N397SW

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 74,367 hrs · 58,565 cycles

EMERGENCY LIGHTS INOP IN FWD CABIN. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT M1674, STA. 324, OPS CHECKED GOOD IAW B737-300 AMM 33-51-51

Part: BATTERY PACK — DISCHARGED (M01670/STA.700) · airframe 73,256 hrs · 58,020 cycles

CABIN, LH SIDE 9-10-11 EMERGENCY LIGHT IS INOP AT STA. 700. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK ASSY (M01670). PERFORMED OPS CHECK NORMAL AS PER AMM 33-51-51/33-51-02.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 72,628 hrs · 57,669 cycles

EMERGENCY BATTERY PACK DEAD AT M1197 DISC D3122 STA 960L.. REMOVED AND REPLACED BATTERY PACK AT M1197 STA. M960L IAW B-737-300 AMM 33-51-02. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 72,628 hrs · 57,669 cycles

EMERGENCY BATTERY PACK DEAD AT M1137 DISC D2966 STA 975R.. REMOVED AND REPLACED BATTERY PACK AT M1137 STA. 975R IAW B-737-300 AMM 33-51-02. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 72,628 hrs · 57,669 cycles

EMERGENCY BATTERY PACK DEAD AT M1133 DISC D2958 STA 326L.. REMOVED AND REPLACED BATTERY PACK AT M1133 STA 326L IAW B737-300 AMM 33-51-02. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 72,628 hrs · 57,669 cycles

EMERGENCY BATTERY PACK DEAD AT M1134 DISC D2960 STA 634L.. REMOVED AND REPLACED BATTERY PACK AT M1134 STA 634L IAW B737-300 AMM 33-51-02. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 72,628 hrs · 57,669 cycles

EMERGENCY BATTERY PACK DEAD AT M1135 DISC D2962 STA 622R.. REMOVED AND REPLACED BATTERY PACK AT M1135 STA 622R IAW B-737-300 AMM 33-51-02. OPS CHECK GOOD.

Part: LENS — BROKEN (EXIT SIGN) · airframe 71,329 hrs · 56,740 cycles

FORWARD ENTRY EXIT SIGN BROKEN. R&R LENS PER SIP.

Part: COVER — UNSECURE (CABIN) · airframe 70,717 hrs · 56,306 cycles

FORWARD ENTRY EMERGENCY EXIT LIGHT COVER FELL OFF. REPLACED COVER PER MM.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 70,360 hrs · 56,044 cycles

AIR TURNBACK, ON CLIMB OUT PASSING 10,000 FEET ENGINE AND ELECTRIC A HYDRAULIC LOW PRESS LIGHT ILLUMINATED. R&R A SYSTEM ENGINE DRIVEN HYDRAULIC PUMP IAW AMM.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 70,091 hrs · 55,857 cycles

R2 DOOR SLIDE GIRT BAR LOOSE. SECURED THE GIRT BAR IAW SIP.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 70,070 hrs · 55,846 cycles

FORWARD ENTRY EMERGENCY LIGHT LENS BROKEN. R & R THE LENS IAW MM.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 70,022 hrs · 55,812 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN FELL OFF. SECURED THE SIGN IAW AMM.

Part: TARGET — FAULTED (LT MLG) · airframe 69,799 hrs · 55,647 cycles

AFTER GEAR RETRACTION, LEFT GEAR DISAGREE LIGHT REMAINED ILLUMINATED THEN INTERMITTENT, ALL GEAR APPEARED AND FELT TO BE RETRACTED. RETURNED TO DEPARTURE. R & R THE TARGET ASSEMBLY IAW MM.

Part: BRACKET — CRACKED (RT PYLON) · airframe 69,799 hrs · 55,647 cycles

RT PYLON INTERCOSTAL BRACKET CRACKED AT FASTENER HOLES INSIDE PANEL 5853R FORWARD UPPER CORNER. R&R BRACKET PER SRM.

Part: SKIN — CRACKED (RT WING) · airframe 69,799 hrs · 55,647 cycles

RT WING LOWER SKIN PLAN CRACKED AT FSS 239, FASTENER HOLE TO PYLON FITTING. REPAIRED SKIN IAW EA.

