs · 59,365 cycles

FUSELAGE SKIN CRACKED AT STATION 915, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,981 hrs · 59,365 cycles

FUSELAGE SKIN CRACKED AT STATION 732, STRINGER 7R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,981 hrs · 59,365 cycles

FUSELAGE SKIN CRACKED AT STATION 355, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,981 hrs · 59,365 cycles

FUSELAGE SKIN CRACKED AT STATION 743, STRINGER 5R. REPAIRED SKIN IAW EA.

Part: LIGHT — OUT OF ADJUST (CABIN) · airframe 71,035 hrs · 58,704 cycles

CABIN CEILING EMER EXIT LIGHT OUT OF ADJUSTMENT. ADJUSTED LIGHT IAW AMM.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 71,035 hrs · 58,704 cycles

R2 DOOR EMER EVAC SLIDE, FWD UPPER BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,959 hrs · 58,649 cycles

FORWARD CARGO, AFT CARGO FRAME INNER FLANGE STRAP CRACKED. R & R STRAP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,959 hrs · 58,649 cycles

FORWARD CARGO, AFT CARGO FRAME OTBD FLANGE, UPPER RADIUS FILLER CRACKED. REPAIRED FLANGE IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,959 hrs · 58,649 cycles

C1 DOOR CUT OUT IN FUSELAGE FRAME CRACKED AT BS 492, IN FRAME WEB AT INBD TOP CORNER OF NR 5 DOOR STOP MOUNT AREA. R & R FRAME IAW ACO & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,959 hrs · 58,649 cycles

SKIN CRACKED AT BS 360, BETWEEN STRINGER 5R - 6R. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,724 hrs · 58,448 cycles

LEFT WING OTBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.

Part: ARM — CRACKED (LT MLG) · airframe 70,433 hrs · 58,217 cycles

LEFT MLG BEAM ARM CRACKED. R & R BEAM ARM IAW MM.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 69,355 hrs · 57,442 cycles

RIGHT WING INBD FLAP OTBD TRACK FAIRING DELAMINATED AT OTBD SIDE. R & R FAIRING IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,355 hrs · 57,442 cycles

LEFT WING INBD MID FLAP TE WEDGE, LOWER INBD SKIN DELAMINATED. R & R WEDGE IAW MM.

Part: SIGN — OUT OF ADJUST (CABIN) · airframe 69,355 hrs · 57,442 cycles

RIGHT OVERWING EXIT SIGN OUT OF ADJUSTMENT. ADJUSTED SIGN IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 69,261 hrs · 57,375 cycles

OVERHEAD OVERWING EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 68,894 hrs · 57,115 cycles

DECLARED EMER. ACFT WOULD NOT DEPRESSURIZE, CABIN STUCK AT 6000' IN AUTO. R & R CABIN PRESS CONTROLLER IAW MM.

Part: ANGLE — CRACKED (RT AILERON) · airframe 68,545 hrs · 56,862 cycles

RIGHT WING LOWER L ANGLE FOR AILERON WHIPPER PANEL CRACKED AT INBD END AT RSS 529. R & R L ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,545 hrs · 56,862 cycles

WEB CRACKED BETWEEN BS 986 TO 1016 LBL 45. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,545 hrs · 56,862 cycles

FRAME WEB CRACKED AT BS 616 STRINGER 16R. REPAIRED FRAME IAW EA & ER.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,545 hrs · 56,862 cycles

COMPRESSION BEAM SPLICE FITTING CRACKED AT BS 727 LBL 45.5. REPAIRED FITTING IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,545 hrs · 56,862 cycles

COMPRESSION BEAM SPLICE FITTING CRACKED AT BS 727 RBL 45.5. REPAIRED FITTING IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,545 hrs · 56,862 cycles

FUSELAGE SKIN CRACKED AT BS 298 STRINGER 21R. REPAIRED SKIN IAW ER & EA.

Part: SUPPORT FITTING — CORRODED (EMERGENCY EXIT) · airframe 68,545 hrs · 56,862 cycles

LEFT OVERWING EMER EXIT HATCH LOWER DOOR HANDLE SUPPORT FITTING CORRODED. R & R FITTING IAW SRM & DWG.

Part: SUPPORT FITTING — CORRODED (EMERGENCY EXIT) · airframe 68,545 hrs · 56,862 cycles

RIGHT OVERWING EMER EXIT HATCH LOWER DOOR HANDLE SUPPORT FITTING CORRODED. R & R FITTING IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,545 hrs · 56,862 cycles

FLOORBEAM HORIZONTAL CHORD CORRODED AT BS 986 BETWEEN LBL 5 TO LBL 40. REPAIRED CHORD IAW ER & EA.

Part: TOGGLE — LOOSE (TE FLAP) · airframe 68,545 hrs · 56,862 cycles

RIGHT WING INBD FORE FLAP INBD TOGGLE OTBD FWD ROLLER LOOSE. R & R TOGGLE IAW AMM.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 68,545 hrs · 56,862 cycles

RIGHT WING NR 2 PYLON UPPER AFT PANEL SUPPORT BEAM INBD L ANGLE CRACKED. R & R L ANGLE IAW SRM.

Part: KEELBEAM — DELAMINATED (FUSELAGE) · airframe 68,545 hrs · 56,862 cycles

KEEL BEAM DELAMINATED AT BS 597 RBL 4. R & R KEEL BEAM IAW SRM.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 68,545 hrs · 56,862 cycles

LEFT WING NR 1 PYLON UPPER AFT PANEL SUPPORT INBD L ANGLE CRACKED. R & R L ANGLE IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 68,545 hrs · 56,862 cycles

RIGHT WING TE AT RSS 515 AILERON WHIPPER PANEL OTBD UPPER ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (LT AILERON) · airframe 68,545 hrs · 56,862 cycles

LEFT WING AILERON WHIPPER PANEL OTBD END ANGLE CRACKED AT LOWER FASTENER AT RSS 545. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,545 hrs · 56,862 cycles

FORWARD GALLEY DOOR CUT OUT CRACKED AT BS 294 RBL 57. REPAIRED CUT OUT IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,545 hrs · 56,862 cycles

VERTICAL STIFFENER CRACKED AT BS 328 RBL 30. R & R STIFFENER IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,545 hrs · 56,862 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 359 STRINGER 7L. REPAIRED SPLICE IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 68,545 hrs · 56,862 cycles

MAIN WW BEADED PRESS DECK CRACKED AT BS 666 BETWEEN RBL 39 TO 41. REPAIRED DECK IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,545 hrs · 56,862 cycles

FLOORBEAM CORRODED AT BS 312 BL 0. REPAIRED BEAM IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 68,545 hrs · 56,862 cycles

CHORD CRACKED AT BS 727 STRINGER 18A LT. REPAIRED CHORD IAW ER & EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 68,545 hrs · 56,862 cycles

CHORD CRACKED AT BS 727 STRINGER 18A RT. REPAIRED CHORD IAW ER & EA.

