N17329

Part: SLIDE — NO DISCREPANCY (ZONE 200) · airframe 6,827 hrs · 2,350 cycles

R2 DOOR SLIDE PRESSURE IN THE RED. PRESSURE TOO HIGH, INSPECTED SLIDE PRESSURE WITHIN LIMITS ACCORDING TO AMM 25-66-01-200/801 OK FOR SERVICE.

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 6,300 hrs · 2,198 cycles

DOOR R2 ESCAPE SLIDE PRESSURE GAGE IS IN RED. ON THE HIGH SIDE FOUND NEEDLE TO WITH WITHIN 1 NEEDLES WITH TO THE RIGHT OF GREEN BAND PER AMM 25-66-01-200-801 DUE TO SLIDES INFLATION CYCLINDER NOT BEING AT A STABLE TEMP FOR MORE THEN 2 HOURS. 52 MINS ON THE GROUND IN EWR WHEN ITEM WAS WRITTEN UP.

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 5,787 hrs · 2,026 cycles

2R AFT DOORSLIDE GAUGE SHOWING RED INSPECTED 2R ESPACE SLIDE PACK INFLATION CYLINDER IAW AMM 25-66-01. NOT MORE THAN ONE NEEDLE WIDTH TO THE RIGHT OF THE GO BAND (GREEN).

Part: SKIN — CRACKED (BS 727E S23R) · airframe 64,402 hrs · 33,043 cycles

APPROXIMATELY .75 INCH SKIN CRACK NOTED RT FUSELAGE 2.5 INCH BELOW AND 15 INCH AFT OF EMERGENCY EXIT LIGHT, JUST AFT OF WHEEL WELL STATION 727E STRINGER 23R. REPAIRED IAW SRM 53-00-01 REPAIR 31.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,006 hrs · 32,866 cycles

FWD CARGO COMPARTMENT DOOR CUTOUT, AFT FRAME SHOWS CRACK INDICATION WITH HFEC AT LOWER STOP UPPER AREA. REMOVED AND REPLACED FWD CARGO AFT DOOR CUTOUT FRAME PER SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,218 hrs · 31,546 cycles

INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT THE AFT LOWER CORNER OF THE R-1 DOOR CUTOUT, STA 328, S18R. REPAIRED IAW SRM 53-10-01. A DIP WAS ISSUED TO INSPECT THE REPAIR WITHIN 60,000 FLIGHT HOURS AFTER REPAIR ACCOMPLISHMENT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,718 hrs · 31,546 cycles

INSPECTION FOUND FUSELAGE SKIN BENEATH NR 1 DME ANTENNA CORRODED AT STA 460, S29L. THE CORRODED SECTION OF SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW ECRA 5331-01305. A DIP WAS ISSUED TO REINSPECT THE REPAIR AT 60,000 FLIGHT CYCLES THEN EVERY 30,000 FLIGHT CYCLES THEREAFTER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,218 hrs · 31,546 cycles

INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN FORWARD OF R-2 DOOR BETWEEN UPPER AND LOWER HINGES AT STA 950. THE INNER SKIN WAS REPLACED IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,218 hrs · 31,546 cycles

INSPECTION FOUND A 0.65" CRACK IN FUSELAGE SKIN AT THE R-2 DOOR UPPER HINGE CUTOUT UPPER FORWARD CORNER. THE SKIN WAS REPAIRED IAW SRM 53-60-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,218 hrs · 31,546 cycles

INSPECTION FOUND FORWARD CARGO COMPARTMENT FRAME CORRODED AT STA 500 BETWEEN STRINGER 26L AND 27L. A SHEAR TIE AND FILLER WERE INSTALLED IAW SRM 53-00-07.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,218 hrs · 31,546 cycles

INSPECTION FOUND A 1/2" CRACK IN FUSELAGE SKIN AT THE R-2 DOOR LOWER HINGE CUTOUT FWD LOWER CORNER, STA 947.5, S13R TO S14R. THE CRACKED AREA OF SKIN WAS CUT OUT AND A REPAIR DOUBLER, TRIPLER, AND FILLER WERE INSTALLED IAW SRM 53-60-01.

