N907HA

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,064 hrs · 79,932 cycles

EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 5DF. R & R EMERGENCY CEILING LIGHT BULB AT ROW 5DF. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (RUDDER TRIM) · airframe 70,033 hrs · 79,893 cycles

RUDDER TRIM INOPERATIVE. INSPECTED AND CLEANED ACTUATOR CONNECTOR. OPS CHECKED GOOD.

Part: HOSE — KINKED (PITOT) · airframe 69,692 hrs · 79,488 cycles

F/O`S ASI READS HIGHER THAN CAPTAIN'S AFTER TAKEOFF AND FOR DURATION OF FLIGHT IAW CHECKLIST. SWITCHED TO ALT SOURCE. NO FIX, FOUND RT PITOT HOSE KINKED. REPLACED HOSE. LEAK CHECKED PITOT SYS. OPS CHECKED GOOD IAW MM 34-11-11 AND 34-11-02.

Part: BULB — DIM (CABIN LIGHT) · airframe 69,557 hrs · 79,316 cycles

CABIN, CEILING EXIT SIGN AT CENTER ISLE OF ROW 1 IS DIM, R & R DIM LIGHTS OF CEILING EXIT SIGN AT CENTER ISLE OF ROW 1 OPS CHECKED GOOD, REINSTALLED CEILING COVER.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 69,557 hrs · 79,316 cycles

-ESCAPE PATH EMERGENCY LIGHT BULB IS INOPERATIVE AT ROW 8 . R & R LIGHT, AISLE MARKER DUE TO BAD WIRE CONNECTION.

Part: CONTROL BOX — INOPERATIVE (ENGINE OIL) · airframe 69,255 hrs · 78,959 cycles

NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED CONTINUOUSLY ON CLIMB. OIL PRESSURE INDICATED NORMAL- IN GREEN ARC. ENGINE WAS SHUTDOWN IN FLIGHT. CREW REPORTED OIL/FUEL TEMPS NORMAL AND DID DECLARE AN EMERGENCY. CONNECTOR LIGHT REMAINS ON. JUMPED CONNECTOR , LIGHT REMAINS ON. R & R LIGHT CONTROL BOX. OPS CHECKED GOOD.

Part: GARLOCK SEAL — DAMAGED (HYD EDP) · airframe 69,185 hrs · 78,878 cycles

NR 1 OIL PRESSURE FLUCTUATED AND STEADILY FELL. FEATHERED NR 1 ENGINE AFTER PRESSURE FELL BELOW 55 PSI AND SHUTDOWN AFTER CONTINOUS ILLUMINATION OF CAUTION LIGHT. FOUND DRAIN LINE AT INBD IGNITER BAY CONNECTED TO PROP SHAFT DRAIN LEAKING. R & R PROP SHAFT SEAL AND DRAIN LINE, NO FIX. FOUND SHAFT SEAL ON ENGINE DRIVEN HYD PUMP AND GARLOC SEAL DAMAGE AND DETERIORATED. R & R SHAFT SEAL IAW AMM 29-10-11 AND GARLOC SEAL IAW MM 72-10-00. OPS AND LEAKED CHECKED GOOD.

Part: LINKAGE — MALFUNCTIONED (SYNC TRANSMITTER) · airframe 69,185 hrs · 78,878 cycles

PSCS SHOWS RT INBD SPOILER DEPLOYED. FOUND RT INBD SPOILER SYNCRO TRANSMITTER LINKAGE OVER CENTERED. REPOSITION AND CHECKED SECURITY. GROUND RAN AND OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 69,147 hrs · 78,833 cycles

ONE EMERGENCY FLOOR LIGHT IS INOPERATIVE AT ROW 9. R & R BULB AT ROW 9 EMERGENCY FLOOR PATH LIGHTING. OPS CHECKED GOOD.

Part: NONE — NONE (NONE) · airframe 69,108 hrs · 78,783 cycles

LEFT AFT EGRESS LIGHT BULB IS INOPERATIVE. CYCLED SWITCH, FOUND LIGHTS TO BE OPERATIONAL. OPS CHECKED GOOD.

Part: NONE — NONE (NONE) · airframe 69,108 hrs · 78,783 cycles

AISLE EMERGENCY LIGHT IS INOPERATIVE AT ROW 7. CYCLED SWITCH, FOUND LIGHT TO BE OPERATIONAL, OPS CHECKED GOOD.

Part: PSEU — MALFUNCTIONED (MLG) · airframe 69,033 hrs · 78,697 cycles

WOW CAUTION LIGHT ILLUMINATED ON LANDING ROLL FOR APPROX THREE SECONDS, THEN EXTINGUISHED. R & R PSEU IAW MM 32-61-50. CHECKED WOW SENSOR GAPS IAW MM 32-10-11.

Part: WIRE — DAMAGED (RT MLG) · airframe 68,701 hrs · 78,301 cycles

RT MLG ALTERNATE INDICATION IS INOPERATIVE. FOUND BROKEN WIRE. INSTALLED ENVIRONMENTAL SPLICE IAW STANDARD PRACTICE. OPS CHECKED GOOD. OK FOR SERVICE. LAST NIGHT, MX R & R SPLICES 3261-E1, 3262-E2. REPLACED LED 3262-CR1 AND 3262-CR2. NO FIX. CHECKED RESISTANCE OF RESISTORS 3262-R1, R2, R3 AND R4 RESISTORS. CHECKED GOOD. CLEANED CONNECTOR 3262-P3. NO FIX. R & R DOWN LOCK HARNESS ON RT MLG IAW MM 32-10-26. OPS CHECKED GOOD.

Part: RELAY — FAILED (AC BUSS) · airframe 68,290 hrs · 77,795 cycles

LT AC BUSS FAILURE IN FLIGHT WITH EMERGENCY LIGHTS FLICKERING. ALSO ASSOCIATED CAUTION LIGHTS ON. R & R 2421-S2 AND 2421-K2. RAN ENGINES FOR OVER 10 MINUTES. OPS CHECKED ALL AC POWER RELATED SYS. NO DISCREPENCIES NOTED AT THIS TIME.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 68,285 hrs · 77,789 cycles

12TH EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R BULB FOR EMERGENCY FLOOR PATH LIGHT. OPS CHECKED GOOD.

Part: UNKNOWN — WARNING LIGHT (AC BUSS) · airframe 68,285 hrs · 77,789 cycles

RT AC BUSS CAUTION LIGHT ILLUMINATED IN FLIGHT WITH ASSOCIATED CAUTION LIGHTS. PROBLEM OCCURED TWO MINUTES AFTER SELECTING PROP HEAT ON. ON PREVIOUS THREE LEGS, NO AC BUSS CAUTION LIGHT WITH PROP HEAT SELECTED OFF. R & R 2421-S2. R & R 2421-K2. RAN ENGINES FOR OVER 10 MINUTES. OPS CHECKED ALL ACFT POWER RELATED SYS. NO DISCREPENCIES NOTED AT THIS TIME.

