N804ME

Part: SLIDE — INOPERATIVE (TAILCONE)

TAILCONE SLIDE PRESSURE AT (0). REMOVED AND REPLACED TAILCONE SLIDE. (K)

Part: BOTTLE — LOW PRESSURE (ESCAPE SLIDE) · airframe 45,915 hrs · 45,928 cycles

TAIL CONE EVACUATION SLIDE BOTTLE PRESSURE GAUGE NOT IN THE GREEN BAND. REMOVED AND REPLACED TAIL CONE SLIDE ASSEMBLY.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,351 hrs · 45,544 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY

Part: FITTING — CORRODED (GALLEY) · airframe 45,283 hrs · 45,501 cycles

GALLEY 1 OUTBOARD FUSE MOUNTED FOOT FRAME STATION 152 X-51 Z0 IS CORRODED. FABRICATED AND INSTALLED FITTINGS.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 45,291 hrs · 45,504 cycles

EXIT ROW WON'T EXTINGUISH WHEN POWER IS REMOVED FROM AIRCRAFT. REPLACED BROKEN WIRE.

Part: STRAP — CORRODED (THRESHOLD) · airframe 45,283 hrs · 45,501 cycles

FOUND SURFACE CORROSION ON THRESHOLD STRAP Z-46, X-18 AND FRAME STATION Y 636-693. FABRICATED AND INSTALLED STRAP.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,283 hrs · 45,501 cycles

FOUND CORROSION ON INBOARD FLANGE OF SEAT TRACK AT FRAME STATION 1136 TO 1146, X +44. Z 0, AROUND BOARD FASTENER HOLES. FABRICATED AND INSTALLED SEAT TRACK.

Part: PANEL — CORRODED (FWD GALLEY) · airframe 45,283 hrs · 45,501 cycles

FOUND FORWARD GALLEY SERVICE DOOR THRESHOLD FLOOR PANEL CORRODED. FABRICATED AND INSTALLED PANEL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,283 hrs · 45,501 cycles

FOUND SEAT TRACK IS CORRODED AT NUTPLATE AS VIEWED FROM AFT CARGO BAY Y 1267 AND X +24, Z 0. FABRICATED AND INSTALLED SEAT TRACK.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,283 hrs · 45,501 cycles

FOUND WEB CRACKED AT FRAME STATION Y 1300 X+48. FABRICATED AND INSTALLED WEB.

Part: STRAP — CORRODED (THRESHOLD) · airframe 45,283 hrs · 45,501 cycles

FOUND SURFACE CORROSION ON THRESHOLD STRAP Z-46, X-18 AND FRAME STATION Y 1155 TO 1219. FABRICATED AND INSTALLED NEW STRAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,283 hrs · 45,501 cycles

SUPPORT ON FLOORBEAM UPPER FLANGE AT FRAME STATION 1169, X-29, Z 0. FABRICATED AND INSTALLED FLOORBEAM.

Part: FITTING — CORRODED (GALLEY) · airframe 45,283 hrs · 45,501 cycles

GALLEY 1 INBOARD FUSE MOUNTED FOOT, FRAME STATION 152 X-45 Z 0. FABRICATED AND INSTALLED FITTINGS.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 45,274 hrs · 45,497 cycles

MASTER WARNING (CABIN ALERT) ILLUMINATED. REMOVED AND REPLACED CABIN PRESSURE CONTROL.

Part: BLADES — BENT (LEFT ENGINE) · airframe 44,817 hrs · 45,203 cycles

LEFT ENGINE COMPRESSOR STALL/SURGE. REMOVED BENT TIPS AS NECESSARY ON VARIOUS ENGINE BLADES AND BLENDED AS REQUIRED PER IAW BOEING MM 72-33-22.

Part: TAB — OBSTRUCTED (ELEVATOR) · airframe 44,813 hrs · 45,199 cycles

NO CONTROL INPUT EVEN WHEN CONTROL COLUMN WAS MOVED AFT. REMOVED SCREW THAT WAS WEDGED BETWEEN ELEVATOR CONTROL TAB STOP AND INBOARD ATTACHED FITTING.

Part: INDICATOR — INOPERATIVE (RT ENG OIL TEMP) · airframe 44,802 hrs · 45,193 cycles

RIGHT ENGINE OIL TEMERATURE PEGGED OVER 165, ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED RIGHT ENGINE OIL TEMERATURE INDICATOR.

Part: SKIN — CORRODED (WING SLAT) · airframe 44,311 hrs · 44,869 cycles

LEADING EDGE AT STATION 375 HAS CORROSION. FABRICATED AND INSTALLED DOUBLER AND FILLER.

