N328EN

Part: BULB — INOPERATIVE (LIGHT SWITCH) · airframe 46,949 hrs · 68,531 cycles

EMERGENCY SWITCH LIGHT "NORM" BACK LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: BRAKE — SMOKE (NR 2) · airframe 46,475 hrs · 67,925 cycles

NR 2 BRAKE ASSEMBLY HOT AND SMOKING AT THE GATE. INSPECTED AFFECTED BRAKE AND TIRE ASSEMBLY IAW SP 32.1. NO SIGNS OF OVERHEAT OR DAMAGE FOUND. OKAY FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (AUTOFEATHER) · airframe 45,968 hrs · 67,254 cycles

AUTOFEATHER ARM LIGHT ILLUMINATED ON T/O WITH SWITCH SELECTED OFF. R & R NR 1 AND NR 2 TSCU.

Part: ANTENNA — MALFUNCTIONED (WX RADAR SYS) · airframe 45,864 hrs · 67,122 cycles

WEATHER RADAR PAINTS ONLY TO THE LEFT. R & R RADAR ANTENNA IAW WITH MM 34-41-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: RADAR — MALFUNCTIONED (WX RADAR) · airframe 45,864 hrs · 67,122 cycles

WEATHER RADAR PAINTS ONLY TO THE LEFT, COULD NOT DUPLICATE ON THE GROUND, R & R RADAR RT AS PRECAUTION IAW MM 34-41-01. OPS CHECKED GOOD.

Part: LIGHT — DISCOLORED · airframe 45,791 hrs · 67,022 cycles

ELECTRICAL ODOR IN COAT CLOSET. PERFORMED HIDDEN DAMAGE INSPECTION NO DEFECTS NOTED. CONTACTS ON WARDOBE LIGHT APPEAR SLIGHTLY DISCOLORED. DEACTIVATED IAW SP 33.1. CABIN INTERIOR NORMAL LIGHTING SYS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,645 hrs · 66,837 cycles

FRONT EMERGENCY LIGHT IS INOPERATIVE. R & R THE EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 4,531 hrs · 66,392 cycles

EMERGENCY FLOOR IS INOPERATIVE AT ROW 12. R & R BULBS, A ROW 12 EMERGENCY FLOOR PATH LIGHT. OPS CHECKED GOOD.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 45,251 hrs · 66,316 cycles

EMERGENCY LIGHTS POWERED ON AUTOMATICALLY AFTER 7 SECONDS. R & R EMERGENCY LIGHT SWITCH IAW 33-51-05. OPS CHECKED GOOD. OK FOR SERVICE.

Part: TRANSCEIVER — MALFUNCTIONED (RADAR) · airframe 44,761 hrs · 65,670 cycles

RADAR PAINTS GROUND DURING TURNS. R & R RADAR RT IAW MM 34-41-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,755 hrs · 65,663 cycles

EMERGENCY FLOOR LIGHT IS INOPERATIVE AT ROW 10DF AND 11DF. R & R BULBS AT EMERGENCY FLOOR LIGHT STRIP. OPS CHECKED GOOD.

Part: ACM — FAILED · airframe 44,262 hrs · 65,003 cycles

WITH APU RUNNING, ODOR WITH SOME HAZE ON FLIGHT DECK. MAINTENANCE FOUND ACM BAD. R & R ACM.

Part: POWER SUPPLY — WEAK (EMERGENCY LIGHT) · airframe 44,066 hrs · 64,748 cycles

AFT LT FUSELAGE EMERGENCY LIGHT IS DIM. R & R POWER SUPPLY 3351, PS3 IAW 33-51-00.

Part: MOUNT — CRACKED (EMERGENCY LIGHT) · airframe 44,066 hrs · 64,748 cycles

RIGHT FORWARD EMERGENCY EXIT SIDEWALL EMERGENCY LIGHT ASSY MOUNT BASE IS CRACKED. R & R SIDEWALL LIGHT ASSY AT RT EMERGENCY SIDEWALL ASSY.

