N9681B

Part: PAD — CRACKED (DOOR STOP) · airframe 52,184 hrs · 26,815 cycles

FORWARD CARGO DOOR STOP PAD, FORWARD UPPER SIDE WAS CRACKED. REPLACED THE STOP PAD IAW RD 51-00-05-1, AND DRAWING 5910141.

Part: PAD — CRACKED (DOOR STOP) · airframe 52,184 hrs · 26,815 cycles

FORWARD CARGO DOOR STOP PAD AT LOWER AFT POSITION WAS CRACKED. REPLACED THE DOOR STOP PAD IAW RD 51-00-05-1, AND DRAWING 5910141.

Part: STOP FITTING — CRACKED (AFT CARGO DOOR) · airframe 52,184 hrs · 26,815 cycles

AFT CARGO DOOR STOP WAS CRACKED AT THE UPPER FORWARD SIDE. REPLACED THE DOOR STOP PAD IAW RD 51-00-05-1 AND DRAWING 5910141.

Part: PORTABLE LIGHT — DEFECTIVE (CABIN) · airframe 51,691 hrs · 26,490 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR SIDE EMERGENCY LIGHT IS ON. REPLACED L1 DOOR PORTABLE EMERGENCY LIGHT AND OPERATIONS CHECK NORMAL PER AMM 33-53-00.

Part: SKIN — CRACKED (BS 1380.8) · airframe 50,699 hrs · 25,848 cycles

FUSELAGE SKIN CRACKED AT BS 1380.8, STRINGER 15L JUST ABOVE THE LEFT PYLON AFT ENGINE MOUNT. AIRCRAFT WAS GROUNDED. REPAIRED THE SKIN IAW SRM 53-01-00, FIG 2, SHEET 3.

Part: BATTERY PACK — NO TEST (ZONE 200 - FUSE) · airframe 50,519 hrs · 25,736 cycles

EMERGENCY CEILING LIGHTS INOPERATIVE FROM ROWS 17 TO 20. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY PACK B5-104 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 50,519 hrs · 25,736 cycles

EMERGENCY CEILING LIGHTS INOPERATIVE FROM ROW 13 TO ROW 16. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY PACK B5-102 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 50,196 hrs · 25,526 cycles

FOWARD FLIGHT ATTENDANT FLASHLIGHT INDICATOR DOES NOT BLINK. REPLACED THE FLASHLIGHT AND HOLDER IAW AMM 25-60-00.

Part: PAN — CORRODED (BS 1312-1320) · corrosion level 2 · airframe 49,921 hrs · 25,343 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION AT FORWARD LOWER CORNER OF AFT LAVATORY PAN BETWEEN STA. 1312 AND STA. 1320. INSTALLED INTERNAL DOUBLER PER E.A. 275489 DRAFT #3.

Part: DOUBLER — CORRODED (BS 1320-1325) · airframe 49,921 hrs · 25,343 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF FUSELAGE SKIN AT AFT LAVATORY SERVICE PANEL BETWEEN STA. 1320 TO STA. 1325. REPLACED DOUBLER PER E.A.275622.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 49,921 hrs · 25,343 cycles

CRACK DISCOVERED ON THE BRACKET OF THE AFT EDGE OF TOP LEFT MLG WHEEL WELL DOOR UPPER ACTUATOR. REPAIRED THE BRACKET IAW SRM 51-10-03 AND 53-10-00-38.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 49,921 hrs · 25,343 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK IDENTIFIED LONGERON 20 AT STA 993 RIGHT WHEEL WELL. REPAIRED ANGLE PER 53-10-00-18.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 49,921 hrs · 25,343 cycles

CORROSION FROM FASTENERS IN THE RIGHT OUTBOARD FLAP CENTER HINGE FITTING TO REAR SPAR. REPLACE UPPER AND LOWER HINGE STUDS, AND HINGE FITTING IAW AMM 57-40-01-201.

Part: FITTING — CRACKED (LT WING) · airframe 49,921 hrs · 25,343 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED LEFT HAND WING FITTING FORWARD SIDE OF REAR SPAR AT OUTBOARD FLAP HINGE OUTBOARD LOWER STUD. REPLACED FITTING PER AMM 57-40-01-201 AND DRAWING 4911393.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 49,921 hrs · 25,343 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND WING OUTBOARD FLAP HINGE AT UPPER AND LOWER STUDS AND INTO HINGE STUD HOLE BORES. REPLACE HINGE ASSEMBLY AND UPPER AND LOWER STUDS PER IPC 57-10-00-10A.

