# Service difficulty reports: N513AA, cancelled Sep 6, 2019

A list on [N513AA, cancelled Sep 6, 2019](https://openairdocs.org/deregistered/N513AA-2019-09-06.md).

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

Page 1 of 4 · 164 reports

- [SDR AALA201706289025](https://openairdocs.org/sdr/AALA201706289025.md): Relay · faulty · Jun 27, 2017 · N513AA · Doug DC982 · APU Start/Ignition System
  > THE AIRCRAFT WAS GROUNDED. R CSD WARN LIGHT (LOW OIL PRESS) FIRST THEN R GEN INOP. DISCONNECTED R CSD PER PROCEDURE. APU WOULD NOT START AT 30,000 OR 28,000 OR 26,000 FEET. NO FAULT LIGHT. THE FLIGHT DECLARED AN EMERGENCY AND DIVERTED TO SDF WITHOUT FURTHER
- [SDR AALA20170628001](https://openairdocs.org/sdr/AALA20170628001.md): Csd · inoperative · Jun 27, 2017 · N513AA · Doug DC983 · Alternator-Generator Drive
  > THE AIRCRAFT WAS GROUNDED. R CSD WARN LIGHT (LOW OIL PRESS) FIRST THEN R GEN INOP. DISCONNECTED R CSD PER PROCEDURE. APU WOULD NOT START AT 30,000 OR 28,000 OR 26,000 FEET. NO FAULT LIGHT. THE FLIGHT DECLARED AN EMERGENCY AND DIVERTED TO SDF WITHOUT FURTHER I
- [SDR AALA20170215008](https://openairdocs.org/sdr/AALA20170215008.md): Hinge Pin · migrated · Feb 12, 2017 · N513AA · Doug DC982 · Flight Compartment Windows
  > AIRCRAFT WAS GROUNDED. FIRST OFFICER SLIDING WINDOW HAS A HINGE PIN ON THE AFT LOCK BAR MIGRATING UPWARD. REPOSITIONED HINGE PIN AND REATTACHED LOWER AFT LINKAGE ROD IAW AMM 56-10-03. OPERATIONAL CHECK GOOD.
- [SDR AALA20170109026](https://openairdocs.org/sdr/AALA20170109026.md): Ballast · burned · Jan 5, 2017 · N513AA · Doug DC982 · Passenger Compartment Lighting
  > DURING MANEUVERING FOR LANDING, THE ENTIRE CABIN AND COCKPIT EXPERIENCED AN UNUSUAL ODOR LASTING 3 OR 4 MINUTES. NO SMOKE OR HAZE PRESENT. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED A BURNED CEILING LIGHT BALLAST AT ROW 8 IAW AMM 33-21-03. OPS CHECKED GOOD.
- [SDR AALA20161101004](https://openairdocs.org/sdr/AALA20161101004.md): Solenoid Valve · leaking · Oct 29, 2016 · N513AA · Doug DC982 · APU Oil System
  > AIRCRAFT NOT GROUNDED. SMOKE AND ODOR IN CABIN PRIOR TO PUSHBACK FROM GATE DUE TO APU DE-OIL SOLENOID VALVE LEAKING OIL INTO INTAKE. REMOVED AND REPLACED VALVE IAW AMM 49-90-05. OPERATIONAL CHECK GOOD.
- [SDR AALA20160424003](https://openairdocs.org/sdr/AALA20160424003.md): Boot · disconnected · Apr 24, 2016 · N513AA · Doug DC982 · Air Distribution System
  > AIRCRAFT WAS GNDED. AIR INTERRUPT, DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. FOUND THE OUTFLOW DUCT CONNECTOR BOOT OFF AT THE AIR CYCLE MACHINE. SECURED BOOT IAW AMM 21-00-00. ACCOMPLISHED OPERATIONAL & LEAK CHECKS. SYS CHECKED
- [SDR AALA20160405017](https://openairdocs.org/sdr/AALA20160405017.md): Web · cracked · Apr 5, 2016 · N513AA · Doug DC982 · Passenger/Crew Doors
  > AIRCRAFT WAS IN BASE MX. FWD ENTRY DOOR INTERNAL WEB SKIN IS CRACKED AT THE TOP FWD CORNER AT CROSSBEAM & NR 1 BEAM. REPAIRED WEB IAW EA 259387 DATED 4 5 16.
