N516AM

Part: CHARGER — DIRTY (CABIN) · airframe 64,764 hrs · 33,889 cycles

RIGHT AND CENTER CEILING EMERGENCY LIGHTS INOPERATIVE. CLEANED CONTACTS ON CHARGER. OPS CHECK NORMAL.

Part: CHARGER — DIRTY (CABIN) · airframe 64,764 hrs · 33,889 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. CLEANED CONTACTS ON CHARGER. OPS CHECK NORMAL.

Part: CHARGER — DIRTY (CABIN) · airframe 64,764 hrs · 33,889 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11 INOPERATIVE. CLEANED CONTACT ON CHARGER. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 64,349 hrs · 33,679 cycles

ROW 7 EGRESS LIGHT MISSING LENS COVER. REPLACED LENS COVER FOR ROW 7 EGRESS LIGHT, OPS CHECK NORMAL.

Part: CASTING — CRACKED (LT SPOILER) · airframe 64,202 hrs · 33,600 cycles

LEFT WING TRAILING EDGE HAS A CRACK IN RADIUS OF GROUND SPOILER ACTUATOR CASTING AT INBOARD END OF FORWARD MOUNT LUG. REMOVED AND REPLACED SPOILER CASTING PER AARD 51-10-00-5.

Part: BATTERY PACK — DISCHARGED (CATWALK) · airframe 62,224 hrs · 32,475 cycles

EMERGENCY LIGHTS OVER AFT ACCESSORY COMPARTMENT CATWALK INOPERATIVE. REPLACED BATTERY PACK B5-28.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,016 hrs · 32,365 cycles

EMERGENCY EXIT LIGHTS IN COCKPIT, FORWARD ENTRY, GALLEY AND FORWARD MOST AISLE INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: APU — LEAKING (ZONE 100) · airframe 61,683 hrs · 32,168 cycles

PHX - CREW REPORTED SMOKE IN THE CABIN. EMERGENCY DECLARED FLIGHT RETURNED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND OIL LEAKING FROM AUXILIARY POWER UNIT. REPLACED APU AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,343 hrs · 31,961 cycles

LEFT NUMBER 1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR LEFT NUMBER 1 DOOR. OPS CHECK NORMAL.

Part: RIVET — CRACKED (BULKHEAD) · airframe 60,251 hrs · 31,380 cycles

RIVET HEAD CRACKED AT 4 O’CLOCK POSITION ON BULKHEAD 37, ADJACENT TO RADOME ALIGNMENT PIN. INSTALLED SHIM AND ALIGNMENT PIN PER AARD 53-10-00-19.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,251 hrs · 31,380 cycles

BULKHEAD 37 CRACKED AT 8 O’CLOCK POSITION AT RADOME ALIGNMENT PIN. INSTALLED SHIM AND ALIGNMENT PIN PER AARD 53-10-00-19.

Part: BOOT — LOOSE (ACM) · airframe 59,907 hrs · 31,169 cycles

DFW - CREW REPORTED ON CLIMBOUT THE TAIL COMPARTMENT OVERHEAT LIGHT ILLUMINATED. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT AIR CYCLE MACHINE BOOT OFF AND CLAMP LOOSE. RE-INSTALLED BOOT AND RESECURED CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,842 hrs · 31,126 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEATS 29 DEF. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CHECKED NORMAL.

Part: SKIN — DAMAGED (ZONE 100) · airframe 56,331 hrs · 29,206 cycles

LT ALTERNATE STATIC PORT FAILED WAVINESS CHECK. INSTALLED FLUSH DOUBLER PER SRM 53-03-00.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

FLOOR BOARD SUPPORT CRACK AT STA 1212 AT DOOR FRAME WEB, L28R-L29R. REPLACED FLOORBOARD SUPPORT AT STA 1212, L28R-L29R PER SRM 51-30-00.

Part: PAN — CORRODED (ZONE 100) · airframe 56,223 hrs · 29,143 cycles

FWD CARGO THRESHOLD PAN CORRODED. REPLACED PAN PER SRM 53-05-00 FIG 44.

