N938HA

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,629 hrs · 76,858 cycles

THIRD EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — TRIPPED (PRIMARY INVERTER) · airframe 68,521 hrs · 76,740 cycles

DURING CRUISE FLIGHT, THE PRIMARY INVERTER CAUTION LIGHT ILLUMINATED, ALONG WITH CAPTAIN'S FLIGHT INSTRUMENTS WENT DARK AND TRANSPONDER FAILED. FOLLOWED CHECK LIST AND DECLARED AND EMERGENCY. AIRCRAFT LANDED SAFELY. FOUND PRIMARY AND AUX INVERTER CIRCUIT BREAKERS TRIPPED.

Part: BULB — DIM (EMERGENCY LIGHTS) · airframe 68,411 hrs · 76,615 cycles

EMERGENCY EXIT SIGN ABOVE PAX DOOR DIM. R & R THE BULBS.

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 68,401 hrs · 76,601 cycles

AIRCRAFT IS TOO HOT FOR REVENUE SERVICE. FLIGHT DECK DUCT TEMP AND AIRFLOW IS GOOD. CABIN DUCT TEMP NORMAL WITH POOR AIRFLOW. STANDBY CONDITION, PERFORMED OPS CHECK OF AIR CONDITIONING, IN CABIN AND COCKPIT. CABIN FLOW WITH ENGINE AND APU BLEEDS GOOD. DUCT TEMP 8/10 WITH OAT AT 25 DEG C. OK FOR SERVICE.

Part: CONTROLLER — INOPERATIVE (AUTOPILOT SYS) · airframe 68,285 hrs · 76,466 cycles

UPON ROTATION YAW DAMPER AP SELECT AND HSI SELECT ON 801 PANEL BECAME INOPERATIVE. R&R AFCS CONTROLLER AS REQUIRED IAW AMM 22-10-01. OPS AND TEST ON GROUND GOOD. OK FOR SERVICE.

Part: TSCU — MALFUNCTIONED (NR 2 ENGINE) · airframe 68,025 hrs · 76,144 cycles

DURING TAKEOFF ROLL AT 85 PERCENT TORQUE AUTO FX FAILED TO ARM, REJECTED T/O. LIGHT ILLUMINATED UPON REDUCED POWER. R & R NR 2 ENGINE TSCU IN REF TO 77-10-00 C/W CARDS 72-01-10X & 72-00-10Q. RAN ACFT, OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 68,025 hrs · 76,144 cycles

DURING TAKEOFF ROLL, AUTO FX WOULD NOT ARM AUTOFEATHER SYSTEM. REPLACED RELAY 6121-K5 AS PRECAUTIONARY MEASURE, OPS CK GOOD AT THIS TIME, REF 61-26-00.

Part: FLAP TRACK — CRACKED (RT WING) · corrosion level 2 · airframe 67,968 hrs · 76,073 cycles

RIGHT WING NR 5 FLAPTRACK SHOWS INDICATIONS WHILE PERFORMING EDDY CURRENT INSPECTION AROUND SEVERAL FASTENER HEADS ON OTBD SIDE OF TRACK.

Part: FLAP TRACK — CRACKED (RT WING) · corrosion level 2 · airframe 67,968 hrs · 76,073 cycles

RIGHT WING NR 4 FLAP TRACK SHOWS INDICATIONS WHILE PERFORMING EDDY CURRENT INSPECTION AROUND SEVERAL FASTENER HEADS ON OTBD SIDE OF FLAPTRACK.

Part: PRESSURE SWITCH — MALFUNCTIONED (OIL SYSTEM) · airframe 67,912 hrs · 76,014 cycles

NR 2 ENGINE OIL PRESSURE WARING LIGHT ILLUMINATED INFLIGHT. OIL PRESSURE SHOWS IN GREEN ARC ON GAUGE. ALL OTHER ENGINE PARAMETERS ARE NORMAL. INSPECTED NO LEAKS NOTED. R & R NR 2 LOW OIL PRESSURE SWITCH IAW-8MM 79-36-01. SERVICED WITH 1 QT OF OIL RAN ENGINE FOR 5 MINS AT POWER OPS AND LEAK CHECK GOOD, SWITCH, PN 8D1437.

Part: SKIN — CORRODED (BS 253) · corrosion level 2 · airframe 67,406 hrs · 75,429 cycles

FOUND CORROSION AT BS 253.40, BETWEEN STR 28 AND 30. R & R RIVETS, STRAP AND EXISTING PATCH AT BS 240-5. COMPLIED WITH STEPS 1 THRU 6B OF EA15-2016-024. REPAIRED SKIN AT BS 253.40 BETWEEN STR 28 AND 30 IAW E08-53-16-0098.

