# Service difficulty reports: N416EA, cancelled Apr 30, 2013 A list on [N416EA, cancelled Apr 30, 2013](https://openairdocs.org/deregistered/N416EA-2013-04-30.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR TWAA9903207](https://openairdocs.org/sdr/TWAA9903207.md): Beam · cracked · Feb 26, 1999 · N416EA · Doug DC951 · Service Doors > DURING OP-9, FOUND.5 INCH CRACK IN THE TOP BEAM AFT CORNER OF THE FWD RT SERVICE DOOR. REPAIRED PER THE SRM 52-51.D. - [SDR TWAA9903206](https://openairdocs.org/sdr/TWAA9903206.md): Pressure Panel · cracked · Feb 26, 1999 · N416EA · Doug DC951 · Fuselage Miscellaneous Structure > DURING CHECK-C, FOUND THE HORIZONTAL PRESSURE PANEL AT STATION 83.5 ON THE RT SIDE TUNNEL AREA HAD A.5 INCH CRACK. STOP DRILLED THE CRACK, FABRICATED AND INSTALLED A REPAIR DOUBLER PER THE SRM 53-10-10.5. - [SDR TWAA9815901](https://openairdocs.org/sdr/TWAA9815901.md): Light · shorted · Sep 25, 1998 · N416EA · Doug DC951 · Emergency Lighting > FWD SECTION OF FIRST CLASS FLOOR EGRESS LIGHTING INOPERATIVE. REPLACED SHORTED LIGHT STRIP. CHECK-C 12-17-97 STL. - [SDR TWAA9808001](https://openairdocs.org/sdr/TWAA9808001.md): Power Supply · inoperative · May 19, 1998 · N416EA · Doug DC951 · Emergency Lighting > STL - FLT 625 - DURING PREFLIGHT INSPECTION, FOND AFT EGRESS AND AFT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK MFG P/N 5822-2, FLEX CABLES MFG P/NS 5853-1 AND 5854-3. (M) - [SDR TSAA9808001](https://openairdocs.org/sdr/TSAA9808001.md): Power Supply · inoperative · May 19, 1998 · N416EA · Doug DC951 · Emergency Lighting > STL - FLT 625 - DURING PRE-FLIGHT INSPECTION, FOUND AFT EGRESS AND AFT OVERWING EMERGENCY LIGHTS INOPERABLE. REPLACED BATTERY PACK MFG P/N 5822-2, FLEX CABLES MFG P/N 5853-1 AND P/N 5854-3. OP-15 12-17-97 STL CLOSED. (X) - [SDR TWAA9803302](https://openairdocs.org/sdr/TWAA9803302.md): Power Supply · inoperative · Mar 6, 1998 · N416EA · Doug DC951 · Emergency Lighting > STL - FLT 651 - EGRESS LIGHTS WERE FOUND INOPERATIVE IN THE AFT SECTION OF FIRST CLASS AND THE FORWARD SECTION OF COACH. REPLACED EMERGENCY LIGHT POWER SUPPLY FOR EGRESS LIGHTS AT ROW 6. (M) - [SDR TWAA9713102](https://openairdocs.org/sdr/TWAA9713102.md): Pump · worn · Nov 1, 1997 · N416EA · Doug DC951 · Hydraulic Pump (Electric/Engine), Main > BDL - FLT 290 - DURING CLIMB, THE NR 1 ENGINE, S/N 1705, HYDRAULIC PUMP FAILED DUE TO WEAR. REMOVED AND REPLACED THE HYDRAULIC PUMP MANUFACTURED BY VICKERS. OPERATIONAL CHECK NORMAL. (M) - [SDR TWAA9712404](https://openairdocs.org/sdr/TWAA9712404.md): Connector · dirty · Oct 12, 1997 · N416EA · Doug DC951 · Emergency Lighting > STL - FLT 433 - FIRST SECTION OF COACH EMERGENCY LIGHTS WERE INOPERABLE. CLEANED CONNECTOR AND RECHARGED BATTERIES. CK-C 2-4-97 STL - (X) - [SDR TWAA9790001](https://openairdocs.org/sdr/TWAA9790001.md): Bungee Cyl · broken · Aug 8, 1997 · N416EA · Doug DC951 · Landing Gear Retraction/Extension System > STL - FLT 539 - RIGHT MAIN LANDING GEAR WOULD NOT RETRACT DUE TO A BROKEN BUNGEE CYLINDER. REMOVED AND REPLACED RETRACT BUNGEE CYLINDER, MFG P/N 3914016-6505, MANUFACTURED BY DOUGLAS AIRCRAFT COMPANY. OPERATIONAL CHECK NORMAL. (M) - [SDR 96ZZZM1460](https://openairdocs.org/sdr/96ZZZM1460.md): Power Supply · inoperative · Sep 26, 1996 · N416EA · Doug DC951 · Emergency Lighting > STL - DURING CRUISE, EGRESS LIGHTS ILLUMINATED. CYCLED SWITCH. FOUND BATTERY POWER SUPPLY WEAK, MFG P/N 5822-2. REPLACED BATTERY POWER SUPPLY. EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. - [SDR 96ZZZM1466](https://openairdocs.org/sdr/96ZZZM1466.md): Lights · moisture contam · Sep 24, 1996 · N416EA · Doug DC951 · Emergency Lighting > STL - DURING CRUISE, EGRESS LIGHTS ILLUMINATED IN AFT END OF CABIN. CYCLED SWITCH TO OFF AND BACK TO ARMED. FOUND MOISTURE IN LIGHT TRACK. CLEANED AND DRIED TRACK. LIGHT OPERATION CHECKED NORMAL. - [SDR 96ZZZM658](https://openairdocs.org/sdr/96ZZZM658.md): Batteries · discharged · Mar 11, 1996 · N416EA · Doug DC951 · Emergency Lighting > STL - DURING ROUTINE MAINTENACNE CHECK, EXTERIOR EMERGENCY LIGHTS DID NOT ILLUMINATE. FOUND BATTERIES, MFG P/N 41B030CF00101, WEAK. REPLACED BATTERIES AND EXTERIOR LIGHT OPERATION CHECKED NORMAL. (M) - [SDR 96ZZZM51](https://openairdocs.org/sdr/96ZZZM51.md): Control Vlv · lack of lube · Dec 28, 1995 · N416EA · Doug DC951 · Landing Gear Retraction/Extension System > OKC - FLT NR 265 - AFTER TAKEOFF, FOLLOWING GEAR RETRACTION, GEAR DOOR LIGHT STAYED ON. CHECKED AND LUBRICATED LANDING GEAR VALVE. OPERATIONAL CHECK NORMAL. - [SDR 96ZZZM674](https://openairdocs.org/sdr/96ZZZM674.md): Contl Valve · lack of lube · Nov 28, 1995 · N416EA · Doug DC951 · Landing Gear Door Retract Section > FLT NR 430 - OKC - AFTER TAKEOFF, FOLLOWING GEAR RETRACTION, GEAR DOOR LIGHT STAYED ON. CHECKED AND LUBRICATED LANDING GEAR CONTROL VALVE. OPERATIONAL CHECK NORMAL. (M) - [SDR 96ZZZX229](https://openairdocs.org/sdr/96ZZZX229.md): Angle · cracked · Nov 22, 1995 · N416EA · Doug DC951 · Vertical Stabilizer > STL - DURING CHECK C, FOUND A.3750 INCH CRACK IN RIGHT SIDE OF VERTICAL STABILIZER ATTACH ANGLE, STA 1292. REPAIRED BY INSTALLLING DOUBLER PER SRM 53-05, FIGURE 23. AIRCRAFT TOTAL TIME: 40,618 HOURS, 36,293 CYCLES. - [SDR 96ZZZX228](https://openairdocs.org/sdr/96ZZZX228.md): Angle · cracked · Nov 22, 1995 · N416EA · Doug DC951 · Vertical Stabilizer > STL - DURING CHECK C, FOUND A 2.50 INCH CRACK AT LEFT SIDE OF VERTICAL STABILIZER ATTACH ANGLE, FS 1292. REPAIRED PER SRM 53-05, FIGURE 23. AIRCRAFT TOTAL TIME: 40,618 HOURS, 36,293 CYCLES. ## 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 = 'N416EA' AND deregistration_id = 'N416EA-2013-04-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N416EA-2013-04-30/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, except the copies of manufacturers’ service documents, which belong to their rights holders.