N814NK

Part: LANDING GEAR — VIBRATION (NLG)

AC SHIMMY VERY EXTREME ON LANDING ROLL OUT WHEN BRAKING BETWEEN 60-65 KTS, AC TAIL SWAP WITH 832NK. BLED ALL 4 BRAKES, CHECKED TORQUE VALUES OF ALL 4 MAIN TIRE AXLE NUTS. ALL CHECKED GOOD. NOTE: NR2 BRAKE AFT BLEEDER EMITTING AIR BUBBLES, PURGED AIR FROM SYSTEM. PERFORMED HIGHT DRAG/SIDE LOADS OR UNUSUAL GROUND HANDLING CONDITIONS, NO DEFECTS NOTED. CHECKED NLG TORQUE LINKS UPPER AND LOWER BUSHINGS FOR WEAR-FOUND WITHIN LIMITS. PERFORMED ANTI-SKID SYSTEM MAINT PRACTICES, OPS CHECK GOOD. INSPECTED NLG FOUND FLUID LEVEL LOW AND SCHRADER VALVE DEFECTIVE, SERVICED STRUT AND INSTALLED NEW VALVE, LEAK AND OPS CHECK GOOD. (K)

Part: ACTUATOR — WORN (NLG STEERING)

FLT 461, AFTER LANDING ROLL OUT, AIRCRAFT SHOOK VERY HARD UNTIL AIRCRAFT REACHED 5 TO 10 KTS, UNABLE TO TELL IF IT WAS NOSE OR MAIN WHEEL SHIMMY, AIRCRAFT TAIL SWAP WITH 802. INSPECTED NLG FOUND BOTH STEERING ACTUATORS HAD PLAY. REMOVED AND REPLACED BOTH STEERING ACTUATORS. OPS CHECK NORMAL.

Part: METER — FAILED (COCKPIT)

METER SEL AND HEAT INDICATION GOES RANDOMLY FROM FULL CURRENT (PEGGED) ON ALL SETTINGS EXCEPT "CAPT" "FO" AND "AUX" TO SOMETIMES JUST "RUD LIM" TO SOMETIMES JUST OFF PEGGED, AIRCRAFT TAIL SWAP WITH N835NK. REMOVED AND REPLACED METER SEL AND HEAT SWITCH, OPS CHECK GOOD. NO OTHER DEFECTS NOTED. (M)

Part: AUTOTHROTTLE SYS — MALFUNCTIONED (COCKPIT)

FLL - F/O AND F/A SMELLED A POSSIBLE ODOR OF SOMETHING BURNING, AIRCRAFT ALSO HAD WINDSHEAR WARNING ON INBOARD AND AUTO THROTTLES DID NOT KEEP UP WITH SELECTED SPEED, AIRCRAFT TAIL SWAP WITH 825. RAN ENGINES AT VARIOUS POWER SETTINGS WITH ALL ELECTRICAL SYSTEMS, OPERATED BOTH PACKS AND APU NO ABNORMALITIES OR ODORS. PERFORMED FAULT REVIEW ON STP FOR WINDSHEAR COMP. NO FAULTS FOUND, COULD NOT DUPLICATE. RAN RTS ON BOTH DFGC, BOTH PASS, NO FAULTS NOTED. (M)

Part: ENGINE — MALFUNCTIONED (LEFT)

LOST OIL IN LT ENGINE, QTY 0, PRESSURE 40 PSI, TEMP RISING, SHUT DOWN LT ENGINE BEFORE LOSING ALL OIL PRESSURE, OIL PRESSURE BELOW 10 PSI WHILE WINDMILLING. REMOVED AND REPLACED NR1 ENGINE. (K)

Part: BEARING — FAILED (SCAVENGE PUMPSCA)

ENGINE WAS REMOVED FROM AC, NR1 POSITION FOR REPORTED LOSS OF OIL QUANTITY IN FLIGHT. THE ENGINE WAS SHUTDOWN IN-FLIGHT. INCOMING INSPECTION REVEALED OIL IN THE TAILPIPE AND TURBINE AREA. DISASSEMBLY REVEALED A FAILED BEARING IN THE NR 4 AND NR 5 SCAVENGE PUMP, RESULTING IN OIL PUMP SEIZURE AND LOSS OF OIL SCAVENGING ABILITY. THE PUMP AND BEARING TIME, TIME SINCE OVERHAUL IS UNKNOWN.

Part: LANYARD — DISCONNECTED (L2 SLIDE)

L2 DOOR SLIDE DEPLOY LANYARD CABLE DISCONNECTED. RECONNECTED DEPLOY LANYARD TO GIRT BAR RECEPTACLE.

Part: SKIN — CORRODED (FUSELAGE)

RADIO ALTIMETER ANTENNA HAS CORROSION AT SKIN. REMOVED ANTENNA DOUBLER. LOCATED AND DRILLED NEW DOUBLER. INSTALLED DOUBLER ANTENNA.

