N501AA

Part: CHARGER — INOPERATIVE (CABIN) · airframe 80,979 hrs · 43,386 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY AISLE LIGHTS ARE INOPERABLE FROM ROW 22 TO AFT SEAT. REPLACED BATTERY CHARGER MODULE PER AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: STRAP — CRACKED (VERTICAL STAB) · airframe 80,824 hrs · 43,286 cycles

VERTICAL STABILIZER SPAR, LEADING EDGE SKIN STRAP, FASTENER HOLE NR 6 HAD A CRACK INDICATION. REPLACED THE STRAP IAW DRAWING SG09550005.

Part: LONGERON — CRACKED (BS 990-1003) · airframe 80,824 hrs · 43,286 cycles

CRACKED LONGERON 20R BETWEEN BS 990 AND 1003. REPAIRED THE LONGERON IAW SRM 53-02-00. FIGURE 22.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,822 hrs · 43,285 cycles

ON SHUTTING THE MAIN CABIN DOOR, THE GUST LOCK WOULD NOT RETRACT INTO DOOR. NOTICED DAMAGED METAL AROUND THE GUST LOCK. THE AIRCRAFT WAS GROUNDED. MAINTENANCE BLENDED OUT THE DAMAGE ON THE EDGE OF THE L1 DOOR GUST LOCK CUTOUT, FOUND TO BE WITHIN LIMITS IAW SRM 51-02-00 STEP 1. A. (7) (A). TREATED, PRIMED & PAINTED IAW SRM 51-10-03.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 80,771 hrs · 43,254 cycles

LEFT HYDRAULIC PRESSURE WAS LOW, LIGHT ILLUMINATED IN FLIGHT. HYDRAULIC SYSTEM FAILED INDICATION, EMERGENCY DECLARED AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE PUMP IAW AMM 29-10-05 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 80,744 hrs · 43,238 cycles

AIRCRAFT WAS NOT GROUNDED: AFT FLASHLIGHT AT AFT FLIGHT ATTENDANT STATION HAD A DEAD BATTERY. MAINTENANCE REPLACED BATTERY PER AMM 25-60-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — INOPERATIVE (MEGAPHONE) · airframe 80,718 hrs · 43,222 cycles

FLIGHT ATTENDANT REPORTED THE MEGAPHONE IN THE AFT CABIN WAS INOPERATIVE. REPLACED BATTERIES IN THE MEGAPHONE ASSEMBLY. OPS CHECKED GOOD. OK FOR SERVICE.

Part: SLIDING WINDOW — DELAMINATED (COCKPIT) · airframe 80,635 hrs · 43,176 cycles

CAPTAIN`S SLIDING WINDOW DELAMINATED. REPLACED THE WINDOW IAW AMM 56-10-03.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 80,635 hrs · 43,175 cycles

EMERGENCY LIGHTS INOPERATIVE FROM SEAT 21D TO 32D. RESEATED THE CONNECTOR FOR CONTROL MODULE AB5-3 FOR AFT ZONE. THE AIRCRAFT WAS GROUNDED. PERFORMED AN OPS TEST. OPS CHECKED NORMAL IAW AMM 33-60-98-501.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 80,235 hrs · 42,915 cycles

AFT EMERGENCY LIGHTS ARE DIM WHEN POWERED BY THE AB5-3 BATTERY PACK. REPLACED THE BATTERY PACK IAW MM 33-60-98.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 79,191 hrs · 42,245 cycles

EMERGENCY EXIT LIGHTS, RIGHT SIDE ROW 21, AND OVERWING EXIT DOOR ARE INOPERATIVE. REMOVED AND REPLACED THE MID RIGHT BATTERY PACK, MID LEFT BATTERY PACK, AND MID POWER SUPPLY MODULE IAW AMM 33-60-98. OPS CHECKED GOOD.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 79,191 hrs · 42,245 cycles

EMERGENCY EXIT LIGHTS RIGHT SIDE, ROW 21, AND OVERWING EXIT DOOR ARE INOPERATIVE. REMOVED AND REPLACED MID RIGHT BATTERY PACK, MID LEFT BATTERY PACK, AND MID POWER SUPPLY MODULE IAW AMM 33-60-98. OPS CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 79,191 hrs · 42,245 cycles

CEILING EMERGENCY EXIT LIGHTS FROM ROWS 13 TO 19 ARE INOPERATIVE. REMOVED AND REPLACED THE BATTERY ASSEMBLY AT ROW 13 IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 79,191 hrs · 42,245 cycles

EMERGENCY LIGHTS RIGHT SIDE, ROW 21, AND OVERWING EXIT DOOR ARE INOPERATIVE. REMOVED AND REPLACED MID RIGHT BATTERY PACK, MID LEFT BATTERY PACK, AND MID POWER SUPPLY MODULE IAW AMM 33-60-98. OPS CHECKED GOOD.

Part: SWITCH — FAULTY (THRUST REVERSER) · airframe 79,054 hrs · 42,153 cycles

LEFT ENGINE THRUST REVERSER UNLOCK INDICATION DURING DESCENT. EMERGENCY DECLARED. LANDING UNEVENTFUL. REMOVED AND REPLACED THRUST REVERSER UPPER LATCH INDICATOR SWITCH S1-450 PER AMM 78-32-02. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 79,007 hrs · 42,118 cycles

FLIGHT ATTENDANT EMERGENCY AFT CABIN FORWARD JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-60-00. OPERATIONAL CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 78,856 hrs · 42,027 cycles

AIRCRAFT WAS NOT GROUNDED. AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY WILL NOT TEST. REMOVED AND REPLACED FLASHLIGHT BATTERY PER AMM 25-60-00. OPERATIONAL CHECK GOOD.

Part: LATCH — DIRTY (GIRT BAR) · airframe 78,752 hrs · 41,959 cycles

FLIGHT ATTENDANTS REPORTED THE GIRT BAR BRACKETS AT THE L1, R1 AND L2 DOORS ARE FILLED UP WITH DEBRIS AND ARE DIFFICULT TO ARM OR DISARM. CLEANED GIRT BAR LATCH ASSEMBLIES AT ALL 3 DOORS. OPS CHECKED GOOD IAW AMM 25-62-00.

