N801NK

Part: CONTROLLER — FAILED (CABIN TEMP)

AIRCRAFT WOULDN'T HOLD CABIN PRESSURE. CABIN WARNING VOICE FLOW LIGHT ON. LEFT VALVE TEMP FULL HOT (AUTO) REDUCED TEMP BOTH PACKS LEFT PACK ON 30 SEC FLOW LIGHT ON MASK DROPPED. MANUAL MODE ON OUTFLOW VALVE. PERFORMED TEST ON TEMP CONTROLLER SYSTEM WITH TEST BOX. CONFIRMED LEFT CONTROLLER TO BE BAD. REMVOED AND REPLACED TEMP CONTROLLER. OPS CHECKS GOOD. PERFORMED LEAK CHECK OF DUCTING AND PRESSURIZATION CHECK. FOUND NO OTHER DEFECTS NOTED AT THIS TIME. (M)

Part: SLIDE — DISLODGED (L1 DOOR)

DTW - FOUND L1 DOOR SLIDE PACK FELL OFF. INSTALLED L1 DOOR EVACUATION SLIDE. NO DISCERPANCIES NOTED. (M)

Part: SLIDE — OUT OF POSITION (L1 DOOR)

LGA - FLT 705 - SLIDE PACK FELL OFF L-1. FORWARD ENTRY DOOR SLIDE PACK FELL OFF WHEN OPENING DOOR AT ARRIVAL GATE. GIRT BAR LATCH ON THE FLOOR IS VERY DIRTY AND STICKY. REINSTALLED L1 DOOR SLIDE AND CHECKED GIRT BAR LATCHES FOR OPERATION, OPS NORMAL. (M)

Part: BLADE — DAMAGED (NR 2 ENGINE)

ON PREFLIGHT INSPECTION, FOUND FOD DAMAGE TO THE NR 2 ENGINE C-1 BLADES. REMOVED AND REPLACED NR 2 ENGINE. (M)

Part: LINE — LEAKING (ENGINE OIL)

RT ENGINE WAS LOSING OIL PRESSURE AND QUANTITY. FOLLOWED QRH PROCEDURES SHUT DOWN ENGINE. OIL PRESSURE AT SHUTDOWN 30 PSI OIL TEMP AT SHUTDOWN 135 DEGREES, OIL QTY AT SHUTDOWN 5 QUARTS, OIL PRESSURE WINDMILLING 2 PSI, OIL QUANTITY WINDMILLING 4 QUARTS. FOUND CRACKED FLARE AT OIL LINE FROM OIL BYPASS SWITCH. REPAIRED THIS. MOTORIZED ENGINE WITH REMAINING OIL QUANTITY AND ACHIEVED 30 PSI, ALSO REMOVED OIL FILTER NO CONTAMINENTS FOUND AND REPLACED WITH NEW FILER, SERVICED ENGINE OIL TO FULL QUANTITY AND RAN ENGINE. NO LEAKS AND ALL PARAMETERS NORMAL INDICATIONS. (M)

Part: LINER — DAMAGED (NR 2 ENGINE)

NR 2 ENGINE INLET HAS TWO CUTS ON ACCOUSTIC LINING AT 4 AND 6 O`CLOCK POSITION. REPAIRED NR 2 ENGINE INLET ACCOUSTIC LINING. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: PROXIMITY SWITCH — INOPERATIVE (RT MLG)

MYR - FLT 1582 - RIGHT MAIN LANDING GEAR INDICATION ON DEPARTURE. QRH ACCOMPLISHED AND LANDING GEAR RECYCLED GEAR DOOR OPEN LIGHT INTERMITTENTLY ON WITH NO VIBRATION NOTED. RIGHT MLG LIGHT EXTINGUISHED WHEN REACHING 10000 FT ON DESCENT. TROUBLESHOT SYSTEM, FOUND PROXIMITY SWITCH ELECTRONIC UNIT AT FAULT. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. PERFORMED OPS CHECK. NO FAULTS NOTED. (M)

Part: STRIKER — DEFECTIVE (L/E SLAT)

ACY - FLT 311 - UPON SLAT RETRACT, THE SLAT DISAGREEMENT LIGHT CAME ON AND SLAT OVERSPEED WARNING IN FLIGHT. FOLLOWED QRH PROCEDURES RETURNED TO KACY THERE WAS NO ROLL ASYMMETRY, AIRCRAFT WAS STABLE IN FLIGHT. REMOVED AND REPLACED NR 4 SLAT DRIVE DISAGREE PROX STRIKER PLATE IAW MD-80 SRM CH 51-30. (M)

Part: WIRE — CUT (CABIN)

FTW - FOUND ONE AFT STAIRWAY EMERGENCY LIGHT IS INOPERATIVE. TROUBLESHOT FOUND EMERGENCY LIGHT WIRES CUT AT SPLICE POINTS. RESPLICED WIRES. (M)

Part: CONTACTOR — BENT (BATTERY PACK)

