N29SW

Part: FIRE WARNING — MALFUNCTIONED (COCKPIT)

MASTER FIRE WARNING LIGHT FLICKERED ON AND OFF DURING DESCENT. ON FINAL, LIGHT CAME ON STEADY WITH NO OTHER ASSOCIATED FIRE WARNINGS. LIGHT WAS RESET. (M)

Part: FRAME — CRACKED (FUSELAGE)

FUSELAGE FRAME SECTION AT BS 328 BETWEEN STR 1R AND 4R, CRACKED.

Part: STRINGER — CRACKED (FUSELAGE)

UPPER FUSELAGE MAIN CABIN STRINGER 11R AT BS 540, CRACKED.

Part: STRINGER — CRACKED (FUSELAGE)

UPPER FUSELAGE MAIN CABIN STRINGER 11L AT BS 540 CRACKED.

Part: STRINGER — CRACKED (FUSELAGE)

FUSELAGE STRINGER SECTION 9R FROM BS 755 TO BS 780, CRACKED.

Part: SKIN — DENTED (FUSELAGE)

EXTERNAL FUSELAGE, BETWEEN BS 423 AND BS 435 BETWEEN STR 20R, SKIN DENTED.

Part: STRINGER — CRACKED (FUSELAGE)

PAX CABIN, BS 727+9INCHES, STRINGER NR 1 CRACKED.

Part: ANGLE — CRACKED (FUSELAGE)

LOWER FUSELAGE RIGHT WHEEL WELL, BULKHEAD BS 727, BL 0 AND WL 208 ANGLE, CRACKED.

Part: SKIN — DELAMINATED (SPOILER)

LEFT WING GROUND SPOILER NR 5 WITH UPPER SKIN DELAMINATED.

Part: FRAME — CRACKED (FUSELAGE)

FUSELAGE FRAME SECTION AT BS 344 FROM STR. 4L AND STR 6L, CRACKED.

Part: SKIN — CANNING (FUSELAGE)

EXT. FUSELAGE BS 864 BETWEEN STRINGER 16L AND 17L, SKIN WITH OIL CAN.

Part: STRINGER — CRACKED (FUSELAGE)

FUSELAGE STRINGER SECTION 9L FROM BS 727A+7 TO BS 727B+12, CRACKED.

Part: SKIN — DELAMINATED (L/E SLAT)

LEFT WING SLAT NR 3 UPPER SKIN DELAMINATED.

Part: STRINGER — CRACKED (FUSELAGE)

FUSELAGE STRINGER SECTION FROM BS 429 TO BS 450 AT STR 4R, CRACKED.

Part: FLOORBEAM — CRACKED (FLOORBEAM)

PAX CABIN FROM BS 520 RBL 25 AND WL 208, FLOOR BEAM CRACKED.

Part: FLOORBEAM — CRACKED (FUSELAGE)

FORWARD C/C, FLOOR BEAM, LOWER CHORD, RBL 25 INCHES, WL 201 WITH CRACK.

Part: SKIN — DELAMINATED (L/E FLAP)

LEFT WING, IB FORE FLAP UPPER SKIN DELAMINATED.

Part: STRINGER — CORRODED (FUSELAGE)

AFT C/C BAY, STA967, STR 27R CORRODED.

Part: SKIN — DELAMINATED (SPOILER)

RIGHT WING, FLIGHT SPOILER NR 8 UPPER SKIN, DELAMINATED.

Part: STRINGER — CRACKED (FUSELAGE)

FUSELAGE STRINGER SECTION FROM BS 306 TO BS 326 AT STR 4R, CRACKED.

Part: STRINGER — CRACKED (FUSELAGE)

FUSELAGE STRINGER SECTION 27L FROM BS 960 TO BS 1016, CRACKED.

Part: SKIN — CRACKED (FUSELAGE)

EXTERNAL FUSELAGE, E & E COMPARTMENT, DOOR AROUND CUT OUT SKIN WITH SHARP EDGES AND CRACKED.

Part: SKIN — DELAMINATED (SPOILER)

LEFT WING, GROUND SPOILER NR4 UPPER SKIN DELAMINATED.

Part: FRAME — CRACKED (FUSELAGE)

LOWER FUSELAGE LEFT WHEEL WELL, BS 663.75 LBL 25 AND WL 208 CHORD, CRACKED.

