N371SW

Part: ACM — OVERSERVICED (AC BAY) · airframe 67,662 hrs · 56,355 cycles

DIVERSION, DECLARED EMER DURING CLIMB, ACRID SMELL DEVELOPED IN COCKPIT. FOUND RT AIR CYCLE MACHINE OVER SERVICED OIL IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A LT LOWER FWD FASTENER HOLE. R & R CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

LOWER STUB FRAME CRACKED AT BS 294. R & R STUB FRAME IAW SRM & DWG.

Part: LIGHT — DELAMINATED (CABIN) · airframe 67,642 hrs · 56,343 cycles

FORWARD EEPLS DELAMINATED. R & R EEPLS IAW MM.

Part: SIGN — DELAMINATED (CABIN) · airframe 67,642 hrs · 56,343 cycles

AFT LAVATORY MOUNTED EMER EXIT SIGN FASTENER ATTACH POINTS DELAMINATED. R & R SIGN IAW AMM.

Part: SIGN — CORRODED (CABIN) · airframe 67,642 hrs · 56,343 cycles

FORWARD LAVATORY MOUNTED EMER EXIT SIGN FASTENER ATTACH POINTS CORRODED. REMOVED & INSTALLED SIGN ASSEMBLY IAW AMM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

RIGHT AFT WING TO BODY FAIRING SUPPORT STRUCTURE HORIZONTAL SHELF OTBD CHORD CRACKED AT BS 727 STRINGER 19R. R & R CHORD IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

VERTICAL STIFFENER CRACKED AT BS 328 RBL 32. R & R STIFFENERS IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

R1 THRESHOLD WEB CORRODED. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

RIGHT CREASE BEAM CORRODED BETWEEN BS 946.5 TO967. R & R CREASE BEAM IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

BUTT JOINT STRINGER SPLICE CRACKED AT BS 908 STRINGER 4. R & R SPLICE IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

SKIN CRACKED AT BS 360 STRINGER 3R. REPAIRED SKIN IAW AAR & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

FLOORBEAM CORRODED AT BS 986.5 STRINGER 0. REPAIRED FLOORBEAM IAW SRM.

Part: BRACKET — CRACKED (TE FLAP) · airframe 67,642 hrs · 56,343 cycles

LEFT WING NR 3 FLAP FAIRING SPRING DOOR, SPRING RETAINER BRACKET CRACKED. R & R BRACKET IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO 328 RBL 32. R & R INTERCOSTAL IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

CREASE BEAM INBD CHORD CORRODED AT AFT GALLEY DOOR THRESHOLD. R & R CREASE BEAM IAW SRM DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

INTERCOSTAL ANGLE CRACKED AT BS 348 STRINGER 16L. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

AFT CARGO DOOR CUT OUT FWD LOWER CORNER FUSELAGE SKIN CRACKED FROM FASTENER TOWARDS SKIN EDGE. REPAIRED CUT OUT IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

FRAME SHEAR TIE ATTACH ANGLE CRACKED AT BS 294.5 STRINGER 13L. R & R ANGLE IAW DWG & SRM.

Part: HINGE — LOOSE (R2 DOOR) · airframe 67,642 hrs · 56,343 cycles

R2 DOOR UPPER HINGE LOOSE. REPAIRED HINGE IAW MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

FLOORBEAM CORRODED AT BS 344 BETWEEN RBL 2 TO LBL 10. REPAIRED BEAM IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A RT LOWER FWD FASTENER HOLE. R & R CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,642 hrs · 56,343 cycles

FORWARD CARGO COMPARTMENT FRAME CRACKED AT BS 520 BETWEEN STRINGER 20L TO 21L. REPAIRED FRAME IAW SRM.

Part: TAB — WARPED (RT AILERON) · airframe 67,443 hrs · 56,203 cycles

RIGHT WING AILERON TAB WARPED. R & R TAB IAW MM.

