N648GT

ATA 2612

Part: FIRE DETECTOR — MALFUNCTIONED (NR 2) · airframe 89,789 hrs · 17,426 cycles

STATUS MESSAGE LT ENGINE FIRE LOOP 2. REMOVED AND REPLACED THE FIRE DETECTOR IAW AMM 26-11-02, PERFORMED ENGINE FIRE & OVER HEAT TEST IAW AMM 26-11-00. TEST PASSED MESSAGE CLEARED.

ATA 2910

Part: HYDRAULIC SYSTEM — UNKNOWN · airframe 89,704 hrs · 17,403 cycles

HYDRAULIC QTY-1.37 WITH OVERFILL APPEARED DURING CLIMB, WENT DOWN TO -1.15 AFTER CENTER HYD PUMPS WERE SWITCHED OFF. CENTER HYD SYS SERVICED PROPERLY IAW MM 12-12-01.

ATA 7110

Part: RIVET — DAMAGED (NR 1 COWLING) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 1 LT CORE COWL UPPER AFT RIB MISSING HEAD OF RIVET. DRILLED OUT DAMAGED RIVET AND INSTALLED NEW RIVET IAW SRM 51-40-02.

ATA 2822

Part: HOUSING — DIRTY (FUEL PUMP) · airframe 89,709 hrs · 17,403 cycles

LEFT WING BOOST PUMP BONDING RESISTANCE BETWEEN PUMP HOUSING TO WING FOUND HIGH. PUMP HOUSING CLEANED AND PERFORMED RESISTANCE CHECK. FOUND WITHIN LIMITS IAW SWPM 20-20-00.

ATA 7110

Part: RIB — CRACKED (LT COWLING) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 2 LT CORE COWL AFT RIB CRACKED. ENGINE NR 2 REPLACE CORE COWL IAW AMM 71-11-06.

ATA 5311

Part: FRAME — DAMAGED (FUSELAGE) · airframe 89,709 hrs · 17,403 cycles

PERFORMED REPAIR DOUBLER AT AFT CARGO LOWER FRAME WEB, STA 1153, RBL-2, REF IAI NRC M0377, WORK PERFORMED IAW REA MF2012R0211, REV A, DATED JUN 13 2016 AND AS INSTRUCTED BY MESSAGE IAI-TLS-16-0004-02B, DATED 17 MAY 2016 AND MESSAGE IAI-TLS-16-000.

ATA 7110

Part: RIVET — DAMAGED (NR 1 COWLING) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 1 RT CORE COWL UPPER AFT RIB MISSING HEAD OF RIVET. DRILLED OUT DAMAGED RIVET AND INSTALLED NEW RIVET IAW SRM 51-40-02.

ATA 2150

Part: SPRING — BROKEN (CHECK VALVE) · airframe 89,709 hrs · 17,403 cycles

BYPASS RT CHECK VALVE SPRING BROKEN. CHECK VALVE REPLACED IAW AMM 21-51-02.

ATA 2912

Part: FILTER — DEFECTIVE (HYDRAULIC SYS) · airframe 89,709 hrs · 17,403 cycles

C HYD PUMPS OVERHEAT, ALL C HYD PUMPS GOT OVERHEATED, THEN ELECT 1, ELEC 2 AFTER THAT, C HYD PRESSURE STARTED TO SURGE AND DROPPED TO "0". ADP FILTER MODULE REPLACED IAW MM 29-11-03.

ATA 7110

Part: NUT PLATE — MISSING (NR 2 ENGINE) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 2 RT C-DUCT UPPER SKIRT FAIRING NUT PLATE MISSING. INSTALLED NEW NUT PLATE IAW SRM 51-40-02.

ATA 7110

Part: DUCT — DENTED (NR 1 ENGINE) · airframe 89,709 hrs · 17,403 cycles

NR 1 ENGINE DENT FOUND IN THE TOP SIDE OF THE LT C-DUCT RAIL. C-DUCT REPLACED, NRC M0150 REPLACEMENT.

ATA 7110

Part: STRIP — CORRODED (RT COWLING) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 1 RT CORE COWL UPPER STRIP STRUCTURE CORRODED. CORRODED PART REMOVED AND NEW WEAR STRIP, PN 224-2301-122 WAS INSTALLED USING RIVETS IAW SRM 51-40-02.

