N12319

Part: SKIN — CRACKED (BS 727E) · airframe 66,965 hrs · 34,256 cycles

LEFT FUSELAGE STATION 727E HAS A CRACK IN THE SKIN. REPAIRED PER SRM 53-00-01, PROCEDURE 5, REPAIR 31.

Part: SKIN — CRACKED (BS 747 S22L) · airframe 66,965 hrs · 34,256 cycles

DURING C SCAN INSPECTION FOUND 1 INCH LONG CRACK ON STRINGER 22L 7 INCHES FWD OF STATION 747. REPAIRED IN ACCORDANCE WITH SRM 53-00-01, PROCEDURE 5, REPAIR 31.

Part: SKIN — CRACKED (BS 727E S24L) · airframe 66,965 hrs · 34,256 cycles

DURING C SCAN INSPECTION FOUND 1 INCH LONG CRACK ON STRINGER 24L 3 INCHES AFT OF STATION 727E. REPAIRED CRACK PER SRM 53-00-01, PROCEDURE 5, REPAIR 31.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

FOUND FUSELAGE SKIN CRACKED 2 INCHES AT STA 727D, 17-23 R. REPAIRED IAW ECRA 5331-01303.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

FOUND CRACKED FRAME AT STA 727, S 14L. REPAIRED IAW ECRA 5311-01317.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

FOUND CRACKED FRAME AT STA 887 NSTR 9RT. REPAIRED IAW ECRA 5310-04623.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,288 hrs · 32,074 cycles

INSPECTION FOUND TWO SMALL CRACKS ON THE OUTBOARD FLANGE OF THE LBL 45 LONGITUDINAL FLOORBEAM JUST FORWARD OF STA 727B. REPAIRED IAW ECRA 5311-01316.

Part: CHANNEL — CRACKED (FUSELAGE)

FOUND CRACK AT STA 360 STR 14 LEFT. REPAIRED IAW ECRA 5311-01314.

Part: FRAME — CRACKED (BS 827 S9L) · airframe 62,278 hrs · 32,074 cycles

FOUND CRACKED FRAME AT STA 827 STR 9LT. REPAIRED IAW ECRA 5310-04622.

Part: FRAME — CRACKED (BS 827 S9R) · airframe 62,287 hrs · 32,074 cycles

FOUND CRACKED FRAME AT STA 827 STR9 RT. REPAIRED IAW ECRA 5310-04622.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

FOUND CRACKED FRAME AT STA 847 STR 9RT. REPAIRED IAW ECRA 5310-04624.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

FOUND CRACKED FRAME AT STA 887, STR 9LT. REPAIRED IAW ECRA 5310-04623.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

FOUND CRACKED FRAME AT STA 847 STR 9LT. REPAIRED IAW ECRA 5310-04624.

Part: FRAME — CRACKED (BS 807 S9L)

FOUND CRACKED FRAME AT STA 807, STR 9LT. REPAIRED IAW ECRA 5310-04626.

Part: FRAME — CRACKED (BS 907 S9R) · airframe 62,278 hrs · 32,074 cycles

FOUND CRACKED FRAME AT STA 907, STR 9 RT. REPAIRED IAW ECRA 5310-04625

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

LEFT OB SEAT TRACK FLOOR SPT CRACKED AT STA 727B. REPAIRED IAW ECRA 5311-01316.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 62,287 hrs · 32,074 cycles

LWR FWD CORNER NEAR LIGHTNING HOLE HAS A 1/2 IN CRACK ON INNER SKIN. REPAIRED IAW ECRA 5230-01790.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

L1 DOOR FRAME CRACKED AT NR 6 AFT DOOR STOP. REPAIRED IAW ECRA 5210-01934

Part: DOOR FRAME — CRACKED (FUSLEAGE) · airframe 62,287 hrs · 32,074 cycles

L1 DOOR FRAME CRACKED AT NR 7 AFT DOOR STOP. REPAIRED IAW ECRA 5210-01934.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,287 hrs · 32,074 cycles

NR 12 INTERCOSTAL CRACKED AT STA 294.5 TO 303.9. REPAIRED IAW ECRA 5311-01314.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

L1 DOOR FUSELAGE OPENING CLIP CRACKED IN RADIUS ON S15L, STA 348. REPAIRED IAW ECRA 5311-01314.

