N914DE

Part: COVER — UNSERVICEABLE (TAILCONE SLIDE) · airframe 57,661 hrs · 44,822 cycles

TAIL CONE SLIDE COVER IS NOT SERVICEABLE. REPLACED SLIDE COVER IAW AMDS WC 5350-4644.

Part: CABLE — CHAFED (TAILCONE) · airframe 57,661 hrs · 44,822 cycles

TAILCONE CABLE HAS AREA OF WEAR AND CHAFING. REPLACED THE CABLE.

Part: SLIDE — DETACHED (TAILCONE) · airframe 57,661 hrs · 44,822 cycles

TAILCONE SLIDE IS DETACHED FROM PACKAGING. INSTALLED SLIDE ON AMDS 5350-4644.

Part: SPAR — CRACKED (RT WING) · airframe 57,661 hrs · 44,822 cycles

RT WING AT STATION XRS 164 IS CRACKED AT APPROX 6:00 POSITION AT LOWER LUG, CRACK IS APPROX .250" LONG. RT WING AFT SPAR AT STA XRS164 REPAIRED BY DOUBLER INSTALLATION. ALL WORK ACCOMPLISHED AND RECORDED ON NR 22 AND PRI 551374-14AD REV 0, 1, 2, AND 3.

Part: DOOR — OUT OF ADJUST (O2 COMPARTMENT) · airframe 57,661 hrs · 44,822 cycles

FIRST CLASS LAV, OXYGEN COMPARTMENT DOOR BINDING DOES NOT FREELY DROP. ADJUSTED DOOR PER CMM 35-10-11. OPS CHECK GOOD.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 57,661 hrs · 44,822 cycles

NR 2 RT FLAP HINGE UPPER INBD AND LOWER INBD MOUNTING STUDS CORRODED. REPLACED THE HINGE FITTING AND UPPER & LOWER MOUNTING STUDS IAW AMDS 5710-01110-05B.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 57,390 hrs · 44,616 cycles

AFT OVERHEAD COCKPIT EMERGENCY LIGHTS INOPERATIVE. ATTEMPTED RELAMP. R & R BATTERY. OPS NORMAL, OK FOR SERVICE IAW AMM 33-53.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 57,120 hrs · 44,418 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 20DE INOPERATIVE. REPLACED THE WIRE HARNESS AND PIG TAIL AT SEAT 20DE IAW AMM 33-50. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,876 hrs · 44,234 cycles

LEFT AND RIGHT OVERWING EXIT DOORS AFT, OVERHEAD INTERIOR EXIT SIGN INOPERATIVE. INSTALLED NEW BATTERY IN BATTERY PACK FOR AFT OVERWING DOORS UPPER EXIT SIGNS. OPS CK OK. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,876 hrs · 44,234 cycles

RIGHT EXTERIOR OVERWING EXIT LIGHT INOPERATIVE. INSTALLED NEW BULB IN EXTERIOR OVERWING EXIT LIGHT. OPS CK OK. OK FOR SERVICE.

Part: APU — SMOKE · airframe 56,816 hrs · 44,191 cycles

PERFORMED ATB DUE TO REPORTED SMOKE IN CABIN ON CLIMB OUT. AN EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE APU AND PERFORMED PACK SYSTEM INSPECTION/CLEANING. A VERIFICATION FLIGHT WAS ACCOMPLISHED AND THE ACFT WAS RETURNED TO SERVICE.

Part: BOTTLE — LOW PRESSURE (ESCAPE SLIDE) · airframe 56,371 hrs · 43,889 cycles

THE CREW REPORTED THAT THE L1 EMERGENCY ESCAPE SLIDE PRESSURE WAS LOW. MAINTENANCE R & R THE L1 EMERGENCY EXCAPE SLIDE.

