N326EN

Part: LAMP — EXPOSED (EMERGENCY LIGHT) · airframe 51,773 hrs · 59,910 cycles

PDIS 326 33-51 1550503 03DEC17 CLT CLOSE FLOOR LEVEL EMERGENCY EXIT LIGHTING HAS EXPOSED LAMP IN ROW 2, AND MULTIPLE BULBS INOP. 69013 00 MM FACT 03DEC17 11:20 CLT RELAMPED INOP BULB AND REPLACED BULB COVER AT ROW 2 AS REQUIRED. OPS CHECK GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,431 hrs · 59,449 cycles

6TH AND 7TH EMERGENCY LIGHTS INOPERATIVE. R & R THE BULBS.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 51,350 hrs · 59,337 cycles

AUTOFEATHER FAILED TO ARM DURING TAKEOFF ROLL. AUTOFEATHER SYSTEM, INSPECTED THE SWITCHES ON CONTROL CONSOLE. NO FAULTS FOUND. GROUND RAN ACFT IAW MANUAL. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: WHEEL — UNKNOWN (NR 2 MLG) · airframe 51,228 hrs · 59,175 cycles

NR 2 MLG WHEEL STOPPED SPINNING IMMEDIATELY AFTER TAKEOFF AND ON LANDING SMOKE WAS COMING FROM BRAKE AREAS REPORTED BY A PASSENGER. JACKED THE RIGHT MLG AND INSPECTED FOR DEFECTS. NONE FOUND. NOTED NEW BRAKES INSTALLED IN NR 3 POSITION. AIRCRAFT OK FOR SERVICE.

Part: TERMINAL — DAMAGED (EMERGENCY LIGHT) · airframe 50,808 hrs · 58,622 cycles

EMERGENCY LIGHT NR 4 FROM FWD DAMAGED. REPLACED THE TERMINAL SPLICE, OPS CHECKED GOOD.

Part: CONTROL BOX — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 47,857 hrs · 69,701 cycles

AUTOFEATHER WILL NOT ARM WITH ENGINES RUNNING. SLAVED IN AUTO CONTROL BOX NO FIX. RECONNECTED ORIGINAL AUTO FX CONTROL BOX. RAN ACFT & CHECKED ARMING LEVEL GRAPH FOR AUTO FX AT 20 DEG C. AUTO FX WILL NOT ARM BELOW 32 DEGREES. SYS OPS CHECKED GOOD, OK ON GND RUN, OK FOR SERVICE.

Part: AHRS — FALSE INDICATION (COCKPIT) · airframe 50,628 hrs · 58,384 cycles

DURING TAXI, AHRS DATA INVALID MESSAGE FOLLOWED BY ADI ROLL MISMATCH AND THEN CAPTAIN`S ADI ROLLED. PERFORMED AHRS OPERATIONAL CHECK, OPS CHECKED GOOD. OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 505,985 hrs · 58,336 cycles

EMERGENCY LIGHT INOPERATIVE. FOUND AND REPAIRED A BROKEN WIRE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,308 hrs · 57,961 cycles

FLOOR EMERGENCY LIGHT IS INOPERATIVE AT ROW 5D. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: BRUSH BLOCK — DIRTY (PROP HEAT) · airframe 49,759 hrs · 57,260 cycles

EMERGENCY LIGHTS FLICKERING, WHEN PROPELLER HEAT NR 2 A PHASE SELECTED AT 1050 RPM. INSPECTED AND CLEANED BRUSH BLOCK CONNECTOR AND SLIP RINGS WITH NO DEFECTS NOTED. REMOVED AND REPLACED THE NR 1 BRUSH BLOCK IAW MM 61-10-11. GROUND RAN AIRCRAFT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,541 hrs · 56,987 cycles

MOST AFT CABIN FLOOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: LENS — JAMMED (LIGHT SWITCH) · airframe 49,443 hrs · 56,874 cycles

F/A EMERGENCY LIGHT SWITCH DIFFICULT TO ACTIVATE, DEACTIVATE. R & R F/A EMERGENCY LIGHT LENS COVER IAW 33-51-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 49,120 hrs · 56,453 cycles

BURNING RUBBER ODOR IN AIRCRAFT WITH APU AND ENGINE BLEEDS ON-LINE. INSPECTED FOR DEFECTS, NONE NOTED AT THIS TIME. GROUND RAN ENGINES AND APU. NO ODOR DETECTED. SYSTEM OPS NORMAL. OK FOR SERVICE.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 49,204 hrs · 56,562 cycles

FA REPORTED A STRONG ODOR AFTER TAKE OFF IN CABIN ROW 3. R & R SIDEWALL LIGHT BALLAST IAW AMM 33-21-02, OPS CHECKED GOOD.

Part: LIGHT — DIM (CABIN) · airframe 48,958 hrs · 56,232 cycles

CABIN LOWER SIDEWALL EMERGENCY LIGHT DIM AT 11AC. R & R LIGHT BULBS ON EMERGENCY EXIT SIGN AT 11AC. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,666 hrs · 55,849 cycles

EMERGENCY LIGHT INOPERATIVE. R & R BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,666 hrs · 55,849 cycles

EMERGENCY LIGHT INOPERATIVE. R & R THE BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,588 hrs · 55,749 cycles

EMERGENCY LIGHT INOPERATIVE AT 10DF SECOND RED LT. R & R BULB.

