N694SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 96,947 hrs · 67,164 cycles

SKIN CRACKED AT BS 380, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 96,947 hrs · 67,164 cycles

SKIN CRACKED AT BS 500C+16, STRINGER 7R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 96,947 hrs · 67,164 cycles

SKIN CRACKED AT BS 908, STRINGER 8R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 96,947 hrs · 67,164 cycles

SKIN CRACKED AT BS 500B+3, STRINGER 3L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 96,947 hrs · 67,164 cycles

SKIN CRACKED AT BS 500D+6, STRINGER 8L. REPAIRED SKIN IAW EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 96,019 hrs · 66,469 cycles

R1 COCKPIT WINDOW PANE ARCED. R & R R1 WINDOW ASSEMBLY IAW MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 95,902 hrs · 66,382 cycles

AFT PRESS BULKHEAD CHORD CRACKED AT STATION 1016, STRINGER 6L. REPAIRED CHORD IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 95,902 hrs · 66,382 cycles

AFT PRESS BULKHEAD CHORD CRACKED AT STATION 1016, STRINGER 6R. REPAIRED CHORD IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 95,789 hrs · 66,294 cycles

R1 DOOR SLIDE DISLODGED. REPOSITIONED SLIDE IAW MM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 95,246 hrs · 65,922 cycles

PRESSURE BULKHEAD ATTACH ANGLE CRACKED AT BS 1016, RBL 16. R & R ANGLE IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 95,246 hrs · 65,922 cycles

PASSENGER CABIN UPPER FLOORBEAM T CAP CORRODED AT BS 1016, BETWEEN LBL 4 - 10. REPAIRED T CAP IAW SRM & EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 95,246 hrs · 65,922 cycles

AFT STRINGER FITTING CORRODED AT BS 1016, STRINGER 23R. R & R FITTING IAW SRM & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 95,246 hrs · 65,922 cycles

AFT PRESS BULKHEAD LOWER FRAME CORRODED AT BS 1016, BETWEEN STRINGER 26R - 22R. REPAIRED FRAME IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 94,915 hrs · 65,693 cycles

R1 DOOR OVERHEAD EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 94,605 hrs · 65,491 cycles

L1 DOOR EMER LIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,602 hrs · 65,489 cycles

LEFT AFT CABIN EMER DOOR LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,602 hrs · 65,489 cycles

FORWARD GALLEY AREA EMER LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 94,602 hrs · 65,489 cycles

LEFT EMER EXIT EXTERIOR LIGHT BULB INOPERATIVE. R & R BULB IAW MM.

Part: SUPPORT ARM — CRACKED (LT WING) · airframe 94,602 hrs · 65,489 cycles

LEFT WING NR 1 A FRAME FAIRING SUPPORT ARM CRACKED. R & R SUPPORT ARM IAW CMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

CENTER WING SECTION FLOORBEAM LOWER CHORD CRACKED AT BS 664 LBL 24.8. REPAIRED CHORD IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

TIE CLIP CRACKED AT BS 351.2 STRINGER 18L. R & R TIE CLIP IAW SRM & DWG.

Part: SPLICE — CRACKED (RT WING) · airframe 94,602 hrs · 65,489 cycles

SPLICE ASSEMBLY CRACKED AT REAR SPAR ON LOWER SURFACE OF WING BETWEEN RSS 180 TO 210 RT SIDE. R & R SPLICE ASSEMBLY IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

ANGLE CRACKED AT BS 289 STRINGER 13R. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

ANGLE CRACKED BETWEEN BS 289 TO 288.5 STRINGER 12R. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

RIGHT SKIN CUT OUT CRACKED AT BS 291.5 WL 232.50. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

RIGHT SKIN CUT OUT CRACKED AT BS 291.5 WL 229.50. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

SKIN CUT OUT CRACKED AT BS 291.5 WL 233.50 RT SIDE. REPAIRED CUT OUT IAW EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 94,602 hrs · 65,489 cycles

RIGHT WING NR 8 FLAP TRACK TRANSMISSION ATTACHMENT CORRODED ON UPPER SURFACE. REPAIRED FLAP TRACK IAW CHM.

Part: FLAP — CRACKED (LT WING) · airframe 94,602 hrs · 65,489 cycles

LEFT WING OTBD FORE FLAP CRACKED INBD RIB AT WBL 355. R & R FORE FLAP IAW SRM & DWG.

Part: FLAP — CRACKED (LT WING) · airframe 94,602 hrs · 65,489 cycles

LEFT WING OTBD FORE FLAP CRACKED AT OTBD RIB AT WBL 355. R & R FORE FLAP IAW SRM & DWG.

Part: SLEEVE — CORRODED (TE FLAP) · airframe 94,602 hrs · 65,489 cycles

RIGHT WING NR 8 FLAP TRACK TRANSMISSION ATTACHMENT CORRODED AT NR 3 HOLE POSITION. REPAIRED SLEEVE IAW CMM.

Part: POST — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

FUSELAGE SKIN LT SIDE CABIN WINDOW POST C - D CRACKED AT BS 213.3 STRINGER 9L. REPAIRED POST IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

FRAME CRACKED AT BS 312 STRINGER 6L. REPAIRED FRAME IAW EO & EA.

Part: SLEEVE — CORRODED (TE FLAP) · airframe 94,602 hrs · 65,489 cycles

RIGHT WING NR 8 FLAP TRACK TRANSMISSION ATTACHMENT CORRODED AT NR 4 HOLE POSITION. REPAIRED SLEEVE IAW CMM.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 94,602 hrs · 65,489 cycles

RIGHT MAIN WW ANGLE CRACKED AT BS 680. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

FRAME CRACKED AT BS 500C BETWEEN STRINGER 20L TO 21L. REPAIRED FRAME IAW EO & EA.

Part: SKIN — CRACKED (RT WING) · airframe 94,602 hrs · 65,489 cycles

RIGHT WING LE SKIN AT KRUEGER FLAP SEAL DOOR CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

INNER CHORD CRACKED AT BS 351.2 STRINGER 17L. R & R CHORD IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 94,602 hrs · 65,489 cycles

LEFT WING LE SKIN AT KRUEGER FLAP SEAL DOOR CUT OUT CRACKED AT LES 213. REPAIRED SKIN IAW EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 94,602 hrs · 65,489 cycles

RIGHT WING NR 5 FLAP TRACK HOLE CORRODED. REPAIRED FLAP TRACK IAW EO & EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

BULKHEAD WEB CRACKED AT BS 1016 RBL 1. REPAIRED WEB IAW EO & EA.

Part: ANGLE — CRACKED (RT WING) · airframe 94,602 hrs · 65,489 cycles

RIGHT WING ANGLE CRACKED ON MLG STABILIZER BEAM, REAR SPAR. R & R ANGLE IAW SRM.

