N652SW

Part: HOOK — OUT OF ADJUST (R1 DOOR) · airframe 59,632 hrs · 46,625 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED HOOK IAW AMM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 59,564 hrs · 46,584 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOWER RETAINING FLAP LOOSE. SECURED SLIDE ASSEMBLY IAW SIP.

Part: MOUNT — CRACKED (R2 DOOR) · airframe 59,435 hrs · 46,499 cycles

R2 DOOR FWD SLIDE MOUNT CRACKED. R & R MOUNT IAW SRM.

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 59,417 hrs · 46,488 cycles

LEFT WING NR 4 SPOILER DELAMINATED ON TOP SURFACE. R & R NR 4 SPOILER IAW AMM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 59,417 hrs · 46,488 cycles

M1675 EMER EXIT LIGHT BATTERY PACK FAULTY AT BS 318, LBL 3. R & R BATTERY BACK IAW AMM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 59,417 hrs · 46,488 cycles

M1673 EMER EXIT LIGHT BATTERY PACK FAULTY AT BS 973, LBL 7. R & R BATTERY PACK IAW AMM.

Part: SKIN — CRACKED (LT WING) · airframe 59,417 hrs · 46,488 cycles

LEFT WING TE SKIN CRACKED, AT FASTENER HOLE AT RSS 239. REPAIRED SKIN IAW SRM & EA.

Part: SPLICE PLATE — CRACKED (LT WING) · airframe 59,417 hrs · 46,488 cycles

LEFT WING REAR SPAR UPPER TE SPLICE PLATE CRACKED AT RSS 202. R & R SPLICE PLATE IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 59,417 hrs · 46,488 cycles

RIGHT WING UPPER SKIN FASTENER HOLE CRACKED AT RSS 249. R & R SKIN IAW EA & SRM.

Part: SKIN — CRACKED (LT WING) · airframe 59,417 hrs · 46,488 cycles

LEFT WING UPPER SKIN MOST AFT FASTENER HOLES CRACKED, BETWEEN RSS 235 - 267. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 59,417 hrs · 46,488 cycles

RIGHT WING UPPER SKIN CRACKED AT RSS 237, AFT FASTENER ROW. REPAIRED SKIN IAW EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 59,417 hrs · 46,488 cycles

RIGHT WING TUBING SUPPORT ANGLE AFT WEB CRACKED AT STATION 196. R & R WEB IAW DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,417 hrs · 46,488 cycles

RIGHT STOW BIN BULLNOSE EMER EXIT LIGHT INOPERATIVE AT ROW 16. R & R LIGHT IAW AMM.

Part: SPAR — CRACKED (RT WING) · airframe 59,417 hrs · 46,488 cycles

RIGHT WING AFT SPAR, UPPER CHORD CRACKED AT RSS 221, NR 5 FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 59,417 hrs · 46,488 cycles

LEFT WING AFT SPAR UPPER CHORD CRACKED AT RSS 221, NR 5 FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 59,234 hrs · 46,376 cycles

LEFT WING NR 2 LE SLAT UPPER SKIN DELAMINATED. R & R SLAT ASSEMBLY IAW MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 58,861 hrs · 46,137 cycles

FORWARD GALLEY FLASHLIGHT STRAP BROKEN. R & R STRAP IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 58,615 hrs · 45,972 cycles

FORWARD ENTRY EXIT LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 58,422 hrs · 45,846 cycles

RIGHT WING NR 6 SLAT DELAMINATED. R & R NR 6 SLAT IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,187 hrs · 45,687 cycles

EMERGENCY LIGHT INOPERATIVE AT M1673. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,187 hrs · 45,687 cycles

EMERGENCY LIGHT INOPERATIVE AT M1670. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,187 hrs · 45,687 cycles

EMERGENCY LIGHT INOPERATIVE AT M1668. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,187 hrs · 45,687 cycles

EMERGENCY LIGHT INOPERATIVE AT M1674. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,187 hrs · 45,687 cycles

EMERGENCY LIGHT INOPERATIVE AT M1672. R & R BATTERY PACK IAW AMM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

FORWARD LOWER CORNER OF AFT GALLEY DOOR STUB FRAME CRACKED AT BS 960, STRINGER 17R. REPAIRED STUB FRAME IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 887, BETWEEN STRINGER 27L - 27R. REPAIRED FRAME IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

INNER CHORD CRACKED AT BS 348.2, STRINGER 17L. REPAIRED CHORD IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

FUSELAGE INTERCOSTAL CRACKED AT STATION 277 TO 292, STRINGER 14R. REPAIRED INTERCOSTAL IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

WEB CRACKED BETWEEN BS 277 - 291.5, STRINGER 14R. R & R WEB IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 16L. R & R CHANNEL IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

ANGLE CRACKED BETWEEN BS 277 TO 291.5, BETWEEN STRINGER 13R TO 14R. REPLACED ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,207 hrs · 44,988 cycles

RIGHT WING NR 5 SLAT, LE SLAT SKIN CRACKED AT 37" INBD SIDE. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

ANGLE CRACKED BETWEEN BS 277 TO 291.5, BETWEEN STRINGER 10R TO 11R. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 57,207 hrs · 44,988 cycles

RIGHT WING OTBD TE STRUCTURE ANGLE CRACKED, WBL 203. R & R ANGLE IAW SRM & DWG.

Part: STRUCTURE — CORRODED (LT HORIZ STAB) · airframe 57,207 hrs · 44,988 cycles

LEFT HORIZONTAL STABILIZER CTR SECTION CHORD CORRODED ON FRONT SPAR UPPER AFT CLEVIS AFT FACE. REPAIRED CHORD IAW SRM & EA.