Part: UNKNOWN — UNKNOWN · airframe 68,266 hrs · 77,765 cycles

ON CLIMB OUT, LT AC BUSS, LT TRU AND LT ELEVATOR HORN HEAT CAUTION LIGHTS ILLUMINATED. RETURN TO FIELD. INSPECTED BOTH 1 AND 2 ENGINES PROP BRUSH BLOCKS AND CLEANED CONNECTOR PLUGS AS WELL. INSPECTED BOTH ENGINES PROP HEATER LEADS. NO DEFECTS NOTED. GROUND RAN BOTH ENGINES WITH PROP HEAT ON. WINDSHIELD HEAT AND ELEVATOR HORN HEAT ON. LOADS ARE GOOD. OPS CHECKED GOOD.

Part: BRUSH BLOCK — SATURATED (ELEVATOR HEAT) · airframe 68,265 hrs · 77,764 cycles

ON CLIMBOUT, RT AC BUSS, RT TRU AND RT ELEVATOR HORN HEAT CAUTION LIGHTS CAME ON. STAYED ON FOR ENTIRE FLIGHT. NR 2 BRUSH BLOCK WAS OILED SOAKED. R & R NR 2 PROP BRUSH BLOCK. OPS CHECKED GOOD. OPS CHECKED IAW WC 24-20-04Q. BUS CONTACTOR OPS CHECKED NORMAL. OPS CHECKED ELEVATOR HORN HEAT IAW AMM 30-10-00. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: GENERATOR — INOPERATIVE (NR 2) · airframe 68,266 hrs · 77,765 cycles

ON CLIMB OUT, RT AC BUSS, RT TRU AND RT ELEVATOR HORN HEAT CAUTION LIGHTS ILLUMINATED. ACFT WAS AIR TURNBACK. R & R NR 2 AC GENERATOR, GCU IAW WC 24-20-11R. OPS AND LEAK CHECKED GOOD.

Part: CONNECTOR — SATURATED (BRUSHBLOCK) · airframe 68,232 hrs · 77,728 cycles

DURING CRUISE FLIGHT AT 12K, SELECTED PROP HEAT ON AND RT AC BUSS FAULT OCCURED. INSPECTED BOTH PROP BRUSH BLOCKS, FOUND NR 2 PROP BRUSH BLOCK CONNECTOR PLUG SOAKED WITH DEICE FLUID. CLEANED AND DRIED CONNECTOR PLUG AS REQUIRED. GROUND RAN BOTH ENGINES WITH PROP HEAT ON. OPS AND LOADS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (WINDSHIELD HEAT) · airframe 67,707 hrs · 77,074 cycles

RIGHT WINDSHIELD HOT LIGHT ILLUMINATED. INSPECTED SENSOR WIRING ARRANGEMENT. FOUND TO BE ON PRIMARY SENSOR. CHECKED SENSORS RESISTANCE. FOUND TO BE WITHIN LIMITS IN REF TO PPO CMM 56-10-01. SENSOR REF 30-41-00. OPS CHECKED GOOD AT THIS TIME.

Part: DOOR — OUT OF RIG (MLG) · airframe 67,527 hrs · 76,842 cycles

LEFT DOOR AMBER LIGHT REMAINED ILLUMINATED WITH GEAR UP. RECYCLED GEAR STILL ILLUMINATED. FORWARD DOOR REMAINED OPEN. ACFT RETURNED TO FIELD. RERIGGED NR 1 FORWARD GEAR DOOR IAW MM32-10-21. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 67,516 hrs · 76,833 cycles

FORWARD CENTER CEILING EMERGENCY EXIT SIGN IS INOP. FOUND FORWARD CENTER CEILING LIGHT WIRE UNPLUGGED AND MATRIX CONNECTOR DAMAGED. R & R MATRIX CONNECTOR AND PLUGGED WIRES ACCORDINGLY. OPS CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 67,516 hrs · 76,833 cycles

LEFT FORWARD EXTERIOR EMERGENCY LIGHT IS DIM. R & R BATTERY. OPS CHECKED GOOD.

Part: BRACKET — CORRODED (BS 600) · airframe 67,516 hrs · 76,832 cycles

SURFACE CORROSION AT ANGLE BRACKET JUST BELOW FLOOR AT STA X600 FRONT OF UPPER BAG BAY FLOOR. CORROSION WAS REMOVED, APPLIED ALODINE AND PRIMER TO ANGLE BRACKET AT STA X600.

Part: BOLT — CORRODED (RT WING) · airframe 67,516 hrs · 76,832 cycles

RT WING TO FUSELAGE STRUT HAD RUSTED BOLT AND BORE INSIDE OF PANEL 264CR. CLEANED BORE WITH BARREL BRUSH. CORROSION WAS TRANSFERED FROM CORRODED BOLT. INSTALLED NEW BOLT AND PLI WASHER.

Part: FLOORBEAM — CORRODED (BS 600) · airframe 67,516 hrs · 76,832 cycles

UPPER BAG BAY FLOORBEAM ABOVE STR 31S AT BS 600 HAS CORROSION. REMOVED CORROSION FROM UPPER BAGBAY FLOORBEAM. ALODINED AND PRIMED AREA.

Part: BOLT — CORRODED (LT WING) · airframe 67,516 hrs · 76,832 cycles

AFT OTBD BOLT AND BORE IF LT AFT WING TO FUSELAGE STRUT IS RUSTED INSIDE OF PANEL 263CL. REAMED HOLE IAW DWG 85320339. CLEANED CORRSION, R & R BOLT AND PLI WASHER.

Part: BOLT — CORRODED (LT WING) · airframe 67,516 hrs · 76,832 cycles

FORWARD INBD BOLT IS PITTED ON AFT STRUT, LT WING TO FUSELAGE ATTACH POINT. R & R BOLT AND PLI WASHERS.

Part: SEAT TRACK — CORRODED (BS 424) · corrosion level 2 · airframe 67,516 hrs · 76,832 cycles

MINOR CORROSION AT RIGHT OTBD SEAT TRACK AT BS 424. SEAT TRACK OUT OF LIMITS IAW RD8-53-1342. REMOVED & INSTALLED NEW SEAT TRACK IAW DWG 85320777.

Part: BOLT — RUSTED · airframe 67,516 hrs · 76,832 cycles

LEFT AFT STEEL STRUT TO WING RIB BOLT IS RUSTED AND BORE OF STRUT. REAMED HOLE TO .541 IAW DWG 85320229. CLEANED CORROSION AND R & R BOLT AND NEW PLI WASHERS.

Part: SEAT TRACK — CORRODED (BS 501) · airframe 67,516 hrs · 76,832 cycles

SURFACE CORROSION AT LT OTBD SEAT TRACK AT BS 501. REMOVED CORROSION ON LT SEAT TRACK IAW RD8-53-1342. COMPLIED WITH HFEC INSPECTION. NO DEFECTS NOTED.

Part: SHEAR TIE — CORRODED (BS 270.5) · airframe 67,516 hrs · 76,832 cycles

CORROSION ON FRAME LEG AT STA X270.500 BETWEEN STR 32P AND 31P. CLEANED CORROSION, APPLIED ALODINE AND PRIMER.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,516 hrs · 76,832 cycles

AIRSTAIR DOOR OPENING THRESHOLD HAS SURFACE CORROSION AROUND NUT PLACES ON TOP AND BOTTOM SIDES OF THRESHOLD. REMOVED AIRSTAIR DOOR OPENING THRESHOLD AND INSTALLED IAW DWG 85321241.

