N612SW

Part: BEAM — CORRODED (LT MLG) · airframe 63,785 hrs · 51,210 cycles

LEFT MLG ACTUATOR WALKING BEAM CORRODED AT ACTUATOR ATTACH POINT. R & R BEAM IAW SRM.

Part: FITTING — CRACKED (WING) · airframe 63,785 hrs · 51,210 cycles

UPPER SHEAR TIE FITTING CRACKED AT RS 179.56. R & R FITTING IAW DWG & SRM.

Part: SUPPORT FITTING — CORRODED (RT SPOILER) · airframe 63,785 hrs · 51,210 cycles

RIGHT WING NR 5 GND SPOILER ACTUATOR, INBD SUPPORT FITTING HINGE BORES FOR SPOILER CORRODED. R & R FITTING IAW SRM.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 63,785 hrs · 51,210 cycles

LEFT WING REAR SPAR GROUP OF 7 HOLES, HOLE NR 5, CRACKED IN AFT SUPPORT FITTING AT 9 O' CLOCK POSITION. REPAIRED FITTING IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,785 hrs · 51,210 cycles

LEFT WING REAR SPAR, GROUP OF 12 HOLES, HOLE NR 5, CRACKED IN UPPER SPAR CHORD, AT 6 & 12 O'CLOCK POSITION. R & R CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 613,785 hrs · 51,210 cycles

LEFT WING REAR SPAR, GROUP OF 12 HOLES, HOLE NR 6 CRACKED IN UPPER SPAR CHORD, AT 2 O'CLOCK POSITION. R & R CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,785 hrs · 51,210 cycles

LEFT WING REAR SPAR, GROUP OF 12 HOLES, HOLE NR 5 CRACKED IN REAR SPAR WEB, AT 6 & 12 O'CLOCK POSITION. R & R WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 63,785 hrs · 51,210 cycles

RIGHT WING REAR SPAR, GROUP 12 HOLES, NR 5 CRACKED IN WEB AT 6 & 12 O'CLOCK POSITION. R & R WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 63,785 hrs · 51,210 cycles

RIGHT WING REAR SPAR, GROUP OF 12 HOLES, HOLE NR 5 CRACKED IN REAR SPAR UPPER CHORD, AT 6 & 12 POSITION. R & R SPAR IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,785 hrs · 51,210 cycles

LEFT WING REAR SPAR GROUP OF 12 HOLES, HOLE NR 6 CRACKED IN REAR SPAR WEB, AT 6 & 12 O'CLOCK POSITION. R & R WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,785 hrs · 51,210 cycles

LEFT WING REAR SPAR, GROUP OF 12 HOLES, CRACKED IN REAR SPAR WEB, AT 5 & 10 O'CLOCK POSITION. R & R WEB IAW EA.

Part: VALVE — FAULTY (BLEED AIS SYS) · airframe 63,554 hrs · 51,050 cycles

DIVERSION, DECLARED EMER, CABIN ALTITUDE WARNING HORN & LIGHT ON, DURING CLIMB OUT PASSING FL190. NO AUTO FAIL OR ASSOCIATED LIGHTS OR INDICATIONS. OFF SCHEDULE DESCENT LIGHT ON DURING DESCENT. CABIN ALTITUDE REACHED 17,000'. MASKS DEPLOYED IN CABIN AUTOMATICALLY. R & R NR 1 PRE-COOLER VLV IAW AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 63,251 hrs · 50,827 cycles

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

Part: LIGHT — OUT OF ADJUST (CABIN) · airframe 62,729 hrs · 50,425 cycles

LEFT EMER EXIT OVERHEAD BIN BULLNOSE LIGHT OUT OF ADJUSTMENT AT ROW 22. ADJUSTED LIGHT IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 62,413 hrs · 50,198 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MM & MT.

Part: CHARGER — DAMAGED (CABIN) · airframe 62,246 hrs · 50,083 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 5. REPAIRED BATTERY CHARGER IAW WDW.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 62,246 hrs · 50,083 cycles

M167S EMER LIGHT L1187 INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: PLATE — BROKEN (CABIN) · airframe 62,246 hrs · 50,083 cycles

G1 GALLEY EMER LIGHT BASE PLATE BROKEN. R & R LIGHT IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

INTERCOSTAL CRACKED BETWEEN BS 847 - 867, STRINGER 19R. R & R INTERCOSTAL IAW DWG.

Part: FAIRING — CRACKED (TE FLAP) · airframe 62,246 hrs · 50,083 cycles

LEFT WING NR 2 FLAP FAIRING TAIL CONE CRACKED FROM TWO HOLES TO THE FWD EDGE. REPAIRED FAIRING IAW SRM.

