# Service difficulty reports: N418EA, cancelled Mar 25, 2013 A list on [N418EA, cancelled Mar 25, 2013](https://openairdocs.org/deregistered/N418EA-2013-03-25.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR TWAA9909503](https://openairdocs.org/sdr/TWAA9909503.md): Longeron · damaged · Jul 7, 1999 · N418EA · Doug DC951 · Fuselage Main, Longeron/Stringer > DURING CHECK-C MAINTENANCE, THE AFT CANTED BELT RING AT STA 1243, LONGERON 3L, HAD ELONGATED HOLES AT ATTACH POINTS. REPAIRED LONGERON SECTION PER SRM 53-02, PAGE 53. - [SDR TWAA9909502](https://openairdocs.org/sdr/TWAA9909502.md): Longeron · damaged · Jul 1, 1999 · N418EA · Doug DC951 · Fuselage Main, Longeron/Stringer > DURING CHECK-C MAINTENANCE, THE CANTED BELT RING AT STA 1243, LONGERON 4L, HAD ELONGATED HOLES AT THE BELT RING ATTACH POINTS. INSTALLED A SECTION OF LONGERON PER SRM 53-02, FIG 18. - [SDR TWAA9902703](https://openairdocs.org/sdr/TWAA9902703.md): Slide · air leak · Feb 20, 1999 · N418EA · Doug DC951 · Escape Slide > THE FWD LT CABIN DOOR ESCAPE SLIDE WAS FOUND WITH LOW AIR BOTTLE PRESSURE. REPLACED THE SLIDE PER MC82501. CHECK-C 3-30-98 STL. - [SDR TWAA9819502](https://openairdocs.org/sdr/TWAA9819502.md): Coalescer · contaminated · Dec 8, 1998 · N418EA · Doug DC951 · Humidity Control System > AFTER SOME TIME IN CRUISE FLIGHT AN OFFENSIVE ODOR WAS REPORTED IN THE FRONT PART OF THE CABIN. THERE WERE SOME REPORTS OF THROAT IRRITATION. REPLACED BOTH WATER SEPARATORS AND RAN THE PACKS ON FULL HOT FOR TWO HOURS. CHECK-C 3-30-98 STL. - [SDR TWAA9819501](https://openairdocs.org/sdr/TWAA9819501.md): Coalescer · contaminated · Dec 8, 1998 · N418EA · Doug DC951 · Humidity Control System > AN OFFENSIVE ODOR WAS REPORTED IN THE GALLEY AND FRONT PORTION OF THE AIRPLANE. SOME THROAT AND EYE IRRITATION. CLEANED THE ENTRANCE AND GALLEY FLOORS, OVERHEAD BAG COMPARTMENTS, AND PSU'S IN AREA. REPLACED BOTH AIR CONDITIONING WATER SEPARATORS. CHECK-C 3 - [SDR TWAA9809101](https://openairdocs.org/sdr/TWAA9809101.md): Skin · delaminated · Mar 20, 1998 · N418EA · Doug DC951 · Wing, Plate/Skin > STL - DURING OP 9 MAINTENANCE CHECK, FOUND DELAMINATION IN RT WING UPPER PANEL JUST FWD OF AILERON. REMOVED AND REPLACED UPPER WING PANEL JUST FWD OF AILERON. REF SRM 51-30-2 AND 20-30-0. (M) - [SDR TWAA9808905](https://openairdocs.org/sdr/TWAA9808905.md): Support · cracked · Mar 20, 1998 · N418EA · Doug DC951 · Fuselage Miscellaneous Structure > STL - DURING OP 9 MAINTENANCE CHECK, FOUND CRACK IN LOWER ANGLE ON RT SIDE OF LOWER RADAR SUPPORT BRACKET INSIDE NOSE WHEEL WELL. FABRICATED NEW ANGLE PER SRM 51-10-02. INSTALLED ANGLE PER SRM 51-30-02. (X) - [SDR TWAA9809404](https://openairdocs.org/sdr/TWAA9809404.md): Support · cracked · Mar 18, 1998 · N418EA · Doug DC951 · Fuselage Miscellaneous Structure > MCI - DURING OP 9 MAINTENANCE CHECK, FOUND ONE INCH CRACK IN CENTER OF CENTER SUPPORT IN BIRD CAGE. REPAIRED CRACK IN CENTER SUPPORT IN BIRD CAGE PER SRM 53-01 PAGE 10. (X) - [SDR TWAA9808904](https://openairdocs.org/sdr/TWAA9808904.md): Support · cracked · Mar 18, 1998 · N418EA · Doug