N911HA

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,006 hrs · 79,685 cycles

EMERGENCY LIGHT INOPERATIVE. R & R BULB . OPS CHECKED GOOD.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 69,991 hrs · 79,666 cycles

WHILE IN FLIGHT, NR 1 RUDDER ISOLATION VALVE AND NR 1 RUDDER HYD ILLUMINATED; NR 1 QTY WAS INDICATING 0.8 QTS, PRESSURE ON BOTH MAIN HYD 3000 PSI. INSPECTED AND CLEANED NR 1 GEARWELL, SERVICED NR 1 HYD SYS AND GROUND RAN ACFT. FOUND UPPER HYD LINE LEAKING ON NR 1 SPOILER UNLOADING VALVE. INSTALLED TEMP FLEX LINE. LEAK CHECK GOOD, C/L'S EXTINGUISHED. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,661 hrs · 79,268 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 3DF. R & R BULB AT ROW 3DF. OPS CHECKED GOOD.

Part: BULB — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 69,661 hrs · 79,268 cycles

FORWARD RT TOP EMERGENCY EXIT SIGN IS DIM. R & R BULBS AT RT TOP EMERGENCY EXIT SIGN. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 69,372 hrs · 78,919 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,112 hrs · 78,606 cycles

TWO FLOOR EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 1 AND 8. R & R BULBS. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 68,943 hrs · 78 cycles

EMERGENCY ESCAPE PATH FLOOR LIGHT IS INOPERATIVE. R & R EMERGENCY ESCAPE PATH FLOOR LIGHT BULB AT ROW 7DF IAW 33-51-00. OPS CHECKED GOOD.

Part: PRESSURE SENSOR — FAILED (HYD SYSTEM) · airframe 68,850 hrs · 78,266 cycles

NR 1 RUDDER HYD, RUDDER PRESSURE AND RUDDER FULL PRESSURE LIGHT CAME ON IN FLIGHT. STAYED ON DURING THE DURATION OF FLIGHT. CREW DEPRESSED NR 1 RUDDER PUSH OFF SWITCH ON GROUND WITH APU POWER ONLY AND RUDDER PRESSURE CAUTION LIGHT REMAINED ON. R & R RUDDER DUEL PRESSURE REGULATOR. OPS AND LEAKED CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 68,573 hrs · 77,929 cycles

BROKEN WIRE IN EMERGENCY LIGHTS POWER SUPPLY AT LOCATION PS4. R & R EMERGENCY LIGHT POWER SUPPLY AT LOCATION PS4. SECURE WITH RETAINED HARDWARE. REINSTALLED EMERGENCY BATTERY. RECONNECTED ELECTRICAL PLUG.

Part: CONNECTOR — DIRTY (TE FLAPS) · airframe 68,515 hrs · 77,854 cycles

FLAP DRIVE CAUTION LIGHT FLICKERING DURING CRUISE FLIGHT. ON CONTINUOUSLY FOR APPROX 30 MINUTES. STAYED OUT AFTER LANDING. FLAP OPS NORMAL. INSPECTED AND CLEANED CONNECTOR ON TORQUE SENSOR. GROUND RAN AIRCRAFT. FLAPS OPS CHECKED NORMAL AT THIS TIME. LIGHT REMAINED EXTINGUISHED.

Part: WHEEL — DAMAGED (MLG) · airframe 68,332 hrs · 77,643 cycles

DURING WALK AROUND, CREW FOUND NR 4 WHEEL ASSY DAMAGED. R & R NR 3 AND 4 MAIN WHEEL ASSEMBLIES IAW MM 32-41-11. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,382 hrs · 77,910 cycles

EMERGENCY FLOOR PATH LIGHTS INOPERATIVE AT ROW 1DF. R & R BULB. OPS CHECKED GOOD.

Part: RELAY — FAILED (INTAKE HEAT) · airframe 68,164 hrs · 77,431 cycles

AT 5000 FEET, NR 2 ENGINE INTAKE HEAT INOPERATIVE. R & R RELAY 3021-K2. GROUND RAN ACFT. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: RADAR — FAULTED (WX SYSTEM) · airframe 68,002 hrs · 77,229 cycles

WEATHER RADAR IS INOPERATIVE, SHOWS ANT FAULT MESSAGE. ACFT RETURNED TO FIELD. R & R RADAR R/T. OPS CHECKED GOOD IAW MANUAL 34-41-02. OPS CHECKED GOOD. NO DEFECTS NOTED. OK FOR SERVICE.

Part: BULB — FAILED (SWITCH PANEL) · airframe 67,970 hrs · 77,192 cycles

AFTER F/A'S PA ANNOUNCEMENT DURING TAXI OUT, EMERGENCY SWITCH BACK LIGHT AND PA SWITCH BACK LIGHT WERE FOUND TO BE INOP WITH ELECTRICAL SMELL FROM PANEL AREA. ALL SWITCH FUNCTION NORMAL. RELAMP BACK LIGHT BULBS AND INSPECTED F/A'S CONTROL PANEL. NO SIGNS OF BURNING. INSPECTED COAT CLOSET AREA FOR ANY SOURCE OF SMELL AND FOUND NOTHING. OPS CHECKED GOOD, REF MM 23-50-00.

Part: SWITCH — FAILED (EMERGENCY LIGHT) · airframe 67,790 hrs · 76,974 cycles

F/A EMERGENCY LIGHT SWITCH ON LIGHT INOPERATIVE. R & R EMERGENCY LIGHT SWITCH S2 IAW WIRING MANUAL 33-51-00. BOTH OPS CHECKED GOOD.

