N9401W

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 64,835 hrs · 31,773 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. NR 2 ENG EXPERIENCED COMPRESSOR STALLS IN FLIGHT. POWER REDUCED TO IDLE FOR DESCENT & LANDING. ENG NOT SHUT DOWN. R & R NR 2 ENG IAW MCM 71-91-99. PERFORMED OPERATIONAL CHECK OF NR 2 ENG, OK FOR SERVICE. POWER PLANT ENGINEERING INDICATES ENG BORESCOPE FOUND NO DAMAGE. SUSPECT COMPRESSOR PERFORMANCE & HOT SECTION DETERIORATION DUE TO TIME SINCE LAST VISIT.

Part: BLEED VALVE — MALFUNCTIONED (LT ENGINE) · airframe 64,717 hrs · 31,708 cycles

RETURNED, ACCOUNT LT ENG COMPRESSOR STALL ON CLIMB OUT. EMER LANDING WAS DECLARED, UNEVENTFUL LANDING. ACFT REMOVED FROM SERVICE. REPLACED LT ENG PRBC IAW MM 75-31-01. ENG OPERATIONS CHECKED NORMAL.

Part: SKIN — WORN (TE FLAP) · airframe 63,723 hrs · 31,105 cycles

RIGHT OTBD FLAP, 2ND FROM OTBD WEDGE UPPER SKIN WORN. R & R SKIN ASSEMBLY IAW ESO 80096 REPAIR GENERAL 2 D 1 PAGE 601.

Part: SKIN — WORN (TE FLAP) · airframe 63,723 hrs · 31,105 cycles

RIGHT OTBD FLAP, 2ND FROM OTBD WEDGE LOWER SKIN WORN. R & R SKIN ASSEMBLY IAW ESO 80096 REPAIR GENERAL 2 D 1 PAGE 601.

Part: TRANSMITTER — FAULTED (PRESSURE RATIO) · airframe 63,205 hrs · 30,840 cycles

AUTOPILOT DISENGAGED ON APPROACH. AN EMERGENCY WAS NOT DECLARED, LANDED UNEVENTFULLY. REMOVED AND REPLACED LEFT ENGINE PRESSURE RATIO TRANSMITTER PER AMM 77-11-02.

Part: TRANSMITTER — FAULTY (RT ENGINE) · airframe 63,205 hrs · 30,840 cycles

AIR INTERRUPT, EMER WAS NOT DECLARED. LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. AUTOPILOT DISENGAGED ON APPROACH, RETURNED. R & R RT ENG PRESS RATIO TRANSMITTER IAW AMM 77-11-02. ALSO REFERENCE SDR AALA20150309003. SUPPLEMENTAL CLOSED.

Part: ACM — FAILED (RIGHT) · airframe 62,732 hrs · 30,597 cycles

WHILE AT FL 290, WITH ANTI-ICE ON & IAS 300, THE PRESSURIZATION FLOW LIGHT CAME ON. ACCOMPLISHED PROCEDURE ON QRH & WERE UNABLE TO STOP CABIN ALTITUDE FROM CLIMBING. DESCENDED TO FL 230 & REGAINED CONTROL OF PRESSURIZATION. EMERGENCY DECLARED, LANDED UNEVENTFULLY. REMOVED AND REPLACED RIGHT ACM IAW AMM 21-51-01 SYSTEM OPS CHECKS NORMAL. NO LEAKS NOTED.

Part: PAN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 61,910 hrs · 30,177 cycles

FORWARD CARGO DOOR PAN HAS CORROSION. REPAIRED DOOR PAN IAW EA MD80-53-036324.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,910 hrs · 30,177 cycles

SKIN CRACKED AT LOWER FASTENER IN SHEAR TIE AT STATION 1380 & LONGERON 14 LT. INSTALLED DOUBLER IAW AARD 53-30-00-02.

Part: PORTABLE LIGHT — DEFECTIVE (CABIN) · airframe 61,910 hrs · 30,177 cycles

PORTABLE EMER LIGHT CAME ON BUT WOULD NOT SHUT OFF. R & R PORTABLE EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 61,910 hrs · 30,177 cycles

CRACK IN LONGERON 2 RT AT STATION 1418. SPLICED IN NEW LONGERON SECTION IAW SRM 53-02-00 FIGURE 18.

Part: FORMER — CRACKED (LE SLAT) · airframe 61,774 hrs · 30,102 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-04.