Part: APU — MALFUNCTIONED · airframe 43,744 hrs · 64,320 cycles

APU FAILED WITH BLEEDS ON AND HEAVY FUEL ODOR. INSPECTED APU. NO EVIDENCE OF FUEL LEAKAGE. RESTARTED APU WITH BLEED ON. APU FAILS AFTER GEN SELECTED. OPS NORMAL WITH BLEEDS ONLY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,799 hrs · 63,075 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 3. R & R THE BULB, OPS CHECKED GOOD.

Part: DOOR — BINDING (LT MLG) · airframe 42,768 hrs · 63,030 cycles

AFTER RETRACTING MLG, LT AMBER GEAR DOOR LIGHT ILLUMINATED. RECYCLED GEAR, LIGHT EXTINGUISHED, AIRSPEED INCREASED TO 165 KNOTS. NOTICED LT MLG DOOR DID NOT RETRACT. REDUCED AIRSPEED TO 140 KNOTS. SELECTED GEAR DOWN, LT MLG DID NOT EXTEND. PERFORMED ALTERNATE EXTENSION. AFT GEAR DOOR FORWARD INSERT CAME LOOSE, JAMMING DOORS. SEQUENCING VALVE WOULD NOT ALLOW EXTENSION WITHOUT DOORS OPEN. ALTERNATE EXTENSION HAD TO BE UTILIZED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,650 hrs · 62,880 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 8. R & R BULBS AT ROW 8. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 42,479 hrs · 62,652 cycles

CARGO BAY SMOKE WARNING LIGHT ILLUMINATED. INSPECTED CARGO BAY, NO SMOKE DAMAGE NOTED. PERFORMED CHECK ON SMOKE DETECTORS, NR 2 WILL NOT TEST. R & R NR 2 CARGO BAY SMOKE DETECTOR IAW AMM 26-12-01. OK FOR SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (AUTOFEATHER SYS) · airframe 42,183 hrs · 62,262 cycles

AUTOFEATHER DID NOT ARM DURING TAKEOFF. R & R NR 1 TSEU. GROUND RAN ACFT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: ELECTRONIC UNIT — FAILED (AUTOFEATHER) · airframe 42,132 hrs · 62,198 cycles

ABORTED TAKEOFF AT 110KTS DUE TO AUTOFEATHER NOT ARMING AT 0AT OF 35C. R & R NR 1 AND NR 2 TSEU'S. GROUND RAN ACFT IAW RUN-UP MANUAL. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,487 hrs · 61,364 cycles

THIRD RED EMERGENCY LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-03. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (SWITCH LIGHT) · airframe 41,136 hrs

GREEN EMERGENCY SWITCH BACK-LIGHT IS INOPERATIVE. R & R GREEN EMERGENCY LIGHT SWITCH BULB AND RE-SECURED LENS.

Part: GAUGE — MALFUNCTIONED (FUEL TEMP) · airframe 41,005 hrs · 60,784 cycles

NR 1 ENGINE FUEL TEMP INDICATOR PEGGED FULL HOT. R & R FUEL TEMP GAUGE AND GROUND RAN ACFT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: THRESHOLD — CORRODED (PAX DOOR) · airframe 40,871 hrs · 60,615 cycles

PAX DOOR THRESHOLD IS CORRODED AROUND NUT PLATES. R & R PAX DOOR THRESHOLD MEMBER.

Part: SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 40,871 hrs · 60,615 cycles

CARGO DOOR FUSELAGE SURROUND HAS LOWER SILL CORRODED UNDER ANCHOR NUT. CLEANED AND BLENDED CARGO DOOR SILL IAW SRM 53-00-16. BLENDDED WITHIN LIMITS.

Part: BRACKET — CRACKED (LT NACELLE) · airframe 40,871 hrs · 60,615 cycles

LT NACELLE, PRESSURE MANIFOLD SUPPORT BRACKET IS CRACKED. R & R SUPPORT BRACKET IAW SRM 51-42-05.

