N554AA

Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,863 hrs · 33,528 cycles

BIRD STRIKE DAMAGE TO FS SKIN JUST ABOVE FIRST OFFICER WINDOW AT STATION 148.55 & LONGERON 4 TO 5 RT. ACCOMPLISHED REPAIR IAW EA MD80-53-031441.

Part: PIN — CRACKED (RADOME) · airframe 64,104 hrs · 33,082 cycles

CRACK AT STA 37, LOWER RT RADOME GUIDE PIN. CUT OUT CRACK AND INSTALLED DOUBLER AND FILLER IAW AARD 53-10-00-19.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,104 hrs · 33,082 cycles

CRACK IN SKIN AT STATION 1309 ABOVE LONGERON 7 LT. CUT OUT CRACK AND INSTALLED TEMPORARY DOUBLER IAW SRM 53-04-02, FIG 2, SHEET 29 AND PARA 3.C. (1)(C).

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,104 hrs · 33,082 cycles

LOWER RT TAILCONE CANT FRAME AT STA 1510 CRACKED AROUND ALIGNMENT PIN. INSTALLED DOUBLER IAW SRM 53-01-00 AND SRM 51-30-05.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 63,173 hrs · 32,576 cycles

RIGHT CENTER EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED BATTERY PACK. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 63,173 hrs · 32,576 cycles

SEAT 7D ESCAPE PATH LIGHT MISSING LENS. REPLACED LENS FOR SEAT 7D ESCAPE PATH LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 63,173 hrs · 32,576 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY PACK. OPS CHECK NORMAL.

Part: LIGHT — MISSING (CABIN) · airframe 63,173 hrs · 32,576 cycles

SEAT 7D ESCAPE PATH LIGHT MISSING LAMP. REPLACED LAMP FOR SEAT 7D ESCAPE PATH LIGHT. OPS CHECK NORMAL.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 63,173 hrs · 32,576 cycles

LEFT NUMBER 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,173 hrs · 32,576 cycles

STANDBY EMERGENCY LIGHTS IN FORWARD GALLEY INOPERATIVE. REPLACED LAMP FOR STANDBY EMERGENCY LIGHTS IN FORWARD GALLEY. OPS CHECK NORMAL.

Part: CONTROL VALVE — STICKING (AC BAY) · airframe 62,481 hrs · 32,216 cycles

CAPTAIN REPORTED TEMPERATURE DROP AND LOSS OF PRESSURIZATION. ACCOMPLISHED RAPID DESCENT CAUSING ALL THE OXYGEN MASKS TO DEPLOY. EMERGENCY DECLARED AND LANDED DFW WITHOUT INCIDENT. FOUND TEMPERATURE SENSORS DIRTY AND CLOSED. FOUND RIGHT PACK TEMPERATURE CONTROL VALVE INTERMITTENT AND STICKING IN FULL CLOSED AND FULL OPEN. CLEANED TEMPERATURE SENSOR. REPLACED RIGHT PACK TEMPERATURE CONTROL VALVE. CHANGED OXYGEN CONNECTIONS AND STOWED MASKS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 62,022 hrs · 31,944 cycles

FORWARD CARGO DOOR FRAME DAMAGE AT STATION 370 ON FORWARD UPPER CORNER OF FRAME. INSTALLED DOUBLER REPAIR PER SRM 53-05-00 FIGURE 105.

Part: PORTABLE LIGHT — BROKEN (CABIN) · airframe 61,063 hrs · 31,440 cycles

LOCK TAB BROKEN ON PORTABLE EMERGENCY LIGHT AT LEFT NUMBER 1 DOOR. REPLACED PORTABLE EMERGENCY LIGHT AT LEFT NUMBER 1 DOOR.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,335 hrs · 31,042 cycles

FRAME 1418 WAS FOUND TO BE CRACKED AT LEFT NUMBER 2 DOOR RIGHT. INSTALLED DOUBLER PER SRM 53-03-00 FIGURE 31A AND EA MD80-53-011668.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 60,335 hrs · 31,042 cycles

AFT NOSE LANDING GEAR DOOR, LEFT SIDE HAS A CRACK BEYOND STOP DRILLED AT AFT HINGE CUTOUT. INSTALLED DOUBLER PER SRM 53-05-00 FIGURE 62.

