N942UW

Part: LIGHT — DEFECTIVE (EXTERIOR) · airframe 71,940 hrs · 25,597 cycles

THREE RIGHT EXTERIOR DOOR EXIT LIGHTS INOPERTIVE. SECURED THE EXTERIOR EXIT LIGHTS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — NO TEST (CABIN) · airframe 71,940 hrs · 25,597 cycles

RIGHT FLOOR EMERGNECY LIGHT INOPERATIVE, ROWS 1 TO 11. REPLACED THE LIGHT AND ACCOMPLISHED SATISFACTORY OPEARTIONAL CHECK.

Part: LIGHT — LOOSE (CABIN) · airframe 71,414 hrs · 25,489 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT, FLOOR LIGHT STRIP AT SEAT 17 IS COMING UP. RESECURED LIGHT STRIP AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — UNSECURE (ROWS 17-18) · airframe 70,645 hrs · 25,328 cycles

LEFT SIDE FLOOR MOUNTED EMERGENCY LIGHT STRIP BETWEEN SEAT ROWS 17 AND 18 ARE NOT SECURE AND LIFTING UP. SECURED THE EMERGENCY LIGHT.

Part: LENS — MISSING (CABIN) · airframe 70,000 hrs · 25,194 cycles

AIRCRAFT WAS NOT GNDED. SEAT 10B LENS COVER IS MISSING. INSTALLED LENS COVER AT SEAT 10B & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR SEAL — DEFECTIVE (L1 DOOR) · airframe 69,656 hrs · 25,107 cycles

AIRCRAFT WAS GNDED. A VERY LOUD SQUEAL FROM THE L1 DOOR WAS REPORTED & THE FLIGHT CREW DECLARED AN EMER & RETURNED. FOUND THE L1 DOOR PRESS SEAL CUT & LEAKING IN THE UPPER FWD CORNER OF THE DOOR. REPLACED THE DEFECTIVE PRESS SEAL & ACCOMPLISHED A SATISFACTORY LEAK CHECK IAW AMM 52-09-01.

Part: BOTTLE — LEAKING (L4 DOOR) · airframe 69,603 hrs · 25,094 cycles

AIRCRAFT WAS NOT GNDED. 4L DOOR ASSIST BOTTLE PSI 0. REPLACED 4L DOOR ASSIST BOTTLE IAW AMM 52-11-30.

Part: LANYARD — OUT OF POSITION (ZONE 800) · airframe 69,081 hrs · 24,988 cycles

AIRCRAFT WAS NOT GNDED. LT AFT DOOR WILL NOT ARM. OPENED LT AFT DOOR. FOUND LANYARD IN THE WAY OF DOOR GIRT BAR, CLOSED DOOR. OPERATIONAL CHECKED GOOD.

Part: LANYARD — OUT OF POSITION (L4 DOOR) · airframe 68,969 hrs · 24,964 cycles

AIRCRAFT WAS NOT GNDED. DOOR 4L SLIDE LIGHT DOES NOT ILLUMINATE WHEN ATTEMPTING TO ARM. REPOSITIONED SLIDE LANYARD & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LANYARD — OUT OF POSITION (L4 DOOR) · airframe 68,943 hrs · 24,956 cycles

AIRCRAFT WAS NOT GNDED. L4 DOOR DOES NOT ARM. FOUND SLIDE LANYARD INTERFERING WITH DOOR ARMING. STOWED LANYARD & PERFORMED OPERATIONAL CHECK OF ARMING SYS. OPERATIONAL CHECKED NORMAL IAW AMM 52-11-00-206-021.

Part: D-RING — LOOSE (R1 DOOR) · airframe 68,943 hrs · 24,956 cycles

AIRCRAFT WAS NOT GNDED. FLIGHT ATTENDANT WAS UNABLE TO ARM THE R1 DOOR SLIDE. FOUND D RING LOOSE. SECURED D RING. CYCLED & ARMED DOOR SEVERAL TIMES. OPERATIONAL CHECKED GOOD.

Part: FITTING — DEFECTIVE (GIRT BAR) · airframe 68,771 hrs · 24,914 cycles

AIRCRAFT IN HEAVY MX. RT EMER EXIT DOOR, FWD GIRT BAR FITTING DEFECTIVE. REPLACED GIRT BAR FITTING & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 25-66-03-404-012.

