N16807

Part: DOUBLER — GOUGED (THRUST REVERSER) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND DOUBLER AT NR 2 ENGINE LOWER T/R O/B CORNER BENT AND GOUGED. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-0.

Part: SKIN — DENTED (SPOILER) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND RT GROUND SPOILER SKIN DENTED IN TWO PLACES ON UPPER SURFACE. THE DENTED AREAS WERE REMOVED AND DOUBLERS WERE INSTALLED IAW SRM 57-04, FIGURE 5.

Part: PAN — CRACKED (LT MLG DOOR) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND A 1.25 INCH CRACK IN LT MLG I/B DOOR FORWARD LOWER PAN. THE CRACK WAS STOP DRILLED IAW EA 9-52812-A0807. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.

Part: DOUBLER — GOUGED (CARGO DOOR) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND REPAIR DOUBLERS AT FORWARD AND AFT LOWER CORNER OF AFT CARGO DOOR GOUGED. THE DOUBLERS WERE REMOVED AND REPLACED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.

Part: PAN — CRACKED (CARGO DOOR) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND A 2" CRACK IN MID CARGO DOOR OUTER PAN AT LOWER EDGE AFT STOP AREA. A DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8 AND ECRA 5230-01554.

Part: SKIN — BULGED (CARGO DOOR) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND AFT CARGO DOOR SKIN BULGED AT RIVET NUTS HOLDING SEAL RETAINER AROUND DOOR. THE RIVET NUTS WERE REMOVED IAW SRM 51-30-7. A DOUBLER WAS INSTALLED IAW SRM 51-10-3, 51-30-2, AND ECRA 5230-01554. RIVET NUTS WERE INSTALLED IAW SRM 51-30-7.

Part: DOOR FRAME — GOUGED (EXIT DOOR) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND LT FORWARD EMERGENCY EXIT DOOR JAMB UPPER LATCH CUTOUT GOUGED. A REPAIR DOUBLER WAS INSTALLED IAW EA 9-5330-2-A0822 AND ECRA 5330-03018.

Part: ANGLE — CORRODED (FS 1155-1174) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND T-ANGLE CORRODED IN AFT PIT BETWEEN FS 1155-1174, LBL 50 (ATTACHED TO LOWER FACE OF CUSP WEB). THE T-ANGLE WAS REMOVED AND A NEW T-ANGLE WAS INSTALLED IAW SRM 51-30-5.

Part: INTERCOSTAL — CORRODED (FS 769-788) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND INTERCOSTAL NUTPLATE HOLES CORRODED IN MID CARGO PIT AT FS 769-788, LONGERON 27L-28L. THE INTERCOSTAL AND FITTING WERE REMOVED AND A NEW INTERCOSTAL AND FITTING WERE INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND 51-10-3.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND A 1 INCH CRACK AT AFT END UPPER SURFACE OF NR 1 PYLON ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-30-1, AND 51-30-5.

Part: RIB — CRACKED (THRUST REVERSER) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND NR 2 AND 5 I/B INTERNAL RIBS OF NR 2 ENGINE UPPER T/R BUCKET CRACKED. THE CRACKS WERE 0.025" LONG. NEW RIBS WER INSTALLED IAW SRM 51-30-1.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND AFT FUSELAGE TO VERTICAL STABILIZER ANGLE ON RT SIDE CRACKED. THE OLD SPLICE WAS REMOVED AND A REPAIR ANGLE AND SPLICE WERE INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 23A AND 23B.

Part: STOP — CORRODED (CARGO DOOR) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND AFT CARGO DOOR STOPS NR 8, 12, AND 14 CORRODED AND WORN. REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW ECRA 5330-02819.

Part: CARGO TRACK — CORRODED (FS 541-636) · airframe 52,294 hrs · 24,378 cycles

INSPECTION FOUND CORROSION AT FASTENER HOLES ON UPPER AND LOWER SURFACES OF RT CARGO TRACK IN MID PIT AT STA 541-636. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-3, 51-10-4, AND 51-30-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT FS 1079-1136. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-5 AND 51-30-1.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND LT CUSP WEB CORRODED FROM FS 1117-1174 FORWARD OF L-2 DOOR. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-4, AND 51-10-3.

