N7541A

Part: BATTERY — DISCHARGED (CABIN) · airframe 75,273 hrs · 39,786 cycles

AIRCRAFT WAS NOT GROUNDED. OVERHEAD CEILING EMERGENCY EXIT LIGHTS L2-711, L2-712, L2-713, L2-714, AND L2-715 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY B5-102 PER AMM 33-53-00 AND WDM 33-51-12. OPERATIONAL CHECK GOOD.

Part: INDICATOR — UNRELIABLE (COCKPIT) · airframe 74,993 hrs · 39,610 cycles

THE AIRCRAFT WAS NOT GROUNDED. AT 34000 FT, DFGC ON NR2 CAPTS MACH SHOWED .799 AND AIS ABOUT 240 KTS, F/OS SIDE .680 ABOUT 240KTS. DISCONNECTED AUTO THROTTLE AND RETURN TO .750 ON F/OS SIDE TO CAPTURE. RAN AIRSPEED UNRELIABLE CHECKLIST AND SWITCHED STATIC AIR ON CAPTS SIDE TO ALT. ON DESCENT MACH ON CAPTS SIDE WOULD READ NORMAL, THEN GO HIGH TO .760-.790 SEVERAL TIMES. THE FLIGHT DECLARED AN EMERGENCY GOING INTO COS, AND LANDED WITHOUT FURTHER INCIDENT. PERFORMED FUNCTIONAL CHECK OF CAPTS AIRSPEED IND WITH NO DEFECTS NOTED. PLACARDED CAPTS MACH INDICATOR PER MEL 34-01B. REPLACED CAS MACH AIRSPEED INDICATOR, OPS CHECK OK PER MM 34-13-01. CLEARED DEFERRAL.

Part: DOOR FRAME — CRACKED (LT MLG DOOR) · airframe 74,939 hrs · 39,576 cycles

A CRACK WAS FOUND IN THE LEFT MAIN LANDING GEAR WHEEL WELL FORWARD DOOR FRAME AT FASTENER HOLE. REPAIRED RD 53-10-00-12.

Part: DOOR FRAME — CRACKED (RT MLG DOOR) · airframe 74,939 hrs · 39,576 cycles

A CRACK WAS FOUND IN THE RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD DOOR FRAME AT FASTENER HOLE. REPAIRED IAW RD 53-10-00-12.

Part: ATTACH ANGLE — CORRODED (LT MLG) · corrosion level 2 · airframe 74,939 hrs · 39,576 cycles

CORROSION ON LEFT MAIN LANDING GEAR TRAPEZOID ATTACH ANGLE OUTBOARD AND ABOVE BRAKE ACCUMULATOR. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-30-01.

Part: FRAME — WORN (BS 1510) · airframe 74,939 hrs · 39,576 cycles

WORN AREA ON AFT ACCESSORY COMPARTMENT LOWER AFT SURFACE OF THE CANTED FRAME AT BS 1510 DUE TO INTERFERENCE WITH THE TAILCONE. REPAIRED IAW SRM 51-70-05, AND EA 257983.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 74,833 hrs · 39,504 cycles

THE AIRCRAFT WAS NOT GROUNDED. FA REPORTED FLASHLIGHT AT AFT TAIL CONE JUMPSEAT DOES NOT FLASH. REPLACED AFT FLASHLIGHT AND BATTERY. OPS TEST OK PER AMM 25-60-00.

Part: BATTERY — FAILED (CABIN) · airframe 74,586 hrs · 39,347 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT CEILING LIGHTS FROM ROWS 7 TO 11 FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY B5-100 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: MEGAPHONE — FAILED (CABIN) · airframe 74,586 hrs · 39,347 cycles

AIRCRAFT WAS NOT GROUNDED. AFT EMERGENCY CABIN PORTABLE MEGAPHONE FAILED TEST. REMOVED AND REPLACED MEGAPHONE IAW AMM 23-34-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — FAILED (CABIN) · airframe 74,586 hrs · 39,347 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT CEILING LIGHTS FROM ROWS 28 TO 30 FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY B5-107 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 74,514 hrs · 39,301 cycles

EMERGENCY LIGHT LENS COVER MISSING AT TAIL CONE RELEASE HANDLE. REPLACED THE LENS COVER AND LIGHT ASSY IAW AMM 33-53-01.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 74,514 hrs · 39,301 cycles

TAIL CONE SLIDE RELEASE HANDLE LIGHT LENS MOUNTING CLIP BROKEN ON OUTBD END. REMOVED AND REPLACED TAIL CONE SLIDE HANDLE LIGHT ASSY IAW AMM 33-53-01.

