# Service difficulty reports: N576AA

A list on [N576AA](https://openairdocs.org/aircraft/N576AA.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 2 · 83 reports

- [SDR AALA20150909009](https://openairdocs.org/sdr/AALA20150909009.md): Duct Seal · blown · Sep 9, 2015 · N576AA · Doug DC982 · Airfoil Anti/De-ice System
  > AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE HOT FLOOR, SMOKE & FUMES WERE REPORTED ON LT SIDE OF ACFT AT ROWS 22 - 27. ENG & WING ANTI-ICE WERE ON AT TIME OF HEAT & FUMES. FOUND ANTI-ICE DUCT COUPLING SEAL BLOWN IN
- [SDR AALA20140905007](https://openairdocs.org/sdr/AALA20140905007.md): Engine · malfunctioned · Sep 5, 2014 · N576AA · Doug DC982 · Engine (Turbine/Turboprop)
  > LEFT ENG LOW OIL PRESS LIGHT ILLUMINATED & LOW OIL PRESS GAUGE AT ZERO. LT ENG WAS SHUTDOWN, SINGLE ENG TIME 15 MINUTES. EMER DECLARED FLIGHT RETURNED, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT ENG. SYS GND CHECKED NORMAL OPERATION O
- [SDR AALA20140719004](https://openairdocs.org/sdr/AALA20140719004.md): Engine · failed · Jul 19, 2014 · N576AA · Doug DC982 · Engine (Turbine/Turboprop)
  > AIRCRAFT SHOOK & RT ENG LOST OIL PRESS. RT ENG WAS SHUTDOWN, SINGLE ENG TIME 15 MINUTES. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT ENG ON 07/21/2014. SYS GND CHECKED NORMAL OPERATION OPEN.
- [SDR AALA20140405007](https://openairdocs.org/sdr/AALA20140405007.md): Skin · cracked · Apr 3, 2014 · N576AA · Doug DC982 · Fuselage Main, Plate/Skin
  > FUSELAGE FWD SKIN CRACKED AT AFT HINGE CUT OUT FOR LT AFT NLG DOOR. INSTALLED DOUBLER IAW SRM 53-05-00-001 FIGURE 62.
- [SDR AALA20140403001](https://openairdocs.org/sdr/AALA20140403001.md): Valve · open · Apr 2, 2014 · N576AA · Doug DC982 · Aircraft Fuel Distribution System
  > DFW CREW REPORTED ON CLIMB OUT FUEL TANK IMBALANCE APPROACHING LIMITS. ALL PUMPS & CROSS FEED VLVS OPERATED NORMALLY. SUSPECTED FUEL TRANSFER PROBLEM. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. UPON ARRIVAL FOUND LT & RT FUELING VLVS I
- [SDR AALA20140328009](https://openairdocs.org/sdr/AALA20140328009.md): Rib · cracked · Mar 28, 2014 · N576AA · Doug DC982 · Leading Edge Devices
  > LEFT NR 4 SLAT RIB CRACKED. INSTALLED RIB DOUBLER REPAIR IAW EA MD80-57-034150.
- [SDR AALA20140328006](https://openairdocs.org/sdr/AALA20140328006.md): Rib · cracked · Mar 28, 2014 · N576AA · Doug DC982 · Leading Edge Devices
  > RIGHT NR 4 SLAT RIB CRACKED. INSTALLED RIB REPAIR DOUBLE IAW EA MD80-57-034150.
- [SDR AALA20140207004](https://openairdocs.org/sdr/AALA20140207004.md): Battery Pack · discharged · Feb 7, 2014 · N576AA · Doug DC982 · Emergency Lighting
  > AFT OVERWING EMERGENCY EXIT LIGHTS FAILED TO TEST. REPLACED BATTERY PACK FOR AFT OVERWING EMERGENCY EXIT LIGHTS, OPERATIONS CHECKED NORMAL.
- [SDR AALA20140207003](https://openairdocs.org/sdr/AALA20140207003.md): Portable Light · inoperative · Feb 7, 2014 · N576AA · Doug DC982 · Emergency Lighting
  > LT NR 1 DOOR PORTABLE EMERGENCY LIGHT FAILED TO TEST. REPLACED LIGHT ASSEMBLY, OPERATIONS CHECKED NORMAL.