Part: CARGO TRACK — CORRODED (FS 1211-1332) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND RT AFT PIT TIE DOWN TRACK CORRODED AROUND FASTENER HOLES AT FS 1211-1332. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 53-01, FIGURE 1, 51-10-4, AND 51-10-3.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND MID CARGO DOOR LOWER FORWARD INNER STOP SUPPORT FITTING CRACKED. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND A 1/2 INCH CRACK IN SHEAR FOOT ON BULKHEAD FRAME AT STA 1309, L14R. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND EA 9-5314-2-A0813.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND RT HORIZONTAL STABILIZER FRONT BARREL NUT HOLE CORRODED AT FORWARD LOWER BOLT HOLE. THE CORROSION WAS REMOVED IAW SRM 51-10-5. THE HOLE WAS REAMED AND A BUSHING WAS INSTALLED IAW EA 9-5511-2-A0815 AND ECRA 5511-01037.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND ANGLE CORRODED AT LT CARGO TRACK, FS 522 FALSE BULKHEAD. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND TWO 1 INCH CRACKS IN TAIL COMPARTMENT SKIN AT STA 1485 JUST FORWARD OF RUDDER TRIM ACTUATOR. THE DOUBLER AND ATTACH BRACKET WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, AND 53-34-0, FIGURE 7.

Part: SUPPORT — BENT (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND CENTER SUPPORT IN AFT PIT BENT AT BULKHEAD, STA 1003, BL 0. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-10-3, AND 51-10-4.

Part: SKIN — CRACKED (STA 1485) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND TWO 1 INCH CRACKS IN TAIL COMPARTMENT SKIN AT STA 1485 JUST FORWARD OF RUDDER TRIM ACTUATOR. THE DOUBLER AND ATTACH BRACKET WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, AND 53-34-0, FIGURE 7.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND T-ANGLE CORRODED IN AFT PIT BETWEEN STA 1136 AND 1155, LBL 50. THE T-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, AND 51-30-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND RT O/B SEAT TRACK CORRODED AT STA 352-457. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F, 51-10-3, 51-30-1, AND 51-30-5.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND A 4 INCH CRACK IN FLOOR SUPPORT ANGLE IN AFT PIT AT STA 1003, LBL 12. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 53-01, FIGURE 2, 53-14-3, FIGURE 5, 51-10-3, AND 51-30-2.

Part: BRACKET — CRACKED (STA 1003) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND A 0.030 INCH CRACK IN SUPPORT BRACKET IN AFT PIT AT FORWARD BULKHEAD, STA 1003, LBL 10. THE SUPPORT BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.

Part: SKIN — DENTED (AFT AIRSTAIR) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND LT SIDE OF AFT ENTRANCE AIRSTAIR DOOR EXTERIOR SKIN DENTED. THE DENT WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2, 51-30-2, 51-30-1, AND 52-01, FIGURE 2, SHEET 3.

Part: PAN — CRACKED (LT MLG DOOR) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND AN 8 INCH CRACK IN LT MLG I/B DOOR FORWARD LOWER PAN. A REPAIR DOUBLER AND SHEAR CLIP WERE INSTALLED IAW EA 9-5281-2-A0807 AND SRM 51-10-3.

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND TWO EACH 0.075 INCH CRACKS IN RT HORIZONTAL STABILIZER AFT SPAR HAT SECTION CHANNEL. THE HAT SECTION CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED AT STA 190, L21R. THE SKIN WAS COLD FORMED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2, 53-04, FIGURE 38, AND 51-30-2.

Part: FLOOR PANEL — BENT (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND CABIN RT O/B FLOOR PANEL BENT AT FS 465-541 AND AT FS 541-617. REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 53-24-0, 53-01, 51-30-2, 51-30-3, AND 51-30-4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND CABIN RT CENTER SEAT TRACK CORRODED AT STA 427-925. THE SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIGURE 4B.