Part: WIRE HARNESS — BURNED (LT MLG WW) · airframe 57,498 hrs · 29,800 cycles

LT WING BODY OVERHEAT LIGHT, FLAP IND SHOWED RT FLAP RETRACTED, LT FLAP 0700 POSITION. PRESSURIZATION AUTO FAIL LIGHT ILLUM. EMERGENCY DESCENT. M1205 ELEMENT REMOVED & REPLACED FOR OVERHEAT CONDITION, T/E FLAP POSITION IND REPLACED FOR LOCKOUT ISSUE, PRESSURIZATION CONTL TEST PERFORMED, NO FAULTS. LT O/B LANDING LIGHT REPLACED, C/B TRIPPING. FOUND WIRE BUNDLE W0802 WITH WIRES DAMAGED AT CEILING LT MLG WW STA 713, 1 FT O/B OF JUNCTION. W802 WIRING HARNESS REPLACED, AREAS REPAIRED. BURNED WIRES W570-A-R & W570-A-B BTW S72 LMLG UP-LOCK SENSOR & C/P D4840P, WIRES REPLACED. BURNED WIRES W802-004-20 & W802-005-20 FWD OF SPLICE SP4202 & 4204 FOUND, WIRES RESPLICED. FUEL S/O WIRES O/B OF CANOE FAIRING SPLICED.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 54,992 hrs · 28,557 cycles

INSPECTION FOUND A 0.3 INCH CRACK AT LIGHTENING HOLE IN AFT CARGO DOOR INNER SKIN. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01057.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 54,992 hrs · 28,557 cycles

INSPECTION FOUND TWO 0.3 INCH CRACKS AT LIGHTENING HOLE IN AFT CARGO DOOR INNER SKIN. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01056.

Part: FRAME — CORRODED (FUSELAGE) · airframe 54,992 hrs · 28,557 cycles

INSPECTION FOUND FORWARD SIDE OF FRAME CORRODED IN FORWARD CARGO PIT AT STA 500D BETWEEN S27L AND S28L. INSTALLED REPAIR IAW SRM 53-00-07, FIGURE 205.

Part: STIFFENER — CORRODED (BULKHEAD) · airframe 54,992 hrs · 28,557 cycles

INSPECTION FOUND APB BOTTOM CENTER STIFFENER CORRODED ON LEFT HALF, BS 1016-1020. THE CORRODED AREA WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW ECRA 5311-01213.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,992 hrs · 28,557 cycles

INSPECTION FOUND CABIN RIGHT O/B SEAT TRACK CORRODED AT STA 328-360, RBL 48 TO LBL 48. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.

Part: GALLEY TRACK — CORRODED (FUSELAGE) · airframe 54,992 hrs · 28,557 cycles

INSPECTION FOUND FORWARD GALLEY FLOOR TRACK CORRODED AT STA 275-294, RBL 43. A NEW FLOOR TRACK SECTION WAS INSTALLED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,992 hrs · 28,557 cycles

INSPECTION FOUND CABIN RIGHT I/B SEAT TRACK CORRODED AT STA 328-355, BL 0 TO RBL 23. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 202.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 54,992 hrs · 28,557 cycles

INSPECTION FOUND R-2 DOOR Z-ANGLE CORRODED AT STA 991.5, RBL 46 TO LBL 46. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: STRAP — CORRODED (FUSELAGE) · airframe 51,641 hrs · 26,754 cycles

INSPECTION FOUND AFT BAGGAGE BIN STRAP CORRODED BETWEEN STA 777 AND 847, RBL 20. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,641 hrs · 26,754 cycles

INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CORRODED AT STA 767, LBL 8 AND LBL 12. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5320-01603.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 51,641 hrs · 26,754 cycles

INSPECTION FOUND A .25 INCH CRACK ON LIP OF HOLE CUT ON O/B SIDE OF ACCESS PANEL 5727L OF NR 1 PYLON. REPAIRED ACCESS PANEL IAW ECRA 5430-01230.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,641 hrs · 26,754 cycles

INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CORRODED AT STA 767, LBL 3. THE FLOOR SUPPORT WAS REPAIRED IAW ECRA 5320-01603.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 51,641 hrs · 26,754 cycles

INSPECTION FOUND A .5 INCH CRACK IN MAIN WHEEL WELL PRESSURE DECK AT STA 673, LBL 31. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-51, FIGURE 203.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,641 hrs · 26,754 cycles

INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CORRODED AT STA 767, RBL 3. THE FLOOR SUPPORT WAS REPAIRED IAW ECRA 5320-01603.

Part: STRAP — CORRODED (FUSELAGE) · airframe 51,641 hrs · 26,754 cycles

INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT STRAP CORRODED AT STA 727E, LBL 21. THE FLOOR SUPPORT STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: ARM — OUT OF ADJ (L1 DOOR) · airframe 46,469 hrs · 24,046 cycles

L1 DOOR WILL NOT CLOSE. ADJUSTED L1 DOOR GUIDE ARM. OPS CHECK OK.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 46,160 hrs · 23,894 cycles

INSPECTION FOUND A 2 INCH CRACK IN FORWARD CARGO DOOR INNER SKIN. A REPAIR WAS INSTALLED IAW ECRA 5230-01604.