FTW - FOUND LEFT AND RIGHT OVERWING EXIT SIGNS INOPERATIVE, UPPER SIGNS ONLY. FOUND BATTERY PACK CONTACT BENT. REALIGNED CONTACT. (M)

Part: BLADE — NICKED (NR 1 COMPRESSOR)

NR 1 ENGINE C1 FAN BLADES ARE ROUGH AND HAVE NICKS. NR 1, SN 718528, FAILED BORESCOPE INSPECTION , C-7 DISK 10 BLADES WITH NICKS AND MISSING MATERIAL. 2 BLADES DAMAGED NEAR TIP (1) MEASURES .140 INCH LONG (2) MEASURES .165 INCH LONG WITH A CRACK PROPAGATING UPWARD FROM UPPER EDGE OF NICK. ENGINE REPLACED.

Part: LONGERON — GOUGED (FUSELAGE)

FTW - AFT ACCESSORY COMP GOUGE ON LONGERON 22L FLANGE, STATION 1380. FABRICATED REPAIR DOUBLER, INSTALLED DOUBLER. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FTW - FOUND STATION 546-552 BETWEEN LONGERON 17R AND 18R, 6 INCHES LONG CREASE IN FUSELAGE SKIN. CUT OUT DAMAGE. FORMED FINGER DOUBLER. FORMED SKIN DOUBLER. INSTALLED FINGER DOUBLER AND FILLER. (M)

Part: SKIN — PUNCTURED (RUDDER TAB)

FTW - FOUND RUDDER TAB HAS PUNCTURE MARK (HOLE) APPROX .25 INCH DIAMETER 3 INCHES ABOVE FIXED TAB. RUDDER TRIM TAB FIXED TAB DEBONDED. THIS TAB REPLACED. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

FTW - FOUND L1 DOOR FRAME HAS CRACK STATION 195 Z67. STOP DRILLED CRACK. (M)

Part: SKIN — GOUGED (FUSELAGE)

DENT AT FS 69 ABOVE RT NLG DOOR. REQUIRES PAINT REMOVAL, DYE PENETRANT INSPECTION FOR CRACKS, EVALUATION, REPAINT AND CARRY OVER LOG ITEM FOR FURTHER INSPECTION. UPON FURTHER INVESTIGATION FOUND SKIN TO BE GOUGED AT DENT LOCATION. AREA FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER, INSTALLED DOUBLER AND FILLER.

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT FS 69 ABOVE RIGHT NOSE GEAR DOOR REQUIRES PAINT REMOVAL, DYE PENETRANT INSPECTION, FOR CRACK EVALUATION. AREA FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER. (M)

Part: SKIN — SCRATCHED (ELEVATOR)

FTW - FOUND LEFT ELEVATOR UPPER SURFACE HAS DEEP SCRATCH. FABRICATED NEW SKIN, DOUBLER AND SPLICE. INSTALLED SKIN, DOUBLER AND SPLICE. (M)

Part: SKIN — SCRATCHED (ELEVATOR)

FTW - FOUND LEFT ELEVATOR SURFACE HAS A DEEP SCRATCH AT STATION XH5-170. REMOVED DAMAGED SECTION OF SKIN. FABRICATED NEW SKIN SECTION, FINGER DOUBLER, STRAP, OUTBOARD INTERNAL DOUBLER, SPLICE. INSTALLED DOUBLER SPLICE, REPAIR SKIN, STRAP, DOUBLER. (M)

Part: PANEL — CORRODED (FUSELAGE)

FTW - AFT FUSELAGE UNPRESSURED INTERNAL, HAS LIGHT CORROSION/BARE METAL AT FORWARD FACE PANEL SUPPORT HOUSING AND CANTED. REMOVED FACE PANEL. FABRICATED NEW FACE PANEL. INSTALLED FACE PANEL. (M)

Part: DOOR FRAME — CRACKED (LT MLG DOOR)

FTW - FOUND LEFT MLG DOOR HAS CRACKED AT FORWARD AFT INBOARD FRAME, ANGLE PREVIOUS REPAIR. CUT OUT DAMAGE. FORMED DOUBLER AND FRAME. INSTALLED NEW FRAME AND DOUBLER. (M)

Part: FLOORBOARD — CORRODED (CABIN)

FTW - AFT CARGO FLOORBOARD STATION 1212-1234 SURFACE CORROSION, GOUGES, DRILL STARTS AND ELONGATED HOLES. REMOVED CORROSION GOUGES, MATERIAL OUT OF LIMITS. FORMED NEW FLOORBOARD. (M)

Part: STRUCTURE — CRACKED (MLG DOOR)

