N345SA

Part: WEB — CRACKED (NLG WW) · airframe 92,298 hrs · 56,334 cycles

NOSE WW WEB CEILING CRACKED AT BS 277, RBL 10.16 AFT INBD CORNER OF NLG EMER EXTENSION SPRING BRACKET. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 92,298 hrs · 56,334 cycles

R2 DOOR CUT OUT CRACKED ON FWD LOWER CORNER. REPAIRED CUT OUT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 92,298 hrs · 56,334 cycles

LEFT WING, NR 3 SLAT LOWER SKIN OTBD OF DRIVE ACTUATOR CRACKED. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 91,604 hrs · 55,825 cycles

R1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW SIP.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 91,449 hrs · 55,712 cycles

L1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,449 hrs · 55,712 cycles

R2 DOOR LOWER HINGE ARM CUT OUT, FWD RADIUS CORNER OF FUSELAGE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 90,148 hrs · 54,762 cycles

AFT ENTRY EMER EXIT LIGHT LOOSE. R & R LIGHT ASSEMBLY IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 89,803 hrs · 54,502 cycles

RIGHT EMER EXIT LENS COVER BROKEN AT ROW 4. REPAIRED COVER IAW MM.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 89,410 hrs · 54,236 cycles

LOWER RT OVERWING EXIT SIGN LIGHT LOOSE. SECURED LIGHT IAW MM.

Part: WIRE — BROKEN (CABIN) · airframe 89,319 hrs · 54,175 cycles

EMERGENCY LIGHT WIRE BROKEN AT BS 727D, STRINGER 23R. REPAIRED WIRE IAW WDM & AMM.

Part: WEB — CORRODED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

FLOOR WEB CORRODED AT BS 1016, BETWEEN STRINGER 26L TO 27L. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

FUSELAGE BELLY SKIN CRACKED AT STATION 360 TO 380, BL 0. REPAIRED SKIN IAW SRM.

Part: SUPPORT ANGLE — DAMAGED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

E & E COMPARTMENT SUPPORT ANGLE DAMAGED AT BS 325 STRINGER 26L. REPAIRED ANGLE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

FRAME SHEAR TIE CORRODED AT BS 360, BETWEEN STRINGER 28L TO 28R. R & R SHEAR TIE IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 4R. R & R SPLICE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

FRAME CRACKED AT BS 348 STRINGER 16L. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

AFT CABIN FLOORBEAM T CHORD CORRODED AT BS 987 BETWEEN LBL 15 TO RBL 7. R & R T CHORD IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

INTERCOSTAL CRACKED AT BS 277R STRINGER 10R. R & R INTERCOSTAL IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

R2 DOOR SURROUND STRUCTURE CREASE BEAM CORRODED BETWEEN BS 947 TO 995. R & R CREASE BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

L2 DOOR CREASE BEAM CORRODED AT BS 977. R & R CREASE BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

R2 DOOR SURROUND STRUCTURE CREASE BEAM WEB CORRODED AT BS 991. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

RIGHT CREASE BEAM INNER CHORD DAMAGED AT BS 344. R & R CHORD IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO 328 RBL 11. R & R INTERCOSTAL IAW DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

INTERCOSTAL UPPER T CAP CORRODED BETWEEN BS 294.5 TO 312, RBL 11. REPAIRED T CAP IAW DWG & SRM.

Part: ANGLE — CRACKED (R1 DOOR) · airframe 89,319 hrs · 54,175 cycles

R1 DOOR LOWER EDGE INTERCOSTAL ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: PANEL — CRACKED (LT WING) · airframe 89,319 hrs · 54,175 cycles

LEFT WING NR 2 SLAT ACTUATOR LOWER PANEL CRACKED. R & R PANEL IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

AFT CARGO DOOR CUT OUT LOWER SILL WEB UPPER SURFACE CORRODED AROUND NUTPLATE HOLES. REPAIRED WEB IAW DWG & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

FLOORBEAM UPPER T CAP UPPER CORRODED AT BS 312 LBL 8 TO RBL 12L. R & R T CAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

FUSELAGE FRAME CRACKED AT STATION 727 STRINGER 18A RT SIDE. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,319 hrs · 54,175 cycles

LEFT FRAME OTBD CHORD FWD FLANGE AT CRACKED AT BS 727, STRINGER 18A FWD LOWER HOLE. REPAIRED CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 89,087 hrs · 54,012 cycles

LEFT MAIN WW PRESS DECK CRACKED AT BS 666 LBL 40. REPAIRED DECK IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,087 hrs · 54,012 cycles

FUSELAGE SKIN CRACKED AT BETWEEN BS 307 TO 309 BELOW STRINGER 18R. REPAIRED SKIN IAW EA.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 88,492 hrs · 53,582 cycles

L1 DOOR SLIDE GIRT BAR CAME OUT OF CLIPS DURING OPENING. REINSTALLED GIRT BAR IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,768 hrs · 52,363 cycles

AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R LAMPS IAW AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 86,586 hrs · 52,226 cycles

CLIP CRACKED AT BS 807, BETWEEN STRINGER 25L & 26L. R & R CLIP IAW SRM & DRAWING.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 86,586 hrs · 52,226 cycles

INTERCOSTAL WEB ATTACH CLIP CRACKED AT BS 827, STRINGER 27R. R & R CLIP IAW SRM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 86,586 hrs · 52,226 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. R & R SLIDE IAW MT.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 86,586 hrs · 52,226 cycles

CHANNEL CRACKED AT BS 727, STRINGER 23R. R & R CHANNEL IAW DRAWING & SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 86,586 hrs · 52,226 cycles

STRAP CRACKED AT BS 727, RBL 12. R & R STRAP IAW SRM & DRAWING.

