N936HA

Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 68,354 hrs · 76,737 cycles

IN FLIGHT, RIGHT AC BUSS CAUTION LIGHT ILLUMINATED WITH ASSOCIATED SERVICE SYSTEM FAILURE. NR 2 AC GENERATOR CAUTION LIGHT DOES NOT ILLUMINATED ON ENGINE SHUTDOWN. BULB DOES TEST. REMOVED AND REPLACED THE NR 2 AC GENERATOR IAW WORK CARD 24-20-11R.OPS AND LEAKED CHECKED GOOD.

Part: SWITCH — MALFUNCTIONED (NR 2 GENERATOR) · airframe 68,354 hrs · 76,737 cycles

DURING CLIMB OUT, RIGHT AC BUSS, RIGHT TRU AND RIGHT STALL WARNING CAUTION LIGHTS ILLUMINATED. CYCLED THE NR 2 AC GENERATOR SWITCH. ALL RELATED SYSTEMS OPERATE NORMALLY. GROUND RAN BOTH ENGINES. OPS CHECKED GOOD.

Part: ROTOR — SEIZED (HP) · airframe 68,343 hrs · 76,722 cycles

NR 2 ENGINE FAILS TO SPOOL DURING START CYCLE. REMOVED AND REPLACED THE NR 2 STARTER GEN IAW WORK CARD 24-30-02R. NO FIX. SLAVED NR 2 DC GCU. NO FIX. FOUND NR 2 HP NOT ABLE TO ROTATE.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,707 hrs · 75,942 cycles

INOPERATIVE EMERGENCY LIGHT ROW 1. R & R FIRST AND SECOND LAMP MODULE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LGIHTS) · airframe 67,697 hrs · 75,930 cycles

EMERGENCY LIGHTS INOPERATIVE AT ROW 7 AND THE 2ND AND 3RD LIGHTS FROM FRONT ARE INOPERATIVE. R & R SECOND AND THIRD LIGHT ASSEMBLIES FROM FRONT, NO FIX. R & R BATTERY AT ROW 7AC, LIGHTS AT ALL 3 LOCATION PARTS INSTALLED, REMOVED 8330086, 8240485, JAX167/ORF42.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,546 hrs · 75,759 cycles

FIRST EMERGENCY LIGHT INOPERATIVE. R & R BULB, REINSTALLED BULB COVER AND PATH LIGHT COVER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,511 hrs · 75,727 cycles

NR 2 FLOOR PATH EMERGENCY LIGHT INOPERATIVE. LIFTED UP PROTECTIVE COVER. R & R BULB, RESECURED COVER.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,346 hrs · 75,517 cycles

EMERGENCY LIGHT INOPERATIVE AT LEFT AFT EGRESS. R & R BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,665 hrs · 74,711 cycles

5TH EMERGENCY LIGHT IS INOPERATIVE. R & R BULBS, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,552 hrs · 74,582 cycles

FLOOR EMERGENCY LIGHT IS OUT AT ROW 5DF. R & R BULB AT ROW 5 FLOOR EMERGENCY LIGHTS. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,512 hrs · 74,530 cycles

LEFT AFT FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PS3. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,512 hrs · 74,530 cycles

9TH AND 11TH EMERGENCY LIGHT INOPERATIVE. R & R BULBS AT ROWS 9 AND 11. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,512 hrs · 74,530 cycles

CEILING EMERGENCY LIGHT AT ROW 7 IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD.

Part: LATCH — BROKEN (NLG DOOR) · airframe 66,565 hrs · 74,415 cycles

RING HANDLE FOR NOSE GEAR ALTERNATE EXTENSION DOOR DETACHED. REMOVED BROKEN PORTION OF LATCH ASSY. INSTALLED NEW LATCH ASSY IAW DWG 85310006. OPS CHECKED GOOD.

Part: UPLOCK SENSOR — MALFUNCTIONED (NLG) · airframe 66,141 hrs · 74,073 cycles

AFTER GEAR RETRACTION AND ALL GEAR LIGHTS NORMAL, NOSE GEAR INTERMITTENTLY UNTIL GEAR WAS SELECTED DOWN. NO USUAL SOUNDS HEARD. R & R UPLOCK SENSOR ON NOSE GEAR DRAG STAY. ADJUSTED GAP AND SAFTIED IAW MM 32-52-10. CYCLED GEAR 10 TIMES, OPS CHECKED GOOD.

Part: PSEU — WARNING LIGHT · airframe 66,118 hrs · 74,040 cycles

NOSE GEAR RED UNSAFE LIGHT ILLUMINATED FOR APPROXIMATELY 10 SECONDS WITH ASSOCIATED CLUNK. THE RED NLG LIGHT EXTINGUISHED FOR APPROXIMATELY 10 SECONDS, THEN EXTINGUISHED ON LANDING GEAR RETRACTION. NLG EXTENDED FINE. NO NOISE ON EXTENSION. INSPECTED NLG AND PROXIMITY SENSORS. NO DEFECTS NOTED. SWUNG GEAR 20 TIMES, NO DEFECTS. R & R PSEU DUE TO INTERMITTENT CARD FAULT. COMPLIED WITH FURTHER GEAR SWINGS. NO DEFECTS NOTED IAW MM 32-61-50. OK FOR SERVICE.

Part: INDICATOR — MALFUNCTIONED (OIL PRESSURE) · airframe 65,860 hrs · 73,741 cycles

NR 1 ENGINE OIL PRESSURE AT 70 PSI IN FLIGHT. R & R ENGINE OIL PRESSURE INDICATOR IAW 79-32-00 AND REMOVED 1 SHIM FROM NR 1 ENGINE OIL PRESSURE REGULATOR IAW MM 72-00-00. OPS CHECKED AND LEAK CHECKED GOOD IAW RUN UP MANUAL.