Part: FLAP — LOOSE (RT WING) · airframe 67,435 hrs · 56,198 cycles

RIGHT WING INBD AFT FLAP LOOSE. SECURED AFT FLAP IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 67,435 hrs · 56,198 cycles

LEFT WING INBD AFT FLAP DELAMINATED AT THE INBD LOWER CORNER. REPAIRED AFT FLAP IAW MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 67,411 hrs · 56,179 cycles

L1 DOOR FLOOR STRUCTURE CREASE BEAM CORRODED. R & R BEAM IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,411 hrs · 56,179 cycles

FUSELAGE SKIN CRACKED AT BS 500B+17 STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,411 hrs · 56,179 cycles

FUSELAGE SKIN CRACKED AT BS 500A+7 STRINGER 16L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,411 hrs · 56,179 cycles

FUSELAGE SKIN CRACKED AT BS 460+4 STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,411 hrs · 56,179 cycles

FUSELAGE SKIN CRACKED AT BS 967+11 STRINGER 21L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 66,091 hrs · 55,245 cycles

LT WING LE SKIN CRACKED AT WS 564.50. REPAIRED LE IAW SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 66,091 hrs · 55,245 cycles

EMERGENCY EXIT LIGHT OVERHEAD BIN INOPERATIVE AT ROW NR 1. R & R BATTERY CHARGER IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 66,091 hrs · 55,245 cycles

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

Part: SPINDLE — DELAMINATED (TE FLAP) · airframe 66,042 hrs · 55,203 cycles

LEFT WING OTBD FLAP NR 2 CARRIAGE SPINDLE DELAMINATED. R & R SPINDLE IAW MT.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 65,713 hrs · 54,978 cycles

R2 DOOR EMERGENCY EVAC FWD SLIDE ATTACHMENT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 64,888 hrs · 54,391 cycles

LT WING NR 1 FLAP TRACK FAIRING MID CRACKED AT LE. REPAIRED FAIRING IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,873 hrs · 54,382 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,873 hrs · 54,382 cycles

LT OVER WING LOWER EMERGENCY EXIT DOOR LIGHT BULBS INOPERATIVE. RELAMPED IAW AMM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,873 hrs · 54,381 cycles

FRAME SHEAR TIE CRACKED AT BS 400 BETWEEN STRINGER 15R & STRINGER 16R. REPAIRED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,873 hrs · 54,381 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 500B+6" TO BS 500B+7" STRINGER 15R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,873 hrs · 54,381 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 503.5 TO BS 504.5 STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,873 hrs · 54,381 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 384.5 TO BS 388.5 STRINGER 15R. REPAIRED SKIN IAW EA.

Part: ACTUATOR — FAULTY (LE SLAT) · airframe 64,285 hrs · 53,928 cycles

DIVERSION DECLARED, EMERGENCY CLIMB OUT OF JAX LE DEVICE NR 3 WOULD NOT RETRACT, WAS GREEN OVERHEAD TRANSIT LIGHT. THEN LEVELED OFF LE DEVICE NR 3 TURNED AMBER TRANSIT LIGHT & 4 LE DEVICE TURNED AMBER TRANSIT LIGHT. R&R NR 3 LE ACTUATOR IAW MM. O.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 64,180 hrs · 53,846 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. R&R SLIDE IAW MT.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 64,173 hrs · 53,841 cycles

ON DESCENT BURNING SMELL NOTICED ON LT SIDE BETWEEN ROW 18 TO ROW 19. R&R GASPER FAN IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 63,656 hrs · 53,441 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,260 hrs · 53,169 cycles

FUSELAGE SKIN CRACKED AT STA 500A, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,260 hrs · 53,169 cycles

FUSELAGE SKIN CRACKED AT STA 500D+5.7, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,260 hrs · 53,169 cycles

FUSELAGE SKIN CRACKED AT STA 974, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,181 hrs · 53,109 cycles

A 3.5 INCH SURFACE CRACK LOCATED 5 INCHES AFT OF STATION 440 ABOVE STRINGER 16R. INSTALLED INTERIM REPAIR PER SRM 53-00-01-2R, REPAIR 31, DETAIL 11 AND EA- 1-353-21821.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,181 hrs · 53,109 cycles

A 2.0 INCH FUSELAGE SUBSURFACE CRACK FOUND AT BODY STATION 400 PLUS 5 INCHES ABOVE STRINGER 16R. INSTALLED INTERIM REPAIR PER SRM 53-00-01-2R, REPAIR 31, DETAIL 11 AND EA- 1-353-21822.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,039 hrs · 53,005 cycles