Part: RELAY — FAULTED (TRIM SYSTEM) · airframe 61,357 hrs · 29,874 cycles

CREW REPORTED DURING CLIMB OUT STAB TRIM ELEC CONTROLS ON BOTH THE CAPTAIN & FIRST OFFICER`S YOKE INOPERATIVE. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED R20-17 BRAKE RELAY DOWN TRIM. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,916 hrs · 29,626 cycles

CABIN FWD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,916 hrs · 29,626 cycles

CABIN AFT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: NUT — LOOSE (CABIN) · airframe 60,916 hrs · 29,626 cycles

CABIN CEILING EMERGENCY LIGHT AT STATION 358 LT INOPERATIVE. FOUND GND TERMINAL LOOSE ON FRAME AT STATION 351 UNDER CEILING PANEL. TIGHTENED NUT, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,676 hrs · 29,498 cycles

EMERGENCY LIGHT AT STATION 671 INOPERATIVE. REPLACED BATTERY PACK, OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,676 hrs · 29,498 cycles

LT NR 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES, OPERATIONS CHECKED NORMAL.

Part: INDICATION SYS — FAULTY (FUEL SYSTEM) · airframe 60,630 hrs · 29,478 cycles

RIC CREW REPORTED LOW FUEL QUANTITY INDICATION. EMERGENCY DECLARED LANDED RIC WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PLACARDED FUEL TOTALIZER GROSS WEIGHT INDICATION IAW MEL 28-04B & WING FUEL QUANTITY INDICATION IAW MEL. AIRCRAFT CURRENTLY UNDERGOING MAINTENANCE, SYS GND CHECKED NORMAL OPEN.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,839 hrs · 28,015 cycles

MID GALLEY EMERGENCY FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY. OPS CHECK NORMAL.

Part: TRACK — CORRODED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

CORROSION ON TIE-DOWN TRACK LEFT SIDE STATION 408. INSTALLED DOUBLER ON LEFT TIE-DOWN TRACK PER AARD 53-20-00-13.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

CRACK AT STATION 1418 BELOW LONGERON 2 LEFT. INSTALLED INTERNAL AND EXTERNAL DOUBLERS PER SRM 53-04-00 FIGURE 40 SHEET 1.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

CRACK FOUND AT STATION 1418 BELOW LONGERON 2 RIGHT. INSTALLED INTERNAL AND EXTERNAL DOUBLERS PER SRM 53-04-00 FIGURE 40 SHEET 1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

AFT SERVICE DOOR JAM CUSP, CORROSION ON CUSP AT STATION 1155. INSTALLED REPAIR DOUBLER BETWEEN STATIONS 1136 TO 1155 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

CORROSION ON THE BOTTOM OF THE LEFT CUSP FROM STATIONS 1174 TO 1180. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

PLUG IS BROKEN IN SEAT TRACK NUMBER 4 AT STATION 743. INSTALLED NUMBER 4 SEAT TRACK REPAIR PLUG PER AARD 53-20-00-10.

Part: BEAM — CORRODED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

CORROSION ON CARGO DOOR BEAM BETWEEN STATIONS 636 TO 685. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,839 hrs · 28,015 cycles

CORROSION ON THE GUSSET AT STATION 1260, LONGERON 25 LEFT. INSTALLED GUSSET PER AARD 51-00-05-1.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

DAMAGE TO STATION 218 BELOW LONGERON 5 LEFT. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04-02 FIGURE 2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

DENT WITH PREVIOUSLY BLENDED AREA WITHIN 1 INCH OF STRUCTURE STATION 218 BELOW LONGERON 5 LEFT. INSTALLED DOUBLER PER SRM 53-04-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

FUSELAGE SKIN HAS DENT WITH A GOUGE AT STATION 316 LONGERON 24 LEFT. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04-02.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

DAMAGE TO STATION 311 AT LONGERON 23 LEFT. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04-02 FIGURE 2.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

DAMAGE TO STATION 316 AT LONGERON 24 LEFT. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04-02 FIGURE 2.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

UPPER AFT CORNER OF WINDOW RING PAN BETWEEN STATIONS 1003 AND 1022, LEFT SIDE IS CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

UPPER FORWARD CORNER OF WINDOW RING PAN BETWEEN STATIONS 946 AND 965 LEFT IS CRACKED. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,839 hrs · 28,015 cycles

