N319AM
Registered owner: JONES ARTHUR L, OR (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Jon Hudson | Operator | on 2007-09-13 | Operator named in NTSB report |
Accident & incident history
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.
66 reports on file, 1997-07-24 – 2003-12-30.
Part: COMPUTER — FAULTY (AVIONICS BAY) · airframe 21,377 hrs · 25,179 cycles
DURING TAKEOFF ROLL THE PITCH ASSYMETRIC WARNING CAME ON. REMOVED AND REPLACED THE CREW ALERTING COMPUTER.
Part: INDICATOR — ERRATIC (ITT)
DURING TAKEOFF THE RT ENGINE ITT WENT TO 765 DEGREES. CREW ABORTED THE TAKEOFF AND RETURNED TO BLOCK. REMOVED AND REPLACED THE ITT INDICATOR FOR THE RT ENGINE.
Earlier reports · 1997–2002 · 64 reports
2002
Part: BATTERY — DISCHARGED (CABIN)
MIA - FLT 5069 - FOUND EMERGENCY LIGHTS DON'T WORK WHEN AIRCRAFT IS NOT POWERED UP. LIGHT DON NOT WORK WHEN POWER IS ON IE, OR EXTERNAL POWER RAI ALL 6 BATTERY PACKS (S/N 6506, 6498, 6406, 6635, 6399, 269). (M)
Part: SILL DRAIN — CORRODED (FUSELAGE)
SAW - DURING CPCP2 FOUND SERVICE DOOR SILL DRAIN TRACK CORRODED. REMOVED AND REPLACED SILL PLATE DRAIN TRACK IAW SRM 51-25-01 AND 51-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
SAW - DURING CPCP2 FOUND RIGHT FLOOR SUPPORT FROM FRAME 38 TO 39 CORRODED. REMOVED AND REPLACED AND REPLACED RIGHT FLOOR SUPPORT IAW ATR 42 SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
SAW - DURING CPCP2 FOUND RIGHT FLOOR SUPPORT FROM FRAME 36 TO 38 CORRODED. REMOVED AND REPLACED RIGHT FLOOR SUPPORT IAW ATR42 SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FRAME — CORRODED (FUSELAGE)
SAW - DURING CPCP2 FOUND RIGHT FRAME 37 CORRODED ON AFT SIDE JUST ABOVE SILL PLATE CORRODED. REMOVED AND REPLACED FRAME 37 RIGHT IAW SRM 51-25-02 AND 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FLAP — CORRODED (LT WING)
SAW - DURING INSPECTION, FOUND LEFT OUTBOARD FLAP FORWARD BEAM ATTACH POINT CORRODED. REPLACED LEFT OUTBOARD FLAP ASSY IAW JIC 57-53-00-RAI-10000-006. (M)
Part: FLAP — CORRODED (RT WING)
SAW - DURING INSPECTION, FOUND RIGHT OUTBOARD FLAP OUTBOARD FORWARD BEAM ATTACH FITTING CORRODED. REPLACED RIGHT OUTBOARD FLAP ASSY IAW JIC-57-53-00-RAI-10000-006. (M)
Part: FLAP — CORRODED (LT WING)
SAW - DURING INSPECTION, FOUND LEFT OUTBOARD FLAP MIDDLE FORWARD BEAM ATTACH POINT CORRODED. REPLACED LEFT OUTBOARD FLAP ASSEMBLY IAW JIC 57-53-00-RAI-10000-006. (M)
Part: SUPPORT — CORRODED (PAX DOOR)
DURING CPCP4 INSPECTION, FOUND ALL PAX DOOR TREAD SUPPORTS HAVE CORROSION. REPLACED ALL PAX DOOR TREAD SUPPORTS IAW SRM 51-25-02. (M)
Part: FLAP — CORRODED (LT WING)
SAW - DURING INSPECTION, FOUND LEFT OUTBOARD FLAP AFT BEAM ATTACH FITTING CORRODED. REPLACED LEFT OUTBOARD FLAP ASSEMBLY IAW JIC 57-53-00-RAI-10000-006. (M)
Part: LINK — CORRODED (AILERON)