Part: SEAT TRACK — CORRODED (BS 366-387) · corrosion level 2 · airframe 67,516 hrs · 76,832 cycles

SURFACE CORROSION AT LT OTBD SEAT TRACK BS 387 THRU 366. SEAT TRACK DAMAGE IS OUT OF LIMITS. R & R SEAT TRACK IAW DWG 85320777.

Part: FLOORBEAM — CORRODED (BS 467) · airframe 67,516 hrs · 76,832 cycles

SURFACE CORROSION AT BS 467 FLOORBEAM JUST BELOW LT AND RT INBD SEAT TRACK. CLEANED CORROSION . APPLIED ALODINE AND PRIMER.

Part: SEAT TRACK — CORRODED (BS 330) · airframe 67,516 hrs · 76,832 cycles

SURFACE CORROSION AT LT INBD SEAT TRACK AT BS 330. BLENDED AFFECTED AREA TO WITHIN LIMITS OF RD8-53-1339. HFEC INSPECTION COMPLIED WITH. NO DEFECTS NOTED.

Part: FRAME — CORRODED (BS 222 S31R) · airframe 67,516 hrs · 76,832 cycles

STRINGER 31S AND FRAME LEG IS CORRODED AT STATION X222. CLEANED CORROSION FROM FRAME LEG AND STRINGER 31S AT STA X222. APPLIED ALODINE AND PRIMED AREA.

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · airframe 67,516 hrs · 76,832 cycles

SEVERAL AREAS OF LIGHT CORROSION ON OTBD FLOOR SUPPORT, AROUND AFT ATTACH HOLE FOR WARDROBE FLOOR. CLEANED CORROSION FROM OTBD FLOOR SUPPORT. ALODINED AND PRIMED AREA AS REQUIRED.

Part: SHEAR TIE — CORRODED (BS 222) · airframe 67,516 hrs · 76,832 cycles

FRAME LEG AT STATION X222 HAS SURFACE CORROSION BETWEEN STR 28S AND 29S. REMOVED CORROSION AT FRAME LEG STA X222 BETWEEN STR 28S AND 29S. APPLIED ALODINE AND PRIMER TO AREA.

Part: DOOR — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 67,516 hrs · 76,832 cycles

LAVATORY SERVICE DOOR IS CORRODED. REMOVED CORRODED LAVATORY DOOR. INSTALLED NEW LAVATORY DOOR ASSY IAW DWG 85320983.

Part: SHEAR TIE — CORRODED (BS 240.5 S27-28L) · airframe 67,516 hrs · 76,832 cycles

CORROSION AT FRAME LEG X240.500 BETWEEN STR. 28P AND 27P. REMOVED BRACKET FROM FRAME AT STA.X240.500. REMOVED FRAME SECTION AT STA X240.500, FORMED AND HEAT TREATED FRAME MEMBER IAW DWG 85320497. ALODINED AND PRIMED AS REQUIRED. COMPLIED WITH CONDUCTIVITY TEST.

Part: SHEAR TIE — CORRODED (BS 242 S30-31R) · airframe 67,516 hrs · 76,832 cycles

FRAME LEG AT STATION X242 BETWEEN STR 31S AND 30S HAS SURFACE CORROSION. REMOVED CORROSION FROM FRAME LEG AT STA X242 BETWEEN STR 31S AND 30S. APPLIED ALODINE AND PRIMER.

Part: STRINGER — CORRODED (BS 387 S28L) · airframe 67,516 hrs · 76,832 cycles

CORROSION AT STRINGER 28P WHERE IT MEETS MAIN FRAME X387 .350. REMOVED BRACKET ON STRINGER 28P ATTACH POINT TO MAIN FRAME X387.350. CLEANED MINOR SURFACE CORROSION FROM STRINGER AND APPLIED ALODINE AND PRIMER.

Part: STRINGER — CORRODED (BS 201-242) · airframe 67,516 hrs · 76,832 cycles

STRINGER 31S HAS CORROSION BETWEEN FRAME X242 AND X201. REPAIRED IAW RD8-53-3044. PERFORMED HFEC INSPECTION. NO DEFECTS NOTED. APPLIED ALODINE AND EPOXY PRIMER IAW RD8-53-3044.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,516 hrs · 76,832 cycles

LAVATORY MACHINED DOUBLER ON CUTOUT IS CORRDED. REMOVED MACHINE DOUBLER, INSTALLED NEW MACHINED DOUBLER IAW DWG 85320983.

Part: STRINGER — CORRODED (BS 270-291) · airframe 67,516 hrs · 76,832 cycles

STRINGER 22P HAS CORROSION BETWEEN FRAME X270.500 AND X291.400. FOUND LIGHT CORROSION IN AREA INDICATED. BLENDED, ALODINE AND EPOXY PRIMED TREATED AREA IAW DASH 8 STRUCTURAL REPAIR MANUAL 51-20-11, 51-20-16 AND 51-20-36.

Part: FRAME — CORRODED (BS 383) · airframe 67,516 hrs · 76,832 cycles

CORROSION AT "L" BRACKET ON BOTH SIDES OF MAIN FRAME STA X383, STR 22P. REMOVED FORWARD AND AFT ANGLE ON MAIN FRAME AT STA.X387. BLENDED LIGHT CORROSION TO WITHIN LIMITS IAW SRM 51-20-11. ALODINED, PRIMED AND REINSTALLED IAW DWG 85320777.

Part: FRAME — CORRODED (BS 434.5) · airframe 67,516 hrs · 76,832 cycles

CORROSION AT FRAME STA X434.500 AND STR 22P. REMOVED 1 AFT ANGLE AT MAIN FRAME, STRINGER TO SEAT RAIL WEB AND ANGLE FROM STA 443, STRINGER TIE. CLEANED, BLENDED LIGHT CORROSION TO WITHIN LIMITS. ALODINE AND PRIMED. REINSTALLED IAW SRM 51-20-11 AND DWG 85330511.

Part: FRAME — CORRODED (BS 405.737) · airframe 67,516 hrs · 76,832 cycles

CORROSION AT FRAME BS 405.737 AND STR 21P AND BRACKET BETWEEN STR.22P AND 21P. REMOVED CLEAR FROM STR 22P SEAT RAIL TO FRAME BRACKET. BLENDED LIGHT CORROSION TO WITHIN LIMITS IAW SRM 51-20-11. ALODINED AND PRIMED. REINSTALLED IAW DWG 85320777.

Part: FRAME — CORRODED (BS 445.5) · airframe 67,516 hrs · 76,832 cycles

CORROSION AT FRAME BS 445.500 AND STR. 22P. REMOVED CLEAT AND BLENDED TO WITHIN LIMITS IAW SRM 51-20-11. ALODINE AND PRIMED. REINSTALLED IAW DWG 85320511.

Part: BOLT — RUSTED (WING TO FUSE) · airframe 67,516 hrs · 76,832 cycles

LT AFT WING TO FUSELAGE STRUT HAS RUSTED BOLT AND HOLE AT FORWARD END OF AFT STRUT, OTBD BOLT. CLEANED BOLT HOLE WITH BRUSH. NO CORROSION REMAINED. INSTALLED NEW BOLT AND PLI WASHERS.