Part: PLATE — CRACKED (R1 DOOR) · airframe 62,246 hrs · 50,083 cycles

R1 DOOR INTERNAL SKIN PLATE CRACKED BOTTOM, AFT LIGHTNING HOLE ON FWD SIDE. REPAIRED PLATE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

R2 DOOR INNER CREASE BEAM CHORD CORRODED. REPAIRED CHORD IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

R1 DOOR CREASE BEAM INNER CHORD CORRODED. R & R CREASE BEAM IAW DWG & SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

BULKHEAD WEB CRACKED AT BS 178, RBL 17. REPAIRED WEB IAW SRM & EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

BULKHEAD CHORD CRACKED AT BS 178, RBL 17. REPAIRED CHORD IAW SRM & EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 2L. R & R SPLICE IAW EA & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 5L. R & R CLIP IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD AFT END CRACKED AT BS 727B, LBL 24.8. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED CHORD IAW EA & ER.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

LEFT AIR CONDITION DOOR CUT OUT, FWD OTBD CORNER AIRING SUPPORT CRACKED. R & R SUPPORT IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

RIGHT FWD WING TO BODY FAIRING CUT OUT STRUCTURE CRACKED, AFT OTBD CORNER FWD OF AIR CONDITION DOOR. R & R ANGLE ASSEMBLY IAW SRM & DWG.

Part: REPAIR — CRACKED (R1 DOOR) · airframe 62,246 hrs · 50,083 cycles

R1 DOOR LOWER AFT REPAIR ON VERTICAL SIDE OF INTERNAL STRUCTURE FRAME CRACKED. R & R FRAME IAW DWG & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED ANGLE IAW EA.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 62,246 hrs · 50,083 cycles

AFT CARGO DOOR, AFT END OF CROSSBEAM E INBD T CHORD CRACKED AT THE CTR FASTENER OF THE THREE MOST AFT FASTENERS. R & R DOOR IAW AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

AFT CARGO BAY FLOORBEAM ANGLE CORRODED AT BS 772, RBL 3. REPAIRED ANGLE IAW SRM & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 727D+5, RBL 8. REPAIRED ANGLE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

AFT CARGO BAY SHEAR TIE CORRODED AT BS 747, BETWEEN STRINGER 26L - 27L. R & R SHEAR TIE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

AFT CARGO BAY SIDE WALL SUPPORT J ANGLE CRACKED AT BS 787, BETWEEN STRINGER 23L. R & R J ANGLE IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 727D+5, RBL 3. REPAIRED FLOORBEAM IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,246 hrs · 50,084 cycles

AFT CARGO BAY FLOORBEAM CHANNEL CORRODED AT BS 772, LBL 7. REPAIRED CHANNEL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18L. R & R CHORD IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,246 hrs · 50,083 cycles

FUSELAGE FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18R. R & R CHORD IAW EA, ER & SRM.

Part: LENS — DEFECTIVE (CABIN) · airframe 62,246 hrs · 50,083 cycles

LEFT SIDEWALL EMER EXIT SIDEWALL 2320Z LIGHT LENS INOPERATIVE. R & R LENS IAW DWG.

Part: CABLE — MISROUTED (R2 DOOR) · airframe 62,061 hrs · 49,955 cycles

R2 DOOR EMER EVAC SLIDE CABLE MISROUTED. REROUTED CABLE IAW MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 61,977 hrs · 49,898 cycles

R2 DOOR EMER EVAC SLIDE LOOSE OF CONTAINER. SECURED SLIDE IAW MT.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 61,354 hrs · 49,496 cycles

AFT CARGO FLOOR STRUCTURE INTERCOSTAL ATTACH CLIP CRACKED AT BS 787 STRINGER 27R. R & R CLIP IAW SRM & DWG.

Part: FLAP — DAMAGED (RT WING) · airframe 61,354 hrs · 49,496 cycles

RIGHT WING INBD MID FLAP TE DAMAGED. REPAIRED MID FLAP IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 61,153 hrs · 49,338 cycles

RIGHT WING BRACKET CRACKED AT INBD OF INBD FLAP OTBD TRACK FAIRING. R & R BRACKET IAW SRM.

Part: LIGHT — FAULTY (COCKPIT) · airframe 56,658 hrs · 48,288 cycles

ACRID SMELL WITH SMOKE & FUMES IN COCKPIT BY FIRST OFFICER`S OVERHEAD. R & R FIRST OFFICER`S MAP & KIT LIGHT ASSEMBLY.

