N611SW

Part: SKIN — CRACKED (CARGO DOOR) · airframe 64,390 hrs · 51,717 cycles

FORWARD CARGO DOOR, LOWER DOOR SKIN CRACKED, AT 6:00 POSITION. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 64,072 hrs · 51,493 cycles

LEFT OUTER WING STRUCTURE, FWD OF AILERON NR 2 HINGE, VERTICAL LT ANGLE CRACKED. R & R LT ANGLE IAW SRM.

Part: HINGE — BROKEN (RT SPOILER) · airframe 64,072 hrs · 51,493 cycles

RIGHT WING INBD GND SPOILER, INBD ACTUATOR HINGE BROKEN. R & R SPOILER IAW AMM.

Part: DOOR — CRACKED (CABIN) · airframe 64,072 hrs · 51,493 cycles

R1 DOOR CRACKED AT LOWER FRAME, AFT CORNER AT AFT LOWER CORNER STOP FITTING. INSTALLED DOOR IAW AMM.

Part: LENS — OUT OF ADJUST (CABIN) · airframe 64,072 hrs · 51,493 cycles

LEFT EMER EXIT LIGHT LENS COVER OUT OF ADJUSTMENT. ADJUSTED LENS IAW AMM.

Part: STIFFENER — CRACKED (RT AILERON) · airframe 64,072 hrs · 51,493 cycles

RIGHT WING AILERON NR 2 HINGE STIFFENER CRACKED. R & R STIFFENER IAW SRM.

Part: GIRT BAR — OUT OF POSITION (EVAC SLIDE) · airframe 63,577 hrs · 51,150 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR OUT OF POSITION. R & R SLIDE IAW MT.

Part: LENS — MISSING (EXIT SIGN) · airframe 62,614 hrs · 50,438 cycles

R2 DOOR EMER EXIT SIGN LENS COVER MISSING. R & R COVER IAW AMM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

VERTICAL SUPPORT ANGLE CRACKED AT BS 727D, STRINGER 27L. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

VERTICAL SUPPORT ANGLE CRACKED AT BS 727D, STRINGER 27R. R & R ANGLE IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

FLOOR SUPPORT CHANNEL CRACKED AT BS 787, STRINGER 27L. REPAIRED CHANNEL IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

ANGLE CHANNEL CRACKED AT BS 787, STRINGER 27L. REPAIRED ANGLE IAW SRM.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

KEEL BEAM SKIN PANEL CRACKED AT BS 684, LBL 5. REPAIRED SKIN IAW SRM.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

EXTERNAL SKIN PANEL BETWEEN LT & RT MAIN GEAR CRACKED AT BS 684, RBL 5. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

LONGITUDINAL WEB CRACKED BETWEEN BS 500D TO 520. R & R WEB IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

SKIN CORRODED BETWEEN BS 927 TO 947, LBL 2. REPAIRED SKIN IAW SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

FORWARD SIDE OF PRESS DOME CORRODED AT BS 1016, LBL 1. REPAIRED DOME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 807 TO 787+6, ON UPPER SURFACE. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 727 - 747 ON UPPER SURFACE. REPAIRED WEB IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

INTERCOSTAL WEB CRACKED AT BS 727, LBL 36.5. R & R WEB IAW SRM & DWG.

Part: SUPPORT FITTING — CORRODED (FLAP TRACK) · airframe 62,067 hrs · 50,065 cycles

RIGHT WING NR 8 FLAP TRACK SUPPORT FITTING OUTER BOLT HOLE CORRODED AT RSS 434.742, WBL 355. REPAIRED FITTING IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

LEFT AFT SILL INNER CHORD CORRODED BETWEEN BS 947 TO 1006, LBL 58. R & R CHORD IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

RIGHT AFT MOP SILL INNER CHORD CORRODED. R & R CHORD IAW SRM & DWG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

BULKHEAD WEB CORRODED AT BS 1016, LBL 1. REPAIRED WEB IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

STRAP CRACKED AT BS 727, BETWEEN STRINGER 22 TO 27. R & R STRAP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 787 TO 807 ON TOP SIDE. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 360 - 380. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 500B TO 500C ON BOTTOM SIDE. REPAIRED WEB IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

SHEAR TIE CRACKED AT BS 328, STRINGER 20L. R & R SHEAR TIE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 380 TO 400. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 827 TO 807 ON TOP SIDE. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 847 - 827 ON TOP SIDE. R & R WEB IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

SHEAR TIE CRACKED AT BS 320, STRINGER 20L. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

SHEAR TIE CORRODED AT BS 947.5, BETWEEN STRINGER 23L TO 24L. R & R SHEAR TIE IAW SRM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 62,067 hrs · 50,065 cycles

LEFT WING NR 1 FLAP TRACK CORRODED AT AFT ATTACH PAD UNDER SHIM. R & R NR 1 FLAP TRACK IAW AMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 62,067 hrs · 50,065 cycles

RIGHT WING NR 8 FLAP TRACK CORRODED AT AFT ATTACH PAD UNDER SHIM. R & R FLAP TRACK IAW AMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 62,067 hrs · 50,065 cycles

LEFT WING NR 2 FLAP TRACK CORRODED AT AFT ATTACH PAD. REPAIRED FLAP TRACK IAW AMM.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 62,067 hrs · 50,065 cycles

VERTICAL STABILIZER FLANGE CLIP ON PANEL 9507 CRACKED. R & R CLIP IAW SRM & AMM.

