N716SY

Part: SENSOR — MALFUNCTIONED (TE FLAP) · airframe 48,538 hrs · 24,769 cycles

ON TOP OF CLIMB NOTICED THE LEFT FLAP INDICATOR SHOWED A FLAP ASYMMETRY. RIGHT FLAP AT 0, L FLAP BETWEEN 0 & 1 DEGREES. NO OTHER ABNORMAL INDICATIONS. FOLLOWED QRH PROCEDURE AND PERFORMED FLAPS UP LANDING. PERFORMED FIM TASK. REPLACED LEFT & RIGHT FLAP POSITION INDICATORS. REPLACED NR 2 SKEW SENSOR. PERFORMED PSEU BITE. NO FAULTS. FLAPS OPS CK GOOD. PERFORMED LAND VERIFY. LLM STATUS RESTORED.

Part: SKIN — WORN (TE FLAP) · airframe 46,065 hrs · 23,882 cycles

FOUND WEAR DAMAGE ON THE RIGHT WING OUTBOARD TRAILING EDGE AFT FLAP SKIN JUST OUTBOARD OF THE NR 7 FLAP TRACK FAIRING DURING RIGHT WING INSPECTION. THE THICKNESS OF THE SURFACE SKIN IS COMPLETELY WORN THROUGH DOWN TO THE COMPOSITE CORE TOWARDS THE AFT PORTION OF THE TOTAL DAMAGE. THE TOTAL DAMAGE MEASURES 1.5 INCHES LONG AND 3/4 INCHES WIDE. REMOVED RT WING AFT FLAP. INSTALLED SERVICEABLE RT WING AFT FLAP. OPS CHECK GOOD.

Part: SWITCH — OUT OF ADJUST · airframe 41,996 hrs · 22,488 cycles

DURING DEPARTURE, GEAR LEVER UP GEAR WOULD NOT COME UP, 3 RED & 3 GREEN. REPEATERS 3 GREEN. PERFORMED PSEU BITE. NO FAULTS FOUND. FOUND MANUAL EXTENSION SYSTEM ACCESS DOOR SWITCH OUT OF ADJUSTMENT. REMOVED AND REPLACED DOOR SWITCH AND SWITCH ACTUATOR. PERFORMED LANDING GEAR OPERATIONAL TEST. LANDING GEAR EXTENSION/RETRACTION AND INDICATION OPS CHECKS GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 40,947 hrs · 22,096 cycles

EMERGENCY EXIT LENS AT SEAT 13F MISSING. REPLACED EMERGENCY EXIT LENS AT SEAT 13F.

Part: BRACKET — CRACKED (L2 DOOR) · airframe 40,826 hrs · 22,050 cycles

L2 DOOR PANEL 834DZ, SUPPORT BRACKET CRACKED. REMOVED AND REPLACED THE BRACKET.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 40,826 hrs · 22,050 cycles

FWD WET AREA FLOORBOARD HAS CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: FLOORBOARD — DAMAGED · airframe 40,826 hrs · 22,050 cycles

FWD WET AREA FLOORBOARD HAS A BROKEN EDGE. REPAIRED THE FLOORBOARD.

Part: FLOORBOARD — CORRODED · airframe 40,826 hrs · 22,050 cycles

AFT WET AREA FLOORBOARD HAS CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: FLOORBOARD — DAMAGED · airframe 40,826 hrs · 22,050 cycles

WET AREA FLOORBOARD HAS EVIDENCE OF WATER DAMAGE AND CORRODED INSERTS. REPAIRED THE FLOORBOARD.

Part: CREASE BEAM — CORRODED (BS 947-960) · airframe 40,826 hrs · 22,050 cycles

R2 DOOR CREASE BEAM FROM BS 947-960 HAS CORROSION. REMOVED CORROSION.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 40,826 hrs · 22,050 cycles

FWD WET AREA FLOORBOARD HAS CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 40,826 hrs · 22,050 cycles

FLIGHT DECK R1 WINDOW FRAME, O/B UPPER CORNER OF WINDOW PANE CUTOUT, CRACK IN FRAME ON INNER EDGE TO AFT FACE, .100 X .100. VERIFIED BY NDT INDP. REPAIRED IAW SB.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 40,826 hrs · 22,050 cycles

FWD WET AREA FLOORBOARD HAS CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: FLOORBOARD — CORRODED · airframe 40,826 hrs · 22,050 cycles

AFT WET AREA FLOORBOARD HAS CORRODED AND MISSING INSERTS. REMOVED THE DAMAGED INSERTS. REPLACED THE DAMAGED INSERTS AND THE MISSING INSERTS.

