N687SW

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 84,710 hrs · 65,735 cycles

L1 DOOR EMER EXIT LIGHT FAILED OPERATIONS CHECK. R & R BATTERY PACK IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

TIE STRAP CRACKED AT BS 348.2 STRINGER 16L. REPAIRED TIE STRAP IAW SRM & DWG.

Part: WIRE — DAMAGED (CABIN) · airframe 84,710 hrs · 65,735 cycles

RIGHT SIDE OF AFT ENTRY EMER EXIT LIGHT WIRE DAMAGED. REPAIRED WIRE IAW WDM & AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,710 hrs · 65,735 cycles

L2 DOOR LOWER FWD EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

SHEAR TIE CRACKED AT BS 907 BETWEEN STRINGER 23L TO 24L. R & R SHEAR TIE IAW SRM & EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

FORWARD CGO DOOR CUT OUT AFT FRAME INNER FLANGE STRAP CRACKED AT FASTENER HOLE. R & R STRAP IAW SRM & DWG.

Part: SIGN — BROKEN (CABIN) · airframe 84,710 hrs · 65,735 cycles

L1 DOOR EMER EXIT SIGN ASSEMBLY ATTACHMENT BROKEN. R & R SIGN IAW AMM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

STRINGER CLIP AT DAMAGED BS 727E STRINGER 26L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

STRINGER CLIP CRACKED AT BS 727E STRINGER 26L. R & R CLIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

FORWARD CARGO COMPARTMENT FRAME ATTACH WEB CORRODED AT BS 492 BETWEEN RBL 24 TO 30. R & R WEB IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

FORWARD CARGO COMPARTMENT SKIN CORRODED AT BS 492 STRINGER 28R. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

STRINGER CLIP CORRODED AT BS 727A STRINGER 20L. R & R CLIP IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

SHEAR TIE CORRODED AT BS 927 BETWEEN STRINGER 26R TO 27R. REPAIRED SHEAR TIE IAW SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

FORWARD CARGO COMPARTMENT BEAR STRAP CORRODED AT BS 492 STRINGER 28R. REPAIRED BEAR STRAP IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

ZEE ANGLE CRACKED BETWEEN BS 492.4 TO BS 500A STRINGER 26R. R & R ZEE ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

FORWARD CGO DOOR CUT OUT AFT FRAME AROUND DOOR STOP CRACKED AT BS 492. R & R CUT OUT IAW ACO.

Part: LIGHT — BROKEN (EXTERIOR) · airframe 84,710 hrs · 65,735 cycles

EXTERNAL EGRESS LIGHT BULB BROKEN AT STATION 727D + 6 INCHES BETWEEN STRINGER 22L & 23L. RELAMPED IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

FUSELAGE SKIN CRACKED AT BS 747+13 STRINGER 18L. REPAIRED SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 84,710 hrs · 65,735 cycles

LEFT MAIN WW PRESS DECK CRACKED BETWEEN BS 665 TO 666 LBL 41. REPAIRED DECK IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

SKIN CRACKED AT BS 480+3 STRINGER 26L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

FUSELAGE SKIN CRACKED AT BS 480+5 STRINGER 26L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

FUSELAGE SKIN CRACKED AT BS 747+13 STRINGER 22L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

FUSELAGE SKIN CRACKED AT BS 847+12 STRINGER 22L. REPAIRED SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 84,710 hrs · 65,735 cycles

LEFT MAIN WHEEL PRESS DECK CRACKED AT BS 664 LBL 15. REPAIRED DECK IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

FUSELAGE SKIN CRACKED AT BS 827+16, STRINGER 21L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,710 hrs · 65,735 cycles

FUSELAGE SKIN CRACKED AT BS 460+16 STRINGER 26L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,589 hrs · 65,643 cycles

SKIN CRACKED AT BS 806 STRINGER 26R+4. REPAIRED SKIN IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 84,589 hrs · 65,643 cycles

FUSELAGE SKIN CORRODED AT BS 806, STRINGER 26R+4. REPAIRED SKIN IAW EA.

Part: TAB — CRACKED (RT AILERON) · airframe 84,449 hrs · 65,543 cycles

RIGHT WING AILERON TAB CRACKED AT TAB ROD FAIRING. R & R TAB IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,449 hrs · 65,543 cycles

SKIN CRACKED AT BS 420+17 STRINGER 18L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 82,643 hrs · 64,264 cycles

L1 DOOR INNER SKIN CRACKED AT LOWER HINGE BOX. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 82,535 hrs · 64,189 cycles

R2 DOOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 82,516 hrs · 64,178 cycles

SHEAR TIE CRACKED AT BS 400, BETWEEN STRINGER 15L TO STRINGER 16L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 82,516 hrs · 64,178 cycles

SHEAR TIE DAMAGED AT BS 460, BETWEEN STRINGER 16R TO STRINGER 17R. R & R SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,516 hrs · 64,178 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 505.5 TO BS 506, STRINGER 15R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,516 hrs · 64,178 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 514 TO BS 514.5, STRINGER 15R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,516 hrs · 64,178 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 500+4.5 - 500+5, STRINGER 16R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,516 hrs · 64,178 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 474 TO BS 477, STRINGER 16R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,516 hrs · 64,178 cycles

FUSELAGE SKIN CRACKED AT BS 460, BETWEEN STRINGER 17R TO STRINGER 18R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,516 hrs · 64,178 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 505 TO BS 505.5, STRINGER 15R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,516 hrs · 64,178 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 383.5 TO BS 385.5, STRINGER 19R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,516 hrs · 64,178 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 444.5 TO BS 445.7, STRINGER 16R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,516 hrs · 64,178 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 413.5 TO BS 415, STRINGER 17L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,516 hrs · 64,178 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 508 TO BS 509, STRINGER 15R. REPAIRED SKIN IAW ER & EA.

Part: HYDRAULIC LINE — LEAKING (NLG) · airframe 82,283 hrs · 64,001 cycles

AIR TURN BACK AFTER TAKEOFF WITH GEAR HANDLE UP RED LIGHT REMAINED ON IN NOSE GEAR INDICATOR WHEN HANDLE MOVED TO OFF NOSE GEAR FELL DOWN. R & R LOCK ACTUATOR PRESSURE LINE IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 81,847 hrs · 63,657 cycles

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

Part: ATTACH FITTING — BROKEN (LT SPOILER) · airframe 81,293 hrs · 63,234 cycles

LEFT WING NR 4 GROUND SPOILER ATTACH FITTING BROKEN. R & R SPOILER IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 80,995 hrs · 63,012 cycles

FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER M/M.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

STRINGER CLIP AT BS 274 STRINGER 10 RIGHT IS CRACKED. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: LENS — BROKEN (CABIN) · airframe 80,635 hrs · 62,768 cycles

EMERGENCY LIGHT LENS AT BIN 11RT BROKEN ON BULLNOSE. REMOVED AND REPLACED LENS IAW M/M.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORROSION ON INTERCOSTAL BS 344-360 STR 24R. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 51-10-02 100% MATERIAL LOSS REPAIR BY REPLACEMENT. REMOVED INTERCOSTAL PER SRM 51-40-02. FABRICATED REPLACEMENT PART PER DWG 69-48274 USING 2024T3 03032" C

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

FUSELAGE FRAME CRACKED AT STA 727, STR 18R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

FUSELAGE FRAME CRACKED AT STA 727, STR 18L. REPAIRED FRAME PER EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACK IN FORWARD FLANGE OF Z-STIFFENER O/B HOLE AT DOME CAP STR 1 STIFFENER 1016 BULKHEAD. REPAIRED Z-STIFFENER IAW ATS ER AND EA.

Part: RIVET — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

BS 827 AT STR 7R-8R EXISTING REPAIR AREA HAS CRACK ON AFT SIDE OF WEB 2ND RIVET ROW FROM THE TOP, INBD RIVET (AS MARKED). REMOVED CRACK RIVET FROM THE EXISTING REPAIR BS 827 AT STR 7R-8R AND INSTALLED NEW RIVET PER SRM 51-40-02. 91201U, 25JA

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACK IN FORWARD FLANGE OF Z-STIFFENER O/B HOLE AT DOME CAP STR 21R STIFFENER 1016 BULKHEAD. REPAIRED Z-STIFFENER IAW ATS ER AND EA.

Part: FAIRING — DELAMINATED (RT WING) · airframe 80,635 hrs · 62,768 cycles

RIGHT WING NR 2 IFOT FAIRING HAS AREA OF DELAMINATION ON UPPER SURFACE WHERE BUBBLE FAIRING ATTACHES. REPAIRED THE NR 2 IFOT FAIRING DELAMINATED AREA ON UPPER SURFACE IAW SRM 51-70-04.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

A 3 INCH, VERTICAL, SUB-SURFACE CHEM-MILL CRACK FOUND DURING NDT INSPECTION, AFT SIDE OF BS 908 SPLICE 5 I INCHES BELOW STR-5L TO 3 INCHES ABOVE STR-6L. CHEM-MILL CRACK AT BS 908 SPLICE 5" BELOW STR 5L TO 3" ABOVE STR 6L WAS REPAIRED IAW ATS ER 13-0277 DATED 12FEB13 AND EA 1-353-21723.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

ONE INCH SUB-SURFACE CHEM-MILL CRACK FOUND DURING NDT INSPECTION, ABOVE STR-26L AT BS 383 TO BS 384. REPAIRED CHEM-MILL CRACK OF FUSELAGE SKIN AT BS 383 TO 384 STR 26L IAW ER 13-01261 & EA 1-353-21605 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

BS 540 BULKHEAD HAS CRACK IN THE SPLICE ANGLE BETWEEN STR 21R AND STR 22R. REPAIRED ANGLE IAW ER & EA 1-357-7919

Part: FAIRING — CRACKED (RT WING) · airframe 80,635 hrs · 62,768 cycles

RIGHT WING BUBBLE FAIRING ON TOP OF NR 2 CRACKED. R & R FAIRING IAW SOPM SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

BULKHEAD CRACKED HORIZ STIFFENER BETWEEN RBL10 AND 19 ON 727 BULKHEAD. R & R STIFFENER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CHEM-MILL CRACK AT BS 740 BELOW STRINGER 18 LEFT. REPAIRED CHEM-MILL CRACK OF BS 740 BELOW STR 16 LEFT IAW ER 13-01210 & EA 1-353-21587.

