N128DL

Part: SPRING — WEAK (LIGHT SWITCH) · airframe 84,853 hrs · 35,480 cycles

EMERGENCY LIGHT SWITCH GUARD, SWITCH SPRING IS WEAK. REPLACED LIGHT SWITCH GUARD. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 83,975 hrs · 35,259 cycles

RIGHT EMERGENCY ESCAPE TEST 1 INOPERATIVE. MAINTENANCE REPLACED RT POWER SUPPLY TO BATTERY PACK AND RELAY. SYSTEM OPERATION IS NORMAL.

Part: FAIRING — DAMAGED (NR 1 NACELLE) · airframe 83,515 hrs · 35,124 cycles

UPPER NR 1 PYLON PANEL 431AT, CANOE FAIRING DAMAGED. REPAIRED IAW ERA 401547-14MA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,337 hrs · 35,068 cycles

LOWER FORWARD FASTENER HOLE HAS CRACK INDICATION IN SKIN ONLY. COMPLIED WITH ERA 533651-14AD REV ORIGINAL. PRI 533651-14AD, LP 1862494.

Part: STRUCTURE — CRACKED · airframe 83,337 hrs · 35,068 cycles

FORWARD OUTER CHORD RT HAS CRACK INDICATION USING HFEC AND LFEC INSPECTION AT THE BOTTOM FORWARD FASTENER OF THE SPLICE ANGLE. REPLACED RT SPLICE IAW ERA 533808-14AD.

Part: BULKHEAD — CRACKED (BS 1809) · airframe 83,337 hrs · 35,068 cycles

BS 1809 BULKHEAD LT FED OUTER CHORD HAS A ONE INCH CRACK AFT OF AND JUST BELOW STRINGER 7. REPAIRED IAW SRM 53-80-08.

Part: BEARING — CORRODED (TE FLAP) · airframe 87,949 hrs · 36,416 cycles

LEFT WING LE FLAP NR 4 SUPPORT MECHANISM , 6-6 O/B LINK ASSY. BEARING/RACE HAS CORROSION, REPLACED REACTION LINK SUPPORT.

Part: STRINGER — CRACKED (BS 632) · airframe 81,564 hrs · 34,543 cycles

DURING INSPECTION, FOUND STRINGER 29R AT BS 632 CRACKED. REMOVED DAMAGED STRINGER AND REPLACED.

Part: FILLER — CORRODED (FUSELAGE) · airframe 87,949 hrs · 36,416 cycles

CORROSION AT AFT LAV SERVICE PANEL FWD EDGE ONLY FILLER CORRODED AND REPLACED. ALSO REPLACED LEFT HINGE ATTACHED TO SERVICE DOOR ACTUATOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,709 hrs · 34,306 cycles

DURING WALK AROUND, FOUND ONE INCH GASH IN SKIN. LOCATED ON LT SIDE, AFT OF PACK EXHAUST VENT AND FORWARD OF BULK CARGO DOOR. HOLE IS 2" X 2". ACCOMPLISHED ERA 524302-14.

Part: SKIN — DAMAGED (BS 1263) · airframe 80,709 hrs · 34,306 cycles

FUSELAGE SKIN DAMAGED AT BS 1263 S33L, MANIFACTURED DOUBLER & FILLER IAW INSTRUCTION OF PRI AND SRM 53-00-01 C/W ERA 524302-14.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 79,772 hrs · 34,029 cycles

EMERGENCY LIGHTS AT 11AB & 13AB ARE INOPERATIVE. MAINTENANCE FOUND CONNECTORS DISCONNECTED AT SEATS 11AB & 13AB. SECURED CONNECTORS.

Part: BATTERY PACK — MISSING (EMERGENCY LIGHT) · airframe 79,591 hrs · 33,977 cycles

DURING A CHECK, FOUND OUTSIDE EMERGENCY LIGHT INOPERATIVE. FOUND EMERGENCY LIGHT BATTERY MISSING AT M733 POWER SUPPLY. MX REPLACED POWER SUPPLY BATTERY. SYS OPS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 79,101 hrs · 33,838 cycles

EMERGENCY LIGHTS AT SEAT 27GF ARE INOPERATIVE. MX FOUND BROKEN WIRE AT SEAT TO SIDEWALL AND REPLACED CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: SKIN — DAMAGED (BS 1197) · airframe 78,299 hrs · 33,603 cycles

LOWER SKIN ANTENNA MOUNT LOCATION BS 1197 + 99. ACCOMPLISH ER/A 515975-14.