Part: DOOR FRAME — CRACKED (RT MLG) · airframe 55,992 hrs · 43,634 cycles

RIGHT WHEEL WELL FWD FRAME MLG DOOR JAMB HAS CRACK IN OTBD RADIUS 3" LONG. R & R FWD FRAME IAW DWG 5930584. COMPLETED INSTALLING FWD FRAME IAW DWG 5930584. INSTALLED RT MLG DOOR PROXIMITY SENSOR IAW AMM 32-60-05.

Part: DOOR FRAME — CRACKED (LT MLG) · airframe 55,992 hrs · 43,634 cycles

LEFT WHEEL WELL FWD FRAME MLG DOOR JAMB HAS CRACK IN OTBD RADIUS 3.5" LONG. REMOVED AND DRILLED NEW FWD FRAME IAW DWG 5930584. BEGAN INSTALLING FRAME IAW DWG 5930584. INSTALLED LT MLG DOOR PROXIMITY SENSOR IAW AMM 32-60-05. COMPLETED INSTALLING FWD FRAME IAW DWG 5930584.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 55,817 hrs · 43,503 cycles

MAINTENANCE FOUND AFT EXIT SIGN IN TAIL SECTION INOPERATIVE. A WIRE WAS REPAIRED AND SIGN CHECKED OK.

Part: CHANNEL — DAMAGED (LT WING TE FLAP) · airframe 59,274 hrs · 46,000 cycles

LEFT WING OTBD FLAP AFT HINGE FAIRING CHANNEL HAS AN ELONGATED HOLE, REPAIRED IAW ERA 525967-14, REV ORIG

Part: SCUFF PLATE — CRACKED (CARGO DOORWAY) · airframe 52,233 hrs · 41,018 cycles

CENTER CARGO DOOR CUTOUT SCUFF PLATE IS CRACKED IN TWO PLACES AT INSIDE CORNERS. CARGO DOOR SCUFF PLATE WELDED IAW EA 491023-14MA AND PS 900-7-2-1.

Part: ANGLE — CORRODED (BS 645-683) · corrosion level 2 · airframe 52,233 hrs · 41,018 cycles

CENTER CARGO DOOR CUTOUT, LOWER DOOR SILL ZEE ANGLE HAS NUMEROUS SPOTS OF CORROSION BS 645 - 683. REMOVED CORROSION IAW SRM 53-01, FIG 101. TRIMMED OUT 2 EA, OUT OF LIMIT AREAS ON ZEE ANGLE LOWER FLANGE IAW SRM 53-05, PG 874, FIG 123A, OPTION 2. REPAIRED IAW SRM 53-05. OPT 2 CAT "A". I

Part: SKIN — DAMAGED (BS 186) · airframe 52,233 hrs · 41,018 cycles

UNIDENTIFIED PREVIOUS DEEP BLEND OUT ON FUSELAGE SKIN AT STA 186, BETWEEN LONGERON 27R AND 28R. REMOVED PAINT ON PREVIOUS BLEND AT STA 186 BETWEEN LONGERON 27R & 28R IAW SRM 51-10-3, MECHANICALLY MEASURED & NDT UT THICKNESS REVEALED MAT. LOSS OF .026", ORIG MAT .050" FOUND OUT OF LIMITS IAW SRM 53-04-1, PAGE 6. TRIMMED-OUT DAMAGE TO A 0.8" DIAMETER & ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-04-2, FIG 2, PAGE 20.

Part: TIRE — FAILED (MLG) · airframe 59,274 hrs · 46,000 cycles

MAJOR TIRE SEPARATION ON NR 4 TIRE.

Part: LAMP — INOPERATIVE (SLIDE INDICATOR) · airframe 59,878 hrs · 46,475 cycles

L4 ENTRY DOOR SLIDE LIGHT ARMING INDICATOR INOPERATIVE. REPLACED THE LAMP. CHECKED GIRT BAR ENGAGEMENT. LAMP AND GIRT BAR FUNCTION OK. OK FOR SERVICE.

