N905DA

Part: BOTTLE — EMPTY (DOOR SLIDE) · airframe 59,973 hrs · 32,694 cycles

AFT DOOR SLIDE DECAL ABOVE DOOR PUNCTURED AND NITROGEN BOTTLE DEPLETED. SERVICED BOTTLE AND INSPECTED TAILCONE RELEASE SYSTEM. TAILCONE EGRESS SYSTEM CHECKS OK. (LP# 3019259)

Part: ACCUMULATOR — LEAKING (RT ELEVATOR) · airframe 59,576 hrs · 32,439 cycles

DURING TAXI IN, AFTER STARTING THE APU AND TURNING ON APU AIR. THE CABIN FILLED WITH A THIN HAZE AND A SLIGHT BURNING ODOR WHEN AWAY WHEN APU AIR WAS REMOVED. PULLED AND COLLARED APU CIRCUIT BREAKERS. FOUND RT ELEVATOR ACCUMULATOR LEAKING IN TAIL COMPARTMENT. R & R THE RT ELEVATOR ACCUMULATOR IAW AMM 27-33-04. OPS OK, NO LEAKS.

Part: UNKNOWN — ODOR (CABIN) · airframe 58,608 hrs · 31,870 cycles

CREW REPORTED A BURNING ODOR NEAR ROW 16DEF AT 15,000FT. MAINTENANCE TROUBLESHOT. NO TROUBLE FOUND. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 58,511 hrs · 31,817 cycles

R1 DOOR SLIDE PACK NOT PINNED. REPLACED DOOR SLIDE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,378 hrs · 31,733 cycles

EMERGENCY FLOOR LIGHTNING DAMAGED OR INOPERATIVE. FOUND STRIP AND REATTACHED.

Part: CYLINDER — LOW PRESSURE (TAILCONE) · airframe 58,214 hrs · 31,636 cycles

TAIL CONE NITROGEN CYLINDER LOW. SERVICED.

Part: LIGHT — MISSING (ROW 26) · airframe 57,959 hrs · 31,512 cycles

FOUND THE EMERGENCY LIGHT MISSING AT ROW 26. REPLACED THE LIGHT IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,959 hrs · 31,512 cycles

SEVERAL EMERGENCY LIGHTS ON CAT WALK INOPERATIVE. REPLACED THE LAMPS IAW MM. OPS CHECKED OK.

Part: WINDOW — ARCED (COCKPIT) · airframe 57,662 hrs · 31,344 cycles

SIGNIFICANT ELECTRICAL SPARKS COMING FROM UPPER LEFT SIDE OF CAPTAIN SIDE FRONT WINDOW. STOPPED WORKING. CONFIRMED ARCING. COMPLIED WITH REPETITIVE INSPECTION OF ERA 554759-14, REV O.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,940 hrs · 30,945 cycles

MID CABIN CEILING EMERGENCY EXIT LENS COVER MISSING. REINSTALLED THE LENS.

Part: LIGHT — DETACHED (CABIN) · airframe 56,940 hrs · 30,945 cycles

EMERGENCY LIGHT STRIP DETACHED. ATTACHED THE LIGHT.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 56,926 hrs · 30,939 cycles

CRACK INDICATION FOUND FORWARD OF BARREL NUT HOLE, RIGHT UPPER AFT SKIN. COMPLIED WITH EAR 551219-14AD, SECTION 1.

Part: SKIN — DAMAGED · airframe 56,900 hrs · 30,928 cycles

FOUND SURFACE DAMAGE OF THE FUSELAGE SKIN IN THE AREA COMMON TO THEE ATG4 ANTENNA. COMPLIED WITH ERA 551318-00.

Part: BAYONET — WORN (TAILCONE) · airframe 56,812 hrs · 30,863 cycles

DURING A TAILCONE EMERGENCY RELEASE FUNCTIONAL CHECK, FOUND THE BAYONETS WORN. REMOVED AND REPLACED.

Part: LIGHT — UNSECURE (CABIN) · airframe 56,682 hrs · 30,787 cycles

TWO FOOT SECTION OF EMERGENCY EXIT FLOOR LIGHT STRIP NO LONGER ATTACHED. REPLACED.

Part: ROLLER — MISSING (MLG DOOR) · airframe 55,993 hrs · 30,388 cycles

DIVERTED DUE TO LT MLG RED UNSAFE INDICATION. THE ACFT DIVERTED DUE TO INADEQUATE FUEL LOAD CONTINUED WITH GEAR DOWN. MAINTENANCE FOUND LT MAIN GEAR DOOR UPLOCK MISSING BOLT AND ROLLER ASSY. R & R LT AND RT MAIN LANDING GEAR DOORS AND DOOR ACTUATORS TO PREPARE ACFT FOR FERRY FLIGHT. MAINTENANCE INSTALLED NEW LT MAIN UPLOCK BOLTS AND ROLLER. ADJUSTED LEFT AND RT DOOR LATCH MECHANISMS. REINSTALLED DOORS AND ACTUATORS. OPS AND INDICATION CHECKS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 55,949 hrs · 30,361 cycles

AT FL 270, PASSENGERS IN FIRST CLASS AND F/A REPORTED AN ELECTRICAL ODOR, MOSTLY IN FIRST CLASS. TROUBLESHOT WITH NO TROUBLE FOUND. PERFORMED DUCT BURNOUT. PERFORMED VERIFICATION FLIGHT.

Part: SUPPORT — CRACKED (JACKSCREW) · airframe 55,185 hrs · 29,904 cycles

JACKSCREW GIMBALL SUPPORT STRUCTURE 49 CHANNEL CRACKED. REPAIRED IAW PRI/ERA 544045-14, REV O.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,837 hrs · 29,704 cycles

EMERGENCY LIGHT SWITCH WON'T TURN ON LIGHTS. R & R OVERWING EMERGENCY BATTERY PACKS. OPS CHECKS OK.

Part: CUSP WEB — CRACKED (BS 962) · airframe 53,599 hrs · 28,934 cycles

CUSP MEMBRANE CRACKED, BS 962, L18R. REPAIRED IAW SRM 53-20-02.

Part: SKIN — CRACKED (BS 1542) · airframe 53,594 hrs · 28,931 cycles

SKIN CRACKED AT BS 1542, LT SIDE JUST OTBD OF AIRSTAIR CUTOUT. REPAIRED IAW SRM 53-00-01, FIG 6.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,309 hrs · 28,150 cycles

LAST 2 OVERHEAD EMERGENCY LIGHTS AND 1 AFT ACCESSORY WALKWAY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND REPLACED THE LAMP IAW MM.