Part: SKIN — CRACKED (BS 1197) · corrosion level 2 · airframe 78,299 hrs · 33,603 cycles

FUSELAGE CRACKED AT FS 1197 +121 AND S39L. C/W PRI 515975-14, REV.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 77,873 hrs · 33,474 cycles

ROW 33 G, F AISLE EMERGENCY LIGHT IS INOPERATIVE. CONNECTED SEAT CONNECTOR. SYS OPS IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,674 hrs · 33,423 cycles

FOUND BY MX R1 DOOR RT OVERWING EMERGENCY LIGHTS WILL NOT TURN OFF. MX REPLACED THE POWER SUPPLY M731. SYS OPS NORMAL

Part: FLOORBEAM — CRACKED (BS 1197) · airframe 73,328 hrs · 33,337 cycles

DURING INSPECTION FOUND CRACK ORIGINATING FROM FLOOR PANEL HOLE ON UPPER ANGLE OF FLOORBEAM AT FS 1197+110 RBL 40. FLOORBEAM UPPER ANGLE REPAIRED IAW SRM 53-00-51, FIG 201, REPAIR 2.

Part: FLOORBEAM — CRACKED (BS 1562) · airframe 73,328 hrs · 33,337 cycles

DURING INSPECTION FOUND FLOORBEAM UPPER ANGLE AT FS 1562, RBL 85, CRACKED. FLOORBEAM REPAIRED IAW ERA 511252-14, REV 1(NRC 250-021).

Part: SKIN — DENTED (NR 8 SLAT) · airframe 77,364 hrs · 33,337 cycles

NR 8 SLAT L/E FOUND DENTED. REPAIRED CARRIED OUT IAW SRM 57-43-01, REPAIR 1.

Part: FLOORBEAM — CRACKED (BS 1087 RBL 40) · airframe 77,364 hrs · 33,337 cycles

DURING INSPECTION, FOUND CRACK ON UPPER CHORD OF FLOORBEAM AT FS 1087, RBL 40. FLOOORBEAM UPPER CHORD REPAIRED IAW SRM 53-00-51, FIG 201. REPAIR 2.

Part: STRINGER — CRACKED (BS 434 S38L) · airframe 77,364 hrs · 33,337 cycles

STRINGER FOUND CRACKED AT FS 434 -456 STR38L. REPAIRED CARRIED OUT IAW SRM 53-00-03, REPAIR 2.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 77,341 hrs · 33,333 cycles

EMERGENCY LGITHS AT SEAT 30GF ARE INOPERATIVE. MX REPAIRED DAMAGED WIRE ON SEAT HARNESS. SYS OPS IS GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 75,266 hrs · 32,717 cycles

GOUGE AFT OF FWD CARGO DOOR. REPAIRED DAMAGED PER SRM 53-00-01.

Part: WIRE — SHORTED (EMERGENCY LIGHT) · airframe 75,156 hrs · 32,688 cycles

EMERGENCY LIGHTS AT ROW 6EF ARE INOPERATIVE. MAINTENANCE FOUND THE SEAT HARNESS DISCONNECTED AND SHORTED WIRES AND RESEATED WIRES PER 33-51-31 WDM. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,933 hrs · 32,348 cycles

EMERGENCY PATH LIGHTS AT R2 DOOR IN LAV WALL IS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: FAILSAFE — CRACKED (FS 966) · airframe 71,907 hrs · 31,794 cycles

A CRACK WAS FOUND DURING INSPECTION OF THE FAILSAFE FITTING IN THE RT AND LT MLG WELLS. REPAIR IAW ERA 481063-14.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 71,709 hrs · 31,740 cycles

ON A CHECK, FOUND EMERGENCY PATH LIGHTS CONNECTOR AT SEAT 34GF BROKEN AND REPLACED HARNESS. SYS OPERATION IS NORMAL.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 71,059 hrs · 31,571 cycles

DURING A CHECK MX, FOUND AN EMERGENCY LIGHT CONNECTOR AT SEAT 25AB BROKEN AND REPLACED. SYS OPS IS NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 70,334 hrs · 31,368 cycles

EMERGENCY LIGHTS AT SEATS 27AB AND 27FG ARE INOPERATIVE. MX REPAIRED THE POWER CONNECTION AT SEAT 27A. SYS OPS IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,861 hrs · 30,993 cycles

AFT EXTERIOR EMERGENCY LIGHTING ON RT AND LT SIDE OF FUSELAGE IS INOPERATIVE. MX REPLACED THE BATTERY PACK UNIT AND RE-LAMPED THE EXTERIOR LIGHTS. SYS OPERATION IS NOW NORMAL.

