N425MJ
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.
78 reports on file, 1995-09-30 – 2012-10-26.
Part: TORQUE SENSOR — INOPERATIVE (LT ENGINE) · airframe 31,377 hrs · 34,977 cycles
CREW REPORTED THAT ON THE TAKEOFF ROLL, THE ANALOG PORTION OF NR 1 TORQUE GAUGE WENT TO ZERO. DIGITAL PORTION NORMAL. ACFT REMOVED FROM SERVICE. R & R LT ENGINE TORQUE SENSOR IAW 72-01-60 AND LT ENGINE AFU IAW 72-01-10. PERFORMED OPS CHECK IAW EX-055007-CS-20000-001 AND 61-21-66 AND 61-00-00. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.
Part: ENGINE — OVERTORQUED (NR 1) · airframe 31,381 hrs · 34,979 cycles
THE CREW REPORTED THE NR 1 ENGINE FAILED IMMEDIATELY AFTER TAKEOFF. CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. ACFT REMOVED FROM SERVICE. PERFORMED ENGINE NR 1 GROUND OPS CHECK IAW W/C EX-055007-CS-20000-001 NO DEFECTS NOTED. DETERMINED THE ENGINE HAD AN OVER TORQUE ISSUE. FUNCTIONAL CHECK FLIGHT WAS FOUND TO BE SATISFACTORY. ACFT RETURNED TO SERVICE.
Part: UNKNOWN — UNKNOWN (NR 1 ENGINE) · airframe 31,377 hrs · 34,977 cycles
CREW REPORTED THAT AT 17,000 FT IN CRUISE, ACFT WENT INTO A PARTIAL NR 1 ENGINE FAILURE. ACFT YAWED LEFT, RECEIVED AN ELEC ON CAP, TORQUE AND NP WENT BELOW 40 PERCENT. AFTER 30-20 SECS OR 50 FULL POWER CAME BACK ONLINE BY ITSELF. LANDED WITHOUT INCIDENT. ERASED NR 1 ENGINE EEC MEMORY IAW JIC 73-23-00 PRO 10010, PERFORMED ENGINE 1 RUN CHECK AND COULD NOT DUPLICATE WRITE UP. ENGINE RUNNING GOOD, NO DEFECTS NOTED. THE ACFT WAS RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,200 hrs · 34,747 cycles
CREW REPORTED THE EMERGENCY FORWARD LIGHTS WILL STAY ON AFTER SWITCH SET TO ARM, BUT IF SWITCH IS RESET REAR LIGHTS WILL COME ON AND THE FORWARD LIGHTS WILL GO OUT. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED AND OPS TEST OF THE EMERGENCY LIGHTING SYS IAW JOB CARD EX 335000-OPT 10000-001. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 31,200 hrs · 34,747 cycles
FLIGHT 4772, THE CREW REPORTED THE CAPTAINâS FLASHLIGHT IS IN NEEDBATTERIES. THE ACFT WAS REMOVED FROM SERVICE. REPLACED BATTERIES ON CAPTAINâS FLASHLIGHT. OPS CHECKED GOOD IAW AMM 25-60-00. THE ACFT WAS RETURNED TO SERVICE.
Part: UNKNOWN — SMOKE (CABIN) · airframe 31,142 hrs · 34,685 cycles
THE CREW REPORTED THAT DURING THE VISUAL APPROACH, THE COCKPIT STARTED GETTING HOT. THE CREW PLACED THE PACKS ON MANUAL AND THE PROBLEM DID NOT CORRECTED ITSELF. ON FINAL APPROACH THE CREW SMELLED A FAINT ELECTRICAL BURN SMELL. THE CREW DECLARED AN EMERGENCY. TAXING TO THE RAMP THE F/A CALLED AND DECLARED SMOKE ODOR AND THE CABIN GETTING HOT. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED DETAILED VISUAL INSP ON CABIN AND FLIGHT COMPT ELECTRICAL SYS AND FOUND WORKING PROPERLY, PERFORMED OPS TEST OF TEMP CONTROL ON CABIN AND FLIGHT COMPT AND NO SMELL OR ABNORMAL SMOKE SMELL ON ACFT IAW JIC 21-61-00-OPT-10000. THE ACFT WAS RETURNED TO SERVICE.
