N811NK

Part: DOOR — DAMAGED (MLG)

MCO - FLT 138 - RIGHT HYDRAULIC LEAK, NO QTY OR PRESSURE, FURTHER INSPECTION REVEALED DAMAGE TO LOWER SECTION OF MAIN LANDING GEAR DOORS. AIRCRAFT SWAP. REPAIRED RT MLG AND LT MLG DOORS IAW MD80 SRM 52-05, INSTALLED TEMP REPAIR. (M)

Part: FRAME — CRACKED (FUSELAGE)

DTW - FOUND 7 INCH CRACK ON STATION 1463 AT 8:00 POSITION A/C LEFT. REMOVED DAMAGED AREA AND INSTALLED REPAIR IAW SRM. (M)

Part: TARGET — OUT OF ADJUST (LT MLG DOOR)

FLL - FLT 1265 - FOUND MAIN GEAR DOOR OPEN LIGHT ON AT CRUISE ALT WENT OUT WITH RT HYD PUMP ON. ADJUSTED LEFT GEAR DOOR SENSOR TARGET. (M)

Part: TAB — DELAMINATED (RT ELEVATOR)

FOUND RIGHT ANTI-FLOAT TAB DELAMINATED AT OUTBOARD TIP. REMOVED RT ELEVATOR ANTI-FLOAT TAB. INSTALLED RT ELEV ANTI-FLOAT TAB. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT DOOR JAM CORROSION. REMOVED CORROSION. FABRICATED DOOR BEAM REPAIR. INSTALLED REPAIR PARTS. (M)

Part: LENS — CRACKED (SMOKE GOGGLES)

F/O'S SMOKE GOGGLE LENS CRACKED (2) ALL 3 GOGGLES NEED BAG REPLACED. REMOVED AND REPLACED F/O'S SMOKE GOGGLES. (M)

Part: LANYARD — INOPERATIVE (L1 DOOR SLIDE)

FLL - FOUND L1 DOOR LANYARD EVAC SLIDE BROKEN. REMOVED AND REPLACED LANYARD EVAC SLIDE AT L1 DOOR. (M)

Part: DOOR — INOPERATIVE (MLG)

ENROUTE, THE GEAR DOOR OPEN LIGHT CAME ON. TURNED ON THE HYD`S AND THE LIGHT WENT OUT. AFTER TURNING OFF THE HYD`S THE LIGHT CAME BACK ON. TURNED ON RT HYD AND LEFT IN HI. PERFORMED PROXIMITY TEST, MAIN GEAR DOORS, TEST PASSED. VERIFIED GEAR DOOR ROLLER AND HOOK MEASUREMENTS, WITHIN TOLERANCES CLEANED GEAR DOOR PROXIMITY SWITCHES.

Part: LANYARD — DISENGAGED (EVAC SLIDE)

L1 DOOR PACK SLIDE LANYARD DISENGAGED FROM DOOR (SLIDE DID NOT FALL OFF OF DOOR). REINSTALLED LANYARD.

Part: CABLE — DISLODGED (EXIT SLIDE)

FOUND DOOR 1R EMERGENCY EXIT SLIDE HAS CABLES PROTRUDING FROM COVER. REPLACED SLIDE ASSEMBLY, DOOR 1R. (M)

Part: CABLE — DEFECTIVE (RT MLG)

FLL - FLT 196 - DURING TAXI, RIGHT BRAKE LOCKED UP WITHOUT APPLYING BRAKES. REMOVED AND REPLACED RUN 97B BRAKE VALVE RETURN CABLE. (M)

Part: SLIDE — UNSECURE (L1 DOOR)

ACY - FLT 330 - L1 SLIDE PACK NEEDS SECURING. REINSTALLED PACK. (M)

Part: LANYARD — DISCONNECTED (R1 DOOR)

LGA - FLT 703 - FOUND DOOR R1 SLIDE LANYARD CABLES NOT ATTACHED. ATTACHED CABLE TO GIRT BAR. (M)

Part: CAP — MISSING (CABIN)

DTW - FLT 1689 - FOUND SAFETY GLOW FLOOR TRACK RIGHT AT EXIT ROW 26 MISSING END CAP AND INSERT ASSEMBLY. FOUND MISSING ASSEMBLY IN CABIN RESECURED. (M)

Part: CONTROLLER — MALFUNCTIONED (PACK AUTO TEMP)

ACY - FLT 1148 - AFTER TAKEOFF FROM ACY, THE AFT LEFT AND RIGHT DETECTORS WENT OFF AND FLIGHT ATTENDANT'S SAID AN OIL HAZE WAS IN THE AIR. LOOKED AT CABIN TEMP VALVE AND RIGHT VALVE WAS MAX TO THE RIGHT. PUT RIGHT VALVE TO MANUAL AND DROVE VALVE TO COLD. A/C CLEARED OF HAZE IN THE AFT AND DETECTORS WENT OFF. REMOVED AND REPLACED RIGHT AUTO TEMP CONTROLLER. SYSTEM CHECKS GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MCO - EMERGENCY LIGHT BELOW WATER SEPARATOR BAGS INOPERATIVE. SECURED WIRES TO LIGHT ASSEMBLY OF EMERGENCY LIGHT BELOW WATER SEPARATOR BAGS. OPS CHECK OK. (M)

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG)

FLL - FLT 268 - AFTER TAKEOFF, RIGHT MAIN GEAR RED LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ON WTIH GEAR HANDLE UP-FOLLOWED QRH PROCEDURE AFTER WHICH GEAR LIGHTS INDICATED NORMAL, CONTINUED TO ACY. BITE CHECK OF PSEU SENSORS SHOWS NO FAULTS AT THIS TIME. CHECKED GEAR DOOR AND GEAR UP AND DOOR LATCH PROX SENSORS FOR CORRECT ADJUSTMENT AND SECURITY. CLEANED CONNECTORS ON BOTH SENSORS. CLEANED SENSOR AND TARGET AREA, PERFORMED STANDARD ELECTICAL T/S OF SENSORS PER ACCEPTED PCTS. NO DEFECTS NOTED AT THIS TIME. (M)