Part: BEAM — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACK NOTED IN LONGITUDINAL BEAM UPPER CHORD VERTICAL LEG BS 664 RBL 24 AT UPPER HOLE. REPAIRED CRACK IN LONGITUDINAL BEAM UPPER CHORD VERTICAL LEG BS 664 RBL 24 IAW ER 13-01133 & EA 1-357-7890.

Part: BEAM — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

VERTICAL FLANGE OF UPPER CHORD OF LONGITUDINAL BEAM CRACKED AT BS 665.5 RBL 24.5 WL 207. REPAIRED BEAM IAW ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACK IN BS 663 FRAME AT I/B SIDE OF STRINGER 2L MOUSE HOLE. CRACK IN BS 663 FRAME AT I/B SIDE OF STR 2L MOUSE HOLE WAS REPAIRED IAW ATS ER 13-01224 DATED OF 08FEB2013 AND EA 1-353-21682.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACK IN BS 663 FRAME AT I/B SIDE OF STRINGER 3L MOUSE HOLE. CRACK IN BS 663 FRAME AT I/B SIDE OF STRINGER 3L MOUSE HOLE WAS REPAIRED IAW ATS ER 13-01224 DATED 08FEB13 AND EA 1-353-21682.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

SSID 11813-53 FIG F-38B, STRINGER SPLICE CRACK IN LOWER HORIZONTAL FLANGE BS 540 STR 10R CRACK LENGTH .75" LONG. BS 540 STR 10R STRINGER SPLICE WAS REMOVED AND REPLACED IAW ATS ER 13-01171 DATED 29JAN13 AND EA 1-353-21583.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACKED STRINGER UPPER FLANGE BS 1011 STR 7L. REMOVED AND REPLACED STRINGER BS 1011 S-7L PER SRM 51-40-02-0G-0, DRW 65-52788, SRM 51-40-05-0G-0, SRM 51-20-01-0G-0, SOPM 20-41-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORROSION ON FRAME ON INNER FLANGE BS 993 STR 17R. CORROSION ON BS 993 FRAME INNER FLANGE AT STR 17R WAS REPAIRED IAW ATS ER 13-01186 DATED 07FEB2013 AND EA 1-353-21666 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACKED STRINGER CLIP AT BS 767 STR 16L. REMOVED AND REPLACED CLIP IAW TECH DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORROSION ON STRINGER 24R BS 355-360. STR 24R AT BS 351 TO 360 HAS 80% MAT LOSS. FOUND TO BE OUT OF LIMITS PER SRM 53-00-03-1A-1. REMOVED STR SECTION FROM BS 351-360 AND REPAIRED IAW SRM 53-00-03-2R-1.

Part: RIB — CRACKED (RT WING) · airframe 80,635 hrs · 62,768 cycles

RIGHT WING RIB LOWER CHORD CRACKED AT STA 135.5, BETWEEN STR 2 AND STR 3. REPAIRED RIB PER EA.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 80,635 hrs · 62,768 cycles

LOWER WING SKIN TO PANEL ATTACH ANGLE CRACKED ON I/B SIDE FSS 222. REMOVED CRACKED ATTACH ANGLE ON RT WING I/B SIDE FSS 222 AND INSTALLED NEW FABRICATED ATTACH ANGLE IAW SRM 51-40-02-0G-0 PARA 4, 7 AND 9 2656U 18JAN13.

Part: STRAP — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

FLOORBEAM TENSION STRAP CRACKED AT BS 328, LBL 14. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,634 hrs · 62,768 cycles

STRINGER CORRODED AND PILLOWING AT BS 347-360, STR 25R. REPAIRED STRINGER SECTION AT BS 328+3 - 360+7 STR 25R IAW SRM 53-00-03-2R-1 REPAIR 1.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACKED ATTACH ANGLE FOR CABLE PULLEY SUPPORT CHANNEL BS 697 RBL 1 WL 207. REMOVED AND REPLACED ANGLE IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 666 AND BS 670, RBL 24.5. REPAIRED CHORD IAW ER & EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACKED ATTACH ANGLE FOR CABLE PULLEY SUPPORT CHANNEL BS 697 LBL 1 WL 207. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACKED RIVET HEAD BETWEEN LT NR 1 AND NR 2 FLIGHT DECK WINDOWS. REMOVED AND REPLACED SKIN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACK IN FWD ENTRY DOOR THRESHOLD SUPPORT ANGLE AT BS 318 AND WL 208 AT LBL 60. REMOVED AND REPLACED FWD ENTRY DOOR THRESHOLD SUPPORT ANGLES P/N 66-2738-1 PER SRM 51-40-05, SRM 51-40-02 AND DRAWING 66-2738.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORROSION ON ANGLE FWD SIDE OF FLOORBEAM UNDER UPPER FLANGE BS 344 LBL 56 WL 208. REMOVED & REPLACED CORRODED ANGLE ON FWD SIDE OF FLOORBEAM ON UPPER FLANGE BS 344 LBL 56 WL 208 PER 737-300 SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

FORWARD LWR STUB FRAME CRACKED AT FWD LWR STOP PAD FITTING AT BS 296 AND STRINGER 16R. REMOVED AND REPLACED FWD LWR TUB FRAME IAW DWG 65-45807 AND 51-40-02 88324U 12FEB13.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACK IN INTERCOSTAL BETWEEN STRINGERS 12R AND 13R AT BS 344. REMOVED AND REPLACED CRACKED INTERCOSTAL WITH NEW P/N 65-45813-29 IAW SRM 51-40-02, 51-40-05, AND DWG 65-45813 88952U 22JAN13.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

BS 500D BETWEEN STR 27R-28R, FRAME CORRODED BELOW FAILSAFE CHORD. REMOVED AND REPLACED FRAME IAW SRM.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORROSION FWD GALLEY DOOR CUTOUT UPPER HINGE SUPPORT FITTING CORRODED AT BS 293 AND STRINGER 10R ON INBOARD FLANGE. REMOVED CORRODED UPPER HINGE SUPPORT FITTING FWD SERVICE DOOR & INSTALLED NEW SUPPORT FITTING PER SRM 51-40-02-0G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORRODED ON FLOORBEAM UPPER FLANGE BS 328 RBL 9-RBL 57 208. REMOVED AND REPLACED CHORD PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACK IN INTERCOSTAL AT STRINGER 4L AND BS 309. REMOVED AND REPLACED INTERCOSTAL AT S-4L AND BS 309 PER DRW 50-08261, SRM 51-40-02-0G-10, SRM 51-40-05-04-0, AMM 51-21-41-377-032, AND AMM 51-21-99-307-001.

Part: FRAME — CHAFED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CHAFE ON INNER FLANGE OF FRAME AT BS 277 AND STRINGER 3R. REPAIRED CHAFE ON INNER FLANGE OF FRAME AT BS 277 STR 32 IAW SRM 53-00-07-2R-1.

Part: SPLICE PLATE — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

BULKHEAD CRACKED AT BS 540 IN THE SPLICE PLATE BETWEEN STR 21L AND 22L. REPAIRED BULKHEAD SPLICE PLATE BETWEEN PER ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORRODED ON FLOORBEAM UPPER FLANGE BS 328 LBL 50 WL 208. REMOVED AND REPLACED CHORD PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORRODED ON FLOORBEAM UPPER FLANGE BS 294.5 RBL 26-44 WL 208. REMOVED AND REPLACED CHORD IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACK IN STUB FRAME AT BS 296 AND STRINGER 7R. REMOVED CRACKED UPPER FWD STUB FRAME BS 296 & INSTALLED NEW STUB FRAME PER SRM 51-40-20G.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACK IN SHEAR TIE AT BS 277 JUST BELOW STRINGER 8L. REMOVED AND REPLACED SHEAR TIE AT BS 277 JUST BELOW STRINGER 8L IAW SWG 65-45805/SRM 51-40-02.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACK IN BEAR STRAP AT BS 291 TO BS 293 BETWEEN AT STRINGERS 9R AND 10R. REPAIRED SKIN IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

(FWD CARGO BAY) BS 500, STR 28L-28R, CORROSION ON SHEAR TIE AND FRAME WEB. REPAIRED FWD CARGO BAY BS 500 STR 28L-28R SHEAR TIE AND FRAME WEB PER SRM 53-00-07-2R-7 REPAIR 4.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

BS 500B STR 16L HAS CRACKED STRINGER CLIP AT INBOARD FASTENER ON WEB (AS MARKED). REMOVED AND REPLACED STRINGER CLIP P/N 69-35340Y2 PER SRM 51-40-05, SRM 51-40-02 AND DRAWING 65C22908.

