N680DA

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,751 hrs · 39,675 cycles

SHIP 0680 EMERGENCY INTERIOR LIGHT ON CEILING PANEL INOPERATIVE AT SEAT 42. CORRECTIVE ACTION: FOUND LOOSE CONNECTION ON LIGHT WIRE. OPS CHK GOOD. (5001860)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,939 hrs · 39,125 cycles

SHIP 0680 -ATB/DE- AIRCRAFT RETURNED TO ATL AFTER QRH COMPLETION FOR LE SLAT ASYM INDICATION. CORRECTIVE ACTION: C/W OVERWEIGHT LANDING INSP. FOUND SLAT LOSS SWITCH TRIPPED AND RT O/B SLAT LOSS SWITCH CABLE TENSION OUT OF RIG, REPLACED R/H LEADING EDGE SLAT POSITION TRANSMITTER AND COMPLETED RIG. C/W NO GO ODI STEPS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,926 hrs · 39,115 cycles

SHIP 0680 -MISC/DE- CREW ELECTED DE AFTER QRH COMPLETION FOR LE SLAT ASYM INDICATION. CORRECTIVE ACTION: FOUND R/H O/B SLAT LOSS SWITCH TRIPPED. CABLE AND SLAT LOSS SYSTEM INTACT. FOUND R/H O/B SLAT ROTARY ACTUATOR NBR 20 TORQUE INDICATOR TRIPPED. R/R NBR 20 ROTARY ACTUATOR AND R/H O/B SLAT LOSS SWITCH. C/W MCC LOGS. A/C RTS.

Part: HINGE — MISINSTALLED (L2 DOOR) · airframe 88,544 hrs · 40,120 cycles

SHIP 680 NO. 2 PASSENGER DOOR FWD FRAME UPPER HINGE CUTOUT SHORT EDGE DISTANCE ON FACTORY SRM REPAIR DOUBLER. CORRECTIVE ACTION: REF ERA 608571-14. (2870814)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 86,590 hrs · 38,931 cycles

SHIP 680 AD - AWR - DAMAGES WERE FOUND ON LH ENG DRAG FTG AND CLAMP-UP HOLES 1-10 AS FOLLOW: HOLE #1 TO #10 CORROSION ON SKIN AND FITTING ALL AROUND, ADDITIONALLY HOLE #7 GOUGE ON FITTING AT 6 CLOCK POSITION, IN REFERENCE TO JOB 068-0001 / CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00191: LH ENG DRAG FTG AND CLAMP-UP HOLES 1,6,7,9 AND 10 WERE REPAIRED CARD 5720-01100-04A AND 2, 3, 4, 5 AND 8 WERE REPAIRED PER PRI 609107-14AD REV. 5 AND ER/A 609107-14AD REV ORIG SECTION I: PERMANENT REPAIR. (2810384)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 86,590 hrs · 38,931 cycles

SHIP 680 AD - AWR - DAMAGES WERE FOUND ON LH ENG DRAG FTG AND CLAMP-UP COUNTERSINKS 11-18 AS FOLLOW: COUNTERSINK #11 WORN AREAS BETWEEN 3 TO 4 CLOCK POSITION; COUNTERSINK #12 WORN AREAS BETWEEN 10 TO 11 CLOCK POSITION; COUNTERSINK #13 CORROSION BETWEEN 5 TO 11 CLOCK POSITION AND WORN AREAS BETWEEN 3 TO 4 CLOCK POSITION; COUNTERSINK #14 CORROSION AND WORN AREA AT 5 CLOCK POSITION; COUNTERSINK #15 CORROSION BETWEEN 4 TO 7 CLOCK POSITION; COUNTERSINK #16 CORROSION BETWEEN 5 TO 9 CLOCK POSITION; COUNTERSINK #17 CORROSION BETWEEN 5 TO 12 CLOCK POSITION AND WORN AREAS BETWEEN 5 TO 8 CLOCK POSITION; COUNTERSINK #18 CORROSION AT 7 CLOCK POSITION AND WORN AREAS AT 3 AND BETWEEN 5 TO 7 CLOCK POSITIONS, IN REFERENCE TO JOB 072-0001 / CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00194: COUNTERSINKS OF HOLES #11 TO #18 WERE REPAIRED PER PRI 609107-14 REV. 0 AND ER/A 609107-14AD REV. ORIG SECTION I: PERMANENT REPAIR. (2808347)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,590 hrs · 38,931 cycles

SHIP 680 A.A.-A.D. DISBOND (2.000 IN X 2.000 IN) AT ISS 158, UPPER SURFACE LE SLAT 5 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACTION: SUMMARY OF NRC: 00005 AT ISS 158, UPPER SURFACE LE SLAT 5 TRAILING EDGE WEDGE, LH WING. WAS REPAIRED PER B757-200 SRM. (2808560)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 86,590 hrs · 38,931 cycles

SHIP 680 AD - AWR - DAMAGES WERE FOUND ON LH ENG DRAG FTG AND CLAMP-UP COUNTERSINKS 1-10 AS FOLLOW: COUNTERSINK #1 CORROSION BETWEEN 9 TO 12 CLOCK POSITON AND WORN AREAS AT 1 AND 5 CLOCK POSITIONS; COUNTERSINK #2 CORROSION BETWEEN 9 TO 11 CLOCK POSITION; COUNTERSINK #3 CORROSION BETWEEN 6 TO 8 CLOCK POSITION AND WORN AREAS BETWEEN 9 TO 3 CLOCK POSITION; COUNTERSINK #4 CORROSION BETWEEN 6 TO 9 CLOCK POSITION AND SCRATCHES BETWEEN 12 TO 3 CLOCK POSITION; COUNTERSINK #5 CORROSION BETWEEN 5 TO 7 CLOCK POSITION; COUNTERSINK #6 CORROSION ALL AROUND; COUNTERSINK #7 CORROSION BETWEEN 5 TO 12 CLOCK POSITION; COUNTERSINK #8 CORROSION BETWEEN 3 TO 7 CLOCK POSITION AND WORN AREAS AT 3 AND BETWEEN 6 TO 12 CLOCK POSITIONS; COUNTERSINK #9 CORROSION BETWEEN 5 TO 6 CLOCK POSITION AND WORN AREAS BETWEEN 8 TO 1 CLOCK POSITION; COUNTERSINK #10 CORROSION AT 8 CLOCK POSITION AND WORN AREAS AT 12 AND 4 CLOCK POSITIONS, IN REFERENCE TO JOB 068-0001 / CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00192: COUNTERSINKS OF HOLES #1 TO #10 WERE REPAIRED PER PRI 609107-14 REV. 0 AND ER/A 609107-14AD REV. ORIG SECTION I: PERMANENT REPAIR. (2808236)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,590 hrs · 38,931 cycles