Part: BOTTLE — LOW PRESSURE (EVAC SLIDE) · airframe 68,147 hrs · 24,737 cycles

L4 DOOR SLIDE BOTTLE LOW PRESS. REPLACED L4 DOOR SLIDE IAW TASK CARD 19L80025002.

Part: OVEN — ABNORMAL (GALLEY) · airframe 17,149 hrs · 14,303 cycles

FWD RT & LT OVENS HAD PEANUTS IN THE BOTTOM FOR THE OVENS NEAR THE HEATING ELEMENT THAT CAUGHT FIRE AND CREATED SMOKE CAUSING THE ACFT TO RETURN TO THE FIELD AND A FIRE EXTINGUISHER TO BE USED.

Part: OVEN — DEFECTIVE (GALLEY) · airframe 67,651 hrs · 24,618 cycles

FLIGHT 750 EN-ROUTE, DURING CLIMB, AT APPROX FL 290, BOTH PILOTS SMELLED A FAINT ODOR OF SMOKE IN THE FLIGHT DECK. THAT WAS WHEN IT WAS NOTICED IN THE FWD GALLEY NR 1 OVEN, AN INFLIGHT FIRE WITH AN ELEC SMOKE ODOR IN THE CABIN & FLIGHT DECK. THE FIRE WAS CONTAINED WITHIN THE OVEN. THE FWD FLIGHT ATTENDANT DONNED A PBE SMOKE HOOD & USED A PORTABLE HALON FIRE EXTINGUISHER TO PUT THE FIRE OUT. THE FLIGHT DECLARED AN EMER & RETURNED TO FIELD. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. R & R NR 1 & 2 FWD GALLEY OVENS IAW CMM 25-00-14. INSPECTED OVEN CONNECTOR FOR BURNS. NO BURNS NOTED ON THE PLUGS. OVENS OPERATIONS CHECKED NORMAL. THE BREAKERS DID NOT POP, FIRE WAS INSIDE THE OVENS. PERFORMED TROUBLESHOOTING CABIN AIR QUALITY JC 19L00021001. R & R PBE IAW AMM 25-60-00 & FIRE EXTINGUISHER IAW AMM 25-60-00.

Part: LENS — MISSING (CABIN) · airframe 67,300 hrs · 24,534 cycles

R4 DOOR LOWER EXIT LIGHT LENS MISSING. INSTALLED CORRECT LENS COVER AT R4 DOOR.

Part: SIGN — DETACHED (CABIN) · airframe 64,194 hrs · 23,672 cycles

DOOR 1R EMER EXIT SIGN MISSING. EXIT SIGN FOUND UNDER DOOR BUSTLE, SIGN REFITTED.

Part: SKIN — DELAMINATED (RT AILERON) · airframe 63,010 hrs · 23,372 cycles

C4 CHECK DELAMINATION ON RT AILERON UPPER SURFACE APPROXIMATELY 16 INCHES INBD OF OTBD END & 4 INCHES AFT OF THE LE. REPAIRED RT AILERON UPPER SURFACE IAW TR 757-5500-11-0338.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,010 hrs · 23,372 cycles

C4 CHECK CORROSION ON FLOOR BEAM UPPER CHORD AT BS 1660, WL 208, RBL 57. REPAIRED FLOOR BEAM UPPER CHORD AT BS 1660, WL 208, RBL 57 IAW SRM 51-40-02-0G & 53-00-51-2R-8.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,010 hrs · 23,372 cycles

C4 CHECK, LEVEL 2 FILIFORM CORROSION ON LT CREASE BEAM BETWEEN BS 1257 TO BS 1263, STRINGER 17L, LBL 64. REPAIRED LT CREASE BEAM BETWEEN BS 1257 TO BS 1263, STRINGER 17L, LBL 64 IAW EA 105715.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,010 hrs · 23,372 cycles

C4 CHECK, LEVEL 2 EXFOLIATION CORROSION ON LOWER SIDE OF FLOOR BEAM T CAP AT BS 1640, LBL 57. REPLACED FLOOR BEAM T CAP AT BS 1640, LBL 57 IAW EA 105649 & SRM 53-00-51.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,010 hrs · 23,372 cycles

