N15841

Part: LONGERON — CRACKED (STA 1418) · airframe 47,595 hrs · 22,872 cycles

INSPECTION FOUND LONGERON 2L CRACKED AT STA 1418. REPAIRED IAW ECRA 5311-01132.

Part: LONGERON — CRACKED (STA 1418) · airframe 47,595 hrs · 22,872 cycles

INSPECTION FOUND A 2" CRACK IN LONGERON 2R AT STA 1418. A SECTION OF LONGERON WAS SPLICED IN IAW ECRA 5311-01132.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,283 hrs · 20,015 cycles

INSPECTION FOUND AFT CARGO FRAME AFT SIDE CORRODED UNDER PAINT AT FS 1309, L24R-24L. THE CORRODED SECTION WAS CUT OUT AND A FRAME REPAIR SPLICE WAS INSTALLED IAW SRM 53-03, FIGURE 2A.

Part: SKIN — CRACKED (LT WING) · airframe 42,283 hrs · 20,015 cycles

INSPECTION FOUND LT WING LEADING EDGE SKIN CRACKED AT APPROXIMATELY STA XIS 60. REPAIR DOUBLERS, SHIMS, ANGLES, AND NUT PLATE STRIPS WERE INSTALLED IAW EA 9-5721-2-AD760 AND ECRA 5721-01057.

Part: FAIRING — CRACKED (RT FLAP HINGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND A 1 INCH CRACK IN RT WING FLAP HINGE FAIRING NR 3 AFT. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 3, SHEET 2, 51-10-4, AND 51-10-3.

Part: SKIN — CRACKED (LT WING) · airframe 42,281 hrs · 20,014 cycles

AN INTERIM REPAIR WAS REMOVED AND A PERMANENT REPAIR WAS INSTALLED WHERE A 1 INCH CRACK EXISTED ON L/E LOWER SURFACE OF LT WING SKIN AT NR 2 SLAT CENTER TRACK CUTOUT, XFS 206. THE INTERIM REPAIR WAS REMOVED IAW SRM 51-10-4. EXTERNAL AND INTERNAL DOUBLERS AND FILLERS WERE INSTALLED IAW ECRA 5730-01670.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND MID CARGO RT CARGO TIE DOWN TRACK CORRODED AT FS 532 - 625 AND FS 693 - 807. THE TIE DOWN TRACK SECTIONS WERE REMOVED AND NEW TRACK SECTIONS WERE INSTALLED IAW SRM 53-05, FIGURE 4.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND MID CARGO RT TRACK FLOOR SUPPORT CORRODED AT FS 598 - 636. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-01, 51-10-04, 51-30-02, AND 51-30-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND LEFT I/B CABIN SEAT TRACK CORRODED AT FS 1117 - 1309. THE CORROSION WAS REMOVED IAW SRM 53-05, FIGURE 4. CORROSION REMOVAL WAS WITHIN LIMITS FROM FS 1212 - 1309. THE SEAT TRACK SECTION FROM FS 1117 - 1212 WAS REPLACED IAW SRM 51-30-1, 53-05, FIGURE 1, AND 51-10-3.

Part: DOOR FRAME — CORRODED (AFT CARGO BAY) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND AFT CARGO DOOR CUTOUT LOWER JAMB CORRODED. A DOUBLER AND STRAP WERE INSTALLED IAW SRM 51-10-4 AND ECRA 5310-03027.

Part: DOUBLER — CORRODED (ANTENNA MOUNT) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND ANTENNA DOUBLER CORRODED ON MOUNTING FLANGE AT FS 700, LONGERON 30. THE ANTENNA DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND NR 2 LEFT T/E FLAP DENTED ON LOWER SIDE. THE DENTED AREA WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 5 AND FIGURE 3.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND FOUR VERTICAL STABILIZER DOGHOUSE ANGLES CRACKED. LOCATIONS WERE RT AND LT FWD LOWER AND RT AND LT AFT LOWER AREA. THE CRACKS WERE .5 INCH LONG. THE ANGLES WERE REPAIRED IAW SRM 55-01, FIGURE 2, 55-10-4, 51-10-3, AND 51-30-2.

Part: STRUCTURE — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND CABIN AREA SUPPORT CORRODED AT STA 200, LBL 10. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, 51-10-4, 51-10-3, AND 51-30-5.

Part: STRUCTURE — CRACKED (RT WING LE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE I/B SUPPORT. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.

Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND COCKPIT RT METAL FLOOR PANEL CORRODED AND DENTED. THE FLOOR PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 53-24-0.