Part: ISOLATION MOUNT — DAMAGED (ENGINE)

RT ENGINE FORWARD LOWER VIBRATION ISOLATOR NEEDS TO BE REPLACED. REMOVED AND REPLACED RT ENGINE FORWARD LOWER VIBRATION ISOLATOR. (M)

Part: ISOLATION MOUNT — DAMAGED (ENGINE)

RIGHT ENGINE FORWARD UPPER VIBRATION ISOLATOR NEEDS TO BE REPLACED. REMOVED AND REPLACED RIGHT ENGINE FORWARD UPPER VIBRATION ISOLATOR. (M)

Part: ENGINE — FAILED (RIGHT)

RIGHT ENGINE FAILURE AT 80 KTS. REMOVED AND REPLACED NR 2 ENGINE. (M)

Part: HINGE — BROKEN (TAILCONE)

FOUND TAILCONE RELEASE ARM DOOR IN AFT F/A STATION BROKEN. RESECURED HINGE. REPLACED RIVETS. (M)

Part: LIFE RAFT — FAILED (CABIN)

DTW - FOUND DURING MINI-EVACUATION DEMONSTRATION, ONE CHAMBER OF RAFT FAILED TO INFLATE. REMOVED AND REPLACED AFT. (M)

Part: CONNECTOR — LOOSE (BATTERY PACK)

MCO - TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. SECURED LOOSE OUTPUT CONNECTION ON BATTERY PACK FOR TAIL COMP EMERGENCY LIGHTS, OPS CHECKOK IAW MM 33-53-00. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CARGO COMPARTMENT APPROX STATION 370 INTERCOSTAL BY LONGERON 30 HAS CORROSION. REMOVED INTERCOSTAL. FABRICATED NEW FS 370 INTERCOSTAL. INSTALLED INTERCOSTAL. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN STATION 200-260 RBL 24 TO 44 FLOORBOARD HAS CORROSION AT INSERTS/SOFT MUSHEY. FABRICATED PANEL. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND CABIN PRESSURE FLOORBOARD RIGHT STATION 265-313 4 EACH RIVETS PULLED THROUGH SKIN AND CRACKED. REMOVED CRACKED SKIN. FABRICATED NEW FLOORBOARD SKIN. INSTALLED NEW SKIN. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

FTW - FOUND IN PAX CABIN CORROSION AT FS 258 LONGERON 18R. FABRICATED REPAIR FILLER AND REPAIR DOUBLER. REPAIR PARTS INSTALLED. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

FTW - FOUND PAX CABIN FLOOR WEB CRACKED AT LONGERON 18L STATION 325. CUT OUT DAMAGED WEB. FABRICATED FLOOR WEB AND DOUBLER. INSTALLED WEB AND DOUBLER. (M)

Part: DOUBLER — CORRODED (LAVATORY)

FTW - FOUND AFT CABIN LAVATORY AREA LEFT FLOOR ANGLE DOUBLER CORRODED. FABRICATED A NEW ANGLE DOUBLER. (M)

Part: LONGERON — CORRODED (FUSELAGE)

MAIN CABIN FS 256, STR 17R, CORRODED. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED LONGERON SECTION AND LONGERON SPLICES. INSTALLED LONGERON AND SPLICES.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

INTERCOSTAL ASSY STA 630 TO 636, RBL 3, CORRODED. DISASSEMBLED INTERCOSTAL ASSY. GUSSET FOUND TO BE OUT OF LIMITS. FABRICATED NEW PART.

Part: LONGERON — CRACKED (FS 370)

MAIN CABIN FS 370, STR 16, CRACKED. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED LONGERON SECTION AND SPLICE. INSTALLED LONGERON AND SPLICES.

Part: LONGERON — CRACKED (FUSELAGE)

PAX CABIN, LONGERON 17L CRACKED AT STATIONS 236, 370 AND 427. REMOVED LONGERON 17L FROM STA 417 TO STA 436. REMOVED CRACKED LONG. 17L FROM STA 303 TO STA 323. REMOVED LONGERON 17L FROM FS 230-250. REMOVED LONGERON 17L FROM FS 380 - FS 398. LOCATED AND DRILLED SPLICE. INSTALLED LONGERON REPAIRS AND SPLICES.

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND MAIN CABIN FS 1297 STRINGER 18R WEB CRACKED. STOP DRILLED CRACKS, TWO. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT STATION 160 LBL 10 HAS CORROSION. FABRICATED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FS 200)

FTW - FLOOR SUPPORT STATION 200 RBL 9-44 HAS CORROSION. FABRICATED NEW FLOOR SUPPORT. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

FTW - FOUND MAIN CABIN FS 1174 RIGHT OUTBOARD FLOOR PANEL CRACKED. REMOVED DAMAGED FLOOR PANEL. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. REINSTALLED FLOOR PANEL. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND WEB STATION 200-218 RBL 26 LBL 26 HAS CORROSION. FABRICATED WEB PANEL. (M)

Part: FITTING — CORRODED (FUSELAGE)

FTW - FOUND MAIN CABIN FS 1022 STATION 181 T-FITTING CORRODED. REMOVED T-FITTING, LOCATED AND DRILLED NEW PART. INSTALLED FITTING. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT STATION 160-200 RBL 44 HAS CORROSION. REMOVED FLOOR SUPPORT AT STATION 160-200 RBL 44. FABRICATED REPLACEMENT FLOOR SUPPORT. REPLACEMENT FLOOR SUPPORT FS 160-200 RBL 44 TO BE INSTALLED AS W/O B00059 05-N-81. (M)