Part: STRAP — FRAYED (TAILCONE SLIDE) · airframe 51,544 hrs · 27,628 cycles

TAILCONE RT SIDE SLIDE DEPLOY D-RING STRAP FRAYED. R & R RT TAILCONE DEPLOY D RING STRAP.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 50,310 hrs · 26,852 cycles

PERFORMED AIR TURN BACK DUE TO NR 2 ENGINE COMPRESSOR STALLS ABOVE IDLE DURING CLIMBOUT. EMERGENCY WAS DECLARED. BOROSCOPED ENGINE. R & R SEVERAL PARTS. ENGINE STILL STALLING. R & R NR 2 ENGINE.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 50,006 hrs · 26,671 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND L1 EMERGENCY LIGHT INOPERATIVE. FOUND WIRE BAD FROM S3-558 TO P1-2301. R & R B5-235 POWER PACK BATTERY. OPERATION CHECKED GOOD.

Part: TARGET — BROKEN (MLG DOOR) · airframe 48,551 hrs · 25,787 cycles

ON LANDING, DECLARED EMERGENCY DUE TO GEAR DOOR OPEN LIGHT WITH THREE GEAR GREEN DOWN & LOCKED MANUAL GEAR EXTENSION. COULD NOT DETERMINE WHICH DOOR WAS CAUSE OF MALFUNCTION. LANDED WITH GEAR DOORS DOWN. MX FOUND RIGHT MLG TARGET BROKEN. R & R RT MLG TARGET IAW MM. OPS CHECKS OK.

Part: SKIN — PUNCTURED (BS 1192) · airframe 58,735 hrs · 31,947 cycles

HOLE IN FUSELAGE SKIN BS 1192, STRINGER 26L. REPAIRED IAW SRM 53-30-03.

Part: SKIN — CORRODED (BS 1364) · airframe 48,551 hrs · 25,787 cycles

AFT CARGO COMPARTMENT, BS 1364+9, LONGERON 25L, FUSELAGE SKIN IS CORRODED. COMPLIED WITH PRI 516032-14, REV ORIGINAL AND ERA 516032-14, REV O.

Part: INTERCOSTAL — CORRODED (BS 1379-1395) · airframe 48,551 hrs · 25,787 cycles

AFT CARGO COMPARTMENT, BS 1395 - 1379, AFT LONGERON 22L, INTERCOSTAL HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R ANGLE IAW SRM 51-30-02 AND 51-70-01.

Part: LONGERON — CORRODED (BS 1364) · airframe 48,542 hrs · 25,782 cycles

AFT CARGO COMPARTMENT LONGERON 25L, BS 1364, CORRODED. R & R LONGERON IAW ERA 516024-14.

Part: FLOOR SUPPORT — CORRODED (BS 773) · airframe 48,542 hrs · 25,782 cycles

AFT CARGO COMPARTMENT BS 773 FLOOR SUPPORT SPLICE STRAP HAS UPPER SURFACE CORROSION ON SEVERAL AREAS. TASK 53-260. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPLACED NEW SPLICE STRAP IAW SRM 53-00-53, 51-20-01 PG 14 AND 17.

Part: SKIN — WORN (NR 1 PYLON) · airframe 48,542 hrs · 25,782 cycles

NR 1 PYLON, FORWARD LOWER SURFACE, SKIN IS WORN ON OTBD SIDE. REPAIRED NR 1 PYLON, FORWARD LOWER SURFACE SKIN IAW ERA, PRI 514901-14, REV O, REV 1, REV 2.

Part: SKIN — WORN (NR 1 PYLON) · airframe 48,542 hrs · 25,782 cycles

WEAR FOUND ON THE LOWER SKIN OF THE NR 1 PYLON. PERMANENT REPAIR ACCOMPLISHED.

Part: STRAP — CORRODED (BS 1364-1379) · airframe 48,542 hrs · 25,782 cycles

AFT CARGO COMPARTMENT LEFT SIDE BS 1364 TO 1379, LONGERON 23L, STRAP IN CHANNEL CORRODED ABOVE LAVATORY DRAIN HSG. TASK 53-302-07. REMOVED STRAP. CORROSION FOUND TO BE OUT LIMITS. FABRICATED, DRILLED, ALODINED, PRIMED AND INSTALLED STRAP IAW SRM 51-30-05, 51-10-05, 53-00-01, AND 51-10-03.

Part: SKIN — CORRODED (BS 956) · airframe 48,542 hrs · 25,782 cycles

WING CENTER SECTION, UPPER SKIN, BS 956, LBL 42-60 HAS SEVERAL AREAS OF CORROSION THAT EXTEND UNDER CHORD COMMON TO FUSELAGE SKIN. REPAIRED IAW ERA 516023-14, REV O.

Part: SKIN — CORRODED (BS 954) · airframe 48,542 hrs · 25,782 cycles

WING CENTER SECTION, UPPER SKIN, UPPER SURFACE STATION 954, XCW 42-60 (LBL) BOTH SKINS FORWARD AND AFT OF BUTT JOINT ARE CORRODED. CORROSION EXTENDS UNDER CHORD COMMON TO FUSELAGE SKIN.

Part: SHEAR TIE — CORRODED (BS 1277) · airframe 48,542 hrs · 25,782 cycles

AFT CARGO COMPARTMENT, STA 1277, RBL 1-3 SHEAR TIE IS CORRODED. R & R INTERCOSTAL AT STA 1277, L30 IAW SRM 51-30-05.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 48,542 hrs · 25,782 cycles

F/O OTBD SEAT TRACK CORRODED ON OTBD SIDE. R & R F/O SEAT TRACK.

Part: FRAME — CORRODED (BS 1364) · airframe 48,551 hrs · 25,787 cycles

AFT CARGO COMPARTMENT LT SIDE, BS 1364, LONGERON 23L - 25L, FRAME CORRODED ON AFT SIDE. TASK 53-302-07. R & R FRAME IAW SRM 53-10-02, 51-30-02 AND 51-30-05.

Part: ANGLE — WORN (VERTICAL STAB) · airframe 48,542 hrs · 25,782 cycles

VERTICAL STABILIZER PANEL 350AB HAS AREA OF WEAR, A CRACK ON ANGLE AFT OF SEAL. REMOVED DAMAGE, FABRICATED REPAIR ANGLE, ALODINED, PRIMED AND INSTALLED IAW SRM 55-00-01, 51-70-01, 51-30-02 AND DWG 5912176, PG 4.