Part: WINDOW — CRACKED (COCKPIT) · airframe 68,219 hrs · 56,606 cycles

NR 1 OUTER WINDOW PANE ARCED & CRACKED. R & R WINDOW IAW MM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 67,604 hrs · 56,152 cycles

MLG WW PRESS DECK BEADED WEB CRACKED AT STATION 667, LBL 36. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,440 hrs · 54,602 cycles

SKIN CRACKED BETWEEN STATION 433 TO 436, STRINGER R. REPAIRED DOUBLER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,440 hrs · 54,602 cycles

SKIN CRACKED BETWEEN STATION 433 TO STATION 436, STRINGER 2R. REPAIRED SKIN IAW SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 65,281 hrs · 54,485 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: LENS — CRACKED (CABIN) · airframe 65,143 hrs · 54,385 cycles

L1 DOOR THRESHOLD EMERGENCY EXIT LIGHT LENS CRACKED. R & R LENS IAW M/M.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 64,312 hrs · 53,773 cycles

L1 DOOR FWD LOWER FRAME CRACKED. REMOVED AND REPLACED L1 DOOR PER MM.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 64,312 hrs · 53,773 cycles

FORWARD FRAME CRACKED AT L1 DOOR. REMOVED AND REPLACED L1 DOOR ASSY PER MM.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 63,982 hrs · 53,552 cycles

F/A'S REPORT FWD GALLEY SERVICE DOOR DIFFICULT TO OPEN. ADJUSTED AND LUBRICATED DOOR AS PER MM.

Part: RUB STRIP — CRACKED (KRUEGER FLAP) · airframe 63,662 hrs · 53,314 cycles

CRACK ON RUB STRIP LOCATED ON DOOR WING LEADING EDGE KRUEGER FLAP L/E 118.56 LT WING. REPLACED RUB STRIP LOCATED ON DOOR WING LEADING EDGE KRUEGER FLAP LEADING EDGE 118.56 LT WING IAW B737-300 SRM 51-10-02 ITEM 8 AND B737-300 SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 63,662 hrs · 53,314 cycles

SUPPORT ANGLE CRACKED AT STA 27.00 INTERNAL STRUCTURE O/B SIDE FAIRING NR 3 LEFT WING. REPLACED ANGLE IAW SRM AND DWG.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 63,662 hrs · 53,314 cycles

CRACK ON RETAINER SEAL OF ACCESS PANEL 9207R RT HORIZONTAL STABILIZER TRAILING EDGE. REPLACED RETAINER SEAL OF ACCESS PANEL 9207R RT HORIZONTAL STABILIZER TRAILING EDGE IAW SRM B737-300 51-10-02 ITEM 8 AND DWG 65-53746.

Part: ACCESS PANEL — CRACKED (HORIZ STAB) · airframe 63,662 hrs · 53,314 cycles

CRACKS (4) AROUND FASTENER HOLE ACCESS PANEL 9207R HORIZONTAL STABILIZER RIGHT. REPAIRED FASTENER HOLE OF ACCESS PANEL 9207R IAW B737-300 SRM 51-70-17-0G-0.

Part: RIB — CRACKED (TE FLAP) · airframe 63,662 hrs · 53,314 cycles

RIGHT WING RIB CRACKED AT TRAILING EDGE EXHAUST GATE I/B END OF O/B FLAP WBL 184.40. REPLACED RIB IAW SRM AND DWG.

Part: WEB — CRACKED (NLG WW) · airframe 63,662 hrs · 53,314 cycles

CRACK ON WEB LOCATED AT BS 227.8 TO BS 231 BL 0 OF NOSE WHEEL WELL. REPLACED WEB LOCATED BETWEEN BS 227.8 TO BS 259.5 BL 0 OF NOSE WHEEL WELL AS PER SRM B737-300 51-10-02 ITEM 8 SRM B737-300 51-40-02. DWG 65-45819 AND ACO 7820-53.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

GALLEY DOOR AT UPPER CORNER CRACKED AT BS 328, STR 7R. REPAIRED SKIN EA AND SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED AT BS 727E AND S-20L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 727E AND STR 20L AFT CARGO COMPARTMENT IAW SRM B737-300 51-10-02 PART 8, 51-40-02 AND DRAWING 65C25228.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 63,662 hrs · 53,314 cycles

RIGHT WING SUPPORT ANGLE CRACKED AT WBL 71.24+10" TRAILING EDGE. REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE LOCATED AT BS 927 AND S-22L AFT CARGO COMPARTMENT. REMOVED AND REPLACED TIE CLIP AND FASTENER LOCATED AT BS 927 AND S-22L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-40-02, 51-10-02 ITEM 8 AND DRAWING 65-46559 SHEET 3.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCTAED AT BS 787 AND S-20R AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 787 AND STR 20R AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND INSTALLED FASTENERS IAW B737-300 SRM 51-40-02 AND DRAWING #65-46550.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON ANGLE LOCATED BETWEEN BS 927 AND BS 947.5 BL 0 AFT CARGO COMPARTMENT CEILING PANEL AREA. REPLACED ANGLE LOCATED BETWEEN BS 927 AND BS 947.5 BL 0 AFT CARGO COMP CEILING AREA IAW SRM 737-300 51-40-02 AND DRAWING 69-36656.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED AT BS 727E AND S-21L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 727E AND STR 21L AFT CARGO COMPARTMENT IAW SRM B737-300 51-10-02 PART 8, 51-40-02 AND DRAWING 65C25228.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED AT BS 787 AND S-21R AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 787 AND STR 21R AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND INSTALLED FASTENERS IAW B737-300 SRM 51-40-02 AND DRAWING # 65-4655