Part: FLOOR SUPPORT — CORRODED (BS 967-986) · airframe 40,826 hrs · 22,050 cycles

FLOOR SUPPORT BETWEEN BS 967 - 986.5 LBL 16 HAS CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT.

Part: SKIN — CRACKED (BS 540) · airframe 40,826 hrs · 22,050 cycles

DURING HFEC INSPECTION, FOUND A CRACK INDICATION IN THE SKIN JUST BELOW STRINGER 22L, BS 540 BULKHEAD UPPER FRAME. REMOVED DAMAGE, HFEC CUT-OUT & HOLE, NO OTHER DEFECT NOTED, FABRICATED DOUBLER, TRIPLER, AND FILLERS. TREATED AND PRIMED ALL REPAIR. INSTALLED DOUBLER, TRIPLER, AND FILLERS.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 40,826 hrs · 22,050 cycles

FWD WET AREA FLOORBOARD HAS CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: COVER — GOUGED (RT WING TE FLAP) · airframe 40,826 hrs · 22,050 cycles

RIGHT WING INBOARD FLAP, HAS A DEEP GOUGE. REPAIRED RT I/B FLAP SLAT FAIRING. REMOVED AND INSTALLED RT COVER PLATE PANEL.

Part: FLOORBOARD — DAMAGED · airframe 40,826 hrs · 22,050 cycles

AFT WET AREA FLOORBOARD HAS EVIDENCE OF WATER DAMAGE AND CORRODED INSERTS. REPAIRED THE FLOORBOARD.

Part: FLOORBOARD — DAMAGED · airframe 40,826 hrs · 22,050 cycles

AFT WET AREA FLOORBOARD HAS EVIDENCE OF WATER DAMAGE AND CORRODED INSERTS. REPAIRED THE FLOORBOARD

Part: INSERT — CORRODED (FLOORBOARD) · airframe 40,826 hrs · 22,050 cycles

FWD WET AREA FLOORBOARD HAS CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 40,826 hrs · 22,050 cycles

FWD WET AREA FLOORBOARD HAS CORRODED INSERTS. REPAIRED THE FLOORBOARD.

Part: FLOOR SUPPORT — DAMAGED (BS 294-312) · airframe 40,826 hrs · 22,050 cycles

FLOOR SUPPORT BETWEEN BS 294.5 - 312, LBL 11 HAS A SCRIBE LINE. REPLACED THE FLOOR SUPPORT.

Part: BRACKET — CRACKED (R2 DOOR SEAL) · airframe 40,826 hrs · 22,050 cycles

R2 DOOR AFT SWEEPER SEAL BRACKET IS CRACKED. REMOVED AND REPLACED SEAL BRACKET.

Part: FLOOR SUPPORT — CORRODED (BS 727D) · airframe 40,826 hrs · 22,050 cycles

AFT CARGO FLOOR PANEL SPLICE AT BS 727D IS CORRODED IN SEVERAL AREAS. BLENDED CORROSION ON FLOOR PANEL TEE SPLICE. VERIFIED 100% MATERIAL LOSS AND FOUND TO BE OUT OF LIMITS.

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 40,826 hrs · 22,050 cycles

LEFT INBOARD AFT FLAP IS PUNCTURED 29 INCHES INBOARD FROM THE OUTBOARD EDGE AND 4 INCHES FORWARD OF THE TRAILING EDGE. REPAIRED LT WING FLAP.

Part: SKIN — WORN (WING) · airframe 40,826 hrs · 22,050 cycles

WING PANEL 651EB HAS WEAR MARKS. REPAIRED THE PANEL.

