N14308

Part: SKIN — CRACKED (BS 727D S23R) · airframe 61,487 hrs · 32,940 cycles

A WALKAROUND INSPECTION FOUND A CRACK IN THE FUSELAGE SKIN AT STA 727D, S23R. THE SKIN WAS REPAIRED IAW ECRA 5330-03745.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR SKIN AT AFT EDGE OF HANDLE CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, REPAIR 3.

Part: CHANNEL — CRACKED (FWD CARGO DOOR) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CHANNEL AT FORWARD LOWER STOP. REPAIRED IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR JAMB UPPER HINGE INTERCOSTAL AT STA 294.5, S10L. A REPAIR WAS INSTALLED IAW ECRA 5311-01350.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND TWO 1 INCH CRACKS IN R-1 DOOR SKIN CUTOUT AT STA 328, S16R. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5331-01337.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR JAMB LOWER HINGE INTERCOSTAL AT STA 294.5, S13L TO S14L. A REPAIR WAS INSTALLED IAW ECRA 5311-01349.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN FRAME AT DRAIN HOLE, STA 440, BL 0. A REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 201.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR INNER SKIN BETWEEN LIGHTENING HOLES ABOVE HANDLE. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01089.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A 1 INCH CRACK IN RIGHT I/B SEAT TRACK I/B MOUNT FLANGE AT STA 727B, RBL 24.8. A LONGITUDINAL FLOORBEAM REPAIR WAS INSTALLED IAW ECRA 5321-01492.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A 1 INCH CRACK AT TWO EACH HOLES IN I/B CHORD AT STA 639, S16R TO S17R. THE INNER CHORD WAS REPLACED AND A REPAIR WAS INSTALLED IAW ECRA 5311-01347.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A 1 INCH CRACK IN RIGHT I/B SEAT TRACK O/B MOUNT FLANGE AT STA 727B, RBL 45.5. A LONGITUDINAL FLOORBEAM REPAIR WAS INSTALLED IAW ECRA 55321-01492.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A 1 INCH CRACK IN LEFT O/B SEAT TRACK I/B MOUNT FLANGE AT STA 727B, LBL 45.5. A LONGITUDINAL FLOORBEAM REPAIR WAS INSTALLED IAW ECRA 5321-01492.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND FORWARD BAGGAGE BIN FRAME CORRODED AT STA 500B BETWEEN STRINGER 25R AND S26R. A SHEAR TIE REPAIR WAS INSTALLED IAW SRM 53-00-07, REPAIR 7.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND FRAME CORRODED AT STA 947.5 BETWEEN S21L AND S21R, LBL 10 TO RBL 10. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,977 hrs · 32,712 cycles

INSPECTION FOUND CRACKS TO THE LONGITUDINAL FLOORBEAM FLANGES AT STA 727B, LBL 45.5, RBL 45.5 AND RBL 24.8. REPAIRS WERE PERFORMED IAW ECRA 5321-01492.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A HOLE IN FUSELAGE SKIN CAUSED BY A LIGHTNING STRIKE AT STA 375, S24R. A SKIN REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 807, S9R. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04647.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 827, S9R. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04647.

Part: STRAP — CRACKED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A 1 INCH CRACK IN WEB STRAP JUST FORWARD OF L-2 DOOR AT STA 947.5, S10L TO S11L. A NEW WEB STRAP WAS INSTALLED IAW SRM 51-40-02.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND LEFT KEEL BEAM CORRODED IN A/C DISTRIBUTION BAY AT STA 500D-520. THE KEEL BEAM WAS REPAIRED IAW SRM 53-30-12, FIGURE 201.

Part: STRINGER — CORRODED (BS 294-323) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND STRINGER 28R CORRODED AT STA 294-323. THE STRINGER WAS REPLACED IAW SRM 51-40-02.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 60,977 hrs · 32,712 cycles

INSPECTION FOUND A CRACK EMANATING FROM THE DOORSTOP CUTOUT IN THE AFT EDGE BEAM OF THE L-1 DOOR. THE EDGE BEAM WAS REPAIRED IAW ECRA 5210-01944.

Part: FRAME — CORRODED (BS 1006) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND FRAME CORRODED AT STA 1006 FROM S25R TO 26L. THE CORRODED SECTION OF FRAME WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 201, REPAIR 1.

