N554UA

Part: SWITCH — REVERSED (EXTINGUISH SYS) · airframe 72,613 hrs · 21,590 cycles

FOUND FWD AND AFT CARGO FIRE EXTINGUISHING ARMING SWITCHES REVERSED. SWAPPED LENSE CAPS, TEST OK. CONFIRMED POSITIONS WITH PILOTS FLIGHT MANUAL.

Part: COMPRESSOR — NOISY · airframe 72,110 hrs · 21,493 cycles

CLICKING SOUND COMING FROM UNDER THE AFT GALLEY FLOOR. NOISE STOPS WHEN P6 K21 CIRCUIT BREAKER IS OPENED. REPLACED COMPRESSOR.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,947 hrs · 21,462 cycles

EXTERNAL FUSELAGE DENTED STA 334 STR 25L. REMOVED DAMAGE HFEC C-W P ER NDT MANUAL PT6. 51-00-19. REPAIR ACCOMPLISHED PER ECRA 5311- 01565. THE FUSELAGE SKIN REPAIR INSTALLED BETWEEN BS 216-343 AND STR 21L-25L.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,947 hrs · 21,462 cycles

FLOORBEAM UPPER SURFACE HAS CORROSION BULGE BETWEEN MATING SURFACES AT NUT PLATES BS 1680 RBL 40 - RBL 45, WL 208. MAJOR REPAIR ACCOMPLISHED: REPAIRED FLOORBEAM UPPER CHORD AT BS 1680 RBL 40 PER ECRA 5365-01070.

Part: STRUCTURE — DAMAGED (R4 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R4 DOOR INTERIOR ABOVE LOWER HINGE WEB - LIGHTENING HOLE. MAJOR REPAIR ACCMP'D: REMOVED CRACK & PERFORMED HFEC IAW NDT MANUAL PT6, 51-00-19. FABRICATE AND INSTALLED REPAIR PER ECRA 5211-01253.

Part: FRAME — DENTED (FUSELAGE) · airframe 71,947 hrs · 21,462 cycles

FORWARD PIT, LEFT FRAME STA 660 DENTED ABOVE STR 24. MAINT TEXT: DAMAGE REMOVED AND HFEC PERFORMED PER NDT MANUAL 51-00-16. REPAIR INSTALLED PER ECRA. RII INSPECTION ACCOMPLISHED AND REPAIR COMPLETED PER ECRA 5330-04326.

Part: FRAME — DENTED (FUSELAGE) · airframe 71,947 hrs · 21,462 cycles

FORWARD PIT, LEFT FRAME STA 660 DENTED ABOVE STR 24. DAMAGE REMOVED AND HFEC PERFORMED PER NDT MANUAL 51-00-16. REPAIR INSTALLED PER ECRA5330 -04326.

Part: FITTING — OUT OF ADJUST (R1 DOOR) · airframe 71,947 hrs · 21,462 cycles

R-1 DOOR WON'T ARM. REMOVED AND RE-INSTALLED SLIDE COVER PER MM AND ADJUSTED FLOOR FITTING AND PERFORMED SYSTEMS TEST GOOD PER MM.

Part: FEEDER CABLE — CHAFED (CABIN) · airframe 71,947 hrs · 21,462 cycles

FOUND CHAFED FEEDER CABLES ABOVE CLOSET AT BS 400. REMOVED VIDEO SYSTEM CONTROL PANEL, DIGITAL VIDEO FILE SERVER AND FORWARD LEFT CLOSET. REPAIRED FEEDER CABLE OUTER JACKET PER BSWPM 20-10-13 AND RE- INSTALLED VIDEO PANEL AND DIGITAL FILE SERVER AND OPS GOOD PER MM ON NON ROUTINE 40840.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 71,947 hrs · 21,462 cycles

EMERGENCY EXIT IDENTIFIER AT AFT LEFT DOOR HAS BROKEN CONNECTOR. RETERMINATED EXIT LIGHT AFT LEFT DOOR D6676 PER BSWPM 20-72-25 AND WDM 33-51-22. PERFORMED A OPS TEST GOOD OF LIGHT ASSY L783 EXIT LIGHT PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN FLOOR BEAM T-CAP CORRODED AT BS 324, RBL 50 - RBL 60. REMOVED DAMAGED SECTION OF T-CAP AND MACHINED A NEW CHORD AND SPLICE ANGLE & INSTALLED PER SRM 53-10-08, REPAIR 1. PER SRM, TABLE 202, THIS IS A CAT B REPAIR AND REQUIRES FUTURE NDT INSPECTIONS BEGINNING AT 37,500 TOTAL AIRFRAME CYCLES, AND EVERY 12,000C THEREAFTER. CURRENT PTC IS 21462.