Part: HINGE FITTING — CRACKED (MLG) · airframe 40,871 hrs · 60,615 cycles

RT NACELLE MLG FORWARD HINGE CRACKED IN EACH SIDE OF HINGE BLOCK. R & R CENTER DOOR INTERCOSTAL AND REPLACED WITH NEW IAW SRM 51-42-05 AND SRM 51-42-45.

Part: WIRE — CRUSHED (EMERGENCY LIGHT) · airframe 40,761 hrs · 60,464 cycles

TWO EMERGENCY LIGHTS WILL NOT ILLUMINATE AT ROW 11. FOUND WIRES CRUSHED. R & R LIGHT ASSY IAW MM 20-45-08. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMEGENCY LIGHT) · airframe 40,695 hrs · 60,374 cycles

EMERGENCY LIGHT SWITCH GREEN LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,549 hrs · 60,184 cycles

AFT EMERGENCY EXIT ESCAPE PATH LIGHT IS INOPERATIVE. R & R BULB, REINSTALLED LENS COVER. OPS CHECKED GOOD.

Part: EEC — FAILED (NR 2 ENGINE) · airframe 40,517 hrs · 60,156 cycles

NR 2 TORQUE SLOW TO ADVANCE DURING TAKEOFF ROLL. TORQUE READS 0 PERCENT AT FLIGHT IDLE. R & R NR 2 EEC PERFORMED ENG RIG WC 70-00-02Q. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 40,471 hrs · 60,104 cycles

SEVERAL FLOOR EMERGENCY LIGHTS ARE INOPERATIVE WITH 2 ADJACENT LIGHTS DAMAGED. CAPPED BROKEN FLOOR EMERGENCY LIGHT WIRES AT ROW 12 AND TEMP REPAIRED LIGHT AFT OF BROKEN WIRES AT ROW 12.

Part: MANIFOLD — FAILED (NLG STEERING) · airframe 40,161 hrs · 59,695 cycles

DURING APPROACH, AFTER GEAR EXTENSION, LOUD NOISE FROM NOSE AREA AND LOST NR 2 HYDRAULIC QTY FOLLOWED BY ISO VALVE CAUTION LIGHT, .5 QUARTS REMAINED. R & R NOSE WHEEL STEERING MANIFOLD IAW MM 32-50-16. OPS AND LEAKED CHECKED GOOD.

Part: MANIFOLD — LEAKING (NLG STEERING) · airframe 40,161 hrs · 59,695 cycles

DURING APPROACH, AFTER GEAR EXTENSION, LOUD NOISE FROM NOSE AREA WAS HEARD AND LOST NR 2 HYD QTY FOLLOWED BY ISO VALVE CAUTION LIGHT. ABOUT .5 QT REMAINS. R & R MANIFOLD IAW MM 32-50-16. OPS & LK CK GOOD SWUNG NLG SEVERAL TIMES W/O ANY ANOMOLIES.

Part: TSCU — FAILED (AUTOFEATHER) · airframe 40,108 hrs · 59,627 cycles

DURING TAKEOFF ROLL, AUTOFEATHER FAILED TO ARM. FOUND AUTOFEATHER DID NOT TEST STATICALLY. CYCLED POWER LEVERS, OPS CHECKED GOOD. R & R NR 2 TSCU IAW 72-01-10 AND INSPECTED POWER LEVER MICROSWITCHES. GROUND RAN ACFT. OPS CHECKED GOOD AT THIS TIME.

Part: CONNECTOR — DIRTY (AUTOFEATHER) · airframe 40,076 hrs · 59,589 cycles

AUTO FEATHER FAILED TO ARM DURING TAKEOFF ROLL. ABORTED TAKEOFF AT 85 KNOTS. INSPECTED AND CLEANED CONNECTORS ON NR 1 AND NR 2 TSEU. GROUND RAN ACFT, AUTO FEATHER SYS. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: RELAY — FAILED (AUTOFEATHER SYS) · airframe 40,076 hrs · 59,589 cycles

AUTOFEATHER DOES NOT TEST STATICALLY ON EITHER SIDE. R & R RELAY 6121-K5. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,864 hrs · 59,304 cycles

WHITE FLOOR EMERGENCY LIGHT INOP AT ROW 4DF. R & R BULB AT 4DF, OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 59,873 hrs · 59,316 cycles

LEFT AFT FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. REMOVED LENS, R & R BULB, AT SAID LOCATION. REINSTALLED LENS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,840 hrs · 59,278 cycles

RED EMERGENCY EXIT LIGHT IS INOP AT ROW 11. REMOVED LENS, R & R BULBS. OPS CHECKED FOOD. REINSTALLED LENS.

