N141AE

Part: SHAFT SEAL — FAILED (NR 2 ENGINE)

DURING CLIMB ABOVE 700 MSL NR 2 OIL PRESSURE LIGHT CAME ON. PRESSURE SHOWED FLUCTUATIONS BETWEEN 30-60 PSI. LARGE FLUCTUATIONS EXECUTED PRECAUTIONARY SHUTDOWN AND RETURN TO MCO. LANDING UNEVENTFUL. INFLIGHT EMERGENCY DECLARED. REPLACED PROP SHAFT SEAL. (M)

Part: O-RING — DAMAGED (NR 2 ENGINE S/G)

MIA - FLT 5277 - DURING FLIGHT, THE NR 2 ENGINE WAS SHUTDOWN DUE TO LOW OIL PRESSURE AND BOTH OIL LIGHTS FLASHING. MAINTENANCE INSPECTED ENGINE AND FOUND THE STARTER GENERATOR DRIVE SHAFT O-RING WAS DAMAGED. MAINTENANCE REPLACED THE O-RING ON STARTER GENERATOR SHAFT. OPS AND LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERIVCE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - FLT 5211 - FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING LIGHT AT 7B DOES NOT WORK. REMOVED AND REPLACED LIGHT STRIP IAW AMM. OPS CHECK GOOD. (M)

Part: CONNECTOR — DAMAGED (RT MLG)

MIA - FLT 5237 - RIGHT MLG CYCLING IN FLIGHT. MAINTENANCE DUPLICATED PROBLEM WITH AIRCRAFT ON JACKS. FOUND GROUND AT 5000VN CONNECTOR DAMAGED. REPLACED THE CONNECTOR IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WARNING LIGHT — ILLUMINATED (MLG)

TPA - FLT 5239 - DURING CRUISE FLIGHT, THE RIGHT MAIN LANDING GEAR UNLOCK LIGHT CAME ON INTERMITTENTLY WITH ASSOCIATED VIBRATIONS AT AIRSPEEDS OF 170 KNOTS AND ABOVE. (M)

Part: UPLOCK — INOPERATIVE (RT MLG)

MIA - FLT 5253 - AFTER TAKEOFF FROM MIA, THE NOSE GEAR UNLOCK LIGHT ILLUMINATED AND THE GEAR STARTED TO MAKE A CLUNKING NOISE AS IT TRIED TO RETRACT REPEATEDLY. THE HYDRAULIC SYSTEM ALSO SHOWED A FLUCTUATION. THE AIRCRAFT WAS RETURNED SAFELY TO MIA WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG UPLOCK BOX IAW ATR MM. OPERATIONAL AND LEAK CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WASHER — BROKEN (LDG DOOR)

JAX - FLT 5254 - AFTER TAKEOFF, CREW REPORTED THE RIGHT MAIN GEAR STARTED TO CYCLE BETWEEN 160 AND 170 KNOTS. GEAR WAS NORMAL BELOW 160 KNOTS. LANDING GEAR WAS PUT ON MEL AT THIS TIME. FOUND LANDING GEAR DOOR ATTACHMENT LINK ROD LOCKING WASHER BROKEN. REMOVED AND REPLACED SAME. OPS CHECK GOOD. (M)

Part: SELECTOR VALVE — INOPERATIVE (HYDRAULIC BAY)

MIA - FLT 5305 - AFTER TAKEOFF, GEAR INTRANSIT LIGHT WOULD NOT GO OUT. FOLLOWED AOM PROCEDURES RETURNED LANDING WITH NORMAL GEAR DOWN INDICATIONS. S/D MAINTENANCE REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW ATR MM. OPS AND LEAK CHECK WAS SATISFACTORY. AIRCRAFT PASSED FUNCTIONAL CHECK FLIGHT AND WAS RETURNED TO SERVCE. (M)

Part: CONNECTOR — INOPERATIVE (MLG)

ORD - FLT 4219 - WHEN CREW SELECTED GAER UP IDLE GATE FAILED TO RETRACT TO FLIGHT POSITION. GEAR RETRACTION TOOK APROXIMATELY ONE MINUTE, THEN RETRACTED ITSELF AND GEAR RETRACTED NORMAL. MAINTENANCE REMOVED AND REPLACED RELAY 41GB AND CANNON PLUG 5001VC. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: RELAY — FAILED (MLG)

