N711SY

Part: VALVE — FAULTED (HIGH STAGE)

BLEED TRIP OFF LIGHT ILLUMINATED DURING CLIMB, FAULT CODE 361 012 01. COMPLETED FIM 36-10 TASK 809 AND WAS SWAPPED HIGH STAGE VALVE BETWEEN NR 1 AND NR 2 ENGS IAW 36-11-06/401. INSTALLATION TEST NORMAL. SWAPPED BLEED AIR REGULATOR BETWEEN NR 1 AND NR 2 ENG IAW AMM 36-11-04/401. INSTALLATION TEST NORMAL.

Part: SKIN — WORN (RT WING SLAT) · airframe 58,533 hrs · 30,855 cycles

RH LE SLAT #7 BARE METAL SHOWING ON UNDERSIDE ALONG AFT EDGE. FOUND TRAILING EDGE WEAR BEYOND REPAIRABLE LIMITS PER SRM 57-42-01-2R-6 REPAIR 6. REMOVED #7 SLAT REF AMM 27-81-21. INSPECTED INTERFACE, OK TO INSTALL. INSTALLED NEW SLAT IAW AMM 27-81-21-400-801. SLAT ACCOMPLISHED TASK 27-81-21-400-801. COMPLETED LEADING EDGE #7 SLAT ADJUSTMENT REF AMM 27-81-00-820-803. FINISHED INSTALLATION AND RIG REF AMM 27-81-00. OK FOR SERVICE. COMPLETED RII OF #7 SLAT INSTALLATION.

Part: STRUCTURE — CORRODED (AFT CARGO DOOR) · airframe 58,533 hrs · 30,855 cycles

AFT CARGO DOOR, CORROSION ON LOWER AFT INSIDE CORNER NEXT TO INSULATION BUTTON. SEE SRM 52-30-01/1A01 FOR LIMITS. METAL THICKNESS .071 MATERIAL 7075T6. REMOVED CORROSION AT 2 LOCATIONS WITH CUTOUTS AT LOWER AFT CORNER AND LOWER INNER SKIN FWD OF AFT STOP FITTING. DIMENSIONS SUBMITTED TO ENGINEERING FOR DISPOSITION. HFEC OF CUTOUTS ACCOMPLISHED BY NDI. NO CRACKS. TREATED AND PRIMED.PERFORMED 10X DETAILED VISUAL INSPECTION.NO DAMAGE OR CORROSION NOTED.INSTALLED INSULATION BLANKET. IAW SRM 51-20-01. REPAIRED AFT CARGO DOOR INNER SKIN CORROSION PER EA 52-0007.

Part: STRUCTURE — WORN (NR 1 SLAT) · airframe 58,533 hrs · 30,855 cycles

#1 SLAT UNDER TRAILING EDGE HAS WORN ANTI ABRASION PAINT NUMEROUS SPOTS. OUTBOARD TRAILING EDGE WEAR IS BEYOND ALLOWABLE LIMIT AND WILL REQUIRE REPAIR PER SRM 57-42-01-2R-6 REPAIR 6. REPAIRED REF SRM 57-42-01-2R-6

Part: SPAR — CRACKED · airframe 58,533 hrs · 30,855 cycles

11" CRACK ON WING CENTER SECTION REAR SPAR BETWEEN 45.64 AND 31.83 STIFFENERS. COMPLETED INTERIM REPAIR IAW SRM 57-10-10-2R-2 PARAGRAPH 6. ITEM WILL BE PLACED ON GMM/MTI FOR TRACKING PURPOSES FOR A DETAILED VISUAL INSPECTION EVERY 3,000 FLIGHT CYCLES. IF ADDITIONAL DAMAGE IS FOUND DURING THE DETAILED VISUAL INSPECTION THE INTERIM REPAIR MUST BE REPLACED WITH A PERMANENT REPAIR AS GIVEN IN SRM 51-70-04, REPAIR 10.

Part: SKIN — DAMAGED (RT WING SLAT) · airframe 58,533 hrs · 30,855 cycles

RH LE SLAT #6 BARE METAL SHOWING ON UNDERSIDE ALONG AFT EDGE. FOUND TRAILING EDGE WEAR BEYOND SRM REPAIRABLE LIMITS PER SRM 57-42-01-2R-6 REPAIR 6. REMOVED #6 SLAT REF AMM 27-81-21. PERFORMED INTERFACE INSPECTION AND OK TO INSTALL NEW SLAT. INSTALLED NEW SLAT IAW AMM 27-81-21-400-801. COMPLETED LEADING EDGE #6 SLAT ADJUSTMENT REF AMM 27-81-00-820-803. FINISHED INSTALLATION WITH RIG, REF AMM 27-81-00. OK FOR SERVICE. COMPLETED RII OF #6 SLAT INSTALLATION.