Part: BRUSH BLOCK — INOPERATIVE (PROPELLER) · airframe 67,381 hrs · 76,465 cycles

EMERGENCY LIGHTS FLICKER ON TAKEOFF ROLL. R & R RIGHT BRUSH BLOCK IAW 61-10-11 AND FUSE 2421 F10. IN RT AC CONTACTOR BOX. GROUND RAN ACFT, OPS CHECKED GOOD, OK 4 SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYD SYSTEM) · airframe 67,212 hrs · 76,252 cycles

ROLL SPOILER INBD HYD CAUTION LIGHT ILLUMINATED IN FLIGHT. PRESSURE AND QUANTITIES ARE NORMAL. R & R INBD LOW PRESSURE SWITCH. GROUND RAN ACFT. OPS AND LEAKED CHECKED GOOD. OK FOR SERVICE.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 67,042 hrs · 76,034 cycles

F/A EMERGENCY SWITCH LIGHT BACKLIGHTING IS INOPERATIVE. R & R F/A EMERGENCY LIGHT SWITCH IAW WIRING DIAGRAM 33-51-00. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 67,018 hrs · 75,998 cycles

EMERGENCY LIGHT AT ROW 4DF IS INOPERATIVE. REMOVED LENS, REMOVED AND REPLACED BULB. REINSTALLED LENS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,810 hrs · 75,734 cycles

EMERGENCY LIGHT AT ROW 6DF INOPERATIVE. R & R BULB AT ROW 6DF. OPS CHECKED GOOD.

Part: WARNING HORN — FALSE ACTIVATION · airframe 66,813 hrs · 75,738 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF WITH PROPER CONFIGURATION. WILL NOT TURN OFF. RETURNED TO GATE. RACKED PSEU. OPS CHECKED GOOD. PREFORMED PSEU SYS TEST. OPS CHECKED GOOD IAW AMM 32-61-50.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 66,668 hrs · 75,571 cycles

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

Part: CONNECTOR — DAMAGED (HYD SYSTEM) · airframe 66,391 hrs · 75,251 cycles

ROLL SPOILER INBD HYD CAUTION LIGHT ILLUMINATED IN FLIGHT. R & R CONNECTOR PLUG 2762-P1 IAW WIRING MANUAL 27-14-00. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,018 hrs · 74,830 cycles

EMERGENCY EGRESS LIGHT AT AIRSTAIR DOOR HAS LAMP OUT. R & R LIGHT AS REQUIRED. OPS CHECKED GOOD.

Part: RVDT — OUT OF ADJUST (WARNING HORN) · airframe 65,931 hrs · 74,733 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF WHEN POWER LEVERS ARE ADVANCED. MADE ADJUSTMENTS TO RT RVDT IAW MM 27-52-61, BULLETIN 27-27. OPS CHECKED GOOD. PANEL 632FB R & R TO FOM.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 65,868 hrs · 74,653 cycles

FLOOR PATH EMERGENCY LIGHT INOPERATIVE AT ROW 6. R & R BULB. OPS CHECKED GOOD.

Part: BRACKET — CRACKED · airframe 65,843 hrs · 74,622 cycles

AFT DE-ICE PRESSURE REGULATOR BRACKET IS CRACKED. R & R DEICE PRESSURE REGULATOR BRACKET, FRABRICATED FROM DWG 85410993.

Part: ANGLE — CRACKED (NACELLE) · airframe 65,843 hrs · 74,622 cycles

OTBD NACELLE TO FRONT SPAR CLOSING ANGLE IS CRACKED ON NR 1 NACELLE. REMOVED SIDWALL ANGLE. FABRICATED NEW ANGLE IAW DWG 85710407. INSTALLED NEW ANGLE IAW EO 8-57-12-0082.

Part: STRUCTURE — CRACKED (NACELLE) · airframe 65,843 hrs · 74,622 cycles

NR 1 FINGERNAIL DECK WHEEL HUMP HAS CRACK ALONG AFT SIDE (INBD HUMP). REPAIRED DAMAGE IAW RD8-54-1494.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 65,843 hrs · 74,622 cycles

UPPER INBD SIDE SKIN IS CRACKED 1 INCH FORWARD OF NR1 NACELLE FRONT WING SPAR, LOWER FLANGE. REMOVED RIVETS AT CRACK LOCATION, FOR FURTHER INSPECTION. COMPLIED WITH DYE PEN INSPECTION IAW RD8-54-1557. NO CRACKS FOUND. REPAIRED DAMAGE IAW EO8-54-12-0077 AND RD8-54-1557.

Part: FLAP TRACK — CORRODED (NR 2 FLAP) · airframe 65,843 hrs · 74,622 cycles

NR 2 FLAP TRACK IS CORRODED ON MATING SURFACE. R & R NR 2 FLAP TRACK ASSY.

Part: ANGLE — CORRODED (NACELLE) · airframe 65,843 hrs · 74,622 cycles

INBD NACELLE TO FORWARD SPAR CLOSING ANGLE IS CORRODED ON NR 1 NACELLE. REMOVED INBD CLOSING ANGLE, FABRACATED INBD SIDEWALL ANGLE IAW DWG 85710414. INSTALLED INBD SIDEWALL ANGLE IAW DWG 85710413.

Part: ATTACH ANGLE — CRACKED (NACELLE) · airframe 65,843 hrs · 74,622 cycles

OTBD AFT ATTACH ANGLE FOR FILLET PANEL IS CRACKED. FABRACATED NEW ANGLE IAW DWG 85418256. REMOVED OLD CRACKED ANGLE. INSTALL NEW ANGLE IAW DWG 85410042.