Part: BEAM — CORRODED (ZONE 100) · airframe 56,331 hrs · 29,206 cycles

AFT CARGO DOOR BEAM HAS CORROSION. INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-03.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 56,334 hrs · 29,207 cycles

CORROSION ON LT TIE DOWN TRACK IN THE AFT CARGO. INSTALLED NEW TIEDOWN TRACK PER AARD 51-00-00-12.

Part: DOUBLER — DAMAGED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

DAMAGE HOLE ON HORSE SHOE COLLAR DOUBLER AT STA 845 RT. NEW REPAIR DOUBLE WAS INSTALLED PER 51-30-05.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

CORROSION ON CUSP. REPLACED CUSP PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,336 hrs · 29,208 cycles

CORROSION ON SUB-FLOOR AT STA 200 12 INCHES FORWARD OF NR 6 SEAT TRACK. REMOVED CORROSION ON SUB-FLOOR AT STA 200 12 INCHES FORWARD OF NR 6 SEAT TRACK AND INSTALLED / DOUBLER AT STA 200 TO 218 PER AARD 53-20-16-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,334 hrs · 29,207 cycles

CORROSION ON RT CUSP AT STA 1168. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

CRACK IN RT CUSP STA 802-807. NEW CUSP SHEET WAS INSTALLED PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

LONGERON L4 CRACKED. REMOVED AND REPLACED L4 FROM STA 148-226 PER SRM 53-02-00.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

INTERCOSTAL CRACKED BETWEEN FLOORBEAMS AT BL NR 0. INSTALLED NEW INTERCOSTAL PER SRM 51-30-02.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 56,334 hrs · 29,207 cycles

CORROSION ON RT CUSP. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,334 hrs · 29,207 cycles

AFT CARGO J-ANGLE, RT SIDE OF L30, STA 1147-1155 CORROSION.

Part: BEAM — CORRODED (ZONE 100) · airframe 56,331 hrs · 29,206 cycles

CORROSION ON MID CARGO THRESHOLD BEAM. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,334 hrs · 29,207 cycles

G-2 MOUNT, FWD END OF NR 6 SEAT TRACK HAS CORROSION. REMOVED AND REPLACED G-2 MOUNT AT FWD END OF NR 6 SEAT TRACK PER SRM 51-10-00.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

CORROSION ON LT CUSP AT AFT SERVICE DOOR UNDER GIRT BAR BRACKET. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

RT CUSP CORRODED. INSTALLED NEW CUSP SHEET PER SRM 51-01-00.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 56,334 hrs · 29,207 cycles

CORROSION ON RT CUSP AT STA 196-200. REMOVED CORRODED AREA AND INSTALLED 7075-T6 DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

RT CUSP CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BRACKET — CORRODED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

CORROSION ON GIRT BAR FITTING BRACKET AT AFT SERVICE DOOR. INSTALLED NEW GIRT BAR BRACKET PER SRM 51-01-00.

Part: BRACKET — CORRODED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

CORROSION ON LT CUSP UNDER GIRT BAR BRACKET AT AFT SERVICE DOOR. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BRACKET — CORRODED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

CORROSION ON FWD GIRT BAR BRACKET AT AFT SERVICE DOOR. INSTALLED NEW GIRT BAR BRACKET PER SRM, 51-01-00.

Part: STRUCTURE — CORRODED (ZONE 200) · airframe 56,334 hrs · 29,207 cycles

CORROSION ON SUBFLOOR AT STA 200, 12 INCH FORWARD OF NR 6 SEAT TRACK. INSTALLED DOUBLER AT STA 200 TO 218 PER AARD 53-20-16-00.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

NR 3 SEAT TRACK CORRODED OUT OF LIMITS. INSTALLED PLUG REPAIR PER AARD 53-20-00-10.

Part: RIB — WORN (ZONE 600) · airframe 56,334 hrs · 29,207 cycles

SECOND RIB CRACKED FROM OTBD END ON RT WING NR 5 SLAT. REMOVED AND REPLACED RIB PER ESO 80117.

Part: STOP — CRACKED (ZONE 800) · airframe 56,331 hrs · 29,206 cycles

AFT LOWER STOP PAD FITTING CRACKED ON AFT CARGO DOOR. INSTALLED NEW FITTING PER ESO 80174.