Part: FRAME — CRACKED (BS 312.35) · airframe 67,516 hrs · 76,832 cycles

FRAME AT BS 312.35 IS CRACKED BETWEEN STR 22P AND 23P. REPAIRED IAW EO8-53-12-0392.

Part: STRINGER — CORRODED (BS 215.5 S27R) · airframe 67,516 hrs · 76,832 cycles

STRINGER 27S IS CORRODED AT STATION X215.500, JUST BELOW LAV SERVICE PORT. REMOVED STR 27S BELOW LAV. REMOVE PRIMER AND FOUND CORROSION TO BE MINOR. LIGHTLY CLEANED, ALODINED AND PRIMED. REINSTALLED STRINGER 27S.

Part: SEAT TRACK — CORRODED (BS 330) · airframe 67,516 hrs · 76,832 cycles

SURFACE CORROSION AT LEFT INBD SEAT TRACK BS 330. BLENDED AFFECTED AREA TO WITHIN LIMITS OF RD8-53-1339. COMPLIED WITH HFEC INSPECTION. NO DEFECTS NOTED.

Part: INTERCOSTAL — CORRODED (BS 242-252) · corrosion level 2 · airframe 67,516 hrs · 76,832 cycles

INTERCOSTAL AT STRINGER 27S FROM BS 242 TO 252 IS CORRODED AND CRACKED AT FORWARD END. ALODINED AND HEAT TREATED NEW INTERCOSTAL IAW DWG 85320813. COMPLIED WITH CONDUCTIVITY CHECK, ALODINED AND PRIMED. INSTALLED NEW FABRICATED INTERCOSTAL IAW DWG 85320854. CONDUCTIVITY CHECKED GOOD.

Part: STRINGER — CORRODED (BS 234.5 S27R) · corrosion level 2 · airframe 67,516 hrs · 76,832 cycles

STRINGER 27S IS CORRODED AND RIVETED FRAME MEMBER IS CRACKED AND CORRODED AT STA X234.500. REMOVED FRAME MEMBER CORROSION WAS FOUND TO BE ISOLATED TO FRAME MEMBER ONLY. NO CORROSION WAS FOUND ON STR 27S. INSTALLED NEW FABRICATED FRAME MEMBER IAW DWG 85320854. CONDUCTIVITY CHECK WAS GOOD.

Part: STRINGER — CORRODED · corrosion level 2 · airframe 67,516 hrs · 76,832 cycles

STRINGER 27S IS CORRODED AT STA X242.00. REMOVED FRAME MEMBER AT STA X222 TO STA X242 FOR BEING CORRODED AND STR 27S WAS EVALUATED. FORMED AND HEAT TREATED INTERCOSTAL IAW DWG 852808. CORROSION WAS FOUND TO BE ISOLATED TO FRAME MEMBER ONLY. NO CORROSION WAS FOUND ON STR 27S. INSTALLED NEW FABRICATED FRAME MEMBER IAW DWG 85320854 ALODINED, PRIMED AS REQUIRED. CONDUCTIVITY CHECK WAS GOOD.

Part: SHEAR TIE — CORRODED (BS 270 S31-32R) · airframe 67,516 hrs · 76,832 cycles

FRAME LEG AT BS 270, STR 31S AND 32S ARE CORRODED. CLEANED FRAME LEG IAW SRM 51-20-11. ALODINED AND PRIMED AS REQUIRED.

Part: SHEAR TIE — CORRODED (BS 252 S31-32R) · airframe 67,516 hrs · 76,832 cycles

FRAME LEG AT BS 252.00, STR 31S AND 32S ARE CORRODED. CLEANED FRAME LEG AT STA X252, STR 31S AND 32S IAW SRM 51-20-11. ALODINED AND PRIMED AS REQUIRED.

Part: STRINGER — CORRODED (BS 488 S23L) · airframe 67,516 hrs · 76,832 cycles

SEVERAL AREAS OF CORROSION AT STRINGER 23P AND FORWARD AND AFT OF FRAME BS 488. FOUND LIGHT CORROSION AT AREAS INDICATED. BLENDED, ALODINED AND EPOXY PRIMED AREA IAW -8 SRM 55-20-11, 51-20-16 AND 51-20-36 AND CORROSION PREVENTION CONTROL MANUAL, CHAPTER 4.

Part: HINGE — CORRODED (SPOILER) · airframe 67,515 hrs · 76,832 cycles

OTBD ROLL SPOILER HINGE ASSY HAS CORRODED FORWARD MOUNT BOLT AND NUT. CLEANED OFF LIGHT SURFACE CORROSION ON OTBD ROLL SPOILER HINGE ASSY HARDWARE. APPLIED LPS 3 AS NEEDED.

Part: SKIN — CORRODED (ANTENNA MOUNT) · airframe 67,515 hrs · 76,832 cycles

POSSIBLE CORROSION UNDER FORWARD RADIO ALTIMETER ANTENNA. UPON REMOVAL OF RADIO ALTIMETER ANTENNA AND PLATE. FOUND PITTING AND TOOLING GOUGE MARKS ON SKIN OF FUSELAGE. AFTER FURTHER INSPECTION. FOUND DEEPER SCRATCHES TO BE .003". FOUND TO BE WITHIN LIMITS IAW SRM 53-00-26 AND SRM 51-20-11.

Part: TRANSCEIVER — FAILED (WX RADAR) · airframe 67,354 hrs · 76,623 cycles

WEATHER RADAR NOT PAINTING KNOWN WEATHER AS REPORTED BY ATC. R & R WEATHER RADAR R/T. OPS CHECKED GOOD IAW MM 34-41-04.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 67,315 hrs · 76,575 cycles

BAG BAY SMOKE WARNING LIGHT ILLUMINATED CONTINUOSLY. NO SMOKE IN BAG BAY (DOOR OPEN WITH LIGHT ON). R & R NR 2 BAG BAY SMOKE DETECTOR IAW MM 27-12-01. OPS CHECKED GOOD. CLEARED MEL.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 67,160 hrs · 76,393 cycles

FIRST CEILING EMERGENCY LIGHT INOPERATIVE. R & R BULB AS REQUIRED. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 67,160 hrs · 76,393 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. R & R BULB AS REQUIRED. OPS CHECKED GOOD.

Part: ACM — FAILED · airframe 67,089 hrs · 76,311 cycles

HUMMING NOISE AND VIBRATION NOTICED IN FWD COCKPIT AREA. 15 MINUTES LATER, BURNING ODOR IN FLIGHT DECK AND CABIN AREA. INSPECTED AND FOUND ACM LOCKED UP. R & R ACM IAW WORKCARD 21-50-03L. OPS AND LEAKED CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY — WEAK (EMERGENCY LIGHTS) · airframe 66,456 hrs · 75,588 cycles

LEFT AFT EMERGENCY EGRESS LIGHT IS INOP. R & R EMERGENCY LIGHT BATTERY AT ROW 3AC. OPS CHECKED GOOD.