Part: FAILSAFE — CRACKED (LT MLG WW) · airframe 68,807 hrs · 30,978 cycles

THE LT SIDE FAILSAFE FITTING PASSED THE HFEC AND ULTRASONIC INSPECTIONS IAW SI 01-086393-12AD. A CRACK INDICATION WAS FOUND ON THE RT SIDE FAILSAFE FITTING IAW SI 01-086393-12AD WHICH REQUIRES REPAIR SO MX ELECTED TO ACCOMPLISH THE REPAIR/MOD TO THE LT SIDE FAIL SAFE FITTING TO TERMINATE THE REPEAT INSP REQUIREMENTS. REPAIRED IAW ERA 481061-14AD REVISION 1.

Part: FAILSAFE — CRACKED (MLG WW) · airframe 68,807 hrs · 30,978 cycles

A CRACK INDICATION WAS FOUND AT THE LOWER BOLT HOLE DURING THE ULTRASONIC INSP OF THE FAILSAFE FITTING IN THE RT MLG WHEEL WELL IAW SI 01-086393-12AD. REPAIRED IAW ERA481062-14AD REV 1.

Part: SKIN — CORRODED (BS 772 S36R) · airframe 63,176 hrs · 29,269 cycles

FUSELAGE SKIN CORROSION AT FS 772, S-36R LAP JOINT. DAMAGED SKIN CUT OUT AND REINFORCED WITH EXTERNAL DOUBLERS.

Part: SKIN — CORRODED (BS 772 S36R) · airframe 63,176 hrs · 29,269 cycles

MX REPORTED FINDING TWO PULLED FASTENERS AT THE STRINGER 36R LAP JOINT AT APPROX FS 772. AFTER FURTHER EVALUATION MX FOUND THE LOWER SKIN INTERNAL TO THE LAP JOINT WITH CORROSION DAMAGE. REPAIRED IAW ERA 467891-14.

Part: DRIVE ASSY — FAILED (LE FLAPS) · airframe 62,539 hrs · 28,991 cycles

DURING APPROACH LEADING EDGE DISAGREE FSEU FAULTS O/B SLAT PDU RVDT M548 AND FLAP LEVER RVDT MIS R M603. FLAPS SLATS RUN NML. RAN FLAPS SEVERAL MORE TIMES AND SLATS LOCKED UP WITH SAME FAULTS AS BEFORE. REPLACED SLAT PD RVDT NR 2 NEEDS RIG. REMOVED AND REPLACED FLAP HANDLE POSITION RVDT PER AMM. RIGGED PDU RVDT PER AMM. RAN FLAPS SEVERAL TIMES CK GOOD.

Part: SPAR — GOUGED (LT WING) · airframe 62,278 hrs · 28,888 cycles

LT WING FRONT SPAR WEB DENTED/GOUGED. CUTOUT DAMAGE AND INSTALLED A REPAIR DOUBLER.

Part: FRAME — CORRODED (MLG ATTACH) · airframe 60,298 hrs · 28,234 cycles

DURING HMV INSPECTION FOUND RT MLG SUPPORT BEAM SIDE FRAME LUG FWD FLANGE AND BORE SURFACE HAD PITTING CORROSION. FLANGE AND BORE SURFACE CORROSION REMOVED PER SRM 53-50-90.

Part: BULKHEAD — CRACKED (BS 1725) · airframe 60,298 hrs · 28,234 cycles

BULKHEAD OUTER CORD STRAP FOUND CRACKED AT STRINGER-7R BS 1725 (AREA APPROX 1"). REPAIRED PER ERA 461617-14AD. REQUIRES REPETITIVE INSPECTION AT 37,500 CYCLES.