Part: STRUT — CORRODED (FUSELAGE) · airframe 86,586 hrs · 52,226 cycles

LT KEEL BEAM STRUT ASSEMBLY CORRODED ON LOWER SURFACE AT BS 645, LBL 6.5. REPAIRED STRUT ASSEMBLY IAW EA & ER.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 86,586 hrs · 52,226 cycles

FRAME WEB ATTACH ANGLE AT BS 807, STRINGER 27R CRACKED AT A FASTENER HOLE. R & R ANGLE IAW DRAWING & SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 86,586 hrs · 52,226 cycles

AFT LAVATORY PAN BEAR STRAP LOWER SURFACE COMMON TO LOWER SKIN CORRODED. R & R BEAR STRAP IAW SRM & DRAWING.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 86,586 hrs · 52,226 cycles

BEAR STRAP CORRODED ON POTABLE WATER BEAR STRAP INNER SURFACE OTBD OF STRINGER 25L. R & R BEAR STRAP IAW SRM & DRAWING.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 86,586 hrs · 52,226 cycles

STRINGER CORRODED AT ABS 967, STRINGER 25L. R & R STRINGER IAW DRAWING & SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 86,586 hrs · 52,226 cycles

LT KEEL BEAM CORRODED ON OTBD VERTICAL FLANGE AT BS 727+10. R & R BEAM IAW SRM & DRAWING. .

Part: LENS — BROKEN (CABIN) · airframe 86,471 hrs · 52,140 cycles

FWD ENTRY "EXIT" LIGHT LENS COVER BROKEN. R&R LIGHT ASSEMBLY MM.

Part: ACM — FAULTY (AC BAY) · airframe 85,785 hrs · 51,610 cycles

IN CRUISE, HAD ELECTRICAL SMOKE ODOR COMING FROM ROWS 14-15. ON FINAL: HAD VISIBLE SMOKE FROM AN AREA AROUND THE F/O'S RT KNEE. R & R LEFT ACM IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 85,625 hrs · 51,501 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: SEAL — CRACKED (KRUEGER FLAP) · airframe 85,362 hrs · 51,311 cycles

RIGHT WING I/B KRUEGER FLAP ICE SEALS CRACKED. REMOVED AND REPLACED SEALS PER AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 84,788 hrs · 50,898 cycles

EXIT ROW SIGNAL LIGHT IS LOOSE AT EXIT ROW ON F/O SIDE ROW 11. RE-SECURED PER M/M, OPS CHECK GOOD PER M/M.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 84,626 hrs · 50,787 cycles

AFT SERVICE DOOR SLIDE GAUGE NOT VISABLE IN WINDOW. REPOSITIONED AFT SERVICE DOOR SLIDE IAW MT 325-61-06. AFT SERVICE DOOR SLIDE GAUGE IS NOW VISIBLE IN WINDOW. 55973U, 11JAN13

Part: SKIN PANEL — CRACKED (NR 1 PYLON) · airframe 84,626 hrs · 50,787 cycles

NR 1 ENGNIE PYLON I/B PANEL 5753L HAS CRACKED AND DELAMINATED SKIN AT UPPER FASTENER ROW. REPAIRED CRACKED AND DELAMINATED SKIN AT UPPER FASTENER ROW OF NR 1 ENGINE PYLON I/B IAW SRM 54-50-70-01-1, SRM 54-50-70-1A-1 AND SRM 51-70-10-2R-0.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,626 hrs · 50,787 cycles

RIGHT OVERHEAD BIN EMERGENCY LIGHT BETWEEN SEAT ROWS 4 AND 5 DOES NOT ILLUMINATE. RELAMPED EMERGENCY EXIT AISLE LIGHT BETWEEN ROW 4/5 RIGHT PER MM 33-51-21-962-001 STEP 2.

Part: LUG — BROKEN (LT SPOILER) · airframe 84,536 hrs · 50,721 cycles

LEFT I/B GND SPOILER HAS BROKEN MOUNT LUG. REMOVED AND REPLACED LEFT I/B GND SPOILER ASSY PER M/M.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CORROSION FOUND ON STRINGER SPLICE AT BS 540-1" STR 26RH. REPLACED STRINGER SPLICE LOC AT BS 540-1" STR 26RT FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8, 51-40-02 AND DWG 65-45768.