Part: SKIN — CRACKED (RT WING) · airframe 80,635 hrs · 62,768 cycles

RIGHT WING FIXED L/E CRACKED ABOVE NR 4 FLAP NACELLE DOOR. REPAIRED LEADING EDGE PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

(FWD CARGO BAY) BS 500-500A STR 28R IS CORRODED. STR 28R BS 500-500A WAS DETERMINED TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-03-1A-1. REPAIRED STR 28R BS 500-500A IAW SRM 53-00-03-2R-1 83802U 07FEB13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CRACK ON PREVIOUS REPAIR ON STUB FRAME AT BS 296 AND STRINGER 17R. REMOVED AND REPLACED STUB FRAME ACCOMPLISHED ON NRC T177332 88324U 12FEB13.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

SKIN CRACKED AT AFT UPPER CORNER OF DOOR CUTOUT. REMOVED AND REPLACED SKIN IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORRODED BS 1006-1020 WL 208 LBL 27 ON FLOOR STRAP. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORRODED BS 1006-1020 WL 208 LBL 17 ON FLOOR STRAP. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: PLATE — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORROSION BS 986 WL 208 LBL 45 GIRT BAR SUPPORT PLATE IS CORRODED. REMOVED CORRISION IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-1A-1. FABRICATED NEW SUPPORT PLATE IAW DWG 69-68869.

Part: STRAP — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORROSION BS 1010 - 1016 WL 208 LBL 2-5 CORROSION ON SUPPORT STRAP. REMOVED AND REPLACED STRAP IAW DWG AND SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORROSION BS 986 WL 208 RBL 45 GIRT BAR SUPPORT PLATE IS CORRODED. REMOVED CORRISION IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-1A-1. FABRICATED NUT SUPPORT PLATE IAW DWG 69-68869 88952U 30JAN13.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,636 hrs · 62,769 cycles

FUSELAGE SKIN CRACKED AT STA 500D+6, STR 17R. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

FRAME AT BS 344 BETWEEN STRINGERS 21L-22L IS CRACKED. FRAME AT BS 344 BETWEEN STRINGER 21L-22L CRACK WAS REPAIRED IAW ATS ER 13-01084 DATED 13FEB13 AND EA 1-353-21745.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

STRINGER CLIP CRACKED AT BS 907 AND STRINGER 25R. REMOVED & REPLACED STRINGER CLIP AT BS 907 & STRINGER 25R PER SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORROSION ON STRINGER CLIP AT BS 767 AND STRINGER 23R WL 153. REMOVED & REPLACED STRINGER CLIP AT BS 767, STRINGER 23R PER B737-300 SRM 51-40-02 & DRAWING #65-46549.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

STRINGER AND STRINGER TIE FITTING CORRODED AT BS 907 AND STR 27R. REPAIRED STRINGER AT BS 907 STR 27R IAW ER 13-01325 & EA 1-353-21718.

Part: CHANNEL — CRACKED (RT PYLON) · airframe 80,635 hrs · 62,768 cycles

RIGHT PYLON AFT STRUT FAIRING LOWER O/B HORIZONTAL CHANNEL AFT END CRACKED. REMOVED AND REPLACED CHANNEL PER SRM.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

FRAME FAILSAFE CHORD CRACKED AT BS 947 BETWEEN STRINGERS 25L AND 26L. REPAIRED FAILSAFE CHORD AT BS 947 BETWEEN S25L-S26L IAW ER 13-01223 & EA 1-353-21637 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

SHEAR TIE CRACKED ON VERT LEG AT BS 907 BETWEEN STRINGERS 26R AND 25R. REPAIRED SHEAR TIE IAW SRM 53-00-07-2R-3 88324U 2FEB13.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CARGO LINER SUPPORT ATTACH BRACKET CRACKED AT BS 727, LBL 1. REMOVED AND REPLACED BRACKET IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

SHEAR TIE CORRODED AT BS 887, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 80,634 hrs · 62,768 cycles

FLOORBEAM LOWER CHORD CRACKED AT BS 663, LBL 24.8. REPAIRED BEAM PER ATS ER AND EA.

Part: STAND OFF — CRACKED (SPOILER) · airframe 80,635 hrs · 62,768 cycles

RIGHT WING STAND-OFF CRACKED AT NR 5 I/N SPOILER ACTUATOR SUPPORT FITTING. REMOVED AND REPLACED BRACKET IAW SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORROSION ON SHEAR WEB AT RBL 6 BETWEEN BS 787 AND BS 807. REPLACED SHEAR WEB AT RBL 6 BETWEEN BS 787 AND 807 WITH FABRICATED PART IAW DWG 65-47958 & 737-300 SRM 51-40-02-0G-0.

Part: SEAL — DEBONDED (NR 8 SPOILER) · airframe 80,635 hrs · 62,768 cycles

RIGHT WING NR 8 SPOILER OUTBOARD HINGE OUTBOARD HORSE SHOE SEAL DISBONDED. REMOVED AND REPLACED NR 8 SPOILER OUTBOARD HINGE OUTBOARD HORSE SHOE SEAL IAW AMM 27-61-11-404-010 E4D.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE IAW SRM.

Part: RIB — CRACKED (NR 2 PYLON) · airframe 80,635 hrs · 62,768 cycles

RIGHT WING NR 2 PYLON LWR AFT SHORT RIB CRACKED. REMOVED AND REPLACED RIGHT WING NR 2 PYLON LOWER AFT SHORT RIB PER SRM 51-40-02-0G-0.

Part: WEB — CRACKED (NLG WW) · airframe 80,635 hrs · 62,768 cycles

LEFT NLG W/W WEB CRACKED AT BS 252.3 WL 181-174. REMOVED AND REPLACED PER SRM.

Part: RETAINER — CRACKED (NR 6 SPOILER) · airframe 80,635 hrs · 62,768 cycles

(RIGHT WING) NR 6 SPOILER INBOARD LOWER BLADE SEAL INBOARD SECTION OF SEAL RETAINER CRACKED. REMOVED AND REPLACED SEAL RETAINER ON NR 6 SPOILER INBOARD LOWER BLADE SEAL, IAW SRM 51-40-02-0G-0. 56179U 17JAN13

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORROSION ON STRINGER CLIP AT BS 747 AND STRINGER 26R. REMOVED & REPLACED STRINGER CLIP AT BS 747, STRINGER 26R PER B737-300 SRM 51-40-02-0G-0 AND DRAWING 65-46548. MATERIAL REF:P/O LINE 402047. P/N 69-35350-1.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORROSION - STRINGER 26R CORRODED AT BS 827. REPAIRED STRINGER 26R AT BS 827 IAW SRM 53-00-03-2R-1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

SHEAR TIE CORRODED AT BS 827, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CORROSION ON SHEAR TIE BETWEEN STRINGERS 25L AND 26L AT BS 807. REPAIRED SHEAR TIE BETWEEN STRINGERS 25L AND 26L PER BS 737-300 SRM 53-00-07-2R-3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,636 hrs · 62,769 cycles

SHEAR TIE CORRODED AT STA 727E, RBL 5. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

SHEAR TIE CORRODED AT BS 847, BETWEEN STR 26L AND 25L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: WEB — CRACKED (NLG WW) · airframe 80,635 hrs · 62,768 cycles

RIGHT NLG WW WEB CRACKED AT BS 252.3, WL 181-174.5. REMOVED AND REPLACED PER SRM.

Part: RIB — CRACKED (NR 1 PYLON) · airframe 80,635 hrs · 62,768 cycles

(LEFT WING) NR 1 PYLON LOWER AFT HALF RIB IS CRACKED JUST BELOW TORQUE TUBE CUTOUT. REMOVED LEFT WING NR 1 PYLON LOWER AFT HALF RIB PER SRM 51-40-02-0G-0. 4318C, 19JAN13. LOCATED THE NEW RIB, DRILLED AND INSTALLED PER SRM 51-40-02-0G-0.

Part: SEAL — DEBONDED (NR 2 SPOILER) · airframe 80,635 hrs · 62,768 cycles

(LEFT WING) NR 2 SPOILER PANEL O/B HINGE I/B HORSE SHOE SEAL IS DISBONDED. REMOVED AND REPLACED NR 2 SPOILER O/B HINGE I/B HORSE SHOE SEAL IAW AMM 27-61-11-404-010 56179 15JAN13.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CHEM-MILL CRACK IN FUSELAGE SKIN, 415 OVER STRINGER 15 LEFT. CHEM-MILL CRACK IN FUSELAGE SKIN, 415 OVER STRINGER 15 LEFT WAS REPAIRED IAW ATS ER 13-01002 DATED 24JAN2013 AND EA 1-353-2154.1

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CHEM-MILL CRACK IN FUSELAGE SKIN, BS 415 OVER STRINGER 26 LEFT LAP. CHEM-MILL CRACK IN FUSELAGE SKIN BS 415 OVER STR 26 LEFT LAP WAS REPAIRED IAW ATS ER 13-01006 DATED 21JAN13 AND EA 1-353-21504 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CHEM MILL CRACK IN FUSELAGE SKIN, BS 500B+5 OVER STRINGER 23 RIGHT. TRIMMED OUT CRACK AT BS 500B+5 ABOVE STR 23 RT IN AN AREA OF 1" X 4". HFEC VERIFIED NO CRACKS. INSTALLED REPAIR PER SRM 53-00-01 REPAIR 31. ASSESSED THE REPAIR TO BE A CATEGORY

Part: REINFORCEMENT — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

BS 500D FUSELAGE FRAME REINFORCEMENT CRACKED AT 1.04" WIRE PENETRATION HOLE BETWEEN STR 20R-21R. BS 500D FUSELAGE FRAME REINFORCEMENT CRACKED AT 1.04" WIRE PENETRATION HOLE BETWEEN STR 20R-21R. REPAIRED PER SRM 53-00-07-2R-13.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

FUSELAGE SKIN CRACKED AT BS 500B+5, STR 15L. REPAIRED SKIN IAW ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

CHEM-MILL CRACK IN FUSELAGE SKIN, BS 754 OVER STRINGER 25 LEFT LAP. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

FUSELAGE SKIN CRACKED AT BS 500+14, STR 17L. REMOVED AND REPLACED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 80,635 hrs · 62,768 cycles

EMERGENCY LIGHT AT SEAT ROW 19DEF LOOSE (MARKED). REBONDED EMERGENCY LIGHT AT SEAT ROW 19DEF IAW SOPM 20-50-12 PAR AI TYPE 71 STEPS (1) THRU (6).