Part: MOUNT — CORRODED (GALLEY) · airframe 40,826 hrs · 22,050 cycles

BOTH CENTER DIVIDERS ON G4 GALLEY FLOOR MOUNTS ARE CORRODED. REMOVED AND REPLACED FLOOR MOUNTS FOR BOTH CENTER DIVIDERS, ON G4 GALLEY.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 40,826 hrs · 22,050 cycles

FWD WET AREA FLOORBOARD HAS CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: FLOOR SUPPORT — DAMAGED (BS 967-986) · airframe 40,826 hrs · 22,050 cycles

FLOOR SUPPORT BETWEEN BS 967 - 986.5, RBL 16 HAS A SCRIBE LINE. REMOVED DAMAGE. FOUND OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 40,826 hrs · 22,050 cycles

FWD WET AREA FLOORBOARD HAS CORRODED INSERTS. REPAIRED THE FLOORBOARD.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 40,826 hrs · 22,050 cycles

AFT CARGO FLOOR PANEL 140CF HAS CORROSION AT FWD ENTRY SIDE. BLENDED CORROSION. VERIFIED DAMAGE EXCEEDS 3 ICHES IN LENGTH AND FOUND TO BE OUT OF LIMITS. FABRICATED NEW FLOOR PANEL.

Part: DOOR — CRACKED (NR 2 NACELLE) · airframe 40,826 hrs · 22,050 cycles

NR 2 OUTBOARD FAN COWL, STRUCTURE AFT OF OIL SERVICE DOOR IS CRACKED IN RADIUS. REMOVED AND REPLACED STRUCTURE AFT OF NR 2 ENGINE OIL SERVICE DOOR

Part: FLOORBOARD — CORRODED · airframe 40,826 hrs · 22,050 cycles

AFT WET AREA FLOORBOARD HAS CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: SCUFF PLATE — CORRODED (AFT CARGO BAY) · airframe 40,826 hrs · 22,050 cycles

AFT CARGO BAY FWD ENTRY SCUFF PLATE IS CORRODED. REMOVED COROSION .

Part: ANGLE — DENTED (BS 500A) · airframe 40,826 hrs · 22,050 cycles

RIGHT ZEE ANGLE AT BS 500A+16 HAS A DENT. REMOVED & REPLACED THE ANGLE.

Part: INSERT — MISSING (FLOORBOARD) · airframe 40,826 hrs · 22,050 cycles

AFT WET AREA FLOORBOARD HAS PULLED AND MISSING INSERTS. REPLACED THE INSERT.

Part: WINDOW FRAME — CRACKED · airframe 38,277 hrs · 21,163 cycles

NR 1 WINDOW POST CRACK. PERFORMED PERMANENT REPAIR TO NR 1 WINDOW POST.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 36,007 hrs · 20,278 cycles

EMERGENCY LIGHTS ON ROWS 6-8-9 FAIL CAPACITY TEST. R & R BATTERY PACK ON PWR SUPPLY MODULE. OPS CKS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,803 hrs · 19,861 cycles

LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, CHARGER AND BATTERY PACK.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 35,503 hrs · 18,234 cycles

RIGHT HORIZONTAL STABILIZER, RIB NR 7 HAS 3 CRACKS. REPAIRED.

Part: FRAME — CORRODED (BS 986) · airframe 35,503 hrs · 18,234 cycles

FRAME BS 986 RBL 6 ON UPPER SURFACE CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED FRAME.

Part: CARGO TRACK — CRACKED (BS 727E) · airframe 35,503 hrs · 18,234 cycles

AFT CARGO BAY, CARGO TRACK CRACKED AT BS 727E. REMOVED DAMAGED CARGO TRACK BS 727 - 887 AND INSTALLED NEW.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 35,503 hrs · 18,234 cycles

GALLEY WALL SUPPORT Z-ANGLE BETWEEN THE LT AFT GALLEY MOUNTS CORRODED AT AFT END. REMOVED CORROSION AND REMAINING THICKNESS IS OUT OF LIMITS. R & R WALL SUPPORT.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 35,503 hrs · 18,234 cycles

GALLEY WALL SUPPORT Z-ANGLE BETWEEN THE RT AFT GALLEY MOUNTS CORRODED AT BOTH ENDS. REMOVED CORROSION AND REMAINING THICKNESS IS OUT OF LIMITS. R & R WALL SUPPORT.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 34,588 hrs · 19,774 cycles

LEFT HORIZONTAL STABILIZER RIB NR 1 IS CRACKED ON FWD OTBD END. R & R LT STAB RIB NR 1.

