N806NK
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.
190 reports on file, 1999-12-02 – 2003-12-29.
Part: SEAL — DAMAGED (NR 2 ENGINE)
NR 2 ENGINE FUEL LEAK. INSTALLED SEAL ON LINE GOING FROM PYLON TO NR 2 FUEL BRIDLE LINE. PERFORM LEAK AND OPERATIONAL CHECK OF FUEL DISTRIBUTION FUEL BRIDLE. (M)
Part: PROXIMITY SENSOR — FAILED (LT MLG)
RED LIGHT REMAINED ON IN LEFT MAIN GEAR AFTER RAISING HANDLE. RECYCLED GEAR ALL INDICATIONS NORMAL. RAISED GEAR AND LEFT MAIN RED LIGHT ON AGAIN. NO VIBRATIONS RUMBLINGS OR WARNINGS ABOVE 300 KIAS. LEFT ALL HYDRAULIC PUMPS ON HIGH AS A PRECAUTION AND CONTINUED FLIGHT. GEAR INDICATIONS NORMAL WITH GEAR DOWN. TROUBLESHOT AND FOUND LEFT MAIN GEAR UPLOCK SENSOR D1-26 AT FAULT. REMOVED AND REPLACED D1-26 PROX SENSOR AS PER MM 32-60-05. OPS NORMAL ON GORND AS PER MM 32-60-05. (M)
Part: TRANSMITTER — FAILED (FUEL FLOW)
RSW - FLT 1504 - LEFT ENGINE HAD EXCESSIVE FUEL FLOW 5100 NR/HR AT CRUISE ALT 31,000 FEET DID QRH FOR HIGH FUEL FLOW. TROUBLESHOT TO FUEL FLOW TRANSMITTER, REMOVED AND REPLACED LEFT FUEL FLOW TRANSMITTER. OPS AND LEAK CHECK GOOD. (M)
Part: CONTROL VALVE — STUCK (LT PACK TEMP)
VERY COLD IN CABIN, BOTH PACKS IN AUTO-LOST PRESSURE CABIN ALT CLIMBING EVEN THOUGH OUTFLOW VALVE FULL FWD AND LOCKED EMERGENCY DECENT AND DIVERTED. CAUGHT CABIN ALT (COULD NOT CONTROL CABIN) AND IT DESCENDED WITH AIRCRAFT RIGHT AIRCRAFT PAC SHUTDOWN CABIN ALT LIGHT ON. TRANSFER LOCKOUT AND STANDBY BLUE LIGHTS ON. TROUBLESHOT SYSTEM FOUND LEFT WING ANTI-ICE THERMOSTAT GASKET BLOWN. ALSO FOUND LEFT PACK TEMP CONTROL VALVE STRUCK IN COLD POSITION, REMOVED AND REPLACED VALVE. INSTALLED NEW GASKET LEFT WING ANTI-ICE THERMOSTAT PERFORMED CABIN PRESSURE OPERATION. NO DEFECTS NOTED. BOTH TEMP CONTROL VALVES OPERATES NORMALLY IN AUTO AND IN MANUAL, OK TO CONT.
Earlier reports · 1999–2002 · 186 reports
2002
Part: BLADE — DAMAGED (NR 1 ENGINE)
FTW - FOUND DURING DAILY INSPECTION, TWO BLADES IN NR 1 ENGINE C1 STAGE DAMAGED. INSPECTED TWO BLADES OUT OF LIMITS IAW 72-00-00. REMOVED AND REPLACED 1 BLADE IN MATCH SET AMM 72-33-00. (M)
Part: ENGINE — VIBRATION (NR 1)
DURING CRUISE, A STRONG VIBRATION NOTICED AND ERRATIC EPR AND OIL QUANTITY. HIGH OIL TEMPERATURE, REDUCED LT THROTTLE AND VIBRATION SUBSIDED BUT DID NOT GO AWAY. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AND LANDING. REPLACED NR 1 ENGINE IAW MM. OPS CHECK GOOD ON ENGINE RUN.
Part: SKIN — CRACKED (FUSELAGE)
DTW - FOUND AFT CARGO PIT DOOR SKIN CRACKED AT HANDLE POCKET AREA. STOP DRILLED CRACK AND INSTALLED SCUFF PLATE IAW MD80 SRM 52-05. (M)
Part: WIRE — DISCONNECTED (A/C BAY)
DTW - FOUND EMERGENCY LIGHTS ABOVE TAIL COMPARTMENT WALKWAY INOPERATIVE. RECONNECTED WIRES TO LIGHT. OPS CHECKS GOOD IAW 33-53-02. (M)
Part: PROXIMITY SENSOR — FAULTY (LT MLG)
ORD - FLT 1226 - RED LEFT MAIN GEAR INDICATOR LIGHT FLICKERED OCCASIONALLY IN CLIMB-OUT FROM FL200 TO FL280 THEN REMAINED OUT. FOUND LEFT MAIN UPLATCH PROXIMITY SENSOR BAD. REMOVED AND REPLACED LEFT MAIN UP LATCH PROX SENSOR. SYSTEM OPS CHECKS GOOD. PERFORMED PROX BOX TEST. OPS CHECK GOOD. (M)
Part: WIRE — BROKEN (LT MLG)
MCO - FLT 1927 - CLIMBING THROUGH 10,000 FEET LEFT RED GEAR UNSAFE LIGHT CAME ON PERFORMED QRH PROCEDURE. LIGHT REMAINED ON. FOUND BROKEN WIRE AT LEFT POSITION SWITCH. REPAIRED BROKEN WIRE. OPS CHECK NORMAL IAW MD80 MM 32-60-01. (M)
Part: COMPUTER — MALFUNCTIONED (COCKPIT)
FLT 1453 - ORD - AUTO PILOT WILL NOT ENGAGE ON NR 1 OR NR 2 DFGC. FOUND A/P HEAR BEAT FAILS ON BOTH NR 1 AND NR 2 DFGC. REMOVED AND REPLACED NR 1 AND NR 2 DFGC. OPS CHECKED GOOD PER MD80 MM 22-01-05. NO OTHER DISCREPANCIES NOTED. (M)
Part: CONTROL PANEL — FAILED (NAVIGATION)
FLT 1751 - SJU - DFGS 2 WHEN SELECTED WILL NOT CAPTURE VOR RADIAL COURSE BECAUSE THE SYSTEM WILL NOT ARM. IT WILL ARE THE LOCK INSTEAD BUT THERE IS NO LOCALIZER FRQ DIALED IN. AUTOPILOT WILL DISENGAGE DFGS NR 1 WORKS FINE. REMOVED AND REPLACED NR 2 VHF/NAV CONTROL PANEL PERFORMED RTS CHECK TEST SYSTEM GIVES 'GO' INDICATION. (M)
Part: GYRO — FAULTY (E/E BAY)
FLT 779 - LGA - WITH DFGC NR 2 SELECTED AND AP ENGAGED, YOKE OSCILLATES BACK AND FORTH. REVIEWED FLIGHT LOGS ON STP FO NR 1 AND NR 2 AND DETERMINED SENSOR SIGNAL FAULTS ON NR 2 ATTITUDE SYSTEM RECORDED ON SEVERAL FLIGHT LEGS. REMOVED AND REPLACED THE NR 2 VG, OPS CHECK GOOD. (M)
Part: GYRO — FAULTY (E/E BAY)
MCO - FLT 1864 - FOUND AUTOPILOT DFGC ON NR 1 HAS ERRATIC JERKING PITCH CONTROL ESPECIALLY NOTICEABLE IN CLIMB/DESCENT. REVIEWED THE FLT MEMORY LOGS ON THE NR 1 DFGC SYSTEM AND DETERMINED ATTITUDE SENSOR FAULTS ON SEVERAL FLIGHT LEGS. REMOVED AND REPLACED THE VERTICAL NR 1 VERTICAL GYRO, OPS CHECK GOOD. (M)
Part: SERVO — DAMAGED (AUTOPILOT SYS)
LGA - FLT 779 - FOUND AUTO PILOT PUMPS UP AND DOWN IN CLIMBS, TURNS AND CRUISE. DETERMINED M PINS AND P DAMAGED ON THE J2 RECEPTACLE ON THE ELEVATOR SERVO. REMOVED AND REPLACED THE ELEVATOR SERVO, OPS CHECK GOOD. (M)
Part: LATCH — OUT OF ADJUST (RT MLG DOOR)
FTW - FOUND RIGHT MLG UNSAFE LIGHT ILLUMINATED ON RETRACT, EXTINGUISHED ON CLIMB-OUT. AFTER TROUBLESHOOTING FOUND MAIN GEAR DOOR LATCH MECH. NO PROPERLY ADJUSTED. INSTALLED SHIM AND ADJUSTED MAIN GEAR DOOR LATCH MECH. (M)
Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG DOOR)
FTW - FOUND RIGHT GEAR MLG DOOR INDICATES RED. RIGHT MLG LIGHT STAYED ON WITH TRANSFER PUMP. ADJUSTED PROX SENSOR IAW MD80 33-60-05. (M)
Part: CONTROL HANDLE — OUT OF ADJUST (COCKPIT)
FTW - TEST FLIGHT FAILED, UNABLE TO RAISE GEAR HANDLE. PERFORMED TROUBLESHOOTING AND FOUND LANDING GEAR CONTROL LEVER AND ANTI-RETRACTION LATCH OUT OF RIG. ADJUSTED LANDING GEAR CONTROL LEVER AND ANTI-LATCH. (M)
Part: COMPUTER — FAILED (COCKPIT)
FTW - FOUND DFGS 1 AND 2 RTS FAIL TEST WITH FOLLOWING FAULTS, NOTED AIL MECH TORQUE 1 FAIL, AIL MECH TORQUE 2 FAIL, SPOILER POSITION FAIL. NR 18 PER POSITION XMITTER. ADJUSTED FLAP POSITION TRANSMITTERS FOR AIL MECH. TORQUE 1 FAIL AND AIL MECH TORQUE 2 FAIL. (M)
Part: WIRE — DISCONNECTED (TAILCONE)
FTW - FOUND EMERGENCY EXIT LIGHTS IN TAIL CONE INOPERATIVE. T/S SYSTEM FOUND WIRES NOT CONNECTED. CONNECTED WIRES TO CORRECT LIGHT ASSEMBLY. (M)
Part: WIRE — BROKEN (HORIZ STAB)
FTW - FOUND ALTERNATE TRIM CONTROL LEVERS ON CONTROL PEDESTAL INOPERATIVE. TROUBLESHOT, FOUND 4 SPLICE IN THE TAIL (HORIZ STAB) PULLED OUT, NEED TO RESPLICE. REPAIRED BROKEN WIRES RESPLICED. (M)
Part: FITTING — CORRODED (FUSELAGE)
FTW - MID CARGO FITTING STATION 827 RIGHT INBOARD CORRODED GOUGED AND BARE METAL. REMOVED CORROSION. FABRICATED FITTING. PART WAS INSTALLED. (M)
Part: BRACKET — CORRODED (FUSELAGE)
FTW - FOUND BRACKET CORRODED AT STATION Y 826, ABOVE LONGERON 29R, FOUND AFTER REMOVAL OF LONGERON. BRACKET OUT OF LIMITS. FORMED BRACKET. (M)
Part: BRACKET — CORRODED (FUSELAGE)
FTW - FOUND BRACKET CORRODED AT STATION Y826, ABOVE LONGERON 29L. FOUND AFTER REMOVAL OF LONGERON. MATERIAL LOSS OUT OF LIMITS. FORMED NEW BRACKET. (M)
Part: SUPPORT BRACKET — CORRODED (FUSELAGE)
FTW - FOUND R1 DOOR THRESHOLD FLOOR SUPPORT AND TWO GIRT BAR LATCH SUPPORT BRACKETS CORRODED. GIRT BARS FOUND OUT OF LIMITS. LOCATE AND DRILLED GIRT BARS FITTING. (M)
Part: FLOOR SUPPORT — CRACKED (FUSELAGE)
FTW - FOUND FLOOR SUPPORT CRACKED AT FS 148, -X45, -X45 TO -X54. REMOVED FLOOR SUPPORT. FORMED NEW SUPPORT, INSTALLED. (M)
Part: FLOORBOARD — CRACKED (FUSELAGE)
FTW - PASSENGER CABIN, AFT FUSELAGE AREA FLOORBOARD X 45L FROM STATION Y 1115 TO STA Y 1256 CORNER CRACKED, INSERTS MISSING AND BROKEN. FORM NEW PANEL. (M)
Part: BRACKET — CRACKED (FUSELAGE)
FTW - FOUND BRACKET CRACKED AT FS 1338, ABOVE LONGERON 24R. REMOVED BRACKET, FORMED NEW BRACKET. INSTALLED NEW BRACKET. (M)
Part: FLOORBOARD — CRACKED (FUSELAGE)
FTW - PASSENGER CABIN, AFT FUSELAGE AREA FLOORBOARD FROM STATION 1115-1236 CORNER CRACKED, INSERTS MISSING AND BROKEN. FORM NEW PANEL. (M)
Part: FITTING — DAMAGED (FUSELAGE)
FTW - FOUND MID CARGO STATION 779 TO 826 LONGERON FITTING L30 CHAFING, GOUGES, AND CORROSION. REMOVED CORROSION, MAT FOUND TO BE OUT OF LIMITS. REPLACED LONGERON 30 END FITTING WITH NEW LONGERON END FITTING. (M)
Part: FITTING — CORRODED (FUSELAGE)
FTW - FOUND MID CARGO STATION 788 TO 826 LONGERON FITTING 29R GOUGES, CHAFING CORROSION. FOUND LONG FITTING OUT OF LIMITS. LOCATED AND DRILLING LONGERON 29R. PART INSTALLED. (M)
Part: FITTING — CORRODED (FUSELAGE)
FTW - FOUND MID CARGO FITTING STATION 827 RIGHT INBOARD GAUGES BARE METAL. REMOVED CORROSION MATERIAL FOUND TO BE OUT OF LIMITS. FABRICATED A NEW FITTING. PART WAS INSTALLED ON 18-N-00375. (M)
Part: FITTING — CORRODED (FUSELAGE)
FTW - MID CARGO FITTING STATION 827 LEFT INBOARD CORROSION GAUGES AND BARE METAL. REMOVED CORROSION. FABRICATED FITTING. PART INSTALLED. (M)
Part: FITTING — CORRODED (FUSELAGE)
FTW - FOUND MID CARGO FITTING TWO STATION 827 OUTBOARD LEFT GAUGES, BARE METAL. REMOVED CORROSION MATERIAL FOUND TO BE OUT OF LIMITS. FABRICATED TWO NEW FITTINGS. PART WAS INSTALLED. (M)
Part: LONGERON — CORRODED (FUSELAGE)
FTW - FOUND MID CARGO STATION 788 TO 826 LONGERON 29L ELONGATED HOLES, GOUGES, AND CORROSION. FOUND LONGERON OUT OF LIMITS. LOCATED AND DRILLING LONGERON 29L. PART WAS INSTALLED. (M)
Part: FITTING — DAMAGED (FUSELAGE)
FTW - FOUND MID CARGO FITTING STATION 827 OUTBOARD RIGHT CHAFING ELONGATED HOLES, GOUGES, BARE METAL. FABRICATED A NEW FITTING PER SPIRIT AIRLINES EA 5310-0212. (M)
Part: CONTROL QUADRANT — CORRODED (FLIGHT CONTROL)
FTW - FOUND RUDDER AND ELEVATOR CABLE QUADRANT AFT OF PRESSURE BULKHEAD STATION 1338 -X30 CABLE KEEPER AND QUADRANT CORRODED AND BLUEWATER STAINED. REPLACED CABLE KEEPER PINS ON RUDDER AND ELEVATOR CABLE QUADRANT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND COCKPIT FLOOR SUPPORT STATION 150 PLUS X5 TO -X5 CORROSION. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)
Part: ATTACH FITTING — CORRODED (TAIL CONE)
FTW - FOUND TAIL CONE BENT UP AT HOUSING TAIL CONE ATTACH PLATE SHEAR, 12 PLACES. UPON INSPECTION, FOUND ATTACH PLATE CORROSION. FORMED REPAIR DOUBLERS. INSTALLED REPAIR DOUBLERS. (M)
Part: DOUBLER — CRACKED (FUSELAGE)
FTW - FOUND SEAT TRACK CLOSEOUT DOUBLER HAS CORROSION AND IS CRACKED STATION 200 PLUS X43. REMOVED SEAT TRACK DOUBLER. FORM NEW DOUBLER. INSTALLED DOUBLER. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND CABIN FLOOR SUPPORT AT STATION 1155 PLUS X24 TO PLUS X48 IS CORRODED. REMOVED CABIN FLOOR SUPPORT. FORMED LOCATED AND DRILLED FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)