Part: RIB — CRACKED (LT WING) · airframe 94,602 hrs · 65,489 cycles

LEFT WING IN SPAR RIB WEB CRACKED AT WBL 198.60 BETWEEN STRINGER 5 & REAR SPAR. REPAIRED WEB IAW EO & EA.

Part: POST — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

LEFT WINDOW POST C - D CRACKED BETWEEN BS 211.8 TO 219.8. REPAIRED POST IAW EA.

Part: SUPPORT ANGLE — CRACKED (LT PYLON) · airframe 94,602 hrs · 65,489 cycles

LEFT PYLON SUPPORT ANGLE CRACKED AT BS 280.35. R & R ANGLE IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 94,602 hrs · 65,489 cycles

RIGHT WING WBL 114 RIB UPPER CHORD AT STRINGER 2 CRACKED. REPAIRED CHORD IAW EO & EA.

Part: WEB — CRACKED (RT WING) · airframe 94,602 hrs · 65,489 cycles

RIGHT WING FUEL TANK WEB CRACKED AT WBL 198.6 RIB, NEXT TO UPPER STRINGER 5. REPAIRED WEB IAW EO & EA.

Part: RIB — CRACKED (LT WING) · airframe 94,602 hrs · 65,489 cycles

LEFT WING WBL 114 RIB UPPER CHORD AT STRINGER 2 CRACKED. REPAIRED CHORD IAW EO & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE WEB CRACKED AT BS 294.5 STRINGER 7L. R & R WEB IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

SKIN CRACKED AT BS 259.5 + 6 STRINGER 9L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

FUSELAGE SKIN CRACKED AT BS 559+3 STRINGER 10R. REPAIRED SKIN IAW EO & EA.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 94,602 hrs · 65,489 cycles

RIGHT WING NR 7 SUPPORT BRACKET LOCATED ON PLATE TRANSITION CRACKED. R & R BRACKET IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 94,602 hrs · 65,489 cycles

LEFT WING NR 1 SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 94,602 hrs · 65,489 cycles

RIGHT WING NR 8 SUPPORT BRACKET CRACKED LOCATED ON PLATE TRANSITION. R & R BRACKET IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (RT PYLON) · airframe 94,602 hrs · 65,489 cycles

RIGHT PYLON ACCESS PANEL 5843R SUPPORT ANGLE CRACKED AT STATION 366. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (RT PYLON) · airframe 94,602 hrs · 65,489 cycles

NUMBER 2 ENG PYLON TRACK INTERFACE FITTING CRACKED ON INTERNAL STRUCTURE OF ACCESS PANEL 5869R & NAC STATION 344. REPAIRED FITTING IAW EA & EO.

Part: PLATE — CORRODED (CABIN) · airframe 94,602 hrs · 65,489 cycles

R2 DOOR FLOOR ATTACH FITTING PLATE & HARDWARE CORRODED ON LT & RT SIDE OF ESCAPE SLIDE. R & R PLATE ASSEMBLY IAW MM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 94,602 hrs · 65,489 cycles

LEFT WING NR 2 SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: PLATE — CORRODED (CABIN) · airframe 94,602 hrs · 65,489 cycles

R1 DOOR FLOOR ATTACH FITTING PLATE & HARDWARE CORRODED ON LT & RT SIDE OF ESCAPE SLIDE. R & R PLATE ASSEMBLY IAW MM.

Part: WEB — CRACKED (RT PYLON) · airframe 94,602 hrs · 65,489 cycles

RIGHT PYLON ACCESS PANEL 5843R WEB CRACKED AT STATION 354. R & R WEB IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 94,602 hrs · 65,489 cycles

RIGHT WING INBD AFT FLAP DELAMINATED ON UPPER SKIN OTBD END. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

SKIN CRACKED AT BS 259.5 + 11, STRINGER 9L. REPAIRED SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 94,602 hrs · 65,489 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 672 RBL 41.5. REPAIRED WEB IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 19L TO 20L. REPAIRED FRAME IAW EO & EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 94,602 hrs · 65,489 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 672 RBL 42.5. REPAIRED WEB IAW EO & EA.

Part: ANGLE — CRACKED (TE FLAP) · airframe 94,602 hrs · 65,489 cycles

LEFT WING NR 3 FLAP TRACK FAIRING ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 94,602 hrs · 65,489 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 672 RBL 38.5. REPAIRED WEB IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

RIGHT FRAME INNER CHORD CRACKED AT BS 639 WL 208. REPAIRED FRAME IAW EO & EA.

Part: PLATE — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

E & E COMPARTMENT PLATE CRACKED AT BS 328 RBL 31.6. R & R PLATE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

SHEAR TIE CORRODED AT BS 827 BETWEEN STRINGER 26R TO 25R. R & R SHEAR TIE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

FUSELAGE SKIN CRACKED AT STATION 727C + 14 STRINGER 1. REPAIRED SKIN IAW SRM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

E & E COMPARTMENT PLATE CRACKED AT BS 328 RBL 45.5. R & R PLATE IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

CHORD CRACKED AT BS 727 STRINGER 18A RT SIDE IN AFT LOWER FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A LT AT AFT LOWER FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A LT 8 O'CLOCK UPPER FWD FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A RT SIDE. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 662 LBL 24.5 DOWNWARD DIRECTION CTR WING BOX. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

FUSELAGE SKIN CRACKED AT BS 259.5 + 6, STRINGER 9L. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A LT SIDE, 8 O'CLOCK POSITION. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

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

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 94,602 hrs · 65,489 cycles

CHORD CRACKED AT BS 727 STRINGER 18A LT AT FWD LOWER FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: SLIDE — UNSECURE (R2 DOOR) · airframe 94,542 hrs · 65,442 cycles

R2 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: SKIN — CRACKED (GALLEY DOOR) · airframe 94,391 hrs · 65,323 cycles

FORWARD GALLEY DOOR EXTERIOR SKIN CRACKED 4 INCHES FROM BOTTOM & 7 INCHES FROM FWD EDGE. R & R DOOR IAW AMM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 94,391 hrs · 65,323 cycles

R1 DOOR EXTERIOR SKIN CRACKED. R & R DOOR IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,069 hrs · 65,089 cycles

FRAME CRACKED AT BS 277, BETWEEN STRINGER 14R TO 15R. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,069 hrs · 65,089 cycles

SKIN CRACKED AT BS 280, STRINGER 9L. REPAIRED SKIN IAW EA.

Part: BRACKET — CRACKED (RT NACELLE) · airframe 93,662 hrs · 64,801 cycles

RIGHT WING NR 6 FLAP CRACKED ANGLE BRACKET INSIDE RT AFT NACELLE AT NACELLE STATION 267 INBD OF NR 6 FLAP TRANS. R & R BRACKET IAW SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 94,602 hrs · 65,489 cycles

NUMBER 4 LE SLAT DELAMINATED AT OTBD AFT WEDGE. REPAIRED SLAT IAW SRM.