Part: BATTERY — WEAK (EMERGENCY LIGHTS) · airframe 66,456 hrs · 75,588 cycles

OVERHEAD CENTER AISLE EMERGENCY LIGHT AT ROW 7 INOPERATIVE. R & R EMERGENCY LIGHT BATTERY AT ROW 3AC. OPS CHECKED GOOD.

Part: WARNING LIGHT — MALFUNCTIONED (MLG) · airframe 66,411 hrs · 75,571 cycles

DURING GEAR EXTENSION, RT MLG UNSAFE LIGHT REMAINED ON DURING GEAR EXTENSION. COMPLIED WITH EMERGENCY CHECKLIST, ALT VISUAL INDICATION INDICATED RT GEAR UNSAFE.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 66,355 hrs · 75,508 cycles

ROW 4 RED EMERGENCY LIGHTS POSITIONED IMPROPERLY ON FLOOR. REPOSITION EMERGENCY LIGHTS AT ROW 4.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 66,301 hrs · 75,442 cycles

CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 7. REMOVED LENS, R & R BULB AT ROW 7. REINSTALLED LENS.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 66,301 hrs · 49,442 cycles

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

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 66,255 hrs · 75,392 cycles

EMERGENCY EXIT DOOR SIGN IN ROW 4DF IS INOPERATIVE. RELAMPED EMERGENCY EXIT SIGN AT SEAT 4DF AND REINSTALLED LIGHT COVER.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 66,198 hrs · 75,328 cycles

EMERGENCY FLOOR PATH LIGHT IS INOP AT ROW 4. R & R EMERGENCY FLOOR PATH LIGHT LAMP AT ROW 4, CLOSED ACCESS PANEL. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 66,187 hrs · 75,315 cycles

ROW 2AC EMERGENCY CEILING LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: FAILSAFE — FAILED (MLG DOOR) · airframe 65,419 hrs · 74,410 cycles

RT FWD MAIN GEAR DOOR WILL NOT CLOSED AFTER GEAR RETRACTION. R & R FAIL-SAFE PLATE, BELL CRANK LEVER TUBE HINGE PIN IAW MM 32-10-21 AND PERFORMED ALTERNATE EXTENSION IAW MM 32-35-00.

Part: INDICATOR — STUCK (RADAR) · airframe 65,409 hrs · 74,400 cycles

RADAR STUCK IN STANDBY MODE AND WILL NOT CLEAR. R & R RADAR INDICATOR AND OPS CHECKED GOOD.

Part: SOCKET — CRACKED (CABIN LIGHTS) · airframe 65,350 hrs · 74,336 cycles

DURING TAXI, ELECTRIC SMELL IN CABIN AND FLIGHT DECK. OVERHEAD LIGHTS AND C/B'S ARE ACTIVATED. FOUND OVERHEAD POWER STRIP FIXED, END SOCKET CRACKED. R & R LIGHT STRIP AT ROW 2DF. OPS CHECKED GOOD. CABIN INTERIOR NORMAL LIGHTING SYS, COMPLIED WITH SPECIAL PROCEDURES 33-1. C/B'S REMAINS LT MAIN, A1 AND B1 PULLED AND COLLARED.

Part: ENGINE — ODOR (NR 2) · airframe 65,288 hrs · 74,275 cycles

STRONG BURNING ODOR IN COCKPIT DURNING APPROACH AND AFTER LANDING, ONLY WHEN BLEEDS ARE ON. R & R NR 2 ENGINE ASSY IAW WORK CARD 71-00-01R AND 71-00-02X.

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 65,279 hrs · 74,266 cycles

PAX DOOR WARNING LIGHT ON IN FLIGHT. ENTRY DOOR INDICATION W/MOD APPENDEX 5. COMPLIED WITH. CIRCUIT BREAKER B/4 PULLED FOR FLIGHT OPS. PUSHED IN AFTER LANDING.

Part: BRAKE ASSY — OVERHEATED (MLG) · airframe 65,247 hrs · 74,224 cycles

NR 3 AND NR 4 BRAKE ASSY OVERHEATED AND CAUGHT FIRE DURING TAXI CHECK. R & R NR3 AND NR4 BRAKE ASSY IAW WORKCARD 32-42-11X.

Part: BRAKE ASSY — FIRE (MLG) · airframe 65,247 hrs · 74,224 cycles

NR 3 AND NR 4 MAIN WHEEL ASSY OVERHEATED. CAUGHT ON FIRE. R & R NR 3 AND NR 4 MAIN WHEEL ASSY IAW 32-10-03I.

Part: UNKNOWN — ODOR (CABIN) · airframe 65,241 hrs · 74,218 cycles

ACFT ESPECIALLY AFT AREA SMELLS LIKE BURNING PLASTIC IN FLIGHT. INSPECTED SIDEWALL AND OVERHEAD LIGHTING, NO DEFECTS NOTED. OK FOR SERVICE.

Part: SEAL — FAILED (PAX DOOR) · airframe 64,970 hrs · 73,900 cycles

F/A REPORTS DAYLIGHT VISIBLE AROUND PAX DOOR IN FLIGHT. LOAD SQUEAL NOISE HEARD. REPLACED DOOR STOP TENSION BOLT AND BUSHING AT THE FORWARD NR 5 POSITION AND ADJUSTED II -8, MM 52-10-00. FOUND DOOR SEAL PULLING APART ALONG TOP OF DOOR WAY. R & R DOOR SEAL IAW -8, MM 52-5-00. PRESSURIZED ACFT. NO LEAKS.

Part: VALVE — INOPERATIVE (NR 1 OIL TEMP) · airframe 64,034 hrs · 72,879 cycles

NR 1 ENGINE OIL TEMP RUNNING AT 120 DEGREES. DEVERTED, R & R NR 1 OIL COOLER THERMO VALVE IAW CMM79-20-11, OPS CHECKED AND LEAK CHECKED GOOD.

Part: RELAY — FAILED (PAX DOOR) · airframe 63,582 hrs · 72,354 cycles

PAX DOOR WARNING LIGHT ILLUMINATED AT DEPARTURE TIME. SYS WAS DEACTIVATED IAW MEL 52-5, APPENDIX 5, EARLIER THAT DAY. CIRCUIT BREAKER PULLED AND COLLARED. MX INSPECTED PAX DOOR SENSORS AND MASTER WARNING PANEL CONNECTOR. RESEATED CONNECTOR. NO FIX. R & R RELAY 5271-K1, R & R ANNUNCIATOR WARNING PANEL. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (PAX DOOR WARNING) · airframe 63,582 hrs · 72,354 cycles

AFTER TAKEOFF, PAX DOOR WARNING LIGHT ILLUMINATED. R & R DOOR CLOSED PROX SENSOR IAW MM 52-10-00. OPS CHECKED GOOD.

Part: WIRE — MISINSTALLED (PAX DOOR WARNING) · airframe 63,572 hrs · 72,345 cycles

PASSENGER DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. INSPECTED SENSOR AND WIRING FOR HANDLE IN CLOSET. FOUND WIRE PULLED OFF BARREL MATRIX CONNECTOR. R & R MATRIX AND REINSTALLED WIRES. OPERATED DOOR. OPS CHECKED GOOD AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,155 hrs · 71,890 cycles

ROW 1DF SIDEWALL EMERGENCY LIGHT HAS ONE BULB INOP. RELAMPED ROW 1DF SIDEWALL EMERGENCY LIGHT BULB IAW AMM 33-30-00.