DURING WALKAROUND NOTED SKIN CRACK APPROX 3" LONG STA 500D +13" ON STR 15L. REPAIRED SKIN CRACK PER EA 1-353-21570 CONTACT ENGINEERING BEFORE 2800 CYCLES REF SAM 943 S/N T031858 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,039 hrs · 53,005 cycles

DURING WALKAROUND NOTED SKIN CRACK APPROX 3" LONG STA 500D +13" ON STR 15L. REPAIRED SKIN CRACK PER EA 1-353-21570 CONTACT ENGINEERING BEFORE 2800 CYCLES REF SAM 943 S/N T031858

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,438 hrs · 52,569 cycles

CRACK FUSELAGE SKIN LEFT STR 1 AT BS 392. REMOVED AND REPLACED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,382 hrs · 52,532 cycles

FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB IAW AMM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 62,382 hrs · 52,532 cycles

LEFT WING PUNCTURED ON I/B FORE FLAP LOWER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: TIE — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

STRINGER TIE CRACKED AT BS 500B, STR 2R. REMOVED AND REPLACED TIE IAW DWG AND SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

STRINGER TIE CLIP CRACKED AT BS 500C, STR 2L. REMOVED AND REPLACED TIE CLIP IAW DWG AMD SRM.

Part: TIE — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

STRINGER TIE CRACKED AT BS 500C, STR 2R. REMOVED AND REPLACED TIE IAW SRM & DWG.

Part: TIE — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

STRINGER TIE CRACKED AT BS 500C, STR 3R. REMOVED AND REPLACED TIE IAW SRM AND DWG.

Part: TIE — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

STRINGER TIE CRACKED AT BS 500B, STR 1. REMOVED AND REPLACED TIE IAW SRM AND DWG.

Part: TIE — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

STRINGER TIE CRACKED AT BS 500C, STR 1. REMOVED AND REPLACED TIE IAW DWG AND SRM.

Part: TIE — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

STRINGER TIE CRACKED AT BS 500B, STR 2L. REMOVED AND REPLACED TIE IAW SRM & DWG.

Part: TIE — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

STRINGER TIE CRACKED AT BS 500B, STR 3R. REMOVED AND REPLACED TIE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP CRACKED AT BS 500A, STR 1. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP AT BS 520, STR 2L. REMOVED AND REPLACED TIE CLIP IAW DWG AND SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP CRACKED AT BS 500A, STR 2R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP CRACKED AT BS 500A, STR 2L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 62,382 hrs · 52,532 cycles

LEFT HORIZONTAL STABILIZER RIB LOWER CHORD CRACKED AT STA 120.30. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: WEB — CRACKED (VERTICAL STAB.) · airframe 62,382 hrs · 52,532 cycles

VERTICAL STABILIZER WEB CRACKED AT STA 13.33. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: SLAT — DELAMINATED (RT WING) · airframe 62,382 hrs · 52,532 cycles

RIGHT WING NR 5 SLAT O/B END DELAMINATED. REPAIRED NR 5 SLAT IAW SRM.

Part: SPINDLE — CRACKED (TE FLAP) · airframe 62,382 hrs · 52,532 cycles

LEFT WING NR 1 O/B FLAP O/B SPINDLE CARRIAGE CRACKED. REMOVED AND REPLACED SPINDLE IAW AMM AND MT.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

WEB CRACKED BETWEEN BS 927 TO BS 947.5, LBL 17.2. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

CLIP CRACKED AT BS 336, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

CLIP CRACKED AT BS 320, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

CLIP CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (TE FLAP) · airframe 62,382 hrs · 52,532 cycles

RIGHT WING NR 6 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 360, LBL 45.6. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: DOUBLER — CRACKED (NLG WW) · airframe 62,382 hrs · 52,532 cycles

NLG WHEEL WELL DOUBLER CRACKED AT BETWEEN BS 251.6 TO BS 268.25, BETWEEN WL 169.1 TO WL 185. REPAIRED DOUBLER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP CRACKED AT BS 727E, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 62,382 hrs · 52,532 cycles

LEFT WING CRACKED ON ANGLE LOCATED AT LEVEL RSS 527 TRAILING EDG AREA. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

FUSELAGE FRAME CRACKED AT BS 947.5, STRINGER 19L. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

WEB CRACKED BETWEEN BS 500A TO BS 500B, STR 26L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

