N531UA

Part: SWITCH — DIRTY (ENTRY DOOR) · airframe 65,807 hrs · 25,929 cycles

EICAS MSG DISPLAYED STEADY. LT FWD ENTRY DOOR OPEN. LIGHT DID NOT DISPLAY. INSPECTED & CHECKED LT FWD ENTRY DOOR LATCHING & INDICATION. CLEANED & LUBED DOOR LATCH SWITCH PLUNGER. NR 1 ENTRY DOOR & ADJUSTMENT TEST SYS SATISFACTORY. OPERATIONS CHECKED SATISFACTORY IAW AMM 52-71-00-753-053. NO ADDITIONAL FAULTS NOTED. ACFT RELEASED TO SERVICE

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 63,521 hrs · 24,320 cycles

AIR RETURN TO DEPARTURE DUE TO A BIRD STRIKE OF THE NR 1 ENGINE. ENGINE SECURED. IN FLIGHT. ACFT GROUNDED NO OPS. ENGINE BEYOND REPAIR WITH CORE DAMAGE OUT OF LIMITS AT C2 FAN. NR 1 ENGINE R & R.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 64,483 hrs · 25,018 cycles

FLASHLIGHT BRACKET BROKEN. REPLACED HARDWARE IAW AMM 25-64-00.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 63,500 hrs · 24,357 cycles

SMOKE IN COCKPIT, SUSPECTED LT PACK. ITEM WAS INITIALLY DEFERRED IAW MEL 21-51-01-01 CAT C NO FLY DATE 02-01-14, ACFT GNDED. INTEGRITY OF LT PACK SYS VERIFIED. APU & LT PACK SYS WERE RUN IAW AMM 49-11-00 & AMM 21-00-00. FAULT COULD NOT BE REPLICATED. OPERATIONS CHECKED GOOD. SYS ANALYSIS SUGGEST SMOKE WAS DUE TO PRE DEPARTURE DE-ICING OF ACFT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,435 hrs · 24,227 cycles

EMERGENCY FLASHLIGHT UNDER SUPERNUMERARY SEAT IS INOPERATIVE. R & R FLASHLIGHT BATTERY IN SUPERNUMERARY AREA WITH SERVICEABLE UNIT IAW AMM, ACFT WAS GNDED.

Part: DOOR — OPEN (VENT) · airframe 62,955 hrs · 23,895 cycles

DURING TAKEOFF ROLL, AT APPROX 85 KNOTS, MAIN CARGO DOOR WARNING ILLUMINATED. NO HIGH ENERGY BRAKING WAS REQUIRED DURING REJECTED TAKEOFF. VERIFIED "VENT DOOR" ON PANEL WAS ILLUMINATED, VENT DOOR NOT FULLY STOWED. CYCLED MAIN CARGO DOOR IAW PRECISION CONVERTED FREIGHTERS AMM 52-30-00/513. OPS CHECKS GOOD.

Part: SHEAR TIE — CORRODED (BS 1701) · airframe 62,904 hrs · 23,842 cycles

SHEAR TIE IN THE AFT LOWER CARGO COMPARTMENT BS 1701 BUTT LINE ZERO FOUND WITH CORROSION OUT OF LIMITS. FABRICATED NEW SHEAR TIE IAW SRM 53-60-07. PRIMED AND PAINTED IAW SRM 51-20-01. INSTALLED NEW SHEAR TIE IAW SRM 51-40-02.

Part: FLASHLIGHT — FAILED (CABIN) · airframe 62,827 hrs · 237,621 cycles

SUPERNUMERARY EMERGENCY FLASHLIGHT FAILED TO CHARGE PROPERLY. R & R THE EMERGENCY FLASHLIGHT IAW AMM 25-64-00, PAGE 204. OPS CHECKS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 62,824 hrs · 23,757 cycles

COCKPIT EMERGENCY FLASHLIGHT BATTERY DEAD. R & R EMERGENCY FLASHLIGHT BATTERY IAW PRECISION CONVERSIONS SUPPLEMENTAL MM PC-0118-06, 25-60-00. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 62,694 hrs · 23,658 cycles

ENTRANCE EMERGENCY FLASHLIGHT INOPERATIVE. R & R EMERGENCY FLASHLIGHT BATTERY. OPS CHECKED GOOD IAW AMM 25-64-00.

