N943HA

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,488 hrs · 76,220 cycles

EMERGENCY CEILING LIGHT AT ROW 4 INOPERATIVE. R & R THE BATTERY AT ROW 3AC IAW 33-51-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 66,445 hrs · 75,003 cycles

SEVERAL EMERGENCY LIGHTS OUT DUE TO SWITCH LEFT ON. R & R EMERGENCY LIGHT BATTERIES IAW W/C 33-50-05R.

Part: PLATE — CORRODED · corrosion level 2 · airframe 66,410 hrs · 74,958 cycles

PASSENGER DOOR AFT GOOSE NECK HARDWARE RENTION PLATE BADLY CORRODED, LOCATED ADJACENT TO TOP STEP 12668. FABRICATED PLATE AND R & R PAX DOOR AFT GOOSE NECK HARDWARE RETENTION PLATE IAW DWG 85210303, PART INSTALLED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,442 hrs · 73,827 cycles

FORWARD LT FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,306 hrs · 73,655 cycles

ROW 9DF FLOOR EMERGENCY LIGHT IS OUT. REMOVED LENS, R & R ROW 9DF FLOOR EMERGENCY LIGHT, RESECURED LENS WITH RETAINED HARDWARE.

Part: UNKNOWN — UNKNOWN · airframe 65,165 hrs · 73,491 cycles

EMERGENCY LIGHTS IN THE CABIN AND BOTH INTAKE BYPASS AMBER LIGHTS FLICKERING IN FLIGHT. ONLY WITH BOTH PROPELER RPM AT 1050. PROPELLER HEAT WAS OFF. CLEANED BOTH A/C GENERATOR CONNECTOR PLUGS. GROUND RAN A/C AT 1050-1200 WITH NO DEFECTS NOTED. OK FOR SERVICE.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 65,111 hrs · 73,425 cycles

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

Part: WARNING LIGHT — ILLUMINATED · airframe 64,625 hrs · 72,824 cycles

RIGHT AC BUSS AND RT TRU ILLUMINATED DURING FLIGHT. R & R NR 2 AC GENERATOR IAW WORK CARD 24-20-11R. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,608 hrs · 72,806 cycles

MIDDLE OVERHEAD CABIN EMERGENCY EXIT LIGHT IS INOPERATIVE. R & R BULB IN OVERHEAD EMERGENCY EXIT LIGHT. OPS CHECKED GOOD.

Part: VALVE — MALFUNCTIONED (NR 2 ENGINE OIL) · airframe 63,462 hrs · 71,415 cycles

NR 2 OIL TEMP DROPS TO 45-50 DEGREES IN CLIMB WITH SAT OF -4 DEGREES C WITH LOW ALT SAT OF +15 DEGREES C IN CRUISE. NR 2 OIL TEMP IS 50-55 DEGREES C. RETURN TO FIELD. R & R ENGINE OIL TEMP BULB AND LEAK CHECKED, NO FIX. R & R NR 2 ENGINE OIL COOLER DIVERTER VALVE IAW 79-20-11. RAN ACFT, OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,156 hrs · 69,842 cycles

PAX DOOR FLOOR EMERGENCY LIGHT BULB IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,973 hrs · 69,609 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,804 hrs · 69,396 cycles

EMERGENCY FLOOR LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT BATTERIES IAW WC 33-50-05R AND 33-50-03Q. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (WINDSHIELD) · airframe 61,682 hrs · 69,242 cycles

RIGHT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED WITH WINDSHIELD SELECTED TO NORMAL. R & R RIGHT WINDSHIELD CONTROLLER. GROUND RAN ACFT. OPS CHECKED GOOD IAW MM 30-41-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,388 hrs · 67,657 cycles

RED EMERGENCY PATHWAY LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-00.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYS) · airframe 60,213 hrs · 67,443 cycles

RADAR INOPERATIVE, PAINTS INACCURATE WEATHER BEYOND 20 MILES. R & R RADAR TRANSCEIVER IAW MM 34-41-04 AND BULLETIN 34-18. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BRUSH BLOCK — MALFUNCTIONED (PROP HEAT) · airframe 60,118 hrs · 67,323 cycles

EMERGENCY LIGHTS FLICKERING IN FLT (PROP HEAT OFF) F/A PANEL LIGHTING INTERMITTENT IN FLT ALSO, CLEANED AND RESEATED BRUSH BLOCKS ON NR 1 AND NR 2 ENGINES. UPPER FWD COWLING ON BOTH ENGINES REMOVED AND REINSTALLED GROUND RUN CHECK GOOD.