Part: CUSP WEB — CORRODED (BS 1214-1219) · airframe 48,542 hrs · 25,782 cycles

PASSENGER CABIN CUSP WEB, STA 1214-1219, RBL 57-59 HAS CORROSION. TASK 53-211-02. INSTALLED WEB REPAIR IAW SRM 53-20-02.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 48,542 hrs · 25,782 cycles

LEFT WING INBD FLAP LOWER SURFACE DENTED 13.5" FWD OF T/E AND 13" FROM INBD EDGE. REPAIRED IAW ERA 516035-14, REV O, LT WING INBD FLAP LOWER SKIN DENT AND GOUGE AND PRI 516035-14, REV O.

Part: SKIN — CORRODED (BS 1364-1379) · airframe 48,542 hrs · 25,782 cycles

CORROSION FOUND ON SKIN BS 1364-1379 L25L UNDER AFT LAVATORY SERVICE PAN. WORK PERFORMED IAW ERA 516032-14 REV O.

Part: CUSP WEB — CORRODED (BS 1214-1219) · airframe 48,542 hrs · 25,782 cycles

PASSENGER CABIN CUSP WEB, STA 1214-1219, RBL 57 - 59 HAS CORROSION. INSTALLED WEB REPAIR IAW SRM 53-20-02.

Part: SKIN — CORRODED (BS 955) · airframe 48,542 hrs · 25,782 cycles

SECTION I OF ERA 516023-14 ISSUED TO REPAIR CORROSION ON CENTER WING SECTION UPPER SKIN AT BS 955 BETWEEN LBL 42 & 60. ACCOMPLISH SECTION II REPETITIVE INSPECTION EVERY 24 MONTHS STARTING 02JUL13.

Part: CASTING — GOUGED (FUSELAGE) · airframe 48,542 hrs · 25,782 cycles

ELEVATOR AND TAB MECHANISM INSTALLATION, BS 1160, RBL6, 5" BELOW FLOOR LEVEL, CASTING IS GOUGED. REPAIRED IAW PRI ERA 51603-14, REV O AND FINAL ERA 516031-14.

Part: BELLCRANK — GOUGED (ELEVATOR) · airframe 48,542 hrs · 25,782 cycles

ELEVATOR BELLCRANK ARM IS GOUGED, BS 1165, RBL 12, THREE INCHES BELOW FLOOR LEVEL. REPAIRED BELLCRANK IAW PRI ERA 516029-14, REV O AND FINAL ERA 516031-14, REV O.

Part: STRUCTURE — BENT (CARGO DOOR) · airframe 48,542 hrs · 25,782 cycles

AFT CARGO DOOR LOWER INBD EDGE IS BENT BS 1225-1260. STRAIGHTEND EDGE IAW SRM 52-01-01, PARA 8C, ERA 516038-14 REV O.

Part: MECHANISM — GOUGED (STAB TAB) · airframe 48,542 hrs · 25,782 cycles

RIGHT HORIZONTAL STABILIZER L/E FLOAT TAB MECHANISM GOUGED. REPAIRED IAW ERA 514984-14, REV O AND FINAL ERA 514894-14, REV O.

Part: PULLEY BRACKET — WORN (HORIZONTAL STAB) · airframe 48,542 hrs · 25,782 cycles

RIGHT HORIZONTAL STABILIZER ANTI-FLOAT TAB PULLEY BRACKET WORN. REPAIRED IAW PRI ERA 514894-14, REV O AND ERA 514894-14, REV O.

Part: SUPPORT FITTING — DAMAGED (RT MLG ACTUATOR) · airframe 48,542 hrs · 25,782 cycles

RIGHT MLG RETRACT ACTUATOR SUPPORT FITTING BORE IS OVER 1.5260 REWORK LIMIT IAW 5740-01140-0201. REPAIRED IAW PRI ERA 514907-14AD, REV O.

Part: SUPPORT FITTING — OUT OF LIMITS (RT MLG) · airframe 48,542 hrs · 25,782 cycles

RIGHT MLG RETRACT ACTUATOR SUPPORT FITTING INBD BORE IS OVER 2.2755 RE-WORK LIMIT IAW 5740-01140-0201. REPAIRED RT MLG BUSHING IAW PRI ERA 51490-14AD, REV O AND FINAL ERA 514904-14AD, REV O.

Part: DOOR FRAME — CORRODED (E/E BAY DOOR) · airframe 48,542 hrs · 25,782 cycles

E & E COMPARTMENT INTERIOR DOOR FRAME LONGERON 28R LIGHTENING HOLE HAS CORROSION. REPAIRED CUTOUT IAW ER/A 516026-14, REV O.

Part: BRACKET — GOUGED (HORIZONTAL STAB) · airframe 48,542 hrs · 25,782 cycles

LEFT HORIZONTAL STABILIZER FLOAT TAB BRACKET GOUGED. REPAIRED IAW ERA 514894-14, REV O.

Part: ATTACH BRACKET — CORRODED (DOOR FRAME) · airframe 48,542 hrs · 25,782 cycles

AFT CARGO BAY DOOR FRAME BS 1269, HAS CORROSION ON FORWARD SIDE OF LOWER CORNER ABOVE THERSHOLD PLATE ATTACH BRAKET. TASK 53-123-02. REMOVED CORROSION FROM CORNER ATTACH BRACKET. FOUND TO BE OUT OF LIMITS. INSTALLED NEW BRACKET IAW SRM 51-30-02 AND 51-30-05. (LP# 0965251)

Part: SKIN — CORRODED (BS 830) · corrosion level 2 · airframe 48,542 hrs · 25,782 cycles

RT SIDE FORWARD WING TO BODY, UNDER THE FAIRING LOWER AREA ON FUSELAGE SKIN STA 830, CORROSION AROUND FASTENER HOLE. CUTOUT DAMAGED AREA AND INSTALLED DOUBLER AND TRIPLER IAW SRN 53-30-01.

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 48,542 hrs · 25,782 cycles

CABIN FORWARD WET AREA FLOOR STRUCTURE LT SIDE BS 200 LBL 57, FLOOR SUPPORT CORRODED. TASK 53-211-01. BLENDED ANGLES BEYOND LIMITS. R & R FLOOR SUPPORT IAW SRM 51-30-02, 51-30-05, 51-30-08 AND DWG 9910078.

Part: FLOOR SUPPORT — CORRODED (BS 1364) · airframe 48,542 hrs · 25,782 cycles

AFT LAVATORY AREA BS 1364 RBL 15 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT IAW SRM 51-30-05.