Part: SKIN — CRACKED (FS 1725 S7R) · airframe 60,298 hrs · 28,234 cycles

DURING INSPECTION OF THE FS 17.25 SKIN AND CHORD STRAP AREA AT S-7R PER 01-451043-03AD, CRACKS WERE FOUND. THE EA PROVIDED A CRACK REPAIR PER 767 SRM 53-80-01 REPAIR 5, HOWEVER THE CRACK EXTENDED OUTSIDE OF THE TYPICAL AREA. DUE TO THIS, BOEING WAS CONTACTED AND PROVIDED AMOC 8100 APPROVAL OF A MODIFIED SRM REPAIR PER ERA 461617-14AD.

Part: FLOORBEAM — CORRODED (BS 654) · airframe 60,298 hrs · 28,234 cycles

FWD CARGO COMPT FLOORBEAM CHORD FOUND AT STATION 654+110 LBL 20 AND REPAIRED ON NR 52120 SRM 53-00-07 FIGURE 201, REPAIR 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,298 hrs · 28,234 cycles

FWD CARGO COMPT FLOORBEAM CHORD FOUND CORROSION AT STA 434 RBL44 AND WAS REPAIRED ON SRM 53-00-07 FIG 201 REPAIR SCHEME ON NR 520726.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,298 hrs · 28,234 cycles

FWD CARGO COMPT FLOORBEAM CHORD CORRODED AT STA 456 RBL 44 AND REPAIRED PER 53-00-07 FIG 201 ON NR 52071

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 60,298 hrs · 28,234 cycles

CABIN BS 996 TO 999 LBL 33 FLOOR SUPPORT LWR FACE FOUND CRACKED - REPAIRED PER SRM 53-00-51 REPAIR 3

Part: FLOORBEAM — CORRODED (CABIN) · airframe 60,298 hrs · 28,234 cycles

CABIN BS 325, 20 TO 25 FLOORBEAM UPPER SURFACE FOUND CORRODED REPAIRED ON NR 51553.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 60,298 hrs · 28,234 cycles

CABIN BS 998 TO 999 RBL SEAT TRACK LWR FACE FOUND CRACKED. REPAIRED ON NR 515558.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 60,298 hrs · 28,234 cycles

CABIN BS 998 TO 999 RBL FLOOR SUPPORT LWR FACE FOUND CRACKED. REPAIRED PER 53-00-51 FIG 201 ON NR 515601.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,298 hrs · 28,234 cycles

CABIN BS RBL 15 TO 40 FLOOR BEAM FOUND CORRODED, REPAIRED ON NR 51179 PER 53-00-01 FIG 101.

Part: SLIDE — UNSERVICEABLE (PAX DOOR) · airframe 60,298 hrs · 28,234 cycles

RT FWD DOOR SLIDE RELEASE CABLE FOUND DETACHED DURING DOOR INSPECTION, THE R-1 DOOR SLIDE HAS BEEN REPLACED, S/N OFF PA0828.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 60,298 hrs · 28,234 cycles

UPON REMOVAL OF THE R1 DOOR SLIDE BUSTLE IT WAS DISCOVERED THAT THE DOOR SLIDE HAD BECOME PARTIALLY UNLACED. IT APPEARS THAT ONE OF THE CABLES THAT ACTUATE THE CAM BAR WHICH RELEASES THE TENSION ON THE LACING CORDS WAS SOME HOW RELEASED. THE SLIDE WAS REPLACED ON NRC 50024.

Part: UNKNOWN — ODOR (CABIN) · airframe 60,183 hrs · 28,192 cycles

FLIGHT ATTENDANTS REPORT BURNING SMELL IN CABIN. ELECTRICAL COMPONENT ODOR, SUSPECTED POSSIBLE LIGHTING PROBLEM. INSPECTED A/C CABIN MID SECTION WITH NO DISCREPANCIES NOTED CHECKED LOWER CARGO COMP ALL OK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,174 hrs · 28,190 cycles

FUSELAGE SKIN CRACKED AT STA 1197+99 AND BL0. CUT OUT CRACK AND INSTALLED REPAIR DOUBLER AND TRIPLER.

Part: ENGINE — FAILED (NR 2) · airframe 59,777 hrs · 28,021 cycles

DURING DESCENT INTO MCO, RT ENG FAILED. UNKNOWN REASON FOR FAILURE NO VIBRATION OR NOISES NO BY CREW. A/C WAS LEVEL AT 11000 FEET RUNNING FINE. CLEARED TO 9000 FEET RT ENGINE FAILED TO RESPOND AT 9000 FT. CARD MESSAGE. T/S PER FIM BOROSCOPED HPC ALL NML. PERFORMED BORESCOPE INSPECTION OF HPC PER FIM 71-05-00. NO DAMAGE FOUND REMOVED AND STARTED INSTALLATION OF NEW MEC. REMOVED FUEL PUMP AND STARTED INSTALL PER AMM. FOUND FUEL FILTER BOWL ASSY DAMAGED. PERFORMED WINDMILL CHECK ALL NML. FOUND TO PWR RUN. ALL TESTS NORMAL.