Part: UNKNOWN — ODOR (CABIN) · airframe 31,127 hrs · 34,667 cycles
THE CREW REPORTED THAT DURING THE VISUAL APPROACH TO THE COCKPIT STARTED GETTING HOT. THE CREW PLACED THE PACKS ON MANUAL AND THE PROBLEM DID NOT CORRECTED ITSELF. ON FINAL APPROACH THEY DETECTED A FAINT ELECTRICAL BURN ODOR. TAXING TO THE RAMP THE F/A CALLED AND DECLARED ODOR OF SMOKE AND THE CABIN GETTING HOT. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED DETAILED VISUAL INSPECTION ON CABIN AND FLIGHT COMPARTMENT ELECTRICAL SYS AND FOUND WORKING PROPERLY, PERFORMED OPS TEST OF TEMP CONTROL ON CABIN AND FLIGHT COMPT AND NO ODOR OR ABNORMAL SMOKE ODOR ON ACFT IAW JIC 21-61-00-OPT-10000. THE ACFT WAS RETURNED TO SERVICE.
Part: STRUCTURE — CORRODED (LT WING) · airframe 31,097 hrs · 34,631 cycles
DURING MX INSPECTION, FOUND THE LT WING ELECTRIC FUEL PUMP SURROUNDING AREA CORRODED. ACFT REMOVED FROM SERVICE. REMOVED CORROSION IAW 51-21-42, BLEND OUT REF 51-21-58. PERFORMED EDDY CURRENT INSPECTION ON BLENDED AREA IAW NTM MANUAL 51-60-00, NO DEFECTS NOTED. PERFORMED ROTO TEST IN THE AFFECTED FASTENERS HOLES. APPLIED ALODINE 1200 TO THE AFFECTED AREA IAW EO E2-5700-491. ACFT RETURNED TO SERVICE.
Part: RIB — CORRODED (RT WING) · corrosion level 1 · airframe 31,097 hrs · 34,631 cycles
DURING MX INSPECTION, FOUND THE RT WING RIB 5, WITH TWO RIVETS WITH CORROSION. ONE NEAR WATER DRAIN VALVE AND THE OTHER NEAR L/E. ACFT REMOVED FROM SERVICE. REMOVED SURFACE CORROSION IAW SRM 51-21-42. ACFT RETURNED TO SERVICE.
Part: UNKNOWN — ODOR (CABIN) · airframe 30,902 hrs · 34,387 cycles
FLIGHT 4899, CREW REPORTED CABIN HAD A FOUL ODOR FROM ROWS 4 TO 13. AIRCRAFT REMOVED FROM SERVICE. CLEANED CABIN INTERIOR SEATS AND FLOOR ON RAMP AS PER JIC 12-21-12. AIRCRAFT RETURNED TO SERVICE.
Part: AUDIO CONTROL — MISINSTALLED · airframe 30,729 hrs · 34,161 cycles
ON FLIGHT 4873, THE CREW REPORTED THE EMERGENCY AUDIO CANCEL IS NOT BREAK WIRED. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED EMERGENCY AUDIO CANCEL BREAK WIRED IAW JIC 25-60-00. THE ACFT WAS RETURNED TO SERVICE.