Part: WIRE — BROKEN (SWITCH) · airframe 59,789 hrs · 66,913 cycles

AFTER GEAR EXTENSION, CREW HEARD A SINGLE POP NOISE, THEN AFTER ROLL OUT, WHEN FLAPS WHERE SELECTED TO 5 DEGREES FROM 15 DEGREES, FLAPS DID NOT MOVE. BUT WHEN ZERO WAS SELECTED, THE FLAPS RETRACTED FULLY. MOVING FLAP SELECTOR TO ZERO, A RESISTANCE WAS FELT. REPAIRED BROKEN WIRE ON FLAP SELECTOR ARMING SWITCH AT CENTER COUNCIL. OPS CHECKED GOOD IAW DASH 8 MM 27-52-00 AND WIRING DIAGRAM 27-50-00.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 59,731 hrs · 66,833 cycles

EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 3. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,576 hrs · 66,639 cycles

SIDEWALL LIGHT IS DIM AT ROW 4DF. R & R BULB.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,528 hrs · 66,579 cycles

EMERGENCY CEILING LIGHT AT ROW 10 IS DIM. REPLACED LAMP, INSTALLED COVER. OPS CHECKED GOOD.

Part: ACTUATOR — LEAKING (SPOILERS) · airframe 59,276 hrs · 66,252 cycles

HYDRAULIC QTY DROPPED TO 1QT. JUST BEFORE TAKEOFF AND ISO VALVE CAUTION LIGHT ILLUMINATED. SERVICED NR 1 HYD AND OPERATED NR1 HYD SYS AND FOUND RT INBD SPOILER ACTUATOR LEAKING. R & R RT INBD SPOILER ACTUATOR IAW MM 27-14-05. OPS AND LEAKED CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,622 hrs · 65,459 cycles

SECOND MOST FORWARD EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R FLOOR PATH LIGHT BULB. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,385 hrs · 65,163 cycles

ROW 5, OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. REMOVED LIGHT LENS PANEL, R & R BULB. OPS CHECKED GOOD. INSTALLED PANEL WITH RETAINED HARDWARE.

Part: STRINGER — CORRODED (BS 201.3) · corrosion level 1 · airframe 58,385 hrs · 65,163 cycles

CORROSION AT STR 31P AND FRAME X201.300 ON THE LT SIDE OF TENSION FITTING. BLENDED CORROSION IAW SRM 51-20-11, ALODINED AND PRIMED AREA IAW SRM 51-20-16 AND 51-20-36.

Part: SEAT TRACK — CORRODED (GALLEY AREA) · corrosion level 2 · airframe 58,385 hrs · 65,163 cycles

CORROSION ON RT INBD SEAT TRACK AROUND ATTACH POINT FOR GALLEY. REMOVED CORRODED PORTION OF SEAT TRACK IAW RD8-53-3074. SPLICE IN NEW PORTION OF SEAT TRACK IAW RD8-53-3074.

Part: FRAME — CORRODED (BS 436.5 S31L) · corrosion level 1 · airframe 58,385 hrs · 65,163 cycles

MINOR CORROSION ON FRAME LEG AT BS 436.500 AND STR 31S. BLENDED CORROSION IAW SRM 51-20-11, ALODINED AND PRIMED IAW SRM 51-20-16, 51-20-36.

Part: FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 58,385 hrs · 65,163 cycles

BOTTOM OF AIRSTAIR DOOR OPENING THRESHOLD FITTING IS CORRODED. R & R THRESHOLD MEMBER IAW ENG DWG 85321241.

Part: STRINGER SPLICE — CORRODED (BS 448.5) · corrosion level 2 · airframe 58,385 hrs · 65,163 cycles

CORROSION AT STRINGER 32S AND AFT OF FRAME 488.500. REMOVED STRINGER SPLICE AT BS 488.5. REMOVED STRINGER SECTION FROM BS 488.5 THROUGH 528. REINSTALLED STRINGER SPLICE AND STR SECTION FROM BS 488.5 TO 528 IAW DWG 85330033.