Part: STRUCTURE — VIBRATION (FUSELAGE) · airframe 44,101 hrs · 44,761 cycles

DURING CRUISE PILOT REPORTED A LOUD HUMMING SOUND AND VIBRATION. VISUALLY INSPECTED ALL LANDING GEARS AND WHEEL WELLS, INSPECTED AIRCRAFT FUSELAGE, DOORS,WINGS AND PANELS. PERFORMED ENGINE VIBRATION TEST. NO DEFECTS FOUND.

Part: SLIDE — DISCHARGED (AFT GALLEY) · airframe 43,270 hrs · 44,266 cycles

AFT GALLEY SLIDE PRESSURE INDICATOR IS INDICATING IN THE RED (READS 2000 PSI). REMOVED AND REPLACED AFT GALLEY DOOR SLIDE.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 43,172 hrs · 44,196 cycles

CAPTAIN'S AFT INBOARD SEAT TRACK IS WORN. FABRICATED AND INSTALLED CHANNEL.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,172 hrs · 44,196 cycles

CORROSION ON INTERCOSTAL AT FRAME STATION 775 BETWEEN LONGERON 27 AND 28 LEFT. FABRICATED AND INSTALLED INTERCOSTAL.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 43,172 hrs · 44,196 cycles

FIRST OFFICER'S AFT INBOARD SEAT TRACK IS WORN. FABRICATED AND INSTALLED SEAT TRACK TEE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,172 hrs · 44,196 cycles

AFT BAGGAGE PIT, RIGHT SEAT TRACK BETWEEN STATION 1212 AND 1325 HAS SEVERAL AREAS OF CORROSION. FABRICATED AND INSTALLED TRACK.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,172 hrs · 44,196 cycles

FLOOR SUPPORT FITTINGS AT FRAME STATION 430 BETWEEN NUMBER 30 AND 29 RIGHT LONGERON HAS MODERATE CORROSION ON THE UPPER SURFACE, ALSO NUT PLATES ARE CORRODED. FABRICATED AND INSTALLED FITTING AND INSTALLED TWO EACH NUT PLATES.

Part: GENERATOR — INOPERATIVE (LEFT) · airframe 43,044 hrs · 44,117 cycles

LEFT GENERATOR FAILED. REMOVED AND REPLACED LEFT GENERATOR.

Part: GENERATOR — INOPERATIVE (LEFT) · airframe 43,016 hrs · 44,100 cycles

AIRCRAFT CROSSTIE LOCKOUT ILLUMINATED WITH LEFT GENERATOR OFF LIGHT. REMOVED AND REPLACED LEFT ENGINE GENERATOR.

Part: WINDOW FRAME — LIGHTNING STRIKE (FUSELAGE) · airframe 42,999 hrs · 44,093 cycles

LIGHTNING STRIKE ON LEFT SIDE CABIN WINDOW NR 29 FRAME ON LOWER FORWARD CORNER. BLENDED OUT DAMAGE, ACCEPTABLE AS TEMPORARY REPAIR TO BE PERMANENTLY REPAIRED ON OR BEFORE 7,000 CYCLES.

Part: WINDOW FRAME — LIGHTNING STRIKE (FUSELAGE) · airframe 42,999 hrs · 44,093 cycles

LIGHTNING STRIKE ON CABIN WINDOW FRAME 29 AFT LOWER SIDE. BLENDED OUT DAMAGE, ACCEPTABLE AS TEMPORARY REPAIR TO BE PERMANENTLY REPAIRED ON OR BEFORE 7,000 CYCLES.

Part: WINDOW FRAME — LIGHTNING STRIKE (NR 34 AFT UPPER) · airframe 42,999 hrs · 44,093 cycles

LIGHTNING STRIKE ON LEFT SIDE CABIN WINDOW FRAME NR 34 ON AFT UPPER SIDE. BLENDED OUT DAMAGE, ACCEPTABLE FOR STRENGTH AS IS.

Part: SEPARATOR — INOPERATIVE (CABIN AIR) · airframe 42,943 hrs · 44,067 cycles

STRONG FUMES IN CABIN. REMOVED AND REPLACED WATER SEPARATOR.

Part: GENERATOR — INOPERATIVE (ENGINE) · airframe 42,928 hrs · 44,058 cycles

LEFT GENERATOR LIGHT CAME ON, WAS ABLE TO RESET LEFT GENERATOR, THEN FOURTY-FIVE MINUTES LATER LEFT GENERATOR LIGHT CAME ON AGAIN, STARTED AUXILIARY POWER UNIT, BUT UNABLE TO POWER LEFT SIDE OF ELECTRICAL POWER SYSTEM. REMOVED AND REPLACED GENERATOR CONTROL UNIT.

