N386SW

Part: ACTUATOR — INOPERATIVE (RT MLG UPLOCK) · airframe 70,738 hrs · 57,264 cycles

RIGHT MLG UNSAFE LIGHT INDCATION, RETURNED TO DEPARTURE. R & R RT MLG UPLOCK ACTUATOR.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 70,362 hrs · 56,996 cycles

AFT GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED A WIRE IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 70,155 hrs · 56,850 cycles

RIGHT WING EMERGENCY EXIT DOOR LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 69,916 hrs · 56,694 cycles

L2 DOOR EXIT LIGHT INOPERATIVE. REPAIRED EXIT LIGHT WIRING IAW MM.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 69,916 hrs · 56,694 cycles

L2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE WIRE IAW SWPM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 69,764 hrs · 56,591 cycles

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

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 69,764 hrs · 56,591 cycles

LEFT WING INBOARD TRAILING EDGE FLAP DELAMINATED ON OUTBOARD END. R & R AFT FLAP IAW AMM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 69,764 hrs · 56,591 cycles

RT WING SPAR ACCESS PANEL INBOARD SUPPORT BRACKET ASSEMBLY CRACKED. R&R BRACKET ASSEMBLY IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 69,764 hrs · 56,591 cycles

MAIN CABIN FORWARD F/A LT EMERGENCY FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: LINK ASSY — CORRODED (LT MLG) · airframe 69,764 hrs · 56,591 cycles

LEFT MLG HANGER LINK CORRODED AT BUSHINGS LOCATIONS. R & R SWING LINK IAW AMM.

Part: LINK — CORRODED (RT MLG) · airframe 69,764 hrs · 56,591 cycles

RIGHT MLG HANGER SWING LINK CORRODED AT BUSHINGS LOCATION. R & R SWING LINK IAW AMM.

Part: GLOWSTRIP — DIRTY (CABIN) · airframe 69,764 hrs · 56,591 cycles

MAIN CABIN PHOTOLUMINESCENT EMERGENCY LIGHT DIRTY. CLEANED LIGHT IAW AMM.

Part: SKIN — CRACKED (RT WING) · airframe 69,764 hrs · 56,591 cycles

RIGHT WING NUTPLATE STRIP SKIN FASTENER HOLE CRACKED AT RSS 254. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,764 hrs · 56,591 cycles

LEFT WING NUTPLATE STRIP SKIN FASTENER HOLE CRACKED AT RSS 253. REPAIRED SKIN IAW EA.

Part: LINK ASSY — CORRODED (RT MLG) · airframe 69,764 hrs · 56,591 cycles

RIGHT MLG UPPER FORWARD TRUNNION LINK CORRODED. R & R LINK ASSEMBLY IAW AMM.

Part: SUPPORT FITTING — CORRODED (RT WING) · airframe 69,764 hrs · 56,591 cycles

RT WING NR 8 FLAP TRACK SUPPORT FITTING CORRODED. R & R FITTING IAW DWG & SRM.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 69,764 hrs · 56,591 cycles

LEFT WING NR 5 FLAP TRACK MOUNT FLANGE CORRODED AT MOUNT HOLES. R & R NR 5 FLAP TRACK IAW AMM & EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,764 hrs · 56,591 cycles

RT WING OUTBOARD AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 69,764 hrs · 56,591 cycles

R1 DOOR LOWER SILL WEB CORRODED BETWEEN BS 300 - 340. R & R WEB IAW SRM & DWG.

Part: SPAR — CRACKED (RT WING) · airframe 69,764 hrs · 56,591 cycles

RT WING REAR UPPER SPAR WEB CRACKED INBD AND OTBD OF RSS 224.14. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 69,764 hrs · 56,591 cycles

LEFT WING AFT UPPER SPAR WEB CRACKED INBD OF RSS 224.14. REPAIRED WEB IAW EA.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 69,764 hrs · 56,591 cycles

L1 DOOR LOWER HINGE FITTING CRACKED. REPAIRED FITTING IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,764 hrs · 56,591 cycles

INTERCOSTAL STIFFENER OUTER CHORD CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STR 11R TO STR 12R. R & R CHORD IAW EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 69,764 hrs · 56,591 cycles

L1 DOOR UPPER HINGE CUTOUT BEAR STRAP CRACKED AT BS 303.95, WL 258.88. REPAIRED BEAR STRAP IAW SRM & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,764 hrs · 56,591 cycles

STRINGER CLIP CRACKED AT BS 277, STR 10R. R & R CLIP IAW EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 69,764 hrs · 56,591 cycles

MAIN CABIN FORWARD WET R1 DOOR LOWER SILL CHORD CORRODED BETWEEN BS 294.5 TO BS 360, RBL 54. R & R CHORD IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,764 hrs · 56,591 cycles

FORWARD GALLEY DOOR THRESHOLD SCUFF PLATE ANGLE SUPPORT CORRODED AROUND FASTENER HOLES. R & R ANGLE IAW SRM.

Part: SPAR — CRACKED (RT WING) · airframe 69,764 hrs · 56,591 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT WBL 157, ABOVE MLG SUPPORT FITTING. REPAIRED CHORD IAW EA.

Part: FLAP TRACK — CORRODED (LT WING TE FLAP) · airframe 69,764 hrs · 56,591 cycles

LEFT WING FLAP TRACK NR 1 ATTACHMENT TO WING CORRODED. R & R THE FLAP TRACK IAW AMM.

