N596AA

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 65,604 hrs · 27,962 cycles

MID CARGO - AFT LOWER DOOR STOP PAD BRACKET ON DOOR IS CRACKED. INSTALLED DOOR STOP PAD FITTING PER ARRD 51-00-05-1.

Part: COMPUTER — INOPERATIVE (LE SLAT) · airframe 65,604 hrs · 27,962 cycles

DFW - CREW REPORTED WHEN FLAPS WERE SELECTED TO 15 DEGREE, AUTO SLAT FAIL LIGHT ILLUMINATED AND SLAT DISAGREE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH SWC. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PAN — CRACKED (FUSELAGE) · airframe 65,544 hrs · 27,937 cycles

RIGHT WINDOW AT STATION 1221, WINDOW RING PAN HAS CRACK AT RADIUS AFT UPPER LOCATION IN PAN. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SLIDE — DAMAGED (ENTRY DOOR) · airframe 64,616 hrs · 27,463 cycles

FLIGHT ATTENDANT REPORTED FORWARD ENTRY DOOR EVACUATION SLIDE LANYARD AND SLIDE PACK TAIL DAMAGED. REPLACED FORWARD LEFT NUMBER 1 ENTRY DOOR EVACUATION SLIDE.

Part: SENSOR — FAULTY (LE SLAT) · airframe 61,229 hrs · 25,753 cycles

DFW - CREW REPORTED SLAT OVERSPEED WARNING FOLLOWED BY SLAT DISAGREE WARNING ON CLIMBOUT. REDUCED SPEED AND WARNING STOPPED IMMEDIATELY. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FAULTY LEFT WING SLAT SENSOR C. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BRACKET — BROKEN (LT MLG WW) · airframe 60,726 hrs · 25,498 cycles

PHX - CREW REPORTED LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING CLIMBOUT. GEAR WAS CYCLED WITH NO CHANGE IN WARNING LIGHT. FLIGHT RETURNED PHX LANDED WITHOUT INCIDENT. FOUND BROKEN BRACKET IN LEFT WHEEL WELL WHICH HOLDS THE UP AND LOCKED PROXIMITY SENSOR. REPLACED CRANK ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

CORE BOLTS IN AFT CARGO DOOR BEAM ARE CORRODED. INSTALLED BEAM DOUBLER PER AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

RIGHT CUSP CORRODED BEYOND LIMITS FROM STATIONS 218 TO 221 JUST OUTBOARD OF NUMBER 6 SEAT TRACK. REMOVED AND REPLACED CUSP SHEET FROM STATIONS 218 TO 237 PER AARD 53-20-00-16 AND EA MD80-51-011436.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

NUMBER 5 SEAT TRACK UPPER OUTBOARD FLANGE CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK FROM STATIONS 200 TO 248 PER SRM 53-05-00 FIGURE 4F.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

CORROSION ON AFT CARGO DOOR FRAME WEB BEYOND LIMITS STATIONS 1206 TO 1218. REMOVED DAMAGE AND INSTALLED NEW WEB SPLICE PER AARD 53-10-00-24.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

AFT CARGO, CORROSION IN LONGERON 30 SPLICE AT STATIONS 1293 TO 1299. REPLACED SPLICE PER SRM 51-30-05 AND EA MD80-51-011436.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

G2 GALLEY OUTBOARD MOUNT CORRODED. INSTALLED NEW GALLEY MOUNT PER SRM 51-30-05.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

RIGHT AFT TIE DOWN TRACK CORRODED. REPLACED RIGHT AFT TIE DOWN TRACK PER SRM 51-30-01.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

STATION 218 INBOARD FITTING CORRODED. INSTALLED NEW FITTING PER SRM 51-30-05.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

CORROSION ON SUBFLOOR STATIONS 200 TO 218 BETWEEN NUMBER 5 AND 6 SEAT TRACKS. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 58,428 hrs · 24,419 cycles

LONGERON 2 LEFT CRACKED AFT OF STATION 1418. INSTALLED LONGERON SPLICE REPAIR AT STATION 1418 LONGERON 2 LEFT PER AARD 53-30-00-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

NUMBER 2 SEAT TRACK CORRODED BEYOND LIMITS STATIONS 1302 TO 1307. REMOVED AND REPLACED SEAT TRACK FROM STATIONS 1222 TO 1309 PER SRM 53-05-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