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED AT BS 1006 AT S-22R AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 1006 AT S-22R AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02 AND DRAWING 65-46567.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON UPPER AFT REVEAL LOCATED BS 328 AND BETWEEN STR 8R TO STR 7R FWD GALLEY DOOR CUTOUT. REPLACED UPPER AFT REVEAL LOC BS 328 AND BETWEEN STR 7R TO STR 8R FWD GALLEY DOOR CUTOUT IAW SRM B737-300 51-10-02 PART 8 AND 51-40-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED AT BS 787 AT LEVEL S-22R AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS787 AT LEVEL STR 22R AFT CARGO COMPARTMENT IAW SRM B737-300 51-10-02 PART 8, 51-40-02 AND DWG 65-46550.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

ANGLE CRACKED BETWEEN BS 312 TO 328, BETWEEN STR 26L TO 27L ELECTRONIC COMPARTMENT. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

TIE CLIP CRACKED AT BS 380, STR 22L OF THE E/E COMPARTMENT. REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

STRAP CRACKED AT BS 312, RBL 31 UNDER GALLEY AND LAVATORY E/E COMPARTMENT. REPLACED STRAP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

SUPPORT ANGLE CRACKED AT BS 380, STR 20L OF THE E/E COMPARTMENT. REPLACED ANGLE IAW SRM DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON STRAP LOCATED AT BS 312 AND AT LEVEL OF BL 0 UNDER FWD GALLEY AND LAVATORY E/E COMPARTMENT. REPLACED STRAP LOCATED AT BS 312 AND AT LEVEL OF BL 0 UNDER FWD GALLEY AND LAVATORY E/E COMPARTMENT IAW SRM B737-300 51-40-02 AND DWG 65-45834.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

BRACKET WEB CRACKED AT BS 294.5, STR 23L FUSELAGE LOWER LOBE. REPLACED SHEAR TIE IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

STRAP CRACKED AT BS 328, RBL 46 UNDER GALLEY AND LAVATORY E/E COMPARTMENT. REPLACED STRAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON EXTERNAL SKIN LOWER HINGE AT BS 947.5, BETWEEN STR 14L TO STR 15L. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 63,662 hrs · 53,314 cycles

CRACK ON VERTICAL ANGLE LOCATED AT WS 537.806 OF THE RIGHT WING FIXED TRAILING EDGE. REPLACED VERTICAL ANGLE LOC WS 537.806 OF THE RIGHT WING FIXED TRAILING EDGE IAW B737-300 SRM 51-10-02, 51-40-02 AND DWG N. 65-46460.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 63,662 hrs · 53,314 cycles

CRACKED LOWER STIFFENER AT STAB STA 120.30 INTERNAL STRUCTURE MAIN BOX LEFT HORIZ STAB. REMOVED AND REPLACED STIFFENER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 807 STR 25L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOC AT BS 807 STR 25L AFT CC IAW SRM B737-300 51-40-02, 51-10-02 ITEM 8 AND DWG 65-46551.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 1006 STR 26L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 1006 STR 26L AFT CARGO COMPARTMENT IAW SRM B737-300 51-10-02 PART 8,51-40-02 AND DRAWING 69-35364.

Part: BOLT — CORRODED (LT AILERON) · airframe 63,662 hrs · 53,314 cycles

RUST ON BOLTS LOCATED ON BALANCE PANEL AREA OF THE LT AILERON. REPLACED BOLTS LOCATED ON BALANCE PANEL AREA OF THE LT AILERON IAW CMM 57-50-21.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27L AND STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: TIE DOWN — CRACKED (CARGO BAY) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TRACK TIE DOWN LOCATED AT BSTA 747 AND RBL 13.80 AFT CARGO COMPARTMENT. REPAIRED TRACK TIEDOWN SECTION LOC BETWEEN BS 747+10 TO BS 767+10 AND RBL 13.8 AFT CC IAW B737-300 SRM 53-00-53 REPAIR 2 AND DWG 65-46592.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCTED AT BS 986.5 STR 20L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 986.5 STR 20L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND DRAWING 65-46564.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED AT BS 887 STR 20L AFT CARGO COMPARTMENT. REPLACED NEW TIE CLIP LOC AT BS 887 STR 20L AFT CARGO COMP IAW SRM B737-300 51-40-02 AND DWG 65-46557.

Part: VALVE — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON RETAINER VALVE LOCATED BS 380+3" AND BETWEEN STR 28R AND STR 28L IN FWD CARGO COMPARTMENT. REPLACED RETAINER VALVE LOC BS 380+3" AND BETWEEN S-28R AND S-28L IN FWD CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 787 STR 25L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BSTA 787 STR 25L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND INSTALLED FASTENERS IAW B737-300 SRM 51-40-02 AND DRAWING #65-4655.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 947.5 STR 27L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOC AT BS 947.5 S-27I AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 SRM 51-40-02 AND DRAWING 65-46560.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 63,662 hrs · 53,314 cycles

CRACK ON ALL FASTENER HOLE OF BALANCE PANEL 9538 OF VERTICAL STABILIZER. REPAIRED RUDDER BALANCE PANEL 9538 IAW B737-300 SRM 51-70-07-0G-0.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 947.5 STR 25R AFT CARGO COMPARTMENT. REPLACED STRINGER TIE CLIP LOC AT BSTA 947.5 STR 25R AFT CARGO COMPARTMENT IAW EA 1-353-2122/R0. AND EO AEM-HC5-547/12.R0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

