N616SW

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 66,471 hrs · 52,720 cycles

LEFT EMERGENCY EXIT UPPER PANEL SIGN LOOSE AT FORWARD END. R & R THE SIGN IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,153 hrs · 52,514 cycles

AFT WING TO BODY EMERGENCY LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: PRIORITY VALVE — FAULTY (MLG WW) · airframe 65,803 hrs · 52,285 cycles

AFTER TAKEOFF WHEN LANDING GEAR LEVER PLACED IN UP POSITION ALL LIGHTS WENT OUT. WHEN HANDLE PLACED IN OFF POSITION, BOTH RED AND GREEN LIGHTS ILLUMINATED AND ACFT WAS SLOW TO CLIMB WITH NOTICEABLE YAW TO THE RT. WHEN HANDLE PLACED IN UP IAW QRH, LIGHTS WENT OUT AND YAW WENT AWAY. R & R MLG PRIORITY MODULAR VALVE IAW AMM.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 65,733 hrs · 52,238 cycles

CENTER CEILING EXIT LIGHT LOOSE. SECURED SIGN IAW MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 65,107 hrs · 51,826 cycles

L1 DOOR EXIT SIGN COVER LOOSE. SECURED COVER IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 65,041 hrs · 51,784 cycles

L1 DOOR EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 64,816 hrs · 51,644 cycles

LEFT WING NR 1 SLAT, LOWER SKIN CRACKED, AT TWO EACH FASTENERS AT INBD AUXILIARY TRACK AREA. REPAIRED SKIN IAW SRM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 64,816 hrs · 51,644 cycles

ENTRY DOOR EXTERIOR EMER LIGHT INOPERATIVE. R & R POWER SUPPLY IAW MM.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 64,800 hrs · 51,632 cycles

NOSE LANDING GEAR WW AFT BULKHEAD CRACKED AT RT LOWER CORNER. REPAIRED BULKHEAD IAW EA.

Part: CAP — LEAKING (LT WING) · airframe 64,688 hrs · 51,558 cycles

FUEL LEAKED ON TOP OF LT WING. R & R LT CAP IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 64,520 hrs · 51,458 cycles

FORWARD ENTRY EMER EXIT FLOOR LIGHT PLASTIC COVER LOOSE. SECURED COVER IAW SIP.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 64,482 hrs · 51,433 cycles

EMERGENCY LIGHT BETWEEN ROW 21 & 22 INOPERATIVE. R & R BATTERY CHARGER IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 64,302 hrs · 51,306 cycles

L1 EXIT DOOR BULKHEAD EXIT LIGHT LENS LOOSE. SECURED LENS IAW SIP.

Part: LENS — LOOSE (CABIN) · airframe 63,963 hrs · 51,071 cycles

LEFT CTR WING EXIT LIGHT LENS LOOSE. SECURED LENS IAW AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 63,685 hrs · 50,867 cycles

LEFT FWD EXIT SIGN COVER MISSING. INSTALLED SIGN IAW SIP.

Part: SKIN — CRACKED (L1 DOOR) · airframe 63,179 hrs · 50,502 cycles

L1 DOOR INNER SKIN CRACKED AT UPPER FWD CORNER. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,920 hrs · 50,306 cycles

L2 DOOR EMER EXIT LIGHT AT COMMON TO AFT LAV FWD WALL BULB INOPERATIVE. R & R BULB IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

STRINGER CLIP CRACKED AT BS 908, STRINGER 21R. R & R CLIP IAW SRM.

Part: CARRIAGE — CORRODED (LT WING) · airframe 62,920 hrs · 50,306 cycles

LEFT WING NR 2 CARRIAGE A FRAME ATTACH POINT BOLT HOLE CORRODED. R & R CARRIAGE IAW SRM.

Part: FITTING — CRACKED (RT WING) · airframe 62,920 hrs · 50,306 cycles

RIGHT WING REAR SPAR FITTING CHORD CRACKED AT INBD END. REPAIRED CHORD IAW SI.