Part: BATTERY — DISCHARGED (MEGAPHONE) · airframe 74,469 hrs · 39,274 cycles

AFT MEGAPHONE INOPERATIVE. REPLACED AFT MEGAPHONE BATTERIES IAW GENERAL MAINT PRACTICES. CKS GOOD. THE AIRCRAFT WAS NOT GROUNDED.

Part: BOOT — DISCONNECTED (AC BAY) · airframe 74,280 hrs · 39,166 cycles

AIRCRAFT WAS GROUNDED. ORD-DTW FLIGHT RETURNED TO ORD ACCOUNT UNABLE TO PRESSURIZE. NO EMERGENCY DECLARED. TURNED ON LEFT PACK AND RECEIVED PRESSURIZATION FLOW LIGHT. UNEVENTFUL LANDING. LEFT PACK TURBINE DISCHARGE DUCT BOOT DISCONNECTED FROM TURBINE DISCHARGE PORT. RECONNECTED DUCT IAW AMM 21-51-01. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 74,249 hrs · 39,144 cycles

EMERGENCY EXIT LIGHT FORWARD GALLEY LOWER AISLE WALL HAS A DETACHED LENS. REPLACED THE LENS AND ASSEMBLY IAW AMM 33-60-98. OPS CHECKED GOOD.

Part: SUPPORT — CRACKED (BS 218 BULKHEAD) · airframe 74,222 hrs · 39,129 cycles

CRACKED SUPPORT STRUT ON BULKHEAD LOWER END BETWEEN STRINGER 23L AND 24L. REPAIRED SUPPORT STRUT PER SRM 53-01-00-001.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,222 hrs · 39,129 cycles

AIRCRAFT IN BASE MAINTENANCE.. CRACK ON UPPER FASTENER HOLE AT LONGERON 25L. INSTALLED LONGERON REPAIR SECTION PER SRM 51-30-00, SRM 53-02-00 AND AARD 53-00-00-05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,222 hrs · 39,129 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK IN LONGERON LOWER FASTENER AT LONGERON 24L AND STATION 200. REPAIRED LONGERON PER SRM 51-30-00.

Part: LINE — FAULTY (HYDRAULIC SYS) · airframe 73,955 hrs · 38,960 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED ON APPROACH ACCOUNT RIGHT HYDRAULIC PUMP FAILURE. LANDING UNEVENTFUL. REMOVED AND REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP ASSEMBLY IAW AMM 29-10-05 (AALA20170106036) AND THE ENGINE DRIVEN HYDRAULIC SUPPLY LINE IAW AMM 20-30-02. OPERATIONAL AND LEAK CHECK GOOD.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 73,955 hrs · 38,960 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED ON APPROACH ACCOUNT RIGHT HYDRAULIC PUMP FAILURE. LANDING UNEVENTFUL. REMOVED AND REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP ASSEMBLY IAW AMM 29-10-05 AND THE ENGINE DRIVEN HYDRAULIC SUPPLY LINE IAW AMM 20-30-02 (AALA20170110009). OPERATIONAL AND LEAK CHECK GOOD.