ATA 3610

Part: CONTROLLER — FAILED (BLEED AIR SYS) · airframe 89,709 hrs · 17,403 cycles

ON SUPPLY BITE MODULE, M129, LT HPC TEST FAIL. HPC ON NR 1 ENGINE REPLACED IAW AMM 36-11-08/401.

ATA 2711

Part: TRIM SYSTEM — OUT OF ADJUST (AILERON) · airframe 89,704 hrs · 17,403 cycles

AILERON TRIM, MAX TRIM TO THE LT EXCEEDED LIMIT 6.1, OK TO THE RT: 5.3, MAX LIMIT 5.9. ADJUSTED AILERON TRIM CONTROL TO RT WING DOWN 30 DEGREES, 5.6 UNIT YOLK, LT WING DOWN 30 DEGREES -5.7 UNIT YOLK IAW MM 27-11-00.

ATA 2620

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 89,709 hrs · 17,403 cycles

CARGO FIRE PANEL, COCKPIT P8 PANEL, BOTTLE DISCHARGE LIGHT DOES NOT COME ON WHEN TESTED. APU AND FIRE CONTROL PANEL REPLACED IAW AMM 26-22-03.

ATA 2822

Part: PUMP — FAULTY (LT WING) · airframe 89,709 hrs · 17,403 cycles

LEFT FWD BOOST PUMP REPLACED, LT WING IS NOT OPERATING PROPERLY. LEFT FWD BOOST PUMP REPLACED IAW AMM 28-22-03.

ATA 7830

Part: LATCH — BENT (THRUST REVERSER) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 2 RT C-DUCT LATCH HUG GUARD BEND. LATCH REPLACED IAW AMM 78-31-01.

ATA 2432

Part: SCREW — CORRODED (MAIN BATTERY) · airframe 89,709 hrs · 17,403 cycles

MAIN BATTERY FOUND CORRODED, SCREWS HOLDING THE BATTERY. REPLACED THE CORRODED BATTERY SCREWS HOLDING THE MAIN BATTERY IAW MM 24-31-01.

ATA 4950

Part: HOUSING — CORRODED (APU) · airframe 89,709 hrs · 17,403 cycles

APU SURGE VALVE HOUSING CORRODED. REPLACED HOUSING IAW AMM 49-53-06.

ATA 2620

Part: CAP — DAMAGED (FIRE BOTTLE) · airframe 89,709 hrs · 17,403 cycles

NOSE WW ON P-40 PANEL LIGHT CAPS OF FIRE BOTTLE ARM LIGHT. BOTTLE DISCHARGE LIGHTS ARE DAMAGED. REPLACE LIGHT CAPS OF FIRE BOTTLE ARMED AND BOTTLE DISCHARGE IAW AMM 26-15-01.

ATA 7400

Part: PLUG — CORRODED (IGNITION BOX) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 1, NR 2 PLUGS ON THE IGNITION BOX ARE CORRODED. ENGINE NR 1, NR 2 PLUGS ON THE IGNITION BOX WERE CLEANED OF CORROSION IAW SWPM 20-60-01.

ATA 7334

Part: TRANSMITTER — FAULTY (FUEL SYSTEM) · airframe 89,709 hrs · 17,403 cycles

NR 2 ENGINE FUEL PRESSURE SHOWS 200 PSI WHEN ENGINE NOT RUNNING. FUEL PRESSURE TRANSMITTER REPLACED IAW AMM 73-33-01.

ATA 2432

Part: SCREW — CORRODED (MAIN BATTERY) · airframe 89,709 hrs · 17,403 cycles

APU BATTERY, FOUND CORRODED SCREWS HOLDING THE BATTERY. REPLACED THE CORRODED BATTERY SCREWS HOLDING THE APU BATTERY IAW AMM 24-31-04.

ATA 2611

Part: TUBE — DAMAGED (SMOKE DETECTION) · airframe 89,709 hrs · 17,403 cycles

AFT CARGO STA 1197 SMOKE DETECTION TUBING DAMAGED. AFT CARGO STA 1197 DAMAGED SMOKE DETECTION TUBING REPLACED IAW AMM 26-16-01.

