N935HA

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,810 hrs · 77,548 cycles

SECOND FROM FRONT, FLOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB. REINSTALLED PROTECTIVE COVER. OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — TRIPPED (STANDY PUMP) · airframe 68,434 hrs · 77,102 cycles

NR 1 STANDBY PUMP CIRCUIT BREAKER TRIPPED. RESET THE CIRCUIT BREAKER. GROUND RAN ACFT AND OPERATED SYSTEMS. SYSTEMS OPS NORMAL.

Part: ROD — OUT OF ADJUST (LT MLG DOOR) · airframe 68,421 hrs · 77,086 cycles

LEFT AMBER GEAR LIGHT CONTINUES TO FLICKER ON & OFF AFTER TAKEOFF. PERFORMED SEVERAL GEAR SWINGS. FOUND FWD DOOR SAGGING. ADJUSTED ROD END ON FWD GEAR DOOR. DID SEVERAL GEAR SWINGS. OPS CHECKED GOOD IAW AMM 32-10-21.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG) · airframe 68,322 hrs · 76,972 cycles

CLOSE WOW C/L ILLUMINATED AT 14,000 FT. NO INDICATION ON LANDING GEAR SELECT PANEL. TRANSCRIBED TO HA300 SEQ 5 ON 20JUL16 WORK PACKAGE INSPECTED WOW PROXIMITY SWITCHES ON ALL GEAR. NO DISCREPANCIES FOUND. PERFORMED PSEU TEST FOUND CODE 01-NLG WOW 2, RT FLAGGED. R & R NLG WOW 2, RT PROXIMITY SWITCH. GAP MUST BE SET AND GEAR SWUNG FOR OPS CHECK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,306 hrs · 76,956 cycles

15TH FLOOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,634 hrs · 76,121 cycles

FLOOR EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 1, 5 AND 9. R & R BULBS AND ROWS 1, 5 AND 9. OPS CHECKED GOOD.

Part: FLAP TRACK — CORRODED (LT WING) · corrosion level 2 · airframe 67,557 hrs · 76,033 cycles

CORROSION ON LT WING, NR 4 FLAP TRACK, INBD SIDE, BEHIND THE TRACK SUPPORT BRACKET. R & R NR 4 FLAP TRACK IAW MM57-50-42.

Part: SUPPORT BRACKET — CORRODED (FLAP TRAK) · corrosion level 2 · airframe 67,557 hrs · 76,033 cycles

NR 4 LT, INBD FLAP TRACK SUPPORT BRACKET HAS PITTING ON CAVITY FACE. R & R NR 4 FLAP TRACK SUPPORT BRACKET IAW MM 57-50-42.

Part: SWITCH — OUT OF ADJUST (SPOILERS) · airframe 75,502 hrs · 75,502 cycles

ON TAKEOFF ROLL, INBD AND OTBD GROUND SPOILER CAUTION LIGHTS ILLUMINATED. SPOILERS DID NOT MOVE. INSPECTED AND FOUND MICROSWITCH 2761 IS OUT OF ADJUSTMENT. RIGGED SWITCH IAW MM 76-10-13. OPS CHECKED SPOILERS. OPS CHECKED GOOD AT THIS TIME.

Part: SKIN — DEBONDED (BS 467-488) · airframe 66,959 hrs · 75,335 cycles

DISBOND DISCOVERED AT BS 467 TO 488, STR 32S TO STR 32P. PREVIOUS REPAIRED USING EO8-53-11-0651. REMOVED BOTTOM SKIN SECTION BS X424 TO BS X488.50, STR 32S TO STR 32P. INSTALLED NEW SKIN IAW DWG 85330022. SEALED, PRIMED AND PAINTED AS NEEDED.