Part: PLATE — CRACKED (CABIN) · airframe 84,217 hrs · 50,489 cycles

CRACK ON STOP PLATE (2EA) OF EMERGENCY EXIT LIGHT. REPLACED STOP PLATE (2EA) OF EMERGENCY EXIT LIGHT IAW SRM 51-10-02.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CRACK ON FWD CORNER REVEAL LOC AT BS 303 AND LEVEL STR 18L E/E COMPARTMENT. REPLACED FWD CORNER REVEAL (DEPRESSOR SEAL CORNER) LOCATED AT BS 303 AND LEVEL STR 18L E/E COMPARTMENT IAW SRM B737-300 51-10-02 PAGE 8 ITEM 8 AND DWG # 65-45800.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CRACK INDICATION FOUND AROUND THE SLOT-SHAPED CUTOUT IN THE BS 303.9 FRAME WEB AT THE DOOR STOP FITTING STR 16L. REPAIRED WEB HOLE PER ACO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

ANGLE CRACKED AT BS 344, BETWEEN STR 20L TO STR 23L. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CORROSION ON FRAME LOCATED AT BS 312 S-28L E/E COMPARTMENT. REPAIRED FRAME LOCATED AT BS 312 S-28L E/E COMPARTMENT IAW B737-300 SRM 53-00-07-2R-5 AND SRM 51-40-02. FOR INSPECTION REQUIREMENT SEE TLD #T030369.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

SHEAR TIE CORRODED AT BS 312, BETWEEN STR 28L TO STR 28R. REPLACED EXISTING REPAIR LOCATED ON SHEAR TIE FRAME BS 312 BETWEEN STR 28L TO STR 28R ELECTRONIC COMPARTMENT IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

TIE CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CORROSION ON SUPPORT ANGLE LOCATED ON BS 328 STRINGER 27R, E/E COMPARTMENT. REPLACED SUPPORT ANGLE LOCATED ON BS 328 STRINGER 27R E/E COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 SRM 51-40-02 AND DRAWING #65-45829.

Part: FRAME — CORRODED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CORROSION ON FRAME LOCATED AT BS 330.62 BETWEEN STR 27L TO STR 28L E/E COMPARTMENT. PERFORMED REPAIR ON FRAME LOCATED ON BS 330.62 BETWEEN STR 27L TO STR 28L E/E COMP AS PER SRM B737- 300 53-00-07-2R-5 FOR INSPECTION REQUIREMENT SEE TLD S/N T0303.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

TIE CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CORROSION ON SHEAR TIE LOCATED ON FRAME AT BS 312 BETWEEN STR 27L TO STR 28L E/E COMPARTMENT. REPLACED SHEAR TIE LOCATED ON FRAME AT BS 312 BETWEEN STR 27L TO STR 28L E/E COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8 AND DWG 65-45810.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CORROSION SHEAR TIE AT BS 330.62, BETWEEN STR 27L TO STR 28L E/E COMPARTMENT. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

TIE CLIP CRACKED AT BS 380, STR 20L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

STRINGER SPLICE CORRODED BETWEEN BS 351.2 TO BS 360+7, STR 28R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

FRAME CORRODED AT BS 328, STR 27R. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CRACKED STUD FRAME AT UPPER FWD CORNER BS 300 BETWEEN STR 7R TO STR 10R FWD GALLEY DOOR. REPLACED FRAME IAW SRM DRAWING SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CORRODED STRINGER 28L AT BS 294.5 TO BS 323.7 E/E COMPARTMENT. REPAIRED STRINGER 28L IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

STRINGER CORRODED BETWEEN BS 294.5 TO BS 323.7, STR 28R. REMOVED AND REPLACED STRINGER SECTION PER SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

SUPPORT ANGLE CORRODED AT BS 344, STR 27R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CRACK ON TIE CLIP LOCATED ON BS 291 STR 6R FWD PAX CABIN AROUND INTERNAL STRUCTURE OF FWD GALLEY DOOR. REPLACED TIE CLIP LOCATED ON BS 291 STR 6R FWD PAX CABIN AROUND INTERNAL STRUCTURE OF FWD GALLEY DOOR IAW B737-300 SRM 51-10-02 AND DWG 65-458.

Part: FITTING — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 84,217 hrs · 50,489 cycles

LEFT WING INBOARD FORE FLAP UPPER SKIN DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 84,217 hrs · 50,489 cycles

RIGHT WING INBOARD AFT FLAP UPPER SKIN DELAMINATED. REMOVED AND REPLACED AFT FLAP IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CRACK ON FRAME OF BS 344 AND AT LEVEL STR 22L IN E/E COMPARTMENT. REPLACED FRAME OF BS 344 AND AT LEVEL STR 22L IN E/E COMPARTMENT IAW B737-300 SRM 51-10-02 AND DRAWING #65-45815, SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

FRAME CRACKED AT BS 520, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 84,217 hrs · 50,489 cycles

CRACK ON ANGLE LOCATED INTERNAL AREA OF FLAP TRACK FAIRING AT WBL 185.00 AND FAIRING STA 27.00 LEFT WING FIXED TRAILING EDGE. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