Part: CARGO TRACK — CORRODED (CARGO BAY)

FWD PIT RT CARGO TRACK CORRODED IN NUMEROUS AREAS. CUT OUT DAMAGED CARGO TRACK. FABED NEW SPLICE REPAIR. DRILLED AND LOCATED NEW REPAIR. INSTALLED CARGO TRACK REPAIR.

Part: PAN — CORRODED (CARGO DOORWAY)

FWD PIT, LOWER DOOR JAMB PAN NUMEROUS AREAS OF CORROSION. REMOVED LOWER SECTION OF DOOR JAMB PAN. DRILLED AND LOCATED NEW DOOR JAMB. INSTALLED DOOR JAMB SEC AND SPLICES.

Part: LANYARD — MISROUTED (TAILCONE)

FLL - INSPECT TAILCONE FOR PROPER INSTALLATION DUE OT PREVIOUS ITEM 262316-1. FOUND KEVLAR LANYARD IMPROPERLY ROUTED, RE-ROUTED TAILCONE KEVLAR LANYARD AND INSPECTED TAILCONE INSTALLATION. (M)

Part: CONNECTOR — DAMAGED (NLG UNSAFE LIGHT)

DTW - FLT 1923 - INTERMITTENT NLG UNSAFE LIGHT ON ARRIVAL. FOUND PUSHBACKED PIN 'B' ON CONNECTOR R5-1157. RESEATED AND RESECURED PUSHBACKED PIN 'B' ON CONNECTOR R5-1157. PERFORMED BITE, OPS CHECK ON PSEU. BITE OPS CHECK OK. NO FAULTS NOTED ON NLG DOWNLOCK SENSOR. (M)

Part: DOWNLOCK SENSOR — FAILED (MLG)

LGA - FLT 706 - UNSAFE NOSE GEAR LIGHT STAYED ON WHEN GEAR HANDLE DOWN PIN WAS EXTENDED. FOUND NOSE GEAR SENSOR DOWN LOCK FAILED. REMOVED AND REPLACED NOSE GEAR DOWN SENSOR AND OPS CHECK GOOD, GEAR SWING GOOD. (M)

Part: SMOKE GOGGLES — CRACKED (COCKPIT)

DTW - FIRST OFFICERS SMOKE GOGGLES CRACKED. REPLACED FIRST OFFICERS SMOKE GOGGLES. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

AFTER LANDING, RIGHT AFT LAV CALL BUTTON DINGING CONSTANTLY. REMOVED AND REPLACED RIGHT AFT LAVATORY SMOKE DETECTOR. OPS CHECK GOOD. NO OTHER DEFECTS NOTED. (M)

Part: SIGN — MISSING (G4 GALLEY)

SAFETY GLO 'EXIT SIGN' LOCATED AT G4 GALLEY IS MISSING. RE-INSTALLED SAFETY GLO 'EXIT' SIGN LOCATED AT G-4 GALLEY. (M)

Part: STUD — INOPERATIVE (GROUND)

BOTH OVERHEAD EMERGENCY LIGHTS AT STA 636 ARE INOPERATIVE. REMOVED AND REPLACED GROUND STUDS 5221 AND 5222.

Part: PANEL — DAMAGED (FUSELAGE)

RIGHT OUTBOARD LOWER WEDGE PANEL UPPER SIDE HAS DENT/ GOUGE. CUT OUT DAMAGED SKIN. FABRICATED REPAIR DOUBLER. MATERIAL SUBSTITUATION FOR FILLER AND DOUBLER FROM 2014T6 TO 7075T6. INSTALLED REPAIR DOUBLER AND FILLER.

Part: FLOORBOARD — BROKEN (FUSELAGE)

FLOORBOARD (CABIN) AT STA 826-886 (CENTER) FWD LT CORNER BROKEN. REMOVED DAMAGED CORRECTED ON FLOORBOARD. FABRICATED NEW COVER. INSTALLED NEW COVER.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD LAV PARTITION MODULE ASSEMBLY CORRODED AT LOWER BASE PANEL SUPPORT. FABRICATED NEW FLOOR PANEL SUPPORT.

Part: WEB — DAMAGED (FUSELAGE)

CORRODED WEB AT L18R FS 769-788, FS 788-807, FS 826-845 AND FS 886-905. FS 788-807, FS 826-845 AND FS 881-905 FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA AT L18R STA 826 TO 845. CUT OUT DAMAGED AREA AT L18R STA 886-905. CUT OUT DAMAGED AREA AT L18R STA 788-807. FABRICATED 3 EA DOUBLERS. INSTALLED 3 EA DOUBLERS.