Part: STRAP — CRACKED (TE FLAP) · airframe 57,207 hrs · 44,988 cycles

RIGHT WING NR 6 FIXED FLAP TRACK FAIRING STRAP CRACKED AT WBL 191.00. R & R STRAP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

FRAME CRACKED AT BS 520, BETWEEN STRINGER 20R TO 21R, AT 7 O CLOCK POSITION. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

FRAME CRACKED AT BS 520 BETWEEN STRINGER 20R TO 21R, AT 5 O'CLOCK POSITION. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 57,207 hrs · 44,988 cycles

RIGHT WING OTBD TE STRUCTURE ANGLE CRACKED AT WS 537.806. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 57,207 hrs · 44,988 cycles

RIGHT WING INBD TE PULLEY SUPPORT BRACKET CRACKED AT RSS 230. R & R BRACKET IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 57,207 hrs · 44,988 cycles

RIGHT WING INBD TE STRUCTURE ANGLE CRACKED AT WBL 71.24. R & R ANGLE IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

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

Part: WEB — CRACKED (NLG) · airframe 57,207 hrs · 44,988 cycles

RIGHT NLG WW WEB CRACKED AT BS 243.7+3.5, WL 169.1. REPAIRED WEB IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

R2 DOOR CUT OUT SKIN CRACKED AT FWD LOWER CORNER BETWEEN BS 947.5 TO 967+6.5, BETWEEN STRINGER 15R TO 19R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 57,207 hrs · 44,988 cycles

LEFT WING INBD FIXED LE SKIN CRACKED AT BS 213. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

MAIN WW ANGLE CRACKED AT BS 727, LBL 15.5. R & R ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT OBS 670, LBL 24.5. REPAIRED CHORD IAW SRM & EA.

Part: SKIN — CRACKED (RT WING) · airframe 57,207 hrs · 44,988 cycles

RIGHT WING EXTERNAL SKIN OF INBD FIXED LE CRACKED AT STATION 208. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 20L TO 21L. REPAIRED FRAME IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 57,207 hrs · 44,988 cycles

LEFT MAIN WW FAIRING SUPPORT STRUCTURE CHORD CRACKED AT BS 680. R & R CHORD IAW SRM & DWG.

Part: STRUCTURE — CORRODED (LT HORIZ STAB) · airframe 57,207 hrs · 44,988 cycles

LEFT HORIZONTAL STABILIZER CTR SECTION CHORD CORRODED ON FRONT TOP UPPER FWD CLEVIS FWD FACE. REPAIRED CHORD IAW SRM & EA.

Part: GIRT BAR — UNSECURE (L1 DOOR) · airframe 56,579 hrs · 44,528 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR FELL OUT INADVERTENTLY, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED SLIDE IAW MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,346 hrs · 44,373 cycles

RIGHT EMER LIGHT INOPERATIVE BETWEEN ROW 20 - 24. R & R BATTERY PACK IAW AMM.

Part: LATCH — FAULTY (COCKPIT) · airframe 56,267 hrs · 44,316 cycles

RIGHT EMER ESCAPE ROPE DOOR LATCH FAULTY. R & R LATCH IAW SIP.

Part: LATCH — OUT OF ADJUST (COCKPIT) · airframe 56,267 hrs · 44,316 cycles

FIRST OFFICER EMER ESCAPE ROPE DOOR LATCH OUT OF ADJUSTMENT. ADJUSTED LATCH IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 55,816 hrs · 44,022 cycles

L1 DOOR EMER EXIT SIGN LENS COVER CRACKED. R & R COVER IAW AMM.

Part: SIGN — UNSECURE (CABIN) · airframe 55,553 hrs · 43,846 cycles

RIGHT OVERWING EXIT ROW SIGN FELL OFF. SECURED SIGN IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,118 hrs · 43,558 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: PAN — CRACKED (LT NACELLE) · airframe 54,578 hrs · 43,155 cycles

LEFT AFT ENG MOUNT HEAT SHIELD PAN ASSEMBLY CRACKED FWD OTBD CORNER. REPAIR PAN ASSEMBLY IAW EA.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 54,301 hrs · 42,944 cycles

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

Part: LENS — MISSING (CABIN) · airframe 54,279 hrs · 42,930 cycles

RIGHT CABIN OVERHEAD BIN BULLNOSE EMER EXIT LIGHT LENS MISSING AT ROW 9. INSTALLED LENS IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,279 hrs · 42,930 cycles

LEFT WING NR 1 SLAT SKIN CRACKED AT LOWER SURFACE AFT FASTENER ROW AT INBD AUXILIARY TRACK. REPAIRED SKIN IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 54,245 hrs · 42,904 cycles

RIGHT WING INBD AFT FLAP ASSEMBLY DELAMINATED. R & R AFT FLAP ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,490 hrs · 42,358 cycles

L1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

TIE STRAP CRACKED AT BS 350, STRINGER 16L. R & R TIE STRAP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

FRAME CRACKED AT BS 348.2, STRINGER 15L. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

SKIN CRACKED AT BS 500D, STRINGER 14R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

SKIN CRACKED AT BS 500C + 16, STRINGER 14R. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

SHEAR TIE CRACKED AT BS 380, BETWEEN STRINGER 14L TO STRINGER 15L. R & R SHEAR TIE IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

STRINGER CRACKED AT BS 829, STRINGER 11L. REPAIRED STRINGER IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

STRINGER CRACKED AT BS 744, STRINGER 9R. REPAIRED STRINGER IAW EA.