CRACK ON WINDOW RING BELT, LOWER FORWARD CORNER, STATION 807. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: CLAMP — BROKEN (WATER SEPARATOR) · airframe 56,614 hrs · 27,380 cycles

HSV - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMBOUT. EMERGENCY DECLARED, FLIGHT RETURNED TO HSV AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT WATER SEPARATOR HOUSING CLAMP BROKEN. REPLACED WATER SEPARATOR ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSOR — FAULTY (OIL SYSTEM) · airframe 54,914 hrs · 26,509 cycles

BOI - INFLIGHT DFW-SEA. CREW REPORTED LEFT ENGINE OIL TEMP HIGH. PERFORMED IN FLIGHT ENGINE SHUTDOWN, (SINGLE ENGINE TIME 15 MIN). EMERGENCY DECLARED FLIGHT DIVERTED BOI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED OIL TEMPERATURE SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: INDICATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 54,366 hrs · 26,272 cycles

DFW - CREW REPORTED FUEL LOW LEVEL LIGHT CAME ON WITH 8,000 LBS. OF FUEL. PERFORMED QRH AND LIGHT EXTINGUISHED THEN CAME BACK ON. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FUEL LEVEL LOW LIGHT PLACARD INOPERATIVE PER MEL 28-12. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,359 hrs · 26,267 cycles

CANT FRAME 1510 IS CRACKED AT ALIGNMENT PIN ABOVE LOWER RIGHT TAIL CONE LATCH. INSTALLED REPAIR ANGLE ON 1510 CANT FRAME PER EA MD80-53-020295.

Part: LANDING GEAR — MALFUNCTIONED (MLG) · airframe 50,847 hrs · 24,517 cycles

DFW - CREW REPORTED ON DESCENT RECEIVED THREE GEARS IN THE RED INDICATION. CREW PROCEEDED WITH MANUAL GEAR EXTENSION AND UPON LANDING GEAR DOOR CONTACTED RUNWAY. AIRCRAFT REMOVED FROM SERVICE. AIRCRAFT FERRIED TO TUL FOR FURTHER MAINTENANCE. REPAIRED RIGHT MAIN GEAR SKID PER SRM 52-05-00. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: AUGMENT VALVE — FAILED (BLEED AIR SYS) · airframe 50,715 hrs · 24,460 cycles

AMA - INFLIGHT COS-DFW. CREW REPORTED LEFT PNEUMATIC SYSTEM PRESSURE RUNNING EXTREMELY HIGH AND WAS UNCONTROLLABLE. FLIGHT DIVERTED AMA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FLIGHT WAS FERRIED TO DFW FOR MAINTENANCE. REPLACED LEFT AUGMENTATION VALVE THAT HAD FAILED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 50,626 hrs · 24,411 cycles

NOSE WHEEL WELL RIGHT AFT CORNER AFT HINGE CUTOUT IS CRACKED. INSTALLED DOUBLER PER AARD 53-00-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 50,626 hrs · 24,411 cycles

LONGERON 2 LEFT CRACKED AFT OF STATION 1418. ACCOMPLISHED SPLICE REPAIR PER AARD 53-30-00-2.

Part: SKIN — DAMAGED (LE SLAT) · airframe 50,626 hrs · 24,411 cycles

LEFT HIGH LIFT OUTBOARD NUMBER 4 SLAT DAMAGED UNDER GAP SEAL AT CENTER TRACK. CUT OUT DAMAGED SKIN, MANUFACTURED AND INSTALLED FLUSH PATCH PER SRM 57-09-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,683 hrs · 23,565 cycles

EMERGENCY LIGHTS AT STATION 1200 INOPERATIVE. REPLACED BATTERY PACK AT STATION 1200.

Part: BATTERY PACK — UNSERVICEABLE (CABIN) · airframe 46,380 hrs · 22,585 cycles

WITH ELECTRICAL POWER OFF THE EMERGENCY LIGHTS IN THE AFT ACCESSORY BAY ARE ON. TURNING MAIN AIRCRAFT BATTERY SWITCH ON CAUSES LIGHTS TO GO OFF. LIGHT RETURNS ON WHEN BATTERY SWITCH IS OFF. INSTALLED SERVICEABLE 8130 BATTERY PACKS IN B5-27 AND B5-28 POSITIONS, SYSTEM OPERATIONS TESTS GOOD.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