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

SKIN CRACKED BS 400+6, STR 16R. REPAIRED SKIN IAW ATS ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,635 hrs · 62,768 cycles

REFERENCE LOG PAGE 0008357868: FOUND SURFACE CRACK ABOVE STR 16R AT B/S 400+6 APPROX 2.5" EXPOSED PROTRUDING FROM REPAIR JUST FWD. SURFACE CRACK ABOVE STR 16R AT BS 400+6 WAS REPAIRED IAW ATS ER 13-01015 DATED 21JAN13 AND EA 1-353-21512.

Part: BUSHING — CORRODED (FUSELAGE) · airframe 79,736 hrs · 62,119 cycles

UPPER AFT FUSELAGE VERTICAL STABILIZER RIGHT PRIMARY CLEVIS FITTING AT BS 1087, FORWARD LUG AFT FACES CORRODED. REMOVED AND REPLACED BUSHING IAW EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,736 hrs · 62,119 cycles

UPPER AFT FUSELAGE VERTICAL STABILIZER RIGHT PRIMARY CLEVIS FITTING AFT LUG FORWARD FACE, LIGHT PITTING CORRODED AT STA 1089. REPAIRED FITTING IAW EA.

Part: LUG — CORRODED (FUSELAGE) · airframe 79,736 hrs · 62,119 cycles

UPPER AFT FUSELAGE VERTICAL STABILIZER LEFT PRIMARY CLEVIS FITTING AT STA 1089 AFT LUG FWD FACE CORRODED. REPAIRED LUG IAW EA.

Part: BUSHING — CORRODED (FUSELAGE) · airframe 79,736 hrs · 62,119 cycles

UPPER AFT FUSELAGE VERTICAL STABILIZER LEFT PRIMARY CLEVIS FITTING AT BS 1087, FORWARD LUG AFT FACE, CORRODED. REPAIRED BUSHING IAW EA.

Part: BUSHING — CORRODED (FUSELAGE) · airframe 79,736 hrs · 62,119 cycles

VERTICAL STABILIZER FUSELAGE AFT LEFT FAILSAFE CLEVIS LUG FACES CORRODED. REMOVED AND REPLACED BUSHINGS IAW EA.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 79,736 hrs · 62,119 cycles

VERTICAL STABILIZER AFT SPAR, RT PRIMARY ATTACH LUG, CORRODED AROUND AFT BUSHING FACE. REPAIRED LUG IAW EA.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 79,736 hrs · 62,119 cycles

VERTICAL STABILIZER AFT SPAR, LEFT PRIMARY ATTACH LUG, CORRODED AROUND AFT BUSHING FACE. REPAIRED LUG IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,736 hrs · 62,119 cycles

STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: STRUCTURE — CORRODED (VERTICAL STAB) · airframe 79,736 hrs · 62,119 cycles

LEFT VERTICAL STABILIZER CORRODED BETWEEN STA 265.10 TO STA 275.00. REMOVED AND REPLACED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,736 hrs · 62,119 cycles

SKIN CRACKED AT BS 500A+3, RBL 15. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 79,736 hrs · 62,119 cycles

SHEAR TIE CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED SHEAR TIE IAW EA.

Part: ATTACH BRACKET — CRACKED (R2 DOOR) · airframe 79,734 hrs · 62,118 cycles

R2 DOOR EMERGENCY EVAC SLIDE AFT BOLT ATTACH BRACKET STANDOFF CRACKED. REMOVED AND REPLACED BRACKET ASSY PER M/M.

Part: PANEL — PUNCTURED (SPOILER) · airframe 79,734 hrs · 62,118 cycles

LEFT WING NR 2 SPOILER PANEL PUNCTURED. REMOVED AND REPLACED NR 2 SPOILER PER AMM.

Part: COVER — LOOSE (CABIN) · airframe 79,734 hrs · 62,118 cycles

RIGHT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT COVER LOOSE. RE-SECURED COVER PER AMM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 77,933 hrs · 60,771 cycles

DURING SCHEDULED HC2 CHECK FOUND LT WING NR 2 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,731 hrs · 60,620 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 405, STR 15L. REPAIRED SKIN IAW ER.

Part: MOTOR — FAULTY (TE FLAP) · airframe 77,485 hrs · 60,425 cycles

AIR TURNBACK, AFTER TAKEOFF FLAPS WOULD NOT RAISE WITH FLAP HANDLE. REMOVED AND REPLACED T/E FLAP HYDRAULIC DRIVE MOTOR PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 77,204 hrs · 60,212 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT. DID NOT DEPLOY. REMOVED AND REPLACED SLIDE IAW MT.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 77,066 hrs · 60,108 cycles

DECLARED EMERGENCY - ON FINAL PASSING 6500FT GASPER FAN TURNED ON WITH STRONG SMELL OF SMOKE DETECTED BY FLIGHT ATTENDANTS. GASPER FAN TURNED OFF, EMERGENCY DECLARED. REMOVED AND REPLACED GASPER FAN P.

Part: TIRE — FAILED (RT MLG) · airframe 76,866 hrs · 59,947 cycles

ONE OF THE RT MAIN TIRES FAILED DURING THE TAKEOFF ROLL, THE CREW ABORTED THE TAKEOFF AND THE SECOND RT MAIN TIRE SUBSEQUENTLY FAILED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 516D, STR 20R. REPAIRED SKIN PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, RBL 8. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 667, LBL 24.5. REPAIRED BEAM PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, RBL 5. REPAIRED SHEAR TIE PER ER AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CORRODED AT BS 908, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED AT BS 398, STR 25L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 767+13, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 754, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 764, STR 19L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN BL 0 TO RBL 5. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED AT BS 662, LBL 24.5. REPAIRED BEAM PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT KEEL BEAM CORRODED AT BS 787. REPAIRED BEAM PER EA AND SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 460, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 485, STR 16R. REPAIRED SKIN PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, RBL 5. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 661, BL 0. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663, BL 0. REPAIRED BEAM PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 11. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 740D, STR 21L. REMOVED AND REPLACED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 755, STR 24L. REMOVED AND REPLACED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 887+13, STR 16R. REMOVED AND REPLACED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 987, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 987, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING AFT FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND CORROSION AFT PIT SHEAR TIE BILGE AREA STA 747, RBL 7. REPAIRED PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND CRACK ON STRINGER CLIP STA 987, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND CORROSION AFT PIT SHEAR TIE BILGE AREA STA 727C, LBL 9. REPAIRED PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND CORROSION AFT PIT SHEAR TIE BILGE AREA STA 747, LBL 3 TO RBL 3. REPAIRED PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND CRACK ON STRINGER CLIP STA 947, BETWEEN STR 21L AND 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND CRACK STA 754, STR 20L. REPAIRED PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND CORROSION AFT PIT FLOOR SUPPORT STA 767 +5, LBL 8. REPAIRED PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND CRACK STA 500D, STR 15R. REPAIRED PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND CRACK IN LONGITUDINAL FLOORBEAM, STA 727B, RBL 24.5. REPAIRED PER EA/ER.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND CORROSION AFT PIT FLOOR SUPPORT STA 767 +5, LBL 12. REPAIRED PER SRM AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND CORROSION AFT PIT FLOOR SUPPORT STA 767 +5, RBL 3. REPAIRED PER SRM AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,939 hrs · 59,232 cycles

DURING SCHEDULED 26Y CHECK, FOUND CORROSION AFT PIT SHEAR TIE BILGE AREA STA 807, LBL 3. REPAIRED PER SRM.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 75,658 hrs · 59,026 cycles

DURING SCHEDULED OTS CHECK, FOUND FAIL SAFE ANGLE CRACKED AT BS 440, STR 16L. REPAIRED ANGLE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,658 hrs · 59,026 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CRACKED AT BS 440, BETWEEN STR 15L TO STR 15L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,658 hrs · 59,026 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 833, STR 23L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,658 hrs · 59,026 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,658 hrs · 59,026 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 395, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,658 hrs · 59,026 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 376, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,658 hrs · 59,026 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 440, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,658 hrs · 59,026 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 372, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,658 hrs · 59,026 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 783, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,658 hrs · 59,026 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 395, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 912, STR 23L. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND RT MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,347 hrs · 58,801 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERHEAD BIN EMERGENCY EXIT LIGHT INOP AT ROW 23. REMOVED AND REPLACED BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 19L TO STR 22L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 19L TO STR 22L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 19L TO STR 22L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD L1 DOOR EMERGENCY EXIT LIGHT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 4R. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SI AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED CLIP PER SI AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED CLIP PER SI AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,347 hrs · 58,801 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4R. REMOVED AND REPLACED CLIP PER SI.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 74,975 hrs · 58,514 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR AFT CENTER FRAME CRACKED. REMOVED AND REPLACED R1 DOOR PER MM.

