N12349

Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 55,326 hrs · 28,869 cycles

INSPECTION FOUND A 0.58 INCH CRACK IN FORWARD CARGO DOOR INNER SKIN AROUND FORWARD LIGHTENING CUTOUTS SPRING COMPARTMENT. A REPAIR WAS INSTALLED IAW ECRA 5232-01075.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,326 hrs · 28,869 cycles

INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT STA 294, S12L FORWARD OF L-1 DOOR. A REPAIR WAS INSTALLED IAW ECRA 5310-04535.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,326 hrs · 28,869 cycles

INSPECTION FOUND A .75 INCH CRACK IN STRINGER SPLICE CHANNEL AT STA 360, S14L AFT OF L-1 DOOR. A REPAIR WAS INSTALLED IAW ECRA 5310-04535.

Part: FITTING — CRACKED (HORIZ STAB) · airframe 55,326 hrs · 28,869 cycles

INSPECTION FOUND A 5 INCH CRACK IN HORIZONTAL STABILIZER CENTER SECTION -X- BRACE RT FORWARD LOWER CORNER FITTING. THE FITTING WAS REPLACED IAW SRM 51-40-02.

Part: PAN — CRACKED (C-2 DOOR) · airframe 55,326 hrs · 28,869 cycles

INSPECTION FOUND A 0.8 INCH CRACK IN C-2 DOOR PAN AT FORWARD MID SECTION. THE DOOR PAN WAS REPAIRED IAW SRM 51-40-02.

Part: PAN — CRACKED (FUSELAGE) · airframe 55,326 hrs · 28,869 cycles

INSPECTION FOUND A .75 INCH CRACK IN C-1 DOOR PAN LOWER FORWARD CORNER NEXT TO UPLATCH HOOK, STA 440-500, S17R TO S27R. THE PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 51-10-02, STEP 8 AND SRM 51-40-02, STEP 4 AND 5.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 55,326 hrs · 28,869 cycles

AFT CARGO COMPARTMENT BELT FRAME STA 794, S25R - S22R, LOWER SIDE AT C-2 DOOR CUTOUT, STRAP AND REPAIR DOUBLER HAVE SOME CORROSION BY NUT PLATES. REPAIRED BELT FRAME IAW SRM 53-60-53.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 55,326 hrs · 28,869 cycles

INSPECTION FOUND A 1 INCH CRACK IN LT KEEL BEAM AT STA 540, S29L. THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12, FIGURE 201, PAGE 205.

Part: STIFFENER — CORRODED (BS 1016) · airframe 55,326 hrs · 28,869 cycles

INSPECTION FOUND RT CHANNEL STIFFENER CORRODED AT LOWER APB STA 1016, RBL 1. THE CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW BOEING DRAWING 65C28106 AND EA 5310-04045, REV A, OPS 2.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 55,326 hrs · 28,869 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, LBL 4 TO LBL 36. THE CORRODED FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 53-00-51.

Part: BULKHEAD — CORRODED (BS 1014 S27L-27R) · airframe 55,326 hrs · 28,869 cycles

INSPECTION FOUND FORWARD SIDE OF AFT PRESSURE BULKHEAD CORRODED AT STA 1014 BETWEEN S27R AND S27L. THE AREA WAS REPAIRED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 907-947) · airframe 55,326 hrs · 28,869 cycles

INSPECTION FOUND THE LEFT I/B SEAT TRACK CORRODED AT STA 907 TO 947.5, LBL 25. THE SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 616) · airframe 55,326 hrs · 28,869 cycles

INSPECTION FOUND A .25 INCH CRACK IN LEFT MAIN FRAME BELOW MAIN DECK AT STA 616, LBL 60 TO LBL 61. THE MAIN FRAME WAS REPAIRED IAW ECRA 5311-01158.

Part: SENSOR — INTERMITTENT (NLG) · airframe 52,488 hrs · 27,528 cycles

LANDING GEAR UNSAFE LIGHT CAME ON THEN INTERMITTENT AFTER LEVEL AT FL35. REPLACED NLG SENSOR PER AMM 32-61-51.

Part: ACCESS PANEL — CRACKED (NR 1 PYLON) · airframe 51,080 hrs · 26,810 cycles

INSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL NR 5724 CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01204.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 51,080 hrs · 26,810 cycles

INSPECTION FOUND A .5 INCH CRACK IN LT OB SEAT TRACK, OB FLANGE AT STA 727B. A REPAIR WAS INSTALLED IAW ECRA 5321-01202.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,542 hrs · 26,551 cycles

THE EMERGENCY EXIT SIGN AT L-2 DOOR WAS FOUND FLICKERING ON AND OFF. THE BATTERY CHARGER AND BATTERY PACK AT L-2 DOOR WERE REMOVED AND REPLACED IAW MM 33-51-51, PAGES 201-207. AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT WAS GOOD.

Part: SPOILER · airframe 45,554 hrs · 23,697 cycles

#3 SPOILER DENTED AND CRACKED .75X.75 INCHES JUST FWD AND OB OF ACTUATOR ATTACH POINT. INSTALLED DOUBLER PER SRM 57-70-01, FIG 204.

Part: WEB — CORRODED (STA 793-847) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND AFT CARGO DOOR CUTOUT THRESHOLD WEB CORRODED AT STA 793-847. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: WEB — CORRODED (STA 767-847) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND CORROSION UNDER FLANGE OF VERTICAL THRESHOLD WEB AT AFT BAGGAGE BIN DOORWAY FROM STA 767-847. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: CHANNEL — CORRODED (STA 727D+5) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNELS CORRODED AT STA 727D+5", RBL 8 AND LBL 8. REPAIR ANGLES WERE INSTALLED AT EACH LOCATION IAW ECRA 5320-01603.