SHIP 680 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609107-14AD . CORRECTIVE ACTION: ACCOMPLISH SECTION VI REPETITIVE UT INSPECTIONS PRIOR TO 43,731 TOTAL FLIGHT CYCLES, AND REPETITIVELY EVERY 4,800 CYCLES THEREAFTER PER ERA ERA 609107-14AD (2806408)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,590 hrs · 38,931 cycles

SHIP 680 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609107-14AD. CORRECTIVE ACTION: ACCOMPLISH SECTION IV REPETITIVE BHEC INSPECTIONS (1-10) PRIOR TO 41,931 TOTAL FLIGHT CYCLES, AND REPETITIVELY EVERY 3,000 CYCLES THEREAFTER PER ERA 609107-14AD (2806399)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,590 hrs · 38,931 cycles

SHIP 680 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609107-14AD CORRECTIVE ACTION: ACCOMPLISH SECTION III REPETITIVE DVI INSPECTIONS PRIOR TO 41,931 TOTAL FLIGHT CYCLES, AND REPETITIVELY EVERY 3,000 CYCLES THEREAFTER PER ERA 609107-14AD (2806395)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,590 hrs · 38,931 cycles

SHIP 680 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609107-14AD. CORRECTIVE ACTION: REF ERA 609107-14AD. (2806394)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,590 hrs · 38,931 cycles

SHIP 680 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609107-14AD. CORRECTIVE ACTION: ACCOMPLISH SECTION V REPETITIVE BHEC INSPECTIONS (11-18) PRIOR TO 44,931 TOTAL FLIGHT CYCLES, AND REPETITIVELY EVERY 6,000 CYCLES THEREAFTER PER ERA 609107-14AD (2806404)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,590 hrs · 38,931 cycles

SHIP 680 A.A.-A.D. DISBOND (2.250 IN X 1.500 IN) AT OSS 523 UPPER SURFACE LE SLAT 8 TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00007: UPPER SURFACE LE SLAT 8 TRAILING EDGE WEDGE, RH WING AT OSS 523. WAS REPAIRED PER B757-200 AMM 51-21- 14 AND B757-200 SRM (2803909)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,590 hrs · 38,931 cycles

SHIP 680 A.A/A.D.DAMAGES WERE FOUND AS FOLLOWS: NICK ON COUNTERSINK AT HOLE 14 BTW 4-6 HRS AND BTW 10-12 HRS, HOLE 18 6 HRS AND 2 HRS. RH ENG DRAG FTG CLAMP-UP RH WING (REF. CARD). CORRECTIVE ACTION: SUMMARY OF NRC 00237: NICK ON COUNTERSINK AT HOLE 14 BTW 4-6 HRS AND BTW 10-12 HRS, HOLE 18 6 HRS AND 2 HRS. RH ENG DRAG FTG CLAMP-UP RH WING WERE REPAIRED PER ERA 609153-14AD REV ORIGINAL SECTION I PERMANET REPAIR PART. B AND PRI 609153-14 REV. 3. (2800473)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 86,590 hrs · 38,931 cycles

SHIP 680 A.A/A.D. DAMAGES WERE FOUND AS FOLLOWS: CORROSION ON HOLE 5 FITTING BTW 6-8 HRS, HOLE 3 SKIN BTW 9-12 HRS, HOLE 8 SKIN/ FITTING BTW 3-5 HRS, HOLE 6 SKIN BTW 5-6 HRS ALSO GOUGES ON HOLE 4 SKIN 6 HRS, HOLE 2 SKIN 5 HRS, HOLE 10 FITTING BTW 6-7 HRS, HOLE 9 SKIN 10HRS. RH ENG DRAG FTG CLAMP-UP RH WING (REF. CARD). CORRECTIVE ACTION: SUMMARY OF NRC 00234 : HOLE 5 FITTING BTW 6-8 HRS, HOLE 3 SKIN BTW 9-12 HRS, HOLE 8 SKIN/FITTING BTW 3-5 HRS, HOLE 6 SKIN BTW 5 -6 HRS ALSO GOUGES ON HOLE 4 SKIN 6 HRS, HOLE 2 SKIN 5 HRS, HOLE 10 FITTING BTW 6-7 HRS, HOLE 9 SKIN 10HRS. RH ENG DRAG FTG CLAMP-UP RH WING (REF. CARD 5720-01100-04B STEP14.C) WERE REPAIRED PER ERA 609153-14AD REV ORIGINAL SECTION I PERMANET REPAIR PART. A TO D AND PRI 609153-14 REV. 3. (2800278)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,590 hrs · 38,931 cycles

SHIP 680 A.A/A.D. NICK ON COUNTERSINK AT HOLE 5 BTW 4-7 HRS AND BTW 11-1 HRS. RH ENG DRAG FTG CLAMP-UP RH WING (REF. CARD). CORRECTIVE ACTION: SUMMARY OF NRC 00235 : COUNTERSINK AT HOLE 5 BTW 4-7 HRS AND BTW 11-1 HRS. RH ENG DRAG FTG CLAMP-UP RH WING WAS REPAIRED PER ERA 609153-14AD REV ORIGINAL SECTION I PERMANET REPAIR PART. A TO B AND PRI 609153-14 REV. 3. (2800476)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,590 hrs · 38,931 cycles