Part: SKIN — CORRODED (BS 434.124 - 488) · airframe 66,958 hrs · 75,335 cycles

MAINTENANCE FOUND SKIN AROUND MARKER BEACON ATENNA CORRODED AND DISBONDED. BOTTOM SKIN SECTION WAS REMOVED FROM BS 434.124 - 488.50, STR 29P TO 29C. SEALED, PRIMED AND PAINTED AS REQUIRED AND CORROSION LEVEL WAS LEVEL 2.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,946 hrs · 74,115 cycles

FLOOR EMERGENCY EXIT SIGN HAD BULBS OUT AT ROWS 4AC AND 4DF. R & R BULBS A ROW 4AC AND 4DF EMERGENCY EXIT FLOOR SIGN. OPS CHECKED GOOD.

Part: GCU — MALFUNCTIONED (NR 2 GENERATOR) · airframe 65,866 hrs · 74,024 cycles

RIGHT A/C BUSS CAUTION LIGHT ILLUMINATED IN FLIGHT. R & R NR 2 AC GEN AND GCU IAW WC 24-20-11R. GROUND RAN ACFT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LGIHT) · airframe 65,860 hrs · 74,016 cycles

ROW 1 FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,860 hrs · 74,016 cycles

ROW 4AC SIDEWALL EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: SWITCH — FAILED (TE FLAPS) · airframe 65,755 hrs · 73,888 cycles

AFTER TAKEOFF AND CREW SELECTED FLAPS O ZERO, FLAP INDICATOR REMAINED AT 5 DEGREES. NO ASSOCIATED CAUTION LIGHTS ON THE GROUND. FLAPS APPEAR TO BE 5 DEGREES. TROUBLE SHOOT AND FOUND FLAP SELECTED ARMING SWITCH 2752-S1 AT FLAP HANDLE BAD. REPLACED MICROSWITCH 2752-S1 AND RIGGED. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 65,227 hrs · 73,252 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT IS DIM. R & R THE BULB. OPS CHECKED GOOD.

Part: SENSOR — FAILED (NLG WOW) · airframe 65,040 hrs · 73,022 cycles

WOW CAUTION LIGHT ILLUMINATED ON GEAR RETRACTION. REMAINED ON FOR ENTIRE FLIGHT. EXTINGUISHED ON LANDING. CHECKED PSEU MEMORY. FAULT CODE FOR RT NLG SENSOR. SENSOR TESTED BAD. R & R NLG WOW SENSOR. OPS CHECKED GOOD.

Part: CONTROL PANEL — MALFUNCTIONED · airframe 64,752 hrs · 72,680 cycles

NAVAGATION SWITCH ANNUNCIATION 2 CIRCUIT BREAKER TRIPPED, AUTO PILOT DISENGAGE ADVANCE LIGHT ILLUMINATED, F/O FLIGHT DIRECTOR FLAGGED. RETURN TO GATE. R & R GC801 PANEL. OPS CHECKED GOOD IAW MM 22-10-01.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 64,575 hrs · 72,456 cycles

WEATHER RADAR DID NOT PAINT. R & R WEATHER RADAR R/T. OPS CHECKED GOOD IAW 34-41-04 AND BUL. 34-18.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,416 hrs · 72,264 cycles

EMERGENCY LIGHT BATTERY INOPERATIVE. R & R BATTERY IAW WC 33-50-05R.

Part: WIRE — BROKEN (PRESS XMITTER) · airframe 63,757 hrs · 71,447 cycles

NR 2 ENGINE OIL PRESSURE FLUXUATED BETWEEN 50-60 PSI DURING CRUISE FLIGHT. REDUCE POWER, PRESSURE STABILIZES AT 50 PSI. SWAPPED GAUGES, NO FIX. FOUND BROKEN WIRE AT OIL PRESSURE TRANSMITTER, REPLACED PINS IN OIL PSI TRANSMITTER C/P. RAN ACFT, OPS CHECKED OK IAW 20-45-05.

Part: TRANSMITTER — FAILED (NR 2 OIL PRESS) · airframe 63,539 hrs · 71,190 cycles

NR 2 ENGINE OIL PRESSURE AT 48 PSI. R & R OIL PRESSURE TRANSMITTER IAW MM 79-36-03. OPS AND LEAKED CHECKED GOOD.