Part: SKIN — DAMAGED (BS 252) · airframe 67,406 hrs · 75,429 cycles

MULTIPLE RIVETS PULLING THROUGH SKIN AT BS 252, BETWEEN STR 29-31. R & R RIVETS AT BS 252, BETWEEN STR 29-31 IAW EO8-53-16-0098.

Part: WIRE — BROKEN (POWER LEVER) · airframe 67,332 hrs · 75,337 cycles

AUTOFEATHER WILL NOT ARM. FOUND BROKEN WIRE AT NR 1 ENGINE POWER LEVER MICROSWITCH TERMINAL. RESOLDERED WIRE TERMINAL, PERFORMED OPS CHECKED. OPS CHECK GOOD. COMPLIED WITH ENGINE RUNS IAW SR MANUAL. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 66,959 hrs · 74,890 cycles

AFTER GEAR RETRACTION, ALL LIGHTS WENT OUT, THEN NOSE GEAR RED UNSAFE LIGHT FLICKERED ALONG WITH GEAR HANDLE LIGHTS, THEN EXTINGUISHED. NOSE GEAR UNSAFE LIGHT AND GEAR TRANSIT LIGHTS FOR APPROXIMATELY 10-15 SECONDS. CHECKED PSEU MEMORY. FOUND CODE 10. SWUNG GEAR SEVERAL TIMES. "0" DEFECTS NOTED. REPLACED NLG DRAG STAY PROXIMITY SWITCH. SWUNG GEAR, OPS CHECKED GOOD AT THIS TIME IAW MM 32-20-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,410 hrs · 74,220 cycles

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

Part: GENERATOR — NOT REPORTED · airframe 66,209 hrs · 73,980 cycles

R & R NR 1 AC GENERATOR IAW WORK CARD 24-20-11R. R & R NR 1 AC GCU AND SECURED WITH RETAINED HARDWARE. OPS AND LEAKED CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,058 hrs · 73,799 cycles

ONE RED EMERGENCY EXIT FLOOR LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,992 hrs · 73,717 cycles

THIRD FROM AFT EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,370 hrs · 72,988 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,058 hrs · 72,604 cycles

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

Part: PROPELLER — VIBRATION · airframe 64,065 hrs · 71,389 cycles

SEVERE PROPELLER VIBRATION. SHIMED NR 100 AND 200 PROPELLER BLADES IAW MM 61-10-00. . OPS CHECKED GOOD DURING ENGINE RUNS.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 63,615 hrs · 70,856 cycles

WHEN STANDBY HYD PUMPS WERE SELECTED ON, NR 1 AC GENERATOR DROPS OFF LINE, BUT WILL RESET. R & R NR 2 STANDBY AD NR 2 CASE DRAIN FILLER ELEMENT IAW AMM 29-11-17. OPS AND LEAKED CHECKED GOOD IAW SRT MM. OK FOR SERVICE.

Part: BRAKE ASSY — OVERHEATED (LEFT) · airframe 63,223 hrs · 70,391 cycles

SMOKE COMING FROM LT BRAKE WHICH APPEARS TO BE HOT. R & R NR 2 BRAKE ASSY.

Part: RELAY — FAILED · airframe 63,212 hrs · 70,375 cycles

ON TAKE OFF ROLL, AUTO FX DID NOT ARM. RTO SYS TESTS OK AFTERWARDS. R & R RELAY 6121-K5. GROUND-RAN AIRCRAFT IAW -8 RUNUP MANUAL. OK FOR SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED

AUTOFEATHER E/N ARM ON TAKE OFF ROLL WITH TAKE OFF POWER SET. REJECTED TAKE OFF. COMPLIED WITH SELF TEST OF SYSTEM AND CHECKED GOOD.

Part: ACTUATOR — LEAKING (NLG DOOR) · airframe 62,944 hrs · 70,059 cycles

NLG UNSAFE LIGHT FLASHING INTERMITTENTLY WITH GEAR HANDLE, ACCOMPANIED BY NLG ATTEMPTING TO CYCLE. PERFORMED ALTERNATE EXTENSION AND RECEIVED THREE GREEN LIGHTS. PERFORMED NORMAL LANDING. CHECKED PSEU. FOUND NO CODES. CHECKED PROXIMITY SENSORS. FOUND GAPS WITHIN LIMITS. FOUND NOSE GEAR DOOR ACTUATOR LEAKING. R & R ACTUATOR IAW AMM 32-20-26. OPS CHECKED SEVERAL TIMES, OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 62,595 hrs · 69,638 cycles

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

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 62,595 hrs · 69,638 cycles

FWD FUSELAGE RT EMERGENCY LIGHT IS DIM. R & R BULB AT RT FWD EMERGENCY LIGHT FUSELAGE. OPS CHECKED GOOD.