Part: BULB — INOPERATIVE (LIGHT SWITCH) · airframe 48,402 hrs · 55,501 cycles

CABIN EMERGENCY LIGHT PUSH SWITCH BACK LIGHT IS INOPERATIVE. REMOVED SWITCH COVER, R & R BULB. OPS CHECKED GOOD. REINSTALLED COVER.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 48,212 hrs · 55,249 cycles

AFT EMERGENCY FLOOR EGRESS, RED LIGHT INOPERATIVE. REPLACED THE LAMP. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,160 hrs · 55,184 cycles

FLOOR EMERGENCY LIGHT IS OUT AT ROW 6DF. R & R BULBS AT ROW 6DF. OPS CHECKED GOOD.

Part: AMPLIFIER — FAILED (PA SYSTEM) · airframe 47,949 hrs · 54,907 cycles

ELECTRICAL ODOR FORWARD CABIN AT F/A STATION. R & R PA AMP IAW MM 23-30-01. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,795 hrs · 54,705 cycles

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

Part: WIRE — BROKEN (SPOILERS) · airframe 47,629 hrs · 54,496 cycles

ON TAKEOFF ROLL, SPOILER PUSH OFF LIGHT FLICKERED. R & R BROKEN WIRE AT QUADRANT SWITCH. OPS CHECKED GOOD.

Part: SWITCH — FAILED (NR 1 SPOILER) · airframe 47,582 hrs · 54,431 cycles

NR 1 SPOILER CAUTION LIGHT PUSH OFF ILLUMINATED PRIOR TO TAKEOFF. INSPECTED WIRING AT LT AND RT SPOILER CLUTCH QUADRANT. R & R THE RT SWITCH IAW MM 27-62 01 AND MM 27-14-36. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,354 hrs · 54,145 cycles

LEFT AFT MOST EXTERIOR EMERGENCY LIGHT IS DIM. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,354 hrs · 54,145 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,832 hrs · 53,453 cycles

ROW 11 EMERGENCY LIGHT IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,733 hrs · 53,317 cycles

NORMAL GREEN LIGHT ON F/A EMERGENCY LIGHT BUTTON IS INOPERATIVE. R & R BULB FOR EMERGENCY LIGHT SWITCH ON F/A PANEL. OPS CHECKED GOOD.

Part: WINDOW — FAILED (COCKPIT) · airframe 46,650 hrs · 53,209 cycles

LEFT SIDE WINDOW SHATTERED IN FLIGHT AT AROUND 6000 FT. WINDOW HEAT WAS SELECTED ON AND NO OBVIOUS SPIKES IN PRESSURIZATION. 27097 00 CMG FACT 16MAY15, 13:02 CHO. R & R WINDOW IAW W/C 56-00-01R. OPS AND LEAK CHECKED GOOD.

Part: LATCH — WORN (NR 2 NACELLE) · airframe 46,602 hrs · 53,151 cycles

HOLE WORN IN GULLWING DOOR AT LOWER AFT LATCH IN NR 2 NACELLE. REPAIRED GULLWING DOOR IAW EO8-1-15-0079.

Part: STRUCTURE — CHAFED (NR 1 NACELLE) · airframe 46,602 hrs · 53,151 cycles

INBD GULLWING DOOR HAS CHAFE AT BOTTOM EDGE MEMBER INSIDE ABOUT 18.5" FWD OF AFT EDGE OF DOOR FOR NR 1 NACELLE. REPAIRED NR 1 INBD GULLWING DOOR IAW EO8-71-15-0088. COMPLIED WITH HFEC INSPECTION. NO FURTHER DEFECTS NOTED.

Part: MOUNT — CRACKED (TCAS ANTENNA) · airframe 46,602 hrs · 53,151 cycles

TCAS ANTENNA, INSIDE COVER CRACKED AT BOLT HOLES. REMOVED TCAS ANTENNA MOUNTING PLATE. REMOVED DOUBLER BELOW FUSELAGE FOR TCAS ANTENNA. INSTALLED REPAIR DOUBLER IAW EO8-53-15-0094 AND EA15-2015-031A.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,486 hrs · 53,004 cycles

FLOOR EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 1DF AND 13DF. R & R POWER SUPPLY AT PS4 POSITION IAW 33-51-00 AND 33-00-15.

Part: SENSOR — MALFUNCTIONED (STANDBY) · airframe 46,453 hrs · 52,962 cycles

MASTER CAUTION LIGHT ILLUMINATED WHEN TAKEOFF POWER WAS APPLIED. CREW WAS UNABLE TO CANCEL. NO ASSOCIATED CAUTION LIGHTS ILLUMINATED WITH PTR SWITCH. SWAPPED NR 2 STANDBY PUMP SENSOR IAW SP 29.5. OPS CHECKED GOOD AT THIS TIME.

Part: STIFFENER — CRACKED (RUDDER) · airframe 46,315 hrs · 52,790 cycles

STIFFENER ABOVE RIB 26 IS CRACKED ON FORE RUDDER. R & R STIFFENER , INSTALLED NEW STIFFENER WITH SAME TYPE AND MS20470AD3, RIVETS.

Part: STRUCTURE — CRACKED (RUDDER) · airframe 46,315 hrs · 52,790 cycles

LEFT SIDE FORE RUDDER HAS A CRACK APPROXIMATELY 1.25" IN LENGTH, AT TOP RIB 1 FWD OF REAR SPAR. REPAIRED IAW EO8-55-15-0028.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,315 hrs · 52,790 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 11. R & R BULB . OPS CHECKED GOOD.

Part: PCU — FAILED (NR 1 PROPELLER) · airframe 46,304 hrs · 52,775 cycles

NR 1 PROPELLER RPM DROPPED TO 1188 AFTER TAKEOFF. R & R NR 1 ENGINE PCU IAW WC 61-10-10. OPS AND LEAKED CHECKED GOOD.

