N7542A

Part: LIGHT — INOPERATIVE (AC BAY) · airframe 65,325 hrs · 33,846 cycles

TAIL COMPARTMENT FORWARD EMERGENCY LIGHT ABOVE CATWALK INOPERATIVE. REPLACED LAMP FOR TAIL COMPARTMENT FORWARD EMERGENCY LIGHT ABOVE CATWALK. OPERATIONS CHECKED NORMAL.

Part: HEATER — MALFUNCTIONED (CARGO BAY) · airframe 64,049 hrs · 33,130 cycles

AMA - INFLIGHT DFW-ABQ. CREW REPORTED ODOR IN THE FLIGHT DECK. EMERGENCY DECLARED FLIGHT DIVERTED AMA LANDED WITHOUT INCIDENT. FOUND FORWARD CARGO COMPARTMENT HEATER POPPED CIRCUIT BREAKER AND CREATED ODOR. PLACARD FORWARD CARGO COMPARTMENT HEATER AND FLIGHT CONTINUED TO DESTINATION. REPLACED FORWARD CARGO COMPARTMENT HEATER AT RDU ON 05/14/2013. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BULLET — INOPERATIVE (NR 1 ENGINE) · airframe 61,870 hrs · 31,880 cycles

DFW - CREW REPORTED SIGNFICANT ENGINE PRESSURE RATIO SPLIT THAT BECAME WORSE AS ALTITUDE INCREASED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 ENGINE PT2 BULLET. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: UNKNOWN — SMOKE (CABIN & COCKPIT) · airframe 58,651 hrs · 30,131 cycles

DFW - CREW REPORTED SMOKE THAT WAS WHITE AND ACRID IN CABIN AND COCKPIT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE.

Part: RIB — CRACKED (LE SLAT) · airframe 56,761 hrs · 29,085 cycles

NUMBER 5 BRACKET CRACKED IN RADIUS. REMOVED AND REPLACED RIB ASSEMBLY PER ESO 27-80-1.

Part: SKIN — DAMAGED (LE SLAT) · airframe 56,704 hrs · 29,054 cycles

DAMAGE ON INBOARD COVE SKIN ON SLAT NEAR THE KNUCKLE RIB. INSTALLED FLUSH REPAIR ON SLAT COVE SKIN IAW AARD 57-50-00-04.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

SEAT TRACK NUMBER 6 DAMAGED AT STATION 207. INSTALLED SERVICEABLE TRACK PER SRM 53-05-00 FIGURE 4F.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

STATION 207 SEAT TRACK NUMBER 6 FORWARD END OF SEAT TRACK CORROSION OUT OF LIMITS OF SRM 53-01 FIGURE 1 SHEET 3. INSTALLED SEAT TRACK NUMBER 6 AND SPLICE PER SRM 53-05-00 FIGURE 4F.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

WEB STRAP ON DOOR CUTOUT BEAM WEB STATION 1174 IS CORRODED. INSTALLED NEW WEB STRAP ON DOOR CUTOUT BEAM WEB STATION 1174 LONGERON 29 RIGHT TO LONGERON 28 RIGHT PER SRM 51-30-00.

Part: WEB — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 56,671 hrs · 29,034 cycles

CORROSION ON TOP AND BOTTOM OF DOOR WEB STATIONS 1212 TO 1218 LONGERON 28 RIGHT AND LONGERON 27 RIGHT. NEW WEB SPLICE INSTALLED AT STATIONS 1200 TO 1218 FROM LONGERON 30 TO LONGERON 26 RIGHT PER WIP NUMBER 7 AND PER AARD 53-10-00-24.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,671 hrs · 29,034 cycles

CORROSION OUT OF LIMITS LEFT CUSP STATION 1094 TOP SIDE. INSTALLED CUSP REPAIR PER AARD 53-20-00-16 AND SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

CORROSION ON BOTTOM SIDE OF SUB-FLOOR STATION 199 APPROXIMATELY 9 INCHES INBOARD OF FUSELAGE WALL. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

AFT ACCESSORY 1418 FRAME CRACKED AT LONGERON 2 LEFT. INSTALLED DOUBLER PER SRM 53-03-00 FIGURE 31A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

INTERCOSTAL CRACKED AT STATIONS 1287 TO 1309. INSTALLED NEW INTERCOSTAL PER SRM 51-00-00-012.