FTW - FOUND LEFT MLG DOOR HAS A CRACK AT FORWARD AFT INBOARD FRAME, ANGLE PREVIOUS REPAIR. CUT OUT DAMAGE. FORMED DOUBLER AND FRAME. INSTALLED NEW FRAME AND DOUBLER. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FTW - FOUND EXTERNAL FUSELAGE SKIN AT STATION 451, LONGERON 22 LEFT IS DAMAGED/GOUGED. CUT OUT DAMAGED AREA. FORMED NEW REPAIR DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT PREVIOUS REPAIR AT FS 1206 BETWEEN LONGERON 27 AND 29L REQUIRES REPAIR TO BE REACCOMPLISHED TO INCLUDE DENT. REMOVED PREVIOUS REPAIR STATION 1206 LONGERON 27-29L. CUT OUT SKIN FOR REPAIR. FABRICATED FILLER AND DOUBLER, EXTERNAL AND FINGER DOUBLRS. INSTALLED REPAIR. (M)

Part: ISOLATION MOUNT — DAMAGED (NR 1 ENGINE)

FTW - NR 1 ENGINE AFT MOUNT ISOLATOR, INNER CONICAL SURFACE HAS NICKS, SCRATCHES AND WORN PLATING. REMOVED NR 1 ENGINE AFT MOUTN ISLOATOR. INSTALLED SVC, NR 1 ENGINE AFT MOUNT ISOLATER. (M)

Part: PIN — DAMAGED (PAX DOOR)

FTW - FOUND DAMAGE AT FORWARD SERVICE DOOR HOLD OPEN PIN REQUIRES REPAIR. FABRICATED DOUBLER. INSTALLED DOUBLER. (M)

Part: ATTACH FITTING — CRACKED (FUSELAGE)

FTW - FOUND PASSENGER CABIN HAS CRACK AT LEFT BRACKET ATTACH TO THE FRAME AND LONGERON 3L STATION 218. REMOVED ATTACH BRACKET. FORMING BRACKET. INSTALLED BRACKET. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND PASSENGER CABIN HAS CRACKED AT THE WEB, UNDER TEE, LBL 14.5 INCHES, STATION 200. REMOVED DAMAGE. FABRICATED REPAIR. INSTALLED DOUBLER. (M)

Part: NOSE COWL — DELAMINATED (NR 2 ENGINE)

FTW - FOUND NR 2 ENGINE, NOSE COWL 4 O'CLOCK TO 8 O'CLOCK POSITION SOUND SUPPRESSION MATERIAL DELAMINATED. REPLACED DAMAGED NOSE COWL. (M)

Part: SKIN — CRACKED (FUSELAGE)

FTW - FOUND CRACK UNDER FORWARD RIGHT SIDE OF LOWER VHF ANTENNA, SKIN, DURING EDDY CURRENT INSPECTION FOUND 2.5 INCH CRACK. FABRICATED SKIN AND DOUBLER. INSTALLED SKIN AND DOUBLER. (M)

Part: FLOORBOARD — CORRODED (CABIN)

FTW - FOUND COCKPIT FLOORBOARD STATION 120-160 CENTER CORRODED AND MISSING INSERTS. FABRICATED NEW PANEL. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND STATION 148 LBL 7, LIGHT CORROSION ON SUB FLOOR WEB WITH SMALL HOLE THROUGH WEB. CUT OUT PUNCTURED AND CORRODED AREA AT STATION 148 LBL 7 FLOOR WEB. FABRICATED DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER ON STATION 148 LBL 7 SUB FLOOR WEB. (M)

Part: NOSE COWL — DAMAGED (NR 3 ENGINE)

FTW - NR 3 ENGINE NOSE COWL DAMAGED SEVERAL DIFFERENT AREAS. REPLACED DAMAGED NOSE COWL. (M)

Part: CHANNEL — CRACKED (FUSELAGE)

FTW - FOUND ANGLE CRACKED AT FS 937 RBL 7 INCHES STRUCTURE BELOW CENTER WING, KEEL BEAM AREA, NEAR AUX HYD PUMP. REMOVED CHANNEL DAMAGED. FABRICATED CHANNEL. LOCATED AND DRILLED ANGLE TWO REPAIR SPLICE AND 1 STRAP. INSTALLED ANGLE TWO REPAIR SPLICE AND 1 SPLICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND L2 DOOR STATION 1146 AND LBL 55 INCHES FLOOR SUPPORT HAS CORROSION AND A SHANK. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT, INSTALLED SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD ENTRY STATION 196 LBL 22-45 SUBFLOOR IS CORRODED UNDER FLOOR BOARD SUPPORT, .500 INCH HOLE THROUGHT SUB FLOOR AT OUTBOARD END, HIDDEN DAMAGE. REMOVED DAMAGED SUB FLOOR SKIN, FABRICATED REPAIR SKIN AND DOUBLER. INSTALLED REPAIR SKIN AND DOUBLER ON STATION 196 LBL 22-45. (M)

Part: SEAT TRACK — CORRODED (FS 1146)