Part: FASTENER — LOOSE (LT WING LE) · airframe 58,533 hrs · 30,855 cycles

LEFT WING, UPPER L/E 16 LOOSE FASTNERS FROM THE PYLON INBD. ALONG THE AFT SIDE OF PANEL. REMOVED 16 EA LOOSE FASTENERS ON L/H WING UPPER SKIN JUST INBD OF # 1 PYLON. REAMED HOLES TO 1ST OVER 3/16. .199" OPEN HOLE AND COUNTER SINK HFEC ACCOMPLISHED BY NDI. NO CRACKS. PREPPED FASTENER HOLES AND INSTALLED REPLACEMENT FASTENERS. REF SRM 57-41-01-2R-7.

Part: SUPPORT — DAMAGED (RT MLG) · airframe 57,738 hrs · 30,521 cycles

RIGHT MLG SIDE STAY IS RUBBING INTO THE LOWER BEAM SUPPORT AND INTO THE THIRD ROD END SUPPORT MOUNT. REF TASK CARD FOR FIXED T/E PANEL WEAR. REMOVED AND REPLACED ROD SUPPORT AND RECONNECTED ROD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,862 hrs · 30,121 cycles

FWD WINDSCREEN EMERGENCY PATH LIGHT INOP. R+R'D FORWARD L/A PWR SUPPLY BATTERY. OPS CHECK OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,689 hrs · 29,598 cycles

EMERGENCY EXIT LIGHT L2, OVERHEAD INOP. R&R BATTERY L2 DOOR AND OVERHEAD EXIT LIGHT. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,559 hrs · 29,508 cycles

RT AFT EXTERIOR EMG LIGHT AND INTERER EXIT LIGHT INOP. R/R BATTERY PACK. OPS CHK GOOD.

Part: STRUCTURE — CRACKED (LT NR 2 SLAT) · airframe 54,495 hrs · 29,069 cycles

FOUND A CRACK ON THE NR 2 LT LE SLAT. LENGTH OF CRACK IS 1.125 INCH. THE CRACK IS ACCEPTABLE TO FLY FOR 50FC. REMOVED AND REPLACED THE NR 2 LT L/E SLAT. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,301 hrs · 28,915 cycles

9ABC EMERGENCY LIGHT INOP. PLACED 9ABC EMERGENCY AISLE LIGHT ON MEL. R&R THE INOP EMER LIGHT BULB AT 9ABC. OP CHECK GOOD. THIS CLEARS MEL.

Part: PUMP — FAILED (HYD SYSTEM)

LOST OF HYDRAULIC SYSTEM "B" INFLIGHT. POP OUT CIRCUIT BREAKERS ENGINE 2 PUMP DEPRESS VALVE 1 AND SYST "B" STANDBY RUDDER. (QRF RETURN TO AIRPORT). CORRECTIVE ACTION:HAS BEEN CHANGED EDP SYST "B" ENGINE 2 AND CHANGED FILTER SYSTEM B.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,379 hrs · 28,077 cycles

FUSELAGE DENT LOCATED NEAR LAV SERVICE DOOR. REMOVED DENT DAMAGE AT LAV SERVICE DOOR STA 834 BELOW STR 22L AND REPAIRED.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 49,442 hrs · 26,902 cycles

FORWARD CABIN FLOOR PANEL 141A5810-56 HAS CORNER BROKEN OFF. REPAIRED THE FLOOR PANEL.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 49,442 hrs · 26,902 cycles

BS 986 FLOORBEAM CORRODED ON UPPER SURFACE UPPER FLANGE PREVIOUS REPAIR BL 0 TO LBL 45. REMOVED CORROSION IAW EA.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 49,442 hrs · 26,902 cycles

FWD CABIN FLOOR PANEL 141A5810-185 HAS EDGE DAMAGE. REPAIRED FWD CABIN FLOOR PANEL.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · airframe 49,442 hrs · 26,902 cycles

FLOOR SUPPORT CORRODED LBL 20 UPPER FLANGE AFT HOLE BS 967 TO 947. REMOVED CORROSION, ORIGINAL T= .090, AFTER BLENDING T=.059, .031 MATERIAL LOSS OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 49,442 hrs · 26,902 cycles

FORWARD CABIN FLOOR PANEL 141A5810-245 HAS SEVERAL CORRODED INSERTS. REPLACED THE INSERTS.