Part: FRAME — CRACKED (BS 480) · airframe 48,542 hrs · 25,782 cycles

PASSENGER CABIN BS 480 BETWEEN STR 8 AND 9 RIGHT FRAME CRACKED. REPAIRED FRAME IAW ERA 516030-14AD, REV O.

Part: FRAME — CRACKED (BS 440) · airframe 48,542 hrs · 25,782 cycles

PASSENGER CABIN BS 440 FRAME BETWEEN STR 8 AND 9L CRACKED. REPAIRED FRAME IAW ERA 516030-14AD, REV O.

Part: FRAME — CRACKED (BS 480) · airframe 48,542 hrs · 25,782 cycles

PASS CABIN BS 480 BETWEEN STR 8 AND 9L FRAME CRACKED. REPAIRED FRAME IAW PRI ERA 516030-14AD, REV O.

Part: FRAME — CRACKED (BS 440) · airframe 48,542 hrs · 25,782 cycles

PASSENGER CABIN BS 440 BETWEEN S8 AND 9R FRAME CRACKED. REPAIRED FRAME IAW ERA 516030-14AD, REV O.

Part: STRAP — CORRODED (BS 160-200) · airframe 48,542 hrs · 25,782 cycles

PASSENGER CABIN FWD WET AREA FLOOR STRUCTURE RT SIDE BS 160 -200 RBL 54 THRESHOLD STRAP CORRODED. TASK NR 53-211-01. R & R OUT OF LIMITS STRAP AND FILLER AT R1 DOOR FLOOR IAW SRM 53-00-01 AND DWG 9957828.

Part: INTERCOSTAL — DAMAGED (BS 1344-1364) · airframe 48,542 hrs · 25,782 cycles

MAIN CABIN INTERCOSTAL FROM BS 1344-1364, BL 0 CRACKED ON THE TOP FLANGE. R & R DAMAGED INTERCOSTAL IAW SRM 51-70-01, PG 2.

Part: CUSP WEB — CORRODED (BS 1231-1250) · airframe 48,542 hrs · 25,782 cycles

PASSENGER CABIN, LT CUSP WEB, BS 1231-1250 HAS CORROSION AROUND LIGHTNING HOLE TASK 53-211-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED CUSP WEB IAW SRM 53-20-02.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · airframe 48,542 hrs · 25,782 cycles

AFT CARGO COMPARTMENT DOOR FRAME LOWER BEAM HAS CORROSION AROUND RIV NUTS ON INTERIOR INBD SIDE BS 1250 - 1269. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-60-02.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 48,542 hrs · 25,782 cycles

LOWER DOOR FRAME FORWARD FACE HAS CORROSION. REMOVED CORROSION, TREATED AREA, FILLED VOIDS, APPLIED CIC. INSTALLED IAW SRM 51-30-02 AND ERA 516025-14.

Part: FLOOR SUPPORT — CORRODED (BS 1364-1395) · airframe 48,542 hrs · 25,782 cycles

AFT WET AREA RBL 17, BS 1364 - 1395, FLOOR CHANNEL HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED, TREATED, AND PRIMED FLOOR CHANNEL IAW SRM 53-00-01, 51-30-02 AND 51-30-01.

Part: ATTACH ANGLE — CRACKED (BS 1475) · airframe 48,542 hrs · 25,782 cycles

VENTRAL STAIRWAY AREA, STA 1475, FRAME, AFT SIDE LONGERON 2L TO FRAME ATTACH ANGLE CRACKED IN RADIUS. REMOVED AND REPLACED FRAME ATTACH ANGLE IAW SRM 51-30-05.

Part: CHANNEL — DAMAGED (BS 1269) · airframe 48,542 hrs · 25,782 cycles

AFT CARGO COMPARTMENT, BS 1269, LONGERON 29R DRILL START ON TEE CAP. BLENDED DAMAGE, FOUND TO BE OUT OF LIMIT. REMOVED FASTENER, REMOVED ANGLE. INSTALLED SUPPORT CHANNEL IAW SRM 51-30-05M 53-00-01, 51-10-03.

Part: SEAT TRACK — CORRODED (BS 1288-1294) · airframe 48,542 hrs · 25,782 cycles

LEFT OTBD SEAT TRACK, LBL 54, BS 1288 -1294, HAS AREA OF CORROSION ON SEAT TRACK. TASK 53-211-02. REMOVED, FABRICATED NEW AND REPLACED SEAT TRACK IAW SRM 53-20-01, FIG 8, 51-10-05 AND 51-30-02.

Part: SEAT TRACK — GOUGED (BS 522) · airframe 48,542 hrs · 25,782 cycles

LEFT OTBD SEAT TRACK CROWN GOUGED BS 522. R & R OUT OF LIMITS SEAT TRACK SECTION IAW SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 718) · airframe 48,542 hrs · 25,782 cycles

LEFT OTBD SEAT TRACK, LBL 54, BS 718, HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 53-40-01, FIG 6.

Part: SEAT TRACK — CORRODED (BS 794-800) · airframe 48,542 hrs · 25,782 cycles

LEFT OTBD SEAT TRACK LBL 54, BS 794 - 800 HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK BS 589 - 855.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 48,542 hrs · 25,782 cycles

PASSENGER CABIN FLOOR PANEL 222AMG HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR IAW SRM 53-00-01, PG 12.

Part: SEAT TRACK — CORRODED (BS 718) · airframe 48,542 hrs · 25,782 cycles

LEFT OTBD SEAT TRACK, LBL 54, BS 718 CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK BS 589-855 IAW SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 517-523) · airframe 48,542 hrs · 25,782 cycles

RIGHT OTBD SEAT TRACK CROWN, BS 517-523, IS CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 1177-1195) · airframe 48,542 hrs · 25,782 cycles

LEFT OTBD SEAT TRACK, BS 1177 -1195, LBL 54, HAS SEVERAL AREAS OF CORROSION. REPLACE SEAT TRACK IAW SRM 51-30-01.

Part: ANGLE — CRACKED (BS 1460) · airframe 48,542 hrs · 25,782 cycles

TAIL COMPARTMENT CEILING/SIDEWALL SUPPORT FRAME ANGLE CRACKED BS 1460, RBL11. REMOVED SUPPORT FRAME ANGLE AND DRILLED TO FIT NEW ANGLE IAW 51-30-05 AND 51-30-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 48,542 hrs · 25,782 cycles

L2 DOOR THRESHOLD, FORWARD GIRT BAR FITTING SUPPORT ANGLE HAS CORROSION, TASK 53-211-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED, LOCATED AND MATCH DRILLED NEW FITTING AND INSTALLED IAW SRM 51-30-05.