Part: BATTERY — DISCHARGED (PORTABLE LIGHT) · airframe 49,867 hrs · 25,301 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. EMERGENCY PORTABLE LIGHT B5-29 HAS A DEAD BATTERY. REMOVED AND REPLACED LIGHT PER ESO 80232 REVISION 2. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,867 hrs · 25,301 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD PER AMM 33-53-00.

Part: WIRE — DAMAGED (CABIN) · airframe 49,627 hrs · 25,137 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT AT SEAT 14D HAS BARE WIRES. RETERMINATED WIRES AT LIGHT PER AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: TRANSFORMER — BURNED OUT (WINDSHIELD HEAT) · airframe 49,623 hrs · 25,133 cycles

AIRCRAFT WAS GROUNDED. FLIGHT CREW REPORTED SMOKE FUMES IN THE COCKPIT AND THE CABIN. CENTER WINDSHIELD ANTI-ICE CIRCUIT BREAKER TRIPPED. REMOVED AND REPLACED WINDSHIELD ANTI-ICE T1-50 TRANSFORMER PER SWPM 20-20-03. OPERATIONAL CHECK PER AMM 30-41-00 GOOD.

Part: LENS — MISSING (CABIN) · airframe 49,545 hrs · 25,077 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT PROXIMITY LIGHT AT ROW 7 DEF FORWARD HAS A MISSING LENS AND SHROUD. INSTALLED LENS AND SHROUD (AALA201709119018) PER AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,548 hrs · 25,080 cycles

AIRCRAFT WAS GROUNDED. CEILING EMERGENCY EXIT LIGHTS FROM ROWS 8 TO 10 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY AT SEAT 8DEF PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: SHROUD — MISSING (CABIN) · airframe 49,545 hrs · 25,077 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT PROXIMITY LIGHT AT ROW 7 DEF FORWARD HAS A MISSING LENS AND SHROUD. INSTALLED LENS (AALA20170910006) AND SHROUD PER AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (ZONE 200) · airframe 49,548 hrs · 25,080 cycles

AIRCRAFT WAS GROUNDED. TAILCONE RELEASE HANDLE EMERGENCY LIGHT HAS A BROKEN WIRE. REPAIRED BROKEN WIRE PER WDM 33-51-13. OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 49,401 hrs · 24,981 cycles

AIRCRAFT WAS NOT GROUNDED. SMOKE DETECTOR IN THE FORWARD LAVATORY DID NOT SOUND WHEN A PASSENGER WAS SMOKING. ACCOMPLISHED SMOKE DETECTOR TEST PER AMM 26-19-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 48,898 hrs · 24,646 cycles

THE AIRCRAFT WAS NOT GROUNDED. OVERWING EMER LIGHTS REMAIN ON W/ POWER OFF. REPLACED BATT PACK FOR SAME IAW AMM 33-50-00 CKS GOOD.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 48,653 hrs · 24,501 cycles

AFT GALLEY MEGAPHONE INOP PER F/A. REPLACED AFT GALLEY MEGAPHONE IAW MM 25-60-00. OPS CK GOOD. THE AIRCRAFT WAS NOT GROUNDED.

Part: COMPUTER — FAULTY (COCKPIT) · airframe 48,337 hrs · 24,296 cycles

ACTIONED AIRSPEED UNRELIABLE CHECKLIST DUE TO MULTI UNRELIABLE AIRSPEED -RELATED INDICATIONS. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO AUS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT CADC IAW AMM 34-16-01, OPS CHECKED OK. THE AIRCRAFT WAS GROUNDED. (SEE ALSO SDR'S AALA201704059028, AALA201704069025, AALA201704069026, AND AALA201704069027)

Part: COMPUTER — FAULTY (COCKPIT) · airframe 48,337 hrs · 24,296 cycles

ACTIONED AIRSPEED UNRELIABLE CHECKLIST DUE TO MULTI UNRELIABLE AIRSPEED -RELATED INDICATIONS. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO AUS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT CADC IAW AMM 34-16-01, OPS CHECKED OK. THE AIRCRAFT WAS GROUNDED. (SEE ALSO SDR'S AALA201704069024, AALA201704069025, AALA201704069026, AND AALA201704069027)