Part: CREASE BEAM — CORRODED (BS 947-986) · airframe 49,442 hrs · 26,902 cycles

CREASE BEAM CORRODED IN SEVERAL PLACES FROM BS 947.5 TO 986.5. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMIT. INSTALLED A NEW CREASE BEAM.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 49,442 hrs · 26,902 cycles

INTERCOSTAL AT RBL 32 STA 312 TO 328 IS CRACKED ON UPPER FLANGE AT FWD HOLE INTO THE RADIUS. REMOVED AND REPLACED INTERCOSTAL AT RBL 32 STA. 312 TO 328.

Part: FLOORBOARD — CORRODED (BS 966) · airframe 49,442 hrs · 26,902 cycles

FLOORBOARD IS CORODED AT RBL 16, BS 966.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 49,442 hrs · 26,902 cycles

FORWARD CABIN FLOOR PANEL 141A5810-185 HAS SEVERAL MISSING AND CORRODED INSERTS. REPAIRED FORWARD CABIN FLOOR PANEL 141A5810-185.

Part: INTERCOSTAL — CRACKED (BS 328-312) · airframe 49,442 hrs · 26,902 cycles

INTERCOSTAL AT STA 328 TO 312 AT RBL16 IS CRACKED AT AFT HOLE ON UPPER FLANGE. REMOVED AND REPLACED INTERCOSTAL AT STA 312 TO 328 RBL 16.

Part: FLOORBEAM — DAMAGED (BS 312) · airframe 49,442 hrs · 26,902 cycles

FLOORBEAM BS 312 UPPER FLANGE HAS SCRIBE LINES AND CORROSION FROM LBL 5 TO 52. REPAIRED THE FLOORBEAM.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 49,442 hrs · 26,902 cycles

FORWARD CABIN FLOOR PANEL 141A5810-464 HAS SEVERAL MISSING AND CORRODED INSERTS. REPAIRED THE CABIN FLOOR PANEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,442 hrs · 26,902 cycles

AFT EMERGENCY LIGHT IN HORSESHOE PANEL INOPERATIVE. REMOVED AND REPLACED AFT AISLE EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: NUT PLATE — MISSING (BS 927-947) · airframe 49,442 hrs · 26,902 cycles

BL 0 INTERCOSTAL MISSING ONE NUTPLATE BS 927 TO 947. INSTALLED A NEW NUT PLATE.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 49,442 hrs · 26,902 cycles

BS 986 FLOORBEAM CORRODED ON UPPER SURFACE UPPER FLANGE PREVIOUS REPAIR BL 0 TO RBL 45. REMOVED CORROSION IAW EA.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 49,442 hrs · 26,902 cycles

FORWARD CABIN FLOOR PANEL 141A5810-484 HAS TWO AREAS WHERE THE UPPER LAYER OF FIBERGLASS IS MISSING. REPAIRED THE FLOOR PANEL.

Part: FLOORBEAM — CORRODED (BS 966) · airframe 49,442 hrs · 26,902 cycles

BS 966 FLOORBEAM CORRODED AT RBL 27. REPAIRED THE FLOORBEAM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 49,442 hrs · 26,902 cycles

L1 WINDOW FRAME HAS A CRACK INDICATION ON UPPER LEFT HAND CORNER. END OF CRACK INDICATION MARKED IN BLACK. RESTORED L/H #1 WINDOW FRAME CRACK ON UPPER LEFT HAND CORNER. OPS AND LEAK CHECK GOOD.

Part: STRAP — CORRODED (FUSELAGE) · airframe 49,442 hrs · 26,902 cycles

RIGHT HAND CREASE BEAM STRAP CORRODED AT STA 291. REMOVED & REPLACED RT CREASE BEAM STRAP STA 277 TO 312.

Part: CREASE BEAM — CORRODED (R1 DOOR) · airframe 49,442 hrs · 26,902 cycles

R1 DOOR CREASE BEAM IS CORRODED RBL 60 STA 320 TO 358. REMOVED AND REPLACED R1 DOOR CREASE BEAM.