Part: PUMP — FAILED (LT ENGINE) · airframe 62,550 hrs · 23,581 cycles

LEFT ENGINE OIL TEMP IN AMBER BAND (165 DEG) WITHOUT OIL QUANITY INDICATED. DURING CHECKLIST OIL TEMP INDICATION WENT TO (195 DEG) IN LESS THAN 1 MINUTE. SHUTDOWN ENGINE OIL TEMP AND QUANITY RETURNED TO NORMAL. R & R LEFT ENGINE LUBRICATION/SCAVENGE PUMP AND SCAVENGE PUMP LEAK AND OPS CHECK GOOD.

Part: TRANSMITTER — INOPERATIVE (ZONE 500) · airframe 62,456 hrs · 23,545 cycles

OIL QUANITY ON LT ENGINE DROPPED TO 0 FOLLOWED BY THE OIL TEMP INCREASING TOWARD LIMITS. PERFORMED LT ENG SHUTDOWN CHECKLIST. FOUND LT ENG OIL QTY TRANSMITTER GROUND WIRE BROKEN (DMI 01-05-01-B-07). RAN FIM 79-34, FT 802, FAULT FOR OIL TEMP BLOCK 23. R & R LT ENG OIL TEMP THERMOCOUPLE PROBE, THERMOCOUPLE OPS CK GOOD. ACCOMPLISHED ENGINE WINDMILL INSP ON LT ENG, NO EXTERNAL LEAKS NOTED, NO CHIPS NOTED, NO OIL CONSUMPTION NOTED. LP 13022 & 13023: NR 1 ENG OIL TRANSMITTER IS LOOSE. REMOVED RED LT ENG OIL QTY TRANSMITTER, OP'S CK GOOD. REF DMI 01-05-01-B-07, REPAIRED GROUND WIRE BY RE-TERMINATING RING TERMINAL (AT OIL QTY TRANSMITTER) OPS CK OF OIL QTY SYS GOOD.

Part: SKIN — DELAMINATED (NR 6 SLAT) · airframe 62,374 hrs · 23,504 cycles

STARBOARD INBD NR 6 L/E SLAT HAS DELAMINATION. R & R RT INBD NR 6 L/E SLAT, IAW AMM 27-81-01. INSTALLED NR 6 SLAT.

Part: SLAT — DELAMINATED (LT WING) · airframe 61,729 hrs · 23,166 cycles

DURING SERVICE CHECK FOUND LEFT INBOARD SLAT DELAMINATED. REMOVED AND REPLACED NR 5 SLAT IAW B-757 AMM 27-81-01, OP'S CK GOOD. INSTALLED P/N 114N3002-101, S/N A10091.

Part: SKIN — DENTED (ZONE 100) · airframe 60,829 hrs · 22,622 cycles

RT FUSELAGE DENTED IN THE RED STRIPE BELOW R-2 WINDOW BS 300, STRINGER S-19R-S-20R. REPAIRED ON FASI WO211333, NR14094.

Part: SKIN — DENTED (ZONE 100) · airframe 60,829 hrs · 22,622 cycles

LOWER FUSELAGE AT STA 1670 HAS A DENT BETWEEN STRINGERS 28L AND 29L. REPAIRED ON FASI WO 21133, NR04833.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 60,829 hrs · 22,622 cycles

BS 670, RBL 45.5 INTERCOSTAL IS CRACKED BELOW SEAT TRACK. REPAIRED ON FASI WO 21133, NR 04670.