Part: FIRE BOTTLE — NO TEST · airframe 46,096 hrs · 52,490 cycles

BOTH FORWARD ENGINE FIRE BOTTLES WILL NOT TEST. GAUGE READS ZERO ON FORWARD BOTTLE. MISSING YELLOW DISCHARGE DISC. R & R FIRE BOTTLE AND FORWARD SQUIB IAW WORK CARD 26-20-05X, 26-20-04F AND 26-20-22X. OPS CHECKED GOOD, OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,936 hrs · 52,279 cycles

FIRST 2 RED EMERGENCY FLOOR PATH LIGHTS WILL NOT ILLUMINATED. R & R EMERGENCY BATTERY PACK 33-52-PS2 IAW 33-51-05.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 45,823 hrs · 52,203 cycles

FORWARD RED EMERGENCY LIGHTS ARE INOPERATIVE. INSPECTED AND FOUND CONNECTOR LOOSE. SECURED THE CONNECTOR. OPS CHECKED GOOD.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 45,490 hrs · 51,691 cycles

AUTOFEATHER WILL NOT ARM ON TAKEOFF ROLL. PERFORMED WORK CARD 61-21-04. AUTOFEATHER CONTROL ENABLE ON CHECK. NO DEFECTS NOTED.

Part: LENS — DETACHED (COCKPIT) · airframe 45,489 hrs · 51,691 cycles

DC BUSS CAUTION LIGHT LENS FELL OUT. RESECURED LENS, OK FOR SERVICE.

Part: LINE — RUPTURED (HYD SYSTEM) · airframe 45,396 hrs · 51,575 cycles

AFTER GEAR RETRACTION, NR 2 RUDDER ISOLATION VALVE CAUTION LIGHT ILLUMINATED. RETURNED TO FIELD, NR 2 HYD QTY AT 1 QUART. R & R RUPTURED LINE IAW 32-36-00 WITH TEMP FLEX LINE, SWUNG GEAR IAW 32-30-00. LEAKED CHECKED GOOD AT NR 1 MLG RETRACTION ACTUATOR UP LINE. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,355 hrs · 51,522 cycles

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

Part: BULB — INOPERATIVE (AUTOFEATHER) · airframe 45,292 hrs · 51,430 cycles

AUTO FEATHER SELECT LIGHT IS INOPERATIVE, WILL NOT RESET. R & R BULB. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,270 hrs · 51,400 cycles

EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 4. R & R BULB FOR CEILING LIGHT AT ROW 4. OPS CHECKED GOOD.

Part: ANTENNA — FAILED (WX RADAR SYS) · airframe 45,229 hrs · 51,342 cycles

WEATHER RADAR WILL NOT COME OUT OF STANDBY. R & R RADAR ANTENNA IAW 34-41-01. OPS CHECKED GOOD AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,202 hrs · 51,303 cycles

THREE RED EMERGENCY FLOOR PATH LIGHTS ARE INOPERATIVE BETWEEN ROW 1 AND 2. REPLACED THE LAMPS IN EMERGENCY FLOOR PATH LIGHTS BETWEEN ROW 1 AND 2. OPS CHECKED GOOD. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (ROW 1) · airframe 44,936 hrs · 50,926 cycles

INOPERATIVE FLOOR EMERGENCY LIGHT IN ROW 1AC, & 1DF. R & R LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,936 hrs · 50,936 cycles

SEVERAL INOPERATIVE LAMPS IN EMERGENCY EXITS SIGNS. R & R LAMPS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,309 hrs · 50,130 cycles

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

Part: PUMP — FAILED (HYD SYSTEM) · airframe 43,981 hrs · 49,708 cycles

NR 2 ENGINE HYD PUMP CAUTION LIGHT ILLUMINATED IN FLIGHT WITH LOSS OF HYD QTY, CREW REPORTED NR 2 QTY AT ZERO ON GROUND. FOUND LINE AT PRESSURE MANIFOLD BROKEN, R & R LINE AND ENGINE. ENGINE HYD PUMP AND CASE DRAIN FILTER IAW WC 29-12-03R, 29-00-00 AND 72,00-04L AND OPS AND LEAKED CHECKED GOOD. SERVICE AND BLED HYD SYSTEM IAW 12-10-29.

Part: SOLENOID VALVE — LEAKING (HYD SYSTEM) · airframe 43,945 hrs · 49,662 cycles

LOSS OF NR 2 HYD QTY IN FLIGHT WITH ISOLATION VALVE CAUTION LIGHT ILLUMINATING. INSPECTED NR 2 SYS FOR HYD LEAK. FOUND UNLOADING SOLENOID VALVE ON NR 2 SIDE LEAKING. R & R VALVE IAW CMM 27-58-31 AND MM 27-14-11. GROUND RAN ACFT. OPS CHECKED GOOD. LEAKED CHECKED GOOD. SERVICE HYD SYSTEM AS REQUIRED. OK FOR SERVICE.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 43,886 hrs · 49,585 cycles

EMERGENCY LIGHT IS DIM AT ROW 12. R & R BULB. OPS CHECKED GOOD.

Part: BRAKE ASSY — FAILED (MLG) · airframe 43,565 hrs · 49,182 cycles

DURING TAXI OUT, NR 3 WHEEL BEARING FAILED. NR 2 HYDRAULICS DROPPED TO ZERO, BOTH PRESSURE AND QTY NR 2 ENGINE RAN WITH ZERO PRESSURE AND QTY FOR APPROX 10 MINUTES. INSPECTED NR 2 MLG AND FOUND NR 3 BRAKE BLEEDER PORT DAMAGE AND NR 3 MAIN WHEEL ASSEMBLY DAMAGED. R & R NR 3 MAIN WHEEL ASSY AND BRAKE ASSY. SERVICED NR 2 HYD SYSTEM IAW 32-41-11 AND 32-42-11 AND 12-10-29.