Part: PUMP — FAULTY (NR 1 ENGINE) · airframe 69,377 hrs · 55,360 cycles

DECLARED EMERGENCY, HYDRAULIC SYSTEM A QUANTITY AND PRESSURE LOSS. SYSTEM A ENGINE & ELECTRIC LOW PRESSURE LIGHTS ILLUMINATED. REPLACED NR 1 ENGINE HYDRAULIC PUMP PER AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 69,346 hrs · 55,337 cycles

RT OVERWING "EXIT/SALIDA" SIDEWALL SIGN LENS COVER MISSING. INSTALLED COVER IAW AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 69,265 hrs · 55,277 cycles

FWD ENTRY EXIT LIGHT LENS LOOSE. SECURED THE LENS IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 69,207 hrs · 55,241 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER IAW SIP.

Part: WIRE — DAMAGED (CABIN) · airframe 69,169 hrs · 55,216 cycles

MID CABIN CEILING EMERGENCY EXIT SIGN FELL OFF. REPAIRED WIRE PER SWPM & SIP.

Part: LENS — BROKEN (EXIT SIGN) · airframe 68,485 hrs · 54,729 cycles

L1 DOOR EMERGENCY EXIT SIGN LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: STRAP — BROKEN (CABIN) · airframe 68,460 hrs · 54,705 cycles

FLOORBEAM STABILIZER STRAP BROKEN AT BS 312, BL 0. REPAIRED STRAP IAW SRM.

Part: WEB — CRACKED (BS 945-951) · airframe 68,460 hrs · 54,705 cycles

L2 DOOR INNER TORQUE TUBE COVER PLATE WEB CRACKED BETWEEN BS 945 TO 951. R & R THE WEB IAW SRM AND DWG.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 68,460 hrs · 54,705 cycles

AFT CARGO BAY DOOR CUTOUT CENTER NOSE SCUFF PLATE CRACKED. R & R SCUFF PLATE IAW SRM AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,460 hrs · 54,705 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 859, LBL 3. REPAIRED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,460 hrs · 54,705 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 859, LBL 8. REPAIRED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,460 hrs · 54,705 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 772, RBL 8. R & R SUPPORT IAW SRM & EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,460 hrs · 54,705 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 772, RBL 3. R & R SUPPORT IAW SRM & EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 68,460 hrs · 54,705 cycles

AFT CARGO BAY INTERCOSTAL WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 20. R & R WEB ASSY IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 772) · airframe 68,460 hrs · 54,705 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 772, LBL 3. R &R THE FLOOR SUPPORT IAW EA AND SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,460 hrs · 54,705 cycles

AFT CARGO BAY SHEAR TIE CORRODED AT BS 867, BETWEEN LBL 2 TO LBL 4. REPAIRED SHEAR TIE IAW SRM.

Part: ANGLE — CRACKED (R/H WING) · airframe 68,460 hrs · 54,705 cycles

RIGHT WING AILERON WIPER WEB ATTACH ANGLE CRACKED AT RSS 552. R & R THE ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,460 hrs · 54,705 cycles

L2 DOOR FUSELAGE SKIN CRACKED AT UPPER HINGE CUTOUT FORWARD EDGE. REPAIRED CUTOUT IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 68,460 hrs · 54,705 cycles

LEFT WING WIPER WEB ANGLE CRACKED AT RSS 552. R& R THE ANGLE IAW SRM.

Part: STIFFENER — CRACKED (BS 663) · airframe 68,460 hrs · 54,705 cycles

VERTICAL STIFFENER CRACKED AT BS 663, RBL 6.5. REPAIRED STIFFENER IAW ER AND EA.

Part: FITTING — LOOSE (L1 DOOR) · airframe 68,460 hrs · 54,705 cycles

L1 DOOR EMERGENCY EVAC SLIDE FORWARD GIRT BAR FLOOR FITTING LOOSE. R & R FITTING IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,460 hrs · 54,705 cycles

FLOORBEAM CORRODED AT BS 328, LBL 30. REPAIRED FLOORBEAM IAW SRM.

Part: CONTROL MODULE — FAULTY (AUTOTHROTTLE) · airframe 68,377 hrs · 54,651 cycles

DURING CLIMB OUT, LANDING GEAR LEVERS MOVED TO UP POSITION, WARNING HORN SOUNDED THREE RED LIGHTS ILLUMINATED AND NO GREEN LANDING GEAR LIGHTS. MOVED LEVERS TO DOWN POSITION RESULTED IN 3 GREEN LIGHTS NO RED AND NO WARNING HORN. R & R LT AUTO THROTTLE PACK ASSEMBLY M1639 IAW AMM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 68,170 hrs · 54,520 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOW PRESSURE. R & R SLIDE IAW MAINTENANCE.

Part: HINGE — BROKEN (RT SPOILER) · airframe 67,405 hrs · 54,016 cycles

RIGHT WING INBD GND SPOILER NR 5, 2ND FROM INBD HINGE BROKEN. R & R NR 5 GND SPOILER IAW MM.