INTERCOSTAL WEB CRACKED BETWEEN BS 294.5 TO BS 303.9, STR 15L. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 84,217 hrs · 50,489 cycles

CRACK ON SUPPORT ANGLE LOCATED TRAILING EDGE AT WBL 85 LEFT WING. REPLACED SUPPORT ANGLE LOCATED TRAILING EDGE AT WBL 85 LEFT WING IAW SRM B737-300 51-10-02 PART 8 AND DRAWING 65-68270.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 84,217 hrs · 50,489 cycles

CRACK ON SUPPORT ANGLE LOCATED WBL 185 AND FAIRING STA 27.00 INTERNAL AREA OF FLAP TRACK FAIRING 6 RIGHT. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: WEB — CRACKED (NLG WW) · airframe 84,217 hrs · 50,489 cycles

LEFT NLG WHEEL WELL WEB CRACKED AT BS 251.62, WL 162.1. REPAIRED WEB PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CRACK ON STRAP LOCATED BETWEEN BS 312 TO BS 328 AND RBL 33 UNDER FLOOR STRUCTURE IN E/E COMPARTMENT. REPLACED STRAP LOCATED BETWEEN BS 312 TO BS 328 AND RBL 33 UNDER FLOOR STRUCTURE IN E/E COMPARTMENT IAW B737-300 SRM 51-10-02 PART 8 AND DRAWING N. 65-4583.

Part: WEB — CRACKED (NLG WW) · airframe 84,217 hrs · 50,489 cycles

RIGHT NLG WHEEL WELL WEB CRACKED AT BS 251.62, WL 163.1. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CRACK AROUND FASTENER HOLE AND FWD GALLEY DOOR FWD DOOR CUTOUT. REPAIRED FWD GALLEY DOOR UPPER FWD DOOR CUTOUT IAW B737-300 EO AEM-HC53-510/12 R0 AND EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 84,217 hrs · 50,489 cycles

CRACK ON ANGLE LOCATED FWD FACE FLAP TRACK FAIRING ACCESS #3601 R RIGHT WING. REPLACED ANGLE SUPPORT LOC FWD FACE FLAP TRACK FAIRING ACCESS 3601 R RIGHT WING IAW B737-300 SRM 51-10-02 ITEM 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CRACK (2EA) LOCATED AROUND OF GROUND SERVICE CUT OUT LOCATED BETWEEN BS 526 AND BS 530 AT LEVEL OF STR 28L LOWER LOBE FUSELAGE. REPAIRED SKIN CUT OUT IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CRACK ON BULKHEAD NR 1545 OF AFT CARGO COMPARTMENT. REPAIRED ON AFT BULKHEAD NR 1545 OF AFT CC IAW AMM 25-01-12-308-009.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 84,217 hrs · 50,489 cycles

LEFT OVERWING EMERGENCY DOOR FRAME CRACKED ON UPPER SURFACE. REMOVED AND REPLACED DOOR IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

TIE CLIP CRACKED AT BS 947.5, STR 27R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

CRACK ON AFT BULKHEAD NR 1547 OF AFT CARGO COMPARTMENT. REPAIRED ON AFT BULKHEAD NR 1547 OF AFT CC IAW AMM 25-01-12-308-009.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 84,217 hrs · 50,489 cycles

WEB PUNCTURED BETWEEN BS 927 TO BS 947.5, LBL 25. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (L1 DOOR) · airframe 84,217 hrs · 50,489 cycles

CRACK ON SUPPORT ANGLE LOC ON FWD ENTRY DOOR LOWER AREA FWD CORNER. SUPPORT ANGLE LOC ON FWD ENTRY DOOR LOWER AREA FWD CORNER REPLACED IAW SRM 737-300 51-10-02 AND DRAWING N. 65-49649 AND 51-40-02.

Part: LENS — BROKEN (CABIN) · airframe 83,902 hrs · 50,254 cycles

LEFT WING EMERGENCY EXIT LOWER EXIT LIGHT LENS BROKEN. REPAIRED LENS PER EA.

Part: LIGHT — LOOSE (CABIN) · airframe 83,771 hrs · 50,149 cycles

EEPLS LOOSE AT ROW 8. SECURED EEPLS PER AMM.

Part: ATTACH FITTING — BROKEN (NR 5 SPOILER) · airframe 82,910 hrs · 49,495 cycles

RIGHT WING INBOARD NR 5 GROUND SPOILER ATTACH LUG BROKEN. REMOVED AND REPLACED SPOILER ASSY PER M/M.