Part: FLAP TRACK — CORRODED (NR 2 FLAP) · airframe 65,843 hrs · 74,622 cycles

NR 2 FLAP TRACK BADLY CORRODED ON MATING SURFACE. R & R NR 3 FLAP TRACK.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 65,843 hrs · 74,622 cycles

UPPER STAIR AFT SUPPORT BRACKET IS CORRODED. REMOVED UPPER STAIR AFT SUPPORT BRACKET. MADE NEW BRACKET AND INSTALLED IAW DWG 85210303.

Part: BRACKET — CORRODED (PAX DOOR) · corrosion level 2 · airframe 65,843 hrs · 74,622 cycles

TOP AFT BRACKET IS CORRODED. R & R TOP AFT BRACKET UNDER PAX STAIRS IAW DWG 85210302.

Part: STOP — CORRODED · airframe 65,843 hrs · 74,622 cycles

AFT NR 5 STOP IS WORN AND CORRODED. REMOVED OLD STOP ONLY. INSTALLED AFT NR 5 STOP.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 65,843 hrs · 74,622 cycles

MID CROSS BRACE AFT BRACKET IS CORRODED. CLEANED LIGHT CORROSION, ALODINED AND PRIMED MID CROSS BRACE AFT BRACKET UNDER STAIRS.

Part: STRUCTURE — CORRODED (BS 539 S24R) · airframe 65,843 hrs · 74,622 cycles

CORROSION FOUND ON FORWARD OF STR X539 FROM STR 24S. CLEANED CORROSION ON FORWARD STR X539 AND STR S4S IAW SRM 51-20-11. ALODINED AND PRIMED AREA AS REQUIRED.

Part: STIFFENER — CRACKED (RADOME) · airframe 65,843 hrs · 74,622 cycles

BOTH VERTICAL STIFFNERS UNDER RADOME CRACKED AT TOP RIVET. TRIM DAMAGED AREA OUT ON BOTH STIFFNERS IAW RD8-53-7275. COMPLIED WITH HFEC INSPECTION. NO DEFECTS NOTED. COMPLETED REPAIRS AS REQUIRED IAW RD8-53-7275.

Part: STRINGER — CORRODED (BS 424-436) · airframe 65,843 hrs · 74,622 cycles

STRINGER BETWEEN X424 AND X436 AND STA 23S IS CORRODED. CLEANED CORROSION BETWEEN X424 AND X436, STA 23S IAW SRM 51-20-11. ALODINED AND PRIMED AS REQUIRED.

Part: FLOOR SUPPORT — CORRODED (BS 539) · airframe 65,843 hrs · 74,622 cycles

AFT FLOOR SUPPORT AT X539 HAS CORROSION. CLEANED CORROSION AT AFT FLOOR SUPPORT AT X539 IAW SRM 51 20-11. ALODINED AND PRIMED AS REQUIRED.

Part: STRINGER — CORRODED (BS 445) · airframe 65,843 hrs · 74,622 cycles

STRINGER FWD ON X445 AND STR 23S IS CORRODED. CLEANED CORROSION AT X445 FRAME AND STR 23S IAW SRM 51-20-11. ALODINED AND PRIMED AS REQUIRED.

Part: MODULE — FAILED (EMERGENCY LIGHT) · airframe 65,820 hrs · 74,592 cycles

ROW 2 EMERGENCY FLOOR LIGHT IS DIM. INSTALLED ROW 2 EMERGENCY FLOOR LIGHT MODULE, INSTALLED BULB AND CLOSED ACCESS PANEL. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 65,820 hrs · 74,592 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 9. R & R FLOOR EMERGENCY PATH LAMP AND CLOSED ACCESS PANEL.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 65,790 hrs · 74,552 cycles

ROW 1 RED EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R BULBS, OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 65,790 hrs · 74,552 cycles

EMERGENCY LIGHT AT ENTRANCE ON BASE OF F/A WALL HAS 2 INOP BULBS. R & R BULBS. OPS CHECKED GOOD.

Part: BEARING — DAMAGED (ELEVATOR) · airframe 65,747 hrs · 74,496 cycles

INBOUND CREW REPORTED THAT ACFT PITCH CONTROL WAS SLOW TO RESPOND DURING TAKEOFF AND LANDING, MORE EFFORT REQUIRED. R & R RT ELEVATOR BEARINGS.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 65,087 hrs · 73,740 cycles

ROW 4DF EMERGENCY SIDEWALL LIGHT IS NOT WORKING. REMOVED LENS, R & R BULB, REINSTALLED LENS. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,043 hrs · 72,589 cycles

EMERGENCY LIGHT CAUTION LIGHTS DID NOT ILLUMINATE WHEN EMERGENCY LIGHTS WERE TURNED OFF. NOW LIGHTS WILL NOT TURN ON FROM COCKPIT OR F/A STATION. R & R ALL EMERGENCY LIGHT BATTERIES IAW 33-50-03Q, OPS CHECKED GOOD AT THIS TIME.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 63,674 hrs · 72,202 cycles

ODOR DETECTED IN COCKPIT AND BOARDING AREA. INSPECTED COCKPIT, COAT CLOSET AND AVIONICS RACK AND UNDER CABIN FLOOR. NO ODOR NOTICED. ACFT OK FOR SERVICE.