Part: SENSOR — OUT OF ADJUST (TE FLAP TORQUE) · airframe 62,476 hrs · 69,488 cycles

FLAP DRIVE CAUTION LIGHT FLICKERED ON AND OFF IN FLIGHT AND ON GROUND. R & R FLAP DRIVE TORQUE SENSOR IAW MM 27-52-51. ADJUSTED SENSOR IAW WC 27-50-11Q. INSPECTED FLAP DRIVE TORQUE TUBES, NO DEFECTS NOTED. OPS CHECKED GOOD.

Part: BULB — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 62,455 hrs · 69,462 cycles

LT FUSELAGE AFT EXTERIOR EMERGENCY LIGHT IS DIM. R & R BULB. OPS CHECKED GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 62,298 hrs · 69,284 cycles

THIRD AND FOURTH FLOOR LEVEL EMERGENCY LIGHTS ARE INOPERATIVE. R & R POWER SUPPLY PS2 IAW MM 33-53-01. OPS CHECKED GOOD.

Part: ACTUATOR — INOPERATIVE (SPOILERS) · airframe 62,027 hrs · 68,967 cycles

TAXIING ON BOTH ENGINES, FLIGHT/TAXI SWITCH SELECTED TO FLIGHT, ROLL SPOILER INBD CAUTION LIGHT ILLUMINATED, FOLLOWED BY NR 1 ISOLATION VALVE CAUTION LIGHT ILLUMINATED WITH HYD QTY OF .7. R & R INBD ROLL SPOILER ACTUATOR IAW MM 27-14-05. OPS AND LEAKED CHECKED GOOD.

Part: CONNECTOR — FAILED (RADAR) · airframe 61,889 hrs · 68,793 cycles

RADAR FAILED ON CLIMBOUT IN A TURN FROM DEPARTURE. CLEANED AND REMOVED CORROSION FROM RADAR RT CONNECTOR PLUG. R & R RADAR RT OPS CHECKED GOOD IAW MM 34-41-04.

Part: HOSE — DISCONNECTED (DE ICE BOOTS) · airframe 61,659 hrs · 68,509 cycles

BOTH LT AND RT DEICE BOOTS WILL NOT INFLATE IN NR 5 POSITION. FOUND DEICE HOSE DISCONNECTED AT TAIL RT INBD BOOT. RESECURED HOSE AS REQUIRED. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 61,484 hrs · 68,289 cycles

ROW 4AC AND 4DF EMERGENCY SIDEWALL LIGHTS ARE INOP. REMOVED LENS, REMOVED AND REPLACED BULBS. REINSTALLED LENS. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 61,212 hrs · 67,955 cycles

SECOND EMERGENCY FLOOR LIGHT IS INOPERATIVE. R & R EMERGENCY FLOOR LIGHT. OPS CHECKED GOOD. RESECURED LENS.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 61,088 hrs · 67,815 cycles

EMERGENCY EXIT SIGN OVER AIRSTAIR DOOR HAS BULB INOPERATIVE. REMOVED LENS, REMOVED AND REPLACED BULBS. REINSTALLED LENS. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 60,938 hrs · 67,637 cycles

FLOOR EMERGENCY LIGHT IS INOPERATIVE, 7TH FROM FRONT. R & R BULB. OPS CHECKED GOOD. REINSTALLED FLOOR LENS COVER.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 60,687 hrs · 67,331 cycles

RT AFT FUSELAGE EXTERIOR EMERGENCY LIGHT IS DIM. R & R BULB, OPS CHECKED GOOD.

Part: SENSOR — FAILED (CABIN TEMP) · airframe 60,674 hrs · 67,314 cycles

STRONG ODOR IN AFT CABIN WITH ENGINE BLEEDS ON. RETURN TO GATE FOUND AUTO TEMP TO BE INOPERATIVE. MANUAL CONTROL OPS NORMAL. R & R CABIN ZONE TEMP SENSOR IAW MM 21-60-44. OPS CHECKED GOOD. NO ODOR.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,198 hrs · 66,700 cycles

FOURTH RED FLOOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED PLASTIC COVER, REMOVED BULB, INSTALLED NEW BULB. REINSTALLED LIGHT LENS COVER. OPS CHECKED GOOD.

Part: DOOR — OPEN (MLG) · airframe 59,987 hrs · 66,446 cycles

GEAR FAILED TO RETRACT AFTER TAKEOFF. MAINT INSPECTED AND FOUND OVERHEAD BYPASS DOOR OPEN. MAINT CLOSED DOOR AS REQUIRED.

Part: WARNING LIGHT — FALSE ACTIVATION (NLG) · airframe 59,861 hrs · 66,295 cycles

NOSE GEAR RED UNSAFE LIGHT ILLUMINATED INTERMITTENTLY WITH GEAR DOWN AND LOCKED. COULD NOT DUPLICATE. R & R PSEU IAW -8MM 32-61-50 FOR MX CONVIENCE. OPS CHECKED GOOD. NO FURTHER MX ACTION REQUIRED.