Part: SKIN — DENTED (FUSELAGE)

EXTERNAL FUSELAGE BS890 BETWEEN STR 20R AND STR 21R DENTED.

Part: FLOORBEAM — CRACKED (FUSELAGE)

FUSELAGE FLOOR BEAM SECTION UPPER CHORD AT BS 328 BETWEEN RBL 24.5 AND RBL40, CRACKED.

Part: SPAR — CRACKED (CENTER WING)

WING - CENTER WING BOX - REAR SPAR CRACKED - STA 663.0/ RBL6.150/ WL 170.4

Part: STRINGER — CRACKED (FUSELAGE)

PAX CABIN, STA 618, STRINGER 17R, HORIZONTAL FLANGE CRACKED.

Part: FRAME — CRACKED (FUSELAGE)

PAX CABIN, BS 727, AT STR 14L LEVEL FRAME CRACKED. PROBABLE CAUSE IS FATIGUE.

Part: BULKHEAD — CRACKED (FUSELAGE)

AFT PRESSURE BULKHEAD - BS 1016 WEB CRACKED, Y CHORD INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAX CABIN, STA 947 FLOOR BEAM UPPER FLANGE CORRODED AT LBL 50.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND PASSENGER CABIN, STATION 947 FLOORBEAM UPPER FLANGE CORRODED AT LBL 50. THE CORRODED FLOORBEAM SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW EO COO-3-53-233-01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND PASSENGER CABIN, STATION 947 FLOORBEAM UPPER FLANGE CORRODED AT LBL 50. THE CORRODED FLOORBEAM SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW EO COO-3-53-233-01. (M)

Part: SKIN — DENTED (FUSELAGE)

THE FUSELAGE SKIN AT BS 890 BETWEEN STRINGER 20R AND 21R WAS FOUND DENTED. THE DAMAGED AREA WAS REPAIRED IAW BOEING FAX COO-SJD-01-003292MM DATED 6/11/2001. (M)

Part: SKIN — DENTED (FUSELAGE)

THE FUSELAGE SKIN AT BS 890 BETWEEN STRINGER 20R AND 21R WAS FOUND DENTED. THE DAMAGED AREA WAS REPAIRED IAW BOEING FAX COO-SJD-01-00392M DATED 6/11/2001. (M)

Part: SPLICE — CRACKED (FUSELAGE)

FOUND PASSENGER CABIN BS 540, STRINGER 11R SPLICE HAS CRACK. THE PART WAS REPLACED IAW SRM 51-10-1 PAGE 8 AS RM 51-30-2. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

FOUND FLOORBEAM FOUND CRACKED AT BS 520 RBL 25 WL 208. THE DAMAGED AREA WAS REPAIRED IAW SB 737-53-1120. (M)

Part: STRINGER — CRACKED (FUSELAGE)

FOUND STRINGER AT STATION BS 727B STRINGER 9 LEFT HAS CRACK. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIG 3. (M)

Part: SKIN — CANNING (FUSELAGE)

THE FUSELAGE SKIN WAS FOUND WITH OIL CANNING. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-30-3 FIGURE 3. (M)

Part: SKIN — DELAMINATED (SPOILER)

THE UPPER SKIN OF SPOILER NR 8 WAS FOUND DELAMINATED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-246-01. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

FOUND FLOORBEAM AT BS 520 RBL 25 INCH LOWER CHORD HAS CRACK. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-9 FIGURE 7. (M)

Part: FRAME — CRACKED (FUSELAGE)

FOUND LOWER FUSELAGE BS 663.75 LBL 25 INCHES WL 208 CHORD CRACKED. THE DAMAGED AREA WAS REPAIRED PER SB 737-53-1184. (M)

Part: SLAT — DELAMINATED (WING)

THE NR 3 SLAT WAS FOUND DELAMINATED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-239-01. (M)

Part: SKIN — DELAMINATED (SPOILER)

THE UPPER SKIN OF THE NR 5 SPOILER WAS FOUND DELAMINATED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-248-01 DATED JUNE 8-01. (M)

Part: SKIN — CRACKED (E/E DOOR)

FOUND RIGHT AFT CORNER SKIN OF E/E COMPARTMENT DOOR HAS CRACK. THE DAMAGED AREA WAS REPAIRED IAW SRM 52-00-3 FIGURE 5. (M)