Part: FLAP TRACK — CORRODED (RT WING TE FLAP) · airframe 69,764 hrs · 56,591 cycles

RIGHT WING OUTBOARD NR 7 FLAP TRACK ATTACHMENT TO THE WING CORRODED. R & R NR 7 FLAP TRACK ASSY IAW AMM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 69,764 hrs · 56,591 cycles

R2 DOOR LOWER SILL WEB CORRODED. R & R WEB IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,764 hrs · 56,591 cycles

FLOORBEAM CORRODED AT BS 986, RBL 35. R & R FLOORBEAM IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,764 hrs · 56,591 cycles

L1 DOOR FRAME CRACKED AT BS 312. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,764 hrs · 56,591 cycles

FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,764 hrs · 56,591 cycles

R1 DOOR FUSELAGE SKIN LOWER AFT CORNER CRACKED. REPAIRED SKIN IAW SRM.

Part: SPAR — CRACKED (RT WING) · airframe 69,764 hrs · 56,591 cycles

RIGHT WING REAR SPAR CRACKED AT RSS 224.14, ON CHORD. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 69,764 hrs · 56,591 cycles

LEFT WING REAR UPPER SPAR CHORD CRACKED AT RSS 224.14. REPAIRED CHORD IAW EA.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 69,764 hrs · 56,590 cycles

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

Part: STRAP — CORRODED (FUSELAGE) · airframe 69,764 hrs · 56,590 cycles

AFT CARGO FLOOR STRAP CORRODED AT BS 794.3, BETWEEN STRINGER 25R - 26R. R & R STRAP IAW DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 69,764 hrs · 56,590 cycles

AFT CARGO INBD INTERCOSTAL THRESHOLD CLIP CORRODED AT BS 794. R & R CLIP IAW DWG.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 69,764 hrs · 56,590 cycles

BRACKET CORRODED AT BS 794.3, STRINGER 25.26R. R & R BRACKET IAW DWG.

Part: SCUFF PLATE — CRACKED (CARGO DOOR) · airframe 69,764 hrs · 56,590 cycles

AFT CARGO DOOR SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SKIN — CORRODED (RT WING) · airframe 69,299 hrs · 56,284 cycles

RIGHT WING UPPER SKIN AT REAR SPAR CORRODED, BETWEEN APPROX WBL 447 - 448. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,299 hrs · 56,284 cycles

RIGHT AFT WING SKIN FASTENER HOLE, AT WING STATION RSS 251 CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CORRODED (RT WING) · airframe 69,299 hrs · 56,284 cycles

RIGHT WING UPPER SKIN AT REAR SPAR AREA CORRODED, BETWEEN APPROX WBL 439 - 444. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,299 hrs · 56,284 cycles

RIGHT WING UPPER SURFACE SKIN CRACKED AT APPROX WBL 174, AT REAR SPAR FASTENER HOLE. REPAIRED SKIN IAW SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 68,923 hrs · 56,038 cycles

NUMBER 5 LE SLAT DELAMINATED. R & R SLAT ASSEMBLY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 68,819 hrs · 55,972 cycles

FORWARD ENTRY EXIT LIGHT LENS LOOSE. INSTALLED LENS IAW MM.

Part: LENS — UNSECURE (CABIN) · airframe 68,819 hrs · 55,972 cycles

FORWARD ENTRY EMER EXIT LIGHT LENS COVER FELL OFF. REINSTALLED COVER AMM.

Part: SIGN — UNSECURE (CABIN) · airframe 68,584 hrs · 55,816 cycles

L1 DOOR EMER EXIT SIGN FELL OFF. SECURED SIGN IAW SIP.

Part: LENS — BROKEN (EXIT SIGN) · airframe 68,096 hrs · 55,472 cycles

FORWARD GALLEY RT SIDE EMER EXIT LIGHT LENS COVER BROKEN. R & R SIGN ASSEMBLY IAW MM.

Part: FLAP TRACK — CRACKED (TE FLAP) · airframe 67,801 hrs · 55,258 cycles

RIGHT WING NR 5 FLAP TRACK CRACKED AT FWD INBD BOLT HOLE. R & R NR 5 FLAP TRACK IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,710 hrs · 54,482 cycles

EXTERNAL FUSELAGE SKIN CRACKED AT FWD RT CORNER OF CONDITIONED AIR DOOR CUT OUT. REPAIRED SKIN IAW ER & EA.

Part: ATTACH ANGLE — CRACKED (RT AILERON) · airframe 66,133 hrs · 54,094 cycles

RIGHT WING AILERON AFT BALANCE BAY OTBD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 65,395 hrs · 53,593 cycles

AIR TURN BACK CABIN ALT WARNING HORN & LIGHT CAME ON AT 29'000. R & R MAIN OUTFLOW VLV IAW AMM.

Part: ACTUATOR — LEAKING (LE SLAT) · airframe 64,219 hrs · 52,726 cycles

RIGHT WING NR 6 SLAT ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,219 hrs · 52,726 cycles

RIGHT EMERGENCY EXIT BULLNOSE LIGHT INOPERATIVE AT ROW 9. R & R BULB IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 64,219 hrs · 52,726 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,219 hrs · 52,726 cycles

LEFT EMER EXIT BULLNOSE LIGHT INOPERATIVE AT ROW 14. R & R BULB IAW MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

WEB CORRODED BETWEEN BS 380 TO BS 400, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: CHANNEL — CRACKED (NLG WW) · airframe 64,219 hrs · 52,726 cycles

RIGHT NLG WW CHANNEL CRACKED. R & R CHANNEL IAW SRM & DWG.