Part: LEAD — DAMAGED (PROPELLER) · airframe 63,517 hrs · 71,159 cycles

EMERGENCY LIGHTS FLICKERED DURING CLIMBOUT, CYCLED EMERGENCY LIGHT CONTROL SWITCH AND OPS CHECKED NOMAL. INSPECTED AND FOUND BAD PROPELLER LEAD ON NR 2 PROP, NR 3 BLADE. R & R LEAD. OPS CHECKED GOOD. OK FOR SERVICE.

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 63,463 hrs · 71,088 cycles

EMERGENCY LIGHTS FLICKER ON & OFF INFLIGHT. R & R EMERGENCY LIGHT CONTROL BOX. OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.

Part: BRUSH BLOCK — MALFUNCTIONED (NR 1 ENGINE) · airframe 63,463 hrs · 71,088 cycles

EMERGENCY LIGHTS FLICKERS ON & OFF INFLIGHT. R & R NR 1 ENGINE BRUSH BLOCK IAW MM 61-10-11. OPS CHECKED GOOD. THE AC CONTACTOR BOXES WERE INSPECTED AND NO DEFECTS WERE NOTED.

Part: BRUSH BLOCK — FAILED (PROPELLER) · airframe 63,357 hrs · 70,955 cycles

RT AC BUSS FAILURE IN FLIGHT WITH ASSOCIATED CAUTION LIGHTS. GROUND RAN ACFT. COULD NOT DUPLICATE. INSPECTED NR 2 AC CONTACTOR BOX WIRING. NO DISCREPANCES NOTED. NR 2 PROP BLADES AND LEADS. INSPECTED NR 2 ENGINE LIP HEATER. R & R 2 BRUSH BLOCK AS PRECAUTION. TAXIED ACFT AND CHECKED ACFT DE-ICE SYSTEM. OK FOR SERVICE.

Part: ADI — FAILED (STANDBY) · airframe 63,326 hrs · 70,911 cycles

STANDBY ATTITUDE INDICATOR DID NOT FUNCTION PROPERLY. SLOWLY ROLLS INTO LT BANK AND NOSE DOWN ATTITUDE. R & R STANDBY ADI. OPS CHECKED GOOD IAW 34-22-00.

Part: DADC — FAILED (NR 1) · airframe 63,326 hrs · 70,911 cycles

BOTH TRANSPONDERS ARE INOPERATIVE. R & R NR 1 DADC. SYSTEM CHECKS GOOD IAW AMM 34-12-02 AND SB 34-68.

Part: BRACKET — CRACKED · airframe 63,294 hrs · 70,876 cycles

RT FRONT SPAR TEE DUCT LOWER BRACKET IS CRACKED. REMOVED ANGLE BRACKET.

Part: BRACKET — CRACKED · airframe 63,294 hrs · 70,876 cycles

FRONT SPAR TEE DUCT LT UPPER BRACKET IS CRACKED. R & R ANGLE BRACKET.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 63,294 hrs · 70,876 cycles

PAX DOOR STAIR FORWARD UPPER INSIDE ANGLE IS CORRODED. R & R PAX DOOR STAIR FWD UPPER ANGLE.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 63,294 hrs · 70,876 cycles

PAX DOOR THRESHOLD SURFACE IS CORRODED. R & R PAX DOOR THRESHOLD IAW SRM 53-00-16.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 63,133 hrs · 70,690 cycles

LEFT AFT EXTERIOR FUSELAGE EMERGENCY LIGHT IS DIM. REMOVED LENS, R & R BULB, AT SAID LOCATION, REINSTALLED LENS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,133 hrs · 70,690 cycles

CEILING EMERGENCY LIGHT AT ROW 8 IS INOPERATIVE. REMOVED LENS, R & R BULB, REINSTALLED LENS. OPS CHECKED GOOD.

