N329EN

Part: SWITCH — FAILED (MLG INHIBIT) · airframe 53,975 hrs · 63,760 cycles

WHEN GEAR SELECTOR HANDLE WAS PLACED IN DOWN POSITION, GEAR INDICATION WAS THREE RED AND NO DOOR INDICATION. CREW PERFORMED ALTERNATE EXTENSION AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND LANDING GEAR DOWN INHIBIT SWITCH WIRING TO BE AT FAULT. R & R THE 3261-S25 LANDING GEAR INHIBIT SWITCH. OPS CHECKED GOOD IAW WDM 32-30-01.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 53,947 hrs · 63,722 cycles

GEAR DID NOT EXTEND AFTER HANDLE SELECTION. CREW INTIATED A GO AROUND AND APROXIMATELY 30 SECONDS AFTER HANDLE SELECTION GEAR CAME DOWN AND LOCKED. UNSAFE INDICATION UNTIL GEAR CAME DOWN AND LOCKED. R & R THE LANDING GEAR SELECTOR VALVE IAW WC 32-30-41R, OPS CHECKED GOOD.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR) · airframe 53,802 hrs · 63,529 cycles

WEATHER RADAR WILL NOT PAINT. REMOVED AND REPLACED THE WEATHER RADAR R/T, OPS CHECKED GOOD IAW MM 34-41-01. OK FOR SERVICE.

Part: INDICATOR — FAILED (VSI/TRA) · airframe 53,482 hrs · 63,143 cycles

CAPTAIN`S TCAS DISPLAY WENT BLANK, CIRCUIT BREAKER TRIPPED. INDICATOR PRODUCED SMOKE. VERTICAL SPEED INDICATOR. R & R THE CAPTAIN'S VSI/TRA INDICATOR. OPS CHECKED GOOD IAW AMM 34-47-02.

Part: WARNING LIGHT — FALSE ACTIVATION (SERVICE DOOR) · airframe 53,335 hrs · 62,951 cycles

WARNING LIGHT ILLUMINATED ON TAKE-OFF FOR SERVICE DOOR. INSPECTED DOOR AND HANDLE OPERATED SEVERAL TIMES. NO FAULTS FOUND. OK FOR SERVICE

Part: TIRE — FAILED (MLG) · airframe 5,272,830 hrs · 62,146 cycles

TIRE BLOWN ON TAKE OFF. CONTINUED TO DESTINATION AND LANDED SAFELY. PERFORMED INSPECTION OF ALL MAIN TIRES. R & R.

Part: FIRE WARNING — FALSE ACTIVATION (APU BAY) · airframe 52,558 hrs · 61,927 cycles

APU FAILED. GAVE FIRE DETECTION WARNING LIGHT, RED DISC POPPED ON TAIL. APU FIRE EXTINGUISHING SYSTEM. INSPECTED APU BAY NO SIGN OF FIRE. FIRE BOTTLE EMPTY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 51,899 hrs · 61,072 cycles

EMERGENCY LIGHTS ARE DIM AND MULTIPLE LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACKS IAW 33-50-05R AND 33-50-03Q. OPS CHECKED GOOD.

Part: WARNING HORN — FALSE ACTIVATION · airframe 51,667 hrs · 60,779 cycles

TAKEOFF WARNING HORN SOUNDED WHEN POWER LEVER ADVANCED. FLAPS WERE CYCLED HORN EXTINGUISHED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 51,638 hrs · 60,740 cycles

REJECTED TAKEOFF DUE TO WARNING HORN SOUNDING CYCLE FLAPS FROM 5 TO 10 AND BACK TO 5, OPS NORMAL AT THIS TIME. C/W WITH CARD 31-50-03, TAKEOFF WARNING SYS. OPS CHECK, NO DEFECTS NOTED, CLEAR MEL.

Part: PRESSURE SWITCH — DEFECTIVE (HYDRAULIC SYS) · airframe 54,014 hrs · 63,790 cycles

AFTER ENGINE START ROLL SPOILER INBD HYDRAULIC C/IL ILLUMINATED. CYCLED FLIGHT CONTROL SPOILER 1 SWITCH. CAUTION LIGHT EXTINGUISHED. R & R INBD SPOILER HYD PRESSURE SWITCH. GROUND RAN ACFT. LEAK AND OPS CHECK GOOD.

Part: AHRS — MALFUNCTIONED (NR 2) · airframe 51,498 hrs · 60,566 cycles

ON CLIMBOUT, FO YAW DAMPER KICKED OFF AND ADI ROLLED OVER. ADI SELF CLEARED ON GROUND. NR 2 AHRS R & R. YAW DAMPER OPS GOOD IAW MM 22-10-06. NR 2 ADI OPS GOOD IAW MM 34-27-01.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,577 hrs · 59,378 cycles

CABIN EMERGENCY EXIT SIDEWALL LIGHTING IS DIM AT ROW 11AC. R & R BULBS IN EMERGENCY EXIT SIDEWALL LIGHT, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,577 hrs · 59,378 cycles

CABIN FLOOR EMERGENCY EXIT LIGHTING IS INOPERATIVE AT ROW 10. R & R BULBS. OPS CHECKED GOOD.

Part: STARTER GEN — FAILED (NR 2) · airframe 50,042 hrs · 58,661 cycles

NR 2 DC GENERATOR CAUTION LIGHT ILLUMINATED AND STAYED ON. R & R NR 2 START GENERATOR. IAW WC 24-30-02R. OPS AND LEAKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,033 hrs · 54,651 cycles

EMERGENCY FLOOR LIGHT DOES NOT ILLUMINATE IN ROW 1. R & R BULBS IN EMERGENCY FLOOR PATH LIGHT, OPS CHECKED GOOD.