Part: SKIN — GOUGED (FUSELAGE) · airframe 46,160 hrs · 23,894 cycles

INSPECTION FOUND FUSELAGE SKIN GOUGED AT L-1 DOOR TORQUE TUBE UPPER HINGE AREA, BS 312 , S13L. THE GOUGED AREA OF SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 46,160 hrs · 23,894 cycles

INSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 395, STRINGER 20-21R. A DOUBLER WAS INSTALLED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,160 hrs · 23,894 cycles

INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 807 BETWEEN STRINGER 27L AND 27R. A REPAIR WAS INSTALLED IAW SRM 53-00-07.

Part: WEB — CRACKED (CARGO BAY) · airframe 46,160 hrs · 23,894 cycles

INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR JAMB LOWER FORWARD INSIDE CORNER WEB AT STA 440, S25. REPAIRED WEB IAW SRM 51-70-13, FIGURE 1.

Part: RIB — GOUGED (VERTICAL STAB) · airframe 46,160 hrs · 23,894 cycles

INSPECTION FOUND L/E RIB OF VERTICAL STABILIZER GOUGED AT STA 10-40. THE DORSAL FIN RIB WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FITTING — CRACKED (LT WING) · airframe 46,160 hrs · 23,894 cycles

INSPECTION FOUND A 1 INCH CRACK IN LT WING MLG SUPPORT BEAM O/B ATTACH FITTING AT AFT SPAR. A NEW FITTING WAS INSTALLED IAW WORK CARD 03-5743-1-0003.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,160 hrs · 23,894 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 967-986, LBL 18.32. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: INTERCOSTAL — CRACKED (BS 332)

INSPECTION FOUND A .75 INCH CRACK IN INTERCOSTAL AT STA 332, STRINGER 10R. THE INTERCOSTAL WAS REMOVED AND A REPAIR INTERCOSTAL AND REPAIR PARTS WERE INSTALLED IAW EA 5363-01014.

Part: PANEL — CRACKED (NR 3 LE SLAT)

INSPECTION FOUND A 1 CRACK IN LT WING NR 3 SLAT PANEL AT FASTENER I/B OF SLAT ACTUATOR. A REPAIR WAS INSTALLED IAW BOEING DRAWING 65C30133.

Part: SKIN — CRACKED (LT COCKPIT)

INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN OF UPPER WINDOW POST AT CAPTAIN'S NR 2 SLIDING WINDOW. A REPAIR WAS INSTALLED IAW ECRA 5330-02769.

Part: INTERCOSTAL — CRACKED (BS 947.5)

INSPECTION FOUND A 3 INCH CRACK IN INTERCOSTAL IN AFT BAGGAGE BIN AT STA 947.5, BELOW CABIN FLOOR CENTERLINE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-10-2.

Part: FUEL PUMP — INOPERATIVE (NR 2 ENGINE)

THE NR 2 ENGINE FLAMED OUT WHILE ON DESCENT. THE LOW IDLE LIGHT AND NR 2 GEN BUS OFF LIGHT ILLUMINATED AND THEN THE NR 2 LOW OIL PRESSURE LIGHT CAME ON. THE APU WAS STARTED AND NR 2 BUS WAS PUT ON LINE. ENGINE RESTART WAS PERFORMED, BUT THE ENGINE WOULD NOT ACHIEVE IDLE. THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE FUEL PUMP AND FCU WERE REMOVED AND REPLACED IAW MM 73-11-01. LEAK AND OPERATIONAL CHECKS OF THE FUEL PUMP AND FCU WERE GOOD. THE NR 2 ENGINE WAS RUN AND OPERATION CHECKED GOOD.

Part: CHORD — CRACKED (BS 520)

INSPECTION FOUND A 1 INCH CRACK IN FAIL SAFE CHORD AT STA 520, RBL 24.50. A NEW BRACKET WAS INSTALLED IAW SRM 51-10-2.

Part: ANGLE — CORRODED (BS 294.5-328)

INSPECTION FOUND Z-ANGLE CORRODED BETWEEN B.S. 294.5 AND 328. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (BS. 294.5-312)

INSPECTION FOUND FLOOR SUPPORTS CORRODED BETWEEN B.S. 294.5 AND 312 AT RBL 12 AND RBL 14. NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 312-344)

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT LBL 12 BETWEEN B.S. 312-328 AND BETWEEN B.S. 328-344. REPAIRS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03439.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 344 BETWEEN LBL 12 AND LT SIDEWALL. THE CORRODED AREA WAS REMOVED AND REPLACED IAW SRM 53-10-51.

Part: FLOORBEAM — CORRODED (BS 328)

INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 328 BETWEEN RBL 12 AND RT SIDE AND BETWEEN RBL 12 AND LT SIDE. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51, FIGURE 205.

Part: FLOORBEAM — CORRODED (BS 294)

INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 294 BETWEEN LBL 12 AND RBL 12. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 312 BETWEEN LBL 12 AND RT SIDEWALL. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.