Part: INDICATOR — FAULTY (COCKPIT) · airframe 48,337 hrs · 24,296 cycles

ACTIONED AIRSPEED UNRELIABLE CHECKLIST DUE TO MULTI UNRELIABLE AIRSPEED -RELATED INDICATIONS. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO AUS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE F/O'S AIRSPEED INDICATOR IAW AMM 34-13-01, OPS CHECKED OK. THE AIRCRAFT WAS GROUNDED. (SEE ALSO SDR'S AALA201704059028, AALA201704069024, AALA201704069025, AND AALA201704069026)

Part: AIR DATA MODULE — FAULTY (COCKPIT) · airframe 48,337 hrs · 24,296 cycles

ACTIONED AIRSPEED UNRELIABLE CHECKLIST DUE TO MULTI UNRELIABLE AIRSPEED -RELATED INDICATIONS. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO AUS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE AIR DATA SWITCHING UNIT IAW AMM 34-16-03, OPS CHECKED OK. THE AIRCRAFT WAS GROUNDED. (SEE ALSO SDR'S AALA201704059028, AALA201704069024, AALA201704069025, AND AALA201704069027)

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 48,337 hrs · 24,296 cycles

ACTIONED AIRSPEED UNRELIABLE CHECKLIST DUE TO MULTI UNRELIABLE AIRSPEED -RELATED INDICATIONS. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO AUS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE INSTRUMENT SWITCHING PANEL IAW AMM 34-16-03 AND AMM 34-00-00, OPS CHECKED OK. THE AIRCRAFT WAS GROUNDED. (SEE ALSO SDR'S AALA201704059028, AALA201704069024, AALA201704069026, AND AALA201704069027)

Part: SUPPORT — CORRODED (LANDING GEAR) · corrosion level 2 · airframe 46,353 hrs · 23,084 cycles

SUPPORT FOUND CORRODED BEYOND LIMITS.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,017 hrs · 23,482 cycles

BOTH OVERWING EMERGENCY LIGHTS STAY ON WHEN POWERING DOWN. REPLACED THE EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-53-00. ALL EMERGENCY LIGHTS OPS CHECKED OK.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,353 hrs · 23,084 cycles

AIRCRAFT WAS IN BASE MX. LONGERON 30 IS CORRODED AT FS 162. R & R LONGERON IAW SRM 51-30-02, AARD 51-00-05-1 & DWG 5911401.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,353 hrs · 23,084 cycles

AIRCRAFT WAS IN BASE MX. LONGERON 23L HAS CORROSION IN CHANNEL, BETWEEN FS 1287 & 1290. R & R LONGERON STRAP AT LONGERON 23L, BETWEEN FS 1280 & 1300 IAW SRM 51-30-02.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 46,353 hrs · 23,084 cycles

AIRCRAFT WAS IN BASE MX. VERTICAL STIFFENER ON FS 1338 BULKHEAD ABOVE VAULT DOOR IS CRACKED. R & R STIFFENER IAW AARD 51-00-05 & DWG 9915562.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,353 hrs · 23,084 cycles

AIRCRAFT WAS IN BASE MX. FUSELAGE SKIN ABOVE LT NLG DOOR AFT HINGE CUT OUT IS CRACKED. REPAIRED SKIN IAW SRM 53-05-00 FIGURE 158.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 46,353 hrs · 23,084 cycles

AIRCRAFT WAS IN BASE MX. FWD CARGO COMPARTMENT INTERCOSTAL ATTACH ANGLE INBD OF LONGERON 27R AT FS 229 IS CRACKED. R & R ANGLE IAW AARD 51-00-05-1 & DWG PL9915554.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,353 hrs · 23,084 cycles

AIRCRAFT WAS IN BASE MX. FUSELAGE SKIN ABOVE RT NLG DOOR AFT HINGE CUT OUT IS CRACKED. REPAIRED SKIN IAW SRM 53-05-00 FIGURE 158.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,353 hrs · 23,084 cycles

AIRCRAFT WAS IN BASE MX. RT CUSP IS CORRODED BETWEEN FS 389 & 424. REPAIRED CUSP IAW AARD 53-20-00-001 FIGURE 21.