Part: LINK — CORRODED (RT MLG) · airframe 62,920 hrs · 50,306 cycles

RIGHT MLG BEAM SUPPORT SWING LINK CORRODED. R & R LINK IAW AMM & SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,920 hrs · 50,306 cycles

RIGHT WING OTBD AFT FLAP UPPER & LOWER SURFACE DELAMINATED. R & R AFT FLAP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

STRINGER CLIP CRACKED AT BS 807, STRINGER 26R. R & R CLIP IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

FUSELAGE INTERCOSTAL CRACKED AT STATION 292 - 303, STRINGER 16L. REPAIRED INTERCOSTAL IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.0. REPAIRED WEB IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

THESHOLD WEB CORRODED AT STATION 950 - 980, STRINGER 17L. REPAIRED WEB IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

FLOORBEAM STABILIZING STRAP CRACKED AT BS 328, LBL 11. REPAIRED STRAP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

FLOORBEAM CORRODED AT BS 986.5, RBL 5. REPAIRED FLOORBEAM IAW EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

FORWARD ENTRY DOOR THRESHOLD SUPPORT ANGLE CORRODED ON UPPER SURFACE BETWEEN BS 320 TO 335, LBL 60. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

FUSELAGE SKIN CRACKED AT AFT END OF EQUIPMENT COOLING EXHAUST. REPAIRED SKIN IAW ER & EA.

Part: WEB — CRACKED (NLG WW) · airframe 62,920 hrs · 50,306 cycles

RIGHT NLG WW WEB CRACKED AT STATION 258.5, RBL 11. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 62,920 hrs · 50,306 cycles

LEFT NOSE WW WEB CRACKED VERTICALLY AT BONDED DOUBLER EDGE AT BS 258.5. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

LEFT CREASE BEAM WEB CORRODED ON UPPER SURFACE BETWEEN BS 500A TO 500B. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

RIGHT CREASE BEAM WEB CORRODED ON UPPER & LOWER SURFACES BETWEEN BS 460 TO 480, BETWEEN RBL 65 TO 70. R & R WEB IAW SRM.

Part: WIRE — BROKEN (EXIT SIGN) · airframe 62,920 hrs · 50,306 cycles

AFT BULLNOSE LIGHTED EXIT SIGN WIRE BROKEN. R & R SIGN IAW AMM.

Part: STRAP — LOOSE (EMERGENCY EXIT) · airframe 62,920 hrs · 50,306 cycles

RIGHT EMER EXIT HATCH STRAP HOOK STOW POUCH VELCRO LOOSE. R & R STRAP IAW SOPM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

AFT CARGO BAY ON STRINGER END SPLICE UPPER FLANGE CORRODED AT BS 851.5, STRINGER 23R. R & R SPLICE IAW SRM & DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

STRINGER SPLICE CORRODED AT STATION 907, STRINGER 23L. R & R SPLICE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 662, RBL 27.8. REPAIRED BEAM IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

FUSELAGE FRAME CORRODED AT STATION 807, STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

AFT CARGO BAY ON STRINGER END SPLICE UPPER FLANGE CORRODED AT BS 851.5, STRINGER 24R. R & R SPLICE IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 62,920 hrs · 50,306 cycles

RIGHT WING AILERON COVE WEB ATTACH ANGLE CRACKED AT RSS 545. R & R ANGLE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

FUSELAGE FRAME CORRODED AT STATION 807, STRINGER 26R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

FUSELAGE FRAME CORRODED AT STATION 607, BETWEEN STRINGER 27L & 26R. REPAIRED FRAME IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

STRINGER SPLICE CORRODED AT STATION 907, STRINGER 21R. R & R SPLICE IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 62,920 hrs · 50,306 cycles

MAIN WW PRESS DECK CRACKED AT BS 664, RBL 17. REPAIRED DECK IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,920 hrs · 50,306 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT MLG AFT SUPPORT FITTING. REPAIRED CHORD IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

SHEAR TIE CORRODED AT BS 500D, LBL 5. R & R SHEAR TIE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