Part: FORGING — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 747+10 WINDOW FORGING CRACKED. R & R FORGING IAW DWG.

Part: FORGING — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 767+10 WINDOW FORGING CRACKED. R & R FORGING IAW DWG.

Part: SKIN — CRACKED (BS 847) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 847+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 887+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

RIGHT BS 787+10 LOWER FWD WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: FORGING — CRACKED (BS 847) · airframe 53,490 hrs · 42,358 cycles

RIGHT BS 847+10 UPPER AFT WINDOW CORNER FORGING CRACKED. REPAIRED FORGING IAW TC.

Part: SKIN — CRACKED (BS 767) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 767+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

RIGHT BS 767+10 LOWER FWD WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: SKIN — CRACKED (BS 807) · airframe 53,490 hrs · 42,358 cycles

RIGHT BS 807+10 UPPER AFT WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: SKIN — CRACKED (BS 827) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 827+10 UPPER AFT WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (BS 727A) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 727A+10 LOWER FWD WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (BS 767) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 767+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (BS 727E) · airframe 53,490 hrs · 42,358 cycles

RIGHT BS 727E+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

RIGHT BS 887+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 807+10 UPPER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 887+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SRM.

Part: FORGING — CRACKED (BS 847) · airframe 53,490 hrs · 42,358 cycles

RIGHT BS 847+10 LOWER FWD WINDOW CORNER FORGING CRACKED. REPAIRED FORGING IAW TC.

Part: SKIN — CRACKED (BS 747) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 747+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (BS 787) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 787+10 LOWER FWD WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (BS 827) · airframe 53,490 hrs · 42,358 cycles

RIGHT BS 827+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

RIGHT BS 727+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW.

Part: SKIN — CRACKED (BS 727) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 727+10 LOWER FWD WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (BS 727D) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 727D+10 UPPER AFT WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

RIGHT BS 727+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (BS 787) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 787+10 UPPER AFT WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (BS 807) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 807+10 LOWER FWD WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (BS 727E) · airframe 53,490 hrs · 42,358 cycles

LEFT BS 727E+10 LOWER FWD WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

RIGHT BS 807+10 LOWER FWD WINDOW CORNER CUT OUT CRACKED. REPAIRED CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

RIGHT BS 727B+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: PROXIMITY SENSOR — FAULTY (RT MLG) · airframe 53,325 hrs · 42,242 cycles

RT MLG UNSAFE LIGHT ON APPROACH FOR LANDING, CYCLED LANDING TWICE, GOT 3 GREEN LIGHTS, LANDED NORMAL. R & R LANDING GREEN LOGIC CARD M982 & PROXIMITY SENSOR S73 IAW MM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 53,101 hrs · 42,095 cycles

GASPER FAN CB POPPED ELECTRIC SMELL IN COCKPIT. R & R GASPER FAN IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,595 hrs · 41,734 cycles

FUSELAGE SKIN CRACKED AT BS 500B+13, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: COVER — CRACKED (EMERGENCY EXIT) · airframe 52,040 hrs · 41,329 cycles

COVER ON HANDLE ON EMERGENCY EXIT WINDOW ON CAPTAIN'S SIDE CRACKED. R&R COVER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,807 hrs · 41,150 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R&R BULB IAW SIP.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 51,788 hrs · 41,137 cycles

RT OVERWING HATCH EMERGENCY EXIT LIGHT INOPERATIVE. R&R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,580 hrs · 40,965 cycles

AFT ENTRY DOOR EMERGENCY EXIT LIGHT BULBS INOPERATIVE. R&R BULBS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 51,580 hrs · 40,964 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. R&R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 51,580 hrs · 40,964 cycles

LT EMERGENCY EGRESS LIGHT LENS CRACKED AT BS 727C+10, BETWEEN STR 22L AND STR 23L. REMOVED AND REPLACED LIGHT PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FLOOR BEAM TENSION STRAP CRACKED AT BS 328, BL0. R&R STRAP IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,580 hrs · 40,964 cycles

LT WING NR 3 SLAT LOWER SKIN CRACKED AT OB AUX TRACK. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,580 hrs · 40,964 cycles

LT WING NR 4 SLAT LOWER SKIN CRACKED AT OB AUX TRACK. REPAIRED SKIN IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

SIDEWALL SUPPORT STRAP CRACKED AT BS 947 STRINGER 16R. R&R STRAP IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FRAME FAIL SAFE ANGLE CORRODED AT BS 767, BETWEEN STRINGER 25L - 25R. R&R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

SKIN CRACKED AT BS 727A+7, STR 10R. REPAIRED SKIN IAW EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

AUX CHORD CORRODED AT BS 727. R&R CHORD PER SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER CORRODED AT BS 992, STR 21R. R&R STRINGER IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

TRANSVERSE FLOOR BEAM CRACKED AT BS 727B, LBL 24.82. REPAIRED BEAM IAW ER & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FLOOR BEAM UPPER CHORD CRACKED AT BS 652, BBL 0.07. REPAIRED CHORD IAW ER & EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

BULKHEAD LOWER ATTACH ANGLE CORRODED AT BS 947, STR 23R. R & R ANGLE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

RT FLOOR WEB CRACKED BETWEEN BS 178 TO BS 188, WL 208. R&R WEB IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

INTERCOSTAL CORRODED BETWEEN BS 986 TO BS 1006, STR 21R. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD AFT END CRACKED AT BS 727A+18.5, LBL 26. R&R CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD AFT END CRACKED AT BS 727A+17, RBL 47. REPAIRED CHORD IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