C4 CHECK, .960 INCH CRACK IN RADIUS OF SHEAR TIE AT BS 1300 BETWEEN STRINGER 20R TO STRINGER 21R. REPLACED SHEAR TIE AT BS 1300 BETWEEN STRINGER 20R TO STRINGER 21R IAW SRM 51-30-01 & DWG 140N2002.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,010 hrs · 23,372 cycles

C4 CHECK CORROSION ON CABIN FLOOR BEAM UPPER FLANGE AT BS 700 BETWEEN LBL 45 TO LBL 60. REPAIRED CABIN FLOOR BEAM UPPER FLANGE AT BS 700 BETWEEN LBL 45 TO LBL 60 IAW EA 105608 & SRM 53-00-51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,010 hrs · 23,372 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON CABIN FLOOR BEAM UPPER FWD FLANGE OF T CAP AT BS 740 BETWEEN LBL 47 TO LBL 55. REPAIRED CABIN FLOOR BEAM UPPER T CAP AT BS 740 BETWEEN LBL 47 TO LBL 55 IAW SRM 53-00-51-2R-8.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,010 hrs · 23,372 cycles

C4 CHECK, LEVEL 2 CORROSION ON SHEAR TIE AT BS1640, STRINGER 29R. REPLACED SHEAR TIE AT BS 1640, STRINGER 29R IAW DWG 146N3640.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,010 hrs · 23,372 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON MID CABIN CREASE BEAM INBD CHORD ANGLE AT BS1020 + 5.5, LBL 64. REPAIRED CREASE BEAM INBD CHORD ANGLE AT BS 1020 + 5.5, LBL 64 IAW EA 105609.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,010 hrs · 23,372 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM T CAP AT BS 324, RBL 59. REPAIRED FLOOR BEAM T CAP AT BS 324, RBL 59 IAW SRM 53-10-08.

Part: GOVERNOR — MALFUNCTIONED (LT ENGINE) · airframe 62,553 hrs · 23,239 cycles

ENROUTE, LEFT ENGINE ROLLED BACK TO SUB-IDLE ON ROLLOUT. AFTER LANDING, LT ENGINE DROPPED OFFLINE. LT ENGINE OIL PRESSURE 10 PSI (RED). LT ENGINE SHUTDOWN. REPLACED BVCU, TPU & N3 TACH IAW AMM. INSPECTED P4 LINE, NO DISCREPANCIES NOTED. BVCU UNIT PASSED INCOMING TESTS, NO FAULT FOUND. SOLDERED AT PINS 6, 14, R5 & R6 ON PL2 CONNECTOR & PINS 92, 94, R5, R6 & IC1 ON FM1 CIRCUIT BOARD. R & R WORN GROUND STRAP & PEELING PLACARDS. THE STATOR FAILS OHMS TEST & THE BEARINGS WERE DIRTY. STATOR ASSEMBLY REPLACED, UNIT OVERHAULED. FFG UNKNOWN IF REASON FOR RETURN IS DUE TO DISCREPANCY FOUND. FOUND BUFFER PISTON BORE IN CDP, GOV BODY ASSEMBLY & BUFFER PISTON WORN.

Part: WINDSHIELD — BURNED (COCKPIT) · airframe 62,362 hrs · 23,178 cycles

ENROUTE, CAPTAIN'S WINDSHIELD BURNED, AND DELAMINATED. AREA OF BURN AND DELAMINATION AT BASE OF WINDSHIELD TOWARD ACFT CENTERLINE, TWO SPOTS, APPROXIMATELY 6 INCHES IN LENGTH. MAINTENANCE R & R NR 1 WINDOW ASSY ALSO R & R NR 1WINDOW HEAT CONTROLLER.

Part: ROD — LOOSE (L2 DOOR) · airframe 62,056 hrs · 23,086 cycles

L2 DOOR SLIDE ARMING LEVER WILL NOT STAY IN CORRECT ARMED POSITION. FOUND LOOSE ROD ON DOOR ARMING MECHANISM. ADJUSTED ROD. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 61,943 hrs · 23,052 cycles

R1 DOOR EMERGENCY EXIT LENS MISSING. INSTALLED EMERGENCY EXIT LENS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,929 hrs · 23,050 cycles

L4 DOOR OUTSIDE EMERGENCY LIGHT WILL NO ILLUMINATE. R & R EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: SKIN — DELAMINATED (NR 10 SLAT) · airframe 61,758 hrs · 23,011 cycles

FOUND DELAMINATION ON NR 10 SLAT LOWER T/E AT APPROX 30" FROM INBD END & BEHIND INBD AUXILIARY TRACK. REPLACED NR 10 SLAT IAW 19L52027002 & EA 105036.

