N54SW

Part: SUPPORT — CRACKED (FUSELAGE)

LEFT W/W FAIRING SUPPORT PLATE CRACKED AT FS 661. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AS VIEWED FROM THE E/E COMPT, THERE IS CORROSION ON A MAIN DECK FLOOR SUPPORT AT BS 312 LBL 11R, ON ITS LOWER SIDE AROUND A SCREW HOLE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR STRUCTURE, FLOORBEAM UPPER CHORD AT BS 294 RBL 10 TO LBL 10 WL 208 HAS CORROSION. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

FOUND STRINGER SUPPORT TIE CRACKED AT FUSELAGE STATION 727B LONGERON 6L. (M)

Part: STRINGER — CRACKED (FUSELAGE)

BS 727 STRINGER 18A RIGHT, NOTED CRACK IN THE I/B STRINGER 18A WEB STRAP. CRACK EMANATING FROM HOLE AT BS 725.5 AND PROPAGATING DOWN AND FORWARD (LOOKING AT FASTENERS HOLE FROM INSIDE WHEEL WELL, IT WOULD BE THE 8 O'CLOCK POSITION).

Part: TIE CLIP — CRACKED (FUSELAGE)

FOUND STRINGER TIE CLIPS CRACKED AT STATION 727B, STRINGER 3R, 4R, 5R AND 6R. (M)

Part: STRINGER — CRACKED (FUSELAGE)

FOUND BS 727 STRINGER 18A LEFT VERTICAL OUTER CHORD IS CRACKED FROM THE FORWARD HOLE BS 727.5 AND PROPAGATES AFT APPROXIMATELY .25 INCH IN LENGTH. (M)

Part: STRINGER — CRACKED (FUSELAGE)

FOUND BS 727 STRINGER 18A RIGHT, CRACK IN INBOARD STRINGER 18A WEB STRAP. CRACK EMANATING FROM HOLE AT BS 725.5 AND PROPAGATING DOWN AND FORWARD. (M)

Part: ANGLE — CORRODED (FUSELAGE)

FOUND R2 DOOR THRESHOLD AREA HAS CORROSION ON SUPPORT ANGLES BS 950 THROUGH 1006 RBL 52. (M)

Part: CLIP — CRACKED (FUSELAGE)

LEFT CABIN STATION 747 STRINGER 4 AND STRINGER 7 HAS ATTACH CLIPS CRACKED. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

FOUND SHEAR TIE CLIP IS CRACKED AT STATION 616 STRINGER 5R. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND CORROSION AROUND FLOORBEAM FASTENER HOLES AT STATION 344 LBL 10 AND STATION 360 RBL 1. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

FOUND SHEAR TIE IS CRACKED AT STATION 787 STRINGER 6R. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

SHEAR TIE IS CRACKED AT STATION 727A STRINGER 3R, 4R AND 5R. (M)

Part: CLIP — CRACKED (FUSELAGE)

LEFT CABIN STATION 827 STRINGER 6L HAS ATTACH CLIP CRACKED. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

FOUND CRACK IN U-CHANNEL TIE CLIP AT STRINGER 4L FLIGHT STATION 625. (M)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,292 hrs · 79,055 cycles

ON INSPECTION OF THE 178 BULKHEAD NOTED CRACK FROM AFT SIDE ON PILOTS SIDE. (INSPECTED SIDE CHORD AREA ABOVE WL 207). NOTED APPROX 2 INCHES CRACK DOWN RADIUS OF SIDE CHORD.

Part: BULKHEAD — CRACKED (FUSELAGE)

ON INSPECTION OF BS 178 BULKHEAD, NOTED CRACK FROM AFT SIDE ON PILOT SIDE INSPECTED SIDE CHORD AREA ABOVE W/L 207. TWO INCH CRACK DOWN RADIUS OF SIDE CHORD. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

FOUND LEFT FORWARD PIT FUSELAGE STATION 380 LBL 51 FRAME ATTACH ANGLE CRACKED. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FOUND COCKPIT FLOOR LEFT SIDE F/S 227 WL 212 LBL 30 HAS CRACK IN FLOOR SUPPORT FORMER. (M)

Part: SUPPORT BRACKET — CRACKED (VERTICAL STAB)

VERTICAL STABILIZER AFT WEB SUPPORT BRACKET IS CRACKED OUT AROUND FASTENERS AT FIN WL 58.18 AND BS 1088. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND SEAT TRACK AT STATION 400 LBL 43.5 CORRODED. (M)