MBV - DURING FOUND LEFT AILERON DUAL LOAD PATH LINK CORRODED. REPLACED LEFT AILERON DUAL LOAD PATH LINK IAW JIC 27-11-72-RAI-10000-002. (M)
Part: ANGLE — CORRODED (FUSELAGE)
SAW - DURING CPCP2 INSPECTION, FOUND LEFT Z-MEMBER CORRODED. REPLACED LEFT Z-MEMBER IAW ATR42 SRM 51-25-02. (M)
Part: DOOR FRAME — CORRODED (FUSELAGE)
SAW - DURING CPCP2 INSPECTION, FOUND FRAME ON PAX DOOR ABOVE VENT DOOR CORRODED. REPLACED FRAME ON PASSENGER DOOR IAW SRM 51-25-02 AND 51-25-03. (M)
Part: LINK — CORRODED (AILERON)
SAW - DURING INSPECTION, FOUND RIGHT AILERON DUAL LOAD PATH LINK FITTINGS ON WING IS CORRODED. REPLACED WING FITTINGS FOR RIGHT AILERON DUAL LOAD PATH LINK IAW ATR-42 SRM 51-25-02. (M)
Part: CLIP — CORRODED (PAX DOOR)
SAW - DURING CPCP2 INSPECTION, FOUND CLIPS ON PAX DOOR INTERCOSTAL TO CENTER RIB ABOVE VENT DOOR CORRODED. REPLACED CLIPS ON PASSENGER DOOR INTERCOSTAL IAW SRM 51-25-02. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
SAW - DURING CPCP2 INSPECTION, FOUND LEFT FLOOR SUPPORT BETWEEN 39-40 CORRODED. REPLACED FLOOR SUPPORT BETWEEN 39-40 IAW SRM 51-25-02. (M)
Part: ATTACH FITTING — CORRODED (FUSELAGE)
DURING CPCP4 INSPECTION, FOUND RIGHT FORWARD CARGO LOWER PANEL ATTACH FITTINGS CORRODED. REPLACED RIGHT FORWARD LOWER CARGO ATTACH FITTINGS IAW ATR 42 SRM 51-25-01 AND 51-25-03. (M)
Part: FRAME — CORRODED (FUSELAGE)
MBV - FOUND DURING INSPECTION, FRAME 45 CORRODED BETWEEN STRINGER 18L AND 20 R. INSTALLED NEW SHEER TIE ON FRAME 45 BETWEEN STRINGER 18L AND 20R IAW ATR-42 SRM 51-25-02. (M)
Part: FITTING — CORRODED (FUSELAGE)
SAW - DURING CPCP2 INSPECTION, FOUND PAX DOOR SILL PLATE FORWARD TEE FITTING CORRODED. REPLACED PAX DOOR FORWARD TEE FITTING IAW SRM 51-25-03. (M)
Part: LINK — CORRODED (AILERON)
SAW - DURING INSPECTION, FOUND RIGHT AILERON DUAL LOAD PATH LINK CORRODED. REPLACED RIGHT AILERON DUAL LOAD PATH LINK IAW ATR-42 JIC 27-11-72 RAI 10000-002. (M)
Part: ACCESS PANEL — CORRODED (WING)
SAW - DURING CPCP4 INSPECTION, FOUND OVERWING ACCESS PANELS CORRODED. REPLACED OVERWING ACCESS PANELS IAW ATR42 JIC 57-00-00OAC10000-012. (M)
Part: VENTURI — CORRODED (LAVATORY)
SAW - DURING CPCP2 INSPECTION, FOUND LAVATORY VENTURI TUBE CORRODED. REPLACED LAVATORY VENTURI TUBE IAW SRM 51-25-02. (M)
Part: SILL — CORRODED (FUSELAGE)
SAW - DURING CPCP2 INSPECTION, FOUND PASSENGER DOOR SILL PLATE DRAIN TRACK CORRODED. REPLACED PASSENGER DOOR SILL PLATE DRAIN TRACK IAW SRM 51-21-42. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
SAW - DURING CPCP4 INSPECTION, FOUND AFT CARGO SEAT TRACKS TO BE CORRODED. REPLACED SEAT TRACKS IAW EO E1-53MR-271. (M)
Part: FITTING — CORRODED (FUSELAGE)
SAW - DURING CPCP2 INSPECTION, FOUND PAX DOOR SILL PLATE AFT TEE FITTINGS CORRODED. REPLACED AFT TEE FITTINGS ON PAX DOOR SILL PLATE IAW SRM 51-25-04. (M)