Part: WINDOW — FAULTY (COCKPIT) · airframe 59,657 hrs · 48,288 cycles

CLIMBING THRU FL290 FIRST OFFICER & THE CAPTAIN DETECTED AN ACRID SMELL. THE FIRST OFFICER SAW A VERY THIN LAYER OF LIGHT GRAY SMOKE IN THE VICINITY OF HIS OVERHEAD UTILITY LIGHT. SMOKE & FUMES IMMEDIATELY BEGAN TO DISSIPATE. NO ELEC ARCING OR OTHER EVIDENCE OF FIRE WAS NOTED. R & R R1 WINDOW IAW MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 59,188 hrs · 47,955 cycles

RT WING NR 5 LE SLAT UPPER SURFACE DELAMINATED. R & R NR 5 SLAT IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 58,895 hrs · 47,756 cycles

LT WING OTBD TE AFT FLAP DELAMINATED. R & R AFT FLAP IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,246 hrs · 50,083 cycles

LEFT WING NR 1 SLAT SKIN CRACKED AT LOWER SURFACE AFT FASTENER ROW AT OTBD AUX TRACK. REPAIRED SKIN IAW SRM MM.

Part: SKIN — DELAMINATED (LT AILERON TAB) · airframe 57,736 hrs · 46,907 cycles

LT AILERON TAB DELAMINATED ON UPPER SURFACE AREA AROUND CONTROL RODS. R&R TAB ASSEMBLY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 57,629 hrs · 46,822 cycles

RT OVERWING EXIT SIGN LENS LOOSE. SECURED LENS IAW MM.

Part: LIGHT — CRACKED (EXTERIOR) · airframe 56,951 hrs · 46,308 cycles

EXTERIOR EMERGENCY LIGHT AT "L1" DOOR CRACKED. REMOVED AND REPLACED LIGHT IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

STRINGER CLIP CRACKED AT STA 1006, STR 8R. REMOVED & REPLACED CLIP IAW SRM & BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

SKIN CRACKED AT BS 380, STR 14R. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 827+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 847+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 807+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 8. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 887+10 UPPER AFT WINDOW CORNER SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 4, 9, 10. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 4, 6, 9, 10. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 3. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 787+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3, 5. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 727+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 867+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED INDICATION AT HOLES 1, 2, 3, 5, 9, 10. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 727+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 4, 6, 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

RIGHT BS 887+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 6, 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 500B+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 9, 11. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 500+10LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 4, 5,6, 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 420+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 4, 5, 6, 9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 867+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 2. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 500C+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES NR 2, 3, 4, 5, 6, 7, AND 11. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 420+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3, 4, 5, 6, 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 360+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW IR AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 867+10 UPPER AFT WINDOW CORNER SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 727+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 520+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 4, 5, 6, AND 12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 500+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3, 4, 9, 10. REPAIRED IAW AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 440+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 9, 11, 12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 380+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 4, 5, 6, 7, 9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 480+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3, 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 847+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACK INDICATION AT HOLES 1, 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 380+10 LOWER AFT WINDOW CUTOUT CRACKED AT HOLES 1, 2, 3, 4, 5, 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 500C+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 9, 10, 11, 12. REPAIRED SKIN IAW IR AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 807+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED INDICATION AT HOLES 1, 2, 8. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 400+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3, 4, 5, 6, 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 480+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 4, 5, 6, 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 767+10 LOWER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 887+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 400+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 4, 5, 6, 12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACK INDICATION AT HOLES 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACK INDICATION AT HOLES 1, 2, 3, 4. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 440+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 460+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 500A+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 4, 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 787+10 LOWER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,951 hrs · 46,308 cycles

LEFT BS 460+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3, 4, 5, 6, 7. REPAIRED SKIN IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 56,951 hrs · 46,308 cycles

EXIT LIGHT ASSY ON FWD LAV WALL BROKEN. REMOVED & REPLACED LIGHT ASSY PER AMM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 947.5 AND STR 21L IN AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE LOCATED BS 947.5 AND STR 21L TO STR 24L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DRAWING 65-49616.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

SUPPORT ANGLE CRACKED AT BS 727A AND BETWEEN STR 26L AND STR 25L IN CARGO COMPARTMENT. R & R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

SUPPORT ANGLE CRACKED AT BS 727A AND BETWEEN STR 26R AND STR 25R IN AFT CARGO COMPARTMENT. R & R ANGLE IAW SRM AND DWG.

Part: RUB STRIP — CRACKED (NR 1 ENGINE) · airframe 56,714 hrs · 46,148 cycles

CRACK ON RUBSTRIP P/N 69-76746-5 LOCATED ON ACCESS PANEL 57710L OF ENGINE 1. REPLACED RUBSTRIP IAW SRM B737-300 51-40-02-0G-0, 51-10-02-0G-0 ITEM 8 AND DWG 65C27356.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

CRACK ON FRAME LOCATED BS 947.5 AND BETWEEN STR 18L AND STR 19L IN AFT CARGO COMPARTMENT. REPLACED REPAIR FRAME SECTION LOCATED BS 947.5 AND BETWEEN STR 17L TO STR 24L IN AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 AND DWG 65-46947.