Part: ROD END — OUT OF ADJUST (LT MLG DOOR) · airframe 65,955 hrs · 73,852 cycles

LEFT MAIN GEAR DOOR ADVISORY LIGHT REMAINED ON FOR ABOUT 5 MINUTES, AFTER GEAR RETRACTED AND SELF EXTINGUISHED. ADJUST ROD END FOR FORWARD LT GEAR DOOR IAW MM 32-30-00. RETRACTED AND EXTENDED GEAR SEVERAL TIMES. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (ROW 9) · airframe 65,720 hrs · 73,566 cycles

AFT EMERGENCY LIGHT IS INOPERATIVE AT ROW 9. R & R EMERGENCY LIGHT IAW 33-51-11. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE INDICATION (NLG) · airframe 65,354 hrs · 73,118 cycles

NOSE GEAR UNSAFE RED ILLUMINATED ASSOCIATED WITH GEAR HORN SOUNDING, WHILE WAITING FOR TAKEOFF. INSPECTED NOSE GEAR DOWN LOCK SENSOR FOR DEFECTS, NO DEFECTS NOTED. CHECKED SENSOR GAPS, GAPS WITH LIMITS. PERFORMED GEAR SWINGS WITH NO DEFECTS OR ANOMALIES NOTED. OK FOR SERVICE.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 64,710 hrs · 72,374 cycles

EMERGENCY SIDEWALL LIGHT BY PAX DOOR IS DIM. R & R BULB . OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,289 hrs · 71,878 cycles

FLOOR EMERGENCY LIGHT IS INOPERATIVE AT ROW 2. R & R THE BULB. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (BS 182) · airframe 63,774 hrs · 71,262 cycles

MULTIPLE RIVETS ARE PULLING THROUGH THE SKIN AT RT FWD SIDE OF BS 182 STRINGER 31P. REPAIRED IAW EA15-2014-151B AND EO8-53-14-0282.

Part: UNKNOWN — ODOR (CABIN) · airframe 63,285 hrs · 70,674 cycles

BURNING ODOR IN CABIN AT ROWS 4 AND 5. INSPECTED CABIN LIGHTING SYS AND BEHIND CABIN OVERHEAD PANELS. NO DEFECTS NOTED. GROUND RAN ACFT, NO ODOR NOTED AT THIS TIME. OK FOR SERVICE.

Part: GARLOCK SEAL — LEAKING (NR 2 ENGINE) · airframe 63,280 hrs · 70,668 cycles

DURING FLIGHT, AT LOW POWER SETTINGS, HOT ODOR IS EMITTED IN COCKPIT AND CABIN AT HIGH POWER SETINGS AND ON GROUND. INSPECTED BOTH ENGINE AIR SWITCHING VALVES AND APU AREA. NO DISCREPANCIES NOTED. FOUND NR 2 ENGINE GARLOCK SEAL LEAKING. R & R GARLOCK SEAL. NO LEAKS NOTED IAW AND WC 24-30-02R.

Part: SEAL — LEAKING (BLEED SYS) · airframe 63,276 hrs · 70,663 cycles

ELECTRICAL ODOR WHEN BLEEDS ARE SELECTED ON. INSPECTED AND FOUND SEAL BAD IN BYPASS BLEED LINE AND MAJOR LEAK AT HEAT EXCHANGER. R & R SEALS, SECURED HEAT EXCHANGER BLEED LINE. RAN APU, NO LEAKS NOTED.

Part: INVERTER — FAILED (SECONDARY) · airframe 63,223 hrs · 70,601 cycles

ELECTRICAL ODOR IN COCKPIT. SECONDARY INVERTER FOUND TO BE AT FAULT.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 63,167 hrs · 70,532 cycles

LEFT OF EXTERIOR EMERGENCY LIGHT IS DIM. R & R BULB IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (NR 2) · airframe 63,167 hrs · 70,532 cycles

NR 2 EMERGENCY LIGHT IS OUT. R & R NR 2 EMERGENCY LIGHT IAW AMM 33-51-11.

Part: HYDRAULIC SYSTEM — CONTAMINATED · airframe 62,862 hrs · 70,171 cycles

ON CLIMBOUT, NR 1 ENGINE HYD PUMP CAUTION LIGHT ILLUMINATED, FOLLOWED BY RUDDER PRESSURE AND FULL PRESSURE CAUTION LIGHTS. NR 1 MAIN HYD PRESSURE AT 500-1K. PSI AND STANDBY AT 1.5 TO 2K PSI. DURING TAX IN NOSE WHEEL STEERING SHUT OFF. WAS ABLE TO RESET. QTY IN AIR WAS 1.5 QTS, GROUND PUMPS OFF OVER 2 QTS. BLED NR 1 AND NR 2 HYD SYS IAW MM 12-10-29. OPS CHECKED GOOD. SYS CHECKED NORMAL. OK FOR SERVICE. SERVICE SYS TO PROPER LEVELS.

Part: BULB — INOPERATIVE (CONTROL PANEL) · airframe 62,811 hrs · 70,111 cycles

F/A PANEL EMERGENCY LIGHT SWITCH, BACK LIGHT INOPERATIVE WHEN LIGHTS ARE OFF. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,205 hrs · 69,370 cycles

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

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 62,146 hrs · 69,302 cycles

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

Part: APU — ODOR · airframe 61,996 hrs · 69,108 cycles

STRONG FUEL ODOR IN CABIN. GROUND RAN BOTH NR 1 AND NR 2 ENGINES, NO FUEL ODOR NOTED. VERFIED ODOR COMING FROM APU.

Part: WHEEL — MISINSTALLED (NR 4) · airframe 61,281 hrs · 68,242 cycles

BRAKES APPEAR TO BE NOT OPERATING AFTER LANDING. FOUND NR 4 MAIN WHEEL ASSY LOOSE AND INCORRECTLY INSTALLED. FOUND DAMAGE ON NR 4 AXLE. R & R SHOCK STRUT IAW WC 32-20-06F. PERFORMED HIGH SPEED TAXI. OPS CHECKED GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 60,710 hrs · 67,548 cycles

IN FLIGHT, NR 1 SYS LOST HYD PRESSURE. 1/2 QT REMAINED. PRESSURE AT 3000. NR 1 HYD ISOLATION VALVE AND ROLL SPOILER INBD HYD CAUTION LIGHT ILLUMINATED. INSTALLED TEMP FLEX LINE IAW SP 20.2 FROM PRESSURE PORT OF NR 1 ENGINE DRIVEN HYD PUMP TO FIREWALL. SERVICE NR 1 HYD SYS IAW 12-10-29. GROUND RAN ACFT. OPS AND LEAKED CHECKED GOOD.

Part: RECEPTACLE — BURNED (BS 97) · airframe 60,043 hrs · 66,719 cycles

GROUND POWER CART PLUG CAUGHT ON FIRE AFTER BEING INSTALLED ON ACFT FOR APPROX. 40 MINUTES. FIRE DAMAGE WAS FOUND AT DC POWER RECEPTACLE AT FORWARD FRAME STA X97 AND FORWARD OF FORWARD PRESSURE BULKHEAD. ACFT IS IN MX FOR REPAIRS.

