N802NK
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
93 reports on file, 1999-06-14 – 2005-12-13.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,479 hrs · 25,697 cycles
STA 1136, LT IB SEAT TRACK TANG DIMENSION BELOW 0.90. REMOVED DAMAGED AREA DRILLED NEW TRACK, TREATED, PRIMED AND INSTALLED SPLICE. (K)
Part: SEAT TRACK — CORRODED
RT OB SEAT TRACK FS 493 BOTTOM OF TRACK OUT OF LIMITS, CORROSION. REMOVED CORRODED SEAT TRACK SECTION, DRILLED NEW SEAT TRACK, FABRICATED SPLICE AND PLATE, TREATED, PRIMED AND INSTALLED REPAIR. (K)
Part: DOUBLER — CORRODED (FLOOR)
FWD SERVICE DOOR HAS CORROSION ON FLOOR WEB BETWEEN STA 1460 TO 218. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED DOUBLER AND FABRICATED NEW ONE, TREATED PRIMED AND INSTALLED REPAIR DOUBLER. (K)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FLOOR SUPPORT LBL 5, STA 195-200 HAS CORROSION ALONG LENGTH. REMOVED CORROSION AND FOUND ADDITIONAL CORROSION ON UNDERSIDE OF FLOOR SUPPORT TO BE OUT OF LIMITS, FABRICATED NEW SUPPORT, TREATED PRIMED AND INSTALLED NEW SUPPORT. (K)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FORE AND AFT FLOOR SUPPORTS AT STA 170-195 ON OB LT SEAT TRACK HAS SPOTS OF CORROSION ALONG LENGTH. REMOVED CORROSION ON SUPPORTS FOUND TO BE OUT OF LIMITS, FABRICATED NEW FLOOR SUPPORT ANGLE, TREATED PRIMED AND INSTALLED SUPPORT. (K)
Part: SEAT TRACK — CORRODED (BS 1136)
STA 1136, SEAT TRACK HAS CORROSION. FABRICATED, TREATED AND INSTALLED SECTION OF SEAT TRACK AT STA 1136. (K)
Part: DIAPHRAGM — CORRODED
FWD GALLEY AFT CORNER IB HAS A 6 INCH HOLE CORRODED THROUGH SUBFLOOR WEB. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED DIAPHRAGM AND FABRICATED NEW DIAPHRAGM, TREATED PRIMED AND INSTALLED. (K)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,479 hrs · 25,697 cycles
FLOOR SUPPORT AT STA 198 BETWEEN LT SEAT TRACKS IS CORRODED. REMOVED FLOOR SUPPORT, FABRICATED NEW SUPPORT TREATED AND PRIMED, INSTALLED REPAIR. (K)
Part: ANGLE — CRACKED (STA 946)
ANGLE IS CRCKED IN LT MLG WHEEL WELL FWD DOOR JAMB STRUCTURE STA 946. REMOVED CRACKED ANGLE, FORMED NEW ANGLE, TREATED PRIMED AND INSTALLED REPAIR. (K)
Part: PAN — CORRODED (BS 1155)
CORROSION AROUND CEILING PAN WHERE DRAIN GOES THROUGH AFT CARGO ABOVE STRINGER L-18 AT FS 1155. FABRICATED REPAIR FILLER AND DOUBLER, TREATED AND PRIMED FILLER AND DOUBLER, INSTALLED REPAIR AND NEW FLOOR SUPPORT BRACKET. (K)
Part: ODOR — DETECTED (UNKNOWN)
F/A REPORTED SMELL OF RUBBER BURNING, BETWEEN ROWS 7-11, BUT NO SMOKE NOTED, PRECAUTIONARY DIVERSION INTO SDF. INSPECTED BALLAST BETWEEN ROW 7-11, INSPECTED OXYGEN GENERATORS, INSPECTED EMERGENCY POWER SUPPLIES, INSPECTED PSU PANELS. NO DEFECTS NOTED. (M)
Part: ENGINE — FAILED (NR 2)
1500 FT ON CLIMB-OUT LOUD BANG, NR 2 ENGINE FAILURE, ROLLBACK. ENGINE FAILURE CHECKLIST COMPLETED, OVERWEIGHT LANDING PERFORMED. REMOVED AND REPLACED NR 2 ENGINE, OPS AND LEAK CHECK GOOD. (M)
