N14831

Part: SKIN — CRACKED (MCD) · airframe 47,738 hrs · 23,028 cycles

INSPECTION FOUND A 0.44" CRACK IN SKIN AT BOTTOM EDGE OF MAIN CABIN DOOR. THE CRACK WAS LOCATED APPROXIMATELY 16 INCHES AFT OF FORWARD EDGE. A REPAIR WAS INSTALLED IAW ECRA 5210-01478.

Part: SKIN — GOUGED (LH VERT STAB) · airframe 47,738 hrs · 23,028 cycles

INSPECTION FOUND THAT THE LEADING EDGE OF BOTTOM L/H BANANA FAIRING HAD GOUGED SKIN OF VERTICAL STABILIZER. THE LEADING EDGE PLATING WAS REMOVED AND REPLACED IAW SRM 53-30-0.

Part: SKIN — CORRODED (STA 712-731) · airframe 47,738 hrs · 23,028 cycles

INSPECTION FOUND LOWER FUSELAGE SKIN CORRODED BETWEEN STA 712 AND 731, LONGERONS 29R-30. A REPAIR DOUBLER AND TRIPLER WERE INSTALLED IAW ECRA 5331-01116.

Part: APU — LEAKING (TAIL) · airframe 42,158 hrs · 20,058 cycles

THE CABIN AND COCKPIT FILLED WITH SMOKE WHILE IN CRUISE AT 37,000 FT, EN ROUTE FROM SJC TO IAH. EMERGENCY PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS DIVERTED TO SAT WHERE IT LANDED SAFELY. MAINTENANCE FOUND COOLING FAN WHERE IT ATTACHES TO GEARBOX LEAKING OIL. THE APU WAS REMOVED AND REPLACED IAW WORK CARD 08-4900-1-0002. IN ADDITION, BOTH AC PACK COALESCER BAGS WERE REMOVED AND REPLACED IAW MM 21-20-02. OPERATIONAL CHECKS WERE GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

SEAT TRACK CORRODED RIGHT SIDE AT STA 1212 TO 1320. REMOVED DAMAGED SECTION, INSTALLED NEW SECTION PER SRM 51-30-1.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

FWD CARGO RIGHT TIE DOWN TRACK IS CORRODED FROM STA 360 TO 370. REMOVED AND REPLACED DAMAGED SECTION PER SRM 53-10-3, 51-30-1, AND 51-10-4.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

MID PIT LEFT TIE DOWN TRACK CORRODED FROM STA 522 TO 788. REMOVED DAMAGED SECTION AND REPLACED PER SRM 51-10-3 AND 53-05 FIG 4G.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

MID CARGO DOOR INNER SKIN CRACKED (.75) AT UPPER AFT CORNER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EC/RA 5230-01541.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

MID PIT RIGHT TIE DOWN TRACK FROM STATION 522 TO 788 CORRODED. REMOVED DAMAGED SECTION AND REPLACED WITH NEW SECTION PER SRM 51-10-3, 51-10-4, AND 51-30-1.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 41,740 hrs · 19,858 cycles

CARGO TIE DOWN TRACK IN AFT CARGO PIT AT FS 1174 LONG 28 LT IS CORRODED. REMOVED DAMAGED AREA. INSTALLED NEW SECTION PER SRM 53-05 FIG 4G.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

FORWARD LOWER TCAS ANTENNA DOUBLER AND FUSELAGE SKIN CORRODED STA 279 - 294. REPAIRED PER EC/RA 5330-02949.

Part: STRUCTURE — CHAFED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

AFT CARGO DOOR FOWARD LOWER CORNER IS CHAFED. REMOVED DAMAGED AREA. INSTALLED REPAIR PER SRM 52-01 FIG 1.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

FORWARD CARGO DOOR HOLD OPEN BRACKET TO INTERCOSTAL ATTACH BRACKET IS CRACKED (3) AT FS 427. REMOVED AND REPLACED BRACKET PER SRM 51-30-5, 51-10-4, AND 51-10-3.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

AFT CARGO FLOOR SUPPORT TO FRAME 1250 IS CRACKED LONG 26L TO LONG 30 (40). REMOVED AND REPLACED CRACKED SUPPORT PER SRM 51-30-2.

Part: PAN — CORRODED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

FORWARD CARGO DOOR JAMB PAN HAS AREA OF SURFACE CORROSION. REMOVED DAMAGED AREA. INSTALLED REPAIR PER SRM 53-05 FIG 44, 51-30-01, 51-30-02, 51-30-05, AND 51-10-3.