LEFT TIE DOWN TRACK CORRODED AT FASTENER HOLES, STATION 1220-1322. REMOVED AND REPLACED LEFT TIE DOWN TRACK, STATION 1220-1322.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

RIGHT STATIC PORT PLATE DOUBLER RING HAS SEVERAL SMALL AREAS OF CORROSION. REMOVED AND REPLACED RIGHT STATIC PORT DOUBLER RING.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

CORROSION UNDER LEFT STATIC PORT PLATE DOUBLER RING. INSTALLED DOUBLER AND LEFT PRIMARY STATIC PORT PLATE.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

RIGHT TIE DOWN TRACK CORRODED. REMOVED AND REPLACED RIGHT TIE DOWN TRACK FROM STATION 1212-1322 PER SRM 51-30.

Part: FRAME — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON FRAME. INSTALLED FRAME SPLICE REPAIR PER SRM 53-03-00.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON CUSP. REMOVED AND REPLACED CUSP.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

SHEAR TIE CRACKED. INSTALLED SHEAR TIE REPAIR.

Part: FRAME — WORN (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

WORN AREA ON FORWARD SIDE LEFT 1380 FRAME. REMOVED DAMAGE AND INSTALLED DOUBLER.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

RIGHT CUSP CORRODED. INSTALLED NEW CUSP PER SRM 53-30 AND AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON RIGHT CUSP. INSTALLED NEW CUSP.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

FOUND CORROSION ON FLOORBOARD SUPPORT. INSTALLED NEW FLOORBOARD SUPPORT.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

INTERCOSTAL CRACKED IN CEILING OF MID CARGO. REPLACED INTERCOSTAL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

FUSELAGE FRAME UPPER SIDE FORWARD RADIUS HAS THREE EACH HOLES AT STATION 1231 BETWEEN LONGERONS 29 LEFT AND 30. INSTALLED J ANGLE FILLER.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON RIGHT CUSP. REMOVED AND REPLACED CUSP.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON RIGHT CUSP, STATION 1098-1117. INSTALLED CUSP SHEET, STATION 1098 TO STATION 1174 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON RIGHT CUSP, STATION 1174-1193. INSTALLED RIGHT CUSP SHEET, STATION 1174 TO STATION 1250 PER AARD 53-20-00-16.

Part: BEAM — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

LOWER DOOR BEAM CORRODED FROM STATION 1162 TO STATION 1207 ON BOTH VERTICAL AND HORIZONTAL LEGS. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-03.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

CABIN, CORROSION ON RIGHT CUSP AT STATION 389 TO 503. REPLACED CUSP SHEET WITH SERVICEABLE CUSP SHEET.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

OUT OF LIMITS CORROSION REMOVAL. LEFT CUSP BETWEEN BS 560-579 AROUND LIGHTNING HOLE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON SUBFLOOR DIAPHRAM. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

LEFT CUSP CORRODED, STATION 789 TO STATION 804. INSTALLED NEW CUSP SHEET AT LEFT CUSP, STATION 789 TO STATION 804.

Part: CUSP WEB — PUNCTURED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

CUSP HAS PUNCTURED HOLE AT BS 1097 RIGHT UNDER SEAT TRACK NR 6. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON LEFT CUSP. INSTALLED DOUBLERS ON CUSP AFTER CORROSION REMOVAL PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

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

Part: GALLEY TRACK — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

CABIN, CORROSION ON GALLEY TIE DOWN STATION 160 RIGHT BODY LINE 50. REMOVED AND REPLACED TIE DOWN WITH SERVICEABLE TIE DOWN PER SRM 51-00-00.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

CORROSION, BLENDED OUT OF LIMITS. PART REPLACED PER 51-00-00.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON LEFT CUSP, STATION 836-841. DOUBLER INSTALLED PER SRM 51-01-00.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

LEFT CUSP IS CRACKED AND HAS CORROSION AT STATION 1244. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

CUSP CRACKED FROM LIGHTENING HOLE AT STATION 1305. INSTALLED CUSP REPAIR PER AARD 53-20-00-16 AND SRM 53-01

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

RIGHT CUSP HAS CORROSION AT STATION 712 TO 731. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON OUTBOARD LEG OF SEAT TRACK NR 2, STATION 1150 TO STATION 1160. INSTALLED SEAT TRACK NR 2 SPLICE PER SRM 53-05-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON SEAT TRACK NR 5 INBOARD FLANGE AT STATION 200 TO STATION 204. INSTALLED SEAT TRACK SPLICE PER 53-05-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

RIGHT CUSP HAS CORROSION AT STATION 731 TO 750. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

INTERCOSTAL IN CEILING AT STATION 1287 TO 1307 UPPER FRAME IS CRACKED AT 4 EACH FASTENERS. REMOVED AND REPLACED INTERCOSTAL BETWEEN FLOORBEAM AT STATION 1287 AND 1309 PER SRM 51-01.