ATA 2820

Part: CONNECTOR — DAMAGED (FUEL SYSTEM) · airframe 89,709 hrs · 17,403 cycles

AFT CARGO APU FUEL DUCT CLIP IS DAMAGED. AFT CARGO APU FUEL SHROUD REPLACED CONNECTOR.

ATA 4950

Part: PLUG — UNSECURE (APU BAY) · airframe 89,709 hrs · 17,403 cycles

AT APU COMPARTMENT FOUND P-17 PLUG WAS NOT INSTALLED. AT APU COMPARTMENT LT SIDE P-17 PLUG RECONNECTED TO SURGE VALVE TORQUE MOTOR, M5, AND CHECKED IAW AMM 49-53-01.

ATA 2620

Part: COUPLING — DAMAGED (CARGO BAY) · airframe 89,709 hrs · 17,403 cycles

AFT CARGO TUBING EXTINGUISHER ARMFLEX IN BAD CONDITION. AFT CARGO COMPARTMENT FIRE EXTINGUISHER TUBING ARMFLEX REPLACED IAW AMM.

ATA 2822

Part: HOUSING — DIRTY (FUEL PUMP) · airframe 89,709 hrs · 17,403 cycles

RIGHT WING CTR AUXILIARY PUMP BONDING RESISTANCE BETWEEN PUMP HOUSING TO WING FOUND HIGH. PUMP HOUSING CLEANED PERFORMED RESISTANCE CHECK AND FOUND WITHIN LIMITS IAW SWPM 20-20-00.

ATA 2600

Part: PRINTED CKT BOARD — DEFECTIVE (DETECTION SYS) · airframe 89,709 hrs · 17,403 cycles

EICAS MSG FWD CARGO DETECTOR 1, FWD CARGO DETECTOR 2. REPLACED PRINTED CIRCUIT ASSY, M10427, AT P-54 AND CHECK IAW AMM 26-16-00.

ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 89,709 hrs · 17,403 cycles

PERFORMED ABRASION DAMAGE REPAIR AT FUSELAGE LOWER SKIN, BS 1423, STR 24R-STR 25R, REF IAI NRC M0076. THE REPAIR PERFORMED WITH REPAIR DOUBLER AND FILLER IAW SRM 53-00-01, FIG 201, REPAIR 14, DETAIL 1.

ATA 7110

Part: COWLING — DAMAGED (NR 2 ENGINE) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 2 LT CORE COWL SUPPORT ROD DAMAGED. LT CORE COWL REPLACED.

ATA 7830

Part: LATCH — BENT (THRUST REVERSER) · airframe 89,709 hrs · 17,403 cycles

NR1 ENGINE UPPER LATCH HUG GUARD BEND. LATCH REPLACED IAW AMM 78-31-01.

ATA 2421

Part: IDG — DISCONNECTED · airframe 89,709 hrs · 17,403 cycles

IDG WHERE DISCONNECTED ACCORDING TO THE FCF CARD. RECONNECTED IAW MM 24-11-01.

ATA 3610

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 89,709 hrs · 17,403 cycles

LEFT ENGINE HPSOV APPEARED FOR SHORT TIME ON 2-3 OCCASIONS. HPSOV REPLACED IAW MM 36-11-07 CHECKED IN RUN UP AND FOUND OK IAW MM 71-00-00.

ATA 7110

Part: COWLING — CHAFED (NR 2 ENGINE) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 2 LT CORE COWL AFT BRACKET OF HOLD OPEN ROD CHAFING. ENGINE NR 2 REPLACE CORE COWL IAW AMM 71-11-06.

ATA 7721

Part: CABLE — LOOSE (THERMOCOUPLE) · airframe 89,709 hrs · 17,403 cycles

NR 2 ENGINE LT AND RT SIDE 0300 AND 0900 O`CLOCK CORE AREA IN THE THERMOCOUPLE CABLE SLEEVE LOOSE CLOSE THE UNIT. THERMOCOUPLE CABLE REPLACED IAW 77-21-02, UPPER, ENGINE PN CF6-80C2, S/N 704860.

ATA 4910

Part: ACTUATOR — OUT OF ADJUST (APU) · airframe 89,709 hrs · 17,403 cycles

APU INLET DOOR NEED ADJUSTMENT. APU INLET DOOR ACTUATOR READJUSTED IAW AMM 49-15-06-805-001.