SKIN CUTOUT CRACKED AT BS 973, STRINGER 23R. REPAIRED SKIN IAW SRM.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

LONGITUDINAL FLOOR STUB BEAM ATTACH BRACKET CRACKED AT BS 638, RBL 45. R & R BRACKET IAW SRM & DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

CREASE BEAM WEB CRACKED AT BS 638, LBL 65. R&R WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 51,580 hrs · 40,964 cycles

MLG BAY UPPER PRESSURE DECK CRACKED AT BS 672, LBL 31. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

SEAT TRACK CORRODED BETWEEN BS 344 TO BS 480, LBL 25. R&R SEAT TRACK PER SRM.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STUB BEAM ATTACH BRACKET CRACKED AT BS 638, LBL 45. R&R BRACKET IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 727D TO BS 727E, STR 17L. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 460 TO BS 480, STR 17R. R&R WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER CLIP CRACKED AT BS 907, STRINGER 8L. R&R CLIP IAW SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

R1 DOOR CUTOUT SILL WEB CORRODED BETWEEN BS 986 - BS 993, RBL 50. R&R SILL WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER CLIP CRACKED AT BS 727A, STR 4L. R & R CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 767 - 787, STRINGER 17L. R& R WEB IAW SRM & DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER SPLICE CRACKED AT BS 907, STR 4L. R & R SPLICE IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 727B - BS 727C, STRINGER 17L. R&R WEB IAW SRM & DRAWING.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 460 TO BS 480, STR 17R. R&R WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER CLIP CRACKED AT BS 578, STR 11L. R & R CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 727C TO BS 727D, STR 17L. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 727A TO BS 727B, STR 17L. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FWD GALLEY DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED CUTOUT IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER CLIP CRACKED AT BS 616, STR 5R. R & R CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 847 TO BS 867, STR 17L. R & R WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R&R CLIP IAW SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

R2 DOOR CUT OUT SILL WEB CORRODED BETWEEN BS 947 TO BS 986, RBL 50. R&R WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER CLIP CRACKED AT BS 639, STR 4R. R & R CLIP IAW DWG AND SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 887 TO BS 907, STR 17L. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 360 TO 380, STR 17R. REPAIRED WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER CLIP CRACKED AT BS 380, STR 8L. R & R CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 747 TO 767, STR 17L. R&R WEB PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 51,580 hrs · 40,964 cycles

RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED 36-INCH I/B OF O/B END. REPAIRED FORE FLAP IAW ATS J/N 46300.

Part: SUPPORT ANGLE — CRACKED (RT AILERON) · airframe 51,580 hrs · 40,964 cycles

RT WING AILERON I/B CENTER HINGE FITTING I/B SUPPORT ANGLE CRACKED. R&R ANGLE IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FWD OF R1 DOOR CUTOUT INTERCOSTAL OUTBOARD ATTACH ANGLE CRACKED AT BS 291, WL 240. R&R ANGLE IAW SRM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FWD SERVICE DOOR UPPER AFT DOOR STOP BACK PLATE ON AFT SIDE OF DOOR FRAME CRACKED AT STA 332.1, STR 8R. R & R CLIP IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 328, LBL 34. REPAIRED CHORD IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FLOOR BEAM TENSION STRAP CRACKED AT BS 328, LBL 11. R&R STRAP IAW SRM & DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FLOORBEAM CORRODED AT BS 326, RBL 56. REPAIRED BEAM IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FWD ENTRY DOOR THRESHOLD SUPPORT Z CHANNEL CORRODED AT BS 332, LBL 63. R&R ZEE CHORD IAW SRM & DRAWING. .

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 51,580 hrs · 40,964 cycles

LT WING I/B SIDE, UPPER AFT T/E PANEL SUPPORT ANGLE CRACKED. R&R ANGLE IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FRAME CORRODED AT BS 993, BETWEEN STRINGER 16R - STRINGER 17R. REPAIRED FRAME IAW ER & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FLOORBEAM CRACKED AT BS 312, RBL 21. REPAIRED BEAM IAW SRM.

Part: SUPPORT BRACKET — CORRODED (L1 DOOR) · airframe 51,580 hrs · 40,964 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR ATTACH SUPPORT BRACKET CORRODED. REMOVED & REPLACED BRACKET PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FWD SERVICE DOOR CUTOUT UPPER FWD CORNER CRACKED AT STUB FRAME BS 296.5, STR 7R. REPAIRED STUB FRAME IAW ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FLOOR BEAM UPPER FLANGE CORRODED AT BS 986.5, BETWEEN LBL 40 - RBL 45. REPAIRED FLOOR BEAM IAW ER & EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 51,580 hrs · 40,964 cycles

RT WING UPPER T/E SUPPORT ANGLE CRACKED. R&R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 51,580 hrs · 40,964 cycles

RT WING RSS545 WIPER WEB SUPPORT ANGLE CRACKED. R&R ANGLE IAW SRM.

Part: FASTENER — LOOSE (R1 DOOR) · airframe 51,580 hrs · 40,964 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER FWD GIRT BAR HOLDER LOOSE. R & R FASTENERS IAW SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

SHEAR WEB CORRODED BETWEEN A BS 1008 - BS 1016, BETWEEN LBL 38 - LBL 41. R&R SHEAR WEB IAW DRAWING & SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 51,580 hrs · 40,964 cycles

LEFT WING RSS545 WIPER WEB ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SUPPORT BRACKET — CORRODED (L1 DOOR) · airframe 51,580 hrs · 40,964 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR ATTACH SUPPORT BRACKET CORRODED. R&R BRACKET IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER CLIP CRACKED AT BS 727A, STR 21R. R&R CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER CLIP CORRODED AT BS 927, STR 20R. R & R CLIP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

AFT CARGO BAY WEB CRACKED BETWEEN BS 789 - BS 792, BETWEEN STRINGER 24R TO STRINGER 25R. R&R WEB IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN LBL 9 - LBL 11. R&R SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

AFT CARGO BAY STRINGER CLIP CRACKED AT BS 787, STR 20R. R & R CLIP IAW SRM.