Part: CONNECTOR — FAILED (ELEVATOR HEAT) · airframe 62,944 hrs · 71,411 cycles

RT ELEVATOR HORN HEAT CAUTION LIGHT ON IN FLIGHT. R & R RT ELEVATOR HORN HEAT CONNECTOR PLUG AND PINS. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (ENG OIL TEMP) · airframe 62,478 hrs · 70,877 cycles

IN CRUISE, NR1 ENGINE OIL TEMP WENT TO 120 DEGREESC FOR APPROX 17 MINUTES. REDUCED POWER AND INITIATED DECENT. OIL TEMP RETURNED TO GREEN.( NOTE: F/O TIMED DURATION BETWEEN 115 AND 120). R & R NR1 TEMP GAUGE, NO FIX, RETURNED TO ORIGINAL. CLEANED NR1 TEMP BULB CONNECTOR PLUG, NO FIX, R & R NR1 OIL COOLER VALVE ASSY, GROUND RAN ACFT, OPS AND LEAKED CHECKED GOOD AT THIS TIME.

Part: RADAR — INOPERATIVE (WX SYSTEM) · airframe 61,839 hrs · 70,149 cycles

WEATHER RADAR IS NOT WORKING, ANT FLIGHT MESSAGE. R & R RT,OPS CHECKED GOOD IAW BULLETIN 34-18. RADOME SEALED WITH 748.

Part: BYPASS SWITCH — FAILED (NR 2 FUEL FILTER) · airframe 61,639 hrs · 69,917 cycles

NR 2 FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED IN FLIGHT. OIL TEMPS DROPS TO TOP OF YELLOW ARC. R & R NR2 ENGINE FUEL FILTER BYPASS SWITCH IAW MM 72-01-40.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 61,015 hrs · 69 cycles

ROW 2 EMERGENCY PATH FLOOR LIGHT NOT WORKING. RE LAMP ROW 2 FLOOR EMERGENCY FLOOR LIGHT.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 60,957 hrs · 69,140 cycles

ON TAKEOFF ROLL, BAG BAY SMOKE DETECTOR LIGHT ILLUMINATED. ABORTED TAKEOFF. LIGHT WENT OUT UPON CLEARING RUNWAY. F/O VISUALLY INSPECTED FOR SMOKE, NONE NOTED. BAG BAY SMOKE DETECTOR LIGHT EXTINGUISHED, INSPECTED BOTH BAG BAY SMOKE DETECTORS, SMOKE DETECTOR CONNECTOR PLUGS FOR SECURITY, AND SMOKE DETECTOR WIRING FOR DEFECTS. NONE NOTED, PERFORMED HIGH SPEED TAXI. NO BAG BAY SMOKE DETECTOR LIGHT NOTED, OK FOR SERVICE AT THIS TIME.

Part: SPOILER SYS — STIFF · airframe 60,690 hrs · 68,834 cycles

AFTER ROLL SPOILER OUTBOARD CAUTION LIGHT ILLUMINATED, ROLL CONTROL STIFFER THAN NORMAL. MX WILL DO THE OPS TEST OF ROLL SPOILER CONTROL SYS IAW AMM 27-14-00, IF NO PROBLEMS, WILL FERRY FLIGHT TO ROA.

Part: WARNING LIGHT — ILLUMINATED (HYD SYSTEM) · airframe 60,690 hrs · 68,834 cycles

NR 2 ROLL SPOILER HYD CAUTION LIGHT ILLUMINATED AFTER DEPARTURE. CAPTAIN REPORTED CAUTION LIGHT WENT OUT AFTER RETURN TO FIELD, AND MX COULD NOT DUPLICATE PROBLEM EITHER, HAVING MX REMOVED AND REPLACE SWITCH AND BLEED NR 2 SYS.

Part: CONNECTOR — DIRTY (OVERHEAT DETECT) · airframe 60,687 hrs · 68,831 cycles

APU FIRE OVERHEAT DETECTOR WORK CARD 26-10-02Q FAILED TO LIGHT TEST LAMP OM FIRE BOTTLE CONNECTOR. CLEANED CONNECTOR AND RECHECKED WORK CARD 26-10-02Q AND TEST LAMP OPS CHECKED GOOD. SAFETIED CONNECTOR PLUG.

Part: INDICATOR — FALSE INDICATION (FLAPS) · airframe 60,345 hrs · 68,453 cycles

TAKE OFF WARNING SOUNDED ON TAKE OFF ROLL. FOUND FLAP INDICATOR DEFECTIVE, REMOVED AND REPLACED FLAP INDICATOR REF M/M 27-53-05 AND COMPLIED WITH T/O WARNING HORN, OPS CHECKS PER CARD 31-50-00Q

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 2) · airframe 59,946 hrs · 68,015 cycles

AFTER TAKEOFF AT APPROX 1000FT RUDDER PRESS, NR 2 RUD HYDS AND FULL RUDDER PRESS CAUTION LIGHTS ILLUMINATED. GROUND RAN AC, PERFORMED W/C 27-20-05Q, NO DEFECTS NOTED AT THIS TIME. BLED NR 2 HYD SYSTEM, NO DEFECTS NOTED. EVAL FLIGHT REQUESTED, EVAL FLIGHT SATISFACTORY.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 2 HYD SYSTEM) · airframe 59,946 hrs · 68,015 cycles

AFTER TAKEOFF, AT APPROX 1000 FT, NR 2 HYDS AND FULL PRESSURE CAUTION LIGHT ILLUMINATED. ACFT RETURNED TO THE FIELD. MX GROUND RAN THE ACFT AND PERFORMED WORKCARD 27-20-05Q. NO DEFECTS NOTED AT THAT TIME. MX BLED NR 2 HYDAULIC'S. AN EVALUATION FLIGHT WAS DONE AND SIGNED OFF AS SATISFACTORY.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 59,847 hrs · 67,908 cycles