Part: BRACKET — CRACKED (RT WING) · airframe 66,671 hrs · 53,545 cycles

RIGHT WING BRACKET COMMON TO UPPER SPAR CHORD, CRACKED AT RSS 235. R & R CHORD IAW DWG & EA.

Part: SKIN — CRACKED (LT WING) · airframe 66,671 hrs · 53,545 cycles

LEFT WING UPPER WING SKIN AFT SPAR, AFT FASTENER HOLE CRACKED, BETWEEN RSS 267 - 237.5. REPAIRED SKIN IAW EA.

Part: LINK — CORRODED (LT MLG) · airframe 66,671 hrs · 53,545 cycles

LEFT MLG BEAM, SWING LINK CORRODED. REPAIRED SWING LINK IAW EA.

Part: LINK — CORRODED (RT MLG) · airframe 66,671 hrs · 53,545 cycles

RIGHT MLG BEAM, SWING LINK CORRODED. REPAIRED SWING LINK IAW EA.

Part: FITTING — CRACKED (RT WING) · airframe 66,671 hrs · 53,545 cycles

RIGHT WING FASTENER HOLE INBD OF WING RSS 224.14, FITTING CRACKED. REPAIRED FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 66,671 hrs · 53,545 cycles

RIGHT WING FASTENER HOLES, BETWEEN WING RSS 225.14 - RSS 222.14, CRACKED IN UPPER SPAR CHORD. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (RT WING) · airframe 66,671 hrs · 53,545 cycles

RIGHT WING FASTENER HOLE INBD OF WING RSS 224.14, WEB CRACKED. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 66,671 hrs · 53,545 cycles

LEFT WING FASTENER HOLES, BETWEEN WING RSS 223.14 - 222.14, CRACKED IN UPPER SPAR CHORD. REPAIRED CHORD IAW EA.

Part: FITTING — CRACKED (LT WING) · airframe 66,671 hrs · 53,545 cycles

LEFT WING FASTENER HOLE INBD OF WING RSS 224.14, FITTING CRACKED. REPAIRED FITTING IAW EA.

Part: WEB — CRACKED (LT WING) · airframe 66,671 hrs · 53,545 cycles

LEFT WING FASTENER HOLES AT WING RSS 223.14, CRACKED IN UPPER WEB. REPAIRED WEB IAW EA.

Part: SPOILER — DELAMINATED (LT WING) · airframe 66,354 hrs · 53,323 cycles

LEFT WING NR 1 GND SPOILER DELAMINATED. R & R NR 1 GND SPOILER IAW MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 66,257 hrs · 53,253 cycles

LOWER FLOORBEAM SPLICE STRAP CRACKED AT BS 328. REPAIRED STRAP IAW SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 66,257 hrs · 53,253 cycles

R2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: COVER — BROKEN (CABIN) · airframe 66,257 hrs · 53,253 cycles

FORWARD ENTRY EXIT LIGHT COVER BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 64,602 hrs · 52,048 cycles

FORWARD ENTRY EMER EXIT LENS COVER AT FWD WALL MISSING. INSTALLED LENS IAW AMM.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 64,602 hrs · 52,048 cycles

L1 DOOR EXIT SIGN COVER FELL OFF. SECURED COVER IAW MM,

Part: COVER — DETACHED (CABIN) · airframe 64,287 hrs · 51,840 cycles

L1 DOOR EMER EXIT LIGHT COVER LOOSE DETACHED. ATTACHED COVER IAW AMM.

Part: WIRE — BROKEN (CABIN) · airframe 63,714 hrs · 51,466 cycles

AFT EMER EXIT LIGHT LOCATOR INOPERATIVE. REPAIRED BROKEN WIRE IAW AMM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 63,673 hrs · 51,444 cycles

FORWARD ENTRY EXIT SIGN LENS LOOSE. SECURED LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

SKIN CRACKED AT BS 727D+13, BETWEEN STRINGER 27L TO 27R. REPAIRED SKIN IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

STRAP CRACKED AT BS 328 LBL 48. R & R STRAP IAW SRM & DWG.

Part: SUPPORT FITTING — CORRODED (RT WING) · airframe 67,012 hrs · 53,765 cycles

RIGHT WING NR 5 INBD TRACK BORE SUPPORT FITTING CORRODED. REPAIRED FITTING IAW EA.

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

ACCESS PANEL 9508 PLATE CRACKED. R & R PANEL IAW SRM & DWG.