Part: SKIN — WORN (PNEUMATIC DOOR) · airframe 49,442 hrs · 26,902 cycles

RT A/C BAY, GROUND PNEUMATIC DOOR INNER SURFACE HAS AREAS OF WEAR AND MISSING PAINT. BLENDED DAMAGE ON GROUND PNEUMATIC DOOR, ORIGINAL T=.100 AFTER BLENDING T=.075, .025 MATERIAL LOSS, OUT OF LIMITS. FABRICATED NEW DOOR AND INSTALLED.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 49,442 hrs · 26,902 cycles

R1 WINDOW FRAME, UPPER O/B CORNER AT MOST UPPER I/B ATTACH FASTENER HOLE TO #2 WINDOW FRAME, CRACK INDICATION IN HOLE, HOLE MARKED IN BLACK. REMOVED DAMAGE TO R/H FLIGHT DECK #1 WINDOW FRAME AND REPAIRED.

Part: WINDOW — CRACKED (R1) · airframe 49,442 hrs · 26,902 cycles

R1 WINDOW HAS A CRACK INDICATION ON UPPER RIGHT HAND CORNER. END OF CRACK INDICATION MARKED IN BLACK ON FLIGHT DECK SIDE. RESTORED R/H #1 WINDOW FRAME CRACK ON UPPER R/H CORNER. OPS AND LEAK CHECK GOOD.

Part: BRACKET — CRACKED (BS 1016) · airframe 49,442 hrs · 26,902 cycles

PULLEY BRACKET AFT OF BS 1016 FOR THE LEFT HORIZONTAL STAB CABLE "STA", FAIRLEAD ON PULLEY BRACKET IS CRACKED. REMOVED CRACKED FAIRLEAD AFT OF STA 1016 FOR LH HORIZONTAL STAB CABLE & REPLACED WITH NEW.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 49,442 hrs · 26,902 cycles

L1 WINDOW FRAME, UPPER O/B CORNER AT MOST UPPER I/B ATTACH FASTENER HOLE TO #2 WINDOW FRAME, CRACK INDICATION IN HOLE, HOLE MARKED IN BLACK. REPAIRED L/H FLIGHT DECK #1 WINDOW FRAME UPPER O/B CORNER.

Part: SUPPORT — CORRODED (BS 320) · airframe 49,442 hrs · 26,902 cycles

R1 DOOR THRESHOLD SUPPORT ATTACH TO CREASE BEAM IS CORRODED AT STA. 320 RBL 61. REMOVED CORROSION FROM R1 DOOR THRESHOLD SUPPORT ATTACH ANGLE ORIG. "T" 0.090 REMOVED 0.022 REMAINING "T" 0.068 OUT OF LIMITS. SUPPORT ANGLE WAS INSTALLED AS PART OF THE CREASE BEAM ASSY INSTALLATION. REMOVED AND REINSTALLED R1 DOOR THRESHOLD.

Part: SKIN — DELAMINATED (RT WING LE) · airframe 49,442 hrs · 26,902 cycles

RT WING LEADING EDGE PANEL 621CB DELAMINATED ON LEADING EDGE. REPAIRED RH WING LEADING EDGE PANEL 621CB.

Part: SKIN — DAMAGED (RT WING LE) · airframe 49,442 hrs · 26,902 cycles

RIGHT WING LEADING EDGE PANEL 621DB DELAMINATED ON LEADING EDGE. REPAIRED RH WING LEADING EDGE PANEL 621DB.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,442 hrs · 26,902 cycles

FLOOR SUPPORT AT STA 309.9 RBL 5 CORRODED AFT OF GALLEY MOUNT. REMOVED FLOOR SUPPORT AT STA - 294.5 RBL 5. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT.

Part: BEAM — LOOSE (TE FLAP) · airframe 49,442 hrs · 26,902 cycles

NR 6 FLAP FAIRING LOOSE AT AFT CENTER ATTACHMENT. REMOVED & REPLACED NR 6 FLAP FAIRING AFT ATTACH BEAM ASSY.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 49,442 hrs · 26,902 cycles

AFT CABIN FLOOR PANEL HAS SEVERAL MISSING AND CORRODED INSERTS. REPLACED THE INSERTS.