Part: ANGLE — CORRODED (CARGO DOOR) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND UPPER AND LOWER SURFACE OF DOOR Z-ANGLE CORRODED AT RT SIDE OF AFT PIT. THE Z-ANGLE WAS REMOVED AND A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-30-1, 51-10-3, AND 51-30-2.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND LT CARGO TIE DOWN TRACK CORRODED IN MID CARGO COMPARTMENT AT FS 522. THE TIE DOWN TRACK WAS REMOVED AND A REPLACEMENT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4G.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND RT TIEDOWN TRACK CORRODED FROM STA 1211 - 1309 AND LT TIEDOWN TRACK CORRODED FROM STA 1007 - 1309 IN AFT PIT. THE TRACKS WERE REMOVED AND NEW TRACKS WERE INSTALLED IAW SRM 53-05, FIGURE 5, 51-10-3, 51-10-4, AND 51-30-5.

Part: WEB — BENT (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND CABIN SUBFLOOR LIGHTENING HOLE DOUBLER BENT AND TORN AT STA 160, LBL 12. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.

Part: FRAME — CRACKED (LT MLG DOOR) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND A 3 INCH CRACK IN LT MLG WHEEL WELL DOOR FRAME AT O/B FORWARD CORNER. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-1, AND 51-30-8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT FS 936 - 1212. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-05, FIGURE 1.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT STA 294, LONGERON 22L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38G.

Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND A 1 INCH CRACK IN RT UPPER HORIZONTAL STABILIZER BANANA FAIRING ON FORWARD END. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2, 55-10-0, FIGURE 7, AND 51-30-02.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 1126 - 1240. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-2, AND 53-05, FIGURE 4.

Part: PAN — CRACKED (CARGO DOOR) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND A 1.9 INCH CRACK AT CAM LATCH OF FWD CARGO DOOR FWD EDGE OF INNER PAN. THE CRACKED SECTION WAS REMOVED IAW EA 9-5231-2-A0749. A REPAIR ANGLE AND FILLER WERE INSTALLED IAW SRM 52-05, FIGURE 26A, 51-10-3, 51-30-2, AND 51-30-5.

Part: BRACKET — CORRODED (THRESHOLD) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND L-2 DOOR THRESHOLD SUPPORT BRACKETS CORRODED. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE INSTALLED IAW SRM 51-30-5.

Part: DOUBLER — GOUGED (CARGO DOOR) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND FORWARD CARGO DOOR FORWARD LOWER OUTER SKIN DOUBLER LOWER EDGE GOUGED. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2.

Part: PANEL — CRACKED (CARGO FLOOR) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO CENTER FLOOR TRANSITION PANEL AT STA 1212 - 1231. THE CRACKED AREA WAS TRIMMED OUT IAW SRM 53-01, FIGURE 4, SHEET 3. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, 51-10-4, 51-10-3, AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND CABIN FLOOR SUPPORTS CORRODED AT STA 160, RBL 45 AND AT STA 200, RBL 51. THE FLOOR SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-05, 51-10-04, 51-10-2, AND 51-30-1.

Part: BRACKET — CRACKED (CARGO BAY) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND TWO L BRACKETS CRACKED IN FORWARD CARGO PIT AT FORWARD AND AFT END OF CARGO DOOR LATCH SUPPORT. THE CRACKS WERE .25 INCH LONG. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE INSTALLED IAW SRM 51-30-2 AND 51-10-4.

Part: SKIN — DENTED (PAX DOOR) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND L-1 DOOR UPPER AFT I/B EDGE DENTED. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.

Part: BRACKET — CRACKED (CARGO BAY) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND A 1 INCH CRACK IN TWO AFT CARGO PIT L BRACKETS AT FORWARD AND AFT END OF OVERHEAD CARGO DOOR LATCH SUPPORT. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-10-2, 51-10-3, AND 51-30-2.