Part: LIGHT — MISSING (CABIN) · airframe 82,139 hrs · 48,914 cycles

RT EMERGENCY EXIT LIGHT MISSING AT SIDEWALL LOWER AFT CORNER. REPLACED LIGHT PER AMM.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 82,139 hrs · 48,914 cycles

FRAME DAMAGED AT BS 787, STR 27R. REPAIRED FRAME IAW ER AND EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 82,139 hrs · 48,914 cycles

AFT CARGO BAY FRAME DAMAGED AT BS 794, RBL 27 UPPER AFT EDGE. REPAIRED FRAME PER SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 82,139 hrs · 48,914 cycles

STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 82,139 hrs · 48,914 cycles

STRINGER CLIP CORRODED AT BS 794, STR 26R. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,139 hrs · 48,914 cycles

STRINGER CORRODED AT BS 807, STR 26R. REPAIRED STRINGER IAW ER AND EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,139 hrs · 48,914 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,139 hrs · 48,914 cycles

L1 DOOR EMERGENCY EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,139 hrs · 48,914 cycles

ROW 19 EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT AND PER MM.

Part: FLAP — CHAFED (RT WING) · airframe 82,101 hrs · 48,883 cycles

RT WING O/B FORE FLAP I/B END CHAFED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: STRUCTURE — CRACKED (R1 DOOR) · airframe 82,101 hrs · 48,883 cycles

R1 DOOR CRACKED AT LOWER AFT CORNER OF DOOR AT FRAME. REPLACED DOOR PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 82,101 hrs · 48,883 cycles

LT WING NR 2 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED NR 2 SLAT PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,990 hrs · 48,798 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LENS — CRACKED (CABIN) · airframe 81,589 hrs · 48,522 cycles

L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 81,221 hrs · 48,238 cycles

AIR TURNBACK - FWD LAVATORY SMOKE DETECTOR SOUNDED. REMOVED AND REPLACED SMOKE DETECTOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,720 hrs · 47,855 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,720 hrs · 47,855 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EEPLS LIGHT INOP. RELAMPED PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,963 hrs · 46,511 cycles

L1 DOOR LOWER EEPLS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 336, STR 17L. REPAIRED SKIN PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED AT BS 264.6, RBL 23. REPAIRED WEB PER ACO.

Part: SKIN — CRACKED (LE SLAT) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 1 SLAT LOWER SKIN CRACKED AT I/B END. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER EA.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B AFT FLAP T/E WEDGE DELAMINATED. REPAIRED WEDGE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 806, BETWEEN RBL 6 TO LBL 6. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 9L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: BRACKET — LOOSE (L1 DOOR) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR STOW BRACKET LOOSE. REMOVED AND REPLACED BRACKET PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 1R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 14L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: BRACKET — LOOSE (L1 DOOR) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR STOW BRACKET LOOSE. REMOVED AND REPLACED BRACKET PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM SUPPORT U-CHANNEL ANGLE CRACKED AT BS 693, LBL 1. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 78,417 hrs · 46,092 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO BAY RT KEEL BEAM FRAME CORRODED AT BS 767, RBL 9. REPAIRED BEAM PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 78,183 hrs · 45,918 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING AFT FLAP T/E DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SEAL — TORN (CARGO DOOR) · airframe 78,182 hrs · 45,918 cycles

EMERGENCY DESCENT AT 27000FT ON DESCENT, CABIN ALTITUDE HORN SOUNDED. MASKS DROPPED. FOUND AFT CARGO DOOR SEAL TORN. REMOVED AND REPLACED SEAL PER MM AND MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,780 hrs · 45,616 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,780 hrs · 45,616 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: HINGE FITTING — BROKEN (SPOILER) · airframe 77,748 hrs · 45,575 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B GROUND SPOILER O/B HINGE FITTING BROKEN. REMOVED AND REPLACED GROUND SPOILER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,748 hrs · 45,575 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 77,111 hrs · 45,068 cycles

LT WING NR 3 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: MOTOR — FAULTY (TE FLAP) · airframe 76,393 hrs · 44,522 cycles

ON APPROACH TRAILING EDGE FLAPS FAILED TO EXTEND. L/E EXTENDED USING ALT FLAPS SWITCH. ALT FLAP DRIVE TRAILING EDGE AC/C CB TRIPPED LANDED WITH L/E FLAPS ONLY. REMOVED AND REPLACED FLAP HYDRAULIC MOTOR PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 76,175 hrs · 44,369 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 76,161 hrs · 44,357 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 76,161 hrs · 44,357 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING BULLNOSE EMERGENCY EXIT LIGHT INOP BETWEEN ROW 15 TO ROW 16. CHARGED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 76,161 hrs · 44,357 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOP. CHARGED BATTERY PER MM.

Part: SENSOR — BROKEN (STALL WARNING) · airframe 75,977 hrs · 44,207 cycles

AIR TURNBACK - AT APPROXIMATELY 85 KTS DURING TAKEOFF ROLL THE LEADING EDGE FLAP TRANSIT ILLUMINATED, TAKEOFF CONTINUED. STICK SHAKER CAME ON AT LIFT OFF AND REMAINDER ON FOR DURATION OF FLIGHT. ALL OTHER PARAMETERS OK. FOUND RT AOA BROKEN. REMOVED AND REPLACED NR 2 AOA VANE SENSOR AND NR 2 STALL WARNING COMPUTER PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 75,454 hrs · 43,821 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 75,454 hrs · 43,821 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED NEAR OUTBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 75,454 hrs · 43,821 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR LOWER HINGE CUTOUT SKIN CRACKED. REMOVED AND REPLACED DOOR ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,350 hrs · 43,741 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,896 hrs · 51,479 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 986.5, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 73,942 hrs · 42,686 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 73,942 hrs · 42,686 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 73,866 hrs · 42,627 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR CLIP OUT OF ADJUST. ADJUSTED CLIP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND WEB CORRODED AT BS 227, RBL 8. REPAIRED WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 787 TO BS 807, STR 21L. REPAIRED STRINGER PER ER.