Part: WEB — CRACKED (FUSELAGE)
FTW - FOUND CABIN AT STATION 1197, LEFT SIDE, SUB FLOOR/WEB UNDER GALLEY DRAIN FLANGE IS CRACKED. CUT OUT DAMAGED AREA. FABRICATED DOUBLER AND FILLER. INSTALLED REPAIR PARTS. (M)
Part: WEB — CORRODED (FUSELAGE)
FTW - FOUND SUB FLOOR STATION 200-218 APPROX PLUS X23 TO -X48 HAS CORROSION AND BLOWN OUT FASTENER HOLES. REMOVED DAMAGED WEB. FABRICATED NEW SECTION OF SUB FLOOR. INSTALLED WEB. (M)
Part: LONGERON — CORRODED (FUSELAGE)
FTW - FOUND FORWARD B/B LONGERON 30 CORROSION FROM STATION 522 TO 560. MID CARGO CENTER SECTION STATION 560 LONGERON 30 CORROSION. REMOVED CORROSION. REMOVED LONGERON AT STATION 512 TO 585. FOUND MORE CORROSION AT FRAME THAT CONNECT LONGERON AT STATION 541. REMOVED CORROSION AT FRAME STATION 541. REMOVED DAMAGE AREA OF FRAME FS 541 FROM LONGERON 28L TO 28R. INSTALLED LONGERON SPLICE REPAIR. INSTALLED FRAME REPAIR. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
FTW - FOUND CABIN SEAT TRACK LEFT OUTBOARD TRACK FLANGE FROM STATION 1155 TO 1231 IS CORRODED. REMOVED DAMAGE ON SEAT TRACK. INSTALLED SEAT TRACK AND SPLICE FORWARD AND AFT. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FLIGHT AND FORWARD PASSENGER COMPARTMENT FLOOR PANEL RIGHT STATION 148.5 TO STATION 167.5 HAS CRACKED/DAMAGE MUSHY. FABRICATED NEW PANEL. (M)
Part: ACCESS PANEL — DELAMINATED (LT WING)
FTW - FOUND LEFT WING BOTTOM SIDE ACCESS PANEL INBOARD OF MLG, ANTI-SKID VALVE MOUNT PANEL IS DELAMINATED. REMOVED ACCESS PANEL. REPAIRED LEFT WING BOTTOM SIDE PANEL OF MLG. INSTALLED ACCESS PANEL. (M)
Part: WEB — CORRODED (FUSELAGE)
FTW - FOUND COCKPIT AREA FLOOR PANEL WEB CORRODED SEVERAL PLACES BETWEEN STA Y 133 AND Y 160, X30 TO -X22, CORROSION AS FOUND AFTER CORRODED FLOOR SUPPORT REMOVAL. REMOVED COCKPIT WEB LBL 45 TO RBL 20 FS 160-140. FABRICATED NEW WEB. FORMED NEW WEB SPLICE. COPILOTS INBOARD SEAT TRACK OUT OF LIMITS. FLOOR SUPPORT AT STATION 160 X 20 HAS CORROSION. FORMED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT AT STATION 160 X20. INSTALLED WEB AND WEB SPLICE. (M)
Part: WEB — CORRODED (FUSELAGE)
FTW - FORWARD ENTRY AREA FLOOR PAN (WEB) CORRODED SEVERAL PLACES BETWEEN STATION Y 160 AND Y 200, X43 TO -X53, CORROSION WAS FOUND AFTER FLOOR SUPPORTS REMOVAL. REMOVED FLOOR PAN (WEB) FROM STATION 160-200, LBL 43 TO RBL 41. FABRICATED NEW SECTION FLOOR PAN (WEB). FLOOR SUPPORT STATION 195 LBL 16 TO 43 OUT OF LIMITS. FABRICATED NEW FLOOR SUPPORT AT STATION 195 TO LBL 16 TO 43. FORMED NEW WEB SPLICE. INSTALLED WEB SPLICES. INSTALLED FLOOR SUPPORT AT STATION 195 LBL 16 TO LBL 43. (M)
Part: ANGLE — CORRODED (FUSELAGE)
FTW - FOUND 'L' ANGLE CORRODED AT FS 147, BY 12.5, LOWER AREA OF EPC PANEL. REMOVED ANGLE. FORMED 'L' ANGLE. INSTALLED 'L' ANGLE. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FLOOR SUPPORT CORRODED AT STATION Y 147 TO 159, X13 LOWER AREA OF EPC PANEL. REMOVED FLOOR SUPPORT. FORMED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
Part: WEB — CORRODED (FUSELAGE)
FTW - FOUND CABIN RIGHT GALLEY AFT OF SERVICE DOOR G-2, OUTBOARD SIDE HAS CORROSION AT FLOOR AREA. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, INSTALLED REPAIR. (M)
Part: CLIP — CRACKED (RT ENGINE)
FTW - RIGHT ENGINE FORWARD LOWER VIBRATION ABSORBER CLIP CRACKED. REMOVED RIGHT ENGINE FORWARD LOWER VIBRATION ABSORBER CLIP. FABRICATED REPAIR CLIP. INSTALLED REPAIR CLIP. (M)
Part: CAMSHAFT — CORRODED (CARGO DOOR)
FTW - AFT CARGO DOOR LOCK BAR AND MECH ARE RUSTY. REMOVED AFT CAM SHAFT ROD FROM AFT CARGO DOOR. INSTALLED NEW CAM SHAFT ROD ON AFT CARGO DOOR. (M)
Part: PANEL — CORRODED (LT WING)
FTW - FOUND LEFT WING PANEL NR 1165C HAS BARE METAL AND CHAFE MARKS AROUND EDGES. CORROSION FOUND TO BE OF LIMITS. RECEIVED SERVICEABLE PART. (M)
Part: WEB — CRACKED (FUSELAGE)
FTW - FOUND MEMBRANE PANEL AT STATION 973 TO STATION 1003 RIGHT SIDE HAS CRACKED AND PEELING OFF. STOPPED DRILLED THE CRACK. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
FTW - AFT CARGO TRACK STATION 1003-1155 HAS CORROSION AND ELONGATED HOLES. REMOVED CORROSION FROM AFT CARGO TRACK AND Z-ANGLE. FABRICATED NEW CARGO TRACK. INSTALLED CARGO TRACK. (M)
Part: BRACKET — BROKEN (FUSELAGE)
FTW - FOUND CORROSION BETWEEN L30 AND L29R AND ON STRAP AT FUEL TANK. MID CARGO STATION 779 TO 826 LONGERON FITTING L30 CHAFING, GAUGES, AND CORROSION. REMOVED CORROSION. FABRICATED NEW FILLER TWO DOUBLERS. INSTALLED FILLER AND DOUBLER. FABRICATED ANGLE AND STRAP. FABRICATED FINGER DOUBLER. INSTALLED REPAIR ANGLE,STRAP AND TRAP FILLER. AFTER FURTHER EVALUATION FOUND BRACKET BROKEN AT STATION 788 LONGERON 28L. DRILLED UP AND LOCATED NEW BRACKET. INSTALLED NEW BRACKET. (M)
Part: LONGERON — CORRODED (FUSELAGE)
FTW - FOUND FORWARD B/B STATION 408 TO FORWARD BULKHEAD HAS MANY AREAS OF CORROSION ON L30. AREA FOUND TO BE OUT OF LIMITS AT L30 STATION 294. REMOVED LONGERON L30 STATION 264-320. INSTALLED LONGERON L30 STATION 264-320. (M)
Part: FRAME — CORRODED (FUSELAGE)