Part: SKIN — DAMAGED (LT WING AILERON) · airframe 49,442 hrs · 26,902 cycles

LEFT WING AILERON UPPER SURFACE HAS SEVERAL AREAS OF EXPOSED COMPOSITE. REPAIRED THE LEFT WING AILERON UPPER SURFACE.

Part: FLOOR PANEL — CORRODED (AFT CABIN) · airframe 49,442 hrs · 26,902 cycles

AFT CABIN FLOOR PANEL HAS SEVERAL MISSING AND CORRODED INSERTS. REPLACED THE INSERTS TO FLOOR PANEL.

Part: FLOOR PANEL — CORRODED (AFT CABIN) · airframe 49,442 hrs · 26,902 cycles

AFT CABIN FLOOR PANEL HAS SEVERAL MISSING AND CORRODED INSERTS. REPLACED MISSING AND CORRODED INSERTS ON PANEL 147A5810-61.

Part: NOSE COWL — DAMAGED (NR 2) · airframe 49,442 hrs · 26,902 cycles

RT WING NR 2 ENGINE NOSE COWL, THUMBNAIL MATTING SURFACE HAS LIGHT WEAR AND MISSING PAINT. AREAS FROM 10 TO 2 O`CLOCK MARKED. REPAIRED NR 2 RIGHT WING ENGINE NOSE COWL.

Part: PANEL — LOOSE (RT WING) · airframe 49,442 hrs · 26,902 cycles

RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL IS LOOSE. FOUND HOLES TO BE ELONGATED ON UPPER SUPPORT BEAM AT RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL, CUT OUT DAMAGE AND ACCOMPLISHED REPAIR.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 49,442 hrs · 26,902 cycles

LEFT OUTBOARD AFT FLAP, INBOARD TRAILING EDGE CORNER HAS A SMALL AREA OF DELAMINATION. REPAIRED LEFT OUTBOARD AFT FLAP INBOARD TRAILING EDGE CORNER.

Part: TRUNNION — LOOSE (MLG) · airframe 49,442 hrs · 26,902 cycles

LEFT WING MAIN LANDING GEAR, FWD TRUNION RETENTION NUTS SEALENT DISBONDED OR MISSING 4 EA. NUTS. APPLIED FILLET SEAL TO SPECIAL WASHERS NUTS ON LH WINGS MLG, FWD TRUNION RETENTION NUTS.

Part: PANEL — LOOSE (LT WING) · airframe 49,442 hrs · 26,902 cycles

LEFT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL IS LOOSE. REMOVED 2 EACH RETAINERS ON LEFT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL. INSTALLED SERRATED PLATE AND REINSTALLED 2EACH RETAINERS.

Part: SKIN — DENTED (BS 1078) · airframe 48,628 hrs · 26,559 cycles

DENT IN SKIN AT BS 1078 BETWEEN STR 24L AND 25L. REMOVED DENT, WILL REQUIRE REPAIR. CUT OUT DAMAGE. FABRICATED REPAIR DOUBLER FROM .071" 2024-T3 AND DRILLED AS REQUIRED. PRIMED REPAIR DOUBLER AND SKIN IN REPAIR AREA AND INSTALLED FILLER WASHERS AT INITIAL FASTENER LOCATIONS . REPAIR IS READY TO INSTALL. INSTALLED DOUBLER. PRIMED AND PAINTED. JOB COMPLETE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 47,934 hrs · 26,294 cycles

FORWARD LT WINDSCREEN EMERGENCY LIGHT LENS COVER MISSING. INSTALLED LIGHT LENS COVER FWD LT WINDSCREEN.

Part: SKIN — DAMAGED (LT WING) · airframe 47,934 hrs · 26,294 cycles

ON WALK AROUND, FOUND PANEL 571FB ON LT WING LOWER SURFACE, HAVE ALUMINUM FOIL MESH PEELING. PERFORMED REPAIR ON PANEL 571FB IAW SRM. OK FOR SERVICE.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 43,938 hrs · 24,560 cycles

L1 DOOR EXIT SIGN DETACHED. REPLACED SIGN LENS.

Part: PANEL — CORRODED (NACELLE) · airframe 40,841 hrs · 23,306 cycles

PANEL 441DR UNDER SIDE HAS MULTIPLE AREAS WITH SURFACE CORROSION. REPAIRED PANEL 441DR.