Part: PAN — GOUGED (L1 DOOR) · airframe 71,947 hrs · 21,462 cycles

DOOR 1L PASSENGER DOOR EXTERIOR HANDLE PRESSURE PAN IS GOUGED MIN THICKNESS IS .032 PAN HAS A DEEP GOUGE MEASURING .030 DEEP ALSO HANDLE ROTATES COMPLETELY AROUND DOOR VERY HARD TO CLOSE FROM OUTSIDE CAN CLOSE FROM INSIDE THE AIRCRAFT BUT NOT FROM THE OUTSIDE. SRM 52-10-10 SHOWS DOOR PAN .063 THICK 2024 T3. GOUGE DEPTH MEAS .032 INCH DEEP. REPLACED HANDLE BOX ASSY PER CMM, REPLACED HANDLE PAN ASSY PER SRM 51-40-2 AND RECONNECTED LATCHING PUSH RODS AND YOKE CLEVIS.

Part: SKIN — DENTED (L1 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L-1 DOOR EXTERIOR SKIN DENTED APPROXIMATELY 8 INCHES ABOVE LOWER HINGE POINT FWD TO AFT APPROX 4 INCHES. DENT MEASURES L=2.3", W=.6", AND D=.023" FOUND TO BE OUT OF LIMITS PER SRM 52-10-01, FIG 101. CUT OUT DAMAGED SKIN AND FABRICATED A REPAIR DOUBLER PER SRM 52-10-01, REPAIR 7.

Part: SLIDE RAFT — IMPROPER PART (L4 DOOR) · airframe 71,947 hrs · 21,462 cycles

DOOR 4L SLIDE IS NOT EFFECTIVE THIS AIRCRAFT, AND NEEDS TO BE REPLACED WITH A NON RAFT EQUIPPED SLIDE. REPLACED L-4 DOOR SLIDE PER MM ON NON ROUTINE 40823.

Part: ROLLER — OUT OF RIG (R4 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R-4 DOOR LATCH ROLLERS OUT OF RIG. ADJUSTED LATCH ROLLER PER MM ON NON ROUTINE 40129.

Part: FITTING — CHAFED (R4 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN DOOR R-4 CENTERING GUIDE CHAFES FITTING. REPLACED P/N 146N6269-8 TRACK ASSY FITTING R-4 DOOR, AFT UPPER INNER SIDE PER SRM 51-40- 2. RIG CHECK GOOD PER MM.

Part: TORQUE TUBE — CORRODED (R4 DOOR) · corrosion level 2 · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R-4 DOOR INTERIOR LOWER CENTER LATERAL ARMING TORQUE TUBE, 3 EACH BEARINGS CORRODED. REMOVED AND REPLACED LOWER ARMING TORQUE TUBE AND BELLCRANK ASSY AND REPLACED 3 EACH BEARINGS PER CMM 52-11-25 AND MM 20-10-02 AND FUNCTIONAL CHECK GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN FLOORBEAM T-CAP CORRODED AT BS 363, RBL 40. REMOVED DAMAGED SECTIONS OF T-CAP AND FABRICATED A NEW REPAIR CHORD AND SPLICE ANGLES AND STRAPS PER EC-RA 5310-05536 NR 3, AND INSTALLED PER SRM 53-00-51.

Part: FITTING — CORRODED (R4 DOOR) · corrosion level 2 · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R-4 DOOR TORQUE TUBE CENTER BEARING CORRODED COMING APART. REPLACED BEARING 140N2652-19 FITTING ASSY AND INSTALLED ON NON ROUTINE.

Part: GATE — OUT OF ADJUST (R4 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R-4 DOOR FAILED TORQUE TO UNLATCH DOOR BELOW MINIMUM. ADJUSTED UPPER & LOWER GATES PER MM & FUNCTIONAL CHECK GOOD ON NON ROUTINE 40130.