Part: WEB — CRACKED (FUSELAGE)

FOUND FORWARD PIT BS 460 LBL 11 LIGHTENING HOLE IS CRACKED. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND SEAT TRACK CORRODED AT STATION 363 RBL 22.5. (M)

Part: RIB — CRACKED (VERTICAL STAB)

FOUND VERTICAL STAB LEADING EDGE PANEL NR 9545 HAS CRACKED RIB AT 85 INCH FROM LOWER END 9TH RIB. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND CABIN UPPER FLOORBEAM CHORD AT BS 312 LBL 1 HAS CORROSION. (M)

Part: RIB — CRACKED (VERTICAL STAB)

FOUND VERTICAL STABILIZER LEADING EDGE PANEL NR 9545 HAS A CRACKED RIB AT 94 INCHES FROM LOWER END OF 10TH RIB. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND FLOORBEAM LOWER SUPPORT ANGLE CRACKED AT BS 727 LBL 24. (M)

Part: STIFFENER — CRACKED (FUSELAGE)

FOUND VERTICAL STIFFENER IS CRACKED AT LBL 1, BS 947.5 AT UPPER END. (M)

Part: SKIN — CRACKED (FUSELAGE)

FOUND FUSELAGE SKIN AT FLIGHT STATION 800 STRINGER 22L CRACKED APPROXIMATELY 5 INCH LONG. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

FOUND FORWARD PIT STATION 380 STRINGER 19L ATTACH CLIP IS CRACKED. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

FOUND RADAR MOUNT ATTACH ANGLE HAS A .800 INCH LONG CRACK AT LBL 5.7 WL 211 BS 178. (M)

Part: ANGLE — CRACKED (CENTER WING)

FOUND CENTERWING FRONT SPAR SUPPORT ANGLE IS CRACKED AT BS 538 RBL 8. (M)

Part: SLAT — DELAMINATED (LT WING)

FOUND LEFT WING NUMBER TWO SLAT IS DELAMINATED IN SEVERAL AREAS. (M)

Part: FRAME — CRACKED (FUSELAGE)

FOUND LEFT FORWARD PIT STATION 420 ABOVE STRINGER 26 FRAME HAS A CRACK. (M)

Part: STRINGER CLIP — DENTED (FUSELAGE)

FOUND STRINGER CLIP AT STATION 727B S22L IS DENTED. (M)

Part: STRINGER CLIP — DENTED (FUSELAGE)

FOUND STRINGER CLIP DENTED AND GOUGED AT STATION 747 STRINGER 21L. (M)

Part: FRAME — GOUGED (FUSELAGE)

FRAME HAS TWO GOUGES AT BS 747 BETWEEN STRINGER 23L AND STRINGER 22L. (M)

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,292 hrs · 79,055 cycles

FUSELAGE SKIN IS CRACKED AT STA 800 STRINGER 22 LT. CRACK IS 2.6 INCH IN LENGTH.

Part: DUCT — CRACKED (LT ENGINE)

NR 1 ENGINE LEFT SIDE BLEED AIR DUCT ATTACH BRACKET CRACKED. (M)

Part: SKIN — GOUGED (FUSELAGE)

FOUND OUTER SKIN GOUGED ON EXISTING REPAIR AT STATION 380 AT STRINGER 24-25R. ACCOMPLISHED DOUBLER INSTALLATION AND REPAIR IAW 737 SRM 53-30-03 FIG NR 9. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FLT 2544 - ACY - AFT AISLE OVERHEAD BULLNOSE EMERGENCY EXIT LIGHTOUT. REMOVED AND REPLACED AFT AISLE OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT BATTERY POWER SUPPLY CARTRIDGE. SYSTEM TEST NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

ACY - FORWARD BULLNOSE EMERGENCY LIGHT IN CABIN INOPERATIVE. TROUBLESHOT SYSTEM, REPLACED EMERGENCY LIGHT BATTERY PACK ASSEMBLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FLT 807 - ACY - FORWARD SECTION 'E PATH' LIGHTS INOPERATIVE. REPLACED FORWARD SECTION EMERGENCY LIGHT BATTERY PACK. (M)

Part: COVER — CRACKED (ROW 11)

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHTING COVER CRACKED NEXT TO SEAT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (ROW 4)

DURING REPAIR OVERNIGHT CHECK, FOUND FLOOR TRACK EMERGENCY LIGHT INOPERATIVE AT ROW 4. SECURED LOOSE BULB IN SOCKET PER MM.