FTW - PASSENGER CABIN RIGHT SEAT TRACK, RBL 44, STATION 1146 HAS CORROSION, SCRATCHES AND GOUGES. REMOVED DAMAGE AREA OF SEAT TRACK FROM STATION 1126 TO 1147. DRILLED AND LOCATED HOLES IN NEW SEAT TRACK AND SPLICES. FABRICATED SEAT TRACK. INSTALLED NEW SEAT TRACK AND SPLICES. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - REMOVAL OF SUPPORT ANGLE SUB FLOOR WAS FOUND TO HAVE EXFOLIATION. CUT OUT DAMAGED AREA. FABRICATED NEW SUB FLOOR SECTION AND DOUBLER. INSTALLED NEW SUB FLOOR AND DOUBLER. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 180 LBL 14-39 FLOORBOARD SUPPORT IS CORRODED. REMOVED SUPPORT. FABRICATED NEW SUPPORT. INSTALLED NEW SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 160-200 LBL 7, FLOOR BOARD SUPPORT IS CORRODED. REMOVED FLOOR BOARD SUPPORT FABRICATED NEW TRACK, FLOOR BOARD SUPPORT. (M)

Part: FLOORBEAM — DAMAGED (FUSELAGE)

FTW - FORWARD CARGO COMPARTMENT HAS CHAFING/DAMAGE AT FLOORBEAM STATION 389. MATERIAL LOSS OUT OF LIMITS. FABRICATED DOUBLERS. INSTALLED DOUBLERS STATION 389. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 160-200 RBL 7, FLOOR BOARD SUPPORT IS CORRODED. REMOVED DAMAGED SUPPORT. FABRICATED SUPPORT TRACK. INSTALLED NEW FABRICATED TRACK ON STATION 160-200 RBL 7. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 218-237 LBL 43 SUPPORT ANGLE CORRODED 1 EACH, FIGURE 8 HOLE. REMOVED SUPPORT ANGLE. HOLES LOCATED AND DRILLED ON NEW SUPPORT ANGLE. INSTALLED SUPPORT ANGLE. (M)

Part: FLOORBEAM — DAMAGED (FUSELAGE)

FTW - MID PIT FLOORBEAM HAS CHAFING/DAMAGE STATION 655. MATERIAL LOSS OUT OF LIMITS. FORMED ANGLES. INSTALLED ANGLES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT INBOARD SEAT TRACK HAS AREAS OF CORROSION. REMOVED SEAT TRACKS. INSTALLED SEAT TRACKS. (M)

Part: ANGLE — CORRODED (FUSELAGE)

FTW - FOUND STATION 218-237 LBL 18, SUPPORT ANGLE CORRODED ON FORWARD END. FABRICATED NEW SUPPORT ANGLE. INSTALLED NEW SUPPORT ANGLE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 200 LBL 9-13 FLOORBOARD SUPPORT IS CORRODED. REMOVED SUPPORT. FABRICATED NEW SUPPORT. INSTALLED NEW SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 196 LBL 14-43 FLOORBOARD SUPPORT IS CORRODED. REMOVED FLOOR BOARD SUPPORT. FABRICATED FLOOR BOARD SUPPORT. INSTALLED FABRICATED SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 170 BL 0 FLOOR BOARD SUPPORT CORRODED. REMOVED CORRODED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT FROM EXTRUSION. INSTALLED FLOOR SUPPORT. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

FTW - FOUND MID LOWER COMPARTMENT CARGO DOOR HAS CORROSION AT 3RD ANGLE ATTACH TO INTERCOSTAL. REMOVED ANGLE. HOLES DRILLED AND LOCATED ON NEW ANGLE. INSTALLED NEW ANGLE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 160 LBL 7 TO LBL 56 FLOORBOARD SUPPORT HAS AREAS OF CORROSION. REMOVED FLOOR BOARD SUPPORT FROM STATION 160 LBL 7 TO LBL 56. FABRICATED FLOOR BOARD SUPPORT STATION 160 LBL 7 TO LBL 56. INSTALLED FLOOR SUPPORT AT STATION 160 LBL 7 LBL 56. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND STATION 164 LBL 14 AND LBL 42, LIGHT CORROSION ON FLOOR WEB AROUND FITTINGS. AFTER FURTHR EVAL, FOUND THREE FITTINGS CORRODED OUT OF LIMITS. AREA AT STATION 164 LBL 42 FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA. FABRICATED DOUBLER. INSTALLED DOUBLER. DRILLED THREE FITTINGS. INSTALLED THREE FITTINGS. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 160-196 LBL 45, FLOORBOARD SUPPORT IS CORRODED. REMOVED FLOORBOARD SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR BOARD SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 160-168 AND 186-194 LBL 54 TWO FLOORBOARD SUPPORTS ARE CORRODED. REMOVED FLOORBOARD SUPPORTS TWO FABRICATED AND LOCATE AND DRILL NEW PARTS TWO EACH. INSTALLED FLOOR BOARD SUPPORTS TWO EACH. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 200 LBL 7 - RBL 7 FLOORBOARD SUPPORT CORRODED. REMOVED FLOOR SUPPORT. FABRICATED DRILLED AND LOCATED NEW SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 200 RBL 8-45 FLOOR BOARD SUPPORT CORRODED. REMOVED FLOOR BOARD SUPPORT. LOCATED AND DRILLED. INSTALLED FLOOR SUPPORT. (M)