Part: FUEL FILTER — DIRTY (NR 2) · airframe 62,212 hrs · 70,783 cycles

NR 2 FUEL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. ALL OTHER PERIMETERS NORMAL. INSPECTED AND FOUND FUEL FILTER DIRTY, R & R LP AND HP FUEL FILTERS IAW WORK CARD 73-20-02R, 73-10-04R ON NR 2 ENGINE. ALSO, R & R HP FUEL FILTER CONNECTOR PLUG USING SMP RAN ACFT, OPS AND LEAKED CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 61,727 hrs · 70,261 cycles

ONE FLOOR LEVEL EMERGENCY LIGHT AT ROW 8 IS IN OPERATIONAL. RE-LAMPED IAW 33-52-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 61,727 hrs · 70,261 cycles

OVERHEAD EMERGENCY EXIT MARKER FOR ROW 4 IS DIM. REMOVED LIGHT LENS, REMOVED AND REPLACED BURNED OUT LIGHT AS REQUIRED.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 61,641 hrs · 70,181 cycles

ALL EMERGENCY LIGHTS FLICKERED ON CLIMB OUT FOLLOWED BY BOTH INTAKE DOOR ON/HEATER LIGHTS AND PROP SYNC. REMOVED AND REPLACED NR 2 BRUSH BLOCK AND PINS A AND C ON BRUSH BLOCK CONNECTOR IAW 61-10-11, REPLACED RELAY 3061-K2 AND CHANGED ALL SOCKETS IN CONNECTOR 3061-P5.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,576 hrs · 70,115 cycles

ROW 2 FLOOR LEVEL EMERGENCY LIGHT NOT WORKING. REMOVE AND REPLACED ROW 2 FLOOR LEVEL EMERGENCY LIGHT MODULE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,537 hrs · 70,065 cycles

EMERGENCY FLOOR LIGHT AT ROW 4 IS MISSING. INSTALLED NEW EMERGENCY LIGHT.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,537 hrs · 70,065 cycles

EMERGENCY FLOOR LIGHT (RED) AT ROW 1 IS NOT OPERATING. REMOVED AND REPLACED RED EMERGENCY FLOOR LIGHT MODULE.

Part: SENSOR — MALFUNCTIONED (MLG DOOR) · airframe 61,262 hrs · 69,766 cycles

RT DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION UNTIL FLAP RETRACTION. REMOVED AND REPLACED FWD STAY DOOR SENSOR IAW AMM 32-61-00. OPS CHECKED GOOD, CYCLED LANDING GEAR SEVERAL TIMES.

Part: BRUSH BLOCK — DIRTY (PROP HEAT) · airframe 61,248 hrs · 69,751 cycles

EMERGENCY LIGHTS FLICKERING IN FLIGHT. PULLED AND COLLARD RT TRU CIRCUIT BREAKER. PERFORMED W.C'S 33-50-06Q AND 33-50-03Q, CLEANED NR 2 ENG PROP HEAT BRUSH BLOCK. RAN ACFT WITH EMERGENCY LIGHTS ARMED, NO DISCREPANCIES NOTED, OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMEGENCY LIGHTS) · airframe 61,248 hrs · 69,751 cycles

EMERGENCY FLOOR LIGHT OUT AT ROW 3 D/F. FLOOR PROXIMITY EMERGENCY ESCAPE PATH RED LIGHTS. RE-LAMPED EMERGENCY FLOOR LIGHT ROW 3D/F IAW MM 33-51-05. OPS CHECK OK.

Part: WIRE — BROKEN (SPOILER SYS) · airframe 60,071 hrs · 68,427 cycles

SPOILER NR 1 SWITCH LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. INSPECTED SWITCHES AND CONNECTORS AT BOTH SPLR CLUTCHES FOUND WIRE BROKEN AT SWITCH 27-62-57. REPAIRED WIRE ALL SWITCHES AND CONNECTORS CHECK GOOD, OPS GOOD PER MM 27-14-38.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,586 hrs · 67,905 cycles

FORWARD CEILING EMERGENCY LIGHT WAS INOPERATIVE. RELAMPED.

Part: LENS — BROKEN (EMERGENCY LIGHTS) · airframe 59,549 hrs · 67,867 cycles

LOWER EMERGENCY LIGHT SIGN AT ROW 4 A AND C NEED RESECURED. R&R LIGHT ASSY.

Part: RESISTOR — BLOWN (AUTOPILOT SYS) · airframe 59,492 hrs · 67,808 cycles

RAMP PEOPLE ADVISED THAT POWER ON ACFT FLUCTUATED WHILE CLEANING ACFT AND THERE WAS BURNING SMELL. CONTRACT MX CONFIRMS SMELL IS FROM LT AUTOPILOT DISENGAGE LT AND AUTOPILOT DISENGAGE LT CIRCUIT BREAKER POPPED. FOUND RESISTOR ON AUTO PILOT DISENGAGE BOARD BLOWN, REMOVED AND REPLACE AUTO PILOT DISENGAGE PANEL IAW 22-10-01 MM.

Part: SWITCH — DETERIORATED (COCKPIT) · airframe 57,163 hrs · 65,220 cycles

DURING TAKEOFF ROLL, T/O WARNING HORN SOUNDED. CREW ABORTED TAKEOFF. FLAPS WERE CYCLED AND HORN DID NOT SOUND. MAINTENANCE FOUND CONDITION LEVER MICRO SWITCH 3151-S3 TO HAVE A DETERIORATED SOLDER JOINT AT THE SWITCH. SWITCH WAS RESOLDERED AND SYSTEM CHECKED IAW PIEDMONT WORK CARD PROCEDURES. OPS CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CRACKED (BS 636) · corrosion level 3 · airframe 56,486 hrs · 64,473 cycles

ANGLE CRACKED IN THE CARGO BAY AT FUSELAGE STA X618.00 AND Z114.5 ANGLE AT FUSELAGE STA X 618 Z 114.5 RT HAS BEEN DONE IAW DRAWING 85330499 INSTALLED PER SRM 51-40-00.

Part: SPAR — CRACKED (LT WING) · airframe 56,468 hrs · 64,473 cycles

ANGLE FOUND CRACKED AT JUNCTION OF LEFT NACELLE AND FRONT SPAR, STA YW39.00. LT FRONT SPAR BLEED AIR TUBE REMOVED TO ACCESS PER AMM 20-14-01. ANGLE REMOVED AND REPLACED IAW SRM 51-40-00. REINSTALLED BLEED TUBE.

Part: WEB — CORRODED (RUDDER) · airframe 56,486 hrs · 64,473 cycles

WEB FOUND CORRODED ON FORE RUDDER MID HINGE. WEB ON FORE RUDDER MID HINGE LOCALLY FABRICATED AS PER DRAWING NUMBER 85540112, INSTALLATION CARRIED OUT ON WORK CARD SEQ 3041.