SEAT TRACK NUMBER 6 STATIONS 215 TO 216 CORROSION BEYOND LIMITS. INSTALLED REPAIR STRAP AT NUMBER 6 SEAT TRACK STATIONS 215 TO 222 PER EA MD8053-011490.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

STATION 218 INBOARD AFT GALLEY FITTING UNDER LILLIE PAD HAS CORROSION. INSTALLED NEW FITTING PER SRM 51-30-05.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

CORROSION ON SUBFLOOR BELOW GALLEY TIE DOWN FITTING STATION 218 INBOARD OF NUMBER 4 SEAT TRACK OUT OF LIMITS. CUTOUT CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

CORROSION ON SUB FLOOR UNDER G-1 DRAIN PAN. INSTALLED DOUBLER ON SUB-FLOOR UNDER G-1 DRAIN PAN PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

CORROSION ON G1 GALLEY MOUNT STA 160 RBL 50. INSTALLED NEW GALLEY MOUNT PER SRM 51-30-02 AND 51-30-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,428 hrs · 24,419 cycles

AFT CARGO HAS A CRACK IN INTERCOSTAL BETWEEN CABIN FLOORBEAMS STA 1287-1309 AT AIRCRAFT CENTER LINE. REMOVED AND INSTALLED NEW INTERCOSTAL STA 1287 TO 1309 SRM 51-30-05.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

AFT CARGO HAS CORROSION ON FRAME 1271 BETWEEN LONGERON 28L-29R. INSTALLED J-ANGLE REPAIR PER EA NUMBER MD80-53-011489 DATED 6-27-2010.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

CORROSION ON G1 GALLEY MOUNT STA 160 RBL 44. INSTALLED NEW GALLEY MOUNT PER SRM 51-30-02 AND 51-30-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,428 hrs · 24,419 cycles

STATION 1418 FRAME CRACKED AT LONGERON 2 RIGHT. STOP DRILLED CRACKS AND INSTALLED DOUBLERS ON FORWARD AND AFT SIDES OF STATION 1418 PER AARD 53-10-00-15 AND SRM 53-03-00.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 58,428 hrs · 24,419 cycles

CORROSION ON LONGERON 30 STATIONS 1285 TO 1293. REMOVED CORRODED LONGERON INSTALLED NEW LONGERON AND SPLICE PER SRM 53-02-00.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,428 hrs · 24,419 cycles

FUSELAGE FORWARD CRACK IN BULKHEAD AT UPPER LEFT RADOME GUIDE PIN AT LOWER FASTENER. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-19.

Part: CUSP WEB — CORRODED (CABIN) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

LEFT CUSP CORROSION OUT OF LIMITS STATIONS 639 TO 667. INSTALLED NEW CUSP DOUBLER PER AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,428 hrs · 24,419 cycles

FUSELAGE SKIN CRACKED AT NOSE LANDING GEAR DOOR HINGE CUTOUT. STOP DRILLED CRACK INSTALLED DOUBLER REPAIR PER SRM 53-05-00 FIG 62.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,428 hrs · 24,419 cycles

CABIN - LEFT CUSP HAS CORROSION AT STATIONS 452 TO 458. REMOVED CORRODED CUSP AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: RIB — CRACKED (LE SLAT) · airframe 58,428 hrs · 24,419 cycles

RIGHT NUMBER 5 SLAT RIB NUMBER 15 CRACKED. REPLACED DAMAGED OUTBOARD RIB NUMEBR 15 WITH NEW ONE ON SLAT 5 PER IAW ESO 80117.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 58,428 hrs · 24,419 cycles

CRACK IN LEFT CUSP AT STATION 218 INBOARD OF NUMBER 2 SEAT TRACK. REPAIRED PER AARD 53-20-00-16.

Part: WEDGE — DENTED (TE FLAP) · airframe 58,428 hrs · 24,419 cycles

INBOARD FLAP WEDGE ON INBOARD FLAP HAS 3 DENTS. TWO DENTS REMOVED BY DRILLING AND THIRD DENT REMOVED BY CUTTING 1 INCH HOLE. DYE CHECKED AREA FOR CRACKS, NONE FOUND. PLUGGED THE DRILLED HOLES WITH RIVETS PER SRM 57-01-00, FIGURE 2 SHEET 2. REPAIRED 1 IN HOLE WITH FLUSH REPAIR PER SRM 57-01-00 FIGURE 5 SHEET 2 AND FIGURE 8 SHEET 1. USED TI-6AL-4V FOR DOUBLER PER AARD 51-60-00-05.