Part: FASTENER — CORRODED (R4 DOOR) · corrosion level 2 · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R-4 DOOR TORQUE TUBE LOWER HARDWARE CORRODED. REMOVED AND REPLACED TORQUE TUBE HARDWARE PER CMM 52-11-25 AND RIG CHECKED DOOR PER MM ON NON ROUTINE 40154.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,947 hrs · 21,462 cycles

FLOORBEAM T-CAP UPPER SURFACE HAS SEVERAL AREAS OF CORROSION AROUND THE NUT PLATE HOLES AT BS 1640, RBL 0 - RBL 50. MAJOR REPAIR ACCOMPLISHED: REMOVED EXISTING T-CAP REPAIR AND FABRICATED AND INSTALLED A NEW CHORD, SPLICE ANGLES AND STRAPS PER SRM 53-00-51.

Part: CAM — BINDING (R1 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R-1 DOOR UPPER AFT CAM PLATE SHOWS SIGNS OF BINDING DURING THE CLOSING OF THE DOOR. REMOVED AND REPLACED UPPR AFT LATCH CAM ON THE R1 MED IAW B757 AMM 52-11-37 PO 752923. FUNTIONAL CHECK ACCOMPLISHED ON CUST CARD 5S5215119 AND B757 AMM 52-11-04.

Part: ROD — MISINSTALLED (L4 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L-4 DOOR COCKING ROD IMPROPERLY INSTALLED, GREASE FITTING IS NOT FACING INBOARD. REMOVED COCKING ROD AND INSTALLED IAW B757-200 CMM.

Part: SLIDE — LOW PRESSURE (L4 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L-4 DOOR SLIDE PRESSURE LOW, READS 1384 PRESSURE. INSTALLED NEW SLIDE IAW B757-200 AMM.

Part: BEARING — CORRODED (R1 DOOR) · corrosion level 2 · airframe 71,947 hrs · 21,462 cycles

R-1 DOOR UPPER LATERAL LATCHING TORQUE TUBE FWD AND AFT BEARINGS CORRODED. REMOVED AND REPLACED R1 MED UPPER LATERAL TORQUE TUBE BEARINGS FWD AND AFT IAW B757 AMM 20-10-02. FUNCTIONAL CHECK PERFORMED ON CUST CARD 5S521S117 SEQ 5892 AND B757 AMM 52-11-04.

Part: HANDLE — OUT OF ADJUST (R1 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R-1 DOOR HANDLE FAILED UNLATCHING TEST. ADJUSTED R1 MED HANDLE UNLATCHING TORQUE IAW B757 AMM.

Part: MECHANISM — OUT OF ADJUST (L1 DOOR) · airframe 71,947 hrs · 21,462 cycles

DOOR 1L EXTERNAL HANDLE DOES NOT SEAT PROPERLY, VERY DIFFICULT TO CLOSE RESULTING IN 9 MIN DELAY. REMOVED, RE-INSTALLED & ADJUSTED L-1 DOOR HANDLE MECHANISM IAW AMM. REPLACED INNER, CENTER SHAFT, CLUTCH COLLAR AND BEARINGS. ALSO ACCOMPLISHED ECRA 5210-02315.

Part: MECHANISM — FAILED (L1 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L-1 DOOR FAILED BUTTERFLY CHECK. REMOVED, REPLACED & ADJUSTED L-1 DOOR HANDLE MECHANISM IAW B757 AMM. REPLACED INNER & CENTER SHAFT, CLUTCH COLLAR & BEARING FUNCTION CHECK GOOD. ACCOMPLISHED ECRA#5210-02315.

Part: HANDLE — OUT OF ADJUST (L4 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L4 DOOR DOOR HANDLE LATCH FAILED FORCE CHECK. ADJUSTED LATCH FORCE PER MM AND OPS CHECKED GOOD.

Part: WIRE — BROKEN (FUEL PANEL) · airframe 71,947 hrs · 21,462 cycles

RIGHT WING LEADING EDGE FUEL-DEFUEL ACCESS PANEL, LIGHT WIRING IS BROKEN AT SPLICE AND HAS NON ENVIROMENTAL EXPOSED SPLICE. REPAIRED SPLICE PER BSWPM 20-10-13 AND PERFORMED OPS CHECKED GOOD.