ORD - FLT 4219 - AFTER TAKEOFF, WHEN GEAR SELECTED UP. IDLE GATE CYCLED IN AND OUT AND COULD NOT BE PUSHED IN MANUALLY AS PER CHECKLIST. WHEN GEAR SELECTED DOWN FOR LANDING. IDLE GATE OPERATION WAS NORMAL. MAINTENANCE REPLACED RELAYS 22GB AND 58GB IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: UNKNOWN — ODOR (COCKPIT) · airframe 23,124 hrs · 29,098 cycles

ORD - FLT 4218 - ON APPROACH, STRONG TOXIC RUBBERY FUME IN COCKPIT AND ALSO REPORTED BY FLIGHT ATTENDANT. FOUND RESIDUAL ODOR OF DINITROL AV30. RAN ENGINES AND CLEANED EXCESS FLUID. OPS CHECK GOOD. NO FUMES NOTED. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 38 AND 40 CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-00-00. (M)

Part: INTERCOSTAL — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT INTERCOSTAL BETWEEN FRAMES 36 AND 38 CORRODED BEYOND LIMITS. REMOVED AND REPLACED INTERCOSTAL IAW 51-25-02. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 38 AND 40 CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-00-00. REF SIMA2851. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURNG CPCP-2 INSPECTION, FOUND RIGHT FLIGHT ATTENDANT SEAT TRACK CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW EO E9-5300-013. (M)

Part: DRAIN LINE — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND SERVICE DOOR SILL PLATE DRAIN TRACK CORRODED BEYOND LIMITS. REMOVED AND REPLACED DRAIN TRACK IAW SRM 51-25-02. (M)

Part: WIRE — BROKEN (CABIN)

MIA - FLT 5358 - EXTERIOR EMERGENCY LIGHT IN PASSENGER DOOR IS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES 106 AND 116 AT CANNON PLUG 253VC. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — FAILED (CABIN)

MIA - FLT 5208 - WITH BATTERY SWITCH OFF FLOOR EMERGENCY LIGHTS AT 1, 2, 3, 4 AND 8 FROM THE FRONT DO NOT WORK, WITH BATTERY SWITCH OFF EXIT SIGNS OVER FWD EMERGENCY EXITS (BOTH SIGNS) DO NOT WORK. REPLACED BATTERY PACK AT 3WLA IAW JIC 33-51-21 RAI 10010-004. OPERATIONAL TEST OF EMERGENCY LIGHTS GOOD IAW JIC 33-50-0001710000004. REPLACED BATTERY PACK AT 3WLA IAW JIC 33-51-21 RAI 10010-004 OPERATIONAL TEST OF EMERGENCY LIGHTS GOOD IAW JIC 33-50-00-017 100000004. (M)

Part: RECEPTACLE — FAILED (CABIN)

MIA - FLT 5208 - EMERGENCY FLOOR PROXIMITY LIGHT AT ROW 7 IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT LAMP HOLDER AT SEAT 7A IAW AWM 33-51-05 PAGE 1, OPS CHECK GOOD. (M)

Part: WARNING SYSTEM — ACTIVATED (NR 1 ENGINE)

TPA - FLT 5390 - LEFT ENGINE OIL PRESSURE FLUCTUATION WITH INTERMITTENT WARNING ON CREW ALERTING PANEL AND NR 1 ENGINE WARNING LIGHT. (M)

Part: FAN — FAILED (COCKPIT)

SRQ - FLT 5357 - DURING CRUISE FLIGHT, THE NR 1 RECIRCULATION FAN CIRCUIT BREAKER TRIPPED AND THE CREW NOTICED AN ELECTRICAL ODOR IN THE COCKPIT. THE ODOR DISSIPATED AFTER A FEW SECONDS AND THE CIRCUIT BREAKER WAS LEFT EXTENDED. REMOVED AND REPLACED RECIRC FAN IAW AMM. OPS CEHCK GOOD. (M)