Part: POWER SUPPLY — DAMAGED (EMERGENCY LIGHT) · airframe 60,556 hrs · 22,524 cycles

EEL STRIP DAMAGED BETWEEN ROWS 12 AND 14. REPLACED POWER SUPPLY AND JUMPER CABLE FOR SEAT ROWS 9 THROUGH 13. OP CHECKS OKAY.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 59,820 hrs · 22,248 cycles

LIGHTNING STRIKE ON T/O, BIG BANG AND SMOKE ODOR IN COCKPIT. NEED TO INSTALL NEW BASE PLATE AND STATIC WICK ON LT SIDE VERY TOP OF RUDDER, BOTH MISSING DUE TO LIGHTNING STRIKE. INSTALLED DISCHARGE BASE AND PAINTED. STATIC WICK ON AOG Z4071. REPLACED STATIC WICK. REPLACED RADOME.

Part: O-RING — DEFECTIVE (EVAC SLIDE)

LOW BOTTLE. LEAKING AT BALL SHAFT O-RING. REMOVED & REPLACED O-RING.

Part: SEAL — SEPARATED (L1 DOOR) · airframe 57,796 hrs · 21,445 cycles

CREW REPORT: RUBBER DOOR SEAL 1L SEPARATED FROM DOOR. *S/D* SECURED SEAL.

Part: PANEL — FAULTY (FIRE DETECTION) · airframe 57,672 hrs · 21,402 cycles

LEFT ENGINE NR 2 SQUIB DOES NOT TEST PROPERLY. SHORT IN SQUIB TEST PANEL. REPLACED SQUIB TEST PANEL, OPS CHECKED OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,260 hrs · 20,901 cycles

LEFT SIDE FUSELAGE SKIN, PREVIOUS DOUBLER REPAIR HAS A DENT AT BS 598 TO 625, BETWEEN STR 15L-17L. ACCOMPLISHED AT MAJOR REPAIR AT GSO.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,260 hrs · 20,901 cycles

DENT IN EXTERNAL FUSELAGE SKIN AT BS 369 JUST ABOVE STR 19R. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,260 hrs · 20,901 cycles

EEL LIGHT AT SEAT 5AB INOP. UNKNOWN DAMAGE. REMOVED AND REPLACED A SECTION OF EEL AT 5ABC, OPS CHECKED GOOD.

Part: SHAFT — OUT OF POSITION (EMERGENCY EXIT) · airframe 56,260 hrs · 20,901 cycles

THE 4L EMERGENCY POWER ACTUATOR CABLE FAILS TRAVEL CHECK. FOUND SPLINE SHAFT AND LOWER HINGE LINK WERE CLOCKED WRONG. CLOCKED ASSY WITH NEW PARTS AND PASTED CABLE TRAVEL CHECK. ALL OPS NORMALLY.

Part: CONTACT — BROKEN (EMERGENCY LIGHTS) · airframe 56,260 hrs · 20,901 cycles

COACH EEL HAS A LIGHT STRIP WITH BROKEN CONTACTS. REPLACED LIGHT STRIP, OPS CHECKED OK.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 56,260 hrs · 20,901 cycles

EEL FEEDER AT STA 1060 DAMAGED. REPLACED EEL FEEDER, OPS CHECKED OK.

Part: FEEDER CABLE — BROKEN (EMERGENCY LIGHTS) · airframe 56,260 hrs · 20,901 cycles

ONE COACH EMERGENCY ESCAPE LIGHT FEEDER BROKEN. REPLACED FEEDER ASSY, OPS CHECKED OK.