Part: ACM — FAILED · airframe 59,310 hrs · 65,846 cycles

BLUISH COLOR SMOKE IN COCKPIT. MOMENTS BEFORE SMOKE APPEARED, FELT NOTICABLE VIBRATION IN FLOOR PANEL. SHUTDOWN ENGINE AND EVACUATED ACFT. R & R ACM IAW WORKCARD 21-50-03I. OPS CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 59,185 hrs · 65,697 cycles

RT FORWARD EMERGENCY LIGHT IS DIM. R & R EMERGENCY BATTERY. REMOVING 4 BOLTS AND REINSTALLING WITH BOLTS SECURING NEW POWER SUPPLY. OPS CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 59,068 hrs · 65,571 cycles

LEFT FORWARD EMERGENCY EGRESS LIGHT AT AIRSTAIR DOOR IS INOP. R & R LIGHT BATTERY-TOP POSITION IN WARDROBE. OPS CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 59,068 hrs · 65,571 cycles

AFT CEILING AISLE EMERGENCY LIGHT AND LT AFT EMERGENCY EGRESS LIGHT ARE INOPERATIVE. R & R BATTERY ABOVE ROW 3AC. OPS CHECKED GOOD.

Part: POWER SUPPLY — INTERMITTENT (EMERGENCY LIGHTS) · airframe 59,068 hrs · 65,571 cycles

EMERGENCY LIGHT COME ON AND THEN GO OFF AFTER A FEW SECONDS. PATH LIGHTING STAYS ON. R & R EMERGENCY LIGHT POWER SUPPLY UNIT IAW WC 33-50-05R.

Part: HANDLE — MISINSTALLED (SELECTOR) · airframe 58,598 hrs · 65,021 cycles

ALTERNATE STATIC SELECTOR HANDLES ARE 180 DEGRESS OUT. SWAPPER HANDLES 180 DEGREES. OK FOR SERVICE.

Part: BRACKET — CORRODED (BS 182) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

CENTER BRACKET OF CENTER FLOOR CORRODED. R & R WITH MADE REPAIR PART AND INSTALLED WITH BLIND RIVETS IAW SRM 51-40-00.

Part: CHANNEL — CORRODED (BS 200-222) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

JOINT CHANNEL CORRODED IN LAVATORY AREA AT STR 27S BETWEEN STA X200 TO X222. R & R WITH MADE REPAIR PART AND SOLID RIVETS IAW SRM 51-42-05.

Part: STRUCTURE — CORRODED (LT AILERON) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

LEFT AILERON TERMINAL QUADRANT SUPPORT BOX FOUND CRACKED. REMOVED AILERON TERMINAL QUADRANT R & R WITH MADE REPAIRED PART WITH FABRICATED PART IAW SRM 51-42-05 AND DWG 85710896.

Part: FASTENER — CORRODED (LT WING) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

FASTENER CORRODED ON LT WING TO FUSELAGE REAR SPAR LOWER FITTING. R & R REAR SPAR LOWER FITTING IAW AMM 20-14-01.

Part: ROD END — LOOSE (SPOILERS) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

LEFT WING FLIGHT SPOILER INPUT ROD END FOUND LOOSE AND ROD WITH SURFACE CORROSION. REMOVED CORROSION FROM FLIGHT SPOILER INPUT ROD IAW MM 27-14-00. TREATED ROD WITH CORROSION PREVENTION AS REQUIRED.

Part: CONTROL ROD — CORRODED (SPOILERS) · airframe 58,546 hrs · 64,960 cycles

LEFT WING OTBD SPOILER CONTROL ROD FOUND WITH SURFACE CORROSION. REMOVED SPOILER CONTROL ROD IAW 27-14-00. REMOVED CORROSION, TREATED AND REINSTALLED.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

TWO INSERTS ON CENTER FLOOR PANEL 133BZ CORRODED. R & R 2 INSERTS ON CENTER FLOOR PANEL.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

PAX DOOR ENTRY THRESHOLD FOUND CORRODED. R & R PAX DOOR ENTRY THRSHOLD WITH NEW AND INSTALLED WITH SOLID RIVETS IAW SRM 51-47-05.

Part: SKIN — CORRODED (LT NACELLE) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

ON FINGERNAIL OF LT NACELLE, AFT SKINS ON BOTH SIDE HAS SURFACE CORROSION. BLENDED CORROSION ON BOTH SIDES OF LT NACELLE TO WITHIN LIMITS IAW SRM 54-00-16.

Part: STRUCTURE — CORRODED (LT NACELLE) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

LEFT NACELLE AFT SECTION OF NACELLE UNDER THE FINGERNAIL IS CORRODED. REMOVED CORROSION UNDER LT NACELLE FINGERNAIL AFT SECTION IAW SRM 51-20-11.

Part: BOLT — CORRODED (RUDDER) · corrosion level 2 · airframe 56,556 hrs · 64,970 cycles

BOLTS FOUND CORRODED INSIDE FORE RUNNER, BEHIND CENTER HINGE. R & R BOLTS INSIDE FORE RUDDER BEHIND CENTER HINGE IAW SRM 51-42-05 AND DWG 85540003.

Part: PANEL — CORRODED (WING) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

CORROSION FOUND AT MANY PLACES ON LADDER PLATE OF STRESS PANEL 522AT. COMPLIED WITH HFEC INSPECTION ON REWORKED AREAS IAW RD8-57-114. NO CRACK INDICATION FOUND. REPAIRED IAW RD8-57-114.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 58,549 hrs · 64,963 cycles

ON ENGINE START NR 2 HYD QTY WENT BELOW MIN DISPATCH. TRANSFER FLUID FROM NR1 TO MEET MIN ON GEAR RETRACTION, NR 2 ENGINE HYD PUMP CAUTION LIGHT ILLUMINATED. ON GEAR EXTENSION NR 2 ENGINE HYD PUMP NR 2 RUDDER HYD AND RUDDER FULL PRESSURE CAUTION LIGHT ILLUMINATED WITH ASSC DROP NR 2 PRESSURE. BOTH HYD SYS SERVICED TOP LEVEL. RAN ACFT BOTH ENGS AND ALL FLT CONTROLS CYCLED 20 TIMES. NO FAULT FOUND BOTH HYD SYS BLED IAW AMM 29-10-00 AND BOTH SYS LEVELS CHECK GOOD FOR SERVICE. BOTH SYS LEVELS MAINTAINED AND NO CAUTION LIGHTS.