- [SDR AALA20160404007](https://openairdocs.org/sdr/AALA20160404007.md): Frame · worn · Apr 4, 2016 · N513AA · Doug DC982 · Fuselage Main, Frame
  > AIRCRAFT WAS IN BASE MX. LT SIDE OF AFT ACCESSORY FRAME STRUCTURE IS WORN AT CANT 1510, BETWEEN LONGERON 28L & 30L. ACCOMPLISHED REPAIR IAW EA 259344.
- [SDR AALA20160325002](https://openairdocs.org/sdr/AALA20160325002.md): Portable Light · faulty · Mar 24, 2016 · N513AA · Doug DC982 · Emergency Lighting
  > AIRCRAFT WAS NOT GNDED. PORTABLE EMER LIGHT ASSEMBLY AT L1 DOOR WILL NOT SHUT OFF. R & R LIGHT ASSEMBLY IAW AMM 33-53-00. SYS CHECKED NORMAL.
- [SDR AALA20160325001](https://openairdocs.org/sdr/AALA20160325001.md): Battery · discharged · Mar 24, 2016 · N513AA · Doug DC982 · Emergency Lighting
  > AIRCRAFT WAS NOT GNDED. EMER LIGHTS BETWEEN AFT LAVATORIES WILL NOT TEST. R & R EMER LIGHT BATTERY ASSEMBLY IAW AMM 33-53-00. SYS CHECKED NORMAL.
- [SDR AALA20151120002](https://openairdocs.org/sdr/AALA20151120002.md): Longeron · cracked · Nov 20, 2015 · N513AA · Doug DC982 · Fuselage Main, Longeron/Stringer
  > CRACK FOUND AT FASTENER HOLE, UPPER FLANGE ON LONGERON 23L AT STATION 200. REPAIRED WITH SPLICE REPAIR IAW SRM 53-02-00.
- [SDR AALA20150826004](https://openairdocs.org/sdr/AALA20150826004.md): Battery Pack · discharged · Aug 25, 2015 · N513AA · Doug DC982 · Emergency Lighting
  > OVERHEAD EMER LIGHTS INOPERATIVE IN ROWS 3 & 6. R & R BATTERY PACK AT CTR AISLE AT FWD LAVATORY IAW WDM 33- 51-11. SYS CHECKED NORMAL. SEE ALSO AALA20150825022.
- [SDR AALA20150825022](https://openairdocs.org/sdr/AALA20150825022.md): Battery Pack · discharged · Aug 25, 2015 · N513AA · Doug DC982 · Emergency Lighting
  > OVERHEAD EMER LIGHTS INOPERATIVE IN ROWS 3 & 6. R & R BATTERY PACK AT ROW 5 IAW WDM 33- 51-11. SYS CHECKED NORMAL.
- [SDR AALA20150825021](https://openairdocs.org/sdr/AALA20150825021.md): Battery · discharged · Aug 25, 2015 · N513AA · Doug DC982 · Emergency Lighting
  > OVERHEAD EMER LIGHTS INOPERATIVE AT ROWS 12 - 15. R & R BATTERY AT ROW 13 IAW WDM 33-51-11. SYS CHECKED NORMAL.
- [SDR AALA20150825020](https://openairdocs.org/sdr/AALA20150825020.md): Wire Harness · faulty · Aug 25, 2015 · N513AA · Doug DC982 · Light System Wiring
  > SEAT MOUNTED EMER LIGHT AT 13DEF INOPERATIVE. INSTALLED SERVICEABLE WIRE HARNESS AT ROW 13DEF IAW WDM 33-51-11. SYS CHECKED NORMAL.
- [SDR AALA20150326002](https://openairdocs.org/sdr/AALA20150326002.md): Battery Pack · discharged · Mar 25, 2015 · N513AA · Doug DC982 · Emergency Lighting
  > AFT CABIN EMER LIGHTS BETWEEN LAVATORIES WON`T TEST. REPLACED EMER LIGHT CABIN BATTERY PACK FOR AFT AISLE LIGHTS IAW AMM 33-53-00. SYS CHECKED NORMAL.