Part: SKIN — CRACKED (KRUEGER FLAP) · airframe 64,219 hrs · 52,726 cycles

RIGHT WING FIXED LE KRUEGER FLAP SKIN CRACKED AT LES 208. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 64,219 hrs · 52,726 cycles

RIGHT WING NR 6 SLAT SKIN CRACKED ON EXTERNAL SKIN FIXED LE LOWER SURFACE. REPAIRED SKIN IAW SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 64,219 hrs · 52,726 cycles

LEFT WING OTBD TE STABILIZER BEAM BRACKET CRACKED AT WBL 114.00. R & R BRACKET IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 64,219 hrs · 52,726 cycles

RIGHT WING TE ANGLE CRACKED AT WS 170. R & R ANGLE IAW SRM & DWG.

Part: DOOR — BROKEN (LT WING) · airframe 64,219 hrs · 52,726 cycles

LEFT WING NR 2 SLAT LE DOOR ASSEMBLY BROKEN. R & R DOOR ASSEMBLY IAW AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 616, LBL 45.5. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 615, LBL 45.5. REPAIRED WEB IAW EA.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

SUPPORT CLIP CRACKED AT BS 348.2, STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

VERTICAL ANGLE CRACKED AT BS 328, RBL 31.6. REPAIRED ANGLE IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 15L. R & R CHANNEL IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

BULKHEAD NOSE WW INTERNAL AREA SUPPORT ANGLE CRACKED AT BS 294.5, STRINGER 23L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

ATTACHMENT CLIP ANGLE CRACKED AT BS 348.2, STRINGER 15L. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 26L. R & R TIE CLIP IAW SRM.

Part: LATCH — CRACKED (L2 DOOR) · airframe 64,219 hrs · 52,726 cycles

L2 DOOR AFT SIDE EMER EXIT HATCH LATCH CRACKED. R & R LATCH IAW CMM.

Part: FITTING — CRACKED (RT SPOILER) · airframe 64,219 hrs · 52,726 cycles

RIGHT WING NR 5 SPOILER OTBD FITTING CRACKED. R & R FITTING IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

SUPPORT CLIP CRACKED AT BS 328+8, BETWEEN STRINGER 20L TO STRINGER 21L. R & R CLIP IAW SRM & DWG.

Part: STIFFENER — CRACKED (RT WING) · airframe 64,219 hrs · 52,726 cycles

RIGHT WING NR 6 AFT FAIRING LOWER AREA STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: STIFFENER — CRACKED (RT WING) · airframe 64,219 hrs · 52,726 cycles

RIGHT WING NR 6 AFT FAIRING INTERNAL AREA INBD STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

RACK E1 EQUIPMENT ELECTRONIC COMPARTMENT SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 64,219 hrs · 52,726 cycles

RIGHT WING NR 6 AFT FAIRING INTERNAL AREA UPPER STRUCTURE ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 64,219 hrs · 52,726 cycles

VERTICAL STABILIZER TE LOWER STRUCTURE OF ACCESS PANEL 9508R PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: BRACKET — CRACKED (RT WING) · airframe 64,219 hrs · 52,726 cycles

RIGHT WING TE BRACKET CRACKED AT STABILIZER BEAM OTBD POSITION WBL 114.00. R & R BRACKET IAW SRM & DWG.

Part: SPAR — CRACKED (LT WING) · airframe 64,219 hrs · 52,726 cycles

LEFT WING FWD SPAR WEB CRACKED AT BS 540, WBL 70.85. R & R WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

ANGLE CRACKED BETWEEN BS 927 TO BS 947.5, BL 0. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

STUB BEAM FRAME CRACKED AT BS 616, STRINGER 17L. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

AFT CARGO COMPARTMENT CLIP ANGLE CRACKED AT BS 807, STRINGER 25R. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

TIE CLIP CRACKED AT BS 947.5, STRINGER 27L. R & R TIE CLIP IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 360, RBL 45.6. R & R STRAP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

FORWARD ENTRY DOOR ANGLE CRACKED BETWEEN BS 294.5 TO BS 303.9, STRINGER 15L. R & R ANGLE IAW DWG & SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 344, RBL 31.6. R & R STRAP IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

VERTICAL STIFFENER CRACKED AT BS 727, STRINGER 27R. R & R STIFFENER IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

FORWARD ENTRY DOOR ANGLE CRACKED AT BS 348.2, STRINGER 15L. R & R ANGLE IAW SRM & DWG.