Part: SLIDE — FAILED (R1 DOOR) · airframe 92,756 hrs · 64,183 cycles

R1 DOOR EMERGENCY EVAC SLIDE FAILED DEPLOYMENT TEST. R & R SLIDE IAW MT.

Part: COVER — LOOSE (CABIN) · airframe 92,617 hrs · 64,090 cycles

FWD GALLEY EMERGENCY EXIT LIGHT COVER LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 92,588 hrs · 64,065 cycles

SKIN CRACKED BETWEEN BS 711 TO BS 714, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 92,588 hrs · 64,065 cycles

SKIN CRACKED BETWEEN BS 727C+14 TO BS 727C+15.8, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 92,536 hrs · 64,027 cycles

L1 DOOR SLIDE GAUGE HARD TO READ. REPOSITIONED SLIDE APR MT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,901 hrs · 63,540 cycles

FRAME CRACKED AT BS 706, BETWEEN STRINGER 8L & STRINGER 9L. R & R FRAME IAW EA.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 91,901 hrs · 63,540 cycles

L1 DOOR FWD FRAME CRACKED AT LOWER FWD CORNER STOP FITTING. R & R FRAME IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,901 hrs · 63,540 cycles

FRAME CRACKED AT BS 706, BETWEEN STRINGER 8R & STRINGER 9R. R & R FRAME IAW EA.

Part: LENS — CRACKED (CABIN) · airframe 91,901 hrs · 63,540 cycles

RT OVERHEAD EMERGENCY EXIT LIGHT LENS COVER CRACKED. R & R COVER IAW AMM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 91,760 hrs · 63,435 cycles

AT CRUISE AT FL 300, FLIGHT ATTENDANTS REPORTED AN ELECTRICAL SMELL & LIGHT WISPY SMOKE IN REAR OF CABIN. TURNED OFF GASPER FAN & THE SMOKE SMELL IMMEDIATELY WENT AWAY. R&R GASPER FAN IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 91,552 hrs · 63,264 cycles

FORWARD GALLEY OVERHEAD EMERGENCY EXIT SIGN BROKEN. R&R SIGN IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 91,370 hrs · 63,131 cycles

FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS ASSEMBLY MISSING. INSTALLED LENS IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 91,126 hrs · 62,955 cycles

RT WING INBD AFT FLAP LOWER SURFACE AT OUTBD EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 91,126 hrs · 62,955 cycles

LT WING INBD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 91,126 hrs · 62,955 cycles

RT WING INBD AFT FLAP T/E UPPER SURFACE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 90,701 hrs · 62,651 cycles

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

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 90,679 hrs · 62,631 cycles

DIVERSION/DECLARED EMERGENCY. AFTER EXTENDING THE LANDING GEAR THERE WAS NO DOWN AND LOCKED INDICATION. LIGHTS DID NOT TEST. C/W QRH. AFTER LANDING, NOTICED MASTER CAUTION SEC 4 C/B TRIPPED. RESET C/B'S AND OPS CHECKED GOOD PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 90,428 hrs · 62,454 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,142 hrs · 62,262 cycles

FUSELAGE SKIN CRACK AT UPPER FWD CORNER OF AIRSTAIR CUTOUT. CRACK MEASURES 1.25". VERIFIED BY HFEC. REPAIRED FUSELAGE SKIN CRACK AT UPPER FWD CORNER OF AIRSTAIR CUTOUT PER SRM 53-10-01-2R-13 DETAIL II.

Part: MOUNT — CRACKED (RT WING) · airframe 89,696 hrs · 61,928 cycles

RIGHT WING - NR 6 FLAP TRACK FAIRING MOUNT ON RT ENGINE PYLON LWR AFT STRUCTURE IS CRACKED. REMOVED & REPLACED RT WING NR 6 FLAP TRACK FAIRING MOUNT PYLON LOWER AFT STRUCTURE P/N 313A1355 IAW B737 SRM 51-40-05; SRM 51-40-02.

Part: RIB — CRACKED (FLAP FAIRING) · airframe 89,696 hrs · 61,928 cycles

LEFT WING 3 FLAP TRACK FAIRING CRACKED. REMOVED AND REPLACED RIB IAW SRM.

Part: BOLT — CORRODED (SLAT TRACK) · airframe 89,696 hrs · 61,928 cycles

LT WING NR 2 SLAT OUTBOARD TRACK FWD UPPER BOLT IS CORRODED AND IS MISSING PLATING. REMOVED & REPLACED NR 2 SLAT OUTBOARD TRACK FWD UPPER BOLT IAW B737 AMM 27-81-21.

Part: BOLT — CORRODED (SLAT TRACK) · airframe 89,696 hrs · 61,928 cycles

LEFT WING NR 2 SLAT OUTBOARD TRACK UPPER AFT BOLT IS CORRODED. REMOVED & REPLACED NR 2 SLAT OUTBOARD TRACK UPPER AFT BOLT IAW B737 AMM 27-81-21.

Part: BOLT — CRACKED (LE SLAT TRACK) · airframe 89,696 hrs · 61,928 cycles

RIGHT WING 5 SLAT I/B TRACK O/B SIDE OF STRUCTURE HAS LOOSE BOLT. SECURED BOLT IAW MM.

Part: BOLT — CORRODED (SLAT TRACK) · airframe 89,696 hrs · 61,928 cycles

LEFT WING NR 2 SLAT INBOARD TRACK FWD LOWER BOLT IS CORRODED. REMOVED & REPLACED NR 2 SLAT INBOARD TRACK FWD LOWER BOLT IAW B737 AMM 27-81-21.

Part: BOLT — CORRODED (SLAT TRACK) · airframe 89,696 hrs · 61,928 cycles

LT WING NR 1 SLAT OUTBOARD TRACK AFT UPPER BOLT IS CORRODED AND IS MISSING. REMOVED & REPLACED NR 1 SLAT OUTBOARD TRACK AFT UPPER BOLT IAW B737 AMM 27-81-21.

Part: BOLT — CORRODED (SLAT TRACK) · airframe 89,696 hrs · 61,928 cycles

LEFT WING NR 2 SLAT OUTBOARD TRACK LOWER AFT BOLT IS CORRODED. REMOVED & REPLACED NR 2 SLAT OUTBOARD TRACK LOWER AFT BOLT IAW B737 AMM 27-81-21.

Part: BOLT — CORRODED (SLAT TRACK) · airframe 89,696 hrs · 61,928 cycles

LEFT WING NR 3 SLAT OUTBOARD TRACK AFT UPPER BOLT IS CORRODED AND MISSING PLATING. REMOVED AND REPLACED BOLT AT LEFT WING NR 3 SLAT O/B MAIN TRACK AFT UPPER IAW B737 AMM 57-54-01.

