N114DL

Part: FAN — INOPERATIVE (FWD CARGO) · airframe 59,912 hrs · 28,117 cycles

FORWARD EQ SUPPLY FAN 2 EICAS MSG WITH EQUIP COOLING SUPPLY FAN 2 CB POPPED STRONG ELECTRICAL FUMES IN COCKPIT, REPLACED FAN.

Part: WEDGE — DELAMINATED (LT WING FLAP) · airframe 59,771 hrs · 28,056 cycles

IB AFT FLAP TE WEDGE WAS FOUND WITH DAMAGE TO THE LOWER SKIN AND CORE. REPAIRED IAW ERA 091685-14.

Part: SUPPORT BEAM — CORRODED (TE FLAPS) · airframe 59,771 hrs · 28,056 cycles

LEFT AND RIGHT INBOARD FLAP INBOARD AND OUTBOARD SUPPORTS CORRODED. REPAIRED IAW ERA 091244-14.

Part: SKIN — CRACKED (RT WING) · airframe 59,771 hrs · 28,056 cycles

RT LOWER WING SKIN SIDE LINK FITTING ATTACH FASTENER FOUND CRACKED. REPAIRED IAW ERA 091372-14AD.

Part: FITTING — DAMAGED (LT WING SPAR) · airframe 59,771 hrs · 28,056 cycles

LEFT WING FRONT SPAR OUTBOARD PITCH LOAD FITTING HAS TWO DAMAGED HOLES DUE TO TOOLING WHILE ACCOMPLISHING EO 01-074906-03AD. REPAIR IAW ERA 091345-14AD.

Part: STRUCTURE — CORRODED (WING FLAP) · airframe 59,771 hrs · 28,056 cycles

WHILE ACCOMPLISHING THE I/B TRAILING EDGE MAIN FLAP ATTACH BOLT REPLACEMENT PER EA 01-085672-12AD, CORROSION WAS FOUND IN THE BORES OF THE FWD TWO AND AFT ATTACH FOUR HOLES OF THE 9-10 BEAM AND THE ASSOCIATED MATING HOLES ON THE FLAP AND THE FOUR HOLES COMMON TO THE I/B ATTACH SUPPORT BEAM AND THE ASSOCIATED HOLES IN THE FLAP COLLAR FITTING. THIS ERA PROVIDES REPAIRS FOR THE SUBJECT HOLES.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,787 hrs · 25,231 cycles

THE SKIN, BEARSTRAP DOUBLER, INTERCOSTAL CHORD AND WEB SURROUNDING THE ACS HATCH WERE DAMAGED WHEN THE A/C WAS LOWERED FROM JACKS ONTO A LADDER LEFT UNDERNEATH. NEW SECTION OF INTERCOSTAL CHORD SPLICED IN. WEB REPLACED AND SKIN DAMAGE REPAIRED WITH EXTERNAL DOUBLERS. ER/A 334685-14.

Part: SKIN — CORRODED (CENTER WING) · airframe 53,787 hrs · 25,231 cycles

CORROSION FOUND ON THE UPPER SURFACE OF THE CENTER WING UPPER SKIN OVERLAYING THE REAR SPAR AT STATION 955 AND BETWEEN LBL 70 AND 80. 334562-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,787 hrs · 25,231 cycles

FUSELAGE SKIN FOUND DENTED AND INTERNAL BEAR STRAP DEFORMED IN AREA JUST AFT OF THE C2 CARGO DOOR OPENING AT STRINGER 31R. THE STA 1351 FRAME IS BUCKLED IN THE SAME AREA. ER/A 270824-14 REV A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,787 hrs · 25,231 cycles

FUSELAGE SKIN FOUND CORRODED AT STA 1082 AND STR-38L. DAMAGE TRIMMED OUT AND EXTERNAL DOUBLER AND TRIPLER INSTALLED. ER/A 334619-14.