Part: INTERCOSTAL — CRACKED (BS 294-303 S12L) · airframe 62,288 hrs · 32,074 cycles

INSPECTION FOUND A 1 INCH CRACK IN NR 12 INTERCOSTAL AT STA 294.5-303.9, S12L. A NEW INTERCOSTAL WAS INSTALLED IAW ECRA 5311-01314.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

STRINGER 16L, STA 348.2 UPPER ATTACH ANGLE CRACKED AT THE DOOR STOP FITTING FASTENER HOLE. REPAIRED IAW ECRA 5311-01314.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

L1 DOOR STOP FITTING LOWER ATTACH ANGLE CRACKED AT THE DOOR STOP FITTING FASTENER HOLE. REPAIRED IAW ECRA 5311-01314.

Part: SKIN — CRACKED (E&E BAY DOOR) · airframe 62,287 hrs · 32,074 cycles

SKIN CRACKED AT FWD CORNER OF E&E DOOR RIVET. REPAIRED IAW SRM 52-00-01 FIG 201.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

CORRODED AFT CARGO COMPARTMENT FRAME AT STA 847 RBL22. REPAIRED IAW SRM 51-10-2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

SKIN CRACKED AT AFT LOWER CORNER OF R1 DOOR. REPAIRED IAW SRM 53-10-01 FIG 201, REPAIR 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,287 hrs · 32,074 cycles

FUSELAGE SKIN CRACK AT STA 870 STRINGER 23RT. REPAIRED IAW SRM 53-00-01 FIG 201.

Part: FRAME — CRACKED (BS 616) · airframe 62,287 hrs · 32,074 cycles

FRAME CRACKED AT STA 616 JUST BELOW FLOOR LINE ON LEFT SIDE. REPAIRED IAW ECRA 5311-01158.

Part: FRAME — CORRODED (BS 500 S27-28R) · airframe 62,287 hrs · 32,074 cycles

FWD CARGO FRAME CORRODED AT STA 500 BETWEEN STRINGER 27R AND 28R. REPAIRED IAW SRM 53-00-07, REPAIR 4.

Part: FRAME — CRACKED (BS 616 S17R) · airframe 62,288 hrs · 32,074 cycles

INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 616 JUST BELOW FLOORLINE, S17R. THE CRACKED AREA OF FRAME WAS CUT OUT AND A REPAIR ANGLE WAS INSTALLED IAW ECRA 5311-01158.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,288 hrs · 32,074 cycles

INSPECTION FOUND A .75 INCH CRACK IN STRINGER CLIP AT STA 520, STRINGER 16L. A NEW STRINGER CLIP WAS INSTALLED IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 62,288 hrs · 32,074 cycles

INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 1016, RBL 9. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51.

Part: FLOOR SUPPORT — CORRODED (BS 270-294) · airframe 62,288 hrs · 32,074 cycles

INSPECTION FOUND CABIN FLOOR TRACK CORRODED AT STA 270-294.5, RBL 42. A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 51-10-02.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 62,288 hrs · 32,074 cycles

INSPECTION FOUND RT CHANNEL STIFFENER AT THE BOTTOM CENTER OF THE AFT PRESSURE BULKHEAD CORRODED, STA 1016, BL 0.

Part: SKIN — DELAMINATED (FUSELAGE) · airframe 57,248 hrs · 29,632 cycles

DELAMINATION BETWEEN DOUBLER AND SKIN ON LT SIDE OF FUSELAGE AT STA 727B. REPLACED SKIN PER ECRA 5330-03481.