- [SDR AALA20140116013](https://openairdocs.org/sdr/AALA20140116013.md): Skin · damaged · Jan 16, 2014 · N576AA · Doug DC982 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE AT STATION 447.75 & LONGERON 22 RT. INSTALLED DOUBLER IAW SRM 53-04-02.
- [SDR AALA20140116012](https://openairdocs.org/sdr/AALA20140116012.md): Skin · damaged · Jan 16, 2014 · N576AA · Doug DC982 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE AT STATION 331 APPROXIMATELY 2 INCHES ABOVE STRINGER 22 RT. INSTALLED DOUBLER IAW SRM 53-04-02 FIGURE 2.
- [SDR AALA20130308010](https://openairdocs.org/sdr/AALA20130308010.md): Oven · malfunctioned · Mar 8, 2013 · N576AA · Doug DC982 · Buffet/Galleys
  > STL - INFLIGHT DFW-CMH. CREW REPORTED SMOKE IN CABIN COMING FROM FORWARD GALLEY OVEN. EMERGENCY DECLARED FLIGHT DIVERTED STL LANDED WITHOUT INCIDENT. DEFERRED FORWARD GALLEY OVEN PER NEF. FLIGHT CONTINUED TO DESTINATION. SYSTEM GROUND CHECK NORMAL OPERATI
- [SDR AALA20130110005](https://openairdocs.org/sdr/AALA20130110005.md): Battery · not seated · Jan 10, 2013 · N576AA · Doug DC982 · Emergency Lighting
  > TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERIES. OPS CHECK NORMAL.
- [SDR AALA20130110004](https://openairdocs.org/sdr/AALA20130110004.md): Battery · not seated · Jan 10, 2013 · N576AA · Doug DC982 · Emergency Lighting
  > RIGHT CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED BATTERIES. OPS CHECK NORMAL.
- [SDR AALA20130110003](https://openairdocs.org/sdr/AALA20130110003.md): Battery · not seated · Jan 10, 2013 · N576AA · Doug DC982 · Emergency Lighting
  > CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30. RESEATED BATTERIES. OPS CHECK NORMAL.
- [SDR AALA20130109021](https://openairdocs.org/sdr/AALA20130109021.md): Battery Pack · not seated · Jan 9, 2013 · N576AA · Doug DC982 · Emergency Lighting
  > TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY PACK IN RIGHT AFT LAVATORY. OPS CHECK NORMAL.
- [SDR AALA20130109020](https://openairdocs.org/sdr/AALA20130109020.md): Battery Pack · not seated · Jan 9, 2013 · N576AA · Doug DC982 · Emergency Lighting
  > RIGHT AND CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED BATTERY PACK I RIGHT AFT LAVATORY. OPS CHECK NORMAL.
- [SDR AALA20130109019](https://openairdocs.org/sdr/AALA20130109019.md): Battery Pack · discharged · Jan 9, 2013 · N576AA · Doug DC982 · Emergency Lighting
  > CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESEATED BATTERY PACK IN ROW 29.
- [SDR AALA20120817003](https://openairdocs.org/sdr/AALA20120817003.md): Shutoff Valve · malfunctioned · Aug 16, 2012 · N576AA · Doug DC982 · Cabin Pressure Control System
  > PIT - CREW REPORTED LOSS OF PRESSURIZATION CONTROL. EMERGENCY DECLARED FLIGHT LANDED PIT WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PRESSURE REGULATING AND SHUT-OFF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.
- [SDR AALA20120418009](https://openairdocs.org/sdr/AALA20120418009.md): Skin · damaged · Apr 14, 2012 · N576AA · Doug DC982 · Fuselage Main, Plate/Skin
  > LIGHTNING/STATIC DISCHARGE AT FRAME STATION 144 AND LONGERON 14 RIGHT. TRIMMED OUT DAMAGE AND INSTALLED EXTERNAL DOUBLER PER EA MD80-53-023130.