Part: WEB — CORRODED (FUSELAGE)

CORRODED WEB L18R AT FS 256-313, FS 503-522, FS 541-560, AND FS 674-712. MAT ON FS 275-313 IS OUT OF LIMITS. CUT OUT DAMAGED AREA. FORMED NEW DOUBLER REPAIR. INSTALLED NEW DOUBLER REPAIR.

Part: FRAME — CRACKED (FUSELAGE)

CANT 1474 LEFT IN AFT ACCESSORY COMPARTMENT CRACKED FRAME. STOP DRILLED CRACK. FABRICATED DOUBLERS. INSTALLED ANGLE REPAIR.

Part: FRAME — GOUGED (FUSELAGE)

FRAME IS GOUGED AND CRACKED STA 207 BETWEEN STR 5L-6L. FABRICATED REPAIR DOUBLERS. INSTALLED REPAIR DOUBLERS.

Part: INTERCOSTAL — DAMAGED (FUSELAGE)

PAX CABIN FLOOR INTERCOSTAL CRACKED AT FS 1041 OBL. REMOVED DAMAGE INTERCOSTAL. FABRICATED NEW INTERCOSTAL. INSTALLED NEW INTERCOSTAL.

Part: WEB — CORRODED (FUSELAGE)

RT FUSELAGE STA 927 TO 946 CUSP WEB CORRODED. CUT OUT DAMAGED WEB SECTION. FABRICATED NEW WEB SECTION AND DOUBLER. INSTALLED NEW WEB SECTION AND DOUBLER.

Part: PANEL — CHAFED (VERTICAL STAB)

FOUND RIGHT VERTICAL STAB ACCESS PANEL CHAFING ON INTERIOR. FABRICATED DOUBLER. LOCATED AND DRILLED DOUBLER. INSTALLED DOUBLER. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

CABIN FLOORBOARD STA 1003-1079 DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD.

Part: BULKHEAD — CRACKED (FUSELAGE)

AFT ACC AREA BULKHEAD CRACKED AT STA 1463 CANT APPROX LONGERON 3L. REMOVED 2 PART WEB ASSY. FABBED WEB AND DOUBLER ASSY. INSTALLED WEB AND DOUBLER ASSY.

Part: ANGLE — CRACKED (VERTICAL STAB)

RIGHT INNER DORSAL FIN ANGLE CRACKED AT FS 1437. REMOVED RIGHT DORSAL FIN INNER ANGLE. LOCATED AND DRILLED NEW DORSAL FIN INNER ANGLE. INSTALLED INNER DORSAL FIN ANGLE. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - DENT AT FS 373 BETWEEN LONGERONS 21 AND 22R, DENT IS WITHIN ONE INCH OF FRAME AND REQUIRES REPAIR. CUT OUT DAMAGED SECTION. FABRICATED 4 SKIN AND 6 AND 10 DOUBLERS. INSTALLED REPAIR SKIN AND DOUBLERS. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN STATION 200 TO STATION 180 FLOOR PANEL SOFT/MUSHEY CORRODED AT INSERTS. FABRICATED NEW FLOORBOARD. (M)

Part: FLOOR PANEL — DETERIORATED (FUSELAGE)

FTW - FOUND MAIN CABIN STATION 1041 TO STATION 1060 FLOOR PANEL DETERIORATED. FABRICATED A NEW FLOOR PANEL. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN RIGHT SIDE STATION 200 TO STATION 256, FLOOR PANEL SOFT/MUSHEY DETERIORATED INSERTS CORRODED. FABRICATED NEW FLOORBOARD. (M)

Part: WEB — CORRODED (SUBFLOOR)

FTW - FOUND CORROSION AT E/E CABIN SUBFLOOR FS 207, 24 INCHES RBL. CUT OUT WEB. FABRICATED 1 REPAIR DOUBLER. FABRICATED 1 FILLER. INSTALLED 1 DOUBLER REPAIR AND FILLER IN WEB. (M)

Part: SCREEN — DELAMINATED (NR 1 ENGINE)

NR 2 ENGINE NOSE COWL ACOUSTIC DELAMINATING, 11:00 O`CLOCK AS MARK. REPAIRED NR 1 INLET ACOUSTIC SCREEN.

Part: BALLAST — DIRTY (CABIN)

ORD - FLT 1441 - FLIGHT ATTENDANT REPORTED HOT SMELL ROW 9 A/C RIGHT. TURNED OFF SIDEWALL LIGHTS AND HOT SMELL DISAPPEARED, NO SMOKE OR HEAT WAS OBSERVED IN AREA. INSPECTED BALLAST ABOVE ROW 9 A/C RIGHT AND LEFT SIDE. CLEANED DUST OFF BALLAST. NO DEFECTS NOTED, IAW MD-80 MM 33-21-03. (M)

Part: ODOR — DETECTED (CABIN)