Part: STRINGER — CORRODED (BS 445.5) · corrosion level 1 · airframe 58,385 hrs · 65,163 cycles

CORROSION ON STRINGER 31S BETWEEN BS 445.500 AND 467.000. BLENDED CORROSION IAW SRM 51-20-11, ALODINE AND PRIMED IAW SRM 51-20-16, 51-20-36.

Part: FRAME — CORRODED (BS 531.5) · corrosion level 1 · airframe 58,385 hrs · 65,163 cycles

CORROSION AT FRAME LEG STA X531.5 BETWEEN STR 32S AND 31S. BLENDED CORROSION IAW SRM 51-20-11, ALODINED, PRIMED AREA IAW SRM 51-20-16, 51-20-36.

Part: HINGE FITTING — CORRODED (LAV SERVICE) · corrosion level 1 · airframe 58,385 hrs · 65,163 cycles

LAVATORY SERVICE AREA DOUBLER HINGE AND DOOR ARE CORRODED. R & R LAVATORY DOUBLER AND DOOR ASSY IAW DWG 85320983.

Part: FRAME — CORRODED (BS 510) · corrosion level 1 · airframe 58,385 hrs · 65,163 cycles

MINOR CORROSION AT BOTTOM OF VERTICAL FRAME MEMBER AT STA X510.00 BETWEEN STR 32S AND 31S. BLENDED CORROSION IAW SRM 51-20-11, ALODINED, PRIMED AREA IAW SRM 51-20-16, 51-20-36.

Part: STRINGER — CORRODED (BS 445.5 S31R) · corrosion level 1 · airframe 58,385 hrs · 65,163 cycles

CORROSION ON STR 31S, JUST AFT OF FRAME BS 445.5.

Part: SKIN — DEBONDED (BS 506-520) · corrosion level 2 · airframe 58,385 hrs · 65,167 cycles

SKIN DISBONDED ALONG STR 32S FROM X506 TO X520 AND AT FRAME X510 AT FRAME LEGS INBD AND OTBD OF STR 32S. REMOVED RIVETS IN FRAME X510 FROM STR 30S TO 31P, FROM STR31S TO 32S,33S AND 32P. REPAIRED SKIN DISBOND IAW EO8-53-12-0282.

Part: WIRE — LOOSE (CONNECTOR) · airframe 58,131 hrs · 64,867 cycles

ROLL SPOILER INBD HYD CAUTION LIGHT ILLUMINATED IN FLIGHT. REPLACED CONNECTOR ON INBD ROLL SPOILER HYD PRESSURE SWITCH IN NR 1 NACELLE. GROUND RAN ACFT. COULD NOT DUPLICATE ON GROUND IAW -8 WIRING MM 27-19-01 AND MM 33-12-00. ALSO FOUND LOOSE WIRE AT CONNECTOR. REINSTALLED WIRE IN CONNECTOR. RAN ACFT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: RELAY — FAILED (FIRE DETECTION) · airframe 57,851 hrs · 64,542 cycles

APU FAILED AFTER RUNNING APPROX.30 MINUTES, FAULT LIGHT CAME ON FOLLOWED BY CHECK FIRE DETECT LIGHT COMING ON. APU FIRE DETECTION SYS DEACTIVATED IAW S/P APPENDIX 1 26-6. R & R RELAY 2449-K26. RAN APU. OPS CHECKED GOOD AT THIS TIME.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 57,240 hrs · 63,843 cycles

AFT EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 9. R & R LAMP MODULE. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,411 hrs · 62,901 cycles

ROW 4 WALL EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED ROW 4 SIDEWALL EMERGENCY LIGHTS. OPS CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 55,894 hrs · 62,311 cycles

LEFT AFT EMERGENCY EGRESS LIGHT INOP. R & R BULB, PN 81. NO FIX. R & R EMERGENCY LIGHT BATTERY AT POSITION PS3. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 55,853 hrs · 62,265 cycles