Part: BLEED AIR SYS — SMOKE (APU) · airframe 63,076 hrs · 70,628 cycles

APU BLEED AIR CAUSED SMOKE IN CABIN, CLEARED WHEN APU BLEED SELECTED OFF. NO SMOKE OFF ENGINE BLEEDS. APU BLEED AIR.

Part: SOCKET — FAILED (CABIN LIGHT) · airframe 62,499 hrs · 69,921 cycles

OVERHEAD LIGHT AT ROW 8 IS INOPERATIVE. REMOVED PANEL, FOUND MELTED SOCKET, R & R SOCKET AND BALLAST. REINSTALLED PANEL. OPS CHECKED GOOD IAW CMM 33-21-19.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 62,434 hrs · 69,829 cycles

CARGO BAY SMOKE DETECTION WARNING LIGHT ILLUMINATED FOR ABOUT FIVE SECONDS AND EXTINGUISHED. CARGO DOOR WAS OPEN BOTH SYS TESTED NORMAL. R & R FORWARD SMOKE DETECTOR WITH NEW. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,434 hrs · 69,829 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 3. R & R BULB. OPS CHECKED GOOD IAW MM 33-51-11.

Part: CLAMP — LOOSE (HEAT EXCHANGER) · airframe 62,146 hrs · 69,481 cycles

LOW AIRFLOW AND HOT RECIRCULATION AIR TEMP, CABIN TOO HOT FOR ENTIRE FLIGHT WITH DUCT TEMP OF 10. COCKPIT IS NORMAL. INSPECTED AFT CABIN AND BAG BAY, NO LEAKS FOUND. TIGHTENED CLAMP ON HEAT EXCHANGER. GROUND RAN ACFT. DUCT TEMP 11 WITH ADEQUATE AIRFLOW. OK FOR SERVICE.

Part: STRUCTURE — DAMAGED · airframe 61,878 hrs · 69,146 cycles

ACFT STRUCK BY LIGHTNING, ENROUTE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 61,719 hrs · 68,966 cycles

EMERGENCY EXIT CEILING LIGHT AT ROW 7 IS INOPERATIVE. RELAMPED EMERGENCY CEILING LIGHT AT ROW 7 SECURED COVER USING ATTACHED HARDWARE, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,623 hrs · 68,844 cycles

ONE EMERGENCY FLOOR LIGHT IS INOPERATIVE UNDER ROW 9. R & R BULB. REINSTALLED LIGHT ASSY IN FLOOR TRACK. RESECURED WITH CLEAR STRIP.

Part: BULB — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 61,311 hrs · 68,469 cycles

FORWARD AFT EMERGENCY SIGN LIGHT IS DIM. REMOVED BULBS AT LOWER RT EMERGENCY SIGNS. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 61,000 hrs · 68 cycles

FORWARD MOST FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD. REINSTALLED FLOOR COVER.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 60,930 hrs · 67,998 cycles

DRIFT WALL NEAR F/A SEAT HAS 2 EMERGENCY LIGHTS INOPERATIVE. REMOVED LENS, R & R 2 BULBS. REINSTALLED LENS. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 60,675 hrs · 67,686 cycles

EMERGENCY LIGHTS COME ON WHEN SELECTED OFF WHEN CYCLING APU GEN OFF TO ON. ALSO COME ON WHEN SHUTTING ENG DOWN POSITIONED SPADE CONNECTOR ON WIRE 4D22 AT BACK SIDE OF F/A EMERGENCY LIGHT SWITCH. F/A PANEL REMOVED AND REINSTALLED IAW SMP, PERFORMED EMERGENCY LIGHTS, OPS CHECKED IAW W/C 35-50-03Q. OPS CHECED GOOD EMERGENCY LIGHTS OPERATE NORMALLY.

Part: ACTUATOR — FAILED (SPOILERS) · airframe 60,445 hrs · 67,413 cycles

NR 1 HYD SYS LOSS OF CONTENTS AND FAILURE ON LANDING. RUDDER ISOLATION VALVE CAUTION LIGHT ILLUMINATED. R & R RT INBD SPOILER ACTUATOR IAW AMM 27-14-05. FUNCTION AND LEAKED CHECKED GOOD.