Part: RIB — CRACKED (ZONE 500) · airframe 56,334 hrs · 29,207 cycles

SECOND RIB FROM OTBD END CRACKED ON LT WING NR 5 SLAT. REPLACED RIB PER ESO 80117.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

LT CUSP CRACKED AT STA 814. ROUTED OUT CRACK AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

CORROSION BEYOND MANUAL LIMITS AT SEAT TRACK NR 6 AT STA 854-859. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: BRACKET — CRACKED (ZONE 600) · airframe 56,334 hrs · 29,207 cycles

BRACKET CRACKED INSIDE RT WING VENT BOX. REMOVED AND REPLACED BRACKET PER SRM 51-01-00.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,331 hrs · 29,206 cycles

CORROSION ON BOTTOM OF CUSP, RT SIDE, STA 1060-1079. REMOVED CORROSION, INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 56,334 hrs · 29,207 cycles

CRACK IN LT CUSP AT STA. 222. INSTALLED NEW CUSP SHEET PER AARD 53-20-00-16, STA 218 TO 237.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

CORROSION ON SEAT TRACK NR 5 BEYOND LIMITS, STA 234-237. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,334 hrs · 29,207 cycles

NR 1 SEAT TRACK DAMAGED AT STA 636. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: SKIN — CRACKED (WINDOW BELT) · airframe 56,331 hrs · 29,206 cycles

CRACK IN WINDOW BELT UPPER FORWARD CORNER. INSTALLED WINDOW BELT DOUBLER PER AARD 53-10-00-25.

Part: LONGERON — CORRODED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

FUSELAGE AFT SERVICE PAN HAS CORROSION. INSTALLED LONGERON SPLICE AT L22L, BETWEEN STA 1287 AND 1338 PER AARD 53-00-00-05.

Part: GUSSET — CRACKED (ZONE 200) · airframe 56,331 hrs · 29,206 cycles

GUSSET CRACKED AT LT STA 207 L11L. STOP DRILLED AND INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: GUARD — INOPERATIVE

STL - EXPERIENCED UNCOMMANDED FUEL TRANSFER IN FLIGHT. FUEL FEED OUT OF LEFT MAIN TANK. LANDED STL WITHOUT INCIDENT. FOUND REFUELING PANEL SWITCH GUARDS NOT CLOSING SWITCH. CLEANED AND LUBED SWITCH GUARDS AND ADJUSTED DOOR SWITCH RESTRICTOR BAR. PERFORMED CARD 28 96 01 WING FUEL IMBALANCE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

ATL - EMERGENCY LIGHTS FROM SEAT 1 THROUGH 20 INOPERATIVE. REPLACED CHARGER MODULE AND BATTERY PACK FOR EMERGENCY LIGHTS FOR SEATS 1 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FORWARD OF EMERGENCY OVERWING EXIT INOPERATIVE. REPLACED BOTH BATTERY PACK CHARGER MODULES FOR SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FORWARD OF EMERGENCY OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DFW CEILING EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DEN MID CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR MID CABIN CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: DOOR — CRACKED (LT MLG)

FOUND LEFT WW DOOR LANDING CRACKED AT OUTBOARD AFT CORNER, FS 1003. STOP DRILLED CRACK, INSTALL DOUBLER PER SRM 53-01 FIG 2. (M)

Part: ANGLE — CRACKED (FUSELAGE)

TUL - FOUND RIGHT W/W DOOR LAND CRACKED AT AFT OUTBOARD CORNER. INSTALLED DOUBLER PER SRM 53-01 FIG 2, STOP DRILL CRACK. (M)

Part: PIN — LOOSE (CONNECTOR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 21D INOPERATIVE. RESECURED EMERGENCY EXIT PIN IN CANNON PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ON SEAT 2EF INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT LIGHT SEAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND FLOOR WEB CORRODED AT STATION 197 RBL 41. REPLACED FLOOR WEB PER SRM 53-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND FLOOR WEB CORRODED 20 INCHES BY 6 INCHES STATION 150-170 RBL 43-49. INSTALLED DOUBLER PER SRM 53-01 FIG 4 AND AARD 53-00-00-02. (M)

Part: FRAME — DAMAGED (FS 522)

TUL - FOUND FRAME AT FS 522 DAMAGED AT L23-L26, LEFT HAS TOOLING MARKS. INSTALLED DOUBLER PER ESO 80559. (M)