Part: BULKHEAD — CRACKED (BS 522) · airframe 48,542 hrs · 25,782 cycles

FORWARD CARGO BAY AFT BULKHEAD AT BS 522 LONGERON 28L AND 28R CRACKED AND BENT. WORK PERFORMED ON WO 27302/1000/0060, NR 2023138, 362NC.

Part: CUSP WEB — CORRODED (FWD CABIN) · airframe 48,542 hrs · 25,782 cycles

FORWARD CABIN RT CUSP WEB CORRODED AT STA 648, TASK 53-211-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-02, FIG 18, 51-10-03 AND 53-00-01.

Part: FITTING — CORRODED (BS 1395) · airframe 48,542 hrs · 25,782 cycles

AFT CARGO BS 1395, LONGERON SPLICE FITTING 29L HAS CORROSION INSIDE FITTING. LOCATED FORWARD OF STA 1395. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. DRILLED, PAINTED AND INSTALLED NEW FITTING IAW SRM 51-30-05.

Part: ANGLE — CRACKED (CABIN) · airframe 48,542 hrs · 25,782 cycles

PASSENGER CABIN, SMALL PANEL OTBD OF EPC PANEL LOWER ANGLE CRACKED. CUTOUT CRACK ON EPC PANEL, NDT. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-00-01.

Part: WEB — CORRODED (BS 200) · airframe 48,542 hrs · 25,782 cycles

PASSENGER CABIN FORWARD WET AREA FLOOR STRUCTURE RT SIDE BS 200, RBL 50, MEMBRANE WEB CORRODED. TASK 53-211-01. 100 PERCENT MATERIAL LOSS. CUTOUT DAMAGE, INSTALLED REPLACEMENT WEB AND DOUBLER IAW SRM 51-11-01.

Part: FLOOR SUPPORT — CORRODED (BS 166-200) · airframe 48,542 hrs · 25,782 cycles

PASSENGER CABIN FORWARD WET AREA FLOOR STRUCTURE RT SIDE BS 166 -200 RBL 53, FLOOR SUPPORT CORRODED. TASK 53-211-01. CORROSION LOSS 100 PERCENT. R & R FLOOR SUPPORT IAW SRM 51-30-02 AND DWG 9936534.

Part: CUSP WEB — CORRODED (BS 460) · airframe 48,542 hrs · 25,782 cycles

FORWARD CABIN RT CUSP WEB CORRODED AT BS 460. TASK 53-211-02. REPAIRED IAW SRM 53-20-02.

Part: FLOOR SUPPORT — CORRODED (BS 166-200) · airframe 48,542 hrs · 25,782 cycles

CABIN FORWARD WET AREA FLOOR STRUCTURE RT SIDE BS 166 -200, RBL 53, FLOOR SUPPORT CORRODED. TASK 53-211-01. CORROSION LOSS 100 PERCENT. R & R FLOOR SUPPORT IAW SRM 51-30-02.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 48,542 hrs · 25,782 cycles

CANTED FRAME Y1554, RBL 17, INTERCOSTAL AT VERTICAL STAIR ACTUATOR HINGE INNER CORD AND VERTICAL ANGLE CRACKED. REMOVED CRACKED STIFFENER AND ANGLE AND INSTALLED NEW IAW SRM 51-30-05.

Part: SEAT TRACK — CORRODED (BS 200-237) · airframe 48,542 hrs · 25,782 cycles

CABIN FWD WET AREA FLOOR STRUCTURE RT SIDE BS 200 -237+8" RBL 45, SEAT TRACK CORRODED. TASK 53-211-01. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK BS 200-245, RBL45 IAW SRM 53-40-01, PG 30, FIG 6.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 48,542 hrs · 25,782 cycles

FLAP ACCESS PANEL, 530FF/GF HAS CRACKED COMPOSIT AT LEADING EDGE. REPAIRED DAMAGE ON PANEL 530FF/GF ON JOB CARD 2000-8149-02 AND SRM 57-50-02.

Part: CUSP WEB — CRACKED (BS 1344-1361) · airframe 48,542 hrs · 25,782 cycles

LEFT CUSP WEB AT BS 1344 TO 1361 IS CRACKED. REPAIRED CUSP WEB IAW SRM 53-20-02, FIG 9.

Part: SEAT TRACK — GOUGED (BS 579) · airframe 48,542 hrs · 25,782 cycles

CABIN LT INBD SEAT TRACK CROWN GOUGED BS 579. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS. REMOVED AND REPAIRED SEAT TRACK FROM BS 530 TO 589 LBL 22 IAW SRM 53-40-01, FIG 6.

Part: PANEL — DAMAGED (LT WING) · airframe 48,542 hrs · 25,782 cycles

LEFT WING FILLET PANEL 150ML HAS COMPOSITE DAMAGE AT 2 SCREW HOLES. REPAIRED DAMAGE ON FILLET PANEL 150ML. WORK ACCOMPLISHED ON JOB CARD 2000-8149-03 AND SRM 57-50-02, VOL I AND 51-10-04.

Part: ATTACH ANGLE — CORRODED (BS 160) · airframe 48,542 hrs · 25,782 cycles

FWD CABIN WET AREA FLOOR STRUCTURE LT SIDE STA 160, LBL 16-45 ATTACH ANGLE AT BOTTOM OF RELAY CABINET IS CORRODED ON AFT SIDE. TASK 53-211-01. REMOVED CORROSION. INSTALLED NEW ANGLE IAW SRM 51-30-00 AND DWG 9964491.

Part: CUSP WEB — CORRODED (BS 620-628) · airframe 48,542 hrs · 25,782 cycles

FORWARD CABIN RT CUSP WEB CORRODED AT BS 620-628, REPAIRED IAW SRM 53-20-02.

Part: FLOORBEAM — CORRODED (BS 180) · airframe 48,542 hrs · 25,782 cycles

PASSENGER CABIN FORWARD WET AREA FLOORBEAM RT SIDE BS 180, RBL 9 -45, FLOORBEAM CORRODED. TASK 53-211-01. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPLACED FLOORBEAM RT SIDE BS 180, RBL 9 -45 IAW SRM 51-30-02 AND 53-00-01.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 48,542 hrs · 25,782 cycles

BS 200, RBL 9 -RBL 45, FLOORBEAM CORRODED. BLENDED CORROSION. OUT OF LIMITS. R & R FLOORBEAM IAW SRM 51-30-02.