Part: PANEL — CORRODED (RT WING) · airframe 62,067 hrs · 50,065 cycles

RIGHT WING FUEL PANEL 8817 CORRODED AROUND ALL HARDWARE HOLES INTERNAL SKIN. R & R PANEL IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

SHEAR TIE CRACKED AT BS 336, STRINGER 20L. R & R SHEAR TIE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

FLOORBOARD SUPPORT CHORD ANGLE STRUCTURE CRACKED AT BS 351.2, LBL 11.10. R & R ANGLE IAW SRM.

Part: FITTING — DIRTY (L1 DOOR) · airframe 62,067 hrs · 50,065 cycles

L1 DOOR EMER EVAC SLIDE LT FWD GIRT BAR FITTING DIRTY. CLEANED FITTING IAW MM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 670, LBL 24.5. R & R CHORD IAW SRM & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 707 TO 709, RBL 24.8. REPAIRED FLOORBEAM IAW EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

FRAME SUPPORT ANGLE CORRODED ON AFT SIDE OF FRAME AT BS 827, STRINGER 26R. R & R ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 24.8. R & R FLOORBEAM IAW SRM & DWG.

Part: TIE — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

STRINGER TIE CRACKED AT BS 787, STRINGER 23R. R & R TIE IAW DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

SHEAR TIE CORRODED AT BS 787, BETWEEN STRINGER 27L TO 27R. REPAIRED SHEAR TIE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

FUSELAGE SHEAR TIE CORRODED AT STATION 727E, STRINGER 26R. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

SHEAR TIE CORRODED BETWEEN BS 927 TO 943, LBL 2. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

FUSELAGE SHEAR TIE CORRODED AT STATION 727D, STRINGER 27L & 27R. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

SHEAR TIE CORRODED AT BS 727E, BETWEEN STRINGER 27L TO 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

FUSELAGE SHEAR TIE CORRODED AT STATION 727E, STRINGER 27L. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

SHEAR TIE CORRODED AT BS 827, BETWEEN STRINGER 27R TO 26R. REPAIRED SHEAR TIE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

SHEAR TIE CORRODED AT BS 727E, STRINGER 27L. R & R SHEAR TIE IAW SRM.

Part: FITTING — CORRODED (HYDRAULIC SYS) · airframe 62,067 hrs · 50,065 cycles

LEFT WING AREA COVERED BY PANEL 5735L, FWD & AFT HYD LINES END FITTING CORRODED. REPAIRED FITTING IAW AMM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

SHEAR TIE CORRODED AT BS 986.5, BETWEEN STRINGER 24R TO 25R. R & R SHEAR TIE IAW DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

SHEAR TIE CORRODED AT BS 727B, BETWEEN STRINGER 27L TO 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

SHEAR TIE CORRODED AT BS 727E, STRINGER 26R. R & R SHEAR TIE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

RIGHT CREASE WEB CORRODED ON LOWER SURFACE AT BS 500B+4. R & R WEB IAW SRM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 62,067 hrs · 50,065 cycles

RIGHT WING NR 6 FLAP TRACK ASSEMBLY INBD & OTBD TRACK CORRODED FWD END & ALONG THE EDGES. R & R FLAP TRACK ASSEMBLY IAW AMM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 62,067 hrs · 50,065 cycles

RIGHT WING OTBD NR 6 FLAP TRACK ASSEMBLY PYLON COVER ANGLE STRUCTURE CRACKED AT WBL 198.60. R & R ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

FUSELAGE FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A LOWER FWD OPEN BOLT HOLE. R & R CHORD IAW ER & EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 62,067 hrs · 50,065 cycles

RIGHT WING NR 5 FLAP TRACK ROLLER TRACK CORRODED. R & R NR 5 FLAP TRACK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,067 hrs · 50,065 cycles

FUSELAGE FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A LOWER FWD OPEN BOLT HOLE. R & R CHORD IAW ER & EA.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 61,064 hrs · 49,380 cycles

RIGHT WING NR 7 MID FLAP CARRIAGE SPINDLE CORRODED. R & R NR 7 MID FLAP IAW MT.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 61,064 hrs · 49,380 cycles

BULKHEAD Z STIFFENER CRACKED AT BS 1016 RBL 1.5. REPAIRED Z STIFFENER IAW EA.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 61,064 hrs · 49,380 cycles

AFT CARGO DOOR CUT OUT LOWER FWD CORNER BEAR STRAP CORRODED ON INBD SURFACE. REPAIR CUT OUT IAW SI.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,064 hrs · 49,380 cycles

INTERCOSTAL WEB ANGLE CRACKED BETWEEN BS 348 TO 351, STRINGER 16L. R & R ANGLE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,064 hrs · 49,380 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,064 hrs · 49,380 cycles

LEFT FRAME INNER CHORD LOWER INBD CRACKED AT BS 348 WL 208. R & R CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,064 hrs · 49,380 cycles

AFT CARGO DOOR CUT OUT LOWER FWD CORNER CRACKED FROM FASTENER HOLE TO CUT OUT. REPAIRED CUT OUT IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 61,064 hrs · 49,380 cycles

INTERCOSTAL CLIP CRACKED AT BS 348 STRINGER 15L. R & R CLIP IAW EA.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 61,064 hrs · 49,380 cycles

AFT CARGO PIT THRESHOLD WEB CORRODED. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,064 hrs · 49,380 cycles

LEFT FRAME OUTER CHORD LOWER WEB CRACKED BETWEEN BS 348 TO 351, WL 208. LEFT LOWER WEB AT WL 208. R & R WEB IAW EA & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,064 hrs · 49,380 cycles

INTERCOSTAL ANGLE CRACKED AT BS 348 STRINGER 15L. R & R ANGLE IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,645 hrs · 48,353 cycles

FORWARD ENTRY EMERGENCY LIGHT BATTERY PACK INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: LIGHT — MISSING (CABIN) · airframe 59,387 hrs · 48,181 cycles

LT EEPLS STRIP MISSING AT ROW 14. INSTALLED EEPLS IAW MMM.