- [SDR AALA20150326001](https://openairdocs.org/sdr/AALA20150326001.md): Control Module · faulty · Mar 25, 2015 · N513AA · Doug DC982 · Emergency Lighting
  > FORWARD EMER PATH LIGHTS WON`T TEST USING PACK AB5-1. R & R AB5-1 EMER PATH LIGHTING CONTROL MODULE IAW AMM 33-60-00. SYS CHECKED NORMAL.
- [SDR AALA20141013006](https://openairdocs.org/sdr/AALA20141013006.md): Bracket · cracked · Oct 13, 2014 · N513AA · Doug DC982 · Fuselage Main, Structure
  > MID CARGO DOOR STOP PAD CRACKED ON FWD SIDE. REMOVED & INSTALLED SERVICEABLE BRACKET.
- [SDR AALA20141013005](https://openairdocs.org/sdr/AALA20141013005.md): Bracket · cracked · Oct 13, 2014 · N513AA · Doug DC982 · Fuselage Main, Structure
  > CARGO DOOR STOP PAD BRACKET CRACKED. REMOVED & INSTALLED SERVICEABLE BRACKET.
- [SDR AALA20141010002](https://openairdocs.org/sdr/AALA20141010002.md): Shear Tie · cracked · Oct 10, 2014 · N513AA · Doug DC982 · Fuselage Internal Mounting Structure
  > SHEAR TIE CRACKED AT STATION 1437 OTBD OF LONGERON 2 RT. INSTALLED NEW SHEAR TIE IAW DWG 9911840, AARD 51-00-05-1 & SRM 53-05-00-001 FIGURE 99.
- [SDR AALA20141010001](https://openairdocs.org/sdr/AALA20141010001.md): Shear Tie · cracked · Oct 10, 2014 · N513AA · Doug DC982 · Fuselage Internal Mounting Structure
  > SHEAR TIE CRACKED AT STATION 1437 & LONGERON 2 LT. REPLACED CLIP IAW DWG 9911840, SRM 53-05-00-001 FIGURE 99 & AARD 51-00-05-1 REPAIR 1.
- [SDR AALA20140924007](https://openairdocs.org/sdr/AALA20140924007.md): Former · cracked · Sep 24, 2014 · N513AA · Doug DC982 · Leading Edge Devices
  > RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-06.
- [SDR AALA20140924006](https://openairdocs.org/sdr/AALA20140924006.md): Former · cracked · Sep 24, 2014 · N513AA · Doug DC982 · Leading Edge Devices
  > LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 SLAT INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-05.
- [SDR AALA20130815011](https://openairdocs.org/sdr/AALA20130815011.md): Battery Pack · discharged · Aug 15, 2013 · N513AA · Doug DC982 · Emergency Lighting
  > CABIN EMERGENCY LIGHT WOULD NOT ILLUMINATE. REPLACED BATTERY PACK FOR CABIN EMERGENCY LIGHTS. OPERATIONS CHECKED NORMAL.
- [SDR AALA20130521015](https://openairdocs.org/sdr/AALA20130521015.md): Sense Line · disconnected · May 21, 2013 · N513AA · Doug DC982 · Cabin Cooling System
  > CREW REPORTED PRESSURIZATION FLUCTUATION, AUTO PILOT DISCONNECT AND CAPTAINS PITOT FAULT. EMERGENCY DECLARED FLIGHT DIVERTED LIT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. RECONNECTED SENSE LINE FOR LT PACK. SYS GROUND CHECK NORMAL OPERATION. (CL
- [SDR AALA20130501016](https://openairdocs.org/sdr/AALA20130501016.md): Skin · dented · May 1, 2013 · N513AA · Doug DC982 · Fuselage Main, Plate/Skin
  > FUSELAGE DENT AT STATION 207 BETWEEN LONGERON 4 AND 5 LEFT WITH DEEP GOUGE. REMOVED DAMAGE SKIN PER 53-04-03 AND INSTALLED DOUBLER PER SRM 53-04-03 FIGURE 3 AND EA MD80-53-029559.
- [SDR AALA20130501015](https://openairdocs.org/sdr/AALA20130501015.md): Longeron · cracked · May 1, 2013 · N513AA · Doug DC982 · Fuselage Main, Longeron/Stringer
  > LONGERON 4 LEFT IS CRACKED AT STATION 200. INSTALLED LONGERON SPLICE PER SRM 53-02-00 FIGURE 18.