Part: CONNECTOR — UNSECURE (AC BUSS) · airframe 59,765 hrs · 66,562 cycles

RT AC BUSS CAUTION LIGHT ILLUMINATED. RT AC BUS FAILED. CLEANED AND RESECURED CONNECTOR ON NR 2 AC GENERATOR. OPS CHECKED NORMAL IAW MM 24-21-00. OK FOR SERVICE.

Part: GENERATOR — FAILED (NR 1 AC) · airframe 59,468 hrs · 66,205 cycles

LEFT AC "B" PHASE HAS ZERO LOADS AND VOLTS. LT STALL WARNING CAUTION LIGHT. LT PROP "B" PHASE ADVISORY LIGHT DID NOT INDICATE WHEN SELECTED ON. R & R NR 1 AC GENERATOR, GCU AND NR 1 BRUSH BLOCK IAW WC 24-20-11R AND WC 30-61-00. CHECKED GOOD.

Part: COMPUTER — MALFUNCTIONED (FLT GUIDANCE) · airframe 59,188 hrs · 65,863 cycles

AIRSPEED EXCEEDED 45 DEGREE BANK WITH AUTOPILOT AND FLIGHT DIRECTOR ENGAGED. INDICATED AIRSPEED 180 KTS. FLAPS AT ZERO. GEAR UP. NO FULL FLIGHT CONTROL DEFLECTION. COULD NOT DUPLICATE. R & R NR 1 FGC AS PRECAUTION. OPS CHECKED GOOD IAW MM 20-10-01.

Part: TIMER — FAILED (DE ICE BOOT) · airframe 59,161 hrs · 65,834 cycles

LEFT WING OTBD DEICE BOOT WILL NOT INFLATE IN SLOW OR FAST. INFLATES NORMALLY IN MANUAL. R & R AIRFRAME DEICE TIMER. OPS CHECKED GOOD IAW MM 30-10-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,846 hrs · 63,225 cycles

(1) WHITE EMERGENCY FLOOR LIGHT IS INOP AT ROW 2. R & R BULB, OPS CHECKED GOOD.

Part: ACTUATOR — LEAKING (SPOILERS) · airframe 55,482 hrs · 61,691 cycles

WHEN TURNING ONTO RUNWAY, NR 2 HYD SYS WENT INTO ISO AND QUANITY AT HALF QUART. SERVICE NUMBER 2 HYD SYS, RAN ACFT FOUND LT OTBD SPOILER ACTUATOR LEAKING (SHORT SIGN). R & R LT OTBD ROLL SPOILER ACTUATOR IAW DASH 8 MM 27-14-05. OPS AND LEAK CHECK GOOD.

Part: BATTERY — OVERHEATED (MASTER) · airframe 55,273 hrs · 61,446 cycles

MAIN BATTERY HOT WARNING LIGHT ILLUMINATED. APU BLEED WAS ON FULL WITH APU BLEED SELECTED OFF. SMOKE IN CABIN. R & R MAIN BATTERY IAW AMM 24-32-00. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (ENGINE OIL SYS) · airframe 54,358 hrs · 60,409 cycles

NR 1 OIL PRESSURE WARNING LIGHT FLICKERED SEVERAL SECONDS AND OIL PRESSURE FLUX BETWEEN 55-65 PSI THRU CLIMBOUT. R & R NR 1 ENGINE OIL PRESSURE SWITCH IAW ENGINE BUILDUP 71-00-02. SERVICED NR 1 ENGINE WITH 3 QUARTS OF OIL. GROUND RUN WITH NO LEAKS, OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (FIRE DETECTION) · airframe 53,723 hrs · 59,685 cycles

ON FIRE DETECTION PANEL NR 1 FWD AND NR 2 AFT AMBER LIGHTS WILL NOT ILLUMINATED WHEN FUEL OFF HANDLE IS PULLED. INSPECTED AND CONFIRMED FIRE BOTTLE PRESSURES ARE GOOD. CLEANED CONTACTS BEHIND FIRE DETECTION PANEL. PULLED AND RESET C/B K-8,L-8 ON THE LT PANEL AND ON THE RT PANEL G-7, H-7, F-2, G-2, H-2, J-2, K-2 L-2 OPS CHECK GOOD, LIGHTS OPERATES NORMALLY.