Part: COVER — MISSING (CABIN) · airframe 74,458 hrs · 58,103 cycles

RT EMERGENCY EXIT LIGHT COVER MISSING AT ROW 19. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,159 hrs · 57,880 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 799, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,021 hrs · 57,766 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 767, STR 18R. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 73,835 hrs · 57,618 cycles

RT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 19. INSTALLED LENS PER MM.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 73,584 hrs · 57,427 cycles

FWD EMERGENCY FLASHLIGHT HOLDER BROKEN. REMOVED AND REPLACED HOLDER PER MM.

Part: LIGHT — FADED (CABIN) · airframe 73,410 hrs · 57,296 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT EEPLS FADED AT ROW 18. REMOVED AND REPLACED EEPLS PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 73,410 hrs · 57,296 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FWD EMERGENCY EXIT LIGHT BATTERY CHARGER INOP. REMOVED AND REPLACED CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,410 hrs · 57,296 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 922, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,410 hrs · 57,296 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 943, STR 24L. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE DOME BULKHEAD Y-CHORD CORRODED AT BS 1016, 6 O'CLOCK POSITION. REMOVED AND REPLACED BULKHEAD SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 28R TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD FWD SIDE CRACKED AT BS 1016, LBL 3. REPAIRED BULKHEAD PER BAC DWG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD FWD SIDE CORRODED AT BS 1016, LBL 6. REPAIRED BULKHEAD PER BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 827 TO BS 847. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 639, BETWEEN LBL 65 TO LBL 68. REPAIRED FRAME PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR SIGN LIGHT INOP. RELAMPED PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN FS 360 TO FS 380. REPAIRED WEB PER SRM.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING OUT OF ADJUST. REMOVED AND REPLACED FITTING PER MM.

Part: BEAM — CORRODED (HORIZ STAB) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT HORIZONTAL STABILIZER UPPER SURFACE T/E BEAM CORRODED. REPAIRED STABILIZER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME OUTER CHORD CRACKED AT BS 639, BETWEEN RBL 65 TO RBL 68. REPAIRED CHORD PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME WEB CRACKED AT BS 639, BETWEEN RBL 65 TO RBL 68. REPAIRED WEB PER EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT STUB BEAM CRACKED AT BS 639, LBL 63. REPAIRED BEAM PER AAR EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING MID FLAP L/E DELAMINATED. REPAIRED MID FLAP PER SRM.

Part: COVER — CRACKED (EXIT SIGN) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 476, STR 28R. REPAIRED STRINGER PER SRM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO COMPT WEB LOWER ATTACH ANGLE CORRODED AT BS 514, STR 26R. REPAIRED ANGLE PER BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 27L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME STUB BEAM CRACKED AT BS 639, LBL 63. REPAIRED BEAM PER AAR EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN BULBS INOP. RELAMPED PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 616, BETWEEN STR 7L TO STR 8L. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 639, STR 16L. REMOVED AND REPLACED STRINGER PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 616 TO BS 639. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 1016, STR 26R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 967, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT CREASE BEAM WEB CRACKED BETWEEN BS 616 TO BS 639, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947.5, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM CORRODED AT BS 639, STR 16L. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM CRACKED AT BS 620, RBL 63. REMOVED AND REPLACED BEAM PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM CRACKED AT BS 639, STR 17L. REMOVED AND REPLACED BEAM SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 827, STR 26L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 967, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 663, STR 1. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 967, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 559, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED AT BS 663, LBL 24.5. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 767, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 500B, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 807, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26L TO STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 767, STR 26L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT CREASE BEAM CORRODED BETWEEN BS 847 TO BS 867. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND VERTICAL ATTACH ANGLE CORRODED AT BS 685, STR 18L. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 540, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 747, STR 26L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REPAIRED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 727E TO BS 747. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REPAIRED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 2R. REPAIRED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REPAIRED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 72,046 hrs · 56,275 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,924 hrs · 56,188 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 515 TO BS 518, STR 16R. REPAIRED SKIN PER ER.

Part: SIGN — MISSING (CABIN) · airframe 71,775 hrs · 56,084 cycles

LT LOWER OVERWING EMERGENCY EXIT SIGN MISSING. REMOVED AND REPLACED SIGN PER MM.

Part: PLATE — BROKEN (GIRT BAR) · airframe 71,347 hrs · 55,776 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD FLOOR ATTACH PLATE BROKEN. REMOVED AND REPLACED HOLDER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 71,311 hrs · 55,753 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,252 hrs · 55,719 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727E + 16, STR 23L. REPAIRED SKIN PER SWA EA.

Part: WIRE — DAMAGED (CABIN) · airframe 70,914 hrs · 55,489 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 19 DEF. REPAIRED LIGHT WIRES PER MM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 70,914 hrs · 55,489 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L1 DOOR CUTOUT, BS 304.40, WL 261.63. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,914 hrs · 55,489 cycles

DURING SCHEDULED HC2 CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,914 hrs · 55,489 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 502, STR 18R. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,914 hrs · 55,489 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND CORRODED STRINGER 21R, BS 727D. REPAIRED STRINGER PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 70,914 hrs · 55,489 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,914 hrs · 55,489 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 870, STR 24R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,914 hrs · 55,489 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED & REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,749 hrs · 55,371 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,749 hrs · 55,371 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 310, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,749 hrs · 55,371 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,749 hrs · 55,371 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 24L. REPAIRED SKIN PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 70,682 hrs · 55,320 cycles

FWD FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 70,396 hrs · 55,117 cycles

R1 DOOR SLIDE OUT OF POSITION. POSITIONED SLIDE PER MT.

Part: LIGHT — MISSING (CABIN) · airframe 69,969 hrs · 54,818 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT PLATE MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 69,356 hrs · 54,364 cycles

L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED SLIDE ASSY PER MM.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 69,148 hrs · 54,213 cycles

FLIGHT DECK R1 WINDOW ARCED INFLIGHT. R&R WINDOW HEAT CONTROLLER PER MM.

Part: SKIN — CRACKED (BS 933 S22L) · airframe 69,138 hrs · 54,206 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 506B S18R) · airframe 69,138 hrs · 54,206 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506B, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 877 S25R) · airframe 69,138 hrs · 54,206 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 877, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 80,634 hrs · 62,768 cycles

LEFT WING LOWER SKIN PANEL ABOVE THE O/B MID SPAR FITTING HAS A 0.55" CRACK. (REF NRC B583433) PERFORMED INTERIM REPAIR PER EA 1-A57-3318. REINSPECT EVERY 720 DAYS FOR CRACK PROPAGATION. PERFORM A PERMANENT REPAIR ON OR BEFORE THE 28Y CHECK.

Part: SKIN — CRACKED (L/E SLAT) · airframe 69,077 hrs · 54,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED AT AUX TRACK CUTOUT. REMOVED AND REPLACED SLAT ASSY PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,077 hrs · 54,157 cycles

DURING 22Y CK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 550, RBL 28, WL 208. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,077 hrs · 54,157 cycles

DURING 22Y CK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 550, RBL 50, WL 208. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: TAB — CRACKED (LT AILERON) · airframe 69,077 hrs · 54,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING AILERON TAB CRACKED AT INBOARD END. REMOVED AND REPLACED TAB PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 69,077 hrs · 54,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,271 hrs · 53,592 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,271 hrs · 53,592 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,271 hrs · 53,592 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,271 hrs · 53,592 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 68,271 hrs · 53,592 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,271 hrs · 53,592 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,271 hrs · 53,592 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 1006, STR 17R TO STR 19R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,271 hrs · 53,595 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STUB FRAME CORRODED AT BS 312, STR 17R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,271 hrs · 53,592 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,271 hrs · 53,592 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,271 hrs · 53,592 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 312, LBL 12 TO RBL 12. REPAIRED CHORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,271 hrs · 53,592 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 294, LBL 12 TO RBL 4. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,271 hrs · 53,592 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,271 hrs · 53,592 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,271 hrs · 53,592 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,155 hrs · 53,505 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,026 hrs · 53,415 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 393, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,026 hrs · 53,415 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,026 hrs · 53,415 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 840, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,026 hrs · 53,415 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506, STR 17L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,894 hrs · 53,314 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,840 hrs · 53,272 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 870, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,840 hrs · 53,272 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 884, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 67,840 hrs · 53,272 cycles

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

Part: FITTING — CRACKED (GIRT BAR) · airframe 67,840 hrs · 53,272 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CRACKED. REMOVED AND REPLACED FITTING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,840 hrs · 53,272 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 22R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,512 hrs · 53,028 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,512 hrs · 53,028 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 981, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,512 hrs · 53,028 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 23R. REPAIRED SKIN PER SWA EA.