SHEAR TIE CORRODED AT BS 500D, RBL 7. REPAIRED SHEAR TIE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

FRAME SHEAR TIE CORRODED AT BS 500C, LBL 9. R & R FRAME IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD VERTICAL FLANGE CRACKED BETWEEN BS 666 TO 670, LBL 24.5, AT OVAL HOLE UPPER AFT CORNER. REPAIRED BEAM IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,920 hrs · 50,306 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED AT THE MLG AFT SUPPORT FITTING. REPAIRED CHORD IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 62,920 hrs · 50,306 cycles

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

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 62,920 hrs · 50,306 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED ALONG REAR SPAR BETWEEN STAB STATION 157 TO 166. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 62,831 hrs · 50,242 cycles

L1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 62,590 hrs · 50,090 cycles

RIGHT OVERWING EXIT ROW LIGHT LENS LOOSE. R & R LENS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 62,560 hrs · 50,069 cycles

FORWARD ENTRY EXIT LIGHT LENS LOOSE. R & R LENS IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 62,144 hrs · 49,798 cycles

L1 DOOR EMER EXIT LIGHT COVER LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,900 hrs · 49,627 cycles

LEFT EMER EXIT LIGHT INOPERATIVE AT ROW 22. REPAIRED LIGHT IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,794 hrs · 49,562 cycles

BULLNOSE EMER LIGHT AT SEAT ROW 22 ABC INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 61,390 hrs · 49,291 cycles

R1 DOOR FWD FRAME CRACKED AT LOWER RADIUS OF UPPER BINGE CUT OUT. R & R DOOR IAW AMM.

Part: LENS — UNSECURE (CABIN) · airframe 61,322 hrs · 49,241 cycles

FORWARD EMER EXIT LIGHT LENS FELL OFF. REINSTALLED LENS IAW MM.

Part: REGULATOR — FAULTY (BLEED AIR SYS) · airframe 61,284 hrs · 49,213 cycles

AIR TURN BACK CABIN PRESS ALTITUDE WARNING HORN SOUNDED & PRESSURIZATION NEVER RECOVERED. R & R NR 1 ENG PNEU BLEED HIGH STAGE REGULATOR IAW MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 60,858 hrs · 48,896 cycles

R1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 60,542 hrs · 48,678 cycles

FORWARD EMER EXIT LIGHT LENS COVER LOOSE. SECURED COVER ASSEMBLY IAW SIP.

Part: COVER — LOOSE (CABIN) · airframe 60,410 hrs · 48,592 cycles

L1 DOOR EMER EXIT LIGHT COVER LOOSE. R & R COVER IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 59,334 hrs · 47,838 cycles

L1 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: COVER — BROKEN (CABIN) · airframe 58,572 hrs · 47,350 cycles

RT OVERWING EMERGENCY EXIT LIGHT COVER BROKEN. REPAIRED COVER IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,832 hrs · 46,834 cycles

FWD LT SECTION OF EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,311 hrs · 46,433 cycles

R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R&R LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,306 hrs · 46,432 cycles

L1 DOOR EVAC SLIDE LIGHT INOPERATIVE. R&R LAMP IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 57,306 hrs · 46,432 cycles

G4 GALLEY EMERGENCY EXIT LIGHT LENS FRONT FACE BROKEN. R&R LIGHT ASSEMBLY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

FWD RT WINDOW BELT SKIN CRACKED AT STATION 380, STRINGER 14R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

LT BS 727A+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 2. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

LT BS 787+10 LOWER FORWARD SKIN CUTOUT CRACKED AT HOLES 1,3,9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

LT BS 767+10 UPPER AFT SKIN CUTOUT CRACKED AT HOLES 2,3,6. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

LT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

LT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,6. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

LT BS 807+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1,3,9. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

LT BS 827+10 UPPER AFT SKIN CUTOUT CRACKED AT HOLES 2,3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

LT BS 767+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3,4. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

LT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3,5,7. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

LT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3,6. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

LT BS 827+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,5,10. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

RT BS 887+10 UPPER AFT WINDOW CORNER SKIN CUTOUT CRACKED AT HOLES 1,2,3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

RT BS 847+10 UPPER AFT SKIN CUTOUT CRACKED AT HOLES 2,3,6. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

RT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,11. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