Part: WEB — CORRODED (FUSELAGE)
SAW - DURING CPCP2 INSPECTION, FOUND LEFT WEB FROM FRAME 39-40 AT Z-MEMBER CORRODED. REPLACED LEFT WEB FROM FRAMES 39-40 AT Z-MEMBER 39-40 IAW SRM 51-25-02. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
SAW - DURING CPCP8 INSPECTION, FOUND RIGHT FORWARD OUTBOARD, RIGHT FORWARD INBOARD, LEFT FORWARD INBOARD, RIGHT MID OUTBOARD, RIGHT MID INBOARD, LEFT MID OUTBOARD, RIGHT AFT INBOARD, LEFT AFT OUTBOARD SEAT TRACKS TO BE CORRODED BEYOND LIMITS. REPLACED SEAT TRACKS IAW EO E1-53MR-271. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
SAW - DURING CPCP2 INSPECTION, FOUND FLOORBEAMS 36, 38, AND 39 TO BE CORRODED BEYOND LIMITS. REPLACED FLOORBEAMS IAW ATR 42 SRM 51-25-02. (M)
Part: DOOR — CORRODED (E/E BAY)
SAW - DURING CPCP8 INSPECTION, AFT AVIONICS COMPARTMENT DOOR HAS CORROSION AROUND CIRCUMFERENCE. REPLACED AFT AVIONICS COMPARTMENT DOOR IAW ATR 42 STANDARD PRACTICES MM 20-21-12. (M)
Part: ATTACH ANGLE — CORRODED (PAX DOOR)
SAW - DURING CPCP8 INSPECTION, FOUND PASSENGER DOOR LOWER ATTACH ANGLE FOR STEP SHELL IS CORRODED BEYOND LIMITS. REPLACED PASSENGER DOOR LOWER ATTACH ANGLE IAW ATR 42 SRM 51-25-02. (M)
Part: STRINGER — CORRODED (FUSELAGE)
SAW - DURING CPCP8 INSPECTION, FOUND STRINGER 17R TO BE CORRODED. REPLACED STRINGER 17R IAW ATR 42 SRM 51-25-02. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
SAW - DURING CPCP2 INSPECTION, FOUND FLOORBEAM 40 TO BE CORRODED. REPLACED FLOORBEAM 40 IAW ATR 42 SRM 51-25-02. (M)
Part: SKIN — CORRODED (FUSELAGE)
SAW - DURING CPCP8 INSPECTION, FOUND AIRFRAME CUTOUT FOR AFT AVIONICS DOOR IS CORRODED BEYOND LIMITS. REPLACED CUTOUT REINFORCING IAW ATR42 SRM 51-25-02. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
SAW - DURING CPCP8 INSPECTION, FOUND LEFT MID INBOARD AND LEFT FORWARD OUTBOARD SEAT TRACK CORRODED. REPLACED SEAT TRACKS IAW EO E1-53MR-271. (M)
Part: BULKHEAD — CORRODED (FUSELAGE)
SAW - DURING CPCP8 INSPECTION, FOUND GROUNDING POINTS TO RADOME ON FORWARD PRESSURE BULKHEAD HAVE PITTING CORROSION. REPAIRED LOWER RIGHT GROUNDING POINT ON FORWARD PRESSURE BULKHEAD ER-1 IAW ATR42 SRM 53-11-10. (M)
Part: ATTACH FITTING — CORRODED (FUSELAGE)
SAW - DURING CPCP8 INSPECTION, FOUND FORWARD CARGO DRAIN TRACK ATTACH PLATE CORRODED. REPLACED FORWARD CARGO DRAIN TRACK ATTACHED PLATE IAW SRM 51-25-02. (M)
Part: TRACK — CORRODED (FUSELAGE)
SAW - DURING CPCP8 INSPECTION, FOUND FORWARD CARGO DRAIN TRACK CORRODED. REPLACED FORWARD CARGO DRAIN TRACK IAW SRM 51-25-02. (M)
Part: ANGLE — CORRODED (RT WING)
SAW - DURING CPCP8 INSPECTION, FOUND RIGHT WING REAR SPAR UPPER SPAR ANGLE TO BE CORRODED JUST OUTBOARD OF INBOARD AILERON HINGE. REPAIRED IAW ATR FAX DO/TE/S560.0401/02-1004. AIRCRAFT WAS RETURNED TO SERVICE. (M)
2001