Part: PANEL — CORRODED (LAV SERVICE) · airframe 46,380 hrs · 22,585 cycles

AFT LAVATORY SERVICE PANEL HAS CORROSION ALONG LOWER EDGE OF SKIN TO FLANGE. REPAIRED AFT LAVATORY SERVICE PANEL PER SRM 51-10-9 AND ESO 80559 DATED 11/05/08.

Part: SILL — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

MIDDLE CARGO DOOR CUT-OUT LOWER SILL HAS CORROSION, STATION 636 TO STATION 693. REMOVED CORROSION FROM DOOR CUT-OUT LOWER SILL, TREATED AND PRIMED AREA AND INSTALLED DOUBLER AND SEAL RETAINER PER AARD53-10-00-3.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

CRACK IN CUSP AT LEFT SIDE BETWEEN STATION 218 AND 237. REPLACED SECTION OF CUSP.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

INTERCOSTAL CRACKED AT STATION 1271 AND 1287. REMOVED AND REPLACED INTERCOSTAL BETWEEN FLOORBEAM STATION 1271 AND 1287 PER SRM 51-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

CORROSION FOUND ON SCREW HOLE IN CUSP WEB. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON LOWER SIDE OF LEFT CUSP AT STATION 503 TO 522. REMOVED CORROSION PER SRM 51-10-03 AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON CUSP AT AFT SERVICE DOOR AFT GIRT BAR ATTACH FITTING. INSTALLED DOUBLER PER AARD 53-20-00-16

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

FORWARD ENTRY DOOR AFT DOOR JAM WEB CRACKED AT L15 STATION 209. INSTALLED 3 INCH BY 6 INCH T SHAPED DOUBLER OF .040 7075 T6 PER AARD 53-10-00-11.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

FORWARD ENTRY DOOR JAM AFT WEB CRACKED AT L-11 STATION 209. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW AARD 53-10-00-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,380 hrs · 22,585 cycles

CORROSION ON FLOORBOARD SUPPORT AT STATION 200 13 INCH IS INBOARD OF NR 3 SEAT TRACK. INSTALLED NEW FLOORBOARD SUPPORT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,339 hrs · 45,339 cycles

LGA - SEAT MOUNTED EMERGENCY LIGHT AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB5 1 FOR SEAT MOUNTED EMERGENCY LIGHT AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 45,339 hrs · 45,339 cycles

LGA - EMERGENCY LIGHT AT FORWARD GALLEY EXIT SIGN INOPERATIVE. REPAIRED BROKEN WIRE AT TERMINAL FOR EMERGENCY LIGHT AT FORWARD GALLEY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,339 hrs · 45,339 cycles

LGA - SEAT MOUNTED EMERGENCY LIGHT AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB5 4 FOR SEAT MOUNTED EMERGENCY LIGHT AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: FIRE DETECTOR — SHORTED (CARGO BAY)

RDU INFLIGHT T1702/06SEP - AFT CARGO FIRE INDICATION ILLUMINATED AT 35000 FEET. CREW FIRED BOTTLES BUT INDICATION WOULD NOT EXTINGUISH. LANDED RDU WITHOUT INCIDENT. FOUND AFT CARGO COMPARTMENT FIRE DETECTION ELECTRONICS UNIT SHORTED AND INOPERATIVE DUE TO LEAKAGE FROM AFT GALLEY LEAKING COFFEE MAKER AND CLOGGED DRAIN. REPLACED COFFEE MAKER, CLEARED DRAIN, REPLACED AFT CARGO COMPARTMENT FIRE DETECTION ELECTRONICS UNIT AND BOTH AFT CARGO FIRE EXTINGUISHERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT IN FIRST CLASS FORWARD GALLEY CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN FIRST CLASS FORWARD GALLEY CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - AFT SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 21 TO 31 INOPERATIVE. REPLACED AFT BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 21 TO 31. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (CABIN)