Part: PROXIMITY SENSOR — FAULTY (NLG) · airframe 73,917 hrs · 38,937 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. ON APPROACH, NOSE LANDING GEAR WARNING INDICATION LIGHT ILLUMINATED AFTER EXTENDING LANDING GEAR. LANDING GEAR WAS RECYCLED BUT LIGHT REMAINED RED. LANDING UNEVENTFUL. REMOVED AND REPLACED UP POSITION PROXIMITY SENSOR IAW AMM 32-60-05. OPERATIONAL CHECK GOOD.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 73,680 hrs · 38,784 cycles

AIRCRAFT NOT GROUNDED. R1 EMERGENCY EVACUATION DOOR IS DIFFICULT TO ARM. ADJUSTED GIRT BAR CLIP IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 73,676 hrs · 38,781 cycles

AIRCRAFT NOT GROUNDED. R1 DOOR EVACUATION SLIDE GIRT BAR LANYARD APPEARS TO BE IN THE WRONG SIDE LEATHER GIRT BAR POUCH. REROUTED LANYARD IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — INFLT SEPARATION (CABIN) · airframe 73,614 hrs · 38,752 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT AT SEAT 12D INOPERATIVE. REMOVED AND REPLACED LIGHT IAW AMM 33-50-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 73,526 hrs · 38,694 cycles

L1 DOOR EMERGENCY FLASHLIGHT WILL NOT TEST. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW 25-60-00. OPS CHECKED NORMAL.

Part: FRAME — WORN (FUSELAGE) · airframe 71,656 hrs · 37,585 cycles

AFT ACCESSORY STATION 1510 FRAME WORN FROM CONTACT WITH TAIL CONE ON BOTTOM RT. REPAIRED FRAME 1510 IAW EA 257983 & SRM 51-70-05. ACFT IN BASE MX.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 71,656 hrs · 37,585 cycles

FORWARD CARGO, FWD BOTTOM DOOR STOP FITTING CRACKED. INSTALLED NEW DOOR STOP FITTING PN CDK2345-3 IAW AARD 51-00-05. ACFT IN BASE MX.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 71,656 hrs · 37,585 cycles

FUSELAGE E & E COMPARTMENT, CRACK AT INBD END OF CEILING INTERCOSTAL, LT OF L30 AT STATION 180. INSTALLED DOUBLER IAW SRM 51-70-04-01 & NEW CLIP IAW AARD 51-00-05-1. ACFT IN BASE MX.

Part: WIRE — BROKEN (CABIN) · airframe 69,960 hrs · 36,614 cycles

EMERGENCY PATH LIGHT AT SEAT 20D IS INOPERATIVE. FOUND BROKEN WIRE AT SEAT 20D. REPAIRED WIRE IAW AMM 20-10-03. SYS CHECKED NORMAL.

Part: CYLINDER — FAULTY (NLG) · airframe 69,575 hrs · 36,377 cycles

DURING APPROACH, GEAR WAS SLOW TO EXTEND & NOSE GEAR INDICATED UNSAFE, RED LIGHT ILLUMINATED & NLG PIN EXTENSION DID NOT EXTEND. USED ALTERNATE GEAR EXTENSION HANDLE & PERFORMED FLYBY, ALL 3 GEARS EXTENDED. EMERGENCY DECLARED & LANDING UNEVENTFUL. R & R NOSE GEAR BUNGEE CYLINDER IAW AMM 32-32-07. PERFORMED NOSE GEAR LINKAGE ADJUSTMENT & TESTED IAW 32-21-03. PERFORMED LEAK & OPERATIONAL CHECKS. SYS CHECKED NORMAL.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 69,182 hrs · 36,160 cycles

AIR INTERRUPT, DIVERTED & AN EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE THE STANDBY ATTITUDE INDICATOR FAILED & RED FLAG CAME INTO VIEW. R & R THE STANDBY HORIZON INDICATOR IAW AMM 34-28-01 & INVERTER IAW AMM 34-28-02. SYS CHECKED NORMAL.