SHIP 680 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609153-14AD. CORRECTIVE ACTION: REF ERA 609153-14AD. (2796803)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,590 hrs · 38,931 cycles

SHIP 680 A.A.-A.D. DISBOND (1.500 IN X 1.500 IN) ON PREVIOUS REPAIR AT OSS 469, UPPER SURFACE LE SLAT 8 TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00006: UPPER SURFACE (OSS 469) SLAT 8 TRAILING EDGE WEDGE RH WING WAS REPAIRED PER B757-200 SRM. (2793596)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,590 hrs · 38,931 cycles

SHIP 680 AMOC, ER/A 608829-14AD - SECTION I REPAIR IS COMMON TO SSI INSPECTION AREA SSI 53-60-24. REF ERA 608829-14AD. (2771971)

Part: NONE — NONE (NONE) · airframe 86,588 hrs · 38,930 cycles

DTA MONITOR INSPECTION LOG IAW ERA 494839-14 REV. C. ERA 494839-14 REV C.

Part: FITTING — OBSTRUCTED (L2 DOOR) · airframe 86,464 hrs · 38,875 cycles

(AIRCRAFT 680, L/P 7219792) GUST LOCK ON 2L DOOR WILL NOT ENGAGE. CORRECTIVE ACTION: CLEARED DEBRIS FROM L2 DOOR FITTING AND LUBED HOLD OPEN LOCK COLLAR AND OPS CK OK PER B757-AMM-52-11.

Part: STOP FITTING — MISSING (L2 DOOR) · airframe 85,255 hrs · 38,325 cycles

DURING A-CHK FOUND 1 DOOR STOP FITTING MISSING ON L2 AND R2 DOORS. INSTALLED DOOR STOP FITTINGS IAW AMM 52-11-00.

Part: INDICATOR — STICKING (LT DOOR ARMED) · airframe 83,281 hrs · 37,411 cycles

SHIP 680 KNUCKLE-KNOCKER ON AFT LEFT DOOR STICKS. IT POPPED OUT AS ARMED ON TAXI VICE WHEN ARMED. CORRECTIVE ACTION: OPERATED SEVERAL TIMES. KNOCKER OPS CHK NML. (5601926)

Part: NONE — NONE (NONE) · airframe 86,590 hrs · 38,931 cycles

SHIP 680 ERA 571509-14 REVISION A REQUIRES THE FOLLOW-ON SECTION II ONE TIME INPECTION AT THE NEXT C-CHECK. CORRECTIVE ACTION: REF ERA 571509-14. (0868168)

Part: WIRE — DETACHED (LAVATORY FAUCET) · airframe 82,786 hrs · 37,201 cycles

(AIRCRAFT 680, L/P 5189820) ON SVC FOUND WHEN YOU TOUCH LAV K FAUCET AND DOOR YOU GET SHOCKED. RECONNECTED WIRES 8-MM1-004, 8-MM1-044, AND 6-RR1-050 TO GROUND STUD 6. RECONNECTED WIRE 8-MM1-012 TO GROUND STUD 7 PER ZODIAC CMM 25-40-40.

Part: LIGHT — MISSING (SEAT 43D) · airframe 82,701 hrs · 37,155 cycles

(AIRCRAFT 680, L/P 5155698) DURING SERVICE CHECK FOUND SEAT MOUNTED EMERGENCY LIGHT MISSING AT SEAT 43D. REPLACED SEAT MOUNTED LIGHT AND SHROUD AT ROW 43D PER CMM 1041631.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,337 hrs · 36,965 cycles

CORROSION ON STRINGER SPLICE FROM STA 1400 TO 1420 S-28L AT AFT CARGO COMPARTMENT PER TASK NR CP53-153-01I 2020-2379 (C2). LEVEL CORROSION 2, STR 29L BTW STA 1400 TO STA 1420 WAS REPAIRED PER INSTRUCTIONS CONTAINED IN ER/A 571509-14 REV ORIGINAL.

Part: STRAP — BROKEN (EVAC SLIDE) · airframe 82,337 hrs · 36,965 cycles

BROKEN STRAPS ON BOTH UPPER SECURITY PINS OF THE R4 DOOR SLIDE, CARD 2040-0057 (PTAS). EVACUATION SLIDE ASSY 4R WAS REMOVED PER 2040-0057-4R, AND WAS REPLACED FOR A SERVICEABLE PART PER AMDS 2040-0057-4R.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,337 hrs · 36,965 cycles

CORROSION ON BEAM RBL 16, LBL 16, RBL 2 AND LBL 2 ALSO ON STRINGER RBL 10, LBL 10, RBL7 AND LBL 7 FROM STA 1300 TO 1350 AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2 BEAM RBL 16, LBL 16, RBL 2 AND LBL 2 ALSO ON STRINGER RBL 10, LBL 10, RBL7 AND LBL 7 FROM STA 1300 TO 1350 WERE REPAIRED PER SRM 53-00-53 REP 1 FIG 201.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,337 hrs · 36,965 cycles

CORROSION ON RT STRINGERS RBL 2.90, 7.55 AND 10.45 FROM STA 1500 TO 1520 AT AFT CARGO COMPARTMENT CP53-153-01I (C2). CORROSION LEVEL 2. CORROSION ON STGR RBL 2.90 WAS REPAIRED PER SRM 53-00-53 REPAIR 1 FIG 201. CORROSION ON STGR RBL 7.55 AND 10.45 WAS FOUND AT PREVIOUS REPAIR CHANNELS AND BOTH WERE REPLACED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,337 hrs · 36,965 cycles

CORROSION ON STRINGER S-29R BTW STA 1460 TO 1480 AT AFT CARGO COMPARTMENT PER TASK NR CP53-153-01, 2020-2379. REPAIR ON STRINGER S-29R BTW STA 1460 TO 1480 AT AFT CARGO COMPARTMENT WAS ACCOMPLISHED WITH ER/A 571426-14 REV A.

