N411EA, cancelled Oct 2, 2002

Service difficulty reports · 34

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N411EA' AND deregistration_id = 'N411EA-2002-10-02'
  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.

SDR WXOA01012BStringer · crackedLAS - AIRCRAFT FUSELAGE DAMAGED BY GROUND SERVICE EQUIPMENT WITH AIRCRAFT POSITIONED AT GATE. DAMAGE IDENTIFIED AS PUNCTURED FUSELAGE SKIN AT FUSELAGE STATION 1022 LEFT BETWEEN LONGERON 24L AND 26L, AND CRACKED STRINGER AT FUSELAGE STATION 1022L LONGERON 26L.Aug 21, 2001 · N411EA · Doug DC951 · Fuselage Structure (General)SDR WXOA01011Terminal · corrodedFAT - DURING AIRCRAFT SCHEDULED INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE IN TAILCONE COMPARTMENT. MAINTENANCE FOUND CORRODED TERMINAL CONNECTION. CLEANED TERMINALS. EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK NORMAL. (M)Aug 13, 2001 · N411EA · Doug DC951 · Emergency LightingSDR WXOA01010Light · inoperativeFAT - DURING AIRCRAFT SCHEDULED INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE IN TAILCONE COMPARTMENT. MAINTENANCE FOUND INOPERATIVE BULBS. RELAMPED LIGHTS. EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK NORMAL. (M)Aug 7, 2001 · N411EA · Doug DC951 · Emergency LightingSDR WXOA01009Light · inoperativeFAT - DURING AIRCRAFT SCHEDULED INSPECTION, FOUND CABIN EMERGENCY LIGHTS INOPERATIVE AT STATION 1167 (AFT CABIN EXIT DOOR AREA). MAINTENANCE FOUND LOOSE WIRE CONNECTION AND INOPERATIVE BULBS. RESECURED WIRING AND RELAMPED LIGHTS. EMERGENCY LIGHTING SYSTEM OPAug 1, 2001 · N411EA · Doug DC951 · Emergency LightingSDR WXOA00032Floor Support · corrodedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FORWARD CABIN FLOOR STRUCTURE AT FUSELAGE STATION 188, RBL 45, FLOOR SUPPORT SHOWS EVIDENCE OF LEVEL 2 CORROSION ON TOP OF ANGLE. REMOVED DAMAGED FLOOR SUPPORT. FABRICATED REPLACEMENT FLOOR SUPPORNov 14, 2000 · N411EA · Doug DC951 · Fuselage Miscellaneous StructureSDR WXOA00031Angle · corrodedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, AFT AIRSTAIR, 4TH STAIR FROM TOP SHOWS EVIDENCE OF LEVEL 2 CORROSION ON BACK AND LOWER SURFACE OF STEP. REMOVED AND REPLACED STEP ANGLES AND TREAD PER DC9 SRM 51-30-8 AND BOEING DRAWING 9910381. (Nov 14, 2000 · N411EA · Doug DC951 · Entrance StairsSDR WXOA00030Support · corrodedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, AFT CARGO PIT AT FUSELAGE STATION 1167 STRINGER 30, CENTER VERTICAL SUPPORT POST SHOWS EVIDENCE OF MODERATE CORROSION (LEVEL 2) AT LOWER END OF SUPPORT. AREA OF CORROSINO APPROX 4 SQUARE INCHES. RNov 14, 2000 · N411EA · Doug DC951 · Fuselage Miscellaneous StructureSDR WXOA00029Skin · corrodedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, AFT CARGO PIT AT FUSELAGE STATION 1167 STRINGER R28, STRINGER TO FRAME TIE IN SHOWS EVIDENCE OF MODERATE (LEVEL 2) CORROSION. AREA OF CORROSION APPROXIMATELY 1.5 INCHES BY .75 INCH. REMOVED SEALANTNov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Plate/SkinSDR WXOA00028Web · corrodedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FORWARD CARGO DOOR LOWER TORQUE BOX WEB TWO EACH P/N 391Z-509-1 STAINLESS TEAR STRAPS AND P/N'S 5910142-15 AND -16 FAIL/SAFE STRAPS IDENTIFIED TO HAVE LEVEL 1 CORROSION. EIGHT HOLES IN WEB IDENTIFINov 14, 2000 · N411EA · Doug DC951 · Fuselage Miscellaneous StructureSDR WXOA00027Pan · corrodedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND LEVEL 2 CORROSION AT FORWARD CARGO DOOR LOWER PAN. REPAIRED/SPLICED FORWARD CARGO DOOR LOWER PAN PER DC9 SRM 53-05, FIGURE 44. (M)Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Miscellaneous StructureSDR WXOA00012Floorbeam · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND CRACK IN CABIN FLOORBEAM AT FS 1080, LBL 45, STRINGER 18 FLOOR WEB. CRACK REPORTED APPROXIMATELY .75 INCH LONG. STOP DRILLED CRACK AND FABRICATED AND INSTALLED DOUBLER PER DC-9 SRM 53-01. (Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Floor BeamSDR WXOA00015Retainer · damagedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND RIGHT WING INBOARD PANEL NR 2214A TO HAVE DAMAGED RETAINER. REMOVED DAMAGED SECTION OF RETAINER, FABRICATED REPLACEMENT PART FROM 70744 T6 .032, TREATED AND PRIMED COMPONENT AND INSTALLED PERNov 14, 2000 · N411EA · Doug DC951 · Wing Miscellaneous StructureSDR WXOA00014Seal · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND LEFT WING INBOARD FILLET PANEL METAL RUB SEAL DAMAGED. REMOVED DAMAGED RUB SEAL, FABRICATED REPLACEMENT RUB SEAL FROM 2024 T3 .020, TREATED AND PRIMED COMPONENT PER DC-9 SRM 51-10-3 AND INSTANov 14, 2000 · N411EA · Doug DC951 · Wing Miscellaneous StructureSDR WXOA00013Skin · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND CRACK IN LEFT WING VERTICAL VANE. STOP DRILLED CRACK AND FABRICATED AND INSTALLED DOUBLER PER DC-9 SRM 57-01 AND 51-70-4. INSTALLED FASTENERS PER SRM 51-30-1. (M)Nov 14, 2000 · N411EA · Doug DC951 · Wing, Plate/SkinSDR WXOA00026Skin · dentedMHV - DURING AIRCRAFT SCHEDULED INSPECTIN AT REPAIR STATION, FOUND THREE DENTS WITH GOUGES EXISTING ADJACENT TO EXISTING REPAIR AT FUSELAGE STATION 207 TO 229, STRINGER 15 TO 18 LEFT. REMOVED DAMAGED SKIN AND REPLACED IAW DRAWING AVQ-MVH 00-00095C, DC9 SRM 53Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Plate/SkinSDR WXOA00024Skin · dentedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND FUSELAGE SKIN DENT AT FS 283, WL 170. REMOVED DAMAGE AND REPAIRED IAW DC9 SRM 53-04, FIGURE 3B, SHEET 25. REPAIR PARTS ALODINED AND PRIMED IAW SRM 51-10-3. (M)Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Plate/SkinSDR WXOA00025Intercostal · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND FUSELAGE INTERCOSTAL CRACKED AT FUSELAGE STATION 361, STRINGER 19R. FABRICATED REPLACEMENT INTERCOSTAL AND INSTALLED PER DC9 SRM 51-10-2. (M)Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Miscellaneous StructureSDR WXOA00023Skin · gougedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND RIGHT FUSELAGE SKIN GOUGED AT FS 522, WL 175. RESULTING GOUGE AND DENT MEASURES .053 INCH DEEP BY 6.50 INCH LONG BY 3 INCH WIDE. REMOVED DAMAGE AND REPAIRED IAW DC9 SRM 53-04, FIGURE 12B, SHNov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Plate/SkinSDR WXOA00022Longeron · cutMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND FUSELAGE LONGERON SPLICE AT 17L AND STATION 229 DAMAGED. REMOVED DAMAGED SPLICE, FABRICATED REPLACEMENT SPLICE PER DC9 SRM 53-02, FIGURE 8 AND INSTALLED SPLICE PER SRM 53-02, FIGURE 8. (M)Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR WXOA00021Stringer · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND FUSELAGE STRINGER 17L CRACKED AROUND FASTENERS BETWEEN FRAME 237 AND 255. REMOVED AND REPLACED STRINGER 17L PER DC9 SRM 53-02 FIGURE 18 AND 51-10-3. (M)Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR WXOA00020Plate · corrodedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND CORROSION AT FUSELAGE STATION 465 UNDER VHF ANTENNA AT BASE PLATE. REMOVED SURFACE CORROSION, FABRICATED REPLACEMENT ANTENNA BASE PLATE AND INSTALLED PER DC9 SRM 51-10-3 AND 51-30-1. (M)Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Plate/SkinSDR WXOA00019Angle · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND TWO STRUT SUPPORT ANGLES CRACKED AT NOSE LANDING GEAR NOSE WHEEL WELL AREA FUSELAGE STATION 37 L/R STRINGER 28. CRACK LENGTHS APPROXIMATELY 2 INCHES. REMOVED TWO DAMAGED ANGLES, FABRICATED RNov 14, 2000 · N411EA · Doug DC951 · Fuselage Miscellaneous StructureSDR WXOA00018Skin · dentedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND RIGHT WING