Part: PAN — CRACKED (LT MLG DOOR) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND A 1.25 INCH CRACK IN LT I/B MLG DOOR AFT LOWER PAN. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGURE 28. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 28.

Part: EXPANSION JOINT — CRACKED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND EXPANSION JOINTS CRACKED AND BUCKLED AT CABIN FLOOR PANEL CNTER STA 886-939. THE EXPANSION JOINTS WERE REMOVED AND NEW EXPANSION JOINTS WERE INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND FORWARD EDGE OF AFT CARGO DOOR SKIN CORRODED AT CENTER FITTING. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-05,51-10-6, AND 51-30-2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND FRAME CORRODED AT FS 1193, LONGERON 30, IN AFT PIT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, 51-30-1, AND 51-30-2.

Part: PAN — CRACKED (RT MLG DOOR) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND TWO 1/2 INCH CRACKS IN RT MLG I/B DOOR FORWARD LOWER PAN. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5280-01254, 51-10-3, 51-30-2, AND EA 9-5281-2-A0808.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND LOWER SIDE OF MAIN DECK FLOORBEAM GOUGED AT STA 1174, RBL 4 AND AT STA 1193, RBL 4. REPAIRS WERE PERFORMED AT EACH LOCATION IAW SRM 53-05, FIGURE 86, 51-10-3, 51-30-1, AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND AFT SERVICE DOOR ENTRYWAY FLOOR SUPPORT CORRODED AT FS 1155 BETWEEN LT CENTER AND O/B SEAT TRACKS, LBL 44-54.

Part: WEB — CRACKED (STA 200) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND A 1/4 INCH CRACK IN TANG ON TORQUE BOX WEB AT STA 220 AFT OF L-1 DOOR, LONGERON 15L. A DOUBLER WAS INSTALLED IAW EA 9-5314-2-A0811 AND SRM 51-30-5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND LT CABIN FLOORBEAM CORRODED AROUND NUT CLIP HOLES. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 20A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1309-1361, LBL 20. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4 AND 51-30-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND GALLEY FLOOR SUPPORT CORRODED AT STA 225, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-3 AND 51-10-4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1309-1361. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND CABIN FLOORBEAM CORRODED AROUND FASTENER HOLES AT FS 1322, RT SIDE. THE CORRODED AREA WAS CUT OUT IAW SRM 53-05, FIGURE 20A. A REPAIR ANGLE, FILLER, AND WEAR STRIP WERE INSTALLED IAW SRM 51-10-3 AND 53-05, FIGURE 20A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 160-165, LBL 52. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND CABIN FLOOR SUPPORTS CORRODED AT STA 200, RBL 9 - RBL 44, LBL 5 - RBL 5, LBL 10 - LBL 14, AND AT STA 160-200, RBL 44. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-10-3, 51-10-4, 51-30-5, 51-10-5, AND 51-30-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 195-200, LBL 55 AND AT STA 200-256, LBL 14. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, 51-30-5, AND 51-30-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND CABIN FLOOR FRAME CORRODED AROUND NUT CLIP HOLES AT STA 1338, LT SIDE. THE FLOORBEAM WAS REPAIRED IAW SRM 53-05, FIGURE 20A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT FS 1108-1222. THE SEAT TRACK WAS REMOVED AND REPLACED USING A SPLICE REPAIR IAW SRM 51-30-2, 51-30-5, 51-10-2.

Part: SKIN — DENTED (NR 1 FLAP) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND LT NR 1 FLAP T/E PANEL LOWER SKIN DENTED. THE LOWER SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (STA 148-200) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 148-200, LBL 7, STA 160, RBL 11, AND STA 160-195, LBL 45. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-4, 51-10-3, 51-30-1, 51-30-2, 51-30-05, 51-10-2, AND 51-10-05.