Part: SKIN — DAMAGED (LT AILERON) · airframe 58,546 hrs · 64,960 cycles

A LIGHTNING STRIKE FOUND ON LT AILERON TOP SKIN ABOUT 1.500" FORWARD OF REAR SPAR. REMOVE LT AILERON IAW AMM 27-12-11. DAMAGE WAS R & R IAW SRM 57-60-21, FIG 5.

Part: SEAT TRACK — CORRODED (BS 526-548) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

FOUND CORROSION ON RT INBD SEAT TRACK. BLENDED RT SEAT TRACK TO WITHIN LIMITS IAW RD8-53-4936. HFEC INSP CARRIED OUT ON REWORKED AREA IAW RD8-53-4936.

Part: SEAT TRACK — CORRODED (BS 526-548) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

FOUND CORROSION ON LT INBD SEAT TRACK. BLENDED LT INBD SEAT TRACK TO WITHIN LIMITS IAW RD8-53-4936. HFEC INSP CARRIED OUT ON REWORKED AREA IAW RD8-53-4936. NO CRACK INDICATION FOUND.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 58,546 hrs · 64,960 cycles

JOINT CHANNEL CORRODED. FABRICATED JOINT CHANNEL IAW DWG 320872.

Part: SEAT TRACK — CORRODED (BS 504-545) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

FOUND CORROSION ON LT OTBD SEAT TRACK. BLENDED LT OTBD SEAT TRACK TO WITHIN LIMITS IAW RD8-53-3644. HFEC INSP CARRIED OTBD ON REWORKED AREA IAW RD8-53-3644. NO CRACK INDICATION FOUND.

Part: CHANNEL — CORRODED (BS 200-222) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

JOINT CHANNEL CORRODED IN LAVATORY AREA. R & R WITH MADE REPAIR PART AND INSTALLED WITH SOLID RIVETS IAW SRM51-42-05.

Part: SEAT TRACK — CORRODED (BS 504-545) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

FOUND CORROSION ON RT OTBD SEAT TRACK. BLENDED RT OTBD SEAT TRACK TO WITHIN LIMITS IAW RD8-53-3644.

Part: SEAT TRACK — CORRODED (BS 262-424) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

FOUND CORROSION ON RT INBD SEAT TRACK. BLENDED RT SEAT TRACK TO WITHIN LIMITED IAW RD8-53-1339. HFEC INSPECTION CARRIED OUT ON REWORKED AREA IAW RD8-53-1339. NO CRACK INDICATIONS FOUND.

Part: SEAT TRACK — CORRODED (BS 284-526) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

FOUND CORROSION ON LT INBD SEAT TRACK. BLENDED LT SEAT TRACK TO WITHIN LIMITS IAW RD8-53-1339. HFEC INSP CARRIED OUT ON REWORKED AREA IAW RD8-53-1339. NO CRACK INDICATED FOUND.

Part: SEAT TRACK — CORRODED (BS 548-596) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

CORROSION FOUND ON BOTH INBD SEAT TRACK. BLENDED BOTH LT AND RT SEAT TRACK TO WITHIN LIMITS IAW RD8-53-784.

Part: SEAT TRACK — CORRODED (BS 264-504) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

FOUND CORROSION ON RT OTBD SEAT TRACK BETWEEN STR X264 TO X504. BLENDED RT OTBD SEAT TRACK BETWEEN STA X264 TO X504 TO WITHIN LIMITS IAW RD8-53-1342. HFEC CARRIED OUT ON REWORKED AREA IAW RD8-53-1342. NO CRACK INDICATION FOUND.

Part: SEAT TRACK — CORRODED (BS 264-504) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

FOUND CORROSION ON LT OTBD SEAT TRACK BETWEEN STA X 264 TO X 504. BLENDED LT OTBD SEAT TRACK TO WITHIN LIMITS IAW RD8-53-1342.

Part: SEAT TRACK — CORRODED (BS 182-284) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

CORROSION FOUND ON LT INBD SEAT TRACK BETWEEN BS 182 AND 284. SPLICED LT SEAT TRACK IAW RD8-53-3074 AND NEW SEAT TRACK SECTION INSTALLED.

Part: SEAT TRACK — CORRODED (BS 182-262) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

CORROSION FOUND ON RT INBD SEAT TRACK BETWEEN BS 182 TO 262. SPLICED SEAT TRACK IAW RD8-53-3074. INSTALLED NEW SEAT TRACK SECTION.

Part: RETAINER — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

PAX DOOR LOWER SEAL RETAINER ON FUSELAGE CORRODED. R & R PAX DOOR LOWER SEAL RETAINER WITH NEW PART AND INSTALLED WITH SOLID RIVETS IAW SRM 51-42-05.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

PAX DOOR ENTRY THRESHOLD FOUND CORRODED. R & R WITH NEW PART AND SOLID RIVETS IAW SRM 51-47-05.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

RT WING FUEL PUMP CUTOUT LIGHTLY CORRODED ON LOWER SURFACE UNDER CLAMP RING. HFEC AND BOND TEST CARRIED OUT ON AFFECTED AREA IAW RD8-57-1907. NO CRACKS OR DEBOND INDICATION FOUND. RT WING FUEL PUMP CUTOUT ON LOWER SURFACE HAS BEEN REPAIRED IAW RD8-57-1907.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 58,546 hrs · 64,960 cycles

CORROSION FOUND ON THE LOWER SURFACE OF THE MACHINE DOUBLER AROUND LT FUEL PUMP CUTOUT. THE LOWER SURFACE OF THE MACHINED DOUBLER AROUND LT FUEL PUMP CUTOUT BLENDED WITHIN LIMITS IAW RD8-57-1907. HFEC AND BOND TEST CARRIED OUT ON AFFECTED AREA IAW WITH RD8-57-1907. NO CRACK OR DISBOND INDICATION FOUND.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,546 hrs · 64,960 cycles

CORRORSION SPOTS FOUND IN ZONE 120 ON FRAME SKIN FLANGE FROM X136.80 TO X167, BETWEEN STR 30L TO 30R. BLENDED MANY CORRSION SPOTS AND REPROTECTED IAW SRM 51-20-11 AND FOUND TO BE WITHIN LIMITS IAW SRM 53-00-16 AT X136 ON FRAME ANGLE BETWEEN STR 30 TO 32P AT STA X151 ON FRAME FLANGE BETWEEN STR 32P-31S AT STA X167 ON FRAME FLANGE BETWEEN STR 30P-32S. THE REST OF AREA HAS BEEN CLEANED UP AND NO CORROSION FOUND.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,546 hrs · 64,968 cycles

UNDER F/A SEAT FLOOR, STRUCTURE FOUND CORRODED. TEE SUPPORT UNDER F/A SEAT FLOOR REPLACED WITH NEW ONE AND INSTALLED IAW SRM51-42-05.