Part: CONDUIT — OUT OF RIG (TAILCONE) · airframe 48,492 hrs · 38,372 cycles

DURING TAILCONE FUNCTIONAL CHECK, LOWER CONDUITS FOR PULL CABLES IAW STEP 4D5, FOUND OUT OF RIG. REPOSITIONED CONDUIT IAW AMM.

Part: BUSHING — WORN (TAILCONE TEE PIN) · airframe 48,492 hrs · 38,372 cycles

DURING TAILCONE FUNCTIONAL TEST, FOUND TEE PIN BUSHINGS WORN. REPLACED TEE PIN BUSHINGS IAW AMM.

Part: STRAP — SATURATED (TAILCONE SLIDE) · airframe 48,492 hrs · 38,372 cycles

DURING TAILCONE FUNCTIONAL, FOUND AFT AND FORWARD HOLD DOWN STRAPS SOAKED IN HYD FLUID, IN POOR CONDITION. R & R NEW STRAPS ON WC 2500-4484.

Part: CABLE — FRAYED (TAILCONE) · airframe 48,492 hrs · 38,372 cycles

FOUND TAILCONE KEVLAR CABLE FRAYED. R & R KEVLAR INTERIOR CABLE IAW AMM. OPS CHECKS GOOD.

Part: DOOR FRAME — CORRODED (BS 1165) · airframe 48,476 hrs · 38,362 cycles

CORROSION ON DOOR FRAME OF AFT BAG BIN LOWER EDGE AT APPROX BS 1165 STR 28R. REPAIRED IAW SRM 53-05 FIG 123, OPTION 2.

Part: LANYARD — BROKEN (EVAC SLIDE) · airframe 46,186 hrs · 36,808 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND L1 DOOR SLIDE LANYARD CABLE BROKEN. MAINTENANCE REMOVED AND REPLACED SLIDE LANYARD PER AMM. OPERATION CHECKS GOOD.

Part: WINDOW FRAME — DAMAGED (FUSELAGE) · airframe 44,944 hrs · 35,953 cycles

SCRIBE LINES AROUND WINDOW FRAME NR 64 BETWEEN STA Y=807-826 AT FUSELAGE SKIN. REWORKED PER ERA 495214-14 REV ORG.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 44,944 hrs · 35,953 cycles

LIGHTNING STRIKE ON AFT LOWER CORNER OF LT WINDOW BELT FRAME STA 7=712 AT FUS EXTERNAL SKIN. REWORKED PER ERA 495214-14 REV ORG.

Part: WINDOW FRAME — DAMAGED (FUSELAGE) · airframe 44,944 hrs · 35,953 cycles

LIGHTNING STRIKE ON FWD/AFT SECTION OF WINDOW FRAME NR 32 BETWEEN STA Y=503 TO 522 AT FUSELAGE EXTERNAL SKIN. REWORKED PER ERA 495214-14 REV ORG.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 44,944 hrs · 35,953 cycles

TRANSFERED FROM ADF CTL NUM:037166001-ON WALK AROUND FOUND FWD ENTRY OUTER SKIN DAMAGED AT LOWER FWD CORNER DOOR SKIN WAS REPAIRED IAW SRM 52-05D FIG 55.

Part: FRAME — CORRODED (FUSELAGE) · airframe 44,944 hrs · 35,953 cycles

CORROSION ON LOWER CAP OF FRAME AT STA 1380 BETWEEN LONGERONS 27LT AND 27RT. "T" CAP WAS REPAIRED IAW ERA 495215-4 REV ORIG.

Part: FITTING — CORRODED (RT MLG) · airframe 44,944 hrs · 35,953 cycles

EA 09-093855-03AD REV B ME 02 CORROSION ON RT MLG SUPPORT FITTING BUSHING BORE SURFACE. REPAIRED PER AMR 0957393 REV 1.