Part: SKIN — DAMAGED (LT TE FLAP) · airframe 56,260 hrs · 20,901 cycles

LEFT INBOARD MAIN FLAP UPPER SURFACE CONTACTING NR 5 SPOILER, PREVIOUS REPAIR GOUGED. ACCOMPLISHED MAJOR REPAIR

Part: FIRE LOOP — DAMAGED (NR 1 NACELLE) · airframe 56,260 hrs · 20,901 cycles

IN BULLNOSE AREA OF PYLON NR 1, FIRE LOOP 'B ' CONNECTOR D1950 IS BROKEN AND NEEDS TO BE REPLACED. FOUND DAMAGED FIRE LOOP (BROKEN) -UNKNOWN REASONS. REMOVED AND REPLACED FIRE LOOP A, OPS CHECKED GOOD.

Part: FIRE LOOP — BROKEN (NR 1 NACELLE) · airframe 56,260 hrs · 20,901 cycles

IN BULL NOSE AREA OF PYLON NR 1, FIRE LOOP ' A' ON BULL NOSE PANEL BROKEN. FOUND FIRE LOOP BROKEN. REMOVED AND REPLACED FIRE LOOP A, OPS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 56,260 hrs · 20,901 cycles

FOUND MAIN CABIN FLOORBEAM AND PREVIOUS REPAIR CORRODED STA 365, RBL12. ACCOMPLISHED MAJOR REPAIR.

Part: STRUCTURE — DAMAGED (BS 1600 S27-28L) · airframe 56,260 hrs · 20,901 cycles

FOUND DENT AT STATION 1600 BETWEEN STR 27 AND 28 LEFT. FOUND DENT TO HAVE A CRACK. ACCOMPLISHED MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 1648-1681) · airframe 56,260 hrs · 20,901 cycles

MAIN CABIN FLOOR SUPPORT AT STA 1648 TO 1681, RBL 54 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR.

Part: STRUCTURE — DAMAGED (R2 DOOR) · airframe 56,260 hrs · 20,901 cycles

R2 DOOR UPPER HINGE ARM CUTOUT IS DAMAGED. ACCOMPLISHED MAJOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,260 hrs · 20,901 cycles

L2 DOOR UPPER HINGE ARM CUT OUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED.

Part: FRAME — GOUGED (BS 1520 S23-25R) · airframe 56,260 hrs · 20,901 cycles

AFT PIT FRAME GOUGED 4 EA PLACES AT BS 1520 BETWEEN STR 23R AND 25R. MAJOR REPAIR ACCOMPLISHED AT GSO.

Part: ATTACH ANGLE — CORRODED (BS 1380-1440) · airframe 56,260 hrs · 20,901 cycles

AFT CARGO DOOR LOWER SILL ATTACH ANGLE HAS CORROSION ON UPPER SURFACE FROM BS 1380 TO 1440. MAJOR REPAIR ACCOMPLISHED.

Part: SHEAR TIE — CRACKED (BS 1300 S20-21L) · airframe 56,260 hrs · 20,901 cycles

AFT CARGO PIT SHEAR TIE AT STA 1300 BETWEEN STR 20L AND 21L CRACKED. MAJOR REPAIR ACCOMPLISHED AT GSO.

Part: STRINGER — DAMAGED (BS 620 S16L) · airframe 56,260 hrs · 20,901 cycles

CRACK FOUND IN STRINGER 16L AT BS 620, OUT OF FASTENER HOLE. CRACK VERIFIED ON LT EXTERNAL SKIN REPAIR. MAJOR REPAIR ACCOMPLISHED AT GSO.

Part: FRAME — DENTED (BS 1560 S26L) · airframe 56,260 hrs · 20,901 cycles

AFT PIT FRAME INBOARD FLANGE DENTED AT BS 1560 BETWEEN STR 26L AND STR 27L.

Part: FRAME — DENTED (BS 1480 S25L) · airframe 56,260 hrs · 20,901 cycles

AFT PIT FRAME DENTED AT INBOARD FLANGE AT BS 1480 BETWEEN STR 25L AND STR 26L. MAJOR REPAIR ACCOMPLISHED AT GSO.