Part: ACCESS PANEL — CRACKED (LE SLAT) · airframe 82,337 hrs · 36,965 cycles

CRACKED LOWER SKIN, AT SLAT PANEL N?10, STA OSS 809, RT WING (AD). ACCESS PANEL WAS REPAIRED PER ER/A 366767-14MA REV C.

Part: SUPPORT — CORRODED (TE FLAP) · corrosion level 2 · airframe 82,337 hrs · 36,965 cycles

CORROSION ON AFT FAIRING FLAP SUPPORT STA WS 315 AT RT WING INBD MAIN FLAP. LEVEL CORROSION 2, SUPPORT ON FAIRING FLAP WAS REPLACED WHERE ORIG THICKNESS 0.266" REMAINING THICKNESS 0.252" PER SRM 51-40-02 PAR 9 AND B DRAWING 113N2383 REV D.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,337 hrs · 36,965 cycles

CORROSION ON LT STRINGERS LBL2.90 AND LBL10.45 FROM STA 1500 TO 1520 AT AFT CARGO COMPARTMENT. REPAIRED PER SRM 53-00-53 REP 1.

Part: BALLSCREW — CORRODED (TE FLAP) · airframe 82,337 hrs · 36,965 cycles

CORROSION ON BALLSCREW NUT IN INBD FLAP OUTBD BALLSCREW AT RT WING. R&R OUTBOARD BALLSCREW OF INBOARD FLAP AT RT WING. TEST OK.

Part: PLATE — CRACKED (FUSELAGE) · airframe 82,337 hrs · 36,965 cycles

CRACK ON RT SIDE PLATE STA 658 RBL 26 AT FWD CARGO COMPARTMENT. SIDE PANEL RT ON FWD CARGO COMPARTMENT WAS REPLACED PER. SRM 51-40-02 PAR A AND 7 AND SRM 53-00-53 REPAIR 2.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,337 hrs · 36,965 cycles

LEVEL CORROSION II. CORROSION ON STRINGERS FROM STA 1460 TO 1480 RBL-16, RBL-11, RBL-7 AND LBL-16. LEVEL CORROSION 2 STRINGERS FROM STA 1460 TO 1480 RBL-16, RBL-11, RBL-7 AND LBL-16 WERE REPAIRED PER SRM 53-60-53 FIG 1.

Part: BEAM — CRACKED (RT MLG WW) · airframe 82,337 hrs · 36,965 cycles

CRACKED BEAM STA 1070 AND RBL 60 AT RT WHEEL WELL AREA (FYT). REPAIRED PER ER/A 571403-14 REV ORIGINAL.

Part: PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 82,337 hrs · 36,965 cycles

LEVEL CORROSION II. CORROSION ON RT SIDE PANEL FROM STA 1375 TO 1380 AT AFT CARGO COMPARTMENT. RT SIDE PANEL FROM STA 1375 TO 1380 AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 51-40-02 PAR 4 AND 7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,337 hrs · 36,965 cycles

CORROSION ON FLOOR SUPPORT STA 1200 FROM PROJECTION S-23L TO S-27L ALSO S-23R TO S-27R AT AFT CARGO COMPARTMENT (C2). LEVEL CORROSION 2. SUPPORTS WERE REPLACED PER DRAWING 453N1602 REV AT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,337 hrs · 36,965 cycles

INITIAL INSPECTION. CORROSION ON FLOORBEAM UPPER CHORD LWR SURFACE STA 345 LBL 63 AT PAX CABIN FLOOR STRUCTURE. DAMAGE ON BEAM STA 345 LBL 63 LWR SECTION WAS REPAIRED PER ER/A 571242-14 REV ORIGINAL.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,337 hrs · 36,965 cycles

CORROSION ON INTERCOSTAL OF STA 1380 AND S27R AT AFT CARGO COMPARTMENT. (LEVEL CORROSION 2) ANGLE (SHEAR TIE) WAS REPLACED PER DWG 146N5421 REV B AND SRM 51-40-02.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 82,337 hrs · 36,965 cycles

PROTUBERANCE ON PREVIOUS REPAIR ON EXTERNAL FUSELAGE SKIN FROM STA Y=680 TO Y=700 S-28L(FUS). REPAIR DOUBLER WAS REPLACED PER SRM 53-00-01 REP 2.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,337 hrs · 36,965 cycles

CORROSION ON RT PREVIOUS 0REPAIR STRINGERS RBL 7.55 AND 10.45 STA 1510 AT AFT CARGO COMPARTMENT CP53-153-01I (C2). CHANNEL DOUBLER REPAIR ON STRINGERS RBL 7.55 AND 10.45 STA 1510 AT AFT CARGO COMPARTMENT WERE REPLACED PER SRM 53-00-53 REPAIR 1 FIG 201.

Part: FRAME — CRACKED (BS 1560) · airframe 82,337 hrs · 36,965 cycles

CRACKS WERE FOUND INSIDE FOUR BOLT HOLES IN FRAME BS 1560, BETWEEN STRINGERS 22R AND 23R IN THE AFT CARGO BAY. THE HOLES WERE DRILLED TO NEXT OVERSIZE IAW SRM 51-40-05. HEFC WAS ACCOMPLISHED AND NO CRACKS WERE FOUND IAW NDT MANUAL PART 6, 51-00-16.

Part: LIGHT — MISSING (R1 DOOR SLIDE) · airframe 81,892 hrs · 36,775 cycles

R1 DOOR SLIDE ARMED LIGHT MISSING. INSTALLED THE SLIDE LIGHT.