Part: SEAT TRACK — CORRODED (BS 375-379) · corrosion level 2 · airframe 46,353 hrs · 23,084 cycles

SEAT TRACK NR 1 IS CORRODED BETWEEN FS 375 & 379. REPAIRED SEAT TRACK IAW AARD 53-20-00-010.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 46,353 hrs · 23,084 cycles

AIRCRAFT WAS IN BASE MX. AFT CARGO COMPARTMENT INTERCOSTAL AT BL 0 & FS 1280 IS CRACKED. R & R INTERCOSTAL IAW SRM 51-60-00.

Part: SEAT TRACK — CORRODED (BS 283-286) · corrosion level 2 · airframe 46,353 hrs · 23,084 cycles

SEAT TRACK NR 6 IS CORRODED BETWEEN FS 283 & 286. REPAIRED SEAT TRACK IAW AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (BS 600-602) · corrosion level 2 · airframe 46,353 hrs · 23,084 cycles

LT CUSP WEB IS CORRODED BETWEEN FS 600 & 602. REPAIRED CUSP WEB IAW AARD 53-20-00-16.

Part: SKIN — WORN (BS 1401-1418) · airframe 46,353 hrs · 23,084 cycles

FUSELAGE SKIN IS SHOWS WEAR DAMAGE ON LT SIDE, BETWEEN STATIONS 1401 & 1418. REPAIRED SKIN IAW AARD 53-20-00-11 FIGURE 1 REPAIR 11.

Part: INTERCOSTAL — CRACKED (BS 769-786) · airframe 46,353 hrs · 23,084 cycles

FWD CARGO COMPARTMENT CEILING INTERCOSTAL, BETWEEN FS 769 & 786.5, BETWEEN SEAT TRACKS 3 & 4 IS CRACKED. R & R INTERCOSTAL IAW AARD 51-00-05.

Part: SEAT TRACK — CORRODED (BS 798-1088) · corrosion level 2 · airframe 46,353 hrs · 23,084 cycles

SEAT TRACK NR 6 IS CORRODED, BETWEEN FS 798 & 1088. R & R SEAT TRACK SECTION IAW SRM 53-05-00-001, SRM 51-10-01-001 & AMM 53-40-01.

Part: CUSP WEB — CRACKED (BS 218) · airframe 46,353 hrs · 23,084 cycles

AIRCRAFT WAS IN BASE MX. CUSP AT FS 218 JUST OTBD OF NR 5 SEAT TRACK IS CRACKED. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (BS 1287-1309) · airframe 46,353 hrs · 23,084 cycles

AFT CARGO COMPARTMENT INTERCOSTAL AT BL 0, BETWEEN BS 1287 & 1309 IS CRACKED. R & R INTERCOSTAL IAW SRM 51-60-00.

Part: SEAT TRACK — CORRODED (BS 416-419) · corrosion level 2 · airframe 46,353 hrs · 23,084 cycles

SEAT TRACK NR 1 IS CORRODED BETWEEN BS 416 & 419. REPAIRED SEAT TRACK IAW AARD 53-20-00-010.

Part: SEAT TRACK — CORRODED (BS 324-326) · corrosion level 2 · airframe 46,353 hrs · 23,084 cycles

SEAT TRACK NR 6 IS CORRODED, BETWEEN FS 324 & 326. ACCOMPLISHED PLUG REPAIR IAW AARD 53-20-00-010.

Part: CUSP WEB — CORRODED (BS 1244-1245) · corrosion level 2 · airframe 46,353 hrs · 23,084 cycles

LT CUSP IS CORRODED AT APPROX FS 1244, BELOW THE AFT SERVICE DOOR, FWD GIRT BAR BRACKET. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: SUPPORT ANGLE — CRACKED (BS 826-827) · airframe 46,353 hrs · 23,084 cycles

SUPPORT ANGLE AT FS 826, BELOW SEAT TRACK 3 IS CRACKED AT LOWER END. R & R ANGLE IAW AARD 51-00-05-1 & DWG 3925817.

Part: SUPPORT ANGLE — CRACKED (BS 845-846) · airframe 46,353 hrs · 23,084 cycles

SUPPORT ANGLE AT FS 845, JUST BELOW SEAT TRACK 3 IS CRACKED. R & R ANGLE IAW AARD 51-00-06-1 & DWG 3925816.