Part: FLOORBOARD — DETERIORATED (FUSELAGE)

FTW - FOUND FLOORBOARD STATION 130-160 DETERIORATED. FABRICATED NEW FLOORBOARD. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT STATION 200 LBL 15 RBL 5 CORRODED. FABRICATED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT STATION 218 RBL 10 - LBL 12 HAS CORROSION. FABRICATED NEW SUPPORT. (M)

Part: FLOORBOARD — DAMAGED (CABIN)

FTW - PASSENGER CABIN STATION 1309 TO 1360 FLOORBOARD HAS SOFT/MUSHEY BLUE WATER STAINS AND SEVERAL INSERTS DAMAGE. FABRICATED NEW PASSENGER CABIN FLOORBOARD. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND SUPPORT FS 518-636 HAS CORROSION. FABRICATED SUPPORT. (M)

Part: FLOOR PANEL — CORRODED (COCKPIT)

FLIGHT COMPARTMENT STA 138 CORRODED ON WEB UNDER INBOARD CAPTAINS SEAT TRACK. REMOVED DAMAGED AREA OF WEB. FABBED NEW WEB SECTION. FABRICATED SPLICE. INSTALLED SPLICE. INSTALLED NEW WEB SECTION FS 133, FS 160, RBL 4, LBL30.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT STATION 160-200 LBL 45 HAS CORROSION. LOCATED AND DRILLED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (CABIN)

FTW - FOUND FLOOR SUPPORT ANGLE STATION 150-160 LBL 12 CORRODED. FABRICATED PART. (M)

Part: WEB — CORRODED (SUB FLOOR)

FTW - FOUND SUB FLOOR WEB STATION 160-200 LBL 44-54 HAS CORROSION AND CRACKED. FABRICATED WEB. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

MID CARGO RADIO ALT ANTENNA DOUBLER CORRODED FS 687-688, STR 30-27L. REMOVED DOUBLER. LOCATED AND DRILLED HOLES ON DOUBLER. INSTALLED DOUBLER.

Part: LONGERON — CORRODED (FUSELAGE)

MID CARGO STR 30 CORRODED FS712 TO 598. REMOVED LONGERON 30 FROM STA 590 TO 741. REMOVED LONGERON 30 STA 741 TO 759. FABRICATED NEW LONGERON SECTION FROM FUSELAGE STA 590 TO 662. FABRICATED FORWARD LONGERON SPLICE. FABRICATED NEW LONGERON SECTION FROM FUSELAGE STA 662 TO 759. LOCATED AND DRILLED LONGERON 30 SPLICE REPAIR STA 653-673. INSTALLED SPLICE REPAIR (L NR30 STA 653-673). INSTALLED LONGERON 30 FROM STA 590-759.

Part: SHEAR TIE — CORRODED (FUSELAGE)

FTW - FOUND SHEAR TIE ASSEMBLY HAS CORROSION AN GOUGE. FOUND SHEAR TIE TO BE OUT OF LIMITS. FORMED SHEAR TIE. (M)

Part: FLOORBOARD — DETERIORATED (CABIN)

FTW - FOUND FLOORBOARD R1 ENTRY DETERIORATED. FABRICATED NEW R1 ENTRY FLOORBOARD. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT STATION 197 LBL 34 HAS CORRODED. FABRICATED NEW FLOOR SUPPORT. (M)

Part: FLOOR PANEL — DETERIORATED (CABIN)

FTW - FLOOR PANEL STATION 200-260 LBL 20 LBL 44 DETERIORATED. FABRICATED NEW PANEL. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FTW - FOUND FS 1250 L28R FLOOR SUPPORT CRACK IN RADIUS. STOP DRILLED ANGLE SUPPORT IN STATION 1250, L28R. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT STATION 197 LBL LEFT HAS CORRODED. FABRICATED REPAIR SUPPORT. (M)

Part: FLOOR PANEL — DETERIORATED (CABIN)

FTW - FOUND FLOOR PANEL FORWARD ENTRY L-1 DETERIORATED. FABRICATED NEW FLOORBOARD. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT STATION 160-200 LBL 50 HAS CORROSION. DRILLED AND LOCATED NEW PART. (M)

Part: FLOOR PANEL — DETERIORATED (CABIN)

FTW - FOUND FLOOR PANEL STATION 160-200 HAS BLUE WATER AND DETERIORATION. FABRICATED NEW FLOORBOARD. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

FTW - FOUND FLOOR PANEL FORWARD CABIN STATION 200-260 HAS BLUE WATER STAINS AND CRACKED. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT FORWARD CABIN STATION 150-200 LBL 6 IS CORRODED. FABRICATED REPLACEMENT FLOOR SUPPORT. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN WEB STATION 220-240 CORRODED. FABRICATED NEW WEB. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT STA 180, RBL6 TO RBL44 IS CORRODED. REMOVED FLOOR SUPPORT. DRILL AND LOCATE. INSTALLED FLOOR SUPPORT ANGLE. INSTALLED FLOOR SUPPORT.