Part: GIRT BAR — DIRTY · airframe 78,752 hrs · 41,959 cycles

FLIGHT ATTENDANTS REPORTED THE GIRT BAR BRACKETS AT THE L1, R1 AND L2 DOORS ARE FILLED WITH DEBRIS AND ARE DIFFICULT TO ARM OR DISARM. CLEANED THE GIRT BAR LATCH ASSEMBLIESAT ALL 3 DOORS. OPERATIONAL CHECKED GOOD IAW AMM 25-62-00.

Part: LATCH — DIRTY (GIRT BAR) · airframe 78,752 hrs · 41,959 cycles

FLIGHT ATTENDANTS REPORTED THE GIRT BAR BRACKETS AT THE L1, R1 AND L2 DOORS ARE FILLED WITH DEBRIS AND ARE DIFFICULT TO ARM OR DISARM. CLEANED GIRT BAR LATCH ASSEMBLIES AT ALL 3 DOORS. OPS CHECKED GOOD IAW AMM 25-62-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 78,543 hrs · 41,833 cycles

EMERGENCY EXIT LIGHT IN THE AFT AIRSTAIR CEILING THAT SHINES ON THE LANDING RAMP IS INOPERATIVE. REPAIRED THE WIRES IN THE LIGHT IAW WDM 33-51-13. OPS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,544 hrs · 41,833 cycles

WHILE ACCOMPLISHING AD 2004-11-07 ON THE R1 DOOR FRAME CORNERS, MAINTENANCE WAS UNABLE TO ACCOMPLISH HFEC INSPECTION ON TWO FASTENER HOLES ALONG THE EDGE OF THE LOWER AFT DOOR CUTOUT. REPAIRED IAW EA 271024.

Part: SKIN — CRACKED (R1 DOOR AREA) · airframe 78,544 hrs · 41,833 cycles

CRACKS ON TWO FASTENERS ON THE R1 DOOR UPPER FORWARD DOOR FRAME RADIUS. REPAIRED IAW SRM 53-05-00-001, 53-01-00 AND EA 271277.

Part: FRAME — WORN (BS 1510) · airframe 78,544 hrs · 41,833 cycles

WORN AREA ON AFT ACCESSORY COMPARTMENT LEFT LOWER CANTED FRAME AT BS 1510 FROM TAIL CONE INTERFERENCE. REPAIRED IAW SRM 51-70-05 FIGURE 1, AND EA 271237.

Part: FRAME — WORN (BS 1510) · airframe 78,544 hrs · 41,833 cycles

WORN AREA ON AFT ACCESSORY COMPARTMENT RIGHT LOWER CANTED FRAME AT BS 1510 FROM TAIL CONE INTERFERENCE. REPAIRED IAW SRM 51-70-05, FIGURE 1, AND EA 271237.

Part: FRAME — CRACKED (BS 1474) · airframe 78,544 hrs · 41,833 cycles

CRACK ON AFT ACCESSORY COMPARTMENT LEFT CANTED FRAME AT BS 1474, NINE FASTENERS UP FROM AFT STAIRWAY CUT OUT. REPAIRED IAW SRM 51-01-00, AND SRM 53-01-00, FIGURE 4.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,544 hrs · 41,833 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACK ON INTERCOSTAL AFT LOWER FLANGE AT FUSELAGE STATION 1338, RBL24. REPAIRED IAW SRM 53-01-00-001 AND AARD 53-10-00-15.

Part: MOUNT BRACKET — CORRODED (FUSELAGE)

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT GALLEY SERVICE DOOR CUT OUT AFT FLOOR BOARD MOUNT BRACKET AT FUSELAGE STATION 1167, LBL53. REMOVED AND REPLACED BRACKET IAW DRAWING 9930612 AND AARD 51-00-05-1. SEE ALSO AALA20170629004

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 78,544 hrs · 41,833 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT GALLEY SERVICE DOOR CUT OUT CUSP SHEET BETWEEN FUSELAGE STATIONS 1162 AND 1169, LBL48 TO LBL53. REPAIRED IAW AARD 53-20-00-16 STEP 7. SEE ALSO AALA201707059010

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,544 hrs · 41,833 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACKED LONGERON 3L IN THE RADIUS AT FUSELAGE STATION 160. REPAIRED IAW SRM 53-02-00-001 FIGURE 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,544 hrs · 41,833 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACKED LONGERON 4L IN THE RADIUS AT FUSELAGE STATION 160. REPAIRED IAW SRM 53-02-00-001 FIGURE 18.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,544 hrs · 41,833 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT CARGO SHEAR TIE, BELOW FLOOR, AT THE FORWARD SIDE OF FUSELAGE STATION 1231, LONGERON 29R TO 30R. REMOVED AND REPLACED SHEAR TIE IAW AARD 51-60-00-001 AND DRAWING 49738.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 78,544 hrs · 41,833 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACK ON AFT ACCESSORY COMPARTMENT SHEAR TIE AT THE AFT SIDE OF FUSELAGE STATION 1437, LONGERON 12R. REMOVED AND REPLACED SHEAR TIE IAW AARD 51-00-00 AND SRM 51-02-00.

Part: CUSP WEB — CORRODED (BS 579-589) · airframe 78,544 hrs · 41,833 cycles

CORROSION ON LEFT UPPER CUSP WEB BETWEEN BS 579 AND 589. REPAIRED IAW DWG 53-20-00, REPAIR 16.

Part: SHEAR TIE — CRACKED (BS 1380) · airframe 78,544 hrs · 41,833 cycles

CRACK ON AFT ACCESSORY COMPARTMENT SHEAR TIE AT FUSELAGE STATION 1380, BETWEEN LONGERONS 22L AND 23L. REPAIRED IAW DWG 53-10-00 REPAIR 20.