Part: WEB — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

MAIN CUSP WEB IS CORRODED AT LONGERON 18R STA 636 TO 674. REMOVED AND REPLACED CUSP WEB FROM STA 598 TO 712 PER SRM 51-30-1, 51-30-2,AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

AFT CARGO BAY FLOOR SUPPORT AT CARGO DOOR IS CORRODED AT FASTENER HOLES STA 1155. REMOVED CORRODED SECTION. REPLACED FLOOR SUPPORT PER SRM 51-10-3, 53-01 FIG 1, 51-30-2, AND 51-10-4.

Part: FLOOR SUPPORT — DAMAGED (SERVICE DOOR) · airframe 41,740 hrs · 19,858 cycles

FWD SERVICE DOOR SCUFF PLATE INBOARD MOUNT ID DAMAGED AND DRILLED OFF FASTENERS. REMOVED, REPAIRED, AND REINSTALLED FLOOR SUPPORT PER SRM 51-30-2, 51-10-4, AND 51-30-5.

Part: LONGERON — CORRODED (CARGO BAY) · airframe 41,740 hrs · 19,858 cycles

MID PIT STA 655 LONG 30 HAS CORROSION AROUND FASTENERS. REMOVED AND REPLACED LONG 30 PER EA 9-5314-2-A0654, SRM 53-02 AND EC/RA 5310-04004.

Part: WEB — CRACKED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

MAIN CABIN CUSP WEB CRACKED (4) AT FS 1300 LBL 56. REMOVED AND REPLACED CUSP WEB PER SRM 51-30-2, 51-10-4, 51-10-3, 51-30-1, AND 51-30-5.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,740 hrs · 19,858 cycles

SEAT TRACK FS 218 RIGHT O/B HAS SURFACE CORROSION. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK PER SRM 51-10-3, 51-30-1, AND 51-30-2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

AFT PRESSURE BULKHEAD FIRST HORIZONTAL FRAME IS CRACKED AT LT END (.5). REMOVED AND REPLACED FRAME PER SRM 51-30-2, 51-10-4, AND 51-30-5.

Part: SUPPORT BRACKET — CRACKED (WING-BODY FAIRING) · airframe 41,740 hrs · 19,858 cycles

EXTERNAL FUSELAGE STA 875 LEFT HAND KEEL AREA WING TO BODY FAIRING SUPPORT CRACKED (4). REMOVED CRACKED SUPPORT AND INSTALLED NEW FRAME PER SRM 51-30-1, 51-10-03, AND 51-30-02.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 41,740 hrs · 19,858 cycles

FORWARD CARGO FLOOR SUPPORT HAS BARE METAL AND CORRODED AT LOWER SURFACE ABOVE LGR 28R STA 427 TO 465. REMOVED AND REPLACED FLOOR SUPPORT Z ANGLE PER SRM 51-30-2, 51-10-4, AND 51-10-3.

Part: PAN — CORRODED (PAX DOOR) · airframe 41,740 hrs · 19,858 cycles

R1 DOOR FLOOR PAN CORRODED. REMOVED, REPAIRED, AND REINSTALLED FLOOR PAN PER SRM 51-30-1 AND 51-10-4.

Part: ANGLE — CORRODED (CABIN) · airframe 41,740 hrs · 19,858 cycles

CABIN FLOOR SUPPORT ANGLE IS CORRODED AT LBL 55 STA 160 TO 200. REMOVED DAMAGED ANGLE. INSTALLED NEW ANGLE PER SRM 51-30-2, 51-10-3, AND 51-30-5.

Part: CHANNEL — BENT (HOIZONTAL STAB) · airframe 41,740 hrs · 19,858 cycles

LEFT HORIZONTAL STAB TRAILING EDGE SECTION HAT SECTION BENT (3 X 1). REMOVED AND REPLACED HAT CHANNEL PER SRM 51-30-2 AND 51-30-08.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 41,740 hrs · 19,858 cycles

SUPPORT AT FORWARD CORNER OF AFT CARGO DOOR FS 1155 LONGERON 28R CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED DAMAGED SUPPORT PER SRM 51-30-1 AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 417,470 hrs · 19,858 cycles

CABIN FLOOR SUPPORT AT RBL 44 FS 160 - 200 IS CORRODED. REMOVED AND REPLACED DAMAGED FLOOR SUPPORT PER SRM 51-30-2, 51-10-4, 51-30-5, AND 51-10-3.