FTW - RIGHT AFT LAVATORY STATION 1338 -X45 TO -55 FRAME WEB IS CORRODED ON FORWARD AND AFT SIDES, WEB TORN/CRACKED AT X30 TO -33 INBOARD AND OUTBOARD SIDE OF LIGHTENING HOLE. FLOOR SUPPORT BEAM HAS TEAR 1 INCH TO 2 INCHES LONG AT LIGHTENING HOLE FS 1338, 36 INCHES RT OF C/L UNDER RT LAVATORY. REMOVED DAMAGED WEB. FABRICATED WEB AND DOUBLER. INSTALLED WEB AND DOUBLER AT FS 1338 -X10 TO -X58. (M)
Part: FLOOR SUPPORT — CRACKED (FUSELAGE)
FTW - FOUND PASSENGER COMPARTMENT AND FLOOR SUPPORT CRACKED AT MEMBRANE WEB STATION 1309 PLUS X50. FORMED REPAIR DOUBLER. INSTALLED IAW MD80 SRM 51-30-2. (M)
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
FTW - FOUND FORWARD FLIGHT COMPARTMENT FLOOR PANEL STATION 120.050 TO STATION 160 HAS MUSHY SOFT, RIGHT SIDE. FABRICATED NEW FLOOR PANEL. (M)
Part: LONGERON — CORRODED (FUSELAGE)
FTW - FOUND BLUE WATER AND STAINS FOUND IN LONGERON 30 FROM FORWARD BULKHEAD TO BULKHEAD IN FORWARD BAG BAY. REMOVED CORROSION. REMOVED LONGERON 30 STATION 323-494. DRILLED AND LOCATED LONGERON STATION 323-494. INSTALLED LONGERON 30. (M)
Part: FLOOR PANEL — DELAMINATED (FUSELAGE)
FTW - FOUND PASSENGER COMPARTMENT FLOOR PANEL (MEMBRANE PHENOLIC) RIGHT OUTBOARD STATION 1271 TO STATION 1309 HAD DELAMINATED. REPAIRED COMPARTMENT FLOOR PANEL. (M)
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
FTW - PASSENGER COMPARTMENT FLOOR PANEL (CENTER) STATION 1271 TO STATION 1309, HAS MUSHEY SOFT. FABRICATED NEW FLOORBOARD CENTER STATION 1271-1309. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FLIGHT AND FORWARD PASSENGER COMPARTMENT FLOOR PANEL RIGHT OUTBOARD STATION 148.5 TO STATION 167.5 HAS CRACKED MUSHY RACK 8. FORM NEW PANEL FOR STATION 148.5 TO 167.5. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND STATION 1309 -X17 TO +X17 FLOORBOARD SUPPORT UPPER SURFACE IS CORRODED. REMOVED PART. FABRICATED NEW PART AND INSTALLED. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FOUND FLOOR PANEL STATION 598-636 IS CRACKED/DAMAGE MID PIT. FORM NEW PANEL. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
FTW - FOUND INTERNAL ACCESS PANEL CENTER COCKPIT (FLT COMPT) STATION 120 HAS MUSHY SOFT DAMAGE. FABRICATED NEW FLOORBOARD. (M)
Part: ACCESS PANEL — CRACKED (FUSELAGE)
FTW - FOUND MID CARGO JAMB ACCESS PANEL STATION 693 RIGHT CRACKED AND HAS CORROSION AROUND FASTENER HOLES. ACCESS PANEL AREA FOUND OUT OF LIMITS. DRILLED UP AND LOCATED NEW PANEL. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FLIGHT AND FORWARD PASSENGER COMPARTMENT FLOOR PANEL RIGHT OUTBOARD STATION 148.5 TO STATION 167.5 HAS CRACKED MUSHY (SOFT). FORM NEW PANEL FOR STATION 148.5-167.5. (M)
Part: SKIN — CRACKED (CARGO DOOR)
FTW - FORWARD CARGO DOOR AFT SIDE (NEAR LOCK MECH) CHAFED, GOUGED, AND INNER AND OUTER SKIN CRACKED. CUT OUT DAMAGE. FABRICATED FILLER. FABRICATED DOUBLER. INSTALLED FILLER AND DOUBLER. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND AFT CARGO FLOOR SUPPORT STATION 1212 HAS CORROSION AND DOUBLE DRILLED HOLES. FOUND BE OUT OF LIMITS. DRILLED UP AND LOCATED NEW SUPPORT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FLIGHT FORWARD COMPARTMENT PRESSURE AND FLOOR SUPPORT, CORRODED AT SUPPORT FLOOR STATION 120.050. REMOVED FLOOR SUPPORT FROM A/C. FORMED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FLIGHT COMPT FLOOR PANEL UNDER CAPTS SEAT HAS CRACKED/DAMAGE. FABRICATED NEW FLOOR PANEL. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - PASSENGER COMPARTMENT FLOOR PANEL LEFT INBOARD STATION 1271-1309 HAS CRACKED MUSHY SOFT. FABRICATED REPAIR FLOORBOARD. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - PASSENGER COMPARTMENT FLOOR PANEL AT STATION 1271-1309 HAS CRACKED/DAMAGE. FABRICATED NEW PANEL. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FLIGHT AND FORWARD PASSENGER COMPARTMENT FLOOR PANEL STATION 148.5-167.5 HAS CRACKED/DAMAGE. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FOUND FLIGHT AND FORWARD PASSENGER COMPARTMENT FLOOR PANEL LEFT STATION 148.5 TO STATION 167.5 HAS CRACKED/MISSING INSERT. FABRICATED NEW FLOOR PANEL. (M)
Part: LONGERON — CORRODED (FUSELAGE)
FTW - FOUND PIT LONGERON 28R STATION 1117 TO STATION 1155 CORRODED. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED NEW LONGERON SECTION. FABRICATED NEW LONGERON SPLICE. INSTALL LONGERON. INSTALLED SPLICE. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
FTW - AFT PIT CORRODED AT INTERCOSTAL STATION 1193 BETWEEN 28R, 29R. REMOVED CORROSION. FORMED INTERCOSTAL. INSTALLED INTERCOSTAL. (M)
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
FTW - FOUND FLOOR PANEL STATION 946-1003 CENTER MUSHY SOFT AND HAS BLUE WATER STAINS. FABRICATED NEW FLOOR PANEL. (M)
Part: FLOOR PANEL — DELAMINATED (FUSELAGE)
FTW - FOUND FLOOR PANEL STATION 864 TO STATION 886 LEFT SIDE HAS DAMAGE/DELAMINATED. FABRICATED REPAIR FLOORBOARD. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FOUND FLOOR PANEL LEFT STATION 769-826 CRACKED/DAMAGE. FORM NEW PANEL. (M)
Part: CLIP — CORRODED (FUSELAGE)
FTW - FOUND FORWARD B/BAY STATION 372 CLIP FOR THRESHOLD HAS CORROSION. REMOVED CORROSION. REMOVED PARTS CLIPS AND T-ANGLE. FABRICATE CLIP. INSTALLED SUPPORT 2ND CLIP. (M)
Part: PANEL — CORRODED (LT WING)