AT FL310, FLIGHT ATTENDANTS REPORTED FUMES IN CABIN. AFTER THIRD CALL, PEOPLE WERE HAVING A HARD TIME BREATHING. NO SMOKE OR FUMES WERE EVIDENT IN THE COCKPIT. PERFORMED OPS CHECK OF BOTH LEFT AND RIGHT PACKS. NO DEFECTS NOTED AT THIS TIME. (M)

Part: LINER — DAMAGED (NR 1 ENGINE)

NR 1 ENGINE ACCOUSTIC LINE DAMAGED 7 O'CLOCK POSITION FORWARD OF THE FUEL DRAIN, 4 INCH BY 4 INCH AREA. NR 1 ENGINE ACCOUSTIC LINER DAMAGE REINSPECT. TRANSFERRED TO C/O 34708-1. REINSPECTED NR 1 ENGINE ACCOUSTIC LINER DAMAGE OK FOR CONT SERVICE. C/O STILL ACTIVE. REMOVED AND REPLACED NR 1 ENGINE IAW MD80 MM 71-10-00. (M)

Part: WIRE — LOOSE (CABIN)

DTW - FOUND TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT DISCONNECTED. CONNECTED WIRING FOR TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL. (M)

Part: CONTROL BOX — MALFUNCTIONED (ANTI SKID SYSTEM)

DTW - FLT 909 - AT 80 KIAS ON TAKEOFF WHEEL NOT TURNING LIGHT CAME ON ABORTED TAKEOFF. REMOVED AND REPLACED ANTI-SKID CONTROL BOX. BITE TEST AND SYSTEM CHECK OK IAW MD80 MM 32-43-00. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

FTW - AFT CARGO COMPARTMENT JAMB AREA PLATE HAS CORROSION BETWEEN STATION 1155, 1211. FOUND CORROSION TO BE OUT OF LIMITS IAW MD80 SRM 53-01. REMOVED CARGO DOOR JAMB BEAM. INSTALLED NEW AFT CARGO DOOR JAMB BEAM IAW MD80 SRM 51-30-5. (M)

Part: WIRE — BROKEN (AUTOTHROTTLE SYS)

FLT 874 - LAX - AUTO THROTTLE INOPERATIVE ON TAKEOFF AND WOULD NOT ENGAGE. REPAIRED BROKEN WIRE AT 330-59 NR 4, AUTO THROTTLE SYSTEM, OPS CHECK GOOD. RTS ON BOTH NR 1 AND NR 2 CHECKED GOOD. (M)

Part: PLATE — DAMAGED (ELEVATOR)

FTW - RIGHT ELEVATOR INBOARD L/E UPPER PLATE ROD BENT AND CRACKED POPOUT THROUGH THE HEAD OF RIVET AS MARKED. REMOVED PLATE FORM NEW PLATE. LOCATED AND DRILLED. INSTALLED NEW PLATE IAW MD-80 SRM 51-30-2. (M)

Part: BATTERY — DISCHARGED (CABIN)

FTW - FOUND LEFT AND RIGHT LOW OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED BATTERY POWER SUPPLY. INSTALLED BATTERY POWER SUPPLY IAW MD80 MM 33-53-00. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FTW - FOUND 4 OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED BATTERY PACK. INSTALLED BATTERY POWER SUPPLY IAW MM 33-50-00 SYSTEM OP CHECKS GOOD. (M)

Part: SUPPORT — CORRODED (FWD LAVATORY)

FTW - FORWARD LAVATORY SIDE WALL UNATTACHED AND CORRODED AT LOWER AREA. FABRICATED PART IAW SRM MD80 51-10-2. PRIOR TO LINE 1 REMOVED 2 CORRODED SUPPORTS IAW MD 80 SRM 51-30-0. INSTALLED 2 SUPPORTS IAW MD80 SR 51-30-01. (M)

Part: FLOOR SUPPORT — BROKEN (FUSELAGE)

FTW - FOUND FLOOR SUPPORT AT STATION 1136 BETWEEN LONGERONS 28L TO 28R BROKEN IN HALF. REMOVED FLOOR SUPPORT PER SRM MD80 51-30-2. LOCATE AND DRILLED NEW FLOOR SUPPORT PER MD80 SRM 51-10-4. INSTALLED FLOOR SUPPORT AT STATION 1136 BETWEEN LONGERONS 28L TO 28R IAW MD80 SRM 51-30-5. (M)

Part: BRACKET — CORRODED (FUSELAGE)

FOUND E/E COMPARTMENT STATION 150, CORRODED ANGLE AT STATION 150 FRAME AND OUTBOARD SIDE OF AFT LOCKING PIN (RT) HOLE IN DOOR FRAME. REMOVED T-BRACKET. INSTALLED NEW T-BRACKET IAW MD80 SRM 51-30-5. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENTS AT FUSELAGE STATION Y218 BETWEEN LONGERON 7L AND 8L. REWORKED DENT TO ORIGINAL CONTOUR IAW MD80 SRM 53-04 FIG 38 CHECK AREA FOR CRACK IAW NDT MANUAL 08-00-00. NO CRACK FOUND IAW NDT MANUAL 08-00-00. FABRICATED DOUBLER IAW MD80 SRM 53-04 FIG 38. INSTALLED NEW REPAIR IAW MD80 SRM 53-04. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