ROW 9 EMERGENCY FLOOR ESCAPE PATH LIGHT INOP. R & R BULB, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,996 hrs · 61,323 cycles

EMERGENCY FLOOR PATH LIGHT IS INOP AT ROW 1. R & R MARKER AS REQUIRED, OPS CHECKED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,704 hrs · 61,000 cycles

ROW 4DF AND 4AC EMERGENCY EXIT LIGHTS HAVE 1 BULB INOP. R & R BULB IN ROW 4 EMERGENCY EXIT LIGHTS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,937 hrs · 72,316 cycles

EMERGENCY LIGHT BULB IN OP ON ROW 4A SIDEWALL. R & R LIGHT BULB IAW 33-51-00.

Part: WIRE — CHAFED (CABIN) · airframe 53,046 hrs · 59,076 cycles

EMERGENCY LIGHT INOP AT ROW 4AC AT SIDEWALL. REMOVED AND REPLACED EMERGENCY BATTERY IN ACCORDANCE WITH 33-50-05. NO FIX. FOUND CHAFED WIRE ON EMERGENCY EXIT LIGHT AT THRESHOLD ON ROW 4AC, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,019 hrs · 59,040 cycles

SIDEWALL EMERGENCY LIGHT AT ROW 1DF HAVE SEVERAL BURNT BULBS. REMOVED AND REPLACED BULBS AS REQUIRED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,019 hrs · 59,040 cycles

EMERGENCY FLOOR LIGHT AT ROW 7 INOP. REMOVED AND REPLACED BULB AS REQUIRED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,944 hrs · 58,952 cycles

EMERGENCY FLOOR PATH LIGHT IS INOP AT SEAT 4DF. REMOVED AND REPLACED EMERGENCY FLOOR PATH LIGHT LAMP AT SEAT 4DF AND CLOSED ACCESS PANEL.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYS) · airframe 52,879 hrs · 58,881 cycles

WEATHER RADAR BEGAN SPIKING AFTER TAKEOFF FOLLOWED BY TEXT FLIGHT MESSAGE. ALSO HAD STAB OFF MESSAGE. ACFT RETURNED TO THE FIELD. R & R RADAR R/T IAW MM 34-41-02, OPS CHECKED GOOD. OK FOR SERVICE.

Part: WARNING HORN — ACTIVATED · airframe 52,788 hrs · 58,779 cycles

DURING TAKEOFF ROLL AT 60 PERCENT TORQUE WARNING HORN SOUNDED, AUTO FEATHER ARM LIGHT DID NOT ILLUMINATE TILL 65 PERCENT. HORN CONTINUED TO SOUND, TAKEOFF WAS ABORTED. ALL OTHER PARAMETERS WERE WITHIN TAKEOFF SETTINGS. PERFORMED AUTO FEATHER TEST OPERATIONAL CHECKED GOOD IN ACCORDANCE WITH MM. COMPLIED WITH WORKCARD 31-50 00Q. TAKEOFF WARNING SYSTEM OPS CHECKED GOOD. PERFORMED HIGH SPEED TAXI WITH CREW AND COULD NOT DUPLICATE. CHECKED GOOD FOR SERVICE.

Part: UNKNOWN — ODOR (APU) · airframe 51,443 hrs · 57,304 cycles

THE APU BLEEDS WERE TURNED ON AND A ODOR OF FUEL CAME THROUGH CABIN. MX WAS NOTIFIED AND COULD NOT DUPLICATE THE PROBLEM. THERE WAS NO STANDING FUEL IN THE APU HOLE.

Part: FAN — OVERHEATED (E&E BAY) · airframe 50,762 hrs · 56,554 cycles

CAPTAINS ADVISORY DISPLAY COOLING FAN OVERHEATED. REMOVED AND REPLACED OF AVIONICS COOLING FAN.

Part: RECEPTACLE — BROKEN (POWER SUPPLY) · airframe 50,709 hrs · 56,492 cycles

UPON INSPECTION IN SBY, FOUND EMERGENCY LIGHT POWER SUPPLY AT ROW 7AC HAD A BROKEN CAMLOCK RECEPTACLE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD.