Part: OIL SYSTEM — LOW (NR 2 ENGINE) · airframe 59,817 hrs · 66,245 cycles

NR 2 ENGINE OIL PRESSURE LIGHT ILLUMINATED ON TAKEOFF. CREW DEPARTED RUNWAY. OIL PRESSURE NORMAL. INSPECTED ENGINE, FOUND 3 QUARTS LOW. SERVICED AS REQUIRED. GROUND RAN ACFT. NO DEFECTS NOTED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 59,364 hrs · 65,712 cycles

FORWARD FUSELAGE RT EMERGENCY LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PS2 IN COAT CLOSET IAW AMM 33-51-00.

Part: GENERATOR — FAILED (NR 2 AC) · airframe 59,171 hrs · 65,494 cycles

RT AC BUSS CAUTION LIGHT CAME ON IN FLIGHT. R & R NR 2 AC GENERATOR IAW 24-20-11R AND GCU IAW -8 MM 24-21-02. GROUND RAN AND OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,993 hrs · 65,294 cycles

AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R OVERHEAD EMERGENCY LIGHT AT ROW 7 AND SECURED LENS COVER.

Part: PRESSURE SWITCH — FAILED (RUDDER) · airframe 58,969 hrs · 65,265 cycles

RUDDER FULL PRESSURE CAUTION LIGHT ILLUMINATED ON TAXI. R & R BOTH RUDDER FULL PRESSURE SWITCHES. GROUND RAN AIRCRAFT, LEAKED AND OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,905 hrs · 65,199 cycles

BULB OUT IN AFT RT EMERGENCY EXIT LIGHT BAR. R & R EMERGENCY LIGHT BULB. OPS CHECKED GOOD.

Part: HMU — FAILED (NR 1) · airframe 58,715 hrs · 64,985 cycles

PROGRESSIVE POWER LEVER SPLIT AFTER TAKEOFF APPROX 3 KNOB SPLIT, NR 1 POWER LEVER MAX TORQUE AT 70 PERCENT CHECKED RIGGING IAW 76-00-10Q, NO FIX. SWAPPED PROP GAUGES, NO FIX. SWAPPED GAUGES BACK TO ORIGINAL POSITION. R & R PCU IAW 61-10-10RQ, NO FIX. PROP GOVERNOR TEST, NO FIX. R & R HMU IAW WORKCARDS 73-20-01R, 76-00-10Q AND 24-30-02R. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 58,711 hrs · 64,981 cycles

RT UNDERFLOOR CABIN STR 31 CORRODED BETWEEN STA X445.00 AND X467.00. REPLACED WITH NEW PARTS AND INSTALLED WITH SOLID RIVETS IAW RD8-53-1834, RD8-51-015 AND DWG 85330028.

Part: KEELBEAM — DAMAGED (FUSELAGE) · airframe 58,711 hrs · 64,981 cycles

CORROSION FOUND IN WAFFLE DOUBLER BETWEEN FRAME STA X424 AND X434 UNDER STR 31S. HFEC INSPECTION AND BOND TEST CARRIED OUT ON AFFECTED AREA IAW EA09-2012-019. NO CRACKS OR DISBOND INDICATION FOUND. JOINT STRAP AND WAFFLE DOUBLER WERE BLENDED WITHIN LIMITS IAW SRM 53-00-16. REPLACED IAW RD8-51-015 AND DWG 85330028.

Part: FRAME — CORRODED (BS 445) · corrosion level 2 · airframe 58,711 hrs · 64,981 cycles

RT CABIN UNDERFLOOR FRAME STA X445.00 IS CORRODED BETWEEN STR 30 AND 31R. REPAIRED FRAME IAW SRM 53-20-21 AND INSTALLED IAW SRM 51-42-05.

Part: FRAME — CORRODED (BS 436) · corrosion level 2 · airframe 58,711 hrs · 64,981 cycles

RT CABIN UNDERFLOOR FRAME STA 436 IS CORRODED BETWEEN STR 30 AND 31. REPAIRED IAW SRM 53-20-21 AND INSTALLED WITH SOLID RIVETS IAW SRM 51-42-05.

Part: FRAME — CORRODED (BS 488) · corrosion level 2 · airframe 58,711 hrs · 64,981 cycles

RT UNDER FLOOR CABIN AT FRAME STA X488.00 IS CORRODED BETWEEN STR 30 AND 31R. REMOVED CORRODED FRAME IAW SRM 53-20-21 AND INSTALLED IAW SRM 51-42-05.