Part: SKIN — CRACKED (LT WING LE) · airframe 30,602 hrs · 34,016 cycles
DURING MX INSPECTION, FOUND LT WING L/E HAS A CRACK ON THE LT SIDE OF ENGINE. (TOP). ACFT REMOVED FROM SERVICE. REPLACED LT WING L/E IAW JIC.57-40-00. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,501 hrs · 33,896 cycles
THE CREW REPORTED ONE EMERGENCY FLOOR PATH LIGHT INOPERATIVE ON ROW 8. THE ACFT WAS REMOVED FROM SERVICE. R & R FLOOR LIGHT ROW 8 AB IAW AMM JIC 33-50-00. THE OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 30,431 hrs · 33,827 cycles
AFTER NR 2 ENGINE START WITH EMERGENCY EXIT LIGHT SWITCH IN ARM, EMERGENCY LIGHTS IN CABIN ILLUMINATED. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT POWER SUPPLY 62WL AND EMERGENCY LIGHT BATTERY PACKS 62WL, 43WL, 73WL AND 61WL IAW JIC 33-51-21-RAI 10000 AND JIC 33-51-21-RAI-10010 AND FOUND SYS WORKING OK . ACFT RETURNED TO SERVICE.
Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 30,342 hrs · 33,728 cycles
CREW REPORTED THAT AFTER EVERY ENGINE START, THE EMERGENCY LIGHTS IN CABIN ILLUMINATE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT POWER SUPPLY BATTERY 62WL IAW JIC 33-51-21, RAI 10010. OPS TESTED SATISFACTORY. ACFT RETURNED TO SERVICE.
Part: LIGHT — LOOSE (CABIN) · airframe 30,285 hrs · 33,652 cycles
ON FLIGHT 4839, THE CREW REPORTED THE EMERGENCY LIGHT FROM AFT OF GALLEY CART WAS LOOSE. THE ACFT WAS REMOVED FROM SERVICE. REPOSITIONED EMERGENY LIGHT FROM OF GALLEY IAW 33 50 00. OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: LIGHT — LOOSE (CABIN) · airframe 30,268 hrs · 33,632 cycles
FLIGHT 4819, CREW REPORTED EMERGENCY LIGHT FRONT OF GALLEY ARE COMPLETLY LOOSE WITHOUT SCREW. ACFT REMOVED FROM SERVICE. SECURED EMERGENCY LIGHT IAW AMM 33-50-00. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
Part: LIGHT — UNSECURE (CABIN) · airframe 30,149 hrs · 33,483 cycles
FOUND FLOOR EMERGENCY LIGHT COMPLETELY LOOSE FROM ITS ASSEMBLY MOUNT. THE ACFT WAS REMOVED FROM SERVICE. REPOSITIONED FLOOR EMERGENCY LIGHT ON FRONT OF GALLEY CART IAW JIC 33-50-00. OPS CHECKS GOOD. THE ACFT RETURN TO SERVICE.
Earlier reports · 1995–2011 · 60 reports
2011
Part: UNKNOWN — SMOKE (CABIN) · airframe 29,699 hrs · 32,943 cycles
CABIN SMOKE REPORTED BY F/A, WHITE SMOKE VISIBLE IN CABIN. SMOKE SMELLED LIKE BURNING OIL. HAPPENED DURING APPROACH. PERFORMED VARIOUS ENGINE RUN UPS AND VERIFIED LT AND RT AIR PACKS AND LT & RT ENGS IAW JIC 72-00-00 AND 21-10-00. NO OIL ODOR OR SMOKE IN CABIN OR COCKPIT AT THIS TIME, JIC 21-22-0.
Part: FLASHLIGHT — UNKNOWN (COCKPIT) · airframe 29,680 hrs · 32,926 cycles
CAPTAIN`S SIDE FLASHLIGHT NEEDS TO BE REPLACED. CAPTAIN`S FLASHLIGHT INSTALLED IAW 25-60-00.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 29,665 hrs · 32,908 cycles
LAST 4 EMERGENCY EXIT FLOOR LIGHTING ILLUMINATED CONSTANTLY IN FLIGHT. PERFORMED SEVERAL OPS CHECKS OF EMERGENCY LIGHTING IAW EX-335000-OPT, CHECKED GOOD.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 29,665 hrs · 32,908 cycles
MAIN CABIN EMERGENCY STAIR LIGHT ILUMINATED CONSTANTLY IN FLIGHT. PERFORMED SEVERAL OPS CHECKS OF EMERGENCY LIGHTS IAW WC EX-335000-OPT-10000-001. OPS CHECKED GOOD.