FTW - FOUND LEFT WING PANEL NR 1163C HAS BARE METAL AND SURFACE CORROSION AROUND EDGES. REMOVED CORROSION. MAT LOSS IS OUT OF LIMITS. COUNTERSINK NEW PANEL. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FOUND FLOOR PANEL LEFT INBOARD STATION 927-1003 HAS CORROSION UNDER PANEL AND CRACKED. FABRICATED NEW FLOORBOARD. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FOUND FLOOR PANEL INBOARD STATION 826-869 CRACKED/DAMAGED. FABRICATED NEW PANEL. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FOUND FLOOR PANEL LEFT STATION 826-864 CORRODED, BLUE WATER STAINS, CRACKED. FABRICATED FLOORBOARD REPAIR. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FOUND FLOOR PANEL INBOARD LEFT STATION 886-927 CRACKED/DAMAGED. FABRICATED REPAIR FLOORBOARD. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FOUND FLOOR PANEL AFT CABIN FRONT AFT ENTRY DOOR SEVERAL CRACKED, BLUE WATER STAINS, ELONGATED HOLES. FABRICATED NEW PANEL. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FOUND FLOOR PANEL INBOARD RIGHT STATION 886-927 HAS PUNCTURE/CRACKED. FABRICATED REPAIR FLOOR BOARD. (M)
Part: WEB — CRACKED (FUSELAGE)
FTW - FOUND MEMBRANE PANEL CRACKED/DAMAGED AT CORNERS STATION 826-927 RIGHT SIDE. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FOUND FLOOR PANEL INBOARD RIGHT STATION 796-826 CRACKED/DAMAGE. FORM NEW PANEL. (M)
Part: FLOOR PANEL — DELAMINATED (FUSELAGE)
FTW - FOUND FLOOR PANEL RIGHT INBOARD STATION 927-1002 DELAMINATED/DAMAGE. FABRICATED REPAIR FLOORBOARD. (M)
Part: LONGERON — CORRODED (FUSELAGE)
FTW - FOUND CORROSION ON LONGERON 30 IN MANY PLACES FROM STATION 408-446. SECTION OF LONGERON FOUND OUT OF LIMITS. (M)
Part: LONGERON — CORRODED (FUSELAGE)
FOUND CORROSION FORWARD B/BAY LONGERON R-28 STATION 446-427 AS MARKED. AREA FOUND TO BE OUT OF LIMITS. REMOVED Z-ANGLE. FABRICATED Z-ANGLE, LOCATED AND DRILLED Z-ANGLE. INSTALLED Z-ANGLE. (M)
Part: FLOORBOARD — BROKEN (FUSELAGE)
FTW - FOUND COCKPIT FLOORBOARD NR 4415C CRACKED AND BROKEN OUT ALONG EDGE AND LIGHT SURFACE CORROSION ON BACK. FABRICATED A REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
FTW - FOUND FLOOR PANEL STATION 886-946 CENTER HAS CRACK AT FLANGE SUPPORT PANEL DELAMINATED. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 218, X13 TO X7. REMOVED CORROSION. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 200, -X9.5 TO -X46. REMOVED CORROSION. REMOVED FLOOR SUPPORT. FABRICATED, INSTALLED FLOOR SUPPORT. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA, SEAT TRACK CORRODED AT FS 232-X22. REMOVED SECTION AREA FROM STA Y 200 TO Y 266. LOCATED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK AND SPLICE. (M)
Part: ANGLE — CORRODED (SERVICE DOOR)
FTW - FOUND FORWARD GALLEY SERVICE DOOR, ANGLE ATTACHED TO DOOR BELOW INTERIOR DOOR HANDLE HAS LIGHT CORROSION. FABRICATED NEW ANGLE. INSTALLED NEW ANGLE. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT STATION Y160 TO STA Y 197, X55. REMOVED FLOOR SUPPORT. FABRICATED NEW SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 160 X13. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 200, -46 TO -X57. REMOVED CORROSION FROM FLOOR SUPPORT. FABRICATED NEW PART. INSTALLED FLOOR SUPPORT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 200 X5 TO X-5. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA SEAT TRACK CORRODED AT FS 200-255, -X22. REPLACEMENT OF SEAT TRACK FROM STATION 200-226. REMOVED CORRODED SEAT TRACK. LOCATED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK AND SPLICE. (M)
Part: SUPPORT — DAMAGED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA, BEARING SUPPORT FOR FORWARD AIRSTAIR HANDLE MECH, FS 160-164 X10 TO X13. REMOVED BEARING AND SUPPORT. INSTALLED BEARING AND BRACKET ASSEMBLY. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS Y162 TO Y197, X44. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT FS 160 TO 200 X7. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED TRACK. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT FS 160 TO 200, -X7. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 218, -X12. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED NEW FITTING. INSTALLED FITTING. (M)
Part: CHANNEL — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA, CHANNEL CORRODED AT FS 160, X13. FABRICATED CHANNEL AND SPLICE. INSTALLED REPAIR. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT HAS CORROSION AT FS 188 AND 197, UNDER HAT CHANNEL -X54. REMOVED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. PART WAS FABRICATED. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT FS 161 TO 199, -X44. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT AT STATION 161-199. INSTALLED FLOOR SUPPORT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 210 -12. REMOVED CORROSION. REMOVED FLOOR SUPPORT. FORMED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA SEAT TRACK CORRODED AT FS 200 TO 225 -X44. REMOVED CORROSION. REMOVED SEAT TRACK SDT 200 TO 246 -X44. DRILLED AND LOCATED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT FS 180, X13 TO X38. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT FS 237, X13 TO -X15.5. REMOVED CORROSION ON FLOOR SUPPORT. REMOVED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 200 X9 TO X13. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 195-220, X15. REMOVED FLOOR SUPPORT FROM A/C. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 160 X5 TO -X5. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT FS 180, -X9.5 TO -43. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