Part: SKIN — CRACKED (KRUEGER FLAP) · airframe 63,101 hrs · 51,039 cycles

RIGHT WING LE SKIN ON KRUEGER FLAP LE CRACKED AT STATION 208. REPAIRED SKIN IAW EO & EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,101 hrs · 51,039 cycles

LEFT WING INBD FORE FLAP DELAMINATED ON LOWER SKIN. REPAIRED FORE FLAP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

TIE CLIP CRACKED AT BS 380 STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: DUCT — CRACKED (E&E BAY) · airframe 63,101 hrs · 51,039 cycles

DUCT ASSEMBLY CRACKED, LOCATED ABOVE RACK E1-1 AT E & E COMPARTMENT. R & R DUCT ASSEMBLY IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

SUPPORT TIE CLIP CRACKED AT BS 294.5 STRINGER 23L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

TIE CLIP CRACKED AT BS 380 STRINGER 24L. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

WEB CORRODED BETWEEN BS 500A TO 500B STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

WEB CORRODED BETWEEN BS 500A TO 500B STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

STRINGER SPLICE CORRODED AT BS 907+4 STRINGER 18L. R & R SPLICE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

TIE CLIP CRACKED AT BS 947.5 STRINGER 25R. R & R TIE CLIP IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

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

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

AFT CARGO COMPARTMENT CHANNEL CRACKED AT BS 847+12 RBL 8. REPAIRED CHANNEL IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

AFT CARGO COMPARTMENT FRAME LOWER FLANGE CORRODED AT BS 747, BETWEEN STRINGER 26R TO 27R. REPAIRED FRAME IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

CHANNEL CRACKED AT BS 847+12 RBL 3.00. REPAIRED CHANNEL IAW EA.

Part: ACCESS PANEL — CRACKED (VERTICAL STAB) · airframe 63,101 hrs · 51,039 cycles

VERTICAL STABILIZER ACCESS PANEL 9523 CRACKED. R & R PANEL IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

ANGLE CRACKED AT BS 727B BL 0. R & R ANGLE IAW SRM & DWG.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 63,101 hrs · 51,039 cycles

RIGHT WING OTBD LE ACCESS PANEL 6527R CRACKED. R & R PANEL IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

FORWARD BULKHEAD OF AFT CARGO COMPARTMENT CHANNEL CRACKED AT BS 727 RBL 5. R & R CHANNEL IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

TIE CLIP CRACKED AT BS 787 STRINGER 20R. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

WEB CORRODED BETWEEN BS 727 TO 727C STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: FITTING — BROKEN (LT SPOILER) · airframe 63,101 hrs · 51,039 cycles

LEFT WING NR 4 GND SPOILER FITTING BROKEN. R & R NR 4 SPOILER IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

FRAME INNER CHORD CRACKED AT BS 639 STRINGER 16L. REPAIRED FRAME IAW EO & EA.

Part: WEB — CRACKED (R1 DOOR) · airframe 63,101 hrs · 51,039 cycles

R1 DOOR INTERNAL STRUCTURE WEB CRACKED 26 INCHES FROM LOWER EDGE. REPAIRED WEB IAW EA.

Part: PLATE — CRACKED (RT HORIZ STAB) · airframe 63,101 hrs · 51,039 cycles

RIGHT HORIZONTAL STABILIZER ACCESS PANEL 9224R PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 540, LBL 2. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

FORWARD CARGO COMPARTMENT WEB CRACKED AT BS 500D STRINGER 19R. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

FORWARD CARGO COMPARTMENT WEB CRACKED AT BS 500D STRINGER 19L. R & R WEB IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,101 hrs · 51,039 cycles

MAIN WW PRESS DECK CRACKED AT BS 664, LBL 39. REPAIRED DECK IAW EO & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

RIGHT NLG WW WEB CRACKED AT BS 243.7+3.5 WL 169.1. REPAIRED WEB IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

RIGHT WING TO BODY FAIRING LOWER SUPPORT ANGLE CRACKED BETWEEN BS 700 TO 727. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

LEFT WING TO BODY FAIRING SUPPORT STRUCTURE ANGLE CRACKED BETWEEN 3578L & 3501L ACCESS PANELS. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

LEFT MAIN WW AREA BULKHEAD FWD FACE ANGLE CRACKED AT BS 727 LBL 16. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (NLG WW) · airframe 63,101 hrs · 51,039 cycles

LEFT NLG WW WEB CRACKED AT BS 251.6+4 TO 259.5+3 WL 169.1. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A RT SIDE, IN AFT LOWEST HOLE. REPAIRED CHORD IAW EA.