Part: DRAIN — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

AFT CARGO COMPARTMENT DRAIN CRACKED AT LEVEL OF BS 727E, BL0. R & R DRAIN IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

SHEAR TIE CORRODED AT BS 787, BETWEEN STRINGER 27L TO STRINGER 26L. R & R SHEAR TIE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

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

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 344, BL 0. R & R STRAP IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 344, LBL 45.6. R & R STRAP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

WEB CRACKED BETWEEN BS 312 TO BS 328, RBL 31.6. R & R WEB IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

L1 DOOR CUT OUT FRAME INNER CHORD CRACKED AT BS 348.2, STRINGER 15L. STOP FITTING CTR LINE, FWD ENTRY DOOR CUT OUT. REPAIRED CHORD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

AFT CARGO COMPARTMENT CLIP ANGLE CRACKED AT BS 947.5, STRINGER 25L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

ANGLE CRACKED AT BS 947.5, BETWEEN STRINGER 25R TO STRINGER 24R. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

FRAME CRACKED AT BS 727D, LBL 2. REPAIRED FRAME IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

WEB CRACKED AT BS 927, STRINGER 25L. R & R WEB IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

SHEAR TIE ANGLE CORRODED AT BS 887, STRINGER 25L. R & R SHEAR TIE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

TIE CLIP CRACKED AT BS 747, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

FORWARD CARGO COMPARTMENT FLOOR STRUCTURE SIDE PLATE CHANNEL CRACKED AT BS 500B+18, RBL 21.8. R & R CHANNEL IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

CLIP CRACKED AT BS 380, STRINGER 26R. R & R CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

WEB CRACKED BETWEEN BS 500B TO BS 500C, STRINGER 26R. R & R WEB IAW SRM & DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

KEEL BEAM CORRUGATE PLATE CRACKED NEXT TO BS 727. R & R PLATE IAW SRM & DWG.

Part: ANGLE — CRACKED (NR 1 NACELLE) · airframe 64,219 hrs · 52,726 cycles

NR 1 ENG SUPPORT STRUT ACCESS 5757L ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: STRUCTURE — CRACKED (RT MLG WW) · airframe 64,219 hrs · 52,726 cycles

RIGHT WW LOWER CHORD CRACKED AT BS 679.67 AT LEVEL OF WL 172.18. R & R CHORD IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

FRAME INNER CHORD CRACKED AT BS 616, STRINGER 17L. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 667, LBL 24.5. REPAIRED CHORD IAW EA.

Part: SKIN — CANNING (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

FUSELAGE SKIN OIL CANNING BETWEEN BS 500D TO BS 520, BETWEEN STRINGER 6R TO STRINGER 7R UPPER LOBE. REPAIRED SKIN IAW EA & EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

FUSELAGE SKIN CRACKED AT UPPER CORNER OF WINDOW POST C - D RT SIDE BS 211.8+2, STRINGER 9R. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

FRAME OTBD RT CHORD FWD LOWER FASTENER CRACKED AT BS 727, STRINGER 18R. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,219 hrs · 52,726 cycles

FRAME OTBD LT CHORD LOWER FWD FASTENER HOLE CRACKED AT BS 727, STRINGER 18L. REPAIRED CHORD IAW EA.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 63,931 hrs · 52,531 cycles

FIRE WARNING LIGHT ILLUMINATED & BELL SOUNDED FOR 1 SECOND IN DURATION. NO ASSOCIATED ENG, APU OR CARGO FIRE LIGHTS CAME ON. CLEANED CONNECTOR ON AURAL WARNING SPEAKER IAW SIP. R & R LT & RT RED FIRE WARNING 1864 BULBS IAW MM 33-11-81.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,748 hrs · 52,406 cycles

FORWARD CARGO THRESHOLD WEB CORRODED AROUND FASTENER HOLES. REPAIRED WEB IAW SRM & DWG.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 63,504 hrs · 52,251 cycles

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

Part: RELAY — FAULTY (COCKPIT) · airframe 63,127 hrs · 51,980 cycles

AIR TURN BACK DURING TAKEOFF JUST AFTER THE LG HANDLE WAS SELECTED TO THE UP POSITION, THE "A" SYS ELECT LOW PRESSURE LIGHT ILLUMINATED. R & R RELAY IAW MM.

Part: FITTING — MISSING (CARGO DOOR) · airframe 62,667 hrs · 51,649 cycles

AFT CARGO DOOR FWD, 2ND FROM BOTTOM STOP PIN MISSING LOCK CLIP & OUT OF ADJUSTMENT. INSTALLED LOCK CLIP IAW AMM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 59,998 hrs · 49,680 cycles

LENS COVER ON EXIT SIGN BY THE FORWARD ENTRY DOOR TO THE SIDE OF THE FLIGHT ATTENDANT JUMP SEAT FELL OFF. REMOVED AND REPLACED FWD ENTRY DOOR EXIT SIGN ON THE WALL BASE AND LENS PER M/M, OPS CHECK NORMAL.

Part: LENS — BROKEN (CABIN) · airframe 59,206 hrs · 49,094 cycles

EMERGENCY EXIT LIGHT LENS BROKEN ON FWD LAV. REMOVED & REPLACED LENS PER MM.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 59,204 hrs · 49,093 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FORWARD RETAINING CLIP LOOSE. SECURED CLIP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 58,879 hrs · 48,844 cycles

LEFT WING O/B FORE FLAP DELAMINATED ON I/B TRAILING EDGE. REMOVED AND REPLACED FORE FLAP PER M/M.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,370 hrs · 48,459 cycles

SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L AND STR 27L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,370 hrs · 48,459 cycles

STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,370 hrs · 48,459 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27R AND STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,370 hrs · 48,459 cycles

R1 DOOR AFT SIDE 3RD DOOR STOP FROM BOTTOM FRAME CUTOUT CRACKED. REPAIRED SKIN IAW SRM.