Part: STRINGER — CRACKED (FUSELAGE)

FOUND STRINGER CRACKED AT BS 312, STRINGER 4 RIGHT. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 3. (M)

Part: SKIN — DELAMINATED (SPOILER)

THE GROUND SPOILER NR 4 WAS FOUND DELAMINATED IN SEVERAL PLACED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-247-01. (M)

Part: STRINGER — CRACKED (FUSELAGE)

FOUND CRACK IN PASSENGER CABIN BS 767 STRINGER 9R. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 3. (M)

Part: SKIN — CORRODED (FUSELAGE)

FOUND CORROSION ON THE FUSELAGE SKIN AT BS 967, STRINGER 27R. (M)

Part: SPLICE — CRACKED (FUSELAGE)

FOUND PASSENGER CABIN BS 540 STRINGER 11R SPLICE HAS CRACK. THE PART WAS REPLACED IAW SRM 51-10-1 PAGE 8 AND 51-30-2. (M)

Part: FRAME — CRACKED (FUSELAGE)

FOUND CRACK IN FRAME STATION BS 344 STRINGER 6 LEFT. THE DAMAGED AREA WAS REPAIRED IAW SRM 51-40-3 FIGURE 1. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

THE FLOORBEAM WAS FOUND CORRODED AT BS 328, RBL 32. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-9 FIGURE 6. (M)

Part: FLAP — WORN (WING)

THE UPPER SURFACE OF THE INBOARD FORE FLAP WAS SHOWING WEAR. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-A57-243-01, DATED JUNE 06-01. (M)

Part: SPOILER — DELAMINATED (WING)

THE GROUND SPOILER NR 4 WAS FOUND DELAMINATED IN SEVERAL PLACED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-247-01. (M)

Part: FRAME — DAMAGED (FUSELAGE)

THE FRAME WAS FOUND WITH ELONGATED HOLES AT BS 328 BETWEEN STRINGER 2R AND STRINGER 3R. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-4 FIGURE 1. (M)

Part: STRINGER — CRACKED (FUSELAGE)

FOUND STRINGER CRACKED AT BS 440, STRINGER 4 RIGHT. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 3. (M)

Part: SKIN — DENTED (FUSELAGE)

FOUND FUSELAGE SKIN WAS FOUND DENTED AT BS 429 BETWEEN STRINGER 21R AND STRINGER 22R. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-30-3 FIGURE 1. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND LOWER FUSELAGE, BS 727 BULKHEAD, BLO WL 208 ANGLE CRACKED. DAMAGED AREA WAS REPAIRED PER SB 737-53-1053. (M)

Part: STRINGER — CORRODED (FUSELAGE)

AT STRINGER 27L FROM BS 1006 TO BS 1016, CORROSION WAS FOUND. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 1. (M)

Part: STRINGER — CRACKED (FUSELAGE)

FOUND CRACK IN PASSENGER CABIN BS 727 PLUS 9 AT STRINGER NR 1. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 3. (M)

Part: SKIN — DELAMINATED (SPOILER)

THE UPPER SKIN OF THE NR 5 SPOILER WAS FOUND DELAMINATED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-248-01, DATED JUNE 08, 2001. (M)

Part: SKIN — DELAMINATED (SPOILER)

THE UPPER SKIN OF SPOILER NR 8 WAS FOUND DELAMINATED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-246-01. (M)

Part: CONTROLLER — FAILED (COCKPIT)

FLT 2291 - EN ROUTE TO ACY, AUTO MODE ON PRESSURIZATION PANEL FAILED. DESCENDED FROM FL290 AND LEVELED OFF AT FL240 BY USING MANUAL MODE. AIRCRAFT LANDED ACY SAFELY. DEFERRED AUTOMATIC MODE ON PRESSURIZATION PANEL PER MEL 21-14-1. REF MEL 21-14-1. REMOVED AND REPLACED AUTO PRESS CONTROLLER. (M)

Part: CONTROLLER — DAMAGED (PRESSURE PANEL)