Part: LENS — UNSECURE (CABIN) · airframe 81,694 hrs · 36,700 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS: 3C. SEAT MOUNTED EMERGENCY LIGHT AT 3C IS DAMAGED/ PUSHED IN/ INTERIOR. RESECURED SEAT 3C SEAT MOUNTED EMERGENCY PATH LIGHT LENS AS REQUIRED; OPS CHECK NORMAL.

Part: LENS — DAMAGED (CABIN) · airframe 81,694 hrs · 36,700 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:302. RED EMERGENCY PATH LIGHT ON THE AISLE EDGE OF THE 1R CLOSET IS DAMAGED / INTERIOR. RESECURED RED EMERGENCY PATH LIGHTING LENS AS REQUIRED; OPS CHECK NORMAL.

Part: SWITCH — LOOSE (EMERGENCY LIGHTS) · airframe 79,114 hrs · 35,710 cycles

EMER LIGHTS SWITCH LOOSE. DOES NOT CLOSE TO ARMED POSITION. REMOVED AND REPLACED CONTROL PANEL PER AMM 33-51-08. OPS CKS GOOD.

Part: FLOOR SUPPORT — BROKEN (BS 761-780) · airframe 76,615 hrs · 34,900 cycles

CABIN FLOOR SUPPORT BROKEN BETWEEN BS 760 AND 780 BL 0. COMPLIED WITH ER/A 550643-14 REV. ORIGINAL. FABRICATED AND INSTALLED A NEW FLOOR SUPPORT.

Part: WIRE — EXPOSED (SEAT 32F) · airframe 73,971 hrs · 33,837 cycles

SEAT 32F PASSENGER SEAT WIRING EXPOSED ON FLOOR. SECURED WIRES. EMERGECY LIGHT AT SEAT 32DEF INOPERATIVE. FWD TO MCO +PLACARD IAW MEL 33-51-03A. INSTALLED NEW EMERGENCY LIGHT KIT AT 32DEF OK FOR SERVICE. REMOVED PLACARD AND CLEARED MEL 33-51-03A.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 73,795 hrs · 33,749 cycles

FIRST CLASS SEATS EMERGENCY LIGHTS INOPERATIVE. FOUND WIRING SHORTED TO SEAT FRAME AT SEAT 2CD. SPLICED DAMAGED WIRE. WDM 33-51-16, EMERGENCY LIGHTS FOR FIRST CLASS SEATS TEST GOOD.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 73,710 hrs · 33,721 cycles

FIRST CLASS SEAT EMERGENCY LIGHTS INOPERATIVE. FOUND BAD FUSE IN POWER SUPPLY. REPLACED FUSE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,662 hrs · 33,700 cycles

FOUND F/C SEAT MOUNTED EMERGENCY LIGHTS NOT TESTING. T/S REF WDM 33-51. FOUND EMERGENCY FLOOR LIGHT POWER PACK, M9101, BAD. R & R PWR PACK, M9101 AND BATTERY REF AMM 33-51. OPS CKS GOOD.

Part: GENERATOR — FAILED (RIGHT) · airframe 73,323 hrs · 33,548 cycles

ACFT 680, ON TAKEOFF ROLL, RT GENERATOR FAILED AGAIN ON APPLICATION OF TAKEOFF POWER. REJECTED TAKEOFF AT 10 KNOTS. RETURNED TO GATE. T/S RIGHT IDG. REPLACED IAW LOGPAGE 7191082.

Part: IDG — FAILED (RIGHT) · airframe 73,323 hrs · 33,548 cycles

ACFT 680, ON TAKEOFF ROLL, NR 2 IDG DROPPED OFF LINE. ABORTED TAKEOFF. PERFORMED BITE OF BPCU IAW FIM 24-20-00-810-802. FAULTS RIGHT IDG. REPLACED RT IDG IAW AMM 24-11-01. TESTS GOOD AND NO LEAKS IAW AMM 71-00 AND 24-11.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 72,912 hrs · 33,392 cycles

DURING SERVICE CHECK, FOUND ROWS 19-25 EMERGENCY LIGHTS INOPERATIVE. FOUND LOOSE CONNECTOR AT ROW 22. SECURED THE CONNECTOR IAW AMM 33-51. OPS CHECKED GOOD. OK FOR SERVICE.

Part: WINDOW FRAME — DAMAGED (BS 412) · airframe 70,735 hrs · 32,414 cycles

BS 412 WINDOW FRAME CORNER HAS LIGHTNING STRIKE DAMAGE. REPAIRED IAW ERA 493524-14, REV D.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 70,498 hrs · 32,308 cycles

EMERGENCY EXIT ROW LIGHT INOPERATIVE ROW 5. REINSTALLED PIN ON QUICK DISCONNECT.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 70,005 hrs · 32,102 cycles

EMERGENCY LIGHT AT ROW 1 RT INOPERATIVE. REPAIRED BROKEN WIRE IAW SWPM CH 20-30.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 69,401 hrs · 31,839 cycles

LT AFT FUSELAGE SIDE SKIN LIGHT INOPERATIVE. T/S IAW WDM 33-51-14 FOUND BROKEN WIRE FROM D5526 TO POWER SUPPLY PIN 13 W354-0013-16 REPAIR IAW CHAT 20. OPS CHECKED GOOD.

Part: STRUCTURE — CRACKED (L1 DOOR FRAME) · airframe 69,144 hrs · 31,727 cycles

CRACK IN L1 DOOR SURROUND.

Part: SKIN — CRACKED (L1 DOOR AREA) · airframe 69,102 hrs · 31,709 cycles

WHILE PERFORMING NDT INSPECTION OF L1 DOOR CUTOUT IAW TC 5331-01232-02A, HFEC INSPECTION SHOWED TWO CRACKS IN THE BEARSTRAP LAYER. COMPLIED TC 5331-01232-02G. INSTALLED A DOUBLER AND TRIPLER.