Part: WEB — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

RIGHT HAND CUSP WEB AT LONGERON 18R BETWEEN FS 826 AND 845 HAS CORROSION. INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

CABIN FLOOR SUPPORT AT L2 DOOR FS 1148 IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-2 AND 51-10-4.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 41,740 hrs · 19,858 cycles

FORWARD CARGO LEFT TIE DOWN TRACK IS CORRODED FROM STA 389 TO 446. CUT OUT CORRODED SECTION OF TRACK. INSTALLED NEW TRACK PER SRM 51-10-3, 53-01 FIG 1, 51-10-4, AND 51-30-02, -05.

Part: WEB — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

WEB UNDER PILOT AFT INBOARD SEAT TRACK LOOKING FROM E & E BAY IS CORRODED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER PER SRM 53-01, 51-30-02 AND 51-30-01.

Part: WEB — CORRODED (CARGO BAY) · airframe 41,740 hrs · 19,858 cycles

AFT CARGO BAY STA 1180 MAIN DECK FLOOR WEB CORRODED OUTBOARD OF LT OUTBOARD SEAT TRACK. REMOVED SECTION OF WEB AND INSTALLED NEW SECTION PER SRM 51-30-2, 53-01 FIG 2, 51-10-4, AND 51-30-1.

Part: FRAME — DENTED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

AFT CARGO BAY STA 1231 FRAME IS BENT AT LONG 27L. REMOVED AND REPLACED DAMAGED AREA PER SRM 53-03 FIG 5 AND 51-10-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

CABIN FLOOR SUPPORT AT L2 DOOR FS1163 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-02 AND 51-10-04.

Part: INTERCOSTAL — CORRODED (CARGO BAY) · airframe 41,740 hrs · 19,858 cycles

TOP AND BOTTOM SIDE OF HORIZONTAL STIFFENER IN AFT CARGO PIT BETWEEN FS 1307 AND FS 1320 AT LONG 28L CORRODED. REMOVED DAMAGED AREA, INSTALLED NEW INTERCOSTAL PER SRM 51-10-03, 53-01 FIG 1, 51-30-02, AND 51-30-5.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

LEFT SIDE AFT ACCY COMPARTMENT DIVERTER VALVE HOUSING ATTACH BRACKET BROKEN. REMOVED AND INSTALLED NEW BRACKET PER SRM 51-30-2.

Part: SKIN — GOUGED (VERTICAL STAB) · airframe 41,740 hrs · 19,858 cycles

VERTICAL STAB LEFT UPPER PANEL AFT OF ROLLER RUBSTRIP GOUGED. REMOVED AND REPLACED PANEL ON VERTICAL STAB PER SRM 51-30-2, 51-30-5, AND 51-30-1.

Part: ANGLE — CORRODED (CARGO BAY) · airframe 41,740 hrs · 19,858 cycles

FORWARD CARGO FORWARD WALL TO FLOOR PANEL ANGLE IS BENT AND CORRODED. REMOVED AND REPLACED ANGLE PER SRM 51-30-2, 51-10-4, AND 51-10-3.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND FORWARD CARGO DOOR LOWER AFT STOP HAD CHAFED INTO SKIN IN TWO PLACES. A DOUBLER REPAIR WAS INSTALLED AT PLACE IAW SRM 52-03, FIGURE 8.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND AFT CARGO THRESHOLD SUPPORT ANGLE CORRODED ON BOTTOM AT FS 1155 - 1212, L29R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-1.

Part: PAN — CHAFED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND MID CARGO DOOR LOWER SECTION OF FLANGE FOR SEAL RETAINERS CHAFED AT STOP PAD LOCATIONS. THE AREA WAS BLENDED IAW SRM 52-01, FIGURE 1. A REPAIR DOUBLER WAS INSTALLED AT FORWARD AND AFT LOCATIONS IAW SRM 51-10-4, 51-10-3, AND 52-03, FIGURE 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND LEFT CENTER SEAT TRACK CORRODED AT FS 1200 - 1309 AND LEFT I/B SEAT TRACK CORRODED AT FS 1212 - 1231. NEW SEAT TRACK SECTIONS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, AND 53-05, FIGURE 4F.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND AFT CARGO DOOR UPPER FORWARD AND AFT STOPS HAD CHAFED THE SKIN. A REPAIR DOUBLER WAS INSTALLED AT LOCATION IAW SRM 51-10-4, 51-10-3, 52-03, FIGURE 8, AND 51-30-2.