Part: FRAME — CRACKED (BS 136.8 S15) · airframe 58,711 hrs · 64,981 cycles

FRAME CRACKED BS X136.8 AND STR 15. R & R IAW SRM 51-42-05 AND SRM 51-40-10.

Part: FRAME — CRACKED (FUSLAGE) · airframe 58,711 hrs · 64,981 cycles

FRAME CRACKED IN FLIGHT COMPARTMENT RT SIDE AT STA X136.8 AND STR 15. R & R FRAME IN FLIGHT COMPARTMENT RT SIDE. INSTALLED WITH NEW SOLID RIVET AND HI-LOK IAW SRM 57-42-05 AND SRM 51-40-10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,688 hrs · 64,954 cycles

FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE, SECOND FROM FRONT. R & R FLOOR PATH EMERGENCY LIGHT AT SECOND FROM FRONT POSITION.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,688 hrs · 64,954 cycles

CEILING EMERGENCY LIGHT IS INOPERATIVE AT ROW 7. R & R CEILING EMERGENCY LIGHT AT ROW 7.

Part: PUMP — INOPERATIVE (NR 1) · airframe 57,885 hrs · 64,055 cycles

NR 1 STANDBY PRESSURE INDICATES ZERO. R & R RT RCCP. GROUND RUN UP, OPS CHECKED GOOD IAW MM 29-11-17.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 57,680 hrs · 63,816 cycles

EMERGENCY FLOOR EGRESS LIGHT 2ND FROM THE FRONT IS INOP. R & R LAMP IAW 33-52-00.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 57,680 hrs · 63,816 cycles

RT EMERGENCY EXIT LIGHT OVER DOOR HAS BULB INOP. R & R BULB, OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 56,670 hrs · 62,697 cycles

EMERGENCY CEILING LIGHT INOP AT ROW 4. REMOVED LENS, R & R BULB, REINSTALLED LENS.

Part: BRAKE — WORN (NR 4) · airframe 56,360 hrs · 62,360 cycles

SMOKE COMING FROM NR 4 BRAKE. INSPECTED RT BRAKE ASSY AND FOUND NR 3 BRAKE ASSY WORN PAST LIMITS. R & R NR 3 BRAKE ASSY IAW 8MM 32-42-11. NR 4 BRAKE CHECKED GOOD.

Part: CHECK VALVE — FAILED (NLG STEERING) · airframe 54,438 hrs · 60,149 cycles

AFTER GEAR UP SELECTION, NR 2 HYD QTY DROPPED TO 1 QT. AFTER WHICH SPOILER AND NR 2 ISO LIGHTS ILLUMINATED. NO PRESSURE DROP AND QTY REMAINED AT 1QT. R & R CHECK VALVE ON STEERING MANIFOLD. OPS AND LEAKED CHECKED GOOD.

Part: UPLOCK ACTUATOR — MALFUNCTIONED (LT MLG) · airframe 54,153 hrs · 59,804 cycles

AFTER TAKEOFF, DURING GEAR RETRACTION LEFT MAIN GEAR RED IN TRANSIT LIGHT REMAINED ILLUMINATED, CAPTAIN PERFORMED ALTERNATE EXTENSION OF GEAR. REMOVED AND REPLACED LEFT GEAR UPLOCK ACTUATOR IN ACCORDANCE WITH -8 MM 32-30-26. CYCLED GEAR SEVERAL TIMES IN HANGER. OPERATIONAL CHECKED GOOD.

Part: BRAKE ASSY — STICKING (MLG) · airframe 54,134 hrs · 59,779 cycles

ON TAXI OUT, RIGHT BRAKES APPEARS TO BE STICKING AFTER PARK BRAKE WAS SET AND RELEASED. RETURNED TO GATE. BRAKES WERE IN HEAVY SMOKE ON ARRIVAL TO GATE. REMOVED AND REPLACED BOTH INBOARD AND OUTBOARD RIGHT BRAKE ASSEMBLE AND TIRES IN ACCORDANCE WITH -8 MM 32-41-11. TAXIED AIRCRAFT, CHECKED AND LEAKED GOOD, LUBED RIGHT MAIN LANDING GEAR.

Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 59,349 hrs

DURING NORMAL GEAR EXTENSION, NLG DID NOT EXTEND. PERFORMED MANUAL EXTENSION, NLG EXTENDED AND LOCKED INTO POSITION. R & R LANDING GEAR SELECTOR VALVE IAW MM 32-30-41. R & R UPLOCK ACTUATOR IAW MM 32-10-00. OPS AND LEAK CKD GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 53,347 hrs · 58,891 cycles

CABIN--EMERGENCY FLOOR PATH LIGHTS ARE INOPERABLE AT SEAT 2DF. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY PS2 "ABOVE SEAT 1DF" AND CLOSED ACCESS PANELS IAW 33-52-00. P/N OFF+ON 60-3844-3LB SN OFF 0787 SN ON 1779.