Part: UNKNOWN — ODOR (CABIN) · airframe 47,273 hrs · 55,001 cycles

PLASTIC BURNING ODOR EMITTING IN FORWARD CABIN AREA. INSPECTED ACFT WITH NO DEFECTS OR ODOR NOTED. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 42,538 hrs · 47,841 cycles

ELECTRICAL BURNING PDPR IN AFT CABIN NEAR ROW 8-11. DEACTIVATED CABIN OVERHEAD LIGHTS BY PULLING AND COLLARING CIRCUIT BREAKERS S1, S2 AND R2. COMPLIED WITH SPECIAL PROCEDURE 33.1 FOR CABIN INTERIOR NORMAL LIGHTING SYS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,187 hrs · 47,387 cycles

EMERGENCY LAMPS ARE INOPERATIVE AT KNEE LEVEL IN ROW 11AC. R & R BULB IAW MM 33-51-00. OPS CHECKED GOOD.

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 42,088 hrs · 47,243 cycles

EMERGENCY LIGHTS STAY ON IN THE ARM POSITION. R & R EMERGENCY LIGHT CONTROL BOX. OPS CHECKED GOOD IAW MM 33-51-05.

Part: DOOR — MISSING (LT MLG) · airframe 42,057 hrs · 47,203 cycles

LEFT MAIN GEAR CENTER DOOR MISSING. INSTALLED LT MLG DOOR IAW MM 32-10-21. OPS CHECKED GOOD. SWUNG GEAR SEVERAL TIMES. NO DEFECTS NOTED.

Part: RADAR — MALFUNCTIONED (WX RADAR SYS) · airframe 42,042 hrs · 47,185 cycles

WEATHER RADAR MALFUNCTIONED IN FLIGHT. R & R RADAR ANTENNA ASSY AND RADAR R/T IAW AMM 34-41-01. OPS CHECKED GOOD.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 41,909 hrs · 46,996 cycles

SURFACE CORROSION ON STRUCTURE AT PAX DOOR THRESHOLD. LIGHTLY BLENDED SMALL AREAS OF LIGHT CORROSION IAW SRM 51-20-11. ALODINED, PRIMED AREA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 41,909 hrs · 46,996 cycles

RIGHT CARGO TRACK HAS LIGHT CORSSION ON FLANGE. BLENDED CORRODED AREAS. FOUND CARGO TRACK TO BE OUT OF LIMITS IAW RD8-53-784. R & R RT CARGO TRACK IAW DWG 85330129.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 41,909 hrs · 46,996 cycles

LEFT CARGO TRACK HAS CORROSION ON FLANGE. BLENDED CORROSION, FOUND CARGO TRACK TO BE OUT OF LIMITS IAW RD8-53-784. FABRICATED NEW CARGO TRACK SPLICE IAW DWG 85330527. INSTALLED FASTENERS IN AFT SECTION OF CARGO TRACK IAW DWG 85330115.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 41,909 hrs · 46,996 cycles

LEFT INBD SEAT TRACK HAS CORROSION. BLENDED CORROSION. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW RD8-53-833. R & R LEFT INBD SEAT TRACK IAW DWG 85330028 AND RD8-53-4472.

Part: SILL — CORRODED (FUSELAGE) · airframe 41,909 hrs · 46,996 cycles

SURFACE CORROSION ON DOOR SILL AT GALLARY DOOR AREA. LIGHTLY BLENDED ON DOOR SILL. REMOVED TWO SMALL AREAS OF LIGHT CORROSION, ALODINED AND PRIMED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 41,495 hrs · 46,453 cycles

ROW 2 FLOOR LEVEL EMERGENCY LIGHTS IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD,

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 41,223 hrs · 46,101 cycles

ON ROWS 11DF AND 2DF SIDEWALL EMERGENCY LIGHTS ARE DIM. R & R BULBS AT ROWS 11DF AND 2DF SIDEWALL EMERGENCY LIGHTS. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 41,223 hrs · 46,101 cycles

THIRD RED EMERGENCY LIGHT AND 2ND ARROW EMERGENCY LIGHT IS INOPERATIVE. R & R BULB, AT 3RD RED AND 2ND ARROW FLOOR EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: UNKNOWN — SMOKE (MLG) · airframe 40,897 hrs · 45,664 cycles

SMOKE COMING FROM NR 1 MAIN WHEEL ASSY. INSPECTED NR 1 MAIN WHEEL ASSY AND BRAKE. NO DEFECTS NOTED. NO EVIDENCE OF OVERHEATING. TAXIED ACFT. NO DEFECTS NOTED AT THIS TIME.

Part: ANGLE — CRACKED (NACELLE FIREWALL) · airframe 40,415 hrs · 45,023 cycles

CRACK FOUND IN FIREWALL ANGLE ASSY. REMOVED FIREWALL ANGLE. INSTALLED AND DRILLED UP ANGLE, INSTALLED RIVETS, EXCEPT 2 LOWER RIVETS. INSTALLED LOWER 2 RIVETS.

Part: ANGLE — CRACKED (NR 1 NACELLE) · airframe 40,415 hrs · 45,023 cycles

CLOSING ANGLE IS CRACKED IN NR 1 NACELLE. REMOVED CLOSING ANGLE ON FIREWALL. DRILLED NEW ANGLE, INSTALLED NEW ANGLE, SEALED RIVET HEAD AND GAPS WITH SEALANT.