Part: ANGLE — CRACKED (KEELBEAM) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND A 1 INCH CRACK IN LT MLG FORWARD KEELBEAM ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-03, 51-30-05, AND 51-30-01.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND CABIN AREA FLOOR SUPPORTS CORRODED AT STA 200, BL 0 AND AT STA 140 - 200, RBL 7. THE FLOOR SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-02, 51-10-03, 51-10-04, AND 51-30-1.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 160, BL 0. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW 51-30-02, 51-10-04, AND 51-30-05.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND LEFT O/B SEAT TRACK AFT OF L-2 DOOR CORRODED AT FS 1174. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT STA 294, LONGERON 21L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38, VIEW G.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND LOWER SURFACE OF CABIN SUBFLOOR CORRODED AT FS 200 BETWEEN BL 0 AND RT SIDE OF AIRCRAFT. THE SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 53-14-01, FIGURE 11, 51-10-3, AND ECRA 5100-01844.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND A 1 INCH CRACK IN LOWER FLOOR PANEL SUPPORT IN FORWARD CARGO AREA AT FS 522. THE FLOOR PANEL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-10-03.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 168, RBL 28. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SKIN — DENTED (CARGO DOOR) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND AFT CARGO DOOR EXTERIOR SKIN DENTED. REPAIRED SKIN IAW SRM 52-05, FIGURE 1 AND 51-10-3.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200, RBL 29. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, AND 51-10-4.

Part: FITTING — CORRODED (AIRSTAIR) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND FORWARD AIRSTAIRS DOOR MOUNT BASE FITTING CORRODED AT STA 180. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-1.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT FS 465, LONGERON 23R - 24R. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38, VIEW G.

Part: COVER — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT COVER PLATE CORRODED AT FS 160 - 200, RBL 54. THE COVER PLATE WAS REMOVED AND A NEW COVER PLATE WAS INSTALLED IAW SRM 51-30-1.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT STA 446 BETWEEN LONGERON 21R AND 20R. THE DENT WAS REPAIRED BY INSTALLING A DOUBLER AND SHIMS IAW SRM 53-04, FIGURE 38, SHEET 20, VIEW E.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

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

Part: SEAT TRACK — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND CABIN RT CENTER SEAT TRACK CORRODED AT FS 200. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND TWO 1 INCH CRACKS IN RT CUSP WEB AT FS 218 - 237. THE CUSP WEB WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.

Part: STRUCTURE — DENTED (NR 2 ENGINE T/R) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND NR 2 THRUST REVERSER LOWER BUCKET DENTED JUST AFT OF 3RD FRAME AND FORWARD OF 4TH FRAME. A DOUBLER REPAIR WAS INSTALLED AT EACH LOCATION IAW SRM 51-10-4, 51-10-3 AND OVERHAUL MANUAL 78-30-1, FIGURE 401C, SHEET 2.

Part: SKIN — CORRODED (RT WING TE FLAP) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND RIGHT NR 1 T/E FLAP I/B LOWER SIDE OF SKIN CORRODED. THE SKIN WAS REMOVED AND REPLACEMENT SKIN WAS INSTALLED IAW SRM 51-10-1, 57-50-14, 51-30-2, AND 51-30-8.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT STA 485, LONGERON 28L. THE SKIN WAS REPAIRED IAW EA 9-5331-2-A0752 AND ECRA 5331-01081.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND MID CARGO FRAME FLOOR SUPPORT CORRODED AND TORN AT STA 807 FROM STRINGER 24L TO 24R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND FLOORBEAM CORRODED UNDER TWO NUT PLATES AT STA 200, RBL 44.5. THE CORROSION WAS REMOVED IAW SRM 51-10-03 AND THE FLOORBEAM WAS REPAIRED IAW EA 9-5310-2-A0755 AND ECRA 5310-04040.

Part: FLANGE — CRACKED (CARGO DOOR) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR INNER PAN FLANGE IN AREA OF FORWARD CAM LATCH. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGURE 26A, SHEET 2. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A, SHEET 1, 53-05, AND 51-10-3. THE CAMLOCK TUBE WAS REMOVED AND REINSTALLED TO GAIN ACCESS TO AREA IAW SRM 51-10-3.