Part: FRAME — GOUGED (FS 522)

TUL - FOUND FRAME AT STATION 522 GOUGED ON UPPER LOG IN 6 PLACES FROM L23R TOL27R. INSTALLED DOUBLER PER ESO 80559. (M)

Part: SKIN — DENTED (FS 170)

TUL - FOUND DENTS IN BOTH LOWER CORNERS OF OUTER SKIN. INSTALLED REPAIR DOUBLER PER AARD 52-10-00. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP STATION 200-281 RBL 56. CUT OUT CORROSION, INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND CORROSION 3 INCHES BY 3 INCHES, FS 200-218, FORWARD SERVICE DOOR. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND CLASS 2 DOUBLER INSTALLED AT 446, L24L. INSTALLED CLASS 1 PERMANENT REPAIR PER SRM 53-04 FIG 12B SHEETS. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND CANT FRAME 1485 IS CRACKED ON RIGHT SIDE OF STAIR CUTOUT WHERE ACTUATOR CASTING MOUNTS. CUTOUT DAMAGED SECTION OF FRAME AND INSTALLED SPLICED REPAIR AS PER AARD/DH 53-10-00-33 PAGE 1. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND FS 1485 CANT FRAME WEB CRACKED AT LEFT UPPER FASTENER JUST AFT OF LOWER VENT BOX. STOP DRILLED CRACK. INSTALLED DOUBLER PER AARD 53-10-00-32. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND SMELL DENT ABOUT 4 FEET FORWARD OF LEFT GROUND FLOOD LIGHT ON LEFT OF FUSELAGE. INSTALLED PERMANENT REPAIR PER SRM 53-04, FIG 12B, SHEET 5. (M)

Part: SKIN — CRACKED (FS 1380)

TUL - FOUND FUSELAGE SKIN CRACKED STATION 1380 AT LONGERON 14 LEFT. INSTALLED EXTERNAL REPAIR PER SRM 53-01. (M)

Part: FRAME — CRACKED (FS 484)

TUL - FOUND UPPER LEG OF FRAME CRACKED AND BENT AT 484, ABOVE L26L. REPAIRED FRAME PER AARD 53-10-00-17. (M)

Part: SKIN — SCRATCHED (FUSELAGE)

TUL - FOUND SCRATCH AT STATION 1309 BETWEEN L18R-19R. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP CORRODED STATION 992-999. INSTALLED CUSP DOUBLER PER AARD 53-00-00-2. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN FUSELAGE AFT OF FORWARD LEFT LAVATORY SERVICE PANEL. INSTALLED DOUBLER PER SRM 53-04 FIG 13B. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP STATION 665-693 AND CORROSION AND CRACK ON CUSP STATION 712. INSTALLED NEW CUSP SHEET STATION 598-712 SRM 51-01. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CUSP CRACKED AT 1300 BETWEEN SEAT TRACKS NR 1 AND NR 2. CUSP CRACKED AT 1250 BETWEEN SEAT TRACKS NR 1 AND NR 2. CUSP CORRODED AROUND LIGHTENING HOLE AT 1280. INSTALLED NEW CUSP SHEET FROM 1250-1308 LEFT PER SRM 51-01. (M)

Part: LONGERON — CRACKED (FS 160)

TUL - FOUND LONGERON 4L IS CRACKED AROUND FASTENER AT STATION 160. INSTALLED DOUBLER PER SRM 53-14-1 AND SRM 53-02. (M)

Part: SKIN — DENTED (FS 330)

TUL - FOUND DENT ABOVE LEFT FORWARD CABIN WINDOW. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 20. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND AFT CX DOOR BEAM CORRODED 4 INCHES BY 52 INCHES FROM STATION 1160-1212. BLENDED OUT CORROSION FROM 1160-1212 PER AARD 53-10-003, TREATED PRIMED AND PAINTED. INSTALLED DOUBLER FROM 1167-1182 PER AARD 53-10-00-3. (M)

Part: WEB — CORRODED (CABIN)

TUL - FOUND BOTTOM SIDE OF LEFT CUSP CORRODED. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01 FIG 4, SHT 3. (M)

Part: WEB — CRACKED (FS 208)