Part: SEAL — RUPTURED (DOOR) · airframe 78,484 hrs · 41,795 cycles

EMERGENCY DECLARED. EMERGENCY DESCENT INTO DESTINATION DUE TO CABIN PRESSURIZATION WARNING LIGHTS AND ANOMALIES. OXYGEN MASKS DID NOT DEPLOY. PERFORMED CHECK OF OVER PRESSURE SAFETY VALVES IAW 21-32-07, LEAKAGE TEST IAW 21-00-00-501, NEGATIVE PRESSURE RELIEF VALVE DOOR TEST, BITE CHECK OF PRESSURE CONTROLLER IAW 21-32-00. NO FAULTS NOTED. DURING DECAY CHECK, FOUND FORWARD DOOR HAS HOLE IN SEAL AT UPPER FORWARD CORNER OF DOOR . REPAIRED DOOR SEAL RUPTURE IAW SRM 52-04-00. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: BATTERY — FAILED (CABIN) · airframe 78,116 hrs · 41,562 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS OPERATED BY BATTERY ASSEMBLY B5-107 FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY B5-107 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 78,116 hrs · 41,562 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHTS POWERED BY BATTERY PACK AB5-2 ARE DIM. REMOVED AND REPLACED BATTERY PACK AB5-2 IAW AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,116 hrs · 41,562 cycles

WITH FWD ESCAPE PATH LIGHTS ZONE POWERED BY AB5-2 BATTERY MODULE LIGHTS ARE DIM. REMOVED AND REPLACED BATTERY FOR AB5-2 MODULE IAW MM 33-60-98. ESCAPE PATH LIGHTS OP CHK OK. THE AIRCRAFT WAS NOT GROUNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 78,116 hrs · 41,562 cycles

EMERGENCY LIGHTS OPERATED BY BATTERY PACK B5-107 ARE INOP ON TEST. REMOVED AND REPLACED BATTERY PACK B5-107 IAW MM 33-53-00. EMERGENCY LIGHTS OP CHK OK. THE AIRCRAFT WAS NOT GROUNDED.

Part: GASKET — LEAKING (APU OIL CAP) · airframe 77,865 hrs · 41,415 cycles

ODOR AND SMOKE IN THE CABIN. EMERGENCY DECLARED. RETURNED TO DEPARTURE. AIRCRAFT WAS GROUNDED. LANDING UNEVENTFUL. REMOVED AND REPLACED AUXILIARY POWER UNIT OIL CAP GASKET IAW AMM 12-12-01. LEAK AND OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 76,856 hrs · 40,763 cycles

AFT INTERIOR OVERWING EMERGENCY EXIT LIGHTS WILL NOT STAY OFF WHEN POWER WAS REMOVED FROM AIRCCRAFT. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-53-00.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 76,856 hrs · 40,763 cycles

EMERGENCY LIGHTS BETWEEN ROWS 22-26 FAILED TO STAY OFF WHEN POWER WAS REMOVED FROM AIRCRAFT. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-53-00. OPS CHECKED NORMAL.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 76,856 hrs · 40,763 cycles

EMERGENCY LIGHTS AT ROWS 27-32 FAILED TO STAY OFF WHEN POWER WAS REMOVED FROM AIRCRAFT. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-53-00. OPS CHECKED NORMAL.

Part: BULB — DAMAGED (CABIN LIGHTS) · airframe 76,702 hrs · 40,664 cycles

DURING TAXI OUT FLIGHT ATTENDANT REPORTED A STRONG ODOR NEAR CENTER OF AIRCRAFT BY SEAT ROWS 8 AND 9. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND FLUORESCENT BULB DAMAGED BETWEEN ROWS 9 AND 10 ON AIRCRAFT LEFT. INSPECTED BULB RECEPTACLE WITH NO DAMAGE NOTED. REMOVED AND REPLACED BULB IAW AMM 33-10-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,502 hrs · 40,536 cycles

EMERGENCY LIGHT FROM SEATS 21DEF TO 30DEF ARE INOPERATIVE. AIRCRAFT GROUNDED. REMOVED AND REPLACED BATTERY PACKS AB5-2 AND AB5-3 IAW AMM 33-53-01. SEE ALSO AALA20160722002., UNK

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,502 hrs · 40,536 cycles

FORWARD LEFT AND RIGHT ATTENDANTS SIDEWALL EXIT LIGHTS ARE INOPERATIVE. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED BATTERY ASSEMBLY B5-106 IAW AMM 33-53-00. OPERATIONAL CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,502 hrs · 40,536 cycles

BATTERY ASSEMBLY B5-103 REMOVED, SUSPECT BAD. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED BATTERY ASSEMBLY IAW AMM 33-53-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,502 hrs · 40,536 cycles

EMERGENCY LIGHT FROM SEATS 21DEF TO 30DEF ARE INOPERATIVE. AIRCRAFT GROUNDED. REMOVED AND REPLACED BATTERY PACKS AB5-2 AND AB5-3 IAW AMM 33-53-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,502 hrs · 40,536 cycles

LEFT AND RIGHT AFT OVERWING EXIT SIGNS ARE DIM. REMOVED AND REPLACED THE BATTERY ASSEMBLY 33-50-00.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,238 hrs · 39,782 cycles

AIRCRAFT WAS IN BASE MX. SHEAR TIE AT FS 1437, L2L IS CRACKED. R & R SHEAR TIE IAW AARD 51-00-05 & EA 257653.

Part: FITTING — CRACKED (RT SPOILER) · airframe 75,238 hrs · 39,782 cycles

AIRCRAFT WAS IN BASE MX. RT WING GND SPOILER FITTING IS CRACKED AT FWD INBD & OTBD CORNERS. R & R FITTING IAW SRM 51-30-05 & 51-30-02.

Part: CASTING — CRACKED (LT SPOILER) · airframe 75,238 hrs · 39,782 cycles

AIRCRAFT WAS IN BASE MX. LT WING GND SPOILER CASTING IS CRACKED ON INBD EDGE. R & R CASTING IAW SRM 51-30-02, SRM 51-30-05-001 & SRM 51-10-04-001.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,238 hrs · 39,782 cycles

AIRCRAFT WAS IN BASE MX. FUSELAGE SKIN IS CRACKED AT STATION 1437 & L4R. REPAIRED SKIN IAW SRM 53-04-00-001, SRM 53-34-00-001 & SRM 51-00-00-001.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,626 hrs · 39,429 cycles

LONGERON 23L AT STATION 200 CRACKED. REMOVED & INSTALLED NEW SECTION OF LONGERON & REPAIRED SPLICE ON LONGERON 23L, STATION 192 - 235 IAW SRM 53-20-00 FIGURE 18 & SRM 53-14-01 FIGURE 3.