Part: D-RING — UNSECURE (L4 DOOR) · airframe 61,735 hrs · 23,002 cycles

L4 DOOR DIFFICULT TO MOVE HANDLE. RESECURED D-RING. OPS CHECKED GOOD.

Part: LENS — UNSECURE (CABIN) · airframe 61,441 hrs · 22,911 cycles

EMERGENCY LIGHT COVER OFF EMERGENCY EXIT LIGHT COVER LOCATED IN COCKPIT EMERGENCY LIGHT FLOOR LEVEL 2R DOOR. REINSTALLED LENS COVER.

Part: PUSHROD — OUT OF ADJUST (L2 DOOR) · airframe 60,920 hrs · 22,788 cycles

PHL - 2L DOOR SLIDE LIGHT INOP. ADJUSTED GIRT BAR PUSHROD.

Part: STRIP — LOOSE (CABIN) · airframe 60,702 hrs · 22,702 cycles

PHL - DOOR 2L EMERGENCY TRACK FLOOR LIGHTING STRIP LOOSE. SECURED EMERGENCY TRACK LIGHTING.

Part: LENS — BROKEN (CABIN) · airframe 60,539 hrs · 22,644 cycles

PHL - FWD ENTRANCE AISLE EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED FWD ENTRANCE AISLE EMERGENCY LIGHT.

Part: FITTING — BENT (EMERGENCY LIGHT) · airframe 60,515 hrs · 22,637 cycles

CLT - EMERGENCY LIGHT LENS COVER OVER THE 2L ENTRY DOOR KEEPS FALLING OFF. STRAIGHTENED RETAINING CLIPS, LENSE NOW STAYS IN PLACE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 58,330 hrs · 21,984 cycles

PHL - 2L DOOR F/A EMERGENCY FLASHLIGHT, LED LIGHT OUT. REPLACED 2L DOOR F/A EMERGENCY FLASHLIGHT AND BATTERY PACK. OPS CHECK NORMAL OK FOR SERVICE.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 57,996 hrs · 21,885 cycles

C4 CHECK - CRACK IN SHEAR WEB BETWEEN BS 1380 TO BS 1360 BELOW S22R. REPAIRED SHEAR WEB BETWEEN BS 1380 TO BS 1360 BELOW S22R IAW EA 103983.

Part: CABLE — OUT OF POSITION (SLIDE RAFT) · airframe 579,964 hrs · 21,885 cycles

C3 CHECK - R4 DOOR SLIDE ENCLOSURE RETAINING CABLE PULLED OUT OF RETAINERS DURING SLIDE INSTALLATION. REPLACED R4 DOOR SLIDE IAW JOB CARD 19C83625005.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 57,996 hrs · 21,885 cycles

C3 CHECK - 2 AREAS OF DELAMINATION ON NR 9 SLAT UPPER SKIN SURFACES AT 43.5 INCHES FROM OUTBOARD END, 8 INCHES FROM TRAILING EDGE & BETWEEN 5.5 INCHES TO 47.5 INCHES FROM INBOARD END, 8 INCHES FROM TRAILING EDGE. REPLACED NR 9 SLAT IAW AIRWAYS JOB CARD 19L52027002.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 57,996 hrs · 21,885 cycles

C3 CHECK - DELAMINATION ON VERTICAL STABILIZER RIGHT FORWARD TORQUE BOX PANEL BETWEEN VERTICAL STABILIZER STATIONS FSS 119 TO FSS 170. REPLACED VERTICAL STABILIZER RIGHT FORWARD TORQUE BOX PANEL IAW B757 SRM 51-40-02 & BOEING DRAWING 17N2001.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,996 hrs · 21,885 cycles

C3 CHECK - CRACK IN FLOORBEAM STABILIZER STRAP BETWEEN BS 365 TO BS 377, LBL 24.75. REPAIRED FLOORBEAM STABILIZER STRAP BETWEEN BS 365 TO BS 377, LBL 24.75 IAW EA 103963.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,996 hrs · 21,885 cycles

C3 CHECK - CRACK IN FLOORBEAM SUPPORT STRAP BETWEEN BS 365 TO BS 377, BL 0. REPAIRED FLOORBEAM SUPPORT STRAP BETWEEN BS 365 TO BS 377, BL 0 IAW B757 SRM 53-10-51-2R-1 FIG 201 DETAIL VI.