Part: STRINGER — CORRODED (BS 1006 S25L) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND STRINGER 25L CORRODED AT REPAIR CUTOUT AFT OF STA 1006. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPLACED IAW SRM 53-00-03, FIGURE 201, REPAIR 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AROUND FASTENER HOLE AT STA 360, BL 0. THE CORRODED AREA WAS CUT OUT AND REPAIR ANGLES WERE INSTALLED IAW SRM 53-30-51, FIGURE 201, REPAIR 2.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 60,978 hrs · 32,712 cycles

INSPECTION FOUND A 2.5 INCH CRACK IN LEFT SHEAR WEB FORWARD OF STA 639 FUSELAGE FRAME, LBL 50. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02.

Part: CONTROLLER — INOPERATIVE (WINDSHIELD HEAT) · airframe 57,972 hrs · 31,288 cycles

THE CREW REPORTED SMOKE IN THE CABIN WHILE EN ROUTE TO IAH. THE SMOKE REMOVAL CHECKLIST WAS COMPLETED AND AFTER TURNING OFF THE RECIRCULATION FAN THE SMOKE WENT AWAY. ALSO OBSERVED THAT THE RT FWD WINDOW HEAT CIRCUIT BREAKER HAD POPPED. THE CREW WAITED 10 MINUTES AND THEN RESET THE CIRCUIT BREAKER. ELECTRICAL FUMES AND SMOKE COULD BE DETECTED AT THAT TIME, SO THE RT FWD WINDOW HEAT WAS TURNED OFF AND THE CIRCUIT BREAKER WAS PULLED. THE FLIGHT LANDED AT IAH WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE NR 3 WINDOW HEAT CONTROLLER AT FAULT. THE NR 3 WINDOW HEAT CONTROLLER WAS REMOVED AND REPLACED IAW MM 30-41-11. OPERATIONAL CHECKS WERE GOOD.

Part: SHEAR TIE — CORRODED (STA 967) · airframe 56,517 hrs · 30,596 cycles

INSPECTION FOUND FRAME/SHEAR TIE CORRODED AT STA 967 BETWEEN STRINGERS 27L-27R. THE CORRODED SECTION OF SHEAR TIE WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 201, REPAIR 8.

Part: FRAME — CRACKED (NR 2 PYLON) · airframe 56,517 hrs · 30,596 cycles

INSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON FRAME (HORSE COLLAR FITTING) AROUND LOCK FASTENER COLLAR. THE NR 2 PYLON HORSE COLLAR WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: SKIN — CRACKED (BS 727E-747) · airframe 56,196 hrs · 30,432 cycles

INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN BETWEEN STA 727E - 747 JUST BELOW S24R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 31, FIGURE 201, DETAIL XI.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 54,028 hrs · 29,384 cycles

INSPECTION FOUND STRINGER 27L CORRODED AT STA 996. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 54,028 hrs · 29,384 cycles

INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,028 hrs · 29,384 cycles

INSPECTION FOUND FORWARD CARGO COMPARTMENT FLOORBEAM CORRODED AT STA 500D BETWEEN S26L AND S27L, LOWER AREA. THE CORRODED AREA WAS CUT OUT AND FILLER, DOUBLER AND A SHIM WERE INSTALLED IAW SRM 53-00-07, FIGURE 203 AND 204.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 54,028 hrs · 29,384 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED FROM STA 947.5 TO 967 AT RBL 7 AND RBL 46. NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-40-02 AND ECRA 5310-03585.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,028 hrs · 29,384 cycles

INSPECTION FOUND SEAT TRACK CORRODED AT STA 296, RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED IAW BOEING DRAWING 69-40352 AND SRM 51-40-02.

Part: CHANNEL — CRACKED (LT WING) · airframe 54,028 hrs · 29,384 cycles

INSPECTION FOUND THE LT WING T/E NR 3 FLAP TRACK FAIRING AFT END U-CHANNEL CRACKED IN TWO PLACES UNDER THE TRACK. THE CRACKS WERE .25 INCH LONG. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,028 hrs · 29,384 cycles

INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 294.5, RBL 41. THE FLOORBEAM UPPER CHORD SECTION WAS REMOVED AND A NEW UPPER CHORD WAS INSTALLED IAW SRM 53-10-51.