Part: THRESHOLD — CRACKED (AFT CARGO) · airframe 40,841 hrs · 23,306 cycles

AFT CARGO THRESHOLD AFT CORNER HAS A ONE INCH CRACK. WELDED PERMANENT REPAIR OF CRACK.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 40,841 hrs · 23,306 cycles

CABIN FLOORBEAM, BS 986 HAS MULTIPLE CORROSION SPOTS UPPER FLANGE. UPPER FLANGE R & R.

Part: THRESHOLD — CRACKED (AFT CARGO BAY) · airframe 40,841 hrs · 23,306 cycles

AFT CARGO THRESHOLD FWD CORNER HAS ONE INCH CRACK. WELDED PERMANENT REPAIR TO AFT CARGO THRESHOLD FWD CORNER CRACK.

Part: ATTACH ANGLE — CORRODED (BS 727D) · airframe 40,841 hrs · 23,306 cycles

CARGO SIDEWALL ATTACH ANGLE AT FS 727D LT LOWER SIDE IN AFT CARGO IS CORRODED. REMOVED CORROSION FROM CARGO SIDEWALL ATTACH ANGLE. DAMAGE REMOVAL FOUND MATERIAL TO BE OUT OF LIMITS, REPAIRED.

Part: INTERCOSTAL — CORRODED (AFT CARGO) · airframe 40,841 hrs · 23,306 cycles

DURING GVI AFTER TRANSITION PANEL REMOVAL, FOUND CORROSION ON UPPER & LOWER SURFACE OF INTERCOSTAL IN AFT PIT BETWEEN STA 747-767 RT SIDE OTBD OF CARGO TIE DOWN TRACK. R & R INTERCOSTAL IN AFT PIT BETWEEN FS 747 AND FS 767 RT.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,841 hrs · 23,306 cycles

AFT WET AREA FLOOR PANEL "I" HAS PEELING FIBERS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,841 hrs · 23,306 cycles

FWD WET AREA FLOOR PANEL "B" HAS PEELING FIBERS AND CORRODED INSERTS. REPAIRED FLOOR PANEL B.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 40,841 hrs · 23,306 cycles

AFT CARGO CENTER FLOOR PANEL SPLICE STRIP IS CORRODED. BLENDED CORROSION ON AFT CARGO CENTER FLOOR SPLICE STRIP FOUND TO BE OUT OF LIMITS. NEW SPLICE FABRICATED.

Part: BULKHEAD — CORRODED (BS 500D) · airframe 40,841 hrs · 23,306 cycles

FORWARD CARGO COMPARTMENT, AFT BULKHEAD, STA 500D, L27L, LOWER ANGLE SUPPORT FOR BULKHEAD PANEL, ANGLE HAS CORROSION AREAS. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED REPLACEMENT ANGLE. INSTALLED REPLACEMENT SUPPORT ANGLE.

Part: FLOOR PANEL — CRACKED · airframe 40,841 hrs · 23,306 cycles

FLOOR PANEL ASSY AFT SECTION HAS CRACK. REPAIRED FLOOR PANEL.

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 40,841 hrs · 23,306 cycles

NUTPLATE SUPPORT ASSY AT FS 887 IN AFT CARGO FLOOR HAS CORROSION. BLENDED NUTPLATE SUPPORT ASSY STRIP FOUND TO BE OUT OF LIMITS. NEW NUTPLATE SUPPORT ASSY FABRICATED. R & R ASSY.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 40,841 hrs · 23,306 cycles

AFT CARGO NR 3 CENTER FLOOR PANEL & SPLICE STRIP HAVE LIGHT CORROSION ON UPPER AND LOWER SURFACES. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. NEW PANEL FABRICATED.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 40,841 hrs · 23,306 cycles

AFT CARGO NR 2 CENTER FLOOR PANEL HAS LIGHT CORROSION ON UPPER AND LOWER SURFACES. PANEL FOUND TO BE OUT OF LIMITS. CENTER NR 2 FLOOR PANEL WAS FABRICATED IN AFT CARGO BAY.