Part: BUTT JOINT — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

AFT CARGO BAY BUTT JOINT CORRODED AT BS 908, BETWEEN STRINGER 26R - 27R. REPAIRED BUTT JOINT IAW ER & SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER CLIP CRACKED AT BS 947.5, STRINGER 19L. R&R CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FRAME SHEAR TIE CORRODED AT BS 727D, BETWEEN STRINGER 26R - STRINGER 27R. R&R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

SHEAR TIE CORRODED AT BS 500C, BETWEEN LBL 2 TO LBL 4. REPAIRED SHEAR TIE PER ER AND SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

SHEAR TIE CORRODED AT BS 1006, RBL 2. R&R SHEAR TIE IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

SHEAR TIE CORRODED AT BS 1006, BETWEEN STRINGER 23L - STRINGER 24L. R&R SHEAR TIE IAW SRM & DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

AFT CARGO BAY SIDEWALL SUPPORT ANGLE CRACKED AT BS 887, STRINGER 25L. R&R CHANNEL IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

AFT CARGO BAY, ON SUB-THRESHOLD WEB CORRODED BETWEEN BS 794 - BS 847, BETWEEN RBL 20 - RBL 28. R&R WEB IAW SRM & DRAWING.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

OUTFLOW VALVE DOUBLER CORRODED AT BS 982, BETWEEN STRINGER 24R - STRINGER 25R R&R DOUBLER IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER CLIP CORRODED AT BS 867, STRINGER 27R. R&R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

AFT CARGO BAY STRINGER CLIP CRACKED AT BS 792, STR 26R. REMOVED AND REPLACED CLIP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

AFT CARGO BAY WATER TANK SUPPORT ANGLE FOR INTERCOSTAL CRACKED AT BS 947.5, BETWEEN STRINGER 24 - 25R. R&R ANGLE IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

STRINGER CLIP CORRODED AT BS 907, STRINGER 25R. R&R CLIP IAW SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

AFT CARGO BAY FAIL SAFE ANGLE CORRODED AT BS 947.5, BETWEEN STRINGER 25R - 26R. R&R FAIL SAFE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

AFT CARGO BAY BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, BETWEEN STRINGER 21L TO STRINGER 25L. R&R ANGLE IAW SRM.

Part: FASTENER — LOOSE (L1 DOOR) · airframe 51,580 hrs · 40,964 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR RETAINER LOOSE. R & R FASTENER IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

CHORD CRACKED AT BS 727, STRINGER 18A LT. REPAIRED CHORD IAW SWA EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,580 hrs · 40,964 cycles

FWD CARGO DOOR CUTOUT SUB THRESHOLD WEB CORRODED BETWEEN BS 447 TO 479, RBL 30. R & R WEB IAW SRM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 51,580 hrs · 40,964 cycles

L1 DOOR EXTERNAL SKIN CRACKED AT AFT UPPER CORNER AT FASTENER LOCATION. REPAIRED SKIN IAW SRM.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 50,841 hrs · 40,435 cycles

FORWARD SERVICE DOOR AFT LOWER FRAME CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: DOWNLOCK SENSOR — FAULTY (RT MLG) · airframe 50,790 hrs · 40,402 cycles

RIGHT MAIN GEAR INDICATOR STAYED RED WITH NO GREEN DURING GEAR EXTENSION. GEAR WARNING HORN SOUNDED WITH FLAPS 15. NO CHANGE WITH MANUAL EXTENTION, GEAR APPEARED DOWN THROUGH MAIN GEAR VIEWER. AFTER LANDING RIGHT MAIN RED LIGHT EXTINGUISHED AND GREEN LIGHT ILLUMINATED. REMOVED AND REPLACED RIGHT MLG DOWNLOCK SENSOR PER MT.

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 50,589 hrs · 40,265 cycles

F/O SIDE OVERWING EMERGENCY EXIT DOOR HANDLE LOOSE. SECURED HANDLE & OPS CHECKED OK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,579 hrs · 40,258 cycles

FUSELAGE SKIN SHOWS SUB-SURFACE CRACK INDICATION AT STA 500A + 13, 2 INCHES LONG JUST ABOVE STR 10L. REPAIRED IAW EA 1-353-21592.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,579 hrs · 40,258 cycles

A 2 INCH SUB-SURFACE CRACK INDICATION BS 500C + 8 S10L MOD. REPAIRED IAW EA 1-353-21591.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 50,284 hrs · 40,033 cycles

FORWARD ENTRY SLIDE FELL OUT OF CARRIER-NO SLIDE DEPLOYMENT. RE-INSTALLED L-1 DOOR SLIDE PER MAINT TASK MT325-61-06, A/C OK FOR SERVICE.