Part: ANGLE — CORRODED (STA 1006) · airframe 52,899 hrs · 28,783 cycles

INSPECTION FOUND CORROSION ON UPPER SURFACE OF ANGLE AT NUTPLATES, STA 1006, LBL 10. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (STA 967) · airframe 52,899 hrs · 28,783 cycles

INSPECTION FOUND FLOORBEAM CORRODED IN AFT GALLEY AREA AT STA 967, LBL 25. REPAIRED IAW ECRA 5320-01726.

Part: FLOORBEAM — CORRODED (STA 1016) · airframe 52,899 hrs · 28,783 cycles

INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES OF UPPER CAP AT STA 1006 FROM BL 0 TO RBL 40. REMOVED AND REPLACED T-CAP IAW ECRA 5310-03851.

Part: CHANNEL — CORRODED (STA 1006-1016) · airframe 52,899 hrs · 28,783 cycles

INSPECTION FOUND CHANNEL CORRODED ON UPPER SURFACE AND AT NUTPLATES AT STA 1006-1016, LBL 5 TO LBL 9. REMOVED AND REPLACED CHANNEL IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (STA 1006) · airframe 52,899 hrs · 28,783 cycles

INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE OF CAP AND AT FASTENER HOLES AT STA 1006, BL 0 TO RBL 30. THE T-CAP WAS REMOVED AND REPLACED IAW SRM 51-40-04.

Part: FRAME — CORRODED (STA 986) · airframe 52,910 hrs · 28,789 cycles

INSPECTION FOUND R/H O/B FRAME CORRODED AT STA 986, RBL 40. REPAIRED IAW ECRA 5310-03851.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 52,910 hrs · 28,789 cycles

INSPECTION FOUND A .5 INCH CRACK IN PRESSURE DECK AT BS 664 - 675, LBL 30 - 35. REPAIRED IAW SRM 53-60-51, PAGE 213-221.

Part: PRESSURE PANEL — CRACKED (FS 663) · airframe 52,910 hrs · 28,789 cycles

INSPECTION FOUND A 2.75 INCH CRACK IN RT WHEEL WELL PRESSURE DECK AT FS 663, RBL 35. REPAIRED IAW SRM 53-60-51, PAGE 213-231.

Part: SKIN — CRACKED (FWD CARGO DR) · airframe 50,221 hrs · 27,385 cycles

INSPECTION FOUND A 3/4" CRACK AT LIGHTENING HOLE CUTOUT OF FORWARD CARGO DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 5232-01014.

Part: NOSE COWL — DELAMINATED (#1 ENGINE) · airframe 50,221 hrs · 27,385 cycles

INSPECTION FOUND #1 ENGINE NOSE COWL DELAMINATED. THE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-11-01.

Part: SKIN — DELAMINATED (R/H WING L/E) · airframe 50,221 hrs · 27,385 cycles

INSPECTION FOUND R/H WING LEADING EDGE SKIN UNDER O/B EDGE OF #5 SLAT DELAMINATED. REPAIRED IAW ECRA 5721-01048.

Part: ATTACH ANGLE — WORN (STA 1104-1121) · airframe 50,221 hrs · 27,385 cycles

INSPECTION FOUND ATTACH ANGLE ON BOTTOM OF VERTICAL STABILIZER ON R/H SIDE WORN THIN AT STA 1104-1121. THE ATTACH ANGLE WAS REPLACED IAW ECRA 5300-01013, REV B.

Part: SKIN — DELAMINATED (L/H WING L/E) · airframe 50,221 hrs · 27,385 cycles

INSPECTION FOUND L/H WING LEADING EDGE SKIN DELAMINATED AND HILOCK PULLED THROUGH SKIN BEHIND #2 SLAT AT O/B END. REPAIRED IAW ECRA 5721-01048.

Part: SKIN — DENTED (CARGO DOOR)

INSPECTION FOUND AFT CARGO DOOR SKIN DENTED. THE DENTED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-30-01, FIGURE 201.

Part: SKIN — CRACKED (NR 1 PYLON)

INSPECTION FOUND A .5 INCH CRACK AT O/B FORWARD CORNER OF NR 1 ENGINE PYLON ACCESS PANEL 5727L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5340-01230.

Part: FLOORBEAM — CORRODED (BS 967)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 967 ABOUT 20 INCHES FROM CENTERLINE TO BOTH LT AND RT SIDES. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW ECRA 5310-03909.

Part: STRINGER — CRACKED (BS 277)

INSPECTION FOUND A .5 INCH CRACK IN STRINGER 6L AT STA 277. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 203.