EMERGENCY LIGHT SWITCH NORMAL BACK LIGHTING INOPERATIVE. REMOVED AND REPLACE BULB IAW MM 33-20-00.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 59,812 hrs · 67,867 cycles

WEATHER RADAR WILL NOT PAINT WEATHER OR GROUND. REMOVED AND REPLACED WEATHER RADAR RT IAW 34-41-04. OPS CHECK ON GROUND IAW BULLETIN 34-18, IS GOOD AT THIS TIME. OK FOR SERVICE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,400 hrs · 67,392 cycles

THE 14TH BULB EMERGENCY FLOOR LIGHTING INOP. RELAMPED BULB IAW 33-52-00, OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,400 hrs · 67,392 cycles

CABIN - CENTER CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW 33-51-00, OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 59,400 hrs · 67,392 cycles

THE 1ST FLOOR EMERGENCY FLOOR EMERGENCY LIGHT, 14TH FLOOR EMERGENCY FLOOR LIGHT AND CENTER CEILING EMERGENCY LIGHTS ARE INOP. RELAMPED BULBS IN ACCORDANCE WITH MAINTENANCE MANUAL 33-52-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,400 hrs · 67,392 cycles

FIRST ROW FLOOR EMERGENCY LIGHT INOPERATIVE. RELAMPED BULB IAW MM 33-52-00, OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,183 hrs · 67,143 cycles

UPON LINE CHECK AT SBY IT WAS FOUND THAT SEVERAL BULBS WERE BURNED OUT IN THE EMERGENCY EXIT SIGN AT ROW 1. RELAMPED BULBS AND THE OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,082 hrs · 67,024 cycles

NUMBER ONE EMERGENCY ESCAPE PATH LIGHT IN ROW ONE INOPERATIVE. REMOVED AND REPLACED BULB, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,778 hrs · 66,696 cycles

AFT OVER HEAD EMERGENCY LIGHT INOPERATIVE. REMOVED CEILING PANEL BEFORE REMOVING BULB, REINSTALL NEW BULB AND CEILING PANEL. OPS CHECK GOOD

Part: BETA SWITCH — BROKEN (NR 2) · airframe 58,513 hrs · 66,411 cycles

DURING TAKEOFF AND AFTER GEAR RETRACTION, THE NR 2 ENGINE STARTED TO SURGE BETWEEN 60 TO 100 PERCENT TORQUE. AFTER TURNING BACK TO FIELD, THE CONDITION CLEARED. MAINTENANCE CLEANED AND RESEATED THE ECU CONNECTOR, GROUND RAN AIRCRAFT AND NOTED NO DEFECTS. AIRCRAFT WAS THEN RELEASED FOR SERVICE AND DURING TAKEOFF AND GEAR RETRACTION, AGAIN THE NR 2 ENGINE TORQUE SURGED BETWEEN 40 AND 100 PERCENT. AFTER RPM REDUCTION, THE CONDITION CLEARED. DURING TROUBLESHOOTING BY MAINTENANCE, THE NR 2 ENGINE BETA BACKUP SWITCH (6141-S4) WAS FOUND TO BE BROKEN. THE SWITCH WAS CHANGED OUT AND THE AIRCRAFT WAS GROUND RUN AND OPS CHECKED GOOD PENDING AN EVALUATION FLIGHT. THE AIRCRAFT FLEW SATISFACTORILY AND WAS THEN RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 58,300 hrs · 66,155 cycles

RT INBOARD END CAP MISSING PART OF BOTTOM SKIN. FERRY FLIGHT 9310 FROM FLO TO SBY. REMOVED RT INBOARD END CAP AND TWO ASSOCIATED RIBS. INSTALLED TWO NEW RIBS AND NEW END CAP PANEL IAW DRAWING 85520002.

Part: LAMP — BURNED (EMERGENCY LIGHT)

SECOND FLOOR EMERGENCY LIGHT IS INOPERATIVE (FLOOR PROX EMERGENCY ESCAPE PATH RED LIGHTS). REMOVED AND REPLACED BULB, WORK COMPLETE. OPS CHECK GOOD. (S)

Part: LAMP — BURNED (EMERGENCY LIGHTS)

2ND RED FLOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB OPS CHECK GOOD MEL 33-13-2, CLEARED. (K)

Part: SELECTOR VALVE — MALFUNCTIONED (MLG)

LANDING GEAR WOULD NOT RETRACT. GEAR SELECT PANEL BOTH INTRANSIT AND GREEN SAFE LIGHTS ILLUMINATED, DUPLICATED DISCREPANCY ON JACKS FOR THE FIRST TIME. TAPPED ON LANDING GEAR SELECTOR VALVE AND GEAR RETRACTED. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW 32-30-41R, OPS AND LEAK CHECK GOOD. SEE HA300 SEQ 6 ACFT RELEASED FOR EVALUATION FLIGHT DUE TO AFTER GEAR RETRACTION NO GEAR DOORS WILL CLOSE, MAINTENANCE REMOVED AND REPLACED RELAYS 3261-K5, 3261-K6 & 3261-K7 OPS CHECK GOOD ON GROUND, MAINTENANCE ACTION COMPLETE. SUBJECT TO SATISFACTORY EVAL FLIGHT. FACT 24 MAY 08 10:59 SBY EVAL FLT SAT. (S)

Part: DIODE — MALFUNCTIONED (LANDING GEAR) · airframe 57,445 hrs · 65,167 cycles

LANDING GEAR WOULD NOT RETRACT WHEN SELECTED. REPLACED DIODES 3261-CR 3, 4, 5 AND 7. INSPECTED RELAY BASE K9 AND K11 AND CONNECTOR 9811-P94. GEAR SWING AND OPS CHECK GOOD. CHECKED DOOR SOLENOID SEQUENCE VALVE GROUNDS. UNABLE TO DUPLICATE PROBLEM ON JACKS. SYSTEM OPS CHECK GOOD.