RT BS 867+10 LOWER FORWARD SKIN CUTOUT CRACKED AT HOLES 2,3,11. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

RT BS 787+10 UPPER AFT SKIN CUTOUT CRACKED AT HOLES 1,2,4. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

RT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,4,5,6,10. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

RH BS 847+10 LOWER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED AT HOLES 1,2,4,6,8. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

RT BS 827+10 UPPER AFT SKIN CUTOUT CRACKED AT HOLES 2,3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

RT BS 727+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1,5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 46,432 cycles

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

Part: FRAME — CRACKED (BS 328) · airframe 57,162 hrs · 46,330 cycles

FRAME WEB CRACKED AT STA 328, BETWEEN S20-21R. R & R WEB IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,162 hrs · 46,330 cycles

INTERCOSTAL CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED CLIP IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,162 hrs · 46,330 cycles

INTERCOSTAL CRACKED BETWEEN STA 927 TO 947, BL 0. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 57,162 hrs · 46,330 cycles

LEFT WING INBD MIDFLAP BOTH INBD FOREFLAP TRACK SEGMENTS LOOSE. SECURED TRACK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,162 hrs · 46,330 cycles

FRAME WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,162 hrs · 46,330 cycles

FRAME OTBD CHORD FORWARD FLANGE'S LOWER FORWARD HOLE CRACKED STA 727, STR 18L. R & R CHORD IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,162 hrs · 46,330 cycles

INTERCOSTAL CRACKED BETWEEN STA 927 TO 947.5, BL 0. REMOVED AND REPLACED ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (BS 664) · airframe 57,162 hrs · 46,330 cycles

PASSENGER CABIN, PRESSURE DECK CRACKED AT STA. 664, BETWEEN BL0 TO LBL 24.5. REPAIRED WEB IAW EA.

Part: TAIL CONE — CRACKED (FLAP TRACK) · airframe 57,162 hrs · 46,330 cycles

NR 3 FLAP TRACK AFT FAIRING TAIL CONE TIP CRACKED. REMOVED AND REPLACED TAIL CONE IAW SOPM.

Part: FRAME — CRACKED (BS 727) · airframe 57,162 hrs · 46,330 cycles

RIGHT FRAME OTBD CHORD CRACKED AT STA 727. R & R CHORD IAW EA.

Part: FRAME — CRACKED (BS 727) · airframe 57,162 hrs · 46,330 cycles

LEFT FRAME OTBD CHORD CRACKED AT STA 727. R & R CHORD IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,162 hrs · 46,330 cycles

CENTER WING BOX LBL 42" APPROX AT STA 597 WEB CRACKED. REPAIRED WEB IAW EA.

Part: DOOR FRAME — CRACKED (FWD CARGO DOOR) · airframe 57,162 hrs · 46,330 cycles

FWD CARGO DOOR, AFT LOWER FRAME CHAFED AND CRACKED. R & R DOOR IAW AMM & SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 57,162 hrs · 46,330 cycles

LEFT WING T/E PANEL INBD OF NR 5 SPOILER OUTBOARD ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 57,162 hrs · 46,330 cycles

AFT CARGO DOOR CUTOUT AFT LOWER RETAINER CRACKED. REMOVED AND REPLACED RETAINER IAW SRM AND DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,162 hrs · 46,330 cycles

LEFT WING OUTBOARD MAIN FLAP OUTBOARD TRAILING EDGE CORNER DELAMINATED. REPAIRED MAIN FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,960 hrs · 46,189 cycles

FUSELAGE SKIN CRACKED AT BS 807+9, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,960 hrs · 46,189 cycles

FUSELAGE SKIN CRACKED AT BS 787+6, STR 4R. REPAIRED SKIN PER EA.

Part: LENS — MISSING (CABIN) · airframe 55,490 hrs · 45,133 cycles

FORWARD EMERGENCY EXIT SIGN MISSING. INSTALLED LENS PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,461 hrs · 45,108 cycles

FUSELAGE SKIN CRACKED AT BS 767+8, STR 4R. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 54,942 hrs · 44,723 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 54,724 hrs · 44,552 cycles

LEFT WING OUTBOARD AFT FLAP LOWER INBOARD SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER AMM.