DTW - EMERGENCY EXIT LIGHT ON SIDEWALL OF FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY EXIT LIGHT ON SIDEWALL OF FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - OVERHEAD EMERGENCY LIGHTS AT BIN N020 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT BIN N020. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,040 hrs · 15,472 cycles

THE EGRESS LIGHT AT ROW 25, AND THE EGRESS LIGHTS FROM ROW 27 THROUGH 29, WERE INOPERATIVE. REINSERTED LAMP AT ROW 25, AND CLEANED LAMP ASSEMBLY SOCKETS AT ROW 29. CHECK-C 11-16-02 STL. --CLOSED--

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 31,040 hrs · 15,472 cycles

THE EMERGENCY LIGHTS IN THE CEILING ABOVE THE CATWALK IN THE TAIL, THE EMERGENCY LIGHT IN THE TAIL JUST ABOVE THE AFT END AREA OF THE CATWALK, AND THE EMERGENCY EXIT LIGHT AT THE RIGHT FWD WING EXIT, WERE ALL INOPERATIVE. REPLACED THE BATTERIES PN 408822-101 IN THE POWER SUPPLY FOR THE CATWALK CEILING LIGHT, REPLACED THE BULB PN 7732 FOR THE TAIL LIGHT, AND REPLACED THE BULB PN 1315 FOR THE EXIT LIGHT. CHECK-C 11-16-02 STL. --CLOSED--

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,670 hrs · 15,255 cycles

THE EGRESS LIGHTS WERE INOPERATIVE AT ROW 24 AND AFT. REPLACED THE BATTERY PACK BATTERIES. CHECK-C 11-16-02 STL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 27,399 hrs · 13,273 cycles

DURING CHECK-C MAINT THE NUMBER 2 RT LONGERON WAS CRACKED .125 INCH AT STA 1220. REPAIRED PER SRM 53-02, PAGES 49 THRU 53.

Part: SOCKET — BROKEN (AIRSTAIRS) · airframe 25,991 hrs · 12,520 cycles

THE EGRESS LAMP BASE WAS BROKEN IN THE AFT AIRSTAIRS MIDDLE POSITION. REPLACED THE EGRESS BASE. CHECK-C 3-3-01 MCI.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT THE NUMBER 5 CABIN SEAT TRACK, O/B FLANGE, STA 229, HAD CORROSION. REMOVED AND REPLACED FWD SECTION OF TRACK, APPROX 5 INCHES, TO EXISTING SPLICE PER SPM 6-70-01, PARA 4, ITEM A AND B. INSTALLED FASTENERS PER 51-30-2.

Part: STIFFENER — BROKEN (AUX TANK) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT THE FWD FUEL AUX TANK TOP LT SIDE STIFFENER WAS BROKEN APPROX 12 INCHES. INSTALLED 2 CHANNELS AND 1 FILLER PER ARA 17624.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT THE NUMBER 4 CABIN FLOOR TRACK WAS CORRODED AT STA 200 TO 229. SPLICED SECTION OF TRACK PER SRM 53-05, FIG 4F.

Part: WEB — CORRODED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT FOUND FLOOR WEB CORRODED AT STA 1098 TO 1117, AT LONGERON 18R. CUT OUT CORROSION AND INSTALLED REPAIR PER SRM 53-01, FIG 4 SHEET 3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, FORMER 1250 WAS CORRODED TOP AND BOTTOM AT LONGERON 29L TO 29R. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-03, FIG 2A SHEET 4.

Part: RIB — CRACKED (DORSAL FIN) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT NUMBER 3 AND 4 DORSAL FIN RIBS, FROM UPPER EDGE ON LT SIDE, WERE CRACKED. ROUTED AND RADIUSED END OF RIB. INSTALLED REPLACEMENT FILLER ON NUMBER 3 AND 4. INSTALLED 2024-T3 0.050 DOUBLER PICKING UP MINIMUM 3 ROWS OF FASTENERS BEYOND CRACK PER 55-30-102.

Part: CASTING — CORRODED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT FORMER ATTACH CASTING AFT INBOARD LEG WAS CORRODED AT STA 1079, LONGERON 18R. REPLACED CASTING PER SPM 6-70-01.

Part: CASTING — CORRODED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT CABIN LONGERON 18R, STA 732, FORMER ATTACH CASTING INBD LEG HAD CORROSION. REMOVED CORRODED ATTACH CASTING AND REPLACED WITH NEW PER SRM 51-30-1 AND 53-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT FLOOR TRACK AT LBL 44 WAS CORRODED FROM STA 1136 TO 1211. REPLACED TRACK PER SRM 53-05, FIG 4F SHEET 1.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT CABIN FLOOR TRACK AT LBL 22, STA 807 TO 1308, HAD CORROSION REMOVED BEYOND LIMITS. REPLACED FLOOR TRACK FROM STA 807 TO 1308, PER SRM 53-05 PAGE 109.

Part: LATCH — DAMAGED (PAX DOOR) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT A TIME LIMITED REPAIR AT THE FWD CABIN DOOR ON THE LT SIDE, THE GUST LOCK LATCH, REPAIR HAD BLIND FASTENERS. REMOVED REPAIR PATCH AND INSTALLED NEW PERMANENT REPAIR PER SRM 53-04, FIG 24.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT OUTBOARD OF NUMBER 4 FLOOR PANEL, UNDER A-GALLEY DRAIN PAN. REMOVED DRAIN PAN AND FLOOR SUPPORT. FABRICATED FLOOR SUPPORT FROM STOCK PER SPM 6-70-01. INSTALLED SUPPORT AND DRAIN PAN PER SPM 6-70-01.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE LT FLOOR TRACK WAS CORRODED AT STA 1222 TO 1322. REPLACED WITH NEW FLOOR TRACK PER SRM 51-01, PAGE 1 ITEM C.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT RT SIDE OF CABIN FLOOR, MEMBRANE WAS CRACKED OUT NEXT TO SIDE WALL AT STA 1297, JUST FWD OF LAV WALL. INSTALLED DOUBLER PER SRM 53-01 FIG 2, SHEET 3.

Part: WEB — CORRODED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT LONGERON 18R, STA 636 TO 644, FLOOR WEB HAD CORROSION. REMOVED CORROSION BY CUTTING DAMAGE OUT PER SRM 53-01 PAGE 18. INSTALLED REPAIR PER SRM 53-01 PAGE 18.

Part: ANGLE — DAMAGED (F/A SEAT) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT THE AFT BULKHEAD DOOR, RT UPPER HINGE ARM FOR THE FLT ATTENDANT SEAT, HAD DAMAGED ANGLE BELOW THE PIVOT POINT. CUT OUT DAMAGED AREA AND INSTALLED STACKED DOUBLERS PER SRM 52-01, PAGE 9.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT FOUND FLOOR WEB AT LONGERON 18R, STA 484 TO 503, WAS CORRODED. REMOVED CORROSION PER SRM 53-10-3. INSTALLED REPAIR PER SRM 53-01, PAGE 9, WITH 5/32 AD RIVETS.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT FOUND LONGERON 18R, STA 560 TO 579, THE FLOOR WEB HAD CORROSION. CUT OUT CORROSION. INSTALLED DOUBLER PER SRM 53-01, PAGE 9.

Part: WEB — CORRODED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT FOUND CORROSION IN MEMBRANE BETWEEN STA 826 AND 845, AT LONGERON 18L. REMOVED CORROSION PER SPM 6-80-01. TREATED AREA PER SRM 51-10-3 PAGE 54. REINSTALLED FASTENERS PER SRM 51-30-2.

Part: WEB — CORRODED (FUSELAGE) · airframe 25,345 hrs · 12,172 cycles

DURING CHECK-C MAINT FOUND CORROSION IN MEMBRANE BETWEEN STA 845 AND 964 AT LONGERON 18L. CUT OUT CORRODED PIECE FROM MEMBRANE STA 845 TO 855 APROXIMATELY. TREATED REPAIR PARTS AND AREA PER SRM 51-10-3 PAGE 54. REPAIRED DAMAGED AREA PER SRM 51-70-4.

Part: LIGHT — INOPERATIVE (TAIL CONE) · airframe 23,922 hrs · 11,378 cycles

THE EMERGENCY LIGHT IN THE TAIL CONE AREA, AND THE EGRESS LIGHT AT ROW 25D, WERE INOPERATIVE. REPLACED THE LAMP (P/N 1315) IN TAIL CONE, AND THE LAMP (P/N 7732) AT ROW 25D. CHECK-C 11-2-99 STL.