TUL - FOUND LONGERON 15L WEB TANG CRACKED AT 208. FABRICATED AND INSTALLED STRAP ON WEB AT L15L, STATION 208 PER AARD 53-10-00-11 PAGE 1/2. (M)

Part: BRACKET — CORRODED (FUSELAGE)

TUL - FOUND G1 GALLEY TIE DOWN CORRODED INSIDE HOLE. INSTALLED NEW SERVICEABLE TIE DOWN BRACKET PER SRM 51-10-3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION RIGHT CUSP AROUND FASTENERS, LIGHTENING HOLE STATION 541-560. INSTALLED NEW RIGHT CUSP SHEET FROM STATION 503-598 PER SRM 5301. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND STATION 798-801 CUSP CRACKED FOR 3 INCHES RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT FORWARD HALF DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: APU — LEAKING (AFT FUSELAGE)

ABQ - FLT 1724 - AFTER TAKEOFF, CREW REPORTED SMOKE IN CABIN. RETURNED AND LANDED ABQ WITHOUT INCIDENT. REPLACED APU. LEAKING OIL. REPLACED COELESCER BAGS AND ACCOMPLISHED PACK BURN-OUT. SYSTEM GROUND CHECK, NORMAL OPERATION. (X)

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS WOULD NOT ARM FROM FORWARD FLIGHT ATTENDANT STATION. RESEATED POWER PACK CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — FAILED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AFT OF EMERGENCY EXIT WINDOWS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRE IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — OUT OF SEQUENCE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT OVERWING EMERGENCY EXIT LIGHTS WOULD NOT TURN OFF. MAINTENANCE FOUND SWITCHES TO BE OUT OF SEQUENCE. MAINTENANCE RESEQUENCED SWITCHES AND LIGHTS WENT OUT. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M)

Part: COMPRESSOR — SEIZED (LT ENGINE)

DFW - FLT 475 - EN ROUTE DFW-PSP - AFTER TAKEOFF DFW AT 1000 FEET LOST ALL POWER FROM LEFT ENGINE. ALL INDICATIONS SHOWED LEFT ENGINE FAILED. CREW DECLARED AN EMERGENCY AND LANDED OVERWEIGHT AT DFW WITHOUT INCIDENT. TROUBLESHOT SYSTEM AND FOUND LEFT ENGINE COMPRESSOR SEIZED. REPLACED LEFT ENGINE ASSEMBLY. ACCOMPLISHED OVERWEIGHT LANDING AND PYLON INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VALVE — DEFECTIVE (NLG)

LAS - FLT 1342 - AFTER TAKEOFF LAS, NOSE GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO LAS AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPACKED NOSE LANDING GEAR AND REPLACED SERVICE VALVE. ACCOMPLISHED LEAK CHECK AND GEAR RETRACTION WITH NO DEFECTS FOUND. ACCOMPLISHED OVERWEIGHT CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: ACTUATOR — DEFECTIVE (NLG)

PHL - FLT 1511 - AFTER TAKEOFF PHL, NOSE GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO PHL AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED NLG RETRACT CYLINDER. ACCOMPLISHED GEAR RETRACTION AND OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SEALS — DEFECTIVE (NLG STRUT)

LAX - FLT 1680 - AFTER TAKEOFF LAX WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH ASSOCIATED NOISE AND VIBRATION FROM AREA OF NOSE LANDING GER. EXTEND LANDING GEAR AND LL INDICATIONS RETURNED TO NORMAL. AIRCRAFT RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDIGN GEAR STRUT SEALS. SERVICED NOSE LANDING GEAR STRUT WITH HYDRAULIC FLUID AND NITROGEN. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PACKING — LEAKING (NLG STRUT)

DFW - FLT 1727 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED. EXTENDED LANDING GEAR AND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT SCHRADER VALVE PACKING. SERVICED NOSE LANDING GEAR STRUT WITH HYDRAULIC FLUID AND NITROGEN. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED OVERWEIGHT LANDING CHECK WITH NO DEFECTS FOUND. (M)

Part: STRUT — REQUIRED SERVICE (NLG)

ORD - FLT 0362 - AFTER TAKEOFF ORD WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. EXTENDED LANDING GEAR AND ALL INDICATIONS NORMAL. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SERVICED NLG STRUT WITH HYDRAULIC FLUID AND NITROGEN. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)