Part: CUSP WEB — CRACKED (BS 218) · airframe 46,353 hrs · 23,084 cycles

MAIN CABIN CUSP WEB AT FS 218 IS CRACKED, JUST OTBD OF NR 2 SEAT TRACK. REPAIRED CUSP WEB IAW AARD 53-20-00-16.

Part: HEATER — MALFUNCTIONED (PITOT TUBE) · airframe 45,825 hrs · 22,765 cycles

PITOT & STALL HEAT OFF LIGHT ILLUMINATED IN CRUISE. ICING CONDITIONS, RETURNED TO LAND DFW Z30 CIRCUIT BREAKER IS POPPED. FLIGHT DECLARED AN EMER & RETURNED WITHOUT FURTHER INCIDENT. R & R RUDDER Q LIMITER PITOT TUBE HEATER, LEAK CHECK GOOD IAW MM 34-11-02. THE AIRCRAFT WAS GNDED.

Part: POWER SUPPLY — NO TEST (CABIN) · airframe 45,428 hrs · 22,520 cycles

AIRCRAFT WAS NOT GNDED. EGRESS POWER SUPPLY AB5-2 FAILS TO TEST. R & R POWER SUPPLY IAW AMM 33-60-98. SYS CHECKED NORMAL.

Part: POWER SUPPLY — NO TEST (CABIN) · airframe 45,428 hrs · 22,520 cycles

AIRCRAFT WAS NOT GNDED. EGRESS POWER SUPPLY AB5-1 FAILS TO TEST. R & R POWER SUPPLY IAW AMM 3-60-98. SYS CHECKED NORMAL.

Part: WIRE — SHORTED (CABIN) · airframe 43,563 hrs · 21,417 cycles

FORWARD SECTION OF SEAT EMER LIGHTS SHORTED ON WIRE PAIR. REPLACED EXIT LIGHT AT FWD GALLEY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,050 hrs · 21,137 cycles

EMERGENCY PATH LIGHTS DIM WHEN TESTING USING EPM AB5-4. REPLACED EPM BATTERY PACKS FOR AB5-4 IAW AMM 33-60-98. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,054 hrs · 21,138 cycles

EMERGENCY PATH LIGHTS DIM WHEN TESTING USING EPM AB5-1. REPLACED EPM BATTERY PACKS FOR AB5-1 IAW AMM 33-60-98. SYS CHECKED NORMAL.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 42,872 hrs · 21,044 cycles

AIR INTERRUPT, EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. LOSS OF HYD QTY & HYD PRESS ON RT SYS. PERFORMED MANUAL GEAR EXTENSION FOR LANDING. R & R FWD OTBD PRESS LINE TO FILTER HOUSING, ENG DRIVEN HYD PUMP & ELEC PUMP. REFERENCE 20150205004 & 2015020916 FOR ADDITIONAL PARTS INFORMATION.

Part: HYDRAULIC SYSTEM — PRESSURE LOSS · airframe 42,872 hrs · 21,044 cycles

LOSS OF HYD QTY & HYD PRESSURE ON RT SYS. PERFORMED MANUAL GEAR EXTENSION FOR LANDING. EMERGENCY DECLARED, LANDING UNEVENTFUL. PERFORMED MANUAL GEAR EXTENSION FOR LANDING. R & R FWD OTBD PRESSURE LINE TO FILTER HOUSING, ENGINE DRIVEN HYD PUMP & ELEC PUMP.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 42,872 hrs · 21,044 cycles

AIR INTERRUPT, EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. LOSS OF HYD QTY & HYD PRESS ON RT SYS. PERFORMED MANUAL GEAR EXTENSION FOR LANDING. R & R FWD OTBD PRESS LINE TO FILTER HOUSING, ENGINE DRIVEN HYD PUMP & ELEC PUMP. REFERENCE 20150205004 & 20150209017 FOR ADDITIONAL PARTS INFORMATION.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 42,463 hrs · 20,819 cycles

AFT CARGO COMPARTMENT FWD CTR DOOR STOP CASTING IS CRACKED. R & R DOOR STOP CASTING IAW AARD 51-00-05-1 & DWG 5910141.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 42,463 hrs · 20,819 cycles

LONGERON 2 LT CRACKED ON AFT SIDE OF FS 1418. REPAIRED LONGERON IAW SRM 53-02-00-001.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,248 hrs · 20,709 cycles

HOLE IN FUSELAGE SKIN AT STATION 565 BETWEEN LONGERONS 22 & 23 LT. REPAIRED IAW SRM 53-04-03 FIG 2 SHEET 5.