Part: FLOORBOARD — DETERIORATED (CABIN)

FTW - FOUND FORWARD CABIN FLOORBOARD STATION 160-200 DETERIORATED. FABRICATED NEW FLOORBOARD. (M)

Part: CLIP — CORRODED (INTERCOSTAL)

FTW - FOUND AFT PIT INTERCOSTAL CLIP STATION 1220 HAS SURFACE CORROSION, PANEL CORRODED IN FASTENER HOLES. CLIPS IS OUT OF LIMITS. DRILLED NEW CLIP. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - E/E COMPARTMENT STATION 200 LBL 0 LBL 44, FLOORBEAMS AND SUBFLOOR HAVE WATER, INCLUDING INTERCOSTAL STATION 180-200 LBL 44. UPON FURTHER INVESTIGATION, FOUND CRACK BETWEN 2 RIVET HOLES STATION 200 LBL 21 IN SUBFLOOR WEB. LOCATED AND DRILLED REPAIR FOR CRACK. INSTALLED REPAIR ON WEB. (M)

Part: FRAME — CRACKED (FUSELAGE)

FTW - FOUND AFT PIT STATION 1212 FRAME SECTION RIGHT SIDE CRACK. FABRICATED NEW FRAME SECTION. INSTALLED NEW FRAME SECTION. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND CORROSION ON CUSP STATION 220-240 LBL 54. REMOVED CUSP STATION 180-230. FABRICATED NEW CUSP FROM STATION 180-230 LEFT. FABRICATED SPLICE FOR NEW CUSP STATION 180. INSTALLED CUSP SPLICE STATION 180. INSTALLED CUSP STATION 180-230. (M)

Part: FRAME — CRACKED (FUSELAGE)

FTW - FOUND AFT PIT CORROSION AT FRAME SECTION STATION 1155, 1165, 1193 AND 1174, RIGHT SIDE. MATERIAL LOSS OUT OF LIMITS FS 1165 T-CLIP AND FS 1193 T-CLIP. LOCATED AND DRILLED TWO NEW CLIPS. INSTALLED TWO NEW CLIPS. (M)

Part: VANE — GOUGED (TE FLAP)

FOUND LT WING CENTER FIXED VANE OUTBOARD FLAP HAS 2 PLACES GOUGES. BLENDED GOUGES. MATERIAL LOSS FOUND TO BE OT OF LIMITS. REPAIRED LEFT WING CENTER FIXED VANE. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FTW - FOUND CREASE AT FS 294 TO 313 AT LONGERON 25R REQUIRES REPAIR. CUT OUT DAMAGED AREA FS 294-313. FABRICATED 5 DOUBLERS 4 EACH, 7 STRAPS 4 EACH, 9 FINGER DOUBLER, 11 SKIN SECTION. INSTALLED ALL REPAIR PARTS. (M)

Part: PAN — CORRODED (E/E BAY)

FTW - E/E COMPARTMENT HAS CORROSION AT FORWARD AND AFT DOOR PAN. REMOVED E/E COMPARTMENT DOOR PAN. RECEIVED NEW DOOR PAN. COMPLETED INSTALLATION OF NEW DOOR PAN. (M)

Part: INTERCOSTAL — GOUGED (CARGO DOOR)

FTW - FOUND MID CARGO DOOR HEAVY GOUGE INBOARD SIDE OF DOOR FORWARD LOWER RIGHT CORNER. REMOVED INTERCOSTAL. FABRICATED REPAIR DOUBLER. FABRICATED REPAIR INTERCOSTAL. INSTALLED REPAIR PARTS. (M)

Part: DOOR FRAME — CORRODED (CARGO BAY)

FTW - FOUND FORWARD CARGO PIT CORROSION, BARE METAL AND CRACKED DAMAGED SEALANT ALL ALONG INBOARD FRAME AT DOOR JAMB PANEL FROM 3 O'CLOCK TO 9 O'CLOCK POSITION. FOUND CORROSION OUT OF LIMITS. CUT OUT FORWARD CARGO DOOR JAMB PANEL FROM 5 O'CLOCK TO 7 O'CLOCK FS 370-427. LOCATED AND DRILLED NEW FORWARD CARGO DOOR JAMB PANEL FROM 5 O'CLOCK TO 7 O'CLOCK FS 370-427. INSTALLED WEB STATION 364-423 AT FORWARD CARGO DOOR. (M)

Part: BEAM — CORRODED (FUSELAGE)

MID CARGO DOOR FRAME CORROSION, BARE METAL, CRACKED SEALANT ALL ALONG DOOR JAM BEAM. REMOVED DOOR JAMB BEAM L28R STA 598 TO 731 RT. HOLES LOCATED AND DRILLED NEW JAMB BEAM. INSTALLED DOOR JAMB BEAM STA 598 TO 731.

Part: BEAM — CORRODED (CARGO DOORWAY)

FTW - FOUND AFT CARGO PIT CORROSION, BARE METAL AND CRACKED SEALANT ALL ALONG INBOARD FRAME AT DOOR JAMB BEAM. REMOVED DOOR JAMB BEAM. LOCATED AND DRILLED NEW AFT CARGO DOOR BEAM. INSTALLED AFT CARGO DOOR JAMB BEAM. (M)

Part: WARNING SYSTEM — OUT OF ADJUST (COCKPIT)

FLL - AT SPEEDS BELOW 210 KTS WITH THROTTLES PULLED BACK, NO GEAR WARNING HORN. TEST OK ON GROUND. FOR ALL TROUBLE SHOOTING AND TESTING OF THE LANDING GEAR AURAL WARNING, REF MD80 MM 32-60-00. INSPECTED 3 MAIN LANDING GEAR DOWN AND LOCKED PROXIMITY SWITCHES AND DETERMINED OK. PERFORMED AN AST ON THE PROXIMITY S/W ELECTRONICS UNIT. OPS CHECK GOOD IAW MM 32-60-04. VERIFIED BOTH THROTTLE GEAR WARNING SWITCHES AND FLAP, 26 DEGREES S/W OPERATE NORMALLY. VERIFIED THE 'HORN CUT OUT SWITCH'. OPERATED NORMALLY AT BOTH, WITH FLAPS MORE THAN OR LESS THAN 26 DEGREES. INSTALLED PITOT EQUIP ON THE NR 1 SYSTEM AND DETERMINED THE LANDING GEAR AURAL WARNING IS OFF AT MORE THAN 210 KTS AND AURAL WARNING ON AT 210 KTS OR

Part: TERMINAL — BROKEN (TAIL CONE)

FLL - TAIL CONE UPPER CENTER EMERGENCY LIGHT INOPERATIVE. REPLACED BROKEN WIRE TERMINALS REF MM 20-50-01. OPS CHECK OK. (M)