FUSELAGE SKIN CRACKED AT BS 344+2, STR 2L. REPAIRED SKIN PER SRM.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 63,662 hrs · 53,314 cycles

CRACK ON VERTICAL ANGLE AT STRUT TORQUE BOX ACCESS PANEL 5858R ENGINE 2. REPLACED ANGLE IAW SRM AND DWG.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 63,662 hrs · 53,314 cycles

CRACK ON ALL FASTENER HOLE OF BALANCE PANEL 9537 OF VERTICAL STABILIZER. REPAIRED BALANCE PANEL 9537 IAW B737-300 SRM 51-70-07-0G-0.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 63,662 hrs · 53,314 cycles

CRACK ON ALL FASTENER HOLE OF BALANCE PANEL 9536 OF VERTICAL STABILIZER. REPAIRED RUDDER BALANCE PANEL 9536 IAW B737-300 SRM 51-70-07-0G-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

FUSELAGE SKIN CRACKED AT BS 328+10, STR 2L. REPAIRED SKIN PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED AT BS 967 STR 19L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 967 STR 19L AFTER CARGO COMPARTMENT IAW SRM B737-300 51-10-02 PAGE 8 ITEM 8 AND INSTALLED IAW SRM B737-300 51-40-02 AND DWG 65-46563.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK IN THE FUSELAGE SKIN ALONG THE CHEM-MILL STEP AT BS 967+3, STR 5R. REPAIRED SKIN IAW SRM.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 63,662 hrs · 53,314 cycles

CRACK ON ALL FASTENER HOLE OF BALANCE PANEL 9535 OF VERTICAL STABILIZER. REPAIRED RUDDER BALANCE PANEL 9535 IAW B737-300 SRM 51-70-07-0G-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK IN THE FUSELAGE SKIN ALONG THE CHEM-MILL STEP AT BS 947.5, STR 5R. REPAIRED SKIN IAW SRM.

Part: ACCESS PANEL — DELAMINATED (TAILCONE) · airframe 63,662 hrs · 53,314 cycles

DELAMINATION ON ACCESS PANEL 3802R TAIL CONE ACCESS. REPAIRED ACCESS PANEL 3802R, TAIL CONE ACCESS IAW B737-300 SRM 51-70-07-0G-0.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON SUPPORT ANGLE AT BS 540 LBL 1.5 AT MAIN DECK FLOOR STRUCTURE. REPLACED SUPPORT ANGLE IAW SRM.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CORROSION ON FASTENER LOCATED BETWEEN BS 492.4 AND 500 BETWEEN STR 18R AND 19R. REPLACED FASTENER IAW AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED ON BS 500A, STRINGER 18L, FWD CARGO COMP. REPLACED TIE CLIP LOCATED ON BS 500A STRINGER 18L FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02 51-40-02 AND DRAWING 65-46593.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON BRACKET LOCATED AT BSTA 727D BETWEEN STR 27L TO STR 27R AFT CARGO COMPARTMENT. REPLACED BRACKET (CLIP) LOCATED AT BS 727D BETWEEN STR 27L TO STR 27R AFT CC IAW SRM B737-300 51-10-02 ITEM 8 AND DWG 65-65710.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CORROSION ON FASTENER LOCATED ON WEB BETWEEN BS 420 AND BS 440 BETWEEN STR 18R AND STR 19R. REMOVED AND REPLACED FASTENERS IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED ON BS 500B, STRINGER 18L FWD CARGO COMP. REPLACED TIE CLIP LOCATED ON BS 500B STR 18L FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02 51-40-02 AND DRAWING 65C22908.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CORROSION ON FASTENER AT WEB BETWEEN BS 500 AND 500A AND BETWEEN STR 18R AND 19R. REMOVED AND REPLACED FASTENERS IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED ON BS 500, STRINGER 18L, FWD CARGO COMP. REPLACED TIE CLIP LOCATED ON BS 500 STRINGER 18L FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02 51-40-02 AND DRAWING 65-46533.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON CHANNEL LOCATED AT BSTA 727+4" STR 25R AFT CARGO COMPARTMENT. REPAIRED CHANNEL LOC AT BS 727+4 BETWEEN STR 25R TO STR 27R AFT CARGO COMPARTMENT IAW B737-300 SRM 51-70-11-0G-0 AND DWG 65-49614.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE LOCATED ON BS 500A, STRINGER 22L FWD CARGO COMP. REPLACED TIE CLIP LOCATED BS 500A STR 22L FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8 AND DWG#65-46593.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON SUPPORT ANGLE AT BS 540 RBL 1.5 AT MAIN DECK FLOOR STRUCTURE. REMOVED AND REPLACED ANGLE IAW SRM.

Part: VALVE — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON RETAINER VALVE LOCATED BS 420+14" BETWEEN STR 28R AND STR 28L FWD CARGO COMPARTMENT. REPLACED RETAINER VALVE LOC BS 420+17" BETWEEN STR 28R TO STR 28L FWD CC IAW B737-300 SRM 51-10-02 AND 51-40-02.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON HOLES (4EA) LOCATED ON UPPER AFT WING TO BODY FAIRING PANEL 3578L BETWEEN 57" FROM UPPER FWD EDGE. REPAIRED WING TO BODY FAIRING PANEL 3578L IAW B737-300 SRM 51-70-16-0G-0 REP 9.

Part: RUB STRIP — CRACKED (NR 2 NACELLE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON RUBSTRIP LOCATED STRUT ACCESS PANEL 58720R ENGINE 2. REPLACED RUBSTRIP LOCATED STRUT ACCESS PANEL 58720R ENGINE 2 IAW B737-300 SRM 51-10-02 ITEM 8 AND INSTALLED FASTENERS IAW B737-300 SRM 51-40-02 AND DWG 65C26720.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON HOLES 4(EA) LOCATED ON UPPER AFT WING TO BODY FAIRING PANEL 3678R (BETWEEN 57" FWD LOWER EDGE). REPAIRED 3678R IAW B737-300 SRM 51-70-16-0G-0 REP 9.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED ON BS 500C, STRINGER 18L FWD CARGO COMP. REPLACED TIE CLIP LOCATED ON BS 500C STRINGER 18L FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02 51-40-02 AND DRAWING 65C22909.