Part: SENSOR — FAULTY (NLG) · airframe 49,950 hrs · 39,787 cycles

DURING CRUISE, RED & GREEN NOSE GEAR LIGHTS ILLUMINATED WITH THE NOSE GEAR IN THE UP POSITION. ACCOMPLISHED QRH PROCEDURE AND WHEN GEAR LEVER WAS PLACED IN THE DOWN POSITION, ALL GEAR INDICATED DOWN & LOCKED WITH ALL RED LIGHTS EXTINGUISHED. FOUND SENSOR BAD. REMOVED AND REPLACED SENSOR PER MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 49,177 hrs · 39,205 cycles

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

Part: SIGN — UNSECURE (CABIN) · airframe 49,142 hrs · 39,179 cycles

LEFT OVERWING EMERGENCY EXIT SIGN FELL OFF. REPAIRED SIGN PER EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 48,509 hrs · 38,683 cycles

L2 WINDOW ARCED DURING CRUISE. REMOVED AND REPLACED WINDOW PER M/M.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 48,178 hrs · 38,430 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 48,172 hrs · 38,425 cycles

L1 COCKPIT WINDOW ARCED ON TAKEOFF RETURNED TO DEPARTURE. REMOVED AND REPLACED WINDOW PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 47,961 hrs · 38,276 cycles

RT FLOOR EMERGENCY EXIT LIGHTING STRIP LOOSE BETWEEN ROW 5 TO ROW 7. SECURED LIGHTSTRIP PER M/M.

Part: COVER — LOOSE (CABIN) · airframe 47,799 hrs · 38,166 cycles

EMERGENCY EXIT LIGHT BULLNOSE COVER AT ROW 8 LOOSE. SECURED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 47,782 hrs · 38,151 cycles

RT EMERGENCY EXIT BULL NOSE LIGHT COVER MISSING AT ROW 8. INSTALLED COVER IAW MM.

Part: COVER — MISSING (CABIN) · airframe 47,645 hrs · 38,044 cycles

EMERGENCY EXIT LIGHT COVER ON OVERHEAD BIN AT 8R MISSING. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,439 hrs · 37,903 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 378 TO BS 379.75, BL 0. REPAIRED SKIN IAW AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,437 hrs · 37,902 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED BETWEEN BS 378 TO BS 379.75, BL 0. REPAIRED SKIN IAW SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 47,437 hrs · 37,902 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 2 SLAT DELAMINATED AT O/B END. REPAIRED SLAT PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 47,437 hrs · 37,902 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,421 hrs · 37,892 cycles

DURING SCHEDULED MV3 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: PRIORITY VALVE — FAULTY (LT MLG) · airframe 47,171 hrs · 37,701 cycles

ON APPROACH LT MLG WOULD NOT SHOW DOWN AND LOCKED. CYCLED GEAR, LOCKED DOWN LANDED NORMAL. REMOVED AND REPLACED MLG PRIORITY MODULAR VALVE IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,983 hrs · 37,567 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 46,607 hrs · 37,271 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT SIGN LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 46,607 hrs · 37,271 cycles

DURING SCHEDULED CV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: WIRE — LOOSE (COCKPIT) · airframe 46,290 hrs · 37,036 cycles

L1 COCKPIT WINDOW ARCED AT UPPER LT CORNER. SECURED WIRE PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 46,268 hrs · 37,013 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED ON LOWER T/E. REMOVED AND REPLACED AFT FLAP PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,268 hrs · 37,013 cycles

DURING SCHEDULED 14Y CHECK, FOUND MAIN CABIN VERTICAL WEB CRACKED BETWEEN BS 708 TO BS 713, LBL 24.8, WEL 203. REPAIRED WEB PER EA.

Part: STRUCTURE — CHAFED (LE SLAT) · airframe 46,268 hrs · 37,013 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 3 SLAT CAN CHAFED. REPAIRED SLAT CAN PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 46,268 hrs · 37,013 cycles

DURING SCHEDULED 44Y CHECK, FOUND HORIZONTAL WEB CORRODED BETWEEN BS 333 TO BS 343, BETWEEN RBL 59 TO RBL 65. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: ANGLE — CORRODED (R2 DOOR) · airframe 46,268 hrs · 37,013 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR Z-ANGLE CORRODED ON UPPER SURFACE. REPAIRED Z-ANGLE PER EA.

Part: LENS — LOOSE (EXIT SIGN) · airframe 46,268 hrs · 37,013 cycles

DURING SCHEDULED 14Y CHECK FOUND, AFT GALLEY EMERGENCY EXIT SIGN LIGHT LENS LOOSE. REMOVED AND REPLACED LENS ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,268 hrs · 37,013 cycles

DURING SCHEDULED 14Y CHECK, FOUND THREE SMALL CRACKS ON FS STA 867, STR 8R. REPAIRED PER EA.

Part: CSD — FAULTY (NR 1 ENGINE) · airframe 45,905 hrs · 36,730 cycles

AIR TURNBACK, NR 1 CSD LOW OIL PRESSURE LIGHT ILLUMINATED. COMPLETED QRH CHECKLIST, APU WOULD NOT ACCEPT NR 1 GEN. REMOVED AND REPLACED CSD AND OIL COOLER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,857 hrs · 36,693 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND AFT CARGO DOOR UPPER AFT CORNER CUTOUT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 45,837 hrs · 36,676 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,220 hrs · 35,518 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 365, STR 5L. REPAIRED SKIN PER EA.

Part: RIB — CRACKED (RT WING) · airframe 44,048 hrs · 35,391 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING RIB CRACKED AT REAR SPAR STA 545. REMOVED AND REPLACED RIB PER SRM.