Part: NUT PLATE — MISSING (GIRT BAR FITTING) · airframe 58,370 hrs · 48,459 cycles

R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING MISSING BOTH NUT PLATES. REMOVED AND REPLACED FITTING ASSY IAW DWG & SRM.

Part: CABLE — LOOSE (L1 DOOR) · airframe 58,289 hrs · 48,401 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE CASE LANYARD LOOSE. SECURED CABLE PER AMM.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STRINGER DAMAGED AT BS 456 TO BS 484, STR 2L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STRINGER DAMAGED AT BS 848, STR 2R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 440+10, LOWER AFT CORNER. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STT 9L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK FOUND, FUSELAGE SKIN CRACKED AT BS 847+10, UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK FOUND, FUSELAGE SKIN CRACKED AT BS 827+10, LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK FOUND, FUSELAGE SKIN CRACKED AT BS 460+10, LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK FOUND, FUSELAGE SKIN CRACKED AT BS 380+10, LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK FOUND, FUSELAGE SKIN CRACKED AT BS 460+10, LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK FOUND, FUSELAGE SKIN CRACKED AT BS 887+10, LOWER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE STA 294, STR 4R AND 5R MINOR EDGE DAMAGE. REMOVED AND REPLACED SHEAR TIE PER BAC DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 7R. R&R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,345 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 8R. R&R CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT LWR RT AFT WINDOW, BS 420+10 AT HOLE NR 3. REPAIRED SKIN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,346 hrs · 47,706 cycles

DURING SCHEDULED SPV CHECK, FOUND FOUND FUSELAGE SKIN CRACKED AT RT UPPER FWD WINDOW CORNER BS 520+10 AT HOLE NR 3. REPAIRED CRACK PER DOC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,924 hrs · 47,371 cycles

DURING SCHEDULED M3 CHECK, FOUND SKIN CRACKED AT BS 777, STR 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,490 hrs · 47,035 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 500B+12.5 TO BS 500B+14, STR 1R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,490 hrs · 47,035 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 500B+12.5 TO BS 500B+14, STR 1R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,490 hrs · 47,035 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 500B+10 TO BS 500B+10.5, STR 1R. REPARIED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,488 hrs · 47,034 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500B+10.5, STR 1R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,488 hrs · 47,034 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 500B+12.5 TO BS 500B+14, STR 1R+1.5. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WINDOW SKIN CRACKED AT BS 520+10, LOWER AFT CORNER. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (BS 827 S4R) · airframe 56,102 hrs · 46,710 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 827+12, STR 4R. REPAIRED SKIN PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,562 hrs · 46,318 cycles

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

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 55,501 hrs · 46,263 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,501 hrs · 46,263 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 727E+7, STR 4R. REPAIRED SKIN PER EA.

Part: HOOK — LOOSE (R1 DOOR) · airframe 54,490 hrs · 45,517 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 64,218 hrs · 52,726 cycles

RIGHT HORIZONTAL STABILIZER AFT SPAR LOWER SURFACE SKIN CRACKED AT STATION 125. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF LIMITS (L2 DOOR) · airframe 54,046 hrs · 45,173 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 510B, STR 13L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 777, STR 11R. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 510C, STR 13R. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 797, STR 11R. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 797, STR 13L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 500B TO BS 500C. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 510A, STR 13L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 817, STR 11L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 958, STR 17L. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 492.4, STR 23R. REMOVED AND REPLACED FRAME PER EO.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR AFT BRACKET ASSY CRACKED. REMOVED AND REPLACED BRACKET ASSY PER SRM AND BAC DWG.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CORRODED AT BS 1017, BETWEEN STR 27L TO STR 27R. REPAIRED STIFFENER PER ACO AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 860.5, STR 4R. REPAIRED SKIN PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHANNEL CORRODED BETWEEN BS 807 TO BS 867, LBL 12.50. REMOVED AND REPLACED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHANNEL CORRODED AT BS 732D, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT BS 1016, BETWEEN STR 27L TO STR 27R. REPAIRED WEB PER ACO AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHANNEL CORRODED AT BS 740, RBL 3. REPAIRED CHANNEL PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 787, STR 4R. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 664, LBL 24.5. REPAIRED BEAM PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 856, STR 4R. REPAIRED SKIN PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 813, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHANNEL CORRODED AT BS 787, BETWEEN STR 22L TO STR 25L. REMOVED AND REPLACED CHANNEL PER SRM AND BAC DWG.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO DOOR FRAME CRACKED. REMOVED AND REPLACED FRAME PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 296.5, STR 7R. REPAIRED FRAME PER EO.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHANNEL CORRODED AT BS 859, LBL 3.10. REMOVED AND REPLACED CHANNEL PER EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CORRODED AT BS 1016, BETWEEN STR 27L TO STR 27R. REPAIRED STIFFENER PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 761, STR 4R. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 736A, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 500 TO BS 500A, BETWEEN STR 12R TO STR 14R. REPAIRED SKIN PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 951, STR 17L. REPAIRED FRAME PER EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 25R TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, BETWEEN STR 12L TO STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 53,378 hrs · 44,640 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP CRACKED PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND CLIP CRACKED AT BS 727B, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 927, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 294.5, STR 17L. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,378 hrs · 44,640 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,378 hrs · 44,640 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 380, STR 5L. REMOVED AND REPLACED STRINGER PER SRM.