Part: LUG — BROKEN (LT SPOILER) · airframe 59,272 hrs · 48,107 cycles

LT WING INBD GND SPOILER CTR INBD LUG BROKEN. R & R SPOILER IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 58,992 hrs · 47,921 cycles

EE COMPARTMENT STABILIZER STRAP CRACKED AT BS 328 BL 0. R & R STRAP IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 58,992 hrs · 47,921 cycles

EE COMPARTMENT STABILIZER STRAP CRACKED AT BS 314 RBL 31. R & R STRAP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 58,992 hrs · 47,921 cycles

LT WW CUT OUT AFT FAIRING SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 58,992 hrs · 47,921 cycles

EE COMPARTMENT STABILIZER STRAP CRACKED AT BS 314 RBL 46. R & R STRAP IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 58,992 hrs · 47,921 cycles

EE COMPARTMENT STABILIZER STRAP CRACKED AT BS 314 BL 0. R & R STRAP IAW SRM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 57,901 hrs · 47,132 cycles

LT WING NR 2 FLAP TRACK CANOE CRACKED AT INBD FORWARD PORTION OF CENTER SECTION OF CANOE. REPAIRED FAIRING IAW EA.

Part: HYDRAULIC LINE — DAMAGED (LT MLG WW) · airframe 57,654 hrs · 46,946 cycles

AIR TURNBACK, AFTER TAKEOFF WHILE RAISING THE GEAR MASTER CAUTION LIGHT ILLUMINATED WITH SYSTEM ENGINE & ELECTRIC HYDRAULIC LOW PRESSURE LIGHTS. REPLACED NR 2 MAIN.

Part: LIGHT — BROKEN (CABIN) · airframe 57,431 hrs · 46,779 cycles

RT EMERGENCY EXIT LIGHT BROKEN AT ROW 1. R & R EMERGENCY LIGHT HOUSING ASSY IAW AMM.

Part: CONTROLLER — FAULTY (COCKPIT) · airframe 56,829 hrs · 46,357 cycles

R2 SLIDING WINDOW ARCED AND CRACKED AT BOTTOM OF WINDOW AND BOTTOM CORNERS. REMOVED AND REPLACED WINDOW CONTROLLER AND REMOVED AND REPLACED F/O'S SLIDING WINDOW (R2) IAW M/M.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 56,618 hrs · 46,213 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER M/M AND MT.

Part: HOOK — OUT OF ADJUST (R2 DOOR) · airframe 56,592 hrs · 46,189 cycles

R2 DOOR SLIDE GIRT BAR HARD OPERATE. ADJUSTED GIRT BAR HOOKS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

AFT CARGO COMPARTMENT STATION 947 STRINGER CLIP AT S25R IS CRACKED. REMOVED AND INSTALLED S-25R CLIP AT BS 947 IAW SRM 51-40-02 AND BOEING DWG 65-46560.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

AFT CARGO BAY BS 947 STR S-18L STRINGER CLIP IS CRACKED. REMOVED S-18L CLIP AT BS 947 AND INSTALLED NEW S-18L CLIP AT BS 947 IAW SRM 51-40-02 AND BOEING DWG 65-46947.

Part: ATTACH FITTING — CRACKED (NR 1 PYLON) · airframe 56,214 hrs · 45,906 cycles

LEFT WING UPPER SURFACE, NR 1 PYLON PANEL 57710 ATTACH, AFT ATTACH POINT IS CRACKED AND BROKEN. REMOVED AND REPLACED AFT ATTACH NUT PLATE STRIPS ON FIXED FAIRING (PNL) AFT OF PNL 57710L IAW SRM 51-40-02-0G-0. LEAK CHECK GOOD IAW AMM 28-11-00.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

FOUND CLIPS (2EA) AT STRINGER 27R, BS 767 TO BE CORRODED UPON REMOVAL. FOUND CLIP 2 EA AT STRINGER 27R BS 767 TO BE CORRODED RECEIVED CLIP 66-23254-2 FASTENER HOLES IAW SRM 51-40-05 & DWG 66-23254 CLIPS INSTALLED ON NON ROUTINE CARD V# 839942

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

CARGO PIT FRAME 887, BETWEEN STR 17L AND 18L, SHEAR TIE CORRODED. REMOVED AND REPLACED FRAME IAW SRM AND BOEING DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

FRAME AT BS 767 CORRODED. REMOVED AND REPLACED FRAME PER BOEING DWG AND SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

LOWER FUSELAGE ELECTRONICS EQUIPMENT STA 344, BETWEEN STR 25R AND 26R CORRODED. REPAIRED SHEAR TIE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

INTERCOSTAL WEB CRACKED BETWEEN STA 807 TO 827, STR 27R. REMOVED AND REPLACED WEB IAW SRM AND BOEING DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

L1 DOOR SIDE FRAME STR 16L CRACKED AT BOTTOM INNER FITTING ATTACH BOLT. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

ENTRY DOOR SURROUND STRUCTURE INTERCOSTAL WEB CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

CARGO COMPARTMENT STR CLIP CORRODED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP IAW SRM BOEING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

FWD CARGO COMPARTMENT STRINGER CLIP CRACKED AT STA 420 S27L. REMOVED CRACKED STRINGER CLIP LOCATED AND DRILLED NEW STRINGER CLIP IAW SRM 51-40-02, SRM 51-40-03.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