Part: ANGLE — CORRODED (R 2 DOORWAY)

INSPECTION FOUND AFT L-ANGLE UNDER R-2 DOOR CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1.

Part: FAIRING SUPPORT — CRACKED (BS 540)

INSPECTION FOUND A 1 INCH CRACK IN RT WING TO BODY FAIRING SUPPORT AT STA 540, STRINGER 22. A .25 INCH CRACK WAS FOUND IN LT WING TO BODY FAIRING SUPPORT AT STA 540, STRINGER 22. THE SUPPORTS WERE REPAIRED IAW ECRA 5350-01227.

Part: SUPPORT — CRACKED (BS 540)

INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, AIRCRAFT CENTERLINE, LT SIDE. THE ANGLE WAS REPAIRED IAW SRM 51-70-11.

Part: SUPPORT — CRACKED (BS 540)

INSPECTION FOUND A 1.125 INCH CRACK IN FLOOR SUPPORT AT STA 540, AIRCRAFT CENTERLINE, RT SIDE. THE ANGLE WAS REPAIRED IAW SRM 51-70-11.

Part: SKIN — CRACKED (NR 5 LE FLAP)

INSPECTION FOUND THE NR 5 LEADING EDGE SLAT CRACKED AT THREE RIVETS UNDER INBOARD AUXILIARY TRACK. THE CRACKS WERE .25 INCH LONG. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW ECRA 5750-01159.

Part: SKIN — CRACKED (NR 6 LE FLAP)

INSPECTION FOUND A .25 INCH CRACK AT TWO RIVETS (SIX INCHES INBOARD OF ACTUATOR) ON NR 6 LEADING EDGE SLAT. THE SLAT WAS REPAIRED IAW ECRA 5750-01159.

Part: ANGLE — CRACKED (BS 540)

INSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SUPPORT ANGLE AT STA 540, STRINGER 22. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-70-11.

Part: SKIN — CRACKED (NR 1 PYLON)

INSPECTION FOUND A .50 INCH CRACK AT RIVET HOLE OF NR 1 ENGINE PYLON PANEL NR 5724. A DOUBLER WAS INSTALLED IAW ECRA 5430-01204.

Part: INTERCOSTAL — CORRODED (BS 995-1016)

INSPECTION FOUND INTERCOSTAL CORRODED AT NUTPLATE HOLES, STA 995-1016, LBL 37.21. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-2.

Part: INTERCOSTAL — CORRODED (BS 986-1016)

INSPECTION FOUND FLOOR SUPPORT INTERCOSTAL CORRODED AT STA 986-1016, LBL 15. THE FLOOR SUPPORT INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-2.

Part: INTERCOSTAL — CORRODED (BS 947-967)

INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN STA 947-967, RBL 17.61. THE INTERCOSTAL WAS REPLACED IAW SRM 51-40-2.

Part: FLOORBEAM — CORRODED (BS 986)

INSPECTION FOUND FLOORBEAM AT STA 986, LBL 15 TO DOOR SILL AREA CORRODED. THE AREA WAS REPAIRED IAW ECRA 5310-03361.

Part: INTERCOSTAL — CORRODED (BS 947-967)

INSPECTION FOUND FLOOR SUPPORT INTERCOSTAL CORRODED BETWEEN STA 947 AND 967, LBL 17.61. THE FLOOR SUPPORT INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-2.

Part: FLOORBEAM — CORRODED (BS 986.5)

INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLE AT STA 986.5, RBL 40. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03361.

Part: FLOORBEAM — CORRODED (BS 1006)

INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT NUTPLATE HOLE, STA 1006, RBL 20. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03360.

Part: INTERCOSTAL — CORRODED (BS 967-986)

INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN STA 967 AND 986, RBL 18.75. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 51-40-2.

Part: FLOORBEAM — CORRODED (BS 986.5)

INSPECTION FOUND RT SIDE AND CENTER OF FLOORBEAM CORRODED AT STA 986.5, RBL 3, RBL 5, AND RBL 15. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03361.

Part: INTERCOSTAL — CORRODED (BS 967-986.5)

INSPECTION FOUND FLOOR SUPPORT INTERCOSTAL CORRODED BETWEEN STA 967-986.5, LBL 17.61. THE FLOOR SUPPORT INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-2.

Part: FLOORBEAM — CORRODED (BS 967)

INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 967. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03362.

Part: ANGLE — CORRODED (BS 986.5)

INSPECTION FOUND FLOOR SUPPORT ANGLE AT AFT SIDE OF L-2 DOOR FRAME CORRODED AT STA 986.5. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 51-40-2.

Part: FLOORBEAM — CORRODED (CABIN)

INSPECTION FOUND AFT RIGHT LAV WALL FLOORBEAM CORRODED. THE AREA WAS REPAIRED IAW ECRA 5310-03361.