Part: OVERHEAT SENSOR — MALFUNCTIONED (TAILCONE)
CLIMBING THROUGH 27000 FEET WITH ENGINE AND AIRFOIL ICE ON TAIL COMPARTMENT TEMP HI LIGHT ILLUMINATED, PERFORMED MEMORY ITEMS REQUESTED LOWER ALTITUDE AND VECTOR TO MCO, LIGHT EVENTUALLY WENT OUT FOLLOWED BY FLOW LIGHT ON AUTO PRESSURE CONTROLLER, DIVERTED INTO MCO. LEAK CHECK LT/RT PACKS, WING AND TAIL ANTI-ICE DUCTS AND ASSOCIATED DUCTS FOR LEAKS VIA THE APU AND ENGINE BLEED AIR. NO LEAKS NOTED. REMOVED AND REPLACED LT/RT TAIL COMPARTMENT OVERHEAT SENSORS, SYSTEM OPS CHECK GOOD. (M)
Part: SENSOR — CLOGGED (VENTURI)
UPON CLIMB-OUT, "TAIL COMPT TEMP HI" LIGHT ILLUMINATED, AIR RETURN BACK TO ACY. ENGINE GROUND POWER RUN PERFORMED, LEFT AND RIGHT PACKS OPERATED. NO DUCT LEAKS FOUND, RAN PACKS OFF OF AP. NO LEAKS FOUND. FOUND VENTURI SENSOR CLOGGED WITH DEBRIS, OIL SUBSTANCE, CLEANED VENTURI AND PROBE SENSORS. SYSTEM CHECKED NORMAL. (M)
Part: PACKING — DETERIORATED (NR 1 ENGINE)
AT CLIMB, EPR LEFT THROTTLE 1 AND ONE-HALF KNOB WIDTHS FORWARD OF RIGHT THROTTLE AT 210 CL, AIRCRAFT TAIL SWAP WITH 802. FOUND NOSE INLET BULLET PACKING AND GROMMET DETERIORATED. REMOVED AND REPLACED PACKINGS. THROTTLES STAGGER WITHIN LIMIT, LEAK CHECKED PT7 PROBES AND BELLOWS. NO DEFETS NOTED. (M)
Part: ACTUATOR — MALFUNCTIONED (SLATS)
DURING TAXI OUT, SELECTING FLAPS TO 11 FT THE AUTO-SLAT FAIL LIGHT ILLUMINATED AND THE DISAGREEMENT LIGHT REMAINED ON, RETURNED TO THE GATE AD AIRCRAFT TAIL SWAP WITH N811NK. ADJUSTED S1-467 NO HELP, REMOVED AND REPLACED S1-467 WITH SERVICEABLE UNIT FROM STOCK, STILL NO CURE. REMOVED AND REPLACED AUTO-SLAT ACTUATORS, BOTH AND ADJUSTED S1-467. OPS CHECK GOOD. (M)
Part: COMPUTER — MALFUNCTIONED (STALL WARNING)
LGA - ON TAXI OUT, AUTOSLAT FAIL LIGHT ILLUMINATED WITH FLAPS EXTENDED TO 11 DEGREES, AIRCRAFT TAIL SWAP TO 827. TROUBLESHOT SYSTEM VERIFIED FLAP SLAT HANDLE READING. OPS CHECK GOOD. REMOVED AND REPLACED NR 1 AND NR 2 AUTOSLAT ACTUATORS. NO HELP. PERFORMED CONTINUITY CHECKS OF SLAT ACTUATORS. NO FAULTS NOTED. REMOVED AND REPLACED NR 2 STALL WARNING COMPUTERS. SYSTEM CHECKS GOOD. (M)
Part: SKIN — DAMAGED (FUSELAGE)
WHILE PUSHBACK FROM GATE, AIRCRAFT TUG WENT OVER 90 DEGREES AND HIT AIRCRAFT PUTTING HOLE ON THE RT SIDE OF AIRCRAFT APPROX FS 275. REPAIR AT RT FUSELAGE SKIN BETWEEN L22 AND L24, NOSE GEAR SUPPORT WEB HAS BEEN INSTALLED IAW EA, REV.A HAS BEEN ACCOMPLISHED. (K)
Earlier reports · 1999–2004 · 75 reports
2004
Part: LINE — CHAFED (FUEL SYSTEM) · airframe 27,956 hrs · 24,564 cycles
STRONG FUEL SMELL IN CABIN WITH APU RUNNING. ITEM TRANSFERRED TO DMI 02911151 IAW MEL 49-1-0. CAT (C). PLACARD INSTALLED. FOUND FUEL LINE ON FUEL HEATER (APU) CHAFED THROUGH, REMOVED LINE AND ROUTED LINE SO IT DOES NOT CHAFE, LEAK CHECK GOOD.