- [SDR AALA20130424010](https://openairdocs.org/sdr/AALA20130424010.md): Doubler · corroded · Apr 24, 2013 · N513AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION ON DOUBLER UNDER G2 GALLEY MOUNT AT STATION 218. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20130423006](https://openairdocs.org/sdr/AALA20130423006.md): Longeron · cracked · Apr 23, 2013 · N513AA · Doug DC982 · Fuselage Main, Longeron/Stringer
  > LONGERON 2 LEFT CRACKED AT STATION 160. CUT OUT SECTION OF LONGERON FROM STATIONS 150 TO 171 AND INSTALLED SPLICE REPAIR PER SRM 53-02, FIGURE 18.
- [SDR AALA20130422032](https://openairdocs.org/sdr/AALA20130422032.md): Cusp Web · corroded · Apr 22, 2013 · N513AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER SIDE OF RIGHT CUSP AT STATION 218 BELOW NUMBER 6 SEAT TRACK. REMOVED CORRODED CUSP AND INSTALLED NEW CUSP PER AARD 51-00-05-1.
- [SDR AALA20130421001](https://openairdocs.org/sdr/AALA20130421001.md): Pan · cracked · Apr 21, 2013 · N513AA · Doug DC982 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR, NUMBER 1 BEAM FORWARD SIDE PAN CRACKED. STOP DRILLED PER ESO 80174 AND INSTALLED DOUBLER PER EA COMP-52-029331.
- [SDR AALA20130419018](https://openairdocs.org/sdr/AALA20130419018.md): Skin · cracked · Apr 19, 2013 · N513AA · Doug DC982 · Fuselage Main, Plate/Skin
  > LEFT SIDE FUSELAGE SKIN CRACKED AT STATION 1309 ABOVE LONGERON 7 LEFT. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 32.
- [SDR AALA20130419017](https://openairdocs.org/sdr/AALA20130419017.md): Cusp Web · damaged · Apr 19, 2013 · N513AA · Doug DC982 · Fuselage Miscellaneous Structure
  > DAMAGE TO RIGHT CUSP AT STATION 237 BETWEEN STRINGERS 5 AND 6. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.
- [SDR AALA20130419014](https://openairdocs.org/sdr/AALA20130419014.md): Attach Angle · corroded · Apr 19, 2013 · N513AA · Doug DC982 · Fuselage Miscellaneous Structure
  > FORWARD DOOR JAMB LOWER ATTACH ANGLE HAS CORROSION STATION 1155. REMOVED AND REPLACED DOOR JAMB ANGLE PER SRM 51-30-05.
- [SDR AALA20130419010](https://openairdocs.org/sdr/AALA20130419010.md): Skin · cracked · Apr 19, 2013 · N513AA · Doug DC982 · Fuselage Main, Plate/Skin
  > RIGHT SIDE OF FUSELAGE SKIN CRACKED AT STATION 1309 ABOVE LONGERON 7 RIGHT. INSTALLED REPAIR DOUBLER SRM 53-04-00 FIGURE 32.
- [SDR AALA20130418009](https://openairdocs.org/sdr/AALA20130418009.md): Cusp Web · cracked · Apr 18, 2013 · N513AA · Doug DC982 · Fuselage Miscellaneous Structure
  > FASTENER HOLE CRACKED IN CUSP AT STATION 187, RIGHT BUTTLINE 63. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.
- [SDR AALA20130418006](https://openairdocs.org/sdr/AALA20130418006.md): Stiffener · cracked · Apr 18, 2013 · N513AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CRACK IN VERTICAL SUPPORT AT STATION 1338 BELOW LONGERON 1 LEFT. REPLACED VERTICLE STIFFENER PER AARD 51-00-05-1.
- [SDR AALA20130417018](https://openairdocs.org/sdr/AALA20130417018.md): Cusp Web · cracked · Apr 17, 2013 · N513AA · Doug DC982 · Fuselage Miscellaneous Structure
  > RIGHT CUSP IS CRACKED AT STATION 1022. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.