FTW - A .100 INCH DIAMETER HOLE IN FLOOR SUPPORT CHANNEL AND FLOOR AT FS 197 BL 55 LEFT. AREA FOUND TO BE OUT OF LIMITS PER MD80 SRM 53-01-0. FABRICATED NEW DOUBLER PER MD80 SRM 53-01 AND 51-10-4. INSTALLED DOUBLER PER MD80 SRM 53-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - R1 DOOR FLOORBOARD SUPPORT CORRODED. PARTS FOUND TO BE OUT OF LIMITS IAW MD80 SRM 51-10-03. FABRICATED AND DRILLED PARTS IAW SRM 51-10-02, 51-10-04. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - EVIDENCE OF DENT LOCATED APPROXIMATELY STATION 579 L20R C/O 97165-4. REWORKED DENT TO ORIGINAL CONTOUR IAW MD80 SRM 53-04 FIG 38. CHECK AREA FOR CRACK IAW NDT MANUAL 08-00-00. NO CRACK FOUND IAW NDT MANUAL 08-00-00. FABRICATED DOUBLER REPAIR IAW MD80 SRM 53-04. INSTALLED NEW REPAIR IAW MD80 SRM 5-04 FIG 38. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - PASSENGER CABIN SEAT TRACK HAS CORROSION AND BARE METAL IN SEVERAL PLACES AT FS 927-1136. UPON FURTHER EVALUATION, FOUND TO BE OUT OF LIMITS WITH PITS STILL EXISTING IN TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK IAW MD80 SRM 53-05. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FLOOR SUPPORT ANGLE AT AFT LOWER CORNER OF L1 DOOR CORRODED, FS 200L, BL 55L. REMOVED CORROSION IAW MD80 SRM 51-10-3. FABRICATED FLOOR SUPPORT PER SRM MD80 51-10-2. INSTALLED FLOOR SUPPORT IAW MD80 SRM 51-10-3. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD LOWER CARGO COMPARTMENT CORRODED AT RIGHT FLOOR SUPPORT, ABOVE STRINGER 29 RIGHT STATION 408 TO STATION 427. REMOVED CORROSION, REMOVED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW MD-80 SRM 51-10-04. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - PASSENGER CABIN SEAT TRACK HAS CORROSION AT FS 200-408 AT X-18 INCHES. REMOVED CORROSION. REMOVED SEAT TRACK FROM STATION IAW MD-80 SRM 53-04. INSTALLED NEW SEAT TRACK IAW MD-80 SRM 53-04. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

FTW - AFT CARGO FLOOR SUPPORT HOLE ELONGATED AND SURFACE CORROSION STATION 1322 L29. ELONGATED HOLE FOUND TO BE OUT OF LIMITS IAW MD-80 SRM 51-10-04. FABRICATED DOUBLER. INSTALLED DOUBLER ON FLOOR SUPPORT AT STATION 1322 L29 IAW MD80 SRM 51-30-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - PASSENGER CABIN SEAT TRACK HAS CORROSION AND BARE METAL IN SEVERAL PLACES AT FS 1174-1287 AT X PLUS 36 INCHES. REMOVED CORROSION IAW MD80 SRM 53-01. REMOVED CORRODED SECTION STATION 1184 TO 1141 IAW SRM MD80 53-05. INSTALLED COMPLETE SEAT TRACK SECTION FROM STATION 1184 TO 1241 AND 2 SPLICES IAW SRM MD80 53-05. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FUSELAGE SKIN HAS 6 DENTS IN NORM MORE THAN 10 INCHES STATION 351, 360 BETWEEN LONGERON 4 AND 5 RIGHT. REWORKED DENT TO ORIGINAL CONTOUR IAW MD80 SRM 53-04 FIG 38 CHECKED AREA FOR CRACK IAW NDT MANUAL 08-00-00. NO CRACK FOUND IAW NDT MANUAL 08-00-00. FABRICATE DOUBLER IAW MD80 SRM 53-04. INSTALLED NEW DOUBLER REPAIR IAW MD80 SRM 53-04 FIG 38. (M)

Part: WEDGE — DELAMINATED (T/E FLAP)

RIGHT WING, INBOARD FLAP INBOARD OUTBOARD TRAILING EDGE DELAMINATION. REMOVED 2 INBOARD FLAP TRAILING EDGE WEDGES. INSTALLED NEW WEDGES IAW MD-80 SRM 51-30-07. (M)