Part: NOSE BULLET — DETACHED (NR 1 ENGINE) · airframe 68,943 hrs · 36,025 cycles

AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING TAKEOFF THE NR 1 ENG EXPERIENCED COMPRESSOR STALLS. UPON INSPECTION FOUND NOSE BULLET LIBERATED FROM ENG & RESTING IN INLET. REPLACED INLET BULLET IAW AMM 71-10-00. R & R NOSE COWL IAW AMM 71-10-01 & FRONT ACCESSORY DRIVE IAW AMM 72-23-07. PERFORMED MCM 72-96-11 BORESCOPE INSPECTION WITH NO DAMAGE NOTED. PERFORMED POWER ASSURANCE RUN IAW AMM 72-00-00 & BLEED SYS CHECK IAW AMM 72-00-00. SYS CHECKED NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,092 hrs · 35,526 cycles

CRACK IN FUSELAGE SKIN AT STATION 1307 & LONGERON 14 LT. INSTALLED DOUBLER IAW EA.

Part: FITTING — CRACKED (LT SPOILER) · airframe 68,092 hrs · 35,526 cycles

LEFT WING INBD GND SPOILER CASTING CRACKED AT OTBD FWD CORNER. REPLACED CASTING FITTING.

Part: FITTING — CRACKED (RT SPOILER) · airframe 68,092 hrs · 35,526 cycles

RIGHT WING GND SPOILER CASTING CRACKED AT INBD FWD CORNER. REPLACED CASTING FITTING.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 68,092 hrs · 35,526 cycles

CORROSION FOUND ON LT TIE DOWN TRACK IN AFT CARGO AT STATIONS 1191, 1195 & 1232. CUT OUT CORROSION, INSTALLED STRAPS & FILLERS IAW AARD 53-20-00-13.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,092 hrs · 35,526 cycles

INTERCOSTAL FROM STATIONS 1309 TO 1322 LT SIDE UNDER TIE DOWN TRACK CORRODED. INSTALLED NEW INTERCOSTAL IAW AARD 51-00-05-1.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,092 hrs · 35,526 cycles

VAULT DOOR CTR RT STOP INTERNAL STIFFENER CRACKED AT TOP FASTENER HOLE. INSTALLED NEW STIFFENER IAW AARD 51-00-05-1 & DWG 5917579.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,092 hrs · 35,526 cycles

FRAME WEB SUPPORT CORRODED AT STATION 1193 AFT CARGO. R & R WEB SUPPORT BRACKET IAW AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,092 hrs · 35,526 cycles

CORROSION AT SEAT TRACK NR 4 BETWEEN STATIONS 1290 TO 1302. INSTALLED NEW SEAT TRACK & SPLICE FROM STATIONS 1241 TO 1307 IAW SRM 53-05-00 FIGURE 4F.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,092 hrs · 35,526 cycles

CRACK IN FUSELAGE SKIN AT STATION 1309 & LONGERON 14 LT. CRACK CUT OUT, DOUBLER & FILLER INSTALLED IAW EA.

Part: SKIN — GOUGED (ENTRY DOOR) · airframe 68,092 hrs · 35,526 cycles

FORWARD ENTRY DOOR IN CTR OF DOOR ABOVE HANDLE HUB & BELOW WINDOW INSIDE HAS DEEP GOUGE IN DOOR SKIN. INSTALLED REPAIR DOUBLER IAW SRM 52-05-00-001 FIGURE 66 & EA COMP-52-036401.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,092 hrs · 35,526 cycles

SUB FLOOR UNDER AFT GIRT BAR FITTING IS CORRODED AT STATION 1170. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 68,092 hrs · 35,526 cycles

CRACK ON VERTICAL SUPPORT AT STATION 845. INSTALLED NEW SUPPORT IAW AARD 51-10-00-5.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 68,092 hrs · 35,526 cycles

RIGHT AFT OVERWING EXIT DOOR PAN CRACKED AT NR 12 STOP. ACCOMPLISHED REPAIR IAW SRM 52-05-00-001 FIGURE 51 SHEET 3.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 68,092 hrs · 35,526 cycles

AUXILIARY POWER UNIT ENCLOSURE HAS DEEP GOUGE IN EXISTING REPAIR. ACCOMPLISHED REPAIR IAW AARD 53-20-00 REPAIR 11.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 68,092 hrs · 35,526 cycles

CRACK ON VERTICAL SUPPORT AT STATION 864. INSTALLED NEW SUPPORT IAW SRM 53-14-03.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 68,092 hrs · 35,526 cycles