Part: FAN — DEFECTIVE (E/E BAY) · airframe 58,158 hrs · 27,447 cycles

FWD EQUIP EXHAUST FAN STATUS MSG. STRONG ELECTRICAL SMELL AND C/B POPPED ON P6 PANEL. FWD TO MCO AND PLAC PER MEL 21-58-04B. FWD EQUIP EXH FAN C/B COLLARED. VISUALLY INSPECTED FWD EQUIPT EXH FAN. NO VISUAL DAMAGE TO FAN OR SURROUNDING AREA. REPLACED FAN, RESET SYSTEM - ALL OPN NOW NORMAL. MCO/PLAC REMOVED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 57,472 hrs · 27,209 cycles

THE FUSELAGE SKIN WAS STRUCK BY A PLATFORM AND WAS GOUGED AND DENTED OVER A 15 INCH LENGTH. THE DAMAGE WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 57,472 hrs · 27,209 cycles

THE FUSELAGE SKIN SUSTAINED GROUND DAMAGE FROM A WORK PLATFORM. THE GOUGE IS APPROXIMATELY 40 IN. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — DELAMINATED (HORIZONTAL STAB) · airframe 53,533 hrs · 25,649 cycles

THE UPPER SKIN OF THE LT HORIZ STABILIZER WAS FOUND WITH AN AREA OF DELAMINATION ON THE UPPER AND LOWER SURFACE OF THE ALUMINUM HONEYCOMBE SANDWICH ASSEMBLY. THE DELAMS WERE REMOVED WITH A 14 X 8 INCH CUTOUT AND A 13 X 9 INCH CUTOUT. THE CUTOUTS WERE REPAIRED WITH AN ALUMINUM DOUBLER METAL BOND REPAIR PROCEDURE PER ER/A 096372-14.

Part: SKIN — DELAMINATED (HORIZONTAL STAB) · airframe 53,533 hrs · 25,649 cycles

DELAMINATION WAS FOUND ON FWD TORQUE BOX SKIN OF LT HORIZONTAL STABILIZER. DAMAGE WAS LOCATED ON UPPER SKIN, AT FRONT SPAR STA 108. REPAIRED PER ERA 096372-14.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,993 hrs · 24,850 cycles

EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP ON RIGHT SIDE. REMOVED AND REPLACED BATTERY SUPPLY.

Part: WIRE — BROKEN (CABIN) · airframe 51,757 hrs · 24,736 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 26F INOP. REPAIRED BROKEN WIRES AT CONNECTOR, CHECKS GOOD.

Part: COVER — MISSING (CABIN) · airframe 51,757 hrs · 24,736 cycles

SEAT 4EF MISSING EMERGENCY LIGHT COVER ASSY. INSTALLED COVER ASSY.

Part: CAP — MISSING (NR 2 ENG PYLON) · airframe 50,895 hrs · 24,233 cycles

DURING FLIGHT, NR ENGINE PYLON DEPARTED AIRCRAFT. UNDER INVESTIGATION.

Part: BEAM — CORRODED (T/E FLAP) · airframe 49,405 hrs · 23,501 cycles

DURING REPLACEMENT OF BOLTS IAW AD 2003-11-16, CORROSION WAS FOUND IN THE BORES OF THE RH WING INBOARD FLAP, OUTBOARD ATTACH FITTING. 3 OF THE 4 AFT ATTACH LOCATIONS WERE CORRODED IN THE 9-10 BEAM ASSEMBLY. THE HOLES WERE OVERSIZED TO REMOVE THE CORROSION, FREEZE PLUGGED, AND THE MODIFICATION CONTINUED WITHOUT DEVIATION. BOEING APPROVED THE SUBJECT REPAIR VIA 8110-3 FORM.