Part: RUB STRIP — CRACKED (NR 2 NACELLE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON RUBSTRIP LOCATED STRUT ACCESS PANEL 5847R ENGINE 2. REPLACED RUBSTRIP ON ACCESS PANEL 5847R ENGINE 2 IAW SRM B737-300 51-10-02 PART 8 AND DRAWING 311A1100.

Part: VALVE — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON RETAINER VALVE LOCATED BS 440+17" AND BETWEEN STR 28R AND STR 28R AND STR 28L IN FWD CARGO COMPARTMENT. REPLACED RETAINER VALVE LOC BS 440+17" AND BETWEEN STR 28R TO STR 28L FWD CC IAW B737-300 SRM 51-10-02 AND 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON ANGLE LOC BST 500D ON STR 26R FWD CARGO COMPARTMENT. REPLACED ANGLE LOC BST 500D ON STR 26R FWD CARGO COMP IAW SRM B737-300 51-10-02, 51-40-02 AND DRAWING 69-41757.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED ON BS 500 STRINGER 22L, FWD CARGO COMP. REPLACED TIE CLIP LOC ON BS 500 STR 22L FWD CC IAW SRM B737-300 51-10-02 ITEM 8, 51-40-02 AND DWG 65-46533.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CORROSION ON SHEAR TIE AT BS 500D AND BETWEEN STR 28L AND 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED ON BS 440 AND STR 24L IN FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED ON BS 440 AND STR 24L IN FWD CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND DWG #65-46529.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED ON BS 440 AND STR 18L IN FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOC ON BS 440 AND STR 18L IN FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02 51-40-02 AND DRAWING 65-46529.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED BS 480 AND STR 18L IN FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOC BS 480 AND STR 18L IN FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02, 51-40-02 AND DRAWING 65-46532.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED ON BS 420, STRINGER 25R AT FWD CARGO COMP. REPLACED TIE CLIP LOCATED ON B/S 420 STR 25R FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8 AND DWG 65-46527.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED ON BS 460 AND STR 19L IN FWD CARGO COMPARMRNT. REPLACED TIE CLIP LOCATED ON BS 460 AND STR 19L IN FWD CARGO COMPARTMENT IAW B737-300 SRM 51-40-02 AND DWG 65-46529, SRM B737-300 51-10-02 ITEM 8.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON TIE CLIP LOCATED ON BS 460 AND STR 18L IN FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED ON BS 460 S-18L FWD CARGO COMP IAW 51-40-02 AND DRAWING 65-46530.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON SUPPORT ANGLE LOCATED BETWEEN BS 294.5 TO BS 303.9 AND S-16L FWD ENTRY DOOR AREA. REPLACED REPAIR ANGLE LOC BETWEEN BS 294.5 TO BS 303.9 AND STR 16L FWD ENTRY DOOR IAW B737-300 SRM 51-10-02, 51-40-02 AND DWG 65-17684.

Part: STOP PIN — CRACKED (FUSELAGE) · airframe 63,662 hrs · 53,314 cycles

CRACK ON STOP PINS AT EMERGENCY EXIT CUTOUT IN RT SIDE 3 EA AND LT SIDE 2EA. REMOVED AND REPLACED STOP PINS AT EMERGENCY EXIT CUTOUT IN RT SIDE 3EA AND LT SIDE 2EA IAW SRM 51-10-02.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 63,662 hrs · 53,314 cycles

CRACK ON FLOOR PANEL 1537X LOCATED AFT CARGO COMPARTMENT. REPLACED FLOOR PANEL 1537X LOC AFT CARGO COMPARTMENT IAW SRM B737-300 51-10-02 PART 8 AND DRAWING 65-47951.

Part: SKIN — CRACKED (R1 DOOR) · airframe 63,127 hrs · 52,919 cycles

R1 DOOR EXTERIOR SKIN CRACKED AT LOWER HINGE CUTOUT UPPER AFT CORNER. REMOVED AND REPLACED R1 DOOR IAW M/M.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 62,758 hrs · 52,645 cycles

LEFT KEEL BEAM CORRODED BETWEEN BS 500D TO BS 500D +7. REPAIRED BEAM PER SRM.

Part: LATCH — LOOSE (EVAC SLIDE) · airframe 62,562 hrs · 52,500 cycles

L2 DOOR EMERGENCY EVAC SLIDE LATCH LOOSE. SECURED LATCH IAW MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,846 hrs · 51,948 cycles

R2 DOOR SLIDE GIRT NEEDS TO BE RE-INSTALLED, TOO LONG. RE-INSTALLED SLIDE PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,846 hrs · 51,948 cycles

FUSELAGE SKIN CRACK AT BS 420+3.0 BELOW ST 1R. REPAIRED SKIN PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,708 hrs · 51,838 cycles

AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK HOUSING PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 61,441 hrs · 51,627 cycles

LT CREASE BEAM CRACKED AT BS 639, LBL 60. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,441 hrs · 51,627 cycles

FRAME CRACKED AT 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME EA.

Part: FLAP — PUNCTURED (LT WING) · airframe 61,441 hrs · 51,627 cycles

LT WING O/B FORE FLAP PUNCTURED. REPAIRED FORE FLAP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,441 hrs · 51,627 cycles

STAB BEAM WEB CRACKED AT BS 63, LBL 51 NEAR VERTICAL ANGLE. REMOVED AND REPLACED WEB IAW SRM.

Part: SIGN — CRACKED (CABIN) · airframe 61,432 hrs · 51,620 cycles

OVERHEAD EMERGENCY EXIT SIGN CRACKED. REPAIRED SIGN PER MM.