Part: FRAME — DENTED (BS 1540 S36) · airframe 56,260 hrs · 20,901 cycles

AFT PIT FRAME DENTED ON INBOARD FLANGE AT BS 1540 AND STR 26. MAJOR REPAIR ACCOMPLISHED AT GSO.

Part: WEB — GOUGED (R1 DOOR) · airframe 56,260 hrs · 20,901 cycles

R1 DOOR WEB BY UPPER HINGE INTERCOSTAL GOUGED. ACCOMPLISHED AT GSO.

Part: FRAME — DENTED (BS 1440 S25L) · airframe 56,260 hrs · 20,901 cycles

AFT PIT FRAME DENTED STA 1440 AT STR 25L. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: SKIN — DENTED (FWD CARGO DOOR) · airframe 56,260 hrs · 20,901 cycles

DENTED FORWARD CARGO DOOR EXTERNAL SKIN, 40 INCHES AFT OF FORWARD EDGE, 22 INCHES ABOVE BOTTOM EDGE. MAJOR REPAIR ACCOMPLISHED AT GSO.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,101 hrs · 20,833 cycles

EMERGENCY AISLE LIGHTS AT SEAT'S 15A AND 18A INOP. REPLACED BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,084 hrs · 20,826 cycles

SEVERAL EEL AISLE LIGHTS ARE INOP THROUGHOUT THE CABIN. RELAMPED EMERGENCY LIGHT.

Part: FEEDER CABLE — DEFECTIVE (CABIN) · airframe 56,084 hrs · 20,826 cycles

EEL LIGHTS FROM ROWS 32-34 ARE INOPERATIVE. REPLACED FEEDER.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 55,652 hrs · 20,662 cycles

EXTERIOR EMERGENCY LIGHT INOP AT MED 4L. FOUND LAMP BURNED OUT. RELAMPED ASSY- OPS CHECKED NORMALLY.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 55,652 hrs · 20,662 cycles

DOOR 4L DOOR ASSIST BOTTLE READS 2300 AT 70 DEGREES NEEDS SERVICE TO 3000. DUE TO UNKNOWN LEAKAGE. REPLACED BOTTLE.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 57,551 hrs · 21,503 cycles

EMERGENCY LIGHTING STRIP ON FLOOR AT ROW 29-30 HAS BROKEN PLASTIC AND BULB OUT OF SOCKET. INSTALLED BULB AND RE ASSEMBLED LIGHT. OPERATES PROPERLY.

Part: WINDOW — OUT OF TRACK (COCKPIT) · airframe 55,614 hrs · 20,650 cycles

ABORTED T/O AT 110KTS. COPILOT'S BACK WINDOW CAME OPEN AND WAS OFF TRACK. COULD NOT GET IT TO CLOSE. AUTOBRAKES DID ENGAGE. SECURED FO WINDOW BACK IN TRACK AND CLOSED IT PROPERLY, NO REPEATS SINCE ORIGINAL INCIDENT.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 55,180 hrs · 20,483 cycles

FOUND FLOOR EEL LIGHTS OUT FROM 31A TO AFT LAV. FOUND WIRE HARNESS BROKEN.

Part: SKATE ANGLE — DAMAGED (NR 1 NACELLE) · airframe 56,208 hrs · 21,064 cycles

NR 1 PYLON AFT SKATE ANGLE CRACKED OUT OF OUTBOARD ATTACH FASTENER AFT OF AFT ENG MOUNT. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW SKATE ANGLE REPAIR.

Part: OXYGEN SYSTEM — READS LOW (CREW) · airframe 54,796 hrs · 20,340 cycles

FOUND OXYGEN BELOW 1650 PSI. OXYGEN SYSTEM SERVICED TO FULL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,197 hrs · 20,133 cycles

EMERGENCY LIGHTS OUT AT DOOR 2L OUTSIDE. RELAMPED, OK

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,361 hrs · 19,822 cycles

L-2 EMERGENCY LIGHT INOPERATIVE. [SUP 4-17-07] REPLACED EMERGENCY POWER SUPPLY CHARGER. OPS CHECKS NORMAL.