Part: ACCESS PANEL — CRACKED (LT NACELLE) · airframe 56,714 hrs · 46,148 cycles

CRACK ON FWD CORNER OF ACCESS PANEL 57720L LOCATED ON LEFT NACELLE STRUT. REPAIRED ACCESS PANEL 57720L LOCATED ON LEFT NACELLE STRUT IAW B737-300 SRM 51-70-16-OG-0 REPAIR 7.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

CRACK ON SUPPORT ANGLE LOCATED BETWEEN BS 927 AND BS 947 AND BL 0 UPPER FLOOR STRUCTURE OF AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE LOCATED BETWEEN BS 927 AND BS 947 AND BL 0 UPPER FLOOR STRUCTURE OF AFT CARGO COMPARTMENT IAW B737-300 SRM 51-40-02 AND DWG 69-36656.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

CRACK ON SUPPORT ANGLE LOCATED BETWEEN BS 380 AND BS 400 AND BL 0 UPPER FLOOR STRUCTURE OF FWD CARGO COMPARTMENT. REPLACED SUPPORT ANGLE IAW B737-300 SRM 51-10-02 ITEM 8 AND DRAWING 69-35365.

Part: RETAINER — CRACKED (HORIZ STAB) · airframe 56,714 hrs · 46,148 cycles

CRACK ON RETAINER SEAL LOCATED ON ACCESS PANEL 9126L HORIZONTAL STAB. REPLACED RETAINER SEAL LOCATED ON ACCESS PANEL 9126L HORIZONTAL STAB IAW SRM 51-40-02.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

WEB CRACKED AT BS 700+12.5" AT BL 0 LONGITUDINAL FLOORBEAM CENTER SECTION LOWER FASTENER ROW. REPAIRED WEB IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

CRACK ON WEB LOCATED BETWEEN BS 705 TO BS 711 AT RBL 24.82 LONGITUDINAL FLOORBEAM CENTER SECTION. REPAIRED WING CENTER SECTION RBL 24.82 FLOORBEAM WEB BETWEEN STA 698 TO STA 717 LONGITUDINAL FLOORBEAM IAW EA 1-357-7922 REV 0 AND EO AEM-HC57-010/13 REV 0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

CRACK INDICATION IN THE FRAME REINFORCEMENT AT THE 0.50 INCH DIAMETER HOLE LOCATED BETWEEN STR 20L AND STR 21L BS 520. REPAIRED FRAME LOCATED BS 520 AND BETWEEN STR 19L TO STR 22L IAW EO AEM-HC53-033/13 RO AND EA NO 1-353-21791 R0.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

WEB CRACKED AT BS 700+13.5" AT BL 0 LONGITUDINAL FLOORBEAM CENTER SECTION LOWER FASTENER ROW. REPAIRED WEB IAW EA TRUNCATED.

Part: WEB — CRACKED (NLG WW) · airframe 56,714 hrs · 46,148 cycles

CRACK INDICATION FOUND AROUND FASTENER HEAD ON NLG WHEEL WEB RIGHT SIDE LOCATED BS 243.7+3.5" AND WL 169.1 L=0.200" APPROX. REPAIRED WHEEL WEB RIGHT SIDE LOCATED BETWEEN BS 227.8 TO BS 259.5 AND WL 160.1 TO WL 190 RIGHT IAW B737-300 SRM 53-10-14 REPAIR 2, FIG 204 FOR INSPECTION REQUIREMENT SEE TLD: T027940.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

STRAP CRACKED BETWEEN BS 307 TO 349 AND AT LEVEL RBL FLOOR STRUCTURE AREA E/E COMP. R & R STRAP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

WEB CRACKED AT BS 700+7.5" AT BL 0 LONGITUDINAL FLOORBEAM CENTER SECTION LOWER FASTENER ROW. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

WEB CRACKED AT BS 700+9.5" AT BL 0 LONGITUDINAL FLOORBEAM CENTER SECTION LOWER FASTENER ROW. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

ANGLE CRACKED BETWEEN BS 887 TO 907 VOICE RECORDER COVER STRUCTURE AFT CARGO COMPARTMENT. R & R ANGLE IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 56,714 hrs · 46,148 cycles

TWO CRACKS WERE FOUND ON MAIN WHEEL WELL PRESSURE DECK AT BS 663.75 BETWEEN LBL 24.5 AND BL 0 CRACK 1 L=0.340",CRACK 2 L=0.250". REPLACED WEB ON MAIN WHEEL WELL PRESSURE DECK LOCATED BS 663.75 TO BS 675 BL 0 LBL 30 WING CENTER SECTION IAW SRM B737-300 51-10-02 AND DRAWING 65- 45409.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

CRACK ON ANGLE LOCATED INTERNAL LOWER STRUCTURE OF AFT ENTRY DOOR. REPLACED ANGLE IAW SRM B737-300 51-10-02 ITEM 8, SRM B737-300 51-40-02 AND DWG 65-58 299.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