Part: PROPELLER — VIBRATION (NR 2) · airframe 50,042 hrs · 58,661 cycles

SHORTLY AFTER ROTATION, EXPERIENCED STRONG VIBRATION, NR 2 PROP ASSY. RETURNED IMMEDIATELY TO THE FIELD. ON ROLLOUT, GOT NR 2 DC GEN CAUTION LIGHT. ON TAXI WAY SHUTDOWN NR 2 ENGINE. ALL ENGINE AND PROP PARAMETERS GOOD.

Part: BEARING — FAILED (NR 2 WHEEL) · airframe 50,007 hrs · 58,618 cycles

NR 2 WHEEL ASSY HAD FLAMES DURING TAXI PHASE. FIE WENT OUT ON IT'S OWN. INSPECTED AND FOUND WHEEL BEARING FAILURE. R & R BAKE AND NR 2 MAIN WHEEL ASSY IAW MM 32-41-11. NO FIE DAMAGE DURING INSPECTION AND COMPLIED WITH MM 05-50-17.

Part: CONNECTOR — DIRTY (AUTOFEATHER SYS) · airframe 49,228 hrs · 57,641 cycles

AUTOFEATHER FAILED TO ARM ON TAKEOFF. REMOVED, CLEANED AND REINSTALLED CONNECTORS ON BOTH TSU'S. OPS CHECK OF AUTOFEATHER SYSTEM GOOD IAW -8 RUN UP MANUAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,018 hrs · 57,350 cycles

4TH EMERGENCY ESCAPE FLOOR PATH LIGHT IS INOPERATIVE. R & R BULB AT 4TH EMERGENCY FLOOR PATH LIGHT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,018 hrs · 57,350 cycles

5TH EMERGENCY ESCAPE PATH FLOOR LIGHT FROM MOST AFT POSITION IS INOPERATIVE. R & R 5TH EMERGENCY ESCAPE FLOOR PATH LIGHT. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 48,960 hrs · 57,268 cycles

EMERGENCY LIGHTS ARE NOT ILLUMINATED WITH F/A SWITCH. FOUND CONNECTOR 3351, P33, WIRES 5A22, PIN 3 AND 10A22, PIN 6 SWAPPED AND WIRES 16B22, PIN 7 AND 2G22, PIN 8 SWAPPED. INSTALLED ALL WIRES IN CORRECT POSITION IAW 33-51-00. OPS CHECKED GOOD.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 48,887 hrs · 57,170 cycles

DURING TAKEOFF ROLL, AUTOFEATHER WOULD NOT ARM. REJECTED TAKEOFF. POWER DOWN, POWER UP ACFT. CREW CYCLED POWER LEVERS THROUGHOUT RANGE AND GROUND RAN ACFT. AUTOFEATHER SYSTEM, OPS CHECKED NORMAL.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 48,773 hrs · 57,016 cycles

AUTOFEATHER DID NOT ARM DURING TAKEOFF ROLL. POWER DOWN AND POWER UP. OPS CHECKED GOOD ON MAINTENANCE ENGINE RUN.

Part: RELAY — INOPERATIVE (AUTOFEATHER SYS) · airframe 48,781 hrs · 57,030 cycles

AUTOFEATHER WILL NOT ARM ON TAKEOFF ROLL. R & R RELAY 6121-K5. GROUND RAN ACFT IAW MAINTENANCE RUN UP MANUAL. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,511 hrs · 56,660 cycles

4TH FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE. R & R BULB FOR FLOOR PATH EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,461 hrs · 56,597 cycles

LOWER SIDEWALL EMERGENCY LIGHT IS DIM AT ROW 11DF. R & R BULBS FOR LOWER EMERGENCY SIDEWALL LIGHT AT ROW 11DF. OPS CHECKED GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 48,154 hrs · 56,196 cycles

ALL EMERGENCY LIGHTS WILL NOT EXTINGUISH. R & R BATTERY POWER SUPPLY AT PS-6 IAW 33-51-05. OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 48,090 hrs · 56,108 cycles

EMERGENCY EXIT LIGHT IS DIM ON FLOOR BY AIRSTAIR DOOR. R & R BULB. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,063 hrs · 56,076 cycles

EMERGENCY LIGHT BATTERY IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,063 hrs · 56,076 cycles

FORWARD CEILING EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: FITTING — FAILED (RUDDER PEDALS) · airframe 48,024 hrs · 56,020 cycles

WITH OR WITHOUT ENGINES RUNNING, BOTH CAPS AND F/O'S RUDDER PEDALS BIND. GRINDING NOTICE IS HEARD WHEN MOVING PEDALS. FOUND TOP FITTING ON RUDDER PEDAL ADJUSTMENT ASSY FAILED. ALLOWED ASSY TO SAG FORWARD, ALLOWING ASSY TO SCRAPE ON FORWARD PRESSURE BULKHEAD.

Part: WARNING HORN — FALSE ACTIVATION (MLG) · airframe 47,901 hrs · 55,845 cycles

AFTER TAKEOFF, LANDING GEAR SOUNDED INTERMITTENTLY UNTIL GEAR WAS UP AND LOCKED. GEAR EXTENSION WAS NORMAL. OPS CHECKED PE WC 32-60-00. COULD NOT DUPLICATE. R & R SWITCHES 3261-S23 AND 3261-S24 FOR MAINTENANCE CONVENIENCE. OPS CHECKED GOOD.

Part: CONTROL HANDLE — MALFUNCTIONED (MLG) · airframe 47,895 hrs · 55,836 cycles

GEAR WARNING HORN SOUNDED ABOUT 20 SECONDS AFTER GEAR RETRACTED. ALL ADVISORY LIGHTS SHOW NORMAL, HORN STOPS AFTER SOUNDING THE SECOND TIME. PERFORMED LANDING GEAR HORN OPS CHECK IAW 32-30-01. R & R LANDING GEAR CONTROL PANEL AND RELAY 3151-K1. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,869 hrs · 55,802 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 13. R & R LIGHT ASSY, SPLICED WIRES IAW MM 20-45-07.