Part: ISOLATOR — OUT OF LIMITS (NR 1 ENGINE)
DTW - FOUND NR 1 UPPER ISOLATOR REQUIRES CHANGE, OUT OF LIMITS. REMOVED AND REPLACED NR 1 UPPER FORWARD VIBRATION ISOLATOR. (M)
Part: BLADE — LOOSE (NR 1 ENGINE)
FOUND NR 1 ENGINE HAS 5 LPT BLADES LOOSE AT 5 LBS. REMOVED AND REPLACED NR 1 ENGINE. (M)
Part: MANIFOLD — CRACKED (NR 2 ENGINE)
NR 2 ENGINE WAS REMOVED FOR T-4 BLADE NOTCH BREAKOUT AND COMPRESSOR STALLING. TEARDOWN CONFIRMED THAT ONE T-4 BLADE HAD NOTCH BREAKOUT. FURTHER DISASSEMBLY REVEALED A BROKEN 8TH STAGE BLEED MANIFOLD WITH DIFFUSER INNER FAN DUCT AND DIFFUSER OUTER FAN DUCT LINER DELAMINATION ASSOCIATED WITH THE 8TH STAGE BLEED VALVE BEING STUCK OPEN DUE TO THE LOSS OF 8TH STAGE BLEED VALVE MANIFOLD PRESSURE.
Part: SLIDE — DISCHARGED (L2 DOOR)
RSW - FOUND L2 DOOR SLIDE PACK PRESSURE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PACK. (M)
Part: SIGN — INOPERATIVE (EMERGENCY LIGHT)
FTW - FOUND NUMEROUS EMERGENCY LIGHTS IN CABIN INOPERATIVE. EXIT IDENTIFIER MISSING. INSTALLED NEW R1 DOOR EXIT SIGN. (M)
Part: FLOORBOARD — CRACKED (FUSELAGE)
FTW - FOUND FLIGHT COMPARTMENT CENTER FLOOR PANEL STATION 148 TO STATION 160 HAS SEVERAL CRACKS ON EDGES AND CORRODED AT INSERTS. FABRICATED NEW FLOORBOARD. (M)
Part: LONGERON — CHAFED
FTW - FOUND LONGERON 8R AT FS 1280-1401 IN AFT ACC COMP CHAFED. REMOVED SECTION OF LONGERON FROM STATION 1391-1427. LOCATED AND DRILLED NEW SECTION AND ONE SPLICE. INSTALLED NEW SECTION LONGERON AND SPLICE. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
FTW - FOUND CENTER CABIN FLOORBOARD STATION FS 200-256 INSERTS PULLED THROUGH. FABRICATED FLOORBOARD. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FOUND FLOOR SUPPORT AT STATION 200 TO 260 LBL 15 HAS CORROSION. REMOVED FLOOR SUPPORT. FLOOR SUPPORT FABRICATED. INSTALLED FLOOR SUPPORT. (M)
Part: CUSP WEB — CORRODED (FUSELAGE)
RT CUSP WEB AT 1174, 1210 HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE)
FLOOR PANEL LT IB STA 200-260 DELAMINATED EDGE. FAB NEW FLOOR PANEL.
Part: SEAT TRACK — CORRODED (FUSELAGE)
CABIN RT IB SEAT TRACK LT CORRODED AND WORN STA 200-1309. MATERIAL FOUND OUT OF LIMITS FROM STA 200 TO 267. REMOVED RT, IB SEAT TRACK. FABRICATED NEW SECTION SEAT TRACK. INSTALLED SEAT TRACK.
Part: FLOORBOARD — DELAMINATED (FUSELAGE)
PAX CABIN FLOOR PANEL STA 1155-1250 DELAMINATED. FAB NEW CABIN.
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FOUND FLOOR PANEL LEFT OUTBOARD STATION 1097-1155 CRACKED. REPAIRED FLOOR PANEL. (M)
Part: WEB — CRACKED (FUSELAGE)
CABIN FLOOR WEB CRACKED STA 1176, LBL 18 INCHES. FABRICATED DOUBLER REPAIR AND FILLER. INSTALLED WEB DOUBLER REPAIR AND FILLER.