Part: CHANNEL — CORRODED (STA 794) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND CHANNEL CORRODED IN AFT BAGGAGE BIN AT STA 794, RBL 8. REPAIRED IAW SRM 53-00-53.

Part: CHANNEL — CORRODED (STA 794) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNELS CORRODED AT STA 794, LBL 3 AND RBL 3. CHANNEL BEAM REPAIRS WERE INSTALLED AT EACH LOCATION IAW SRM 53-00-53, FIGURE 201.

Part: CHANNEL — CORRODED (STA 727D+5) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNEL CORRODED AT STA 727D+5" RBL 3. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5320-01603.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNEL CORRODED AT STA 727D+5, LBL 12. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5320-01603.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 294-312, RBL 15. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (STA 312) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND CABIN FLOORBEAM UPPER CAP CORRODED AT STA 312. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-10-51.

Part: FLOORBEAM — CORRODED (STA 294.5) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND FLOORBEAM UPPER T CAP CORRODED AT FASTENER HOLES, STA 294.5, LBL 20 TO RBL 58. REPAIRED IAW SRM 53-10-51.

Part: FLOORBEAM — CORRODED (STA 344) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND FLOORBEAM T-CAP CORRODED AT FASTENER HOLES, STA 344. REPAIRED IAW SRM 51-10-51.

Part: WEB — CRACKED (STA 559-578) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND A 3" CRACK IN WEB AT R/H SIDEWALL FLOOR BETWEEN STA 559 AND 578. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02.

Part: STRINGER — CRACKED (STA 500C) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND A 1/2" CRACK IN STRINGER 16L JUST FORWARD OF WING ILLUMINATION LIGHT HOUSING AT STA 500C. A NEW STRINGER WAS INSTALLED IAW SRM 53-30-03 AND 53-00-03.

Part: MOUNT — CORRODED (STA 1012) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND AFT O/B LAV MOUNT CORRODED AT STA 1012, LBL 38. THE LAV MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: CHANNEL — CORRODED (STA 986.5-1006) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND AFT O/B CHANNEL OF WEB CORRODED AT STA 986.5-1006, LBL 38. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: STRINGER — CORRODED (STA 1006-1016) · airframe 45,554 hrs · 23,697 cycles

INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 41,119 hrs · 21,374 cycles

INSPECTION FOUND AFT BAGGAGE BIN DOOR EXTERIOR SKIN GOUGED. THE SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 51-40-02.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 41,119 hrs · 21,374 cycles

INSPECTION FOUND A 0.4 INCH CRACK IN ABB DOOR INTERIOR SKIN AT LIGHTENING HOLE EDGE. THE EXISTING REPAIR DOUBLERS WERE REMOVED AND A NEW SINGLE DOUBLER REPAIR WAS INSTALLED IAW ECRA 5230-01571.

Part: PANEL — CORRODED (BS 847-867)

INSPECTION FOUND RT TRANSITION PANEL CORRODED AT STA 847-867. THE TRANSITION PANEL WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: CHANNEL — CORRODED (BS 294-328)

INSPECTION FOUND R-1 DOOR Z-CHANNEL CORRODED AT STA 294-328. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: SEAT TRACK — CORRODED (BS 328-344)

INSPECTION FOUND SEAT TRACK CORRODED AT FS 328-344. THE CORRODED SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 53-00-52.

Part: FLOORBEAM — CORRODED (BS 294.5)

INSPECTION FOUND FLOORBEAM CAP IN FORWARD GALLEY AREA CORRODED AT FS 294.5, RBL 8. THE FLOORBEAM CAP WAS REPAIRED IAW SRM 53-10-51.

Part: FLOOR TRACK — CORRODED (BS 294.5)

INSPECTION FOUND FORWARD GALLEY FLOOR TRACK CORRODED AT STA 294.5. THE FLOOR TRACK WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 53-00-52.

Part: CORRODED — CORRODED (BS 947)

INSPECTION FOUND CORROSION ON FLOORBEAM/TRACK TIEDOWN IN AFT PIT AT STA 947, LBBL 17.2. A NEW TRACK TIEDOWN WAS SPLICED IN IAW SRM 53-00-53, FIGURE 202.

Part: LIGHT — INOPERATIVE (L 2 DOOR)

THE L-2 DOOR EMERGENCY SLIDE EXIT LIGHT WAS FOUND INOPERATIVE. THE EXIT LIGHT WAS REMOVED AND REPLACED.

Part: NOSE LINK — BROKEN (NR 2 LE FLAP)

EWR - FLT 0725 - THE NR 2 LEADING EDGE FLAP TRANSIT LIGHT ON OVERHEAD PANEL AND FORWARD PANEL LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED WITH THE FLAPS RETRACTED WHILE IN CLIMB. THE AIRCRAFT WAS RETURNED TO EWR. MAINTENANCE FOUND THE NR 2 KRUGER FLAP NOSE LINK AT INBOARD END BROKEN. THE NOSE LINK WAS REPLACED. THE FLAP WAS RIGGED IAW MM 27-81-11. (X)

Part: O-RINGS — CUT (NR 2 GEARBOX)

GSO - FLT 0171 - THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED WHILE ON FINAL APPROACH TO GSO. THE NR 2 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE. THE CREW REPORTED LOSING LESS THAN 8.5 PSI OIL PRESSURE. MAINTENANCE FOUND THE NR 2 ENGINE ANGLE GEARBOX LEAKING AT O-RINGS. THE O-RINGS WERE REMOVED AND REPLACED AND LEAK CHECK WAS GOOD. THE NR 2 ENGINE WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE DUE TO THE OIL LOSS. (X)