Part: TAB — DELAMINATED (RT AILERON) · airframe 54,724 hrs · 44,552 cycles

RIGHT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB PER AMM.

Part: FITTING — BROKEN (LT SPOILER) · airframe 54,632 hrs · 44,478 cycles

LEFT WING GROUND SPOILER FITTING BROKEN. REMOVED AND REPLACED SPOILER IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,212 hrs · 43,402 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,212 hrs · 43,402 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 947.5, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED FRAME SECTION PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 3.0. REPAIRED CHANNEL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 947.5, STR 19L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT STIFFENER CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 639, RBL 45.5. REPAIRED BEAM IAW EA.

Part: STRUCTURE — CORRODED (L1 DOOR) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR INNER CHORD CORRODED BETWEEN STR 270 TO STR 360 , STR 17L. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 3.0. REPAIRED CHANNEL IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 947.5, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED FRAME SECTION PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 907, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 907, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 328+1, STR 17R. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 947.5+12, STR 17R. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITIDUNAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 663 TO BS 671, LBL 24.5. REPAIRED CHORD IAW EA.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND UPPER FLANGE SUPPORT BEAM CORRODED AT BS 986.5, BETWEEN BL 0 TO LBL 45. REPAIRED BEAM IAW EO AND EA.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND UPPER FLANGE SUPPORT BEAM CORRODED AT BS 986.5, BETWEEN BL 0 TO RBL 45. REPAIRED BEAM IAW EO AND EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB BEAM WEB CRACKED AT BS 639, RBL 45.5, WL 208. REPAIRED WEB IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 27L. REPAIRIED FRAME IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPARTMENT ANGLE CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 303.9 TO BS 348.2, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 380, STR 5L. REPAIRED STRINGER IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947.5, BETWEEN STR 27L TO STR 26L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, RBL 3. REPAIRED CHANNEL IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, LBL 3. REPAIRED CHANNEL IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 1088 TO BS 1156. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 597, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT ANGLE CORRODED AT BS 727D, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 27L TO STR 26L. REPAIRED SHEAR TIE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 947.5+13, STR 17L. REPAIRED SKIN IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHANNEL CRACKED BETWEEN BS 303.9 TO BS 348.2, STR 17L. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 800A, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND LOWER INNER CHORD CRACKED AT BS 639, BETWEEN STR 17L TO STR 18L. REPAIRED CHORD IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND ANGLE CORRODED AT BS 727D, STR 27R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AN DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 24R TO STR 27R. REMOVED AND REPLACED FRAME IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.73, STR 10L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 787 TO BS 807, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 867 TO BS 887, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 827 TO BS 847, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED BETWEEN BS 500D TO BS 520, BL 0. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 747 TO BS 767, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 294.5, LBL 53. REPAIRED CHORD IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.73, STR 10R. REPAIRED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 24L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK FOUND, SKIN CRACKED AT BS 526, STR 28R. REPAIRED SKIN IAW EA.

Part: FLAP — PUNCTURED (LT WING) · airframe 49,872 hrs · 40,767 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B FORE FLAP PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: COVER — LOOSE (CABIN) · airframe 51,201 hrs · 41,877 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,163 hrs · 41,845 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT ENTRY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 51,115 hrs · 41,806 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED AT I/B TRAILING EDGE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 47,991 hrs · 39,415 cycles

COVER ON R2 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,310 hrs · 38,914 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 10. RELAMPED PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 47,173 hrs · 38,818 cycles

DURING SCHEDULED 14Y CHECK, FOUND CENTER EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,173 hrs · 38,818 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,173 hrs · 38,818 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,173 hrs · 38,818 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,173 hrs · 38,818 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,173 hrs · 38,818 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 47,173 hrs · 38,818 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN BL 0 TO STR 26L. REPAIRED SHEAR TIE PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,173 hrs · 38,818 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,173 hrs · 38,818 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,173 hrs · 38,818 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,173 hrs · 38,818 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,173 hrs · 38,818 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,173 hrs · 38,818 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,173 hrs · 38,818 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 47,037 hrs · 38,721 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 47,037 hrs · 38,721 cycles