Part: BOLT — MISINSTALLED (LANDING GEAR) · airframe 42,644 hrs · 43,879 cycles

DURING GEAR RETRACTION A LOUD NOISE COMING FROM THE NOSE GEAR AREA. LT FORWARD NOSE GEAR DOOR RETRACT LINK NOT LATCHED COMPLETELY, FOUND RELEASE HANDLE BOLT INSTALLED IMPROPERLY. REPOSITIONED BOLT CLOSED AND LOCKED FORWARD NOSE GEAR DOOR.

Part: PITOT LINE — LEAKING (COCKPIT) · airframe 42,479 hrs · 43,782 cycles

CAPTAIN'S MACH INDICATOR HAS .14 MACH SPLIT AND EIGHT KNOTS SPLIT BETWEEN FIRST OFFICER'S AIRSPEED. SELECTING CENTRAL AIR DATA COMPUTER TO BOTH ON ONE AND TWO CORRECTED THE SPLIT. FOUND MASSIVE LEAK IN PITOT ON NUMBER ONE PITOT SYSTEM, TIGHTENED FITTINGS, LEAK CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,290 hrs · 43,661 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED APPROXIMATELY 1.25 INCH AT STATION 1437 BETWEEN LONGERON 3 AND 4 RT. FABRICATED AND INSTALLED DOUBLER.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 42,290 hrs · 43,661 cycles

FIRST OFFICERS SEAT TRACK (FORWARD INBOARD) HAS WORN AREAS. FABRICATED AND INSTALLED NEW SEAT TRACK.

Part: DOUBLER — DENTED (FUSELAGEW) · airframe 42,290 hrs · 43,661 cycles

DENT LOCATED AT 1 INCH BELOW LONGERON 4 LEFT AND SEVERAL VERY SMALL DENTS LOCATED AROUND THIS DENT AT STATION 219. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: SPACER — CORRODED (CARGO DOORWAY) · airframe 42,290 hrs · 43,661 cycles

AFT CARGO DOOR LOWER JAMB HAS LIGHT CORROSION ALONG THE ENTIRE LENGTH AROUND AND INSIDE SCREW HOLES. FABRICATED AND INSTALLED JAMB SPACER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,290 hrs · 43,661 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED APPROXIMATELY .25 INCH OUT OF RIVER HOLE AT STATION 1437 BETWEEN LONGERON 2 AND 3 LEFT. REMOVED CRACK IN SKIN, FABRICATED AND INSTALLED DOUBLER AND FILLER.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 42,290 hrs · 43,661 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED APPROXIMATELY 1 INCH AT STATION 1437 BETWEEN LONGERON 3 AND 4 LEFT. FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FILLER.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 42,290 hrs · 43,661 cycles

DENT LOCATED BETWEEN LONGERON 26 LEFT AND 25 LEFT AT STATION 694. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: CONTACTOR — INOPERATIVE (HORZ STAB TRIM) · airframe 41,773 hrs · 43,379 cycles

PRIMARY TRIM INOPERATIVE. REMOVED AND REPLACED NOSE DOWN PRIMARY LONGITUDINAL TRIM CONTACTOR.

Part: RETAINER — CORRODED (WINDOW) · airframe 41,747 hrs · 43,364 cycles

RIGHT UPPER COCKPIT WINDOW RETAINER IS CORRODED IN LOWER FORWARD CORNER. REMOVED DAMAGE AND INSTALLED FILLER AND EXTERNAL DOUBLER.

Part: MOTOR — DEFECTIVE (STABILIZER) · airframe 41,697 hrs · 43,338 cycles

PRIMARY TRIM PROBLEM. REMOVED AND REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR AND FIRST OFFICERS YOKE TRIM SWITCH AND REPLACED CONNECTORS.

Part: BOLT — SHEARED (LT MLG WHEEL) · airframe 40,995 hrs · 42,966 cycles

NR 1 MAIN WHEEL ASSY THROUGH BOLT SHEARED OFF. REPLACED NR 1 WHEEL AND TIRE ASSEMBLY.

Part: LINE — DISCONNECTED (ENGINE) · airframe 40,760 hrs · 42,845 cycles

ON LEFT THROTTLE, SPLIT INCREASED WITH ALTITUDE TO ABOUT 1 1/2 KNOBS. -- RECONNECTED PRESSURE TOTAL 2 LINE.

Part: BRACKET — LOOSE (STATION 42) · airframe 40,583 hrs · 42,744 cycles

UPON REMOVAL OF PROXIMITY SWITCH BRACKET, FASTENER HOLE PLUG WAS LOOSE/REMOVED. LOCATED AT STATION 42 CEILING AREA. -- INSTALLED FLANGE BUSHING.