CRACK ON VERTICAL SUPPORT AT STATION 826. INSTALLED NEW SUPPORT IAW AARD 51-10-00-5.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,092 hrs · 35,526 cycles

RIGHT CUSP AT STATION 294 INBD OF NR 6 SEAT TRACK CRACKED. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,092 hrs · 35,526 cycles

RIGHT CUSP SHEET FROM STATIONS 218 TO 237 CRACKED. REPLACED CUSP SHEET IAW AARD 53-20-00-16.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,092 hrs · 35,526 cycles

ANGLE CRACKED FROM STATIONS 1400 TO 1436. REPLACED ANGLE IAW AARD 53-30-00-7.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,092 hrs · 35,526 cycles

SEAT TRACK NR 6 WAS CORRODED FROM STATIONS 216 TO 294. CORRODED SECTION OF SEAT TRACK NR 6 WAS REMOVED FROM STATIONS 216 TO 303 & NEW SECTION SPLICED IN IAW SRM 53-05-00 FIGURE 4F.

Part: RIB — CRACKED (LT WING) · airframe 68,092 hrs · 35,526 cycles

LEFT WING INBD RIB CRACKED AT NR 4 SLAT TRACK. INSTALLED NESTED ANGLE REPAIR IAW EA MD80-57-036356.

Part: RIB — CRACKED (RT WING) · airframe 68,092 hrs · 35,526 cycles

RIGHT WING INBD RIB CRACKED AT NR 4 SLAT TRACK. INSTALLED NESTED ANGLE REPAIR IAW EA MD80-57-036356.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,092 hrs · 35,526 cycles

FUSELAGE SKIN FROM STATIONS 1417 TO 1418 BETWEEN LONGERONS 2 TO 3 LT CRACKED. INSTALLED DOUBLER IAW SRM 53-04-00 FIGURE 40.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 67,188 hrs · 34,980 cycles

THREE LOOSE FASTENERS FOUND ON DETAILED INSPECTION OF VERTICAL STAB LE AT STATION ZFS 52.267 ABOVE THE SPLICE. FURTHER INSPECTION FOUND 7 EXISTING FASTENER HOLES WITH REPAIR COUNTERSUNK BUSHINGS INSTALLED & 14 ADDITIONAL FASTENER HOLES THAT WERE ELONGATED. ENLARGED 14 1/4 FASTENER & 3 3/16 FASTENER HOLES FOR REPAIR COUNTERSUNK BUSHINGS. INSTALLED REPAIR COUNTERSUNK BUSHINGS IN HOLES IAW SRM 55-03-00-001.

Part: DOUBLER — DAMAGED (VERTICAL STAB) · airframe 67,188 hrs · 34,980 cycles

SEVEN LOOSE FASTENERS FOUND ON DETAILED INSPECTION OF VERTICAL STAB LE AT STATION ZFS 52.267 BELOW THE SPLICE. REMOVED EXISTING SMALL DOUBLER & FOUND 18 1/4 FASTENER & 11 3/16 FASTENER HOLES TO BE ELONGATED. INCREASED DIAMETER OF HOLES & INSTALLED STRAIGHT SLUG BUSHINGS IN HOLES. INSTALLED NEW LARGER DOUBLER OVER REPAIRED HOLES IAW SRM 55-03-00 & DWG SGO9550004.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 64,532 hrs · 33,494 cycles

FORWARD ENTRY DOOR FLOOR EMERGENCY LIGHT COVER SMASHED AND WIRES PULLED FROM CONNECTOR. REPLACED BASE LIGHT ASSEMBLY. OPS CHECKED NORMAL.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 63,270 hrs · 32,813 cycles

FUSELAGE SKIN FORMER (SHEAR TIE) DAMAGED AT STATION 427 BETWEEN LONGERONS 20 AND 21 LEFT. INSTALLED SHEAR TIE REPAIR PER SRM 53-03-00 FIGURE 3.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 63,270 hrs · 32,813 cycles