Part: WEB — CORRODED
CABIN STA 1210-1220 STR 18R WEB CORRODED. CUT OUT DAMAGED AREAS. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER.
Part: WEB — CORRODED (FUSELAGE)
CABIN STA 522-541 STR 18R WEB CORRODED. FABBED WEB. INSTALLED WEB.
Part: WEB — CORRODED (FUSELAGE)
FTW - FOUND CABIN STATION 799 STRINGER 18R WEB CORRODED. FABRICATED DOUBLER. ROUTED OUT CRACK. INSTALLED DOUBLER. (M)
Part: CUSP WEB — CRACKED (FUSELAGE)
RT OB CUSP. WEB HAS A CRACK AT STA 270 AND AT STA 278. CUT OUT CRACKED SECTIONS OF CUSP WEB AT STA 270 AND 278. FABRICATED REPAIR DOUBLERS AND SPLICES. INSTALLED REPAIR DOUBLERS.
Part: VANE — CORRODED (TE FLAP)
FOUND INBOARD FLAP VANE OF OUTBOARD FLAP HAS CORROSION AND MISSING SCREW. REMOVED DAMAGED AREA. SKIN ALTERNATE ID 2024T81 SUBSTITUATION FOR 2075T6- .016 HOT BONDED REPAIR. (M)
Part: FLOOR PANEL — CRACKED (COCKPIT)
COCKPIT STA 127 LBL 6 FLOOR WEB CRACKED. TRIMMED OUT CRACK. FABRICATED FILLER AND DOUBLER. INSTALLED DOUBLER AND FILLER.
Part: SEAT TRACK — CORRODED (FUSELAGE)
CABIN RT OB SEAT TRACK LT CORRODED AND WORN. RT OB SEAT TRACK FROM STA 200 TO 300 OUT OF LIMITS. REMOVED SEAT TRACK. LOCATED AND DRILLED HOLES FOR SEAT TRACK FROM STA 200 TO 300 RT OB. INSTALLED NEW SEAT TRACK SECTION.
Part: ANGLE — CORRODED (FS)
FTW - FOUND TEE ANGLE EXFOLIATED IN AFT ACCY COMP AT FS 1474 15 INCHES LBL, NEAR LONGERON 3L. REMOVED 'T' ANGLE. FABRICATE 'T' ANGLE. INSTALLED 'T' ANGLE. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
LT OB CABIN SEAT TRACK LT CORRODED AND WORN STA 200-1309. OUT OF LIMITS FROM STA 200-300 AND 1030-1206. REMOVED LT OB SEAT TRACK STA 1030 TO 1206. INSTALLED LT OB SEAT TRACK STA 200 TO 300. FABRICATED SEAT TRACK LT OB STA 1030-1206. REMOVED LT OB SEAT TRACK FROM STA 1030-1206. INSTALLED 2 EA SPLICES. INSTALLED SEAT TRACK STA 1030-1206.
Part: FLOORBOARD — DAMAGED (COCKPIT)
COCKPIT RT FLOORBOARD, DELAMINADED AND EDGE DAMAGED. FAB RT COCKPIT FLOORBOARD.