Part: CONNECTOR — DIRTY (TORQUE INDICATOR) · airframe 39,752 hrs · 59,172 cycles

AFTER TAKEOFF, NR 2 ENGINE HAD HIGH FUEL FLOW, NH AT 999 AND HAD A 1 KNOB POWER LEVER SPLIT TO MATCH TORQUE. GROUND RAN ACFT. FOUND TORQUE NOT INDICATING CORRECTLY. CYCLED ECU MODE SWITCH. TORQUE RETURNED TO NORMAL. CLEANED BOTH ECU CONNECTOR PLUGS. GROUND RAN ACFT. OPS CHECKED GOOD IAW SRT MANUAL. OK FOR SERVICE.

Part: BRUSH BLOCK — UNKNOWN (PROPELLER) · airframe 39,592 hrs · 58,953 cycles

EMERGENCY LIGHTS FLASH ON/OFF IN FLIGHT. R & R NR 2 BRUSH BLOCK IAW AMM 61-10-11. OPS CHECKED GOOD. GROUND RAN ACFT IAW SRT MANUAL. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 39,570 hrs · 58,926 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT 10DF. R & R BULB.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 39,504 hrs · 58,840 cycles

ON TAKEOFF ROLL, AUTO FEATHER DID NOT ARM. ATTAINED 90 PERCENT TORQUE FOR 2 TO 3 SECONDS. ABORTED TAKEOFF, CREW GROUND RAN ACFT AFTER CYCLING POWER AND CONDITION LEVERS. AUTO FEATHER ARMED AT 76 PERCENT TORQUE. PERFORMED WC 61-21-04 AUTOFEATHER CONTROLLER ENABLE SWITCH. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 39,356 hrs · 58,652 cycles

IN FLIGHT, NR 2 HYD ISO VALVE CAUTION LIGHT ILLUMINATED AND NR 2 HYD QTY WAS AT .5 QUART. NO OTHER ASSOCIATED CAUTION LIGHTS ILLUMINATED. R & R NR 2 ENGINE DRIVEN HYD PUMP IAW WC 29-00-00R. GROUND RAN ACFT. OPS AND LEAKED CHECKED GOOD. OK FOR SERVICE.

Part: TIRE — DEFLATED (MLG) · airframe 39,000 hrs · 58,183 cycles

BOTH MAIN TIRES ON RT GEAR ARE FLAT. R & R NR 3 AND NR 4 MAIN WHEEL ASSY AS REQUIRED IAW -8 MM 32-41-11.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,208 hrs · 57,154 cycles

EMERGENCY LIGHT AT CEILING AT ROW 6AC AND 6DF IS INOPERATIVE. INSTALLED NEW BULB. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,241 hrs · 55,896 cycles

LIGHTNING STRIKE TO RT SIDE OF ACFT. COMPLIED WITH LIGHTNING STRIKE INSPECTION IAW MM 05-50-31, STEPS 1-16.

Part: TERMINAL BLOCK — BURNED (APU) · airframe 37,216 hrs · 55,860 cycles

CREW STATING THAT THERE WAS A NON ELECTRICAL ODOR IN COCKPIT. MX INSPECTED COCKPIT. NO ODOR DETECTED. ODOR COMING FROM APU POWER CABLES & STUD AT FWD BULKHEAD. DEACTIVATED APU START CONTACTOR IAW SP.P 49.1. NO ODOR WITH ENGINES RUNNING & APU DEACTIVATED .