Part: FIREWALL — CRACKED (NACELLE) · airframe 40,415 hrs · 45,023 cycles

AFTER REMOVAL OF ANGLE 85410449-101, A CRACK WAS REVEALED IN FIREWALL. MEASURED 0.673" OTBD SIDE AT 1 O`CLOCK POSITION. REMOVED DAMAGE IAW RD8-54-430. EDDY CURRENT INSPECTED AND FOUND NO FURTHER CRACKS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW RD8-54-430.

Part: PSEU — FAILED (MLG) · airframe 39,886 hrs · 44,333 cycles

LANDING GEAR INOPERATIVE CAUTION LIGHT ON DURING GEAR RETRACTION. R & R PSEU IAW MM 32-61-50 AND COMPLIED WITH RETRACTION AND EXTENSION OPS CHECKS. CYCLED GEAR 6 TIMES. CHECKED GOOD.

Part: SMOKE DETECTOR — ACTIVATED (LAVATORY) · airframe 39,760 hrs · 44,155 cycles

LAVATORY SMOKE DETECTOR ACTIVATED WITH APU BLEED ON. NORMAL WITH OFF ENG BLEEDS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,280 hrs · 43,581 cycles

BULB OUT IN EXIT SIGN AT EMERGENCY EXIT DOOR AT ROW 11DF IS INOPERATIVE. R & R LAMP. OPS CHECKED GOOD.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 39,280 hrs · 43,581 cycles

SECOND FROM BOTTOM LAMP IN EXIT DOOR AT ROW 2DF IS INOPERATIVE. R & R LAMP IN LOWER EXIT SIGN AT ROW 2DF. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 39,244 hrs · 43,535 cycles

ON TAKEOFF ROLL, SMOKE WARNING LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. R & R NR 1 AND NR 2 BAG BAY SMOKED DETECTORS. OPS CHECKED SEVERAL TIMES. NORMAL, OK FOR SERVICE AT THIS TIME.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 38,999 hrs · 43,226 cycles

BULB IN F/A EMERGENCY LIGHT SWITCH IS INOPERATIVE. RELAMP BULB IN F/A EMERGENCY LIGHT SWITCH AS REQUIRED.

Part: PCU — FAILED (NR 2 ENGINE) · airframe 38,668 hrs · 42,808 cycles

NR 2 ENGINE SPOOLED DOWN DURING TAKEOFF ROLL. REJECTED TAKEOFF. PERFORMED ECU ON AND OFF, POWER RUN IAW RUN UP MANUAL WITH CREW. OK FOR SERVICE. NR2 ENGINE TORQUED SURGE BETWEEN 110 AND 75. PROP RPM REMAINED STEADY. TORQUE SURGE STOP WITH REDUCTION OF POWER. R & R PCU IAW WORKCARD 61-10-10R AND COMPLIED WITH RIGGING IAW H76-00-02Q. GROUND RUN AND OPS CHECKED GOOD. PERFORMED HIGH SPEED TAXI WITH NO DEFECTS NOTED AIRCRAFT OK FOR SERVICE.

Part: TIRE — FAILED (MLG) · airframe 42,579 hrs · 48,992 cycles

DURING HIGH SPEED TAXI, NR1 MAIN GEAR TIRE BLEW. R & R NR1 AND 2 MAIN WHEEL ASSY IAW 32-41-11. OK FOR SERVICE.

Part: SOCKET — MELTED (LIQUID WARMER) · airframe 37,813 hrs · 41,688 cycles

ELECTRIC SMELL IN AFT CABIN AREA. INSPECTED OVERHEAD LIGHTS IN CABIN, NO DEFECTS NOTED, FOUND SOCKET IN NR 1 LIQUID WARMER MELTED. R & R ASSOCIATED CIRCUIT BREAKER FOR THE WARMER.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,072 hrs · 40,730 cycles

EMERGENCY EXIT SIGN ON LT SIDE OF PAX DOOR HAS 1 INOPERATIVE LAMP. R & R BULB IN EMERGENCY EXIT SIGN. OPS CHECKED GOOD.

Part: WINDSHIELD — CRACKED (COKCPIT) · airframe 36,997 hrs · 40,637 cycles

F/O'S FRONT WINDSHIELD IS CRACKED. (CRACKED IN FLIGHT AT APPROX 3000 FT, WINDSHIELD HEAT IN WARMUP). R & R F/O'S WINDSHIELD IAW WC 56-00-00R, OPS CHECKED GOOD, OK FOR SERVICE.

Part: WARNING HORN — FALSE ACTIVATION · airframe 36,982 hrs · 40,616 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. CYCLED FLAPS, CONDITION LEVERS AND TRIM, OPS CHECKED GOOD. PERFORMED WC 31-50-03Q. OPS CHECKS ARE SATISFACTORY. CLEARED MEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,530 hrs · 40,030 cycles

EMERGENCY FLOOR PATH LIGHT AT ROW 2 IS INOP. RELAMPED EMERGENCY FLOOR PATH LIGHT AT SAID LOCATION, AD IAW AMM33-20-00.