Part: STRAP — CORRODED (R2 DOOR) · airframe 63,101 hrs · 51,039 cycles

R2 DOOR EMER EVAC SLIDE STRAP HOOK CORRODED. R & R STRAP IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A RT SIDE, LOWEST FWD HOLE. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A LT SIDE, AFT LOWER HOLE. REPAIRED CHORD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

LEFT MLG FWD CUT OUT OF INTERNAL AREA ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,101 hrs · 51,039 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A LT SIDE, FWD LOWER HOLE. REPAIRED CHORD IAW EA.

Part: STRAP — CORRODED (L2 DOOR) · airframe 63,101 hrs · 51,039 cycles

L2 DOOR EMER EVAC SLIDE STRAP HOOK CORRODED. R & R STRAP IAW AMM.

Part: CONTROLLER — FAILED (AC BAY) · airframe 62,162 hrs · 50,381 cycles

AIR TURN BACK, CLIMBING THROUGH 230 BOTH AUTO CONTROLLERS FAILED. R & R NR 1 & NR 2 CABIN PRESS CONTROLLERS IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 61,588 hrs · 49,969 cycles

RT SIDE AFT GALLEY EMERGENCY EXIT LIGHT COVER BROKEN. R & R COVER IAW AMM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 61,162 hrs · 49,678 cycles

RT WING NR 6 SPOILER BOARD DELAMINATED. R & R BOARD IAW MM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 60,131 hrs · 48,928 cycles

INTERCOSTAL UPPER ATTACH ANGLE CRACKED AT STATION 348-2, STRINGER 16L. R&R ANGLE IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 60,131 hrs · 48,928 cycles

INTERCOSTAL INNER TIE STRAP CRACKED AT STATION 348.2, STRINGER 16L. R&R TIE STRAP IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,131 hrs · 48,928 cycles

L1 DOOR INTERCOSTAL ANGLE CRACKED BETWEEN STATION 294.5 TO STATION 303.9, BETWEEN STRINGER 7L TO STRINGER 16L. R&R ANGLE IAW SRM & DRAWING.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 60,131 hrs · 48,928 cycles

INTERCOSTAL ATTACH ANGLE CRACKED AT STATION 348.2, STRINGER 6L. R&R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,131 hrs · 48,928 cycles

INTERCOSTAL INNER CHORD ANGLE CRACKED AT STATION 348.2, STRINGER 16L. R&R ANGLE IAW SRM & DRAWING.

Part: FIRESHIELD — DETERIORATED (NR 1 PYLON) · airframe 59,702 hrs · 48,593 cycles

NR 1 ENG PYLON AFT HEAT SHIELD DETERIORATED. REPLACED NR 1 ENGINE PYLON AFT HEAT SHIELD IAW AMM.

Part: ENGINE — LEAKING (RIGHT) · airframe 59,702 hrs · 48,593 cycles

AIR TURNBACK ON INITIAL CLIMB OUT. F/A REPORT VERY STRONG ODOR IN CABIN AGAIN. FOUND INTEGRAL OIL LEAK AT NR 2 ENGINE. R & R NR 2 ENGINE IAW MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 59,501 hrs · 48,443 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 58,328 hrs · 47,595 cycles

EXIT LIGHT AT L1 BROKEN OFF. REPLACED LENS AND BASE AND VERIFIED NORMAL OPERATION IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 57,809 hrs · 47,222 cycles

CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT HOUSING LOOSE. SECURED LIGHT PER AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,392 hrs · 46,918 cycles

WEB CRACKED AT BS 326.5, RBL 31. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,392 hrs · 46,918 cycles

AFT CARGO DOOR BEAR STRAP FWD LOWER CORNER OF CUTOUT CRACKED BETWEEN BS 787 TO BS 814 AND BETWEEN STR 22R TO STR 26R. REPAIRED SKIN PER SRM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 57,392 hrs · 46,918 cycles

TIE CLIP CORRODED AT BS 794, STR 26R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,392 hrs · 46,918 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 665, LBL 24.5 CENTER WING BOX. REPAIRED CHORD PER EA AND EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

STRINGER CLIP CRACKED AT BS 400, STR 9L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED SPLICE IAW SRM AND BAC DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

STRINGER SPLICE CRACKED AT BS 360, STR 13R. REMOVED & REPLACED SPLICE IAW BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

STRINGER CLIP CRACKED AT BS 360, STR 9R. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

STRINGER CLIP CRACKED AT BS 500C, STR 10R. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 520+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 767+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727C+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 847+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 520+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 440+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

RIGHT FUSELAGE SKIN CRACKED BS 480+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 887+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 360+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727D+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 360+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500C+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,116 hrs · 46,717 cycles

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

Part: SPOILER — DELAMINATED (LT WING) · airframe 56,290 hrs · 46,079 cycles

NR 3 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED NR 3 FLIGHT SPOILER PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 56,203 hrs · 46,019 cycles

FWD INBD EMERGENCY FLASHLIGHT INOP. REMOVED & REPLACED FLASHLIGHT PER M/M.