Part: SKIN — DEBONDED (L1 DOOR SURROUND) · airframe 69,102 hrs · 31,709 cycles

SKIN AND BEARSTRAP DISBONDED AT L1 DOOR CUT-OUT. REPAIR IN AREA OF DAMAGE ROUT-OUT. C/W ERA 524559-14AD, REV ORIGINAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,999 hrs · 31,672 cycles

EXTERIOR EMERGENCY DOOR LIGHTS INOPERATIVE. REPLACED LAMPS . OPS CHECKED GOOD.

Part: SIGN — UNKNOWN (CABIN) · airframe 68,934 hrs · 31,644 cycles

R2 DOOR EMERGENCY EXIT SIGN NEEDS REPLACED, REF NR 5613156. REPLACED EXIT SIGN AT 2R DOOR.

Part: SKIN — DAMAGED (NLG DOOR) · airframe 68,323 hrs · 31,373 cycles

DURING WALK AROUND, FOUND LIGHTNING STRIKE DAMAGE TO LT FWD NOSE GEAR DOOR AND AROUND FWD EQUIPMENT DOOR. COMPLETED LIGHTNING STRIKE INSPECTION IAW AMM 05-51-19. REPAIR ACCOMPLISHED ON N/R 4 AND N/R 6 THRU 13.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,779 hrs · 31,138 cycles

SEAT 3CD EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY IAW AMM 33-51. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,208 hrs · 30,123 cycles

NUMEROUS EMERGENCY EXIT SIGN LAMPS INOPERATIVE. REPLACED LAMPS. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (BS 412) · airframe 65,008 hrs · 30,029 cycles

INSPECTED LEFT NR 1 WINDOW PLUG AND FRAME BS 402 AND SURROUNDING AREA . REPAIRED WINDOW FRAME IAW ERA 493524-14, REV C. TIME LIMITED II REPAIR ON NR CARD 5.

Part: FRAME — CORRODED (BS 1480) · airframe 64,792 hrs · 29,942 cycles

CORROSION ON AFT CARGO FRAME AT BS 1480 FWD AND AFT SIDE BETWEEN STR 29 AND 30L. REPAIRED IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1480 S29-30L) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON AFT CARGO BAY SHEAR TIE AT BS 1480 FWD AND AFT SIDE BETWEEN STR 29 AND 30L. R & R SHEAR TIE IAW SRM 51-40-02, PG 7.

Part: SHEAR TIE — CORRODED (BS 1480 S29-30L) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON AFT CARGO BAY SHEAR TIE AT BS 1480 BETWEEN S29 & 30L. R & R SHEAR TIE IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 365 RBL 6) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON MAIN CABIN FLOORBEAM UPPER TEE BS 365, RBL 6. INSTALLED REPAIR IAW SRM 53-00-51.

Part: DECK PLATE — CORRODED (BS 1680-1720) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON MAIN CABIN DECK PLATE SEVERAL AREAS BETWEEN BS 1680 AND 1720, BL 0 TO LBL 58. REPAIRED IAW SRM 53-60-51, PG 201.

Part: SKIN — CORRODED (BS 740-760 S22R) · airframe 64,791 hrs · 29,941 cycles

ON REMOVAL OF NUTPLATE ON FUSELAGE SKIN FOUND INNER SKIN EXFOLIATED BETWEEN BS 740-760 BETWEEN S22R. REPAIRED IAW SRM 53-00-01, REPAIR 3.

Part: CUSP WEB — CORRODED (BS 740-760 S17R) · airframe 64,791 hrs · 29,941 cycles

MAIN CABIN CUSP WEB HAS CORROSION BETWEEN BS 740 AND 760 S17R. REPAIRED IAW SRM 51-40-02, PG 2.

Part: FLOORBEAM — CORRODED (BS 1640 RBL 56) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON MAIN CABIN FLOORBEAM UPPER TEE BS 1640, RBL 56. REPAIRED IAW SRM 53-00-51, REPAIR 3.

Part: FRAME — DENTED (BS 1400 S25-26L) · airframe 64,791 hrs · 29,941 cycles

AFT CARGO FRAME DENTED ON UPPER FLANGE BS 1400 BETWEEN STR 25 AND 26L. REPAIRED IAW SRM53-00-07.

Part: SKIN — DENTED (BS 1706 S15-16L) · airframe 64,791 hrs · 29,941 cycles

LEFT EXTERNAL FUSELAGE SKIN BS 1706 BETWEEN S15-16L DENTED. REPAIRED IAW ERA 507861-14, REV ORIG.

Part: FLOORBEAM — CORRODED (BS 324 RBL 57) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON MAIN FLOORBEAM UPPER TEE BS 324, RBL 57. REPAIRED IAW SRM 53-10-08, REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 345) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON MAIN CABIN FLOORBEAM UPPER TEE BS 345 RBL 2 TO LBL 17. REPAIRED IAW SRM 53-00-51, REPAIR 3.

Part: DECK PLATE — CORRODED (BS 1680-1720) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON MAIN CABIN DECK PLATE SEVERAL PLACES BETWEEN BS 1680 AND 1720 BL 0 TO RBL 58. REPAIRED IAW SRM 53-60-51.

Part: SKATE ANGLE — CORRODED (BS 688-720) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON MAIN CABIN L2 DOOR LOWER SILL SKATE ANGLE BS 688 TO 720. REPLACED ANGLE IAW SRM 51-40-02.

Part: DOUBLER — CORRODED (BS 700-720) · airframe 64,791 hrs · 29,941 cycles

FWD CARGO BAY RT LAVATORY PAN DOUBLER, CORRODED ON TOP SURFACE AS VIEWED FROM BS 700-720. REPAIRED IAW SRM 51- 40-02.