DURING SCHEDULED SPV CHECK, FOUND LT MLG W/W CEILING CRACKED AT AILERON TOWER SHAFT. REPAIRED CEILING PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 47,037 hrs · 38,721 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OUTBOARD AFT FLAP DELAMINATED AT T/E. REPAIRED FLAP PER SRM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 46,788 hrs · 38,546 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 46,350 hrs · 38,219 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 45,650 hrs · 37,693 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 44,488 hrs · 36,843 cycles

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

Part: SKIN — CRACKED (L1 DOOR) · airframe 43,810 hrs · 36,382 cycles

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

Part: CHARGER — BROKEN (CABIN) · airframe 43,810 hrs · 36,382 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT LIGHT BATTERY CHARGER BROKEN. REMOVED AND REPLACED CHARGER PER MM.

Part: CHARGER — BROKEN (CABIN) · airframe 43,810 hrs · 36,382 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LIGHT BATTERY CHARGER BROKEN. REMOVED AND REPLACED CHARGER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,810 hrs · 36,382 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 43,810 hrs · 36,382 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 43,810 hrs · 36,382 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR SKIN CRACKED AT LOWER HINGE BS 303, WL 303. REPAIRED SKIN PER ER.

Part: RETAINER — BROKEN (BATTERY CHARGER) · airframe 43,810 hrs · 36,382 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY LIGHT BATTERY CHARGER RETAINER BROKEN. REMOVED AND REPLACED RETAINER PER MM.

Part: RETAINER — BROKEN (BATTERY CHARGER) · airframe 43,810 hrs · 36,382 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY LIGHT BATTERY CHARGER RETAINER BROKEN. REMOVED AND REPLACED RETAINER PER MM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 43,588 hrs · 36,220 cycles

UPON LANDING GEAR RETRACTION LT MLG RED LIGHT REMAINED ILLUMINATED WITH GEAR RETRACTED. RED AND GREEN LIGHTS ON WITH GEAR IN OFF POSITION. REMOVED AND REPLACED LT MLG UPLOCK ACTUATOR PER MM.

Part: CIRCUIT CARD — FAULTY (MLG) · airframe 43,585 hrs · 36,218 cycles

AIRTURN BACK, DURING CLIMB LT MLG RED LIGHT ILLUMINATED. CYCLED GEAR, NO CHANGE. FOUND CIRCUIT CARD BAD. REMOVED AND REPLACED CARD PER MM.

Part: LENS — BROKEN (CABIN) · airframe 43,529 hrs · 36,181 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 43,179 hrs · 35,902 cycles

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

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 43,038 hrs · 35,086 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 42,909 hrs · 35,705 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: TORQUE TUBE — WORN (EELVATOR) · airframe 41,390 hrs · 34,593 cycles

DURING SCHEDULED BRDG CHECK, RT HORIZONTAL STABILIZER FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 41,390 hrs · 34,593 cycles

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

Part: SLAT — DELAMINATED (LT WING) · airframe 41,390 hrs · 34,593 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 41,050 hrs · 34,344 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHTS) · airframe 40,773 hrs · 34,123 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,624 hrs · 33,220 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SSWA EA.

Part: MOUNT — BROKEN (NR 5 SPOILER) · airframe 39,511 hrs · 33,130 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING NR 5 SPOILER OUTBOARD MOUNT ASSY BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 38,739 hrs · 32,541 cycles

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

Part: SLIDE — DISCHARGED (L1 DOOR) · airframe 37,137 hrs · 31,432 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 36,813 hrs · 31,040 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 36,634 hrs · 30,905 cycles

EMERGENCY EXIT LIGHT LENS CRACKED AT FWD ENTRY DOOR. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 35,874 hrs · 30,337 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING AFT FLAP PER MM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 45 TO RBL 45. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CRACKED (BS 616) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT BS 616, BETWEEN LBL 65 TO RBL 65, WL 202. REPAIRED FRAME INNER CHORD PER BFG ER.

Part: FRAME — CRACKED (BS 440) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, RBL 39. REPAIRED FRAME PER BFG ER.