Part: SEAT TRACK — CORRODED (BS 182-264) · corrosion level 2 · airframe 56,486 hrs · 64,473 cycles

RIGHT SEAT TRACK RAILS FOUND CORRODED BETWEEN STA X 182 TO X 264. RIGHT SEAT RAIL REMOVED AND REPLACED WITH SOLID RIVETS IAW SRM 51-40-00 AND BOLTS IAW AMM 20-14-00.

Part: CONTROL CABLE — CORRODED (RT ENGINE) · corrosion level 2 · airframe 56,486 hrs · 64,473 cycles

RIGHT ENGINE CONDITION CONTROL AND POWER CONTROL CABLES ARE CORRODED IN THE NACELLE AREA. INSTALLED NEW CONDITION AND POWER CABLES ON RIGHT ENGINE AS PER 76-10-00 RIGGED IAW 76-10-14.

Part: CONTROL CABLE — WORN (SPOILERS) · corrosion level 2 · airframe 56,486 hrs · 64,473 cycles

RIGHT SPOILER INBOARD AND OUTBOARD CABLES WORN TO LIMITS. RIGHT WING SPOILER CABLES REPLACED IAW 27-14-00.

Part: CONTROL CABLE — WORN (AILERON) · corrosion level 2 · airframe 56,486 hrs · 64,473 cycles

RIGHT AILERON INBOARD AND OUTBOARD WING REAR SPAR WORN TO LIMITS. RIGHT INBOARD AND OUTBOARD AILERON CABLES REMOVED AND REPLACED IAW 27-12-00.

Part: HEAT SHIELD — CORRODED (NACELLE) · airframe 56,486 hrs · 64,473 cycles

HEAT SHIELD PANEL AND STRAP AFT NACELLE STRUCTURE CORRODED. LEFT NACELLE FABRICATED PER DRAWING 85410741, 85411027 INSTALLED PER SRM 51-40-00.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,486 hrs · 64,473 cycles

CORROSION ON ORIGINAL STRINGER SPLICE BELOW LAV SERVICE BOX. STRINGER SPLICE BELOW LAV SERVICE BOX FABRICATED IAW 85320873. CORROSION AROUND RIB ANGLE UNDER LAV FLOOR BELOW LAV SERVICE BOX REMOVED AND REPROTECTED AND FOUND WITHIN LIMITS IAW SRM 53-00-16. ANGLE REPLACED AND INSTALLED IAW 51-40-00.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,486 hrs · 64,473 cycles

PAX DOOR ENTRANCE FRAME CORRODED. PAX DOOR ENTRANCE FRAME REMOVED AND REPLACED IAW SRM 51-40-00.

Part: BLANKING PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,486 hrs · 64,773 cycles

DOUBLER AND BLANKING PLATE OF RADIO ALT AFT ANTENNA FOUND CORRODED. DOUBLER AND BLANKING PLATE OF RADIO ALT LOCALLY FABRICATED AS PER SAMPLE. INSTALLED PER SRM 51-40-00.

Part: CONTROL CABLE — WORN (AILERON) · corrosion level 2 · airframe 56,486 hrs · 64,473 cycles

LEFT AILERON INBOARD AND OUTBOARD WING REAR SPAR CABLES (UPPER AND LOWER) WORN TO LIMITS. LEFT WING INBOARD AND OUTBOARD AILERON CABLES UPPER AND LOWER REMOVED AND REPLACED PER SRM 27-12-00.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,486 hrs · 64,473 cycles

ANGLE CRACKED AT FUSELAGE ST 636.00-Z118.5 RT ANGLE AT FUSELAGE ST 636-118.5 HAS BEEN REMOVED AND NEW PART INSTALLED IAW 50-40-00. FABRICATED IAW DRAWING NUMBER 85330499.

Part: CONTROL CABLE — WORN (AILERON) · corrosion level 2 · airframe 56,486 hrs · 64,473 cycles

LEFT AILERON INBOARD AND OUTBOARD WING REAR SPAR CABLES (UPPER AND LOWER) WORN TO LIMITS. LEFT WING INBOARD AND OUTBOARD AILERON CABLES UPPER AND LOWER REMOVED AND REPLACED PER SRM 27-12-00.

Part: CONTROL CABLE — WORN (LT ENGINE) · corrosion level 2 · airframe 56,486 hrs · 64,473 cycles

LEFT ENGINE CONDITION CONTROL UPPER CABLE AND POWER CONTROL UPPER AND LOWER CABLES ARE WORN TO LIMIT. ENGINE 1 UPPER CONDITION CABLE AND BOTH POWER CONTROL CABLES REPLACED AS PER 76-10-11 AND TASK 76-00-00.

Part: CONTROL CABLE — WORN (LT SPOILER) · corrosion level 2 · airframe 56,486 hrs · 64,473 cycles

LEFT SPOILER OUTBOARD (UPPER AND LOWER) CABLES AND SPOILERS INBOARD UPPER CABLE WORN TO LIMIT. REMOVED AND REPLACED OUTBOARD (UPPER AND LOWER) CABLES AND SPOILER INBOARD UPPER CABLE AS PER AMM 27-14-00 SPOILER WING & FUSELAGE CABLES RIGGED PER AMM 27-14-00, OPS CHECK GOOD.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 56,486 hrs · 64,473 cycles

PAX DOOR ENTRANCE THRESHOLD CORRODED. DOOR SEAL REMOVED, PAX DOOR THRESHOLD REMOVED AND REPLACED PER SRM 51-40-00, DOOR SEAL INSTALLED PER AMM 52-05-11.

Part: HYDRAULIC LINE — BURST (NR 2) · airframe 56,232 hrs · 64,212 cycles

AFTER GEAR RETRACTION, LOSS OF NR 2 HYD FLUID IN FLIGHT WITH NR 2 ISO VALVE CAUTION LIGHT AND F/A REPORTING FLUID ENTERING CABIN AREA NEAR ROW 5 & 6 DF THRU PSU'S. FOUND UP HYD LINE BURST IN CABIN, CAPPED BOTH PRESSURE AND RETURN LINES, LEAK CHECK GOOD. AIRCRAFT FERRIED TO SBY FOR INSPECTION, CLEANING AND LINE REPLACEMENT.

Part: BULB — BURNED OUT (MLG INDICATOR) · airframe 54,923 hrs · 62,828 cycles

LT MAIN AND NOSE GEAR GREEN ADVISORY LIGHTS INOP. CREW PERFORMED GO AROUND TO VERIFY THE INDICATIONS, NO EMERGENCY WAS DECLARED. RELAMPED BULBS OPS CHECK GOOD.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 53,420 hrs · 61,196 cycles

NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF LOUD GRINDING NOISE. CYCLED GEAR 15-20 TIMES UNABLE TO DUPLICATE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 52,916 hrs · 60,655 cycles

NR 1 HYDRAULIC DROPPED TO .5 QTS IN FLIGHT ISO VALVE CAUTION LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE DRIVEN PUMP.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 52,001 hrs · 59,643 cycles

ON TOUCHDOWN, LOST NORMAL BRAKING, DUE TO LOSS OF NR 1 HYDRAULIC QUANTITY (NR 1 ISO VALVE CAUTION LIGHT ILLUMINATED) INSPECTED CASE DRAIN NO CONTAMINANTS FOUND, REMOVED AND REPLACED FILTER AND SERVICED HYDRAULICS. REMOVED AND REPLACED LT IB SPOILER ACTUATOR (HOUSING CRACKED).