Part: FLAP — DELAMINATED (RT WING) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: WIRE — DAMAGED (CABIN) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD DOOR EMERGENCY EXIT SIGNS INOP. REPAIRED WIRE PER WDM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 291, WL 138. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND INTERIOR FRAME WEB CRACKED AT BS 291, STR 16R. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304, WL 257. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 304, BETWEEN BS WL 208 TO WL 234. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,786 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 27 TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 3L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 665, LBL 25, WL 208. REPAIRED BEAM PER SRM.

Part: LIGHT — BROKEN (EXTERIOR) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT AFT EXTERNAL EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED AT BS 944, STR 26L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND NR 8 SPOILER DELAMINATED ON UPPER SURFACE. REPAIRED SPOILER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 631, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 987, BETWEEN STR 25R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED AT BS 944, STR 26L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 291, STR 16R. REPAIRED WEB PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, BETWEEN STR 27R TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 917, STR 26L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,787 hrs · 42,561 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,760 hrs · 42,536 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER EA.

Part: FITTING — LOOSE (FUSELAGE) · airframe 72,240 hrs · 41,421 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 72,240 hrs · 41,421 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (NR 3 SLAT) · airframe 72,240 hrs · 41,421 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 3 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,801 hrs · 41,113 cycles

DURING SCHEDULED SPV CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK AND BATTERY CHARGER PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 71,801 hrs · 41,113 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,800 hrs · 41,112 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,800 hrs · 41,112 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: STRINGER CLIP — CRACKED (BS 340 S10R) · airframe 71,800 hrs · 41,112 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 340, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 274 S10R) · airframe 71,800 hrs · 41,112 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 274, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 340 S10R) · airframe 71,800 hrs · 41,112 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 340, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 291 S10L) · airframe 71,800 hrs · 41,112 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 291, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 274 S10R) · airframe 71,800 hrs · 41,112 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 274, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 71,089 hrs · 40,579 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 70,645 hrs · 40,258 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,645 hrs · 40,258 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,645 hrs · 40,258 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,310 hrs · 39,981 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 8 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — MISSING (CABIN) · airframe 70,197 hrs · 39,907 cycles

LEFT OVERWING EMERGENCY EXIT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,001 hrs · 39,777 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 24R. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 69,452 hrs · 39,379 cycles

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

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 68,822 hrs · 38,871 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD CORRODED AT BS 1016, LBL 1. REPAIRED BULKHEAD PER SRM.

Part: TAB — FAILED (RT ELEVATOR) · airframe 68,822 hrs · 38,871 cycles

DURING SCHEDULED BRDG CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: HINGE — WORN (NR 5 SPOILER) · airframe 68,822 hrs · 38,871 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 5 GROUND SPOILER OUTBOARD HINGE WORN. REMOVED AND REPLACED SPOILER PER MM.

Part: FLAP — WARPED (RT WING) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP WARPED AT OUTBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLAP — CRACKED (LT WING) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING INBOARD MID FLAP CRACKED AT INBOARD END. REMOVED AND REPLACED MIDFLAP PER MM.

Part: RIB — CRACKED (RT WING) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING LOWER RIB CHORD CRACKED AT STA 135.5. REPAIRED CHORD PER ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED BETWEEN BS 664 AND BS 660, RBL 1. REPAIRED FLOORBEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 574, STR 17L. REMOVED AND REPLACED WEB PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360. STR 4L. REPAIRED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

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

Part: FRAME — CRACKED (BS 380 S8R) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 660, RBL 24. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 68,815 hrs · 38,864 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8L) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 827 S8R) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 887 S8L) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 867 S8R) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 500A S3R) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 727C S8R) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 663 S9L) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 927 S10L) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S9R) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S8R) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 787 S8L) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING OUTBOARD MID FLAP CRACKED AT NR 2 CARRIAGE CUTOUT. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S3R) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 357) · airframe 68,815 hrs · 38,854 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 357, RBL 1 TO RBL 4. REPAIRED SHEAR TIE PER SWA EA.

Part: BULKHEAD — CORRODED (BS 1016) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD CORRODED AT BS 1016, LBL 1. REPAIRED BULKHEAD PER SRM AND BOEING DRAWING.