Part: FITTING — CORRODED (LT MLG) · airframe 44,944 hrs · 35,953 cycles

EA 09-093855-03AD REV B ME 01 CORROSION ON LT MLG SUPPORT FITTING BUSHING BORE. REPAIRED PER AMR 0957393 REV 1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,944 hrs · 35,953 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN BTW STA Y=1086-1087 LONGERON 29RT-30 AND BTW STA Y=1099-1100 LONGERON 28RT-29RT.

Part: FITTING — CORRODED (RT MLG) · airframe 44,944 hrs · 35,953 cycles

EA 09-093855-03AD REV B ME 02 CORROSION ON RT MLG SUPPORT FITTING SUPPORT. REPAIRED PER AMR 0957393 REV 1.

Part: FITTING — SCRATCHED (LT MLG) · airframe 44,944 hrs · 35,953 cycles

EA 09-093855-03AD REV B ME01 SCRATCHES ON LT MLG SUPPORT FITTING BEARING BORE. REPAIRED PER AMR 0957393 REV ORIG.

Part: FITTING — CORRODED (LT MLG) · airframe 44,944 hrs · 35,953 cycles

EA 09-093855-03AD REV B ME 01 CORROSION ON LT MLG SUPPORT FITTING BUSHING BORE BOTTOM SURFACE. REPAIRED PER AMR 0957393 REV 1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,944 hrs · 35,953 cycles

DURING HMV CORROSION WAS FOUND ON INNER SKIN STA Y=788-793 BTW LONGERON 30 AND 29L AT MID CARGO COMPARTMENT INNER SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: PAN — CRACKED (CARGO DOOR) · airframe 44,944 hrs · 35,953 cycles

DURING HMV A CRACK WAS FOUND ON AFT EDGE OF CARGO COMPARTMENT DOOR PAN BELOW STOP NR 5. DOOR PAN WAS REPAIRED IAW SRM 52-05 FIG 50.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,944 hrs · 35,953 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN FROM STA 1081-1130 BETWEEN LONG 30-35RT FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 44,944 hrs · 35,953 cycles

MAINTENANCE REPAIRED PER SRM 53-04D. DUE ERA 466086-14 REV C LT WINDOW BELT PANEL FS 408-522 ACCOMPLISH PERM REPAIR PER RESTRICTION 4 PRIOR TO 40500 AC CYCLES (TO 216860)

Part: PANEL — DAMAGED (FUSELAGE) · airframe 44,944 hrs · 35,953 cycles

MAINTENANCE REPAIRED PER ERA 466085-14 REV E DUE ERA 466085-14 REV C LT WINDOW BELT PANEL FS 408-522 WINDOW NBR 31 ACCOMPLISH PERM REPAIR PRIOR TO 52630 AC CYCLES (TO 216859)

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,944 hrs · 35,953 cycles

DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN IN STA Y=1099 TO 1105 BETWEEN LONGERON 29RT AND 29LT AT AFT CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: PAN — CRACKED (CARGO DOOR) · airframe 44,944 hrs · 35,953 cycles

CRACKED PAN BELOW FITTING STOP NR 5 OF ADT CARGO COMPT FWD SECTION. REPAIRED PER SRM 52-05.

Part: DOUBLER — CORRODED (CARGO BAY) · airframe 44,944 hrs · 35,953 cycles

DURING HMV CORROSION WAS FOUND ON PREVIOUS REPAIR DOUBLER AT LOWER BEAM FROM STA Y=668-680 OF MID CARGO COMPARTMENT DOOR JAMB. REPAIR DOUBLER WAS REPLACED IAW SRM 53-05 FIG 123.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,944 hrs · 35,953 cycles

DURING HMV A BROKEN FRAME WAS FOUND AT STA Y=1451 AND LONGERON 1. FRAME WAS REPAIRED IAW SRM 53-03D FIG 4.