- [SDR AALA20130416014](https://openairdocs.org/sdr/AALA20130416014.md): Cusp Web · cracked · Apr 16, 2013 · N513AA · Doug DC982 · Fuselage Miscellaneous Structure
  > RIGHT CUSP SHEET IS CRACKED UNDER SEAT TRACK SPLICE AT STATION 800. REPALCED CUSP SHEET PER AARD 51-00-05-1.
- [SDR AALA20130416012](https://openairdocs.org/sdr/AALA20130416012.md): Pan · cracked · Apr 16, 2013 · N513AA · Doug DC982 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR, NUMBER 1 BEAM FORWARD SIDE PAN CRACKED. ACCOMPLISHED NESTED ANGLE REPAIR PER EA COMP-52-029331 AND ESO 80174 PAGE 601B BASED ON SRM 52-03-00 FIGURE 8 WITH SOME EXCEPTIONS.
- [SDR AALA20130416010](https://openairdocs.org/sdr/AALA20130416010.md): Door Frame · cracked · Apr 16, 2013 · N513AA · Doug DC982 · Fuselage Main, Structure
  > DOOR FRAME WEB CRACKED AT SCREW GOUGE, STATION 634, LONGERON 27 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-24 FIGURE 1 (SHEET 3).
- [SDR AALA20130415003](https://openairdocs.org/sdr/AALA20130415003.md): Membrane · corroded · Apr 15, 2013 · N513AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION ON SUB-FLOOR UNDER G-1 GALLEY DRAIN PAN. INSTALLED SUB-FLOOR DOUBLER UNDER G1 GALLEY PAN PER AARD 53-20-00-16.
- [SDR AALA20130412018](https://openairdocs.org/sdr/AALA20130412018.md): Cusp Web · corroded · Apr 12, 2013 · N513AA · Doug DC982 · Fuselage Miscellaneous Structure
  > RIGHT CUSP AT STATION 494 CORRODED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20130412016](https://openairdocs.org/sdr/AALA20130412016.md): Frame · worn · Apr 12, 2013 · N513AA · Doug DC982 · Fuselage Main, Frame
  > FRAME 1380 HAS WEAR ON FORWARD SIDE, CONTACT WITH TEMPERATURE CONTROL VALVE, LEFT. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-28.
- [SDR AALA20130501010](https://openairdocs.org/sdr/AALA20130501010.md): Cusp Web · corroded · Apr 10, 2013 · N513AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CUT OUT AREA OF SUBFLOOR AND EEXISTING DOUBLER CORRODED. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20130420009](https://openairdocs.org/sdr/AALA20130420009.md): Skin · damaged · Apr 10, 2013 · N513AA · Doug DC982 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR HAS SEVERAL SCRATCHES ON EXTERIOR SKIN. INSTALLED NEW EXTERIOR SKIN ON FORWARD CARGO DOOR.
- [SDR AALA20130501014](https://openairdocs.org/sdr/AALA20130501014.md): Longeron · cracked · Apr 9, 2013 · N513AA · Doug DC982 · Fuselage Main, Longeron/Stringer
  > LONGERON 3 LEFT IS CRACKED AT STATION 160. INSTALLED LONGERON SPLICE PER SRM 53-02-00 FIGURE 18.
- [SDR AALA20130501012](https://openairdocs.org/sdr/AALA20130501012.md): Sill · corroded · Apr 9, 2013 · N513AA · Doug DC982 · Fuselage Miscellaneous Structure
  > FORWARD SERVICE DOOR SILL CORRODED AT STATION 198. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-14.
- [SDR AALA20120723001](https://openairdocs.org/sdr/AALA20120723001.md): Battery Pack · discharged · Jul 22, 2012 · N513AA · Doug DC982 · Emergency Lighting
  > CEILING EMERGENCY LIGHTS FROM ROWS 3 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FROM ROWS 3 TO 6. OPS CHECK NORMAL.
- [SDR AALA20120506006](https://openairdocs.org/sdr/AALA20120506006.md): Battery Pack · not seated · May 5, 2012 · N513AA · Doug DC982 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS 3AB AND 3EF INOPERATIVE. RESEATED BATTERY PACK IN BIN 4DEF. OPS CHECK NORMAL.

Next page: https://openairdocs.org/deregistered/N513AA-2019-09-06/reports.md?page=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 = 'N513AA' AND deregistration_id = 'N513AA-2019-09-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N513AA-2019-09-06/reports

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