Part: SHROUD — CRACKED (NACELLE) · airframe 37,143 hrs · 55,769 cycles

AFT NACELLE FIREWALL JET PIPE SHROUD ABOVE THE JET PIPE IS CRACKED AT THE 1 O'CLOCK POSITION. REPAIRED IAW EO8-54-12-0071 FOR NR 2 NACELLE.

Part: STRUT — CHAFED (NR 2 NACELLE) · airframe 37,143 hrs · 55,769 cycles

NR 2 NACELLE OTBD LOWER ENGINE SUPPORT STRUT CHAFED AT THE OIL COOLER RETURN LINE, MEASURED AT 0.012". REPAIRED IAW RD8-54-1264. COMPLIED WITH HFEC INSP. NO DEFECTS NOTED.

Part: FIREWALL — CHAFED (NACELLE) · airframe 37,143 hrs · 55,769 cycles

FORWARD NACELLE FIREWALL OTBD SIDE REPAIR IS CHAFED ON NR 2 NACELLE. REMOVED ORIGINAL REPAIR THAT WS CHAFED. FABRICATED AND DRILLED UP NEW ONE. REPAIRED Z MEMBER IAW RD8-54-081. INSTALLED REPAIR DOUBLER Z MEMBER IAW RD8-54-081.

Part: RCCB — MALFUNCTIONED (PROP FEATHERING) · airframe 37,100 hrs · 55,713 cycles

NR 1 ALTERNATE FEATHER LIGHT DOES NOT ILLUMINATE DURING STATIC OR ENGINE RUN AUTO FEATHER TEST. R & R DIM AND TEST BOX. NO FIX. REINSTALLED ORIGINAL. R & R RCCB 6121 CB3 IAW STANDARD MX PRACTICE. GROUND RAN ACFT IAW -8 RUN UP MANUAL. OPS CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED · airframe 36,879 hrs · 55,423 cycles

TOUCHED RUNWAY WARNING LIGHT ILLUMINATED ON LANDING. ALL MX ACTION IS PENDING COMPLETION OF ACFT MX.

Part: TERMINAL — BURNED · airframe 36,319 hrs · 54,720 cycles

HOT ELECTRIC ODOR IN COCKPIT. POWERED DOWN ACFT. ODOR REDUCED. R & R APU GEN CABLE FROM 2445-K62 TO 2442-TB1 AND TERMINAL STUD 2445-TB1. OPS CHECKED GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 35,892 hrs · 54,151 cycles

RIGHT FORWARD EMERGENCY LIGHT DOOR SIGN IS INOP. R & R POWER SUPPLY AT PS2. OPS CHECKED GOOD.

Part: ENGINE — ODOR (NR 1) · airframe 35,891 hrs · 54,150 cycles

HAZE AND OILY ODOR IN CABIN AFT OF ROW 8 WTH ENGINES OFF AND APU STILL PRESENT WITH CABIN PACK SELECTED OFF. F/A AND PASSENGERS COMPLAINING. R & R NR1 ENGINE IAW WORKCARD 71-00-01 AND 71-02-02.

Part: DOUBLER — CORRODED · airframe 35,820 hrs · 54,054 cycles

MINOR SURFACE CORROSION AT THE UPPER SURFACE AT FUEL BOOST PUMP DOUBLER IN THE RT WING AT APPROX 1 O'CLOCK. REMOVED MINOR SURFACE CORROSION IAW RD8-57-1907. APPLIED ALODINE AND PRIMER TO ALL BARE METAL.

Part: PANEL — CORRODED (WING) · airframe 35,820 hrs · 54,054 cycles

PANEL 623AT HAS CORROSION ON MATING SURFACE. POLISHED MINOR SURFACE CORROSION ON PANEL 623AT. NO FURTHER DEFECTS NOTED. RE-APPLIED ALODINE CASTING TO PANEL MATING SURFACE.