Part: HEAD — MALFUNCTIONED (NR 2 COMM SYSTEM) · airframe 52,483 hrs · 57,945 cycles

UNABLE TO CHANGE RADIO FREQUENCY ON NUMBER TWO NAVIGATION AND BOTH COMMUNICATIONS, RADIO NAVIGATION FREQUENCY PAGE BLANK. DISC THE FOLLOWING RADIO NAVIGATION COMPUTER, ONE AND TWO NAVIGATION HEADS, ADF CONTROL HEAD, ONE COMM HEAD ALL NO FIX. RECONNECT ALL UNITS AS REQ. REMOVED AND REPLACED NR 2 COMM HEAD, OPS CHECK GOOD. RNAV SELF TEST GOOD IAW 34-61-02. OP CHECK BOTH COMM'S CARRYING OUT 2-WAY COMMUNICATION, OP'S CHECK NAV'S USING 401 TEST SET AND OP CHECK ADF USING LOCAL GND STATION. OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 51,677 hrs · 57,072 cycles

1 RED EMERGENCY LIGHT MODULE AT ROW 4 HAS A BROKEN WIRE. R&R D LIGHT MODULE AT ROW 4 IAW STANDARD PRACTICE.

Part: HYDRAULIC LINE — LEAKING (NLG) · airframe 51,465 hrs · 56,822 cycles

AFTER ROTATION, SELECTED GEAR UP, NOSE GEAR CAME UP, NOSE DOORS STAYED OPEN, MAIN GEAR STAYED UNSAFE, GEAR CAME UP NORMALLY WITH 3 GREENS AFTER APPOX 10 SECONDS AND GRINDING SOUND QUIT. INSPECTED AND FOUND NOSE GEAR DOWN LINE LEAKING AT STA X107.00. REMOVED AND REPLACE LINE IAW 29-20-00, OPS AND LEAK CHECKS GOOD IAW MM 12-10-29, CYCLED GEAR SEVERAL TIMES, OK FOR SERVICE.

Part: TORQUE SENSOR — CONTAMINATED (NR 1 ENGINE) · airframe 51,272 hrs · 56,715 cycles

ON TAKEOFF NR 1 ENGINE TORQUE DROP TP 40 PERCENT IN FLUX THE INCREASED OVER 108 PERCENT FOR 15 SECOND PROPELLER RPM DROP TO 350. REMOVED TORQUE SENSOR CONTROL UNIT NR 1 ENGINE. FOUND MOISTURE IN CONNECTOR. REPLACED TORQUE SENSOR CONTROL UNIT.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 51,266 hrs · 56,502 cycles

EMERGENCY EXIT SIGN AT SEAT 4A REMAINS ILLUMINATED CONSTANTLY. INSPECTED AND FOUND LIGHT NOT TO BE ILLUMINATED.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 49,633 hrs · 54,818 cycles

EXIT LIGHT UNDER EMERGENCY EXIT DOOR IS DIM. REMOVED AND REPLACED EXIT LIGHT BULB, OPS CHECKED GOOD.

Part: ELEVATOR — ICED · airframe 49,039 hrs · 54,179 cycles

DURING TAKEOFF ROLL, THE AIRCRAFT REACHED 104 KNOTS AND THE CREW ATTEMPTED TO ROTATE THE AIRCRAFT TO LIFT OFF, BUT WERE UNABLE TO DO SO. THE CAPTAIN IMMEDIATELY ABORTED THE TAKEOFF AND USED THE REMAINDER OF THE RUNWAY FOR STOPPING. CONDITIONS WERE WET AND SNOWY. THE AIRCRAFT WAS THEN TAXIED BACK TO THE GATE WHERE MAINTENANCE INSPECTED THE AREA OF THE ELEVATORS AND DISCOVERED ICE IN THIS AREA. ICE WAS REMOVED FROM THIS AREA AND FURTHER INSPECTION SHOWED NO OTHER DISCREPANCIES. AIRCRAFT WAS THEN RELEASED FOR SERVICE. ADDITIONAL INFORMATION ADDED.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 48,320 hrs · 53,411 cycles

AFTER PUSHBACK AND ENGINE START, FLIGHT GO A BAG COMPARTMENT SMOKE DETECTOR WARNING LIGHT. CAPTAIN NOTIFIED F/A TO HASTILY DEPLANE THE PASSENGERS AND HAD THE F/O CALL FOR A FIRE TRUCK TO CHECK IT OUT. THERE WAS NO FIRE OR SMOKE EVIDENT.

Part: STRINGER — CORRODED (BS 291 S31R) · airframe 47,703 hrs · 52,726 cycles

CORRODED RIGHT UNDERFLOOR. CORROSION ON STRINGER 31 AFT OF STATION 291. AT STRINGER 31 FRAME X291 PREVIOUS REPAIR REPLACED AS PER SRM 53-20-21.