Part: STOP FITTING — CORRODED (CARGO DOOR)
FTW - FOUND FORWARD CARGO PIT ALL SET SCREWS RUSTY AND CORRODED. LOCATED AND DRILLED TWO NEW DOOR STOPS STATION 427 AT L26R AND L21R. INSTALLED NEW TWO DOOR STOPS STATION 427 AND L26R-L21R. INSTALLED NEW TWO DOOR STOPS AT STATION 428/389, L20R. INSTALLED NEW DOOR STOPS AT STATION 370 L26R. (M)
Part: BEAM — CORRODED (CARGO DOOR FRAME)
FTW - FOUND AFT CARGO LOWER DOOR JAMB BEAM HAS CORROSION. REMOVED AFT PIT JAMB BEAM. LOCATED AND DRILLED NEW BEAM. INSTALLED NEW BEAM. UPON FURTHER INSPECTION INTERCOSTAL FOUND TO BE OUT OF LIMITS. FABRICATED NEW INTERCOSTAL. INSTALLED NEW INTERCOSTAL. (M)
Part: SIGN — MISSING (G-4 GALLEY)
DEN - FLT 367 - SAFETY GLOW EXIT SIGN AT G-4 GALLEY L-2 DOOR MISSING. FOUND PIECE SERVICABLE/REINSTALLED EXIT SIGN. (M)
2003
Part: SLIDE — DISLODGED (PAX DOOR)
FOUND L-2 DOOR SLIDE PACK FELL FROM DOOR. REMOVED AND REPLACED L-2 SLIDE PACK. (M)
Part: RIB — CRACKED (LE SLAT)
FOUND SMALL CRACK ON INTERNAL RIB OF NR 1 L/E SLAT ON LT WING. REMOVED AND REPLACED NR 1 SLAT ON LEFT WING. (M)
Part: WIRE — BROKEN (EMERGENCY LIGHT)
AFT STAIRWAY OVERHEAD EMERGENCY LIGHT IS INOPERATIVE DUE TO A BROKEN WIRE. REPAIRED WIRE AT AFT STAIRWAY OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — BROKEN (CABIN)
ACY - FOUND FORWARD EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT ASSEMBLY FUNCTIONAL CHECK GOOD. (M)
Part: LINER — DAMAGED (NR 2 ENGINE)
FLL - NR 2 ENGINE NOSE COWL ACCOUSTIC LINER DAMAGE. NR 2 ENGINE NOSE COWL AND T/R ASSEMBLY, REMOVED AND REPLACED. (M)
Part: WIRE — BROKEN (EMERGENCY LIGHTS)
FLL - TAILCONE EMERGENCY LIGHTS DO NOT WORK. REPAIRED BROKEN WIRES, OPS CHECK NORMAL. (M)
2002
Part: CYLINDER — DEFECTIVE (NLG STEERING)
DTW - ON APPROACH TO DENVER, THE NOSE GEAR DID NOT INDICATE DOWN WHILE THE MAINS DID. AFTER CYCLING THE GEAR, THE SAME INDICATION RESULTED. UPON REVIEW OF PROPER CHECK LIST, WITH MANUAL GEAR EXT, LEVER PULLED, AND GEAR HANDLE DOWN. THE SAME INDICATION RESULTED. THERE WAS SEVERAL ATTEMPTS AT YAWING THE A/C. FINALLY AFTER STOWING THE MANUAL LEVER AND CYCLING THE GEAR, THE SAME INDICATION RESULTED AGAIN. AFTER STOWING THE A/C FOR THE 3RD TIME AND JERKING THE YOKE. THE NOSE GEAR EXTENDED. HAD PROPER INDICATION AND LANDED. REMOVED AND REPLACED RIGHT AND LEFT NOSE STEERING CYL. (M)
Part: CONTACTOR — DIRTY (CABIN)
FTW - FOUND EMERGENCY OVERWING LIGHTS INOPERATIVE. T/S SYSTEM IAW MD80 MM 33-53-00 FOUND FAULTY LAMP CONTACTS, CLEANED CONTACT SYSTEM OPS CHECKS GOOD. (M)
Part: DOOR FRAME — CORRODED (FUSELAGE)
FTW - FOUND MID B/B DOOR, LOWER JAMB CORROSION FROM 636-693. REMOVED JAMB BEAM. LOCATED AND DRILLED NEW DOOR BEAM. INSTALLED JAMB BEAM PER MD80 SRM 51-30-5. (M)
Part: INTERCOSTAL — DAMAGED (FUSELAGE)
FTW - FOUND AFT ACC AREA FRAME T-CAP AT AFT SHROUD OF APU HAS CORROSION AT STATION 1401, 27L-27R. INTERCOSTAL AT FS 1380 TO 1401 LBL 13 IS FOUND TO BE OUT OF LIMITS. FABRICATED NEW INTERCOSTAL. FRAME AT 1394 IS CRACKED. FABRICATED NEW FRAME. REMOVED LOWER T-CAP. LOCATED AND DRILLED NEW LOWER T-CAP. FOUND CRACK ON RT LEG OF VERTICAL BEAM. REMOVED VERTICAL BEAM. LOCATED AND DRILLED NEW RT VERTICAL BEAM. INSTALLED T-CAP. INSTALLED VERTICAL BEAM. INSTALLED RT INTERCOSTAL.