Part: FASTENER — CRACKED (STA 207) · airframe 40,583 hrs · 42,744 cycles

GALLEY SUBFLOOR HAS SMALL CRACKS AROUND FASTENERS HOLES JUST AFT OF SERVICE DOOR ENTERANCE UNDER FLOOR SUPPORT ANGLE STATION 207 RIGHT.

Part: WEB — DAMAGED (FUSELAGE) · airframe 40,583 hrs · 42,744 cycles

GALLEY SUBFLOOR HAS HOLE JUST INBOARD OF SERVICE DOOR ENTRANCE. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: BRACKET — CORRODED (STA 42) · airframe 40,583 hrs · 42,744 cycles

CORROSION ON FORWARD ACCESSORY DOOR APPROXIMATELY SWITCH SUPPORT BRACKET AT STATION 42 CEILING AREA. -- FABRICATED AND INSTALLED SUPPORT BRACKET.

Part: ANGLE — CORRODED (GALLEY SERV DR) · airframe 40,583 hrs · 42,744 cycles

CUSP ANGLE AT FORWARD GALLEY SERVICE DOOR FORWARD AND AFT LOWER JAMB CORNERS HAS AREA OF LIGHT CORROSION

Part: WEB — CRACKED (STA 207) · airframe 40,583 hrs · 42,744 cycles

FORWARD PASSENGER DOOR JAMB WEB HAS A CRACK AT STATION 207 AND LONGERON 15 LEFT. -- FABRICATED AND INSTALLED FILLER AND DOUBLER.

Part: WEB — CRACKED (STA 207) · airframe 40,583 hrs · 42,744 cycles

FORWARD PASSENGER DOOR JAMB WEB HAS A CRACK AT STATION 207 AND LONGERON 11 LEFT. -- FABRICATED AND INSTALLED FILLER AND DOUBLER.

Part: PAN — CRACKED (WINDOW #32) · airframe 40,583 hrs · 42,744 cycles

RIGHT WINDOW #32 WINDOW PAN IS CRACKED AT FASTENER ON TOP FORWARD CORNER JUST AFT OF STATION 845. -- FABRICATED REPAIR ANGLE AND SHIM AND INSTALLED REPAIR.

Part: DOUBLER — CRACKED (BEAM #6) · airframe 40,583 hrs · 42,744 cycles

PASSENGER DOOR BEAM #6 IS CRACKED BY FASTENER 18" AFT OF THE FORWARD EDGE. -- FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: SUPPORT — CORRODED (STA 160-200) · airframe 40,583 hrs · 42,744 cycles

STATION 160 TO 200 FLOORBOARD SUPPORT 18" INBOARD FROM THE GALLEY DOOR HAS CORROSION. -- REMOVED AND REPLACED NEW SUPPORT.

Part: SUPPORT — CORRODED (STA 180) · airframe 40,583 hrs · 42,744 cycles

STATION 180 FLOORBOARD SUPPORT FROM THE AIRCRAFT CENTERLINE OUTBOARD TO THE #4 SEAT TRACK HAS HEAVY CORROSION. -- REMOVED AND FABRICATED AND INSTALLED NEW PART.

Part: ANTENNA — CRACKED (STA 474) · airframe 39,992 hrs · 42,407 cycles

FORWARD LEFT VHF ANTENNA INTERCOSTAL HAS A 6" CRACK RUNNING FORWARD AND AFT AT FUSELAGE STATION 474. -- INSTALLED 5&6 ANGLES TO INTERCOSTALS AND 3 DOUBLER TO SKIN.

Part: INTERCOSTAL — CRACKED (STA 465-484) · airframe 39,994 hrs · 42,408 cycles

FOUND 7 CRACKS IN FUSELAGE SKIN BETWEEN LONGERON 29LEFT AND 30. STATION 465-484. -- INSTALLED 5 AND 6 ANGLES TO INTERCOSTAL AND 3 DOUBLER TO SKIN.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 39,554 hrs · 42,173 cycles

CAPTAIN REPORTED LOSING BACKGROUND COLORS (BLUE/BROWN) ON CAPTAIN'S PFD & THEN ON FIRST OFFICER'S PFD. CHECKED LEFT AND RIGHT AIR CONDITIONING PACKS FOR LOOSE DUCTS, NONE NOTED. PRESSURIZED CABIN TO CHECK PACK FLOW, EACH PACK WOULD PRESSURE CABIN ABOVE GPSID SEPARATELY. CLEANED DIVERTED VALVE ASSY. REMOVED, CLEANED AND REINSTALLED COOLING FAN DIVERTER REF MD80 MM 21-50.