ANGLE CRACKED AT BS 792, STR 18R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

STRINGER SPLICE CORRODED AT BS 907+5, STR 18L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

FRAME CRACKED AT BS 500D, BETWEEN STR 20R AND STR 23R. REPAIRED FRAME IAW EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP CRACKED AT BS 947.5, STR 25R. REPAIRED TIE CLIP IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

SUPPORT ANGLE CRACKED AT BS 727A, BETWEEN STR 25L AND STR 26L. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

STRINGER CRACKED AT BS 867, STR 26R. REPAIRED STRINGER PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP CRACKED AT BS 867, STR 27R. REMOVED AND REPLACED TIE CLIP IAW SRM AND IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

TIE CLIP CRACKED AT BS 867, STR 27L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

WEB CRACKED BETWEEN BS 500B TO BS 500C, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

LEFT KEEL BEAM ANGLE CRACKED AT BS 520+14. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

WEB CRACKED BETWEEN BS 400 TO BS 420, STR 26R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 671, RBL 24.5. REPAIRED CHORD IAW EA AND EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

FUSELAGE SKIN CRACKED AT BS 520+5, STR 2R. REPAIRED SKIN IAW EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,382 hrs · 52,532 cycles

FUSELAGE SKIN CRACKED AT BS 520+3, STRINGER 28L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,361 hrs · 52,517 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,863 hrs · 52,133 cycles

LEFT WING OUTBOARD AFT FLAP DELAMINATED ON UPPER SURFACE OF TRAILING EDGE WEDGE. REMOVED & REPLACED AFT FLAP PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,645 hrs · 51,980 cycles

FUSELAGE SKIN CRACKED AT BS 908+7, STR 24R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,645 hrs · 51,980 cycles

LEFT EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 6. REMOVED AND REPLACED BULB PER AMM.

Part: COVER — MISSING (CABIN) · airframe 61,634 hrs · 51,973 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,917 hrs · 51,424 cycles

EMERGENCY LIGHT INOP AT ROW 10 ABC. RELAMPED PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,917 hrs · 51,424 cycles

STRINGER CLIP CRACKED AT BS 500B, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,917 hrs · 51,424 cycles

STRINGER CLIP CRACKED AT BS 500B, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,916 hrs · 51,423 cycles

FUSELAGE SKIN CRACKED AT BS 500A +14, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,438 hrs · 52,570 cycles

NR 2 SLAT HAS 4EA SKIN CRACKS ON LOWER SKIN AT AFT ROW OF FASTENERS (BELOW O/B AUX TRACK). VERIFIED WITH HFEC. REPAIRED LEFT WING SLAT NR 2 TEE CHORD BETWEEN SS175 AND SS220 IAW EA N 1-357-7551 REV 0 AND EO N AEM-HC57-230/12.R0

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,341 hrs · 51,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT STRINGER CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,907 hrs · 49,918 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE CROWN SKIN CRACKED AT BS 442, STR 2R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,911 hrs · 49,921 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 416, STR 1. REPAIRED SKIN PER EA.

Part: ACTUATOR — FAULTY (LE FLAP) · airframe 58,605 hrs · 49,693 cycles

DECLARED EMERGENCY -- LEADING EDGE DEVICES WOULD NOT EXTEND FOR LANDING. REMOVED AND REPLACED NR 3 L/E FLAP ACTUATOR IAW MM.

Part: WIRE — DAMAGED (CABIN) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 8. REPAIRED WIRE PER SWPM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP AT ROW 17. RELAMPED PER MM.

Part: BATTERY PACK — DISCHARGED (FUSELAGE) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT BS 400. REPAIRED WIRE PER WDM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT EEPLS INOP AT ROW 21. INSTALLED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT EEPLS INOP AT ROW 23. INSTALLED BATTERY PACK PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 59,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.8. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD CARGO DOOR CUTOUT, BS 490, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 831 TO BS 832.4, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 887, STR 7L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 6L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B+13 TO BS 727B+15.4, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 887, STR 7L. REPAIRED SKIN PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 5L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 57,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT CREASE BEAM CRACKED BETWEEN BS 360 TO BS 380, LBL 70. REMOVED AND REPLACED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,306 hrs · 48,700 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 500B, STR 1R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,632 hrs · 48,189 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 933, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,632 hrs · 48,189 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 514A, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,632 hrs · 48,189 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 943 TO BS 945.2, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,632 hrs · 48,189 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 772, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,628 hrs · 48,188 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 514A, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,632 hrs · 48,189 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 514, STR 10L. REPAIRED SKIN PER SRM.