Part: SKIN — CRACKED (NR 1 & 2 PYLONS) · airframe 53,787 hrs · 25,231 cycles

CRACK INDICATIONS FOUND IN THE NR 1 AND NR 2 PYLON O/B SIDELOAD FITTING HOLES. BY REMOVING THE RT WING SKIN PANEL LAYER, IT WAS FOUND THAT THE CRACK INDICATION WAS CAUSED BY AN ENLARGED HOLE IN THAT LAYER, WHICH ACTS AS A SHIM IN THE STACKUP. NO CRACK INDICATIONS FOUND IN REMAINING LAYERS. ER/A 334582-14AD.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 53,787 hrs · 25,231 cycles

SKIN REPAIR AT STA 566 AND STRINGER 32L FOUND WITH TIGHT FASTENER SPACING. EXISTING REPAIR REMOVED AND HOLE PATTERN CUT OUT. NEW DOUBLER INSTALLED TO REPAIR CUTOUT. STRINGER 33L ALSO REPAIRED IN THIS SAME FRAME BAY ER/A 334530-14.

Part: UNKNOWN — ODOR (CABIN)

DURING FLIGHT, AN ACIDIC SMELL FROM R2 DOOR AREA, OVERHEAD AFT RT LAV. FOUND C/B B-1 ON P-33 PANEL POPPED. C/B IS FOR NUMBER 1 EQUIP/GALLEY/LAV VENT FAN. FWD TO MCO. REPLACED K629 AND K835 RELAYS. OPS CHECK GOOD.

Part: MECHANISM — LACK OF LUBE (TE FLAPS)

IN FLT: LOWERED FLAPS TO 1 DEG AND RCVD L /E SLAT DISAGREE LIGHT. SELECT ALT, DID NOT HELP. WHILE LOWERING FLAPS ELECTRICALLY, RCVD T/E FLAP DISAGREE LIGHT. FLAPS LOCKED AT 16 DEG. WHEN LOWERED ELECTRICALLY, L/E SLAT LIGHT WENT AWAY. T/E FLAP LIGHT REMAINED. LUBED LE AND TE FLAPS, OPERATED SAME SEVERAL TIMES. ALL CKS GOOD. FSEU CKS NML.

Part: INDICATOR — FAILED (LE FLAPS)

ON FLAP EXTENSION THE LEFT INDICATOR SHOWED A SPLIT WITH THE RIGHT. CYCLED BACK TO ZERO. FLAP INDICATOR FOLLOWED L/E DISAGREE ON EICAS. NORMAL CONTROL OF AIRCRAFT. REPLACED INDICATOR.

Part: BOTTLE — DISCHARGED (CARGO COMPT)

NR 1 FIRE BOTTLE FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED AND CGO BOTTLE 1 EICAS MSG ILLUMINATED. NR 1 CGO BOTTLE FOUND EMPTY. FWD TO MCO.

Part: RAM AIR TURBINE — FAILED (CENTER HYD SYST)

LOSS OF CENTER HYDRAULIC PRESSURE AND QUANTITY ON TAKEOFF. FOUND FAILURE OF THE RAM AIR TURBINE GROUND CHECKOUT MODULE IN THE RIGHT WHEEL WELL. REPLACED SAME, SYSTEM CHKS OK.

Part: LIGHT — INOPERATIVE (RT OVER WING)

AFT RT OVERWING SLIDE LGT INOP. REPAIRED SHORTED LGT ASSY AND REPLACED FUSE ON PWR SUPPLY.

Part: TILT FUSE — FAILED (RT MLG)

AFTER TAKEOFF, RT MLG WOULD NOT RETRACT. REPLACED TRUCK TILT FUSE, OPS CHECK GOOD.

Part: CHECK VALVE — FAILED (RT MLG)

AFTER TAKEOFF, RT MLG WOULD NOT RETRACT. REPLACED TILT FUSE CHECK VALVE, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT FIXTURE.

Part: ECU CB — TRIPPED (NR 1 ENGINE)

GOT STRONG ELECTRICAL SMELL 30 MINUTES AFTER T/O, SMELL GREW FAINT AND WAS GONE IN 15 MIN. FOUND LEFT ENG CONTROL IDLE C/B OUT, LEFT IT OUT. INSPECTED COCKPIT CIRCUIT BREAKER PANELS, INSTRUMENT PANELS, GENERAL AREA AND E AND E COMPARTMENT, NO EVIDENCE OF BURNS OR SMELLS.