Part: WINDOW FRAME — CRACKED (NR 3) · airframe 35,503 hrs · 18,234 cycles

LEFT NR 3 WINDOW FRAME CRACKED. REPAIRED WITH DOUBLER & TRIPLER.

Part: SUPPORT ANGLE — CORRODED (BS 747-767) · airframe 34,588 hrs · 19,774 cycles

AFT CARGO BAY LEFT TRANSITION ZEE ANGLE IS CORRODED FROM BS 747 - 767. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS, REPAIRED.

Part: STRAP — CORRODED (BS 294) · airframe 35,503 hrs · 18,234 cycles

FWD WET AREA MOP SILL VERTICAL LEG SPLICE STRAP IS CORRODED. CORROSION BEYOND LIMITS. INSTALLED NEW SPLICE STRAP.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 34,588 hrs · 19,774 cycles

FLOOR SUPPORT CRACKED AT FORWARD WET AREA BETWEEN BS 312 & 328, LBL 46. R & R FLOOR SUPPORT.

Part: LIGHT — BROKEN (GALLEY) · airframe 35,503 hrs · 18,234 cycles

G-1 GALLEY EMERGENCY EXIT LIGHT BROKEN. R & R G1 GALLEY EMERGENCY EXIT LIGHT.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 35,503 hrs · 18,234 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 - 328, RBL 32. R & R THE FLOOR SUPPORT.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 35,503 hrs · 18,234 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 - 294.5, BL 0. R & R THE FLOOR SUPPORT.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 35,503 hrs · 18,234 cycles

FLOOR SUPPORT CRACKED AT FORWARD WET AREA BETWEEN BS 328 - 344 LBL 48. R & R THE FLOOR SUPPORT.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 34,588 hrs · 19,774 cycles

FWD WET AREA FLOORBEAM UPPER TEE CORRODED BS 328, RBL 12. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS, REPAIRED THE TEE.

Part: VAPOR BARRIER — CRACKED · airframe 35,503 hrs · 18,234 cycles

FOUND AN 18 INCH CRACK IN LT VAPOR BARRIER BAY 7 BETWEEN LBL 31.83 AND LBL 45.64. REPAIRED THE VAPOR BARRIER.

Part: ANGLE — CORRODED (BS 727E-747) · airframe 34,588 hrs · 19,774 cycles

AFT CARGO BAY LT TRANSITION ZEE ANGLE IS CORRODED FROM BS 727E - 747. BLENDED CORROSION FOUND TO BE OUT OF LIMITS, REPAIRED.

Part: SUPPORT ANGLE — CORRODED (BS 727D-727E) · airframe 34,588 hrs · 19,774 cycles

AFT CARGO BAY LEFT TRANSITION ZEE ANGLE HAS CORROSION FROM BS 727D - 727E. BLENDED CORROSION FOUND TO BE OUT OF LIMITS, REPAIRED.

Part: SUPPORT ANGLE — CORRODED (BS 767-787) · airframe 34,588 hrs · 19,774 cycles

AFT CARGO BAY LT TRANSITION ZEE ANGLE IS CORRODED FROM BS 767 - 787. BLENDED CORROSION FOUND TO BE OUT OF LIMITS AND REPAIRED.

Part: LIGHT — DAMAGED (CABIN) · airframe 34,399 hrs · 19,699 cycles

SELF ILLUMINATING FLOOR PATH LIGHT STRIP DAMAGED AT ROW 9 DEF. REPLACED DAMAGED SECTION.

Part: SENSOR — NO INDICATION (TE FLAP) · airframe 33,971 hrs · 19,552 cycles

T/E FLAP ASSYMETRY. R & R NR 5 SKEW SENSOR.