Part: LIGHT — DETACHED (CABIN) · airframe 57,568 hrs · 21,751 cycles

PHL - EMERGENCY FLOOR LIGHTING STRIP NOT ATTACHED NEAR REAR LEFT LAV. SECURED EMERGENCY LIGHTING STRIP AS NEEDED.

Part: CABLE — STICKING (LE SLAT) · airframe 56,782 hrs · 21,474 cycles

CLT FLT 1857 EN ROUTE CLT TO MCO. BOTH FLAP POINTERS ARE ON 1/2 UNIT WITH THE FLAP LEVER IN UP. L/E SLAT ASYM DISPLAYED. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO FIELD CLT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RIGHT OUTBOARD LOSS SENSING SWITCH CABLE STICKING IN CABLE TUB. INSPECTED, CLEANED AND LUBED CABLE. RESET SWITCH, OPS CHECK OK.

Part: UNKNOWN — SMOKE (CABIN) · airframe 55,894 hrs · 21,209 cycles

BWI FLT 1209 EN ROUTE PHL TO SXM. THE FLIGHT EXPERIENCED A LIGHTNING STRIKE IN NOSE OF ACFT UPON DEPARTURE FROM PHL. A SMOKE AND BURNING SMELL FILLED THE CABIN. THE FLIGHT DECLARED AN EMERGENCY AND DIVERTED TO BWI. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT USING LIGHTNING STRIKE INSPECTION CRITERIA. NO DEFECTS WERE NOTED.

Part: LENS — LOOSE (CABIN) · airframe 55,458 hrs · 21,083 cycles

EMERGENCY EXIT COVER AT DOOR 3R LOOSE. COVER REFITTED.

Part: ROLLER — DEFECTIVE (ELEVATOR)

CLT FLT 1794 EN ROUTE LAS TO CLT. REPORTED AS: "THE CAPTAIN'S AND FIRST OFFICER'S CONTROL COLUMN'S "STICK" WHEN MOVING THROUGH NEUTRAL POSITION TOWARD UP OR DOWN. MOST NOTICEABLE ON TAKEOFF, APPROACH, AND LANDING. CAUSED ABRUPT AIRCRAFT "BUMP" WHEN BREAKING THE COLUMN FREE. VERY BAD IN LANDING FLARE." MAINTENANCE REMOVED AND REPLACED THE ELEVATOR FEEL UNIT ROLLER.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

DCA - THE FLASHLIGHT AT THE RIGHT EMERGENCY EXIT JUMPSEAT WAS INOPERATIVE. REPLACED FLASHLIGHT BATTERY.

Part: SKIN PANEL — DELAMINATED (VERTICAL STAB) · airframe 53,135 hrs · 20,426 cycles

CLT - C2 - MAJOR REPAIR - DELAMINATION ON OUTER SKIN OF RIGHT VERTICAL STABILIZER FORWARD TORQUE BOX PANEL. INSTALLED SERVICEABLE RIGHT VERTICAL STABILIZER FORWARD TORQUE BOX PANEL.

Part: SLAT — DEBONDED (LT WING) · airframe 63,135 hrs · 20,426 cycles

CLT - C2 - MAJOR REPAIR - AREA OF DISBOND ON NR 1 SLAT TRAILING EDGE WEDGE 41 INCHES OUTBOARD FROM THE INBOARD END & 1 INCH AFT OF THE LEADING EDGE. REPLACED NR 1 SLAT IAW B757 AMM 27-81-02-4.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 53,135 hrs · 20,426 cycles

CLT - C2 - MAJOR REPAIR - DELAMINATION ON NR 6 SLAT TRAILING EDGE WEDGE. REPAIRED NR 6 SLAT TRAILING EDGE WEDGE IAW B757 SRM 51-70-10.