FLT 2291 - EN ROUTE TO ACY, AUTO MODE ON PRESSURIZATION PANEL FAILED. DESCENED FROM FL290 AND LEVELED OFF AT FL240 BY USING MANUAL MODE. AIRCRAFT LANDED ACY SAFELY. DEFERRED AUTOMATIC MODE ON PRESSURIZATION PANEL PER MEL 21-14-1. REF MEL 21-14-1. REMOVED AND REPLACED AUTO PRESSURIZATION CONTROLLER. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FLT 801 - ACY, ON DAILY SERVICE CHECK, MID CABIN CENTER AISLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M)

Part: BULKHEAD SUPPORT — CRACKED (BS 663)

DURING SCHEDULED C1 CHECK, FOUND FWD BULKHEAD RT WING SUPPORT FRAME I/B FLANGE HAS 2 CRACK STA 663 AND STRINGER 18. REPAIRED PER BOEING S/B.

Part: STIFFENER — CRACKED (BS 540)

DURING SCHEDULED C-CHECK, FOUND VERTICAL STIFFENER CRACKED AT TOP LIGHTING HOLE (APPROX 12 BELOW FLOOR LEVEL) AT FUSELAGE STA 540, 25 RT OF CENTERLINE. REPAIRED PER BOEING SRM.

Part: LANYARDS — MISINSTALLED (PAX DOOR)

DURING WALKAROUND CHECK, FOUND FWD ENTRY AND BOTH AFT DOOR SLIDE LANYARDS WERE IMPROPERLY INSTALLED. REMOVED AND REINSTALLED THEM PER BOEING M/M.

Part: THRESHOLD — CRACKED (CARGO COMPT)

DURING SCHEDULED RON CHECK, FOUND FWD CARGO THRESHOLD CRACKED AT AFT CORNER AND CENTER SECTIONS\N\NREPAIRED PER BOEING SRM

Part: SLIDE — LOW PRESS (AFT ENTRY)

DURING SCHEDULED RON CHECK, FOUND AFT ENTRY DOOR ESCAPE SLIDE PRESSURE LOW\N\NREPLACED PER BOEING M/M

Part: WIRE — BROKEN (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT LENS AT FWD ENTRY BROKEN. REPLACED PER BOEING M/M.

Part: STRINGER — DAMAGE (BS 500)

DURING SCHEDULED SV CHECK, FOUND STRINGER 9L DAMAGED AT BS 500B AT STRINGER FRAME CAP. REPAIRED PER BOEING SRM.

Part: SPLICE — CUT (BS 362.5)

DURING SCHEDULED SV CHECK, WHILE WORKING ON SKIN, ACCIDENTALLY CUT STRINGER SPLICE AT BS 362, AT S14R. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED SV CHECK, FOUND FRAMES CRACKED AT BS 767, S13L, AND FROM BS 727 TO 777, S4L. REMOVED AND REPLACED SECTION OF FRAME PER BOEING SRM.

Part: STRINGER — GOUGED (BS 787)

DURING SCHEDULED SV CHECK, FOUND STRINGER 10R WITH A DEEP GOUGE AT BS 787. REPAIRED PER BOEING SRM.

Part: STRINGER — MISDRILLED (BS 1008)

DURING SCHEDULED SV CHECK, FOUND DAMAGE TO S13L AT BS 1008, MISDRILLED HOLE. REMOVED AND REPLACED SECTION OF STRINGER PER BOEING SRM.

Part: DOORWAY FRAME — CUT (BS 947.5)

DURING SCHEDULED SV CHECK, FOUND DOORWAY FRAME CUT AT BS 947.5, AT LOWER HINGE CUTOUT. REPAIRED PER TRAMCO EWO 97-0727.

Part: SPLICE — CRACKED (BS 908)

DURING SCHEDULED SV CHECK, FOUND PRODUCTION SPLICE CRACKED AT BS 908, S4L IN TWO PLACES, AND AT BS 360, S4L. REMOVED AND REPLACED SECTION OF SPLICE PER BOEING SRM.

Part: DOOR — GOUGED (CARGO COMPT)

DURING SCHEDULED TERMINAL CHECK, FOUND AFT CARGO DOOR GOUGED. REPAIRED PER BOEING SRM.

Part: ACTUATOR — FAILED (NR 5 LE SLAT)

AFTER TAKEOFF, NR 5 L/E SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO OMA AND MADE AN UNEVENTFUL LANDING. REPLACED SLAT ACTUATOR PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED B-CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. RESECURED LIGHT AND OP CHECKED OK PER BOEING M/M.