Part: ANGLE — CORRODED (FUSELAGE)

FTW - FOUND STATION 160 LBL 14-42 1 INCH ABOVE SUB FLOOR, LOWER PANEL ANGLE HAS EXFOLIATION CORROSION. REMOVED LOWER PANEL ANGLE AT STATION 160 LBL 14-42. FABRICATED NEW ANGLE. INSTALLED FABRICATED ANGLE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 256 LBL 14-20 FLOOR BOARD SUPPORT IS CORRODED. REMOVED FLOOR SUPPORT. FABRICATED FLOOR BOARD SUPPORT. INSTALLED SUPPORT. (M)

Part: FLOORBEAM — DAMAGED (FUSELAGE)

FTW - AFT PIT FLOORBEAM HAS CHAFING/DAMAGE THROUGH HOLE STATION 1174. FABRICATED ANGLE REPAIR AND FILLER. INSTALLED ANGLE AND SHIM. (M)

Part: WEB — PUNCTURED (FUSELAGE)

FTW - FOUND STATION 245 LBL 47-52, CRACK IN EDGE OF LIGHTENING HOLE INBOARD SIDE, PUNCTURE IN FLOOR WEB OUTBOARD OF LIGHTENING HOLE. REMOVED CRACK. FORMING DOUBLER. INSTALLED DOUBLER. (M)

Part: BRACKET — CRACKED (FUSELAGE)

FTW - FOUND FORWARD PIT HAS CRACKED AT BRACKET SUPPORT AFT 2 ANGLE RBL IN INCHES. REMOVED CRACKED BRACKET SUPPORT. FABRICATED NEW BRACKET. INSTALLED BRACKET. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 196-256 LBL 14, FLOOR BOARD SUPPORT IS CORRODED. REMOVED FLOOR BOARD SUPPORT. LOCATED AND DRILLED. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 160-200 RBL 45 FLOOR BOARD SUPPORT IS CORRODED. REMOVED FLOOR BOARD SUPPORT ANGLE FROM STATION 160-200 RBL 45. FORMED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT ON STATION 160-200 RBL 45. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND STATION 200-256 RBL 45 RIGHT OUTBOARD SEAT TRACK HAS AREAS OF CORROSION, NICKS AND BARE METAL. REMOVED AND INSTALLED SEAT TRACK AND SPLICE. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

FTW - FORWARD PIT AFT BULKHEAD FORWARD FACE HAS CRACKED AT UPPER ANGLE LBL 26 INCHES. DRILLED STOP CRACK ON UPPER FLANGE STATION 541 LBL 26. DRILLED AND LOCATED, INSTALLED. (M)

Part: FLOORBEAM — DAMAGED (FUSELAGE)

FTW - FOUND FORWARD CARGO COMPARTMENT CHAFING/DAMAGE AT FLOORBEAM STATION 408. FOUND AREA TO BE OUT OF LIMITS. FABRICATED REPAIR ANGLE. INSTALLED REPAIR PARTS. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - FOUND MID PIT HAS CORROSION AT LONGERON. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS. (M)

Part: FRAME — CRACKED (FUSELAGE)

FTW - FOUND PASSENGER CABIN LEFT OVERWING INTERNAL FRAME HAS CRACKS STATION 965L NR 12. STOP DRILLED CRACK. FORMED REPAIR ANGLES, ROUTED TO HEAT TREAT DEPT. INSTALLED REPAIR ANGLES -3, -5, AND -7 ON STATION 965 LONGERON NR 12. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - FOUND MID PIT HAS CORROSION AT LONGERON 30 STATION 807. REMOVED THE DEEPEST CORROSION AREA. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOORBOARD CORRODED. REMOVED FLOOR SUPPORT. FABRICATED, DRILLED AND LOCATED NEW SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FITTING — CORRODED (FUSELAGE)

FTW - FOUND MID PIT HAS CORROSION AT FORWARD CARGO FITTING STATION 636 RBL 6 INCHES. REMOVED DAMAGED CARGO FITTING. HOLES LOCATED AND DRILLED ON NEW FITTING. INSTALLED NEW FITTING. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND L1 DOOR THRESHOLD FLOOR SUPPORT HAS CORRODED. REMOVED FLOOR SUPPORT DAMAGED. FORMED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: BRACKET — CORRODED (FUSELAGE)

FTW - FOUND MID PIT HAS CORROSION AT BRACKETS ATTACH TO INBOARD BEAM STATION 617 RBL 8 INCHES BOTH SIDES, TWO EACH. REMOVED BRACKETS FROM STATION 617 RBL 8. FABRICATED BRACKETS FROM 7075-T6511. INSTALLED NEW FABRICATED BRACKETS AT STATION 617 RBL 8. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