Part: TE WEDGE — DENTED (LT TE SLAT)

SLAT WAS SENT TO SHOP FOR REPLACEMENT OF T/E WEDGE DUE TO HAIL DAMAGE. WEDGE WAS INSTALLED ACCORDING TO THE CMM 57-43-55.

Part: TE WEDGE — DENTED (LT TE SLAT)

SLAT WAS SENT TO SHOP FOR REPLACEMENT OF T/E WEDGE DUE TO HAIL DAMAGE. WEDGE WAS INSTALLED ACCORDING TO THE CMM 57-43-55.

Part: SKIN — DENTED (NR 8 LE SLAT)

HAIL DAMAGE TO UPPER SURFACE OF NR 7 L/E SLAT. REPLACED WEDGE PER CMM 57-43-61.

Part: TE WEDGE — DENTED (NR 4 LE SLAT)

THE WEDGE OF THE SLAT WAS DENTED DUE TO HAIL DAMAGE. THE WEDGE WAS REPLACED PER THE CMM 57-43-61. THE WEDGE REPLACEMENT IS THE TERMINATING ACTION FOR A.D. 93-14-19.

Part: SKIN — DENTED (NR 4 LE SLAT)

HAIL DAMAGE TO UPPER SURFACE OF NR 4 L/E SLAT. THE TRAILING EDGE WEDGE WAS REPLACED PER CMM 57-43-55. THE PART NUMBER OF THE NEW WEDGE IS 114T4114-17. THIS IS THE TERMINATING ACTION FOR A.D. 93-14-19.

Part: TE WEDGE — DENTED (NR 1 LE SLAT)

HAIL DAMAGE OCCURRED TO UPPER SURFACE OF T/E WEDGE. REPLACED WEDGE IN C/W C.M.M.57-43-41.

Part: TE WEDGE — DENTED (NR 6 LE SLAT)

TRAILING EDGE WEDGE HAD HAIL DAMAGE. REPLACED WEDGE PER CMM 57-43-37. REPAIRS ACCOMPLISHED DURING SHOP VISIT FOR NR 6 L/E SLAT PANEL.

Part: TE WEDGE — DENTED (NR 4 SLAT)

DURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH TRAILING EDGE WEDGE DELAMINATED AND DENTED FROM HAIL. REPLACED WEDGE PER CMM 57-43-55.

Part: TE WEDGE — DENTED (NR 7 SLAT)

T/E WEDGE OF NR 7 SLAT HAS DENTED BY HAIL STORM CHANGED T/E WEDGE PER CMM 57-43-37.

Part: SKIN — DENTED (NR 11 SLAT)

DURING INSPECTION, NR 11 L/E SLAT PANEL UPPER T/E WEDGE WAS FOUND DENTED. REPAIRED PER SRM 57-43-61.

Part: LE SKIN — CHIPPED (RT ELEVATOR)

DURING SHOP INSPECTION, LEADING EDGE WAS FOUND TO BE CHIPPED AT UPPER SURFACE 75.5 INCHES FROM O/B END. REPAIRED AS PER SRM 51-70-03, FOR RIGHT ELEVATOR.

Part: RIB — DELAMINATED (RT ELEVATOR)

DURING SHOP INSPECTION, NR 1 RIB FROM I/B EDGE FOUND TO BE CRACKED AT FWD EDGE, NR 2 RIB FROM I/B EDGE FOUND TO BE CRACKED AT FWD EDGE, AND NR 8 RIB FROM I/B EDGE WAS DELAMINATED AT FWD EDGE. REPAIRED RIBS AS PER SRM 55-20-02, FOR RT ELEVATOR.

Part: ELEVATOR — HOLES (RIGHT)

DURING SHOP INSPECTION, SEVERAL HOLES FOUND. ONE HOLE FOUND 1 DIA, 14 AFT OF SPAR AND 29 FROM O/B EDGE, 1 HOLE FOUND 1 DIA, 27 FROM T/E AND 37 FROM O/B EDGE, 1 HOLE FOUND 1.5 DIA, 14 FROM T/E AND 32 FROM O/B EDGE, AND 1 HOLE FOUND 1 DIA, 21 FROM O/B EDGE AND 25 FROM T/E. REPAIRED AS PER SRM 55-20-01, FOR RT ELEVATOR.