Part: RELAY — DEFECTIVE (AUTOFEATHER SYS) · airframe 52,173 hrs · 57,878 cycles

AUTO FEATHER DID NOT ARM ON T/O ROLL. RETURNED TO GATE. REMOVED AND REPLACED RELAYS 6121-K3, AND 6121-K4. OPS CK GOOD.

Part: WINDSCREEN — CRACKED (COCKPIT) · airframe 53,468 hrs · 59,399 cycles

F/O WINDSCREEN ARCING IN FLIGHT AND IS CRACKED. INSPECTED, FOUND CRACK TO BE CONFINED TO OUTER MOST PAIN ONLY. REMOVED AND REPLACED F/O'S WINDSHIELD IAW TASK CARD.

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 53,436 hrs · 59,364 cycles

NR 1 ENG OIL PRESS CAUTION LIGHT ILLUMINATED ON TAKE OFF ROLL. ABORTED TAKE OFF. INSPECTED OIL SERVICE AND FOUND 3.5 QUARTS LOW. SERVICED TO FULL. CLEANED OIL PRESS SWITCH CONNECTOR AND RESEATED. GROUND RAN NO LEAKS NOTED. OPS CHECK GOOD. WILL MONITOR OIL CONSUMPTION.

Part: HMU — FAILED (NR 2 ENGINE) · airframe 52,578 hrs · 58,411 cycles

DURING CLIMBOUT, NUMBER 2 ENGINE WON'T GO ABOVE 80 PERCENT. REMOVED AND REPLACED NUMBER 2 HYDRO MECHANICAL UNIT IN ACCORDANCE WITH WORKCARD 73-20-01R. GROUND RAN AIRCRAFT. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,082 hrs · 57,883 cycles

SECOND FLOOR EMERGENCY LIGHT INOP. R&R LAMP IAW AMM 33-25-00.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

RT EGRESS LIGHT IS INOPERATIVE FORWARD. REMOVED AND REPLACED EMERGENCY BATTERY IAW W/C 33-50-05R. P/N OFF 61-0478-9, P/N ON 60-1721-1XC S/N OFF 138, S/N ON JAX12. (S)

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

RT EGRESS LIGHT IN INOPERATIVE FORWARD. REMOVED AND REPLACED EMERGENCY BATTERY IAW W/C 33-50-05R. (S)

Part: RECEIVER — FAILED (NR 1) · airframe 50,216 hrs · 58,851 cycles

ON APPROACH INTO CLT NR 1 NAVIGATION RECEIVER FAILED FOLLOWED BY A STRONG ODOR. REMOVED AND REPLACED NR 1 NAV RECEIVER IAW 34-55-05. RAMP CHECK GOOD.

Part: INDICATOR — FAILED (COCKPIT) · airframe 49,641 hrs · 55,254 cycles

ON TAKEOFF ROLL NR 2 ENG TQ IND WENT TO ZERO, SPEED LESS THAN 40KTS, CYCLED CB'S J5 & K5, ENG GROUND RUN GOOD, INDICATION NORMAL. REPLACED TQ IND, INSPECTED & CLEANED ELECTRICAL CONNECTORS ON NR 2 ENG, OPS CHECK GOOD.