Part: INVERTER — ODOR · airframe 4,696 hrs · 54,605 cycles

PASSENGER CABIN HAS STRONG UNDESIRABLE ODOR. R & R SECONDAY INVERTER IAW MM 24-22-01. OPS CHECKED GOOD. NO NOTICEABLE ODOR. OK FOR SERVICE.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 46,786 hrs · 54,387 cycles

EMERGENCY SIDEWALL LIGHT DIM AT ROW 2DF. R & R BULB AT EMERGENCY LIGHT SIDEWALL ROW 2DF. OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 46,656 hrs · 54,228 cycles

EMERGENCY LIGHT BY PAX DOOR IS DIM. R & R BULBS AT EMERGENCY LIGHT BY PAX DOOR. OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 46,597 hrs · 54,166 cycles

EMERGENCY LOWER SIDEWALL LIGHT IS DIM A ROW 2DF. R & R BULBS IN EMERGENCY LIGHT LOWER SIDEWALL PANEL IN ROW 2DF. OPS CHECKED GOOD.

Part: HINGE FITTING — CORRODED (RUDDER) · corrosion level 2 · airframe 46,366 hrs · 53,861 cycles

RUDDER, LOWER HINGE, CORRODED INSIDE BEARING INNER RACE. RUDDER HINGE FITTING R & R IAW RD8-55-164.

Part: SEAT TRACK — CORRODED (BS 577) · corrosion level 2 · airframe 46,366 hrs · 53,861 cycles

RT INBD SEAT TRACK AT BS 577 CORRODED OUT OF LIMITS IAW RD8-53-833. REPLACED SECTION BETWEEN BS 560 AND 591.3 IAW RD8-53-3886, RD8-53-4472, ESR8-20-12-001, AND SRM 51-20-36.

Part: SEAT TRACK — CORRODED (BS 588-661) · corrosion level 2 · airframe 46,366 hrs · 53,861 cycles

LEFT INBD SEAT TRACK HAS BARE METAL FOUND BETWEEN BS 588 AND 661. AFTER INVESTIGATION, SEAT TRACKCORRODED OUT OF LIMITS. R & R SECTION IAW RD8-53-4472 SRM 51-42-05, AND AMM20-14-01 AND DWG 85330115

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,250 hrs · 53,727 cycles

EMERGENCY LIGHT ON FORWARD ENTRANCE BULKHEAD IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: LIGHT — BROKEN (ROW 11F) · airframe 46,187 hrs · 53,656 cycles

EMERGENCY EXIT LIGHT ASSEMBLY IS BROKEN AT ROW 11F LOWER SIDEWALL. R & R LIGHT ASSY. OPS CHECKED GOOD.

Part: BLEED AIR SYS — HAZE (APU) · airframe 46,007 hrs · 53,424 cycles

APU BLEED SELECTED, FLIGHT DECK FILLED WITH BLUE HAZE. MAINTENANCE ISOLATED TO APU BLEED.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,972 hrs · 53,382 cycles

CREW REPORTS OIL ODOR IN APU BLEEDS AND LAV SMOKE DETECTOR GOING OFF. GROUND RAN ACFT WITH APU BLEEDS. ODOR DISIPATED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,922 hrs · 53,317 cycles

28TH FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: VALVE — ODOR (BLEED SYSTEM) · airframe 45,707 hrs · 53,060 cycles

FAINT ODOR IN CABIN WHEN BLEEDS SELECTED ON. FOUND GUIDE PIN FOR NR 1 ENGINE AIR SWITCHING VALVE TWISTED AND CHAFED INTO HOUSING. R & R AIR SWITCHING VALVE IAW MM 72-30-00.

Part: INVERTER — ODOR (COCKPIT) · airframe 45,562 hrs · 52,874 cycles

STRONG FISH ODOR IN COCKPIT. R & R PRIMARY INVERTER 400HZ IAW 24-22-01, OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 45,402 hrs · 52,667 cycles

CEILING EMERGENCY LIGHT IS DIM AT ROW 7. REMOVED LENS, R & R BULB. OPS CHECKED GOOD. REINSTALLED LENS.

Part: ACM — ODOR · airframe 45,389 hrs · 52,651 cycles

FLIGHT COMPARTMENT PACK NOISY WITH ODD ODOR IN AUTO AND MANUAL. MX INSPECTED AND FOUND ACM TO BE FAULTY AND NOT WORKING. THE ODOR DISSAPATED. R & R ACM IAW WC 21-50-03. OPS AND LEAKED CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 45,249 hrs · 52,465 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 8DF. R & R BULB IAW 33-51-03. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 45,249 hrs · 52,465 cycles

CEILING EMERGENCY LIGHT IS INOPERATIVE AT ROW 4. R & R BULB, OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (FUEL SYS) · airframe 44,979 hrs · 52,113 cycles

NR 2 FUEL VALVE OPEN ADVISORY LIGHT IS INOPERATIVE. SLAVED IN FUEL VALVE, NO FIX. R & R ADVISORY LIGHTS DIM AND TEST BOX. OPS CHECKED GOOD.

Part: SOCKET — BURNED (CABIN LIGHTS) · airframe 44,971 hrs · 52,102 cycles

ELECTRICAL ODOR IN FWD CABIN AREA. INSPECTED AND FOUND LIGHT SOCKET AT 3AC BURNED. DEACTIVATED IAW SP33.1. CIRCUIT BREAKERS B1, P3 AND Q3 WERE PULLED AND COLLARD. LIGHTS WILL BE CHANGED.

Part: GENERATOR — MALFUNCTIONED · airframe 44,786 hrs · 51,869 cycles

LIGHTNING STRIKE IN CRUISE FLIGHT. BOTH DC GENERATORS WENT OFF LINE, DID RESET. COMPLIED WITH WC 05-51-31I AND 05-50-31I.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 44,722 hrs · 51,781 cycles

EMERGENCY FLOOR LIGHT IS INOPRATIVE AT GALLEY. R & R BULB. OPS CHECKED GOOD.