Part: PSEU — MALFUNCTIONED (LANDING GEAR) · airframe 57,439 hrs · 65,152 cycles

AFTER DEPARTURE CYCLED GEAR UP AND GEAR DOORS DID NOT CLOSE. RETURNED TO FIELD SELECTED GEAR DOWN. UPON GEAR DOWN SELECTION ALL GEAR DOORS CLOSED. REMOVED AND REPLACED PSEU AND TESTED IAW 32-61-50, CYCLED GEAR IN NORMAL AND ALT OPS SATISFACTORY.

Part: DOOR — OPEN (LANDING GEAR) · airframe 57,439 hrs · 65,152 cycles

ACFT RELEASED FOR EVAL FLT DUE TO GEAR DOOR REMAINS OPEN AFTER GEAR RETRACTION. MX ACTION COMPLETE SUBJECT SATISFACTORY EVAL FLT.

Part: SEQUENCE VALVE — MALFUNCTIONED (NR 1) · airframe 57,439 hrs · 65,152 cycles

UPON GEAR UP SELECTION NOSE AND MAIN GEAR STAYED LOCKED DOWN DUE TO THE FACT THAT THE GEAR DOORS WOULD NOT OPEN. REMOVED AND REPLACED NR 1 MECHANICAL SEQUENCE VALVE IAW MM 32-10-41.

Part: DOOR — CLOSED (LANDING GEAR) · airframe 57,439 hrs · 65,152 cycles

ACFT RELEASED FOR EVAL FLT DUE TO GEAR DOORS WOULD NOT OPEN AND GEAR WOULD NOT RETRACT. MX ACTION COMPLETE SUBJECT SATISFACTORY EVAL FLT. EVAL FLT UNSATISFACTORY.

Part: WIRE — LOOSE · airframe 57,442 hrs · 65,162 cycles

AFTER GEAR WAS RETRACTED VIA NORMAL PROCEDURES, THE GEAR DOORS REMAINED OPEN WITH THE LANDING GEAR DOOR LIGHTS ILLUMINATED. THE GEAR WAS CYCLED AND THEN RETRACTED AGAIN. THE DOORS DID NOT CLOSE AND THE DOOR LIGHTS REMAINED ILLUMINATED. FOUND INHIBIT SWITCH, NR 25 TERMINAL TO HAVE TWO LOOSE WIRES. SECURED WIRING. EVAL FLIGHT, SATISFACTORY. OPERATIONAL CHECK GOOD.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 57,430 hrs · 65,137 cycles

AFTER DEPARTURE CYCLED GEAR UP, GEAR RETRACTED NORMALLY BUT ALL DOORS STAYED OPEN. CYCLED GEAR DOWN DOORS CLOSED NORMALLY, RETRACTED GEAR AGAIN DOORS, REMAINED OPEN AGAIN. REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE, OPS CHECKS GOOD IAW -8 MM 32-30-10.

Part: SELECTOR VALVE — DEFECTIVE (LANDING GEAR) · airframe 57,323 hrs · 65,013 cycles

AFTER SELECTING GEAR HANDLE UP, GEAR DOWN LIGHTS ILLUMINATED FOR APPROXIMATELY 5 MINUTES PLUS GEAR HANDLE LIGHT. THEN HEARD A CLUNK IN NOSE WHEEL AREA AND GEAR RETRACTED NORMALLY. AFTER INSPECTION, REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE PER W/C 32-30-41R. FUNCTIONAL CHECKS GOOD.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 56,990 hrs · 64,659 cycles

ON APPROACH NR 1 HYDRAULIC SYSTEM QTY WAS AT 1.5 QTS, AFTER LANDING COCKPIT GAUGE SHOWED 1.3 QTS. LOSS OF NORMAL BRAKES AND ISO LIGHT ILLUMINATED ON TAXI. NR 1 GAUGE ON NACELLE READS .5 QTS, SERVICED NR 1 HYDRAULIC SYSTEM, RAN AIRCRAFT TWICE AND CYCLED TOE BRAKES, OPS NORMAL AT THIS TIME. NO LEAKS NOTED, ISO LIGHT IS OUT. NOTE: NR 2 SYSTEM FOUND OVERSERVICED FROM FLUID TRANSFER, CORRECTED TO PROPER LEVEL. LEAK CHECK OF COMPLETE NR 1 HYDRAULIC SYSTEM, NO LEAKS FOUND.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 56,552 hrs · 64,163 cycles

AUTO FX DID NOT ARM ON TAKEOFF ROLL, REJECTED TAKEOFF. C/W AUTO FEATHER OPS CK IAW RUN UP MANUAL, OPS NORMAL. CLEANED AND INSPECTED SWITCHES 6121-57, 59, 513, 56, 512, 58, NO DEFECTS NOTED.

Part: RADAR — INOPERATIVE (WX SYSTEM)

PDT FLT 4189 PHL/CRW HAD THE WEATHER RADAR FAIL IN FLIGHT. CAPTAIN TRIED SEVERAL METHODS OF GETTING RADAR TO WORK, FLIGHT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED WEATHER RADAR, OPS CHECK OK.