FTW - FOUND MID PIT CRACKED AT BRACKET ATTACH TO INTERCOSTAL AND BULKHEAD FRAME RBL 16 INCHES STATION 788. REMOVED CRACKED BRACKET AT FRAME RBL 16 INCHES STATION 788, LOCATED AND CB DRILLED NEW FITTING, INSTALLED. (M)

Part: ANGLE — CORRODED (FUSELAGE)

FTW - FOUND MID PIT HAS CORROSION LEFT ANGLE FORWARD FACE BULKHEAD STATION 788, BOTH SIDES. REMOVED ANGLE. DRILLED AND LOCATED HOLES, INSTALLED. (M)

Part: PANEL — CRACKED (LT WING)

FTW - FOUND LEFT WING LOWER L/E PANEL 1166C APPROX 2 INCH CRACK AND TOOL MARKS ON SIN, BARE METAL ON BACK. DAMAGE CUT OUT, FORMED DOUBLER REPAIR AND FILLER. INSTALLED DOUBLER REPAIR AND FILLER. (M)

Part: STRUCTURE — CORRODED (E/E DOOR)

FTW - E/E DOOR INTERNAL SURFACE HAS CORROSION ALL AROUND. MATERIAL LOSS EXCEEDS THE LIMITS PRESCRIBED IN 52-01. REPAIR DUOBLERS FABBRICATED. INSTALLED REPAIR DOUBLER. (M)

Part: ISOLATION MOUNT — WRONG PART (LT ENGINE)

FTW - FOUND LEFT ENGINE FORWARD UPPER AND LOWER VIBRATION ISOLATORS MISMATCH. REMOVED LEFT ENGINE FORWARD UPPER AND LOWER VIBRATION ISOLATORS. INSTALLED NEW UPPER AND LOWER ISOLATORS. (M)

Part: SKIN — DENTED (RT WING)

FTW - FOUND RIGHT WING HAS DENT/DAMAGE AT OUTER SKIN FUELING PANEL 1249C. STOP DRILLED CRACK FOUND IN DENT. FABRICATED DOUBLER. INSTALLED DOUBLER. (M)

Part: PANEL — DELAMINATED (LT WING)

FTW - FOUND LEFT LOWER WING SURFACE TRAPEZOID (SHAPE) PANEL DELAMINATED NEXT TO MLG WHEEL. REPAIRED LEFT LOWER WING SURFACE TRAPEZOID PANEL. (M)

Part: PANEL — DELAMINATED (RT WING)

FTW - FOUND LOWER WING SURFACE TRAPEZOID (SHAPE) PANEL DELAMINATED NEXT TO MLG WHEEL. REPAIRED RIGHT LOWER WING TRAPEZOID PANEL. (M)

Part: PANEL — DELAMINATED (LT WING)

FTW - FOUND LEFT WING UPPER SURFACE PANEL DELAMINATED NEXT TO INBOARD SPOILER. REMOVED PANEL. LOCATED AND DRILLED NEW PANEL. INSTALLED PANEL. (M)

Part: PANEL — DAMAGED (RT WING)

FTW - FOUND RIGHT WING HAD DENT/DAMAGE AT OUTER SKIN FUELING PANEL. STOP DRILLED CRACK FOUND IN DENT. FABRICATED DOUBLER. INSTALLED DOUBLER. (M)

Part: SKIN — DENTED (WINDOW BELT)

FTW - C/O CONTROL NR 0870 ON L/P 84615, FUSELAGE HAS DENT BELOW CAPTAINS CLEARVIEW WINDOW AT APPROX STATION 125. REWORKED DENT. FORMED DOUBLER REPAIR. S/D - DENT AT FS 121 BETWEEN LONGERONS 17 AND 18L REQUIRES REPAIR. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT ON LEFT SIDE OF FUSELAGE FORWARD OF DOOR. CUT OUT DAMAGED AREA. FORMED FILLER AND FINGER DOUBLER. INSTALLED DOUBLER AND FILLER. (M)

Part: RELAY — CORRODED (AUTOPILOT SYS)

FLT 632 - TPA - DURING CLIMBS/DESCENTS IN 'IAS' OR 'MACH' MODE, AP TRIM LIGHT ILLUMINATES. FOUND A/P TRIM RELAY CONTACTS CORRODED. REMOVED AND REPLACED RELAYS. OPS CHECKS GOOD IAW RTS 22-01-05. (M)

Part: CONTROL PANEL — FAULTY (COCKPIT)

TPA - FLT 632 - DURING DESCENT, AUTO PILOT WILL NOT HOLD SELECTED MACH, IAS OR VERTICAL SPEED MODES. AUTO PILOT WILL TEND TO SPEED PAST SELECTED MODE. WHILE AUTO PILOT IS SPEEDING PAST SELECTED MODE, THE AUTO PILOT TRIM ANNUNCIATOR LIGHT WILL ILLUMINATE, WHEN TURNING OFF THE AUTO PILOT TO CORRECT THE MALFUNCTION THE AIRCRAFT TENDS TO PITCH DOWN. REMOVED AND REPLACED DFGC CONTROL PANEL. PERFORMED SYSTEM MAINTENANCE BIT SEQUENCE THREE, DIAGNOSTIC NUMBERS 146 THROUGH 177 PER MD80 MM 22-01-02, RAN RTS CHECK ON NR 1 AND NR 2 SYSTEMS IAW MD80 MM 22-01-05. (M)