Part: SOCKET — BURNED (GALLEY) · airframe 44,513 hrs · 51,509 cycles

F/A SELECTED GALLEY LIGHT ON, WHICH WAS FOLLOWED BY SMOKE IN GALLEY AREA. INSPECTED GALLEY LIGHT ASSY. NO DEFECTS, BUT FOUND HOT JUG LID NOT SECURED PROPERLY AND HOT JUG SOCKET BURNED. R & R HOT JUG AND SOCKET ASSY. OPS CHECKED GOOD. ALSO PERFORMED HIDDEN DAMAGE INSPECTION OF GALLEY AREA AND BAGGAGE COMPARTMENT DAMAGE. NO DEFECTS NOTED AT THIS TIME.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 44,463 hrs · 51,441 cycles

EMERGENCY FLOOR LIGHT AT ROW 5DF IS INOPERATIVE. R & R EMERGENY FLOOR LIGHT AT ROW 5DF, RESECURED LENS, OPS CK GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 43,976 hrs · 50,788 cycles

EMERGENCY FLOOR LIGHT AT ROW 2DF, 4TH FROM BACK IS INOPERATIVE. R & R EMERGENCY FLOOR LIGHT AT ROW 2DF. RESECURED LENS. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 43,940 hrs · 50,748 cycles

EMERGENCY FLOOR LIGHT AT ROW 12 IS INOP. R & R BULB AT EMERGENCY FLOOR LIGHT AT ROW 12. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHTS) · airframe 43,333 hrs · 49,937 cycles

ROW 4 EMERGENCY FLOOR PATH LIGHT HAS LIGHT INOPERATIVE. REMOVED LENS, R & R BULB, REINSTALLED LENS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,960 hrs · 49,463 cycles

ROW 11DF SIDEWALL EMERGENCY LIGHT HAS 1 BULB INOPERATIVE. R & R BULB WITH NEW. OPS CHECKED GOOD.

Part: AHRS — FAILED (COCKPIT) · airframe 42,409 hrs · 48,699 cycles

NR 2 AHRS FAILED AFTER TAKEOFF. FLAGGED ON F/O ADI AND HSI AND CAPT'S RMI. R & R NR 2 AHRS IAW -8 MM34-20-01. OPS CHECKED GOOD. OK FOR CONTINUED SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 42,294 hrs · 48,554 cycles

EXIT LIGHT ON LOWER PORTION OF EMERGENCY EXIT DOOR IN ROW 11DF HAS A BULB INOPERATIVE. R & R BULB IN EMERGENCY EXIT LIGHT IN ROW 11DF. OPS CHECKED GOOD.

Part: INDICATION SYS — MALFUNCTIONED · airframe 42,176 hrs · 48,397 cycles

NR 1 NL INDICATOR EXCEEDED LIMITATIONS ON TAKEOFF ROLL. ABORTED TAKEOFF, ACFT RETURNED TO GATE WITH OUT CALLING MX FIRST. INDICATOR WAS R & R PRIOR TO DEPARTURE. SLAVED IN NEW NL GAUGE, NO FIX. R & R NL PROBE IAW MM 72-01-60.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,091 hrs · 48,286 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 5. R & R EMERGENCY FLOOR PATH LIGHT LAMP AND CLOSED ACCESS PANEL.

Part: LINE — DAMAGED (NR 3 BRAKE) · airframe 42,028 hrs · 48,204 cycles

ACFT ROLLOUT WITH LOSS OF PARK BRAKE PRESSURE AND FLUID LEAK AT THE FRONT OF LANDING GEAR DUE TO BIRD STRIKE TO NR 2 GEAR ON LANDING ROLLOUT. INSPECTED AND FOUND NR 3 BRAKE LINE DAMAGE AT FITTING ON BRAKE ASSY. R & R NR 3 MAIN WHEEL ASSY, NR 3 BRAKE ASSY AND BRAKE HOSES FOR NR 3 AND NR 4 HOSES. REPLENISHED HYD FLUID, OPS AND LEAKED CHECKED. OK FOR SERVICE. IAW 8 MM 32-42-11, 32-41-11 AND BIRD STRIKE INSP 05-50-26. NO DEFECTS NOTED DURING BIRD INSP.

Part: PROPELLER — NOISY (NR 1) · airframe 41,907 hrs · 48,050 cycles

NR 1 PROPELLER MAKING NOISE IN BLADES WHEN TURNED BY HAND. R & R NR 1 PROPELLER ASSY IAW WORKCARD 61-10-06R.

Part: DRAIN — OBSTRUCTED (PITOT TUBE) · airframe 41,840 hrs · 47,971 cycles

PITOT NR 1 HEATER CIRCUIT BREAKER H6 POPPED FOLLOWED BY PITO NR 2 CIRCUIT BREAKER N4 POPPED IN FLIGHT, DURING -15 DEGREES LIGHT PRECIPATION. INSPECTED BOTH PITOT PROBES AND ELECTRICAL CONNECTIONS AT PROBE. RIGHT PROBE FOUND TO HAVE BLOCKED DRAIN HOLE. REPLACED RIGHT PITOT PROBE. F/O PITOT SYS LEAK CHECKED GOOD IAW MM 34-11-13.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 41,515 hrs · 47,538 cycles

EMERGENCY EXIT SIGN AT EMERGENCY EXIT DOOR 11DF HAS BULB INOPERATIVE. R & R BULB IN EMERGENCY EXIT SIGN AT 11DF. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 41,166 hrs · 47,117 cycles

EXIT SIGN AT EMERGENCY EXIT DOOR AT ROW 2DF HAS A BULB INOPERATIVE. R & R BULB FOR EMERGENCY EXIT DOOR SIGN AT SEAT 2F.

Part: PLATE — CORRODED (PAX DOOR) · airframe 40,812 hrs · 46,682 cycles

FWD AIRSTAIR BACKING PLATE CORRODED. FRABRICATED BACKING PLATE IAW SAMPLE AND DWG 85210303.