FUSELAGE SKIN FORMER (SHEAR TIE) DAMAGED AT STATION 446 BETWEEN LONGERONS 20 AND 21 LEFT. INSTALLED SHEAR TIE REPAIR PER SRM 53-03-00 FIGURE 3.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,709 hrs · 32,481 cycles

CEILING EMERGENCY LIGHTS IN COACH CLASS INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FROM SEAT ROWS 14 TO 16. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,709 hrs · 32,481 cycles

FIRST CLASS CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR FIRST CLASS CEILING EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: DOUBLER — CRACKED (VERTICAL STAB) · airframe 62,508 hrs · 32,360 cycles

VERTICAL STABILIZER LEADING EDGE -503 DOUBLER HAS CRACK AT NUMBER 19 LOWER 3/16 FASTENER HOLE RIGHT SIDE. INSTALLED NEW -503 DOUBLER PER SRM 55-03-00.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 62,343 hrs · 32,260 cycles

LEFT NUMBER 1 DOOR EMERGENCY PORTABLE LIGHT DIM. REPLACED LIGHT ASSEMBLY FOR LEFT NUMBER 1 DOOR PORTABLE LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,345 hrs · 30,078 cycles

CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT STATION 500. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,345 hrs · 30,078 cycles

ROW 13 TO 17 EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT FORWARD COACH CABIN STATION 400. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,345 hrs · 30,078 cycles

EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23D.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,345 hrs · 30,078 cycles

TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL CONE EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,345 hrs · 30,078 cycles

OVERWING ESCAPE DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,345 hrs · 30,078 cycles

FORWARD ENTRY COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY COCKPIT EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,345 hrs · 30,078 cycles

AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT RIGHT AFT LAVATORY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,345 hrs · 30,078 cycles

CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT STATION 700. OPS CHECK NORMAL.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,687 hrs · 29,165 cycles

CORROSION ON DIAPHRAGM UNDER FACTORY DOUBLER UNDER THE OUTBOARD G1 MOUNT STATION 165. INSTALLED DOUBLER STATION 160 TO 200 PER AARD53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,687 hrs · 29,165 cycles

CORROSION ON RIGHT CUSP ANGLE STATIONS 195 TO 219. INSTALLED NEW CUSP ANGLE AND REPAIR ANGLE PER SRM 53-05-00 AND BOING DRAWING J060288.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,687 hrs · 29,165 cycles

CORROSION ON CARGO DOOR CUTOUT WEB NUMEROUS PLACES. REMOVED AND REPLACED CARGO DOOR CUTOUT WEB ON FRAME STATIONS 1160 TO 1210.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,687 hrs · 29,165 cycles

CABIN RIGHT CUSP CRACKED STATION 221. INSTALLED NEW CUSP SHEET STATIONS 218 TO 237 PER SRM 51-30-02 AND 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 3 · airframe 56,687 hrs · 29,165 cycles

CORROSION ON CUSP UNDER SEAT TRACK NUMBER 6 AT STATION 238. ACCOMPLISHED DOUBLER REPAIR.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,687 hrs · 29,165 cycles

CRACKS FOUND IN RIGHT CUSP AT STATIONS 1250 TO 1309. REMOVED AND REPLACED WITH NEW SECTION OF CUSP AT STATIONS 1250 TO 1309 PER AARD 53-20-00-16 AND EA MD-80-51-010859.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,687 hrs · 29,165 cycles

CABIN RIGHT CUSP CORRODED STATIONS 641 TO 651. REMOVED CORROSION FROM RIGHT CUSP STATIONS 636 TO 693 AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,687 hrs · 29,165 cycles

HOLE IN RIGHT CUSP AT EDGE OF LIGHTENING HOLE STATION 1246 OUTBOARD OF SEAT TRACK NUMBER 6. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,687 hrs · 29,165 cycles

CORROSION ON SUB FLOOR STATIONS 200 TO 218. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,687 hrs · 29,165 cycles

CUSP MEMBRANE DAMAGE OUT OF LIMITS AT STATIONS 561 TO 566 LEFT PER SRM 51-01 FIGURE 1 SHEET 3. INSTALLED REPAIR DOUBLER STATION 552 TO 570 LEFT CUSP AS PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,687 hrs · 29,165 cycles