Part: LENS — ACTIVATED (COCKPIT) · airframe 67,084 hrs · 52,708 cycles

DIVERSION, ELECTRICAL-RUBBER BURNING ODOR IN COCKPIT. INSPECTED AND FOUND F/O GRIMES LIGHT INTERNAL LENS MELTED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 930 S24L) · airframe 67,041 hrs · 52,680 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 24L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,083 hrs · 51,884 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 927, STR 19L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,058 hrs · 51,869 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 736D, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,805 hrs · 51,675 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,938 hrs · 51,002 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,925 hrs · 50,992 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 762, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 739D S22R) · airframe 64,509 hrs · 50,676 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739D, STR 22R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 733E S25R) · airframe 64,509 hrs · 50,676 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733E, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 731 S23R) · airframe 64,509 hrs · 50,676 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731, STR 23R. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,931 hrs · 50,203 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 504D S16L) · airframe 63,118 hrs · 49,566 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT FUSELAGE SKIN CRACKED AT FWD LOWER CORNER. REPAIRED SKIN PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT FRAME CRACKED AT BS 794, STR 24R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 967, STR 27L. REPAIRED BEAR STRAP PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME WEB CRACKED AT LOWER DOOR STOP FITTING. REMOVED AND REPLACED FRAME WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 360, STR 28R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME WEB CRACKED AT UPPER DOOR STOP FITTING. REMOVED AND REPLACED FRAME WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 967, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB SKIN CRACKED AT LOWER SURFACE STA 133.5. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR CUTOUT UPPER FWD CORNER, BS 298, STR 7R. REPAIRED SKIN PER ER.

Part: SLAT — DELAMINATED (LT WING) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 3 L/E SLAT DELAMINATED AT OUTBOARD T/E WEDGE. REPAIRED SLAT PER SRM.

Part: SKIN — CORRODED (RT SPOILER) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 6 SPOILER UPPER SURFACE CORRODED AT CENTER HINGE. REPAIRED SPOILER PER SRM.

Part: FRAME — CORRODED (CABIN) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, RBL 25. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM WEB CORRODED AT BS 613 TO BS 634, BL 0. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (AFT CARGO BAY) · airframe 62,629 hrs · 49,207 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER INBOARD SIDE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: STRINGER CLIP — CRACKED (AFT CARGO BAY) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DEBONDED (LT MIDFLAP) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD MID FLAP LOWER SURFACE DISBONDED AT INBOARD SIDE. REPAIRED MID FLAP PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, LBL 12. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (AFT CARGO BAY) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 19R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (AFT CARGO BAY) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 26L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (ELEVATOR TAB) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT ELEVATOR TAB CRACKED AT INBOARD UPPER SURFACE CUTOUT. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: STRINGER CLIP — CRACKED (AFT CARGO BAY) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 339, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: COVER — TORN (EVAC SLIDE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PLASTIC COVER TORN. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, STR 26L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 794, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CORRODED AT BS 531, STR 27R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 533, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517, STR 12L. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: TORQUE TUBE — CORRODED (FORE FLAP) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD FORE FLAP, INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 GROUND SPOILER DELAMINATED AT ACTUATOR ATTACH POINT. REPAIRED SPOILER PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. REMOVED AND REPLACED GIRT BAR HOOK RIVETS PER SRM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND PRESSURE BULKHEAD CRACKED AT BS 1016, STR 23R. REPAIRED PRESSURE BULKHEAD PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 354) · airframe 62,629 hrs · 49,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 354, STR 16L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,107 hrs · 48,804 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 62,085 hrs · 48,781 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,844 hrs · 48,608 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 915, STR 25R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 727E) · airframe 61,290 hrs · 48,180 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 61,290 hrs · 48,180 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,290 hrs · 48,180 cycles

DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 60,804 hrs · 47,789 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,774 hrs · 47,764 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 954, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 510) · airframe 60,320 hrs · 47,386 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 16L. REPAIRED SKIN PER SWA EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 60,213 hrs · 47,296 cycles

DURING SCHEDULED RON CHECK, FOUND NLG W/W RT UPPER ACCESS PANEL CUTOUT, AFT INBD CORNER CRACKED AT BS 251.6, LBL 2.0. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,887 hrs · 47,031 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, ABOVE STR 25R. REPAIRED SKIN PER SRM.

Part: SOLENOID — FAULTY (MLG HANDLE) · airframe 59,600 hrs · 46,789 cycles

AIR TURNBACK. LANDING GEAR LEVER WOULD NOT MOVE UP AFTER TAKEOFF. LEVER LOCK SOLENOID FAILURE INDICATED. REMOVED AND REPLACED MLG HANDLE SOLENOID PER MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 58,757 hrs · 46,107 cycles

RIGHT MLG DID INDICATE FULLY RETRACTED AFTER TAKEOFF. RECYCLED GEAR DOWN & UP, THEN INDICATED OK. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR & TRANSFER CYLINDER PER MM.

Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 58,682 hrs · 46,051 cycles

UNSAFE GEAR INDICATION UPON MLG RETRACTION. RECYCLED GEAR HANDLE. NORMAL RETRACT INDICATION. REMOVED AND REPLACED RT MLG ACTUATOR & UPLOCK ACTUATOR PER MM.

Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 58,681 hrs · 46,050 cycles

RT MLG DID NOT INITIALLY RETRACT ON DEPARTURE. CYCLED GEAR LEVER BACK TO UP, GEAR RETRACTED. OPERATED MLG & COULD NOT DUPLICATE PROBLEM. AS A PRECAUTION, REMOVED AND REPLACED RT MLG DOWNLOCK ACTUATOR PER MM.

Part: ANGLE — CRACKED (NR 2 ENG PYLON) · airframe 58,488 hrs · 45,917 cycles

DURING SCHEDULED CHECK, FOUND NR 2 ENGINE UPPER PYLON ATTACH ANGLE, CRACKED. REMOVED AND REPLACED ATTACH ANGLE PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,488 hrs · 45,917 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS FROM BS 756 TO BS 757, BETWEEN STRINGERS 21R AND 22R. REPAIRED SKIN SECTIONS PER SRM.

Part: ACTUATOR — LEAKING (RT MLG) · airframe 57,554 hrs · 45,209 cycles

RIGHT MLG DOWN AND LOCKED DURING FLIGHT. GEAR HANDLE WAS OFF AND ALL OTHER LANDING GEARS STAYED UP AND LOCKED. RIGHT MLG CAME UP WHEN HANDLE WAS RAISED. REMOVED AND REPLACED UPLOCK ACTUATOR PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 57,489 hrs · 45,158 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOE EVAC DOOR SLIDE CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,489 hrs · 45,158 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727C, STRINGER 23R AND BS 727D, STRINGER 24L. REPAIRED SKIN SECTIONS PER EA.

Part: CABLE — FRAYED (R2 DOOR GIRT BAR) · airframe 57,489 hrs · 45,158 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE DOOR GIRT BAR CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE GIRT BAR CABLE PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 57,489 hrs · 45,158 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING TRAILING EDGE INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT T/E INBOARD AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,587 hrs · 44,408 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,576 hrs · 44,401 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 923, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF LIMITS (L2 DOOR) · airframe 56,273 hrs · 44,140 cycles

L2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,141 hrs · 44,034 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727D + 6, STRINGER 20R, BS 727E - 3, STRINGER 23L, BS 750, STRINGER 19L, BS 942.5, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,395 hrs · 43,446 cycles

DURING SCHEDULED SPV, FOUND SHEAR TIES AT BS 360, STRINGERS 14R AND 14L, CRACKED. REPAIRED SHEAR TIES PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,395 hrs · 43,446 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 2 TO BS 500D + 6, STRINGER 12L. REPAIRED SKIN PER EA.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 55,395 hrs · 43,446 cycles

DURING SCHEDULED SPV, FOUND LT WING LOWER ATTACH ANGLE AT WBL 135.5, S2, CRACKED. REMOVED AND REPLACED LT WING ATTACH ANGLE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 55,395 hrs · 43,446 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: HOLDER — CRACKED (FWD CABIN) · airframe 55,395 hrs · 43,446 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY FLASHLIGHT HOLDER CRACKED AT FWD F/A'S SEAT. REMOVED AND REPLACED FLASHLIGHT HOLDER PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,395 hrs · 43,446 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 360, STR 14R. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,395 hrs · 43,446 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 500 + 14. REPAIRED STRINGER PER SRM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 55,389 hrs · 43,444 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT FLIGHT COMPARTMENT WINDOW POST CRACKED. REPAIRED WINDOW POST PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,387 hrs · 43,444 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR FRAME CUTOUT FORWARD LOWER HINGE INNER DOUBLER CRACKED. REMOVED AND REPLACED L1 DOOR CUTOUT DOUBLER PER SRM.

Part: DOOR FRAME — CRACKED (L2 DOOR) · airframe 55,387 hrs · 43,444 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR FRAME CUTOUT LOWER FORWARD CORNER CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,389 hrs · 43,444 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSEKAGE SKIN CRACK AT BS 520 + 4, STRINGER 10R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,389 hrs · 43,444 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520 + 4, STRINGER 10R. REPAIRED FUSELAGE SKIN PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 55,389 hrs · 43,444 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR CUTOUT FRAME CRACKED AT LOWER FWD CORNER. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 55,389 hrs · 43,444 cycles

DURING SCHEDULED 1/4D CHECK, FOUND IN AFT CARGO COMPT STRINGER CLIP CORRODED AT BS727E, STRINGER 26R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,389 hrs · 43,444 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT BELT FRAME SHEAR TIES CORRODED AT BS 727E, BETWEEN STRINGER 26R AND STRINGER 27R. REMOVED AND REPLACED SHEAR TIES PER EA.