Part: RIB — CRACKED (LE SLAT) · airframe 58,428 hrs · 24,419 cycles

RIGHT NUMBER 5 SLAT RIB NUMBER 14 CRACKED. REPLACED NUMBER 14 ATTACHED RIB 2ND FROM OUTBOARD POSITION NUMBER 5 RIGHT SLAT PER ESO 80117.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 58,428 hrs · 24,419 cycles

DAMAGE TO CUSP STATIONS 1083 TO 1085. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,428 hrs · 24,419 cycles

FUSELAGE DENT FOUND STATION 218 BETWEEN LONGERON 16 LEFT AND 17 LEFT. INSTALLED INTERNAL DOUBLER AS PER SRM 53-04-02 DRAWING SG09530001.

Part: PAN — CRACKED (WINDOW) · airframe 58,428 hrs · 24,419 cycles

WINDOW PAN CRACKED AT FORWARD LOWER CORNER AFT SIDE OF STATION 1060 RIGHT. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,428 hrs · 24,419 cycles

WINDOW PAN CRACKED AT UPPER FORWARD CORNER AFT SIDE OF STATION 927 RIGHT. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,959 hrs · 24,199 cycles

DURING EMERGENCY LIGHT TEST FOUND AFT CABIN EMERGENCY LIGHTS INOPERATIVE FROM ROW 27 AFT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK FOR AFFECTED AREA. EMERGENCY LIGHTS OPS CHECKS NORMAL ON RETEST.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,959 hrs · 24,199 cycles

DURING EMERGENCY LIGHT TEST FOUND FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. EMERGENCY LIGHTS OPS CHECK NORMAL ON RETEST.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,716 hrs · 24,094 cycles

EXTERIOR FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 57,716 hrs · 24,094 cycles

SEAT 28D ESCAPE PATH SEAT LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,716 hrs · 24,094 cycles

OVERHEAD EMERGENCY POWER LIGHT AT SEAT 7C INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY POWER LIGHT AT SEAT 7C, OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,532 hrs

LGA - STRIP EXIT LIGHTS AT OVERWING LEFT AND RIGHT EXITS INOPERATIVE. REPLACED BATTERY PACKS FOR STRIP EXIT LIGHTS AT OVERWING LEFT AND RIGHT EXITS.

Part: CONTROL MODULE — INOPERATIVE (CABIN) · airframe 55,532 hrs

LGA - STRIP EXIT LIGHTS AT OVERWING LEFT AND RIGHT EXITS INOPERATIVE. REPLACED CONTROL MODULE FOR STRIP EXIT LIGHTS AT OVERWING LEFT AND RIGHT EXITS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,532 hrs

LGA - CEILING EXIT LIGHTS FROM ROWS 21 TO 27 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EXIT LIGHTS FROM ROWS 21 TO 27.

Part: REGULATOR VALVE — ODOR (CABIN PRESSURE) · airframe 55,106 hrs · 22,900 cycles

STL CREW REPORTED BURNING ODOR IN CABIN. RETURNED STL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AC PILOT PRESSURE REGULATOR AND LEFT AIR CONDITIONING REGULATOR VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 53,757 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD FORWARD ENTRY DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SCHRADER VALVE — INOPERATIVE (NOSE GEAR STRUT)

BOS INFLIGHT T631/14JUL - CREW REPORTED NOSE GEAR TAKEOFF WARNING. UNABLE TO RETRACT NOSE LANDING GEAR. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. INSPECTED AND COMPLETED NOSE LANDING GEAR STRUT REPACK. REPLACED THE SCHRADER VALVE AND PACKING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWITCH — INOPERATIVE (MLG)

STL - DURING APPROACH FIRST ATTEMPT AT GEAR EXTENSION RESULTED IN ALL THREE RED LIGHTS ILLUMINATING AND GEAR DOOR OPEN LIGHT ILLUMINATED. SECOND ATTEMPT SAME RESULT. PUMPS ON GOOD FLUID AND PRESSURE. EMERGENCY EXTENSION CHECKLIST STARTED. GEAR SHOWED ALL SAFE INDICATIONS. LANDED STL WITHOUT INCIDENT. REPLACED THE LANDING GEAR LEVER SWITCH 51 89. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEA - EMERGENCY LIGHTS NEAR B5-23 INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 7 MISSING. REPLACED EMERGENCY EXIT LIGHT AT SEAT 7. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PLATE — CORRODED (HORIZ STAB)