Part: GUIDE — OUT OF ADJUST (L1 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L1 DOOR CENTER GUIDE OUT OF ADJUSTMENT. ADJUSTED CENTERING GUIDE PER MM AND CLEARANCE CHECKED GOOD.

Part: MECHANISM — OUT OF ADJUST (L2 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L2 DOOR FAILED MIDWAY CHECK. ADJUSTED SELECTOR MECHANISM PER MM AND OPS CHECKED GOOD.

Part: HARNESS — FRAYED (L1 DOOR SLIDE) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L1 DOOR ESCAPE SLIDE HARNESS LOWER CENTER ATTACH POINT FRAYED. REPLACED HARNESS WITH SERVICEABLE HARNESS.

Part: PLATE — CORRODED (R1 DOOR) · corrosion level 2 · airframe 71,947 hrs · 21,462 cycles

R1 DOOR LOWER CAM PLATES CORRODED. REPLACED CAM PLATES PER MM.

Part: HANDLE — MALFUNCTIONED (R2 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R2 DOOR FAILED BUTTERFLY CHECK. REMOVED INTERIOR HANDLE, STUB SHAFT, CONTROL CAM, FITTING, CLUTCH COLLAR, INNER SHAFT, YOKE, THRUST COLLAR, BASKET CAM, OUTER SHAFT AND OUTER HANDLE PER MM. INSPECTED COMPONENTS AND REINSTALLED AND ASSEMBLED HANDLE COMPONENTS PER MM. FUNCTIONAL CHECKED GOOD.

Part: GUIDE — GOUGED (R2 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R2 DOOR CUT-OUT CENTERING GUIDE GOUGED. REMOVED AND REPLACED CENTERING GUIDE, IAW MM 52-11-00 AND 25-21-06.

Part: CAM — OUT OF ADJUST (L1 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L1 DOOR FAILED MIDWAY CHECK. ADJUSTED LOCKOUT CAM PER MM.

Part: PLATE — CORRODED (L1 DOOR) · corrosion level 2 · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L1 DOOR UPPER CAM PLATE CORRODED. REPLACED CAM PLATE WITH NEW.

Part: CONTROL ROD — CORRODED (L1 DOOR GIRT BAR) · corrosion level 2 · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L1 DOOR GIRT BAR MECHANISM LOWER AFT CONTROL ROD CORRODED. REMOVED AND REPLACED GIRT BAR CONTROL ROD PER MM.

Part: BEARING — CORRODED (L4 DOOR) · corrosion level 2 · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L4 DOOR LOWER HINGE BEARING AT PIVOT PIN CORRODED. REMOVED BEARING AND INSTALLED NEW BEARING PER MM 20-10-02.

Part: PLATE — CORRODED (R2 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R2 DOOR TORQUE TUBE LOWER TWO CAM PLATES CORRODED. REMOVED UPPER AND LOWER CAM PLATES AND LOWER HINGE. REPLACED BOTH CAMPLATES AND REINSTALLED PLATES AND HINGE PER MM 52-11-02.

Part: HANDLE — NO TEST (R1 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R1 DOOR FAILED BUTTERFLY CHECK. REMOVED INTERIOR DOOR HANDLE, STUB SHAFT AND CAM PLATE. REPLACED CENTER AND INNER SHAFTS, REASSEMBLED DOOR HANDLE ASSY PER MM AND FUNCTIONAL TESTED GOOD.

Part: GUIDE — GOUGED (L2 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L2 DOOR CENTERING GUIDE GOUGED. REMOVED AND REPLACED CENTERING GUIDE PER MM 52-11-00.

Part: CONTROL ROD — BENT (R1 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R1 DOOR ARM-DISARM BUMPER CONTROL ROD BENT. REMOVED AND REPLACED MAIN CABIN R1 DOOR ARM-DISARM BUMPER CONTROL ROD PER AMM AND MM, FIG 505. ADJUSTMENT CHECK GOOD.