Part: FLAP — DELAMINATED (LT WING)

ACY - LEFT FLAP INBOARD TRAILING EDGE DELAMINATED. REPAIRED T/E INBOARD FLAP LEFT FIBERGLASS REPAIR IAW MD80 SRM 57-03. (M)

Part: TORQUE TUBE — CORRODED (CARGO DOOR)

FTW - AFT LOWER CARGO COMPARTMENT CORRODED AT CARGO DOOR, CRANK SHAFT/TUBE TORQUE. REMOVED CORROSION ON TORQUE TUBE FOUND TO BE OUT OF LIMITS IAW MD80 SRM 51-10-3. INSTALLED NEW TUBE P/N 49123171. (M)

Part: ISOLATOR — GOUGED (LT PYLON)

FTW - LEFT PYLON FORWARD UPPER VIBRATION ISOLATOR IS GOUGED. REMOVED LEFT FORWARD UPPER VIBRATION ISOLATOR PER MD80 MM 71-20-02. INSTALLED LEFT FORWARD UPPER VIBRATION ISOLATOR PER MD80 MM 71-20-02. (M)

Part: WIRE — CHAFED (PAX OXYGEN)

FTW - OXYGEN MASK DROP TEST FAILED. T/S SYSTEM FOUND WIRES GOING TO CONNECTOR P1-1209 CHAFING. REPAIRED WIRES IAW OPS 20-10-01 SYSTEM TAKEOFF GROUND TEST GOOD IAW MD80 MM 35-20-00. (M)

Part: WIRE — BROKEN (CABIN)

FTW - R1 DOOR EMERGENCY DOOR LIGHT INOPERATIVE. TROUBLESHOT AND FOUND WIRE BROKEN WIRE AT EMERGENCY LIGHT. RESPLICED WIRE AT LIGHT IAW MD80 WDMSP 20-10-03. OPS CHECK GOOD IAW MD80 MM 33-53-00. (M)

Part: ISOLATOR — GOUGED (RT PYLON)

FTW - RIGHT PYLON FORWARD UPPER VIBRATION ISOLATOR HAS GOUGES ON INTERIOR SURFACE. REMOVED RIGHT PYLON FORWARD UPPER VIBRATION ISOLATOR P/N 7938004-523 S/N 3823 IAW MD80 MM 71-20-02. INSTALLED NEW UPPER ISOLATORS IAW MD80 MM 71-20-03. (M)

Part: FLAP — MISALIGNED (RT WING)

FTW - RIGHT WING INBOARD FLAP INBOARD TRAILING EDGE FLAP MISALIGNMENT PREVIOUS INSTALLATION. REMOVED T/E WEDGE ON INBOARD FLAP. LOCATE AND DRILL TRAILING EDGE. INSTALLED NEW TRAILING EDGE IAW MD80 SRM 51-10-3. (M)

Part: PLATE — GOUGED (RT ENGINE)

FTW - RIGHT FORWARD YOKE UPPER ISOLATOR CUP COVER PLATE GOUGED 2 PLACES INNER RING 4 O'CLOCK AND SCRATCHED AT 10 O'CLOCK POSITION. REMOVED UPPER ISOLATOR IAW MD80 MM 71-20-02. INSTALLED NEW UPPER ISOLATOR CUP IAW MD80 MM 71-20-02. (M)

Part: FRAME — CRACKED (FUSELAGE)

FTW - FRAME ASSEMBLY ANGLE AT STATION Y1427 CRACKED NEAR APU EXHAUST DUCT, BETWEEN LONGERON 11R AND 12R. STOP DRILLED CRACK IAW MD80 SRM 53-01 FIG 2. FABRICATED REPAIR DOUBLERS IAW MD80 SRM 53-01 FIG 2. INSTALLED REPAIR AS REQ'D PER MD80 SRM 53-01 FIG 2. (M)

Part: FLAP — MISALIGNED (RT WING)

FTW - RIGHT WING INBOARD FLAP, OUTBOARD T/E LEADING EDGE FLAP MISALIGNMENT PREVIOUS INSTALLATION. REMOVED TRAILING EDGE FOR REPLACEMENT. INSTALLED NEW TRAILING EDGE IAW MD80 SRM 51-30-2. (M)

Part: AILERON — DELAMINATED (LT WING)

FTW - LEFT WING AILERON TRAILING EDGE IS DELAMINATING. REPAIRED DAMAGED AREA PER SRM MD80 57-03. BALANCED LEFT AILERON PER BOEING DC9/MD80 SRM 57-50-1. (M)

Part: WEDGE — MISALIGNED (T/E FLAP)

FTW - LEFT INBOARD TRAILING EDGE IS MISALIGNED BETWEEN INBOARD AND OUTBOARD SECTIONS. REMOVED LEFT, INBOARD, TRAILING EDGE FLAP THAT WAS MISALIGNED BETWEEN INBOARD AND OUTBOARD SECTIONS. LOCATE AND DRILL T/E WEDGE. INSTALLED TRAILING EDGE WEDGE IAW MD80 SRM 51-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT CORRODED AT STATION Y180 X55 INCHES, BEYOND LIMITS. FOUND FLOOR SUPPORT TO BE OUT OF LIMITS IAW MD-80 SRM 51-10-3. REMOVED IAW MD80 SRM 51-30-20 AND 51-30-8. INSTALLED FLOOR SUPPORT AT STATION Y180 X55 INCHES PER MD80 SRM 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FLOOR SUPPORT CORRODED AT STATION Y164, X41 INCHES. CORRODED FLOOR SUPPORT FOUND TO BE OUT OF LIMITS IAW MD80 SRM 51-10-3. INSTALLED NEW FLOOR SUPPORT FITTING IAW SRM 51-30-5. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND SEAT TRACK RIGHT INBOARD HAS SURFACE CORROSION. REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK. INSTALLED SEAT TRACK IAW MD80 SRM 53-05. (M)