Part: INDICATOR — FAILED (TORQUE) · airframe 49,641 hrs · 55,254 cycles

DURING TAKEOFF ROLL, NR 2 TORQUE INDICATOR DROPPED TO ZERO. SPEED WAS LESS THAT 40 KNOTS. CIRCUIT BREAKERS J5 & K5 (TQ IND & COND) WERE CYCLED AND AIRCRAFT WAS RUN UP. CHECKS WERE GOOD AND AIRCRAFT RELEASED FOR FLIGHT. UPON ARRIVAL AT A MAINTENANCE BASE, THE NR 2 TORQUE INDICATOR WAS REPLACED AND THE CONNECTOR AT THE ENGINE WERE CLEANED. CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACTUATOR — MISRIGGED (RUDDER) · airframe 49,087 hrs · 54,637 cycles

IN FLIGHT WITH CHARTED TORQUE AND CHARTED PITCH, RUDDER REQUIRES ¼ LEFT HAND TRIM FOR, 0 BALL FLIGHT. ADJUSTED RUDDER TRIM ACTUATOR AS PER MM 27-20-37, OPERATION CHECK GOOD.

Part: MECHANISM — LACK OF LUBE (PILOT SEAT) · airframe 48,742 hrs · 54,263 cycles

DURING TAKEOFF ROLL, THE CAPTAINS SEAT BECAME DISLODGED AND FELL FROM THE TRACKS TO THE FLOOR. MTX LUBED VERTICAL ADJUSTMENT LOCK MECHANISM.

Part: RADAR — FAILED · airframe 48,154 hrs · 53,638 cycles

ON CLIMBOUT FROM SBY THE RADAR FAILED. CREW CYCLED CIRCUIT BREAKER WITH NO FIX. FLIGHT RETURN TO THE FIELD. EMERGENCY WAS NOT DECLARED AND FLIGHT LANDED WITH OUT INCIDENT. CREW IN FLIGHT TURNED OFF INDICATOR AND CYCLED C/B BUT DID NOT TURN INDICATOR BACK ON. PERFORMED RADAR FUNCTION TEST, TESTED NORMALLY A/C DEPARTED AGAIN FOR CLT.

Part: HYDRAULIC LINE — MISINSTALLED (NR 1 NACELLE) · airframe 47,157 hrs · 52,553 cycles

GEAR UNSAFE, CYCLED GEAR LEFT GEAR INDICATION REMAINED UNSAFE. NR 2 HYDRAULIC SYSTEM PRESSURE AT 2200, ALTERNATE GEAR EXTENSION PERFORMED WITH ALL GREEN INDICATION AND NR 2 HYDRAULIC SYSTEM AT 3000. FOUND PREVIOUSLY INSTALLED TEMP FLEX HYDRAULIC LINES SWAPPED AROUND IN NR 1 NACELLE. INSTALLED LINES TO CORRECT POSITION.

Part: PSU — BURNED · airframe 45,370 hrs · 50,588 cycles

SMOKE COMING FROM CABIN 1AC AREA. REMOVED AND REPLACED PSU

Part: TUBE — LEAKING (NR 2 HYD SYSTEM) · airframe 44,422 hrs · 49,616 cycles

LOSS OF NR 2 HYDRAULIC QUANTITY IN FLIGHT WITH ASSOCIATED NR 2 ISO VALVE LIGHT AND OB ROLL SPOILER CAUTION LIGHT. NR 2 HYDRAULIC QUANTITY REMAINED AT 2 QUARTS. FOUND TUBE LEAKING AT NR 2 STAY STRUT ACTUATOR.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 44,422 hrs · 49,616 cycles

LOSS OF NR 2 HYDRAULIC QUANTITY IN FLIGHT WITH ASSOCIATED NR 2 ISO VALVE LIGHT AND OB ROLL SPOILER CAUTION LIGHT. NR 2 HYDRAULIC QUANTITY REMAINED AT 2 QUARTS. FOUND TUBE LEAKING AT NR 2 STAY STRUT ACTUATOR.