Part: STRINGER — CRACKED (BS 360)

DURING SCHEDULED SERVICE CHECK, FOUND STR TO FRAME CLIP CRACKED B/S 360, STR 4 RT. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 790)

DURING SCHEDULED SERVICE CHECK, DOUBLER CRACKED ABOVE STR 10R, B/S790. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 540)

DURING SCHEDULED SERVICE CHECK, FOUND STR 10 RT AT BS 540 HAS CRACKED STR SPLICE FITTING PER HFEC. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 908)

DURING SCHEDULED SERVICE CHECK, FOUND NUMEROUS FASTENER HOLES CRACKED STR 14R B/S 908-937, WITH HFEC ROTATING PROBE INSPECTION. REPAIRED PER ACO 6717-53 PART II AND XEA X2-53-194.

Part: STRINGER — CRACKED (BS 990)

DURING SCHEDULED SERVICE CHECK, FOUND NUMEROUS FASTENER HOLES CRACKED STR 14L B/S 990-1016, WITH HFEC ROTATING PROBE INSPECTION. REPAIRED PER ACO 6717-53 PART II AND XEA X2-53-194.

Part: LAMPS — FAILED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND NUMEROUS EMERG EXIT SIDE LIGHT LAMPS INOP. REPLACED PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: SLIDE — LOW PRESS (AFT ENTRY)

DURING WALKAROUND CHECK, FOUND AFT ENTRY DOOR ESCAPE SLIDE PRESSURE LOW. REPLACED PER BOEING M/M.

Part: SKIN — CRACKED (BS 767)

DURING SCHEDULED TERMINAL CHECK, FOUND A 3.5 INCH CRACK ON FUSELAGE SKIN UNDER PAX WINDOW BETWEEN BS 767 AND 787 LT. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND FUSE SKIN CRACKED APPROX 1 INCH ABOVE POTABLE WATER SERVICE DOOR. REPAIRED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 440)

DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN PUNCTURED AND TORN AT BS 440 S27L. REPAIRED PER BOEING SRM.

Part: DOUBLER — CRACKED (FWD SERV DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND A 2 INCH LONG CRACK AT BS 294 BETWEEN S9 AND 10 ON DOUBLER, FWD SERV DOOR. REPAIRED PER SWA RA 1-253-1537.

Part: STRAP — CRACKED (BS 294)

DURING SCHEDULED SERVICE CHECK, FOUND TEAR STRAP CRACKED THROUGH O/B CHORD OF FRAME AT S16R. REPAIRED PER SWA RA 1-353-1536.

Part: SHEAR TIE — CRACKED (BS 271)

DURING SCHEDULED SERVICE CHECK, FOUND BELT FRAME SHEAR TIE CRACKED AT BS 271, BETWEEN S12 AND 13. REPAIRED PER SWA RA 1-353-1535.

Part: SKIN — CRACKED (BS 272-291)

DURING SCHEDULED SERVICE CHECK, FOUND EXTERIOR FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR LOWER HINGE CUT OUT BS 291 TO 272.5. REPAIRED PER BOEING SRM.

Part: BELT FRAME — CRACKED (BS 294)

DURING SCHEDULED SERVICE CHECK, FOUND BS 294 BELT FRAME I/B CHORD CRACKED AT S13R. REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 278/291)

DURING SCHEDULED SERVICE CHECK, FOUND EXTERIOR FUSELAGE SKIN ATTACH ANGLE CRACKED AT BS 278 AND 291. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (AFT GAL)

DURING SCHEDULED B2 CHECK, FOUND FUSELAGE SKIN CRACKED .625 INCH FROM UPPER CUTOUT AT AFT GALLEY DOOR. REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (FWD ENTRY)

DURING WALKAROUND CHECK, FOUND FORWARD ENTRY FRAME CRACKED. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: SKIN — CRACKED (BS 747)

DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN LAP CRACKED AT BS 747, AT S10R. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND CABIN OVERWING EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: CHORD — CRACKED (BS 726)

DURING SCHEDULED D-CHECK, FOUND CHORD CRACKED AT BS 726, RBL 9 WL 202. REPLACED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 999/1002/1005)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 999 LBL 13 WL 208, BS 1002 LBL 12 WL 208 AND BS 1005 LBL 10 WL 208. REPLACED CORRODED SECTION PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN S14 AND 15L. REPLACED WITH NEW PER BOEING SRM.