FLAP TRAILING EDGE LOWER SURFACE TO HAVE A DENT. DIMENSIONS OF DENT .800 INCH BY .500 INCH, .065 INCH DEPTH WITH SHARP CREASE. DENT EXCEEDS LIMITS OF SRM 57-01. REMOVED AREA, FABNov 14, 2000 · N411EA · Doug DC951 · Trailing Edge FlapsSDR WXOA00017Skin · damagedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND RIGHT WING UPPER SKIN SURFACE FORWARD OF OUTBOARD SPOILER HAS CRACK. REMOVED DAMAGED AREA OF SKIN AND REPLACED PER DC9 SRM 57-01, FIGURE 1. ALODINED AND TREATED AREA PER SRM 51-10-2. (M)Nov 14, 2000 · N411EA · Doug DC951 · Wing, Plate/SkinSDR WXOA00016Skin · damagedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND RIGHT WING UPPER SKIN SURFACE INBOARD OF INBOARD SPOILER HAS CRACK AROUND THREE RIVETS AT STATION XRS 137. REMOVED DAMAGED AREA OF SKIN AND REPLACED PER DC9 SRM 57-01, FIGURE 5, SHEET 2. (M)Nov 14, 2000 · N411EA · Doug DC951 · Wing, Plate/SkinSDR TWAA9816504Bulkhead · corrodedDURING CHECK-C MAINT, FOUND AFT CARGO BIN WITH CORROSION AT BOTTOM OF AFT PRESSURE BULKHEAD, STA 1168, LBL 1 IN. INSTALLED NEW T PART NR 5910130-65, AND NEW GUSSET PER SRM 53-13-3, FIG 8 PAGE 19 AND 20.Oct 7, 1998 · N411EA · Doug DC951 · Fuselage Main, BulkheadSDR TWAA9813801Control Cable · brokenDURING TAXI TOWARD THE GATE IN A 90 DEGREE RIGHT ANGLE TURN CREW HEARD LOUD SNAP AND LOST NOSE WHEEL STEERING. ACFT WAS TOWED INTO GATE. REPLACED BROKEN STEERING CABLE 124C PER MNT MANUAL 32-51-1. CHECK-C, 7-19-97 STL.Aug 26, 1998 · N411EA · Doug DC951 · Landing Gear Steering SystemSDR TWAA9810202Bolt · brokenSTL - FLT 617 - AFTER TAKEOFF FROM SGF, THE RT MAIN LANDING GEAR WOULD NOT RETRACT. OPERATED SGF TO STL WITH RT GEAR EXTENDED AT REDUCED AIR SPEED. FOUND RT MLG BUNGEE ACTUATOR PISTON END EYE BOLT BROKEN OFF. REPLACED BUNGEE. CHECK-C 7-19-97 STL. (X)Jun 25, 1998 · N411EA · Doug DC951 · Landing Gear Retraction/Extension SystemSDR TWAA9714902Bearing · failedSTL - FLT 676 - DURING CRUISE, AT FL330, RT ENGINE RUMBLED AND COMPRESSOR STALL WAS EXPERIENCED. REPLACED RT ENGINE. ENGINE WAS DISASSEMBLED AND NR 3 BEARING WAS FOUND FAILED. REPAIRED ENGINE. (M)Dec 17, 1997 · N411EA · Doug DC951 · Turbine Engine Compressor SectionSDR TWAA9727001Tire · failedSTL - DURING TAKEOFF , NR 3 MAIN TIRE BLEW OUT. REMOVED AND REPLACED NR 3 MAIN TIRE, MFG P/N 9560859-7. FUNCTIONAL CHECK NORMAL. (M)Feb 20, 1997 · N411EA · Doug DC951 · TireSDR TWAA9708003Link Assy · malfunctionedHOU - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RIGHT NOSE LANDING GEAR DOOR DID NOT CLOSE. FOUND RIGHT NOSE LANDING GEAR DOOR LINK ASSEMBLY, MFG P/N 3956785-1, MALFUNCTIONING. REPLACED DOOR LINK ASSEMBLY. NOSE LANDING GEAR DOOR OPERATION THEN CHECKED Jan 13, 1997 · N411EA · Doug DC951 · Landing Gear Door Retract SectionSDR TWAA9614801Control Cable · brokenSTL - FLT 627 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, HAD LOUD NOISE FROM NOSE LANDING GEAR AND UNSAFE LIGHT REMAINED ILLUMINATED. FOUND RIGHT NOSE LANDING GEAR DOOR STOP CABLE BROKEN, MFG PN 3926528-1. REPLACED RIGHT NOSE LANDING GEAR DOOR STOP CABNov 29, 1996 · N411EA · Doug DC951 · Landing Gear Door Retract SectionSDR 96ZZZM1526Retract Mech · lack of lubeSTL - AFTER TAKEOFF HAD VIBRATION FROM NOSE LANDING GEAR DOORS AFTER LANDING GEAR RETRACTION. CYCLED LANDING GEAR. FOUND RIGHT NOSE LANDING GEAR DOOR BUNGEE LINK, MFG P/N 3956785-1, DRY AND DIRTY. CLEANED AD LUBRICATED BUNGEE LINK. NOSE LANDING GEAR DOOR OOct 21, 1996 · N411EA · Doug DC951 · Landing Gear Door Retract SectionSDR 96ZZZX3656Wire · brokenHOU - FLT 639 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR. FOUND BROKEN WIRE AT NOSE LANDING GEAR DOWNLOCK SENSOR. MADE AIRWORTHINESS REPAIR TO WIRING. NOSE LANDING GEAR INDICATJun 2, 1996 · N411EA · Doug DC951 · Landing Gear System Wiring
Back to N411EA, cancelled Oct 2, 2002