Part: FRAME — CORRODED (FUSELAGE)
FTW - FOUND AFT ACC AREA FRAME T-CAP AT AFT SHROUD OF APU HAS CORROSION STATION 1401, 27L-27R. INTERCOSTAL AT FS 1380 TO 1401 BL13L IS FOUND TO BE OUT OF LIMITS. FABRICATED NEW INTERCOSTAL. FRAME AT FS 1394 RT BL 13R IS CRACKED. FABRICATED NEW FRAME. REMOVED LOWER T-CAP. LOCATED AND DRILLED NEW LOWER T-CAP. FOUND CRACK ON RIGHT LEG OF VERTICAL BEAM. REMOVED VERTICAL BEAM. LOCATED AND DRILLED NEW RIGHT SIDE VERTICAL BEAM. INSTALLED T-CAP. INSTALLED VERTICAL BEAM. INSTALLED RIGHT INTERCOSTAL. (M)
Part: FRAME — CRACKED (FUSELAGE)
FTW - FOUND AFT ACC AREA FRAME T-CAP AT AFT SHROUD OF APU HAS CORROSION AT STATION 1401, 27L-27R. INTERCOSTAL AT FS 1380 TO 1401 LBL 13 IS FOUND TO BE OUT OF LIMITS. FABRICATED NEW INTERCOSTAL. FRAME AT 1394 RBL 13 IS CRACKED. FABRICATED NEW FRAME. REMOVED LOWER T-CAP. LOCATED AND DRILLED NEW LOWER T-CAP. FOUND CRACK ON RT LEG OF VERTICAL BEAM. REMOVED VERTICAL BEAM. LOCATED AND DRILLED NEW RT VERTICAL BEAM. INSTALLED T-CAP. INSTALLED VERTICAL BEAM. INSTALLED RT INTERCOSTAL.
Part: SEAT TRACK — DAMAGED (FUSELAGE)
FTW - FOUND LEFT OUTBOARD SEAT TRACK APPROXIMATELY STATION 807, 788, 768, 750, 731, 712, 693, 674, 655, 636, 617, 598, 560 AND 541. GOUGES AND CORROSION IN TRACK, APPROX STATION 807, 788, 768, 758 740, 731, 712, 693, 623, 674 AND 655 CORROSION AND GOUGES AT SCALLOPS. MATERIAL LOSS IS OUT OF LIMITS LEFT OUTBOARD SEAT TRACK STATION 715 AND 790. REMOVED DAMAGED SECTION TO SPLICE AT STATION 798. FABRICATED NEW SEAT TRACK SECTION. INSTALLED SEAT TRACK. (M)
Part: SKIN — DENTED (LT NOSE COWL)
FTW - FOUND LEFT ENGINE COWL HAS DENT ON LIP AT 7 O'CLOCK POSITION. REMOVED LEFT ENGINE NOSE COWL. INSTALLED SERVICEABLE NOSE COWL. (M)
Part: SKIN — DENTED (FUSELAGE)
FTW - FUSELAGE TEMP REPAIR ON DENT AT STATION 237 LEFT SIDE BETWEEN LONGERON 19 AND 20. REMOVED TEMP REPAIR DOUBLER AT STATION 237 LEFT SIDE LONGERON 19 AND 20. CUT OUT DAMAGED AREA FROM STATION 239-250 LONGERON 19-20. FABRICATED FINGER DOUBLER. FABRICATED REPAIR DOUBLER. INSTALLED ALL REPAIR PARTS, DOUBLERS, FILLERS, FINGER DOUBLERS, STRAPS. (M)
Part: MEGAPHONE — INOPERATIVE (CABIN)
DEN - FLT 313 - MID MEGAPHONE INOPERATIVE. (M)
Part: SLIDE — OUT OF POSITION (GALLEY DOOR)
LAX - AFT GALLEY DOOR OPENED BY CLEANERS, SLIDE PACK FELL OFF. RESTOWED AFT GALLEY DOOR SLIDE PACK. OPS CHECK IAW MM 25-00-00. (M)
Part: SKIN — CRACKED (RT WING)
FOUND CRACK ON LOWER RIGHT WING AT APPROX STATION XFS 281.750 ABOUT 1 INCH LONG, ON LEADING EDGE NEAR FUEL PANEL. REPAIRED CRACK IAW MD80 SRM 57-06A. (M)