CRACK ON INTERCOSTAL BETWEEN FLOORBEAM CENTER LINE OF AIRCRAFT BETWEEN STATIONS 1309 AND 1287. INSTALLED INTERCOSTAL PER DRAWING 9936580 AND PER SRM 51-60-00, 51-30-05 AND AARD 51-60-00-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,687 hrs · 29,165 cycles

CORROSION UNDER AFT SERVICE DOOR FORWARD GIRT BAR ATTACH BRACKET AREA AT STATION 1140. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 56,687 hrs · 29,165 cycles

VERTICAL SEAT TRACK SUPPORT BELOW SEAT TRACK NUMBER 4 AT STATION 826 IS CRACKED. INSTALLED OF REPAIR OF VERTICAL NUMBER 4 SEAT TRACK SUPPORT AT STATION 826 PER EA MD80-53-010826.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,687 hrs · 29,165 cycles

RIGHT CUSP HAS CORROSION AT VENT BOX STATION 1165. INSTALLED REPAIR DOUBLER ON RIGHT CUSP STATIONS 1158 TO 1174 PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,687 hrs · 29,165 cycles

CUSP MEMBRANE CRACKED AT STATION 532 RIGHT. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SLAT — DENTED (LT WING) · airframe 56,687 hrs · 29,165 cycles

RIGHT WING LEADING EDGE NUMBER 1 SLAT HAS A DENT. REWORKED DENTED AREA TO BE WITHIN LIMITS. DYE CHECKED AREA AND NO CRACKS FOUND PER ESO 80117. CLEARANCE TO INSTALL PANEL PER ESO 80117.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,687 hrs · 29,165 cycles

SEAT TRACK NUMBER 5 CORROSION REMOVAL IS OUT OF LIMITS AT STATION 235. TREATED, PRIMED AND INSTALLED SERVICEABLE PLUG AT STATION 235 PER SRM 53-05-00.

Part: DOUBLER — WORN (TE FLAP VANE) · airframe 56,687 hrs · 29,165 cycles

LEFT OUTBOARD FLAP INBOARD VANE LEADING EDGE DOUBLER IS WORN THROUGH. HOT BONDED DOUBLER ON LEADING EDGE OF LEFT OUTBOARD FLAP INBOARD VANE PER SRM 51-70-02.

Part: RIB — CRACKED (LE SLAT) · airframe 56,687 hrs · 29,165 cycles

RIGHT NUMBER 5 SLAT OUTBOARD RIB IS CRACKED. REPLACED OUTBOARD DAMAGED RIB UNDER ESO 80117.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,687 hrs · 29,165 cycles

CABIN RIGHT CUSP CRACKED AT STATION 532. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: RIB — WORN (LE SLAT) · airframe 56,687 hrs · 29,165 cycles

EXCESSIVE PLAY IN OUTBOARD SLAT MOUNT KNUCKLE OF NUMBER 4 SLAT LEFT WING. REPLACED WORN OUTBOARD SLAT MOUNT RIB PER ESO 80117.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,687 hrs · 29,165 cycles

MUTIPLE 2-3 INCH HAIRLINE SCRATCHES JUST FORWARD OF FORWARD CARGO DOOR, AREA DENTED FROM INSTALLATION OF INTERNAL DOUBLER UNDER LONGERON 21 RIGHT STATIONS 351 TO 361, DENT MEASURES .019" DEEP, 2" X 1.25". REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 12B.

Part: SEAL — BROKEN (FLASHLIGHT) · airframe 53,037 hrs

LGA- EMERGENCY FLASHLIGHT SEAL AT LEFT NUMBER ONE DOOR BROKEN. REPLACED EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 52,866 hrs · 27,047 cycles

FORWARD SIDE OF AFT CARGO DOOR, LOWER STOP PAD FITTING CRACKED. FITTING WAS REMOVED AND REPLACED WITH NEW FITTING SRM 53-01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 52,866 hrs · 27,047 cycles

ANGLE CRACKED AT STATION 1474 AND LONGERON 19 LEFT. REMOVED AND REPLACED ANGLE PER SRM 53-01.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 52,866 hrs · 27,047 cycles

STIFFENER AT STATION 1418 AND LONGERON 2 RIGHT CRACKED IN 2 PLACES. INSTALLED DOUBLER PER SRM 53-01 FIGURE 2.