Part: SERVO — FAULTY (AUTOPILOT SYS)

TPA - FLT 632 - AUTO PILOT IS VERY SLOW TO TRIM DURING LEVEL OFFS AND WITH SPEED CHANGE. AUTO PILOT TRIM COMPARATOR LIGHT ILLUMINATES AND A/P WON'T ALWAYS CAPTURE ALTITUDE. BOTH DFGS 1 AND 2 DO THE SAME. REMOVED AND REPLACED DUPLEX ELEVATOR SERVO DRIVE WITH SERVICEABLE UNIT. RAN RIGHTS CHECK ON NR 1 AND NR 2 SYSTEMS, BOTH SIDES GO. (M)

Part: SERVO — DEFECTIVE (AUTOPILOT SYS)

WHEN LEVEL W/AUTO PILOT THE ALTITUDE WANDERS UP AND DOWN 200 FEET EITHER WAY. AUTO PILOT TRIM LIGHT COMES ON AND REMAINS ON, DISCONNECTING AUTO PILOT CAUSES BIG PITCH (TRIM). AFTER RETRIM AND AUTO PILOT BACK ON SEEMS OK, BUT HAPPENED TWICE. HAPPENS W/ AUTO PILOT IN NR 1 POSITION NO TIME TO CHECK NR 2 AUTO PILOT. REMOVED AND REPLACED DUPLEX ELEVATOR SERVO DRIVE. RAN RTS CHECK ON NR 1 AND NR 2 SYSTEMS, BOTH SYSTEMS GO IAW MFG MM.

Part: SERVO — MALFUNCTIONED (AUTOPILOT SYS)

ACY - FLT 259 - FOUND AUTO PILOT FAILED ON DESCENT A/P TRIM LIGHT WAS ON. A/P FAILED TO CAPTURE ALT ON DESCENT USING NR 1 A/P. REMOVED AND REPLACED ELEVATOR SERVO DRIVE ASSY RTS CHECK RAN, OPS CHECK NORMAL. (M)

Part: WIRE — DISCONNECTED (CABIN)

FLL - FLT 1268 - FOUND EMERGENCY LIGHTING TRACK FROM ROW 22 TO 25 INOPERATIVE. FOUND LIGHT AT SEAT 22 WIRES PULL OUT OF SPLICE, SPLICED WIRES BACK TOGETHER FOR LIGHT. (M)

Part: ANGLE — CORRODED (FUSELAGE)

FTW - FOUND STATION 218-225 LBL 18 ON REMOVABLE OF SUPPORT ANGLE REF 18-NN-00134 SUB FLOOR WAS FOUND TO HAVE EXFOLIATION. CUT OUT DAMAGED AREA. FABRICATED NEW SUB FLOOR SECTION AND DOUBLER. INSTALLED NEW PARTS. (M)

Part: WIRE — DAMAGED (CABIN)

BWI - FLT 2916 - THE EMERGENCY LIGHT PATH HAS SOME RED BULBS INOPERATIVE AT ROW 22. REPAIRED WIRING IAW MM 20-50-01. OPS OK. (M)

Part: WIRE — DAMAGED (CABIN)

BWI - FLT 2916 - FOUND EMERGENCY LIGHT HAS AN INOPERATIVE BULB AT ROW 34. REPAIRED WIRING IAW MM 20-50-00. OPS OK. (M)

Part: WIRE — BROKEN (CABIN)

FLOOR TRACK LIGHTING AT REAR OF AIRCRAFT DETACHED FROM FLOOR. RECONNECT BROKEN WIRES FOR EMERGENCY FLOOR PATH LIGHTING, OPS CHECK OK IAW 20-50-04 MD80 MM NO DEFECTS NOTED AT THIS TIME. (M)

Part: WIRE — BROKEN (CABIN)

DTW - FOUND 2ND TO LAST RED FLOOR TRACK LIGHT OUT. FOUND BROKEN WIRE ON FLOOR TRACK LIGHTING. REPAIRED BROKEN WIRE IAW MD-80 M/M CH 20-50-01. OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - FLT 872 - FLIGHT ATTENDANT STATION C EMERGENCY LIGHT RED LIGHTS INOPERATIVE EXPOSED WIRE. INSTALLED NEW LIGHT BULB IAW MD80 MM 33-53-01. OPS CHECK GOOD. (M)

Part: CHARGER — FAULTY (E/E BAY)

FLT 678 - DTW - BATTERY CHARGER PULSES LEFT 8-10 TIMES PER MINUTE. BATTERY VOLTS NORMAL. QRH COMPLIED WITH. CIRCUIT BREAKER PULLED. CHARGER CIRCUIT BREAKER. REMOVED AND REPLACED BATTERY CHARGER. OPS CHECKED GOOD PER MD-80 MM 24-30-00. NO OTHER DISCREPANCIES NOTED. (M)