Part: WIRE — BROKEN (TRIM SWITCH)
RSW - FLT 926 - CAPTAINS LONGITUDINAL TRIM SWITCH WILL NOT WORK IN THE NOSE DOWN POSITION. REPAIRED BROKEN WIRE C1209A20 IN FORWARD CARGO PIT RIGHT TUNNEL FOR CAPTAINS PRIMARY TRIM, OPS CHECK NORMAL. (M)
Part: BATTERY — DISCHARGED (CABIN)
MCO - AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY IAW M 33-53-00. LIGHTS CHECK OK. (M)
Part: BATTERY — DISCHARGED (CABIN)
FLL - EMERGENCY LIGHTS AT EMERGENCY EXIT AFT ON LEFT AND RIGHT SIDES ROW 22AC AND 22DEF ARE INOPERATIVE. REMOVED AND REPLACED BATTERIES IN THE CONT. UNIT FOR LT AND RIGHT AFT EMERGENCY EXIT ROW OVERHEAD LIGHTS. OPS CHECK GOOD IAW MM 33-50-00. (M)
Part: LATCH — BROKEN (R1 DOOR)
FLT 165 - PBI - FOUND SLIDE PACK R1 DOOR WILL NOT LATCH. REPAIRED BROKEN LATCH. SYSTEM OPERATES NORMALLY IAW MD80 MM 25-62-00, NO OTHER DEFECTS NOTED. (M)
Part: LATCH — BROKEN (SLIDE PACK)
ACY - FOUND SLIDE PACK R1 WILL NOT LATCH. REPAIRED BROKEN LATCH SYSTEM OPERATES NORMALLY IAW MD-80 MM 25-62-00. NO OTHER DEFECTS NOTED. (M)
Part: PUMP — INOPERATIVE (FUEL BOOST)
ORD - FLT 1225 - AFT CENTER BOOST PUMP INOPERATIVE. LOW PRESSURE LIGHT ILLUMINATES WTH AFT CENTER PUMP ONLY RUNNING. PULLED AND RESET CIRCUIT BREAKER. LIGHT GOES OUT FOR 25 SECONDS THE ILLUMINATES. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M)
2001
Part: ACCELEROMETER — FAULTY (AUTOPILOT SYS)
DFGS DOES NOT WORK EITHER AP 1 OR 2, WILL NOT CAPTURE ALTITUDE, HOLD ALTITUDE IN A TURN THERE IS IMMEDIATE DESCENT, DOES NOT WORK IN PERF ON EITHER SIDE BOTH COMMAND BARS DISAPPEAR FROM VIEW WHEN TO GO BUTTONS ARE PUSHED PRIOR TO TAKEOFF THE IAS MACH BUTTON DOES NOT WORK. REMOVED AND REPLACED ACCELEROMETER IAW 22-14-05 AUTO PILOT REQUIRES RTS IAW 22-01-05. (M)
Part: PANEL — CRACKED (RT WING)
DTW - EVIDENCE OF FUEL LEAK AT RIGHT WING LOWER PANEL NR 1406C. FOUND FUEL PANEL 1460C TO BE CRACKED. REMOVED AND REPLACED FUEL PANEL 1460C AT RT LOWER WING SURFACE IAW MD80 MM 57-30-03, REF M22 12343 FOR LEAK CHECK. (M)
Part: LIFE VEST — MISSING (CABIN)
DTW - LIFEVEST MISSING AT SEAT 11A. REPLACED MISSING LIFEVEST AT SEAT 11A IAW MD-80 MM CHAPTER 25-61-00. (M)
Part: LIFE VEST — MISSING (CABIN)
DTW - FLT 476 - LIFEVEST MISSING AT SEAT 9F. REPLACED MISSING LIFE VEST AT SEAT 9F IAW MD-80 MM CHAPTER 25-61-00. (M)
2000
Part: POWER SUPPLY — INOPERATIVE (CABIN)
MIDDLE SECTION OF EMERGENCY TRACK LIGHTING INOP. REPLACED EMERGENCY POWER SUPPLY. OPS CHECK GOOD IAW MD80 M/M 33-53-01.