Part: SLAT — DEBONDED (LT WING) · airframe 52,478 hrs · 20,271 cycles

PHX - B-CHECK - MAJOR REPAIR - NR 5 LEADING EDGE SLAT- OUTBOARD END 18 INCHES INBOARD X 6 INCHES FROM TRAILING EDGE DISBONDED (APPROX) WEDGE. REPLACED NR 5 LEADING EDGE SLAT IAW JOB CARD 19C51227001.

Part: SLAT — DEBONDED (RT WING) · airframe 52,478 hrs · 20,271 cycles

PHX - B-CHECK - MAJOR REPAIR - NR 8 LEADING EDGE SLAT INBOARD END/TRAILING EDGE CORNER DISBONDED 22 (APPROX) WEDGE. REPLACED NR 8 LEADING EDGE SLAT IAW JOB CARD 19L52027002.

Part: ACTUATOR — UNWANTED EXTEND (SPOILER)

MCO FLT 1729 EN ROUTE CLT TO MCO. SPOILER LIGHT ILLUMINATED. EICAS MESSAGE SPOILERS DISPLAYED. WITH SPOILERS SELECTED DOWN. UNCOMMANDED ROLL TO RIGHT. RIGHT OUTBOARD SPOILER PANEL FULLY EXTENDED, WOULD NOT STOW/RETRACT. THE FLIGHT LANDED IN MCO WITHOUT FURTHER INCIDENT. PLACED SPOILERS 1 AND 12 ON MEL. FURTHER ACTION PENDING. (OPEN)

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHL - THE FLASHLIGHT AT L1 DOOR NEEDS A NEW BATTERY. REMOVED AND REPLACED FLASHLIGHT L1 ASSEMBLY.

Part: SLIDE — LOW PRESSURE (L3 DOOR)

BWI - L3 DOOR PRESSURE GAUGE OUT OF RANGE (DOOR SLIDE). REMOVED AND REPLACED L3 SLIDE.

Part: SKIN — CRACKED (TE FLAP) · airframe 47,457 hrs · 19,085 cycles

BFM - C1 - MAJOR REPAIR - CRACK IN RIGHT WING INBOARD TRAILING EDGE FLAP UPPER SURFACE. REPAIRED RIGHT WING INBOARD TRAILING EDGE FLAP UPPER SURFACE IAW B737 SRM 57-53-01.

Part: BEARING — DAMAGED (TE FLAP)

PHL FLT 734 EN-ROUTE PHL TO MAN. DURING CLIMBOUT FROM PHL, THE CREW RECEIVED AN ASYMMETRICAL TRAILING EDGE FLAP DISAGREE MESSAGE. THE CREW DECIDED TO RETURN TO FIELD IN PHL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A LEFT WING OUTBOARD FLAP BEARING ASSEMBLY.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS)

DURING CLIMBOUT, THE CREW RECEIVED AN ASYMMETRICAL TRAILING EDGE FLAP DISAGREE MESSAGE. THE CREW DECIDED TO RETURN TO FIELD. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. (K)

Part: SLIDE — FAILED (ZONE 200)

PHL - WHILE PARKED AT A REMOTE GATE, THE L1 DOOR WAS ACCIDENTALLY OPENED WHILE THE EMERGENCY EVACUATION SLIDE WAS STILL ARMED. THE SLIDE DEPLOYED, BUT DID NOT INFLATE. MAINTENANCE REPLACED THE EMERGENCY EVACUATION SLIDE AT THE L1 DOOR. OK FOR SERVICE. (S)

Part: FAN — OUT OF BALANCE (RT ENGINE)

PHL - FLT 722 EN ROUTE (PHL TO DUB). DURING CLIMBOUT FROM PHL THE RT ENGINE INDICATED VIBRATION OF 2.5 WITH SPIKES UP TO 2.8. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A FAN TRIM BALANCE. VIBRATION LEVELS WITHIN ACCEPTABLE LIMITS. (A)

Part: DRAIN LINE — CRACKED (HYDRAULIC SYS)

PLEASE REVISE RECORD FROM USAABB08116 TO USAABB08117. PHL FLT 723 EN-ROUTE DUB TO PHL. DURING DESCENT INTO PHL, THE LEFT HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO AND THE SYSTEM PRESSURE LIGHT ILLUMINATED. ALSO, EICAS MESSAGE "G L HYD SYS PRESS" DISPLAYED. THE FLIGHT LANDED SAFELY AND WAS ABLE TO TAXI OFF THE RUNWAY, BUT WAS TOWED TO THE GATE. MAINTENANCE REPLACED A HYDRAULIC DRAIN TUBE. SYSTEM OPERATIONALLY AND LEAK CHECKS OK.