Part: FLAP — CORRODED (RT WING) · airframe 55,389 hrs · 43,444 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON RT WING INBOARD FORE FLAP INBOARD ATTACH ARM. REMOVED AND REPLACED RT INBOARD FORE FLAP PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 55,389 hrs · 43,444 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR FRAME CUTOUT CRACKED AT DOOR STOP. REPAIRED R1 DOOR FRAME CUTOUT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,389 hrs · 43,444 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 758, STRINGER 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 55,093 hrs · 43,201 cycles

R1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY. REINSTALLED SLIDE ASSY PER MM.

Part: STRIP — CRACKED (CABIN FLOOR) · airframe 55,082 hrs · 43,192 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP CRACKED AT ROW 9 ABC. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: PROBE — OVERHEATED (PITOT/STATIC SYS) · airframe 54,566 hrs · 42,766 cycles

DECLARED EMERGENCY, STRONG BURNING ODOR DETECTED IN COCKPIT, FOLLOWED BY SMALL AMOUNT OF SMOKE COMING FROM F/O'S AFT RIGHT SIDE PANEL. FOUND F/O'S AUX PITOT PROBE ASSY BURNING STATIC LINE. REMOVED AND REPLACED PITOT PROBE AND STATIC LINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,875 hrs · 42,215 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 500 PLUS 2 AT STR 15R AND BS 747 AT STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,459 hrs · 41,889 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867, BETWEEN STR 21R AND 22R. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 53,281 hrs · 41,745 cycles

DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,705 hrs · 41,268 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, BELOW STR 19R. REPAIRED SKIN PER SRM.

Part: PRIORITY VALVE — FAULTY (RT MLG W/W) · airframe 51,539 hrs · 40,361 cycles

ON DEPARTURE, RT MLG DID NOT RAISE, INDICATED DOWN AND UNSAFE WITH GEAR HANDLE IN UP AND OFF. CYCLED GEAR HANDLE TO UP AND RT MLG CAME UP. RECYCLED GEAR DOWN AND BACK UP ALL INDICATIONS NORMAL. REMOVED AND REPLACED RT MLG POSITION PRIORITY VALVE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 51,189 hrs · 40,069 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE RELEASE CABLE FITTING TO COVER GAP OUT OF LIMITS. REPOSTIONED FITTING PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 51,189 hrs · 40,069 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE IND DATA PLATE OUT OF POSITION. REPOSTIONED DATA PLATE PER MM.

Part: STIFFENER — CRACKED (LT MLG W/W) · airframe 50,445 hrs · 39,463 cycles

DURING SCHEDULED PM CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663.75, LBL 4. REPAIRED STIFFENER PER SWA EA.

Part: STIFFENER — CRACKED (LT MLG W/W) · airframe 50,445 hrs · 39,463 cycles

DURING SCHEDULED PM CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 727, LBL 16. REPAIRED STIFFENER PER SWA EA.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 50,331 hrs · 39,362 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,325 hrs · 39,358 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,963 hrs · 39,049 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS (2 EA) BETWEEN STR'S 22R AND 23R, AT BS 727D PLUS 18 AND BS 766.5. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (BOTH ELEVATORS) · airframe 49,878 hrs · 38,980 cycles

DURING SCHEDULED A1 CHECK, SWA SI 11111-55, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH LEFT AND RIGHT ELEVATOR TAB NR 1 HINGE BUSHINGS PER MM.

Part: FAN — OVERTEMP (A/C BAY) · airframe 49,415 hrs · 38,617 cycles

ODOR DETECTED IN CABIN WHILE ON APPROACH TO MCI. REMOVED AND REPLACED RECIRCULATION FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,612 hrs · 37,189 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED ( 2 EA ) AT BS 727E, STR 22R & 23R. REPAIRED SKIN PER SRM.

Part: SLAT — CRACKED (LH WING) · airframe 47,612 hrs · 37,189 cycles

DURING SCHEDULED C1 CHECK, FOUND # 1 L/E SLAT CRACKED 3/8 INCH LONG AT AFT ROW OF FASTENERS, LOWER SKIN. REPAIRED # 1 L/E SLAT PER SWA RA 1-357-1118.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME CRACKED AT BS 492, RBL 36 & WL 159. REPAIRED FRAME PER BFG ER.

Part: BEAM — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL BEAM CRACKED AT BS 727B, RBL 45 & WL 208. REPAIRED BEAM PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 324, STR 17R. REPAIRED SKIN PER BFG ER.

Part: WEB — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND LOGITUDINAL BEAM WEB CRACKED AT BS 706-708, BL 0 & LBL 25, WL 203. REPAIRED WEB PER BFG ER.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND FRAME SHEAR TIE CORRODED AT BS 480, LBL 10 & WL149. R&R SHEAR TIE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND PRESS WEB CRACKED AT BS 664, LBL 33 & WL 202. REPAIRED WEB PER SWA T1-353-046.

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND BILGE INTERNAL SKIN CORRODED AT BS 500C+19, RBL 5. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (AFT CABIN) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND BS 867 FUSELAGE FRAME CRACKED BETWEEN STRS 8R-9R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 312, BETWEEN LBL 12 & RBL 12. REPAIRED FLOORBEAM PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA CRACKS AT VERTICAL BEAM WEB AT BS180, RBL 17.1, WL 183 & WL 226. R&R VERTICAL BEAM WEB PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 66. REPAIRED FRAME PER BFG T1-153-018.

Part: FITTING — CRACKED (RH WING) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND RH MLG BEAM FITTING CRACKED AT D HOLE. REPAIRED FITTING PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED BETWEEN STR'S 8L & 9L, BS 490, BS 807, BS 827, BS 787 & BS 767. REPAIRED FRAMES PER BFG ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND BILGE FRAME SHEAR TIE CORRODED AT BS 500D, RBL 5. R&R SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED BETWEEN STR'S 8R & 9R, BS 380, BS 767, BS 480, BS 440 & BS 807. REPAIRED FRAMES PER BFG ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CABIN FLOORBEAM UPPER T-CHORD CORRODED AT BS 1016, LBL 10. REPAIRED CHORD.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 440, STR'S 4L & 4R, BS 380, STR 8L & BS 360, STR 4L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 66 & WL 200. REPAIRED FRAME PER SWA T1-153-018.

Part: LENS — BROKEN (CABIN) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D-CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN AT LT OVERWING EXIT. REMOVED AND REPLACED EXIT LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 312, BETWEEN LBL 12 & RBL 12. REPAIRED FLOORBEAM CHORD PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER 25L CORRODED AT BS 352. REPAIRED STR PER SRM.

Part: WEB — CANNING (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL WEB IS OIL CANNED AT BS 312, RBL 28 & WL 206. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D-CHECK, FOUND UPPER FLOORBEAM CHORD CORRODED AT BS 328, BETWEEN RBL 0-65, WL 208. REPAIRED FLOORBEAM CHORD PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 947.5, LBL 52. REPAIRED CHORD PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.1 & WL 225. REPAIRED WEB PER BFG ER.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL WEB STIFFENER CORRODED AT BS 328, RBL 45 & WL 207. REPAIRED STIFFENER PER SRM.

Part: WEB — CHAFED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D CHECK, FOUND LH OVERWING EMERGENCY CUT OUT SILL WEB CHAFED AT BS 635 & 643, WL 221. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,022 hrs · 36,719 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED 2 EA AT BS 559, STR 11R & BS 767, STR 22R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: MOTOR — INOPERATIVE (MLG W/W) · airframe 45,879 hrs · 35,803 cycles

DECLARED EMERGENCY. DURING APPROACH, FLAPS WOULD NOT EXTEND BEYOND POSITION 1. REMOVED AND REPLACED FLAP DRIVE HYDRAULIC MOTOR PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 44,778 hrs · 34,887 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE AT FLOOR. SECURED MOUNT BRACKET PER MM.

Part: STRUCTURE — WORN (ELEVATOR TAB) · airframe 44,778 hrs · 34,887 cycles

DURING SCHEDULED C2 CHECK, FOUND RT ELEVATOR TRIM TAB INBOARD ATTACH HINGE WORN. REMOVED AND REPLACED TRIM TAB PER MM.

Part: COVER — LOOSE (CABIN) · airframe 44,778 hrs · 34,887 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK AFT OF SEAT 23 LOOSE. SECURED TRACK PER MM.

Part: COVER — MISSING (CABIN) · airframe 43,934 hrs · 34,144 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: BEAM — CORRODED (RT MLG) · airframe 43,732 hrs · 33,961 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG STABILIZER BEAM AFT LUGS CORRODED. REMOVED AND REPLACED STAB BEAM PER MM.

Part: WIRE — BROKEN (RT MLG WW) · airframe 43,595 hrs · 33,846 cycles

AIR TURNBACK. LANDING GEAR LEVER WOULD NOT MOVE PAST OFF POSITION UNTIL THE LOCK OVERRIDE TRIGGER USED. REPAIRED BROKEN WIRING AT S106 AIR SENSING SAFETY SWITCH.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,588 hrs · 33,840 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT AND RT SIDE CHORDS CRACKED. REPAIRED CHORD SECTIONS PER SWA SPECIAL ITEMS 10975-53 AND 10976-53.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,588 hrs · 33,840 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 188 LT FRAME CRACKED, WL 207. REPAIRED FRAME SECTION PER SRM.