- [SDR AALA20110610TUL04](https://openairdocs.org/sdr/AALA20110610TUL04.md): Skin · dented · Jun 10, 2011 · N576AA · Doug DC982 · Fuselage Main, Plate/Skin
  > DENTS IN SKIN FROM DOUBLER INSTALL, STATION 1250, STRINGER 1. INSTALLED DOUBLER, TRIPLER, FILLER AND FINGER DOUBLERS PER EA MD80-53-017444 DATED 6-10-11.
- [SDR AALA20110609TUL13](https://openairdocs.org/sdr/AALA20110609TUL13.md): Intercostal · cracked · Jun 9, 2011 · N576AA · Doug DC982 · Fuselage Miscellaneous Structure
  > STATION 1322 INTERCOSTAL CRACKED UNDER RIGHT TIE DOWN TRACK. INSTALLED NEW INTERCOSTAL PER AARD 51-10-00-5.
- [SDR AALA20110609TUL10](https://openairdocs.org/sdr/AALA20110609TUL10.md): Frame · cracked · Jun 9, 2011 · N576AA · Doug DC982 · Fuselage Main, Frame
  > AFT ACCESSORY 1485 CANT FRAME CRACKED AT STAIR ACTUATOR. ACCOMPLISHED INSTALLATION OF DOUBLER PER AARD 53-10-00-33.
- [SDR AALA20110609TUL08](https://openairdocs.org/sdr/AALA20110609TUL08.md): Beam · corroded · Jun 9, 2011 · N576AA · Doug DC982 · Fuselage Main, Structure
  > AFT CARGO DOOR BEAM HAS CORROSION ON WEB STATIONS 1155 TO 1212. REPLACED WEB PER AARD 51-10-00-5.
- [SDR AALA20110608TUL04](https://openairdocs.org/sdr/AALA20110608TUL04.md): Frame · cracked · Jun 8, 2011 · N576AA · Doug DC982 · Fuselage Main, Frame
  > STATION 1474 CANT FRAME CRACKED AFT OF LONGERON 17 LEFT. TRIMMED OUT CRACK AND INSTALLED DOUBLER REPAIR PER EA MD80-53-017388.
- [SDR AALA20110607TUL06](https://openairdocs.org/sdr/AALA20110607TUL06.md): Seat Track · corroded · Jun 7, 2011 · N576AA · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NUMBER 4 LUG AT G-2 GALLEY TIE DOWN AREA STATION 235 CORRODED. INSTALLED NUMBER 4 SEAT TRACK SPLICE AND NEW SECTION OF TRACK FROM STATIONS 200 TO 265 PER SRM 53-05-00 FIGURE 4F.
- [SDR AALA20110606TUL07](https://openairdocs.org/sdr/AALA20110606TUL07.md): Frame · cracked · Jun 6, 2011 · N576AA · Doug DC982 · Fuselage Main, Frame
  > STATION 1418 FRAME CRACKED LONGERON 2 RIGHT. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-03-00 FIGURE 31A.
- [SDR AALA20110606TUL05](https://openairdocs.org/sdr/AALA20110606TUL05.md): Frame · cracked · Jun 6, 2011 · N576AA · Doug DC982 · Fuselage Main, Frame
  > STATION 1418 FRAME CRACKED LONGERON 2 LEFT. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-02-00 FIGURE 31A.
- [SDR AALA20110605TUL04](https://openairdocs.org/sdr/AALA20110605TUL04.md): Seat Track · corroded · Jun 5, 2011 · N576AA · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION BLENDED OUT OF LIMITS ON SEAT TRACK NUMBER 5 STATIONS 200 TO 218. INSTALLED NUMBER 5 SEAT TRACK AT STATIONS 200 TO 245 RIGHT PER SRM 51-10-01 FIGURE 26 SHEET 2.
- [SDR AALA20110605TUL02](https://openairdocs.org/sdr/AALA20110605TUL02.md): Splice · corroded · Jun 5, 2011 · N576AA · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LEFT TIEDOWN TRACK SPLICE STATION 1220. INSTALLED SPLICE ASSEMBLY PER AARD 51-10-00-5.