Part: STRUCTURE — CRACKED (NR 2 NACELLE) · airframe 64,791 hrs · 29,941 cycles

NR 2 PYLON UPPER STRUCTURE CRACKED AT STA 137. REPAIRED IAW ER/A 507876-14 REV ORIGINAL

Part: FLOORBEAM — CORRODED (BS 377.7) · airframe 64,791 hrs · 29,941 cycles

MAIN CABIN FLOORBEAM BS 377.7 CORRODED. REPAIRED FLOORBEAM TEE IAW SRM 53-00-51, REPAIR 3.

Part: FRAME — CORRODED (BS 1480 S26R) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON AFT CARGO BAY FRAME AT BS 1480 JUST OTBD OF SIDE PANEL S26R. R & R FRAME IAW SRM 51-40-02, PG 7.

Part: FRAME — CORRODED (BS 1460 S27L-28R) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON AFT CARGO BAY FRAME FWD TOP AND AFT BS 1460, STR 27L-28R. R & R FRAME IAW SRM 51-40-02, PG 7

Part: STRINGER — CORRODED (BS 1412 S29R) · airframe 64,791 hrs · 29,941 cycles

STRINGER 29R BS 1412 HAS CORROSION. R & R STRINGER BS 1406-1460 IAW SRM 51-40-02, PG 7.

Part: SHEAR TIE — CORRODED (BS 1400 S28-29R) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON ONE SHEAR TIE IN AFT CARGO BAY BS 1400 BETWEEN STR 28-29R. REPLACED SHEAR TIE IAW SRM 51-40-02, PG2, PARA 4B.

Part: KEELBEAM — CORRODED (BS 1406) · airframe 64,791 hrs · 29,941 cycles

KEEL BEAM RT SIDE AT BS 1406 CORRODED. REPAIRED IAW ER/A 507673-14, REV ORIGINAL.

Part: FRAME — DENTED (BS 1500 S26-27L) · airframe 64,791 hrs · 29,941 cycles

DENT ON FRAME BS 1500 BETWEEN S26-27L. INSTALLED FRAME REPAIR IAW SRM 53-00-07, REPAIR 5, FIG 201.

Part: FRAME — CORRODED (BS 1480 S11R) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON AFT CARGO BAY FRAME BS 1480 S11R. R & R FRAME BETWEEN STR 24L-24R IAW SRM 51-40-02, PG 7.

Part: SHEAR TIE — CORRODED (BS 1480) · airframe 64,791 hrs · 29,941 cycles

CORROSION ON AFT CARGO BAY SHEAR TIE AT BS 1480 BETWEEN STR 29 - 30L. R & R SHEAR TIE IAW SRM 51-40-02.

Part: DRAG BRACE — DAMAGED (NR 1 PYLON) · airframe 64,791 hrs · 29,941 cycles

PERMANENT REPAIR NR 1 PYLON DIAGONAL DRAG BRACE FITTING. ACCOMPLISHED ERA 363122-14AD REC C PERMANENT REPAIR ON NRC 207536.

Part: LIGHT — INOPERATIVE (SEAT 34D) · airframe 64,414 hrs · 29,764 cycles

MAINTENANCE DISCOVERED SEAT 34D EMERGENCY PATH LIGHT INOPERATIVE. REPLACED LIGHT ASSY, OPS CHECKED OK.

Part: SKIN — DAMAGED (FWD FUSELAGE) · airframe 64,023 hrs · 29,599 cycles

MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION AND DISCOVERED SIX DAMAGE AREAS FWD OF THE NOSE W/W DOOR RT SIDE BELOW RADOME. REPAIRED LIGHTNING STRIKE DAMAGE SIX PLACES FWD OF NOSE W/W DOOR RT SIDE BELOW RADOME PER SRM 53-00-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,179 hrs · 28,398 cycles

AIRCRAFT WAS DAMAGED BY JET WAY RAMMING INTO THE SIDE OF FUSELAGE AT STA 600-640 STR 15 TO STR 19.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,797 hrs · 28,264 cycles

FASTENER AND SKIN DAMAGED FROM LIGHTNING STRIKE AT WINDOW FRAME UPPER AFT CORNER STA 412. REPAIRED ON NRC 198 PER ER/A 493524-14 REV ORIG.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 60,678 hrs · 28,207 cycles

DURING FLIGHT, CREW NOTICED SMOKE COMING FROM COFFEEMAKER IN THE G2D GALLEY. APPLICABLE CIRCUIT BREAKERS WERE PULLED AND THE SMOKE STOPPED. MAINTENANCE REPLACED THE COFFEEMAKER. WIRE HARNESS INSPECTION SHOWED NO EVIDENCE OF BURNT WIRES. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 58,421 hrs · 27,154 cycles

DURING LAYOVER CHECK, MX FOUND THE ROW 29 & 30 EMERGENCY PATH LIGHTS INOPERATIVE. MX REPAIRED THE WIRING AT EACH LIGHT. OPS CHECK WAS GOOD.

Part: HINGE — LOOSE (L2 DOOR) · airframe 54,465 hrs · 25,164 cycles

AIRCRAFT COULD NOT PRESSURIZE. FOUND L2 DOOR LOWER HINGE SERATED PLATE LOOSE. TIGHTENED SAME DOOR, OPS CHECKS OK. PRESSURIZED ACFT NO LEAKS NOTED.

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 51,360 hrs · 23,655 cycles

CAPT SEAT LOOSE DURING FLIGHT. FOUND AFT LEFT SEAT TRACK STOP FITTING CRACKED REPLACED SEAT TRACK.

Part: SKIN — GOUGED (BS 1338-1362) · airframe 46,825 hrs · 21,729 cycles

THE FUSELAGE SKIN HAS A GOUGE WHERE THE SKY RADIO ANTENNA WAS PREVIOUSLY INSTALLED AT STA 1338-1362 AND S1-2L. THE DAMAGED FUSELAGE SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED.