Part: CONTROLLER — JAMMED (ROLL CONTROL) · airframe 44,052 hrs · 49,208 cycles

ROLL CONTROL JAMMED 10 MILES OUT ON APPROACH, CREW SPLIT YOKES IAW CHECK LIST AND CAPTAINS SIDE FREED. FIRST OFFICER STAYED JAMMED UNTIL JUST BEFORE TOUCH DOWN. CAPTAIN CONTROLLED AIRCRAFT WITH SPOILERS. INSPECTED ROLL CONTROL FOR JAMMING AND BINDING OPS NORMAL AND FREE. NO DEFECTS. DISCUSSED PROBLEM WITH CREW AGAIN AND MOST LIKELY RELATED TO AUTO PILOT NOT DISENGAGING. ISSUED MEL 22-1 AUTOPILOT. MORE TO FOLLOW.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 41,287 hrs · 46,227 cycles

DURING C-CHECK FOUND LIGHTNING BURNS ON FUSELAGE SKIN BETWEEN STA X123 & X136 AND STR 31S/32S. REPAIRED IAW EO8-53-04-0572. WORK SCOPE REQUIRED WAS A MAJOR REPAIR.

Part: TIRE — SEPARATED (MLG WHEEL) · airframe 39,971 hrs · 44,787 cycles

NR 2 MAIN TIRE APPEARED FLAT DURING TAXI OUT. AC ON TAXI WAY, MT GOING OUT TO A/C TO INSPECT A/C PRIOR TO TAXI BACK TO GATE. THE A/C BEHIND THIS A/C NOTICED SMOKE COMING FROM NR 2 BRAKE ASSY. F/A NOTICED TIRE CAME OFF RIM.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 39,255 hrs · 44,052 cycles

DURING PASSENGER BOARDING, CAPTAIN SAW SMOKE COMING FROM AROUND RADAR GRAPHICS UNIT, POWERED DOWN AIRCRAFT, SMOKE DISSIPATED. PERFORMED HIDDEN DAMAGE INSPECTION AND DEACTIVATED RADAR GRAPHICS UNIT IAW EO8-24-03-0979. REPLACED RADAR GRAPHICS UNIT.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 38,066 hrs · 42,779 cycles

CREW REPORTED SMOKE COMING FROM THE F/O'S FRONT WINDSCREEN ELECTRICAL TERMINAL AREA FOLLOWED BY THE WINDSCREEN SHATTERING. REPLACED F/O'S WINDSCREEN.

Part: PSU — CHAFED (CABIN 7AC) · airframe 35,649 hrs · 40,305 cycles

PLASTIC BURNING SMELL FROM OVERHEAD PANEL 1AC. FOUND WIRES PINCHED AND CHAFED AT PSU 7AC. REPLACED PSU.

Part: BOLT — MISSING (MLG DOOR) · airframe 32,777 hrs · 37,300 cycles

NR 1 MLG FWD DOOR CAME OPEN IN FLIGHT. FOUND DOOR ACTUATING ROD TO DOOR HINGE HARDWARE MISSING. REPLACED HARDWARE.

Part: BATTERY — DISCHARGED (CABIN)

FLT 3169 - DCA-PHL - NR 3 AND NR 4 RED ESCAPE PATH LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY 3352 PS1, OPS CHECK GOOD. (M)

Part: SWITCH — FAILED (F/A PANEL)

FLT 3040 - FLL-TPA - DURING PREFLIGHT CHECKS, FOUND THE INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP. MX FREED THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH. AT RON, THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH WAS REPLACED. (M)

Part: B-NUTS — LOOSE (NR 1 HYD SYST)

FLT 3057 - BWI-HPN - NR 1 HYDRAULIC SYSTEMS CONTENTS WENT TO ZERO IN FLIGHT. AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. RETORQUED SEVERAL 'B' NUTS ON HYDRAULIC LINES TOP OF NR 1 NACELLE ABOVE JET PIPE. SERVICED SYSTEM AND BLED, PERFORMED SEVERAL LEAK CHECKS. NO LEAKS NOTED AT THIS TIME.