Part: TERMINAL — DIRTY (BATTERY PACK) · airframe 71,977 hrs · 37,896 cycles

EMERGENCY LIGHT ABOVE THE AFT CABIN VAULT DOOR WOULD NOT EXTINGUISH. CLEANED BATTERY PACK TERMINALS & OPERATIONS CHECKED NORMAL.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,707 hrs · 37,726 cycles

SHEAR TIE CRACKED AT STATION 1380 BETWEEN LONGERON 13 & 14 RT. NESTED ANGLE DOUBLER INSTALLED IAW AARD 53-10-00-20.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 71,507 hrs · 37,600 cycles

VERTICAL STABILIZER LE SKIN & SPAR DAMAGE. REPAIRED DAMAGED FASTENER HOLES IAW EA MD80-55-035970.

Part: FORMER — CRACKED (LE SLAT) · airframe 71,507 hrs · 37,600 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-06.

Part: FORMER — CRACKED (LE SLAT) · airframe 71,507 hrs · 37,600 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 SLAT INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-05.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 71,507 hrs · 37,600 cycles

SEVERAL FASTENER HOLES IN VERTICAL STABILIZER LE ABOVE STATION ZFS 52.267 OVERSIZED BEYOND MANUAL LIMITS. INSTALLED REPAIR BUSHING IAW SRM 55-03-00-001 FIGURE 30.

Part: PORTABLE LIGHT — INTERMITTENT (CABIN) · airframe 71,248 hrs · 37,444 cycles

PORTABLE EMER LIGHT COMES ON INTERMITTENTLY DURING TEST. REPLACED ASSEMBLY B5-29. OPERATIONS CHECKED NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 68,947 hrs · 36,111 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESEATED BATTERIES AT ROW 29DEF. OPERATIONS CHECKED NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 68,947 hrs · 36,111 cycles

EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. RESEATED BATTERIES ABOVE RT AFT LAVATORY CEILING. OPERATIONS CHECKED NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,638 hrs · 35,390 cycles

CROWN SKIN IS CRACKED AT STATION 1309 BETWEEN LONGERONS 7 AND 6 LEFT. INSTALLED REPAIR DOUBLER AND PLUG PER SRM 53-04-00 FIGURE 32 AND BOEING DRAWING 5911014.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,638 hrs · 35,390 cycles

CROWN SKIN IS CRACKED AT STATION 1309 BETWEEN LONGERONS 7 AND 6 RIGHT. INSTALLED REPAIR DOUBLER AND PLUG PER SRM 53-04-00, FIGURE 32.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 67,638 hrs · 35,390 cycles

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

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,638 hrs · 35,390 cycles

LEFT CUSP IS CRACKED AT STATION 559. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,638 hrs · 35,390 cycles

VERTICAL DENT IN FUSELAGE SKIN AT STATION 210, LONGERON 17 RIGHT. INSTALLED DOUBLER PER SRM 53-04-02 FIGURE 2.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 67,638 hrs · 35,390 cycles

SUBFLOOR CORROSION UNDER GALLEY TIEDOWN MOUNT STATION 218 RIGHT BUTTLINE 11. INSTALLED REPAIR DOUBLER UNDER GALLEY TIE-DOWN MOUNT AT STATION 218 RIGHT BUTTLINE 11 PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,638 hrs · 35,390 cycles

SUBFLOOR UNDER GALLEY TIEDOWN MOUNT AT STATION 218, RIGHT BUTTLINE 11 CORRODED. INSTALLED REPAIR DOUBLER UNDER GALLEY TIEDOWN MOUNT AT STATION 218 PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,638 hrs · 35,390 cycles

MEMBRANE FROM STATIONS 200 TO 218 UNDER SEAT TRACK NUMBER FIVE CORRODED. INSTALLED CUSP MEMBRANE DOUBLER FROM STATIONS 200 TO 218 PER AARD 51-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,638 hrs · 35,390 cycles

CRACK IN LEFT CUSP, STATION 431, AT LIGHTENING HOLE. ROUTED OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,638 hrs · 35,390 cycles

CRACK ON LEFT CUSP UNDER HORSE COLLAR AT STATION 885, OUTBOARD OF NUMBER 1 SEAT TRACK. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: TAB — DAMAGED (RUDDER) · airframe 67,638 hrs · 35,390 cycles

RUDDER TAB HAS A HOLE AT UPPER TIP TRAILING EDGE. APPLIED WET OVERLAYS TO REPAIR AREA PER SRM 51-70-01A. PERFORMED A RE-METALLIZING REPAIR OVER THE REPAIR AREA PER AARD 55-40-00-2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,638 hrs · 35,390 cycles

CROWN SKIN CRACKED AT STATION 1309, BETWEEN LONGERONS 7 AND 6 RIGHT. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER PER SRM 53-04-00 FIGURE 32 AND BOEING DRAWING 5911014.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,638 hrs · 35,390 cycles

CROWN SKIN CRACKED AT STATION 1309, BETWEEN LONGERONS 7 AND 6 LEFT. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER PER SRM 53-04-00 FIGURE 32 AND BOEING DRAWING 5911014.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,638 hrs · 35,390 cycles

CABIN SEAT TRACK NUMBER 5 CORRODED. REMOVED AND REPLACED SECTION OF SEAT TRACK PER SRM 53-05-00 FIGURE 4 SHEET 1.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,638 hrs · 35,390 cycles

CABIN, FOWARD GALLEY TIEDOWN FITTING AT STATION 210, RIGHT BUTTLINE 11 CORRODED. REMOVED AND REPLACED TIEDOWN FITTING PER AARD 51-00-05-1 AND BOEING DRAWING 9936535.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,638 hrs · 35,390 cycles

CABIN, FOWARD GALLEY TIEDOWN FITTING AT STATION 161, RIGHT BUTTLINE 10 CORRODED. REMOVED AND REPLACED TIEDOWN FITTING PER AARD 51-00-05-1 AND BOEING DRAWING 9936534.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,638 hrs · 35,390 cycles

CABIN, FORWARD GALLEY TIEDOWN FITTING AT STATION 161, RIGHT BUTTLINE 45 CORRODED. REMOVED AND REPLACED TIEDOWN FITTING PER AARD 51-00-05-1 AND BOEING DRAWING 9936534-517.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,638 hrs · 35,390 cycles

CABIN, FOWARD GALLEY TIEDOWN FITTING AT STATION 218, RIGHT BUTTLINE 11 CORRODED. REMOVED AND REPLACED TIEDOWN FITTING PER AARD 51-00-05-1 AND BOEING DRAWING 9936535.