Part: FITTING — CHAFED (CARGO DOOR)

FTW - AFT LOWER CARGO COMPARTMENT CARGO DOOR AFT LATCH FITTING CHAFED. REMOVED LATCH FITTING IAW BOEING MD80 SRM 51-30-1. FOUND TO BE OUT OF LIMITS IAW BOEING MD80 SRM 53-01 AND 52-30-1. REPLACED LATCH FITTING TORQUE TUBE IAW OHM 52-30-1. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND SEAT TRACK RIGHT INBOARD HAVE CORROSION. REMOVED SEAT TRACK. FABRICATED SEAT TRACK AND DRILLED AS REQUIRED. INSTALLED SEAT TRACK IAW MD80 MM 53-40-1. (M)

Part: TORQUE TUBE — DAMAGED (CARGO DOOR)

FTW - FOUND CENTER LOWER CARGO COMPARTMENT, CARGO DOOR TUBE TORQUE/DAMAGE AT F10D LATCH. REMOVED FORWARD TORQUE IAW MD80 MM 52-30-00. INSTALLED FORWARD TORQUE TUBE IAW MD80 MM 52-30-00 MD80 OHM 52-30-1. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT CORRODED FROM STATION Y244 TO STATION Y249, X14 INCH. VERIFY PORT IS OUT OF LIMITS IAW MD80 SRM 53-05. REMOVED SUPPORT IAW MD80 SRM 51-30-2. INSTALLED NEW FLOOR SUPPORT IAW MD80 SRM 51-30-1 AND 51-30-2. (M)

Part: TORQUE TUBE — CORRODED (CARGO DOOR)

FTW - CENTER LOWER CARGO COMPARTMENT CARGO DOOR CORRODED AT AFT TUBE TORQUE. REMOVED AFT MID CARGO DOOR TORQUE TUBE IAW MD80 MM 52-30-00. INSTALLED AFT TORQUE TUBE IAW MD80 MM 52-30-0 AND MD80 OHM 52-30-1. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND SEAT TRACK LEFT OUTBOARD HAS CORROSION AROUND HI-LOCK. REMOVED CORROSION. REMAINING MATERIAL BEYOND LIMITS. REMOVED SEAT TRACK DAMAGE. REPAIRED SEAT TRACK PER MD80 SRM 53-20-01. INSTALLED SEAT TRACK. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - SEAT TRACK LEFT INBOARD HAS SURFACE CORROSION AROUND HI-LOCK. REMOVED CORROSION. MATERIAL LOSS FOUND OUT OF LIMITS. REMOVED SECTION OF SEAT TRACK OUT OF LIMITS. INSTALLED NEW SECTION OF SEAT TRACK IAW MD80 SRM 53-05-0 AND SRM 51-10-5. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND SEAT TRACK CORRODED FROM STATION Y199 TO STATION Y230, X45 INCHES. REMOVED CORROSION ON SEAT TRACK FROM STATION 199-230 BY 45 INCHES CORROSION REMOVAL OUT OF LIMITS IAW MD80 SRM 53-05. REMOVED SEAT TRACK AT FS 199 FS 230 IAW MD80 SRM 51-30-2. INSTALLED NEW SEAT TRACK IAW MD80 SRM 53-04 FIG 4 AND MD80 SRM 51-30-5. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND STATION 1240 SEAT TRACK LEFT INBOARD HAS SURFACE CORROSION. REMOVED CORROSION IAW MD80 SRM 51-10-3. REMAINING MATERIAL OUT OF LIMITS IAW MD80 SRM 53-05. REMOVED SEAT TRACK FROM STATION 1220-1309 IAW MD80 SRM 51-30-01. INSTALLED NEW SEAT TRACK. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

FOUND SEAT TRACK RIGHT INBOARD GOUGED. FOUND CORROSION TO BE OUT OF LIMITS. CUT OUT THE SECTION OF SEAT TRACK. DRILLED AND LOCATE (FABRICATE) SEAT TRACK. INSTALLED SEAT TRACK AT STATION 1031 IAW MD80 SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND SEAT TRACK CORRODED FROM STATION Y200 TO STA Y256, -X22. CORROSION OUT OF LIMITS PER 53-05. REMOVED SECTION OF SEAT TRACK OUT OF LIMITS STATION 200 TO 265 IAW MD80 SRM 53-05-00. INSTALLED SEAT TRACK IAW SRM 53-05 FIG 4. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND SEAT TRACK LEFT OUTBOARD GOUGED AND HAS SURFACE CORROSION ON TOP OF TRACK. BLENDED GOUGE AND CORROSION. REMAINING MATERIAL OUT OF LIMITS. REMOVED SEAT TRACK. INSTALLED SEAT TRACK IAW MD80 SRM 53-05. (M)

Part: SEAT TRACK — CRACKED (FUSELAGE)

FTW - SEAT TRACK RIGHT OUTBOARD CRACKED IN CENTER OF TRACK. REMOVED SECTION OF SEAT TRACK. FABRICATED SEAT TRACK. INSTALLED SEAT TRACK IAW MD80 SRM 53-40-1. (M)

Part: FLAP — DAMAGED (LT WING)

LEFT WING OUTBOARD FLAP TRAILING EDGE IS DELAMINATING. CUT OUT DAMAGED SECTION OF LEFT WING OUTBOARD FLAP TRAILING EDGE. REPAIRED DAMAGED SECTION OF LEFT WING OUTBOARD FLAP IAW DC9/MD-80 SRM 57-03. (M)

Part: FLAP — DAMAGED (LT WING)