Part: FAN — ODOR (COCKPIT) · airframe 53,201 hrs · 19,767 cycles

IN DESCENT PASSING FL370 CREW DETECTED AN ELECTRICAL BURNING ODOR IN THE COCKPIT WHICH QUICKLY DISSIPATED. [SUP 05-18-07] ACCOMPLISHED INSPECTION BEHIND COCKPIT CB PANELS AND E & E COMP. CREW COMMENT ODOR DISSIPATED BY TURNING OFF RIGHT RECIRCULATION FAN. INSPECTED WIRING FOR RT RECIRC FAN. NO DISCREPANCY FOUND. CAUSE OF ODOR NOT ESTABLISHED. REPLACED RT RECIRC FAN.

Part: SWITCH — NO TEST (FIRE-OVERHEAT) · airframe 52,970 hrs · 19,685 cycles

FIRE-OVERHEAT TEST-ENG-APU-CARGO SYSTEM TEST FAIL. SYSTEM TEST LIGHT WILL NOT ILLUMINATE. [SUP 05-18-07] REPLACED LED AND SWITCH ASSY.

Part: UNKNOWN — VIBRATION · airframe 52,320 hrs · 19,423 cycles

CREW REPORTED A SEVERE VIBRATION FROM TOUCHDOWN THROUGH ROLLOUT. FOUND NLG TORSION LINKS WORN BEYOND IN-SERVICE LIMITS. REPLACED LOWER NLG TORSION LINK ASSY.

Part: SKIN — DENTED (FUSELAGE) · airframe 51,751 hrs · 19,214 cycles

RAMP REPORTED DENT IN FUSELAGE APPROXIMATELY 4FT AFT DOOR 4L. MAJOR REPAIR ACCOMPLISHED ON FUSELAGE SKIN AFT OF DOOR 4L. DENT IS 5" LONG X 1" WIDE. REPAIR DOUBLERS AND TRIPLER INSTALLED AND INSPECTED.

Part: BARREL — DAMAGED (ASPIRATOR)

DAMAGED ASPIRATOR BARREL. THE EXACT CAUSE OF DAMAGE TO THE ASPIRATOR COULD NOT BE DETERMINED, INVESTIGATION HAS ATTRIBUTED THE CAUSE TO ACCIDENTAL DAMAGE DURING THE LAST PACKING PROCESS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 41,967 hrs · 15,610 cycles

FUSELAGE SKIN ON STA 610 AT STR 16LT IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. INSTALLED DOUBLER AND FILLER REPAIR.

Part: TRANSCEIVER — FAULTY (RADAR) · airframe 37,917 hrs · 14,098 cycles

WEATHER RADAR INOPERATIVE. THE POWER OUT IS MEASURING 125W MAXIMUM, DURING TEST. THE MINIMUM ACCEPTABLE POWER OUTPUT FOR A SERVICEABLE UNIT IS 175W. MOST UNITS ARE IN THE 250W RANGE. REPLACED THE A5 ASSEMBLY . THE LRU'S LOW POWER OUT CONDITION CORRELATES TO THE WRITE-UP OF NO RETURN BEYOND 40NM RANGE.

Part: THRESHOLD — CORRODED · airframe 37,429 hrs · 13,917 cycles

AFT CARGO PIT THRESHOLD LOWER BEAM PREVIOUS REPAIR HAD SEVERE EXFOLIATION CORROSION AT REPAIR ANGLE AND BOTH SPLICE PLATES STATION 1436 TO STATION 1383. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. INSTALLED FILLER SECTION AND TWO EA REPAIR ANGLES.