Part: BOLT — CORRODED (SLAT TRACK) · airframe 89,696 hrs · 61,928 cycles

LEFT WING NR 3 SLAT INBOARD TRACK FWD LOWER BOLT IS CORRODED. REMOVED AND REPLACED BOLT AT LEFT WING NR 3 SLAT I/B TRACK FWD LOWER IAW B 737 AMM 57-54-01.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 89,365 hrs · 61,688 cycles

R2 DOOR SLIDE GAUGE IS OUT OF POSITION IN VIEWING WINDOW. REPOSITIONED SLIDE ASSY PER MT.

Part: FLAP — DELAMINATED (RT WING) · airframe 89,365 hrs · 61,688 cycles

RIGHT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY IAW MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

RIGHT WING CENTER SECTION AFT BULKHEAD BS 663.75 CRACKED. REPAIRED BULKHEAD PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER CLIP CRACKED AT BS 348.2, STR 16L. REMOVED AND REPLACED CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FRAME LOWER ANGLE CRACKED AT BS 348.2, STR 16L. REMOVED AND REPLACED ANGLE IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER CORRODED BETWEEN BS 910 TO BS 967, STR 26L. REPAIRED STRINGER PER SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER CORRODED AT BS 970, STR 25L. REMOVED AND REPLACED STRINGER SECTION PER SRM AND DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FRAME INNER CHORD ATTACH CLIP CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER SPLICE CORRODED BS 908, STR 26L. REMOVED AND REPLACED SPLICE PER SRM.

Part: FASTENER — MISSING (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FORWARD ENTRY DOOR FRAME INNER CHORD FASTENER MISSING AT BS 348.2, STR 15L. REMOVED AND REPLACED CHORD IAW SRM, ER, & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FLOORBEAM WEB CRACKED AT BS 294, RBL 52. REPAIRED WEB PER ER AND EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

L1 DOOR LOWER WEB CORRODED BETWEEN BS 332 TO BS 335, LBL 56. REMOVED AND REPLACED WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER CLIP CRACKED AT BS 500D, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

SKIN PUNCTURED AT BS 727, STR 20L. REPAIRED SKIN PER ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FRAME CRACKED AT BS 1040, WL 306 TOP OF CROWN. REMOVED & REPLACED FRAME IAW SRM.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

L1 DOOR FUSELAGE SKIN CUTOUT UPPER DOOR LATCH ATTACH BRACKET CRACKED AT BS 309. REMOVED AND REPLACED BRACKET IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER CLIP CRACKED AT BS 685, STR 9R. REMOVED & REPLACED CLIP PER SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED SPLICE PER ER AND EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

R2 DOOR LOWER WEB CORRODED BETWEEN BS 927 TO BS 947.5, WL 208. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 4R. REMOVED AND REPLACED SPLICE PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FRAME CRACKED AT BS 500B, STR 17R. REPAIRED FRAME PER ER AND EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 89,365 hrs · 61,688 cycles

RIGHT HORIZONTAL STABILIZER FWD VERTICAL RIB STIFFENER CRACKED AT UPPER END STA 184.7. REMOVED AND REPLACED STIFFENER IAW E AND ER.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 89,365 hrs · 61,688 cycles

RIGHT HORIZONTAL STABILIZER FWD VERTICAL RIB STIFFENER CRACKED AT LOWER END STA.92.7. REMOVED AND REPLACED STIFFENER IAW E AND ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

SHEAR TIE CRACKED AT BS 500, STR 16L. REPAIRED FRAME PER ER AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER CORRODED AT BS 747, STR 22L. REPAIRED STRINGER IAW EA AND ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

SHEAR TIE CORRODED AT BS 360, BETWEEN STR 26L AND STR 27L. REPAIRED SHEAR TIE PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

SHEAR TIE CORRODED AT BS 928, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER ER & EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER CORRODED AT BS 907, STR 26L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

SHEAR TIE CORRODED AT BS 380, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER CLIP CRACKED AT BS 500C, STR 23L. REMOVED & REPLACED CLIP IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FRAME CORRODED AT BS 727E O/B OF RIGHT KEEL BEAM AFT SIDE. REPAIRED FRAME PER SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FRAME CORRODED AT BS 867, STR 27R. REPAIRED FRAME PER ER AND EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

SPLICE STRAP CORRODED BETWEEN BS 1006 TO BS 1028, LBL 3. REMOVED AND REPLACED STRAP IAW SRM & BOEING DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 947, LBL 53. REPAIRED CHORD PER ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FLOORBEAM CORRODED AT BS 1006, LBL 10. REPAIRED BEAM PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FRAME CRACKED AT BS 947, STR 18L. REMOVED AND REPLACED FRAME PER DWG AND SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

STRINGER CORRODED BETWEEN BS 270 TO BS 277, STR 22R. REPAIRED STRINGER PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FORWARD ENTRY DOOR THRESHOLD I/B Z-SUPPORT ANGLE CORRODED. REMOVED AND REPLACED Z-ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 709, RBL 25. REPAIRED WEB PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT AT FWD LOWER CORNER. REPAIRED SKIN PER ER AND EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FWD ENTRY DOOR THRESHOLD O/B "Z" SUPPORT ANGLE CORRODED. REMOVED AND REPLACED "Z" SUPPORT ANGLE PER DWG & SRM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

RIGHT CREASE BEAM WEB ATTACH ANGLE CORRODED AT BS 291, STR 17R. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

VERTICAL LONGITUDINAL FLOORBEAM ATTACH ANGLE CRACKED AT BS 727B, WL 207. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

LONGITUDINAL FLOORBEAM VERTICAL WEB CRACKED AT BS 660, WL 207. REPAIRED BEAM PER ER AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 709, LBL 25. REPAIRED WEB PER ER AND EA.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 89,365 hrs · 61,688 cycles

RIGHT SIDE NOSE WHEEL WELL CRACKED AT BS 245, RBL 15. REPAIRED NOSE WHEEL WELL IAW SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 89,365 hrs · 61,688 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT ASSEMBLY CRACKED. REMOVED AND REPLACED LIGHT ASSY PER AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

FUSELAGE SKIN AT FORWARD LAV SERVICE DOOR CUTOUT LOWER EDGE CORRODED BETWEEN BS 268 TO BS 272, STR 22R. REMOVED AND REPLACED SKIN PER SRM AND DWG.

Part: TEE FITTING — CORRODED (NLG WW) · airframe 88,672 hrs · 61,131 cycles

FWD E/E DOOR AND NOSE LANDING GEAR WHEEL WELL CORRODED UNDER LEVELING COMPOUND. REPAIRED "T" CHORD IAW EA AND AMM.