Part: SHEAR TIE — CORRODED (BS 807) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, BETWEEN RBL 4 TO LBL 4. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 17. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (BS 492) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 492.4, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER BFG ER.

Part: FRAME — CORRODED (BS 992) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 992, RBL 55, WL 209. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 303) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER BFG ER.

Part: FRAME — CORRODED (BS 767) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, RBL 7, WL 150. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,959 hrs · 28,886 cycles

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

Part: SHEAR TIE — CORRODED (BS 727E) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, RBL 8. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 907) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 907, BETWEEN STR 19L TO STR 20L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (BS 259) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 259, BETWEEN LBL 11 TO RBL 11. REPAIRED FLOORBEAM PER BFG ER.

Part: SHEAR TIE — CORRODED (BS 500C) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, RBL 17. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, BETWEEN LBL 8 TO RBL 8. REPAIRED SHEAR TIE PER SRM.

Part: FLOOR SUPPORT — CORRODED (BS 270) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR SUPPORT CORRODED AT BS 270, BETWEEN LBL 11 TO RBL 11, WL 208. REPAIRED FLOOR SUPPORT PER SRM.

Part: CREASE BEAM — CORRODED (BS 500A-500B) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 500A TO BS 500B. REPAIRED CREASE BEAM WEB PER SRM.

Part: SHEAR TIE — CORRODED (BS 500C) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, BETWEEN LBL 2 AND RBL 9. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 17. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500C) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, BETWEEN LBL 9 TO RBL 2. REPAIRED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,959 hrs · 28,886 cycles

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

Part: BRACKET — CRACKED (R2 DOOR SLIDE) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD FLOOR BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: SHEAR TIE — CORRODED (BS 500A) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500A, RBL 2. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (BS 300) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 300, WL 208. REPAIRED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (BS 867) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 747) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, RBL 8. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 867) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 747) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (BS 787) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 45 TO RBL 52, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 294) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 294, RBL 25, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 665) · airframe 33,959 hrs · 28,886 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 665, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 32,083 hrs · 27,316 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENRTY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,157 hrs · 26,607 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR CUTOUT LOWER HINGE BOX CRACKED. REMOVED AND REPLACED HINGE BOX PER SRM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 30,339 hrs · 26,000 cycles

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

Part: ACTUATOR — BROKEN (GROUND SPOILER) · airframe 30,232 hrs · 25,860 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD GROUND SPOILER, OUTBOARD ACTUATOR FWD ATTACH POINT BROKEN. REMOVED AND REPLACED LT WING GROUND SPOILER ACTUATOR PER MM.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 30,232 hrs · 25,860 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED RT WING FOREFLAP PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 30,232 hrs · 25,860 cycles

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

Part: STRUCTURE — SEPARATED (T/E FLAP) · airframe 29,792 hrs · 25,496 cycles

LT WING OUTBOARD AFT FLAP T/E, SEPARATED. REPAIRED LT OUTBOARD AFT T/E FLAP PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 29,430 hrs · 25,201 cycles

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

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 29,336 hrs · 25,129 cycles

L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 29,030 hrs · 24,903 cycles

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

Part: LIGHT — CRACKED (ROW 6-8) · airframe 28,370 hrs · 24,358 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP AT ROW 6 TO ROW 8 CRACKED. REPAIRED EEPLS PER MM.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 28,379 hrs · 24,364 cycles

L2 DOOR EVACUATION SLIDE PRESS GAUGE IN THE RED. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: INDICATOR — OUT OF LIMITS (ESCAPE SLIDE) · airframe 26,938 hrs · 23,213 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: FITTING — CORRODED (LT & RT MLG WW) · airframe 25,802 hrs · 22,291 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,769 hrs · 22,263 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BOTH LEFT AND RIGHT SIDE CHORDS CRACKED AT BS 178, WL 207. REMOVED AND REPLACED BOTH LT/RT SIDE CHORDS PER SWA ACO AND SRM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 25,484 hrs · 22,052 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SWITCH — FAULTY (COCKPIT) · airframe 25,373 hrs · 21,969 cycles

DURING SCHEDULED RON, FOUND EMERGENCY LIGHTS ILLUMINATING WHEN OVERHEAD SWITCH IS ARMED. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL SWITCH PER MM.