Part: VALVE — STICKING (ENGINE OIL TEMP) · airframe 51,807 hrs · 59,418 cycles

NR 1 ENGINE OIL TEMPERATURE REACHED 120 DEGREES C AND REDUCED TO 115 DEGREES C WHEN FUEL AUXILLARY PUMP SELECTED ON. REMOVED AND REPLACED OIL COOLER THERMAL VALVE.

Part: WIRE — DAMAGED (SPEED SENSE) · airframe 51,127 hrs · 56,674 cycles

RT AC BUSS LIGHT ILLUMINATED IN FLT WITH ASSOCIATED RT TRU, RIGHT ELEVATOR HEAT AND RIGHT STALL WARNING. REMOVED AND REPLACED CONNECTOR 2421-P6 AT A/C CONTACTOR BOX, REPLACED WIRES 2022B22, 2023B22, 2021B22, 2024B22, 10024G22, 10023G22, 10022G22, 10021M22, 20015G22, 20045C22, 20044C22, 20043C22, 2442-2009D2, 20011B22, 20010B22 NO FIX, PROBLEM RETURNED ON 25 MARCH 2005. R & R RT AC GENERATOR AND GCU NO FIX PROBLEM RETURNED 02 APRIL 2005. REPAIRED SPEED SENSE WIRES NEAR RT AC CONTACTOR BOX. OPS CHECK GOOD

Part: GCU — FAILED (NR 2 A/C GEN) · airframe 51,114 hrs · 58,658 cycles

RIGHT A/C BUSS FAILED ON CLIMBOUT, RETURNED TO FIELD. REMOVED NR 2 A/C GENERATOR CONTROL UNIT.

Part: BUSS — FAILED (RT A/C) · airframe 51,114 hrs · 58,658 cycles

RIGHT A/C BUSS FAILURE IN CLIMBOUT. AIRCRAFT RETURNED TO FIELD. REPLACED RIGHT HAND PROP HEAT WIRES FROM RELAY PANEL NR 1 TO RIGHT WING ROOT CONNECTOR. EVALUATION FLIGHT SATISFACTORY.

Part: CONTROL UNIT — FAILED (ELEVATOR) · airframe 50,938 hrs · 58,475 cycles

RT AC BUSS, TRU STALL WARN, ELEVATOR HORN HTR IN FLT. REMOVED AND REPLACED NR 2 AC GND RUN. OPS CK GOOD. LEFT VARIABLE AC BUS ZERO VOLTS AND LOADS. REMOVED AND REPLACED GCU AND CURRENT LIMITER. REMOVED AND REPLACED R AC GCU AND CURRENT LIMITER.

Part: ECU — FLUCTUATES (Zone 400) · airframe 44,449 hrs · 51,426 cycles

CREW REPORTED #2 ENGINE TORQUE BEGAN FLUCTUATING +/- 10-15%. WHEN #2 ECU WAS SELECTED OFF THE CONDITION STABILIZED BRIEFLY THEN #1 ENGINE TORQUE BEGAN FLUCTUATING +/- 5-10%. AIRCRAFT RETURNED TO DCA. MAINTENANCE FOUND THE #1 ENGINE ECU FLAGGED ON THE ENGINE CONDITION PANEL. REPLACED THE #1 ECU.

Part: HYDRAULIC LINE — LEAKING (NOSE BAY) · airframe 43,632 hrs · 50,516 cycles

After take off the number 2 hydraulic isolation caution light illuminated and roll spoiler outbe caution light illuminaated. Upon gear retraction, the gear would not retract. Replaced hydraulic lind to nose gear drag strut actuator and serviced #2 system. Evaluation flight good.

Part: HOSE · airframe 43,582 hrs · 50,465 cycles

NUMBER 1 OIL PRESSURE WENT TO 20-30 PSI ON CLIMB OUT FROM BWI. SHUT DOWN ENGINE IMMEDIATELY. FOUND FLEXABLE OIL COOLER LINE ON LEFT SIDE OF ENGINE LOOSE. TIGHTENED B-NUT.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 43,162 hrs · 49,990 cycles

A .075 INCH CRACK IN NOSE GEAR BAY CROSS BEAM AT STATION X97. CRACK BRANCHES OUT OF LOWER LT RIVET UNDER DRAG STRUT ACTUATOR MOUNTING BRACKET INTO J-CHANNEL RADIUS. REPAIRED IAW EO8-53-01-504.

Part: VALVE — LEAKING · airframe 42,581 hrs · 49,361 cycles

IN FLIGHT #2 HYDRAULIC SYSTEM QUANTITY DROPPED TO 1 QUART. AIRCRAFT DIVERTED TO ISP. FOUND #2 FLIGHT SPOILER UNLOADING VALVE LEAKING. REPLACED VALVE.

Part: MODULE — FAILED (MLG) · airframe 40,395 hrs

LT FWD GEAR DOOR STAYED OPEN AFTER GEAR RETRACTION. REMOVED AND REPLACED TERMINAL BLOCK 9811TB7 MODULE, OPS CHECK GOOD.

Part: LINE — FAILED (NR 2 HYD SYSTEM)

FLT 3133 - ORF-BWI - NEARING BWI, HYDRAULIC PRESSURE AND QTY DROPPED TO ZERO ON THE NR 2 SYSTEM. INSTALLED TEMPORARY FLEX LINE FROM STEEING MANIFOLD SWITCH TO T-FITTING. SERVICED AND BLED SYSTEM AS REQUIRED. (M)

Part: GAS STRUT — FAILED (AIRSTAIR DOOR)

FLT NR 3172 - PHF-PIT - UPON LANDING IN PIT, THE FLIGHT ATTENDANT WAS UNABLE TO OPEN THE AIRSTAIR DOOR WITHOUT ASSISTANCE. FERRIED THE AIRCRAFT TO ORF FOR REPAIRS. REMOVED AND REPLACED THE FORWARD GAS STRUT. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FLT NR 77 - ORF-PHF - DURING PREFLIGHT CHECKS, THE FIRST TWO ESCAPE PATH RED LIGHTS WERE FOUND INOP. REMOVED AND REPLACED THE POWER SUPPLY AT 3352-PS2. (M)

Part: PROX SENSOR — FAILED (LT MLG)

PHL/SBY - FLT 3185 - AFTER GEAR RETRACTION, LEFT MAIN GEAR DOOR LIGHTS STAYS ILLUMINATED. DOORS APPEAR FULLY CLOSED BY VISUAL INSPECTION. AIRCRAFT CONTINUED ON TO SBY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PROXIMITY SENSOR.

Part: DRIVE CABLE — BROKEN (TE FLAPS)

FLT EN01 - ROA-ORF - FLAP DRIVE CAUTION LIGHT ILLUMINATED WHEN RAISING FLAPS AFTER LANDING. FOUND LEFT INBOARD SECONDARY FLAP DRIVE CABLE BROKEN. REMOVED AND REPLACED INBOARD SECONDARY FLAP DRIVE CABLE.