- [SDR AALA20110604TUL06](https://openairdocs.org/sdr/AALA20110604TUL06.md): Shear Tie · cracked · Jun 4, 2011 · N576AA · Doug DC982 · Fuselage Internal Mounting Structure
  > SHEAR TIE CLIP CRACKED AT STATION 1437 BETWEEN LONGERONS 2 AND 3 RIGHT. REMOVED AND REPLACED SHEAR TIE CLIP AT STATION 1437 BETWEEN LONGERONS 2 AND 3 RIGHT PER AARD 51-10-00-5.
- [SDR AALA20110603TUL07](https://openairdocs.org/sdr/AALA20110603TUL07.md): Cusp Web · cracked · Jun 3, 2011 · N576AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP INBOARD CORNER AT STATION 218 UNDER SEAT TRACK NUMBER 5. INSTALLED DOUBLER ON CUSP CORNER AT STATION 218 RIGHT INBOARD SIDE OF NUMBER 5 SEAT TRACK PER AARD 53-20-00-16.
- [SDR AALA20110603TUL03](https://openairdocs.org/sdr/AALA20110603TUL03.md): Stiffener · cracked · Jun 3, 2011 · N576AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CABIN RIGHT SIDE, STATION 927, BELOW NUMBER 5 SEAT TRACK, LOWER LEG OF VERTICAL STIFFENER FROM FLOORBEAM TO TOP OF TANK IS CRACKED. INSTALLED DOUBLER AND FILLER ALL PER EA MD80-53-017224.
- [SDR AALA20110602TUL05](https://openairdocs.org/sdr/AALA20110602TUL05.md): Bracket · gouged · Jun 2, 2011 · N576AA · Doug DC982 · Fuselage Miscellaneous Structure
  > T-BRACKET GOUGED STATION 1155 LONGERON 29 RIGHT. REMOVED AND REPLACED T-BRACKET STATION 1155 LONGERON 29 RIGHT PER AARD 51-10-00-5, BOEING DRAWING NUMBER 9936073, SRM 51-30-05.
- [SDR AALA20110602TUL04](https://openairdocs.org/sdr/AALA20110602TUL04.md): Shear Tie · corroded · Jun 2, 2011 · N576AA · Doug DC982 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE STATION 1155 BETWEEN LONGERONS 30 AND 29 RIGHT. REMOVED AND REPLACED SHEAR TIE STATION 1155 LONGERONS 30 TO 29 RIGHT PER AARD 51-10-00-5, BOEING DRAWING NUMBER 9936073 AND SRM 51-30-05.
- [SDR AALA20110602TUL01](https://openairdocs.org/sdr/AALA20110602TUL01.md): Fitting · worn · Jun 2, 2011 · N576AA · Doug DC982 · Leading Edge Devices
  > RIGHT NUMBER 5 SLAT INBOARD KNUCKLE FITTING WORN. REPLACED WORN KNUCKLE FITTING BUSHING AND PIVOT PIN AT RIGHT SLAT PER ESO 80117.
- [SDR AALA20110601TUL14](https://openairdocs.org/sdr/AALA20110601TUL14.md): Skin · scratched · Jun 1, 2011 · N576AA · Doug DC982 · Fuselage Main, Plate/Skin
  > FUSELAGE FORWARD SCRATCHES IN SKIN STATION 207 BETWEEN LONGERONS 4 AND 5 LEFT. INSTALLED INTERNAL DOUBLER PER BOEING DRAWING SG09530001.
- [SDR AALA20110601TUL13](https://openairdocs.org/sdr/AALA20110601TUL13.md): Skin · scratched · Jun 1, 2011 · N576AA · Doug DC982 · Fuselage Main, Plate/Skin
  > FUSELAGE FORWARD SCRATCHES IN SKIN STATION 200, BETWEEN LONGERONS 4 AND 5 LEFT. INSTALLED INTERNAL DOUBLER PER BOEING DRAWING SG09530001.
- [SDR AALA20110601TUL02](https://openairdocs.org/sdr/AALA20110601TUL02.md): Rib · cracked · Jun 1, 2011 · N576AA · Doug DC982 · Leading Edge Devices
  > RIGHT NUMBER 5 SLAT NUMBER 14 RIB CRACKED INDICATION. REPLACED RIB RIGHT NUMBER 14 POSITION PER ESO 80117 27-80-1.