Part: SLIDE — IMPROPER (TAIL CONE)

FTW - TAILCONE EMERGENCY EVACUATION SLIDE PACKED IMPROPERLY. REMOVED TAILCONE EMERGENCY EVACUATION SLIDE, INSTALLED EMERGENCY EVACUATION SLIDE IAW MD-80 25-62-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - PASSENGER CABIN SEAT TRACK HAS CORROSION AND BARE METAL IN SEVERAL PLACES AT FS 1174-1287 AT X PLUS 18 INCHES. REMOVED CORROSION IAW MD80 SRM 51-10-3. REMOVED DAMAGE SEAT TRACK. INSTALLED SEAT TRACK IAW MD80 SRM 51-30-1. (M)

Part: PLATE — CRACKED (ELEVATOR)

FTW - FOUND LEFT ELEVATOR PAINT PEELING OFF AND BARE METAL INBOARD SIDE. FOUND CRACK AT INBOARD LEADING EDGE PLATE. REMOVED CRACKED PLATE FROM LEFT ELEVATOR. FABRICATED NEW PLATE. INSTALLED PLATE IAW MD80 SRM 51-20-0 AND 51-30-2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - PAX CABIN SEAT TRACK HAS CORROSION AT FS 200-408 AT X-36 INCHES. FOUND OUT OF LIMITS AT STATION 237.5 IAW MD80 SRM 53-05. FABRICATED AND INSTALLED SEAT TRACK AT STATION 237.5 AND 408 IAW MD80 SRM 51-10-7. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FLOOR SUPPORT CORRODED, FS 168R, BL 11R. REMOVED CORROSION ON FLOOR SUPPORT FS 168R, BL 11R IAW MD80 SRM 53-01. FABRICATED NEW FLOOR SUPPORT FS 168R, BL 11R IAW MD80 SRM 53-01. INSTALLED NEW FLOOR SUPPORT FS 168R, BL 11R, IAW MD80 SRM 51-30-2. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

FTW - CENTER LOWER CARGO COMPARTMENT CORRODED AT LOWER CUTOUT DOOR JAMB FROM STATION 635 TO STATION 693. REMOVED CORROSION ON JAMB. REMOVED JAMB BEAM. INSTALL NEW JAMB BEAM IAW MD-80 SRM 51-30-02. (M)

Part: DRIVE UNIT — WORN (HORIZ STAB)

FOUND HORIZONTAL STABILIZER DRIVE ACME DRIVE AND NUT WEAR OUT OF LIMITS. REMOVED ACME SCREW ASSY FROM LONGITUDE ACTUATOR. INSTALLED ACME SCREW AND NUT ASSY IAW MD80 MM 27-40-01. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - AFT CARGO LONGERON NR 22 RIGHT HAS CORROSION BETWEEN STATION 1309 AND 1322. REMOVED CORROSION. CORROSION OUT OF LIMITS. CUT OUT DAMAGE SECTION OF LONGERON FROM STATION 1297. LOCATED AND DRILLED LONGERON AND FITTINGS IAW MD-80 SRM 53-20-00. (M)

Part: SKIN — CRACKED (CARGO DOOR)

FORWARD CARGO DOOR SKIN AROUND HANDLE IS BENT. STRAIGHTENED SKIN TO ORIGINAL COUNTER, FOUND CRACK TO SKIN. FABRICATED DOUBLER IAW MD-80 SRM 52-05. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FLOOR SUPPORT CORRODED, FS 1338, APPROX BL 45R TOP OF SUPPORT, RIGHT AFT LAVATORY AREA. REMOVED CORROSION IAW MD80 SRM 51-10-3, FLOOR SUPPORT REPLACEMENT WILL BE ACCOMPLISHED ON N/R CARD. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND FLOOR SUPPORT, LEFT AFT LAVATORY AREA, CORRODED TWO PLACES, FS 1338L, APPROX BL24L AND BL60. REMOVED FLOOR SUPPORT IAW MD80 SRM 51-30-2 AND 51-30-5. FABRICATED ANGLE SUPPORT AND INSTALLED PER MD80 SRM 51-30-2 AND 51-30-5. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - PASSENGER CABIN SEAT TRACK HAS CORROSION IN SEVERAL PLACES AT FS 503-674. REMOVED CORROSION. LOCATED AND DRILLED NEW SEAT TRACK IAW MD-80 SRM 51-10-04 AND 53-05. (M)

Part: NOSE COWL — ERODED (RT ENGINE)

FTW - RIGHT NOSE COWL 12 O'CLOCK POSITION HAS DENT AND ERODED BETWEEN 10 AND 2 O'CLOCK. DENT MEASURES 3.50 INCH SPAN BY 1.8 INCH CHORD TO .140 INCH OUT OF LIMITS PER MD80 SRM 54.04A. RIGHT ENGINE NOSE COWL REPLACED WITH SERVICEABLE P/N SQ30645-5093N001919 CHORD B016-7-N-0009. (M)