Part: ATTACH ANGLE — CRACKED (RT WING)
FTW - RIGHT WING CRACK AT ANGLE ATTACH NOSE CAP VORTILON. REMOVED VORTILON FAIRING ATTACH ANGLE. STOP DRILLED CRACK ANGLE. UPON REMOVAL OF VERTICAL ANGLE FITTING FOUND TO BE CRACKED. FABRICATED REPAIR DOUBLERS. LOCATED AND DRILLED HOLES IN NEW ATTACH ANGLE. INSTALLED REPAIR. INSTALLED FITTING. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA, FLOORBOARD FROM STATION 200-260 -X22 TO -X43 HAS INSERTS MISSING, CORNER CRACKED AND EDGES DAMAGED. FABRICATED NEW FLOORBOARD. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA, FLOORBOARD FROM STATION 180-200 -X7 TO -X43 HAS INSERTS MISSING AND DELAMINATION. FORM NEW FLOOR PANEL. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA, FLOORBOARD FROM STATION 160-200 X11 TO X46 HAS MISSING INSERTS, BROKEN INSERTS, EDGES DELAMINATED. FORM NEW PANEL. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FORWARD ENTRY AREA FLOOR SUPPORTS AT R1 DOOR AREA STATION 160 AND 200 -X52 HAVE CORROSION. REMOVED CORROSION. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)
Part: ATTACH ANGLE — CRACKED (FUSELAGE)
FTW - FOUND CRACK ON FLOORBOARD ATTACK ANGLE BETWEEN L26 AND L27 STATION 712. REMOVED ANGLE FOM WELDED. INSTALLED ANGLE. (M)
Part: WEB — CORRODED (FUSELAGE)
FTW - CABIN RIGHT FORWARD GALLEY AFT OF SERVICE DOOR (G-2) LOWER SIDE AT FLOOR HAS CORROSION. REMOVED CORROSION. LOCATED AND DRILLED PARTS. INSTALLED REPAIR PARTS. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
FTW - FORWARD ENTRY AREA, FLOORBOARD FROM STATION 160-200 X6-X6 HAS INSERTS MISSING, BROKEN AND DELAMINATION. FORM NEW PANEL. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FTW - FOUND FRAME AT 731 BETWEEN LONGERON L29 AND R29 HAS CORROSION ON INTERCOSTAL 2 PLACES. REMOVED CORROSION ON FLOOR SUPPORT. REMOVED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
FTW - FOUND FORWARD ENTRY AREA FLOORBOARD FROM STATION 160-200 X48-X55 HAS INSERTS MISSING, BROKEN AND EDGES DAMAGED. FABRICATED NEW FLOORBOARD. (M)
Part: INTERCOSTAL — CRACKED (PAX DOOR)
FTW - FOUND FORWARD PASSENGER DOOR INTERNAL STRUCTURE, FRAME CRACKED BETWEEN LL BEAM 4 AND 5 STATION Y185.5. REMOVED INTERCOSTAL AT STATION Y 185.5 DRILLED AND LOCATED NEW INTERCOSTAL. INSTALLED INTERCOSTAL. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
FTW - FORWARD ENTRY AREA, FLOORBOARD FROM STATION 200-260 X23 TO X44 HAS MISSING INSERTS, BROKEN INSERTS, PUNCTURES AND CORNERS CRACKED. FABRICATED NEW FLOORBOARD. (M)
Part: STRUCTURE — CORRODED (FUSELAGE)
FTW - FOUND CABIN RIGHT FORWARD GALLEY (G-1) INBOARD SIDE AT FLOOR HAS CORROSION. REMOVED CORROSION. FABRICATED REPAIR. INSTALLED PARTS. (M)
Part: SKIN — GOUGED (PAX DOOR)
FTW - FORWARD PASSENGER DOOR EXTERNAL SURFACE (HOLD/OPEN) HOOK CUT OUT AREA HAS GOUGES. REMOVED DAMAGE FROM FORWARD PASSENGER DOOR HOOK CUT OUT AREA OUT OF LIMITS. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER. (M)
Part: WEB — CORRODED (FUSELAGE)
FTW - FOUND CABIN RIGHT FORWARD GALLEY AFT OF SERVICE DOOR (G2) FORWARD SIDE OF AFT BULKHEAD AT FLOOR HAS CORROSION. REMOVED DAMAGED AREA. FABRICATED INNER SKIN. INSTALLED INNER SKIN. (M)
Part: SLIDE — UNSECURE (TAIL CONE)
FTW - FOUND AFT FUSELAGE COMPARTMENT TAIL SLIDE UNPACKED. REMOVED SLIDE. TAIL CONE INSTALLED. (M)
Part: FITTING — CRACKED (NLG)
FTW - FOUND NLG WHEEL WELL LEFT TRUNNION WEB FORWARD UPPER IN FITTINGS CRACKED. REMOVED. INSTALLED NEW FITTINGS. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
FTW - FOUND AFT PIT/CABIN FLOOR, STATION 1155-1174 PLUS X23 LEFT MIDDLE SEAT TRACK AND SPLICE ARE CORRODED. REMOVED SEAT TRACK AT STATION 1098-1211. FABRICATED AND DRILLED UP NEW TRACK AND SPLICES. INSTALLED NEW SEAT TRACK AND TWO SPLICES. (M)
Part: WEB — CORRODED (FUSELAGE)
FTW - AFT PIT/CABIN FLOOR, STATION 1193 PLUS X45 TO SIDE OF BODY, CORROSION ON LOWER SURFACE OF SUB FLOOR. CUTOUT DAMAGED AREA OF SUB FLOOR AT STATION 1193. LOCATED AND DRILLED FILLER AND DOUBLER. INSTALLED REPAIR PART AT STATION 1193. (M)
Part: DOOR FRAME — CRACKED (FUSELAGE)
FTW - FOUND RIGHT FWD MLG DOOR JAMB CRACKED AT INBOARD SUPPORT PREVIOUS DOUBLER REPAIR -X 6.25. REMOVED DOUBLER REPAIR AND TEE ANGLE. AFTER FURTHER EVALUATION ADDITIONAL CRACK WAS FOUND, LOCATED AND DRILLED NEW PARTS. FABRICATED 2 CHANNELS TO BE USED AS SPLICE FOR NEW DOOR JAMB. INSTALLED TWO CHANNELS. (M)
Part: ISOLATOR — MISALIGNED (RT ENGINE)
FTW - RIGHT ENGINE FORWARD LOWER ISOLATOR ALIGNMENT MARK WAS MISALIGNED. REMOVED RIGHT ENGINE FORWARD LOWER ISOLATOR. INSTALLED NEW ISOLATOR. (M)
Part: SKIN — DETERIORATED (RT WING)
FTW - FOUND RIGHT WING LOWER SURFACE DELAMINATED/DETERIORATED AT PANEL TRAPEZOIDAL. REMOVED DELAMINATED SKIN FROM RIGHT WING TRAP PANEL. REPAIRED DELAMINATION. (M)
Part: SKIN — CRACKED (FUSELAGE)
FTW - FOUND RIGHT EXTERIOR FUSELAGE SKIN CRACKED AT STATION Y 1381 LONGERON 14R. REMOVED DAMAGE AT STATION 1381 LONGERON 14R. FABRICATED DOUBLER AND FILLER. INSTALLED REPAIR PARTS. (M)