Part: SKIN — PUNCTURED (RT ELEVATOR)

DURING SHOP INSPECTION, NUMEROUS SKIN PUNCTURES WERE LOCATED ON UPPER SURFACE. REPAIRED AS PER SRM 51-70-17, FOR RIGHT ELEVATOR.

Part: SKIN — DELAMINATED (RT ELEVATOR)

DURING SHOP INSPECTION, DELAMINATION WAS FOUND AT HINGE CUTOUTS. REPAIRED AS PER SRM 55-20-2 PG 102, FOR RT ELEVATOR.

Part: LE SKIN — DELAMINATED (RT ELEVATOR)

DURING SHOP INSPECTION, LOWER SURFACE OF RT ELEVATOR L/E WAS FOUND DELAMINATED AND CRACKED. ALSO, UPPER SURFACE O/B L/E HAD SOME DELAMINATION. REPAIRED AS PER SRM 55-20-02.

Part: SKIN — DAMAGED (LT ELEV)

HAIL DAMAGE IN DFW; DURING SHOP INSP MAINT, FOUND 7 ONE INCH DIAMETER HOLES IN UPPER SKIN. ALL HOLES WERE REPAIRED PER SRM 55-20-01 AND ERA 270858-14.

Part: SKIN — PUNCTURED (LT ELEVATOR)

LT ELEVATOR HAS 7 PUNCTURES ON UPPER SURFACE FROM THE HAIL STORM AT DFW. PUNCTURES WERE REPAIRED PER SRM 55-20-01.

Part: TE WEDGE — DELAMINATED (NR 4 SLAT)

DURING SHOP INSPECTION, NR 4 L/E SLAT PANEL WAS FOUND WITH DELAMINATION TO T/E WEDGE. WEDGE WAS REPLACED PER SRM 57-43-55.

Part: ELEVATOR — DAMAGED (RIGHT)

DURING SHOP INSPECTION FOUND HOLE 1.5 DIA 31 FROM T/E AND 12 FROM I/B EDGE, 1 HOLE FOUND 1 DIA, 37 FROM T/E AND 12 FROM I/B EDGE, 1 HOLE FOUND 1.5 DIA, 11 AFT OF SPAR AND 13 FROM I/B EDGE, AND 1 HOLE FOUND 1.5 DIA, 6 AFT OF SPAR AND 26 FROM I/B EDGE. REPAIRED AS PER SRM 55-20-01, FOR RT ELEVATOR.

Part: WEDGE — DAMAGED (LT HORIZ STAB)

FOUND DURING INSPECTION DFW, HOLE IN T/E WEDGE LEFT HORIZ STAB 3 INCHES FWD OF T/E 30 INCH INBD OF TIP. REPAIRED PER SRM 55-10-01.

Part: SKIN — CRACKED (LT AILERON)

FOUND DURING INSPECTION DFW, 1 CRACK IN UPPER SURFACE OF I/B AILERON. REPAIRED I/B AILERON AS PER SRM 57-60-01 SANDED AND REPAINTED AREA.

Part: SKIN — DAMAGED (LT ELEVATOR)

AFTER HAIL STORM ELEVATOR WAS FOUND DAMAGED. REPAIRED AS PER SRM 55-20-01 REF ERA 270854-14.

Part: SKIN — CRACKED (RT AILERON)

FOUND DURING INSPECTION DFW, 2 EA CRACKS IN O/B END OF O/B AILERON UPPER SURFACE. REPAIRED PER SRM 57-60-02.

Part: LOCK ACTUATOR — BROKEN (LT MLG)

ON CLIMBOUT, WHEN GEAR HANDLE WAS PLACED TO UP THE AMBER DOORS AND GEAR LIGHT STAYED ON. CYCLED GEAR, NO HELP AND RETURNED ATL. FOUND LT MLG, FORWARD JURY BRACE LOCK ACTUATOR PISTON BROKEN. REPLACED SAME OPERATION NORMAL.