Part: INDICATOR — FAILED (TE FLAPS) · airframe 35,694 hrs · 53,887 cycles

ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED WHEN ADVANCING POWER LEVERS, CYCLED FLAPS, OPS CHECKED NORMAL. COULD NOT DUPLICATE ON GROUND RUN. R & R FLAP POSITION INDICATOR. OPS CHECKED GOOD IAW 27-53-05. GROUND RAN ACFT AFTER FLAP INDICATOR REMOVAL AND REPLACEMENT. ALL TAKEOFF PARAMETERS FUNCTION NORMAL WHEN IN AND OUT. ACFT OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,726 hrs · 52,635 cycles

EMERGENCY EXIT SIGN HAS AN INOP LAMP AT ROW 11DF. R & R BULB AT SAID LOCATION. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,547 hrs · 52,417 cycles

5TH FLOOR LIGHT FROM REAR IS INOP ON THE FLOOR TRACK LIGHTING. RELAMP, OPS CHECKED GOOD IAW WORKCARD 33-50-03.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,514 hrs · 52,377 cycles

ONE RED FLOOR EMERGENCY LIGHT AT ROW 1AC IS NOT WORKING. R & R BULB. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 33,074 hrs · 50,557 cycles

NR 2 BAGGAGE SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 32,798 hrs · 50,207 cycles

FWD RED EMERGENCY FLOOR LIGHT DOES NOT WORK. FOUND BROKEN WIRE AT LIGHT MODULE. REPAIRED WIRE IAW 20-45-08.

Part: UNKNOWN — UNKNOWN · airframe 32,793 hrs · 50,201 cycles

REACHING V1 SPEED 110/115 KNOTS, ACFT FAILED TO ROTATE. REJECTED TAKEOFF. VISUALLY INSPECTED ELEVATOR, TRIM TABS, GUST LOCK CONTROL COLUMN QUADRANT CABLES UNDER COCKPIT FLOOR AND CABLE RUNS THROUGH AFT BAY TO VERTICAL STAB. CHECKED OPERATION OF ELEVATOR GUST LOCK AND TRIM TABS. ALL CONTROLS MOVE SMOOTHLY AND FREELY WITH CORRESPONDING MOVEMENT OF SURFACES. NO DEFECTS NOTED AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,288 hrs · 49,586 cycles

CEILING EMERGENCY LIGHT AT ROW 4 IS DIM. REMOVE AND REPLACE BULB, OPS CHECKED GOOD.

Part: OIL SYSTEM — LOW (NR 2 ENGINE) · airframe 31,618 hrs · 48,737 cycles

IN CRUISE FLIGHT, NR 2 ENGINE OIL FLUCTUATED BETWEEN 45-55 PSI, ASSOCIATED WITH NR 2 OIL PRESSURE WARNING LIGHT FLICKERING. PILOTS REDUCED POWER TO 60 PERCENT TORQUE AND THE OIL PRESSURE RETURNED TO NORMAL. THE ENGINE PROGRAM MANAGER WAS CONSULTED CONCERNING ENGINE LIMITATIONS, AIRCRAFT 328EN WAS WITHIN LIMITS PER PMM 05-10-00. INSPECTED NR 2 ENGINE AND FOUND TO BE 4 QTS LOW ON ENGINE OIL. CLEANED OIL PRESSURE SWITCH & TRANSMITTER CONNECTORS, INSPECTED FOR OIL LEAKS, AND ADDED FOR QTS OF OIL TO CORRECT LEVEL. NO OTHER DEFECTS NOTED AT THIS TIME. GROUND RAN ENGINE, OK FOR SERVICE AT THIS TIME.

Part: BULB — BURNED (EMERGENCY LIGHTS)

N/A FLOOR EMERGENCY LIGHT INOP AT ROW 6. REPLACED BULB, OPS CHECK GOOD. (A)

Part: WARNING HORN — FALSE ACTIVATION · airframe 29,109 hrs · 45,554 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. COMPLIED WITH WORK CARD 31-50-03Q. NO DEFECTS OR DISCREPANCIES FOUND. OPERATIONAL CHECK GOOD.