Part: RIB — CRACKED (RT WING) · airframe 42,248 hrs · 20,709 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD SUPPORT RIB IS CRACKED. INSTALLED RT WING NR 4 INBD SUPPORT RIB DOUBLER & HAT BUSHING IAW MCM CARD 57-98-06 & EA MD80-57-037304 DATED 11/8/14.

Part: RIB — CRACKED (LT WING) · airframe 42,248 hrs · 20,709 cycles

LEFT WING LE NR 4 SLAT TRACK INBD SUPPORT RIB IS CRACKED. INSTALLED LT WING NR 4 SLAT INBD SUPPORT RIB DOUBLER & HAT BUSHING IAW MCM CARD 57-98-05 & EA MD80-57-037304 DATED 11/8/14.

Part: APU — FAILED (ZONE 200) · airframe 40,829 hrs · 19,969 cycles

DFW FLIGHT ATTENDANTS REPORTED VISIBLE VAPOR & SMOKE IN AFT PART OF CABIN. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED APU & TEMPERATURE CONTROL VLV ON LT PACK. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: LENS — MISSING (CABIN) · airframe 40,272 hrs · 19,696 cycles

AFT AIR STAIR EMERGENCY SIDEWALL LIGHT MISSING LENS. REPLACED AFT AIR STAIR EMERGENCY SIDEWALL LENS, OPERATIONS CHECKED NORMAL.

Part: DUCT — BLOWN (ANTI-ICE SYS) · airframe 39,566 hrs · 19,314 cycles

TPA INFLIGHT JAX-DFW. INTERMITTENT FIRE INDICATIONS ON LT ENGINE. BRINGING LT THROTTLE BACK SILENCED WARNING. EMERGENCY DECLARED FLIGHT DIVERTED TPA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RUPTURED LT COWL ANTI ICING DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,693 hrs · 18,814 cycles

CRACK IN FS SKIN AT STATION 1380, LONGERON 14 RT. INSTALLED REPAIR DOUBLER IAW SRM 53-01-00 FIGURE 2 SHEET3.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 37,473 hrs · 18,199 cycles

SEAT ROW 22 EMERGENCY LIGHT FOUND UN-PLUGGED. RECONNECTED THE CONNECTOR. OPS CHECK NORMAL.

Part: WIRE — PULLED (EMERGENCY LIGHTS) · airframe 36,004 hrs · 17,470 cycles

ESCAPE PATH LIGHT AT SEAT 31D INOPERATIVE. FOUND WIRE PULLED FROM CONNECTOR. REPLACED CONNECTOR AT SEAT 31DEF. OPS CHECK NORMAL.

Part: WIRE — PULLED (EMERGENCY LIGHTS) · airframe 36,004 hrs · 17,470 cycles

ESCAPE PATH LIGHT AT SEAT 22D INOPERATIVE. FOUND WIRE PULLED FROM CONNECTOR. REPLACED CONNECTOR AT SEAT 22DEF. OPS CHECK NORMAL.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,825 hrs · 16,841 cycles

LEFT CUSP WEB CORRODED AT STATION 880. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (ZONE 200) · airframe 34,825 hrs · 16,841 cycles

LEFT FUSELAGE SKIN BS 229, LONGERONS 17 TO 18 LEFT HAS DEEP DENTS AND GOUGES. INSTALLED DOUBLER PER SRM 53-04-05 FIGURE 2.