Part: LAMP — INOPERATIVE (CABIN) · airframe 22,544 hrs · 28,416 cycles

MIA - FLT 5284 - ONE EMERGENCY EXIT LIGHT ON FLOOR TRACK LIGHTING OUT. REMOVED AND REPLACED LAMP. OPS CHECKED GOOD. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

SAW - DURNG PS-2 INSPECTION, FOUND THE AFT EMERGENCY LIGHTS WOULD NOT EXTINGUISH. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION 18WL IAW JIC 335000-OPT-10000. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CARGO COMPT)

SAW - DURING CPCP1 INSPECTION, FOUND THE AFT CARGO RIGHT OUTBOARD SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW EO-E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — CORRODED (FRAME 26-28)

SAW - DURING CPCP1 INSPECTION, FOUND THE SPECIAL STRINGERS 21L AND 21R BETWEEN FRAMES 26 AND 28 CORRODED. REPAIRED BOTH STRINGERS IAW SRM SPECIAL STRINGER REPAIR SECTION 53-00-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DRAIN TRACK — CORRODED (CARGO DOORWAY)

SAW - DURING CPCP-1 INSPECTION, FOUND THE FORWARD CARGO DOOR SILL DRAIN TRACK, SUPPORT PLATE AND WEB BETWEEN FRAMES 13 AND 18 CORRODED. REMOVED AND REPLACED ALL THREE PARTS IAW SRM 53-37-80. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SUPPORT — CORRODED (CARGO DOORWAY)

SAW - DURING CPCP-1 INSPECTION, FOUND THE FORWARD CARGO DOOR SILL DRAIN TRACK, SUPPORT PLATE AND WEB BETWEEN FRAMES 13 AND 18 CORRODED. REMOVED AND REPLACED ALL THREE PARTS IAW SRM 53-37-80. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ANGLE — CORRODED (FRAME 43-44)

DURING CPCP-1 INSPECTION, FOUND THE LEFT FLOOR SUPPORT ANGLE BETWEEN FRAMES 43 AND 44 CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WEB — CORRODED (CARGO DOORWAY)

SAW - DURING CPCP-1 INSPECTION, FOUND THE FORWARD CARGO DOOR SILL DRAIN TRACK, SUPPORT PLATE AND WEB BETWEEN FRAMES 13 AND 18 CORRODED. REMOVED AND REPLACED ALL THREE PARTS IAW SRM 53-37-80. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ANGLE — CORRODED (FRAME 12)

SAW - DURING CPCP1 INSPECTION, FOUND THE CREASE BEAM RIGHT ANGLE AT FRAME 12 WAS CORRODED. REMOVED AND REPLACED THE ANGLE IAW RM 51-25-04. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE LEFT F/A SEAT TRACK CORRODED AT FRAME 39. INSTALLED NEW LEFT SEAT TRACK PER SRM 51-25-04. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278.

Part: DOOR — CORRODED (FUSELAGE)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND LIGHT CORROSION ON FUSELAGE FLANGES AROUND AFT AVIONICS DOOR (FORWARD). INSTALLED DOUBLER ON FORWARD FLANGE OF AVIONICS DOOR IAW AIRAMS/T/ATR/32986/98, FAX COVER SHEET 141/98/002 AND ATR SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278. 2075T6 - .063 INCH.

Part: FLOORBEAM — CORRODED (CABIN)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND CORROSION ON FLOORBEAM 39. INSTALLED FLOORBEAM IAW ATR SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS/TAC: 23,278.

Part: FRAME — CORRODED (CABIN)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND FRAME 36 CORRODED AT FLOOR LEVEL RIGHT SIDE. REPAIRED FRAME 36 IAW ATR 42 SRM 53-61-40, FIGURE 407. CAUSE OF DAMAGE: ENVIRONMENTAL, LAVATORY/GALLEY SPILL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278.

Part: CLIP — CORRODED (TAIL FUSELAGE)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND 7 NUT PLATES CORRODED AND UNDERNEATH THEM, ALSO TEARSTRAP CLIPS. TREATED PER 51-21-31. REMOVED AND INSTALLED NUT PLATES PER SRM 51-25-00, AND INSTALLED 1 EACH NEW CLIPS TAIL CONE ATTACH POINTS (BOTTOM) PER SRM 51-25-01. CAUSE OF DAMAGE: LAVATORY/GALLEY SPILLS. AIRCRAFT TT: 18,688.4 HOURS/TAC: 23,278.