Part: STIFFENER — CRACKED (RT WING) · airframe 44,048 hrs · 35,391 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING VERTICAL STIFFENER CRACKED AT REAR SPAR STA 545. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 43,833 hrs · 35,227 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING O/B TRAILING EDGE AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,180 hrs · 34,730 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 512D, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,490 hrs · 42,358 cycles

FUSELAGE SKIN CRACKED AT STATION 500D+12, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 41,818 hrs · 33,724 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LENS — CRACKED (CABIN) · airframe 41,480 hrs · 33,468 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: POSITION SWITCH — FAULTY (COCKPIT) · airframe 41,243 hrs · 33,290 cycles

ON APPROACH LANDING GEAR EXTENDED WITH 3 GREEN AND 3 RED LIGHTS. MOVED HANDLE AND RECYCLED GEAR. SAME INDICATIONS, ON THE THIRD EXTENSION ALL INDICATED NORMAL. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER POSITION SWITCH PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 40,803 hrs · 32,966 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 40,803 hrs · 32,966 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT EEPLS LOOSE AT ROW 23. SECURED EEPLS PER MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 40,763 hrs · 32,933 cycles

FWD GALLEY FLASHLIGHT STRAP BROKEN. REMOVED AND REPLACED STRAP PER MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 40,567 hrs · 32,792 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED SIGN PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 767 LBL 8. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, LBL 11. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727, LBL 11. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR UPPER HINGE FITTING CRACKED BS 304.6, WL 258.13. REMOVED AND REPLACED FITTING PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, RBL 11. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 440, RBL 27. REMOVED AND REPLACED FRAME PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,468 hrs · 32,712 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN RBL 18 TO RBL 3. REMOVED AND REPLACED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,468 hrs · 32,718 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — CRACKED (L1 DOOR) · airframe 40,209 hrs · 32,528 cycles

DURING SCHEDULED SPV, FOUND L1 DOOR EMERGENCY LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 40,096 hrs · 32,444 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR MOUNTING BRACKET LOOSE. SECURED BRACKET PER MM.

Part: STRIP — WORN (CABIN) · airframe 39,348 hrs · 31,919 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP WORN AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: STRIP — WORN (CABIN) · airframe 39,348 hrs · 31,919 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP WORN BETWEEN ROW 20 TO ROW 21. REMOVED AND REPLACED EEPLS PER MM.

Part: GASPER FAN — FAULTY (CABIN) · airframe 39,294 hrs · 31,879 cycles

AIR TURNBACK, BURNING SMELL REPORTED IN THE CABIN JUST AFTER TAKEOFF. RETURNED TO THE GATE. ISOLATED SMELL COMING FROM GASPER VENTS. REMOVED AND REPLACED GASPER FAN PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,827 hrs · 31,545 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17, WL 230. REPAIRED WEB PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,996 hrs · 27,980 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT UPPER INBOARD CORNER. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT FWD LOWER END. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 18L. REPAIRED FRAME PER SB.

Part: FRAME — CRACKED (BS 400 S8L) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 380 S8L) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8L) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8R) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727D S8R) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8R) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 867 S8R) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 360 S8R) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: HOOK — LOOSE (R1 DOOR GIRTBAR) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: FRAME — CRACKED (BS 867 S8L) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8L) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727D S8L) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 827 S8R) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (BS 312) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CRACKED AT BS 312. BL 0. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A S16L) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (BS 956-982) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 956 AND BS 982, RBL 70. REPAIRED CREASE BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S25L) · airframe 33,996 hrs · 27,986 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,709 hrs · 27,756 cycles

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

Part: LENS — CRACKED (EMERGENCY LIGHTS) · airframe 32,101 hrs · 26,486 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 32,051 hrs · 26,454 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 31,526 hrs · 26,061 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 31,347 hrs · 25,932 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 31,201 hrs · 25,817 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,905 hrs · 25,572 cycles

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

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 30,852 hrs · 25,531 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 30,417 hrs · 25,200 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS BROKEN AT L1 DOOR. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 28,429 hrs · 23,684 cycles

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

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 27,818 hrs · 23,196 cycles

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

Part: FITTING — CORRODED (LT WING) · airframe 25,885 hrs · 21,623 cycles

DURING SCHEDULED SERVICE CHECK, FOUND CORROSION ON LT MLG STABILIZER FITTING. REMOVED AND REPLACED LT MLG STAB FITTING PER MM.

Part: CABLE — MISROUTED (AFT DOOR SLIDE) · airframe 25,059 hrs · 20,986 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT DOOR EVACUATION SLIDE RELEASE CABLES MISROUTED. REROUTED CABLES PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 25,003 hrs · 20,949 cycles

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

Part: HOOK — LOOSE (R1 DOOR GIRT BAR) · airframe 24,690 hrs · 20,704 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE FWD GIRT BAR HOOK LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE FWD GIRT BAR HOOK PER MM.

Part: HOOK — MISSING (R2 DOOR SLIDE) · airframe 24,492 hrs · 20,548 cycles

R2 DOOR EVAC SLIDE HOOK ATTACH SCREW, MISSING. REMOVED AND REPLACED ATTACH SCREW PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,699 hrs · 19,882 cycles

DURING SPV, FOUND BULKHEAD LOWER LT SIDE FRAME AT BS 178, CRACKED. REMOVED AND REPLACED SIDE FRAME PER ACO.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 23,658 hrs · 19,855 cycles

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

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 23,658 hrs · 19,855 cycles

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

Part: SLIDE — OUT OF ADJUST (L2/R2 DOORS) · airframe 22,893 hrs · 19,239 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH R2 AND L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 21,228 hrs · 17,932 cycles

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

Part: BOTTLE — LOW (ESCAPE SLIDE) · airframe 21,041 hrs · 17,771 cycles

DURING PREFLIGHT INSP, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: HINGE — WORN (RT ELEVATOR TAB) · airframe 20,894 hrs · 17,657 cycles

DURING SCHEDULED C3 CHECK, (SI 11138-55), RT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB ASSY PER MM.