Part: CUSP WEB — DAMAGED (ZONE 200) · airframe 34,825 hrs · 16,841 cycles

CORROSION AND DEEP GOUGE AT LEFT CUSP WEB BS 845. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,825 hrs · 16,841 cycles

RIGHT CUSP WEB CORRODED FROM BS 525 TO 528. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,825 hrs · 16,841 cycles

LEFT CUSP WEB BS 644 TO 645 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: STRUCTURE — CRACKED (ZONE 200) · airframe 34,825 hrs · 16,841 cycles

SUBFLOOR CRACKED AT STATION 198 LEFT BUTTLINE 44. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,825 hrs · 16,841 cycles

RIGHT CUSP WEB CORRODED AT LIGHTENING HOLE BS 495. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (BS 695-700) · corrosion level 2 · airframe 34,825 hrs · 16,841 cycles

LEFT CUSP WEB FROM BS 695 TO 700 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 34,825 hrs · 16,841 cycles

CORROSION ON AFT CARGO DOOR BEAM. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,825 hrs · 16,841 cycles

RIGHT CUSP SHEET AT STATION 1199 CORRODED. INSTALLED RIGHT CUSP DOUBLER FROM STATIONS 1196 TO 1210 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,825 hrs · 16,841 cycles

CORROSION ON RIGHT CUSP FROM STATIONS 830 TO 843. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,825 hrs · 16,841 cycles

RIGHT CUSP SHEET AT STATIONS 1061 TO 1062 CORRODED. REMOVED DAMAGE INSTALLED CUSP DOUBLER AT RIGHT STATIONS 1056 TO 1066 PER AARD 53-20-00-16.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 34,825 hrs · 16,841 cycles

SUBFLOOR CRACKED AT STATION 198 LEFT BUTTLINE 44. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 34,825 hrs · 16,841 cycles

LEFT CUSP DAMAGED FROM STATIONS 677 TO 679. INSTALLED DOUBLER PER AARD 53-10-00-16.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,825 hrs · 16,841 cycles

CORROSION ON SHEAR TIE STATION 1287 LONGERONS 28 RIGHT TO 29 LEFT. REMOVED AND REPLACED DAMAGED SECTION OF SHEAR-TIE PER SRM 53-03-00 FIGURE 3 SHEET 1.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,825 hrs · 16,841 cycles

AFT CARGO FRAME HAS CORROSION AT STATION 1287 LONGERONS 28 LEFT TO 28 RIGHT. INSTALLED REPAIR DOUBLER TO BLENDED AREA OF FRAME PER AARD 53-10-00-14 FIGURE 1 SHEET 1.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,825 hrs · 16,841 cycles

STIFFENER CRACKED AT TOP OUTBOARD FASTENER HOLE ON AFT SIDE OF CANT FRAME 1463 AT 10 O`CLOCK POSITION. INSTALLED NEW STIFFENER PER AARD 51-10-00-5, SRM 53-30-05, 51-60-00.

Part: APU — SHUTDOWN (ZONE 100) · airframe 33,731 hrs · 16,291 cycles

DFW - CREW REPORTED AUXILIARY POWER UNIT AUTO SHUT DOWN IN FLIGHT WITH LEFT ENGINE CONSTANT SPEED DRIVE ON PLACARD. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AUXILIARY POWER UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GENERATOR — FAILED (LEFT) · airframe 33,382 hrs · 16,093 cycles

ABI - INFLIGHT LAX-DFW. CREW REPORTED LEFT ENGINE GENERATOR FAILED WITH APU GENERATOR ON MEL. EMERGENCY DECLARED FLIGHT DIVERTED ABI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT GENERATOR AND CONSTANT SPEED DRIVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN PANEL — DAMAGED (LT WING) · airframe 32,065 hrs · 15,407 cycles

LEFT WING LOWER SKIN PANEL DAMAGED. ACCOMPLISHED EXTERNAL DOUBLER REPAIR PER EA MD80-57-015247.

Part: CASTING — CORRODED (MLG WW) · corrosion level 2 · airframe 30,877 hrs · 14,867 cycles

CORROSION ON CASTING ABOVE ACCUMULATOR OUTBOARD OF HYDRAULIC LINE. REPLACED CASTING PER SRM 51-01-00.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 26,516 hrs · 12,836 cycles

SHEAR TIE ANGLE CRACKED ON AFT SIDE OF FRAME 1451, LONGERON 2L. INSTALLED NEW ANGLE PER SRM 51-01.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 26,516 hrs · 12,836 cycles

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

Part: WEB — WORN (FUSELAGE) · airframe 26,516 hrs · 12,836 cycles

STATION 1380, AFT OF COCKPIT CONTROL VALVE, HOLES WORN THROUGH WEB. INSTALLED DOUBLER PER AARD 53-10-00-28.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 26,516 hrs · 12,836 cycles

LEFT J-ANGLE DOUBLER CRACKED AT FORWARD SIDE OF NOSE GEAR FORWARD HINGE. REPLACED DOUBLER PER AARD 53-10-00-4.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,516 hrs · 12,836 cycles

ANGLE CRACKED AT LONGERON 2R STATION 1451. REMOVED AND REPLACED ANGLE PER SRM 51-01.