Part: SERVO — MALFUNCTIONED (ELEVATOR) · airframe 55,477 hrs · 62,979 cycles

AFTER TAKEOFF THE ELEVATOR WAS SLOW TO MOVE. PITCH WAS VERY SLOW AS WELL. THE CREW DECLARED AN EMERGENCY AND RETURNED TO LGA. THE FLIGHT LANDED AND TAXIED WITHOUT INCIDENT. REMOVED AND REPLACED ELEVATOR SERVO, EVALUATION FLIGHT CHECK SATISFACTORY.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 51,897 hrs · 59,161 cycles

NOSE GEAR DID NOT INDICATE SAFE ON NORMAL OR ALTERNATE INDICATIONS. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,756 hrs · 55,763 cycles

DURING C-CHK, FOUND WIDESPREAD CORROSION ON STR 31S. DUE TO WIDESPREAD NATURE OF DAMAGE, DECISION MADE TO REMOVE ENTIRE STR SECTION FROM X182 TO FS PAR FR.(387) FOR CONVENIENCE IN LIEU OF REPEATED BLENDING AND MEASURING WITH SAME POTENTIAL RESULTS(SPLICE). THIS EO ACCOMPLISHES R/R`D BY PERFOMING SPLICES PER RD8-53-2499. THIS REPAIR IS A MAJOR REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,756 hrs · 55,765 cycles

DURING C-CHK, FOUND CORROSION UNDER COCKPIT FLOOR. THIS EO PERFORMS SPLICE REPAIR FOR STR 31 STARBOARD FOR CORROSION. THIS IS A MAJOR REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 48,756 hrs · 55,765 cycles

DURING C-CHECK, FOUND CORROSION ON SKIN FLANGES OF THE X488 FRAME WHICH WOULD REQUIRE FRAME LEG REPAIRS. DUE TO CONCURRENT, REMOVED AND REPLACED OF STR 31S IN THIS AREA, DECISION MADE TO REPAIR DAMAGE BY REPLACING DAMAGED SECTION OF THE FRAME. THIS EO8-53-04-0658 ACCOMPLISHES REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,756 hrs · 55,765 cycles

DURING C-CHK, FOUND CORROSION UNDER CABIN FLOOR. THIS EO8-53-04-0655 PERFORMD REPLACEMENT OR STR 31 STARBOARD FR X424 TO SECTION END AT X531 FOR CONVENIENCE OF CORROSION REPAIRS. NOTE THAT THE REPLACEMENT SECTION OF STR31 IS CUT AS ALLOWED BY RD.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,756 hrs · 55,765 cycles

DURING C-CHECK, FOUND CORROSION UNDER CABIN FLOOR WHICH RESULTED IN SPLICE REPAIR OF STR 31S . THIS EO PERFORMS SPLICE REPAIR TO X202 FRAME WHICH WAS REMOVED FOR WIDE SPREAD CORROSION. THIS IS A MAJOR REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,756 hrs · 55,765 cycles

THIS EO8-53-04-0670 PERFORMS REPAIR FOR STR 30S FOR CORROSION. THIS IS A MAJOR REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 48,756 hrs · 55,765 cycles

DURING C-CHK, FOUND CORROSION ON STR 31 STARBOARD, WHICH REQUIRED REMOVED AND REPLACED OF THE STRINGER. THIS EO8-53-04-0656 PERFORMS SPLICE OF X467 FRAME, WHICH HAD SECTIONS REMOVED FOR ACCESS FOR STR R/R`D. THIS EO IS A MAJOR REPAIR.

Part: SKIN — DENTED (AILERON) · airframe 48,756 hrs · 55,765 cycles

THIS EO8-57-04-0678 PERFORMS REPAIR FOR DENTED RT AILERON LOWER SKIN (P/N 85740055). NOTED DENT REPORTED AS OIL CANNING. REPAIR CONSISTS OF DRILLING OUT CENTER OF DENT TO RELIEVE OIL CANNING THEN INSTALLING EXTERNAL DOUBLER. THIS EO IS A MAJOR REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,756 hrs · 55,765 cycles

DURING C-CHECK, FOUND CORROSION UNDER CABIN FLOOR WHICH RESULTED IN SPLICE REPAIR OF STR 31S. THIS EO8-53-04-0630 PERFORMS SPLICE REPAIR TP X253 FRAME WHICH WAS REMOVED TO FACILITATE INSTALLATION OF REPLACEMENT SECTION OF STR31S. THIS IS A MAJOR REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,756 hrs · 55,763 cycles

DURING C-CHK, FOUND WIDESPREAD CORROSION ON STR 31S. DUE TO WIDESPREAD NATURE OF DAMAGE, DECISION MADE TO REMOVE ENTIRE STR SECTION FROM X182 TO FR (387) FOR CONVENIENCE IN LIEU OF REPEATED BLENDING AND MEASURING WITH SAME POTENTIAL RESULTS (SPLICE). THIS EO ACCOMPLISHES REMOVED AND REPLACED BY PERFUMING SPLICES PER RD8-53-2499. THIS REPAIR IS A MAJOR REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,756 hrs · 55,765 cycles

DURING C-CHECK, FOUND CORROSION UNDER CABIN FLOOR. THIS EO8-53-04-0632 PERFORMS SPLICE REPAIR TO X222 FRAME WHICH WAS REMOVED FOR WIDESPREAD CORROSION. THIS IS A MAJOR REPAIR.

Part: CONNECTOR — LOOSE (TRANSMITTER) · airframe 47,385 hrs · 54,263 cycles

NR 1 OIL PRESSURE INDICATES 45 PSI WITH NO WARNING LIGHT. FEATHERED ENGINE OIL PRESSURE BECAME ERRATIC. INFLIGHT EMERGENCY DECLARED AND DIVERTED TO CHO. INDICATION PROBLEM, FERRIED AIRCRAFT TO ROA. FOUND LOOSE CONNECTOR ON ENGINE. TIGHTENED AND RAN ENGINE BUT PROBLEM RETURNED. REPLACED OIL PRESSURE TRANSDUCER, GROUND RUN OPERATIONAL AND LEAK CHECK GOOD.