Part: FRAME — DENTED · airframe 37,429 hrs · 13,917 cycles

AFT PIT STATIO 1400 BETWEENS TATION 25L AND 26L FRAME IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL DOUBLER REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,429 hrs · 13,917 cycles

CABIN CREASE BEAM INBOARD CHORD VERTICAL LEG CORRODED STATION 900 TO 1040, LBL 64. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,429 hrs · 13,917 cycles

FORWARD CABIN FLOORBEAM AT STATION 297 RBL 40 CORRODED. MAJOR REPAIR ACCOMPLISHED DOUBLER REPAIR INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,429 hrs · 13,917 cycles

FLOORBEAM AT STATION 365 RBL18 MATERIAL LOSS BEYOND 10 PERCENT LIMIT FORWARD EDGE. MAJOR REPAIR ACCOMPLISHEDFILLER INSTALLED AND TWO EACH ANGLES NESTED UNDER FLOORBEAM CAP.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,429 hrs · 13,917 cycles

AFT PIT FRAME LT SIDE AT STA 1520 ABOVE STRINGER 26L IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED TRIPLER REPAIR TO FRAME AT STA 1520, STRINGER 26L.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,429 hrs · 13,917 cycles

CAB FLOOR CREASE BEAM INNER CHORD UPPER FLANGE BETWEEN STATION 1580 TO 1600, RBL 44, IS CORRODED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR WAS PERFORMED ON CREASE BEAM AT STATION 1580 TO 1600, RBL 44.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 37,429 hrs · 13,917 cycles

AFT PIT FLOOR SUPPORT STATION 1340 TO STATION 1440 RBL 3 IS CRACKED AND CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,429 hrs · 13,917 cycles

FORWARD PIT STATION 684, RBL 16, FLOOR SUPPORT ANGLE CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT ANGLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,429 hrs · 13,917 cycles

CABIN FLOOR BEAM UPPER CHORD STATION 1640 LBL 56 HAS EXCESSIVE MATERIAL REMOVED. MAJOR REPAIR ACCOMPLISHED. FLOORBEAM UPPER CHORD AFT FLANGE REPAIRED AND STRAP INSTALLED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,429 hrs · 13,917 cycles

CABIN FLOOR STATION 660-680 LEFT HAND SIDE CREASE BEAM INNER CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED INNER CHORD.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 37,411 hrs · 13,908 cycles

STATION 1600 LEFT HAND STRINGER 20 HAS FUSELAGE DAMAGED. MAJOR REPAIR ACCOMPLISHED.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,563 hrs · 13,208 cycles

LEFT FUSELAGE SKIN DENTED STA 618 STR 16L.

Part: SKIN — DENTED · airframe 35,563 hrs · 13,208 cycles

EXTERNAL FUSELAGE SKIN DENTED STA 625 TO 637 AT SKIN LAP STRINGER 14L. MAJOR REPAIR ACCOMPLISHED FOR STRINGER REPAIR. EXTERNAL SKIN FLEXED BACK.

Part: WIRE — BROKEN (E/E COMPT)

RETURNED TO FIELD DUE TO PARTIAL ELECTICAL FAILURE. WIRE W2018-0003-06 WAS FOUND BROKEN AT L GENERATOR CIRCUIT BREAKER C901 PHASE C. LOSS OF PHASE C AT L GEN CB CAUSED PARTIAL ELECTRICAL FAILURE. THE WIRE TERMINAL HAD BROKEN DUE TO A ONE-TIME OVERSTRESS APPLICATION. THE WIRE TERMINAL WAS REPLACED.

Part: CONTROL ROD — FAILED (NLG DOOR)

DURING GEAR RETRACTION, HEARD LOUD GEAR DOOR NOISE ACCOMPANIED WITH VIBRATION. RETURNED TO FIELD. NOSE LANDING GEAR DOOR CONTROL ROD FRACTURED DURING GEAR RETRACTION. REPLACE ROD WITH NEW ROD. OPERATION CHECKS NORMAL.