Part: CARGO TRACK — CORRODED (BS 588-658) · airframe 40,812 hrs · 46,682 cycles

CORROSION ON LT CARGO SEAT RAIL BETWEEN STA X588 AND X658. BLENDED CORROSION FROM LT INBD SEAT TRACK IAW RD8-53-4936. COMPLIED WITH HFEC INSP. NO DEFECTS NOTED.

Part: CARGO TRACK — CORRODED (BS 588-658) · airframe 40,812 hrs · 46,682 cycles

SURFACE CORROSION ON RT CARGO SEAT RAIL BETWEEN STA X588 AND X658. BLENDED RT CARGO SEAT RAIL. BLENDED SURFACE WITHIN LIMITS IAW RD8-53-4936. COMPLIED WITH HFEC INSP, NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (BS 197) · airframe 40,812 hrs · 46,682 cycles

CORROSION ON LT INBD SEAT TRACK BETWEEN STA 197 AND X588. BLENDED SEAT TRACK TO WITHIN LIMITS, COMPLIED WITH HFEC AND IAW RD8-53-833. NO DEFECTS NOTED.

Part: FLOOR SUPPORT — CORRODED (BS 593-611) · airframe 40,812 hrs · 46,682 cycles

SURFACE CORROSION FOUND UNDER FLOOR AT SRE 26 AND 27 RT BETWEEN STA 611.50 AND STA 593.50. R & R FLOOR SUPPORT AND 2 JOINT ANGLES WITH NEW PARTS. REMOVED SURFACE CORROSION AND REPROTECTED IAW SRM 51-20-11.

Part: INTERCOSTAL — CORRODED (BS 550-593) · airframe 40,812 hrs · 46,682 cycles

FOUND CORROSION UNDER FLOOR AT STR 27 BETWEEN BS 550 AND 593. R & R INTERCOSTAL AND JOINT ANGLE IAW DWG 85333661,85333667 AND 85333726.

Part: SKIN — CORRODED (LT STAB) · airframe 40,812 hrs · 46,682 cycles

SURFACE CORROSION FOUND ON LT STAB INBD L/E BONDING STRAP. REMOVED CORROSION ON BONDING STRAP OF LT HORIZONTAL STAB INBD L/E. FOUND TO BE WITH IAW SRM 57-10-16.

Part: SEAT TRACK — CORRODED · airframe 40,812 hrs · 46,682 cycles

SURFACE CORROSION ON SURFACE OF LT OTBD SEAT TRACK BETWEEN FS 567 AND 607. LT SEAT TRACK BLENDED WITHIN LIMITS. COMPLIED WITH HFEC INSPECTION. NO DEFECTS NOTED IAW RD8-53-3644.

Part: DRAIN — CORRODED (LAVATORY) · airframe 40,812 hrs · 46,682 cycles

TOILET HEAD ASSY DRAIN CORRODED AT FS180 UNDER CENTER FLOOR. R & R TOILET HEAD DRAIN ASSY.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,812 hrs · 46,682 cycles

FOUND SURFACE CORROSION ON RT OTBD SEAT TRACK BETWEEN FS152 AND 170. BLENDED AND FOUND TO BE WITHIN LIMITS IAW RD8-53-831. COMPLIED WITH HFEC INSP ON REWORKED AREAS IAW RD8-53-831. NO DEFECTS NOTED.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 40,812 hrs · 46,682 cycles

FOUND CORROSION ON PAX DOOR THRESHOLD. PAX DOOR THRESHOLD REPLACED AND INSTALLED WITH SOLID RIVETS IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (BS 197-588) · airframe 40,812 hrs · 46,682 cycles

SURFACE CORROSION FOUND ON RT INBD SEAT TRACK BETWEEN FS197 TO 588. SEAT TRACK WAS BLENDED WITHIN LIMITS IAW RD8-53-833. COMPLIED WITH HFEC INSP. NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED · airframe 40,812 hrs · 46,682 cycles

FOUND SURFACE CORROSION ON LT OTBD SEAT TRACK BETWEEN FS 199 AND 566. BLENDED CORROSION ON LT SEAT TRACK. COMPLIED WITH HFEC INSP AND NO DEFECTS NOTED IAW RD8-53-831.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,812 hrs · 46,682 cycles

SURFACE CORROSION FOUND ON RT OTBD SEAT TRACK BETWEEN FS196 AND 566. BLENDED RT OTBD SEAT TRACK AND FOUND TO BE WITH LIMITS IAW RD8-53-831. COMPLIED WITH HFEC INSP ON REWORKED AREA, NO CRACKS FOUND.

Part: SEAT TRACK — CORRODED · airframe 40,812 hrs · 46,682 cycles

FOUND SURFACE CORROSION ON RT OTBD SEAT TRACK BETWEEN FS567 AND 607. BLENDED SURFACE ON RT OTBD SEAT TRACK. FOUND TO BE WITH LIMITS. COMPLIED WITH HFEC INSP. NO CRACKS FOUND IAW RD8-53-3644.

Part: PANEL — CORRODED (RT WING) · airframe 40,812 hrs · 46,682 cycles

RT WING PANEL 262MT INSERTS ARE CORRODED BEYOND LIMITS. R & R INSERTS IN RT WING PANEL 262MT IAW SRM 51-20-71.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 40,692 hrs · 46,540 cycles

EMERGENCY FLOOR PATH LIGHT INOPERATIVE. R & R EMERGENCY FLOOR PATH LIGHT BULB.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 40,602 hrs · 46,440 cycles

WITH POWER OFF, OVERHEAD EMERGENCY LIGHT AT ROW 11 AND ONE EXTERIOR LIGHT ON RT FUSELAGE ILLUMINATED. ALL OTHER LIGHTS ARE OFF. R & R POWER SUPPLY FOR EMERGENCY BATTERY PS4. OPS CHECKED GOOD IAW AMM 33-51-05.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 40,372 hrs · 46,138 cycles

ROW 1 MOST FORWARD RED EMERGENCY FLOOR LIGHT IS INOP. RELAMP EMERGENCY MOST FORWARD FLOOR LIGHT ,OPS CHECKED GOOD.