Part: PAN — CRACKED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND A 0.4 CRACK IN MID CARGO DOOR FORWARD PAN LEADING EDGE SKIN UNDER FITTING (TWO INCHES ABOVE TORQUE TUBE). THE FITTING WAS REMOVED IAW SRM 51-30-5 AND THE CRACK WAS STOP DRILLED. THE DOOR PAN WAS REPAIRED AND THE FITTING WAS REINSTALLED IAW ECRA 5330-02819 AND SRM 51-30-5.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND AFT CARGO BAY FRAME CORRODED ON AFT SIDE AT STA 1307, LONGERON 27L-27R. THE CORRODED SECTION OF FRAME WAS CUT OUT AND REPAIRED IAW SRM 53-03, FIGURE 2A.

Part: WEB — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND CUSP WEB CORRODED AT FS 560 - 579, LBL 55. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01, FIGURE 4. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-3, AND 51-30-02.

Part: CHANNEL — CRACKED (TE FLAP) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND A 2 INCH CRACK IN U-CHANNEL AT LEFT I/B FLAP WEDGE NR 2 I/B SIDE. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-2 AND 51-10-3.

Part: FITTING — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND GALLEY FLOOR MOUNT FITTING CORRODED AT STA 210, RBL 10. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2, 53-14-1, FIGURE 11, 51-10-3, AND 51-30-1.

Part: WEB — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND CABIN SUBFLOOR WEB CORRODED AT STA 204, LBL 6. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4, 53-14-1, 51-10-4, AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND FLOOR SUPPORT ANGLES CORRODED AT STA 200, RBL 12 - RBL 50 AND LBL 9 - LBL 14. THE FLOOR SUPPORT ANGLES WERE REMOVED AND NEW SUPPORT ANGLES WERE INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND AFT CARGO BAY LEFT I/B MAIN DECK SEAT TRACK CORRODED AT STA 1136 - 1193 AND MAIN CABIN RIGHT O/B SEAT TRACK CORRODED AT STA 1150, RBL 54.5. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW SRM 51-10-4, 51-30-5, AND 51-30-1.

Part: PAN — CHAFED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND AFT CARGO DOOR AFT SIDE THIRD STOP HAD CHAFED SKI. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2 AND ECRA 5330-02819.

Part: FLANGE — CRACKED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND A 1.2 INCH CRACK IN FORWARD CARGO DOOR AFT SIDE SEAL FLANGE AT LATCH CAM. THE CRACK WAS STOP DRILLED IAW SRM 52-05. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A AND 51-30-5.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND FORWARD CARGO DOOR AFT SIDE 2ND THROUGH 5TH STOPS AND TOP STOP CHAFED INTO SKIN. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02819 AND SRM 51-10-4.

Part: BEAM — CORRODED (DOOR JAMB) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND MID CARGO DOOR JAMB BEAM CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-3. THE AREA WAS REPAIRED IAW SRM 51-10-4, 51-10-3, AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND AFT CARGO BAY FLOOR SUPPORT CORRODED AT STA 1155. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-5, 53-14-3, FIGURE 12, 51-10-4, AND 51-10-3.

Part: SKIN — DENTED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND FORWARD EDGE OF FORWARD CARGO DOOR OUTER SKIN DENTED. THE AREA WAS BLENDED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-01, FIGURE 1 AND 52-05, FIGURE 4, PAGE 5.

Part: FLANGE — CHAFED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND MID CARGO DOOR FORWARD FLANGE FOR SEAL RETAINER ATTACHMENT CHAFED AT STOP PAD LOCATIONS. REPAIRED IAW SRM 51-30-1,51-30-2, AND ECRA 5330-02819.

Part: FLANGE — CHAFED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND MID CARGO DOOR T/E SEAL RETAINER ATTACH FLANGE OUTER SURFACE CHAFED AT STOP PAD LOCATIONS. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02819, SRM 51-30-2, AND 51-10-4.

Part: FITTING — CORRODED (GIRT BAR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND R-1 DOOR GIRT BAR LATCH FITTINGS CORRODED. THE FITTINGS WERE REMOVED AND NEW FITTINGS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND CHAFED SKIN AT AFT CARGO DOOR AFT SIDE 1ST, 2ND, 4TH, AND 5TH STOPS. A DOUBLER REPAIR WAS INSTALLED AT EACH LOCATION IAW ECRA 5330-02819, SRM 51-10-4, 51-10-3, AND 51-30-2.