Part: BATTERY — DISCHARGED (CABIN) · airframe 44,317 hrs · 35,528 cycles

DURING LINE CHECK MAINTENANCE FOUND LEFT AND RIGHT OVERWING EXIT UPPER SIGNS INOP. MAINTENANCE REPLACED BATTERIES AT BATTERY PACK 135-105. OPERATION OF EXIT SIGN NOW CHECK OK. (2011-D0575)

Part: COFFEEMAKER — ODOR (AFT GALLEY) · airframe 43,421 hrs · 34,929 cycles

AT TOP OF DESCENT, F/A SMELLED A BURNING RUBBER ODOR NEAR BACK OF THE ACFT. NO SMOKE ACCOMPANIED SMELL. CREW TURNED GALLEY POWER OFF. ODOR DISAPPEARED. MX PERFORMED OPS 5088. NO SMELL NOTED. FOUND COFFEE RESIDUE ON AFT COFFEE MAKER. CLEANED COFFEE MAKER HEATING PLATE AND SURROUNDING AREA. TURNED ON GALLEY POWER AND LT ON FOR APPROX 1 HR. NO ODOR PRESENT.

Part: LIGHT — INOPERATIVE (ROW 28) · airframe 42,810 hrs · 34,518 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHT AT ROW 28 INOP. MX REPLACED LIGHT ASSY IAW MM. OPERATION OF LIGHT NOW CHECK OK.

Part: FUEL CONTROL — INOPERATIVE (NR 1 ENGINE) · airframe 42,759 hrs · 34,477 cycles

FLIGHT CREW ABORTED THE TAKEOFF AT LESS THAN 15 KNOTS, DUE TO THE LT ENGINE NOT RESPONDING TO THROTTLE MOVEMENT. MX REPLACED THE NR 1 ENG FUEL CONTROL IAW AMM.

Part: HEATER — SHORTED (PITOT/STATIC SYS) · airframe 39,833 hrs · 32,517 cycles

AT DEPARTURE PASSENGER NOTICED SMOKE COMING FROM FLOOR VENTS AT ROW 20A. FOUND HEATER BLANKET FOR LEFT STATIC PORT SHORTED. REPLACED STATIC PORT PER AMM, LEAK CHECKS PER AMM.

Part: HEATER — MALFUNCTIONED (PITOT/STATIC SYS) · airframe 39,833 hrs · 32,517 cycles

AT DEPARTURE SMOKE WAS FOUND COMING FROM THE FLOOR VENTS AT ROW 20A. THE AIRCRAFT WAS GROUNDED AND REMOVED FROM SERVICE. MAINTENANCE FOUND THE LEFT STATIC PORT HEATER WAS OVERHEATED AND BURNED P/N 105846-1. THE HEATER BLANKET WAS REMOVED AND REPLACED PER AMM.

Part: LATCH — FAILED (NACELLE DOOR) · airframe 37,585 hrs · 30,643 cycles

ENGINE UPPER COWL DOOR LATCH REPLACED IAW EA 09-056907-12, ME02.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 36,745 hrs · 29,607 cycles

LT WINDOW BELT PANEL FS 408-522, WINDOW CUTOUT 21, 25, 27, 31 LIGHTNING STRIKE DAMAGE. REPAIRED IAW ERA 466085-14.

Part: ACTUATOR — DEFECTIVE (HORIZ STAB) · airframe 34,494 hrs · 26,906 cycles

HORIZONTAL STABILIZER TRIM ACTUATOR REPLACED IAW EA 06-086621-03M ME01.

Part: GEAR — DAMAGED (TE FLAP) · airframe 34,494 hrs · 26,906 cycles

TRAILING EDGE FLAP TRANSMISSION GEAR REPLACED IAW EA 06-097281-03, ME04.

Part: BONDING STRAP — DAMAGED (FUEL FEED) · airframe 34,494 hrs · 26,906 cycles

FRONT SPAR ENGINE FUEL FEED HOSE ELECTRICAL BONDING REPAIRED IAW EA 06-093241-03, ME01, ME02.