CRACKS ON WEB (2EA) LOCATED BETWEEN BS 706 TO BS 711 AND LBL 24.82 LONGITUDINAL FLOORBEAM CENTER SECTION. REPAIRED WING CENTER SECTION FLOORBEAM WEB LBL 24.82 BETWEEN BS 698 TO BS 717 LONGITUDINAL BEAM IAW EA 1-357-7921 REV 0 AND EO AEM-HC57-009/13 R0.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,714 hrs · 46,148 cycles

WEB CRACKD BETWEEN BS 706 TO 711 AT BL 0 LONGITUDINAL FLOORBEAM CENTER SECTION. REPAIRED BEAM IAW EA.

Part: SLAT — FAILED (LT WING) · airframe 56,683 hrs · 46,131 cycles

LEFT WING NR 3 SLAT FAILED TO DE-ICE WITH WING ANTI-ICE SELECTED ON EITHER IN FLT OR ON THE GROUND. R & R NR 3 L/E SLAT IAW MM.

Part: PANEL — CRACKED (LT PYLON) · airframe 56,530 hrs · 46,018 cycles

PANEL 57720L HAS FWD I/B CORNER CRACKED THROUGH FASTENER HOLE. REPAIRED PANEL PER SRM.

Part: STRAP — CRACKED (NR 1 PYLON) · airframe 56,230 hrs · 45,797 cycles

NR 1 ENGINE - UPPER PYLON PANEL (AFT OF PANEL 57710L) NYLON NUT PLATE STRIP CRACKED. INSTALLED REPAIR STRAP PER EA 1-354-1517.

Part: WEB — CRACKED (LT MLG WW) · airframe 56,231 hrs · 45,797 cycles

MAIN W/W CEILING BEADING WEB CRACKED AT STA 664 LBL 32. REMOVED AND REPLACED WEB SRM.

Part: WEB — CRACKED (LT MLG WW) · airframe 56,231 hrs · 45,797 cycles

MAIN W/W CEILING BEADING WEB CRACKED STA 672 LBL 32. REMOVED AND REPLACED WEB IAW SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 55,395 hrs · 45,170 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: STRUCTURE — CRACKED (RT HORIZ STAB) · airframe 55,395 hrs · 45,170 cycles

RIGHT HORIZONTAL STABILIZER CRACKED. REPAIRED STABILIZER PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,395 hrs · 45,170 cycles

SKIN CRACKED BETWEEN BS 870 TO BS 871, STR 2L. REPAIRED SKIN PER ER AND EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 55,395 hrs · 45,170 cycles

CHANNEL STIFFENER CORRODED AT BS 1016, BL 0. REPAIRED STIFFENER IAW EA & ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,395 hrs · 45,170 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 868 TO BS 869, STR 2L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,715 hrs · 44,651 cycles

R1 DOOR FUSELAGE SKIN LOWER HINGE CUTOUT BEAR STRAP CRACKED AT BS 288, STR 14R. REPAIRED SKIN PER SRM.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 54,715 hrs · 44,651 cycles

FWD CARGO DOOR HANDLE CUTOUT CRACKED AT UPPER AFT CORNER. REMOVED AND REPLACED DOOR IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 54,331 hrs · 44,354 cycles