Part: SKIN — CRACKED (LT PYLON) · airframe 57,248 hrs · 29,632 cycles

CRACK IN PYLON SKIN AT 5727L LEFT UPPER PYLON. INSTALLED DOUBLER PER ECRA 5430-01230.

Part: SKIN — DELAMINATED (FUSELAGE) · airframe 57,248 hrs · 29,632 cycles

DELAMINATION BETWEEN SKIN AND DOUBLER ON LT SIDE OF FUSELAGE AT STA 727D. REPLACED SKIN PER ECRA 5330-03431.

Part: FITTING — CRACKED (RT PYLON) · airframe 57,248 hrs · 29,632 cycles

RIGHT PYLON FRAME CRACKED INBOARD AT AFT ACCESS PANEL. INSTALLED NEW FITTING PER SRM 51-40-02.

Part: SPAR — WORN (HORIZONTAL STAB) · airframe 57,248 hrs · 29,632 cycles

HORIZONTAL STABILIZER CENTER SECTION REAR SPAR RIGHT LOWER AFT CLEVIS WORN INTO BY ACCESS PANEL 9224R. BLENDED THE GOUGE PER ECRA 5550-01035.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,786 hrs · 29,386 cycles

INSPECTION FOUND AFT CARGO COMPARTMENT FORWARD DOOR JAMB FRAME CORRODED AT LATCH FITTING, STA 787, S19R TO S27R. A NEW FRAME WAS INSTALLED IAW SRM 51-40 AND ECRA 5310-04456.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,786 hrs · 29,386 cycles

INSPECTION FOUND A 1.75 INCH CRACK IN FRAME AT NR 5 STOP, UNDER STOP, IN RADIUS (STA 794.3, AFT CARGO DOOR OPENING FORWARD FRAME, L18R TO L27R). REPAIRED IAW BOEING DRAWING 65C35243.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 54,004 hrs · 27,910 cycles

INSPECTION FOUND A 2 INCH CRACK IN LT WING NR 3 SLAT PANEL LOWER SKIN. A DOUBLER WAS INSTALLED IAW SRM 57-43-01.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 53,982 hrs · 27,899 cycles

INSPECTION FOUND LT TIEDOWN RAIL CORRODED AT STA 787, S26L. A NEW TIEDOWN RAIL WAS INSTALLED IAW SRM 51-40-02.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND A 2 INCH CRACK IN FORWARD CARGO DOOR INNER SKIN WHERE COUNTER BALANCE CABLE EXITS DOOR. THE CRACKED AREA WAS TRIMMED OUT AND A REPAIR DOUBLER AND STRAP WERE INSTALLED IAW ECRA 5232-01025.

Part: STRAP — CORRODED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND AFT BAGGAGE BIN STRAP JUST INSIDE DOOR WHERE THRESHOLD WEB ATTACHES CORRODED. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND INTERCOSTAL CORRODED ON LOWER SURFACE AT NUT PLATES, BS 500C-500B, S26L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND INTERCOSTAL CORRODED ON LOWER SURFACE AT NUT PLATES, STA 500C-500D, S26L. THE INTERCOSTAL WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 53-30-53 AND 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND SHEAR TIE CORRODED AT AFT SIDE OF FRAME STA 500D O/B OF S28R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND KEELBEAM LOWER CHORD CORRODED AT BS 500B-520, S28L. REPAIRED IAW SRM 53-30-12, FIGURE 202.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, LBL 1. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SKIN — DENTED (NR 2 TE FLAP) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND NR 2 MID FLAP SKIN DENTED AT LEADING EDGE CENTER. REPAIRED IAW SRM 57-53-01.

Part: ANGLE — CRACKED (NR 5 SPOILER) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND A 1 INCH CRACK IN SUPPORT ANGLE ON RT WING TRAILING EDGE PANEL JUST OUTBOARD OF NR 5 SPOILER PANEL. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 57-53-71.