Part: RESTRAINT — CORRODED (GIRT BAR PLATE) · corrosion level 2 · airframe 46,821 hrs · 21,727 cycles

GIRT BAR RESTRAINT PLATE FOUND CORRODED BEYOND LIMITS, LEVEL 2. REPLACED RESTRAINT PLATE AND DOOR SLIDE/RAFT PER JIC 7809-2.

Part: STATIC INVERTER — FAILED · airframe 43,070 hrs · 20,385 cycles

STATUS MESSAGE STBY INVERTER, INV POWER TRU BREAKER POPPED ONP6 PANEL. ELECTRICAL BURNING ODOR IN CABIN AND COCKPIT. REPLACED STATIC INVERTER PER AMM. OPS CK OK. CONFIRMED STATIC INVERTER CAUSED SMELL IN CABIN.

Part: TRANSMITTER — MALFUNCTIONED (RT TE FLAPS) · airframe 36,064 hrs · 17,674 cycles

UPON SELECTING FLAPS 1 DEG T/E FLAP ASYM MESSAGE AND AMBER TRAILING EDGE LIGHT, FOLLOWED PROCEDURE AND LANDED WITH L/E AND 1/2 DEG FLAPS. TROUBLESHOT PER FIM FOUND RT POSITION TRANSMITTER 20 DEG OUT OF LIMITS. POSITIONED TRANSMITTER TO CORRECT VALUE PER M/M, CYCLED FLAPS TO FULL DOWN 30 DEG SEVERAL TIMES, NO FAULTS. OPS CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (E/E BAY) · airframe 27,949 hrs · 13,804 cycles

ON TAKEOFF A/C FELT VERY NOSE HEAVY REQUIRING EXCESSIVE AND UNUSUAL STICK FORCE TO ROTATE TRIM CORRECTLY SET AT 3.6 25.9 PERCENT MAC WEIGHT 187.4. DIVERT TO DFW. REPLACED ELEVATOR FEEL COMPUTER. CHECKS GOOD PER M/M 27-31-19-4.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 26,434 hrs · 13,077 cycles

ON LAYOVER INSP FOUND FC EMERGENCY TRACK LIGHTS INOP. REPLACED BATTERY PACK, SYS OPS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON LAYOVER, FOUND EMERGENCY LIGHTS AT 4C, 5C AND C-2 CARGO DOOR INOP. REPLACED TEE-OFF HARNESS ON 4C AND LAMP ASSEMBLY ON 5C OPS CHECK GOOD. REPLACED BATTERY PACK AND CHARGER (M736). ALL EMERGENCY LIGHTS CHECK GOOD IAW MM.

Part: PWR SUPPLY — INOPERATIVE (CARGO COMPT)

ON L/O, FOUND EMERGENCY LIGHTS AT 4C, 5C AND C-2 CARGO DOOR INOP. REPLACED TEE-OFF HARNESS ON 4C AND LAMP ASSEMBLY ON 5C OPS CHECK GOOD. REPLACED BATTERY PACK AND CHARGER (M736). ALL EMERGENCY LIGHTS CHECK LIGHTS CHECK GOOD IAW MM.

Part: COFFEEMAKER — FAILED (CABIN)

MID CABIN F/A'S AND PAX REPORTED A SMELL IN MID CABIN. ODOR REPORTED TO BE AN ELECTRICAL TYPE ODOR. CKD ALL LIGHT BALLASTS FOR OVRHT, CKD OPN OF ALL OVENS, CKD ALL OTHER GALLEY APPLIANCES. EVERYTHING OK FOR SERVICE. REPLACED TWO MID GALLEY COFFEEMAKERS DUE TO BURNT COFFEE SMELL.

Part: ACTUATOR — MALFUNCTIONED (NLG)

A/C EXPERIENCED NOSE GEAR DISAGREE UPON APPROACH. CREW CYCLED GEAR SEVERAL TIMES TO NO AVAIL. ALTERNATE GEAR EXTENSION OPERATED NORMALLY. A/C LANDED WITHOUT INCIDENT. A/C WAS JACKED AND FOUND THAT UPON EXTENSION NOSE GEAR DOORS OPENED BUT GEAR REMAINED IN WELL. FOUND NOSE LOCK ACTUATOR BAD. REPLACED SAME AND CYCLED NOSE GEAR THROUGH SEVERAL CYCLES. OPERATIONAL CHECK NORMAL PER M/M 32-34-02-04 AND FIM 32-30-00.

Part: INLET DOOR — LOCKED CLOSED (APU)

APU QUIT IN FLIGHT, COULD NOT RESTART DUE TO INLET DOOR FAULT LEFT ENGINE GENERATOR ON MCO. ELP LOCKED INLET DOOR OPEN PER MEL 49-15-01B.

Part: GROUND STUD — DAMAGED (APU BATTERY)

AFT CBN FILLED WITH SMOKE UPON LANDING AFTER F/A TURNED ON OVHD LIGHTS. FOUND GROUND STUDS FOR APU START BAT TO SHOW HEAT DAMAGE. CLEANED AREA AND SECURED STUDS AND RECONNECTED WIRING. DEACT APU, ATL TO ROUTE A/C FOR EO 6-66173 APU GROUND STUD WIRING MOD.

Part: SLIDE BOTTLE — FAILED (LT SLIDE)

LEFT OVERWING SLIDE BOTTLE WOULD NOT TEST. DISARMED/REARMED LEFT OFFWING ESCAPE SYSTEM PER MM 25-65-00. VISUALLY VERIFIED ROUND CRANK HANDLE IN LOCKING POSITION AND VENT HANDLE IN THE OPERATE POSITION. ALSO, VERIFIED PRESSURE BOTTLE SAFETY PIN AND CAPS REMOVED. PRESSURE AND SQUIB TEST OPERATION NORMAL.

Part: WINDSHIELD — FAILED (LT FLT DECK)

COPILOT WINDSHIELD OUTER PANE SHATTERED, CLIMBING THROUGH 10,000 FT. FLIGHT RETURNED JFK. REPLACED WINDSHIELD.