Part: LIGHT — INOPERATIVE (A/C BAY)

FLL - FOUND TWO OVERHEAD EMERGENCY LIGHTS INOPERATIVE IN TAIL COMPARTMENT. REPAIRED WIRE ON FORWARD LAMP AND RELAMPED AFT LIGHT, OPS CHECK NORMAL IAW MM 33-50-00. (M)

Part: COVER — CRACKED (CABIN)

DTW - LEFT AND RIGHT EMERGENCY DOOR LIGHT COVER CRACKED, EXIT. REMOVED AND REPLACED LEFT AND RIGHT EMERGENCY DOOR LIGHT COVER IAW MD80 MM 33-21-00. (M)

Part: ENGINE — OUT OF TOLERANCE (NR 2 ENGINE)

DTW - FLT 506 - THROTTLES SPLIT, ONE KNOW WIDTH AT TAKEOFF POWER. PERFORMED ENGINE RUN, FOUND NR 2 CUT OF TRIM. TRIM NR 2 ENGINE IAW MD-80 MM 71-00-00. FOUND NO THROTTLE SPLIT AFTER TRIM. (M)

Part: SLIDE — OUT OF POSITION (SERVICE DOOR)

DTW - FORWARD SERVICE DOOR EVACUATION SLIDE CAME OFF. INSTALLED SLIDE PACK IAW MD-80 MM 25-62-00. NO DEFECTS NOTED AT THIS TIME. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DISCREPANCY: ONE EMERGENCY TRACK LIGHTING LAMP INOP AT DOOR L-02 (RED LAMPS) CORRECTIVE ACTION: RELAMPED EMERGENCY TRACK LIGHTING. OPS CHECK NORMAL IAW MM 33-50-00.

Part: LIGHT — BROKEN (CABIN)

DTW - EMERGENCY FLOOR PATH LIGHTING TRACK BROKEN/UNSEATED IN SEVERAL LOCATIONS. REPLACED BROKEN FLOOR TRACK FROM ROWS 32-34, RESEATED TRACK AT ROWS 27-29 AND 21-22. EMERGENCY FLOOR PATH LIGHTING OPS CHECK GOOD, REF MD80 MM 33-53-01. (M)

Part: LIGHT — LOOSE (CABIN)

DTW - EMERGENCY TRACK AT 29 AND 30 DEF WILL NOT STAY DOWN. RE-SECURED EMERGENCY TRACK LIGHTING STRIP, REF 33-53-00 MD-80 MM. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

ACY - AFT UPPER EMERGENCY FLASHLIGHT RED LED NOT BLINKING. REMOVED AND REPLACED EMERGENCY FLASHLIGHT. OPS CHECKS GOOD IAW MD 80 MM 25-00. (M)

Part: WIRE — EXPOSED (ROW 22)

DTW - EMERGENCY LIGHTING TRACK WIRING EXPOSED AT ROW 22. REINSTALLED LOOSE COVER OVER EGRESS LIGHTS AT ROW 22 IAW MM 33-50-00. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - SECTION OF AFT CABIN EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPAIRED WIRING IN FLOOR TRACK ACROSS FROM MIC F/A STATION. FUNCTIONAL CHECK GOOD. REF: MD 80 MM 33-1-03 AND MM 20-50-01. (X)

Part: LENS — MISSING (ROW 10)

DTW - EMERGENCY TRACK LIGHTING IS MISSING LENS COVER AND BULBAT ROW 10. INSTALLED NEW TRACK LIGHTING LENS COVER AND BULB AT ROW 10 IAW MD 80 MM 33-53-00. OPS CHECKS GOOD AT THIS TIME. (M)

Part: WIRE — EXPOSED (CABIN)

DTW - EMERGENCY TRACK LIGHTING SHOWING WIRES IN TWO SPOTS ACROSS FROM AFT GALLEY. REMOVED AND REPLACED EMERGENCY LIGHT TRACK COVERING IAW MD80 MM 33-53-00. OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME. (M)

Part: PLACARD — MISSING (MEGAPHONE)

DTW - EMERGENCY MEGAPHONES NOT PLACARDED ' EMERGENCY USE ONLY. INSTALLED 'EMERGENCY USE ONLY' PLACARDS ON EMERGENCY MEGAPHONES AS REQUIRED.(M)

Part: SLIDE — LOOSE (CABIN)

LGA - FLT 403 - GALLEY PACK SLIDE FELL OFF. RETURNED TO GATE ON LEG 2. REINSTALLED SLIDE PACK AND COVER IAW 25-62-00. (M)

Part: PACK — DETACHED (R1 DOORWAY)

DTW - FLT 612 - R1 SLIDE PACK CAME OFF. R1 SLIDE PACK INSTALLED IAW 25-61 OF MD-80 MM. NO DEFECTS NOTED. (X)