Part: FUSE — LEAKING (AC BAY) · airframe 88,664 hrs · 61,126 cycles

DURING CRUISE, SMELLED A FAINT ODOR OF CHLORINE. FLIGHT ATTENDANTS IN AFT GALLEY SMELLED IT STRONGLY & SAW IT WAS COMING FROM THE AFT GALLEY VENTS, DIVERTED AND DECLARED EMERGENCY. FLIGHT DECK CREW O2 WAS USED IN FLIGHT. FOUND NR 2 T/R FUSE ABOVE HEAT EXCHANGER LEAKING. SECURED EXCHANGER IAW AMM. REMOVED AND REPLACED RIGHT AND LEFT WATER SEPARATOR FILTERS IAW AMM. REMOVED AND REPLACED RECIRCULATION FILTER IAW M/M.

Part: SIGN — LOOSE (CABIN) · airframe 88,414 hrs · 60,937 cycles

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

Part: SPOILER — CRACKED (LT WING) · airframe 87,757 hrs · 60,436 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 4 GROUND SPOILER CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 87,757 hrs · 60,436 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: WIRE — EXPOSED (CABIN) · airframe 87,575 hrs · 60,297 cycles

R2 DOOR EMERGENCY EXIT LIGHT WIRES EXPOSED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BULKHEAD — CRACKED (BS 1016 S23R) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND BULKHEAD CRACKED AT BS 1016, S23R. REPAIRED BULKHEAD PER EA.

Part: SLAT — WORN (RT WING) · airframe 86,878 hrs · 59,794 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT I/B SLAT CAN WORN. REMOVED AND REPLACED NR 5 SLAT CAN PER MM.

Part: SLAT — WORN (RT WING) · airframe 86,878 hrs · 59,794 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT O/B SLAT CAN WORN. REMOVED AND REPLACED NR 5 SLAT CAN PER MM.

Part: SLAT — WORN (LT WING) · airframe 86,878 hrs · 59,794 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 L/E SLAT O/B SLAT CAN WORN. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 88,878 hrs · 59,574 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED ON O/B AFT END. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CRACKED (LE SLAT) · airframe 86,837 hrs · 59,757 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 3 SLAT O/B AUX TRACK FITTING COMMON TO LOWER SKIN CRACKED. REPAIRED FITTING PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 86,837 hrs · 59,757 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT LOWER T/E SKIN CRACKED AT I/B END. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS CRACKED AT ROW 12. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS CRACKED AT ROW 6. REMOVED AND REPLACED LENS PER MM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 86,626 hrs · 59,590 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT FUSE INOP. REMOVED AND REPLACED FUSE PER MM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 86,626 hrs · 59,590 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,659 hrs · 63,250 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 685+3, STR 10R. REPAIRED SKIN IAW EA.

Part: PUMP — FAULTY (NR 1 ENGINE) · airframe 86,021 hrs · 59,128 cycles

DECLARED EMERGENCY -- FLASHING MASTER CAUTION FOR NR 1 ENGINE DRIVEN HYDRUALIC PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. A SYSTEM HYDRAULIC QUANTITY DROPPED TO 1/4. REMOVED AND REPLACED NR 1 ENGINE DRIVER HYDRAULIC PUMP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,704 hrs · 58,883 cycles

DURING SCHEDULED MV2 CHECK FOUND, R2 DOOR EMERGENCY LIGHT BULB INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,704 hrs · 58,883 cycles

DURING SCHEDULED MV2 CHECK FOUND, L1 DOOR EMERGENCY LIGHT BULB INOP. RELAMPED PER MM.

Part: GASPER FAN — FAULTY (CARGO BAY) · airframe 85,405 hrs · 58,671 cycles

DECLARED EMERGENCY - FLIGHT ATTENDANT AND PASSENGER REPORTED,"BURNING ELECTRICAL" SMELL IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 85,298 hrs · 58,594 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM CRACKED AT BS 322, RBL 40. REPAIRED BEAM PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 85,298 hrs · 58,594 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN RBL 10 TO RBL 14. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 85,298 hrs · 58,594 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM CRACKED AT BS 314, RBL 26. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 85,298 hrs · 58,594 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN RBL 10 TO RBL 14. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 85,298 hrs · 58,594 cycles

DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, RBL 24.5. REPAIRED BEAM PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 85,298 hrs · 58,594 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT AFT BULKHEAD WEB CRACKED AT BS 663.75. REPAIRED WEB PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 89,365 hrs · 61,688 cycles

RIGHT WING CENTER SECTION AFT BULKHEAD BS 663.75 CRACKED. REPAIRED BULKHEAD PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 85,123 hrs · 58,461 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT EEPLS BROKEN AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 84,771 hrs · 58,204 cycles

RT OVERHEAD EMERGENCY EXIT LIGHT COVER MISSING AT ROW 12. REMOVED AND REPLACED COVER PER MM.

Part: ACTUATOR — BROKEN (SPOILER) · airframe 83,966 hrs · 57,586 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING NR 5 GROUND SPOILER BROKEN. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,830 hrs · 57,478 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, STR 21L. REPAIRED FRAME PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 83,830 hrs · 57,478 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REPAIRED SPLICE PER SRM.

Part: FRAME — CRACKED (BS 500B S20-21L) · airframe 83,830 hrs · 57,478 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 83,830 hrs · 57,478 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING UPPER T/E SUPPORT ANGLE CRACKED. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,477 hrs · 57,191 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 519, STR 28L. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 83,477 hrs · 57,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,477 hrs · 57,191 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 585.0, STR 10L. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 83,477 hrs · 57,191 cycles

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

Part: SPOILER — DELAMINATED (LT WING) · airframe 83,443 hrs · 57,163 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 3 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 81,863 hrs · 55,987 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 81,283 hrs · 55,563 cycles

L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. DID NO DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: LIGHT — LOOSE (CABIN) · airframe 81,112 hrs · 55,448 cycles

DURING SCHEDULED CV CHECK, FOUND RT EMERGENCY EXIT LOWER LIGHT LOOSE. SECURED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,807 hrs · 55,206 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FWD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 80,350 hrs · 54,838 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CORRODED AT BS 988, STR 27L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,350 hrs · 54,838 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 80,350 hrs · 54,838 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 400, BETWEEN STR 14L TO STR 13L. REMOVED AND REPLACED SHEAR TIE PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 80,350 hrs · 54,838 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500, BETWEEN STR 28L AND 28R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,350 hrs · 54,838 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,350 hrs · 54,838 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 1016, BETWEEN STR 26L TO STR 27L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 80,350 hrs · 54,838 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 6 SLAT I/B WEDGE LOWER SKIN DELAMINATED ON I/B END. REPAIRED WEDGE PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 80,350 hrs · 54,838 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOKS LOOSE. SECURED HOOKS PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 80,350 hrs · 54,838 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOKS LOOSE. SECURED HOOKS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,350 hrs · 54,838 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,350 hrs · 54,838 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,350 hrs · 54,838 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SR.