Part: PIN — LOOSE (EMERGENCY LIGHTS) · airframe 29,466 hrs · 32,703 cycles
EMERGENCY LIGHTS AT ROWS 13, 15-17 PAX DOOR. SERVICE DOOR REMAIN ON ARM POSITION. FOUND PUSHED PIN ON PIN B EMERGENCY LIGHT POWER SUPPLY RESEATED PIN IAW SWITCH PANEL 20-10-00 EMERGENCY LIGHTS. OPS CHECKED OK IAW MM 33-50-00.
Part: SKIN — CORRODED (RT WING) · airframe 29,466 hrs
CORROSION ON RT WING LOWER SURFACE AFT OF ELECTRICAL FUEL PUMP AT RIB 4. COMPLIED WITH TDMI 5702E9, PERFORMED DVI OF RT WING FUEL PUMP HOLE, NO CORROSION FOUND AT THIS TIME. TDMI TO REMAIN OPEN FOR RECURRENT INSPECTIONS.
Part: SKIN — CORRODED (LT WING) · airframe 29,466 hrs
CORROSION AROUND WATER DRAIN ON LH WING LOWER SURFACE AT RIB 13. CLEANED LIGHT SURFACE CORROSION AROUND WATER DRAIN IAW SRM 51-21-42. NO MATERIAL LOSS NOTED. TREAT, PRIME AND TOP COAT AREA IAW SRM 51-21-17 & 51-21-27.
Part: UNKNOWN — UNKNOWN (CABIN) · airframe 29,368 hrs · 32,617 cycles
FAS REPORTED THAT MAIN CABIN GOT A LITTLE BIT FOGGY DURING THE APPROACH, (NO ODOR) IAW MM 72-00-00 C/W BOTH ENGINES RUN -UP AND FOUND CABIN AND COCKPIT NORMAL WITH NO FOG.
2010
Part: BATTERY PACK — INOPERATIVE (POWER SUPPLY) · airframe 27,903 hrs · 31,009 cycles
EMERGENCY LIGHTS ARE ON AT ALL TIMES IN FWD CABIN. R & R FWD EMERGENCY LIGHTS POWER SUPPLY 43WL AND POWER SUPPLY BATTERY PACK IAW JIC 33-51-21 10000 AND 33-51-21 10010. OPS TEST SATISFACTORY.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,454 hrs · 30,489 cycles
FWD EMERGENCY LIGHTS STAY ON THIS TIME. REPLACED EMERGENCY LIGHTS POWER SUPPLY FIN NR 43WL IAW JIC 33-51-21. PERFORMED OPS CHECK AND FOUND SYS WORKING PROPERLY.
Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 27,393 hrs · 30,415 cycles
THE EMERGENCY EXIT LIGHT ABOVE THE NR 1 AND NR 2 F/A AND BY THE COCKPIT JUMPSEAT IS ILLUMINATED AT ALL TIME WITH EMERGENCY EXIT LIGHT OFF. REPLACED 2 MINUTES LIGHT SWITCH 9LE. FOUND SYS WORKING OK.
Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 27,295 hrs · 30,311 cycles
EMERGENCY FLOOR LIGHT IN FRONT OF GALLEY CART ARE BROKEN OR LOOSE. R & R PLASTIC COVER OF EMERGENCY LIGHT ON GALLEY AREA IAW MM 33-51-21.