Part: ACCESS PANEL — CORRODED (LAVATORY) · airframe 47,703 hrs · 52,726 cycles

HINGE OF LAV SERVICE PANEL, HEAVY CORROSION. CORROSION ON HINGE OF LAV SERVICE PANEL REMOVED AND REPROTECTED IAW SRM 51-20-11 (0.002") AND LAVATORY SERVICE PANEL REPLACED AND INSTALLED WITH RIVET IAW SRM 51-40-00.

Part: THRESHOLD — CORRODED (CORRODED) · airframe 47,703 hrs · 52,726 cycles

PASSENGER DOOR ENTRANCE LOWER STRIP FOUND CORRODED. PASSENGER DOOR ENTRANCE LOWER STRIP THRESHOLD MEMBER REPLACED WITH NEW PART INSTALLED WITH SOLID RIVETS IAW SRM 51-40-00.

Part: FITTING — CORRODED (BS 291) · corrosion level 2 · airframe 47,703 hrs · 52,726 cycles

CORROSION ON TOILET SERVICING ACCESS BOX RIGHT UNDER FLOOR. TOILET SERVICING BOX FITTING ON RIGHT UNDER FLOOR REPLACED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 47,703 hrs · 52,726 cycles

CORROSION ON STRINGER 31 FWD OF X202. STRINGER 31 FWD OF X202 REPAIRED AS PER RD-8-53-1243.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 45,099 hrs · 49,944 cycles

AFTER DEPARTURE NR 2 HYDRAULIC QUANTITY WENT TO 3/4 QUART. ROLL SPOILER OUTBOARD HYDRAULIC CAUTION LIGHT ILLUMINATED PRESSURE REMAINED NORMAL. REMOVED AND REPLACED BLUE FLEX LINE TO UP SIDE OF NOSE GEAR DRAG STRUT ACTUATOR.

Part: INDICATOR — MALFUNCTIONED (NR 2 FUEL) · airframe 43,463 hrs · 48,696 cycles

NR 2 FUEL GAUGE INDICATES DOUBLE THE FUEL BURN NR 2 FUEL GAUGE, OPS NORMAL DURING FERRY FLT. REFUELED IN LGA. MAGNA STICKED NR 2 TANK AND NR 2 FUEL GAUGE MATCHES MAGNA STICK READING. GAUGE OPS NORMAL AT THIS TIME.

Part: MONITOR — INOPERATIVE (BATTERY TEMP) · airframe 40,774 hrs · 45,170 cycles

RETURN TO FIELD, DUE TO MAIN AND AUX BATTERIES INDICATING 65 DEGREES. REMOVED AND REPLACED BATTERY TEMP MONITOR.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 40,160 hrs · 44,507 cycles

NR 2 HYD QYT DROPPED TO 1 QT INFLT, AIR TURNBACK, INSTALLED TFL FROM BULKHEAD TO T FITTING UNDER GRAVEL GUARD IN NOSE WHEEL WELL, LEAK CHECK GOOD. R&R HYDRAULIC LINE.

Part: BLADE — BURNED (PROPELLER) · airframe 39,389 hrs · 43,680 cycles

WITH PROP HEAT ON NR 2 PROP STARTED GLOWING ORANGE CEASED WITH PROP HEAT OFF REMOVED AND REPLACED NR 2 BLADE AND BLADE RETAINING RING OPS AND LEAK CK GOOD IAW W/C 61-10-07R.

Part: ATTACH FITTING · airframe 36,536 hrs · 40,737 cycles

During A-check inspection a crack was found in the NLG drag strut actuator fitting. The fitting was changed.

Part: TERMINAL — LOOSE (WINDSCREEN HEAT) · airframe 358,294 hrs · 40,019 cycles

AFTER SELECTION OF WINDSHIELD WARM-UP, NOTICED SMOKE FROM FIRST OFFICERS WINDSCREEN AREA. SELECTED TO OFF AND SMOKE DISAPPEARED. INSPECTED ALL WINDSCREEN TERMINALS, TEMP MONITOR IN COAT CLOSET AND WIRES UNDER GLARESHIELD. FOUND ONE LOOSE TERMINAL (L2) ON THE FIRST OFFICERS SIDE. RESECURED L2 AND OPS CHECKED WIND SCREEN HEAT. OPERATIONAL CHECK GOOD.

Part: CIRCUIT BREAKER — INOPERATIVE (#1 NACELLE) · airframe 34,650 hrs · 38,719 cycles

While taxing to gate lost #1 standby hydraulic pump, lost toe brakes. Replaced RCCB, ops check good.