Part: COVER — LOOSE (R1 DOOR) · airframe 52,924 hrs · 44,295 cycles

R1 DOOR EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,772 hrs · 44,180 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SRM.

Part: SLAT — BROKEN (LT WING) · airframe 52,535 hrs · 43,996 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT O/B TRAILING EDGE CORNER BROKEN. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 52,535 hrs · 43,996 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 52,535 hrs · 43,996 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS DAMAGED BETWEEN ROW 1 TO ROW 17. REMOVED AND REPLACED EEPLS PER MM.

Part: PANEL — DELAMINATED (MIDFLAP) · airframe 52,535 hrs · 43,996 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B MIDFLAP T/E WEDGE PANEL DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.

Part: LIGHT — WORN (CABIN) · airframe 52,535 hrs · 43,996 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS WORN AT ROW 11. REMOVED AND REPLACED EEPLS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,526 hrs · 43,989 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,174 hrs · 43,748 cycles

DURING SCHEDULED MV1 CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN LBL 9 TO LBL 11. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,174 hrs · 43,748 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CROWN CRACKED BETWEEN BS 827 TO BS 847, BETWEEN STR 1R TO STR 2R. REPAIRED SKIN PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,174 hrs · 43,748 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 731E, LBL 9. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,148 hrs · 43,725 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 737D, BL 0. REPAIRED SKIN PER EA.

Part: COVER — BROKEN (CABIN) · airframe 52,148 hrs · 43,725 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,148 hrs · 43,725 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 21. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,148 hrs · 43,725 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,932 hrs · 43,582 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 469 TO BS 470, STR 1. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 51,055 hrs · 42,928 cycles

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

Part: MOUNT BRACKET — BROKEN (EVAC SLIDE) · airframe 51,055 hrs · 42,928 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE MOUNT BRACKETS, FWD AND AFT, BROKEN. REMOVED AND REPLACED BRACKETS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 51,055 hrs · 42,928 cycles

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

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 CUTOUT LOWER CHORD CORRODED AT BS 985. REMOVED AND REPLACED CHORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 45. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (BS 380 S8L) · airframe 48,946 hrs · 41,386 cycles

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

Part: FRAME — CRACKED (BS 520 S8L) · airframe 48,946 hrs · 41,386 cycles

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

Part: STRINGER CLIP — CRACKED (BS 380 S8L) · airframe 48,946 hrs · 41,386 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 48,946 hrs · 41,386 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,946 hrs · 41,386 cycles

DURING SCHEDULED14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 48,399 hrs · 40,988 cycles

DURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 125. REPAIRED PER PAE ER.

Part: SIGN — LOOSE (CABIN) · airframe 46,160 hrs · 39,334 cycles

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

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 46,037 hrs · 39,246 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD MID FLAP T/E WEDGE DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,367 hrs · 37,970 cycles

DURING HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT, BS 291, WL 233. REPAIRED SKIN PER SWA EA.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 42,765 hrs · 36,757 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: FAN — FAULTY (E&E BAY) · airframe 42,726 hrs · 36,728 cycles

DECLARED EMERGENCY. ON DESCENT ACRID ODOR IN COCKPIT AND IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: FRAME — CRACKED (BS 303 S14L) · airframe 42,637 hrs · 36,665 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD ENTRY DOOR CUTOUT FRAME CRACKED AT BS 303.9, STR 14L. REMOVED AND REPLACED FRAME SECTION PER EA.

Part: FRAME — CORRODED (BS 460) · airframe 42,637 hrs · 36,665 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 460, BETWEEN STR 28L AND STR 28R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 440 S17R) · airframe 42,637 hrs · 36,665 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 440, STR 17R. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER — CORRODED (BS 887-947 S28R) · airframe 43,637 hrs · 36,665 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER 28R CORRODED AT BS 887 TO BS 947.5. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FLOOR SUPPORT — CORRODED (BS 727C-727D) · airframe 42,637 hrs · 36,665 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPT FLOORBEAM CORRODED AT BS 727C TO BS 727D, STR 28R. REMOVED AND REPLACED FRAME SECTION PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (BS 767-787 S27L) · airframe 42,637 hrs · 36,665 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPT FLOORBEAM CORRODED AT BS 767 TO BS 787, STR 27L. REMOVED AND REPLACED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 616 S15R) · airframe 42,637 hrs · 36,665 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 15R. REPAIRED FRAME PER BOEING SB.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 41,992 hrs · 36,142 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 41,744 hrs · 35,961 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT, AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME SECTION PER ACO.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 41,650 hrs · 35,888 cycles

R2 DOOR EMERGENCY EVAC SLIDE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: WIRE HARNESS — FAULTY (FIRE DETECTION) · airframe 40,083 hrs · 34,691 cycles

AIR TURNBACK/DECLARED EMERGENCY, APU FIRE WARNING LIGHT ILLUMINATED. APU FIRE BOTTLE DISCHARGED. INSPECTED APU COMPARTMENT, EXHAUST & TAIL SECTION-NO EVIDENCE OF FIRE. R&R APU FIRE DETECTION WIRE HARNESS AT FIRE LOOP PER WDM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,982 hrs · 34,617 cycles