Part: SUPPORT ANGLE — CORRODED (BS 546) · airframe 48,542 hrs · 25,782 cycles

FORWARD CABIN RT CUSP WEB ANGLE CORRODED AT BS 546, TASK 53-211-02. REPLACED ANGLE, OUT OF LIMITS.

Part: CUSP WEB — CORRODED (BS 532) · airframe 48,542 hrs · 25,782 cycles

RT CUSP WEB CORRODED AT BS 532. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR DOUBLER IAW SRM 53-20-02, 51-30-02.

Part: SEAT TRACK — CORRODED (BS 1332-1337) · airframe 48,542 hrs · 25,782 cycles

SEAT TRACK CROWN AT BS 1332-1337, RBL22, HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-30-05.

Part: CUSP WEB — CORRODED (BS 984-1003) · airframe 48,542 hrs · 25,782 cycles

LEFT CUSP WEB, BS 984 - 1003 HAS SEVERAL AREAS OF CORROSION, TASK 53-211-02, REMOVED CORROSION, OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER ON LEFT CUSP WEB IAW SRM 53-20-02.

Part: SEAT TRACK — GOUGED (BS 1117) · airframe 48,542 hrs · 25,782 cycles

SEAT TRACK CROWN IS GOUGED AT BS 1117, RBL 54. OUT OF LIMITS. REPAIRED IAW SRM 51-30-01.

Part: SEAT TRACK — GOUGED (BS 1117) · airframe 48,542 hrs · 25,782 cycles

SEAT TRACK, BS 1117, RBL 54, CROWN GOUGED. R & R IAW SRM 51-30-01.

Part: SEAT TRACK — CORRODED (BS 200-237) · airframe 48,542 hrs · 25,782 cycles

CABIN FWD WET AREA SEAT TRACK RT SIDE BS 200 - 237, RBL 22, CORRODED. REMOVED CORROSION, OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 1086) · airframe 48,542 hrs · 25,782 cycles

SEAT TRACK CROWN IS GOUGED AND HAS CORROSION, BS 1086, RBL 54. OUT OF LIMITS. REPAIRED IAW SRM 51-30-01.

Part: CUSP WEB — CORRODED (BS 285) · airframe 48,542 hrs · 25,782 cycles

FWD CABIN LEFT CUSP WEB CORRODED AT BS 285, TASK 53-211-02. REMOVED CORROSION, INSTALLED REPAIR DOUBLER IAW SRM 53-20-02, FIG 18, SHEET 1.

Part: FLOOR SUPPORT — CRACKED (BS 655) · airframe 48,542 hrs · 25,782 cycles

CABIN CENTER FLOOR SUPPORT ANGLE CRACKED AT BS 655. R & R FLOOR SUPPORT IAW SRM 51-10-05 AND 51-30-05.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 48,542 hrs · 25,782 cycles

CENTER CARGO DOOR TOP AFT DOOR STOP PAD FITTING CRACKED. R & R DOOR STOP IAW SRM 51-30-05, VOL II , DRWG 5910141.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 47,054 hrs · 24,999 cycles

EXPERIENCED FUMES IN CABIN. FLIGHT CREW SMELLED A PLASTIC ODOR WITH NO ASSOCIATED SMOKE AFTER TAKEOFF IN THE FORWARD GALLEY. GALLEY POWER WAS TURNED OFF AND THE ODOR DISSIPATED. MX FOUND THE FORWARD GALLEY COFFEEMAKER AT FAULT. R & R SAME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,898 hrs · 24,907 cycles

DURING SERVICE CHECK, FOUND NUMEROUS LAMPS INOPERATIVE ON OVERHEAD EMERGENCY EXIT SIGNS. R & R ALL OVERHEAD EXIT LIGHT BULBS THAT WERE INOPERATIVE. OPERATION CHECKED GOOD.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 46,898 hrs · 24,907 cycles

DURING PSV, THE RT CROWN FUSELAGE SKIN PANEL AT STA 1493, BETWEEN LONGERONS 2R-3R JUST BELOW THE VERTICAL STABILIZER ATTACH ANGLE WAS FOUND TO BE CRACKED. THE CRACK ORIGINATED FROM THE 1ST FASTENER HOLE FROM STA 1493, ABOV STR 3R. (ERA 496882-14AD)

Part: BOTTLE — EMPTY (TAILCONE) · airframe 46,800 hrs · 24,860 cycles

WHILE PERFORMING TAILCONE FUNCTIONAL CHECK, FOUND THE TAILCONE ASSIST BOTTLE READING ZERO PSI. SERVICED AND LEAK CHECKED BOTTLE IAW AMM 12-18-01. CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,202 hrs · 24,504 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND 8 OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN ROWS 15 AND 23. TROUBLESHOT AND FOUND BATTERY PACK AT ROW 19 BAD. CHANGED BATTERY PACK. OPS CHECKED GOOD.

Part: QUICK DISCONNECT — UNSECURE (NR 4 BRAKE) · airframe 45,770 hrs · 24,250 cycles

SHIP 9205 EXPERIENCED A NR 4 BRAKE FIRE AFTER PARKING AT GATE IN FAR. MAINTENANCE FOUND NR 4 BRAKE DISCONNECT UNSECURED. REPLACED NR 4 QUICK DISCONNECT AND NR 3 AND NR 4 BRAKE AND TIRE ASSEMBLIES PER AMM. PERFORMED BITE OF ANTI-SKID/AUTO BRAKE SYSTEMS AND RETURNED TO SERVICE TEST OF SAME. ALL OPERATIONAL CHECKS NORMAL PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,447 hrs · 23,616 cycles

DURING PSV N 10 OCT 11 THE RT CROWN FUSELAGE SKIN PANEL AT STA 1493 BETWEEN LONGERONS 2R - 3R JUST BELOW THE VERTICAL STAB ATTACH ANGLE WAS FOUND TO BE CRACKED. THE CRACK ORIGINATED FROM THE 1ST FASTENER HOLE FROM STA 1493 ABOVE STR 3R. CUT OUT DAMAGE 1.05 BY 1.875. REMOVED FASTENERS IN REPAIR AREA. C/W HFEC INSP TO FASTENER HOLES IN SKIN NO CRACKS FOUND. FABRICATED REPAIR DOUBLER AND SHIMS AND INSTALLED PER ERA 496882-14 ON NRC 204. IDENTIFIED REPAIR AS PERMANENT REPAIR PER PS 900-5-1 NR 04.