Part: RELAY — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 39,771 hrs · 45,368 cycles

ABORTED TAKEOFF, AUTOFEATHER D/N ARMED. DURING RUN UP A/F ARMED HIGHER PLA. (2ND ATTEMPT) R & R AUTOFEATHER ARM RELAY 6121K5 IAW STANDARD MX PRACTICES. CONFIRMED AUTO FEATHER RIGGING GOOD IAW MM 76-10-15. RAN ACFT AND VERIFIED PROPER OPS OF AUTOFEATHER IAW 61-26-00. AUTOFEATHER ARMS AT 31 PERCENT PLA AND 7 PERCENT TORQUE (1) 31 PERCENT PLA AND 71 PERCENT TORQUE (2) OPS CHECKED GOOD, CLEARED MEL.

Part: TARGET — MISSING (MLG WOW) · airframe 39,082 hrs · 44,490 cycles

WOW CAUTION LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. INSPECTED WOW SYS AND FOUND NLG LT WOW SENSOR TARGET MISSING. INSTALLED TARGET IAW CMM32-20-01. OK FOR SERVICE AT THIS TIME.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 39,075 hrs · 44,483 cycles

ROW 8, EMERGENCY LIGHT NOT POSITIONED PROPERTLY. REPOSITIONED FLOOR EMERGENCY LIGHT AT ROW 8 TO IT'S CORRECT POSITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,399 hrs · 43,629 cycles

EMERGENCY CEILING LIGHT AT ROW 9 AND 12 INOP. R & R BATTERY AT POSITION PS6. OPS CHECK GOOD.

Part: APU — LEAKING · airframe 37,745 hrs · 42,818 cycles

KEROSENE/ OIL SMELL IN CABIN AT AFT SECTION OF CABIN. R & R APU IAW WORK CARD 49-20-02X. OPS AND LEAKED CHECKED GOOD. NO OIL OR FUEL SMELL IN APU BLEED AIR.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,658 hrs · 42,711 cycles

ROW 4 FWD FLOOR EMERGENCY PATH LIGHT INOP. R & R BULB IN PATH LIGHT. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,600 hrs · 42,635 cycles

PAX DOOR EMERGENCY LIGHT HAVE 3 LIGHT BULBS NOT WORKING. REMOVED AND REPLACED BULBS IN ACCORDANCE WITH 33-20-00.

Part: SEAL — DIRTY (PAX DOOR) · airframe 37,594 hrs · 42,627 cycles

EXCESSIVE PRESSURIZATION LEAK AND LOUD NOISE COMING FROM PAX DOOR. CLEANED AND PRESSURE CHECKED PAX DOOR SEAL AND RIGHT FORWARD EMERGENCY EXIT DOOR, GROUND RAN AIRCRAFT TO MAX DIFFERENTIAL. NO LEAKS NOTED.

Part: AHRS — FAILED (ZONE 200) · airframe 37,298 hrs · 42,256 cycles

NR 1 AHARS FAILED IN FLIGHT, AHRS INVALID MESSAGE, ROLL PITCH AND HD HARD FAILED. R & R NR1 AHRS IAW MM34-30-01. CHECKED GOOD.

Part: CONTROLLER — INTERMITTENT (EMERGENCY LIGHTS) · airframe 37,219 hrs · 42,156 cycles

WHEN EMERGENCY LIGHT SELECTED ON THEY STAY ON AND TURN OFF AFTER A FEW SECONDS, WHEN LIGHTS ARE SELECTED OFF, THEY REMAINED ON. R & R LIGHT CONTROLLER AS REQUIRED IAW CMM 33-10-52.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 37,219 hrs · 42,156 cycles

F/A EMERGENCY LIGHT SWITCH NOT WORKING. R & R EMERGENCY LIGHT SWITCH AS REQUIRED.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,654 hrs · 41,979 cycles

1 RT FLOOR EMERGENCY FLOOR LIGHT IS INOPERATIVE. R & R LIGHT MODULE, INSTALLED WITH ENVIRONMENTAL SPLICES, OPS CKD GOOD.

Part: CONTROL BOX — FAILED (EMERGENCY LIGHT) · airframe 36,951 hrs · 41,835 cycles

EMERGENCY LIGHTS FLICKERING IN FLIGHT. REMOVED AND REPLACED LIGHT CONTROL BOX, OPS CHECKED GOOD, IAW 33-51-05.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 36,949 hrs · 41,833 cycles

FIRST 2 FLOOR EMERGENCY LIGHTS ARE OPERATIONAL. REMOVED AND REPLACED BATTERY AT 3352-PS1 AND SECURED WITH ATTACHING CAM LOCS.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 36,557 hrs · 41,343 cycles

CABIN EMERGENCY LIGHTS FLICKER. FOUND CABIN LIGHTS GOING TO PS4 E BATTERY POWER PACK OUT AND FLICKERING. REMOVED AND REPLACED POWER SUPPLY AND BATTERY AT PS4. ALSO FOUND WIRE 3351-15D22 PULLED OUT OF BUTT SPLICE IN WARDROBE ADJACENT TO EMERGENCY. LT CONTROL BOX. INSTALLED ENVIRONMENTAL BUTT SPLICES, REMOVED AND REPLACED ALL 7 EMERGENCY. LIGHT BATTERIES. PERFORMED DIODE CK. OPS CK GOOD IAW.

Part: CONTROL BOX — INTERMITTENT (EMERGENCY LIGHTS) · airframe 36,555 hrs · 41,341 cycles

EMERGENCY LIGHTS FLICKERED IN FLIGHT. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL BOX. NO FIX. FOUND BROKEN WIRE AT DIODE CR5, REMOVED AND REPLACED DIODE. OPS CHECKED GOOD, IAW 33-51-00.