DURING SCHEDULED C1 CHECK, FWD CABIN EMERGENCY EXIT BATTERY PACK FAILED DISCHARGE TEST. R&R BATTERY PACK PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 39,976 hrs · 34,610 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,429 hrs · 34,182 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 10 ABC. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 39,010 hrs · 33,853 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: ANGLE — CRACKED (AFT CARGO DOOR) · airframe 39,010 hrs · 33,853 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR CRACKED AT LOWER AFT CORNER ANGLE WEB SUPPORT. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 39,010 hrs · 33,853 cycles

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

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 39,010 hrs · 33,853 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT OTBD UPPER CORNER. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 38,425 hrs · 33,362 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 36,672 hrs · 31,894 cycles

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

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 36,405 hrs · 31,704 cycles

DURING SCHEDULED C1 CHECK, FOUND DELAMINATION ON RT WING T/E OUTBOARD AFT FLAP. REMOVED AND REPLACED RT WING T/E OUTBOARD AFT FLAP PER MM.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 35,162 hrs · 30,721 cycles

FWD RIGHT EMERGENCY EXIT AND BOTH OVERWING EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 35,159 hrs · 30,717 cycles

LEFT OVERWING EMERGENCY EXIT LIGHTS INTERMITTENT WITHOUT BEING SWITCHED ON. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: TERMINAL — LOOSE (EMERGENCY LIGHT) · airframe 35,120 hrs · 30,687 cycles

DURING SCHEDULED A1 CHECK, EMERGENCY EXIT LIGHTS WILL NOT TURN OFF WITH ARMED SWITCH IN OFF POSITION. SECURED GROUND TERMINAL AT AFT F/A PANEL PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT BS 994, RBL 47, CORRODED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS AT BS 328 AND BS 344, RBL 10 TO RBL 59, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 188 STRINGER 15R, BS 188 STRINGER 16L, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT BS 987 RBL 43, CORRODED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM.

Part: BRACKET — CRACKED (CABIN) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND ALL FOUR OVERWING EMERGENCY EXIT LIGHT BATTERY POWER SUPPLY MOUNTING BRACKETS, CRACKED. REMOVED AND REPLACED ALL FOUR MOUNTING BRACKETS PER MM.

Part: GIRT BAR — CORRODED (L1 DOOR SLIDE) · airframe 34,254 hrs · 29,984 cycles

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

Part: CLEVIS — CORRODED (HORIZONTAL STAB) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND LT AND RT HORIZONTAL STAB CENTER SECTION CLEVIS, FWD AND AFT LUGS, CORRODED. REPAIRED HORIZONTAL STAB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT BS 348, LBL 50, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: CLEVIS — CORRODED (VERTICAL STAB) · airframe 34,284 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR CLEVIS, FWD AND AFT LUG, CORRODED. REPAIRED VERTICAL STAB PER ER.

Part: WEB — CRACKED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT LT AND RT BS 188 TO BS 496, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER BAC DRAWING AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 26L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 375, RBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947, LBL 53, CRACKED. REMOVED AND REPLACED FLOORBEAM SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D CHECK, FOUND FRAME BS 787, BETWEEN STRINGER 8R AND STRINGER 8L, CRACKED. REMOVED AND REPLACED SECTION PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND BULKHEAD STIFFENER AT BS 291.5, RT WL 240 TO RT WL 253, CRACKED. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS AT BS 663, STRINGER 10R AND STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,254 hrs · 29,984 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 440, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FAN BLADE — DAMAGED (ENGINE) · airframe 33,071 hrs · 29,010 cycles

DECLARED EMERGENCY/AIR TURN BACK, INFLIGHT ENGINE SHUTDOWN. PASSING APPROX 8000 FEET, HEARD A POP AND FELT SLIGHT VIBRATION. ALL INSTRUMENTS SHOWED NORMAL. CLIMB SEEMED A LITTLE LOW FOR POWER SETTING. ISOLATED VIBRATION TO NR 2 ENGINE. REMOVED AND REPLACED NR 1 AND NR 2 FAN BLADE SETS PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,633 hrs · 28,632 cycles

DURING SCHEDULED C1 CHECK, FOUND BS 378.5 FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUTOUT. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 31,316 hrs · 27,572 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 31,316 hrs · 27,572 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: HOOK — LOOSE (ESCAPED SLIDE) · airframe 30,773 hrs · 27,118 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD RETAINER HOOK LOOSE. SECURED FWD RETAINER HOOK PER MM.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 29,655 hrs · 26,220 cycles

L1 DOOR ESCAPE SLIDE PRESSURE IS LOW. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE PER MM.

Part: SLIDE — TORN (AFT SVC DOOR) · airframe 28,975 hrs · 25,671 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FLAP TORN. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 28,794 hrs · 25,521 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 28,063 hrs · 24,903 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 27,928 hrs · 24,775 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 27,689 hrs · 24,576 cycles

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

Part: TAB — WORN (ELEVATOR) · airframe 27,467 hrs · 24,394 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB CRANK ASSY PER MM.

Part: TAB — WORN (LT ELEVATOR) · airframe 27,467 hrs · 24,394 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 26,301 hrs · 23,459 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE IN FWD CABIN. SECURED EEPLS PER MM.