Part: VALVE — INOPERATIVE (TE FLAPS) · airframe 27,198 hrs · 30,213 cycles
DURING APPROACH AT EIS WHEN SELECT THE FLAPS TO 30 DEG. NEVER WENT DOWN, THE FLAPS WITH WENT AROUND, CAME BACK TO SJU AND THE FLAPS NEVER WENT DOWN TO FLAPS 15 OR 30 DEGREES, WITH MAKE A LANDING WITH FLAPS 0 DEG, FLAP 0 DEG LANDING PROCEDURES. R & R BOTH FLAP VALVE BLOCK FLOW RESTRICTORS IAW JIC 27-54-71, ALSO PERFORMED VISUAL INSP TO FLAP CONTROL SYS, FLAP ACTUATORS, HYD LINES CHECKED FOR RUBBING AND FOUND OK. PERFORMED OPS CHECK OF FLAP CONTROL SYS IAW JIC 27-51-00 AND FOUND WORKING PROPERLY AND LEAK CHECK GOOD.
Part: GOVERNOR — LEAKING (NR 1 ENGINE) · airframe 27,157 hrs · 30,166 cycles
DURING CRUISE NR 1 ENG OIL DEPLETING, HAD WARNINGS, SHUTDOWN ENGINE, DECLARED EMERGENCY AND DIVERTED. MX FOUND OVERSPEED GOVENOR LEAKING. R & R LT ENGINE OVER SPEED GOVERNOR IAW EX-612361-RAI-10000-014 AND RT ENG PROPELLER HP PUMP IAW EX-6112-63-RAI-10000-010 NO LEAKS FOUND AND OIL PRESSURE WORKING PROPERLY AT THIS MOMENT.
Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 27,151 hrs · 30,159 cycles
EMERGENCY LIGHT IN FRONT OF GALLEY HAVE A BROKEN COVER. R & R BOTH GALLEY EMERGENCY LIGHT STRIPS IAW JIC 33-50-00,OPT CHECK SATISFACTORY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,811 hrs · 29,808 cycles
A PLASTIC OR ELECTRICAL BURNING ODOR IS COMING FROM THE FWD PART OF THE PASSENGER CABIN. R & R FLOURESCENT TUBE AT 2CD IAW JIC 33-21-23 RAI 10000-018 END.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 26,664 hrs · 29,623 cycles
EMERGENCY EXIT LIGHT ON STAIRS 1S OUT. RELAMPED EMERGENCY LIGHT REF JIC 33-50-00.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 26,631 hrs · 29,580 cycles
EMERGENCY LIGHT OUT FROM SEAT 14AB TO THE EMERGENCY SIGNS IN THE BACK OF THE CABIN. R & R POWER SUPPLY AND BATTERY FOR EMERG LIGHT IAW 33-51-21 EX 33-51-21, CYC 29580.
2009
Part: FAN — BURNED (ZONE 100) · airframe 25,175 hrs · 27,823 cycles
ON APPROACH TO STT, STRONG ODOR SIMILAR TO ELECTRICAL FIRE, DID NOT NOTICE SMOKE IN CABIN OR COCKPIT. AT THIS TIME NR 2 RECIRCULATING FAN INOPERATIVE AS PER MEL NR 21-03 AUTH 040289-C. MEL CLEARED ON 04-30-09 AT SJU. REMOVED AND REPLACED NR 2 RECIRCULATING FAN AS PER MM JIC NR 21-22-21. OPERATIONAL CHECK OK.
2008
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 23,474 hrs · 26,031 cycles
FWD EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK FROM POWER SUPPLY 61WL AS PER MM NR 33-51-26.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 23,194 hrs · 25,777 cycles
AFT FLOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AT 10B IAW MM 33-51-21. OPS CHECKS NORMAL.