Part: SKIN — CRACKED (WINDOW POST) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND A 2 INCH CRACK IN SKIN OF PILOT'S LT WINDOW POST. REPAIRED IAW SRM 53-10-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND SEAT TRACK CORRODED AT STA 277-294.5, RBL 40. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-10-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,864 hrs · 27,246 cycles

INSPECTION FOUND FLOORBEAM CORRODED ON UPPER FLANGE AT STA 294.5, RBL 35-50. REPAIRED FLOORBEAM IAW SRM 53-10-51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 20 TO RBL 4. REPAIRED IAW SRM 53-10-51.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND A 1INCH CRACK IN FLOOR SUPPORT AT STA 312-328, LBL 10. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED ON UPPER SURFACE AT STA 328-344, LBL 11. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND A .2500 INCH CRACK IN WEB AT STA 386 INBOARD OF CREASE BEAM. THE CREASE BEAM WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 51-70-13.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND SUPPORT ANGLE FOR FORWARD LAV AFT WALL CORRODED AT STA 307. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND A 4 INCH CRACK IN FUSELAGE SKIN AT STA 837-867, STRINGER 1. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 1016, LBL 30. REPAIRED FLOORBEAM IAW SRM 53-00-51.

Part: STIFFENER — CRACKED (NR 3 FLAP TRACK) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND A 1 INCH CRACK IN NR 3 FLAP TRACK FAIRING STIFFENER. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 52,865 hrs · 27,246 cycles

INSPECTION FOUND L-ANGLE ATTACHED TO Z-ANGLE AT R-1 DOOR CORRODED. THE L-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: SKIN — CRACKED (STA 727E) · airframe 52,790 hrs · 27,212 cycles

INSPECTION FOUND A 1.125" CRACK IN FUSELAGE SKIN AT STA 727E, S24R. A REPAIR WAS INSTALLED IAW ECRA 5330-03229 WITH A PERMANENT REPAIR TO FOLLOW NO LATER THAN 31 MARCH 2003.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 52,013 hrs · 26,797 cycles

INSPECTION FOUND A 1 INCH CRACK IN PRESSURE DECK AT BS 664, RBL 40. REPAIRED IAW SRM 53-60-51.

Part: FITTING — TORN (#2 PYLON) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND #2 PYLON AFT FITTING TORN. THE TORN AREA WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5750-03588.

Part: SKIN — DENTED (AFT CARGO DR) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND THE AFT CARGO DOOR SKIN DENTED AT TWO LOCATIONS. A DOUBLER REPAIR WAS INSTALLED AT EACH LOCATION IAW SRM 52-00-01.

Part: SKIN — CRACKED (#3 SLAT) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND A 2" CRACK IN #3 SLAT LOWER BULLNOSE SKIN AT TWO RIVETS BELOW STOP O/B OF THE ACTUATOR. THE CRACKED AREA WAS CUT OUT AND FILLER AND SPLICE PLATE WERE INSTALLED IAW SRM 57-43-01, FIGURE 206.

Part: STOP FITTING — WORN (CARGO DOOR) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND AFT CARGO DOOR FORWARD LOWER, FORWARD SECOND FROM BOTTOM, AND AFT UPPER STOP FITTINGS WORN. NEW STOP FITTINGS WERE INSTALLED IAW SRM 51-10-02, 51-10-01, AND 51-40-00.

Part: SKIN — GOUGED (C-1 DOOR) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND C-1 DOOR SKIN GOUGED 11 INCHES FROM BOTTOM AND 21 INCHES FROM FORWARD EDGE. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.

Part: FLAP — GOUGED (WING) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND NR 1 FOREFLAP GOUGED ON O/B END. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-37.

Part: SKIN — GOUGED (#1 MID FLAP) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND #1 MID FLAP SKIN GOUGED ON L/E AT O/B END. THE GOUGED AREA WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 57-53-01.