Part: WEDGE — OUT OF ADJ (T/E FLAP)

FTW - FOUND INBOARD FLAP LEFT, INBOARD TO OUTBOARD SECTIONS ARE OUT OF ALIGNMENT. REMOVED TRAILING EDGE WEDGE. INSTALLED NEW TRAILING EDGE WEDGES IAW MD-80 SRM 51-30-02. (M)

Part: SKIN — CHAFED (LT WING)

FTW - LEFT WING L/E TOP SIDE OUTBOARD SLAT IS CHAFING. FOUND TO BE OUT OF LIMITS. LOCATE AND DRILL WING OUTBOARD L/E SUPPORT. INSTALLED O/B, L/E SUPPORT IAW MD80 SRM 51-30-2. (M)

Part: SKIN — DELAMINATED (RUDDER)

FTW - FOUND LEFT SIDE OF RUDDER HAS DELAMINATED IN MANY PLACES. REMOVED DAMAGED AREAS OF DELAMINATED. REPAIRED LEFT SIDE OF RUDDER IAW BOEING. BALANCED RUDDER PER SRM 55-40-01. (M)

Part: TAB — DENTED (ELEVATOR)

FTW - RIGHT ELEVATOR GEAR TAB HAS MANY DENTS. CLEANED DENTS. REPAIRED DENTS ON RIGHT ELEVATOR GEAR TAB IAW MD-80 SRM 55-04. (M)

Part: SKIN — DENTED (ELEVATOR TAB)

FTW - RIGHT ELEVATOR CONTROL TAB HAS MANY DENT (TOP SIDE). CLEANED DENT AREAS 6 ON RIGHT INBOARD ELEVATOR CONTROL TAB IAW DC9/MD-80 SRM 55-04 PAR 5B. REPAIRED DENTS ON RIGHT ELEVATOR CONTROL TAB IAW DC9 MD80 SRM 55-04. (M)

Part: TERMINAL — BROKEN (WARNING HORN)

FTW - APU FIRE WARNING HORN WILL NOT SOUND DURING SYSTEM TEST. REPLACED BROKEN TERMINAL LUG FOR HORN GROUND. OPS CHECK GOOD PER MD-80 MM 26-10-00. (M)

Part: COMPUTER — FAULTY (COCKPIT)

FTW - ALTITUDE SELECTOR ON DFGCP IS INTERMITTENT. REMOVED DFGCP IAW MD80 MM 22-01-02. INSTALLED DFGCP IAW MD80 MM 22-01-02. DFGS RTS WILL BE ACCOMPLISHED ON C-CHECK CARD B16-09R-01. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT LEFT FUSELAGE AFT OF L1 DOOR (3FT) DENT IS 2 INCHES BY 3 INCHES BY 0.080. CUTOUT DAMAGED AREA. FORMED FINGER DOUBLER. FORMED SKIN PLUG. INSTALLED DOUBLER AND SKIN PLUG IAW MD80 SRM 51-10-31. (M)

Part: LOCK — CORRODED (CARGO DOOR)

AFT CARGO COMPARTMENT DOOR FORWARD AND AFT LOCKING MECH ARE OXIDIZED. REMOVED OXIDATION AFT CARGO DOOR FORWARD LOCKING MECH MATERIAL LOST FOUND TO BE OUT OF LIMIT IAW MD80 SRM 52-01. REMOVED AND REPLACED TUBE LOCKING MECH IAW MD80 MM 52-31-00. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND FUSELAGE SKIN DENT AT STATION 351 LONGERON 24 DEPTH .03. CUT OUT DAMAGED AREA IAW MD80 SRM 53-04. FABRICATED FINGER DOUBLER AND FILLER. INSTALLED REPAIR IAW MD80 SRM 53-04. (M)

Part: GYRO — FAULTY (NR 2)

FLL - FLT 41 - AUTO PILOT JERKS UP AND DOWN IN PITCH MODE (UNCOMFORTABLE) IN EITHER DFGC 1 OR 2 WHEN VERTICAL GYRO SW SET AT RIGHT ON AUXILIARY, AUTO PILOT VERY SMOOTH BOTH 1 AND 2 DFGC. REMOVED AND REPLACED NR 2 VERTICAL GYRO, OPS CHECK NORMAL IAW MM 34-23-00 AND RIGHTS CHECK ACCOMPLISHED OK IAW MM 22-01-05. (M)

Part: AUTOTHRUST SYS — MALFUNCTIONED (COCKPIT)