ATA 7830

Part: LATCH — LOOSE (THRUST REVERSER) · airframe 89,709 hrs · 17,403 cycles

NR 2 ENGINE UPPER LATCH LOOSE. LATCH REPLACED IAW 78-31-01.

ATA 7830

Part: LATCH — LOOSE (THRUST REVERSER) · airframe 89,709 hrs · 17,403 cycles

NR 2 ENGINE UPPER C-DUCT LATCH LOOSE. LATCH LINK, BUSHING AND PINS REPLACED IAW AMM 78-31-01.

ATA 7110

Part: COWLING — DAMAGED (NR 2 ENGINE) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 2 LT FAN COWL AFT PART, INSIDE CORNER DAMAGED. PERFORMED GRAPHITE AND FIBER REPAIR ON FAN COWL IAW SRM 54-22-01.

ATA 2600

Part: DETECTOR — BROKEN (RT NACELLE) · airframe 89,709 hrs · 17,403 cycles

RIGHT NACELLE STRUT, THERMAL SWITCH DUCT LEAK DETECTOR, TS238, FOUND BROKEN. NACELLE STRUT, REPLACED THE THERMAL SWITCH DUCT LEAK DETECTOR, TS238, IAW 26-18-01 AND TESTED IAW 26-18-01.

ATA 4950

Part: VALVE — LOOSE (APU) · airframe 89,704 hrs · 17,403 cycles

APU BLEED PRESSURE DROPPED FOLLOWED BY PACK SURGE ON GROUND AFTER ENGINES SHUTDOWN. PERFORMED PNEUMATIC LEAK TEST ON APU SENSOR LINES FOUND SURGE VALVE LOOSE. RE-TIGHTENED IAW MM 49-53-02.

ATA 2121

Part: COOLING FAN — BROKEN (E&E BAY) · airframe 89,709 hrs · 17,403 cycles

FWD CARGO RT ELECTRONIC EQUIPMENT BAY COOLING SUPPLY FAN BLADE IS BROKEN. COOLING SUPPLY FAN REPLACED IAW AMM 2-58-06.

ATA 7400

Part: SCREW — CORRODED (IGNITION BOX) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 2 ON THE UPPER IGNITION BOX, THE PLUGS SCREWS ARE CORRODED. ENGINE NR 2 ON THE UPPER IGNITION BOX THE PLUGS SCREWS WERE CLEANED FORM CORROSION IAW SWPM 20-60-01.

ATA 7921

Part: GASKET — DAMAGED (NR 2 ENGINE) · airframe 89,709 hrs · 17,403 cycles

NR 2 ENGINE FUEL LEAK FROM FUEL/OIL HEAT EXCHANGER. GASKET REPLACED IAW AMM 72-21-01.

ATA 7200

Part: SEAL — TORN (NR 2 ENGINE) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 2 IN THE INTERMEDIATE CASE ON THE BLADE, SEAL IS TORN. PERFORMED SEALANT ON THE ENGINE NR 2 IN THE INTERMEDIATE CASE BLADES IAW AMM 51-31-00.

ATA 2820

Part: PRESSURE SWITCH — DEFECTIVE (FUEL SYSTEM) · airframe 89,709 hrs · 17,403 cycles

LEFT AFT FUEL PUMP C/B POPPED ON GROUND WAS RESET AND REMAINED OK. PRESSURE SWITCH REPLACED IAW MM 28-42-01.

ATA 7110

Part: RIVET — DAMAGED (NR 2 ENGINE) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 2 C-DUCT LT AND RT AFT INTERNAL PART, SUNK RIVETS. DRILLED OUT DAMAGED RIVETS AND INSTALLED NEW RIVETS IAW SRM 51-40-02.

ATA 7110

Part: RIVET — DAMAGED (NR 1 ENGINE) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 1 RT C-DUCT AFT INTERNAL PART, SUNK RIVETS. RIVETS REPLACED IAW SRM 51-40-02.

ATA 2150

Part: BULB — BROKEN (AC BAY) · airframe 89,709 hrs · 17,403 cycles

LEFT PACK OUTLET TEMP BULB, TS39, FOUND BROKEN TEMP BULB REPLACED IAW MM 21-52-06.