Part: TAPE — LOOSE (NACELLE) · airframe 29,081 hrs · 45,514 cycles

PAX AND F/A REPORTED SMALL FIRE COMING FROM NR 1 NACELLE , CENTER GEAR DOOR AREA. CREW PULLED FUEL OFF HANDLE, NO INDICATION ON FIRE LOOP. F/A POINTED OUT TO MX WHERE FIRE WAS REPORTED, MX FOUND A 4 INCH PIECE OF EROSION TAPE LOOSE ON STRUT, WHICH WAS A YELLOW COLOR AND WAS FLAPPING AROUND. MX INSPECTED GEAR AREA AND AREA; NO EVIDENCE OF SMOKE OR FIRE, OPENED UP ENGINE COMPARTMENT, NO DEFECTS NOTED. MX REMOVED TAPE, PERFORMED ENGINE FIRE TEST AND GROUND RAN AIRCRAFT, NO DEFECTS NOTED.

Part: WARNING SYSTEM — MALFUNCTIONED (SERVICE DOOR) · airframe 28,605 hrs · 44,916 cycles

DURING TAKEOFF ROLL THE SERVICE DOOR WARNING LIGHT ILLUMINATED. CREW ABORTED TAKEOFF. DOOR WAS CYCLED OPEN/CLOSED 2 TIMES AND PROXIMITY SENSOR RIGGING CHECKED IAW AMM 52-45-00. NO DISCREPANCIES FOUND.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 28,382 hrs · 44,653 cycles

SMELL COMING FROM SEAT 2AC OVERHEAD. DEACTIVATED SIDEWALL LIGHTING SYSTEM. REPLACED BALLAST, BULB AND LAMP HOLDER.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,947 hrs · 44,126 cycles

THE EMERGENCY LIGHTS SWITCH ON FLIGHT ATTENDANTS PANEL IS INOP. FERRIED A/C TO MDT. REMOVED AND REPLACED THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH ASSEMBLY. THE OPS CHECK WAS GOOD.

Part: TRANSMITTER — FAILED (OIL PRESSURE) · airframe 27,056 hrs · 43,032 cycles

NR 2 ENGINE OIL PRESSURE WENT TO ZERO ON TAKEOFF ROLL, ALL OTHER ENGINE PERIMETERS NORMAL, NO CAUTION LIGHTS. CHECKED OIL LEVEL, FOUND TO BE ABOVE ADD 1 QT. CLEANED C/P'S ON OIL PRESSURE S/W AND TRANSMITTER, NO FIX. SWAPPED OIL PRESSURE GAUGE IN FLT DECK, NO FIX. INSTALLED BACK IN ORIGINAL POSITION. REMOVED AND REPLACED PRESSURE TRANSMITTER GROUND RAN A/C OPS CHECK AND LEAK CHECK GOOD IAW 71-00-02. PART NUMBER TO FOLLOW.

Part: TRANSMITTER — FAULTY (NR 2 ENGINE) · airframe 27,056 hrs · 43,032 cycles

NR 2 ENGINE OIL PRESSURE WENT TO ZERO ON TAKEOFF ROLL, ALL OTHER ENGINE PERIMETERS NORMAL, NO CAUTION LIGHTS. CHECKED OIL LEVEL FOUND TO ABOVE ADD 1 QT. CLEANED C/P'S ON OIL PRESSURE S/W AND TRANSMITTER NO FIX. SWAPPED OIL PRESSURE GAUGE IN FLT DECK NO FIX. INSTALLED BACK IN ORIGINAL POSITION. (MECHANIC IN SYR SHORT SINGED AT THE LOG BOOK AT THIS POINT) REMOVED AND REPLACED PRESSURE TRANSMITTER GROUND RAN A/C OPS CHECK AND LEAK CHECK GOOD IAW 71-00-02. PART NUMBER TO FOLLOW.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,991 hrs · 42,956 cycles

EMERGENCY ESCAPE PATH LIGHTING FLOOR LIGHT NR 14 INOP. REMOVED AND REPLACED LIGHT BULB.