Part: SKIN — DENTED (CARGO DOOR)

INSPECTION FOUND FORWARD CARGO DOOR EXTERIOR SKIN DENTED. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.

Part: FRAME — CRACKED (BS 616)

INSPECTION FOUND MAIN FRAME CRACKED AT STA 616, S18L AND S18R. THE CRACKS WERE 1 AND .75 INCH LONG. DOUBLERS WERE INSTALLED IAW ECRA 5360-01024.

Part: GALLEY TRACK — CORRODED (BS 328-360)

INSPECTION FOUND RT O/B GALLEY MOUNT TRACK CORRODED AT STA 328-360. THE MOUNT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-2.

Part: SKIN — DENTED (BS 344-360)

INSPECTION FOUND FUSELAGE SKIN DENTED FROM STA 344-360, WL 190R. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURES 201, 202, AND 223.

Part: FLOORBEAM — CORRODED (BS 294)

INSPECTION FOUND CABIN FLOORBEAM UPPER SURFACE CORRODED AT STA 294 FROM LBL 20 TO RBL 30. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED USING SPLICE ANGLES IAW SRM 53-10-51, FIGURE 205.

Part: STRINGER — CRACKED (BS 500)

INSPECTION FOUND A .75 INCH CRACK IN STRINGER 16R AT BS 500C. THE CRACKED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-00-03, FIGURE 201.

Part: SKIN — DENTED (BS 328)

INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 328, WL 190. THE SKIN WAS REPAIRED IAW SRM 53-00-01.

Part: WIRE — BROKEN (ROW 25)

INSPECTION FOUND ROW 25 EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN/PULLED FROM SPLICE. THE SPLICE WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY LIGHTING CHECKED GOOD.

Part: SKIN — CORRODED (BS 986.5-1016)

INSPECTION FOUND FUSELAGE SKIN CORRODED BETWEEN STA 986.5 AND 1016, WL 208.10. A REPAIR WAS INSTALLED IAW SRM 53-00-01 AND ECRA 5331-01008.

Part: SUPPORT — CORRODED (BS 986-1010)

INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN BS 986.5 TO 1010, LBL 15. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 967-987)

INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN STA 967 TO 986.5, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (BS 967)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, LBL 4. REPAIRED IAW SRM 53-30-51.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE L-1 AND R-1 DOOR EXIT LIGHTS DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK.

Part: POWER SUPPLY — INOPERATIVE (ROW 11-12)

HOU - THE EMERGENCY EXIT SIGN, BETWEEN ROW 11 AND ROW 12, FAILED THE 15 MINUTE DURATION TEST. THE POWER SUPPLY (CHARGER AND BATTERY) FOR THE EXIT SIGN WAS REMOVED AND REPLACED AND OPERATION WAS RESTORED. (M)

Part: DNLOCK SENSOR — INOPERATIVE (NLG)

IAH - FLT 0692 - THE NLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR WAS EXTENDED ON APPROACH TO IAH. THE TOWER REPORTED THE NLG WAS NOT DOWN. DURING A FLY-BY, A VISUAL INSPECTION ALSO CONFIRMED NLG WAS NOT DOWN. CYCLING GEAR TWICE AND USING MANUAL EXTENSION PROCEDURES RESULTED IN NO CHANGE. AN EMERGENCY WAS DECLARED, GEAR WAS RETRACTED AGAIN, AND ANOTHER APPROACH WAS ATTEMPTED. WHEN GEAR WAS EXTENDED, MLG LIGHTS WERE NORMAL, BUT NO NLG GREEN LIGHT, NLG LIGHT WAS SWITCHED WITH LT MLG GREEN LIGHT AND NLG SHOWED DOWN AND GREEN. ACFT LANDED WITHOUT INCIDENT. MX FOUND NLG DOWNLOCK SENSOR AT FAULT. SENSOR REMOVED AND REPLACED PER MM 32-61-41. OPER CHKS GOOD DURING GEAR SWING. (X)

Part: SKIN — DAMAGED (FUSELAGE)

FLT NR 1698 - IAH - HOLE IN FORWARD SIDE OF AIRCRAFT FWD OF L-1 DOOR REPAIRED PER SRM 53-00-01 BLIND RIVIT REPAIR. INSPECTION EVERY 2500 FLT HOURS. REPLACE PRIOR TO 20,000 FLT HOURS. INITIATED DIP NR 24087. (W)