R1 DOOR EMERGENCY EVAC SLIDE GAUGE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: SLAT — DAMAGED (RT WING) · airframe 52,953 hrs · 43,346 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT WING NR 6 I/B SLAT CAN DAMAGED AT AFT UPPER WELD SEAM. REMOVED AND REPLACED SLAT CAN PER EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND UPPER CHORD CRACKED AT BS 294.5, LBL 50.5. REPAIRED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 328, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 183, RBL 5.7. REMOVED AND REPLACED WEB PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500A, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER CUTOUT CORNER. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM PER EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER FORWARD CORNER. REPAIRED SKIN PER EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 294, STR 7R. REPAIRED FRAME PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: SKIN — CRACKED (R1 DOOR) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR SKIN CRACKED AT BS 299, BETWEEN BEAM 4 TO BEAM 5. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM PER EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 505B, STR 11L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 505A, STR 11L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR FORWARD LOWER CUTOUT CORNER. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500A, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE WEB CORRODED BETWEEN BS 827 TO BS 847, STR 18R. REPAIRED WEB PER EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500A, BETWEEN STR 28R TO STR 27R. REPAIRED FRAME PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHANNEL CRACKED AT BS 729, RBL 3.0. REMOVED AND REPLACED CHANNEL PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 767 TO BS 787. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 28R TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND ANGLE CORRODED AT BS 767, BETWEEN STR 25R TO STR 25L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500A, BETWEEN STR 28L TO STR 27L. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 332.1 TO BS 334. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 1. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 2L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 312, BL 0. REPAIRED BEAM PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 500A TO BS 500B, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 6L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 639, LBL 46. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, BETWEEN STR 13L TO STR 14L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND ANGLE CRACKED AT BS 335, STR 21L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947.5, LBL 54. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 687, STR 2L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 360, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 277, STR 5L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 500B TO BS 500C, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: SLAT — DELAMINATED (LT WING) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B END NR 2 SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28R TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED BETWEEN BS 867 TO BS 907, STR 25R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B AFT FLAP O/B END DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SKIN PANEL — DELAMINATED (MIDFLAP) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING LOWER SKIN WEDGE PANEL I/B MID FLAP I/B END DELAMINATED. REPAIRED MID FLAP PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO DOOR FRAME CRACKED ON AFT LOWER CORNER. REMOVED AND REPLACED FRAME PER BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 727D TO BS 727E, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER BAC DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 727B TO BS 727C, STR 17R. REPAIRED BEAM PER DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 639, STR 14R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SLAT — DELAMINATED (RT WING) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT I/B END DELAMINATED. REPAIRED SLAT PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 907 TO BS 927, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: SLAT — DELAMINATED (RT WING) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 SLAT I/B END DELAMINATED. REPAIRED SLAT PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND DELAMINATION ON UPPER SKIN, OUTBOARD FORE FLAP. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (TE FLAP) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND CRACK ON RT WING LWR SURFACE OF INBOARD FORE FLAP. REPLACED FLAP PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND CORROSION ON UPPER CHORD FLOORBEAM FWD PAX COMPARTMENT, STA 344, BETWEEN LBBL 10 AND RBBL 10. REPAIRED CHORD PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND CRACK ON FWD CARGO COMPARTMENT SHEAR TIE, STA 520 BETWEEN STR 27R AND 28R. REPLACE TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND CRACK ON AFT CARGO COMPARTMENT SHEAR TIE, STA 1006 BETWEEN STR 27 AND 27R. REPLACE TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED CLIP PER SRM & BAC DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM & BAC DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP SRM.

Part: HOUSING — CRACKED (CABIN) · airframe 51,103 hrs · 41,919 cycles

DURING SCHEDULED 16Y CHECK, FOUND CRACK ON EMERGENCY LIGHT HOUSING OF BULL NOSE N.2 AND 4 LT. REPLACE EMERGENCY LIGHT HOUSING PER MM.

Part: LENS — LOOSE (CABIN) · airframe 50,514 hrs · 41,488 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,376 hrs · 41,388 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE ANGLE CRACKED AT BS 360, BETWEEN STR 14L TO STR 15L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 50,376 hrs · 41,388 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CHANNEL CRACKED AT BS 359, STR 14L. REMOVED AND REPLACED CHANNEL PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 50,204 hrs · 41,258 cycles

LT EEPLS LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 49,490 hrs · 40,721 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 49,490 hrs · 40,721 cycles

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

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 48,282 hrs · 39,838 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: STIFFENER — CRACKED (R1 DOOR) · airframe 47,865 hrs · 39,520 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR STIFFENER CRACKED AT AFT LOWER CORNER. REMOVED AND REPLACED R1 DOOR PER MM.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 46,455 hrs · 38,459 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR UPPER HINGE FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,455 hrs · 38,459 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: MOUNT — CRACKED (R2 DOOR) · airframe 46,455 hrs · 38,459 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE UPPER AFT MOUNT CRACKED. REMOVED AND REPLACED MOUNT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,455 hrs · 38,459 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,455 hrs · 38,459 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,455 hrs · 38,459 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,455 hrs · 38,459 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,455 hrs · 38,459 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,455 hrs · 38,459 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 44,960 hrs · 37,386 cycles

RT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 44,951 hrs · 37,381 cycles

RT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER SWA EA.

Part: LENS — LOOSE (CABIN) · airframe 44,798 hrs · 37,281 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 44,798 hrs · 37,281 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 44,760 hrs · 37,256 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 44,607 hrs · 37,144 cycles

L1 DOOR SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,635 hrs · 36,441 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, LBL 5.7. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,635 hrs · 36,441 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, LBL 17. REPAIRED WEB PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 42,202 hrs · 35,413 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,080 hrs · 35,323 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 41,229 hrs · 34,684 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT HORIZONTAL STABILIZER NR 6 HINGE FITTING CORRODED. REPAIRED FITTING PER ER.