Part: ENGINE — POWER LOSS (NR 1) · airframe 50,445 hrs · 56,197 cycles

ON CLIMBOUT AT 500 FEET THE NR 1 ENGINE TORQUE DECREASED TO 50 WITH ASSOCIATED NR 1 ENGINE AUTO FEATHER AND THE NR 1 PROPELLER WENT TO 200 RPM. THE NR 1 ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED TO MDT. THE FLIGHT LANDED WITHOUT INCIDENT. NO REPORTS OF ANY PASSENGER ISSUES.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,003 hrs · 53,442 cycles

DURING ROUTINE POST FLIGHT, THE RIGHT HAND AFT EMERGENCY EGRESS LIGHT AND ONE OF THE CENTER CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHANGED THE ROW 7DF EMERGENCY LIGHT BATTERY PACK (3351-PS4). SYSTEM OPS CHECKS WERE GOOD.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 47,620 hrs · 53,023 cycles

DURING CRUISE FLIGHT, CREW NOTED THAT ISO VALVE CAUTION LIGHT ILLUMINATED. HYDRAULIC QUANTITY OF NR 1 SYSTEM HAD DROPPED TO 1 QUART. CREW ADVISED MAINTENANCE CONTROL AND DECISION WAS MADE TO DIVERT TO MDT. AIRCRAFT LANDED WITH 0 DEGREE FLAP SETTING, TAXIED TO RAMP AREA AND WAS THEN TOWED TO GATE. MAINTENANCE DISCOVERED PROBLEM WITH NR 1 ENGINE DRIVEN HYDRAULIC PUMP AND REPLACED THAT UNIT. OPS AND LEAK CHECKED PUMP IAW MM PROCEDURES. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — MISRIGGED (NR 1 NACELLE) · airframe 47,297 hrs · 52,666 cycles

LEFT MAIN GEAR DOOR AMBER LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION, CYCLED GEAR AND LIGHT ILLUMINATED AGAIN. RETURNED TO FIELD. FOUND LEFT MAIN GEAR FORWARD DOOR (CODE 07) FAULTED. CLEANED AND ADJUSTED SENSOR PER DASH 8 MAINTENANCE MANUAL. CYCLED GEAR 10 TIMES, OPS CHECK GOOD.

Part: STRINGER SPLICE — CORRODED (BS 531 S32R) · airframe 47,054 hrs · 52,393 cycles

CORROSION FOUND ON SPLICE STRINGER 32 RIGHT SIDE AT STA 531. SPLICE STRINGER 32 RIGHT AT 531 REPLACED WITH NEW PART LOCALLY MADE AS PER DWG 85300129 AND INSTALLED.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 47,054 hrs · 52,393 cycles

SEVERE CORROSION FOUND ON LOWER AFT PAX DOOR BRACKET (INBOARD). LOWER AFT PAX DOOR BRACKET I/B REPLACED WITH NEW PART INSTALLED WITH BOLT IAW AMM 20-14-01.

Part: INDICATOR — INOPERATIVE (WX RADAR SYS) · airframe 43,845 hrs · 48,906 cycles

WEATHER RADAR WILL NOT PAINT. REPLACED WEATHER RADAR INDICATOR. PART INFORMATION TO FOLLOW.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYS) · airframe 43,845 hrs · 48,906 cycles

WEATHER RADAR WILL NOT PAINT. REMOVED AND REPLACED RADAR R/T.

Part: LIGHT — MALFUNCTIONED (MLG) · airframe 43,788 hrs · 48,836 cycles

LANDING GEAR WAS SELECTED UP ALL GEAR HANDLE LIGHTS EXTINGUISHED. THREE SECONDS LATER RIGHT GEAR DOOR AMBER LIGHT ILLUMINATED. CREW CONFIRMED AFT GEAR DOORS OPENED/CYCLED.