Part: SPLICE — CORRODED (BS 907)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, S20R. REPLACED WITH NEW PER BOEING SRM.

Part: CLIP — CRACKED (BS 787/747/947)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 787 S24R AND S20R, BS 727A S25L, BS 747 S20L AND S22L AND AT BS 947, S25R. REPLACED PER BOEING SRM.

Part: FLOOR BEAM — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CRACKS AT BS 500B LT IN RADIUS OF UPPER FLANGE. REPAIRED PER SWA ACO 595-53.

Part: SPLICE — CORRODED (BS 909)

DURING SCHEDULED D-CHECK, FOUND STRINGER AND STRINGER SPLICE CORRODED AT BS 909 LBL171 WL 171. REPLACED WITH NEW PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 987/947)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 987 LBL 3 TO 19 WL 208 AND BS 947 RBL 10 WL 208 AND LBL 4, 12, 22, WL 208. REPLACED CORRODED SECTION PER BOEING SRM.

Part: FRAME — CRACKED (BS 344)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 344 LBL 45 WL 170. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 178 WL 195 LBL 24. REPLACED PER BOEING SRM.

Part: CLIPS — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 747 S22R AT BS 727A S19R AND AT BS 520 S19L. REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED 2 PLACES, ONE AT LBL 10 AND AT LBL 11, WL 219. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 495)

DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT BS 495, S23 AND 22R AND AT BS 1012, S7L. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND SUPPORT ANGLE CRACK AT BS 178 WL 194 LBL 23. REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 179)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AND FAIL-SAFE CHORD CRACKED AT BS 179 LBL 55. REPAIRED PER BOEING SRM.

Part: STRAP — CRACKED (BS 492)

DURING SCHEDULED D-CHECK, FOUND DOOR FRAME STRAP CRACKED AT BS 492 RBL 54 WL 180. REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 182)

DURING SCHEDULED D-CHECK, FOUND CRACKED VERTICAL STIFFENER WEB AT BS 182 LBL 18 WL 184. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 440)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED 2 PLACES AT BS 440 LBL 55 AND 57 WL 177 AND 175. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD BS 178 CRACK ON LEFT SIDE AT WL 194 IN RADIUS OF SIDE CHORD. REPAIRED PER SWA ACO 96-0017.

Part: BULKHEAD — CRACKED (APU COMPT)

DURING SCHEDULED D-CHECK, FOUND APU COMPARTMENT UPPER BULKHEAD CRACKED AT LIGHTENING HOLE BETWEEN BS 1136 AND 1121 RIGHT SIDE AND BETWEEN BS 1121 AND 1104 LEFT SIDE. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD SKIN CRACKED AT BS 178 WL 235 APPROX LBL 13. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 440)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440 RBL 37 WL 160. REPAIRED PER TRAMCO EWO 96-0041.

Part: STRINGERS — CORRODED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND STRINGERS CORRODED BS 907 LBL 21 WL 168, BS 903 RBL 21 WL 168 AND BS 908 TO 906 RBL 19 WL 165. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727-578)

DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 727+11, 757, AND 758, STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0203.

Part: STIFFENER — CRACKED (BS 178)

DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT VERTICAL STIFFENER, BS 178, RBL 6, WL 184. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (BS 470-490)

DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 470, 471, AND 490, STRINGER 10L. REPAIRED PER TRAMCO EWO 95-0203.

Part: SKIN — CRACKED (BS 391)

DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATION AT BS 391, STRINGER 14L. REPAIRED PER TRAMCO EWO 95-0203 AND 95-0205.

Part: STIFFENER — CRACKED (BS 178)

DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATION AT VERTICAL STIFFENER, BS 178, LBL 6, WL 184. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: BULKHEAD SKIN — CRACKED (BS 178)

DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 178 BULKHEAD SKIN, WL 218, RBL 10-12, AT WL 187 TO 203, AND WL 202 TO 188, RBL 5.7. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (BS 986.5)

DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATION AT AFT ENTRY DOOR UPPER AFT CORNER, BS 986.5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.