Part: FRAME SPLICE — CRACKED (COCKPIT) · airframe 58,546 hrs · 64,960 cycles

CRACK FOUND ON PILOT'S SIDE FRAME SPLICE ANGLE ABOVE NOSE WHEEL STEERING HAND CONTROL. REMOVED LT TOP CONTROL PANEL FOR ACCESS. LT FUSELAGE FRAME STA X136 AT STR 15AM, REPLACED ANGLE SPLICE AND 2 STRAPS. INSTALLED WITH SOLID RIVETS IAW SRM 51-42-05.

Part: SUPPORT — CRACKED (LT WING) · airframe 58,546 hrs · 64,968 cycles

LEFT WING AILERON TERMINAL QUADRANT SUPPORT BOX CRACKED. LT AILERON TERMINAL QUADRANT SUPPORT BOX REPLACED WITH MADE REPAIR PART FABRICATION COVERED BY WO9120.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,535 hrs · 64,945 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD. REINSTALLED PANEL.

Part: SWITCH — LACK OF LUBE (CARGO DOOR) · airframe 58,169 hrs · 64,524 cycles

BAG DOOR WARNING LIGHT ILLUMINATED WITH ACFT PRESSURED. LIGHT WENT OUT DURING DEPRESSURIZING AND BLEEDS OFF. FOUND AFT BAG DOOR PROXIMITY SWITCH STUCK IN WRONG POSITION. CLOSED AND LUBED SWITCH. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 64,279 hrs · 145 cycles

LT FORWARD EGRESS LIGHT IS DIM. R & R BULB IAW 33-51-00.

Part: WIRE — FAILED (FIRE SUPPRESSION) · airframe 57,948 hrs · 64,279 cycles

APU FIRE BOTTLE TEST LIGHT WILL NOT ILLUMINATE. FILAMENT TESTED OK. APU COMPARTMENT FOUND WIRES GOING INTO DIODE BELOW SQUIB CONNECTOR PLUG TO NOT BE PROPERLY SEATED. R & R DIODE AND PROPERLY SEATED WIRES.

Part: AHRS — FAILED (NR 1) · airframe 57,704 hrs · 63,993 cycles

AHRS DATA INVALID MESSAGE ON TAKEOFF WITH ASSOCIATED FD AND YD FAILURE. (NR 1 AHRS ALREADY ON MEL). R & R NR 2 AHRS COMPUTER IAW MM 34-20-06. OPS CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 57,604 hrs · 63,872 cycles

NR 2 FWD FLOOR PATH LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY IAW AMM 33-51-00.

Part: PCU — FAILED (PROPELLER) · airframe 57,500 hrs · 63,756 cycles

ON CLIMB OUT, NR 2 NP REACHED 1245 AND DROPPED TO 1236, THEN CREW RETARDED TO 1050 AND RETURNED TO FIELD. PROP OVERSPEED WITHIN LIMITS OF MM 61-10-00. R & R NR 2 PCU IAW WC 61-10-10. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 56,894 hrs · 63,095 cycles

MINOR COCKPIT SMOKE IN FLIGHT, THEN CB'S F8, F9 AND G9 POPPED AND SMOKE STOPPED (INVERTER BREAKER). COMPLIED WITH HIDDEN DAMAGE INSPECTION WITH NONE NOTED. RESET C/B'S F8, F9 AND G9. GROUND RAN ACFT WITH C/B F8 POPPING WITH IN 5 SECONDS, ALL OTHER INVERTERS OPS NORMAL. REF LOG PAGE 58506-2 FOR ACTION.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 56,773 hrs · 62,951 cycles

2 RED FLOOR LIGHTS AT ROW 1 ARE INOP. R & R BOTH FLOOR MODUALS, NO FIX, LOWERED PSU AT 7AC, REPLACED EMERGENCY LIGHT BATTERY, RESECURED PSU, OPS CHECKED GOOD.

Part: SWITCH — FAILED (OVERTEMP) · airframe 56,689 hrs · 62,857 cycles

PAC HOT CAUTION LIGHT FLICKERED ON AND OFF. STOPPED CYCLING WITH BLEEDS SELECTED OFF, STRONG HOT ODOR WITH POWER SETTINGS REDUCED. R & R ACM OVERTEMP SWITCH IAW 21-50-31 AND OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (NLG STEERING) · airframe 56,101 hrs · 62,209 cycles

NOSE WHEEL STEERING CAUTION LIGHT ILLUMINATED AFTER GEAR RETRACTION. REMAINED ON AFTER NOSE WHEEL STEERING SWITCH CYCLED. RAN NOSE WHEEL STEERING ON GROUND AND ON JACKS, OK FOR SERVICE. NO DISCREPANCIES NOTED. CYCLED GEAR SEVERAL TIMES, OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,197 hrs · 61,207 cycles

EMERGENCY PATH LIGHT INOP AT ROW 1. R & R PATH LIGHT BULB AT ROW 1. OPS CHECKED GOOD.

Part: FIRE LOOP — MALFUNCTIONED (APU BAY) · airframe 54,838 hrs · 60,788 cycles

APU FAULT LIGHT ILLUMINATED FOLLOWED BY MASTER WARNING AND CHECK FIRE DETECTION LIGHT. R & R APU FIRE LOOP. OPS CHECK GOOD AT THIS TIME.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 54,704 hrs · 60,626 cycles

AFTER TAKEOFF, RETRACTED GEAR, AFTER 2 MINUTES, GOT THE NOSE GEAR RED UNSAFE LIGHT WITH ASSOCIATED IN TRANSIT LIGHT ON SELECTOR HANDLE FOR APPROX 30-40 SECONDS. NOTED ASSOCIATED THUMP AND ALL CLEARED.COMPLIED WITH ALTERNATE GEAR EXTENSION. JACKED AND SWUNG GEAR SEVERAL TIMES, NO DEFECTS NOTED. R & R PSEU FOR TROUBLESHOOTING. REF MM 32-61-50. SWUNG GEAR SEVERAL MORE TIMES. OPS CHECKED GOOD AT THIS TIME.