Part: SKIN — CRACKED (#3 SLAT) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND A 4" CRACK IN #3 SLAT SKIN AT I/B L/E. THE CRACKED AREA WAS CUT OUT AND FILLER AND SPLICE PLATE WERE INSTALLED IAW SRM 57-43-01, FIGURE 206.

Part: SKIN — GOUGED (FWD CARGO DR) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND FORWARD CARGO DOOR EXTERNAL SKIN GOUGED AT AFT END OF HANDLE CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.

Part: SKIN — DENTED (STA 420) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT STA 420, S24R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, PAGE 18, FIGURE 8.

Part: SKIN — DENTED (STA 360-368) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND EXTERIOR FUSELAGE SKIN DENTED AT STA 360-368, S17L. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-30-01.

Part: SKIN — DENTED (STA 460) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND EXTERIOR FUSELAGE SKIN DENTED AT STA 460, S22L. THE SKIN WAS REPAIRED IAW SRM 53-00-01.

Part: SKIN — DENTED (AFT CARGO DR) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND AFT CARGO DOOR SKIN DENTED 5 INCHES FROM UPPER EDGE AND 29 INCHES FROM LEADING EDGE. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 219.

Part: ATTACH ANGLE — BENT (STA 460) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND FRAME 460 ATTACH ANGLE BENT AT BELLY OF AIRCRAFT. NEW ATTACH ANGLES WERE INSTALLED IAW SRM 53-00-07.

Part: SKIN — DENTED (FWD CARGO DR) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND FORWARD CARGO DOOR SKIN DENTED IN TWO PLACES. A DOUBLER WAS INSTALLED A EACH LOCATION IAW SRM 52-30-1.

Part: SKIN — CANNING (FUSELAGE) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND FUSELAGE BELLY SKIN OIL CANNING AROUND ANTENNA BETWEEN STA 460-480, S26R/L. THE DAMAGED SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01.

Part: SKIN — DENTED (STA 1040) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND FUSELAGE BELLY SKIN DENTED AT STA 1040, BL 0. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202.

Part: SKIN — DENTED (STA 727E) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND R/H FUSELAGE SKIN DENTED AT STA 727E BETWEEN S21R AND S22R. THE DENTED AREA OF SKIN WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 208.

Part: SKIN — DENTED (STA 843) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND L/H FUSELAGE SKIN DENTED AT STA 843 BETWEEN S22L AND S23L. THE DENTED AREA OF SKIN WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 202.

Part: SLAT — DELAMINATED (R/W #6 POSN.) · airframe 49,336 hrs · 25,427 cycles

INSPECTION FOUND R/H WING #6 L/E SLAT DELAMINATED AT UPPER SURFACE I/B END. THE SLAT WAS REPAIRED IAW SRM 51-70-10.

Part: SKIN — DENTED (BS 906)

INSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 906, S10L. REPAIRED IAW ECRA 5330-02793.

Part: SKIN — DENTED (CARGO DOOR)

INSPECTION FOUND C-1 DOOR SKIN DENTED. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01.

Part: WIRE — BROKEN (ROW 16)

EMERGENCY EXIT AISLE PATH LIGHT AT ROW 16 INOP. REMOVED AND REPLACED LIGHT SOCKET FOR AISLE PATH EMERGENCY EXIT LIGHT AT ROW 16. LIGHT OPS CHECK NORMAL.

Part: FLOORBEAM — CORRODED (BS 986.5)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5. A REPAIR WAS INSTALLED IAW ECRA 5310-03836.

Part: ANGLE — CORRODED (BS 727)

INSPECTION FOUND FLOOR SUPPORT ANGLES AT LBL 3, RBL 3, LBL 8, AND RBL 8, STA 727D CORRODED. A REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-00-53.

Part: SEAT TRACK — CORRODED (BS 344)

INSPECTION FOUND SEAT TRACK NR 2 CORRODED AT STA 344. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52, FIGURE 202.