Part: DRAIN — CRACKED (HYDRAULIC SYS)

PHL FLT 723 EN ROUTE DUB TO PHL. DURING DESCENT INTO PHL, THE LT HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO AND THE SYSTEM PRESSURE LIGHT ILLUMINATED. ALSO, EICAS MESSAGE "G L HYD SYS PRESS" DISPLAYED. THE FLIGHT LANDED SAFELY AND WAS ABLE TO TAXI OFF THE RUNWAY, BUT WAS TOWED TO THE GATE. MAINTENANCE REPLACED A HYDRAULIC DRAIN TUBE. SYSTEM OPERATIONALLY AND LEAK CHECKS OK. (A)

Part: DRAIN — CRACKED (HYDRAULIC SYS)

PHL FLT 723 - EN ROUTE DUB TO PHL. DURING DESCENT INTO PHL, THE LT HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO AND THE SYSTEM PRESSURE LIGHT ILLUMINATED. ALSO, EICAS MESSAGE "G L HYD SYS PRESS" DISPLAYED. THE FLIGHT LANDED SAFELY AND WAS ABLE TO TAXI OFF THE RUNWAY, BUT WAS TOWED TO THE GATE. MAINTENANCE REPLACED A HYDRAULIC DRAIN TUBE. SYSTEM OPERATIONALLY AND LEAK CHECKS OK. (A)

Part: SKIN — DEBONDED (L/E SLAT) · airframe 45,613 hrs · 18,723 cycles

MCN - MAJOR REPAIR - A CHECK WINGLET MOD - RT WING NR 10 SLAT TRAILING EDGE HAS 2 AREAS THAT ARE DEBONDED, SS 790 AND SS 802. REPAIRED RT WING NR 10 SLAT TRAILING EDGE, SS 790 AND SS 802 IAW B757 SRM 51-70-10 REPAIR 2 AND 4. (S)

Part: FITTING — CRACKED (LT WING) · corrosion level 2

WINGLET MOD/ ETOPS MOD - NR 6110937, LEFT WING RIB 22 LOWER FITTING CRACKED, WS 681.5. REPLACED LEFT WING RIB 22 LOWER FITTING, WS 681.5 IAW DWG 112N5136. (K)

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 45,613 hrs · 18,723 cycles

MCN - EMERGENCY EQUIPMENT - ETOPS WINGLET MOD - MAIN CABIN FLASHLIGHT INOPERATIVE WHEN BATTERY LEADS ARE CONNECTED. REMOVED AND REPLACED BATTERY ON MAIN CABIN FLASHLIGHT. (S)

Part: LANYARD — FRAYED (EVAC SLIDE)

LAS R4 DOOR ESCAPE SLIDE LANYARD HANGING AND FRAYED. MAINTENANCE REPLACED SLIDE, ALSO RIGGED DOOR SLIDE ARMED INDICATION.

Part: FITTING — CRACKED (NR 1 NACELLE) · airframe 43,988 hrs · 18,066 cycles

CLT - MAJOR REPAIR-RON- NR 4214235/EO5407R146, CRACK AT NR 2 FASTENER HOLE (AFT INBD) OF NR 1 ENGINE DIAGONAL BRACE FITTING INSIDE PYLON EO 547R146. REPAIRED IAW EA100041.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,401 hrs · 17,785 cycles

BFM - MAJOR REPAIR - C-4 CHECK - NR 6003912, CORROSION ON FLOOR SUPPORT WEB, BS 340 - BS 395, RBL 14 - RBL 23. REPLACED FLOOR SUPPORT WEB, BS 340 - BS 395, RBL 14 - RBL 23 IAW B757-200 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,401 hrs · 17,785 cycles

BFM - MAJOR REPAIR - C-4 CHECK - NR 6003954, CORROSION ON FLOOR SUPPORT WEB, BS 340, LBL 21 - LBL 30. REPLACED FLOOR SUPPORT WEB, BS 340, LBL 21 - LBL 30 IAW B757-200 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,401 hrs · 17,785 cycles