Part: ANGLE — CRACKED (ZONE 600) · airframe 36,247 hrs · 39,677 cycles

(V0XR) RT AFT WING SPAR TO FUSELAGE CLOSING ANGLE CRACKED. R & R RT AFT WING SPAR ANGLE. W/C 2095

Part: ANGLE — CRACKED (ZONE 500) · airframe 36,247 hrs · 39,677 cycles

(V0XR) FWD WING SPAR TO FUSELAGE CLOSING ANGLE AT 4L TO 6L IS CRACKED. REMOVED AND REPLACED WING SPAR TO FUSELAGE CLOSING ANGLE. W/C 2092

Part: INTERCOSTAL — DAMAGED (ZONE 400) · airframe 36,247 hrs · 39,677 cycles

(V0XR) CHANNEL BEHIND SKIN ON LOWER FWD INBD CORNER OF NR1 NACELLE HAS BLOWN OUT HOLES. (APPROX .25) R & R DAMAGED INTERCOSTAL. W/C 4077

Part: ANGLE — CRACKED (ZONE 600) · airframe 36,247 hrs · 39,677 cycles

(V0XR) FWD WING SPAR TO FUSELAGE (CLOSING ANGLES). R & R FWD WING SPAR TO FUSELAGE, CLOSING ANGLES. W/C 2094

Part: ANGLE — CRACKED (ZONE 600) · airframe 36,247 hrs · 39,677 cycles

(V0XR) FWD WING SPAR TO FUSELAGE (CLOSING ANGLES) AT 4R-6R CRACKED. REMOVED AND REPLACED FWD WING SPAR TO FUSELAGE, CLOSING ANGLES. W/C 2093

Part: BRACKET — CRACKED (FUSELAGE) · airframe 36,247 hrs · 39,677 cycles

(V0XR) BRACKET OF FWD SIDE OF OTBD INTERCOSTAL IS CRACKED. REMOVED AND FABRICATED NEW BRACKET. W/C 4085

Part: SHROUD — CRACKED (ZONE 600) · airframe 36,247 hrs · 39,677 cycles

(V0XR) LARGE CRACK ON FINGERNAIL SHROUD/ EXHAUST OUTLET LOOKING AFT AT 10 O'CLOCK POSITION AND SMALL CRACK AT RIVET ROW 6. REPLACED FINGERNAIL SHROUD. W/C 4007

Part: ATTACH BRACKET — CRACKED (LT NACELLE) · airframe 36,247 hrs · 39,677 cycles

(V0XR) LT NACELLE INBD ATTACHMENT BRACKET IS CRACKED. R & R BRACKET. W/C 4071.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 36,247 hrs · 39,677 cycles

(V0XR) LT ELEVATOR INBD UPPER SKIN IS DAMAGED. BLENDED UPPER SKIN AREA, W/C 3034.

Part: BRACKET — CRACKED (RT NACELLE) · airframe 36,247 hrs · 39,677 cycles

(V0XR) RT NACELLE INBD ATTACHMENT BRACKET IS CRACKED. R & R BRACKET. W/C 4072.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 36,247 hrs · 39,677 cycles

(V0XR) RT ELEVATOR CTR HINGE AREA BOTTOM L/E INBD SKIN IS CRACKED. BLENDED HINGE AREA, W/C 3032.

Part: FLAP TRACK — CRACKED (ZONE 100) · airframe 36,247 hrs · 39,677 cycles

(V0XR) CRACK ON LT NR 2 FLAP TRACK. R & R FLAP TRACK. W/C 5042

Part: FLAP TRACK — CRACKED (ZONE 100) · airframe 36,247 hrs · 39,677 cycles

(V0XR) CRACK ON LT NR 1 FLAP TRACK. R & R FLAP TRACK. W/C 5038

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 36,247 hrs · 39,677 cycles

(V0XR) SIDE WALL SUPPORT BRACKET CRACKED AT STA X642 Z-20. R & R BRACKET. W/C 2051.

Part: ANGLE — CRACKED (ZONE 500) · airframe 36,247 hrs · 39,677 cycles

(V0XR) LT ANGLE ON LT FINGERNAIL CRACKED IN 2 PLACES UNDER RIVET HEADS. R & R ANGLE. W/C 4040

Part: DOOR FRAME — CRACKED (BS 607) · airframe 38,247 hrs · 39,677 cycles

(V0XR) FWD LOWER CARGO DOOR FRAME X.607.00 CRACKED. R & R LOWER CARGO FRAME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,021 hrs · 39,398 cycles

THE 4TH FLOOR EMERGENCY LIGHT FROM FRONT IS INOP (RED). RE-LAMPED BULB, OPS CHECKED GOOD.

Part: HOLDER — ODOR (CABIN LIGHTS) · airframe 35,851 hrs · 39,188 cycles

HOT ELECTRICAL ODOR AT ROW 10 A/C. REMOVED AND REPLACED LAMP HOLDER AND BALLAST IN ACCORDANCE WITH 33-00-00. CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,947 hrs · 45,717 cycles

FLOOR LEVEL EMERGENCY LIGHTS 1,2,4 AND7 ARE NOT WORKING. REMOVED FLOOR LENS COVER, REPLACED LAMPS AT SPECIFIED LOCATIONS AND RESECURED FLOOR LENS COVER. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,758 hrs · 39,075 cycles

EMERGENCY FLOOR PATH LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULB, OPERATIONAL CHECKED GOOD.

Part: CONNECTOR — FAILED (HYD PRESS XMITER) · airframe 45,267 hrs

NR 2 ENG HYD PUMP CAUTION LIGHT ILLUMINATED WITH NO MAIN PRESSURE, QUANTITY IS GOOD. R & R NR 2 PRESSURE TRANSMITTER CONNECTOR PLUG. GROUND RAN ,OPS CKD GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 34,268 hrs · 37,207 cycles

ODOR NOTED BY F/A DURING GEAR RETRACTION ONLY. INSPECTED UNDER CABIN FLOOR AND IN AND ABOVE COAT CLOSET. GROUND RAN. NO DEFECTS NOTED.