Part: ODOR — DETECTED (CABIN) · airframe 39,116 hrs · 41,965 cycles

BURNING ODOR CAME FROM CABIN FLOOR IN SEAT 19AB AREA. INSPECTED SEAT 19AB IMMEDIATELY AFTER LANDING AND NO SMELL WAS NOTED. INSPECTED THE FOLLOWING: BALLAST FOR LOWER SIDEWALL LIGHTING EMERGENCY BATTERY PACK IN CEILING PHONES, PSU PANELS AND O2 GENERATOR. RAN ENGINES AND PRESSURIZED AIRCRAFT WITH WARM PACKS. INSPECTED WHEEL WELL AREA AND CARGO COMPARTMENTS. ALL THE ITEMS INSPECTED WERE OK. THE ONLY SMELL NOTED WAS IN THE AFT CARGO COMPARTMENT BEFORE THE BAGS WERE REMOVED AND THERE WAS A STRONG AMMONIA SMELL. ALSO INSPECTED THE RECIRCULATION FAN FOR OPERATION. AIRCRAFT OK FOR SERVICE.

Part: BEAM — CRACKED (GALLEY SVC DOOR) · airframe 38,255 hrs · 41,537 cycles

GALLEY SERVICE DOOR #4 BEAM IS CRACKED IN OUTBOARD RADIUS AT FWD END -- STOP DRILLED CRACK. LOCATED, DRILLED AND INSTALLED REPAIR DOUBLERS.

Part: ATTACH ANGLE — CORRODED (T/E FLAP) · airframe 38,255 hrs · 41,537 cycles

RIGHT HAND WING FLAP NR 8 RIB (COUNTING FROM INBOARD-OUTBOARD) THE LOWER INBOARD ATTACH ANGLE IS EXFOLIATED. REMOVED, FABRICATED, DRILLED AND INSTALLED LOWER INBOARD ATTACH ANGLE.

Part: SKIN — GOUGED (FWD SVC DOOR) · airframe 38,255 hrs · 41,537 cycles

FUSELAGE SKIN GOUGED AT AFT EDGE OF FORWARD SERVICE DOOR HOLD OPEN CUP -- BLENDED DAMAGE. INSTALLED REPAIR PLATE AND DOUBLERS IN ACCORDANCE WITH SRM 53-04, FIGURE 24.

Part: SPAR CAP — CRACKED (R/H FLAP) · airframe 38,255 hrs · 41,537 cycles

RIGHT HAND FLAP LOWER AFT FLAP SPAR CUP IS CRACKED JUST OUTBOARD OF FLEX JOINT -- REMOVED CRACKED SPAR CAP, LOCATED, DRILLED AND INSTALLED NEW SPAR CAP.

Part: BEAM — CRACKED (GALLEY SVC DOOR) · airframe 38,255 hrs · 41,537 cycles

GALLEY SERVICE DOOR #1 BEAM IS CRACKED IN OUTBOARD RADIUS AT FORWARD END -- STOP DRILLED CRACK. LOCATED, DRILLED AND INSTALLED REPAIR DOUBLERS.

Part: FITTING — CRACKED (GALLEY SVC DOOR) · airframe 38,255 hrs · 41,537 cycles

GALLEY SERVICE DOOR #3 BEAM IS CRACKED IN OUTBOARD RADIUS AT FORWARD END -- STOP DRILLED CRACK. REMOVED AND REPLACED FITTING.

Part: ATTACH ANGLE — CORRODED (T/E FLAP) · airframe 38,255 hrs · 41,537 cycles

RIGHT HAND WING FLAP NOSE RIB INBOARD ATTACH ANGLE HAS MODERATE CORROSION PRESENT. THE NOSE RIB IS LOCATED JUST BELOW NR 1 AND NR 2 FIXED VANE SPLICE AREA. REMOVED NOSE RIB ATTACH ANGLE. DRILLED, FABRICATED AND INSTALLED TEE. INSTALLED NOSE RIB.

Part: FRAME — CRACKED (FRAME 1485) · airframe 38,255 hrs · 41,537 cycles

CANTED FRAME 1485, AFT ACCESSORY COMPARTMENT HAS A 5/8 INCH CRACK AROUND A FASTENER LOCATED APPROXIMATELY 6 INCHES OUTBOARD OF EMERGENCY LIGHT CLUSTER -- STOP DRILLED CRACK, FABRICATED, LOCATED AND DRILLED UP DOUBLER. INSTALLED REPAIR.