Part: BOLT — MISSING (PAX DOOR) · airframe 26,616 hrs · 42,495 cycles

UNABLE TO OPEN THE PAX DOOR FROM THE INSIDE. FERRYING AIRCRAFT TO CLT FOR REPAIRS. REPLACED MISSING BOLT AND WASHER THAT SUPPORTS OUTER SKIN RIGHT SIDE AT BOTTOM STEP, OPS CHECK GOOD.

Part: WIRE — CHAFED · airframe 25,165 hrs · 40,683 cycles

INFLIGHT FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, CIRCUIT BREAKER C-5 ON THE RIGHT SECONDARY BUSS POPPED (INTAKE DEFECTOR ACT 2) NO FURTHER SMOKE NOTED. FOUND WIRES NR 2331-1Q112022-2, NR 3151-4N22-2, NR 2441-10J22-2 AND NR 3021-20002M20-2 CHAFED ON CLOSET FLOOR BOARD, CUT AND REMOVED BURNED SECTION OF WIRE AND RETERMINATED USING SPLICES M81824-1-1. RESECURED WIRE BUNDLE AND ADDED TEFLON SHEET HA1417-1 ADDED PROTECT FROM CHAF C/W OPS CK OF DC GEN, T/O WARNING HORN,EXT PWR,ENG INTAKE BYPASS ALL SYS OPS CK GOOD.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 24,810 hrs · 40,249 cycles

AFTER SELECTING THE NR 1 BLEED ON THE NR 1 ENGINE TORQUE SURGED APPROX 10 PERCENT. REPLACED 2121-K1 AND 2121-K3. PROBLEM RETURNED SEE REPORT HNAA0600074.

Part: PRESSURE SWITCH — FAILED (NR 1 BLEED SYS) · airframe 24,810 hrs · 40,249 cycles

AFTER SELECTING NR 1 BLEED ON NR 1 ENGINE TORQUE SURGED APPROX 10 PERCENT FOLLOWED BY THE NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED. REMOVED AND REPLACED PRESSURE SWITCHES.

Part: SOCKET — BURNED (OVERHEAD LIGHT) · airframe 24,306 hrs · 39,604 cycles

OVERHEAD LIGHT AT ROW 3 LEFT SIDE IS SMOKING. FOUND LAMP CARRIER DAMAGED, DEACTIVATED IAW SPECIAL PROCEDURES 33.1.

Part: FUEL CONTROL — INOPERATIVE (ENGINE) · airframe 21,766 hrs · 36,363 cycles

ENGINE SHUT DOWN IN FLIGHT AND RETURNED TO GATE. REMOVED AND REPLACED MFC, OPS AND LEAK CHECK GOOD C/W WORKCARD 76-00-02Q AND TRIMMED ENGINE PER DASH 8 RUNUP MANUAL.

Part: LINE — LEAKING (BLEED SYSTEM) · airframe 20,792 hrs · 35,141 cycles

BURNING SMELL IN CABIN AREA, STRONGER AT ROW 12 AND 13 WITH NO BLEEDS SELECTED. FOUND BLEED, ROW 6, REPLACED LINE.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 19,097 hrs · 33,046 cycles

WHEN LANDING GEAR SELECTED DOWN, NOSE AND MAIN LANDING GEAR DID NOT EXTEND. ALL RED GEAR UNSAFE LIGHTS ILLUMINATED. WHEN ALTERNATE EXTENDED GEAR OPS NORMAL, GEAR DOWN LOCKED (GREEN) ILLUMINATED. MADE UNEVENTFUL LANDING. ADDITIONAL INFO IS TO FOLLOW.

Part: TAB — DAMAGED (ELEVATOR)

REPAIR TO ELEVATOR SPRING TAB TRAILING EDGE.

Part: WHEEL — SEPARATED · airframe 15,022 hrs · 27,730 cycles

ON LANDING #1 MAIN WHEEL ASSY DEPARTED THE AIRCRAFT. REPLACED WHEEL ASSY.