Part: LIGHT — LOOSE (CABIN) · airframe 34,240 hrs · 37,171 cycles

EMERGENCY LIGHT AT ROW 11 IS LOOSE FROM WALL. RESECURED LIGHT ASSY TO WALL AND OPS CK GOOD.

Part: PIPE — BROKEN (NR 2 ENGINE) · airframe 33,773 hrs · 36,545 cycles

NR 2 ENGINE HIGH ITT, 765 AT 85 PERCENT AND FUEL FLOW HIGHER THAN NR 1 ENGINE. FOUND Y-PIPE JUST AFT OF NR 2 HP VALVE BROKEN. REMOVED AND REPLACED Y-PIPE USING ORIGINAL HARDWARE AND CLAMPS, OPS & LEAK CHECK GOOD IN ACCORDANCE WITH 21-11-00 AND ALL ENGINE PARAMETERS WITHIN LIMITS.

Part: PLATE — CRACKED (RT WING) · airframe 33,224 hrs · 35,865 cycles

DURING C-CHECK INSP, A CRACK WAS FOUND IN THE FWD, INBD CORNER OF THE WING BOX LADDER PLATE UNDER STRESS PANEL 622AT. AN ENGINEERING ORDER WAS ISSUED REFERENCING RD8-57-4107 TO INCORPORATE RD8-57-2387 TO REPAIR THE LADDER PLATE. REPAIR WORK WAS THEN COMPLETED.

Part: PLATE — CRACKED (LT WING) · airframe 33,224 hrs · 35,865 cycles

DURING C-CHECK INSP, A CRACK WAS FOUND IN THE AFT OTBD CORNER OF THE WING BOX LADDER PLATE UNDER STRESS PANEL 522AT. AN EO WAS ISSUED REFERENCING RD8-57-4106 TO INCORPORATE RD8-57-2375 TO REPAIR THE LADDER PLATE. REPAIR WORK WAS THEN COMPLETED.

Part: PLATE — CRACKED (WING BOX)

DURING C-CHECK INSPECTIONS, A CRACK WAS FOUND IN THE AFT OTBD CORNER OF THE WING BOX LADDER PLATE UNDER STRESS PANEL. AN EO WAS ISSUED REF RD8-57-4106 TO INCORPORATE RD8-57-2375 TO REPAIR THE LADDER PLATE. REPAIR WORK WAS THEN COMPLETED. (K)

Part: SILL — CORRODED (FUSELAGE) · airframe 33,224 hrs · 35,865 cycles

DURING C-CHECK INSPECTIONS, CORROSION WAS FOUND ON THE LOWER DOOR SILL FOR THE AFT RT SERVICE DOOR. AREA OF CORROSION WAS CLEANED, ALODINE AND PRIMER APPLIED IAW DEHAVILLAND STRUCTURAL REPAIR MANUAL.

Part: LINK — BROKEN (NLG STEERING) · airframe 33,233 hrs · 35,864 cycles

IN PREPARATION FOR LANDING AT PHL THE FLIGHT CREW SELECTED THE GEAR DOWN AND THE NOSE GEAR INDICATOR WAS RED. THE MAIN GEAR INDICTED NORMAL. THE FLIGHT CREW DID THE ALTERNATE EXTENSION AND THE NOSE GEAR DID NOT COME DOWN. THE AIRCRAFT LANDED WITH THE NOSE STILL RETRACTED, , THERE WERE NO INJURES REPORTED. UPON INSPECTION, LINK ON THE STEERING ACTUATOR FOUND BROKEN. STEERING ACTUATOR AND LINKS REPLACED. ACFT FERRIED TO SBY. DURING INSPECTION AFTER A NOSE GEAR UP LANDING, THE FRAME MEMBER AT X167.5 WAS BUCKLED BETWEEN STRINGERS 32S AND 32P.FRAME MEMBER WAS REPLACED IAW DEHAVILLAND STRUCTURAL REPAIR MANUAL PROCEDURES. AIRCRAFT HAS NOT BEEN RELEASED YET DUE TO OTHER ONGOING WORK.

Part: BALLAST — FAILED (CABIN LIGHTS)

STRONG ELECTRICAL ODOR IN CABIN OVERHEAD ISLE BETWEEN ROWS 2 AND 4, OVERHEAD FLUORESCENT LIGHT FAILED. AIRCRAFT WAS ON GROUND. INSPECTED AREA AND FOUND OVERHEAD LIGHT AT 2DF SOCKET BURNED. INSTALLED NEW BULB, NO FIX. INSPECTED SOCKETS, REMOVED AND REPLACED BALLAST INSTALLED NEW BULB OPERATIONAL CHECK GOOD. REMOVED BALLAST, BR9000-21, CONFORMED WITH REQUIREMENTS OF AD 2006-17-10, AND SHUT POWER OFF TO THE LIGHT FIXTURE. (K)

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

RT AFT EMERGENCY LIGHT INOP. R&R D BULB NO FIX. R&R BATTERY 3351 PS4 ROW 12 RT SIDE IAW AMM 31-51-05. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

EMERGENCY EXIT SIGN BY MAIN CABIN DOOR HAS SEVERAL LAMPS INOP. REPLACED BURNT OUT LAMPS AND SECURED COVER. OPS CHECK GOOD.