FWD CARGO COMPARTMENT FRAME CLIP CORRODED STA 420 S26R. NO SRM ALLOWABLE DAMAGE LIMITS FOR CLIP AT STA 420, S-26R, REMOVED CORRODED CLIP AND INSTALLED NEW CLIP AT STA 420, S-26R IAW SRM 51-40-02 & DWG 65-20726.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

CARGO COMPARTMENT BILGE FRAME CORRODED AT BS 500A, LBL 2. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

L1 DOOR SIDE FRAME STR 16L CRACKED AT TOP INNER FITTING ATTACH BOLT. REMOVED AND REPLACED IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

CARGO COMPARTMENT FLOOR SUPPORT RAIL CORRODED AT BS 825, RBL 8. REMOVED AND REPLACED RAIL IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

CARGO COMPARTMENT BILGE SIDE OF FRAME CORRODED AT BS 787, BETWEEN RBL 9 TO RBL 14. REMOVED AND REPLACED FRAME IAW SRM.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 56,214 hrs · 45,906 cycles

CARGO COMPARTMENT FLOOR SUPPORT RAIL CORRODED BS 814, RBL 3. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

CARGO COMPARTMENT BULKHEAD SUPPORT ANGLE CORRODED BS 947, BETWEEN STR 21R TO STR 25R. REMOVED AND REPLACED IAW SRM AND DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 56,214 hrs · 45,906 cycles

NR 4 SLAT O/B END, UPPER SURFACE DELAMINATED ON EDGE. REPAIRED SLAT IAW SRM AMM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,214 hrs · 45,906 cycles

BILGE AREA, STA 1006 FROM LBL 5 TO RBL 5, SHEAR TIE CORRODED ON BOTH FWD AND AFT SIDES. REPLACED SHEAR TIE PER SRM.

Part: LENS — MISSING (CABIN) · airframe 56,162 hrs · 45,862 cycles

ROW 10 BULLNOSE (CAPT SIDE) EMERGENCY LIGHT LENS, MISSING ASSEMBLY LOOSE. RE-SECURED LIGHT ASSY & REPLACED LENS.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 55,747 hrs · 45,565 cycles

LEFT MAIN LANDING GEAR WHEEL WELL CEILING BEADED WEB CRACKED AT BS 664, LBL 32. REPAIRED WEB PER SRM.

Part: FLAP — DAMAGED (RT WING) · airframe 55,516 hrs · 45,385 cycles

RIGHT WING I/B AFT FLAP DAMAGED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 55,516 hrs · 45,385 cycles

RIGHT WING I/B MID FLAP DELAMINATED. REMOVED AND REPLACED MID FLAP ASSY PER MM.

Part: FLAP — DAMAGED (RT WING) · airframe 55,516 hrs · 45,385 cycles

RIGHT WING I/B FORE FLAP DAMAGED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 55,008 hrs · 44,997 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,166 hrs · 44,346 cycles

R2 DOOR DOOR SLIDE LIGHT INOP. RELAMPED PER MM.

Part: SKIN — GOUGED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

FUSELAGE SKIN STA 420 STR 8L HAS EXISTING GOUGE. REPAIRED EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 887+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 827+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 767+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN AT BS 887C+10 UPPER AFT WINDOW CORNER CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

LT FUSELAGE SKIN CRACKED AT BS 827+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

LT FUSELAGE SKIN AT BS 727B+10 UPPER AFT WINDOW CORNER CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN AT BS 360+10 LOWER FWD WINDOW CORNER CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN AT BS 530 UPPER FORWARD WINDOW CORNER CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 440+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN AT BS 500C+10 UPPER FORWARD WINDOW CORNER CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

LT FUSELAGE SKIN CRACKED AT BS 887+10 UPPER AFT WINDOW CORNER. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 500A+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 500B+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

LT FUSELAGE SKIN CRACKED AT BS 847+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN AW SB.

Part: SKIN — CRACKED (BS 727) · airframe 54,166 hrs · 44,346 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA AND REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 400+10 LOWER AFT WINDOW CORNER. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 480+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 847+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

LT FUSELAGE SKIN CRACKED AT BS 827+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

LT FUSELAGE SKIN CRACKED AT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

LT FUSELAGE SKIN CRACKED AT BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

LT FUSELAGE SKIN CRACKED AT BS 887+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 400+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 480+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 500+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

LT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 460+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 500A+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 420+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

LT FUSELAGE SKIN CRACKED AT BS 847+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

LT FUSELAGE SKIN CRACKED AT BS 807+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN AT BS 360+10 UPPER FORWARD WINDOW CORNER CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 420+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 500B+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

LT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 500+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

LT FUSELAGE SKIN CRACKED AT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 380+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

RT FUSELAGE SKIN CRACKED AT BS 440+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CORRODED (LE SLAT) · airframe 54,101 hrs · 44,297 cycles

LT WING NR 2 SLAT O/B TRAILING EDGE LOWER SURFACE CORRODED. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,560 hrs · 43,165 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 513, STR 10L. REPAIRED SKIN IAW ER.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,560 hrs · 43,165 cycles

DURING SCHEDULED OTS CHECK, FOUND RT WING NR 6 SLAT L/E LOWER SKIN CRACKED AT O/B END. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,559 hrs · 43,165 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 513, STR 10L. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 52,239 hrs · 42,918 cycles

LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 19R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 727E TO BS 747, STR 17R. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED BETWEEN BS 500B TO BS 500C, STR 17L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STR 5L TO STR 7L. REPAIRED WEB PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN LBL 0 TO LBL 13. REPAIRED FRAME SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND BULKHEAD UPPER PRESSURE WEB CRACKED AT BS 1016, STR 7R. REPAIRED WEB PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED AT BS 805, LBL 3. REPAIRED SKIN PER EA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR AFT LOWER FRAME CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND BULKHEAD UPPER PRESSURE WEB CRACKED AT BS 1016, BL 0. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLIGHT DECK WEB CRACKED AT FWD OUTBOARD MOUNT HOLE. REPAIRED WEB PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN RBL 0 TO RBL 6. REPAIRED SHEAR TIE PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 40 TO RBL 44. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND CRACKED STRINGER CLIP STA 663.75, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND STR 27R, BS 440 FWD CARGO COMPARTMENT SPLICE PLATE ATTACHING HOLES DAMAGE AND CORRODED. REPLACED STRINGER PER EA.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND DAMAGED STRINGER CLIP STA 747, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: FLANGE — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND CORROSION ON INBOARD FLANGE AT STA 807, STR 27L. REPAIRED FLANGE PER EA.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND DAMAGED STRINGER CLIP STA 847, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND CORROSION ON FLOORBEAM AT STA 767, LBL 13. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 1. REMOVED AND REPLACED BEAM SECTION PER SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR AFT LOWER FRAME CRACKED AT LOWER DOOR STOP FASTENER HOLE. REMOVED AND REPLACED DOOR PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORROSION AT STA 847+5, LBL 3 AT NUT PLATE HOLE. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORROSION AT STA 847+5, LBL 8 AT NUT PLATE HOLE. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORROSION AT STA 847+5, RBL 3 AT NUT PLATE HOLE. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORROSION AT STA 847+5, LBL 13 AT NUT PLATE HOLE. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR BEAM CORROSION AT STA 847+5, RBL 8 AT NUT PLATE HOLE. REPAIRED FLOORBEAM PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, RBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, RBL 17. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 508A, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 51,271 hrs · 42,153 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 514A, STR 10L. REPAIRED SKIN PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 180, LBL 17. REPAIRED WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED AT BS 440, STR 27R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 184, LBL 17. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,271 hrs · 42,153 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, RBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: COVER — MISSING (CABIN) · airframe 51,178 hrs · 42,089 cycles

LT EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 44,346 cycles

FUSELAGE SKIN CRACKED AT BS 500B +10, STR 10L. REMOVED AND REPLACED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,766 hrs · 41,774 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 49,151 hrs · 40,528 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LENS — FADED (CABIN) · airframe 49,030 hrs · 40,444 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS FADED. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,842 hrs · 40,305 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 510C, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,501 hrs · 40,058 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 389.5, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,501 hrs · 40,058 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 737E, STR 10R. REPAIRED SKIN PER EA.

Part: HINGE FITTING — BROKEN (SPOILER) · airframe 47,515 hrs · 39,325 cycles

DURING SCHEDULED 2CH2 CHECK, FOUND NR 5 GROUND SPOILER INBOARD HINGE FITTING BROKEN. REMOVED AND REPLACED SPOILER ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 47,515 hrs · 39,325 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED AT UPPER INBOARD SIDE. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,515 hrs · 39,325 cycles

DURING SCHEDULED 2CH2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 47,515 hrs · 39,325 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND KEEL BEAM CRACKED AT BS 715, LBL 6. REPAIRED KEEL BEAM PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,037 hrs · 38,986 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FWD EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,796 hrs · 38,804 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 378 TO BS 379, BETWEEN LBL 2 TO LBL 3. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT AT BS 305, BETWEEN WL 238 TO WL 239. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT AT BS 305, WL 260. REPAIRED SKIN PER AAR EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 386 TO BS 392. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CORRODED AT BS 374, STR 28L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 380, LBL 5. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND NOSE WHEEL WELL SNUBBER SPRING ATTACHMENT WEB CRACKED AT BS 259, LBL 7.75. REPAIRED SKIN PER ACO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CORRODED AT BS 374, STR 28L. REPAIRED STRINGER PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 767 TO BS 772. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRIP — DELAMINATED (CABIN) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS STRIPS DELAMINATED. REMOVED AND REPLACED EEPLS STRIPS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: RIB — CRACKED (RT WING) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED14Y CHECK, FOUND RT WING LOWER RIB CHORD CRACKED BETWEEN STR S2 & S3. REPAIRED RIB CHORD PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,526 hrs · 38,597 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 45,911 hrs · 38,146 cycles

R1 DOOR EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 45,911 hrs · 38,146 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 45,483 hrs · 37,822 cycles

LT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,199 hrs · 37,635 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7, WL 182. REPAIRED BEAM PER SWA EA.

Part: BULKHEAD — CRACKED (BS 178) · airframe 45,112 hrs · 37,574 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL WEB CRACKED AT BS 178, RBL 5.7, WL 182. REPAIRED WEB PER SWA EA.

Part: COVER — MISSING (CABIN) · airframe 44,975 hrs · 37,485 cycles

FWD EMERGENCY EXIT SIGN LENS COVER MISSING. INSTALLED COVER PER MM.