Part: SELECTOR PANEL — INOPERATIVE (MLG) · airframe 47,172 hrs · 54,035 cycles

WHEN SELECTED LANDING GEAR DOWN, 3 UNSAFE LIGHTS, GEAR DID NOT OPERATE, RECYCLED GEAR HANDLE, GEAR OPERATED NORMALLY. REMOVED AND REPLACED LANDING GEAR SELECTOR PANEL, OPS CHECK GOOD. (OPEN)

Part: STRUT — FLAT · airframe 41,473 hrs · 48,061 cycles

UPON GEAR RETRACTION, MAIN GEAR CAUTION LIGHTS REMAINED ON WITH W.O.W. CAUTION LIGHT. CYCLED GEAR, CAME DOWN AND LOCKED WITH THREE GREEN INDICATION. RETRACTED GEAR AGAIN, NOSE DOOR CAUTION LIGHT REMAINED ON WITH W.O.W. CAUTION LIGHT. EXTENDED GEAR AND RETURNED TO DEPARTURE FIELD. FOUND NLG SHOCK STRUT FLAT. RESEALED NLG STRUT CHARGING VALVE AND SERVICED STRUT.

Part: TUBE — BENT (NLG) · airframe 39,849 hrs · 46,295 cycles

NOSE LANDING GEAR DID NOT INDICATE LOCKED DOWN WITH NORMAL AND ALTERNATE INDICATION. CREW RETRACTED GEAR AND PERFORMED ALTERNATE EXTENSION. NORMAL INDICATION STILL SHOWED UNSAFE, BUT ALTERNATE INDICATION SHOWED GEAR AS LOCKED DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NLG DRAG STRUT PIVOT TUBE BENT. REPLACED PIVOT TUBE.

Part: CONTROL UNIT — CONTAMINATED (MLG WW) · airframe 39,620 hrs · 46,056 cycles

DURING TAKEOFF ROLL, THE LEFT AC BUS CAUTION LIGHT ILLUMINATED. CREW ABORTED TAKEOFF. FOUND DEICE FLUID CONTAMINATION IN NR 1 AC GENERATOR CONNECTOR. CLEANED CONNECTOR. ALSO REPLACED NR 1 AC GEN CONTROL UNIT.

Part: INVERTER — OVERHEATED (COCKPIT) · airframe 39,282 hrs · 45,674 cycles

CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE COCKPIT. REPLACED THE SECONDARY INVERTER.

Part: LIGHT — INOP (CABIN)

FIRST EMERGENCY LIGHT (FWD) ON FLOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT OPS CHECK GOOD.

Part: WIRE — BROKEN (LT MLG)

DURING GEAR EXTENSION LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED (RED LIGHT). CYCLED GEAR SEVERAL TIMES WITH SAME RESULTS. PERFORMED ALTERNATE EXTENSION AND ALTERNATE GEAR INDICATION 3 POINTS DOWN AND LOCKED. REPAIRED BROKEN WIRE AT STABILIZER STAY STRUT PROXIMITY SENSOR. ALL INDICATIONS NORMAL.

Part: TQ SENSOR TSCU — FAILED (NR 1 ENGINE)

FLT EN73 - PHF-ORF - DURING CLIMB-OUT, NR 1 ENGINE TORQUE ROLLED BACK FROM 90-30 PERCENT, ENGINE AUTOFEATHERED AND THE CREW SHUT ENGINE DOWN. THE AIRCRAFT CONTINUED TO ORF AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 ENGINE TORQUE SENSOR AND THE TORQUE SIGNAL CONDITIONING UNIT. (M)

Part: TQ SIGNAL COND — FAILED (NR 1 ENGINE)

FLT EN73 - PHF-ORF - DURING CLIMB-OUT, NR 1 ENGINE TORQUE ROLLED BACK FROM 90-30 PERCENT, ENGINE AUTOFEATHERED AND THE CREW SHUT ENGINE DOWN. THE AIRCRAFT CONTINUED TO ORF AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 ENGINE TORQUE SENSOR AND THE TORQUE SIGNAL CONDITIONING UNIT. REFERENCE HNAA9791132.

Part: EEL BATTERY — DISCHARGED (CABIN)

FLT 3158 - HPN-PHL - DURING PREFLIGHT WALKAROUND, FOUND THE CENTER OVERHEAD EMERGENCY DOWN LIGHTS AND EGRESS LIGHTS INOP. REMOVED AND REPLACED PS4 POWER SUPPLY AND BATTERY.

Part: EEL POWER SUPPLY — FAILED (CABIN)

FLT 3158 - HPN-PHL - DURING PREFLIGHT WALKAROUND, FOUND THE CENTER OVERHEAD EMERGENCY DOWN LIGHTS AND EGRESS LIGHTS INOP. REMOVED AND REPLACED PS4 POWER SUPPLY AND BATTERY.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT)

FLT 3306 - CLT-CAK - NR 1 ALTIMETER FLAGGED ON CLIMB-OUT AT 8000 FEET, AIRCRAFT TURNED BACK AND LANDED IN CLT WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ALTIMETER. PROBLEM RETURNED LATER IN THE DAY. FOUND WIRES CHAFED AT RNAV COMPUTER 3461-1-P3-1. CAPPED AND STOWED WIRING, MEL'D RNAV COMPUTER.