2007
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,428 hrs · 25,089 cycles
FLOORBEAM FR 38, TOP SURFACE IS CORRODED BETWEEN STR 17-20 AND UNDER CLIPNUT. FLOORBEAM AT FRAME 38 REPAIRED AS PER SRM 53-00-00 FIG 450.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,428 hrs · 25,089 cycles
LT I/B SEAT TRACK BETWEEN FRAME 29-36 CORRODED. SEAT TRACK FRAME 29-36 LT I/B REPLACED IAW SRM 51-25-04.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,428 hrs · 25,089 cycles
LT O/B SEAT TRACK BETWEEN FRAME 29-36 CORRODED. SEAT TRACK FRAME 29-36 LT OUTB REPLACED IAW SRM 51-25-04.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,089 hrs
FLOORBEAM AT FRAME 39, TOP SURFACE IS CORRODED AT STR 17, AND UNDER CLIPNUTS. FLOORBEAM AT FRAME 39 REPAIRED IAW SRM 53-00-00 FIG 429.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 22,428 hrs · 25,089 cycles
GUTTER ON RT THRESHOLD BETWEEN FRAME 36-39 IS CORRODED. GUTTER IS REMOVED AND REPLACED AS PER SRM 51-25-01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,428 hrs · 25,089 cycles
LT O/B SEAT TRACK BETWEEN FRAME 29-36 CORRODED. SEAT TRACK FRAME 29-36 LT OUTB REPLACED IAW SRM 51-25-04.
2005
Part: SPRING — BROKEN (NLG DRAG BRACE)
(REF SDR2005045) ON GROUND, AFTER ENGINE START, AN UNSAFE LANDING GEAR INDICATION ON NR 2 PANEL WAS ON. FOUND NOSE GEAR SPRING BROKEN. REPLACED NOSE LANDING GEAR DRAG BRACE ASSEMBLY.
2004
Part: WINDSHIELD — CRACKED (COCKPIT)
DURING CRUISE AT FL 240, CAPTAIN WINDSHIELD CRACKED. AIRCRAFT DIVERTED TO SANTO DOMINGO. REMOVED AND REPLACED CAPTAINS WINDSHIELD ASSY. (M)
Part: WIRE HARNESS — DAMAGED (RT MLG)
LANDING GEAR WOULD NOT RETRACT AFTER TAKE0FF. AIRCRAFT RETURN TO THE AIRPORT. REPLACED RT MLG INTERMEDIATE HARNESS.
2001
Part: SENSOR — FAILED (NR 2 ENGINE)
MIA - FLT 5265 - CREW REPORTED A RIGHT ENGINE POWER LOSS AT 1200 FEET. POWER LOSS LASTED APPROX 3-5 SECONDS THEN GRADUALLY RETURNED TO NORMAL. MAINTENANCE REMOVED AND REPLACED THE TWO TORQUE SENSOR (S/N''S CH771, CH395) ON THE RIGHT ENGINE IAW PWC MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
2000
Part: ANGLE — CORRODED (CABIN)
SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT ZEE MEMBER BETWEEN FRAMES 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION, MAINTENANCE FOUND THE LEFT FLOOR SUPPORT BETWEEN FRAMES 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SILL — CORRODED (PAX DOOR)
SAW - DURING CPCP-2 INSPECTION, MAINTENANCE FOUND THE PAX DOOR SILL PLATE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL PLATE IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT AFT INBOARD AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT AFT INBOARD AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: LIGHT — BROKEN (CABIN)
DFW - FOUND SERVICE DOOR EMERGENCY LIGHT BY THE FLOOR IS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. (M)
Part: BULB — BURNED OUT (CABIN) · airframe 13,037 hrs · 13,960 cycles