Part: BRACKET — CRACKED (SPOILER) · airframe 56,671 hrs · 29,034 cycles

LEFT SPOILER ACTUATOR FITTING WAS FOUND CRACKED AND REPAIRED PER AARD 57-20-00-15 AND ESO 80559 DATED 12-5-08. REMOVED AND REPLACED GROUND SPOILER BRACKET PER AARD 57-20-00-15.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

RIGHT CUSP CRACKED AT STATION 240. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FRAME — WORN (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

FUSELAGE FRAME AT STATION 1041 RIGHT HAS DEEP WEAR 7 INCHES ABOVE CUSP AT FRAME FITTING. REPAIR WAS COMPLETED PER EAMD80-53-010080 AND SRM 51-70.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

RIGHT CUSP CRACKED AT STATIONS 991 TO 993. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

VERTICAL STIFFENER AT AFT BULKHEAD STATION 1338 CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-15.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

CUSP CRACKED BETWEEN STATIONS 240 TO 259, 3 PLACES CRACKS RANGE FROM 1.5 INCHES TO 2.5 INCHES. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

CUSP TEE CORRODED OUT OF LIMITS AT STATION 200 JUST AFT OF FORWARD SERVICE DOOR. INSTALLED DOUBLER PER AARD 53-20-00-14.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

SUB FLOOR CORRODED OUT OF LIMITS AT STATION 200 FORWARD OF NUMBER 6 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

CRACKED WINDOW PAN STATION 1155 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

DENT IN FUSE STATION 242 BETWEEN LONGERONS 15 AND 16 LEFT. INSTALLED DOUBLER PER BOEING REPAIR DOCUMENT SG09530001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,671 hrs · 29,034 cycles

CORROSION BEYOND LIMITS SEAT TRACK NUMBER 1 STATION 395. REMOVED CORROSION AND INSTALLED PLUG REPAIR PER AARD 53-20-00-10.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

FUSELAGE STATION 788 LEFT WINDOW PAN CRACKED AT UPPER FORWARD CORNER. DAMAGED AREA REMOVED AND DOUBLER INSTALLED PER AARD 56-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

WINDOW PAN CRACKED AT STATION 807 AT LONGERON 14 RIGHT. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

SUBFLOOR CRACKED 3 PLACES AT STATION 218 OUTBOARD OF NUMBER 2 SEAT TRACK. CRACKS MEASURE 1.5 INCHES, 2.5 INCHES AND 1.5 INCHES LONG. INSTALLED DOUBLER PER AARD 53-20-00-16 FIGURE 3 SHEET 1.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

CRACKED WINDOW PAN STATION 1174. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

CRACKED WINDOW PAN AT STATION 1022 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

WINDOW PAN CRACKED AT STATION 807 AT LONGERON 12 RIGHT. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

LEFT CUSP CORRODED BEYOND LIMITS AT STATIONS 537 TO 539 LEFT. INSTALLED DOUBLER PER AARD53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

CRACKED WINDOW PAN STATION 1060. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

RIGHT CUSP CRACKED BETWEEN LIGHTENING HOLES AT STATIONS 991 TO 993. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

G2 GALLEY TIE DOWN FITTING CORRODED BEYOND LIMITS AT STATION 218 INBOARD OF NUMBER 4 SEAT TRACK. INSTALLED REPLACEMENT TIE DOWN FITTING PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

RIGHT CUSP CORRODED BEYOND LIMITS BETWEEN STATIONS 1263 TO 1265. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

CRACKED WINDOW PAN AT STATION 1022. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

CRACKED WINDOW PAN STATION 1231. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

LEFT AFT LAVATORY/VAULT DOOR FRAME STIFFENER CRACKED. INSTALLED REPLACEMENT STIFFENER PER SRM 51-30.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

CRACKED WINDOW PAN STATION 1079. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

CRACKED WINDOW PAN STATION 1041. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

CRACKED WINDOW PAN AT STATION 946 LEFT UPPER FORWARD SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

CRACKED WINDOW PAN STATION 1060 AFT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,671 hrs · 29,034 cycles

CRACKED WINDOW PAN STATION 1060. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,671 hrs · 29,034 cycles

PREVIOUS DENT AT STATION 1242 LONGERON 24 LEFT. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 38 SHEET 22.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,262 hrs

LGA - FLOOR EXIT SIGN ACROSS FROM FORWARD LAVATORY INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR FLOOR EXIT SIGN ACROSS FROM FORWARD LAVATORY.

Part: BATTERY — NOT SEATED (CABIN) · airframe 54,262 hrs

LGA - CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED BATTERIES IN CHARGER FOR CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES.

Part: BATTERY — NOT SEATED (CABIN) · airframe 54,262 hrs

LGA - TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERIES IN CHARGER.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 53,680 hrs

DFW - TAIL COMPARTMENT SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR TAIL COMPARTMENT SLIDE LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 53,680 hrs

DFW - EMERGENCY PATH LIGHTING ON AFT GALLEY CEILING PANEL INOPERATIVE. REPLACED LAMPS FOR EMERGENCY PATH LIGHTING ON AFT GALLEY CEILING PANEL.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 53,680 hrs

DFW - EMERGENCY PATH LIGHTING LENS FROM SEAT 7D MISSING. REPLACED LENS FOR EMERGENCY PATH LIGHTING AT SEAT 7D.