Part: ACTUATOR — FAILED (L/E FLAP) · airframe 24,210 hrs · 21,025 cycles

AIR TURNBACK, DURING CLIMB NR 2 KRUEGER FLAP WOULD NOT RETRACT. REMOVED AND REPLACED NR 2 KRUEGER FLAP ACTUATOR PER MM.

Part: TAB — WORN (LT ELEVATOR) · airframe 22,991 hrs · 20,032 cycles

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

Part: LENS — MISSING (FWD ENTRY DOOR) · airframe 22,759 hrs · 19,836 cycles

DURING SCHEDULED BC2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 21,244 hrs · 18,604 cycles

EEPLS COVER MISSING AT ROW 8. INSTALLED COVER PER MM.

Part: FLAP — DELAMINATED (RH WING) · airframe 20,958 hrs · 18,361 cycles

DURING RON, FOUND RH T/E INBD AFT FLAP DELAMINATED. R&R FLAP PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 18,804 hrs · 16,589 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. RE-INSTALLED EVAC SLIDE ASSY PER MM.

Part: ACTUATOR — INOPERATIVE (RT WING) · airframe 18,508 hrs · 16,346 cycles

AIR TURNBACK, RT KRUEGER FLAP WOULD NOT RETRACT. REMOVED AND REPLACED RT KRUEGER FLAP ACTUATOR. OPS CK GOOD PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 18,330 hrs · 16,209 cycles

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

Part: FRAME — CORRODED (CARGO BAY) · airframe 17,171 hrs · 15,266 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME CORRODED AT BS 794, RBL 22 - RBL 35, WL 157. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (CABIN) · airframe 17,171 hrs · 15,265 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 299.5 FRAME CRACKED AT FLOOR LEVEL RBL 60. REPAIRED STUB FRAME PER SRM.

Part: FITTING — CORRODED (GIRT BAR ATTACH) · airframe 17,171 hrs · 15,265 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR GIRT BAR FLOOR ATTACH FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,196 hrs · 14,444 cycles

EEPLS INOP AT MID CABIN. REPAIRED WIRING PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,106 hrs · 14,369 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT MID CABIN. RESECURED LIGHT WIRES PER MM.

Part: LIGHT — LOOSE (ROW 16)

EEPLS LOOSE AT ROW 16. SECURED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN)

EEPLS WIRES EXPOSED AT ROWS 15, 16, AND 17. REMOVED AND REPLACED TRACK SECTION PER MM.

Part: COVER — LOOSE (ROW 14)

EEPLS TRACK COVER LOOSE AT ROW 14. REINSTALLED TRACK COVER PER MM.

Part: TIRE — WORN (NLG)

ABORTED TAKEOFF, AIRCRAFT VEERED TO THE LEFT DURING TAKEOFF. RUNWAY WAS WET. FOUND NLG TIRES WORN. REMOVED AND REPLACED BOTH NLG TIRE/WHEEL ASSY'S.

Part: STRUT — OVERSERVICED (NLG)

REJECTED TAKEOFF AT APPROX 70 KNTS AFTER 2 OR 3 SIGNIFICANT YAWS TO LEFT AND RIGHT, ACCOMPANIED BY LOUD BANGS/BUMPS. APPEARED TO COME FROM NOSE WHEEL WELL AREA. INSPECTED ALL TIRES, BRAKES AND STRUTS AND FOUND NOSE STRUT OVERSERVICED. SERVICED STRUT PER MM. HIGH SPEED TAXI CKD OK.

Part: CHARGER — INOP (EMER EXIT)

DURING SCHEDULED SC CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER BOEING MM.

Part: BATTERY — DISCHARGED (PAX DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: FANS — SMOKING (CABIN)

EN ROUTE, NOTED AN ELECTRICAL SMELL AND HAZE IN CABIN. TURNED OFF GASPER AND RECIRCULATING FANS, SMELL AND HAZE DISAPPEARED. INSPECTED AND RAN RECIRCULATING AND GASPER FANS ON GROUND, NO SMELL OR SMOKE NOTED.