Part: SPOILER — BROKEN (LT WING) · airframe 56,405 hrs · 48,006 cycles

LEFT WING I/B GROUND SPOILER O/B ACTUATOR ATTACHMENT LUG BROKEN. REMOVED AND REPLACED GROUND SPOILER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,791 hrs · 47,549 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 5L. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 62,381 hrs · 52,532 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 115.00. REPAIRED SKIN IAW EA AND EO.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 55,550 hrs · 47,363 cycles

DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY INOP AT BS 332, LBL 7. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,146 hrs · 34,922 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 733B, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,073 hrs · 47,007 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 434 TO BS 437, STR 1. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,073 hrs · 47,007 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 485, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,073 hrs · 47,007 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 504D, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,073 hrs · 47,007 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 493 TO BS 497, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,073 hrs · 47,007 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 505, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,073 hrs · 47,007 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 442.5 TO BS 445.5, STR 1. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,073 hrs · 47,007 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 453 TO BS 456, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,073 hrs · 47,007 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 504D, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,073 hrs · 47,007 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 453 TO BS 456, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,073 hrs · 47,007 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 493 TO BS 497, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,073 hrs · 47,007 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 434 TO BS 445.5, STR 1. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,324 hrs · 46,436 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,282 hrs · 46,405 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,281 hrs · 46,405 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 520, STR 9R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,261 hrs · 46,388 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 512D, STR 10L. REPAIRED SKIN PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,261 hrs · 46,388 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,893 hrs · 45,394 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND AFT SERVICE OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: TIRE — BLOWN (RT MLG) · airframe 52,914 hrs · 45,412 cycles

RT MLG TIRE NR 3 & 4 BLEW ON LANDING. SUBSEQUENT WHEEL FIRE. R&R RT MLG TIRES PER MM.

Part: BATTERY — ACTIVATED (FLASHLIGHT) · airframe 52,693 hrs · 45,245 cycles

AFT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 24L. REPAIRED SKIN PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 24L. R&R CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 941 TO BS 943, STR 24L. REPAIRED SKIN PER EA.

Part: RIB — CRACKED (RT WING) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING FUEL TANK WING RIB LOWER CHORD CRACKED AT WBL 135, BETWEEN STR 2 TO STR 3. REPAIRED RIB PER ACO.

Part: RIB — CRACKED (RT WING) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING FUEL TANK WING RIB LOWER CHORD CRACKED AT WBL 135, BETWEEN STR 2 TO STR 3. REPAIRED RIB PER ACO.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER ACO.

Part: DOOR FRAME — CRACKED (GALLEY DOOR) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD GALLEY DOOR AFT FRAME CRACKED. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND CENTER WING BOX LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 671, LBL 24. REPAIRED BEAM PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED R1 DOOR UPPER HINGE CUTOUT, BS 304, WL 258. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND CENTER BOX WING, LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 667, LBL 24. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM CORRODED AT BETWEEN BS 727E TO BS 747. REMOVED AND REPLACED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB BETWEEN BS 727D TO 727E CORRODED. REMOVED AND REPLACED BEAM PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 500B, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED R1 DOOR LOWER HINGE CUTOUT, BS 291, WL 233. REPAIRED SKIN PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 6Y CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 559, STR 2R. REPAIRED SKIN PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND BEAR STRAP SKIN CORRODED AT BS 493, BETWEEN STR 27R TO STR 28R. REPAIRED SKIN PER SRM.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE HINGE FITTING CRACKED AT L1 DOOR UPPER HINGE CUTOUT. R&R FITTING PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 627, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 747 S26-27R) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (BS 727E-747) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BETWEEN BS 727E TO BS 747. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (BS 807-827 S17L) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BETWEEN BS 807 TO BS 827, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT UPPER STOP FITTING. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 18. REPAIRED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED AT L2 DOOR, BETWEEN BS 950 TO BS 990. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED AT R2 DOOR BETWEEN BS 996 TO BS 947. REMOVED AND REPLACED BEAM PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT I/B END DELAMINATED AT EDGE. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 38, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CORRODED (LT MLG W/W) · airframe 49,945 hrs · 43,261 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG SIDE SUPPORT FITTING LUG CORRODED AT BS 685. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (RT MLG W/W) · airframe 49,945 hrs · 43,261 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG SIDE SUPPORT FITTING LUG CORRODED AT BS 685. REPAIRED FITTING PER SWA EA.