Part: TRANSITION PANEL — CORRODED (AFT CARGO BAY) · airframe 40,841 hrs · 23,306 cycles

RIGHT TRANSITION PANEL IN THE AFT CARGO BETWEEN 727E AND FS 747 HAS CORROSION. R & R RT TRANSITION PANEL.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 40,841 hrs · 23,306 cycles

AFT CARGO NR 3 CENTER FLOOR PANEL FWD SMALL PLATE HAS CORROSION ON LWR SURFACE. BLENDED AND FOUND TO BE OUT OF LIMITS. NEW PLATE FABRICATED.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 40,841 hrs · 23,306 cycles

AFT CARGO NR 1 CENTER FLOOR PANEL HAS LIGHT CORROSION ON UPPER AND LOWER SURFACES. REMOVED CORROSION & BLENDED. FOUND TO BE OUT OF LIMITS. FABRICATED NEW FLOOR PANEL.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 40,841 hrs · 23,306 cycles

AFT CARGO NR 2 FLOOR SUPPORT HAS LIGHT CORROSION ON LOWER SURFACE. STRIP FOUND TO BE OUT OF LIMITS. FABRICATED NEW FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 40,841 hrs · 23,306 cycles

AFT CARGO NR 2 FLOOR SUPPORT HAS LIGHT CORROSION ON LWR SURFACE. BLENDED & FOUND TO BE OUT OF LIMITS. NEW FLOOR SUPPORT FABRICATED.

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 40,841 hrs · 23,306 cycles

RBL 13.84 FROM BS 794.3 TO 847 IN AFT CARGO BAY HAS SEVERAL AREAS OF CORROSION. REMOVED CORRODED CARGO TRACK. INSTALLED NEW CARGO TRACK.

Part: SKIN — GOUGED (FUSELAGE) · airframe 40,841 hrs · 23,306 cycles

SKIN ON INSIDE OF AFT CARGO DOOR CUTOUT LOWER AFT CORNER IS GOUGED. REPAIRED AFT CARGO DOOR CUTOUT LOWER AFT CORNER.

Part: SKIN — GOUGED (FUELAGE) · airframe 40,841 hrs · 23,306 cycles

SKIN ON LOWER FORWARD INSIDE OF AFT CARGO DOOR CUTOUT IS GOUGED. REPAIRED AFT CARGO INNER SKIN LOWER FORWARD SIDE.

Part: INTERCOSTAL — CORRODED (AFT CARGO) · airframe 40,841 hrs · 23,306 cycles

INTERCOSTAL ON RT SIDE OF AFT CARGO FLOOR FROM FS 867 TO FS 887 HAS CORROSION. INTERCOSTAL ON RT SIDE OF AFT CARGO FROM FS 867 TO FS 887 OUT OF LIMITS. R & R INTERCOSTAL TRANSITION PANEL.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 40,841 hrs · 23,306 cycles

PASSENGER COMPARTMENT AFT WET AREA FWD OF L2 DOOR FLOOR SUPPORT STRUCTURE CORRODED. R & R FLOOR SUPPORT.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 40,841 hrs · 23,306 cycles

RIGHT OTBD AFT FLAP LOWER SKIN CHAFED OVER OTBD EDGE OF CANOE. REPAIRED RT OTBD AFT FLAP LWR SKIN OVER OTBD EDGE OF CANOE FAIRING.

Part: CHANNEL — CORRODED (PAX CABIN) · airframe 40,841 hrs · 23,306 cycles

PASSENGER COMPARTMENT AFT WET AREA LT SIDE MOP SILL FWD OF L2 DOOR CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. R & R MOP SEAL.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 40,841 hrs · 23,306 cycles

RIGHT OTBD AFT FLAP LOWER SKIN CHAFED OVER INBD EDGE OF CANOE. REPAIRED RT OTBD AFT FLAP LWR SKIN OVER INBD EDGE OF CANOE FAIRING.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 40,841 hrs · 23,306 cycles

PASSENGER COMPARTMENT AFT WET AREA RT SIDE FLOOR STRUCTURE AT STA 967 SEVERAL SPOTS AROUND NUT PLATE CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 40,841 hrs · 23,306 cycles

PASSENGER COMPARTMENT AFT WET AREA RT SIDE AFT OF R2 DOOR FLOOR SUPPORT STRUCTURE AT STA 986.5 POSITION CORRODED. REPAIRED CORROSION ON FLOOR SUPPORT STRUCTURE.

Part: SILL — CORRODED (FWD CARGO BAY) · airframe 40,841 hrs · 23,306 cycles

FORWARD CARGO BAY LOWER SILL CORRODED & CHAFED SEVERAL PLACES. REMOVED CORROSION FROM SILL AND FOUND TO BE OUT OF LIMITS. REPLACED FWD PIT LOWER SILL.