Part: CREASE BEAM — CRACKED (BS 520) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM CRACKED AT BS 520, RBL 70. REPAIRED CREASE BEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 773) · airframe 68,815 hrs · 38,864 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 773, RBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: LAMP — INOPERATIVE (EXTERIOR) · airframe 68,814 hrs · 38,863 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,924 hrs · 28,164 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,915 hrs · 38,157 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER AFT CORNER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 66,874 hrs · 37,374 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: SKIN — CRACKED (BS 741E-745E) · airframe 66,706 hrs · 37,243 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 741E TO BS 745E, STR 23R TO STR 24R. REPAIRED SKIN PER SWA EA'S.

Part: HOUSING — CRACKED (SPOILER ACTUATOR) · airframe 66,176 hrs · 36,816 cycles

DURING SCHEDULED A1 CHECK, FOUND LT WING NR 4 SPOILER OUTBOARD ACTUATOR HOUSING CRACKED. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,673 hrs · 36,417 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,673 hrs · 36,417 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,673 hrs · 36,417 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 17R CRACKED AT BS 179. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,673 hrs · 36,417 cycles

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

Part: STRINGER SPLICE — CRACKED (BS 361 S16L) · airframe 65,673 hrs · 36,417 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 361, STR 16L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (BS 349 S16L) · airframe 65,673 hrs · 36,417 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 349, STR 16L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 359 S15L) · airframe 65,673 hrs · 36,417 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 359, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: VERTICAL BEAM — CRACKED (BS 178 BULKHEAD) · airframe 65,673 hrs · 36,417 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM CRACKED AT BS 178, LBL 5.7, WL 186. REPAIRED VERTICAL CHORD PER SRM.

Part: CREASE BEAM — CRACKED (BS 180 S17R) · airframe 65,673 hrs · 36,417 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 180, STR 17R. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 360 S14L) · airframe 65,673 hrs · 36,417 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FLOORBEAM — CRACKED (BS 180) · airframe 65,673 hrs · 36,417 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 180, RBL 15.33. REMOVED AND REPLACED FLOORBEAM WEB PER SRM.

Part: TAB — WORN (LT ELEVATOR) · airframe 65,654 hrs · 36,399 cycles

CLIMBING THROUGH FL250, 280 KNOTS A VERY NOTICEABLE VIBRATION FELT THROUGHOUT CABIN. REMOVED AND REPLACED LT ELEVATOR TRIM TAB PER MM.

Part: SKIN — CRACKED (BS 727E) · airframe 63,778 hrs · 34,944 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 22R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 744) · airframe 63,778 hrs · 34,944 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 744, STR 25R. REPAIRED SKIN PER SWA EA & SRM.

Part: SIGN — BROKEN (CABIN) · airframe 62,828 hrs · 34,178 cycles

FWD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — ERRATIC (CABIN) · airframe 62,539 hrs · 33,964 cycles

SEVERAL CABIN INTERIOR EMERGENCY EXIT LIGHTS ILLUMINATED. CYCLED EMERGENCY LIGHTS ARM SWITCH PER MM. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 62,400 hrs · 33,860 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,369 hrs · 33,836 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKS AT BS 769 AND BS 783, STR 22R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 62,023 hrs · 33,544 cycles

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

Part: CIRCUIT CARD — FAULTY (E&E BAY) · airframe 60,866 hrs · 32,650 cycles

DIVERSION, AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. CYCLED GEAR, NO HELP. REMOVED AND REPLACED S 846, S 845, M 1215 AND M 983, CARDS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 60,545 hrs · 32,420 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT LENS AT ROW 6 ABC, LOOSE. SECURED LIGHT LENS PER MM.

Part: SKIN — CORRODED (RUDDER) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND TOP RT SIDE OF RUDDER CORRODED. REMOVED AND REPLACED RUDDER PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL STIFFENER AT BS 663, RBL 5, CRACKED. REMOVED AND REPLACED STIFFENER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 727E + 10, STRINGER 26R, CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME INNER CHORD AT LT BS 616, WL 208, CRACKED. REMOVED AND REPLACED FRAME CHORD SECTION PER T1-153-018.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM WEB AT BS 617, RBL 63, CRACKED. REMOVED AND REPLACED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER T-CAP AT BS 312, LBL 12 TO LBL 13, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: FITTING — CRACKED (HORIZ STAB) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND HORIZONTAL STAB CENTER SECTION UPPER FITTING AND THRUST BEAM, CRACKED. REMOVED AND REPLACED FITTING PER MM.