Part: LINK ASSY — WORN (NLG DOOR) · airframe 39,651 hrs · 21,317 cycles

RETURN AIR TURN-AROUND FOR HEAVY VIBRATION UNDER COCKPIT AFTER GEAR RETRACTION. GEAR LEVER SELECTED TO DOWN VIBRATION STOPPED. FOUND LT NOSE GEAR DOOR OPEN ON TAXI IN 952847. SUSPECT LT FWD NOSE GEAR DOOR LINK FAILED. REPLACED LT FWD DOOR LINK. JACKED ACFT. CYCLED GEAR SEVERAL TIMES. OPS AND INDICATION OF NOSE GEAR AND DOORS CK SATISFACTORY.

Part: CONNECTOR — DAMAGED (GENERATOR) · airframe 38,511 hrs · 20,641 cycles

L ENGINE GENERATOR OVERHEAT MESSAGE APPEARED IN FLIGHT THEN EXTINGNISHED. FOUND OIL COOLING LINE LEAKING AND GENERATOR FAILED.REPLACED OIL COOLING LINE AND GENERATOR. CONNECTORS DAMAGED. WILL NEED HARNESS ASSY MFG P/N 290W5211-509 DPN 242710080. DUE TO HARNESS POOR CONDITION REMOVED INPUT SHAFT AND INSTALLED SHAFT FERRY PLUG. RAN ENGINE.LEAK CK GOOD. GENERATOR COOLING LINE WILL STILL NEED LEAK CHECK AFTER HARNESS REPLACEMENT. CONTINUE ON MCO. GEN NOW OPS GOOD.

Part: SKIN — DAMAGED (BS 588 L27R) · airframe 37,960 hrs · 20,312 cycles

MX FOUND A DENT AND GOUGE AT BS 588, L27R, DAMAGED AREA IS ROUGHLY 25 INCHES LONG AND CROSSES OVER A BUTT SPLICE, BS 568. REPAIRED IAW ERA 473851-14. (ERA 473851-14)

Part: BALLAST — SHORTED (CABIN LIGHTS) · airframe 34,472 hrs · 18,271 cycles

FLT ATTENDANT REPORT STRONG ODOR OF SMOKE LIKE MATCH BEING LIT BETWEEN 19-25. NOR VISUAL IND OF SMOKE. IT DISSIPATED AFTER 5 MIN. NO ABNORMAL INDICATIONS NO SMOKE DETECTOR ALARMS. OP VIDEO SYS, CKS NML O2 GENERATORS AND VDUS INSP. INSPECTED BATTERY PACKS FOR EMERG LIGHTS ALL OK. FOUND FAILED FLUORESCENT OVERHEAD LIGHT BALLAST. REMOVED BULB ROW 18-19, FWD TO MCO AND PLAC PER MEL 33-20-01A. NEEDS BALLAST AND BULBS, REPLACED BALLAST AND LIGHT AT 18 AND 19. OPS NORMAL MCO AND PLAC REMOVED.

Part: FITTING — CUT (HORIZONTAL STAB) · airframe 33,547 hrs · 17,773 cycles

HORIZ STAB TORQUE BOX AFT END CUT BY ELEVATOR CABLE FOUND OFF CABLE RUN PULLEY. REPLACED FITTING IAW BOEING DRAWING 5940483 AND MD90 SRM 51-10-05.

Part: ENGINE — FOD (NR 1) · airframe 33,479 hrs · 17,735 cycles

AT FL310, LEFT ENGINE SHUT DOWN IN FLT HEARD BANG AND FELT SHUTTER N1 RAPIDLY DECREASED, EGT INCREASED TO 730 OIL PRESS WENT TO -0-. C/W BORESCOPE INSP FOUND FOD BEYOND M/M LIMITS. DAMAGE STA AT 3RD STG HPC. STG 2.5 LPC BLADES ARE CLEAN ENG CHANGE REQUIRED. REPLACED LT ENG AS PER TRANS 2T102.

Part: STARTER — OVERHEATED (APU) · airframe 31,737 hrs · 16,761 cycles

APU AUTO SHUTDOWN ON TAXI OUT, ACS FAULT ON OAP, AND STRONG ELECTRICAL SMELL IN CABIN. INSTALLED NEW STARTER PER M/M. INSPECTED APU COMP. NO PROBLEMS NOTED. REPLACED APU START RELAY. APU OPS CHECKS NORMAL. STARTER LEAK CHECK GOOD. NO FAULTS.

Part: WARNING LIGHT — ILLUMINATED (NR 2 ENGINE) · airframe 30,291 hrs · 15,922 cycles

ON TAKEOFF AT KOAK, EOAP DISPLAYED RT EECEDP BUSS FAIL. TROUBLESHOT PER FIM, MESSAGE CLEARED.

Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 28,258 hrs · 14,823 cycles

CRACK OF 2 INCH ON SKIN OF AFT FUSELAGE STA Y=953.604 AND INTERSECTION OF LONGERON 23 LT. REPAIRED SAME.

Part: STRUT — LEAKING (NOSE) · airframe 27,245 hrs · 14,299 cycles

AFTER LIFT OFF NOSE GEAR FAILED TO RETRACT WITH RED NOSE LIGHT REMAINING ILLUMINATED. AFTER FOLLOWING CORRECTIVE PROCEDURES THE NOSE GEAR OPERATED CORRECTLY. FOUND NOSE STRUT FLAT AND VALVE LEAKING. REPLACED O-RING AND RESERVICED STRUT WITH OIL AND AIR. OPERATED NOSE GEAR PER AMM 32-30-00-720-801 AND WAS NORMAL.

Part: O-RING — DAMAGED (SCHRADER VALVE) · airframe 25,457 hrs · 13,438 cycles

AFTER TAKEOFF NOSE GEAR FAILED TO RETRACT. DURING POM PROCEDURE GEAR HANDLE WOULD NOT RAISE. CONTINOUS T/O AURAL WARNINGS OF FLAPS, STABILIZER, SLATS IN AIR. NO PRESSURIZATION AUTO FAIL INOP 1 AND 2. AUTO SPOILERS INOP OAP MESSAGE. ALSO HAD LEFT AND RIGHT STRAKE FAULT MESSAGE ON STATUS MSG. TAIL TEMP FAULT AND STRAKE ICE MSG ON OAP. FOUND O-RING ON NOSE GEAR STRUT SERVICING SCHRADER VALVE IN POOR CONDITION. REPLACED SAME. SERVICED NOSE STRUT PISTON PER MM. INSP NLG STRUT PISTON IN FULL EXT. CHECKED GOOD CYCLED ALL 3 GEARS SEVERAL TIMES, OPS AND INDICATION NORMAL.