Part: SKIN — GOUGED (FUSELAGE) · airframe 49,405 hrs · 23,501 cycles

SKIN DENT AND GOUGE FOUND AT STATION 1370 AND STR 29R. REPAIR PER ER/A 385435-14

Part: MEGAPHONE — INOPERATIVE (F/C CABIN) · airframe 48,556 hrs · 23,077 cycles

FIRST CLASS MEGAPHONE INOP. REPLACED FIRST CLASS MEGAPHONE.

Part: DOOR — DAMAGED (NR 2 NACELLE) · airframe 48,258 hrs · 22,933 cycles

ON APPROACH INTO SJU RT SHOCK STRUT DOOR FELL OFF. DOOR WAS RECOVERED IN A HOUSE CARPORT, NO PERSONAL INJURIES. UPON INSPECTION FOUND TWO HYD BRAKE LINES DAMAGED. ALSO, THE TRUNNION DOOR WAS DAMAGED. REMOVED SAME, REPLACED DOOR. REPAIRED OTHER DAMAGE.

Part: ODOR — DETECTED (CABIN) · airframe 46,167 hrs · 21,918 cycles

RTB - CREW REPORTS ELECTRICAL ODOR IN MID GALLEY / CABIN AREA. ONLY DETECTABLE ODOR COMING FROM MID GALLEY LIFE RAFT STOWAGE COMPT, SEEMS TO BE COMING FROM LIFE RAFT ITSELF. RAN ENGS PACKS AND LOADED ALL ELECTRICS TAXIED A/C IN SAME CONFIG AS CREW UNABLE TO DUPLICATE. REMOVED LIFE RAFT PER MEL 25-99-02B, FWD TO MCO AND PLAC.

Part: SKIN PANEL — DELAMINATED (HORIZ STAB) · airframe 46,144 hrs · 21,904 cycles

A 2 FOOT, 6 INCH DIA AREA WAS FOUND DISBONDED ON THE LEFT HORIZONTAL STABILIZER UPPER INBOARD FORWARD SKIN PANEL BETWEEN FS 53.659 AND FS 80.896. THE DISBONDED SECTION OF HONEYCOMB CORE WAS REPLACED PER SRM 51-70-10 BY DEPT 382 ON SHOP ORDER H05277. THE PANEL WAS REINSTALLED ON THE A/C.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR) · airframe 44,685 hrs · 21,148 cycles

ON CLIMBOUT APPROX 5 MIN AFTER T/O, F/A'S REPORTED STRONG ODOR/FUMES HOT SMELL IN MID CABIN AREA. UPON TURNING OFF RT PACK SMELL WENT AWAY. RECYCLED RT PACK AND HOT SMELL RETURNED. RETURNED TO ATL. MTC IN PROGRESS. REPLACED RT ENG HPSOV AND CONTROLLER PER M/M. BOTH CHECK GOOD. RAN BOTH PACKS O OF ENG AIR AT HIGH POWER. NO SMELLS/FUMES NOTED. OK FOR SERVICE.

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR) · airframe 44,685 hrs · 21,148 cycles

ON CLIMBOUT APPROX 5 MIN AFTER TAKEOFF. FLIGHT ATTENDANT REPORTED STRONG ODOR AND HOT SMELL IN MID CABIN AREA. UPON TURNING OFF RIGHT PACK SMELL WENT AWAY. RECYCLED RIGHT PACK AND HOT SMELL RETURNED. RETURNED TO ATL. REPLACED RT ENG HP VALVE, RT HP CONTROLLER, RAN BOTH PACKS AND ENGINE AT HIGH PWR SETTINGS. THERE WERE NO FUMES OR HOT SMELL NOTICED.

Part: FSEU — SHORTED (MAIN E/E COMPART) · airframe 43,293 hrs · 20,513 cycles

AT LEVEL OFF GOT FLAP/SLAT ELEC MESSAGE C/B P11G16 POPPED SMOKE IN COCKPIT. FOUND FLAP/SLAT ELECTRONICS UNIT HAD A TRANSFORMER THAT HAD OVERHEATED. REPLACED THE FLAP / SLAT ELECTRONICS UNIT AND TESTED PER MAINT MANUAL. OPERATED FLAPS IN ALTERNATE AND NORMAL MODES ALL CHKS OK.