Part: LIGHT — INOPERATIVE (DOOR STEP)
MIA - FLT 5037 - FOUND CABIN DOOR STEP EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY IAW ATR 42 AMM. (M)
Part: MODULE — FAULTY (CABIN)
FLL - FLT 5419 - DURING CLIMB, THE FLIGHT ATTENDANT REPORTED THE SMELL OF SMOKE FOLLOWED BY VISIBLE SMOKE IN CABIN. CREW COMPLIED WITH AIR CONDITION SMOKE PROCEDURES AND SMOKE SEEMED TO STOP. AFTER FLIGHT, FURTHER REPORTS INDICATE THAT SMOKE POSSIBLY CAME FROM THE AFT RIGHT (10 OR 11CD) OVERHEAD LIGHTING FIXTURES (READING LIGHTS). MAINTENANCE FOUND THE READING LIGHT MODULE AT SEAT 11CD TO BE AT FAULT. MODULE WAS REMOVED AND REPLACED IAW ATR MM. OPERATIONAL CHECK AS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
MIA - FLT 5247 - CREW REPORTED THE PASSENGER DOOR EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN POWER SUPPLY UNIT 15WL IAW AMERICAN EAGLE WORK CARD. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED SERVICE. (M)
Part: LIGHT — INOPERATIVE (PAX DOOR)
MIA - MAINTENANCE REPORTED THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT RETURNED TO SERVICE. (M)
2000
Part: SOCKET — DIRTY (CABIN) · airframe 17,080 hrs · 19,455 cycles
NAS - EXTERNAL EMERGENCY LIGHT IN PASSENGER DOOR IS INOPERATIVE. MAINTENANCE CLEANED LIGHT SOCKET. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY — INOPERATIVE (CABIN)
SAW - DURING PS-2 CHECK, FOUND EMERGENCY LIGHTS BATTERY PACK AT 18WL INOPERATIVE. REMOVED AND REPLACED BATTERY IAW JIC 335121-RAI-10000. OPS CHECK GOOD. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING MBV-1 INSPECTION, FOUND RIGHT AFT INBOARD AND RIGHT AFT OUTBOARD SEAT TRACKS (P/N S53678001202, S53678001201) CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SEAT TRACK IAW EO E9-5300-013. (M)
Part: PLATE — CORRODED (KEELBEAM)
SAW - DURING MBV-1 INSPECTION, FOUND LOWER KEEL BEAM PLATE BETWEEN FRAMES 25A AND 27A CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED KEEL BEAM PLATE IAW SRM 51-25-03. (M)
Part: ANGLE — CORRODED (CARGO BAY) · airframe 16,508 hrs · 18,584 cycles
SAW - DURING MBV-1 INSPECTION, FOUND RIGHT AFT CARGO ZEE MEMBER CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED ZEE MEMBER IAW SRM 51-25-03. (X)
Part: GUIDE — CORRODED (TE FLAP)
SAW - DURING MBV-1 INSPECTION, FOUND RIGHT OUTBOARD FLAP INBOARD DEFLECTOR ALL THREE CAM GUIDES CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED CAM GUIDES (P/N''''S S5751014900300, S57510148003000, D57510150003000)IAW SRM 57-53-20. (M)
Part: CONTROL UNIT — FAILED (CABIN) · airframe 16,437 hrs · 18,505 cycles
MIA - FLT 5349 - SMELL, BURNING ODOR FROM AVIONICS RACK BEHIND CAPTAIN'S SEAT. REMOVED AND REPLACED FDAU IAW ATR MM 31-30-00. OPS CHECKED GOOD. (X)
1999
Part: SKIN — DENTED (FUSELAGE)