FTW - LEFT OUTBOARD TRAILING EDGE FLAP HAS BEEN TEMP REPAIRED AT TRAILING EDGE, OUTBOARD SURFACE. CUT OUT DAMAGED SECTION OF LEFT, OUTBOARD, TRAILING EDGE FLAP. REPAIRED DAMAGED SECTION OF LEFT, OUTBOARD, TRAILING EDGE FLAP IAW DC9 MD80 SRM 57-03. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FLOOR SUPPORT CORRODED AT STATION Y164, X15 INCHES (RECEPTACLE HOLE). REMOVED FLOOR SUPPORT IAW MD80 SRM 53-01. INSTALLED NEW FLOOR SUPPORT PER SRM MD80 51-10-5. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

FTW - CENTER WING TANK TO FUSELAGE SKIN ATTACH ANGLE CORRODED, FS 880L UNDER FLOORWEB. FABRICATED AND DRILLED REPAIR DOUBLERS IAW MD80 SRM 51-10-1 AND EA SCB008. INSTALLED REPAIR IAW EA SCB 008. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - WEB CORRODED AT FRAME FUSELAGE STATION 1412 LOWER AREA. REMOVED CORROSION FROM WEB IAW MD80 SRM 51-10-3. WEB FOUND TO BE OUT OF LIMITS IAW MD80 SRM 53-01. FABRICATED NEW WEB IAW MD80 SRM 53-14-4. INSTALLED WEB AT STATION 1412 IAW MX80 SRM 51-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - AFT LOWER CARGO COMPARTMENT, CORROSION AT FLOOR SUPPORT STATION 1211. FLOOR SUPPORT 1211 WAS FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT STATION 1211. INSTALLED AFT CARGO FLOOR SUPPORT STATION 1211 IAW MD80 SRM 51-30-2 AND 51-30-5. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

FTW - FOUND SEAT TRACK RIGHT INBOARD GOUGED AND PITTED. REMOVED AND SEAT TRACK. FABRICATED, DRILLED AND LOCATED SEAT TRACK. INSTALLED SEAT TRACK IAW MD80 SRM 53-04. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FLOOR SUPPORT CORRODED AT STATION Y174, X44 INCH. SUPPORT FOUND TO BE OUR OF LIMITS IAW MD80 SRM 51-24-00. REMOVED FLOOR SUPPORT IAW MD80 SRM 51-30-2. FABRICATED NEW FLOOR SUPPORT IAW MD80 SRM 51-10-1. INSTALLED FLOOR SUPPORT IAW MD80 SRM 51-50-2. (M)

Part: DAMPER — WORN (RUDDER)

FTW - LOWER RUDDER DAMPER CONTROL ARM ATTACH RIVETS ARE SHEARED OFF COMPLETELY. CONTROL ARM SHOWS WEAR FROM FREE MOVEMENT AND DAMPER MAY HAVE FAILED CAUSING SHEAR. REMOVED LOWER RUDDER DAMPER IAW MD80 MM 27-20-05. INSTALLED LOWER RUDDER IAW MD80 MM 27-20-05. (M)

Part: FLOOR PANEL — CORRODED (COCKPIT)

FTW - COCKPIT FLOOR PANEL BENEATH CO-PILOTS SEAT IS CORRODED. REMOVED FLOOR PANEL, CORRODED OUT OF LIMITS. FORM NEW PANEL PER MD80 SRM 51-10-2. (M)

Part: FLOOR PANEL — CORRODED (COCKPIT)

COCKPIT FLOOR PANEL BENEATH PILOT SEAT IS CORRODED. FOUND TO BE OUT OF LIMITS. FORMED NEW PANEL IAW MD80 SRM 53-21-0. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FLOOR SUPPORT CORRODED AT STATION Y198, X46. REMOVED CORROSION IAW MD-80 51-10-3. FOUND TO BE OUT OF LIMITS IAW MD80 SRM 53-05-00. FABRICATED NEW SUPPORT IAW MD80 SRM 51-00-00. INSTALLED IAW MD80 SRM 51-30-2. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - CENTER FLOORBOARD FS 826-886 CRACKED AFT EDGE. AFTER FURTHER EVALUATION P/N 993639-15 (TWO PIECES) AND P/N 9936639-13 (TWO PIECES) WERE FOUND TO BE OUT OF LIMITS IAW MD80 SRM 51-01. FABRICATED 2 NEW PIECES OF EDGE TRIM IAW MD80 SRM 53-05. INSTALLED SUPPORTS (TWO PIECES) AND EDGE TRIMS (TWO PIECES) PER SRM MD80 51-30-1 ON FLOORBOARD. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - FLOOR PANEL CRACKED AFT EDGE FS 927.2R, OUTBOARD PANEL. STOP DRILLED CRACK IAW MD80 SRM 53-05-0. FABRICATED DOUBLER IAW MD80 SRM 53-05-0. INSTALLED DOUBLER IAW MD80 SRM 51-30-2. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - CENTER LOWER CARGO COMAT, CORRODED AT 29L STRINGER STATION 712 TO STATION 731. REMOVED CORROSION ON LONGERON 29L IAW MX80 SRM 51-10-3, MATERIAL LOSS OUT OF LIMITS. CUT OUT DAMAGED SECTION OF LONGERON. FABRICATED SPLICE FOR LONGERON PER DC9/MD80 SRM 53-02 FIG 14. FABRICATED SPLICE PER DC9/MD80 SRM 53-02 FIG 14. INSTALLED LONGERON AND SPLICES (TWO PIECES) IAW SRM MD80 53-02 FIG 18 AND SRM MD80 51-30-5. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - CENTER LOWER CARGO COMPARTMENT CORRODED AT DOUBLER LEFT SIDE STRINGER 30 STATION 750. REMOVED CORROSION FROM FORWARD FRAME AT STATION 750 IAW MD80 SRM 51-10-3. FOUND TO BE OUT OF LIMITS. FRAME P/N 9936454-5. SPLICE AND DOUBLER REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW MD80 SRM 51-10-3. FORMED SPLICE IAW MD80 SRM 53-34-0 FIG 2, FORMED DOUBLER IAW MD80 SRM 53-34-0 FIG 2. INSTALLED FRAME, SPLICE AND DOUBLER IAW MD80 SRM 51-30-5 AND 51-30-2. (M)