Part: LENS — MISSING (CABIN) · airframe 54,409 hrs · 44,704 cycles

RT OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING AT ROW 8. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,811 hrs · 44,249 cycles

DURING SCHEDULED CV CHECK FOUND, FUSELAGE SKIN CRACKED AT L2 DOOR BS 986.5, STR 7L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,261 hrs · 43,848 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED BETWEEN BS 727C+11 TO BS 727D+9, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,261 hrs · 43,848 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 727D+9, STR 4R. REPAIRED SKIN PER EA.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 52,995 hrs · 43,646 cycles

R2 DOOR EVAC SLIDE LOOSE. SECURED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 52,929 hrs · 43,595 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED AT BS 867, STR 26R. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 24L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR UPPER POSITION EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 847 TO BS 867, STR 23R. REPAIRED STRINGER PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT UPPER SURFACE I/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 727E + 2.5, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 17L TO STR 27R. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 751.5, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 732D, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 27R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 772, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: SKIN — CRACKED (FOREFLAP) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING FORE FLAP I/B LOWER SKIN CRACKED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED AT BS 1016, BL 0. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 616, BETWEEN STR 17R TO STR 18R. REPAIRED FRAME PER EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: SLAT — DELAMINATED (LT WING) · airframe 52,187 hrs · 43,034 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB FRAME WEB CRACKED AT BS 296, STR 7R. REPAIRED FRAME PER EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 52,187 hrs · 43,034 cycles

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

Part: SKIN — CRACKED (FOREFLAP) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING FORE FLAP I/B LOWER SKIN CRACKED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED AT BS 463, BETWEEN STR 18R TO STR 19R. REPAIRED SKIN PER SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN DOUBLER CRACKED BETWEEN BS 360 TO BS 384, BETWEEN STR 28R TO STR 27L. REMOVED AND REPLACED DOUBLER PER BAC DWG AND EO.

Part: SKIN — DELAMINATED (SPOILER) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SPOILER SKIN DELAMINATED. REPAIRED SPOILER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 360 TO BS 470, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 440, STR 6R. REMOVED AND REPLACED CLIP PER EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (TE FLAP) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING MID FLAP LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 907 TO BS 927, STR 21R. REMOVED AND REPLACED STRINGER PER SRM.

Part: FITTING — CRACKED (GIRT BAR) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP CRACKED. REPAIRED CLIP PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED AT BS 967, STR 21R. REMOVED AND REPLACED STRINGER PER EO AND BAC DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 927 TO BS 947.5, STR 21R. REMOVED AND REPLACED STRINGER PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708.5, LBL 24.5. REPAIRED BEAM PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 727 TO BS 727A, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED CHANNEL PER SRM.

Part: FLOORBEAM — BROKEN (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER FLANGE BROKEN AT BS 312, RBL 21. REPAIRED BEAM PER SRM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SLAT I/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND BEAM CHORD CORRODED AT BS 986.5, BETWEEN RBL 13 TO RBL 45. REPAIRED CHORD PER TI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 13R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 28. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND CROSS BEAM CRACKED AT BS 947.5, LBL 53. REPAIRED BEAM PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 639, LBL 45.50. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, RBL 8. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,037 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,037 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,037 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, RBL 45.50. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,037 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,187 hrs · 43,034 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,989 hrs · 42,887 cycles

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

Part: TAB — CRACKED (AILERON) · airframe 51,243 hrs · 42,324 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING AILERON TAB CRACKED. REMOVED AND REPLACED TAB PER MM.