Part: WEB — CRACKED (FS 916) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND A 1/4 INCH CRACK IN CUSP WEB AT FS 916, RBL 18. THE CRACKED AREA WAS CUT OUT AND A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4, 53-14-3, FIGURE 10, AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160-200, RBL 54. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT FS 1125-1222. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-1, 51-10-4, 53-05, FIGURE 4F, 51-10-3, AND 51-30-5.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND A 4 INCH CRACK CUSP WEB AT FS 1222, LT CENTER SEAT TRACK. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 53-14-3, 51-10-3, AND 51-30-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND LT CENTER SEAT TRACK AT STA 1032-1125 AND LT I/B SEAT TRACK AT STA 1032-1309 CORRODED. THE SEAT TRACKS WERE REMOVED AND NEW TRACKS WERE INSTALLED IAW SRM 53-05, FIGURE 4, 51-30-1, 51-30-2, 51-10-2, 51-10-4, 51-10-3, AND 51-30-5.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,251 hrs · 24,391 cycles

INSPECTION FOUND A 1 INCH CRACK IN FORWARD ENTRY SUB FLOOR WEB AT FS 160, RBL 11 AND AT LBL 11. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW ECRA 5320-02100, SRM 53-01, FIGURE 4, 51-10-3, AND 51-30-2.

Part: SUPPORT — BROKEN (BS 604)

MBB LT TIEDOWN RAIL CENTER FLOOR SUPPORT FLANGE MOUNTING EAR BROKEN AT STA 604. INSTALLED REPAIR PER EC/RA 5320-01533.

Part: LATCH — LACK OF LUBE (CABIN)

OXYGEN COMPARTMENT 30 RT DID NOT OPEN ON TEST. LUBRICATED LATCH PER MM 35-20-00.

Part: LATCH — LACK OF LUBE (CABIN)

OXYGEN COMPARTMENT 7RT DID NOT OPEN ON TEST. LUBRICATED LATCH PER MM 35-20-00.

Part: LATCH — LACK OF LUBE (CABIN)

OXYGEN COMPARTMENT 23 RT DID NOT OPEN ON TEST. LUBRICATED LATCH PER MM 35-20-00.

Part: LATCH — LACK OF LUBE (CABIN)

OXYGEN COMPARTMENT 26LT DID NOT OPEN ON TEST. LUBRICATED LATCH PER MM 35-20-00.

Part: BEAM — CORRODED (BS 1193)

CORROSION ON I-BEAM BTWN STA 1193 AND 1212 AT L-29RT. REMOVED AND REPLACED I-BEAM PER SRM 51-30-2.

Part: LATCH — OUT OF ADJUST (TAIL CONE)

TAIL COMPARTMENT TAILCONE OUT OF RIG. OUTSIDE HANDLE PULL LOW, DELTA TRIANGLE NOT 90 DEGREES, CATCHES ON RIGHT SIDE LATCHES. ADJUSTED LATCH LEVER CABLES AND ADJUSTED LOWER RIGHT LATCH LEVER. PERFORMED ADJUSTMENT TEST PER MM 53-53-00.

Part: SKIN — DENTED (BS 275 & 332)

INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 332 BETWEEN LONGERON 23L AND 22L AND A STA 275 BETWEEN LONGERON 23L AND 22L AND STA 313 BETWEEN LONGERON 24L AND 23L. THE DENTS WERE REPAIRED IAW SRM 53-04, FIGURE 38, SHEET 18.

Part: SKIN — DENTED (BS 275)

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 275 BETWEEN LONGERON 17L TO 18L. A REPAIR WAS INSTALLED IAW ECRA 5330-02445.

Part: JAMB — CORRODED (CARGO DOORWAY)

INSPECTION FOUND FORWARD BAGGAGE BIN LOWER DOOR JAMB PAN CORRODED. THE CORRODED SECTION OF PAN WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 44.