Part: DUCT — CRACKED (BLEED AIR SYS) · airframe 33,547 hrs · 25,674 cycles

DURING CLIMBOUT AT 22K FT A TAIL COMPT TEMP HIGH MSG ILLUM. RAN PROCEDURE VIA THE QRH AND LIGHT EXTINGUISHED WHEN HP BLEED OFF. DISPATCH RECOMMEND DIVERT TO ATL DUE TO ICING IN NY AREA. FOUND RT SPIDER DUCT CRACKED. DUCT REPLACED, LEAK CHECK OK.

Part: APU — LEAKING (AFT) · airframe 32,724 hrs · 24,964 cycles

RIGHT AFTER T/O AFT LAVATORIES SMOKE DETECTORIES WENT OFF WITH WHITE HAZY SMOKE IN THE AFT CABIN AND ODD SMELL. FOUND APU INLET WET WITH OIL FROM INTERNAL LEAK. REPLACED SAME AND PERFORMED DUCT BURNOUT.

Part: MOTOR — UNSERVICEABLE (PRIMARY TRIM) · airframe 31,206 hrs · 23,862 cycles

PRIMARY TRIM MOTOR QUIT IN FLIGHT. REPLACED PRIMARY TRIM MOTOR. CHECKS OK PER AMM.

Part: APU — SMOKE (AFT) · airframe 30,482 hrs · 23,346 cycles

APU CAUSED SMOKE IN THE CABIN AFTER LANDING IN LGA WITH LAV SMOKE DETECTOR GOING OFF. FOUND APU LEAKING OIL INTO INLET. PERFORMED PNEUMATIC SYSTEM DUCT BURN OUT OPN 5089. ALL NORMAL NO SMOKE OR ODOR IN CABIN, ALSO DEF APU PER MEL 49-00-01A.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 29,598 hrs · 22,700 cycles

CORROSION ON C3 CARGO BIN LOWER DOOR JAMB BEAM. REMOVED CORROSION FROM C3 CARGO DOOR JAMB BEAM AND WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-05D FIG 63 SHEET 2. DOOR JAMB BEAM WAS REPAIRED IAW SRM 53-05D FIG 63.

Part: BEAM — CORRODED (DOOR FRAME) · airframe 29,598 hrs · 22,700 cycles

CORROSION ON C2 CARGO DOOR JAMB BEAM. REMOVED CORROSION FROM C2 CARGO BIN LOWER DOOR JAMB BEAM AND WAS FOUND OUT OF LIMITS IAW SRM 53-05D FIG 63 SHEET 2. REPAIRED DAMAGED AREA PER SRM 53-05D FIG 63.

Part: OIL FILTER — CLOGGED (NR 2 ENGINE) · airframe 27,789 hrs · 21,456 cycles

DURING CRUISE AT FL330 RT OIL STRAINER CLOG MESSAGE ILLUMINATED. LIGHT EXTINGUISHED WITH ENGINE AT IDLE POWER. CONTINUED OPERATION WITH ENGINE AT IDLE. CHECKED RIGHT ENGINE CHIP DETECTOR, ALL OK. REPLACED RIGHT ENGINE OIL FILTER, LEAK CHECK GOOD AT IDLE AND CRUISE POWER SETTINGS.

Part: O-RING — DETERIORATED (NR 2 ENGINE) · airframe 27,349 hrs · 21,146 cycles

RT EPR INDICATES HIGH ALL OTHER INDICATIONS NORMAL WITH THROTTLES ALLIGNED AT 15,000 FT 20 DEG TAT RT EPR IND 1.9 AND LT EPR IND 1.4. RAN ALT TEST OF ENGINE PRESSURE RATIO INDICATING SYSTEM PER AMM OPN CKS OK. FOUND O-RINGS ON NOSE BULLET PROBE IN POOR CONDITION REPLACED SAME. OK FOR SVC.