Part: O-RING — LEAKING (ADAPTER)

NR 1 ENG OIL PRESSURE WARNING LIGHT ILLUMINATED IN FLIGHT ALONG WITH A NR 1 ENG OIL PRESSURE OF 40 PSI. SHUTDOWN NR 1 ENG PER CHECKLIST. AFTER LANDING FOUND OIL DRIPPING FROM BOTTOM OF NR 1 ENG. 00 ESP HISTORY: NONE. FACT 19AUG08 05:05 CHS, FOUND PCU AND ADAPTER LEAKING. REPLACED ALL O-RINGS AND REINSTALLED AND RIGGED PCU IAW WORKCARDS 61-1-0-10R AND 76-00-02Q AND COMPLIED WITH MM 05-50-00 (EXCLUDING PATCH CHECK). NO DEBRIS OR DEFECTS FOUND. GROUND RAN, ENG LEAK AND OPS CHECK GOOD. (S)

Part: LIGHT — UNSECURE (CABIN) · airframe 31,823 hrs · 34,135 cycles

CABIN AFT FLOOR EMERGENCY LIGHTS NOT SECURE. RESECURED LIGHTS AS REQUIRED.

Part: CONTACTOR — DAMAGED (START SYS) · airframe 31,266 hrs · 33,832 cycles

WHILE TAXIING IN EWN, NR 2 SIDE DC BUSS FAULTED AND THERE WAS SOME SMOKE ON NR 2 SIDE. THE SMOKE WAS FOUND TO BE COMING FROM THE APU. FOUND THE STARTER GENERATOR OVERHEATED AND APU START CONTACTOR WELDED. NO DAMAGE FOUND IN THE APU AREA. REPLACED THE START CONTACTOR K-62 AND INSPECTED WIRING, NO DEFECTS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 31,443 hrs · 33,684 cycles

BURNING SMELL DETECTED IN ACFT WITH BLEEDS ON, GND RAN ENG WITH BLEEDS SEL ON FULL HOT 20 MIN, CND.

Part: WIRE — LOOSE (WINDSCREEN) · airframe 31,235 hrs · 33,427 cycles

SMOKE COMING FROM F/O WINDSHIELD NEAR HEATER TERMINAL. MAINTENANCE INSPECTED WIRING AND FOUND A LOOSE WIRE ON THE FIRST OFFICERS WINDOW AT THE HEATER TERMINAL L2. WIRING INSPECTED FOR DAMAGE, NO DEFECTS NOTED. TIGHTENED CONNECTOR, OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,732 hrs · 31,597 cycles

F/A REPORTS EMERGENCY LIGHTS DO NOT WORK. REMOVED AND REPLACED EMERGENCY BATTERY PACKS.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 27,131 hrs · 28,370 cycles

LOST NUMBER 2 HYDRAULIC FLUID AFTER GEAR RETRACTION, SYSTEM WENT INTO ISOLATION, ONE QUART LEFT IN SYSTEM, PRESSURE NORMAL. REMOVED AND REPLACED THE BLUE FLEXIBLE UP LINE TO NOSE GEAR DRAG STRUT ACTUATOR, SERVICED AND BLED SYSTEM.

Part: LATCH — UNLATCHED (NACELLE) · airframe 27,045 hrs · 28,262 cycles

TWO INBOARD COWL LATCHES CAME LOOSE. INSPECTED AND SECURED LATCHES AS REQUIRED.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 24,636 hrs · 25,178 cycles

IN FLIGHT NR 2 HYDRAULIC SYSTEM WENT TO 1 QT AND NR 2 ISO VALVE CAUTION LIGHT ILLUMINATED. NO OTHER CAUTION LIGHTS AND QUANTITY REMAINED ABOVE 1QT. FLIGHT DIVERTED TO MDT WHERE IT WAS FOUND HYDRAULIC FLUID WAS LEAKING FROM BEHIND THE NR 2 NACELLE GRAVEL GUARD. LINES WERE CAPPED OFF AND AIRCRAFT WAS FERRIED TO SBY. INSTALLED HYDRAULIC LINE IN NR 2 NACELLE FOR GEAR DOOR DOWN PRESSURE AND REPLACED HYDRAULIC LINE IN NR 1 NACELLE FOR STAY STRUT ACTUATOR.

Part: SWITCH — INOPERATIVE (WARNING SYSTEM) · airframe 24,528 hrs · 25,052 cycles

ON CLIMB-OUT, BETA WARNING HORN SOUNDED. ALL ENGINE PARAMETERS NORMAL. DEACTIVATED SYSTEM. R&R MICRO SWITCH ACTUATOR AT M/S 3151-S9 IN CENTRAL COLLUM. OPS CHECK GOOD.

Part: DISPLAY — INOPERATIVE (WX RADAR SYS) · airframe 22,806 hrs · 22,883 cycles

WITH WEATHER RADAR ON, GRAPHICS AND WEATHER COMPRESS'S TOWARD CENTER OF RADAR SCREEN. RETURNED TO FIELD. REMOVED AND REPLACED INDICATOR, OPS CHECKED GOOD.

Part: COMPUTER — FAULTY (CABIN PRESSURE) · airframe 17,477 hrs · 15,914 cycles

AFTER TAKEOFF, WITH PRESSURIZATION CONTROL ON AUTO, AIRCRAFT STARTED TO PRESSURIZE OUT OF CONTROL, SELECTED TO DUMP POSITION. REPLACED PRESSURIZATION COMPUTER.

Part: CONTROL BOX — INOPERATIVE · airframe 16,435 hrs · 14,493 cycles

EMERGENCY LIGHTS ILLUMINATED IN FLIGHT. REPLACED EMERGENCY LIGHTS CONTROL BOX.

Part: ACTUATOR — LEAKING · airframe 16,349 hrs · 14,381 cycles

AIRCRAFT LOST MOST OF #2 HYDRAULIC SYSTEM FLUID. FOUND #2 MAIN LANDING GEAR DOORS AFT ACTUATOR LEAKING. REPLACED ACTUATOR.