Part: SIGN — INTERMITTENT (EMERGENCY LIGHTS) · airframe 36,527 hrs · 41,307 cycles

MAIN OVERHEAD EMERGENCY EXIT SIGN AT ROW 11 FLICKERED. EVALUATED CONNECTION IN LAMP, SECURED AND NO EVIDENCE OF DEFECT NOTED. OPS CHECKED NORMAL AT THIS TIME.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (PROPELLER) · airframe 36,506 hrs · 41,281 cycles

EMERGENCY LIGHTS FLICKER IN FLIGHT. REMOVED AND REPLACED NR 2 BRUSH BLOCK AND CLEANED CONNECTOR AND SLIP RINGS FOR T/S. GROUND RAN, OPS CHECKED GOOD FOR PROP HEAT OPERATION, EMERGENCY LIGHTS DID NOT FLICKER, OPS CHECK OK FOR SERVICE.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 35,386 hrs · 39,846 cycles

EMERGENCY LIGHTS FLICKERED 4 TO 5 TIMES ON CLIMBOUT, 9000 THRU 15000 FT TO CRUISE (FLIGHT LEVEL) RIGHT TRANSFORMER RECTIFYING UNIT .25 LOAD & LOWEST VOLTAGE 23.4 V ON RIGHT SECONDARY BUS. REMOVED, REPLACED EMERGENCY LIGHTS SWITCH PER DASH 8 WIRING MANUAL 33-51-01. OPS CHECKED LIGHTS PER DASH 8 MAINTENANCE MANUAL 33-51-05. OPS CHECKS GOOD. OPS CHECKED LEFT AND RIGHT TRANSFORMER RECTIFYING UNIT PER DASH 8 MAINTENANCE MANUAL BOTH TRANSFORMER RECTIFYING UNIT OPS CHECK GOOD PER 24-31-04. OK FOR SERVICE.

Part: CONTROL BOX — FAULTY (CABIN) · airframe 35,386 hrs · 39,846 cycles

EMERGENCY LIGHTS FLICKER INTENTIONALLY ON TAKEOFF (AFTER GEAR RETRACTION) UNTIL LEVELING OFF IN CRUISE WITH RIGHT SECONDARY VOLTAGE DOWN TO 25 VOLTS. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL BOX IN ACCORDANCE WITH 33-51-00, GROUND RAN AIRCRAFT, CHECKED TRU'S AND SECONDARY VOLTAGE AND NO EMERGENCY LIGHT FLICKERING. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL BOX — FAULTY (CABIN) · airframe 35,326 hrs · 39,766 cycles

EMERGENCY LIGHTS FLICKER WHEN SELECTING GEAR UP OR DOWN. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL BOX IN ACCORDANCE WITH 33-51-00. AIRCRAFT RELEASED FOR EVALUATION FLIGHT DUE TO EMERGENCY LIGHTS FLICKER DURING GEAR EXTENSION AND RETRACTION. MAINTENANCE ACTION COMPLETE, EVALUATION SATISFACTORY.

Part: PLATE — CORRODED (FUSELAGE) · airframe 35,198 hrs · 39,597 cycles

PANEL 523AT, 623AT LADDER PLATE CORRODED. PERFORM ULTRSONIC AND EDDY CURRENT NO DAMAGE FOUND. REPAIR PANEL IAW RD8-57-455 AND RD8-57-4187.

Part: WEB — DAMAGED (LT INTAKE) · airframe 35,198 hrs · 39,597 cycles

LT ENGINE BOTTOM COWLING INBD INTAKE WEB DAMAGE. REPAIR INTAKE WEB IAW RD8-71-74.

Part: STAND OFF — CORRODED (FUSELAGE) · airframe 35,198 hrs · 39,597 cycles

WIRE BUNDLE CLAMPS (4QT) CORRODED IN ZONE AREA 261 (FWD ROOT FAIRING). REMOVED AND REPLACE CLAMPS IAW MM 20-14-01.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 35,198 hrs · 39,597 cycles

CORROSION FOUND ON PAX DOOR THRESHOLD. REMOVED AND REPLACE THRESHOLD IAW STRUCTURAL REPAIR MANUAL 51-40-00.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 35,198 hrs · 39,597 cycles

CORROSION FOUND UNDER LAVATORY DRAIN AIRFOIL AT STA 175. REPAIRED IAW EO8-53-09-3062 PERFORM EDDY CURRENT NO DEFECT FOUND.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 35,198 hrs · 39,597 cycles

LT AND RT SEAT RAIL BETWEEN STA X423 TO X588 CORRODED. REMOVED AND REPLACE SEAT RAIL IAW RD8-53-833.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 35,198 hrs · 39,597 cycles

LT FWD INBD SEAT RAIL CORRODED AT STA X197. REMOVED AND REPLACE SEAT RAIL IAW RD8-53-27-97.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 35,198 hrs · 39,597 cycles

LT INBD SEAT TRACK CORRODED AT MANY LOCATIONS BETWEEN STA X109.0 TO X662. REMOVED AND REPLACE SEAT TRACK IAW RD8-53-833.

Part: BUSHING — CORRODED (FLAP TRACK) · airframe 35,198 hrs · 39,597 cycles

LT AND RT FLAP TRACK BEAM NR 1 HOLLOW BOLT BUSHING CORRODED. REMOVED AND REPLACED BUSHING IAW MM 57-50-11.

Part: FLAP TRACK — CORRODED (ZONE 500) · airframe 35,198 hrs · 39,597 cycles

FOUND LT WING NR FOUR FLAP TRACK CORRODED. REMOVED AND REPLACE FLAP TRACK IAW 57-50-41.

Part: FLAP TRACK — CORRODED (ZONE 600) · airframe 35,198 hrs · 39,597 cycles

RT WING FLAP TRACK NR 5 CORRODED. REMOVED AND REPLACED FLAP TRACK IAW MM 57-52-51.

Part: FLAP TRACK — CORRODED (ZONE 500) · airframe 35,198 hrs · 39,597 cycles

FOUND LT WING NR 4 FLAP TRACK CORRODED. REMOVED AND REPLACE FLAP TRACK IAW 57-50-41.