Part: CLIP — CORRODED (FUSELAGE)
FTW - FOUND AFT PIT CABIN FLOOR STATION 1271-1309 PLUS X17, STRAP AT BOTTOM OF FLOORBEAMS CORRODED. STRAP CLIP FOUND TO BE CORRODED OUT OF LIMITS. REMOVED CLIP. FABRICATED NEW CLIP. INSTALLED CLIP. (M)
Part: DOOR — DELAMINATED (RT MLG)
FTW - FOUND RIGHT MLG FLYWING DOOR POP-UP/DELAMINATED. REMOVED DELAMINATED AREA ON RIGHT MLG FLY WING DOOR. FORMED FILLER AND DOUBLER. BONDED FILLER AND DOUBLER TO RIGHT MLG FLY WING DOOR. (M)
Part: INTERCOSTAL — CRACKED (FUSELAGE)
FTW - FOUND AFT PIT/CABIN FLOOR STATION 1287-1309 XO, UPPER FLANGE IN INTERCOSTAL IS CRACKED AT FASTENER HOLES. FABRICATED, LOCATED AND DRILLED INTERCOSTAL. INSTALLED INTERCOSTAL. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
FTW - AFT PIT/CABIN FLOOR, STATION 1155-1174 PLUS X45 LEFT INBOARD SEAT TRACK AND SPLICE ARE CORRODED. REMOVED SEAT TRACK STATION 1079-1155 AND SPLICE AT STATION 1155. FABRICATED REPAIR SEAT TRACK SPLICE. INSTALLED REPAIR SEAT TRACK AT STATION 1079-1155. (M)
Part: FORMER — CORRODED (RT WING)
FTW - FOUND RIGHT WING CORRODED AT NOSE CAP SECTION ATTACH, FORMERS VORTILON. FORMED FORMER. DRILLED AND LOCATED. INSTALLED ATTACHED FORMED ANGLE. (M)
Part: FLAP — CRACKED (RT WING)
FTW - FOUND RIGHT WING OUTBOARD FLAP T/E CRACKED/DAMAGED, THREE EACH. REPAIRED RIGHT WING OUTBOARD FLAP TRAILING EDGE. (M)
Part: RIB — CORRODED (RT WING)
FTW - FOUND RIGHT LOWER CENTER WING CORRODED AT RIB NR 8, FROM MLG DOOR JAMB. REMOVED CORROSION. RIB SPLICE FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF THE RIB SPLICE. FABRICATED NEW SECTION OF RIB SPLICE AND REPAIR. INSTALLED RIB SPLICE AND DOUBLER, STRAP. (M)
Part: BRACKET — CRACKED (RT WING)
FTW - FOUND RIGHT WING, UPPER DOG LEG, BRACKET ATTACH TO BODY CRACKED. REMOVED DAMAGED BRACKET RIGHT WING UPPER SURFACE. FABRICATED NEW BRACKET. INSTALLED NEW BRACKET. (M)
Part: RIB — CRACKED (RT WING)
FTW - FOUND RIGHT LOWER CENTER WING CRACKED AT THE NR 1 RIB, FROM DOOR JAMB. REMOVED NR 1 RIB CRACKED. FORMED INNER DOUBLER. LOCATED AND DRILLED. INSTALLED REPAIR PARTS. INSTALLED NR 1 RIB RIGHT LOWER CENTER WING. (M)
Part: SPAR — CRACKED (SPOILER)
FTW - FOUND LEFT OUTBOARD FLIGHT SPOILER, OUTBOARD FORWARD CORNER IS BOWED, DELAMINATED AND WORKING RIVETS, AN AREA 4 INCH SPAN BY 1.50 INCH CHORD. REMOVED PAINT ON OUTBOARD CORNER AND FOUND CRACK IN SPAR. STOP DRILLED CRACK IN SPAR. INSTALLED DOUBLERS TO DAMAGED AREA. CUT OUT PIECE OF CORE TO FIT CORNER AT LEFT INBOARD LOWER CORNER. FABRICATED FILLER AND DOUBLER TO FIT UNDER INBOARD CORNER. PERFORMED HOT BOND REPAIR WITH CORE, FILLER, AND DOUBLER. (M)
Part: SKIN — DELAMINATED (SPOILER)
FTW - FOUND LEFT MIDDLE FLIGHT SPOILER, UPPERSIDE HAS AN AREA OF DELAMINATION 3 INCH SPAN BY 9 INCH CHORD, CENTER AREA OF SPOILER. DUE TO EXTENSIVE DAMAGE OF UPPER SKIN AND CORE, BONDED NEW CORE AND UPPER SKIN FULL SPAN OF PART. (M)
Part: SYNCRONIZER — FAILED (NR 1 ENGINE)
FTW - NR 1 ENGINE AT LOW LIMIT WOULD COMPLETELY UNSPOOL. PERFORMED TEST OF ENGINE SYNCHRONIZER SYSTEM. SYSTEM FAILED TEST, NO SYNCHRONIZATION OF ENGINE. PERFORMED ADJUSTMENT SYNCHRONIZER ENGINE ACTUATOR. SERVICED FUEL CONTROL UNIT ACCELERATION CHAMBER WITH SILICON. DRAINED FUEL CONTROL MOISTURE TRAP. OPS CHECK FAILED STEP 9. REMOVED ENGINE SYNCHRONIZER ACTUATOR. INSTALLED SERVICEABLE ENGINE SYNCHRONIZER. (M)
Part: THRESHOLD — CORRODED (FUSELAGE)
FTW - FOUND MID CARGO DOOR CUT OUT AT BASE OF THRESHOLD HAS CORROSION. JAMB BEAM MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED DOOR JAMB BEAM. DRILLED UP AND LOCATED NEW DOOR JAMB BEAM. INSTALLED DOOR JAMB BEAM. (M)
Part: PITOT TUBE — LEAKING (PITOT/STATIC SYS)
FTW - AUTO-PILOT IN IAS WOULD HUNT FOR THE AIRSPEED. LEAK CHECK ON CAPTAINS AND COPILOTS PITOT TUBE, BOTH PITOT TUBES FAILED LEAK CHECK. CAPTAINS AND FIRST OFFICERS LEAK CHECKS OF PITOT SYSTEMS ACCOMPLISHED. (M)
Part: THRESHOLD — CORRODED (FUSELAGE)
FTW - FOUND AFT CARGO AT THRESHOLD CUT OUT THERES CORROSION. REMOVED CORROSION ON THE BEAM, OUT OF LIMITS. REMOVED BEAM FROM STA Y-1117, Y-1250, -X=16 INCHES. AFTER FURTHER EVALUATION, FOUND AFT LOWER SEAL DEPRESSOR OUT OF LIMITS. FABRICATED DRILLED AND LOCATED NEW SEAL DEPRESSOR. INSTALLED SEAL DEPRESSOR. (M)
2001
Part: SWITCH — FAULTY (COCKPIT)
FLT 503 - MCO - AFTER GEAR RETRACTION 3 RED LIGHTS (GEAR), AS PER QRH EXTEND GEAR/RETRACT 3-RED LIGHTS REMAIN GEAR APPEARS TO BE UP FLEW REMAINDER OF FLT 7 MACH/300 KNOTS. FOUND LANDING GEAR CONTROL LEVER SWITCH TO BE AT FAULT. REMOVED AND REPLACED SAME PER MM CH 32-60-01. OPS CHECK GOOD. (M)
Part: FLAP — CRACKED (LT WING)
ACY - LEFT TRAILING EDGE FLAP HAS CRACK AT APPROX STATION XW154. REPAIRED FLAP TRAILING EDGE FLAP IAW SRM 57-03 AS REQUIRED. (M)
Part: DOUBLER — CRACKED (T/E FLAP)
ACY - FOUND SCAB PATCH ON SECONDARY FLAP CRACKED, LEFT WING. REPAIRED LEFT WING SECONDARY FLAP IAW SRM 57-50-09 AND CH 57-0105 SRM. (M)
Part: WEB — CRACKED (NR 2 COWL)
FOUND NR 1 ENGINE COWLING WEB CRACKED AT 3 O'CLOCK POSITION. REPAIRED DAMAGED WEB IAW DC9/MD80 SRM 54-01. (M)
Part: PROXIMITY SENSOR — OUT OF ADJ (LT MLG DOOR)