Part: PANEL — DELAMINATED (LE SLAT) · airframe 51,243 hrs · 42,324 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 3 SLAT T/E WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 51,175 hrs · 42,273 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 49,252 hrs · 40,832 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EEPLS LOOSE AT ROW 3. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSLEAGE) · airframe 47,371 hrs · 39,501 cycles

DURING SCHEDULED 14Y CHECK, FOUND, FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BS 292.5, WL 261. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 291. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 406, BL 0. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 426, RBL 1.5. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT FUSELAGE SKIN CRACKED BETWEEN BS 299 TO BS 304, BETWEEN WL 235 TO WL 243. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 426, BL 0. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

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

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

DURING SCHEDULED 14Y CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWS EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 7L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

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

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 47,363 hrs · 39,494 cycles

DURING SCHEDULED 14Y CHECK, FOUND R1 COCKPIT WINDOW CUTOUT FRAME CRACKED AT UPPER LT CORNER. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,363 hrs · 39,494 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 45,800 hrs · 38,401 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 12 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 45,800 hrs · 38,401 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 19 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: TAB — LOOSE (LT ELEVATOR) · airframe 45,485 hrs · 38,172 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT ELEVATOR TRIM TAB ROD END LOOSE. R&R ELEVATOR TAB PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 45,464 hrs · 38,156 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,904 hrs · 37,754 cycles

DURING SCHEDULED HC2 CHECK, FOUND AFT SERVICE DOOR LOWER HINGE CUTOUT CRACKED AT LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,904 hrs · 37,754 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED AT LOWER CORNER. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,663 hrs · 35,224 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 470, RBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,663 hrs · 35,224 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 415 AND BS 430, RBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,663 hrs · 35,224 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 390, RBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 41,663 hrs · 35,224 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 639, STR 16R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S11L) · airframe 40,121 hrs · 33,998 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,121 hrs · 33,998 cycles

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

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 38,011 hrs · 32,329 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS COVER BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 37,577 hrs · 31,998 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 37,577 hrs · 31,998 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 37,080 hrs · 31,605 cycles

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

Part: LIGHT — LOOSE (L1 DOOR) · airframe 35,922 hrs · 30,666 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,602 hrs · 30,398 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 35,580 hrs · 30,382 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 33,608 hrs · 28,827 cycles

BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 16 DEF, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 33,489 hrs · 28,731 cycles

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

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 33,409 hrs · 28,669 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED CABLE PER MM.

Part: PANEL — CRACKED (LT WING SPOILER) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND LT WING NR 4 SPOILER PANEL OUTBOARD HINGE FITTING CRACKED. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: SPAR — CORRODED (VERTICAL STAB) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR RT AND LT PRIMARY CLEVIS FWD LUGS CORRODED. REPAIRED VERTICAL STAB PER ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 747, FROM RBL 9 TO RBL 13, WL 146, CORRODED. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 807, BL 0, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 303.9, STRINGER 16L, CRACKED. REPAIRED FRAME SECTION PER SB AND SRM.

Part: RIB — CRACKED (RT WING) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING LOWER RIB CHORD AT WING STATION 135.5, BETWEEN STRINGER 2 AND STRINGER 3, CRACKED. REPAIRED RIB CHORD PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB FROM RIGHT BS 188 TO BS 196, CRACKED. REPAIRED FLOORBEAM WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND 7 EACH CRACKS ON FUSELAGE FRAMES FROM BS 787 TO BS 907, STRINGER 8R AND BS 787, BS 827, STRINGER 8L. REPAIRED FRAME SECTIONS PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 847, RBL 18, CORRODED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND LEFT AND RIGHT HORIZONTAL STABILIZER FITTING FWD AND AFT SPARS CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727D, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND AFT PRESSURE BULKHEAD STRAP AT BS 1016, RBL 2, WL 208, CORRODED. REMOVED AND REPLACED STRAP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 500 + 15, LBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D CHECK, FOUND 3 EACH FRAMES CRACKED AT BS 380, BS 400, BS 440, STRINGER 8L. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727E, FROM RBL 8.10 TO RBL 13.80, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CORRODED (AFT CARGO COMPT) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, FROM RBL 5 TO RBL 20 CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH CRACKS ON FLOORBEAMS AT BS 986.5, LBL 52 TO RBL 52, BS 947, RBL 53. REPAIRED FLOORBEAM SECTIONS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 747 TO BS 867, LBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,244 hrs · 28,537 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 31,984 hrs · 27,500 cycles

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

Part: PLACARD — MISSING (L2 DOOR) · airframe 31,272 hrs · 26,934 cycles

L2 DOOR EVAC SLIDE MISSING PLACARD. INSTALLED PLACARD ON L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 30,995 hrs · 26,732 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 1 L/E SLAT SKIN CRACKED OUTBOARD END. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 30,995 hrs · 26,732 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 2 L/E SLAT UPPER SKIN ON TRAILING EDGE INBOARD AFT CORNER DELAMINATED. REPAIRED L/E SLAT PER EA.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 30,995 hrs · 26,732 cycles

DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB BUSHINGS PER MM.