Part: LENS — WRONG PART (EMERGENCY LIGHTS) · airframe 53,680 hrs

DFW - SEAT 21D HAS WRONG COLOR LENS ON EMERGENCY PATH LIGHTING. REPLACED LENS ON SEAT 21D FOR EMERGENCY PATH LIGHTING.

Part: ENGINE — MAKING METAL (NR 1) · airframe 53,468 hrs · 27,281 cycles

DFW INFLIGHT - CREW REPORTED NUMBER ONE ENGINE OIL CLOG INDICATION. REDUCED NUMBER ONE ENGINE TO IDLE AND RETURNED TO DFW. LANDED WITHOUT INCIDENT. FOUND METAL IN OIL FILTER. REPLACED NUMBER ONE ENGINE AT DFW ON 31 JAN 2009.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 53,087 hrs · 27,071 cycles

STIFFENER ON AFT SIDE OF FRAME STATION 1418 AT LONGERON 2R IS CRACKED AT ATTACH POINTS. REPAIRED PER SRM 53-01-00.

Part: FRAME — CRACKED (ZONE 200) · airframe 53,087 hrs · 27,071 cycles

FRAME CRACKED AT STATION 1418 LONGERON 2L. REPAIRED PER SRM 53-01-00 FIGURE 2.

Part: FITTING — CRACKED (ZONE 500) · airframe 53,087 hrs · 27,071 cycles

CRACK IN GROUND SPOILER ACTUATOR FITTING LEFT WING. REPAIRED PER AARD 57-20-00-15 AND ESO 80559 DATED 12-05-08.

Part: FRAME — CRACKED (ZONE 100) · airframe 53,087 hrs · 27,071 cycles

CANT FRAME CRACKED STATION 1510 BELOW MAIN LIGHT SWITCH LEFT SIDE AT TAIL CONE ALIGNMENT PIN. INSTALLED DOUBLER PER EA MD80 53-005083.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,087 hrs · 27,071 cycles

SHEAR TIE CRACKED AFT SIDE OF STATION 1451 FRAME AT LONGERON 2R. REPLACED WITH SERVICEABLE SHEAR TIE PER SRM 53 01.

Part: FRAME — CRACKED (ZONE 100) · airframe 53,087 hrs · 27,071 cycles

FRAME CRACKED, STA 1510 BELOW RT LOWER TAIL CONE LATCH AT 2 EACH ALIGNMENT PINS. INSTALLED REPAIR DOUBLER IAW 53-005083.

Part: ACM — SEIZED (A/C BAY)

TUS INFLIGHT T1540/24AUG. CREW REPORTED BURNING SMELL IN CABIN AND COCKPIT AND FLIGHT ATTENDANT REPORTED LIGHT SMOKE INSIDE AFT STAIR AREA. RETURNED TO TUS AND LANDED WITHOUT INCIDENT. FOUND RT AIRCONDITIONING PACK AIR CYCLE MACHINE HAD SEIZED. REPLACED RT PACK AIR CYCLE MACHINE. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,946 hrs · 51,946 cycles

LGA - EMERGENCY LIGHTS AT REAR SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT REAR SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN AFT CABIN FOR TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT STATION 909R FOR AFT OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DEN - OVERHEAD EMERGENCY LIGHTS AT ROW 26 INOPERATIVE. REPLACED BATTERY PACK B5-106 FOR OVERHEAD EMERGENCY LIGHTS AT ROW 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY CEILING LIGHTS BETWEEN AFT LAVATORIES IS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY CEILING LIGHTS BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SAN EMERGENCY EXIT LIGHT SWITCH AT THE FORWARD FLIGHT ATTENDANT PANEL LEFT ON. REPLACED ALL EMERGENCY LIGHT BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (CABIN)

DFW OVERHEAD EMERGENCY LIGHT AT ROW 28 INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR OVERHEAD EMERGENCY LIGHTS FOR ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUCTURE — CORRODED (FUSELAGE)

TUL - FOUND CORRODED STATION 1155-1212. DOUBLER INSTALLED PER AARD 53-10-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 3 SEAT TRACK CORRODED FROM STATION 1174-1287. SPLICE INSTALLED FROM STATION 1174-1287 PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 2 SEAT TRACK CORRODED BEYOND LIMITS ON SEAT AT STATIONS 1287-1288. MECHANIC INSTALLED SEAT TRACK REPAIR PLUG PER SRM 53-05. (M)

Part: SKIN — DENTED (FUSELAGE)