Part: WINDOW FRAME — CRACKED · airframe 40,841 hrs · 23,306 cycles

LEFT NR 3 WINDOW FRAME HAS TWO CRACK INDICATIONS IN SECOND LOWER CORNER FASTENER HOLE. COMPLIED WITH NR 3 LEFT WINDOW FRAME REPAIR.

Part: WINDOW FRAME — CRACKED · airframe 40,841 hrs · 23,306 cycles

RIGHT NR 3 WINDOW FRAME HAS TWO CRACK INDICATIONS IN SECOND LWR CORNER FASTENER HOLE. COMPLIED WITH NR 3 RT WINDOW FRAME REPAIR.

Part: SENSOR — FAILED (SLATS) · airframe 38,863 hrs · 22,487 cycles

SELECTING FLAPS 1 AND FLAPS 5, NO L/E DEVICES EXTENDED NOR TRAILING FLAPS EXTENDED. PERFORMED NNC AND EXTENDED LEDS USING ALT FLAPS MASTER SWITCH. LANDED WITH NORMAL FLIGHT LOADS. CONFIRMED PROBLEM TO INTERMITTENT SKEW SENSOR NR 1. REPLACED SKEW SENSOR NR 1.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 38,626 hrs · 22,393 cycles

LEFT HORIZONTAL STAB LWR SKIN HAS 1.5" CRACK AT STAB STA 129.5 LOCATED 17" AFT OF FWD SPAR. CRACK ENDS MARKED BY HFEC. REMOVED L/E OF LEFT STAB. CUTOUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER. INSTALLED LEFT STAB L/E.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 38,626 hrs · 22,393 cycles

RIGHT HORIZONTAL STAB LWR SKIN HAS 1" CRACK 8.5" AFT OF FWD SPAR AND 1" CRACK 17" AFT OF FWD SPAR AT STAB STA 129.5. REMOVED RIGHT L/E OF HORIZONTAL STAB CRACK ENDS MARKED BY HFEC. REMOVED SEALANT FROM L/E FAYING SURFACE. REMOVED DAMAGE AND INSTALLED DOUBLER.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 37,324 hrs · 21,875 cycles

ROW 1 O2 MASKS FELL DOWN ON DEPARTURE ON RUNWAY. RE-PACKED & RE-SECURED ROW 1 DF PSU O2 MASKS. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,277 hrs · 19,736 cycles

OPS CHECK OF EMERGENCY LIGHTS REVEALS AFT RIGHT CABIN LIGHTS INOP. REMOVED AND REPLACED AFT RIGHT EMERGENCY LIGHT BATTERY PACK M1 672 REF AMM 33-51-06. OPS CHECKS GOOD.

Part: ACTUATOR VALVE — FAULTY (FUEL SYSTEM) · airframe 31,906 hrs · 19,557 cycles

UNCONTROLLED FUEL IMBALANCE. FOUND P6-3 B-7 C/B POPPED (FUEL CROSS FEED). REMOVED, INSTALLED & TESTED ENG. FUEL CROSSFEED VALVE ACTUATOR IAW AMM 28-22-21. OPS CHECK GOOD. OK FOR SERVICE.

Part: LIGHT — FAILED (CABIN) · airframe 29,662 hrs · 18,757 cycles

DURING ACCOMPLISHMENT OF TASK CARD 330550000 EMERGENCY FLOOR PATH LIGHTS AT EMERGENCY EXIT FAILED CAP CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,662 hrs · 18,757 cycles

DURING ACCOMPLISHMENT OF TASK CARD 330550000 EMERGENCY FLOOR PATH LIGHTS AT ROW 3/4 FAILED CAP CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,250 hrs · 17,206 cycles

DURING A FUNCTIONAL CHECK, MAINTENANCE DISCOVERED EMERGENCY TRACK LIGHT COVER MISSING & LIGHT INOPERATIVE IN ROW 8. MAINTENANCE REPLACED MISSING COVER, REMOVED & REPLACED LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,619 hrs · 16,956 cycles

DURING A FUNCTIONAL CK, MX DISCOVERED THAT THE EMERGENCY FLOOR PATH LIGHTING AT SEAT ROW 1C WAS INOP. MX RELAMPED THE FLOOR PATH LIGHT AT SEAT ROW 1C AND THE LIGHT FUNCTIONS NORMAL.