Part: COVER — BENT (L1 DOOR) · airframe 71,947 hrs · 21,462 cycles

L1 DOOR LOWER HINGE COVER BENT. REMOVED BENT HINGE COVER AND INSTALLED NEW COVER, IAW SM-50-52-11-01-JD.

Part: SPRING — FAULTY (R1 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN R-1 DOOR EXTERIOR TORQUE TUBE HINGE DOOR DOES NOT EXTEND INTO THE CLOSED POSITION PROPERLY. REMOVED AND REPLACED SPRING PART #66-14641-1, IAW 757 GNMM 1-0-1-080.

Part: SPRING — FAULTY (L2 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L-2 DOOR UPPER HINGE FLAPPER DOOR DOES NOT EXTEND PROPERLY TO THE CLOSED POSITION. REMOVED AND REPLACED SPRING PART # 140N2025-1 IAW 757 GNMM 1-0-1-080.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,947 hrs · 21,462 cycles

SKIN DENTED 15 INCHES BELOW WATER DRAIN BELOW 2L. INSPECTED SKIN WITH HFEC IAW NDT 51-00-01. NO CRACKS FOUND. REPAIRED DENT IAW SRM 53-00-01 FIG 201 REPAIR 3. HFEC ACCOMPLISHED IAW NDT MANUAL PT 6 51-00-19 AND 51-00-16.

Part: SNUBBER — WORN (L1 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L-1 DOOR SNUBBER WORN WITH FULL PIN EXTENSION, DOES NOT SLOW DOOR. ISSUED ON-CONDITION JIC FOR SNUBBER REPLACEMENT 5S521S125, 5S521S111 AND 5S521S110 AS DOCUMENTED.

Part: SNUBBER — WORN (L4 DOOR) · airframe 71,947 hrs · 21,462 cycles

MAIN CABIN L-4 DOOR SNUBBER WEAR INDICATOR RECESSED WORN BEYOND LIMITS. ISSUED ON-CONDITION JIC 5S521S129 FOR SNUBBER REPLACEMENT, AS DOCUMENTED ON NON ROUTINE 40157.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 70,033 hrs · 21,093 cycles

NO SIDE TONE WITH CAPT'S OXYGEN MASK. RPLC'D NR 1 AUDIO CONTROL PANEL, CHECK OKAY.

Part: SPRING — BROKEN (EXIT LATCH) · airframe 67,298 hrs · 20,559 cycles

RT FWD OVERWING LATCH DOOR LOWER HANDLE NOT FLUSH. FOUND SPRING BROKEN. REPLACED RT OVERWING EMERGENCY EXIT HATCH PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,274 hrs · 20,174 cycles

EMERGENCY LIGHT INOP AT DOOR NR 3 LT. SECURED BULB. CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,258 hrs · 20,171 cycles

EMERGENCY EXIT LIGHT SEAT 8B INOPERATIVE. TROUBLESHOT EMERGENCY EXIT LIGHT SEAT 8B TO A BAD LAMP. R & R SEAT 8B EMERGENCY LIGHT AND OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (SMOKE DETECTOR) · airframe 65,258 hrs · 20,171 cycles

FWD LAV SMOKE DETECTOR CONNECTOR FOUND DISCONNECTED AND DAMAGED DURING TEST. REMOVED AND REPLACED DAMAGED CONNECTOR & OPS CHECK GOOD PER MM ON NON ROUTINE 2303N00032.

Part: LIGHT — INOPERATIVE (SEAT 22C) · airframe 64,326 hrs · 19,987 cycles

SEAT 22C EMERGENCY LIGHT STRIP INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP PER MM.

Part: LIGHT — INOPERATIVE (SEAT 25C) · airframe 64,326 hrs · 19,987 cycles

SEAT 25C EMERGENCY LIGHT STRIP INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP PER MM. OPS GOOD.

Part: LIGHT — INOPERATIVE (SEAT 18ABC) · airframe 63,854 hrs · 19,896 cycles

SEAT MOUNTED EMERGENCY LIGHT ASSY INOP AT SEAT 18ABC. REPLACED LIGHT ASSY. OPS CHECKD OK.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 61,331 hrs · 19,402 cycles

F/C LAV SMOKE DETECTOR NOT POWERED. REPLACED SMOKE DETECTOR, OP CHECKS GOOD.