Part: FIRE LOOP — FAULTY (APU) · airframe 42,113 hrs · 35,400 cycles

DECLARED EMERGENCY. APU FIRE WARNING INFLIGHT, FIRE BOTTLE DISCHARGED. REMOVED AND REPLACED APU LOWER FIRE DETECTOR LOOP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,901 hrs · 35,245 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 10L. REPAIRED SKIN PER SWA EA.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 41,224 hrs · 34,724 cycles

ON CLIMBOUT RIGHT MLG DID NOT INDICATED UP AND LOCKED. CYCLED GEAR NO CHANGE. REMOVED AND REPLACED RIGHT MLG UPLOCK ACTUATOR PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 41,125 hrs · 34,652 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING OUTBOARD MID FLAP INBOARD L/E DELAMINATED. REPAIRED FLAP PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 40,887 hrs · 34,466 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: ACTUATOR — FAILED (RT MLG) · 34,241 cycles

DECLARED EMERGENCY / DIVERSION. RIGHT MLG STAYED DOWN AND LOCKED DURING CLIMB. FERRY TO HOU FOR MAINTENANCE. REMOVED AND REPLACED RIGHT MLG RETRACT ACTUATOR PER MM.

Part: SKIN — CRACKED (BS 706) · airframe 39,313 hrs · 33,233 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT KEEL BEAM SKIN CRACKED AT BS 706, LBL 6.50. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 706) · airframe 39,313 hrs · 33,233 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT KEEL BEAM SKIN CRACKED AT BS 706, RBL 6.50. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 39,299 hrs · 33,228 cycles

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

Part: STRUCTURE — CRACKED (L/E SLAT) · airframe 38,243 hrs · 32,411 cycles

DURING SCHEDULED C3 CHECK, FOUND LEFT WING NR 1 L/E SLAT CRACKED AT LOWER AFT CORNER. REPAIRED SLAT PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 38,246 hrs · 32,411 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 37,346 hrs · 31,695 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 37,346 hrs · 31,695 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,079 hrs · 31,492 cycles

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

Part: RELIEF VALVE — MALFUNCTIONED (RT WING) · airframe 36,323 hrs · 30,876 cycles

DIVERSION, ON DEPARTURE FROM SAT, FUEL SPRAY REPORTED OUT OF RT WING, IMBALANCE OF 600 POUNDS. RESET RT WING PRESSURE RELIEF VALVE PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 35,463 hrs · 30,236 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 35,333 hrs · 30,128 cycles

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

Part: SENSOR — OUT OF ADJUST (RT MLG) · airframe 34,502 hrs · 29,474 cycles

RT MLG UNSAFE LIGHT INDICATION, CYCLED THE GEARS AND OPERATED NORMAL. ADJUSTED RT MLG UPLOCK SENSOR PER MM.

Part: LOGIC CARD — FAULTY (MLG SYSTEM) · airframe 34,481 hrs · 29,453 cycles

AIR TURNBACK, UNSAFE LANDING GEAR INDICATION AFTER GEAR RETRACTION. WARNING HORN ALSO SOUNDED. REMOVED AND REPLACED LANDING GEAR M990 LOGIC CARD PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 34,403 hrs · 29,391 cycles

DURING SCHEDULED RON CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,921 hrs · 28,183 cycles

DURING SCHEDULED D-CHECK, L2 DOOR EMERGENCY EXIT LIGHT BATTERY WOULD NOT CHARGE. REMOVED AND REPLACED BATTERY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,921 hrs · 28,183 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 32,904 hrs · 28,165 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,904 hrs · 28,165 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,904 hrs · 28,165 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,904 hrs · 28,165 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,904 hrs · 28,165 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,904 hrs · 28,165 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,904 hrs · 28,165 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,904 hrs · 28,165 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,904 hrs · 28,165 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 32,904 hrs · 28,165 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 747) · airframe 32,904 hrs · 28,165 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,894 hrs · 28,159 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 727A + 4, RBL 2, WL 155. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,894 hrs · 28,159 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,894 hrs · 28,159 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME AT BS 767, STR 27L TO STR 25R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,894 hrs · 28,159 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA LONGITUDINAL FLOORBEAMS CORRODED AT BS 727E +2, LBL 2 & RBL 7, WL 155. REPAIRED FLOORBEAMS PER SRM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 32,894 hrs · 28,159 cycles

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

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 32,894 hrs · 28,159 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,894 hrs · 28,159 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAME CHORDS CRACKED AT BS 616, LBL 65 & RBL 65, WL 202. REPAIRED FRAME CHORDS PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,894 hrs · 28,159 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,885 hrs · 28,151 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON RT CREASE BEAM WEB AT BS 370 & BS 406. REPAIRED CREASE BEAM WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,885 hrs · 28,151 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON LT CREASE BEAM WEB AT BS 500 + 10, BS 500A + 15 & BS 500C + 15. REPAIRED CREASE BEAM WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,881 hrs · 28,149 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500D, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,881 hrs · 28,149 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER BOEING S/B.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 32,269 hrs · 27,648 cycles

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

Part: FITTING — WORN (LT ELEVATOR) · airframe 31,719 hrs · 27,257 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB INBOARD HINGE HAS PLAY. REMOVED AND REPLACED INBOARD ELEVATOR TAB HINGE FITTING PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 31,524 hrs · 27,080 cycles

FWD OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 31,198 hrs · 26,787 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 31,190 hrs · 26,779 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 30,813 hrs · 26,478 cycles

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

Part: BUSHING — WORN (LT ELEVATOR) · airframe 30,806 hrs · 26,470 cycles

DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE BUSHING AND HARDWARE PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,806 hrs · 26,470 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR HINGE BOX PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 30,806 hrs · 26,470 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: CABLE — FRAYED (R2 DOOR SLIDE) · airframe 30,806 hrs · 26,470 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 30,333 hrs · 26,075 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 30,268 hrs · 26,023 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 30,149 hrs · 25,915 cycles

R2 DOOR EVAC SLIDE OUT OF ADJUST. DISCREPANCY ALSO OCCURRED AT SJC ON SAME DAY. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 30,141 hrs · 25,907 cycles

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

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 29,882 hrs · 25,696 cycles

DURING SPV, FOUND BULKHEAD PRESSURE WEB AT BS 1016, BETWEEN SRTINGER 27L AND STRINGER 26L, CORRODED. REPAIRED PRESSURE WEB PER ER.