Part: FLOORBEAM — CORRODED (CABIN)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND CORROSION ON FLOORBEAM 38. INSTALLED FLOORBEAM PER SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278.

Part: FLOORBEAM — CORRODED (CABIN)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND NUT PLATE HOLES CORRODED ON FLOORBEAM 36. INSTALLED REPLACEMENT FLOORBEAM 36 IAW ATR 42 SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278.

Part: DOOR — CORRODED (FUSELAGE)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND LIGHT CORROSION ON AFT AVIONICS DOOR FLANGES (FWD AND AFT). REMOVED AND REPLACED WITH NEW DOOR IAW ATR 42 SRM 20-21-00. CAUSE OF DAMAGE: ENVIRONMENTAL, LAVATORY, GALLEY SPILL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278.

Part: FLOORBEAM — CORRODED (CABIN)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE LEFT SIDE STR 21 BETWEEN FRAMES 44 AND 45 CORRODED. REMOVED AND REPLACED STR 21 LT IAW ATR SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS/TAC: 23,278. (X)

Part: SEAT TRACK — CORRODED (CABIN)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE RIGHT AFT INBOARD SEAT TRACK CORRODED FORWARD OF FRAME 35. COMPLETE REPLACMENT OF RT AFT INBOARD SEAT TRACK BY COUNTERSINK HOLES, INSTALLED HILOCKS, AND RIVETS ON AFT SUPPORT BRACKETS IAW ATR 42 SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL, LAVATORY, GALLEY SPILL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278.

Part: SEAT TRACK — CORRODED (CABIN)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE LAVATORY WALL SEAT TRACK BETWEEN FRAMES 39 AND 41 CLIP NUT HOLE CORRODED AFT AREA. INSTALLED SERVICEABLE SEAT TRACK BETWEEN FRAMES 39 AND 41 LAVATORY WALL IAW ATR 42 SRM 51-25-04. CAUSE OF DAMAGE: ENVIRONMENTAL, LAVATORY/GALLEY SPILL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278.

Part: SEAT TRACK — CORRODED (CABIN)

DURING A CPCP 4 INSPECTION, PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND FORWARD LEFT INBOARD SEAT TRACK FLOORBOARD CLIP HOLES CORRODED BETWEEN FRAMES 13 AND 16. INSTALLED SEAT TRACK PER SRM 51-21-04. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278.

Part: ZEE MEMBER — CORRODED (FUSELAGE)

DURING CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE Z-MEMBER CORRODED IN THE RIGHT AFT BAGGAGE COMPARTMENT AT FLOORBOARD AREA. INSTALLED RIGHT Z-MEMBER IAW ATR SRM 51-25-03. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS/TAC: 23,278. (X)

Part: SEAT TRACK — CORRODED (CABIN)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE RT AFT OUTBOARD SEAT TRACK CORRODED FORWARD FRAME 35. REMOVED AND INSTALLED AFT OUTBOARD SEAT TRACK WITH NEW IAW ATR SRM 53-63-00. CAUSE OF DAMAGE: ENVIRONMENTAL, LAVATORY/GALLEY SPILLS. AIRCRAFT TT: 18,688.4/TAC: 23,278.

Part: FLOORBEAM — CORRODED (CABIN)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE RT SIDE STR 21 BETWEEN FRAMES 44 AND 45 CORRODED. REMOVED AND REPLACED STR 21 RT IAW ATR SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS/TAC: 23,278. (X)

Part: SEAT TRACK — CORRODED (CABIN)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE RIGHT F/A SEAT TRACK CORRODED AT FRAME 39. INSTALLED NEW SEAT TRACK IAW ATR SRM 51-25-04. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS/ TAC: 23,278.

Part: DOOR — CORRODED (FUSELAGE)

DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND LIGHT CORROSION ON FUSELAGE FLANGES AROUND AFT AVIONICS DOOR (AFT). INSTALLED DOUBLER ON AFT FLANGE OF AVIONICS DOOR IAW AIRAMS/T/ATR/32986/98, FAX COVER SHEET 141/98/002 AND ATR SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278. 2075T6 - .063 INCH.