Part: BRACKET — CRACKED (TAILCONE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND A .5 INCH CRACK IN TAIL CONE UPPER LT LOCK PIN SUPPORT MOUNT BRACKET LOWER LEG ON THE AFT END. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-2.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND CABIN FLOOR MOUNT SUPPORT CORRODED AT FS 160, RBL 51. THE FLOOR MOUNT SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-02, 51-10-04, AND 51-30-05.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND THREE DENTS IN FUSELAGE SKIN AT FS 408, LONGERONS 29L, 28L, AND 27L. THE SKIN WAS REPAIRED IAW EA 9-5334-2-A0747 AND SRM 53-04, FIGURE 38, SHEET 20.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND LT FUSELAGE SKIN CREASED AT STA 237 BETWEEN LONGERONS 16L AND 17L. THE CREASED SKIN SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-30-2, AND 51-30-5.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND FORWARD PIT LT TIE DOWN TRACK CORRODED AT FS 389 - 522. THE TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND TWO 2 INCH CRACKS IN SUBFLOOR THAT HAD GONE PAST STOP DRILL AT STA 218, RBL 56. THE EXISTING REPAIR DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-01, 53-01, FIGURE 4, 51-30-06, 51-10-04, AND 51-10-03.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT STA 313, L24R. THE DENTED AREA WAS REWORKED IAW SRM 53-04, FIGURE 38. THE OLD REPAIR WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 & 12B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT FS 218 - 309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4F.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND CUSP WEB CORRODED AT STA 200, RBL 29. THE CORRODED AREA OF WEB WAS CUT OUT IAW SRM 53-01, FIGURE 4. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-4, 51-30-2, AND 53-14-1.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 42,281 hrs · 20,014 cycles

INSPECTION FOUND CABIN RT CENTER SEAT TRACK CORRODED AT FS 220 - 240. THE SEAT TRACK WAS REPLACED IAW SRM 53-05.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 41,201 hrs · 19,479 cycles

THE RT GEAR INDICATION LIGHTS DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED FOR LANDING AT EWR. A GO-AROUND WAS PERFORMED AND THE GEAR WAS VISUALLY CONFIRMED DOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT GEAR SOCKET WAS PUSHED BACK AND NOT LOCKED. THE LANDING GEAR INDICATOR WAS REMOVED AND REPLACED IAW MM 32-60-03. OPERATION OF THE LANDING GEAR INDICATION LIGHTS CHECKED GOOD.

Part: SKIN — CRACKED (WS 206)

INSPECTION FOUND A 2 CRACK IN LT WING LEADING EDGE LOWER SKIN FOUR INCHES OUTBOARD OF NR 2 SLAT CENTER TRACK CUTOUT AT STA XFS 206. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5730-01670. A DIP WAS INITIATED TO PERMANENTLY REPAIR THE AREA WITHIN 21 DAYS.

Part: WEB — CORRODED (BS 1212-1219)

INSPECTION FOUND WEB CORRODED IN AFT BAGGAGE BIN AT AFT SIDE OF DOOR CUTOUT NUT PLATE STRIP UNDER TIEDOWN, STA 1212 TO 1219.5, LONGERON 26L. THE AREA WAS REPAIRED IAW ECRA 5332-01003.

Part: LATCH LEVERS — OUT OF ADJUST (TAIL CONE)

THE PULL FROM INTERIOR, EXTERIOR, AND AFT CABIN DOOR TAIL CONE RELEASE HANDLES WAS LOW. THE TAIL CONE LATCH LEVERS WERE ADJUSTED IAW MM 53-53-02.

Part: ANGLE — CRACKED (DORSAL FIN)

INSPECTION FOUND A .25 INCH CRACK IN RT SIDE DORSAL FIN ATTACH ANGLE AND A .25 INCH CRACK IN LT SIDE DORSAL FIN ATTACH ANGLE. THE ANGLES WERE REPLACED IAW WORK CARD 08-5340-1-0007 AND 08-5340-1-0008.

Part: BEAM — CRACKED (SERVICE DOOR)

INSPECTION FOUND A .75 INCH CRACK IN FORWARD SERVICE DOOR BOTTOM HORIZONTAL BEAM (NR 4) AT FORWARD END IN RADIUS NEXT TO SKIN. THE BEAM WAS REMOVED AND A NEW BEAM WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.

Part: SHOCK STRUT — LOW PRESSURE (NLG)

THE LANDING GEAR WOULD NOT RETRACT TO UP AND LOCKED POSITION AFTER TAKEOFF. THE GEAR WAS CYCLED AND RETRACTED TO UP AND LOCKED POSITION AFTER TWO ATTEMPTS. THE AIRCRAFT LANDED NORMALLY AT SEA. MAINTENANCE FOUND THE NOSE STRUT PRESSURE LOW. THE NOSE STRUT WAS SERVICED PER CHART ON NOSE WHEEL WELL AND A DIP WAS ISSUED FOR FULL SERVICE AT NEXT RON. FULL NOSE STRUT SERVICE WAS COMPLIED WITH AT EWR THE FOLLOWING DAY AND THE DIP WAS CLOSED.

Part: RIB — CRACKED (WING LE)

INSPECTION FOUND A .25 INCH CRACK IN WING LEADING EDGE RIB OUTBOARD OF NR 8 SLAT TRACK. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5710-01749.