Part: BULKHEAD — CRACKED (BS 1016 S6L) · airframe 48,073 hrs · 41,865 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 6L. REPAIRED BULKHEAD PER SRM.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 48,029 hrs · 41,827 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT OVERWING EMERGENCY EXIT HATCH LOWER FRAME CRACKED AT LOWER CENTER FITTING. REMOVED AND REPLACED LOWER FRAME PER SRM.

Part: ROD END — BROKEN (VERTICAL STAB) · airframe 48,029 hrs · 41,827 cycles

DURING SCHEDULED 14Y CHECK, FOUND VERTICAL STABILIZER STANDBY ACTUATOR, INPUT ROD END BROKEN. REMOVED AND REPLACED ROD END PER MM.

Part: FRAME — CRACKED (BS 380 S8L) · airframe 48,029 hrs · 41,827 cycles

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

Part: FRAME — CRACKED (BS 907 S8R) · airframe 48,029 hrs · 41,827 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 48,029 hrs · 41,827 cycles

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

Part: FRAME — CRACKED (BS 867 S8L) · airframe 48,029 hrs · 41,827 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 360 S8R) · airframe 48,029 hrs · 41,827 cycles

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

Part: FRAME — CRACKED (BS 400 S8L/R) · airframe 48,029 hrs · 41,827 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 45,227 hrs · 39,592 cycles

DURING SCHEDULED A1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD EDGE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: MOTOR — BROKEN (NR 1 ENGINE) · airframe 45,217 hrs · 39,583 cycles

NR 1 ENGINE EGT EXCEEDED LIMITS ON CLIMBOUT. MAX OF 934 FOR APPROX 2 SECONDS. FOUND VBV SHAFT BROKEN. REMOVED AND REPLACED VBV MOTOR AND SHAFT ASSY PER MM.

Part: HINGE FITTING — SHEARED (LT WING SPOILER) · airframe 45,082 hrs · 39,470 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING NR 5 GROUND SPOILER HINGE FITTING SHEARED. REMOVED AND REPLACED NR 5 SPOILER PER MM.

Part: FITTING — SHEARED (LT WING SPOILER) · airframe 45,082 hrs · 39,470 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING NR 4 GROUND SPOILER HINGE FITTING SHEARED. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: SHUTOFF VALVE — LEAKING (HYDRAULIC SYS) · airframe 44,799 hrs · 39,240 cycles

ON SHORT FINAL -A- HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED. AFTER LANDING -A- HYDRAULIC SYSTEM QUANTITY FELL TO ZERO. REMOVED AND REPLACED FLIGHT CONTROL SHUTOFF VALVE PER MM.

Part: SKIN — CRACKED (BS 500D S12L) · airframe 44,439 hrs · 38,974 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12L. REPAIRED SKIN PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 44,443 hrs · 38,977 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 44,443 hrs · 38,977 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 44,439 hrs · 38,974 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 358, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,439 hrs · 38,974 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 43,327 hrs · 38,079 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 6 ABC TO ROW 8 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: BOLT — WORN (LT ELEVATOR) · airframe 43,278 hrs · 38,041 cycles

DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE HARDWARE PER MM.

Part: SKIN — CRACKED (BS 944 S25R) · airframe 43,139 hrs · 37,930 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 42,999 hrs · 37,819 cycles

DURING SCHEDULED A2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 42,795 hrs · 37,651 cycles

DURING SCHEDULED A1 CHECK, FOUND PHOTOLUMINESCENT STRIP WORN AT ROW 8. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 42,255 hrs · 37,220 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT UPPER WEDGE DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,763 hrs · 36,820 cycles

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

Part: SKIN — CRACKED (BS 500D) · airframe 41,268 hrs · 36,410 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15R. REPAIRED SKIN PER SRM & SWA EA.