Part: BEAM — CRACKED (SERVICE DOOR)

INSPECTION FOUND A 1.375 INCH CRACK IN FORWARD SERVICE DOOR NR 4 BEAM. THE NR 4 BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: FUEL TUBE — RUPTURED (NR 2 ENGINE)

THE NR 2 ENGINE FLAMED OUT WHILE EN ROUTE FL330. THE NR 2 ENGINE WAS RESTARTED. THE NR 2 ENGINE FLAMED OUT A SECOND TIME AND WAS RESTARTED AGAIN. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE NR 2 ENGINE FUEL FLEX TUBE RUPTURED. THE FUEL FLEX TUBE WAS REMOVED AND REPLACED IAW MM 73-11-02, PAGE 216. THE FUEL FILTER WAS REPLACED AS A PRECAUTIONARY MEASURE. IN ADDITION, THE MOISTURE TRAP AND SENSE LINE WERE CHECKED WITH NO DEFECTS NOTED. A LEAK CHECK WAS PERFORMED WITH NO LEAKS FOUND. A POWER ASSURANCE RUN WAS PERFORMED ON THE NR 2 ENGINE AND OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — CRACKED (RT RUDDER)

INSPECTION FOUND A .75 INCH CRACK IN RT SIDE OF RUDDER SKIN. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 4, SHEET 2.

Part: LONGERON — CRACKED (BS 984-1003)

INSPECTION FOUND A .5 INCH CRACK IN LONGERON 20R AT STA 984 TO 1003. THE CRACK WAS ROUTED OUT AND A DOUBLER WAS INSTALLED IAW ECRA 5310-03363.

Part: SUPPORT — CORRODED (CABIN)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FORWARD ENTRY UNDER MAIN CABIN DOOR THRESHOLD. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SUPPORT — CORRODED (CABIN)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FORWARD ENTRY UNDER PANEL H. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.

Part: SKIN — DENTED (BS 389)

INSPECTION FOUND A DENT IN FUSELAGE SKIN BELOW CARGO DOOR AT STA 389, LONGERON 29R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 19.

Part: SUPPORT — CORRODED (CABIN)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FORWARD ENTRY UNDER PANEL G. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-1.

Part: PANEL — CRACKED (LT WING TE)

INSPECTION FOUND A 1 INCH CRACK AND CHAFING IN LT WING LOWER TRAILING EDGE PANEL NR 1510. THE AREA WAS REPAIRED IAW SRM 51-70-01.

Part: BRACKET — CRACKED (BS 864)

INSPECTION FOUND A 1.5 CRACK BRACKET AT LT SIDE JUST BOTTOM/CENTER OF FUSELAGE FORWARD OF STA 864. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-5.

Part: LOCK PIN — WORN (TAILCONE)

THE TAILCONE HUNG UP ON UPPER RIGHT LATCH DURING DROP TEST. MAINTENANCE FOUND UPPER RIGHT BAYONET LOCK PIN WORN. THE LOCK PIN WAS REPLACED AND THE TAILCONE WAS ADJUSTED IAW MM 53-53-00.

Part: OIL COOLER — INOPERATIVE (NR 2 ENGINE)

THE NR 2 ENGINE OIL TEMPERATURE APPROACHED REDLINE AFTER TAKEOFF FROM SFO. THE TEMPERATURE INCREASE WAS ACCOMPANIED BY OIL PRESSURE DROP. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE OIL COOLER AT FAULT. THE OIL COOLER WAS REMOVED AND REPLACED. THE ENGINE WAS RUN WITH NO LEAKS NOTED AND ALL ENGINE INDICATIONS WERE NORMAL. PART TOTAL CYCLES, 12,240.

Part: GENERATOR — FAILED (NR 1 ENGINE)

FLT 0462 - LAX - THE NR 1 ENGINE GENERATOR FAILED IN FLIGHT AND WOULD NOT RESET. THE APU WAS STARTED TO COVER BUS. THE APU GENERATOR SUBSEQUENTLY FAILED AND WOULD NOT RESET. THE AIRCRAFT WAS RETURNED TO LAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU INLET SCREEN DIRTY. THE INLET SCREEN WAS CLEANED. THE APU WAS RUN FOR 30 MINUTES AND APU GENERATOR FREQUENCY AND VOLTAGE WAS NORMAL. IN ADDITION, THE NR 1 ENGINE GENERATOR, CSD, AND CSD OIL COOLER WERE REMOVED AND REPLACED. LEAK AND OP CHECKS WERE GOOD. (M)