Part: LINE — LEAKING (TAIL) · airframe 25,899 hrs · 20,098 cycles

DURING CRUISE AT FL370 RT HYD DECREASED TO 7 QTS. DURING RT SYSTEM HYD FAILURE CK LIST, HYD QTY DECREASED TO 4 QTS. FOUND #2 PRESSURE LINE TO CASE DRAIN FILTER LEAKING - REPLACED SAME

Part: ACM — LEAKING (A/C BAY) · airframe 24,387 hrs · 18,999 cycles

F/A REPORTED SMOKE IN CABIN IMMEDIATELY AFTER T/O. SMOKE DISAPPEARED AFTER POWER WAS REDUCED. RTN TO CVG FOR IMMEDIATE LANDING. BOTH REAR LAV SMOKE DETECTORS ACTIVATED. REMOVED LT ACM DUCTING AND FOUND OIL RESIDUE. SUSPECT LT ACM LEAKING. ACM P/N219001545. REINSTALLED ACM DUCTING. FWD LT A/C PACK TO MCO AND PLAC PER MEL 21-00-01A. SENSE LINE DISCONNECTED AT FLOW CONTROL VLV. REPLACED COALESCER BAGS AFTER DUCT BURNOUT PER MM. OK FOR SERVICE.

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 24,314 hrs · 18,940 cycles

BURNING SMELL WHEN ENGINE ANTI-ICE USED. INSPECTED A/C - NTF. PERFORMED DUCT BURNOUT.

Part: WARNING LIGHT — FALSE INDICATION (COCKPIT) · airframe 23,637 hrs · 18,447 cycles

ALL 3 GEAR LIGHTS INDICATED RED ON EXTENSION. F/O WIGGLED HANDLE AND ALL WENT GREEN. TOWER CONFIRMED GEAR DOWN ON FLYBY. JACKED AIRCRAFT AND SWUNG GEAR. UNABLE TO DUPLICATE OR FIND FAULT.

Part: APU — LEAKING (AFT FUSELAGE) · airframe 21,235 hrs · 16,636 cycles

DURING CLIMB, LEFT AFT LAV SMOKE ALARM ACTIVATED. F/A REPORTED SMOKE SMELL AND HAZE IN CABIN. DIVERTED TO EWR. FOUND APU LEAKING OIL AND BEING INGESTED. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS. REPLACED APU.

Part: COALESCER BAG — CONTAMINATED (ACM) · airframe 21,036 hrs · 16,490 cycles

OILY SMELL AFT CABIN AFTER T/O, SET OFF SMOKE DETECTORS. PERFORMED DUCT BURNOUT.

Part: WARNING SYSTEM — MALFUNCTIONED (CABIN PRESSURE) · airframe 20,911 hrs · 16,398 cycles

AFTER TAKEOFF FROM TUS, HAD MASTER CAUTION AND AUTO 1 AMBER INOP LIGHT ON PRESS CONTROLLER. PERFORMED PRESSURIZATION SYSTEM TEST PER M/M, NO FAULTS NOTED.

Part: SKIN — DENTED (BS 427)

A DENT WAS FOUND AT STA 427 BETWEEN L29L AND 30. REPAIRED PER ERA 333340-14, REV A.

Part: TIRES — FAILED (RT MLG)

ON TAKEOFF ROLL AT 15O KTS, TAIL COMPT TEMP HI MSG. ABORTED TAKEOFF. WHEELS NR 1 NR 2 AND NR 4 FUSE PLUGS MELTED AND TIRES DEFLATED. FOUND HOT AIR LEAK AROUND RT PACK HEAT EXCHANGER, DEFERRED RT PACK.

Part: BATTERY — DISCHARGED (CABIN)

AFT CABIN FLASHLIGHT INOP. REPLACED BATTERY.

Part: SKIN — CRACKED (FWD FUSELAGE)

A .5 INCH CRACK AT RT NLG DOOR AFT HINGE CUTOUT IN FUSELAGE SKIN FOUND AT B-2 LTR CK. REPAIRED PER SRM 53-05 FIG 62.