Part: VALVE — INOPERATIVE (MLG WW) · airframe 43,520 hrs · 33,779 cycles

DECLARED EMERGENCY, A-SYS HYD FAILED DURING APPROACH. REMOVED AND REPLACED A-SYS HYD MODULE CHECK VALVE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 43,070 hrs · 33,402 cycles

DURING SCHEDULED C4 CK, FOUND EEPLS TRACK COVER CRACKED AT ROW 1. REMOVED AND REPLACED TRACK COVER PER MM.

Part: BATTERY — INOPERATIVE (CABIN)

EEPLS INOP AT FWD END AND FWD SERVICE DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EEPLS BATTERY PACK.

Part: SKIN — CRACKED (CARGO DOOR)

DURING SCHEDULED C3 CHECK, FOUND AFT CARGO DOOR OUTER SKIN CRACKED AT HANDLE CUT OUT. REPAIRED SKIN PER SWS RA NR 1-352-0343.

Part: LINE — LEAKING (NLG WW)

AIR TURNBACK, AFTER TAKEOFF, NLG WOULD NOT RETRACT. REMOVED AND REPLACED DOWNLOCK ACTUATOR HYDRAULIC LINE.

Part: LEVER — MALFUNCTIONED (LANDING GEAR)

AIR TURNBACK, LANDING GEAR LEVER WOULD NOT GO INTO UP POSITION AFTER TAKEOFF. PERFORMED LANDING GEAR RETRACTION TEST AND LANDING GEAR SAFETY SENSOR TEST PER MM. OPS CK GOOD.

Part: CONTROLLER — MALFUNCTIONED (E&E COMPT)

AIR TURNBACK, DURING FLIGHT AT 37,000 FEET, CABIN ALTITUDE WARNING HORN SOUNDED ALERTING THE CABIN ALTITUDE WAS 10,000 FT. DECLARED EMERGENCY LANDING. CABIN ALTITUDE NEVER GOT ABOVE 10,000 FT AND THE DESCENT WAS NORMAL. INSPECTED ALL DOOR PRESS SEALS, PRESS DUCTINGS, C/W BITE CHECK ON PRESS CONTROLLER, PRESSURIZED ACFT AND PERFORMED LEAK CHECK. NO LEAKS FOUND AND PRESS SYSTEM OP CHECKED GOOD. LATER AT HOU, REMOVED AND REPLACED PRESS RATIO AUTO CONTROLLER PER MM.

Part: PSU — DEPLOYED (ROW 18 DEF)

DIVERTION, DURING CRUISE, PAX O2 MASKS DEPLOYED AT ROW 18 DEF (DIVERTION FROM LAX). DEFERRED PER MEL AND LATER AT HOU. REMOVED AND REPLACED PSU PER MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD ENTRY AND SERVICE DOORS. RELAMPED PER MM.

Part: SKIN — CRACKED (NR 4 LE SLAT)

DURING SCHEDULED 1/4D CHECK, FOUND NR 4 SLAT 2 EA CRACKS AT LAST ROW OF RIVETS JUST OUTBOARD OF ACTUATOR ROD END. REPAIRED PER BOEING DRAWING 65C30133 AND ER 99-5204.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND 3EA CRACK AT BS 178 BULKHEAD, BETWEEN RBL1-RBL7. REPAIRED PER SRM.

Part: SCREW — MISSING (LT EMER EXIT EEL)

DURING SCHEDULED 1/4D CHECK, FOUND LEFT OVERWING EXIT SIGN LAMP RETAINING SCREW MISSING. REMOVED AND REPLACED SCREW PER MM.

Part: STEERING — FROZEN (NLG)

ON LANDING WHILE TRYING TO CLEAR RWY THE NWS TILLER WOULD NOT MOVE EITHER DIRECTION. AFTER APPLYING EXCESSIVE FORCE, WAS ABLE TO STEER A/C TO TUG FOR TOW IN. IT WAS EXTREMELY STIFF AND HAD A GRINDING FEEL. DUE TO WATER ACCUM ON NOSE GEAR STEERING FROZEN AT ALTITUDE, LUBRICATED NOSE GEAR PER M/M. TAXIED A/C, OP CK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND OVER HEAD EMERGENCY LIGHT INOP, RT SIDE 4E. RELAMPED PER BOEING MM.

Part: CONTROLLER — FAILED (CABIN)

AIRCRAFT ROUTED FROM MCO TO PVD DIVERTED TO BWI. WHILE CRUSING AT FL 370, CABIN ALT WARNING HORN SUDDENTLY CAME ON, CABIN PRESSURIZATION WAS RAPIDLY CLIMBING THROUGH 10,000 FT. EMERGENCY DESCENT COMMENCED, OUTFLOW VALVE CLOSED MANUALLY. PACKS WERE PUT ON HIGH, THE CABIN STAB PASSING 28,000 FT A/C LEVELED AT 23,000 FT. PRESSURIZATION THEN MAINTAINED USING STANDBY MODE. FLIGHT ATTENDANT REPORTED AIR RUSHING OUT REAR OF A/C BY THE DOORS. CABIN ALT MAXED OUT AT 11,000 FT, SO MASK DID NOT DROP. A/C MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER AND PRESSURIZATION CONTROL PANEL AND ACCOMPLISHED SYSTEM TESTS PER BOEING MM. REPAIRED PER BOEING SRM.

Part: HYD MODULE — FAILED (RIGHT)

WHEN RT PACK TURNED ON CABIN AND COCKPIT FILLED WITH SMOKE. SMOKE CONTINUED WITH APU BLEED ON OR OFF. APU INOP DUE TO OIL SMELL IN CABIN WITH PACKS ON. REMOVED AND REPLACED HYD PRESSURIZATION MODULE PER BOEING MM. REMOVED AND REPLACED WATER SEPARATOR BAGS PER BOEING MM. LK AND CK GOOD .

Part: FRAME — DAMAGED (BS 1064)

DURING SCHEDULED C4 CHECK, FOUND Z-FRAME AT BS 1064 APU BLEED CUTOUT HOLE, DAMAGED 7 AROUND RADIUS. REPAIRED PER SWA RA 1-353-1797.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED CHARGER AND BATTERY PER BOEING M/M.

Part: GCU — INOPERATIVE (NR 1 ENGINE)

EN ROUTE, NR 1 ENGINE GENERATOR DROPPED OFF LINE. APU GEN WAS ALREADY ON MEL. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NR 1 GENERATOR CONTROL UNIT PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT AT MID CABIN AREA INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: STRAP — CRACKED (BS 344)

DURING SCHEDULED BC1 CHECK, FOUND FLOORBEAM STRAP AT BS 344 IN E/E BAY CRACKED LEFT SIDE. REPAIRED PER BOEING SRM.

Part: LAVATORY — REQD SERVICE (CABIN)

DURING CLIMBOUT, CREW NOTED BLUE WATER FROM FORWARD LAV WAS LEAKING AND FLOWING DOWN CENTER AISLE. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. DRAINED AND RESERVICED FWD LAVATORY PER BOEING M/M, NO DEFECTS NOTED.

Part: SOCKET — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT SOCKET PER BOEING M/M.

Part: LAMP — INOPERATIVE (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE, JUST AFT OF FORWARD SERVICE DOOR. RELAMPED PER BOEING M/M.

Part: SLIDE — EXPIRED DATE (PAX DOOR)

DURING SCHEDULED A2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE CLOSE TO EXPIRATION DATE. REPLACED SLIDE ASSEMBLY PER BOEING M/M.

Part: SKIN — DENTED (BS 500)

DURING SCHEDULED D-CHECK, FOUND 2 FUSELAGE SKIN DENTS 2 INCHES APART, AT BS 500C BETWEEN S26 AND 25L. INSTALLED REPAIR PER BOEING SRM.

Part: SKIN — DENTED (BS 337)

DURING SCHEDULED D-CHECK, FOUND A FUSELAGE SKIN DENT, AT BS 337 AT S25. INSTALLED REPAIR PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED D-CHECK, FOUND TOP CHORD OF FLOORBEAM CORRODED AT BS 344, LBL 7 AND AT RBL 1, WL 208. REPLACED DAMAGED SECTIONS PER BOEING SRM.

Part: SILL — CORRODED (AFT SERVICE DOOR)

DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR MOPSILL CORRODED AT BS 913 TO 987, RBL 53, WL 208. REPLACED PER BOEING SRM.

Part: SILL — CORRODED (PAX DOOR)

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR MOPSILL CORRODED AT BS 639, LBL 55, WL 208. REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 204-312)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORTS CORRODED AT BS 277 TO 204, LBL 11, WL 208, AT BS 294 TO 312, LBL 11 AND RBL 11, WL 208. REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 847-867)

DURING SCHEDULED D-CHECK, FOUND WEB FLOOR SUPPORT CORRODED FROM BS 847 TO 867, WL 156, RBL 26. REPLACED PER BOEING SRM.

Part: BULKHEAD ANGLE — CORRODED (BS 520)

DURING SCHEDULED D-CHECK, FOUND FLOOR TO AFT BULKHEAD SUPPORT ANGLE CORRODED AT BS 520, LBL 24 TO RBL 24. REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 270)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 270 AND AT BS 947.5, LBL 6 TO 17. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.