Part: SKIN — DENTED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND MID CARGO DOOR OUTER SKIN FORWARD EDGE DENTED. REPAIRED IAW SRM 52-05, FIGURE 4, 51-10-3, AND 51-30-2.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 41,740 hrs · 19,858 cycles

INSPECTION FOUND FORWARD CARGO DOOR FORWARD SIDE FIRST THROUGH FIFTH STOPS FROM TOP HAD CHAFED INTO SKIN. REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW ECRA 5330-02819.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 41,470 hrs · 19,858 cycles

INSPECTION FOUND CHAFED SKIN AT AFT CARGO DOOR FORWARD SIDE 1ST, 4TH, AND 5TH STOPS. A DOUBLER REPAIR WAS INSTALLED AT EACH LOCATION IAW ECRA 5330-02819, SRM 51-30-2, AND 51-10-4.

Part: LONGERON — CORRODED (BS 486-490)

INSPECTION FOUND LONGERON 30 IN FORWARD CARGO COMPARTMENT CORRODED FROM STA 486 TO 490. A NEW LONGERON WAS FABRICATED AND INSTALLED IAW SRM 53-02.

Part: COVER — BROKEN (LT EXCAPE ROPE)

THE LT OVERWING ESCAPE ROPE COVER WAS FOUND BROKEN FROM ITS MOUNTS. THE COVER WAS REPLACED IAW MM 25-61-00.

Part: SWITCH — INOPERATIVE (APU)

THE APU HAD A BRIEF HISTORY OF AUTO SHUTDOWN IN FLIGHT WITH APU LOW OIL PRESSURE LIGHT ILLUMINATING. THE APU WAS IN OPERATION DUE TO THE AC CROSSTIE BEING ON PLACARD. THE APU WAS RUN WHILE ON RON AT IAH AND THE AUTO SHUTDOWN COULD NOT BE DUPLICATED. THE WIRING TO DOOR ACTUATOR, THREE SPEED SWITCH, FCU SOLENOID, AND LOW OIL PRESSURE SWITCH WERE INSPECTED WITH NO FAULTS FOUND. THE OIL PRESSURE SWITCH WAS REPLACED AS A PRECAUTIONARY MEASURE.

Part: STATOR SUPPT — BROKEN (NR 2 ENGINE)

THE TOWER REPORTED TO FLIGHT CREW THAT THEY SAW SPARKS COMING FROM NR 2 ENGINE AFTER TAKEOFF. ENGINE POWER WAS NORMAL AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. *S/D* SHOP FINDINGS REVEALED THE 8TH STAGE STATOR SUPPORT HAD BROKEN.

Part: SKIN — IMPACTED (LT MLG DOOR)

INSPECTION FOUND LT MLG DOOR SKIN DAMAGED AND FORMER BENT DUE TO IMPACT DAMAGE FROM BLOWN TIRE. THE FORMER WAS REPLACED AND A SKIN REPAIR SPLICE WAS INSTALLED IAW SRM 52-05, FIGURE 38 AND SRM 51-01, PAGE 4E.

Part: SKIN — TORN (LT TE FLAP)

INSPECTION FOUND INBOARD LOWER TRAILING EDGE SKIN OF LT FLAP ASSEMBLY TORN WITH BENT SPAR. THE LOWER SKIN PANEL WAS REPLACED AND A SPAR SPLICE WAS INSTALLED IAW SRM 57-50-14.

Part: DOOR PAN — GOUGED (CARGO DOOR)

HOU - INSPECTION FOUND A GOUGE INBOARD OF HOLD OPEN ON AFT CARGO DOOR PAN. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5230C01117. (M)

Part: SKIN — DENTED (BS 120)

HOOU - INSPECTION FOUND A SMALL DENT IN LEFT FUSELAGE SKIN AT STATION 120 ABOVE LONGERON 19. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38. (M)

Part: FLOOR SUPPORT — CORRODED (BS 1155)

HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED AT STATION 1155. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-5. (M)

Part: SUPPORT — CORRODED (G-2 GALLEY)

HOU - INSPECTION FOUND CORROSION ON G-2 GALLEY FORWARD ATTACH POINT SUPPORT. A SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. (M)

Part: MOUNT SUPPORT — CORRODED (C-2 GALLEY)

HOU - INSPECTION FOUND THE C-2 GALLEY AFT MOUNT SUPPORT CORRODED. THE MOUNT SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5. (M)

Part: FLOOR SUPPORT — CRACKED (BS 788)

HOU - INSPECTION FOUND A .875 INCH CRACK IN CABIN FLOOR SUPPORT AT STATION 788, AIRCRAFT CENTERLINE. A NEW DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2. (M)

Part: SKIN — DENTED (BS 154)

HOU - INSPECTION FOUND A SMALL DENT IN FORWARD LOWER FUSELAGE SKIN AT STATION 154, LONGERON 26L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 21. (M)