Part: WEB — CRACKED (FWD SVC DOOR) · airframe 25,845 hrs · 23,111 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT WEB BEAM CRACKED AT LOWER FITTING. REMOVED AND REPLACED WEB PER SRM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 25,845 hrs · 23,111 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 25,845 hrs · 23,111 cycles

DURING SCHEDULED 1/4D CHECK, FOUND TIE CLIP CRACKED AT BS 727B, STR 26R. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 24,559 hrs · 21,979 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS # 3, # 4, # 11 & # 24. R&R EEPLS COVERS PER MM.

Part: COVER — BROKEN (CABIN FLOOR) · airframe 24,475 hrs · 21,901 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP & COVER BROKEN AT ROW 7. R&R EEPLS COVER AND RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,323 hrs · 21,769 cycles

EEPLS INOP AT OVERWING EXIT. RELAMPED EEPLS LIGHT PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 23,345 hrs · 20,952 cycles

EEPLS WIRES EXPOSED AND NUMEROUS TRACK COVERS MISSING. SECURED WIRING AND INSTALLED TRACK COVERS PER MM.

Part: COVER — MISSING (CABIN) · airframe 23,326 hrs · 20,935 cycles

TWO EEPLS TRACK COVERS MISSING. INSTALLED TRACK COVERS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 22,958 hrs · 20,643 cycles

EEPLS LOOSE FROM OVERWING EXIT TO ROW 16. SECURED EEPLS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 22,347 hrs · 20,160 cycles

EEPLS BULB BROKEN UNDER TRACK COVER AT EMERGENCY EXIT ROW. R&R BULB PER MM.

Part: WIRE — INOPERATIVE (ROW 11) · airframe 22,124 hrs · 19,985 cycles

EEPLS INOP AT ROW 11. RE-CONNECTED LOOSE WIRES PER MM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 22,039 hrs · 19,912 cycles

EEPLS COVER MISSING AT EMERGENCY EXIT. INSTALLED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 21,901 hrs · 19,796 cycles

EEPLS HAS EXPOSED WIRE. RESEATED EEPLS TRACK COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 21,540 hrs · 19,460 cycles

EEPLS LOOSE AT MID CABIN. SECURED LIGHT ASSY PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,430 hrs · 19,364 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED LBL 5, WL 201. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,430 hrs · 19,364 cycles

DURING SCHEDULED SPECIAL VISIT FOUND BS 178 BULKHEAD CRACKED, RBL 5, WL 201. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 21,430 hrs · 19,364 cycles

EEPLS WIRING LOOSE AT OVERWING EXIT. SECURED WIRES PER MM.

Part: COVER — MISSING (ROW 14) · airframe 20,728 hrs · 18,771 cycles

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

Part: SLIDE — DISLODGED (SERVIC DOOR) · airframe 20,536 hrs · 18,614 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 20,156 hrs · 18,280 cycles

EEPLS TRACK COVER LOOSE AT ROW 12. SECURED AND RELAMPED TRACK SECTION PER MM.

Part: SKIN — DELAMINATED (TE FLAP)

DURING SCHEDULED C2 CHECK, FOUND LEFT WING OUTBOARD AFT FLAP LOWER SURFACE DELAMINATED ON INBOARD SIDE. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: RELEASE RING — DAMAGED (EVAC SLIDE)

DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE RELEASE RING MISSING SOLDER. SOLDERED RING PER MM.

Part: SLIDES — SAGGING (DOORS)

DURING SCHEDULED A1 CHECK, FOUND FWD SERVICE AND BOTH AFT DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASSY'S PER MM.

Part: LENS — MISSING (EMER EXIT)

EEPLS MISSING LENS AT OVERWING EXIT. INSTALLED LENS PER MM.

Part: SENSOR — OUT OF ADJUST (RT MLG)

AFTER TAKEOFF MLG WOULD NOT RETRACT, HANDLE WOULD NOT GO PAST OFF POSITION. ADJUSTED GROUND SHIFT CABLE AND AIR SAFETY SENSOR PER MM.

Part: WIRE — BROKEN (PASSENGER DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT SIGN INOP. REPAIRED BROKEN WIRE AND REMOVED AND REPLACED CONTACT.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM, BS 986, LBL 31-RBL 31. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM, BS 947, LBL 5. REPAIRED FLOORBEAM PER SRM.

Part: STRAP — OUT OF POSITION (SERVICE DOOR)

AFTER TAKEOFF LOUD BANGING NOISE HEARD BY CABIN CREW IN FWD SERVICE DOOR AREA. NOISE GOT LOUDER WITH INCREASED AIRSPEED. AIRCRAFT RETURNED TO PDX AND FOUND FWD SERVICE DOOR STRAP OUTSIDE A/C THROUGH HINGE. FOUND SIX INCHES OF SAFETY STRAP PROTRUDING FROM LOWER HINGE. NO DAMAGE NOTED AND SEAL OK. STOWED STRAP.

Part: BULB — MISSING (CABIN)

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR VERTICAL EMERGENCY EXIT SIGN MISSING TWO BULBS. INSTALLED TWO BULBS IN FWD ENTRY DOOR VERTICAL EMERGENCY EXIT SIGN PER BOEING MM, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHTS INTERMITTENT FROM ROW 2 AND FWD. REMOVED AND REPLACED FWD LIGHT ASSY PER BOEING MM AND RECONNECTED LOOSE SOCKET AT ROW 2.

Part: LAMP — FAILED (CABIN)

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE FWD ENTRY INOP. RELAMPED PER BOEING.