Part: BRACKET — CRACKED · airframe 33,506 hrs · 37,466 cycles

AILERON CONTROL QUADRANT MOUNTING BRACKET ON L/H WING REAR SPAR FOUND CRACKED AT OUTBOARD END OF THE LOWER FLANGE TO 1/16" BEYOND THE FIRST RIVET HOLE. REPAIRED IAW ESR8-57-01-012A.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 32,670 hrs · 36,580 cycles

DURING INSPECTION, (NOSE LANDING GEAR BAY) THE FORWARD LEFT HAND SIDE OF NOSE WHEEL BAY WAS CRACKED AT J-CHANNEL SIDEWALL. REPAIRED IAW RD8-53-675.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,102 hrs · 35,973 cycles

FIRST TWO RED EMERGENCY FLOOR LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK 3352-P2.

Part: UNKNOWN — ODOR (LAVATORY)

HEAVY FUEL ODOR IN LAV. INSPECTED AND FOUND UNIDENTIFIED FLUID IN LAV. DRAINED LAV AND PLACED ON MEL 25-7 (INOP AND NO USE).

Part: TEMP MONITOR — FAILED (COCKPIT)

SMOKE IN COCKPIT AROUND BATTERY TEMP MONITOR.

Part: ANGLE — CHAFED (NR 1 NACELLE)

NR 1 ENG HORSE COLLAR CHAFED ON INBOARD SIDE, FWD ANGLE DOUBLER. PART OF MONOCOQUE STRUCTURE OF NAC CAUSE BY BONDING STRAP DEPTH= .016. BLENDED AREA IAW EO8-54-99-727.

Part: LIGHT — INOPERATIVE (ROW 4A)

SBY - FLT 3303 - LOWER EMERGENCY LIGHT BROKEN AT ROW 4A. REMOVED AND REPLACED EMERGENCY LIGHTS ASSY. OPS CHECK GOOD. (M)

Part: BATTERY — DISCHARGED (CABIN)

DURING ORIGINATING CHECK FOR FLIGHT 3287 FROM TLM TO MCO, TWO FORWARD RED ESCAPE PATH LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY 3352 PS2. (M)

Part: BATTERY — DISCHARGED (CABIN)

ROA/DCA - FLT 3199 - FIRST TWO EMERGENCY PATH LIGHTS INOPERATIVE. FIRST FOUR WHITE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PS4. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

PHF/PIT - FLT 3163 - DURING PRE-FLIGHT CHECKS, FOUND THE FIRST TWO RED ESCAPE PATH LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY 3352-PS2. (X)

Part: WIRE — FAILED (NLG)

FLT 3397 - YYZ-BWI - ON APPROACH INTO BWI, THE NOSE GEAR RED UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE LIGHT ON. THE AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NOSE LANDING GEAR DOWNLOCK PROX SENSOR WIRES CUT. REMOVED AND REPLACED SENSOR. (M)

Part: HYD RESERVOIR — REQUIRED SERVICE (NR 2 SYSTEM)

SBY/LYN - FLT EN14 - AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED UP, THE NR 2 HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED THEN WENT OUT. UPON GEAR DOWN SELECTION, THE GEAR WOULD NOT EXTEND AND THE RIGHT FORWARD DOOR ONLY OPENED HALF WAY. PERFORMED ALTERNATE GEAR EXTENSION AND RETURNED TO SBY WITHOUT INCIDENT. BLED NR 2 HYDRAULIC SYSTEM RESERVOIR AND SWUNG THE GEAR. (X)

Part: EEL BASE — FAILED (CABIN)

PHL/DCA - FLT 3257 - DURING PRE-FLIGHT WALK-AROUND, FOUND TWO FORWARD RED FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY BATTERY AND BASE. REFERENCE CONTROL NR 95ZZZX4240.

Part: EEL BATTERY — DISCHARGED (CABIN)

PHL/DCA - FLT 3257 - DURING PRE-FLIGHT WALK-AROUND, FOUND TWO FORWARD RED FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY BATTERY AND BASE. REFERENCE CONTROL NR 95ZZZX4241.

Part: BRAKE ASSY — FAILED (MLG)

FLT 3099 - MIA-JAX - LEFT BRAKE CHATTERS VIOLENTLY ON TAXI, RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES. (W)

Part: BRAKE ASSY — FAILED (MLG)

FLT 3099 - MIA-JAX - LEFT BRAKE CHATTERS VIOLENTLY ON TAXI, RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES. (W)

Part: WOW SENSOR — FAILED (NR 2 MLG)

SBY-CHO - FLT 3156 - WEIGHT ON WHEELS CAUTION LIGHT CAME ON DURING TAKEOFF. ACFT TURNED BACK AND LANDED IN SBY WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 MLG I/B WEIGHT ON WHEELS SENSOR.