SAW - AIRCRAFT ARRIVED FOR REPAIR OF LARGE DENT AFT OF PASSENGER DOOR BETWEEN FRAMES 40 AND 41 AT STRINGER 12. REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 405. AIRCRAFT RETURNED TO SERVICE. (M)
Part: WIRE — BROKEN (PAX DOOR)
MSN - FLT 9751 - PASSENGER DOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. FOUND BROKEN WIRE AT THE LIGHT ASSEMBLY. DISASSEMBLED LIGHT CONNECTOR, INSTALLED NEW PINS FOR WIRES AND REASSEMBLED CONNECTOR. OPERATIONAL CHECK GOOD. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
GRR - CENTER CABIN EMERGENCY FLOOR LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK FOR POWER SUPPLY AND THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
GRR - CENTER CABIN EMERGENCY FLOOR LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK FOR POWER SUPPLY AND THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)
1998
Part: HOT JUG — MALFUNCTIONED (GALLEY)
ORD - FLT 4068 - BURNING RUBBER SMELL IN THE AREA OF THE HOT JUGS. FOUND BURNED HOT JUG RECEPTACLE, MEL'D THE HOT JUG. ON 11-19-98, THE LEFT HOT JUG RECEPTACLE WAS REPLACED AND THE MEL WAS CLEARED. (M)
Part: DRAIN TRACK — CORRODED (SERVICE DOORWAY)
SAW - DURING CPCP1 INSPECTION, FOUND THE SERVICE DOOR DRAIN TRACK BETWEEN FRAME 36 AND 39 CORRODED. REMOVED AND REPLACED THE DRAIN TRACK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SUPPORT — CORRODED (CARGO BAY)
SAW - DURING CPCP1 INSPECTION, FOUND THE RIGHT AFT CARGO ZEE MEMBER CORRODED. REMOVED AND REPLACED THE ZEE MEMBER. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP1 INSPECTION, FOUND THE RIGHT AFT INBOARD AND OUTBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP1 INSPECTION, FOUND THE RIGHT AFT INBOARD AND OUTBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP1 INSPECTION, FOUND THE RIGHT AFT INBOARD AND OUTBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SILL — CORRODED (PAX DOOR)
SAW - DURING CPCP1 INSPECTION, FOUND THE PASSENGER DOOR SILL PLATE BETWEEN FRAME 36 AND 39 CORRODED. REMOVED AND REPLACED THE SILL PLATE. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FLOORBEAM — CORRODED (CABIN)
SAW - DURING CPCP1 INSPECTION, FOUND FLOORBEAM 36 AND 38 CORRODED. REMOVED AND REPLACED BOTH FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FLOORBEAM — CORRODED (CABIN)
SAW - DURING CPCP1 INSPECTION, FOUND FLOORBEAM 36 AND 38 CORRODED. REMOVED AND REPLACED BOTH FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M)
1997
Part: POWER UNIT — BURNED (CABIN)
BWI - FLT 4943 - DURING CLIMB-OUT OF DCA, THE FLIGHT ATTENDANT ALERTED THE CAPT OF SMOKE IN AFT CABIN. AIRCRAFT LANDED SAFELY AT BWI. FOUND POWER UNIT AT SEAT 10D BURNED.
Part: SILL — CORRODED (CARGO DOORWAY)
SAW - FORWARD CARGO DOOR SILL CORRODED, FOUND DURING HEAVY CHECK. REMOVED AND REPLACED CHANNEL IAW 51-25-03, PREPPED AND PAINTED CHANNEL IAW 51-21-31. (M)