Part: BEARING — WORN (LT AILERON) · airframe 41,229 hrs · 34,684 cycles

DURING SCHEDULED BRDG CHECK, LT AILERON FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING AND BUSHING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,229 hrs · 34,684 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,229 hrs · 34,684 cycles

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

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 41,229 hrs · 34,684 cycles

DURING SCHEDULED BRDGH CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 3 DEF. SECURED STRIP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,229 hrs · 34,684 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,229 hrs · 34,684 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,229 hrs · 34,684 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,229 hrs · 34,684 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,229 hrs · 34,684 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,229 hrs · 34,684 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,229 hrs · 34,684 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,229 hrs · 34,684 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,229 hrs · 34,684 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,229 hrs · 34,684 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 41,229 hrs · 34,684 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,118 hrs · 34,591 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 40,961 hrs · 34,467 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 40,569 hrs · 34,148 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 39,842 hrs · 33,555 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 39,570 hrs · 33,335 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (LT TE FLAP) · airframe 39,570 hrs · 33,335 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FRAME — CRACKED (BS 348 S16L) · airframe 38,552 hrs · 32,531 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME WEB CRACKED AT BS 348, STR 16L. REPAIRED FRAME WEB PER SRM AND EA.

Part: STRINGER SPLICE — CRACKED (BS 348 S16L) · airframe 38,552 hrs · 32,531 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED STRINGER SPLICE PER ACO.

Part: HOOK — LOOSE (L1 DOOR SLIDE) · airframe 38,336 hrs · 32,377 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 38,080 hrs · 32,176 cycles

L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,624 hrs · 31,798 cycles

DURING SCHEDULED C2 CHECK, FOUND FLT COMPT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 37,624 hrs · 31,798 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED UPPER CORNER. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,673 hrs · 31,054 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 34,874 hrs · 29,660 cycles

DURING SCHEDULED RON CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. FOUND WIRE NR W1460-509-20 BROKEN BETWEEN CONNECTORS NR D2976 AND D10714. REMOVED AND REPLACED BROKEN WIRE AND LIGHT ASSY PER WDM AND MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,836 hrs · 29,630 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 COCKPIT WINDOW POST CRACKED AT UPPER OUTBOARD CORNER. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 616, RBL 65, WL 200. REPAIRED FRAME CHORD PER BFG ER.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FWD & AFT FAILSAFE CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,618 hrs · 28,658 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 616, LBL 65, WL 200. REPAIRED FRAME CHORD PER BFG ER.

Part: CLIP — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, RBL 5 TO LBL 5. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (CABIN FLOOR) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 500A AND BS 500B, RBL 60. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 360, BS 400, BS 440 AND BS 500A, STR 8R TO STR 9R. REPAIRED FRAMES PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 685, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 52 TO RBL 52. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, LBL 58, WL 216. REPAIRED FRAME PER BFG ER.

Part: FITTING — CORRODED (GIRT BAR) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD AND AFT FLOOR FITTINGS CORRODED. REMOVED AND REPLACED FLOOR FITTINGS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 380, BS 400 AND BS 440, STR 8L TO STR 9L. REPAIRED FRAMES PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 7 TO RBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (CABIN FLOOR) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 837, LBL 70. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, RBL 7 TO RBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FWD CARGO) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 440, STR 23R TO STR 25R. REPAIRED FRAME PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CORRODED (FWD CARGO) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 492.4, RBL 28. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 787 AND BS 867, STR 8R TO STR 9R. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,618 hrs · 28,658 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 787 AND BS 867, STR 8L TO STR 9L. REPAIRED FRAMES PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 33,252 hrs · 28,366 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,907 hrs · 28,095 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 32,878 hrs · 28,077 cycles

R1 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 31,538 hrs · 27,009 cycles

DURING SCHEDULED RON, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 31,429 hrs · 26,913 cycles

R1 DOOR EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 31,039 hrs · 26,596 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD EMERGENCY EXIT OVERHEAD LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 31,039 hrs · 26,596 cycles

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

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 30,691 hrs · 26,291 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 30,669 hrs · 26,275 cycles

DURING SPV, FOUND STRINGER 1 AT BS 862, CRACKED. REPAIRED STRINGER SECTION PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 30,484 hrs · 26,116 cycles

DURING SCHEDULED RON, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 30,371 hrs · 26,001 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,150 hrs · 25,822 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT EQUIPMENT COOLING EXHAUST DUCT CUTOUT, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 29,774 hrs · 25,517 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 29,088 hrs · 24,979 cycles

R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 27,815 hrs · 23,954 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER LENS LOOSE. SECURED LENS COVER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 27,736 hrs · 23,885 cycles

R1 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: CABLE — FRAYED (ESCAPE SLIDE) · airframe 26,423 hrs · 22,812 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 25,963 hrs · 22,438 cycles

FWD SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: FITTING — CORRODED (LT & RT MLG) · airframe 25,853 hrs · 22,347 cycles

DURING SCHEDULED A1 CHECK, FOUND BOTH LT & RT MLG WALKING BEAM FITTINGS CORRODED. REMOVED AND REPLACED BOTH LT & RT MLG WALKING BEAM FITTINGS PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 24,524 hrs · 21,285 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS FOR AFT ROD END ON RT TAB PER MM.