Part: INDICATOR — INOPERATIVE (WX RADAR SYS) · airframe 54,372 hrs · 60,244 cycles

WEATHER RADAR WOULD NOT PAINT KNOWN WEATHER OR GROUND. RADAR INDICATOR. OPS CHECKED IAW MM 34-41-04,NO FIX, STILL UNABLE TO PAINT GROUND OR WEATHER ON RADAR. R & R RADAR R/T IAW SB 34-18. OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.

Part: INDICATOR — FALSE INDICATION (FLAP POSITION) · airframe 52,789 hrs · 58,485 cycles

STICK SHAKER ATTIVATED IN FLIGHT AT ABOUT 220 KNOTS FOR ABOUT 10 MINUTES WHILE DECENDING UNTIL 15 MILES OUT. BOTH STALL SYSTEMS TEST NORMAL ON THE GROUND. R/R FLAP POSITION INDICATOR, PERFORMED FUNCTIONAL TEST OF STALL WARN SYS. CALIBRATED NR 1 AND 2 STALL WARNING COMPUTERS PER MM 27-33-00 OPS CK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 52,054 hrs · 57,663 cycles

ONE EMERGENCY ESCAPE PATH FLOOR LIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 51,114 hrs · 56,622 cycles

DURING OPERATIONS, AN OIL ODOR WAS NOTICED IN THE COCKPIT WITH BLEEDS SELECTED ON. OIL LEVELS IN BOTH ENGINES AND THE ACM UNIT WERE CHECKED AND FOUND TO BE GOOD. BOTH ENGINE NACELLES WERE INSPECTED FOR EVIDENCE OF OIL LEAKS, WITH NONE BEING FOUND. ENGINES WERE RUN ON THE GROUND WITH BLEEDS SELECTED ON WITH NO ODORS BEING DETECTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: BRAKE ASSY — SMOKE (MLG)

NR 2 BRAKE ASSY SMOKING. RETURNED TO GATE. INSPECTED BRAKE ASSY, NO DEFECTS NOTED. FLIGHT 4615 PHF. (S)

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS)

EMERGENCY EXIT SIGN ABOVE AIRSTAIR DOOR ENTRANCE INOPERATIVE. REMOVED AND REPLACED 3351, PS1 BATTERY PACK IAW 33-52-00. (K)

Part: AUTOFEATHER SYS — MALFUNCTIONED (COCKPIT) · airframe 49,735 hrs · 49,735 cycles

AUTOFEATHER FAILED TO ARM ON TAKEOFF ROLL. CYCLED ARM SWITCH OPS NORMAL AT THIS TIME. COULD NOT DETERMINE FROM THE INFORMATION AVAILABLE IF THIS WAS AN ABORTED TAKEOFF.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 49,572 hrs · 54,938 cycles

DURING RON MAINTENANCE, THE LEFT FORWARD FUSELAGE EMERGENCY EGRESS LIGHT WAS DIM AND THE 2 MOST FORWARD EMERGENCY FLOOR PATH LIGHTS WERE INOPERATIVE. POWER SUPPLY 3351-PS3 WAS REPLACED ALONG WITH THE BULB IN THE FORWARD FUSELAGE POSITION. SYSTEM OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,572 hrs · 54,938 cycles

DURING RON MAINTENANCE, THE EMERGENCY LIGHT LOCATED UNDER THE LEFT EMERGENCY EXIT DOOR WAS FOUND TO BE DIM. SEVERAL BULBS IN THE LIGHT PANEL WERE FOUND TO BE INOPERATIVE. THE BULBS WERE REPLACED AND OPS CHECKED GOOD.

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 48,853 hrs · 54,177 cycles

ACFT YAWED TO THE LEFT ON CLIMBOUT, CREW NOTED NR 1 ENG TQ WAS AT 30 PERCENT. ALL OTHER ENG INST APPEARED NORMAL. CREW SHUTDOWN AND DECLARED AN EMERGENCY AND RETURNED TO PHL. MX INSPECTED NR 1 ENG AND ONLY DEFECT NOTED WAS ENG 2 QTS LOW ON OIL. SERVICED ENG AND CREW PERFORMED 3 HIGH POWER RUNS WITH NO DEFECTS NOTED. ACFT FERRIED FROM PHL TO ROA. ROA REMOVED AND REPLACED NR 1 HMU AND FUEL PUMP; REMOVED AND REPLACED EEC.

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 48,853 hrs · 54,177 cycles

ACFT YAWED TO THE LEFT ON CLIMBOUT, CREW NOTED NR 1 ENG TQ WAS AT 30 PERCENT. ALL OTHER ENG INST APPEARED NORMAL. CREW SHUTDOWN AND DECLARED AN EMERGENCY AND RETURNED TO PHL. MX INSPECTED NR 1 ENG AND ONLY DEFECT NOTED WAS ENG 2 QTS LOW ON OIL. SERVICED ENG AND CREW PERFORMED 3 HIGH POWER RUNS WITH NO DEFECTS NOTED. ACFT FERRIED FROM PHL TO ROA. ROA REMOVED AND REPLACED NR 1 HMU AND FUEL PUMP AND REMOVED AND REPLACED EEC.

Part: BRACKET — CRACKED (LT SPOILER) · airframe 47,632 hrs · 52,896 cycles

LEFT FLIGHT SPOILER DOG BONE HOLE BRACKET CRACKED. TEST WITH HIGH FREQ EDDY CURRENT, NO CRACK FOUND. LEFT INBOARD FLIGHT SPOILER DOG BONE HOLE WEB REPAINTED IAW E08-57-07-3187-SEG 9734.