Part: GUIDE ARM — WORN (L1 DOOR) · airframe 30,156 hrs · 26,075 cycles

AIR TURNBACK, PRESSURIZATION LEAK AT L1 DOOR. REMOVED AND REPLACED L1 DOOR UPPER GUIDE ARM PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 30,052 hrs · 25,998 cycles

DURING SCHEDULED C2 CHECK, RT ELEV TAB FAILED FREEPALY CHECK INSPECTION. REMOVED AND REPLACED TAB HINGE ATTACH BUSHINGS PER SI 11139-55.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,964 hrs · 25,923 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 5, WL 198. REPAIRED WEB PER SRM.

Part: LENS — LOOSE (ESCAPE SLIDE) · airframe 28,313 hrs · 24,559 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND COVER LENS LOOSE. SECURED COVER LENS PER MM.

Part: COFFEEMAKER — OVERHEATED (AFT GALLEY) · airframe 28,242 hrs · 24,500 cycles

DURING APPROACH, F/A SMELLED BURING ODOR IN AFT GALLEY. FOUND NR 1 COFFEEMAKER CIRCUIT BREAKER TRIPPED. REMOVED AND REPLACED NR 1 COFFEEMAKER PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 25,413 hrs · 22,247 cycles

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

Part: BRACKET — BROKEN (AFT SVC DOOR) · airframe 24,649 hrs · 21,621 cycles

DURING SCHEDULED 1/D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE MOUNTING BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,626 hrs · 19,985 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT SIDE CHORDS CRACKED AT BS 178, WL 207-208. REMOVED AND REPLACED BOTH CHORDS PER SWA ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 22,626 hrs · 19,985 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, LWR RH ANTENNA MOUNT. REPAIRED WEB PER SRM.

Part: BRACKET — LOOSE (ENTRY DOOR) · airframe 20,880 hrs · 19,375 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED GIRT BAR ASSY BRACKET PER MM.

Part: CABLE — FRAYED (ENTRY DOOR) · airframe 21,880 hrs · 19,375 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED GIRT BAR CABLE PER MM.

Part: LIGHT — BROKEN (SERVICE DOOR) · airframe 23,011 hrs · 20,554 cycles

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

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 19,278 hrs · 17,202 cycles

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

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 19,005 hrs · 16,956 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR AND BOTH AFT DOOR EVACUATION SLIDE GIRT ASSY''''S OUT OF ADJUST. ADJUSTED SLIDE PLAY PER MM.

Part: COMPRESSOR — CONTAMINATED (NR 1 ENGINE) · airframe 18,928 hrs · 16,892 cycles

BURNED OIL ODOR NOTICED DURING TAKEOFF, CLIMB AND DESCENT. REMOVED AND REPLACED BOTH ACM''''S C/W NR 1 ENG BORESCOPE INSP AND FOUND EVIDENCE OF OIL RESIDUE AT COMPRESSOR SECTION BLADES. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,927 hrs · 16,890 cycles

HOT OIL ODOR DETECTED IN CABIN WITH TAKEOFF THRUST APPLIED. SHUT-OFF LT A/C PACK AND ODOR WENT AWAY. DURING DESCENT AND LANDING TURN A/C PACK ON AND ODOR DID NOT APPEARED. RAN LT A/C PACK. NO DEFECT NOTED. OIL QTY OK.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 18,907 hrs · 16,870 cycles

FWD ENTRY DOOR EVACUATION SLIDE ACCIDENTALLY DISLODGED FROM CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 18,119 hrs · 16,227 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF POSITION. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR)

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

Part: LEVER — FAILED (COCKPIT)

AIR TURBACK, LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RESET LANDING GEAR LATCH C/B. OPS CK GOOD.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND BS 986 FLOORBEAM UPPER FACE CORRODED ON RBL 31.5. REPAIRED BEAM PER SWA RA NR 1-353-2172.

Part: SELECTOR — MALFUNCTIONED (COCKPIT)

DURING DESCENT, PASSING 29,000 FEET CABIN RATE WENT TO 2000 FPM DESCENT UNTIL PASSING 24000 FEET AND THEN RETURNED TO NORMAL. REMOVED AND REPLACED CABIN PRESSURE SELECTOR PANEL PER MM.

Part: CONTROLLER — MALFUNCTIONED (E & E BAY)

DURING DESCENT FROM 29,000 FT, AT 23,000 THE CABIN RATE WENT FROM 500 FPM TO 2000 FPM. AT 20,000 FEET CABIN RATE WENT 500 FPM CLIMB, THEN SETTLED BACK TO 500 FPM DESCENT. REMOVED AND REPLACED NR 2 PRESSURE CONTROLLER PER MM.