Part: DUCT — BROKEN (AC BAY) · airframe 67,547 hrs · 35,341 cycles

DFW - CREW REPORTED "TAIL COMPT TEMP HI LIGHT" ILLUMINATED ON CLIMBOUT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DUCT THAT WAS BROKEN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY — OUT OF POSITION (COCKPIT) · airframe 66,210 hrs · 34,579 cycles

EMERGENCY LIGHTS IN COCKPIT STAY ON WITH SWITCH OFF (EMERGENCY SWITCH NO HELP). REPOSITIONED BATTERIES IN FORWARD EMERGENCY LIGHT PACK. OPS CHECKS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 65,673 hrs · 34,277 cycles

EMERGENCY EXIT LIGHTS FOR COCKPIT PORT FRONT DOORS AND FIRST CLASS OVERHEAD AISLE LIGHTS INOPERATIVE. REPLACED CHARGER AND BATTERIES, OPS CHECK NORMAL.

Part: DOWNLOCK SENSOR — INOPERATIVE (RT MLG) · airframe 64,819 hrs · 33,803 cycles

TUS - CREW REPORTED LOWERED GEAR AND GOT ALL 3 GREEN, BUT ON FINAL GOT GEAR WARNING HORN AND UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR AND WARNING INDICATION REMAINED. EMERGENCY DECLARED FLIGHT LANDED TUS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT GEAR DOWN AND LOCK SENSOR D-127. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CLAMP — BROKEN (AC BAY) · airframe 63,741 hrs · 33,197 cycles

DFW - CREW REPORTED TAIL COMPARTMENT TEMPERATURE OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED QRH AND LIGHT EXTINGUISHED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CLAMP FROM AIR CYCLE MACHINE TO HEAT EXCHANGER THAT WAS BROKEN. REPLACED JOINT SEALS ON LEFT PACK TO HEAT EXCHANGER THAT WERE LEAKING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,892 hrs · 32,750 cycles

LEFT NUMBER 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NUMBER 1 DOOR BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,892 hrs · 32,750 cycles

AFT CATWALK EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP AT AFT OVERHEAD PANEL AT CATWALK. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 62,892 hrs · 32,750 cycles

ROW 21A EMERGENCY EXIT SIGN IS OPERATIVE. REPLACED LAMP FOR ROW 21A EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (AC BAY) · airframe 62,892 hrs · 32,750 cycles

TAIL CONE CATWALK CEILING EMERGENCY LIGHT IS INOPERATIVE. REPLACED LAMP FOR TAIL CONE CATWALK CEILING EMERGENCY LIGHT. OPS CHECKS NORMAL.

Part: ACM — SEIZED (AC BAY) · airframe 62,041 hrs · 32,289 cycles

STL - INFLIGHT ORD-DFW. CREW REPORTED CABIN PRESSURIZATION PROBLEMS AND FLOW LIGHT ILLUMINATED, 500 TO 600 FPM CLIMB IN CABIN. FOLLOWED QRH PROCEDURE AND CABIN CONTINUED TO CLIMB. EMERGENCY DECLARED FLIGHT DIVERTED STL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT AIR CYCLE MACHINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: VANE — GOUGED (TE FLAP) · airframe 60,316 hrs · 31,339 cycles

LEFT NUMBER 5 FLAP VANE IS GOUGED. BLENDED OUT MINOR SCRATCHES AND APPLIED HOT BOND REPAIR PER SRM 51-70-02.

Part: VANE — GOUGED (TE FLAP) · airframe 60,316 hrs · 31,339 cycles

RIGHT WING FLAP VANES NUMBER 5 FLAP VANE HAS DEEP GOUGES IN UPPER SIDE. INSTALLED HOT BOND REPAIR PER SRM 51-70-2.

Part: BATTERY — NOT SEATED (CABIN) · airframe 57,434 hrs

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,434 hrs

LGA AFT EXTERIOR FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REPLACED LAMP AFT EXTERIOR FUSELAGE EMERGENCY LIGHTS.

Part: BATTERY — NOT SEATED (CABIN) · airframe 57,434 hrs

LGA TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERIES FOR TAIL COMPARTMENT EMERGENCY LIGHTS.

Part: PROXIMITY SENSOR — FAILED (ZONE 700) · airframe 56,329 hrs

LAX, INFLIGHT PSP TO DFW - CREW REPORTED UNSAFE NOSE LANDING GEAR INDICATION ON TAKEOFF. EXTENDED MAIN LANDING GEAR WITH THREE GREEN INDICATIONS. DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED D1 32 PROXIMITY SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FRAME — CRACKED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

0.250 CRACK AT RIGHT CANT FRAME STATION 1474, AFT OF ELEVATOR ACCUMULATOR ACCESS. 5.5 INCH BY 3.5 INCH, .040 7075 T6 DOUBLER INSTALLED AFTER END OF CRACK STOP DRILLED.

Part: STRAP — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

STRAP CORRODED IN LONGERON 23L FROM 1287 TO 1306. REMOVED AND REPLACED WITH SERVICEABLE STRAP.

Part: BRACKET — CRACKED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

NUMBER 4 SEAT TRACK SUPPORT BRACKET CRACKED STATION 864. REMOVED AND REPLACED WITH SERVICEABLE SUPPORT BRACKET.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CORROSION ON SEAT TRACK BLENDED BEYOND LIMITS. REPLACED SEAT TRACK.