Part: BRACE — CORRODED (NR 1 AND 2 PYLON) · airframe 42,707 hrs · 20,236 cycles

THE BUSHINGS IN THE FORWARD AND AFT LUGS OF THE NR 1 AND 2 PYLON DIAGONAL BRACES WERE FOUND ROTATED / MIGRATED. THIS CONDITION WAS FOUND DURING REMOVAL/INSTALLATION OF THE PYLON WHICH HAD BEEN REMOVED FOR OTHER REWORK. REMOVAL OF THE BUSHINGS REVEALED MINOR CORROSION IN THE FWD BORES.

Part: STIFFENER — CRACKED (WING CENTER BOX) · airframe 42,707 hrs · 20,236 cycles

THE WING CENTER SECTION FRONT SPAR VERTICAL STIFFENER LOCATED AT LBL 10.94 WAS FOUND CRACKED AT ITS TOP END. THE DAMAGE WAS IN THE WEB OF THE STIFFENER AT THE OVERWING LONGITUDINAL FLOORBEAM TO STIFFENER JOINT.

Part: INDICATOR — LEAKING (LEFT ENG STRUT) · airframe 42,300 hrs · 20,025 cycles

DURING CLIMB LEFT HYD QTY EICAS MSG ILLUMINATED. PER POM PRIMARY PUMP SELECTED OFF AND QTY CONTINUED TO DECREASE. DEMAND PUMP SELECTED OFF WITH SAME RESULT. BOTH PUMPS OFF AND QTY STABILIZED. FOUND DPI ON LEFT HYD MODULE LEAKING. REPLACED INDICATOR AND O-RINGS. SVCD HYD SYS. LEAK CKS GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,388 hrs · 19,606 cycles

THE FUSELAGE SKIN WAS EXTENSIVELY DENTED AND GOUGED BY A GROUND EQUIPMENT STRIKE BETWEEN FS 1417 & 1439 AND BETWEEN STRINGERS 36L & 36R. THE SKIN WAS CUT AT FS 1417 AND AT FS 1439 FROM THE LAP JOINT AT STRINGER 36L TO THE LAP JOINT AT STRINGER 36R. THE SKIN CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 378668-14, REV A.

Part: FUEL LINE — LOOSE (NR 1 ENGINE)

ON DESCENT AT FL200 WITH ENGINE ANTI-ICE TURNED ON AND AUTO THROTTLES ENGAGED RT ENGINE ADV TO FULL POWER AND LT ENGINE REMAINED AT IDLE. N1 COMMAND BUG SHOWED FULL POWER REQUESTED ENGINE STAYED AT IDLE. MAINT FOUND FUEL LINE CONN AT FUEL FLOW METER LOOSE AND LEAKING. REINSTALLED MOUNT BOLTS AND SAFETIED PER M/M. MOTORED ENG NO FURTHER LEAKS RAN ENG PER PFHB IND NORM.

Part: SKIN — DENTED (BS 1241)

FUSELAGE / SKIN / STA 1241 / STRG. 33L : REPAIR FOR SKIN DENT. THE SKIN JUST AFT OF THE STA 1241 FRAME WAS FOUND DENTED AT S-33L. NO UNDELYING STRUCTURE WAS FOUND DAMAGE. THE SKIN DENT WAS CUTOUT AND REPAIRED WITH A DOUBLER PER SRM. ER/A 363147-14 WAS ISSUED TO TRACK THE DTA ASPECTS OF THE REPAIR.

Part: PSEU — FAILED (NLG)

NOSE A/G DISAGREE AND HORN WITH CONFIG WARN. BITE ON PSEU SHOWS S266 BAD. REPLACED, NO HELP. REPLACED PSEU, CKS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

LEFT AFT CABIN EMERGENCY AISLE LIGHTS DO NOT ILLUMINATE. REPLACED PWR SUPPLY M739, OPN NOW NORMAL.

Part: LIGHT — INOPERATIVE (OVERWING EXIT)

LEFT AFT EMERGENCY OVERWING LIGHT INOP. RELAMPED LEFT AFT EMERGENCY LIGHT, CHECKS GOOD.

Part: TE WEDGE — DELAMINATED (NR 12 LE SLAT)

THE RT WING NR 12 SLAT TE WEDGE WAS FOUND WITH THE UPPER SKIN DELAMINATED. THE DAMAGE LOCATION IS 3.5 INCHES FROM THE TE EDGE, 10 INCHES FROM THE I/B EDGE COVERING 3.5 DIA. ACCOMPLISHED REPAIRS PER DL ERA 273469-14 REV A.