Part: BEAM — CRACKED (MAIN CABIN DR)

INSPECTION FOUND A .75 INCH CRACK ON UPPER HORIZONTAL BEAM AT AFT CORNER OF MAIN CABIN DOOR AND A 1 INCH CRACK WAS FOUND ON UPPER HORIZONTAL BEAM AT FORWARD CORNER OF MAIN CABIN DOOR. DOUBLER REPAIRS WERE INSTALLED IAW SRM 52-05, FIGURE 31, SHEET 10 SECTION T-T AND SECTION U-U.

Part: DOOR JAMB — CORRODED (MID BAG BIN)

INSPECTION FOUND MID BAGGAGE BIN DOOR JAMB PAN LOWER SECTION CORRODED AROUND FASTENERS. THE LOWER DOOR JAMB WAS REPAIRED IAW SRM 53-05-63.

Part: FLOOR SUPPORT — CORRODED (BS 200)

INSPECTION FOUND FORWARD CABIN RT SIDE FLOORBOARD SUPPORT CORRODED AT STA 200, 9 INCHES RIGHT OF CENTER TO RIGHT CENTER FLOOR TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-03.

Part: FLOOR SUPPORT — CORRODED (BS 180)

INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT CORRODED, RT SIDE, STA 180. THE FLOOR SUPPORT WAS REMOVED AND REPLACED.

Part: FLOOR SUPPORT — CORRODED (BS 160-198)

INSPECTION FOUND FORWARD CABIN LT SIDE FLOORBOARD SUPPORT ANGLE CORRODED AT STA 160 TO 198, 5 INCHES INBOARD OF FORWARD ENTRY DOOR CUTOUT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-2.

Part: FLOOR SUPPORT — CORRODED (BS 148.5-199)

INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT CORRODED AT STA 148.5 TO 199. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 57-30-0.

Part: FLOOR SUPPORT — CORRODED (BS 160-200)

INSPECTION FOUND FORWARD CABIN RT SIDE FLOORBOARD SUPPORT CORRODED AT STA 160 TO 200. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-03.

Part: ANGLE — CORRODED (BAGG DOOR JAMB)

INSPECTION FOUND Z-ANGLE AT AFT BAGGAGE BIN LOWER DOOR JAMB CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-03.

Part: FLOOR SUPPORT — CORRODED (BS 198-203)

INSPECTION FOUND FORWARD CABIN LT SIDE FLOORBOARD SUPPORT ANGLE CORRODED AT STA 198 TO 203. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-03.

Part: FLOOR SUPPORT — CORRODED (BS 200)

INSPECTION FOUND FORWARD CABIN FLOORBOARD SUPPORT AT AIRCRAFT CENTERLINE CORRODED AT STA 200. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-03.

Part: FLOOR SUPPORT — CORRODED (BS 148.5-199)

INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT CORRODED AT STA 148.5 TO 199. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-03.

Part: FLOORBOARD — CORRODED (COCKPIT)

INSPECTION FOUND COCKPIT FLOORBOARD AT FIRST OFFICER'S SEAT TRACK CORRODED. THE FLOORBOARD WAS REPLACED IAW SRM 51-10-02.

Part: DOUBLER — CRACKED (BS 194)

INSPECTION FOUND WING LEADING EDGE SPLICE DOUBLER CRACKED BETWEEN NR 5 AND NR 6 SLAT TRACK, STA 194. THE AREA WAS REPAIRED IAW ECRA 5710-01645.

Part: SKIN — CREASED (BS 503-541)

INSPECTION FOUND A CREASE IN FUSELAGE SKIN FROM STA 503 TO 541 AT LONGERON 22R. THE SKIN WAS REPAIRED IAW ECRA 5330-02421.

Part: SKIN — DENTED (BS 236)

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 236, LONGERON 17L TO 18L. THE DENTED AREA OF SKIN WAS CUT OUT AND A REPAIR WAS INSTALLED IAW ECRA 5330-02420.

Part: SKIN — DENTED (BS 227)

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 227. THE AREA WAS REPAIRED IAW SRM 51-10-03.

Part: DOOR JAMB — CRACKED (RT MLG DOOR)

INSPECTION FOUND A 1 INCH CRACK IN RT MLG DOOR JAMB. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2.

Part: CLIPS — OUT OF ADJUST (TAILCONE)

THE TAILCONE EXTERIOR RELEASE HANDLE HAD EXCESSIVE PULL OUT OF CLIPS. THE TAILCONE EXTERIOR RELEASE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.