Part: HINGE — WORN (RT ELEVATOR) · airframe 24,524 hrs · 21,285 cycles

DURING SCHEDULED C4 CHECK, FOUND PLAY AT RT ELEVATOR OTBD HINGE. SECURED RT ELEVATOR OTBD HINGE FITTING PER MM.

Part: ACTUATOR — FAILED (KRUEGER FLAP) · airframe 23,203 hrs · 20,159 cycles

AIR TURNBACK, DURING FLAP RETRACTION, THE L/E AMBER LIGHT AND NR 4 KRUEGER FLAP GREEN LIGHT SHOWED FULL EXTEND. RECYCLED FLAPS, NO HELP. VISUAL INSPECTION SHOWED NR 4 KRUEGER FLAP WAS STUCK FULL DOWN. REMOVED AND REPLACED NR 4 KRUEGER FLAP ACTUATOR PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,159 hrs · 20,122 cycles

AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,624 hrs · 19,736 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND LT OUTBOARD CHORD CRACKED AT BS 178, WL 207 AT LBL 26.0. REMOVED AND REPLACED CHORD PER SRM.

Part: SOLENOID — FAILED (COCKPIT) · airframe 21,716 hrs · 18,992 cycles

AIR TURNBACK, AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR LEVER LATCH SOLENOID. OPS CHECK GOOD PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 20,941 hrs · 18,356 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — LOOSE (FWD ENTRY DOOR) · airframe 20,846 hrs · 18,260 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: FLAP — DELAMINATED (RH WING) · airframe 20,845 hrs · 18,259 cycles

DURING SCHEDULED C4 CHECK, FOUND RH OTBD AFT T/E FLAP DELAMINATED AT INBD END. R&R FLAP PER MM.

Part: LIGHT — BROKEN (ENTRY DOOR) · airframe 18,095 hrs · 15,949 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. R&R EMERGENCY EXIT LIGHT ASSY PER MM.

Part: WIRE — SHORTED (COCKPIT) · airframe 17,219 hrs · 15,242 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY LIGHT TEST SWITCH IN COCKPIT INOP. REPAIRED SHORTED WIRE PER MM.

Part: FRAME — CORRODED (CABIN) · airframe 17,219 hrs · 15,242 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 993 FRAME CORRODED, RBL 50, WL 209. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (CABIN) · airframe 17,219 hrs · 15,242 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 957 FRAME CORRODED, STRINGER 16R TO STRINGER 17R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 17,219 hrs · 15,242 cycles

DURING SCHEDULED D-CHECK, FOUND BS 986 FLOORBEAM CORRODED ON UPPER FLANGE, RBL 25 TO RBL 40. REPAIRED FLOORBEAM PER SRM AND TRM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 17,068 hrs · 15,106 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH FWD DOOR EVACUATION SLIDE GIRT ASSY''S OUT OF ADJUST. REINSTALLED BOTH SLIDES PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 16,898 hrs · 14,965 cycles

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

Part: VALVE — INOPERATIVE (FUSELAGE) · airframe 16,209 hrs · 14,371 cycles

DIVERSION- AT 37,000 FT, CABIN CLIMBED TO 4,000 FT AND COULD NOT CONTROL PRESS IN ALT OR MANUAL MODES. DEFERRED PER MEL 21-14. AT BWI REMOVED AND REPLACED BOTH CABIN PRESS RELIEF VALVES PER MM.

Part: LIGHT — LOOSE (CABIN)

EEPLS LIGHTS LOOSE AT MID CABIN. SECURED LIGHTS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

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

Part: INDICATOR — MOVED (SLIDE)

FWD SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR)

FWD SERVICE DOOR EVACUATION SLIDE PRESS GAUGE OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — LOW PRESS (PAX DOOR)

DURING SCHEDULED OVERNIGHT CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE PRESS LOW. REMOVED AND REPLACED FWD ENTRY DOOR SLIDE ASSY PER MM.

Part: SLIDE — DETACHED (SERVICE DOOR)

FWD SERVICE DOOR EVACUATON SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: LENS — BROKEN (PASSENGER DOOR)

FWD ENTRY WAY, EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: GIRT BAR — NOT LATCHED (PASSENGER DOOR)

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE AFT GIRT BAR HOOK NOT LATCHING. REMOVED AND REPLACED LATCH - HOOK ASSY PER SRM.

Part: AIR DISTRIBUTION — ODOR (CABIN)

ON TAXI OUT, A PASSENGER INFORMED F/A OF A FUME SMELL IN THE CABIN. RETURNED TO GATE. INSPECTED AREA, OPERATED BOTH PACKS AND GASPER FANS. NO DESCREPANCIES NOTED.