Part: INTERROGATOR — ODOR (DME) · airframe 61,076 hrs · 19,353 cycles

DURING TAKEOFF SMELLED ELECTRICAL ODOR, NO SMOKE, AFTER SAFELY AIRBORNE SAW R DME CB POPPED. ELECTRIC ODOR DISSIPATED QUICKLY AFTER CB POPPED. REPLACED RIGHT DME INTERROGATOR, TESTS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,730 hrs · 19,283 cycles

SEAT MOUNTED EMERGENCY LIGHT INOP AT SEAT ROW 18ABC. REPLACED LIGHT ASSY, OP CHECK OKAY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,766 hrs · 19,101 cycles

DOOR NR 2 LEFT EMERGENCY EXTERIOR SLIDE LIGHT IS INOP. RELAMPED EMERGENCY LIGHT, CHECKS GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 59,298 hrs · 19,013 cycles

EEL LIGHT ON SEAT 18C IS MISSING. REPLACED LIGHT ASSY, OPS OK.

Part: LIGHT — MISSING (CABIN) · airframe 59,287 hrs · 19,011 cycles

EMERGENCY LIGHT STRIP MISSING FROM AISLE SEAT 15 ABC. REPLACED LIGHT ASSY, CHECKS GOOD.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 58,328 hrs · 18,826 cycles

G2A GALLEY EMERGENCY LIGHT FEEDER CABLE DAMAGED. REPAIRED G2A GALLEY EMERGENCY LIGHT FEEDER CABLE AND OPS CHECK GOOD.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 58,328 hrs · 18,826 cycles

G1B GALLEY EMERGENCY LIGHT FEEDER CABLE DAMAGED. REPAIRED G1B EMERGENCY LIGHT FEEDER CABLE AND OPS CHECK GOOD.

Part: PANEL — DELAMINATED (APU BAY) · airframe 58,328 hrs · 18,826 cycles

APU COMPARTMENT RT INTERIOR PANEL DELAMINATED. FABRICATED A CORE PLUG, INNER SKINS AND DOUBLER AND INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,328 hrs · 18,826 cycles

AFT PIT FRAME DENTED BS 1440, STR 26L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME DENT AT STA 1440 WITH FABRICATED J-ANGLE REPAIR.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 58,328 hrs · 18,826 cycles

A-ZONE EEL SEAT CABLE DAMAGED. REPLACED CONNECTOR, OPS CHECKS GOOD.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 58,328 hrs · 18,826 cycles

G4A GALLEY EMERGENCY LIGHT FEEDER CABLE DAMAGED. RE-TERMINATED AND INSTALLED G4A GALLEY EMERGENCY LIGHT FEEDER CABLE AND LIGHT ASSY, OPS CHECKS GOOD.

Part: FEEDER CABLE — DAMAGED (A-ZONE) · airframe 58,328 hrs · 18,826 cycles

A-ZONE EMERGENCY LIGHT SEAT FEEDER CABLE DAMAGED. REPAIRED WIRES, OPS CHECKS GOOD.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,328 hrs · 18,826 cycles

FWD CARGO COMPT, FRAME HAS SEVERAL DENTS AT LT BS 540 AND BETWEEN STR 24L-25L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED J-DOUBLER REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,328 hrs · 18,826 cycles

EXT FUSE STA 560 TO STA 600 BELLY SKIN (LBL 10 TO RBL 10) HAS NUMEROUS ARCHIVED DENTS. MAJOR REPAIR ACCOMPLISHED. CUTOUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,328 hrs · 18,826 cycles

FWD CARGO COMPT, FRAME HAS A DENT BS 520 AND BETWEEN STR 24L-25L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,328 hrs · 18,826 cycles

AFT PIT FRAME DENTED BS 1460, STR 26L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: GATE — CORRODED (L4 DOOR) · airframe 58,328 hrs · 18,826 cycles

L-4 DOOR LOWER GATE CORRODED. DAMAGE EXCEEDS LIMITS. INSTALLED NEW GATE.

Part: TUBE — DAMAGED (SMOKE DETECTOR) · airframe 58,328 hrs · 18,826 cycles

FWD PIT SMOKE DETECTOR TUBE CUT AND DETERIORATED STA 640, RBL 20. LOCATION LWR PART OF UPPER FLOORBEAM. INSTALLED NEW SMOKE DETECTOR TEE TUBE.