Part: STRAP — CRACKED (FUSELAGE) · airframe 29,863 hrs · 25,683 cycles

DURING SPV, FOUND BULKHEAD STRAP AT BS 178, RBL 6 TO RBL 25, CRACKED. REMOVED AND REPLACED STRAP PER SRM AND BAC DRAWING.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 29,711 hrs · 25,571 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 29,462 hrs · 25,373 cycles

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

Part: BULB — MALFUNCTIONED (NR 2 ENG OIL) · airframe 29,377 hrs · 25,308 cycles

DECLARED EMERGENCY, INFLIGHT SHUT DOWN, AIR TURNBACK. DURING CRUISE NR 2 ENG OIL TEMP IN YELLOW BAND, C/W QRH, OIL TEMP STILL IN YELLOW BAND, MOMENTARLY IN RED BAND, SHUT DOWN NR 2 ENG. REMOVED AND REPLACED NR 2 ENG OIL TEMP BULB PER MM.

Part: FAN — FAULTY (E/E BAY) · airframe 29,279 hrs · 25,229 cycles

BURNING ODOR IN CABIN. REMOVED AND REPLACED RECIRCULATING FAN PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 28,961 hrs · 24,976 cycles

DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BUSHING PER MM.

Part: LENS — MISSING (CABIN) · airframe 28,961 hrs · 24,976 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 28,265 hrs · 24,415 cycles

R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 28,265 hrs · 24,415 cycles

L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 27,993 hrs · 24,203 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT LENS BROKEN OUTBD OF FWD F/A'S SEAT. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — DISLODGED (FWD ENTRY DOOR) · airframe 27,312 hrs · 23,659 cycles

DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 27,159 hrs · 23,531 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS FELL OFF. REINSTALLED LENS PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 26,351 hrs · 22,869 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 26,235 hrs · 22,772 cycles

DURING SCHEDULED C2 CHECK, FOUND RT OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD AFT CORNER. REMOVED AND REPLACED OUTBOARD T/E AFT FLAP PER MM.

Part: MODULE — FAULTY (COCKPIT) · airframe 25,762 hrs · 22,382 cycles

DECLARED EMERGENCY. CABIN PRESSURIZATION CONTROLLER FAILED, COULD NOT MAINTAIN CABIN PRESSURE. RAPID DECOMPRESSION OCCURRED. FWD F/A'S O2 MASK DID NOT FALL DOWN. PRESSURIZATION CONTROLLER OPERATED PARTIALLY DURING SHORT FINAL. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER, OVERHEAD MODULE, AND OUTFLOW VALVE. OPS CHECK GOOD PER MM.

Part: FLAP — CRACKED (RT WING) · airframe 25,519 hrs · 22,201 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBD T/E FORE FLAP LOWER SURFACE CRACKED. REMOVED AND REPLACED FLAP ASSY PER MM

Part: FLAP — CRACKED (LT WING) · airframe 25,519 hrs · 22,201 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBD T/E FORE FLAP LOWER SURFACE CRACKED. REMOVED AND REPLACED FLAP ASSY PER MM

Part: HOOK — LOOSE (L1 DOOR) · airframe 25,519 hrs · 22,201 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR ESCAPE SLIDE COVER FWD HOOK LOOSE. SECURED L1 DOOR ESCAPE SLIDE COVER FWD HOOK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,519 hrs · 22,201 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME LOWER SIDE CRACKED AT BS 460, STR 28. REPAIRED CRACKED SECTION OF FUSELAGE FRAME PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 24,748 hrs · 21,561 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FITTING — CORRODED (LT AND RT MLG W/W) · airframe 24,748 hrs · 21,561 cycles

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

Part: TRUNNION — CORRODED (LT & RT MLG) · airframe 24,748 hrs · 21,561 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11251-32, BOTH RT AND LT MLG FAILED TRUNNION PIN INSPECTION. REMOVED AND REPLACED BOTH MLG PER MM.

Part: SENSOR — FAILED (KRUEGER FLAP) · airframe 23,571 hrs · 20,557 cycles

AIR TURNBACK, ON DEPARTURE NR 3 KRUEGER FLAP WOULD NOT RETRACT. REMOVED AND REPLACED S173 FULL EXTEND SENSOR PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 23,416 hrs · 20,422 cycles

DURING SCHEDULED C3 CHECK, SWA SI 11111-55, FOUND LT ELEVATOR TAB CONTROL MECHANISM FWD LINKS WORN. REMOVED AND REPLACED LT ELEVATOR LINKS AND BUSHINGS PER MM.

Part: BRACKET — LOOSE (AFT ENTRY DOOR) · airframe 22,542 hrs · 19,726 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET HAS A BROKEN RIVET. REMOVED AND REPLACED RIVET PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 22,542 hrs · 19,726 cycles

DURING SCHEDULED C2 CHECK, FOUND RT OTBD AFT FLAP DELAMINATED ON LOWER INBD CORNER, LOWER SURFACE. REMOVED AND REPLACED OTBD AFT FLAP PER MM.