Part: BEAM — CRACKED (FUSELAGE) · airframe 80,350 hrs · 54,838 cycles

DURING SCHEDULED 24Y CHECK, FOUND STUB BEAM SUPPORT ANGLE CRACKED AT BS 639, LBL 46, WL 207. R&R STUB BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,917 hrs · 54,521 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 305, STR 18R. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 79,201 hrs · 54,024 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD EMERGECY EXIT LIGHT LENS MISSING AT ROW 19. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 79,082 hrs · 53,943 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE LIGHT LENS MISSING AT ROW 4. REPLACED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 78,976 hrs · 53,874 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 78,229 hrs · 53,362 cycles

DURING SCHEDULED SPV CHECK, AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 77,798 hrs · 53,028 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,798 hrs · 53,028 cycles

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

Part: STRUCTURE — CRACKED (NR 2 SLAT) · airframe 77,798 hrs · 53,028 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT LOWER INBOARD END. REPAIRED SLAT PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,269 hrs · 52,645 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BAR — CORRODED (RT WING) · airframe 76,605 hrs · 52,128 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING MLG STABILIZER BAR CORRODED. REMOVED AND REPLACED STABILIZER BAR PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 76,080 hrs · 51,727 cycles

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

Part: HINGE — WORN (LT ELEVATOR TAB) · airframe 75,180 hrs · 51,016 cycles

DURING SCHEDULED CABIN VISIT, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE ASSY PER SWA EA.

Part: HINGE — WORN (ELEVATOR TAB) · airframe 75,203 hrs · 51,038 cycles

DURING SCHEDULED CABIN VISIT CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,447 hrs · 50,405 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,447 hrs · 50,405 cycles

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

Part: GLOWSTRIP — WORN (CABIN) · airframe 74,317 hrs · 50,302 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT MID CABIN EELS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 74,317 hrs · 50,302 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT AFT CABIN EELS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: STRUCTURE — CRACKED (RT WING SLAT) · airframe 74,307 hrs · 50,294 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SPAR — CRACKED (RT WING) · airframe 74,307 hrs · 50,294 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING AFT SPAR CASTING CRACKED AT STA 228. REMOVED AND REPLACED AFT SPAR CASTING PER SRM.

Part: STRINGER — CORRODED (BS 1006-1016) · airframe 74,307 hrs · 50,294 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 26R CORRODED BETWEEN BS 1006 AND BS 1016. REMOVED AND REPLACED STRINGER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,307 hrs · 50,294 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 3 TO LB 5. REPAIRED FLOORBEAM PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 74,307 hrs · 50,294 cycles

DURING SCHEDULED 22Y CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT BS 259, RBL 7.75 TO LBL 7.75. REPAIRED CEILING PANEL PER ACO.

Part: SLAT — CRACKED (RT WING) · airframe 74,307 hrs · 50,294 cycles

DURING SCHEDULED 22Y CHECK, FOUND RIGHT WING NR 5 L/E SLAT CRACKED AT INBOARD END. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,307 hrs · 50,294 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,307 hrs · 50,264 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,307 hrs · 50,294 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,307 hrs · 50,294 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,307 hrs · 50,294 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: LENS — CRACKED (EMERGENCY LIGHTS) · airframe 74,055 hrs · 50,105 cycles

DURING SCHEDULED C2 CHECK, FOUND LT LOWER AFT EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 73,484 hrs · 49,684 cycles

DURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STAB UPPER SKIN CORRODED AT REAR SPAR STA 198. REMOVED AND REPLACED HORIZONTAL STAB PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED RADIO ALTIMETER ANTENNA CUTOUT BS 406, RBL 1.5. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 26L. REPAIRED SKIN PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 727, STR 22R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 908, STR 7L. REPAIRED FRAME SECTION PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, LBL 65. REPAIRED FRAME SECTION PER ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 21L CRACKED AT BS 397. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23L CRACKED AT BS 517B. REPAIRED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 23R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 25L CORRODED AT BS 928. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 25L CRACKED AT BS 424. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (BS 639) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, RBL 65, WL 216. REPAIRED FRAME SECTION PER ER.

Part: STRINGER SPLICE — CRACKED (BS 540 S19L) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 540, STR 19L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (BS 947 S7L) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 947, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S8L) · airframe 73,480 hrs · 49,680 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 13R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 360 S13L) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13L. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 13L. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 13R. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 13R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500, STR 13L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 13L. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,480 hrs · 49,680 cycles

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

Part: STRINGER CLIP — CRACKED (BS 928 S21L) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 928, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 360 S14R) · airframe 73,480 hrs · 49,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: BOLT — WORN (ELEVATOR) · airframe 73,044 hrs · 49,330 cycles

DURING SCHEDULED C1 CHECK, LEFT ELEVATOR CONTROL TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT TAB NR 1 HINGE BOLT PER MM.

Part: SKIN — CRACKED (BS 500 S10R) · airframe 72,526 hrs · 48,917 cycles

DURING SCHEDULED THRU CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 10R. REPAIRED SKIN PER SWA EA.

Part: BOLT — WORN (LT ELEVATOR TAB) · airframe 72,189 hrs · 48,648 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR NR 1 TAB BOLTS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,189 hrs · 48,648 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, STR 23L. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,189 hrs · 48,648 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 72,189 hrs · 48,648 cycles

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

Part: GLOWSTRIP — WORN (CABIN) · airframe 72,189 hrs · 48,648 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 ABC. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,189 hrs · 48,648 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 900, STR 25L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 729D) · airframe 71,719 hrs · 48,310 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729D, STR 24R. REPAIRED SKIN PER SWA EA AND SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,567 hrs · 48,187 cycles

DURING SCHEDULED RON CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 4 DEF. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (BS 730E S23R) · airframe 71,567 hrs · 48,187 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 742) · airframe 71,048 hrs · 47,811 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 742, STR 19R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 291) · airframe 71,027 hrs · 47,797 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE FRAME CRACKED AT R1 DOOR CUTOUT, BS 291.5, STR 16R. MX FERRY TO DAL FOR REPAIRS. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 514D) · airframe 70,777 hrs · 47,603 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514D, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,209 hrs · 47,166 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 835, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,209 hrs · 47,166 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 25L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,209 hrs · 47,166 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,209 hrs · 47,166 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,209 hrs · 47,166 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 762, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,209 hrs · 47,166 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,209 hrs · 47,166 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,209 hrs · 47,166 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,209 hrs · 47,166 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,209 hrs · 47,166 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,209 hrs · 47,166 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 70,146 hrs · 47,122 cycles

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

Part: SKIN — CRACKED (BS 863) · airframe 70,090 hrs · 47,076 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 863, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 780) · airframe 70,090 hrs · 47,076 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 780) · airframe 70,090 hrs · 47,076 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 23L. REPAIRED SKIN PER SWA EA.