Part: PAN — CORRODED (FWD CARGO COMPT.) · airframe 38,255 hrs · 41,537 cycles

FORWARD CARGO COMPARTMENT AIRCRAFT DOOR JAMB BOTTOM HAS 3 AREAS OF CORROSION-BOTH DOOR STOP FITTINGS AND ONE SPOT IN BETWEEN -- REMOVED EXTERNAL SCUFF PLATE AND FLOOR BOARD SUPPORTS TO FACILITATE OTHER MAINTENANCE. REMOVED LOWER PAN SECTION. INSTALLED SCUFF PLATE, FLOOR BOARD SUPPORTS AND NEW LOWER PAN SECTION.

Part: SKIN — DENTED (FWD PAX DOOR) · airframe 38,255 hrs · 41,537 cycles

FORWARD PASSENGER DOOR HAS A DENT ON EXTERNAL SKIN JUST AFT OF FORWARD VERTICAL FRAME BETWEEN #1 AND #2 HORIZONTAL BEAM -- REMOVED DAMAGED AREA, FABRICATED FAIRING, DOUBLER AND TAPERED SHIM. LOCATED, DRILLED AND INSTALLED REPAIR.

Part: ANGLE — CRACKED (AFT CARGO DOOR) · airframe 38,255 hrs · 41,537 cycles

AFT CARGO DOOR AFT LOWER STOP FITTING ATTACH ANGLE CRACKED -- REMOVED, DRILLED UP NEW ATTACH ANGLE AND INSTALLED NEW LOWER STOP FITTING.

Part: INTERCOSTAL — MISDRILLED (AFT CARGO DOOR) · airframe 38,255 hrs · 41,537 cycles

AFT CARGO DOOR LOWER AFT STOP INTERCOSTAL MISDRILLED -- REMOVED, FABRICATED AND INSTALLED INTERCOSTAL.

Part: ATTACH ANGLE — CORRODED (T/E FLAP) · airframe 38,255 hrs · 41,537 cycles

RIGHT HAND WING FLAP NR 8 RIB (COUNTING FROM INBOARD) FORWARD RIB ATTACH ANGLE IS EXFOLIATED. REMOVED, FABRICATED AND INSTALLED NEW ANGLE.

Part: ANGLE — MISDRILLED (AFT CARGO DOOR) · airframe 38,255 hrs · 41,537 cycles

AFT CARGO DOOR LOWER AFT STOP INTERCOSTAL INSTALL INNER ANGLE MISDRILLED -- REMOVED, DRILLED UP AND INSTALLED NEW ANGLE.

Part: ANGLE — CORRODED (R/H FLAP) · airframe 38,255 hrs · 41,537 cycles

RIGHT HAND FLAP HAS EXFOLIATION CORROSION PRESENT ON AN ANGLE THAT CONNECTS A FLAP RIB TO THE LEADING EDGE FLAP SPAR. ANGLE IS LOCATED APPROXIMATELY 24 INCHES INBOARD OF FLAP MIDDLE SUPPORT FITTING -- REMOVED LEADING EDGE RIB TO FACILIATATE OTHER MAINTENANCE. REMOVED, FABRICATED AND INSTALLED ANGLE STIFFENER. INSTALLED LEADING EDGE RIB.

Part: FITTING — CRACKED (MID CARGO DOOR) · airframe 38,255 hrs · 41,537 cycles

MID CARGO DOOR LOWER AFT STOP FITTING TO PAN ATTACH FITTING CRACKED -- REMOVED, LOCATED, DRILLED AND INSTALLED STOP FITTING.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 37,393 hrs · 41,056 cycles

AFTER ENGINE START LEFT GENERATOR DROPPED OFF LINE WITH A/C CROSS TIE LIGHT ON. GENERATOR AND CROSSTIE RESET. REPLACED LEFT GENERATOR CONTROL PANEL, OPERATIONAL CHECK GOOD.

Part: CIRCUIT BREAKER — FAILED (COCKPIT) · airframe 36,929 hrs · 40,813 cycles

WHEEL WELL OVERHEAT SENSOR CIRCUIT BREAKER TRIPPED. CHECK ALL SENSORS FOR OPERATION, REPLACED EFFECTED CIRCUIT BREAKER.

Part: GYRO — FAILED (COCKPIT) · airframe 36,870 hrs · 40,783 cycles

AFTER TAKEOFF, FIRST OFFICERS PFD LOST SKY/GROUND. NUMBER TWO COMPASS FROZE AND NUMEROUS FMA ANNUNCIATORS APPEARED. REMOVED AND REPLACED NUMBER TWO LITTON GYRO. SYSTEM OPERATIONS CHECKS GOOD.

Part: SKIN — CRACKED (PAX DOOR) · airframe 35,837 hrs · 40,200 cycles

FOUND 3/8 INCH CRACK ON LOWER FORWARD CORNER OF PASSENGER DOOR. -- INSTALLED DOUBLER IAW MD80/DC9 SRM (STRUCTURAL REPAIR MANUAL).