EWR - FLT 1456 - GEAR DOOR LIGHTS STAYS ON. AFTER GEAR RAISED LIGHT GOES OUT, WHEN HYD SWITCHED TO LOW LIGHT ON, STAYED ON AND FLICKERING IN FLIGHT. READJUSTED LEFT MLG DOOR PROX SENSOR IAW MM 32-60-05. OPS CHECK GEAR WARNING SYSTEM SEVERAL TIMES. OPS NORMAL. (M)
Part: TARGET — OUT OF ADJ (LANDING GEAR)
FLT 460 - EWR - GEAR DOOR OPEN LIGHT CAME ON IN FLIGHT, WENT OUT WITH HYD IN HIGH. ADJUSTED PROX SENSORS TARGET IAW MM 32-60-05, GEAR WARNING SYSTEM OPS CHECK GOOD. (M)
Part: TARGET — CONTAMINATED (LANDING GEAR)
FLT 460 - EWR - GEAR DOOR OPEN LIGHT ON IN FLIGHT, WENT OUT WITH HYD IN HIGH POSITION. NO OTHER UNSAFE CONDITIONS PRESENT IN GEAR HANDLE. CLEANED GEAR DOOR SWITCH FOUND GREASE ON TARGET, ACCOMPLISHED PROXIMITY TEST OF GEAR DOOR WIRING, NO DEFECTS NOTED. OPS CHECK OF GEAR WARNING SYSTEM OK IAW MM 32-60-05. (M)
Part: WARNING SYSTEM — MALFUNCTIONED (CARGO BAY)
DTW - FLT 632 - CARGO SMOKE DETECTOR LIGHT CAME ON IN FLIGHT. AFT CARGO LOOP B DETECTOR LIGHT ALSO CAME ON. NO HORN, NO MASTER CAUTION, NO MASTER WARNING LIGHTS WENT OUT AFTER 2-3 MINUTES. PERFORMED CARGO SMOKE DETECTION SYSTEM CHECK, OPS CHECK GOOD IAW BARFIELD MM 26-16-00. NO FAULT FOUND. (M)
Part: WIRE — EXPOSED (CABIN)
FLT 506 - DTW - AT ROW 9 EMERGENCY FLOOR TRACK LIGHTS HAS EXPOSED WIRES FAA WRITE-UP. RE-INSTALLED FLOOR TRACK LIGHTS IAW MM 33-50-00. OPS CHECK GOOD. (M)
Part: INDICATOR — FAILED (COCKPIT)
DTW - FLT 629 - AFTER PUSHBACK, ALL FUEL QUANTITY VARIED BY SEVERAL THOUSAND LBS, WENT BLANK, FLASHED ETC. REPLACED FUEL QUANTITY INDICATOR. OPS CHECK NORMAL IAW MD-80 MM 28-40-00. (M)
Part: LANYARD — DETACHED (SLIDE)
TPA - SLIDE PACK RELEASE LANYARD NOT ATTACHED. RE-ATTACHED RELEASE LANYARD THROUGH GIRT BAR MM 25-62-00. (M)
Part: SLIDE — LOOSE (PAX DOOR)
ORD - FLT 781 - SLIDE PACK DOOR IS LOOSE. RE-INSTALLED SLIDE PACK ON L1 DOOR IAW MM 25-02-00. OPS CHECK OK. (M)
Part: ENGINE — FAILED (RT ENGINE)
PBI - FLT 509 - RIGHT ENGINE FAILED. THE RIGHT OIL STRAINER CLOGGING LIGHT CAME ON. ALL INDICATIONS WERE NORMAL. REF MM 71-00, TASK-CARD NR 0191, INSTALLED SERVICEABLE ENGINE. (M)
2000
Part: WIRE — EXPOSED (CABIN)
DTW - FLOOR TRACK LIGHTING EXPOSED BETWEEN AFT LAVS. INSTALLED MISSING 2 INCH PIECE OF FLOOR TRACK LIGHTING COVER IAW MD 80 MM 33-50-00; OPS CHECK NORMAL. (X)
Part: COVER — MISSING (CABIN)
FLL - FLT 447 - ON RED AISLE PATH LIGHT MISSING FROM EXIT ROW. INSTALLED RED LIGHT COVER FOR EMERGENCY EXIT LIGHTING. (M)
Part: COVER — LOOSE (CABIN)
MBL - FLT 403 - EMERGENCY FLOOR PATH LIGHTING COVER CAME LOOSE AT ROW 22. SECURED EMERGENCY FLOOR PATH LIGHTING COVER AT ROW 22 IAW MM 33-50-0. (M)
Part: LIGHT — INOPERATIVE (CABIN)
CABIN MID SECTION (B573) EMERGENCY LIGHTS INOPERATIVE. REPLACED B-573 EMERGENCY LIGHT PACK IAW MD 80MM 33-53-00. OPS CHECK NORMAL. (M)
Part: WIRE — BROKEN (ROW 17 - 21)
MLB - EMERGENCY FLOOR LIGHTS INOPERATIVE ROWS 17-21. REPLACED MISSING LENS AND BULB, REPAIRED BROKEN WIRES. OPS CHECK GOOD IAW MM 33-53-00. (M)
Part: LIGHT — INOPERATIVE (ROWS 17 - 21)
MLB - EMERGENCY FLOOR LIGHTS INOPERATIVE ROWS 17, 18, 19, 20, 21. REPLACED MISSING LENS AND BULB. REPAIRED BROKEN WIRES. OPS CHECKS GOOD. (M)
Part: LIGHT — LOOSE (ROW 21)
MLB - 403 - AISLE PATH LIGHT COVER (EMERGENCY EXIT ROW 21) POPPED OUT. SECURED AISLE PATH COVER (EMERGENCY) EXIT ROW 21. (M)
Part: LIGHT — LOOSE (CABIN)
EWR - FLT 447 - EMERGENCY FLOOR LIGHT LOOSE NEAR FORWARD OVERWING EXIT. SECURED LIGHT LENS, OPS CHECKS GOOD. (M)
Part: LENS — BROKEN (ROW 23)
PBI - FLT 951 - EMERGENCY STRIP LIGHT BROKEN AT ROW 23. REPLACED BROKEN LENS AND RELAMPED EMERGENCY STRIP LIGHT ROW 23. OPS CHECKED GOOD. (M)
Part: LENS — LOOSE (CABIN)
RED EMERGENCY PATH LENS COVER MISSING. FOUND AND REINSTALLED RED LENS FROM EMERGENCY PATH LIGHT. OPS CHECKS GOOD. (M)
Part: COVER — LOOSE (ROWS 27)
MLB - FLT 403 - EMERGENCY EXIT LIGHTING COVER CAME LOOSE FROM ROW 27. INSTALLED COVER OK IAW MM 33-50-0. (M)
Part: WIRE — EXPOSED (ROW 30)
DTW - EMERGENCY FLOOR LIGHTING WIRES VISIBLE AT ROW 30. (FAA). SECURED EMERGENCY FLOOR LIGHTING WIRES IAW MD 80 MM 33-50-00 FOUND SECTION (1 INCH) REMOVED, RE-INSTALLED. OPS CHECK NORMAL. (X)
1999
Part: LENS — MISSING (CABIN)
DTW - FLT 372 - M 460 - OVERWING EXIT FLOOR TRACK LIGHT LENS MISSING (FAA). M 461 - MISING LIFE VEST PLACARDS IN FRONT OF SEATS 1D, E, F. (FAA). M 460 - REPLACED MISSING FLOOR TRACK LIGHT LENS. IAW MD-80 MM CHAP 33-53-01. M 461 - REPLACED MISSING LIFE VEST PLACARDS IN FRONT SEATS 1, D, E, F. IAW MD-80 MM CHAP 11-41-00. (X)
Part: DUCT — LOOSE (LT PACK)
PBI - FLT 350 - P556 - JUST PRIOR TO STARTING TO DESCEND OUT OF FL 350, CABIN ALTITUDE STARTED CLIMBING. COULD NOT CONTROL PRESSURIZATION. STARTED RAPID DESCENT, MASKS DEPLOYED AT 14,000 FEET CABIN ALTITUDE. P 557 - LT A/C VALVE INOPERABLE IN AUTO AND MANUAL. REF ITEM P557 - SECURED DUCT LT PACK. NO OTHER DEFECTS NOTED. REF MM 21-00-00-501 CABIN PRESSURIZATION CHECKED GOOD. P557 - FOUND DUCT BLOWN OFF LT PACK WATER SEPARATE SECURED DUCT. LEAK CHECK DUCT. OPS CHECKED LT PACK REF MM 21-20-00 A501. (X)
Part: UNKNOWN — SMOKE (RT MLG)
ON LANDING IN MCO, TOWER AND OTHER AIRCRAFT REPORTED SMOKE COMING FROM RIGHT MAIN TIRE AREA. TRANSFERRED TO DMI NR 310 PER MEL 32-10 CAT C PLACARD INSTALLED, DISPATCH NOTIFIED. (M)