Part: COVER — LOOSE (L1 DOOR SLIDE) · airframe 69,518 hrs · 46,630 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED SLIDE COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,261 hrs · 46,422 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 741, STR 23L. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,261 hrs · 46,422 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,261 hrs · 46,422 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15L. REPAIRED SKIN PER SWA EA AND SRM.

Part: LENS — LOOSE (CABIN) · airframe 68,394 hrs · 45,700 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 67,578 hrs · 45,071 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,716 hrs · 44,409 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 737, BS 837, STRINGER 24L. REPAIRED SKIN SECTIONS PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,701 hrs · 44,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR LOWER AFT CORNER SKIN CUTOUT CRACKED. REPAIRED DOOR CUTOUT SKIN PER EA.

Part: FITTING — CRACKED (SRVC DOOR HINGE) · airframe 66,701 hrs · 44,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT SERVICE DOOR LOWER HINGE FITTING CRACKED. REMOVED AND REPLACED DOOR HINGE FITTING PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,701 hrs · 44,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR CUTOUT LOWER CORNER SKIN CRACKED. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,701 hrs · 44,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP AT BS 663, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,701 hrs · 44,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 765, STRINGER 21R, BS 870, STRINGER 23R. REPAIRED SKIN SECTIONS PER EA AND SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,701 hrs · 44,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 4 EACH CRACKS ON BULKHEAD SKIN AT BS 1016, PANELS 1, 2, 5 AND 7. REPAIRED BULKHEAD PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,701 hrs · 44,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 4 EACH FUSELAGE SKIN CRACKS FROM BS 570 TO BS 602, STRINGER 4L. REPAIRED SKIN SECTIONS PER SRM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 66,701 hrs · 44,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LEFT WING NR 1 L/E SLAT CRACKED. REPAIRED NR 1 L/E SLAT PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,701 hrs · 44,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH SHEAR TIES AT BS 500, RBL 12 AND LBL 19, CORRODED. REPAIRED SHEAR TIES PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,701 hrs · 44,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 690, STRINGER 4L, CRACKED. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,701 hrs · 44,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT FWD CARGO COMPT, BS 500, RBL 20, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 66,701 hrs · 44,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, LBL 32, CRACKED. REPAIRED WEB PER SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 66,701 hrs · 44,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR LOWER FWD STOP FITTING GUSSET CRACKED. REPAIRED GUSSET PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,590 hrs · 43,467 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 878, STRINGER 25L, BS 827, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,666 hrs · 42,761 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 FUSELAGE SKIN CRACKS AT BS 805, STR 22L AND BS 775, STR 23L. REPAIRED SKIN PER SRM.

Part: CABLE — MISROUTED (L2 & R2 DOORS) · airframe 64,666 hrs · 42,761 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH AFT DOOR EVACUATION SLIDE CABLES MISROUTED. REROUTED STRAP CABLES PER MM.

Part: FAN — FAULTY (FWD GALLEY) · airframe 64,521 hrs · 42,654 cycles

DURING CRUISE F/A REPORTS STRONG ACRID SMELL IN FORWARD GALLEY. GALLEY POWER WAS REMOVED SMELL WENT AWAY. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,325 hrs · 41,746 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, BELOW STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,023 hrs · 39,891 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727D AND BS 727E, ABOVE STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,023 hrs · 39,891 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 500D + 3 AT STR 12R AND BS 773 AT STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 60,305 hrs · 39,336 cycles

AFT ENTRY DOOR EMERGENCY EVACUATION SLIDE COMING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — LOOSE (AFT ENTRY DOOR) · airframe 59,292 hrs · 38,533 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. REMOVED AND REPLACED SLIDE PER MM.

Part: WEB — CORRODED (LT A/C BAY) · airframe 58,478 hrs · 37,818 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL WEB CORRODED AT BS 545, WL 152 AND LBL 41. REPAIRED WEB PER BFG ER.

Part: FLOORBEAM — CRACKED (AFT CABIN) · airframe 58,478 hrs · 37,818 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS727A PLUS 18, WL 208 AT LBL 47. REPAIRED FLOORBEAM PER BFG ER.

Part: FITTING — CORRODED (FWD ENTRY DOOR) · airframe 58,478 hrs · 37,818 cycles

DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,478 hrs · 37,818 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 520, STR 27L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,478 hrs · 37,818 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188 AT WL 210 LT. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 58,478 hrs · 37,818 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 907, STR 4R AND 4L. REPAIRED STR SPLICES PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,478 hrs · 37,818 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 777, LBL 67 AT WL 208. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,478 hrs · 37,818 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 334, STR 22L. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 58,478 hrs · 37,818 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED (2 EA) AT BS 636, WL 208, LBL 67 AND RBL 67. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,478 hrs · 37,818 cycles

DURING SCHEDULED D-CHECK, FOUND LOWER CHORD CRACKED AT BS 188, WL 209 RT. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,478 hrs · 37,818 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,478 hrs · 37,818 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L AND 15L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CAP — CRACKED (CABIN) · airframe 58,316 hrs · 37,681 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP CRACKED. REMOVED AND REPLACED END CAP PER MM.

Part: CHAIN — CHAFED (EVAC SLIDE) · airframe 58,316 hrs · 37,681 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE RELEASE CHAIN CHAFED. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 57,638 hrs · 37,163 cycles

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

Part: SLAT — CRACKED (RT WING) · airframe 57,583 hrs · 37,112 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT WEDGE LOWER SKIN CRACKED AT OUTBOARD END. REMOVED AND REPLACED NR 5 L/E SLAT PERMM.

Part: CAP — MISSING (CABIN) · airframe 57,583 hrs · 37,112 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,583 hrs · 37,112 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 INCHES AT BS 510, STR 12L. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 57,353 hrs · 36,936 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 57,019 hrs · 36,671 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 5 EA ) AT BS 178, RBL 5.0, WL 199 TO WL 218. REPAIRED WEB PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 57,019 hrs · 36,671 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL CHORD CRACKED .25 INCH LONG AT BS 178, WL 184 & LBL 5.8. REPAIRED CHORD PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,019 hrs · 36,671 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED ( 2 EA ) AT BS 180, RBL 17.1, WL 182 & WL 227. REPAIRED WEB PER SRM & SWA RA 1-353-2699.