BFM - MAJOR REPAIR - C-4 CHECK - NR 6003741, CORROSION ON FLOORBEAM, BS 365.25, LBL 11.5 - RBL 50.5. REPAIRED FLOORBEAM, BS 365.25, LBL 11.5 - RBL 50.5 IAW USAIRWAYS TYPICAL REPAIR 53-15-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,401 hrs · 17,785 cycles

BFM - MAJOR REPAIR - C-4 CHECK - NR 6003909, CORROSION ON FLOORBEAM, BS 377.7, LBL 59 - RBL 30. REPAIRED FLOORBEAM, BS 377.7, LBL 59 - RBL 30 IAW USAIRWAYS TYPICAL REPAIR 53-15-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,401 hrs · 17,785 cycles

BFM - MAJOR REPAIR - C-04 CHECK - CORROSION FOUND ON FLOOR SUPPORT, BS 324 - BS 418, BL 0. REPLACED FLOOR SUPPORT, BS 324 - BS 418 IAW B757-200 SRM 51-40-02, 51-10-02, AND 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,401 hrs · 17,785 cycles

BFM - MAJOR REPAIR - C-04 CHECK - CORROSION FOUND ON FLOOR SUPPORT WEB, BS 395, RBL 27 - RBL 44. REPLACED FLOOR SUPPORT WEB, BS 395, RBL 27 - RBL 44 IAW B757-200 SRM 51-10-02, 53-00-51 AND 51-20-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,401 hrs · 17,785 cycles

BFM - MAJOR REPAIR - C-04 CHECK - CORROSION FOUND ON FLOOR SUPPORT, BS 395, RBL 46 - RBL 60. REPLACED FLOOR SUPPORT, BS 395, RBL 46 - RBL 60 IAW B757-200 SRM 53-00-51, 51-10-01 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,401 hrs · 17,785 cycles

BFM - MAJOR REPAIR - C-4 CHECK - NR 6003955, CORROSION ON FLOOR SUPPORT WEB, BS 324 - BS 345, LBL 32. REPLACED FLOOR SUPPORT WEB, BS 324 - BS 345, LBL 32 IAW B757-200 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,401 hrs · 17,785 cycles

BFM - MAJOR REPAIR - C-04 CHECK - CORROSION FOUND ON FLOOR SUPPORT WEB, BS 324 - BS 345, LBL 20. REPLACED FLOOR SUPPORT WEB, BS 324 - BS 345, LBL 20 IAW 757-200 SRM 51-40-02, SDR 51-42-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,401 hrs · 17,785 cycles

BFM - MAJOR REPAIR - C-4 CHECK - NR 6003914, CORROSION ON FLOOR SUPPORT WEB, BS 377.7 - BS 395, RBL 12. REPLACED FLOOR SUPPORT WEB, BS 377.7 - BS 395, RBL 12 IAW B757-200 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,401 hrs · 17,785 cycles

BFM - MAJOR REPAIR - C-04 CHECK - CORROSION FOUND ON LT HAND TUNNEL ABOVE NLG FLOOR SUPPORT WEB, BS 310 - BS 324, LBL 20. REPLACED LT HAND TUNNEL ABOVE NLG FLOOR SUPPORT WEB, BS 310 - BS 324, LBL 20 IAW 757-200 SRM 51-40-02, SRM 51-42-08, AND SRM 51-40-02.

Part: ELECTRICAL BOX — SMOKE (SEAT 10AC) · airframe 42,909 hrs · 17,571 cycles

FLIGHT 1729, BOS-CLT: ON DESCENT INTO CLT, SMOKE BEGAN TO FILL THE CABIN. CREW ACCOMPLISHED SMOKE IN CABIN PROCEDURES AND THE CABIN CLEARED. MAINTENANCE FOUND THE SEB AT ROW 10AC TO BE THE SOURCE. REMOVED SEB AND CABLE. RELEASED PER MEL. [07-10-07] REPLACED SEAT ROW 10AC AND WIRING HARNESS AT 10B.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,540 hrs · 16,616 cycles

DURING MAINTENANCE, 4R EMERGENCY EXIT LIGHT FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER.