N9627R

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,791 hrs · 22,343 cycles

MID CABIN OVERHEAD CEILING EMER LIGHTS INOPERATIVE. R & R BATTERY PACK BF-104 AT ROW 20 IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,791 hrs · 22,342 cycles

AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL. ACFT WAS OVERWEIGHT. DURING CLIMB THROUGH 10,000 FEET A STRONG BURNT RUBBER SMELL WAS REPORTED IN CABIN BUT DISSIPATED QUICKLY. ACCOMPLISHED MCM 21-96-01 WITH NO FINDINGS. R & R BOTH LT & RT AIR CONDITIONING REGULATORS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,791 hrs · 22,343 cycles

FOUND AFT CABIN OVERHEAD EMER LIGHTS BY LAVATORIES INOPERATIVE. R & R BATTERY PACK IAW 33-53-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,791 hrs · 22,343 cycles

FIRST CLASS CABIN OVERHEAD CEILING EMER LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,604 hrs · 21,726 cycles

INFLIGHT FLIGHT ATTENDANTS REPORTED SMOKE ODOR IN AFT CABIN. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. ACCOMPLISHED PACK BURN WITH NO FAULTS FOUND. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SHUTOFF VALVE — INOPERATIVE (RT ENGINE) · airframe 43,855 hrs · 20,870 cycles

LAS CREW REPORTED RT HAND ENG HIGH OIL TEMPERATURE INDICATION. ACCOMPLISHED QRH & SHUT DOWN RT HAND ENG IN FLIGHT, SINGLE ENG TIME 22 MINUTES. EMERGENCY DECLARED FLIGHT RETURNED LAS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AIR FUEL HEATER SHUT-OFF VLV. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: ENGINE — SURGES (LEFT) · airframe 43,289 hrs · 20,551 cycles

DFW CREW REPORTED LT ENGINE SURGES FOLLOWED BY ENGINE VALVE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT HAND ENGINE AT DFW ON 9/12/2013. SYSTEM GROUND CHECKED NORMAL OPERATION OPEN.

Part: GENERATOR — FAILED (RT ENGINE) · airframe 41,720 hrs · 19,684 cycles

DFW - CREW REPORTED MULTIPLE INTERMITTANT POWER INTERRUPTIONS FOLLOWED BY RIGHT HAND GENERATOR FAILURE INDICATIONS. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED GENERATOR, CONSTANT SPEED DRIVE, OIL COOLER AND TWO OIL LINES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSE LINE — LOOSE (AC PACK) · airframe 40,682 hrs · 19,171 cycles

ORD - CREW REPORTED UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. THE OUTFLOW VALVE WAS CLOSED AND LEFT PACK SHOWED 50 ON THE PRESSURE GAUGE. RIGHT PACK WAS ON A PLACARD INOPERATIVE. EMERGENCY DECLARED FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND AIR PRESSURE SENSE LINE ON LEFT PACK LOOSE. RE-TIGHTENED AND TORQUED SENSE LINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SPRING — BROKEN (EMERGENCY EXIT) · airframe 37,656 hrs · 17,647 cycles

FOUND SPRING BROKEN ON AFT FUSELAGE EMERGENCY EXIT PRESSURE BULKHEAD DOOR ARM ASSEMBLY. REPLACED BROKEN SPRING IAW AMM 53-5302-2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,228 hrs · 16,922 cycles

THE 1510 CANT FRAME CRACKED ABOVE LEFT LOWER TAIL CONE LATCH. INSTALLED DOUBLER PER EA MD80-53-015073 1/27/2011.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,228 hrs · 16,922 cycles

CUSP SECTION STATIONS 579 TO 598 CORRODED BEYOND MANUAL LIMITS. INSTALLED NEW SECTION OF CUSP.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,228 hrs · 16,922 cycles

CABIN HAS CORROSION IN SUB FLOOR WEBBING BETWEEN AFT SERVICE DOOR OPENING, NUMBER 2 SEAT TRACK AND BETWEEN STATIONS 1136 TO 1174. INSTALLED TITANIUM SPLICE REPAIR DOUBLER PER AARD 53-20-00-16.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,228 hrs · 16,922 cycles

CABIN - FUSELAGE DOUBLER CORRODED ON TOP OF RIGHT CUSP AT STATION 592. INSTALLED NEW FUSELAGE SPLICE DOUBLER RIGHT STATIONS 585 TO 592 PER SRM 51-30-05.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 36,228 hrs · 16,922 cycles

SEVERAL DAMAGED HOLES IN LEFT CUSP STATIONS 1089 TO 1098 AT NUMBER 2 SEAT TRACK FLANGE. INSTALLED REPAIR DOUBLER AT LEFT CUSP STATIONS 1080 TO 1098 AT THE NUMBER 2 SEAT TRACK PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 36,228 hrs · 16,922 cycles

CORROSION ON BOTTOM SIDE OF RIGHT CUSP STATION 898. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16 AND SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,228 hrs · 16,922 cycles

SEAT TRACK NUMBER 4 TOP FLANGE OUT OF LIMITS. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 51-30-01.

Part: SKIN — DENTED (CARGO DOOR) · airframe 36,228 hrs · 16,922 cycles

AFT CARGO DOOR HAS EXCESSIVE DENTS ON EXTERIOR SKIN. REMOVED AND REPLACED EXTERIOR SKIN ON AFT CARGO DOOR PER ESO 80174.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,228 hrs · 16,922 cycles

INTERCOSTAL BETWEEN CABIN FLOORBEAMS STATIONS 1287 TO 1309 IS CRACKED. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL PER AA DRAWING EDK1904, SRM 51-30-05 AND SRM 51-30-02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,228 hrs · 16,922 cycles

WEB AFT OF DOOR OPENING HAS CORROSION LONGERON 26 TO 25 RIGHT. INSTALLED WEB SPLICE DOUBLER PER SRM 51-7-0-04.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 36,228 hrs · 16,922 cycles

CABIN HAS A CRACK IN FORWARD SHEAR TIE ON RIGHT AFT LAVATORY WALL STATION 1307 ABOVE LONGERON 16. INSTALLED NEW SHEAR TIE PER AARD 51-10-00-5 AND BOEING DRAWING 9912243-543.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,228 hrs · 16,922 cycles

CORROSION OUT OF LIMITS, LEFT SIDE CUSP, STATION 717. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 36,228 hrs · 16,922 cycles

MID CARGO DOOR: OUTER SKIN REPAIR HAS HIGH RIVETS AND DENTS, MARKED. INSTALLED OUTER SKIN DOUBLER AT MID CARGO DOOR SRM 52-05 FIGURE 1 SHEET 1.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,228 hrs · 16,922 cycles

DENT STATION 218 IN RED STRIPE RIGHT SIDE. INSTALLED INTERNAL DOUBLER PER SRM 53-04-00 FIGURE 38 SHEET 20 AND 22.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,569 hrs · 15,260 cycles

ONE INCH CRACK IN UPPER J-ANGLE, FORWARD SIDE OF FRAME STATION 1418 AT LONGERON 2 LEFT. FABRICATED AND INSTALLED DOUBLER AT FRAME 1418 AND LONGERON 2 LEFT PER ENGINEERING AUTHORIZATION MD80-53-007990.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,568 hrs · 15,260 cycles

LONGERON 20 FITTING IS CRACKED AT LOWER FLANGE ABOVE FLAP TRACK RIGHT SIDE. INSTALLED DOUBLER ON LONGERON 20 PER AARD 53-10-00-18 MSR 023198.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 32,569 hrs · 15,260 cycles

FORWARD CARGO DOOR AT LOWER DOOR STOP CASTING CRACKED. REMOVED AND REPLACED DOOR-STOP FITTING PER ESO-80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 32,569 hrs · 15,260 cycles

MID CARGO DOOR FORWARD MID STOP CASTING CRACKED. REMOVED AND REPLACED STOP-PAD FITTING PER ESO-80174.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,569 hrs · 15,260 cycles

APPROXIMATELY 1 INCH CRACK IN FUSELAGE SKIN AT LEFT STATION 1474. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,814 hrs · 14,932 cycles

SFO - OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,814 hrs · 14,932 cycles

FUSELAGE DAMAGED AT STATION 905 BETWEEN LONGERONS RIGHT 2 & RIGHT 5. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER, TRIPLER & FINGER DOUBLERS PER EA MD80-53-006823.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

AUS - EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED PORTABLE LIGHT ASSEMBLY AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL VALVE — LEAKING (THRUST REVERSER)

SFO ON GROUND T1951/07JUL - AFTER LANDING FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN. TURNED OFF APU BLEED AIR AND SMOKE BEGAN TO DISSIPATE. FOUND THRUST REVERSER HYDRAULIC LEAK AT CONTROL VALVE B NUT. TIGHTENED NUT AND NO LEAKS FOUND. REPLACED APU DUE TO HYDRAULIC FLUID INGESTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY FLOOD LIGHT IN COCKPIT INOPERATIVE. RELAMPED EMERGENCY FLOOD LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT)

DFW - AFT EMERGENCY FLOOD LIGHT AT STAIR WELL INOPERATIVE. CLEANED CONNECTOR FOR AFT EMERGENCY FLOOD LIGHT AT STAIR WELL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT OVERWING EXIT SIGN INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHTS AT SEAT ROW 3 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT SEAT ROW 3. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS AT RIGHT AND LEFT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT AND LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS AT CENTER AISLE CEILING AT SEAT ROWS 23, 24, AND 26 INOPERATIVE. RELAMPED EMERGENCY LIGHT AT CENTER AISLE CEILING AT SEAT ROWS 23, 24, AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

BOS - EMERGENCY LIGHTS AT FORWARD AND AFT RAFT STORAGE LOCATION INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD BIN FOR EMERGENCY LIGHTS AT FORWARD AND AFT RAFT STORAGE LOCATION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

AISLE EMERGENCY EXIT ARROW LIGHT AT FORWARD FIRST CLASS INOPERATIVE. REPINNED CONNECTOR FOR FORWARD EMERGENCY EXIT ARROW LIGHT IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - OVERHEAD EMERGENCY LIGHTS AT ROW 29 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — CORRODED (EMERGENCY LIGHT)

LGA - CEILING EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. CLEANED CORROSION ON NUMBER 2 EMERGENCY BATTERY PACK IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (CABIN) · airframe 10,978 hrs · 5,566 cycles

RIGHT OVERWING FLOOR EGRESS LIGHTS INOP. REPLACED WIRE SECTION AND REPLACED MISSING COVERS. LENS MFG PN 0105607 3015MI-932831/ COVER MFG PN 0105601003 PA57-932841/ WIRE SECTION MFG PN 0105606 0055MI-93289 LAST CHECK C PERFORMED IN STL 11/16/2001. --CLOSED--

Part: TERMINAL · airframe 10,808 hrs · 5,468 cycles

THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 26 AFT. REPLACED TERMINAL BOARD THAT MAY HAVE BEEN ACCIDENTLY KICKED BY A PASSENGER. CHECK-C 11-16-01 STL. --CLOSED--

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 9,620 hrs · 4,518 cycles

BOTH COCKPIT EMERGENCY LIGHTS FAILED TO ILLUMINATE. TIGHTENED WIRE TERMINAL AT B5-23 AND REPLACED THE BATTERIES IN THE POWER SUPPLY.

Part: POWER SUPPLY (FWD CABIN) · airframe 8,637 hrs · 4,192 cycles

THE EMERGENCY LIGHTS AT THE COCKPIT DOOR STAYED ON WHEN POWER REMOVED. REPLACED THE POWER SUPPLY. CHECK-C 12-17-00 JFK. --CLOSED--

Part: MODULE (ROW 12 TO 15) · airframe 8,398 hrs · 4,078 cycles

THE EGRESS LIGHTS AT ROW 12 TO 15 WERE INOPERATIVE. REPLACED THE LAMP MODULE. CHECK-C 12-17-00 JFK. --CLOSED--

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,402 hrs · 4,081 cycles

THE EXIT LIGHT AT THE FWD EXIT DOOR HAD LENS FALLING OFF, THE COCKPIT CEILING EMERGENCY EXIT LIGHT WAS INOPERATIVE, THE EGRESS EXIT LIGHT AT THE AFT GALLEY DOOR WAS INOPERATIVE, THE EGRESS LIGHT ON THE FLOOR FROM SEAT 30D TO AFT LAV WAS INOPERATIVE, AND THE EGRESS LIGHT AT SEAT 14D WAS INOPERATIVE. REPLACED EXIT LIGHT P/N 0105610-001, REPLACED LAMP P/N AML-43, REPLACED LAMP P/N 2232, SECURED LOOSE CONNECTOR AT SEAT 30D, AND REPLACED LAMP P/N 7732 AT SEAT 14D. CHECK-C 12-17-00 JFK.

Part: LIGHT — INOPERATIVE (ROW 28) · airframe 5,678 hrs · 2,797 cycles

THE FLIGHT DECK AND FWD GALLEY EMERGENCY LIGHTS, EGRESS LIGHT AT ROW 28D, AND THE OVERHEAD EMERGENCY LIGHTS IN THE AFT GALLEY WERE INOPERATIVE. THE RED LENS FOR EGRESS LIGHTS IN THE AFT CABIN WAS MISSING. REPLACED THE BATTERIES IN THE BATTERY PACK FOR THE FWD EMERGENCY LIGHTS (P/N 014597-101), REPLACED THE LAMP AT ROW 28C (P/N 7732), REPLACED THE BATTERIES IN THE BATTERY PACK FOR THE AFT GALLEY (P/N 014597-101) AND REPLACED THE RED LENS FOR THE AFT CABIN EGRESS LIGHTS (P/N 0105607-301). CHECK-C 11-5-99 STL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 4,370 hrs · 2,210 cycles

THE CAPTAINS BRIEF CASE LIGHT AND CAPTAINS YOKE LIGHT WERE INOPERATIVE. FOUND WIRING BURNED/OVERHEATED NEAR TERMINAL STRIP S3-51, WIRE CONNECTED TO CIRCUIT BREAKER B1-267 WAS BURNED, AND CIRCUIT BREAKER B1-267 WAS BURNED. SPLICED IN NEW WIRING AT S3-51, SPLICED NEW WIRE AND TERMINAL TO WIRE LEADING TO CB B1-267, AND REPLACED CB B1-267. CHECK-C 11-5-99 STL.

Part: LAMP — FAILED (GALLEY DOORWAY)

TWO RED EGRESS LIGHTS WERE INOPERATIVE AT THE AFT GALLEY DOOR. REPLACED A LAMP ASSEMBLY, (P/N 0105606-002) AND A LAMP MODULE, (P/N 0105606-004).

Part: AIR DIST — ODOR (CABIN)

MCI - ON CLIMBOUT HAD A HAZE AND HOT SMELL IN THE CABIN. ACCOMPLISHED PACK BURN OUT AND CHECKED TAIL COMPARTMENT FOR LEAKS, FOUND NONE.