DC951 · Fuselage Miscellaneous Structure > STL - DURING OP 9 MAINTENANCE CHECK, FOUND.0312 INCH IN CRACK IN UPPER ANGLE ON RT SIDE OF LOWER RADAR SUPPORT BRACKET, INSIDE NOSE WHEEL WELL. CLEANED UP CRACK AND BLENDED TO SRM LIMITS PER SRM 53-01, PAGE 4, FIG 1. (X) - [SDR TWAA9715301](https://openairdocs.org/sdr/TWAA9715301.md): Retract Mech · malfunctioned · Dec 29, 1997 · N418EA · Doug DC951 · Landing Gear Door Retract Section > STL - FLT 407 - NOSE GEAR DOOR VIBRATION AFTER GEAR RETRACTED ON TAKEOFF. CYCLED GEAR, NO HELP. UPON RETURN TO GATE FOUND LEFT NOSE GEAR DOOR DOWN. CLOSED GEAR DOOR AND PERFORMED GEAR DOOR PULL CHECK. CHECKED NORMAL. (M) - [SDR TWAA9762002](https://openairdocs.org/sdr/TWAA9762002.md): Retract Mech · malfunctioned · May 21, 1997 · N418EA · Doug DC951 · Landing Gear Door Retract Section > DFW - FLT 374 - AFTER TAKEOFF, LEFT NOSE GEAR DOOR DID NOT CLOSE FOLLOWING GEAR RETRACTION. INSPECTED NOSE GEAR DOOR LINKAGE AND MECHANISM AND PROPERLY LOCK GEAR DOOR IN UP POSITION. (M) - [SDR TWAA9751001](https://openairdocs.org/sdr/TWAA9751001.md): Coffeemaker · failed · Apr 18, 1997 · N418EA · Doug DC951 · Buffet/Galleys > STL - FLT 619 - DURING CRUISE, COFFEEMAKER EMITTED SMOKE. REMOVED AND REPLACED WORN COFFEEMAKER, MFG P/N 50198A, MANUFACTURED BY NORDSKOG INDUSTRIES, INC. OPERATIONAL CHECK NORMAL. (M) - [SDR 96ZZZX4916](https://openairdocs.org/sdr/96ZZZX4916.md): Power Supply · inoperative · Sep 8, 1996 · N418EA · Doug DC951 · Emergency Lighting > STL - FLT 517 - DURING GROUND OPERATION CHECK, OVERWING EXIT LIGHTS REMAINED ILLUMINATED. FOUND BATTERY PACK WEAK, MFG P/N 41B030CF00101, AND POWER SUPPLY MALFUNCTIONING, MFG P/N 60-1177-5. REPLACED BATTERY PACK AND POWER SUPPLY AND OVERWING EXIT LIGHT OPERA - [SDR 96ZZZX4915](https://openairdocs.org/sdr/96ZZZX4915.md): Battery Pack · discharged · Sep 8, 1996 · N418EA · Doug DC951 · Emergency Lighting > STL - FLT 517 - DURING GROUND OPERATION CHECK, OVERWING EXIT LIGHTS REMAINED ILLUMINATED. FOUND BATTERY PACK WEAK, MFG P/N 41B030CF00101, AND POWER SUPPLY MALFUNCTIONING, MFG P/N 60-1177-5. REPLACED BATTERY PACK AND POWER SUPPLY AND OVERWING EXIT LIGHT OPERA - [SDR 96ZZZM629](https://openairdocs.org/sdr/96ZZZM629.md): Filter Clog Ind · malfunctioned · Mar 4, 1996 · N418EA · Doug DC951 · Engine Oil Indicating System > BNA - DURING DESCENT NR 2 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. REMOVED AND REPLACED OIL FILTER. PLACARDED FILTER CLOG INDICATOR LIGHT. (M) - [SDR 95ZZZM684](https://openairdocs.org/sdr/95ZZZM684.md): Floor Beam · cracked · Oct 6, 1995 · N418EA · Doug DC951 · Fuselage Main, Floor Beam > STL - DURING C-CHECK, FOUND A TWO INCH CRACK IN FLOOR BEAM AT CENTER AISLE AREA, STATION 239. REPAIRED PER ARA 8749. - [SDR 95ZZZM542](https://openairdocs.org/sdr/95ZZZM542.md): Control Cable · failed · Sep 13, 1995 · N418EA · Doug DC951 · Landing Gear Door Retract Section > STL - DURING CLIMB AFTER LANDING GEAR RETRACTION, HAD SEVERE VIBRATION FROM NOSE GEAR AREA. CYCLED LANDING GEAR AND VIBRATION CONTINUED. FOUND LEFT NOSE LANDING GEAR DOOR STOP CABLE, MFG P/N 3926528-1, TENSION LOW. RIGGED CABLE TENSION AND NOSE LANDING GEAR - [SDR 95ZZZX2348](https://openairdocs.org/sdr/95ZZZX2348.md): Longeron · cracked · Apr 11, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/Stringer > STL - DURING SPECIAL CHECK, FOUND CRACK IN LONGERON 4L, STA 832. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES. - [SDR 95ZZZX2344](https://openairdocs.org/sdr/95ZZZX2344.md): Longeron · cracked · Apr 11, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/Stringer > STL - DURING SPECIAL CHECK, FOUND A.50 INCH CRACK IN LONGERON 3L, STA 794 AND STA 832. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES. - [SDR 95ZZZW607](https://openairdocs.org/sdr/95ZZZW607.md): Longeron · cracked · Apr 11, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/Stringer > STL - DURING SPECIAL CHECK, FOUND A.5 INCH CRACK IN LONGERON 3L, STATION 794 AND STA 832. REPAIRED PER SRM 53-02, FIGURE 2. - [SDR 95ZZZW604](https://openairdocs.org/sdr/95ZZZW604.md): Longeron · cracked · Apr 11, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/Stringer > STL - DURING SPECIAL CHECK, FOUND A CRACK IN LONGERON 4L, STATION 832. REPAIRED PER SRM 53-02, FIGURE 2. - [SDR 95ZZZX2350](https://openairdocs.org/sdr/95ZZZX2350.md): Longeron · cracked · Apr 10, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/Stringer > STL - DURING SPECIAL CHECK, FOUND A 1.50 INCH CRACK IN LONGERON 4L, STA 794. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES. - [SDR 95ZZZX2347](https://openairdocs.org/sdr/95ZZZX2347.md): Longeron · cracked · Apr 10, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/Stringer > STL - DURING SPECIAL CHECK, FOUND A ONE INCH CRACK IN LONGERON 2R, STA 832. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES. - [SDR 95ZZZX2346](https://openairdocs.org/sdr/95ZZZX2346.md): Longeron · cracked · Apr 10, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/Stringer > STL - DURING SPECIAL CHECK, FOUND.50 INCH CRACK IN LONGERON 3R, STA 734. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES. - [SDR 95ZZZW609](https://openairdocs.org/sdr/95ZZZW609.md): Longeron · cracked · Apr 10, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/Stringer > STL - DURING SPECIAL CHECK, FOUND A 1.5 INCH CRACK IN LONGERON 4L, STA 794. REPAIRED PER SRM 53-02, FIGURE 2. - [SDR 95ZZZW606](https://openairdocs.org/sdr/95ZZZW606.md): Longeron · cracked · Apr 10, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/Stringer > STL - DURING SPECIAL CHECK, FOUND A.5 INCH CRACK IN LONGERON 3R, STATION 734. REPAIRED PER SRM 53-02, FIGURE 2. - [SDR 95ZZZW603](https://openairdocs.org/sdr/95ZZZW603.md): Longeron · cracked · Apr 10, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/Stringer > STL - DURING SPECIAL CHECK, FOUND A ONE INCH CRACK IN LONGERON 2R, STATION 832. REPAIRED PER SRM 53-02, FIGURE 2. ## 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 = 'N418EA' AND deregistration_id = 'N418EA-2013-03-25' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N418EA-2013-03-25/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.