Part: SLIDE — DETACHED (SERVICE DOOR) · airframe 35,597 hrs · 40,075 cycles

AFT SERVICE DOOR SLIDE FELL OUT. MAINTENANCE REINSTALLED AFT SERVICE DOOR SLIDE.

Part: NOSE COWL — DENTED (LEFT ENGINE) · airframe 34,934 hrs · 39,718 cycles

MCO - FLT 90 - ON APPROACH, HAD BIRD STRIKE ON LEFT ENGINE INLET. INSPECTED AND FOUND LEFT ENGINE INLET COWL RING DENTED. REMOVED AND REPLACED LEFT ENGINE COWL. (X)

Part: FUEL CONTROL — INOPERATIVE (LT ENGINE) · airframe 34,921 hrs · 39,712 cycles

PHX - FLT 931 - N2 DROPPED TO 40 PERCENT, DISCONTINUED TAKEOFF. REMOVED AND REPLACED FUEL CONTROLLER. (X)

Part: CONTROL BOX — MALFUNCTIONED (ANTI-SKID SYSTEM) · airframe 34,878 hrs · 39,695 cycles

MKE - FLT 5 - 'WHEEL NOT TURNING'. ANNUNCIATOR CAME ON DURING TAKEOFF. DISCONTINUED AT 60 KNOTS. RETURNED TO GATE. MAINTENANCE PERFORMED TROUBLESHOOTING PROCEDURE PER MM 32-43-00. INSPECTED ALL TRANSDUCERS, NO DEFECTS NOTED. REMOVED AND REPLACED ANTI-SKID BOX. (X)

Part: CONNECTOR — LOOSE (CONTROL VALVE)

FLT 930 - MKE - WHEEL NOT TURNING LIGHT CAME ON AT 70-80 KNOTS. ABORTED TAKEOFF AND RETURNED TO GATE. LIGHT WENT OUT AFTER CLEAR OF RUNWAY. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF WHEEL LOCK-UP. ALL TIRES CHECKED NORMAL. FOUND BOTH INBOARD ANTI-SKID CONTROL VALVES. CANNON PLUGS LOOSE. CLEANED AND RECONNECTED. SELF TEST AND OPS CHECK GOOD. (M)

Part: LONGERON — CHAFED (AFT BULKHEAD)

MKE - FOUND LONGERON 18 LEFT CHAFED FROM LEFT THRUST REVERSER HYDRAULIC LINE APPROXIMATELY 10 INCHES AFT OF AFT PRESSURE BULKHEAD. REMOVED DAMAGED LONGERON, AND REPLACED, AND INSTALLED LONGERON. (M)

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 33,955 hrs · 39,225 cycles

FOUND AFT GALLEY DOOR EMERGENCY EVACUATION SLIDE PACK DISLODGED FROM COVER. MAINTENANCE REINSTALLED SLIDE.

Part: SKIN — CRACKED (RT WING)

RIGHT WING LEADING EDGE CRACKED. MAINTENANCE INSTALLED DOUBLER.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 33,261 hrs · 38,902 cycles

AFT GALLEY SERVICE DOOR SLIDE PACK FELL OUT. MAINTENANCE REINSTALLED SLIDE ASSEMBLY.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 33,260 hrs · 38,902 cycles

AFT GALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE DROPPED OUT OF CONTAINMENT PACKAGE. MAINTENANCE REINSTALLED SLIDE PACK.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 33,262 hrs · 38,903 cycles

AFT GALLEY SERVICE DOOR PACK FELL OUT. MAINTENANCE REINSTALLED SLIDE PACK.

Part: SLIDE — LOOSE (GALLEY DOOR)

THE AFT GALLEY SLIDE PACK WAS LOOSE. MTC RESECURED AFT GALLEY SLIDE PACK.

Part: EVAC SLIDE — DETACHED (GALLEY DOOR)

EMERGENCY SLIDE ON AFT GALLEY DOOR NEEDS TO BE RESECURED TO SLIDE DOOR ASSEMBLY. INSTALLED AFT GALLEY SLIDE DOOR.

Part: COVER — LOOSE (DOOR SLIDE)

THE AFT GALLEY DOOR SLIDE COVER CAME LOOSE. MTC RESECURED THE AFT GALLEY SLIDE COVER.

Part: SKIN — CRACKED (CABIN DOOR)

FORWARD ENTRANCE DOOR SKIN AROUND HOLD OPEN HOOK IS CRACKED AND HAS SCRATCHED SKIN WHERE HOOK ENGAGES. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.