MIA - FLT 5322 - DISCOVERED PASSENGER DOOR STAIR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECKED GOOD. (X)
Part: BATTERY — DISCHARGED (CABIN) · airframe 12,983 hrs · 13,900 cycles
MIA - FLT 5239 - AFT FLOOR PROXIMITY LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (X)
Part: SOCKET — INOPERATIVE (CABIN) · airframe 12,959 hrs · 13,876 cycles
MIA - FLT 5352 - CREW REPORTED EMERGENCY LIGHT ON MAIN ENTRANCE DOOR IS OUT. REPLACED THE PASSENGER DOOR EMERGENCY LIGHT SOCKET ASSEMBLY. OPERATIONAL CHECK WAS GOOD, AIRCRAFT RETURNED TO SERVICE. (X)
Part: STATIC LINE — OBSTRUCTED (NR 2 ENGINE)
NAS - FLT 5289 - NR 2 TORQUE DID NOT RESPOND AFTER POWER MGT WAS SELECTED TO CLIMB. TORQUE WAS 90 PERCENT AT TAKEOFF AND STAYED THERE AFTER CLIMB WAS SELECTED. TORQUE RESPONDED TO MANUAL POWER SETTINGS WITH NO OTHER PROBLEMS NOTED. FOUND SHIPPING PLUG STILL INSTALLED ON NR 2 ENGINE EEC STATIC PORT. REMOVED SAME. PERFORMED ENGINE RUN AND GROUND CHECKS IAW AMM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
1999
Part: SEAT TRACK — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT INBOARD SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 36 CORRODED. MAINTENANCE REPAIRED FLOORBEAM 36 IAW SRM 53-00-00 FIGURE 435. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — DENTED (FRAME 46-47)
SAW - DURING MBV-2 INSPECTION CLEARED TDMI NR 425MQ53023 TWO DENTS IN THE LEFT SIDE OF THE FUSELAGE SKIN 18 INCHES FORWARD OF THE TAILCONE, BETWEEN FRAMES 46 AND 47 AND BETWEEN STRINGERS 13 AND 16. FORWARD DENT MEASURED 1.5 INCHES INBOARD DIAMETER BY .018 DEEP AND AFT DENT MEASURED 1.75 LONG BY .023 DEEP. REPAIRED THE DENTS IAW SRM 53-00-00 FIGURE 403. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — DENTED (FRAME 31-32)
SAW - DURING MBV-2 INSPECTION, FOUND A DENT IN THE LEFT SIDE OF THE FUSELAGE SKIN BETWEEN FRAMES 31 AND 32 AND BETWEEN STRINGER 10 AND 12, MEASURING 3 INCHES IN DIAMETER BY .038 DEEP. REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 403. AIRCRAFT RETURNED TO SERVICE. (M)
1998
Part: LIGHT — FAILED (CABIN)
DFW - EMERGENCY LIGHT STRIP INOPERABLE AT GALLEY AREA. REPLACED REAR EMERGENCY LIGHT STRIP AND PERFORMED OPERATIONAL CHECK IAW ATR JIC 33-51-21. OPERATION WAS GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED. THE LEFT FORWARD OUTBOARD, LEFT CENTER OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, RIGHT CENTER OUTBOARD AND THE RIGHT FLIGHT ATTENDANT. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. (M)
Part: SKIN — DAMAGED (FUSELAGE)
DURING MBV-1 INSPECTION, MAINTENANCE REPORTED A RIVET AT FRAME 23 RIGHT STRINGER 18 WITH A BURN HOLE IN THE COUNTER SINK. MAINTENANCE INSTALLED A PATCH TO THE RIGHT LOWER SIDE OF FUSELAGE IAW SRM 53-00-00 PAGE 526. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FLOORBEAM — CORRODED (CABIN)
SAW - DURING MBV-1 INSPECTION, MAINTENANCE REPORTED FLOORBEAM 36 WAS CORRODED. MAINTENANCE REPAIRED FLOORBEAM 36 IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: VALVE — INOPERATIVE (NR 1 PACK)