Part: ROLLER — MISSING (LT MLG DOOR) · airframe 58,978 hrs · 30,289 cycles

ATL - CREW REPORTED GEAR DOWN AND YELLOW GEAR DOOR OPEN LIGHT WOULD NOT GO OUT. ACCOMPLISHED QRH PROCEDURE AND GO AROUND. EMERGENCY DECLARED FLIGHT LANDED ATL LANDED WITHOUT INCIDENT. GROUND REPORTS LEFT GEAR DOOR HALF OPEN AND RIGHT DOOR CLOSED. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT MAIN LANDING GEAR DOOR LATCH ROLLER AND ASSOCIATED HARDWARE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: HOSE — LOOSE (PITOT/STATIC SYS) · airframe 58,062 hrs · 29,782 cycles

DFW - CREW REPORTED CAPTAINS AIRSPEED WENT TO ZERO WITH A FLAG. AFTER AIRBORNE AND CENTRAL AIR DATA COMPUTER WAS SWITCHED TO BOTH ON 2, CAPTAINS AIRSPEED SLOWLY STARTED INCREASING TO 300 KNOTS. BOTH STANDBY AND FIRST OFFICERS AIRSPEED INDICATED 250. PULLED CB U31 AFTER OVERSPEED WARNING CAME ON. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. FOUND NUMBER 1 CADC NUMBER 1 PITOT HOSE LOOSE. REPLACED NUMBER 1 CADC. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SWITCH — FAULTY (NLG) · airframe 57,215 hrs · 29,323 cycles

DFW - CREW REPORTED NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. CYCLED GEAR AND NO HELP. EMERGENCY DECLARED VERIFIED GEAR EXTENDED AND LANDED AT DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSE GEAR GROUND INTERLOCK SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,529 hrs · 28,939 cycles

CORROSION ON SUBFLOOR AT STATION 201 RIGHT SIDE OUTBOARD EDGE. INSTALLED REPAIR DOUBLER ON SUBFLOOR AT STATION 201 RIGHT SIDE OUTBOARD EDGE PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,529 hrs · 28,939 cycles

CABIN RIGHT CUSP CRACKED STATION 223. INSTALLED NEW SECTION CABIN RIGHT CUSP STATIONS 218 TO 223 PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,529 hrs · 28,939 cycles

CORROSION ON SUBFLOOR FROM STATIONS 160 TO 178 JUST AFT OF G1 GALLEY DRAIN PAN. INSTALLED SUBFLOOR DOUBLER FROM STATION 148 RIGHT TO STATION 200 RIGHT PER AARD 53-20-00-16.

Part: PAN — CORRODED (FUSELAGE) · airframe 56,529 hrs · 28,939 cycles

CORROSION ON CARGO DOOR PAN FROM STATIONS 389 TO 427. REPAIRED FORWARD CARGO LOWER DOOR JAMB/PAN PER SRM 53-05-00 FIGURE 44.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,529 hrs · 28,939 cycles

LEFT CUSP CRACKED AT STATION 225. REPLACED CUSP SHEET STATIONS 218 TO 237 PER AARD 53-20-00-16.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,529 hrs · 28,939 cycles

BRACKET BROKEN INSIDE OF AFT VAULT DOOR FRAME ON RIGHT SIDE AT 13 INCHES FROM FLOOR. INSTALLED NEW SERVICABLE BRACKET PER SRM 51-01-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,529 hrs · 28,939 cycles

CORROSION ON CUSP UNDER GIRT BAR FITTINGS AT AFT SERVICE ENTRY DOOR. INSTALLED TITANIUM DOUBLER UNDER GIRT BAR FITTINGS AT AFT SERVICE ENTRY DOOR PER SRM 51-10-03.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,529 hrs · 28,939 cycles

CORROSION ON BOTTOM OF LEFT CUSP STATION 511. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,529 hrs · 28,939 cycles

CORROSION ON BOTTOM OF LEFT HAND CUSP STATION 511., INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BEAM — CRACKED (DOOR) · airframe 56,529 hrs · 28,939 cycles

NUMBER 6 BEAM CRACKED AT OUTBOARD AFT BOLT. INSTALLED REPAIR DOUBLER PER AARD 52-10-00-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,529 hrs · 28,939 cycles

CRACK AND CORROSION IN LEFT CUSP STATIONS 845 TO 820. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER ON CUSP STATIONS 840 TO 820 LEFT SIDE PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,529 hrs · 28,939 cycles

LONGERON 20 RIGHT CRACKED ABOVE INBOARD FLAP ACTUATOR. INSTALLED DOUBLER PER AARD 53-10-00-18

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,529 hrs · 28,939 cycles

ANGLE AT AFT PRESSURE BULKHEAD ABOVE DOORWAY APPROXIMATE CENTER IS CRACKED AT TOP. INSTALLED REPAIR DOUBLER ABOVE VAULT DOOR PER AARD 53-10-00-15.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN CRACKED AT STA 1079 LEFT HAND TOP AFT CORNER OF WINDOW. INSTALLED REPAIR ANGLE AT UPPER AFT WINDOW CORNER STA 1079 LEFT HAND SIDE PER AARD REF 53-10-00-25.