Part: SKIN — CRACKED (BS 500D) · airframe 41,268 hrs · 36,410 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12R. REPAIRED SKIN PER SRM & SWA EA.

Part: ATTACH FITTING — CORRODED (RT WING) · airframe 39,953 hrs · 35,354 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT MLG STABILIZER BEAM FWD & AFT ATTACH FITTINGS CORRODED. REMOVED AND REPLACED STABILIZER BEAM PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,953 hrs · 35,354 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EA AFT CARGO FLOOR SUPPORT BEAMS CORRODED AT BS 770, LBL 3 & RBL 8. REPAIRED BEAMS PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 39,219 hrs · 34,771 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 38,909 hrs · 34,540 cycles

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

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 38,450 hrs · 34,189 cycles

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

Part: BUSHING — WORN (LT ELEVATOR TAB) · airframe 38,450 hrs · 34,189 cycles

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

Part: SKIN — CRACKED (RT WING) · airframe 36,622 hrs · 32,690 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT WING L/E SKIN AT WS 213, CRACKED. REPAIRED L/E SKIN PER ER.

Part: FLAP — DELAMINATED (RT WING) · airframe 36,001 hrs · 32,208 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 35,934 hrs · 32,153 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,999 hrs · 29,023 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 17R. REPAIRED SKIN PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,999 hrs · 29,023 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,999 hrs · 29,023 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 31,307 hrs · 28,435 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN DOOR WAS OPENED. REINSTALLED SLIDE PER MM.

Part: BALLAST — FAILED (CABIN) · airframe 30,939 hrs · 28,125 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT BALLAST PER MM.

Part: LENS — MISSING (AFT SVC DOOR) · airframe 30,437 hrs · 27,707 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR ONERHEAD EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 30,437 hrs · 27,707 cycles

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

Part: SLAT — CRACKED (LH WING) · airframe 28,247 hrs · 25,868 cycles

DURING SCHEDULED C1 CHECK, FOUND # 1 L/E SLAT CRACKED ( 2 EA ) AT AFT ROW OF FASTENERS NEAR CENTER AUX TRACK. REPAIRED SLAT PER SWA RA 1-357-1107.

Part: MODULE — FAILED (WHEEL WELL) · airframe 28,202 hrs · 25,829 cycles

B SYSTEM HYDRAULIC FAILURE DURING LANDING. R & R B HYDRAULIC SYS MODULE PER MM.

Part: MOUNT — LOOSE (EVAC SLIDE) · airframe 6,994 hrs · 4,196 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE MOUNT LOOSE. SECURED MOUNT PER MM.

Part: SWITCH — FAILED (APU) · airframe 26,266 hrs · 24,206 cycles

DIVERSION - APU OVERSPEED LIGHT ILLUMINATED. LEFT BUS OFF LIGHT ILLUMINATED. (NR 1 GENERATOR ALREADY ON MEL). REMOVED AND REPLACED APU 3-SPEED SWITCH PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 25,635 hrs · 23,700 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN DOOR WAS OPENED. REINSTALLED EVAC SLIDE MM.

Part: FIRE LOOP — MALFUNCTIONED (APU) · airframe 25,613 hrs · 23,681 cycles

AIR TURNBACK WHILE APU WAS OFF, RECEIVED APU FIRE INDICATION, BOTTLE WAS DISCHARGED AND LIGHT EXTINGUISHED. R&R LOWER APU FIRE LOOP DETECTOR - OPS CHECK GOOD PER MM.

Part: LIGHT — INOPERATIVE (ENTRY DOOR) · airframe 25,435 hrs · 23,539 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 25,391 hrs · 23,496 cycles

DURING SCHEDULED 1/4D CHECK, FOUND F/O P-1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 25,391 hrs · 23,496 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR LOWER FRAME CRACKED AT AFT CORNER. R&R FWD SVC DOOR PER MM.

Part: LENS — CRACKED (GALLEY) · airframe 25,391 hrs · 23,496 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 4 GALLEY EMERGENCY EXIT LIGHT LENS CRACKED. R&R LENS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 25,391 hrs · 23,496 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 1.5 CRACK ON LT HORIZ STAB LOWER SKIN BELOW INBD BALANCE BAY. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 25,391 hrs · 23,496 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD EMERGENCY EXIT SIGN LENS LOOSE. SECURED LIGHT ASSY PER MM.