Part: SKIN — CRACKED (BS 470/500/510)

DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510B, AT S10L, BS 470, AT S10L, AND AT BS 500-500A, AT S10L. REPAIRED SKIN PER BOEING SRM.

Part: SKIN — CRACKED (BS 315)

DURING SCHEDULED B-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 315 BETWEEN S7 AND 8L. REPAIRED PER SWA RA 1-253-1531 AND ACO 6317-53.

Part: SKIN — CRACKED (PAX DR CUTOUT)

DURING SCHEDULED B-CHECK, FOUND FWD FORWARD ENTRY DOOR CUTOUT UPPER RADIUS ON FUSELAGE SKIN CRACKED. REPAIRED PER SWA ACO 6317-53 AND RA 1-253-1521.

Part: SKIN — GOUGED (BS 294.5)

DURING SCHEDULED B-CHECK, FOUND FUSELAGE SKIN GOUGED BEYOND SRM LIMITS AT BS 294.5 AND S8L. REPAIRED PER SWA RA 1-253-1521.

Part: LIGHT — INOPERATIVE (COCKPIT)

DURING SCHEDULED RON CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT PER BOEING M/M.

Part: SKIN — CRACKED (AFT ENTRY AREA)

DURING SCHEDULED A CHECK, FOUND AFT ENTRY DOOR UPPER HINGE SKIN CUTOUT CRACKED AT LOWER RADIUS. REPAIRED PER SWA RA T1-A52-005.

Part: FIRE WARNING — ACTIVATED (APU)

DIVERTED TO SPS DUE TO APU FIRE WARNING IN FLIGHT. DISCHARGED FIRE BOTTLE. INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. DEFERRED APU FIRE DETECT SYSTEM AND FIRE BOTTLE PER MEL AND CONTINUED.

Part: FIRE WIRE — SHORTED (APU)

DIVERSION DUE TO APU FIRE WARNING IN FLIGHT. FIRE BOTTLE WAS DISCHARGED. INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. DEFERRED FIRE DETECT SYSTEM PER MEL, FOUND AND REPAIRED SHORTED WIRE PER BOEING M/M.

Part: CONTROL PANEL — MALFUNCTIONED (NR 2 ENGINE)

DURING DESCENT, NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. REMOVED AND REPLACED ENGINE/APU FIRE CONTROL PANEL, CLEANED AND RESECURED ENGINE FIRE LOOP CONNECTORS PER BOEING M/M.

Part: BLKHD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKS AT BS 178 BULKHEAD WEB AT LBL 5.7 AND RBL 5.7, ALONG SIDE I/B ROW OF FASTENER HOLES BETWEEN WL 207 AND 218. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (FS 520/521)

DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACK INDICATIONS AT THE FOLLOWING LOCATION: BS 520 AND 521, STRINGER 10L. REPAIRED PER TRAMCO EWO 95-0058.

Part: SKIN — CRACKED (BS 380)

DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 380, S14R. REPAIRED PER TRAMCO EWO 95-0058.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACKED FROM BS 480 TO 500B, 808, 858, STRINGER 10R. REPAIRED PER TRAMCO EWO 95-0058.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACK INDICATIONS AT THE FOLLOWING LOCATIONS: BS 380, 381, 400 TO 431, 450 TO 461, 490, 500, 500 PLUS 1, AND 500A TO 500B, STRINGER 10L. REPAIRED PER TRAMCO EWO 95-0058.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACK INDICATIONS AT THE FOLLOWING LOCATION: BS 379 TO 399, 479 TO 500, 500 PLUS 9, 500A, 500A PLUS 9, 500A PLUS 10, 500B PLUS 1, 588, 628, 684 TO 706, 746, 747, 777, 816, 817, 846, 847, 886, 887, 916, 945, 965 TO 995, STRINGER 4R. REPAIRED PER TRAMCO EWO 95-0058.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACK INDICATIONS AT THE FOLLOWING LOCATIONS: BS 400, 410, 420, 430, 440, 461 TO 500A, 500B, 500B PLUS 10, 586, 587, 605, 626, 705, 727A, 777, 778, 818, 838, 848, 868, 878, 888, 898, 925, STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0058.

Part: SKIN — DENTED (BS 413)

DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN DENTED AT BS 413, BETWEEN S5 AND 6R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.