Part: FLAP TRACK — CORRODED (ZONE 500) · airframe 35,198 hrs · 39,597 cycles

FOUND LT WING NR 4 FLAP TRACK CORRODED. REMOVED AND REPLACE FLAP TRACK IAW 57-50-41.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

THE EMERGENCY SWITCH LIGHT ON THE FLIGHT ATTENDANTS AUDIO CONTROL PANEL WAS FOUND TO BE BURNT OUT. LINE MX CHANGED THE LAMP AND OPS CHECKS WERE GOOD. ACFT CONTINUED IN SERVICE.

Part: AUTOFEATHER SYS — FAILED · airframe 33,889 hrs

ABORTED TAKEOFF, RETURNED TO GATE. MX GROUND RAN AIRCRAFT AUTOFEATHER ARMED AT APPROX 80 PERCENT, TORQUE AT 40 DEGREES, PLA OK FOR SERVICE. AUTOFEATHER HAD FAILED TO ARM AT 85 PERCENT TORQUE ON TAKEOFF ROLL. (K)

Part: AUTOFEATHER SYS — INOPERATIVE

ABORTED TAKEOFF DUE TO AUTOFEATHER NOT ARMING ON THE TAKEOFF ROLL, ABORTED TAKEOFF AT 90-95 KNOTS, RETURNED TO GATE. GROUND RAN AC AUTOFEATHER ARMS AT ABOUT 74 PERCENT TORQUE, OK FOR SERVICE. (K)

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,604 hrs · 37,618 cycles

NR 3 AND NR 4 RED EMERGENCY LIGHTS INOP, ON CABIN AISLE FLOOR. REMOVED AND REPLACED BATTERY AT LOCATION PS5 AT CEILING IN CABIN.

Part: RELAY — FAULTY (AUTOFEATHER SYS) · airframe 33,598 hrs · 37,610 cycles

ON TAKEOFF ROLL, AUTO FEATHER ARM LIGHT EXTINGUISHED.

Part: EEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 32,619 hrs · 36,401 cycles

DURING CRUISE, THE NR 1 ENGINE TORQUE GAUGE DROPPED TO ZERO AND DIGITAL GAUGE READ DASHES FOR 2 OR 3 SECONDS ACCOMPANIED BY THE NR 1 ENGINE SURGING AND CAUTION LIGHTS ILLUMINATING. CREW WAS UNSURE WHICH CAUTION LIGHT. CREW WAS UNSURE IF TORQUE OR NP CHANGED. AIRCRAFT DIVERTED TO BWI AND LANDED NORMALLY. ENGINE EEC WAS CHANGED BY MAINTENANCE AND AIRCRAFT WAS RUN UP AND ENGINE TRIMMED IAW MM PROCEDURES. ALL CHECKS WERE GOOD AT THIS TIME AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BETA SWITCH — MALFUNCTIONED (NR 1 ENGINE) · airframe 24,850 hrs · 26,680 cycles

NR 1 ENGINE BETA LOCKOUT FAILURE AT 500 FT, ENGINE OSCILLATED AT 1000 PROP RPM, TORQUE REACHED 112 PERCENT FOR 1 SECOND (CREW RETARDED THE CONDITION LEVER AND PROP RPM DROPPED TO 900 OSCILLATION STOPPED) CONSULTED MM AND ENGINE PROGRAM MAN. DETERMINED AC DID NOT EXCEED LIMITS. DEACTIVATED BETA LOCKOUT SYSTEM IAW WITH MEL. C/W WORK CARD 61-20-10 AND GROUND RUN FOUND NO DEFECTS NOTED CLEAR MEL.

Part: TIRE — FAILED (NLG) · airframe 24,734 hrs · 26,539 cycles

AFTER LANDING A/C VEERED TO THE RIGHT. NOSEWHEEL STEERING AND LEFT RUDDER WOULD NOT RECOVER A/C TO CENTERLINE APPLIED LEFT BRAKE A/C RECOVERED TO CENTERLINE. LEFT MAIN TIRE BLOWN. REMOVED AND REPLACED LEFT MAIN TIRE, RIGHT MAIN TIRE AND NR 3 & 4 BRAKE ASSY.

Part: SPRING — BROKEN (NR 2 MLG) · airframe 22,123 hrs · 23,378 cycles

ON APPROACH TO CLT THE RIGHT MAIN GEAR HAD UNSAFE LIGHT. USED ALTERNATE GEAR EXTENTION ON NEXT APPROACH. RIGHT GEAR RED LIGHT, DOOR LIGHT AND HANDLE LIGHT ON. ALTERNATE INDICATION SHOWS ALL GEAR DOWN AND LOCKED. FOUND SPRING ON THE STABILIZER STAY STRUT BROKEN, REPLACED BOTH INBOARD AND OUTBOARD SPRINGS.

Part: HYDRAULIC LINE — LEAKING · airframe 20,653 hrs · 21,439 cycles

ON APPROACH TO EWN CREW REPORTED LOSS OF #1 HYDRAULIC SYSTEM CONTENTS. RESULTING IN #1 RUDDER ISOLATION. PRESSURE DID NOT GO BELOW 3000 PSI AND QUANTITY DID NOT GO BELOW .6 QUARTS. INSTALLED TEMPORARY FLEX LINE AT LEFT INBOARD ROLL SPLIOLER ACTUATOR UNLOADING HYDRAULIC LINE.

Part: WHEEL — DEPARTED (MLG)

AFTER TAKEOFF AT APPROXIMATELY 500 FEET, NUMBER 3 TIRE FELL OFF AIRCRAFT. AIRCRAFT RETURNED TO FIELD. REPLACED WHEEL ASSEMBLY AND FERRIED AIRCRAFT TO ORF WHERE THE LOWER PISTON AND AXLE WERE REPLACED AND NEW WHEEL ASSEMBLIES INSTALLED.