Part: GUSSET — CRACKED (ZONE 200) · airframe 56,272 hrs · 29,153 cycles

GUSSET IS CRACKED AT LEFT STATION 207 WHERE IT ATTACHES TO INTERCOSTAL AT LONGERON 15 LEFT. INSTALLED "T" DOUBLER AT STATION 207 AND LONGERON 15 LEFT PER SRM 53-10-00-11.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CORROSION ON CUSP FROM STATION 598 TO STATION 617 LEFT HAND. REMOVED AND INSTALLED SERVICEABLE CUSP SHEET FROM STATION 598 TO STATION 712 PER AARD 53-20-00-16.

Part: BEAM — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CARGO DOOR BEAM CORRODED/PITTED IN SEVERAL AREAS FROM STATION 1155 TO STATION 1211. BLENDED CORROSION, REMOVED CORROSION, WITHIN LIMITS PER ESO 80559 DATED 11/21/08.

Part: CUSP WEB — CRACKED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CRACK IN CUSP AT LIGHTENING HOLE STATION 222 LEFT AT NR 2 SEAT TRACK. REPAIRED CUSP PER AARD 53-20-00-16 USING NEW CUSP MATERIAL FROM STATION 218 TO STATION 237.

Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CORROSION ON AFT CARGO DOOR CUT-OUT BOX FRAME FORWARD SIDE OF DOOR, STATION 1148 TO STATION 1155 BETWEEN LONGERON 26 RIGHT AND LONGERON 27 RIGHT. BLENDED OUT DAMAGE, FOUND TO BE OUT OF LIMITS. INSTALLED WEB REPAIR PER ESO 80559 DATED 11/26/08.

Part: LONGERON — CRACKED (ZONE 200) · airframe 56,272 hrs · 29,153 cycles

LONGERON 4 LEFT CRACKED AT STATION 160 AND STATION 200. REMOVED LONGERON FROM END CAP AT STATION 148 TO PRODUCTION SPLICE AT STATION 234. INSTALLED NEW LONGERON.

Part: STOP FITTING — CORRODED (ZONE 200) · airframe 56,272 hrs · 29,153 cycles

AFT DOOR FRAME STOP FITTING CORROSION. REMOVED AND REPLACED FITTING.

Part: SKIN — CRACKED (ZONE 300) · airframe 56,272 hrs · 29,153 cycles

CRACK IN RIGHT ELEVATOR UPPER SKIN ALONG TOE, OUTBOARD OF GEAR TAB. INSTALL DOUBLER REPAIR PER ESO 80559 DATED 11/25/08.

Part: ANGLE — CRACKED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CRACK IN TEE ANGLE OUTBOARD AND AFT OF VENTRAL STAIRS ACTUATOR RIGHT SIDE, 1497 TO 1510 CANT FRAME. INSTALLED NEW TEE ANGLE PER SRM 51-30-05.

Part: STOP FITTING — CORRODED (ZONE 200) · airframe 56,272 hrs · 29,153 cycles

AFT DOOR FRAME STOP FITTING CORROSION. REMOVED AND REPLACED FITTING.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CORROSION AROUND TIE DOWN TRACK FASTENERS LEFT SIDE STATION 1210 TO 1322 (AFT CARGO). REMOVED AND REPLACED WITH SERVICEABLE TRACK PER SRM 51-10-01.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

TIE DOWN TRACK SPLICE PLATE CORRODED STATION 1212 TO 1225 (AFT CARGO, LEFT SIDE). REMOVED AND REPLACED WITH SERVICEABLE TRACK SPLICE PLATE.

Part: BRACKET — CRACKED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

NUMBER 3 SEAT TRACK LOWER SUPPORT BRACKET CRACKED AT STATION 864. REMOVED AND REPLACED WITH SERVICEABLE BRACKET.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CORROSION ON CUSP STATION 560 TO 579, LEFT SIDE. REPAIRED PER AARD 53-20-00

Part: STIFFENER — CRACKED (ZONE 200) · airframe 56,272 hrs · 29,153 cycles

STIFFENER CRACKED ABOVE VAULT DOOR JAMB O TOP FORWARD SIDE STATION 1338. REPAIRED PER AARD 53-10-00-15.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CORROSION ON CUSP STATION 1022, LEFT SIDE. REPAIRED PER SRM 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CORROSION ON CUSP STATION 579 TO 598 LEFT SIDE. REPAIRED PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CORROSION TOP LEFT CUSP FROM STATION 1136 TO STATION 1174. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

NR 6 SEAT TRACK CORROSION OUT OF LIMITS STATION 855 TO STATION 857. REMOVED CORROSION ROUTED AND INSTALLED SEAT TRACK PLUG.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CORROSION ON NUMBER 1 SEAT TRACK STATION 470. INSTALLED REPAIR PLUG AARD 53-20-00-10.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CENTER WING, INTERCOSTAL LOWER SUPPORT ANGLE CRACKED STATION 825. REPAIRED PER ESO 80559 DATED 11-21-08.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CORROSION ON CUSP FROM STATION 1164 TO STATION 1178. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

NR 3 SEAT TRACK HAS CORROSION OUT OF LIMITS. REMOVED CORROSION, ROUTED AND INSTALLED SEAT TRACK PLUG.

Part: BRACKET — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

CORROSION ON TOP OF GIRT BAR BRACKET, AFT SERVICE DOOR, FORWARD BRACKET. REPLACED GIRT BAR BRACKET.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

FORWARD CARGO, RIGHT SIDE STATION 237 INTERCOSTAL ATTACH ANGLE AT FRAME BELOW TIE DOWN TRACK IS CRACKED. REMOVED AND REPLACED WITH SERVICEABLE ANGLE PER SRM 51-01-00.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 56,272 hrs · 29,153 cycles

NR 6 SEAT TRACK CORROSION OUT OF LIMITS STATION 933 TO STATION 936. REPAIRED DAMAGE BY INSTALLING PLUG PER AARD 53-20-00-10.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 56,272 hrs · 29,153 cycles

WINDOW FRAME, CRACK IN FRAME TOP CORNER RIGHT SIDE STATION 886. REPAIRED PER AARD 53-10-00-25.