TUL - FOUND RIGHT INBOARD HORIZONTAL STAB PIVOT BEARING LUG PLATES ARE CORRODED. REPLACED RIGHT INBOARD HORIZ STAB LUG PLATES AND MACHINED PIVOT BORE PER FCDKF0488A, 9, D/E. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FORWARD ENTRY DOOR TORQUE BOX INNER SKIN EXTENSION CRACKED STATION 207 AT LONGERON 15L. INSTALLED DOUBLER PER AARD 53-10-00-11. (M)

Part: PLATE — CORRODED (HORIZ STAB)

TUL - FOUND LEFT OUTBOARD HORIZONTAL STAB PIVOT BEARING LUG PLATES ARE CORRODED. REPLACED LEFT OUTBOARD LUG PLATES AND MACHINED PIVOT BORE PER FCD0488A, 9, D/E. (M)

Part: PLATE — CORRODED (HORIZ STAB)

LEFT INBOARD HORIZONTAL STABILIZER PIVOT BEARING LUG PLATES ARE CORRODED. 1.5 INCH X 1.5 INCH AREA, BEYOND LIMITS. REPLACED LEFT INBOARD HORIZONTAL STABILIZER LUG PLATES AND MACHINED PIVOT BORE IAW FCO 0488A, 9, D AND E.

Part: PLATE — CORRODED (HORIZ STAB)

TUL - FOUND RIGHT OUTBOARD HORIZONTAL STAB PIVOT BEARING LUG PLATES ARE CORRODED. REPLACED RIGHT OUTBOARD LUG PLATE AND MACHINED PIVOT BORE PER FCO KF0488A, 9, D/E. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 3, FS 1174. INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 3. INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND L2R CRACKED AT END FITTING. REMOVED DAMAGED SECTION OF 2R. INSTALLED SPLICE AND DOUBLER PER AARD 53-30-00-2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK NR 2 CORRODED INBOARD SIDE STATION 1201. ACCOMPLISHED REPAIR IAW SRM 53-05-00. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION IN CUSP WEB 1212-1231. CUT OUT, CORRODED AREA 1212-1219 AND INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3.

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN SKIN FORWARD OF RIGHT FLOOD LIGHT. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 12B, INCORPORATED REPAIR E58 NR 4207681 AND 4207640 ONE DOUBLER. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN SKIN STATION 534 LONGERON 20R. CONDITION 1-B PER 53-04 FIG 38. INSTALLED DOUBLER PER SRM 5304. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND GOUGE ON SKIN FS 1305 BELOW 18R, FROM COWLING DRAIN MAST CONTACT BELOW PYLON. FOUND DAMAGE AREA TO BE CONDITION 3 PER SRM 53-04 FIG 38 SHEET 3. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 20. (M)

Part: CLIP — CRACKED (FUSELAGE)

TUL - FOUND RIGHT UPPER FORWARD WINDOW CLIP CRACKED STATION 947. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25 PAGE 1/2. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT AND SCRATCH APPROX STATION 235 BETWEEN L17 AND L18 LEFT. BUMPED OUT DENT, DYE CHECKED, NO CRACK FOUND. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: LANDING GEAR — MALFUNCTIONED (NLG)

DFW - FLT 1658 - EN ROUTE DFW-TUL - SHORTLY AFTER TAKEOFF, NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. ACCOMPLISHED GEAR RETRACTION PER THE MM. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (L1 DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT PORTABLE ASSEMBLY AT L1 DOOR INOPERATIVE. RECONNECTED EMERGENCY LIGHT CONNECTOR AT PORTABLE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HYDRAULIC LINE — LEAKING (ACM BAY)

ORD - FLT 862 - EN ROUTE ORD-EWR, SHORTLY AFTER TAKEOFF DETECTED ELECTRICAL SMELL IN CABIN. FLIGHT ATTENDANT REPORTED SEEING SMOKE AT AFT CABIN. RETURNED ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED HYDRAULIC LINE. REPLACED COALESCER BAGS. PERFORMED PACK BURNOUT PER THE MM. NO SMELL OR SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED FIRST CLASS EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — MISWIRED (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 21 AND AFT INOPERATIVE. CORRECTED FLAT WIRE POLARITY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)