ATA 2822

Part: HOUSING — DIRTY (FUEL PUMP) · airframe 89,709 hrs · 17,403 cycles

RIGHT WING BOOST PUMP BONDING RESISTANCE BETWEEN PUMP HOUSING TO WING FOUND HIGH. PUMP HOUSING CLEANED PERFORMED RESISTANCE CHECK AND FOUND WITHIN LIMITS IAW SWPM 20-20-00.

ATA 7110

Part: RIVET — LOOSE (NR 1 COWLING) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 1 LT CORE COWL AFT RIB, 8 O'CLOCK, RIVET LOOSE. DRILLED OUT DAMAGED RIVET AND INSTALLED NEW RIVET IAW SRM 51-40-02.

ATA 2150

Part: CONDENSER — CRACKED (AC BAY) · airframe 89,709 hrs · 17,403 cycles

RIGHT PACK AIR CONDITIONER CONDENSER CRACKED, PN 194276-5, SN 41-2006 CONDENSER REPLACED IAW AMM 21-52-05.

ATA 5320

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 89,709 hrs · 17,403 cycles

PERFORMED OUTER CHORD DAMAGE REPAIR AT SEC 41, STA 266.5, STR 11L-12L, REF IAI NRC C0054. WORK PERFORMED IAW REA MB02012R0048, REV, NEW, DATE 16 MAY 2016. RELATED TO IAI CNV DWG 371-53-11-C3023, REV F AND IAW SRM 51-70-12.

ATA 7830

Part: BUSHING — WORN (THRUST REVERSER) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 1 RT C-DUCT, UPPER LATCH LOOSE. REPLACED KINK ASSY, REPLACED BUSHINGS. PINS THREADED AND SPACERS IAW AMM 78-31-01.

ATA 7110

Part: NUT PLATE — DAMAGED (NR 1 COWLING) · airframe 89,709 hrs · 17,403 cycles

PYLON NR 1 RIGHT CORE COWL AREA LOWER PART, NUT PLATE INSTALLED. REMOVED DAMAGED NUT PLATE AND INSTALLED NEW NUT PLATE IAW SRM 51-40-02.

ATA 2120

Part: TUBE — CRACKED (AC BAY) · airframe 89,709 hrs · 17,403 cycles

LEFT AIR CONDITION PACK HOT AIR SUPPLY TUBE, PN 220103 IS CRACKED. AIR CONDITION PACK HOT AIR SUPPLY TUBE REPLACED IAW AMM 21-51-10.

ATA 7297

Part: WIRE HARNESS — CONTAMINATED (NR 2 ENGINE) · airframe 89,709 hrs · 17,403 cycles

NR 2 ENGINE FAN AREA ELECTRICAL HARNESS DIRTY WITH OIL. CLEANED IAW AMM 72-00-00.

ATA 2130

Part: RELIEF VALVE — FAILED (CARGO BAY) · airframe 89,709 hrs · 17,403 cycles

AFT CARGO LT UPPER PRESSURE RELIEF VALVE FAIL IN TEST. REPLACED PRESSURE RELIEF VALVE IAW AMM 21-32-01.

ATA 5347

Part: SEAT TRACK — DIRTY (COCKPIT) · airframe 89,704 hrs · 17,403 cycles

PILOT SEAT HINGE FRICTION WHEN MOVING HORIZONTALLY THROUGH CORNER. PILOT SEAT TRACKS CLEANED AND LUBRICATED, CHECKED FOR OPS AND FOUND OK IAW MM 25-11-01/601.

ATA 5420

Part: SEAL — TORN (NR 2 ENGINE) · airframe 89,709 hrs · 17,403 cycles

NR 2 ENGINE RT FAN UPPER SIDE SEAL TORN. REPLACED SEAL IAW AMM 51-40-02.

ATA 7110

Part: COWLING — DAMAGED (NR 2 ENGINE) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 2 RT FAN COWL FWD AND AFT PART MISSING MATERIAL. PERFORMED FILLER AND GRAPHITE AND FIBERGLASS PLIES REPAIR ON FAN COWL. INNER SURFACE BOTH CORNERS IAW SRM 54-22-01.