Part: LIGHT — DAMAGED (G2B GALLEY) · airframe 58,328 hrs · 18,826 cycles

G2B GALLEY EEL LIGHT DAMAGED. REPAIRED 2 EA EEL LIGHTS FOR G2B GALLEY, OPS CHECKS GOOD. BOTH HAD BROKEN PIN.

Part: LIGHT — DAMAGED (G2B GALLEY) · airframe 58,328 hrs · 18,826 cycles

G2B GALLEY EEL LIGHT DAMAGED. REPAIRED 2 EA EEL LIGHTS FOR G2B GALLEY, OPS CHECKS GOOD. BOTH HAD BROKEN PIN.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,328 hrs · 18,826 cycles

AFT CARGO COMPARTMENT, FRAME DENTED BS 1380, STR 25L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,328 hrs · 18,826 cycles

AFT PIT FRAME DENTED BS 1420 AND STR 26L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: GATE — CORRODED (R4 DOOR) · airframe 58,328 hrs · 18,826 cycles

R-4 DOOR LOWER GATE CORRODED. INSTALLED NEW GATE.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,328 hrs · 18,826 cycles

FWD PIT BILGE, FRAME AT STA 660 RT SIDE HAS A DENT BETWEEN STR 24R-25R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,328 hrs · 18,826 cycles

AFT PIT FRAME DENTED BS 1400, STR 26L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: MECHANISM — OUT OF ADJUST (L1 DOOR) · airframe 58,328 hrs · 18,826 cycles

DOOR 1L EMERGENCY POWER TRIGGER MECHANISM OUT OF ADJUSTMENT. ACCOMP ADJUSTMENT AND OPS CHECKS GOOD.

Part: CABLE — OUT OF ADJUST · airframe 58,328 hrs · 18,826 cycles

LT OFF WING BACK UP CABLE DIMENSION FROM SUPPORT SHROUD TO THE BACK UP CABLE THREADS FOUND OUT OF LIMITS. ADJUSTED THE SUPPORT SHROUD TO CABLE BACK UP CABLE THREAD DIMENSION NOW AT .060.

Part: OVEN — SHORT (GALLEY) · airframe 57,701 hrs · 18,706 cycles

FIRST CLASS OVEN OVERHEATING. FLT DIVERTED. INTERNAL SHORT IN GALLEY OVEN. REPLACED BOTH FORWARD GALLEY OVENS. OPS CHECKED NORMAL.

Part: CIRCUIT CARD — FAULTY (FIRE DETECTION) · airframe 54,916 hrs · 18,176 cycles

AFT CARGO FIRE WARNING SYSTEM INOPERATIVE. INDICATION ISSUE WITH FIRE DET CIRCUIT CARD. REPLACED BOTH FWD AND AFT FIRE DET CIRCUIT CARDS, ACCOMPLISHED ALL CHECKS FOR SYSTEM OPS.

Part: CIRCUIT CARD — FAULTY (FIRE DETECTION) · airframe 54,913 hrs · 18,175 cycles

FLIGHT DIVERTED DUE TO AFT CARGO FIRE INDICATION. INDICATION ISSUE WITH CONTROL CARD. REPLACED FIRE DET CIRCUIT CARD M10427 FOR FWD AND AFT CARGO SMOKE DETECTION. ALL OPS CHECKS PERFORMED WERE SATISFACTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,065 hrs · 18,014 cycles

WALL MOUNTED EEL LIGHTS OUT BELOW GALLEY 1 AND GALLEY 3.

Part: WIRE — BURNED (AFT LAVATORY) · airframe 52,465 hrs · 17,707 cycles

ACFT RTBL WITH DOOR 3L AFT LAVATORY BURNING ODOR DUE TO A BURNED WIRE. 09-14-07 ON TROUBLESHOOTING FOUND TOILET TANK FILL LINE SHUTOFF VALVE CONNECTOR HAS BURNED WIRES. CAPPED WIRES & TIED BACK. CONNECTOR SECURED AT AREA FOR RE-USE. LAVATORY TO SERVICE FROM INSIDE OR MANUALLY OPEN SHUTOFF VALVE FOR SERVICING.