Part: CASTING — CRACKED (SPOILER) · airframe 56,529 hrs · 28,939 cycles

LEFT HAND GROUND SPOILER CASTING CRACKED. INSTALLED NEW CASTING PER SRM 51-02-00

Part: CASTING — CRACKED (SPOILER) · airframe 56,529 hrs · 28,939 cycles

RIGHT HAND GROUND SPOILER CASTING CRACKED. INSTALLED NEW CASTING.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

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

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN R-45 CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN CRACKED AT STATION 1041 LEFT SIDE TOP AFT CORNER. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN R-36 CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN CRACKED AT WINDOW R-30 STATION 778 FORWARD UPPER CORNER. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN AT 1079 LEFT TOP AFT CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN CRACKED AT WINDOW R-31 STATION 797 FORWARD UPPER CORNER. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN CRACKED AT STATION 1022 LEFT TOP AFT CORNER OF WINDOW. INSTALLED DOUBLER AT STATION 1022 LEFT TOP AFT CORNER OF WINDOW PER AARD 53-10-00-25.

Part: FITTING — BROKEN (FUSELAGE) · airframe 56,529 hrs · 28,939 cycles

FITTING BROKE BELOW NUMBER 2 SEAT TRACK AT STATION 927. REPLACED FITTING PER SRM 51-01-00.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN CRACKED AT WINDOW R-36 LOWER AFT. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,529 hrs · 28,939 cycles

RIGHT CUSP STATIONS 488 TO 492 CORRODED BEYOND LIMITS. CUT OUT CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,529 hrs · 28,939 cycles

WEBBING CRACKED STATION 208 LONGERON 15 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 56,529 hrs · 28,939 cycles

CORROSION G2 FORWARD INBOARD TIE DOWN. REPLACED G2 MOUNT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,529 hrs · 28,939 cycles

SEAT TRACK NUMBER 1 CORRODED STATIONS 1084 TO 1090. INSTALLED SEAT TRACK REPAIR PER AARD 53-20-10-10.

Part: PAN — DAMAGED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN CRACKED AT WINDOW R-46 LOWER FORWARD. REPAIRED CRACK AT RIGHT RING PAN LOWER FORWARD AREA WINDOW 46 BY REMOVING EAR AND INSTALLING ANGLE BRACKET PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN CRACKED AT WINDOW R-49 LOWER FORWARD. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN CRACKED AT STATION 1060 LEFT FORWARD BOTTOM CORNER OF WINDOW. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN CRACKED AT WINDOW R-54 LOWER AFT. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN R-32 CRACKED UPPER FORWARD CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN CRACKED R-42. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN CRACKED R-50. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

R-51 WINDOW PAN CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN CRACKED AT WINDOW R-34 UPPER FORWARD. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,529 hrs · 28,939 cycles

WINDOW PAN R-32 CRACKED LOWER AFT CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: REGULATOR VALVE — INOPERATIVE (ANTI-ICE SYS) · airframe 54,315 hrs · 27,707 cycles

BNA - INFLIGHT DCA-DFW. ICE PROTECT PRESSURE ABNORMAL LIGHT ILLUMINATED. EMERGENCY DECLARED, LANDED BNI WITHOUT INCIDENT. REPLACED PRESSURE REGULATING VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRANSFORMER — INOPERATIVE (COCKPIT) · airframe 54,264 hrs · 27,676 cycles

DFW - CREW REPORTED AIRFOIL ANTI-ICE ABNORMAL PRESSURE LIGHT ON IN FLIGHT AND FIRST OFFICER WINDSHIELD CIRCUIT BREAKER POPPED. RETURNED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE WINDSHIELD, CONTROLLER, AND TRANSFORMER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FRAME — CRACKED (ZONE 200) · airframe 53,021 hrs · 26,990 cycles

FRAME 1418 CRACKED AT LONGERON 2 LEFT. INSTALLED DOUBLER IN ACCORDANCE WITH ENGINEERING AUTHORIZATION 53-005415 AND SRM 53-01.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,021 hrs · 26,990 cycles

BOTTOM OF FLOOR PAN CORRODED AND CRACKED AT DRAIN FOR GALLEY. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FRAME — CRACKED (ZONE 200) · airframe 53,201 hrs · 26,990 cycles