Part: WEB — CRACKED (FWD FUSELAGE) · airframe 57,019 hrs · 36,671 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 179 VERTICAL BEAM WEB CRACKED, LBL 17.1, WL 225. R&R VERTICAL BEAM WEB PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 56,966 hrs · 36,624 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: HOOK — LOOSE (SERVICE DOOR) · airframe 56,574 hrs · 36,295 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED GIRT BAR HOOKS PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 56,574 hrs · 36,295 cycles

DURING SCHEDULED BC3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 56,196 hrs · 35,978 cycles

AIR TURNBACK, DECLARED EMERGENCY. LOSS OF A-SYSTEM HYDRAULIC PRESSURE. QUANTITY DROPPED TO ZERO AFTER RAISING THE GEAR AND FLAPS. REMOVED AND REPLACED WORN LT MLG ACTUATOR HYD LINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,634 hrs · 35,500 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED BEHIND AFT LOWER WING TO BODY FAIRING Rt SIDE. REPAIRED SKIN PER SRM.

Part: HINGE — BROKEN (L/E SLAT) · airframe 54,940 hrs · 34,921 cycles

DURING SCHEDULED C1 CHECK, FOUND INBOARD GROUND SPOILER OUTBOARD HINGE BROKEN IN TWO PIECES AND INBOARD HINGE BEARING WORN. REMOVED AND REPLACED GROUND SPOILER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,940 hrs · 34,921 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AND END CAP MISSING AT AFT GALLEY. RELAMPED AND INSTALLED END CAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,408 hrs · 33,656 cycles

EXTERNAL FUSELAGE SKIN CRACKS AT LEFT AFT SIDE OF WING-TO-BODY FAIRING AROUND EMERGENCY EXIT LIGHT. REPAIRED SKIN PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 52,985 hrs · 33,284 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 51,751 hrs · 32,245 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP IN AFT SECTION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: ACTUATOR — FAILED (LH MLG) · airframe 51,558 hrs · 32,182 cycles

AIR TURNBACK, LT MLG WOULD NOT STAY UP AND LOCKED. CONFORMED WITH MLG EXTENSION AND RETRACTION ADJUSTMENT. LATER ON AT HOU, R & R LT MLG LOCK AND RETRACT ACTUATORS PER MM.

Part: FRAME — CRACKED (FWD CARGO DOOR)

DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR CRACKED AT LOWER FRAME NEAR AFT END. REMOVED AND REPLACED DOOR ASSY PER MM.

Part: FRAME — CRACKED (AFT CARGO DOOR)

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR CRACKED AT LOWER FRAME NEAR AFT END. REMOVED AND REPLACED DOOR ASSY PER MM.

Part: SKIN — CRACKED (NR 5 LE SLAT)

DURING SCHEDULED 1/4D CHECK, FOUND NR 5 L/E SLAT SKIN CRACKED. REPAIRED SLAT PER SWA RA NR A57-0691 AND BOEING DRAWING.

Part: CLIP — CRACKED (BS 380)

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED, BS 380, STRINGER 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: PITOT TUBE — BIRD STRIKE (FWD FUSELAGE)

AIR TURNBACK---- DURING TAKEOFF, A MOMENTARY STALL WARNING INDICATED FOLLOWED BY 50 KNOTS DIFFERENCE IN AIR SPEED INDICATION. DISCOVERED BIRD STRIKE DEBRIS AT RT PITOT TUBE. REMOVED AND REPLACED RT PITOT TUBE ASSY, NO OTHER DAMAGES FOUND.

Part: ACTUATOR — MALFUNCTIONED (RT MLG)

AIR TURNBACK, CLIMBING AT 12000 FT, WITH GEAR HANDLE IN OFF POSITION, RT MAIN GEAR EXTENDED, BOTH RED AND GREEN LIGHTS ON, CYCLED GEAR, WITH GEAR DOWN HAD THREE GREEN LIGHTS. REMOVED AND REPLACED UPLOCK ACTUATOR, LEAK AND OPS CKECKED GOOD.

Part: SKIN — CRACKED (BS 767)

DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, NEAR S18R. REPAIRED PER BOEING SRM.

Part: SENSOR — MALFUNCTIONED (LT STALL WARNING)

AIR TURNBACK DUE TO STALL WARNING AT LIFTOFF. AIRSPEED NORMAL ON ALL INDICATIONS. WARNING QUIT AT TOUCHDOWN. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED LT AOA SENSOR AND OPS CK GOOD PER BOEING MM. AIRCRAFT RECERTIFIED TO CAT IIIA STATUS.

Part: SKIN — DAMAGED (BS 887)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 887, STR 21R. REPAIRED DAMAGE PER BOEING SRM.

Part: SKIN — DAMAGED (FUSELAGE)

UNITED AIRLINES BAG CART WAS BLOWN INTO SIDE OF A/C DURING STORM IN THE MIDDLE OF THE NIGHT. A V-SHAPED TEAR APPROX 5 INCHES BY 9 INCHES IN RT SIDE FUSELAGE APPROX 4 INCHES BEHIND AFT CARGO DOOR. REPAIRED DAMAGE PER BOEING SRM.

Part: BULB — FAILED (ROW 16)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT AT ROW 16 OVERHEAD BIN IS INOPERATIVE. RELAMPED PER BOEING MM.

Part: CIRCUIT BREAKER — FAILED (NR 1 GCU)

DURING ENGINE START SMOKE STARTED COMING OUT OF THE CIRCUIT BREAKER PANEL IN THE VICINITY OF THE G1 GENERATOR CONTROL UNIT. REMOVED AND REPLACED PER BOEING MM.

Part: STRINGER — CORRODED (BS 354)

DURING SCHEDULED D CHECK, FOUND STRINGER 25L CORRODED AT BS 354. REPAIRED PER TRAMCO 97-0483.

Part: ANGLE — CORRODED (BS 616-639)

DURING SCHEDULED D CHECK, FOUND L ANGLE CORRODED AT BS 616-639, AT S15L. REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 947)

DURING SCHEDULED D CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 947, AFT SIDE OF BULKHEAD AT S22L. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 1016)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 0-35. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 294.5)

DURING D CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5, LBL 2-12 AND RBL 20, WL 208. REPLACED SECTION AND SPLICE ANGLES PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 277-294)

DURING D CHECK, FOUND FLOOR SUPPORT CORROSION AT BS 277-294, LBL 11, WL 208. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 360)

DURING D CHECK, FOUND FLOORBEAM CORROSION AT BS 360, RBL 25-58, WL 208. REPAIRED PER T1-A53-014.

Part: SLIDE — LOW PRESS (PAX DOOR)

DURING WALKAROUND INSPECTION, FOUND LEFT AFT ENTRY DOOR ESCAPE SLIDE PRESSURE BELOW SERVICEABLE LIMITS. REPLACED SLIDE ASSEMBLY PER BOEING M/M.

Part: SKIN — DAMAGED (BS 1040)

DURING SCHEDULED C3 CHECK, FOUND DAMAGED TO FUSELAGE AT BS 1040, BETWEEN S27L AND 26L. REPAIRED PER BOEING SRM.