Part: WARNING LIGHT — INOPERATIVE (NR 2 ENGINE) · airframe 25,147 hrs · 13,302 cycles

AFTER ARRIVAL AT GATE AND DURING PASSENGER NORMAL EXIT, RAMP STATED, A TAILPIPE FIRE IN NR 2 ENG. NO FIRE INDICATION OR LIMIT EXCEEDENCE NOTED. TAILPIPE FIM PROCEDURE ACCOMPLISHED IAW POM. ENG WAS ALREADY SHUT DOWN. CLEANED NR 5 BEARING CAVITY AND RAN ENGINE PER PFHB.

Part: SEAL — LEAKING (NLG STRUT) · airframe 24,185 hrs · 12,800 cycles

NOSE GEAR INDICATION SHOWED IT DID NOT RETRACT AFTER TAKEOFF. THERE WAS THE ASSOCIATED NOISE WITH AN EXTENDED NOSE GEAR. THE HANDLE WAS LOWERED ALL GEAR DOWN/LOCKED. A NORMAL LANDING WAS PERFORMED. FOUND NOSE STRUT SERVICING VALVE SEAL LEAKING,STRUT WAS FLAT. REPLACED VALVE ASSEMBLY, LEAK CHECKS GOOD IAW MM.

Part: STRUCTURE — BIRD STRIKE (LE SLAT) · airframe 22,373 hrs · 11,882 cycles

SUBJECT INBOARD LE SLAT WAS FOUND DAMAGED DUE TO BIRD STRIKE, REPAIR PER E/A 417937-14

Part: SWITCH — FAILED (PYLON FLAP) · airframe 20,164 hrs · 10,772 cycles

PYLON FLAP FAULT EOAP MESSAGE DURING TAKEOFF, RESULTING IN REJECTED TAKEOFF AT 110 KIAS. FOUND PYLON FLAP SWITCH S1-711 FAILED. REPLACED SAME PER MM.

Part: FUSE — BROKEN (LT MLG WW) · airframe 18,819 hrs · 10,102 cycles

RT HYD SYS DUMPED ON TAXI OUT. A/C RETURN TO GATE. CONTRACT MTC FOUND RT OTBD ANTI-SKID CONTROL VALVE FUSE BROKEN FROM VALVE. REPLACED SAME.

Part: VALVE — LEAKING (NLG STRUT) · airframe 18,544 hrs · 9,958 cycles

NOSE GEAR WOULD NOT RETRACT. FOUND SERVICING VALVE ON STRUT LEAKING. REPLACED SAME.

Part: SEAL — DAMAGED (LAVATORY) · airframe 18,309 hrs · 9,832 cycles

TOILET SHROUD SEAL WAS FOUND DAMAGED. A REPLACEMENT SEAL WAS MANUFACTURED PER ER/A 401873-14AD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,771 hrs · 8,472 cycles

EMERGENCY ESC LIGHT AT 22C INOP. REPLACED EMERGENCY LIGHT ASSY AT 22C.

Part: LIGHT — MISSING (CABIN) · airframe 15,332 hrs · 8,215 cycles

EMERGENCY TRACK LIGHTS MISSING AT ROWS 3 13 AND 17. INSTALLED LIGHT AND LENS AT SEAT 3 AND 17. SPLICED IN NEW SOCKET AT SEAT 13, ALL OPERATIONAL CHECKS OK.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,885 hrs · 7,998 cycles

THE STATION 1520.225 CANTED BULKHEAD WEB WAS FOUND WITH 2 CRACKS IN THE JOGGLED PORTION OF THE WEB AT STRINGERS 8L AND 8R (11:00 & 1:00 POSITIONS). THE CRACKED SECTION OF WEB AT EACH LOCATION WAS CUT AND REMOVED TO THE EXISTING FACTORY SPLICE LOCATION. THE REMOVED SECTIONS WERE REPLACED WITH ALUMINUM DOUBLERS INSTALLED PER ER/A 369664-14, REV A.

Part: LIGHT — INOPERATIVE (SEATS 32-37)

EMERGENCY TRACK LIGHTING AT SEATS 32-37 INOP. FOUND FAULTY WIRE SPLICES AT SEAT 33. INSTALLED PROPER SPLICE, OPS CK GOOD.

Part: GENERATOR — FAILED (RT ENGINE)

RT GEN FAILED DURING INITIAL TAKEOFF ROLL AT 70KTS OAP MESSAGE RT ELEC SYSTEM FAIL. EPCU FAULTS CEU. REPLACED CEU RAN ENGINE. A/C POWER SYSTEM CHECK GOOD.

Part: TEMP SENSOR — MALFUNCTIONED (RT TAIL COMPT)

RT TAIL HIGH TEMP ILLUM AFTER T/O. REPLACED RT HI TEMP SENSOR RAN ENGS W/PYLON PLATES OPENED. NO LEAKS NOTED RAN ENG TO T/O PWR FOR 4 MINS ALL IND NRML.

Part: PRESSURIZATION — MALFUNCTIONED (CABIN)

AFTER T/O, A/C WOULDN'T PRESSURIZE WITH 1 PAC RT PAC ON MCO. PRESSURIZED A/C WITH APU AND ENGS A/C PRESSURIZED NORMAL, INSP TAIL COMP FOR LEAKS, NONE FOUND. BITE CHECKED AUTO PRESS CONTROLLER NBO FAULTS. CREW REPORTED THEY DID NOT TRY MANUAL OPP OF PRESSURIZATION. NO TROUBLE FOUND.

Part: HEATER — MALFUNCTIONED (RT STRAKE)

OFF SKED LANDING, ANTI-ICE PROBLEMS, POSSIBLE STRAKE HEATER TROUBLE. REPLACED RT STRAKE.

Part: INLET — DIRTY (APU)

SULFUR SMELL IN CABIN. DIVERTED TO ONT. OIL FOUND IN APU INLET. DEFERRED APU INOP. FLIGHT CONT'D TO SLC. CLEANED APU INLET, PERFORMED BURN-OUT, NO ODORS.

Part: STRUT — REQD SERVICE (NLG)

ON TAKEOFF, NOSE LANDING GEAR FAILED TO RETRACT. FOUND NOSE GEAR STRUT FLUID LOW. SERVICED STRUT AND GEAR CYCLED, OPS NORMAL.

Part: EEL WIRE — LOOSE (CABIN)

DURING TEST, LAST 12 EMERGENCY FLOOR TRACK LIGHTS ARE INOP. FOUND LOOSE POWER WIRE IN TRACK. RECONNECTED WIRE, OPERATION NORMAL.