Part: CONTROL VALVE — FAULTY (MLG WW) · airframe 60,915 hrs · 51,237 cycles

AIR TURNBACK/DECLARED EMERGENCY. AFTER FLAPS 1 TAKE OFF T/E FLAPS FAILED TO RETRACT WHEN FLAP HANDLE WAS MOVED TO "UP" NO OVERSPEED. REMOVED AND REPLACED T/E FLAP CONTROL VALVE ASSY IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 60,885 hrs · 51,216 cycles

L2 DOOR EMERGENCY EXIT SIGN LIGHT COVER LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: COVER — LOOSE (CABIN) · airframe 60,757 hrs · 51,124 cycles

RT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 60,683 hrs · 51,066 cycles

FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 60,598 hrs · 51,003 cycles

FWD O/B EMERGENCY FLASHLIGHT INDICATOR INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 60,286 hrs · 50,769 cycles

AFT INBOARD FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 60,047 hrs · 50,595 cycles

DURING SCHEDULED CV CHECK, FOUND RT EMERGENCY EXIT SIGN LOOSE AT ROW 10. SECURED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,047 hrs · 50,595 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 440+3, STR 1. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,047 hrs · 50,595 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 440+1, STR 2R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,047 hrs · 50,595 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 430+2, STR 1. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 59,072 hrs · 49,846 cycles

DURING SCHEDULED HC2 CHECK FOUND, LT WING I/B AFT FLAP DELAMINATED ON O/B EDGE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 59,072 hrs · 49,846 cycles

DURING SCHEDULED HC2 CHECK FOUND, LT WING NR 2 SLAT DELAMINATED AT I/B TRAILING EDGE WEDGE. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 58,223 hrs · 49,192 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING I/B AFT FLAP O/B T/E ENDCAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,223 hrs · 49,192 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER CORNER. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 58,223 hrs · 49,192 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,223 hrs · 49,192 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,223 hrs · 49,192 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN RBL 5 TO LBL 5. REPAIRED SHEAR TIE PER SRM AND SI.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 58,223 hrs · 49,192 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT OVERWING CREASE BEAM WEB CRACKED AT BS 637, STR 17L. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,825 hrs · 48,328 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 433, STR 1. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 56,457 hrs · 47,849 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER EA.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 56,203 hrs · 47,653 cycles

L2 DOOR EVAC SLIDE LOOSE. SECURED EVAC SLIDE PER MT.

Part: LENS — LOOSE (CABIN) · airframe 55,789 hrs · 7,344 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT PER EA AND BAC DWG.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 55,553 hrs · 47,172 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,553 hrs · 47,172 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,996 hrs · 46,028 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING O/B AFT FLAP SKIN DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LENS — MISSING (CABIN) · airframe 53,778 hrs · 45,861 cycles

RIGHT BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 16. INSTALLED LENS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 53,172 hrs · 45,401 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BS 292, WL 255. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REPAIRED SHEAR TIE PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 20L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 292, WL 230. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE BROKEN AT BS 520, BETWEEN STR 23R TO STR 24R. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 312, BL 0. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 5 TO RBL 18. REPAIRED BEAM PER ER.

Part: RIB — CRACKED (RT WING) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135, BETWEEN STR 3R TO STR 2R. REPAIRED CHORD PER ACO.

Part: FABRIC — WORN (EVAC SLIDE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT FABRIC WORN. REMOVED AND REPLACED SLIDE PER MT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 402 TO BS 408, STR 24R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 380, STR 21L. REPAIRED STRINGER PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 887 TO BS 907. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: COVER — DAMAGED (CABIN) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LIGHT COVER ON SIDEWALL DAMAGED. REMOVED AND REPLACED COVER PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 21L CRACKED AT BS 460 TO BS 500. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 19L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 19L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 23R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 16R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 22L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND LT I/B TRAILING EDGE FORE FLAP DELAMINATED AT O/B END. REPAIRED FLAP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24. REPAIRED BEAM PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 928, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 380 TO BS 400. REPAIRED BEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 847, STR 15R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND INTERNAL DOUBLER SKIN CORRODED AT BS 950, BETWEEN STR 23L TO STR 24L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: ATTACH BRACKET — CORRODED (GIRT BAR) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR ATTACH BRACKET CORRODED, BS 312. REMOVED AND REPLACED BRACKET PER SRM.

Part: FLAP — PUNCTURED (LT WING) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING I/B AFT FLAP PUNCTURED. REPAIRED AFT FLAP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOOR STUB BEAM CRACKED AT BS 639, LBL 45. REMOVED AND REPLACED BEAM PER DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 847, STR 14R. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 5R. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR. 6L. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. R&R CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME ANGLE CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT LOWER T/E SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,505 hrs · 44,924 cycles

DURING SCHEDULED SPV CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BETWEEN BS 380 TO BS 400. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,343 hrs · 44,802 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SRM.

Part: GARLOCK SEAL — LEAKING (NR 1 ENGINE) · airframe 52,203 hrs · 44,709 cycles

DIVERSION, NR 1 ENG OIL QUANTITY LOSS INDICATION. FOUND OIL LEAK AT NR 1 ENG FUEL PUMP. REMOVED AND REPLACED GARLOCK SEAL PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,926 hrs · 43,849 cycles

DURING SCHEDULED MV2 CHECK, FOUND BEADED PRESSURE DECK WEB CRACKED AT BS 540, LBL 25. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,926 hrs · 43,849 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729D, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,926 hrs · 43,849 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,926 hrs · 43,849 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,942 hrs · 43,149 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 973, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,295 hrs · 42,657 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,295 hrs · 42,657 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505D, STR 14R. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,294 hrs · 42,650 cycles

DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,294 hrs · 42,650 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, RBL 1.5. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,294 hrs · 42,650 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,294 hrs · 42,650 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,294 hrs · 42,650 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,294 hrs · 42,650 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 430) · airframe 49,294 hrs · 42,650 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, BL 0. REPAIRED SKIN PER ACO.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 48,862 hrs · 42,323 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LENS MISSING AT ROW 12 DEF. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 48,027 hrs · 41,655 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,027 hrs · 41,655 cycles

DURING SCHEDULED C2 CHECK, FOUND RT FWD CABIN EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — BROKEN (R1 DOOR) · airframe 48,027 hrs · 41,655 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE COVER BROKEN. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 47,832 hrs · 41,494 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 47,675 hrs · 41,381 cycles