Part: WIRE — BROKEN (CABIN) · airframe 23,405 hrs · 11,088 cycles

THE FIRST 3 EGRESS LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. FOUND A BROKEN WIRE. REPLACED LAMP ASSEMBLY. CHECK-C 22-20-99 STL.

Part: BATTERY PACK — DISCHARGED (BS 830)

THE MIDDLE CABIN EMERGENCY LIGHTS WOULD NOT SHUT OFF. REPLACED THE BATTERY PACK. CHECK-C 11-20-99 STL.

Part: WHEEL — FAILED (NR 2)

DURING TAKEOFF, THE NUMBER 2 WHEEL ASSEMBLY FAILED. RUBBER FROM THE TIRE CAUSED DAMAGE TO THE LT LANDING GEAR, GEAR WIRING, T/E FLAP AND THEN ENTERED THE LT ENGINE. A LOUD BANG WAS HEAR FROM THE ENGINE AND THE CREW SHUT IT DOWN. THE FLIGHT RETURNED TO BWI. REPLACED THE WHEEL ASEMBLY, AND REPAIRED THE DAMAGE, INCLUDING REPLACEMENT OF THE ENGINE FIRST STAGE FAN. CHECK-C 12-5-98 MCI.

Part: POWER SUPPLY — INOPERATIVE (ROW 22-23)

EGRESS LIGHTING EMERGENCY EXIT STRIPS WERE MISSING AT ROW 22 AND 23, AND IN FRONT OF LAVS. REPLACED THE EGRESS LIGHT POWER SOURCE (P/N 5822-2) AND THE RED LENS AT ROWS 21, 29, 32 AND 33. LENS (P/N 0105607-301). CHECK-C 12-15-98 MCI.

Part: LIGHT — BROKEN (CABIN)

DURING PREFLIGHT INSPECTION FOUND EGRESS LIGHT SEGEMENT BROKEN. REPLACED LIGHT SEGMENT. CC-02D 12-15-98 MCI.

Part: BULB — FAILED (CABIN)

FOUND FLOOR EGRESS LIGHTS OUT ROWS 5 TO 25 AND ROW 27. REPLACED LAMPS. CHECK-C 12-8-98 MCI.

Part: BATTERY PACK — DISCHARGED (EMER EXIT)

FOUND OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. CHECK-C 12-16-97.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

STL - DURING MAINTENANCE GROUND CHECK, FOUND AFT MOST EGRESS LIGHT SECTION INOP. REPLACED POWER SUPPLY BATTERIES. (M)

Part: CHIP DETECTOR — FAILED (NR 1 ENGINE)

CMH - FLT 139 - DURING CRUISE, NR 1 ENGINE LOST OIL QUANTITY AND WAS SHUT DOWN IN FLIGHT. CHIP DETECTOR RETAINING PINS FAILED AND SPRING VALVE FAILED TO CLOSE. REMOVED AND REPLACED CHIP DETECTOR PLUG AND HOUSING, MFG P/N B7670, MANUFACTURED BY VICKERS, INC. OPS CHECK NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

STL - DURING PREFLIGHT, EGRESS LIGHT STRIPS BETWEEN ROWS 12 THROUGH 16 WERE INOPERATIVE. REMOVED AND REPLACED WORN LIGHT STRIP, MFG P/N 0105606-003. OPERATIONAL CHECK NORMAL.

Part: LPT 3 SEAL — FAILED (NR 2 ENGINE)

LNK - FLT 235 - DURING CRUISE SHUT DOWN NR 2 ENGINE, SN 1402, DUE TO OIL LOSS. FOUND OIL LEAK IN TURBINE AREA. REPLACED NR 2 ENGINE AND ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 9,465 HOURS; 4,437 CYCLES. CHECK C-1D - 12-23-95 - JFK. FURTHER INVESTIGATION INTO NR 2 ENGINE SHUT-DOWN REVEALED A FAILED LPT 3 SEAL RESULTING IN THE OIL LOSS. THE SEAL HAS BEEN REPLACED AND ENGINE, SN 1402, HAS BEEN RETURNED TO SERVICE.

Part: ENGINE — OIL LEAK (NR 2)

LNK - FLT 235 - DURING CRUISE, SHUT DOWN NR 2 ENGINE, SN 1402, DUE TO OIL LOSS. FOUND OIL LEAK IN TURBINE AREA. REPLACED NR 2 ENGINE AND ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 9,465 HOURS; 4,437 CYCLES. CHECK C-1D - 12-23-95 - JFK.