Part: BATTERY PACK — DISCHARGED (EMER EXIT DOOR)

LEFT AND RIGHT OVERWING EMERGENCY LIGHT INOP. REPLACED EMERGENCY EXIT BATTERY PACK.

Part: EFIS — INOP (LT COCKPIT)

THE CAPTAINS NAVIGATION DISPLAY IS BLANK ON BOTH ON 1 AND BOTH ON 2. MAINTENANCE REMOVED AND REPLACED CAPTAINS EFIS DISPLAY UNIT.

Part: COVER — LOOSE (GALLEY DR SLIDE)

LOOSE RETAINING PINS ON BOTTOM OF AFT GALLEY SERVICE DOOR SLIDE COVER. ADJUSTED RETAINER PINS AND SLIDE COVER.

Part: DOUBLER — CRACKED (COCKPIT)

FOUND COUNTER SINK CRACKS ON STEEL DOUBLER AT UPPER AFT CORNER OF RIGHT CLEARVIEW RETAINER. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.

Part: SKIN — OUT OF LIMITS (LEFT WING)

THE LEFT WING LOWER SKIN AFT SPAR AT XRS 477 HAS A BLEND OUT REPAIR. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.

Part: FRAME — CORRODED (BS 1385)

FRAME AT STATION 1385 HAS MODERATE CORROSION AT LONGERON 24R TO 27R. MTC FABRICATED AND INSTALLED FORMER.

Part: ANGLE — CORRODED (BS 1380)

THE FRAME AT STATION 1380 TO SKIN ATTACH ANGLE HAS MODERATE CORROSION. MTC FABRICATED AND INSTALLED NEW TEE.

Part: SKIN — OUT OF LIMITS (RIGHT WING)

RIGHT LOWER WING SKIN AT AFT SPAR IN BETWEEN 2 EXISTING DOUBLERS JUST OUTBOARD OF INBOARD FLAP ACTUATOR HAS BLEND OUT EXCEEDING LIMITATIONS. MTC FABRICATED AND INSTALLED DOUBLERS.

Part: INTERCOSTAL — CORRODED (BS 1407)

THE INTERCOSTAL AT FS 1407 AT LONGERON 24L HAS MODERATE CORROSION. MTC FABRICATED AND INSTALLED INTERCOSTAL FRAME.

Part: FRAME — CORRODED (BS 1474)

FOUND CORROSION ON LEFT CARTED FRAME AT STATION 1474. MTC FABRICATED AND INSTALLED NEW FRAME.

Part: JAMB — CORRODED (VENTRAL STAIRWAY)

THE AFT VENTRAL STAIRWAY FORWARD LEFT JAMB HAS MODERATE CORROSION AT FORWARD END. MTC FABRICATED AND INSTALLED NEW ANGLE.

Part: LONGERON — CORRODED (BS 1338-1401)

FOUND CORROSION ON LONGERON 24L AT STATION 1338 TO 1401. MTC FABRICTED AND INSTALLED NEW LONGERON.

Part: INTERCOSTAL — CORRODED (BS 1380-1395)

THE INTERCOSTAL HAS MODERATE CORROSION FROM STATION 1380 TO 1395. MTC FABRICATED AND INSTALLED INTERCOSTAL.

Part: WEB — CORRODED (BS 1401)

FOUND CORROSION AT STATION 1401 FRAME AND FRAME TO SKIN ATTACH ANGLE. MTC FABRICATED AND INSTALLED FRAME WEB.

Part: INTERCOSTAL — MISREPAIRED (BS 1380)

FOUND PREVIOUS REPAIR ON INTERCOSTAL FROM STATION 1380 TO 1395 AT L28L. MTC FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: SKIN — DAMAGED (BS 562)

FUSELAGE SKIN CREASE FROM STATION 562 TO 601 BELOW LONGERON 20R EVALUATED TO CONDITION 2 OF TABLE C IN DC-9 SRM. MTC FABRICATED AND INSTALLED REPAIR DOUBLERS.

Part: FITTING — CORRODED (BS 1325)

SHOVEL CLIP AT FS 1325 AT L24L IS CORRODED BEYOND LIMITS. MTC FABRICATED AND INSTALLED NEW SHOVEL CLIP FITTING.

Part: FRAME — MISDRILLED (BS 927)

FOUND A MISDRILLED HOLE ON FRAME AT FUSELAGE 927 AT L5L. MAINTENANCE FABRICATED AND INSTALLED BUSHING AND REPAIR DOUBLER.

Part: LONGERON — CRACKED (BS 1309)

FOUND CRACK ON LONGERON 8 RIGHT AT STATION 1309. MTC FABRICATED AND INSTALLED NEW LONGERON AND SPLICE.