Part: ATTACH FITTING — CORRODED (CABIN) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVAC SLIDE AFT GIRT BAR ATTACH FITTING, CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM T-CAP AT BS 344, LBL 9, CORRODED. REMOVED AND REPLACED FLOORBEAM T-CAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 767 + 5, LBL 13, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR UPPER FWD CORNER, AT DOOR CUTOUT, CORNER V-FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT NR 3 & NR 4 STOP FITTINGS. REMOVED AND REPLACED R1 DOOR PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 60,514 hrs · 32,289 cycles

DURING SCHEDULED 1/2D CHECK, FOUND MLG W/W CEILING BEADED WEB CRACKED AT BS 663, LBL 32 & RBL 43. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 60,514 hrs · 32,289 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPT FLOORBEAM CORRODED AT BS 767, LBL 3. REPAIRED BEAM PER SRM & SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,514 hrs · 32,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 360, BETWEEN STRINGER 14R AND STRINGER 15R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 59,675 hrs · 31,737 cycles

DURING SCHEDULED C1 CHECK, FOUND 5 EACH CRACKS AT LT WING NR 2 L/E SLAT. REPAIRED NR 2 L/E SLAT SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,202 hrs · 31,355 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 621, STRINGER 4L, CRACKED. REPAIRED SKIN PER EA.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,147 hrs · 31,305 cycles

BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 3 ABC, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 57,813 hrs · 30,235 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING INBOARD AFT FLAP PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 57,813 hrs · 30,235 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER MM.

Part: HINGE — WORN (LT ELEVATOR) · airframe 56,359 hrs · 29,060 cycles

AIRFRAME VIBRATION FELT, IN AFT CABIN FELT STRONGER. REMOVED AND REPLACED LT ELEV TAB NR 1 HINGE BUSHING AND REMOVED AND REPLACED LT ELEV TAB PER MM AND SWA SI.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,130 hrs · 28,093 cycles

DURING SCHEDULED C4 CHECK, FOUND LT AFT CABIN SIDEWALL EMERGENCY EXIT LIGHTS INOP. RELAMPED PER MM.

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 54,138 hrs · 27,316 cycles

AIR TURNBACK/DECLARED EMERGENCY, LOST HYD A-SYS PRESSURE AND QUANTITY INDICATIONS AFTER TAKEOFF. REMOVED AND REPLACED LEFT MLG RETRACT ACTUATOR HYD LINE PER MM.

Part: BUSHING — WORN (ELEVATOR) · airframe 53,848 hrs · 27,086 cycles

DURING FLIGHT VIBRATION FELT FROM AFT CABIN. REMOVED AND REPLACED RT ELEVATOR TAB ASSY PER MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,255 hrs · 25,791 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FAIL/SAFE STRAP CRACKED AT BS 794, BETWEEN STR 19R AND 27R. REPAIRED STRAP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,685 hrs · 24,517 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED 1.25 INCHES LONG AT BS 178, WL 201 AND RBL 5.0. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,486 hrs · 23,572 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT END OF E&E EQUIPTMENT COOLING CUT OUT. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 48,268 hrs · 22,515 cycles

EMERGENCY LIGHT LENS MISSING AT ROW 22 LT SIDE. INSTALLED LENS PER MM.

Part: WEDGE — DELAMINATED (SLAT) · airframe 47,636 hrs · 21,962 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 4 L/E SLAT INBOARD AND NR 5 L/E SLAT OUTBOARD T/E WEDGES DELAMINATED. REPAIRED WEDGES PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,347 hrs · 21,732 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT FUSELAGE EXTERNAL EMERGENCY LIGHT INOP AT BS 773. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 45,668 hrs · 20,318 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING O/B AFT FLAP I/B END DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SENSOR — MISSING (LT MLG) · airframe 44,899 hrs · 19,662 cycles

LT MLG INDICATED UNSAFE AFTER GEAR EXTENSION. DISCOVERED LT MLG DOWNLOCK SENSOR ATTACHING HARDWARE MISSING FROM SENSOR. INSTALLED MISSING HARDWARE ON DOWNLOCK SENSOR PER MM.

Part: SENSOR — LOOSE (LH MLG) · airframe 44,899 hrs · 19,662 cycles

DECLARED EMERGENCY. LT MLG INDICATED UNSAFE AFTER GEAR EXTENSION. RECYCLED GEARS AND INDICATION STILL PRESENT. C/W ALTERNATE GEAR EXTENTION PROCEDURES AND VERIFIED LT MLG DOWN AND LOCKED THROUGH VIEWING PORT AND TOWER CONFIRMED GEAR DOWN. REPOSITIONED AND SECURED LT MLG DOWN LOCK SENSOR PER MM.

Part: CABLE — FRAYED (ESCAPE SLIDE) · airframe 44,756 hrs · 19,520 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE RELEASE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: KEEL BEAM — CORRODED (BS 723)

DURING SCHEDULED TRANSITION CHECK, FOUND LT KEEL BEAM CORRODED AROUND NUT CLIP HOLES ON UPPER CHORD, BS 723. REPAIRED KEEL BEAM PER ER NR 99-6539.

Part: SHEAR TIE — CORRODED (BS 233)

DURING SCHEDULED TRANSITION CHECK, FOUND SHEAR TIE CORRODED, BS 233, WL 208, RBL 45. REMOVED AND REPLACED SHEAR TIE ASSY PER SRM.

Part: FLOORBEAM — CORRODED (BS 312 - 328)

DURING SCHEDULED TRASITION CHECK, FOUND FLOORBEAMS UPPER SURFACE CORRODED, BS 312, LBL 2 TO RBL 11, AND BS 328, RBL 25 TO RBL 42. REPAIRED FLOORBEAMS PER SRM.