Part: LIGHT — LOOSE (ROW 10)
CLE - FLT 1404 - EMERGENCY EXIT AISLE PATH LIGHTING RAISED AT ROW 10. RESET PATH LIGHTING TRACK COVER INTO TRACK IAW CH 33. (M)
Part: COVER — LOOSE (CABIN)
DTW - EMERGENCY PATHWAY LIGHT COVER LOOSE. REATTACHED PATHWAY LIGHT COVER. (M)
Part: COVER — LOOSE (CABIN)
CLE - EMERGENCY PATHWAY LIGHT COVER STRIP IS LOOSE. SECURED ALL FLOORS COVERS. OPS CHECKS GOOD. (M)
Part: COVER — LOOSE (CABIN)
MCO - FLT 135 - PLASTIC COVERING ON EMERGENCY TRACK LIGHTING COMING OFF AROUND ROW 8. SECURED PLASTIC COVERING ON EMERGENCY TRACK LIGHTING ON ROW 8 SECTION PER MM 33-50-00. (M)
Part: LIGHT — INOPERATIVE (ROW 8)
DTW - EMERGENCY AISLE LIGHTING OUT AT SEAT ROW 8. RELAMPED OPS CHECK GOOD IAW MD 80 MM 33-40-00. (M)
Part: WARNING SYSTEM — ACTIVATED (COCKPIT)
CLE - FLT 1401 - AFTER PUSH BACK, WARNING ON OVERHEAD SPEAKER. RESET RADIO ALT. OPS CHECK GOOD. (X)
Part: LIGHT — MISSING (CABIN)
DTW - RIGHT OVERWING EMERGENCY EXIT ROW EPL TRACK MISSING 2 SMALL DIVIDER COVERS UNDER THE TOP CLEAR PLASTIC COVER. INSTALLED MISSING COVERS IN EPL TRACK AT RIGHT OVERWING EMERGENCY EXIT ROW. (M)
Part: LIGHT — LOOSE (ROW 20-22)
DTW - FLT 378 - AISLE PATH LIGHTING BAR OFF THROUGH ROWS 20-22, A/C RIGHT. REMOVED AND REPLACED BULBS IN EMERGENCY LIGHTS FLOOR. (M)
Part: LIGHT — INOPERATIVE (AIRSTAIR)
DTW - EMERGENCY LIGHT IN VENTRAL STAIRS INOPERATIVE. RELAMPED EMERGENCY LIGHT IN AFT VENTRAL STAIRS, OPS CHECKED GOOD PER MD80 MM 33-22-00. NO OTHER DISCREPANCIES NOTED. (M)
Part: COVER — LOOSE (CABIN)
EMERGENCY PATH LIGHT COVER OFF. INSTALLED COVER. (M)
Part: LIGHT — LOOSE (ROW 8)
CLE - FLT 1402 - AISLE TRACK LIGHT LOOSE AT ROW 8. SECURED TRACK LIGHT SECTION ROW 7 THROUGH 10. OK FOR SERVICE. (M)
Part: COVER — MISSING (CABIN)
DTW - EMERGENCY LIGHT COVER IN FORWARD GALLEY MISSING. INSTALLED EMERGENCY LIGHT COVER IN FORWARD GALLEY IAW MD80 MM 33-50-00. OPS CHECK GOOD. (M)
1999
Part: LIGHT — LOOSE (CABIN)
FLL - FLT 47 - COVER ON AISLE TRACK LIGHTING LOOSE, CARPET STICKING UP. RESECURED TRACK LIGHTING AND CARPET AS REQUIRED. (M)
Part: LIGHT — LOOSE (CABIN)
DTW - FLT 712 - EMERGENCY FLOOR LIGHTING TRACK, 1ST THREE ROWS, WILL NOT STAY ATTACHED TO FLOOR. RESECURED FLOOR LIGHTING TRIM COVER IAW MD-80 MM 33-50-00. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DTW - EMERGENCY FLOOR TRACK LIGHTS BETWEEN ROWS 17 AND 21 INOPERATIVE. RESET BATTERIES AT STATION B5-237 PACK. OPERATIONAL CHECK GOOD IAW MM 33-50-00. (M)
Part: LIGHT — INOPERABLE (ROWS 6-16)
DTW - EMERGENCY EXPRESS LIGHTS ROWS 6-16 DO NOT ILLUMINATE. PERFORMED OPERATION CHECK, OPERATION CHECKED GOOD IAW MD-80 MM 33-50. (X)
Part: LIGHT — INOPERATIVE (CABIN)
DTW - EMERGENCY LIGHT PASSENGER OVERHEAD SOME BURN OUT. ALSO, TAIL COMPARTMENT LENS MISSING ON LIGHT. TAIL COMPARTMENT EMERGENCY RAMP LIGHT. EMERGENCY LIGHT AND LENS REPLACED IAW MD 82/83 MM 33-00-50. (M)