Part: WIRE HARNESS — SHORTED (NR 2 ENGINE) · airframe 43,196 hrs · 48,174 cycles

NR 2 FAILED IN FLIGHT. REMOVED AND REPLACED ENGINE HARNESS.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,812 hrs · 46,661 cycles

A 6 INCH CRACK, 1.5 INCH CRACK DOUBLER SEPARATION AND NUMEROUS AREAS OF SURFACE CORROSION ON BELLY SKIN. REMOVED AND REPLACED SKIN PANEL.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,812 hrs · 46,661 cycles

SKIN PANEL DISBOND FOUND DURING C-CHECK INSPECTION. CORROSION BETWEEN WAFFLE DOUBLER AND SKIN PANEL. PANEL DISTORTED AROUND RIVET ROWS AND RIVETS FAILED (HEADS MISSING). VERIFIED DISBOND USING ULTRASOUND. DISBOND OF PANEL IS BETWEEN X123 AND X167, STR 32S AND 30P. REMOVE AND REPLACE ENTIRE SKIN PANEL.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,812 hrs · 46,661 cycles

A 6 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMINATING FROM PRESSURIZATION DRAIN AFT. PERFORMING ULTRASOUND INSPECTION VERIFIED NUMEROUS AREAS OF DISBOND/CORROSION BETWEEN WAFFLE DOUBLER AND SKIN PANEL. DAMAGED AREA FROM X425 TO X445 STRINGER 30P TO 31S. REMOVED AND REPLACED SKIN PANEL.

Part: SELECTOR PANEL — INTERMITTENT (MLG) · airframe 42,062 hrs · 46,815 cycles

ON FINAL APPROACH, GEAR WOULD NOT EXTEND ON GO AROUND GEAR EXTENDED NORMAL. REPLACED LANDING GEAR HANDLE EVALUATION FLIGHT SATISFACTORY.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 38,225 hrs · 42,758 cycles

AFTER STBY HYD PUMP SELECTED ON, NR 1 STBY HYD PUMP CAUTION LIGHT ILLUMINATED. FOLLOWING NR 1 ENG S/D WHILE TAXI TO GATE , NORMAL BRAKES WHERE NOT AVAILABLE.

Part: FUSE — BROKEN (NLG) · airframe 38,119 hrs · 42,647 cycles

UPON GEAR RETRACTION THE NOSE GEAR FAILED TO RETRACT AND MAIN GEAR DOORS REMAINED OPEN. THE NOSE GEAR RED UNSAFE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD. FOUND STEERING FUSE BROKEN AND CABLE SUPPORT BROKEN DUE TO OVER STEERING. PERFORMED TOWING FUSE BREAKAGE INSPECTION PER MM 32-50-00. REPAIRED AND REPLACED DAMAGED PARTS AS NECESSARY.

Part: PUSHROD — STRIPPED (RUDDER) · airframe 31,364 hrs · 35,380 cycles

DURING INSPECTION, THE LOWER RUDDER RADIUS ROD FORWARD ROD END WAS FOUND LOOSE. THE THREADED PORTION OF THE PUSH ROD THREADS WERE FOUND STRIPPED AND CHAFED INTO THE ROD.

Part: BATTERY — DISCHARGED (CABIN)

LEFT AFT EMERGENCY EGRESS LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY 3351-P5.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT)

HPN - FLT 3260 - AFT CEILING AISLE DOWN EMERGENCY LIGHT AND EMERGENCY EXIT SIGN AT ROW 4 INOP. RECYCLED CB L-1 (EMERGENCY LIGHTS CONTROL). OPS CHECK GOOD. (M)

Part: SWITCH — DIRTY (AUTOFEATHER SYST)

FLT 3023 - BWI-DCA - DURING TAKEOFF ROLL, AUTOFEATHER FAILED TO ARM. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. CYCLED POWER LEVERS, CLEANED AND INSPECTED AUTOFEATHER MICROSWITCHES. PERFORMED AUTOFEATHER SYSTEM AND POWER UPTRIM CHECK. OPS CHECK GOOD. (M)

Part: HYD FLEX LINE — LEAKING (NR 2 HYD SYSTEM)

FLT 3154 - BWI-GSO - DURING FLIGHT, THE NR 2 SYSTEM HYDRAULIC FLUID QUANTITY BEGAN DROPPING. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO BWI, LANDING WITHOUT INCIDENT. FOUND THE PRESSURE LINE TO INBOARD GROUND SPOILER ACTUATOR LEAKING. INSTALLED A TEMPORARY FLEX LINE TO THE RIGHT INBOARD GROUND SPOILER FROM THE CENTER WING AREA. (M)