Part: SHROUD — DAMAGED (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 15D NEEDS NEW SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CSD — LOW PRESSURE (RT ENGINE)

DFW INFLIGHT T1436/14JUN - RIGHT ENGINE CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT CONSTANT SPEED DRIVE AND RIGHT GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: O-RING — LEAKING (APU)

ORD - AFTER TAKEOFF CREW REPORTED SMOKE IN FORWARD PART OF CABIN. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND APU OIL LEAK. REPLACED O-RING AND PERFORMED HIGH PRESSURE PNEUMATIC DUCTING BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: APU — LEAKING (APU BAY)

DFW - SMOKE IN CABIN AFTER MAXIMUM POWER TAKEOFF. SMOKE CLEARED UP DURING CLIMB. SMELLED LIKE OIL BURNING. LANDED DFW WITHOUT INCIDENT. FOUND OIL LEAK FROM APU. PERFORMED WORK CARD 21-92-12. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

DTW - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

BOS - EMERGENCY TRACK LIGHTING FROM SEAT 20DEF FORWARD INOPERATIVE. REPLACED BATTERY PACK ABOVE SEAT 20DEF AND IN FIRST CLASS GALLEY AND SPLICED TWO CHAFED WIRES FOR EMERGENCY TRACK LIGHTING FROM SEAT 20DEF FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (CABIN)

EWR - EMERGENCY LIGHTING FROM ROWS 1 TO 20 INOPERATIVE. REPAIRED WIRING AT SEAT ROW 1 FOR EMERGENCY LIGHTING FROM ROWS 1 TO 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

DFW - FORWARD CABIN SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED LIGHT SOCKETS AT SEATS 18D THROUGH 10D FOR FORWARD CABIN SEAT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DTW COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN)

TUL - EMERGENCY LIGHTS IN COCKPIT INOPERATIVE WHEN TESTED. RESET EMERGENCY LIGHT ARM AND TESTED CIRCUIT BREAKER FOR EMERGENCY LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (ROW 20)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT ROW 20 INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT AT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

ORD - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS FROM ROW 22-26 INOPERATIVE. SECURED CEILING EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM SEAT 20 FORWARD INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND DOOR BEAM HAS NUMEROUS AREAS OF CORRSOSION. DOUBLER INSTALLED PER AARD 53-10-03. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 6 SEAT TRACK NR 2 GALLEY AREA. REPAIRED PER AARD 53-20-00-04. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN RADIUS OF LONGERON 4L AT STATION 160. REMOVED CRACKED SECTION OF 4L LONG AT STATION 160 OF INSTALLED NEW SECTION PER SRM 53-02-00. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

TUL - FOUND HOLE IN OUTBOARD FLANGE OF NR 5 SEAT TRACK AT STATION 205. INSTALLED STRAP ON OUTBOARD FLANGE OF NR 5 SEAT TRACK STATION 205 PER 53-20-00-13, TREATED AND PRIMED. (M)

Part: LIGHT — INOPERATIVE (L2 DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HARNESS — INCORRECT (CABIN)

DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH SEAT LIGHTS DIM. ONE WIRE HARNESS OF DUAL BATTERY POWERED SYSTEM NOT CONNECTED DUE TO INCORRECT HARNESS LENGTH. SPLICED ADDITIONAL WIRE INTO HARNESS BETWEEN SEATS 19 AND 20. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: VALVE — LEAKING (LT TR UNIT)

DFW - FLT 892 - ON TAXI TO GATE AFTER LANDING DFW FROM FAT, CABIN FILLED WITH SMOKE. REPLACED LEFT THRUST REVERSER ISOLATION VALVE. ACCOMPLISHED PACK BURN OUT OF BOTH AIR CONDITIONING PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)