Part: HINGE — WORN (LT ELEVATOR TAB) · airframe 20,894 hrs · 17,657 cycles

DURING SCHEDULED C3 CHECK, (SI 11138-55), LT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED NR 1 LT ELEVATOR TAB ATTACH HINGE BUSHING/HARDWARE PER MM.

Part: CABLE — MISROUTED (AFT SVC DOOR) · airframe 19,050 hrs · 16,203 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 19,050 hrs · 16,203 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SEAL — LEAKING (NR 1 ENGINE) · airframe 18,249 hrs · 15,567 cycles

IN-FLIGHT SHUTDOWN, DECLARED EMERGENCY, NR 1 ENGINE LOW OIL PRESS LIGHT ILLUMINATED, OIL QUANITY ZERO. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. REMOVED AND REPLACED SEAL ON OIL SCAVENGE LINE ON TRANSFER GEAR BOX PER MM.

Part: TRUNNION — SHEARED (RT MLG) · airframe 18,213 hrs · 15,537 cycles

DECLARED EMERGENCY, UPON GEAR EXTENSION HEARD LOUD BANG AND ASSOCIATED VIBRATION. FOUND RT MLG RETRACT TRUNNION SHEARED. REMOVED AND REPLACED RT MLG PER MM.

Part: BRACKET — LOOSE (FWD ENTRY DOOR) · airframe 18,205 hrs · 15,531 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED GIRT BAR BRACKET PER MM.

Part: SLIDE — LOOSE (FWD SVC DOOR) · airframe 17,506 hrs · 14,983 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 17,030 hrs · 14,570 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 727 PLUS 5, LBL 12. REPAIRED FLOORBEAM PER SWA RA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,030 hrs · 14,570 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 927, STR 26R. REPAIRED FRAME PER SRM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 16,326 hrs · 13,981 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: CABLE — OUT OF POSITION (ENTRY DOOR) · airframe 15,255 hrs · 13,136 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE RELEASE CABLE OUT OF POSITION. REPOSITIONED CABLE PER MM.

Part: HINGE — LOOSE (LT & RT ELEVATOR) · airframe 14,365 hrs · 12,400 cycles

DURING SCHEDULED C4 CHECK, FOUND LT & RT ELEVATORS OUTBOARD HINGES LOOSE. REMOVED AND REPLACED ELEVATOR HINGE PLATE ASSY'S PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 13,490 hrs · 11,636 cycles

EEPLS LOOSE AT ROW 12. SECURED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 13,267 hrs · 11,449 cycles

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

Part: WIRE — EXPOSED (CABIN) · airframe 12,605 hrs · 10,895 cycles

EEPLS WIRING EXPOSED. INSTALLED EEPLS TRACK COVER PER MM.

Part: WIRE — CHAFED (RT WING) · airframe 12,554 hrs · 10,852 cycles

DECLARED EMERGENCY. DURING CRUISE NOTICED SPLIT FLAP INDICATION. ACFT HANDLED NORMALLY. FOLLOWED QRH - NORMAL LANDING. REPAIRED SHORTED WIRE BETWEEN CONNECTORS D4867P & D229 PER BAC WDM.

Part: LENS — MISSING (CABIN) · airframe 12,453 hrs · 10,766 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS RED LENS MISSING AT AFT SECTION. INSTALLED LENS PER MM.

Part: SLIDE — DISCHARGED (SERVICE DOOR) · airframe 9,462 hrs · 8,251 cycles

DURING SCHEDULED A1 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — LOW PRESSURE (PASSENGER DOOR)

LEFT AFT ENTRY DOOR EMERGENCY EVACUATION SLIDE, BOTTLE PRESSURE LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LANDING GEAR — DEER STRIKE (RIGHT)

JUST AFTER MAIN GEAR TOUCH DOWN ON RWY 33L, AIRCRAFT STRUCK A DEER WITH RIGHT MAIN GEAR. ANIMAL PARTS FOUND ON RIGHT MAIN GEAR STRUT. ALSO, RIGHT MAIN GEAR BRAKE WAS LOST. INSPECTED RT MLG AREA, FOUND GROUND SHIFT CABLE, SHIMMY DAMPER, ANTISKID HARNESS AND BOTH BRAKE LINES DAMAGED. REMOVED AND REPLACED GROUND SHIFT CABLE, NR 3 TIRE AND BRAKE, NR 4 TIRE AND BRAKE, RT MLG SHIMMY DAMPER, BOTH BRAKE LINES AND ANTISKID HARNESS PER BOEING MM.

Part: GROUND STUD — LOOSE (CARGO DOOR)

AIR TURNBACK DUE TO FWD CARGO DOOR LIGHT CAME ON AFTER TAKEOFF. AIRCRAFT MADE AN UNEVENTFUL LANDING. FOUND DOOR SWITCH GROUND STUD LOOSE, MOVED GROUND TERMINAL FROM GROUND STUD NR GD00200A TO NR GD01008D. OPS CHECK GOOD AS PER BOEING MM. (LP 185388)

Part: BEARING — FAILED (NR 1 ENGINE)

INFLIGHT SHUTDOWN OF NR 1 ENGINE ON CLIMBOUT AT 19K AFTER COMPRESSOR STALL WITH ASSOCIATED OIL QTY AND PRESSURE LOSS. SUSPECT NR 3 BEARING FAILURE. AIRCRAFT RETURN TO PVD AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED ENGINE AND PERFORMED POWER ASSURANCE RUN PER BOEING MM.