DFW - FOUND TWO LARGE DENTS WITH CREASES, STATION 427 TO 439, ABOVE AND BELOW BOTH SIDES OF LONGERON 24L. CUT OUT DAMAGE ON UPPER FORWARD DENT, COLD WORKED AND DYE CHECKED LOWER AFT DENT, INSTALLED PLUG AND INTERNAL FINGER DOUBLER PER SRM 53-04, FIGURE 38, SHEET 24. (M)

Part: SKIN — GOUGED (FUSELAGE)

DFW - FOUND DEEP DENT WITH GOUGE, STATION 351, BELOW LONGERON 27L. CUTOUT DAMAGED AREA, PLUGGED AND INSTALLED INTERNAL FINGER DOUBLER PER SRM 53-04-00, FIGURE 38, SHEET 24. (M)

Part: SKIN — GOUGED (FUSELAGE)

DFW - FOUND STATION 281 OUTBOARD OF LONGERON 26L, OUTER SKIN GOUGED. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53-04. (M)

Part: SKIN — DAMAGED (FUSELAGE)

DFW - FOUND AIRCRAFT FUSELAGE DAMAGE, LEFT SIDE OF FUSELAGE, STATION 278 TO 398 LONGERON 21L TO 26L. CUT OUT DAMAGED SKIN AND STRUCTURE. REPAIRED SKIN PER SRM 53-04, REPAIRED FRAMES PER SRM 53-03 (Z FRAME) 53-10-00-17 (J ANGLE). REPAIRED FORMERS (SHEAR TIES) PER SRM 53-03 FIG 6 AND 7 AND REPAIRED LONGERONS, NEW SPLICED IN SECTIONS PER SRM 53-02 INCH (FLUSH SKIN PANEL REPAIR). INCORPORATED ESO'S 80559 DATED 2/15/2002 80559 DATED 2-5-2002, ESO 80559 DATED 2/5/2002. (M)

Part: ACM — LEAKING (ACM BAY)

DFW - FLT 347 - DURING CLIMB THROUGH ABOUT 20000 MGL, A STRONG ODOR OF FUEL WAS PRESENT IN THE CABIN AND IN THE COCKPIT WHEN LEFT PACK WAS TURNED OFF. THE SMELL DISSIPATED WHEN BOTH PACKS BACK ON. DURING CRUISE, THE ODOR RETURNED. AIR CYCLE MACHINE LEAKING OIL ON TURBINE. REPLACED AIR CYCLE MACHINE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SENSOR — OUT OF ADJUST (MLG DOOR)

DTW - FLT 2080 - EN ROUTE DFW-DTW, WHEEL GEAR DOOR OPEN LIGHT ILLUMINATED IN CRUISE. TURNED RIGHT HYDRAULIC PUMP ON HIGH TO KEEP LIGHT EXTINGUISHED. LANDED DTW WITHOUT INCIDENT. ADJUSTED GAP ON GEAR DOOR PROXIMITY SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STATOR — FAILED (RT ENGINE)

DFW - FLT 1171 - DURING CLIMB-OUT AT 20,000 FT F/A REPORTED LOUD NOISE. 5 MINUTES LATER, AT 31,000 WHILE LEVELING OFF, RT ENGINE HAD 3 MAJOR COMPRESSOR STALLS THEN ENG FAILED TO PRODUCE POWER. ACCOMP EMERG DIVERSION TO DFW. RAN ENG TO IDLE TO TOUCHDOWN, ENG COULD NOT PRODUCE ANY POWER WITH THROTTLE MOVEMENT. OIL PRESS WAS NORMAL AND RT OIL TEMP HIGH AT 130 DEGREES. REPLACED RT ENG, PERFORMED ENG RUN UP. SYSTEM GROUND CHECKED NORM OPS.INSPECTION OF THE ENG REVEALED VERY HEAVY DAMAGE TO THE FAN BLADES. THE FAN HADAPPROX 10 FAN BLADES WITH DAMAGE THAT APPEARED TO BE CAUSED BY ICE INGESTION. THE DAMAGE CONSISTED OF HEAVY TIP CURL, THE WORST HAD APPROX 1.5 INCH DEFLECTION WITH NO NICK OR TEARS. THE HEAVY

Part: BALLAST — FAILED (ROW 11 AB)

RDU - FLT 1275 - DURING FLIGHT, ELECTRICAL FUMES WERE NOTED IN FORWARD COACH. MAINTENANCE FOUND A FAULTY LIGHT BALLAST AT SEAT ROW 11AB. REPLACED LIGHT BALLAST OVER SEAT ROW 11AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (LDG GEAR LEVER)

DFW - FLT 2034 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, GEAR UNSAFE LIGHT ILLUMINATED WITH NO ABNORMAL HYDRAULIC QUANTITY OR PRESSURE INDICATIONS. RECYCLED LANDING GEAR AND LANDING GEAR EXTENDED AND LOCKED NORMALLY. AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED LANDING GEAR LEVER SWITCH S1-89. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)