Part: THROTTLE — OBSTRUCTED (NR 2 ENGINE) · airframe 22,308 hrs · 19,530 cycles

AIR TURNBACK, IN FLT ENGINE SHUTDOWN, DURING CLIMBOUT DISCOVERED THE NR 2 ENGINE THROTTLE WOULD NOT RETARD BELOW 88 PERCENT N1, HAD TO SHUT ENGINE DOWN AND LAND SINGLE ENGINE. FOUND DEBRIS IN THE THROTTLE QUADRANT AT 6 O'CLOCK ENGINE POSITION. REMOVED DEBRIS, THROTTLES OPS NORMAL PER MM.

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 21,215 hrs · 18,646 cycles

FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. REPOSITIONED SLIDE PER MM.

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 21,131 hrs · 18,567 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 21,122 hrs · 18,561 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SLIDE — DRAGGING (FWD ENTRY DOOR) · airframe 21,112 hrs · 18,551 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 20,851 hrs · 18,334 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM.

Part: BEARING — WORN (RH ELEVATOR.) · airframe 20,794 hrs · 18,287 cycles

DURING SCHEDULED C4 CHECK, RH ELEVATOR FAILED FREE PLAY CHECK. R&R RH ELEVATOR BEARING PER MM.

Part: TAB — WORN (LH ELEVATOR) · airframe 20,794 hrs · 18,287 cycles

DURING SCHEDULED C4 CHECK, LH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R LH ELEVATOR TAB PER MM.

Part: STRAP — BROKEN (CABIN) · airframe 20,439 hrs · 17,990 cycles

EMERGENCY FLASH LIGHT STRAP BROKEN AFT LOWER. R&R STRAP PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 20,287 hrs · 17,861 cycles

DURING SCHEDULED RON CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (SERVICE DOOR) · airframe 19,841 hrs · 17,481 cycles

FWD SVC DOOR SKIN CRACKED AT UPPER LEFT CORNER. REMOVED AND REPLACED FWD SVC DOOR PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 19,557 hrs · 17,255 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. R&R EVAC SLIDE ASSY PER MM.

Part: TORQUE LINK — WORN (RT MLG) · airframe 17,861 hrs · 15,896 cycles

DURING SCHEDULED C1 CHECK, FOUND RT MLG UPPER AND LOWER TORQUE LINKS WORN. REMOVED AND REPLACED UPPER TORQUE LINK (P/N 65-67963) AND LOWER TORQUE LINK.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,213 hrs · 15,328 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 L-ANGLE CRACKED, BS 310, STRINGERS 10R AND 7R. REMOVED AND REPLACED BOTH L-ANGLES PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 17,213 hrs · 15,328 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 986 FLOORBEAM CORRODED, RBL 32 TO RBL 40. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,213 hrs · 15,328 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT FWD I/B CORNER OF FWD SERVICE DOOR CUTOUT, BS 295. REPAIRED FRAME PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 17,036 hrs · 15,185 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACKS LOOSE. SECURED EEPLS TRACKS PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 17,036 hrs · 15,185 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,016 hrs · 15,173 cycles

EEPLS INOP AT ROWS 6 - 10. REPAIRED WIRES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,837 hrs · 15,014 cycles

EEPLS INOPERATIVE AT ROW 14. R&R LIGHT ASSY PER MM.

Part: SENSOR — INOPERATIVE (COCKPIT) · airframe 16,786 hrs · 14,973 cycles

DIVERSION. LOST ALL N1 INDICATORS ON CDU, CAPTAINS VSI INOPERATIVE, ILS INOPERATIVE, CABIN PRESS INOPERATIVE IN AUTO AND ALT MODES. CHECKED WITH BITE CHECK OF LANDING GEAR SAFETY SENSORS, AND R & R GROUND SENSE PROX CARD M990 AND AIR GROUND RELAY R320. OPS CHECK GOOD.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 16,751 hrs · 14,940 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER AS DOOR WAS CLOSING DUE TO GIRT BAR NOT PROPERLY STOWED. REINSTALLED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,705 hrs · 14,896 cycles

EEPLS INOP AT OVERWING EXITS. RECONNECTED WIRES AND SECURED LIGHT TRACK PER MM.

Part: COVER — MISSING (CABIN) · airframe 16,573 hrs · 14,783 cycles

EEPLS TRACK COVER MISSING AT ROW 14. INSTALLED TRACK COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 16,382 hrs · 14,618 cycles

EEPLS TRACK LOOSE AT ROW 12. SECURED TRACK ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,363 hrs · 14,598 cycles

DURING SCHEDULED D-CHECK, FOUND EEPLS INOP AT MID CABIN. REPAIRED EEPLS WIRES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,387 hrs · 14,639 cycles

MID CABIN EMERGENCY EXIT OVERWING LIGHTS INOP. SECURED LIGHT ASSY''S AND OPS CK GOOD PER MM.

Part: LIGHT — LOOSE (CABIN)

EEPLS TRACK ASSY PULLED UP FWD OF OVERWING EXITS. SECURED TRACK ASSY PER MM.

Part: WIRE — LOOSE (CABIN)

EEPLS WIRES EXPOSED AT OVERWING EXIT. REPAIRED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN)

EEPLS TRACK PULLED UP AT OVERWING EXIT. RESECURED LIGHT ASSY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

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

Part: SLIDE — LOOSE (PASSENGER DOOR)

FWD ENTRY DOOR SLIDE CAME OUT OF CONTAINER. RESTOWED SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (ROW 12)

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY TRACK LIGHTING SECURED WITH TAPE AT ROW 12. REMOVED TAPE AND SECURED LIGHTING PER BOEING MM.

Part: CHARGER — INOPERATIVE (CABIN)

DURING SCHEDULED C1 CHECK, FOUND CENTER CABIN FLOOR TRACK LIGHTING INOP. REPLACED BATTERY CHARGER PER BOEING M/M.