Part: ENGINE — ODOR (NR 2) · airframe 46,825 hrs · 52,036 cycles

DURING DESCENT WITH POWER LEVERS AT FLIGHT IDLE THE FLIGHT ATTENDANT NOTICED SMOKE IN FORWARD SECTION OF CABIN, SHUT DOWN RIGHT HAND BLEED WITHOUT IMPROVEMENT, SHUT DOWN BOTH BLEEDS AND SMOKE DISSIPATED. REMOVED AND REPLACED NR 1 ENGINE. MAINTENANCE EVALUATION FLIGHT REQUIRED. EVALUATION FLIGHT UNSATISFACTORY. OIL ODOR IN CABIN AND FLIGHT DECK WITH NR 2 BLEED SELECTED ON, WHEN POWER IS REDUCED TO 20-30 PERCENT TORQUE. REMOVED AND REPLACED NR 2 ENGINE.

Part: ENGINE — OVERSERVICED (NR 2) · airframe 46,821 hrs · 52,030 cycles

STRONG BURNING ODOR IN FLIGHT DECK AND CABIN AFTER REDUCING POWER ON APPROACH. SELECTED BLEEDS OFF AND ODOR WENT AWAY. SELECTED BLEEDS BACK ON, ON GROUND NO BURNING ODOR NOTICED. INSPECTED AND FOUND NR 2 ENGINE OIL LEVEL ONE QUART OVER SERVICED. SERVICED TO CORRECT LEVEL, RAN NR 1 AND NR 2 ENGINES AND APU FOR ONE HOUR, NO BURNING ODOR EVIDENT AT THIS TIME, CHECKED HP BLEED VALVE FOR CONTAMINATION, NONE FOUND.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,796 hrs · 52,003 cycles

DURING DESCENT WITH POWER AT OR NEAR FLIGHT IDLE OILY ODOR IN AIRCRAFT BLEEDS, WHEN POWER IS INCREASED, ODOR WENT AWAY. INSPECTED AIR SWITCHING VALVE AND NL DUMMY PROBE, NO OIL NOTED. REMOVED AND REPLACED STARTER GENERATOR GARLOCK SEAL. REMOVED AND REPLACED BOTH FLEX LINES TO OIL COOLER. (NO FIX SEE REPORT HNAA0600217 DATED 02JAN07)

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 46,765 hrs · 51,972 cycles

SMOKE IN COCKPIT AND CABIN DURING FLIGHT. GROUND RAN AIRCRAFT WITH BLEEDS ON INSPECTED APU AREA FOR LEAKS OF ANY KIND, NONE FOUND. INSPECTED ALL INTERIOR LIGHTS FOR CONDITION AND PROPER OPERATION NO DEFECTS FOUND AT THIS TIME. NOTE: HEAT EXCHANGER WAS CHANGED AT RON THE PREVIOUS NIGHT, THIS WAS FIRST FLIGHT OF THE DAY. SUSPECT SMALL AMOUNT OF CLEANING FLUID WAS CAUSE OF SMOKE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 46,765 hrs · 51,972 cycles

SMOKE IN COCKPIT AND CABIN DURING FLIGHT. GROUND RAN AIRCRAFT WITH BLEEDS ON, INSPECTED APU AREA FOR LEAKS, NONE FOUND. INSPECTED ALL INTERIOR LIGHTS FOR CONDITION AND PROPER OPERATION. NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 46,765 hrs · 51,972 cycles

SMOKE IN COCKPIT AND CABIN DURING FLIGHT. GROUND RAN AIRCRAFT WITH BLEEDS ON INSPECTED APU AREA FOR LEAKS OF ANY KIND, NONE FOUND. INSPECTED ALL INTERIOR LIGHTS FOR CONDITION AND PROPER OPERATION NO DEFECTS FOUND AT THIS TIME. NOTE: HEAT EXCHANGER WAS CHANGED AT RON THE PREVIOUS NIGHT, THIS WAS FIRST FLIGHT OF THE DAY. SUSPECT SMALL AMOUNT OF CLEANING FLUID WAS CAUSE OF SMOKE.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,723 hrs · 51,925 cycles

ODOR OF OIL IN CABIN. ODOR CLEARED BEFORE TAKEOFF THEN RETURNED LAST MIN OF APPROACH. CHECKED NR 1 AND NR 2 ENGINE OIL AND ACM OIL QUANTITY, PERFORMED ENGINE RUN WITH BLEEDS BOTH ON AND OFF UNABLE TO DUPLICATE ON GROUND.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 45,907 hrs · 51,039 cycles

NR 2 ISO HYDRAULIC CAUTION LIGHT CAME ON AFTER TAKEOFF AND NR 2 HYDRAULIC QUANTITY SHOWS ZERO. FOUND LANDING GEAR ACTUATOR LINES LEAKING. REMOVED AND REPLACED LINES.

Part: GCU — FAILED (NR 1 AC GEN) · airframe 45,491 hrs · 50,583 cycles

AFTER T/O, NR 2 AC GEN FAILED IN FLIGHT WOULD NOT RESET. REMOVED AND REPLACED AC GENERATOR AND GENERATOR CONTROL UNIT. PART INFORMATION TO FOLLOW.

Part: CONNECTOR — SHORTED (NR 1 ENG OIL) · airframe 42,294 hrs · 47,119 cycles

NR 1 ENGINE OIL PRESSURE WARINING LIGHT ILLUMINATED ON CLIMBOUT. OIL PRESSURE WAS CONFIRMED NORMAL. MAINTENANCE CLEANED MOISTURE FROM WING ROOT CANNON PLUG, OPS CHECK GOOD.

Part: SKIN PANEL — DEBONDED (FUSELAGE) · airframe 41,885 hrs · 46,691 cycles

DURING BOND TESTING, FOUND WIDE SPREAD DISBOND ON SKIN PANEL AT STRS 27P & 28P FROM FRAME X325 TO X424. REMOVED AND REPLACED SKIN PANEL FROM X325 TO X 424.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,885 hrs · 46,691 cycles

DURING C CHECK, FOUND WIDE SPREED CORROSION THAT REQUIRED STR 31 REMOVAL AND REPLACEMENT. FRAME X253 REQUIRES A FRAME SPLICE WHICH IS A MAJOR REPAIR TO ALLOW INSTALLATION OF REPLACEMENT STRINGER. FRAME SPLICE WAS DONE IAW PIEDMONT EO 8-53-05-0024.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,885 hrs · 46,691 cycles

DURING C CHECK, FOUND WIDESPREAD CORROSION ON STR 31S. DUE TO WIDE SPREAD DAMAGE, DECISION WAS MADE TO REMOVE ENTIRE STR SECTION FROM X182 TO F /SPAR FS (X387) FOR CONVENIENCE. THIS IS A MAJOR REPAIR. REPAIR DONE IAW PIEDMONT E0 8-53-05-0023.