ATA 2711

Part: TRIM SYSTEM — OUT OF ADJUST (AILERONS) · airframe 89,704 hrs · 17,403 cycles

AILERON TRIM-MAX TRIM TO THE LT EXCEED LIMIT 6.2, OK TO THE RT: 5.3. MAX LIMIT 5.9. DUE TO TEST TRIM ON RT WING DOWN POSITION, FOUND THE CONTROL WHEEL TURNS TO 29.4 DEGREES TO LT WING DOWN POSITION, FOUND 32.0 DEGREES RT WING DOWN 5.3 UNIT. LT WING DOWN 5.9 UNIT IAW MM 27-11-00.

ATA 7830

Part: LOCK — CORRODED (THRUST REVERSER) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 1 CORROSION FOUND ON THE RT C-DUCT LOCK. CORROSION CLEANED AND TREATED ACCY TO AMM 51-05-03.

ATA 7110

Part: BRACKET — DAMAGED (NR 2 COWLING) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 2 RT CORE COWL BRACKET. STOW PIN OF HOLD OPEN ROD DAMAGE BRACKET. ADAPTER REPLACED AMM 71-11-11.

ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 89,709 hrs · 17,403 cycles

PERFORMED EXTERNAL SKIN DAMAGE REPAIR B/T STA 1197+44 TO STA 1197+66, STR 39R-39L, REF IAI NRC M0548. THE REPAIR PERFORMED WITH DOUBLER AND FILLER IAW SRM 53-00-01, FIG 201, REPAIR 29.

ATA 2150

Part: SENSOR — FAULTY (AC BAY) · airframe 89,709 hrs · 17,403 cycles

LEFT PACK COMPRESSOR OUTLET SENSOR, TS41, FOUND FAULTY, READS HIGH RESISTANCE. OUTLET SENSOR REPLACED IAW MM 21-51-06.

ATA 7110

Part: PROTECTOR — PEELING (NR 2 COWLING) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 2 RT FAN COWL-MID OTBD PART DIVISOR MATERIAL. CHECK FAN COWL FWD L/E FOUND EDGE PROTECTOR PEELING OFF, BONDED EDGE PROTECTOR USING EA 9394 ADHESIVE PASTE IAW CMM 71-13-22.

ATA 2121

Part: COOLING FAN — BROKEN (E&E BAY) · airframe 89,709 hrs · 17,403 cycles

FWD CARGO LT ELECTRONIC EQUIPMENT BAY COOLING SUPPLY FAN BLADE IS BROKEN. COOLING SUPPLY FAN REPLACED IAW AMM 21-58-06.

ATA 3620

Part: SENSOR — FAILED (BLEED AIR SYS) · airframe 89,709 hrs · 17,403 cycles

RIGHT WING, PRV EXIT PRESSURE SENSOR, M1843, FAIL TO TEST. REPLACED RT WING PRV EXIT PRESSURE SENSOR AND TESTED IAW AMM 36-21-03.

ATA 2820

Part: HOUSING — DIRTY (PUMP) · airframe 89,709 hrs

LT WING JETTISON PUMP CTR AUXILIARY BONDING RESISTANCE BETWEEN PUMP TO WING HIGH RESISTANCE. PUMP HOUSING CLEANED AND PERFORMED RESISTANCE CHECK AND FOUND WITHIN LIMITS IAW SWPM 20-20-00.

ATA 3610

Part: CONTROLLER — FAULTY (BLEED AIR SYS) · airframe 89,709 hrs · 17,403 cycles

LEFT ENGINE HPSOV APPEARED FOR SHORT TIME ON 2-3 OCCASIONS. LT HP CONTROLLER REPLACED IAW MM 36-11-08, PN OFF 773289-15, SN OFF 861110, PN ON 773289-15, SN ON 890320.

ATA 7110

Part: COWLING — DELAMINATED (NR 2 ENGINE) · airframe 89,709 hrs · 17,403 cycles

ENGINE NR 2 FAN COWL RT INTERNAL ZONE MATERIAL DELAMINATION. REMOVED DELAMINATION SKIN FROM INBD CORNER EDGE, REPAIR WITH GRAPHITE AND FIBER PLIES IAW AMM 54-22-01.