Part: CONTROL PANEL — DEFECTIVE (COCKPIT)

FLT 967 - MCO - CIRCUIT BREAKER FOR DFGS SWITCH A POSITION C17 POPPED DID NOT RESET. TROUBLESHOT DFGS NR 1 AND NR 2 FOUND DEFECTIVE DIGITAL FLT GUIDANCE CONTROL PANEL. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL PANEL IAW MM 22-01-02. SYSTEMS GROUND CHECK GOOD IAW MM 22-00-00. (M)

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT)

FLT 967 - MCO - YAW DAMP ANNUNCIATOR ON IN FLIGHT. REMOVED AND REPLACED DIGITAL FLIGHT GUIDANCE CONTROL PANEL SYSTEM. GROUND CHECKS GOOD IAW MM 22-00-00. (M)

Part: TARGET — OUT OF ADJ (LT MLG DOOR)

FLT 657 - RSW - FOUND GEAR DOOR OPEN ANNUNCIATOR ILLUMINATED AT 33,000, GEAR UP LIGHTS OUT. TURN PUMPS ON HIGH AND ON. ON LEFT MLG DOOR FOUND LEFT TARGET SENSOR GAP OUT OF LIMITS. ADJUSTED TARGET SENSOR TO LIMITS IAW MD-80 MM 32-50-05. (M)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

EWR - FLT 456 - AT CRUISE, GEAR DOOR OPEN LIGHT COMES ON PUMPS ON HIGH LIGHT GOES OUT. PRESS BLEEDS DOWN LIGHT COMES BACK ON. AFTER 20-30 MINUTES LIGHT GOES OUT. BITE TEST, NO MALFUNCTION ON THE GROUND CHECK AND CLEANED CANNON PLUG AND SENSOR FOR GEAR BOX. OK TO CONTINUE MM 32-60-04. (M)

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT)

EWR - FLT 294 - GOING THROUGH 15,000 FT LOST AUTO PILOT, AUTO THROTTLE, YAW DAMPNER AND MACH TRIM. ALSO, ABILITY TO ADJUST SPD/MACH AND LIGHTING ON FMA FOR ALTITUDE. TESTED DIGITAL FLIGHT GUIDANCE SYSTEM. RTS CHECK. ALL CHECK NORMAL PER MM 22-01-05. (M)

Part: RESERVOIR — LACK OF LUBE (HYD SYSTEM)

FLL - FLT 439 - FOUND GEAR DOOR OPEN LGIHT AT FL350. PLACED HYDRAULICS TO HIGH AND ON LIGHT EXTINGUISHED. SERVICED RT RESEVOIR TO FULL BLED AIR FROM SYSTEM OPS CHECK OK IAW 29-00-00 AND 32-00-00. (M)

Part: SLIDE — OUT OF POSITION (L2 DOOR)

UPON ARRIVAL, RAMP AGENT OPENED L2 DOOR IN WHICH SLIDE FELL TO THE GROUND AND BUSTED SLIDE PACK SHELL. REMOVED AND REPLACE L2 SLIDE PACK IAW MD-80 MM 25-60-00. (M)

Part: PANEL — UNSECURE (COCKPIT DOOR)

FLT 1594 - COCKPIT DOOR KEEPS FALLING OUT. RESECURED COCKPIT DOOR LEFT BLOW OUT PANEL IAW MD-80 MM 52-10-00. NO FURTHER DEFECTS NOTED. (M)

Part: SERVO — FAULTY (AUTOPILOT SYS)

LGA - FLT 384 - ON TAKEOFF, AUTOTHROTTLES STOPPED SHORT OF FLEX POWER. DID NOT REDUCE WHEN CLIMB POWER SELECTED RAPID, SMALL CHANGES IN CRUISE. DID NOT ATTEMPT TO USE THEM ON DESCENT AND APPROACH. REMOVED AND REPLACED AUTO THROTTLES SERVO PER MM 22-01. PERFORMED DFGS RTS PER MM 22-01-05. OPS CHECK GOOD. (M)

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT)

DTW - FLT 656 - AUTOTHROTTLES ON TAKEOFF, WHEN CLIMB POWER WAS SELECTED. THROTTLES STAYED AT TAKEOFF POWER. SET MANUALLY THEN REAPPLIED AUTO THROTTLES. AT LEVEL OFF, THROTTLES STAYED SET TO CLIMB POWER. REMOVED AND REPLACED TRI IND, SYSTEM OPS CHECK GOOD IAW MD-80 MM 34-18-02. THIS CLEARS DMI NR 108049-1. (M)

Part: LIGHT — DISCONNECTED (CABIN)

DTW - EMERGENCY LIGHT TRACK, RED AFTER FORWARD CABIN, WILL NOT ILLUMINATE. RECONNECTED FLOOR TRACK LIGHTING IAW MD 80 MM 25-62-00. OPS CHECKED GOOD AT THIS TIME. NO DEFECTS NOTED AT THIS TIME. (X)

Part: CONNECTOR — LOOSE (ROW 20)

EWR - FLT 135 - AFT SECTION OF PATH LIGHTING NOT WORKING. RESEATED BATTERY PACK CONNECTOR AT ROW 20 RT. OPS CHECKED GOOD. (X)

Part: LIGHT — INOPERATIVE (ROW 1-4)

DTW - OVERHEAD EMERGENCY LIGHTS INOPERATIVE, AISLES 1 THROUGH 4. REMOVED AND REPLACED EMERGENCY BATTERY PACK BATTERIES STATION 247. SYSTEM CHECKS GOOD IAW MM 33-52-00. (M)