Part: FLOORBEAM — CORRODED (BS 947.5)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 947.5, RBL 24 TO LBL 17. A REPAIR WAS INSTALLED IAW SRM 53-60-51.

Part: SEAT TRACK — CORRODED (BS 330-360)

INSPECTION FOUND NR 3 SEAT TRACK IN NR 2 GALLEY AREA CORRODED FROM STA 330 TO 360. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52, FIGURE 202.

Part: FLOORBEAM — CORRODED (BS 328)

INSPECTION FOUND FLOORBEAM CAP IN FORWARD GALLEY AREA CORRODED AT STA 328. A FLOORBEAM REPAIR WAS INSTALLED IAW SRM 53-10-51, FIGURE 205.

Part: CHANNEL — CORRODED (L1 DOORWAY)

INSPECTION FOUND FORWARD ENTRY DOOR (L-1) Z-CHANNEL CORRODED. A NEW SECTION OF Z-CHANNEL WAS INSTALLED IAW SRM 51-10-2.

Part: FLOORBEAM — CORRODED (BS 967)

INSPECTION FOUND TOP OF FLOORBEAM CORRODED AT STA 967, RBL 4. THE CORRODED AREA WAS REPAIRED IAW SRM 53-10-51.

Part: FLOORBEAM — CORRODED (BS 312-328)

INSPECTION FOUND CORROSION ON FLOORBEAM NUT PLATES AND ON DOUBLER AT STA 312 TO 328. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-70-12.

Part: YAW DAMPER — MALFUNCTIONED (E & E COMPT)

WHILE CLIMBING THROUGH 5,000 FEET WITH THE AUTOPILOT OFF, THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL. THE YAW DAMPER INDICATOR PEGGED FULL RIGHT. THE YAW DAMPER WAS TURNED OFF AND THE FLIGHT WAS CONTINUED. THE YAW DAMPER WAS TURNED ON WHILE AT CRUISE WITH AUTOPILOT ON AND OPERATION WAS NORMAL. MAINTENANCE REMOVED AND REPLACED THE MAIN RUDDER PCU, THE STANDBY RUDDER PCU, AND THE YAW DAMP COUPLER. *S/D* SHOP TEARDOWN REVEALED THE FOLLOWING (1) YAW DAMPER COUPLER (P/N 4030952-906) RATE GYRO ROUGH RUNNING. (2) STANDBY RUDDER PCU (P/N 1U1150-1) ROD SEAL LEAKAGE WITH PACKING WORN, FOUND BOLTS, CORRODED. (3) MAIN RUDDER PCU (P/N 65C37052-9) LEVER ASSEMBLIES AND ROD END BEARINGS WORN, MANIFOLD CORRODED.

Part: BATTERY PACK — INOPERATIVE (CABIN)

THE OVERHEAD EMERGENCY EXIT LIGHTS AT LT DOOR FAILED CAPACITY CHECK. THE BATTERY PACK WAS REMOVED AND REPLACED.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE EMERGENCY EXIT AISLE LIGHTS AT ROWS 15 TO 23 LT AND ROWS 14 TO 21 RT FAILED CAPACITY CHECK. THE BATTERY PACK WAS REMOVED AND REPLACED.

Part: OIL PRESS IND — OUT OF ADJUST (APU)

THE APU LOW OIL PRESSURE LIGHT NEVER WENT OUT WHEN APU GEN OFF BUS LIGHT WAS ON DURING APU START ON DESCENT INTO EWR. THE APU THEN AUTO SHUTDOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. ONE QUART OF OIL WAS ADDED TO THE APU. THE APU STARTED NORMALLY ON THE SECOND ATTEMPT, BUT THE APU WOULD NOT COME ON LINE. THE APU OIL PRESSURE WAS FOUND AT 110 PSI DURING TROUBLESHOOTING USING THE APU TEST BOX. THE OIL PRESSURE WAS ADJUSTED TO 100 PSI. NO EXTERNAL LEAKS WERE NOTED, ALL PARAMETERS WERE WITHIN LIMITS.