FRAME CRACKED AT STATION 1418 AT LONGERON 2 RIGHT. INSTALLED DOUBLER ON FRAME 1418 LONGERON 2 RIGHT PER ENGINEERING AUTHORIZATION MD80 53-005415 AND SRM 53-01-00.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 52,605 hrs

LGA - AFT EMERGENCY FLASHLIGHT STRAP BROKEN. REPLACED STRAP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 52,605 hrs

LGA - FORWARD JUMPSEAT UPPER FLASHLIGHT SAFETY STRAP IS BROKEN. REPLACED SAFETY STRAP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 53,141 hrs · 27,184 cycles

FORWARD CARGO DOOR, LOWER FORWARD STOP, TEE FITTING CRACKED. REMOVED AND REPLACED TEE FITTING.

Part: BATTERY PACK — DISCHARGED (CABIN) · 52,014 cycles

DFW EMERGENCY LIGHT EXIT SIGNS AT AFT LT AND RT OVERWING DOORS INOPERATIVE. REPLACED BATTERY PACK AT STATION 1100 FOR EMERGENCY LIGHT EXIT SIGNS AT AFT LT AND RT OVERWING DOORS. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — DISCHARGED (CABIN) · 52,014 cycles

DFW EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 11 TO 17 INOPERATIVE. REPLACED BATTERY PACK AT STATION 700 FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 11 TO 17. SYSTEM GROUND CHECKED NORMAL OPS.

Part: SHROUD — BROKEN (CABIN) · airframe 52,014 hrs

DFW - EMERGENCY LIGHT AT SEAT 29D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · 52,014 cycles

DFW EMERGENCY LIGHTS AT SEAT ROWS 20 TO AFT CABIN ARE DIM. REPLACED BATTERY PACK AT STATION 1154 FOR EMERGENCY LIGHTS AT SEAT ROWS 20 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,854 hrs

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

NR 1 FLEX PANEL EMERGENCY PATH LIGHTING AND NR 2 AND NR 3 OVERHEAD EMERGENCY ESCAPE PATH LIGHTING AT STATIONS 925, 812 AND 642 INOPERATIVE. REPLACED BATTERY PACKS FOR NR 1 FLEX PANEL EMERGENCY PATH LIGHTING (BATTERY PACK B5 28) AND NR 2 (BATTERY PACK B5 104) AND NR 3 (BATTERY PACK B5 102) OVERHEAD EMERGENCY ESCAPE PATH LIGHTING AT STATIONS 925, 812 AND 642. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN)

DFW SEAT MOUNTED EMERGENCY LIGHT AT SEAT 30D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 30D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

AUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 11AB, 9DEF, 9AB, AND 8AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS AT ROW 9-12 INOPERATIVE. SECURED BATTERY PACK CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK CORRODED AT STATION 1236. MACHINED OUT DAMAGED AREA AND INSTALLED PLUG PER SRM 53-05-00 PAGE 8C PAGE 8D. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING ASSEMBLY AT 11D DIM. REPLACED EMERGENCY EXIT PATH LIGHTING ASSEMBLY AT 11D DIM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: RETRACT MECH — LACK OF LUBE (NLG)

DFW - FLT 496 - EN ROUTE ELP/DFW DURING GEAR RETRACTION, CREW HEARD A GRINDING NOISE AND RED NOSE GEAR LIGHT STAYED ILLUMINATED FOR APPROXIMATELY A MINUTE, THEN CYCLED OFF AND ON SEVERAL TIMES BEFORE EXTINGUISHING. CONTINUED ON TO DFW. GEAR EXTENDED NORMALLY. LANDED DFW WITHOUT INCIDENT. LUBED NOSE LANDING GEAR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED PORTABLE LIGHT AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ANNUNCIATOR — LOOSE (RT MLG)

TPA - FLT 1478 - DURING APPROACH TO TPA WHEN LANDING GEAR EXTENDED, RT MLG GREEN LIGHT FAILED TO ILLUMINATE. AIRCRAFT MADE A FLY-BY THE TPA TOWER AND LANDED WITHOUT INCIDENT. MAINTENANCE RESEATED AND SECURED ANNUNCIATOR BASE HOUSING. SYSTEM GROUND CHECKED, NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS SECTION INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — LOW PRESSURE (ENTRY DOOR)

TPA - DURING OVERNIGHT CHECK, FORWARD ENTRY DOOR EMERGENCY EVACUATION SLIDE BOTTLE PRESSURE NOTED OUT OF GREEN RANGE. REPLACED FORWARD ENTRY DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)