Part: FRAME — CRACKED (ZONE 200) · airframe 56,272 hrs · 29,153 cycles

WINDOW FRAME, CRACK IN FRAME TOP CORNER LEFT SIDE STATION 1060. REPAIRED PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 56,272 hrs · 29,153 cycles

WINDOW FRAME, CRACK IN FRAME TOP AFT CORNER RIGHT SIDE STATION 1079. REPAIRED PER AARD 53-10-00-25.

Part: FRAME — CRACKED (ZONE 200) · airframe 56,272 hrs · 29,153 cycles

WINDOW FRAME, CRACK IN FRAME TOP CORNER LEFT SIDE STATION 1098. REPAIRED PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 56,272 hrs · 29,153 cycles

WINDOW FRAME, CRACK IN FRAME AFT TOP CORNER RIGHT SIDE STATION 1060. REPAIRED PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 56,272 hrs · 29,153 cycles

WINDOW FRAME, CRACK IN FRAME TOP CORNER RIGHT SIDE STATION 927. REPAIRED PER AARD 53-10-00-25.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 66,136 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 12 TO 16 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 13DEF FOR INOPERATIVE EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 12 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,682 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 32 INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 32. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,682 hrs

LGA - EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — BROKEN (FLASHLIGHT)

LGA - EMERGENCY FLASHLIGHT AT AFT CABIN HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY EXIT LIGHT SIGN AT AFT CABIN DOOR DAMAGED. REPLACED EMERGENCY EXIT LIGHT SIGN AT AFT CABIN DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 25 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEAT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT OVERHEAD TAIL CONE INOPERATIVE. REPLACED BATTERY PACK B5 27 FOR OVERHEAD EMERGENCY LIGHTS AT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CYLINDER — INOPERATIVE (NLG)

INFLIGHT T1107/22AUG CREW REPORTED NOSE GEAR VIBRATION AFTER GEAR RETRACTION THAT INCREASED AS THEY ACCELERATED. LANDED TPA WITHOUT INCIDENT. REPLACED LT AND RT GEAR DOOR CYLINDERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: COVER — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT AFT STAIRS AFT FLIGHT ATTENDANT JUMPSEAT COVER MISSING. REPLACED COVER FOR EMERGENCY LIGHT AT AFT STAIRS AFT FLIGHT ATTENDANT JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FUEL CONTROL — INOPERATIVE (ZONE 600)

JFK - DURING IDLE POWER DESCENT RIGHT HAND ENGINE BECAME INRESPONSIVE. AT LEVEL OFF ADVANCED THROTTLE AND ENGINE N1 REMAINED AT 20 PERCENT. RIGHT ENGINE GAS TEMPERATURE 200 DEGREES AND LOW FUEL FLOW. ACCOMPLISHED QRH ENGINE FAILURE INFLIGHT SHUT DOWN CHECKLIST. ENGINE WINDMILLED BUT WOULD NOT RESTART PER CHECKLIST. DURING WINDMILL N1 APPROXIMATELY 20 PERCENT AND NORMAL OIL QUANTITY AND PRESSURE. N2 WAS 30 PERCENT DURING WINDMILL. LANDED JFK WITHOUT INCIDENT. REPLACED FUEL PUMP AND FUEL CONTROL FOR RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

ORD - CEILING EMERGENCY LIGHTS BETWEEN ROWS 13 AND 19 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS BETWEEN ROWS 13 AND 19. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (CABIN PRESSURE)

ORD INFLIGHT T2301/08NOV, SHORTLY AFTER TAKEOFF AIRCRAFT HAD PRESSURIZATION PROBLEM. CREW DROPPED OXYGEN MASKS AND RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED OUTFLOW VALVE ACTUATORS, SELECTOR, BOTH PRESSURE CONTROLLERS, AND LEFT OXYGEN CANISTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LINKAGE — SHEARED (NLG)

RDU - INFLIGHT T583/22 STRONG VIBRATION FROM NOSE GEAR ON TAKEOFF JUST AFTER GEAR RETRACTION. RETURNED TO RDU AND LANDED WITHOUT INCIDENT. FOUND SHEARED BOLT ON UNLOCK HANDLE ON GEAR DOOR. REPLACED LEFT GEAR DOOR LINKAGE AND ADJUSTED LEFT AND RIGHT LINKAGE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SEA - SEVERAL AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

PHX AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK/CHARGER AT STATION 1190R FOR AFT CABIN CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: ENGINE — FAILED (RIGHT)

ABQ INFLIGHT T1508 ON TAKE OFF ON ROTATION HEARD A LOUD BANG FROM RIGHT ENGINE ACCOMPANIED BY POWER LOSS AND AIRCRAFT YAW. RETURNED FOR LANDING. NUMBER 1 AND NUMBER 2 HAD ROTATION OIL PRESSURE ALSO IN GREEN. RETURNED TO ABQ AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. CHANGED RIGHT HAND ENGINE DUE TO NUMBER 2 ENGINE TURBINE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — LOOSE (CABIN)

DFW - EMERGENCY CEILING LIGHTS AT SEATS 7 THROUGH 10 INOPERATIVE. RELAMPED BATTERY PACK FOR EMERGENCY CEILING LIGHTS AT SEATS 7 THROUGH 10. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

RDU FORWARD AUXILIARY EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD AUXILIARY EXIT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SECTION 22 THROUGH 26 DIM. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DOWNLOCK SENSOR — OUT OF ADJUST (NLG)

TPA - FLT 408 - ON LANDING TOUCHDOWN AT TPA NOSE GEAR WARNING RED LIGHT AND AURAL WARNING SOUNDED. GO AROUND EXECUTED. ACCOMPLISHED EMERGENCY PROCEDURE, GEAR LOWERED NORMALLY WITHOUT FURTHER INCIDENT. LANDED TPA WITHOUT FURTHER INCIDENT. NOSE GEAR PIN INSTALLED AFTER LANDING. ADJUSTED NOSE GEAR DOWN LOCK SENSOR GAP TO PROPER DIMENSION. CHANGED PROXIMITY BOX AS A PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEATS AND SIDE WALL INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE AT SEAT 19DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — GOUGED (FUSELAGE)

TUL - FOUND GOUGES IN DOOR CUT OUT WEB UNDER RIGHT TIE DOWN TRACK STATION 1215. REMOVED AND REPLACED WEB ASSEMBLY, SRM 51-01. (M)