Part: DUCT — CRACKED (RIGHT) · airframe 26,346 hrs · 12,763 cycles

DFW - TAIL COMPARTMENT HIGH TEMPERATURE LIGHT WAS ILLUMINATED. EMERGENCY DECLARED, LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. DUCT LEAK SUSPECTED AT HIGHER POWER SETTINGS. REPLACED RIGHT TURBINE DISCHARGE DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DUCT — CRACKED (AC BAY) · airframe 26,337 hrs · 12,757 cycles

DFW - TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. RETURNED TO DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED GASKET ON PNEUMATIC SUPPLY LOW TEMP SENSOR AND REPLACED CRACKED DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,178 hrs

SFO - EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: CSD — FAILED (NR 1 ENGINE) · airframe 24,058 hrs

ONT INFLIGHT T1419/19MAY STL TO LAS. NUMBER ONE ENGINE CONSTANT SPEED DRIVE OIL PRESSURE LOW INDICATION DURING FLIGHT. LANDED ONT WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE CONSTANT SPEED DRIVE AND CONSTANT SPEED DRIVE AIR/OIL HEAT EXCHANGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

BOS - EMERGENCY LIGHT AT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS AT SEAT ROW 24 INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROW 24. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS AT SEAT ROW 11 INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROW 11. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS AT SEAT ROW 15 INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROW 15. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - FOUND EMERGENCY LIGHTS AT LOCATION B5102 BETWEEN STATIONS 900 AND 1000 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LOCATION B5102 BETWEEN STATIONS 900 AND 1000. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BLADE — FAILED (LT ENGINE)

SEA INFLIGHT T875/01FEB, AFTER TAKEOFF AT 6000 MEAN SEA LEVEL HEARD A BAND AND INDICATIONS FOR LEFT ENGINE ROLLED BACK TO ZERO. ENGINE SHUTDOWN WAS COMPLETED AND RETURNED TO SEA AND LANDED WITHOUT INCIDENT. THERE WERE NO FIRE INDICATIONS AND NO BOTTLES USED. FLIGHT DATA RECORDED DOWNLOADED AND REVEALED A COMPRESSOR BLADE FAILURE. REPLACED LEFT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY ESCAPE PATH LIGHTING AT FORWARD GALLEY FLOOR INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY CONNECTOR FOR AT FORWARD GALLEY FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT)

TPA - EMERGENCY PATH SEAT MOUNTED LIGHTING AT SEAT 22DEF INOPERATIVE. FOUND AREA WHERE LIGHT MODULE MOUNTS TO SEAT AND WIRING HARNESS RETAINING FIXTURE ARE DAMAGED. SEAT NEEDS REPLACED. SEAT NOT IN STOCK AT TPA. PLACARD EMERGENCY ESCAPE PATH LIGHTING SYSTEM PER MEL 33-17, AUTHORITY 4-1313-C. REPLACED WIRE HARNESS AND SECURED TO SEAT FIXURE FOR EMERGENCY ESCAPE PATH LIGHTING AT SEAT 22DEF. CLEARED MEL 04-1313-C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW LEFT HAND AND RIGHT HAND EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-125 FOR LEFT HAND AND RIGHT HAND OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

AUS DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY OVERHEAD LIGHTS AT 14DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY OVERHEAD LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (LT ENGINE)

STL - FLT 1055 - EN ROUTE STL-SFO - ON CLIMB-OUT LEFT ENGINE HYDRAUILC PRESSURE LOW. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,644 hrs · 5,314 cycles

THE NEXT TO LAST RED EGRESS LIGHT ADJACENT TO AFT LAVS, AND THE LOWER LAMP IN EMERGENCY SLIDE LAMP TRIPLE FIXTURE IN TAIL CONE, WERE INOPERATIVE. RESEATED LAMP FOR EGRESS LIGHT, AND REPLACED BATTERIES IN POWER SUPPLY FOR TAIL CONE. CHECK-C 11-13-02 STL.