DURING SCHEDULED SERVICE CHECK, L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 47,137 hrs · 46,972 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 46,430 hrs · 40,426 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: BULKHEAD — CRACKED (BS 178) · airframe 46,352 hrs · 40,365 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 1, WL 186. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: SKIN — CRACKED (BS 937 S24L) · airframe 46,166 hrs · 40,223 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 522 S28R) · airframe 46,166 hrs · 40,223 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 522, STR 28R, AIR CONDITIONING DOOR CUTOUT RIGHT FWD CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,448 hrs · 38,883 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 525, STR 10R. REPAIRED SKIN PER SWA EA.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 43,693 hrs · 38,324 cycles

DURING SCHEDULED A1 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: NUT — CORRODED (RT WING) · airframe 43,556 hrs · 38,219 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT MLG INBOARD TRUNNION NUT CORRODED. REMOVED AND REPLACED TRUNNION NUT PER MM & CCO.

Part: DOOR FRAME — CRACKED (AFT CARGO) · airframe 42,509 hrs · 37,408 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED CARGO DOOR PER MM.

Part: FRAME — CRACKED (BS 303.9) · airframe 41,757 hrs · 36,837 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER SWA EA & SRM.

Part: STRINGER CLIP — CRACKED (BS 767) · airframe 41,757 hrs · 36,837 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 27R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,757 hrs · 36,837 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, RBL 8. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,757 hrs · 36,837 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L & STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SPAR — CRACKED (RT WING) · airframe 41,757 hrs · 36,837 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING FWD SPAR PLATE CRACKED AT WBL 70.85. REPAIRED WING SPAR PER SWA EA & SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,757 hrs · 36,837 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,757 hrs · 36,837 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 468, BL 0, AT DME ANTENNA NR 1 CUTOUT. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,757 hrs · 36,837 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 378.5, LBL 2.8, AFT SIDE OF E & E COOLING EXHAUST PORT. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,757 hrs · 36,837 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 359, STR 14L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,543 hrs · 36,658 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SWA EA.

Part: HOOK — SHEARED (L1 DOOR) · airframe 40,509 hrs · 35,860 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK SHEARED OFF. RE-INSTALLED HOOK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 39,725 hrs · 35,257 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,595 hrs · 35,140 cycles

DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 8 DEF, LOOSE. SECURED LIGHT ASSEMBLY PER MM.

Part: FIRE DETECTOR — FAILED (NR 1 ENGINE) · airframe 38,523 hrs · 34,290 cycles

AIR TURN BACK, 1 TO 2 MINUTES AFTER DEPARTURE THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED, THEN NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED. ALL LIGHTS EXTINGUISHED WHEN THROTTLES RETARDED FOR DESCENT. REMOVED AND REPLACED NR 1 ENGINE CONTROL PANEL AND NR 1 FIRE DETECTOR UNIT PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 37,648 hrs · 33,577 cycles

AFT ENTRY DOOR EMERGENCY EXIT LENS LOOSE. REMOVED AND REPLACED AFT ENTRY DOOR EMERGENCY EXIT SIGN BASE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 37,631 hrs · 33,562 cycles

L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,451 hrs · 33,408 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 927 + 5, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,975 hrs · 32,980 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 20 ABC INOP. RELAMPED LIGHT PER MM.

Part: GASPER FAN — MALFUNCTIONED (E/E BAY) · airframe 35,611 hrs · 31,952 cycles

F/A'S REPORTED SMELL OF ELECTRICAL SMOKE IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 34,154 hrs · 30,797 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,743 hrs · 30,449 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) AT BS 360, BETWEEN STR 7R AND STR 8R AND AT BS 400, BETWEEN STR 8L AND STR 9L. REPAIRED FRAMES PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,743 hrs · 30,449 cycles

DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 862 AND BS 881. REPAIRED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED (2 EA) AT BS 616, WL 201 AT LBL 65 & RBL 65. REPAIRED FRAME PER SWA T1 & BFG ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,743 hrs · 30,449 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR 2R AND STR 3R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,743 hrs · 30,449 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: HINGE FITTING — CORRODED (LT & RT ELEVATOR) · airframe 33,743 hrs · 30,449 cycles

DURING SCHEDULED D-CHECK, FOUND BOTH LT/RT ELEVATOR NR 6 HINGE FITTINGS CORRODED. REMOVED AND REPLACED BOTH LT/RT NR 6 HINGE FITTINGS PER SRM AND SWA ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,743 hrs · 30,449 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 480, WL 148, RBL 4 TO LBL 4. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,743 hrs · 30,449 cycles

DURING SCHEDULED D CHECK, FOUND BOTH LH & RH FUSELAGE FRAMES CRACKED AT BS 188, WL 208. R&R LH & RH FRAMES PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 33,743 hrs · 30,449 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEBS CORRODED AT LH BS 825, RH BS'S 442, BS 500 + 8 & BS 880. REPAIRED CREASE BEAM WEBS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,743 hrs · 30,449 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,743 hrs · 30,449 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 328, WL 208 & LBL 28 AND BS 344, WL 208 & LBL 8. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,743 hrs · 30,449 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,743 hrs · 30,449 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) AT BS 663, STR'S 10R & 10L, BS 560, STR 7R & BS 706, STR 11R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: FASTENER — LOOSE (ENTRY DOOR) · airframe 33,137 hrs · 29,990 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED FASTENERS PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 31,231 hrs · 28,448 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 31,103 hrs · 28,337 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 29,300 hrs · 26,906 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 4 L/E SLAT TRAILING WEDGE DELAMINATED AT INBD END. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.