Part: RADAR — INOPERATIVE (E/E BAY) · airframe 24,811 hrs · 23,007 cycles

AIR TURNBACK, AIRCRAFT RADAR FAILED DURING FLIGHT. REMOVED AND REPLACED INDICATOR (P/N 2041222-321) AND R/T UNIT PER MM.

Part: COVER — LOOSE (CABIN) · airframe 24,705 hrs · 22,915 cycles

EEPLS TRACK LIGHT COVER LOOSE AT ROW 14. SECURED TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,060 hrs · 21,567 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROWS 15 AND 16. RECONNECTED WIRING PER MM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C3 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AROUND AFT SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: BLADES — SHINGLED (NR 2 ENGINE)

AIR TURNBACK, DURING CLIMB NR 2 ENG INGESTED BIRD. VIBRATION DEVELOPED IN ENG. C/W BIRD STRIKE INSP, BORESCOPE INSP. NO DAMAGED NOTED EXCEPT FOR NR 2 AND NR 27 FAN BLADES WHICH WERE SHINGLED. UNSHINGLED FAN BLADES PER MM.

Part: HANDLE — BROKEN (LT EMER EXIT)

DURING SCHEDULED RON, FOUND LT OVERWING EMERGENCY DOOR HANDLE COVERPLATE BROKEN. REMOVED AND REPLACED HANDLE PER MM.

Part: BLEED VALVE — FAILED (NR 2 ENGINE)

ABORTED TAKEOFF, NR 2 ENGINE SLOW TO ACCELERATE, MAX N1 WAS 76 PERCENT TAKEOFF ABORTED AT 90 KNOTS. REMOVED AND REPLACED VARIABLE BLEED VALVE MOTOR AND MASTER BLEED VALVE (P/N 10042AV) PER MM.

Part: INDICATOR — MALFUNCTIONED (NR 2 FUEL FLOW)

NR 2 FUEL FLOW INDICATOR SPORADIC, RUNS TO ZERO AND BACK UP. REMOVED AND REPLACED FUEL FLOW INDICATOR PER MM.

Part: WIRE — DAMAGED (CABIN)

DURING PREFLIGHT, FOUND FLOOR TRACK LIGHTING IN MID CABIN INOP. REPLACED AND REPAIRED WIRING AS REQUIRED PER BOEING M/M.

Part: STRAP — CRACKED (BS 344)

DURING SCHEDULED C2 CHECK, FOUND FLOORBEAM STRAP CRACKED JUST ABOVE AND O/B OF BATTERY IN E & E BAY OF BS 344. REPAIRED FLOORBEAM STRAP PER BOEING SRM.

Part: WIRE — LOOSE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY TRACK LIGHTING INOP 5 LIGHTS AT OVERWING EXIT ROW. RECONNECTED WIRING TO LIGHTS. OPS CHECK OK PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EGRESS LIGHTS OUT MID AIRCRAFT WIRING LOOSE AND COVERS. REINSTALLED TRACK LIGHTING WIRING PER BOEING MM.

Part: SKIN — CRACKED (RT TE FOREFLAP)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED I/B FOREFLAP SKIN O/B OF TRACK. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 380-400)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INTERCOSTAL AT BS 380-400 C/L. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 747)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FLOORBEAM UNDER CARGO NET TIE DOWN LUG AT BS 747, RBL 14. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (GALLEY DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FWD SERVICE DOOR ENTRY Z ANGLE. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 540)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INTERCOSTAL FWD SIDE AND AFT SIDE AT BS 540, RBL 1; AND AFT SIDE AT 540, LBL 1. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — DAMAGED (BS 485)

DURING SCHEDULED SERVICE CHECK, FOUND DAMAGED CLOSURE WEB EDGE AT BS 485 ABOVE STR 25R. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 727-767)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT TRANSITION ANGLE AT BS 727- 767. REMOVED AND REPLACED PER BOEING SRM.

Part: DOOR POST — CRACKED (BS 286)

DURING SCHEDULED 1/2D CHECK, FOUND FWD DOOR POST CRACKED AT FLOOR LEVEL BS 286. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 947-993)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT Z ANGLE AT BS 947 - 993, RBL 50. REMOVED AND REPLACED PER BOEING SRM.