Part: LIGHT — INOPERATIVE (R1 DOOR SLIDE) · airframe 52,166 hrs · 17,649 cycles

DOOR 1R SLIDE ARM LIGHT NOT ON WITH DOOR ARMED. CLEANED CONTACTS ON PROX SWITCH AND REPLACED LED LAMP. CHECKS OK.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 52,134 hrs · 17,643 cycles

MED 2R FWD FRAME CRACKED, 3-8 INCH LONG, AT UPPER HINGE CUTOUT LWR RADIUS. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR.

Part: HARNESS — BUCKLED (SLIDE) · airframe 50,483 hrs · 17,330 cycles

SLIDE ASSY HARNESS BUCKLES AT DOOR 1L WILL NOT LATCH SLIDE PACK CORRECTLY ONTO DOOR ASSY. REPLACED SLIDE ASSY HARNESS AS WELL AS SLIDE ASSY. CAUSE OF FAILURE NOT ESTABLISHED AT THE TIME.

Part: WARNING MESSAGE — ILLUMINATED · airframe 48,267 hrs · 16,904 cycles

LANDED UNDER AMBER ALERT DUE TO TRAILING EDGE FLAP DISAGREE INDICATION. FSEU SHOWS MESSAGE "RT FLAP DRIVE" MESSAGE NUMBER 315. REPLACED FSEU NR 1 AND 2 AND RH FLAP POSITION TRANSMITTER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,740 hrs · 13,612 cycles

CABIN FLOORBEAM UPPER CAP CORRODED AT STA 324, RBL 45, 50, 53, 57 AND 58 (BOTH FWD AND AFT SIDES OF UPPER CAP) MAJOR REPAIR ACCOMPLISHED. FLOORBEAM CAP REPLACED.

Part: SILL — DAMAGED (PAX DOOR) · airframe 36,740 hrs · 13,612 cycles

LT ENTRY DOOR WAY CUT OUT UPPER SILL HAS 4 HOLES DRILLED INTO IT. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,740 hrs · 13,612 cycles

CABIN FLOORBEAM HAS CORROSION UNDER GUTTER AT BS 365, RBL 59-61. MAJOR REPAIR ACCOMPLISHED. INSTALLED CABIN FLOOR BEAM UPPER CAP "I" BEAM REDUCED SPLICE LENGTH REPAIR.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,740 hrs · 13,612 cycles

FWD NOSE COMPARTMENT STATION 202, AT STRINGER 18 RIGHT HORIZONTAL FLOOR SUPPORT ANGLE CRACKED IN RADIUS AND ALONG HORIZONTAL FLOOR WEB. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT ANGLE WEB.

Part: STRINGER — DENTED (FUSELAGE) · airframe 33,410 hrs · 12,336 cycles

STRINGER 16L DENTED AT STATION 613. MAJOR REPAIR ACCOMPLISHED. STRINGER SPLICE CHANNEL INSTALLED WITH SPACER WHERE STRINGER WAS REMOVED.

Part: FAN — FAILED (COCKPIT)

FLIGHT DIVERTED TO EWR DUE TO THE SMELL OF SMOKE IN THE COCKPIT. *S/D* ELECTRICAL SMELL WAS ATTRIBUTED TO THE LEFT RECIRCULATION FAN. THE LEFT FAN WAS REPLACED.

Part: BOTTLE GUAGE — BROKEN (1L DOOR)

DOOR 1L EMERGENCY POWER ASSIST BOTTLE INDICATOR BROKEN. *S/D* REPLACED BOTTLE ASSEMBLY PER MM 52-11-30.

Part: LIGHT — INOPERATIVE (CABIN)

LEFT EXTERIOR EMERGENCY EXIT AFT LIGHT WAS INOP. REPLACED THE LIGHT. OPERATIONAL CHECK WAS NORMAL.

Part: ACTUATOR — MALFUNCTIONED (NR 6 SLAT)

LANDED UNDER AMBER ALERT DUE TO SLAT ASYMMETRY INDICATION. SLAT CORRECTED FROM FLAP ORIGINALLY REPORTED. REPLACED NR 6 SLAT ROTARY ACTUATOR.