FLT 706 - DTW - ON INITIAL CLIMB-OUT AT KLGA, WHEN CL WAS SELECTED ON THE TRC, WITH A/T SYSTEM ENGAGED. LEFT ENGINE CAME BACK TO NORMAL CLIMB POWER SETTING. RIGHT ENGINE VER RAPIDLY CAME BACK TO ALMOST FLIGHT IDLE. THIS HAPPENED SO FAST, UNABLE TO STOP IT IN TIME BEFORE HEAT SYSTEM ACTIVATED. AUTO THROTTLE SYSTEM WAS DISENGAGED AND NORMAL CLIMB POWER WAS OBTAINED BY MANUAL THROTTLES MOVEMENT. AUTOTHROTTLE SYSTEM WAS LATER RE-ENGAGED AND PERFORMED NORMALLY. PERFORMED FUNCTINAL CHECK ON AUTO-THROTTLE SYSTEM, RTS AND FLIGHT FAULT REVIEW. NO FAULTS FOUND. OPS CHECK GOOD PER MD-80 MM 22-01-05. COULD NOT DUPLICATE. (M)

Part: WIRE — DISCONNECTED (CABIN)

EMERGENCY PATH LIGHTING PORTION NO LIGHTS. FOUND DISCONNECTED WIRES AT SEVERAL AREA, RECONNECTED WIRES. OPS CHECK NORMAL. (M)

Part: COVER — BROKEN (CABIN)

ORD - FLT 781 - EMERGENCY EXIT LIGHTING C1 DEF PORTION BROKEN. RE-INSTALLED FLOOR TRACK COVER AT 1 DEF EMERGENCY LIGHT COVER. OPS CHECK OK IAW MM 33-53-01. (M)

Part: TRACK — OUT OF POSITION (CABIN)

FLL - FLT 784 - FLOOR STRIP LIGHTS POPPED UP NEAR ROW 11, WIRES EXPOSED. RESEATED ELT FLOOR STRIP AT ROW 11. OPS CHECK NORMAL AT THIS TIME PER ATA 33-51. (M)

Part: WIRE — BROKEN (CABIN)

DISCREPANCY: EMERGENCY LIGHTS NEED REPAIR IN CABIN. CORRECTIVE ACTION: REPAIRED BROKEN WIRE AT ROW 21 EEL LIGHT. OPS CHECK OK PER M/M 33-53-01.

Part: LIGHT — MISSING (ROW 1)

RSW - FLOOR TRACK LIGHT COVER MISSING AT ROW ONE, WHITE LIGHT. REPLACED MISSING FLOOR TRACK LIGHT COVER IAW MD80 MM 33-33-00. OPS CHECK GOOD, THIS CLEARS DMI 119100-3, MAINTENANCE CONTROL NOTIFIED AND PLACARDS REMOVED. (M)

Part: COVER — MISSING (ROW 1)

DTW - FLT 607 - FLOOR TRACK LIGHT COVER MISSING AT ROW ONE, WHITE LIGHT. REPLACED MISSING FLOOR TRACK LIGHT COVER IAW MD80 MM 33-53-00. OPS CHECK GOOD. THIS CLEARS DMI 119100-3; MAINTENANCE CONTROL NOTIFIED. (M)

Part: COVER — LOOSE (CABIN)

DTW - FLT 606 - EMERGENCY LIGHT COVER FOR FLOOR LIGHTING NEEDS RESECURING. RESECURED EMERGENCY FLOOR LIGHT COVER IAW MD80 MM 33-53-01. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - EMERGENCY TRACK LIGHTS 2 INOPERATIVE FLOOR TRACK LIGHTS OUT AT ROW 25 AND 26. TRANSFERRED TO DMI NR 86885-1 DUE DATE 4/2/200. CAT C, MAINTENANCE CONTROL NOTIFIED, PLACARD INSTALLED. (M)

Part: WIRE — EXPOSED (SEAT 15 & 34)

DTW - EAPL WIRES EXPOSED SEATS NR 15 AND 34. INSTALLED NEW EMERGENCY TRACK AT AISLE NR 15 AND 34. (M)

Part: WIRE — EXPOSED (ROW 28)

DTW - FLOOR TRACK ILGHTING AT ROW 28 HAS GAP AND WIRES EXPOSED. INSTALLED NEW FLOOR TRACK LIGHTING COVER PIECE TO FILL THE GAP IAW MD80 MM 33-50-00. (M)

Part: LENS — MISINSTALLED (CABIN)

FLOOR TRACK LIGHTING AT EMERGENCY EXIT ROWS, RED LIGHTS ARE AT SEATS AND NOT AT ROWS (AISLES). CHANGED WHITE LENS COVERS TO RED IAW MD80 MM 33-50-00. (M)

Part: MASK — WILL NOT TEST (CABIN)

DTW - AFT F/A STATION AND F/A STATION AT G4 GALLEY, 02 MASKS DID NOT DROP ON CHECK. CLEANED AND RESET LATCH ASSEMBLIES. OPS CHECK NORMAL IAW MD80MM 35-20-00. (M)