# Service difficulty reports: N411EA, cancelled Oct 2, 2002

A list on [N411EA, cancelled Oct 2, 2002](https://openairdocs.org/deregistered/N411EA-2002-10-02.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR WXOA01012B](https://openairdocs.org/sdr/WXOA01012B.md): Stringer · cracked · Aug 21, 2001 · N411EA · Doug DC951 · Fuselage Structure (General)
  > LAS - 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.
- [SDR WXOA01011](https://openairdocs.org/sdr/WXOA01011.md): Terminal · corroded · Aug 13, 2001 · N411EA · Doug DC951 · Emergency Lighting
  > FAT - 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)
- [SDR WXOA01010](https://openairdocs.org/sdr/WXOA01010.md): Light · inoperative · Aug 7, 2001 · N411EA · Doug DC951 · Emergency Lighting
  > FAT - DURING AIRCRAFT SCHEDULED INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE IN TAILCONE COMPARTMENT. MAINTENANCE FOUND INOPERATIVE BULBS. RELAMPED LIGHTS. EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK NORMAL. (M)
- [SDR WXOA01009](https://openairdocs.org/sdr/WXOA01009.md): Light · inoperative · Aug 1, 2001 · N411EA · Doug DC951 · Emergency Lighting
  > FAT - 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 OP
- [SDR WXOA00032](https://openairdocs.org/sdr/WXOA00032.md): Floor Support · corroded · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Miscellaneous Structure
  > MHV - 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 SUPPOR
- [SDR WXOA00031](https://openairdocs.org/sdr/WXOA00031.md): Angle · corroded · Nov 14, 2000 · N411EA · Doug DC951 · Entrance Stairs
  > MHV - 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. (
- [SDR WXOA00030](https://openairdocs.org/sdr/WXOA00030.md): Support · corroded · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Miscellaneous Structure
  > MHV - 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. R
- [SDR WXOA00029](https://openairdocs.org/sdr/WXOA00029.md): Skin · corroded · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Plate/Skin
  > MHV - 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 SEALANT
- [SDR WXOA00028](https://openairdocs.org/sdr/WXOA00028.md): Web · corroded · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Miscellaneous Structure
  > MHV - 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 IDENTIFI
- [SDR WXOA00027](https://openairdocs.org/sdr/WXOA00027.md): Pan · corroded · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Miscellaneous Structure
  > MHV - 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)
- [SDR WXOA00012](https://openairdocs.org/sdr/WXOA00012.md): Floorbeam · cracked · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Floor Beam
  > MHV - 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. (
- [SDR WXOA00015](https://openairdocs.org/sdr/WXOA00015.md): Retainer · damaged · Nov 14, 2000 · N411EA · Doug DC951 · Wing Miscellaneous Structure
  > MHV - 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 PER
- [SDR WXOA00014](https://openairdocs.org/sdr/WXOA00014.md): Seal · cracked · Nov 14, 2000 · N411EA · Doug DC951 · Wing Miscellaneous Structure
  > MHV - 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 INSTA
- [SDR WXOA00013](https://openairdocs.org/sdr/WXOA00013.md): Skin · cracked · Nov 14, 2000 · N411EA · Doug DC951 · Wing, Plate/Skin
  > MHV - 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)
- [SDR WXOA00026](https://openairdocs.org/sdr/WXOA00026.md): Skin · dented · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Plate/Skin
  > MHV - 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 53
- [SDR WXOA00024](https://openairdocs.org/sdr/WXOA00024.md): Skin · dented · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Plate/Skin
  > MHV - 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)
- [SDR WXOA00025](https://openairdocs.org/sdr/WXOA00025.md): Intercostal · cracked · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Miscellaneous Structure
  > MHV - 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)
- [SDR WXOA00023](https://openairdocs.org/sdr/WXOA00023.md): Skin · gouged · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Plate/Skin
  > MHV - 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, SH
- [SDR WXOA00022](https://openairdocs.org/sdr/WXOA00022.md): Longeron · cut · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Longeron/Stringer
  > MHV - 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)
- [SDR WXOA00021](https://openairdocs.org/sdr/WXOA00021.md): Stringer · cracked · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Longeron/Stringer
  > MHV - 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)
- [SDR WXOA00020](https://openairdocs.org/sdr/WXOA00020.md): Plate · corroded · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Main, Plate/Skin
  > MHV - 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)
- [SDR WXOA00019](https://openairdocs.org/sdr/WXOA00019.md): Angle · cracked · Nov 14, 2000 · N411EA · Doug DC951 · Fuselage Miscellaneous Structure
  > MHV - 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 R
- [SDR WXOA00018](https://openairdocs.org/sdr/WXOA00018.md): Skin · dented · Nov 14, 2000 · N411EA · Doug DC951 · Trailing Edge Flaps
  > MHV - 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, FAB
- [SDR WXOA00017](https://openairdocs.org/sdr/WXOA00017.md): Skin · damaged · Nov 14, 2000 · N411EA · Doug DC951 · Wing, Plate/Skin
  > MHV - 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)
- [SDR WXOA00016](https://openairdocs.org/sdr/WXOA00016.md): Skin · damaged · Nov 14, 2000 · N411EA · Doug DC951 · Wing, Plate/Skin
  > MHV - 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)
- [SDR TWAA9816504](https://openairdocs.org/sdr/TWAA9816504.md): Bulkhead · corroded · Oct 7, 1998 · N411EA · Doug DC951 · Fuselage Main, Bulkhead
  > DURING 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.
- [SDR TWAA9813801](https://openairdocs.org/sdr/TWAA9813801.md): Control Cable · broken · Aug 26, 1998 · N411EA · Doug DC951 · Landing Gear Steering System
  > DURING 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.
- [SDR TWAA9810202](https://openairdocs.org/sdr/TWAA9810202.md): Bolt · broken · Jun 25, 1998 · N411EA · Doug DC951 · Landing Gear Retraction/Extension System
  > STL - 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)
- [SDR TWAA9714902](https://openairdocs.org/sdr/TWAA9714902.md): Bearing · failed · Dec 17, 1997 · N411EA · Doug DC951 · Turbine Engine Compressor Section
  > STL - 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)
- [SDR TWAA9727001](https://openairdocs.org/sdr/TWAA9727001.md): Tire · failed · Feb 20, 1997 · N411EA · Doug DC951 · Tire
  > STL - DURING TAKEOFF, NR 3 MAIN TIRE BLEW OUT. REMOVED AND REPLACED NR 3 MAIN TIRE, MFG P/N 9560859-7. FUNCTIONAL CHECK NORMAL. (M)
- [SDR TWAA9708003](https://openairdocs.org/sdr/TWAA9708003.md): Link Assy · malfunctioned · Jan 13, 1997 · N411EA · Doug DC951 · Landing Gear Door Retract Section
  > HOU - 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
- [SDR TWAA9614801](https://openairdocs.org/sdr/TWAA9614801.md): Control Cable · broken · Nov 29, 1996 · N411EA · Doug DC951 · Landing Gear Door Retract Section
  > STL - 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 CAB
- [SDR 96ZZZM1526](https://openairdocs.org/sdr/96ZZZM1526.md): Retract Mech · lack of lube · Oct 21, 1996 · N411EA · Doug DC951 · Landing Gear Door Retract Section
  > STL - 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 O
- [SDR 96ZZZX3656](https://openairdocs.org/sdr/96ZZZX3656.md): Wire · broken · Jun 2, 1996 · N411EA · Doug DC951 · Landing Gear System Wiring
  > HOU - 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 INDICAT

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N411EA-2002-10-02/reports

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