N728AE
Service difficulty reports not matched to an aircraft · 34
They name N728AE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N728AE' AND registry_match IS NULL ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N728AE' AND registry_match IS NULL ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SIMA20121201004Light · inoperativeDURING B INSPECTION FOUND THE MAIN DOOR OVERHEAD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR OVERHEAD EMERGENCY LIGHT BULB IAW EMB 135 AMM 33-50-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RSDR SIMA20120813005Lamp · inoperativeDURING MAINTENANCE INSPECTION, FOUND SERVICE DOOR EMERGENCY LIGHT WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICE DOOR LIGHT LAMP IAW AMM 33-50-09. OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.SDR SIMA201135503Controller · malfunctionedON FLIGHT 4554 THE CREW REPORTED THAT AT 30,000 FEET IN LIGHT CHOPPY WEATHER HAD AN UNCOMMANDED RIGHT TURN FOLLOWED BY RED "AP" ON PFD AT 2,500 FEET. THE AIRCRAFT YAWED NOSE RIGHT WITH ONLY YAW DAMP ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND RESDR SIMA201126601Module · inoperativeON FLIGHT 3349 THE CREW REPORTED THAT AFTER TAKEOFF THE CABIN ALTIMETER DID NOT CHANGE UNTIL 9000 FEET. AFTER THAT IT CHANGED RAPIDLY AT 15000 FEET. IT (CABIN ALT) WAS AT 3300 FEET AND IT WAS SUPPOSE TO BE AT 1300 FEET THE CABIN NEVER PRESSURIZED. THE CREW SDR SIMA201034001Battery · dischargedDURING THE MAINTENANCE BASE VISIT FOUND THE NR 1 EMERGENCY LIGHT SYSTEM BULBS TO HAVE DIM LIGHTS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY AND CHARGER. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200824603Proximity Switch · out of adjustON FLIGHT 4700 CREW REPORTED AFTER TAKEOFF LG AIR GRND FAIL CAUTION CAME ON. COULD NOT RETRACT LANDING GEAR. COMPLIED AOM VOL 1. RETURNED TO AIRPORT. NORMAL LANDING WAS MADE LANDING WAS NOT OVERWEIGHT. LESS THAN 300 FEET PER MINUTE WEIGHT WAS 38000 LBS. SDR SIMA200816403Squat Switch · malfunctionedON FLIGHT 4732 - AFTER TAKEOFF CREW REPORTED THAT WHEN GEAR HANDLE SELECTED UP THEY RECEIVED A LANDING GEAR AIR/GND FAIL MESSAGE AND GEAR WOULD NOT RETRACT. RETURNED TO RDU. AFTER LANDING RECEIVED MULTIPLE CAUTIONS/WARNINGS INCLUDING 1C 1-2 WOW INOP, AHRS 1-SDR SIMA200807907Carbon Seal · faultyON FLIGHT 4564, CREW REPORTED STRONG SMOKE SMELL AND LAV SMOKE DETECTOR GOING OFF. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER 2 ENGINE IAW W/C 71-000-00. REMOVED AND REPLACED THE NUMBER 4 CARBON SEAL. AIRCSDR SIMA200728304Landing Gear · unknownAFTER TAKEOFF CREW REPORTED AIR/GROUND FAIL WARNING. REPLACED GEAR HANDLE PN 7455501 SN 0589. REPLACED LGEU PN 355022002 SN 5270. ALSO, CLEANED AND SERVICED ALL LG STRUTS PERFORMED FUNCTIONAL TEST OF EXTENSION AND RETRACTION IAW AMM 32-30-00. CHECKED ALL 5SDR SIMA200726803Connector · looseAFTER TAKEOFF FROM RDU GEAR WOULD NOT RETRACT UNLESS OVERRIDE USED. FOUND LOOSE CONNECTOR ON RT MLG NR 2 WOW SWITCH. RESECURED CONNECTOR AND PERFORMED EXT/RETRACTION OPS CHECKS IAW EMB AMM 32-30-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200620824Floor Support · corrodedDURING HMBV INSPECTION, PREVIOUS REPAIR OF THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED CORROSION, FABRICATED REPAIR PARTS, FILLER DOUBLER, PLATE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 33, CHAPTERS 53-00-01. RETURNED AIRCRSDR SIMA200620807Floor Support · corrodedDURING HMBV INSPECTION, FOUND CENTER OMEGA BEAM TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUTOUT, FABRICATING A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 22, CHAPTERS 53-00-10 AND 51-40-02. RETURNED AIRCRAFSDR SIMA200620806Floor Support · corrodedDURING HMBV INSPECTION, FOUND CENTER OMEGA BEAM TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUTOUT, FABRICATING A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 33, CHAPTERS 53-00-10 AND 51-40-02. RETURNED AIRCRAFSDR SIMA200620805Sill · corrodedDURING HMBV INSPECTION, FOUND CARGO DOOR OPENING LOWER SILL TO BE CORRODED. REMOVED THE CORRODED LOWER SILL AND INSTALLED SERVICEABLE SILL IAW EMB SRM, SRM 145/1142 REV 33, CHAPTERS 51-40-02, 03, 51-40-06 AND EMB CPM, CPM 145/1132 REV 13, CHAPTERS 51-21-04, 5SDR SIMA200620825Floor Support · corrodedABI - DURING HMBV INSPECTION, LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUTOUT, FABRICATING TWO SHIMS AND FILLER. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 33, CHAPTER 53-00-10 FIG 202. RETURNED AIRCRAFT TO SERVSDR SIMA200612803Engine · malfunctionedCREW HEARD A LOUD BANG AT START OF TAKEOFF ROLL, ALL ENGINE PARAMETERS WERE FINE GOT EITHER AN E2 OUT OR E2 FAIL. CREW WAS UNSURE RETURNED TO GATE IN JFK. REPLACED ENGINE NR 2. ENGINE NR 2 P/N OFF/ON AE3007A1/3, ENGINE NR 2 S/N OFF CAE311947, S/N ON CAE3117SDR SIMA200525502Smoke Detector · will not testAFT BAGGAGE SMOKE DETECTOR WILL NOT TEST. REPLACED SMOKE DETECTOR NR 1 IAW EMB 135 AMM 26-15-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200430802Module · inoperativeCREW REPORTED A SMOKE SMELL IN COCKPIT AND GALLEY AREA, AIRCRAFT WAS DIVERTED AND SAFELY WITH NO INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE SIDE WALL LIGHT CONTROL MODULE IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200419706Plate · corrodedDURING A CPCP INSPECTION, MAINTENANCE FOUND THE CABIN INTERIOR STRUCTURE FORWARD RIGHT SERVICE DOOR SIDE JUNCTION PLATE FOR FLOORBEAM CONNECTION HAS CORROSION. INSTALLED NEW JUNCTION PLATE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200419702Gusset · corrodedSAW - DURING A CPCP INSPECTION, MAINTENANCE FOUND CABIN INTERIOR CENTER SUPPORT BEAM AT FRAME 19 CORRODED. REMOVED AND REPLACED GUSSETT IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200419705Threshold · corrodedSAW - DURING AN IMBV INSPECTION, MAINTENANCE FOUND THE INTERIORS STRUCTURE RIGHT SERVICE DOOR ENTRANCE THRESHOLD TO HAVE CORROSION. INSTALLED NEW RIGHT SERVICE DOOR THRESHOLD IAW EMB SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200419703Beam · corrodedDURING A CPCP INSPECTON, MAINTENANCE FOUND CORROSION ON CENTER HAT BEAM AT FRAME 20. REMOVED AND REPLACED HAT BEAM IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200419704Support · corrodedSAW - DURING A CPCP INSPECTION, MAINTENANCE FOUND CABIN INTERIOR FORWARD STRUCTURE CENTER SUPPORT AT FRAME 17 CORRODED. REMOVED AND REPLACED CABIN INTERIOR FORWARD STRUCTURE SUPPORT TEE FRAME 17 IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200419701Bracket · corrodedSAW - DURING A CPCP INSPECTION, MAINTENANCE FOUND INTERNAL FUSELAGE JUST INSIDE PASSENGER DOOR, TWO BRACKETS HAVE CORROSION. REMOVED AND REPLACED BRACKETS P/N 145-24131-005, 145-24131-007, IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200407202Wire · damagedNR 3 AND 4 EMERGENCY LIGHT STRIPS ARE INOPERATIVE. REPAIRED WIRE SPLICE IAW AMM 70-03-03. OPS CHECK GOOD. (M)SDR SIMA200402003Floorbeam · corrodedTHE LT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. CUT OUT DAMAGE SECTION OF LT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED EXTERNAL ANGLE, FILLER, PLATE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 24, CHAPTESDR SIMA200213011Floorbeam · corrodedABI - DURING INSPECTION, FOUND FORWARD DIGITAL CORRODED AT RIVETS AND NUTPLATE BETWEEN FRAME 16 AND 18. REMOVED CORROSION BY CUT OUT. REPAIRED IAW EMB 145, SRM 145/1142, CHAPTER 53 REV 17 53-21-10, AND STANDARD SRM PRACTICES. (M) (M)SDR SIMA200214821Floor Support · corrodedABI - THIS IS A LEVEL 2 FINDING. CENTER BEAM GUSSET CORRODED AT FRAME 20. REMOVED AND INSTALLED NEW CENTER BEAM IAW EMB 135 SRM 51-40-02. (M)SDR SIMA200214820Crossbeam · corrodedABI - THIS IS A LEVEL 2 FINDING. FLOOR EXTENSION CROSSMEMBER CORRODED AT FRAME 22. REMOVED AND REPLACED CROSSMEMBER IAW EMB 135 SRM 51-40-02. (M)SDR SIMA200214819Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING. LEFT OMEGA BEAM CORRODED AT FRAME 20. BLENDED AND TREATED CORROSION IAW EMB GST-1472/02. (M)SDR SIMA200214818Support · corrodedABI - THIS IS A LEVEL 2 FINDING. RAMP SUPPORT CORRODED AT FRAME 20. INSTALLED SERVICEABLE RAMP IAW EMB 145 SRM 51-40-02. (M)SDR SIMA200214817Gusset · corrodedABI - THIS IS A LEVEL 2 FINDING. FORWARD DIAMOND GUSSET CORRODED AT FRAME 20. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 135 SRM 51-40-02. (M)SDR SIMA200126006Control Unit · faultyLGA - FLT 4545 - RETURN TO FIELD DUE TO RUMBLING NOISE COMING FROM NOSE AREA. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE SPOILER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SDR SIMA200119402Light · inoperativeCMH - MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEATS 7 AND 8 ARE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR LIGHT STRIP IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Back to N728AE