Part: TRACK — CORRODED (FUSELAGE)

TUL - FOUND 1.5 INCH BY 13 INCHES OF CORROSION ON BOTTOM OF LEFT TIE DOWN TRACK STATION 1212-1225 AT FASTENER HOLES. REMOVED CORROSION. INSTALLED DOUBLER PER AARD 53-20-00-13. (M)

Part: FRAME — DAMAGED (AFT CARGO BAY)

TUL - FOUND DAMAGED BELL FRAME STATION 1231 BETWEEN LONGERON 26L AND LONGERON 24L. INSTALLED DOUBLER PER ESO 80559 DATED 12-7-2000. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT LEFT FUSELAGE STATION 229 BELOW LONGERON 19, .125 INCH DEEP. INSTALLED DOUBLER PER SRM 53-04 FIG 38-24. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN SKIN AT TWO FASTENERS FS 1380 ABOVE 14R. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND 3 DENTS JUST ABOVE LEFT LONGERON 18 STATION 237. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN FUSELAGE SKIN STATION 222 LEFT SIDE ABOVE LONGERON 16L. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND .125 INCH DEEP DING APPROX .75 INCH LONG 4 INCHES FORWARD OF LEFT AOA VANE AT LONGERON 19. INSTALLED DOUBLER REPAIR PER AARD 53-30-00-2. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FS 1380 LONGERON 13L TO 14L SKIN CRACKED .5 INCH BY 3 INCHES, AT 3 FASTENER HOLES. REMOVED DAMAGE. INSTALLED DOUBLER REPAIR PER SRM 53-01. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND SKIN DENTED 1 INCH BY 1.5 INCH AREA, ABOVE FORWARD LAVATORY SERVICE PANEL STATION 266 ABOVE LONGERON 19, .0625 IN DEEP AND 1 INCH LONG. CUT OUT DAMAGED AREA. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 25. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 6 SEAT TRACK CORRODED AT FORWARD CLOSET STATION 218-215 TIE DOWN AND TRACK ASSY. REPAIRED IAW ESO80559 DATED 11/29/2000. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND INTERIOR SKIN AT STATION 1184 HAS DEEP BLENDS INTO 1ST LAYER OF SKIN, 1.5 INCH BY 2.5 INCH. CUT OUT DAMAGED AREA. INSTALLED DOUBLER REPAIR PER ESO 80559 DATED 11-29-2000. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND SMALL DENT, 2.5 INCH BY 2.5 INCH, LEFT FUSELAGE STATION 315 BETWEEN LONGERON 22 AND 23. CUT OUT DAMAGE AND INSTALLED DOUBLER AND PLUG PER SRM 53-04 FIG 38. (M)

Part: DOUBLER — WRONG PART (FUSELAGE)

TUL - FOUND CLASS II DOUBLER REPAIR INSTALLED ON RIGHT SIDE OF FUSELAGE BETWEEN LONGERON 22R AND 23R STATION 1309. INSTALLED CLASS I FINGER DOUBLERS PER SRM 53-04, FIG 12B. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION .5 INCH BY .5 INCH, ON CUSP STATION 1189. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION, 1 INCH BY 6 INCH, ON CUSP STATION 160 RBL 45 - RBL 51. REMOVED AND INSTALLED NEW CUSP WEB DOUBLER PER SRM 53-01. (M)

Part: SEAT TRACK — GOUGED (CABIN)

TUL - FOUND SEAT TRACK NR 1 WORN AND GOUGED STATION 1055-1052. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION 1 INCH BY 3 INCHE AREA, ON SEAT TRACK NR 6 STATION 640. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON NR 2 SEAT TRACK, 1 INCH BY 1 INCH, AT STATION 1239. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 3 SEAT TRACK CORRODED, 1.5 INCH BY 4 INCHES, STATION 1301-1305. REMOVED CORRODED SECTION OF TRACK. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP CORRODED TOP AND BOTTOM STATION 541-560. INSTALLED CUSP DOUBLER PER SRM 53-01 FIG 4 SHT 3. (M)

Part: BEAM — CORRODED (AFT CARGO BAY)

TUL - FOUND AFT CARGO DOOR CUTOUT MAIN LOWER DOOR BEAM CORRODED STATION 1155 TO 1212, AT LONGERON 28R. REMOVED AND REPLACED DOOR FRAME LOWER BEAM SRM 51-01. (M)

Part: STRINGER — CRACKED (FUSELAGE)

TUL - FOUND STRINGER 4L CRACKED AT FASTENER STATION 160. REMOVED DAMAGED SECTION AND SPLICED IN NEW SECTION PER SRM 53-02 FIG 18. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND SUB FLOOR CRACKED STATION 176 INBOARD 12 INCHES OF FORWARD ENT DOOR OPENING, CUTOUT. REMOVED DAMAGED SECTION OF WEB. INSTALLED DOUBLER REPAIR PER AARD 53-00-00-02. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN SKIN STATION 257 BETWEEN LONGERON 8L AND 9L. COLD WORKED DENT AND INSTALLED TWO ROW DOUBLER PER SRM 53-04 FIG 38. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP BOTTOM SIDE CORRODED 2.5 INCHES BY 6 INCHES, STATION 615-617. REMOVED CORROSION. INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 4-3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION 5 INCH BY 7 INCHE AREA, ON CUSP STATION 1117-1136 RIGHT. INSTALLED REPAIR DOUBLER PER SRM 53-01 AT RIGHT CUSP STATION 1129 TO 1134. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND WINDOW FRAME CRACKED AT STATION 902 LONGERON 14R. INSTALLED DOUBLER ON WINDOW RING PAN AT STATION 902 LONGER 14R PER AARD 53-10-00-25. (M)

Part: ENGINE — FAILED (RIGHT)

DFW - FLT 225 - AFTER TAKEOFF, SMOKE IN CABIN. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT, NOT OVERWEIGHT. REPLACED RT ENGINE. ACCOMPLISHED ENGINE RUN WITH NO DEFECTS. SYSTEM GROUND CHECKED NORMAL OPERATION. SYSTEM FUNCTIONAL CHECKED NORMAL OPERATION. (M)