Part: ACTUATOR — FAILED (SPOILERS) · airframe 39,303 hrs · 43,863 cycles

LOST NR 1 HYDRAULIC, QUANTITY WHEN FIGHT/TAXI SWITCH SELECTED TO FLIGHT. REMOVED AND REPLACED INBOARD ROLL SPOILER ACTUATOR.

Part: ACM — ODOR (TAIL) · airframe 37,247 hrs · 41,687 cycles

FAINT MELTING PLASTIC ODOR REPORTED BY PASSENGER AND FLIGHT ATTENDANT, RETURNED TO GATE. INSPECTED AIRCRAFT, SUSPECT INVERTERS, MEL'D. PASSENGER IN ROW 9 COMPLAINED OF BURNING ODOR ON DESCENT. THE ODOR BECAME STRONGER AS DESCENT CONTINUED, CONFIRMED BY FLIGHT ATTENDENT. COULD NOT TELL IF ELECTRICAL OR SMOKE. ON FERRY FLIGHT ODOR AGAIN IN CABIN AND FLIGHT DECK. DIVERTED TO RDU. RAN AIRCRAFT, OK WITH BLEEDS OFF, FERRIED TO ORF. REPLACED AIR CYCLE MACHINE.

Part: COVER — BROKEN · airframe 36,788 hrs · 41,189 cycles

CREW REPORTED FIRST OFFICERS CONTROL YOKE WAS BINDING. FOUND PIECES OF THE FO'S CONTROL COLUMN UPPER PLASTIC COVERS BROKEN OFF AND LODGED IN THE CONTROL CHAIN UPPER SPROCKET. REMOVED PLASTIC PIECES AND TRIMED COVERS PER EO.

Part: ANGLE — CRACKED · airframe 34,771 hrs · 39,055 cycles

#1 NACELLE HORSECOLLAR FRAME FWD ANGLE CRACKED. REPAIRED I.A.W. EO8-54-02-0173.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 34,169 hrs · 38,452 cycles

CRACK IN NOSE GEAR BAY CROSSBEAM AT STATION X97. CRACK IS AT BOTTOM OF J-CHANNEL AT DRAG STRUT ACTUATOR BRACKET. REPAIRED IAW EO8-53-01-508.

Part: COFFEEMAKER — OVERHEATED (GALLEY) · airframe 30,819 hrs · 34,898 cycles

THERE WAS AN HOT ELECTRICAL SMELL IN THE FLIGHT ATTENDANT EMERGENCY EQUIPMENT CLOSET. FOUND WIRES OVERHEATED IN GALLEY LIQUID WARMER ELECTRICAL SOCKET. REPAIRED WIRES.

Part: VALVE — FAILED (OIL COOLER) · airframe 30,245 hrs · 34,309 cycles

ON CLIMBOUT, NR 1 ENGINE OIL TEMP RED LINED AND NR 1 FUEL TEMP FOLLOWED. AIRCRAFT RETURNED TO THE FIELD. REPLACED THE NR 1 OIL TEMP REGULATING VALVE.

Part: FUEL HEATER — OVERTEMP (NR 1 ENGINE) · airframe 30,245 hrs · 34,309 cycles

ON CLIMBOUT, NR 1 ENGINE OIL TEMP RED LINED AND NR 1 FUEL TEMP FOLLOWED. AIRCRAFT RETURNED TO THE FIELD. REPLACED NR 1 ENGINE OIL TO FUEL HEATER.

Part: BATTERY — DISCHARGED (CABIN)

SIX FRONT CABIN FLOOR EMERGENCY LIGHTS ARE OUT. REMOVED AND REPLACED PS2 BATTERY.

Part: SPRING — BROKEN (LAV TRASH BIN)

LAVATORY TRASH BIN DOOR WILL NOT STAY CLOSED. REPLACED BROKEN SPRING ON TRASH BIN DOOR.

Part: SKIN — CRACKED (NR 1 NACELLE)

ORF - NR 1 NACELLE EXHAUST FINGERNAIL IS CRACKED AT THE OUTBOARD FORWARD SIDE SKIN AND HAS SEVERAL LOOSE RIVETS AND MISSING RIVETS AT THE TOP FORWARD SKIN. REPAIRED CRACKED SKIN AND REPLACED RIVETS. (M)

Part: LIGHT — INOPERATIVE (ROW 4F)

CLT - FLT 3138 - ROW 4F EMERGENCY EXIT SIGN IN BROKEN. LIGHTS WORKS OK. REPAIRED EXIT SIGN AS REQUIRED. (M)

Part: PSEU — FAILED (LANDING GEAR)

FLT 3290 - ORF-PHF - AFTER GEAR UP SELECTION, GOT VIBRATION ALONG WITH 3 RED AND 3 GREEN LIGHTS AND NOSE WHEEL YELLOW GEAR DOOR LIGHT. VISUAL INSPECTION CONFIRMED MAIN LANDING GEAR DOWN AND DOORS OPEN. PERFORMED ALTERNATE GEAR EXTENSION, DECLARED EMERGENCY AND RETURNED TO ORF WITHOUT INCIDENT. REMOVED AND REPLACED THE PROXIMITY SWITCH ELECTRONIC UNIT (PSEU). (M)

Part: RETRACT MECH — MALFUNCTIONED (LT MLG DOOR)

FLT NR 3335 - DCA-PHL - AFTER GEAR RETRACTION, THE LEFT DOOR ADVISORY LIGHT ILLUMINATED. THE GEAR DOOR WAS CONFIRMED OPEN AND GEAR WAS RETRACTED IN THE WELL. THE GEAR WAS SELECTED DOWN AND BACK UP, THE LIGHT WENT OUT AND ALL WAS NORMAL. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. MAINTENANCE ADJUSTED THE ROD LENGTH OF THE FORWARD GEAR DOOR ROD AS A PRECAUTION. (M)

Part: CONNECTOR — WET (SMOKE DET)

FLT 3282 - EWN-CLT - EN ROUTE TO CLT, THE SMOKE WARNING LIGHT CAME ON AND WOULD NOT RESET. AIRCRAFT CONTINUED ON TO CLT AND LANDED WITHOUT INCIDENT. DRIED WATER, AND RESET THE CANNON PLUG ON THE NR 2 SMOKE DETECTOR. (M)