DFW - FLT 3620 - UPON ARRIVAL TO DFW, CREW SMELLED SMOKE AND CALLED FOR CFR. PAX AND CREW DEPLANED RAPIDLY. NO EMERGENCY EVACUATION ON THE TAXIWAY. NO FIRE DETECTED. CREW THEN BROUGHT A/C BACK TO GATE. NO FURTHER INCIDENTS REPORTED. A/C RETURNED TO SERVICE. CREW REPORTED SMOKE IN COCKPIT FROM ACM. NR 1 PAC VALVE CIRCUIT BREAKER POPPED JUST PRIOR TO SMOKE. MAINTENANCE R/I'D THE NR 1 PAC VALVE PER ATR72 JIC'S. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
HOUR - EMERGENCY LIGHT BATTERY PACK GALLEY EXIT LIGHT DEAD POSITION 62WL. RAI'D BATTERY PACK 62WL, OPS CHECKED GOOD. A/C RETURNED TO SERVICE. (M)
1997
Part: POWER SUPPLY — FAILED (CABIN)
ORD - FLT 4360 - EMERGENCY LIGHTS IN FORWARD PART OF CABIN ON IN FLIGHT. RAI'D BATTERY PACK AND POWER SUPPLY UNIT AT 43WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FAN — FAILED (NR 2)
ABI - FLT 3814 - EN ROUTE FROM MAF TO DFW, CREW NOTED SMOKE IN COCKPIT AND CABIN THROUGH AIR CONDITIONING SYSTEM. FLIGHT DIVERTED TO ABI AND LANDED SAFELY. MAINTENANCE INSPECTED AND CONFIRMED THE NR 2 RE-CIRCULATION FAN FAILED. THE FAN WAS DEFERRED IN ABI AND THE ACFT WAS RE-POSITIONED TO DFW. UPON ARRIVAL IN DFW, THE FAN WAS REPLACED. PERFORMED OPERATIONAL CHECK AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X)
Part: BELLCRANK — LOOSE BEARING (RT AILERON)
DFW - DURING COMPLIANCE OF AD 93-22-10 REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM, MX FOUND A BELLCRANK IN RIGHT WING AT THE AILERON WITH A LOOSE CENTER BEARING. BELLCRANK REMOVED AND REPLACED, AND OPS CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY — DISCHARGED (CABIN)
LBB - FLT 3892 - EVERY OTHER LIGHT INOP OF AFT EMERGENCY FLOOR LIGHTS. RAI'D EMERGENCY BATTERY PACK 73WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
1996
Part: BATTERY PACK — DISCHARGED (CABIN)
ORD - FLT 4321 - FORWARD EMERGENCY FLOOR LIGHTS WILL NOT RESET OR GO OUT WHEN SWITCH IS IN DISARM. RAI BATTERY PACK ASSEMBLYS. (M)
Part: POWER SUPPLY — FAILED (CABIN)
ORD - FLT 4310 - REMOVED AND REPLACED EMERGENCY POWER SUPPLY AT 43WL IAW ATR 72 JIC 33-51-21. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ORD - FLT 4131 - DURING FLIGHT, FORWARD ROW OR EMERGENCY LIGHTS CAME ON. CHANGED BATTERY PACK FOR EMERGENCY LIGHTS AT 43WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
1995
Part: LINK ASSY — FAILED (MLG DOOR)
ORD - FLT NR 4373 - LEFT MAIN GEAR DOOR NOTED TO BE OUT OF NORMAL POSITION IN FLIGHT. MAINTENANCE FOUND DOOR SUPPORT LINK TO HAVE FAILED. REPLACED LINK ASSY, PERFORMED GEAR RETRACTION TEST AND RELEASED AIRCRAFT FOR SERVICE. (M)
Part: HMU — MALFUNCTIONED (NR 2 ENGINE)
ORD - FLT NR 4058 - NR 2 TQ DROPPED TO 50 PERCENT WITH POWER LEVERS IN NOTCH. ATTEMPTED EEC RESET, CAUSING ENGINE FAILURE. WHEN TQ DROPPED TO 50 PERCENT ALL OTHER PARAMETERS FOLLOWED. REPLACED RT ENGINE FUEL SYSTEM COMPONENTS INCLUDING FLOW DIVIDER, FUEL PUMP, HMU, MFC AND FUEL NOZZLES. PERFORMED ENGINE GROUND CHECKS. AIRCRAFT RETURNED TO SERVICE. (M)