Part: FRAME — CRACKED (COCKPIT) · airframe 25,559 hrs · 23,760 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CRACK AT AT R-1 COCKPIT WINDOW FRAME, UPPER OUTBOARD CORNER. REPAIRED FRAME PER PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,559 hrs · 23,760 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 BS 178 BULKHEAD WEB CRACKS AT LBL 5, WL 198 - 210. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,559 hrs · 23,760 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 5, WL 198 AND 201. REPAIRED BULKHEAD PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 25,559 hrs · 23,760 cycles

DURING SCHEDULED 1/4 CHECK, FOUND AFT B/B FLOORBEAM CORROSION AT BS 770, RBL 3 - 7. REPAIRED FLOORBEAM PER RA 1-A53-2021.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,559 hrs · 23,760 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LT AND RT SIDE CHORDS CRACKED AT WL 207. REMOVED AND REPLACED SIDE CHORDS PER ACO 7338-53 AND 7342-53.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,559 hrs · 23,760 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 7, WL 213. REPAIRED BULKHEAD PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 25,559 hrs · 23,760 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 360 - 380. REPLACED WEB PER SRM.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 25,249 hrs · 23,489 cycles

AFTER GEAR RETRACTION, MOVED GEAR HANDLE TO OFF POSITION AND ALL GEAR WARNING RED LIGHTS ILLUMINATED. CYCLED GEAR HANDLE AND GREEN LIGHTS ILLUMINATED. C/W LANDING GEAR EXTENSION/RETRACTION TEST, NO DEFECTS NOTED PER MM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 25,046 hrs · 23,315 cycles

FWD OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BUSHING — WORN (WING TE FLAP) · airframe 24,629 hrs · 22,981 cycles

DIVERSION, ACFT VIBRATION FELT DURING CLIMB. C/W ACFT VIBRATION INSP, ADJUSTED ALL AFT T/E FLAP DEAD WEIGHT ROLLERS AND REMOVED AND REPLACED RIGHT I/B GROUND SPOILER FWD ATTACH FITTING BUSHINGS AND BOLT.

Part: SLIDE — DISCHARGED (PAX DOOR) · airframe 24,115 hrs · 22,537 cycles

FWD ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 23,898 hrs · 22,355 cycles

AFT SERVICE DOOR EVACUATION SLIDE PARTIALLY SEPARATED FROM CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 23,802 hrs · 22,270 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT FWD AND MID CABIN. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: WIRE — EXPOSED (CABIN)

EEPLS WIRES EXPOSED IN TRACK BY OVERWING EXIT. REINSTALLED WIRING AND TRACKS PER MM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FWD LOWER CORNER OF DOOR FRAME. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED SCREW HOLE ON FLOORBEAM AT BS 986 JUST INSIDE DOOR. REPAIRED PER BOEING TI-A53-014.

Part: ANGLE — CORRODED (BS 947-1006)

DURING SCHEDULED 1/2D CHECK, FOUND LT Z ANGLE CORRODED IN SEVERAL PLACES FROM BS 947 TO 1006. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 947-1006)

DURING SCHEDULED 1/2D CHECK, FOUND RT Z ANGLE CORRODED IN SEVERAL SPOTS FROM BS 947 TO 1006. REPAIRED PER BOEING SRM.

Part: GUSSET — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FWD SERVICE DOOR AT GUSSET IN LWR AFT CORNER. REMOVED AND REPLACED PER BOEING SRM.

Part: COVER — GOUGED (LT EMER EXIT)

DURING SCHEDULED 1/2 D CHECK, FOUND EMERGENCY EXIT COVER GOUGED AROUND THE EDGES. REPAIRED PER BOEING SRM.

Part: SEAL — CRACKED (NR 1 LE FLAP)

DURING SCHEDULED 1/2 D-CHECK, FOUND NR 1 KRUGER FLAP SEAL CRACKED OUT/BD TOP. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (RT WING)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED SUPPORT ANGLE JUST OUT/BD OF PYLON AND IN/BD OF PANEL 8715R. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD ANGLE — CRACKED (BS 727)

DURING SCHEDULED 1/2 D CHECK, FOUND CRACKED SUPPORT ANGLE FOR FWD BULKHEAD PANEL AT 727 + 2, RBL 4. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — DAMAGED (CARGO DOORWAY)

DURING SCHEDULED 1/2 D CHECK, FOUND DAMAGED WEB AT FWD SIDE OF AFT CARGO DOOR CUT OUT. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 492-500)

DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED TRANSITION ANGLE AT BS 492-500A, RBL 24. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 793-847)

DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED THRESHOLD WEB AT BS 793 - 847, RBL 25. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 500)

DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED FLOOR ANGLE AT BS 500 D, RBL 24, LBL 24. REMOVED AND REPLACED PER BOEING SRM.

Part: FLAP — DENTED (LT WING)

DURING SCHEDULED 1/2 D CHECK, FOUND OUTBD T/E FLAP DENTED 1.5 BY 1 WIDE WITH UPPER SURFACE BULGED; INBD OF NR 1 CANOE. REPAIRED PER BOEING SRM.

Part: WEB — DAMAGED (CARGO BIN)

DURING SCHEDULED 1/2 D CHECK, FOUND DAMAGED WEB AT AFT SIDE OF AFT CARGO DOOR CUTOUT. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 767-787)

DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED TRANSITION ANGLE AT BS 767 - 787, RBL 20. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 787)

DURING SCHEDULED 1/2 D CHECK, FOUND CRACKED FLOORBEAM BELOW TIE DOWN FITTING AT BS 787, RBL 14. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 727-787)

DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED LT TRANSITION ANGLE FROM BS 727 TO 787, LBL 20. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2 D CHECK, FOUND SCREW HOLE ON FLOORBEAM AT BS 986 CORRODED. REPAIRED PER SWA T1-A53-014.

Part: ANGLE — CORRODED (BS 277-360)

DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED Z ANGLE AT BS 277 TO 360. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 500)

DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED TRANSITION ANGLE AT BS 500A-500D, RBL 24. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 380-520)

DURING SCHEDULED 1/2 D CHECK, FOUND CRACKED INTERCOSTAL AT NUT PLATE HOLE BS 380-400; AND BS 500-520. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (PAX DOORWAY)

DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED L ANGLE SUPPORT THAT ATTACHES TO Z ANGLE FOR THRESHOLD. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND, FOUND AFT UPPER CABIN FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER BOEING M/M.