- [SDR AALA20110601TUL01](https://openairdocs.org/sdr/AALA20110601TUL01.md): Rib · cracked · Jun 1, 2011 · N576AA · Doug DC982 · Leading Edge Devices
  > LEFT NUMBER 5 SLAT NUMBER 14 RIB CRACK INDICATION. REPLACED NUMBER 14 RIB WITH NEW ONE IAW ES0 27-80-1.
- [SDR AALA20110529TUL05](https://openairdocs.org/sdr/AALA20110529TUL05.md): Pan · cracked · May 29, 2011 · N576AA · Doug DC982 · Fuselage Main, Structure
  > WINDOW RING PAN CRACKED LEFT SIDE, LOWER FORWARD CORNER AT STATION 984. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20110529TUL04](https://openairdocs.org/sdr/AALA20110529TUL04.md): Pan · cracked · May 29, 2011 · N576AA · Doug DC982 · Fuselage Main, Structure
  > WINDOW RING PAN CRACKED RIGHT SIDE, LOWER FORWARD CORNER AT STATION 984. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20110529TUL03](https://openairdocs.org/sdr/AALA20110529TUL03.md): Pan · cracked · May 29, 2011 · N576AA · Doug DC982 · Fuselage Main, Structure
  > WINDOW RING PAN CRACKED RIGHT SIDE, LOWER AFT SIDE OF STATION 845. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20110529TUL02](https://openairdocs.org/sdr/AALA20110529TUL02.md): Pan · cracked · May 29, 2011 · N576AA · Doug DC982 · Fuselage Main, Structure
  > WINDOW RING PAN CRACKED RIGHT SIDE, UPPER FORWARD CORNER AT STATION 886. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20110529TUL01](https://openairdocs.org/sdr/AALA20110529TUL01.md): Pan · cracked · May 29, 2011 · N576AA · Doug DC982 · Fuselage Main, Structure
  > WINDOW RING PAN CRACKED RIGHT SIDE, UPPER FORWARD CORNER AT STATION 927. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20110527TUL09](https://openairdocs.org/sdr/AALA20110527TUL09.md): Pan · cracked · May 27, 2011 · N576AA · Doug DC982 · Fuselage Main, Structure
  > WINDOW RING PAN CRACKED LEFT SIDE UPPER FORWARD CORNER AT STATION 788. INSTALLED DOUBLER PER AARD 53-10-00-25.
- [SDR AALA20110527TUL08](https://openairdocs.org/sdr/AALA20110527TUL08.md): Pan · cracked · May 27, 2011 · N576AA · Doug DC982 · Fuselage Main, Structure
  > WINDOW RING PAN CRACKED RIGHT SIDE FORWARD LOWER CORNER AT STATION 1155. TRIMMED OUT CRACKED TAB AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20110527TUL07](https://openairdocs.org/sdr/AALA20110527TUL07.md): Pan · cracked · May 27, 2011 · N576AA · Doug DC982 · Fuselage Main, Structure
  > WINDOW RING PAN CRACKED LEFT SIDE LOWER AFT CORNER AT STATION 826. CUT OUT CRACKED AREA OF WINDOW RINGPAN. INSTALLED DOUBLER PER AARD 53-10-00-25.
- [SDR AALA20110527TUL06](https://openairdocs.org/sdr/AALA20110527TUL06.md): Pan · cracked · May 27, 2011 · N576AA · Doug DC982 · Fuselage Main, Structure
  > WINDOW RING PAN CRACKED RIGHT SIDE FORWARD LOWER CORNER AT STATION 1211. TRIMMED OUT CRACKED TAB AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20110527TUL05](https://openairdocs.org/sdr/AALA20110527TUL05.md): Pan · cracked · May 27, 2011 · N576AA · Doug DC982 · Fuselage Main, Structure
  > WINDOW RING PAN CRACKED LEFT SIDE LOWER FORWARD CORNER AT STATION 1041. INSTALLED REPAIR ANGLE AS PER AARD 53-10-00-25.

Next page: https://openairdocs.org/aircraft/N576AA/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 = 'N576AA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N576AA/reports

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