# Service difficulty reports: N558AA A list on [N558AA](https://openairdocs.org/aircraft/N558AA.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 · 73 reports - [SDR AALA20150205005](https://openairdocs.org/sdr/AALA20150205005.md): Link · missing · Feb 5, 2015 · N558AA · Doug DC982 · Landing Gear Door Retract Section > EMERGENCY DECLARED & LANDING UNEVENTFUL. RT MLG DOOR DID NOT LATCH CLOSED ON LANDING. FOUND DOOR UP LATCH ROLLER & ARM MISSING. REPLACED LINK ASSEMBLY. SYS CHECKED NORMAL. - [SDR AALA20140406003](https://openairdocs.org/sdr/AALA20140406003.md): A/C Pack · failed · Apr 6, 2014 · N558AA · Doug DC982 · Cabin Cooling System > BHM INFLIGHT JAX DFW, CREW REPORTED RT PACK FAILED WITH LT PACK ON PLACARD. EMERGENCY DECLARED FLIGHT DIVERTED BHM LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT PACK COALESCE BAG. SYS GND CHECKED NORMAL, OPERATION CLOSED. - [SDR AALA20140220008](https://openairdocs.org/sdr/AALA20140220008.md): Valve · malfunctioned · Feb 20, 2014 · N558AA · Doug DC982 · Fuel Transfer Valve > ELP INFLIGHT DFW-SAN CREW REPORTED UNWANTED FUEL TRANSFER IN FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED ELP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CHECK VLV FLUSH PROCEDURE. OPERATED PUMPS & NO TRANSFER NOTED. SYS GND CHECKED NO - [SDR AALA20140110001](https://openairdocs.org/sdr/AALA20140110001.md): Power Supply · inoperative · Jan 10, 2014 · N558AA · Doug DC982 · Emergency Lighting > AFT SECTION OF EMERGENCY SEAT LIGHTING INOPERATIVE. REPLACED AFT SEAT LIGHTING POWER SUPPLY & BATTERY. OPERATIONS CHECKED NORMAL. - [SDR AALA20131007001](https://openairdocs.org/sdr/AALA20131007001.md): Casting · cracked · Oct 6, 2013 · N558AA · Doug DC982 · Wing Miscellaneous Structure > RT WING, CRACK ON INBD SIDE OF RIB CASTING INBD OF NR 4 SLAT TRACK. INSTALLED REPAIR FITTING ON NR 4 SLAT TRACK INBD SUPPORT RIB IAW EA MD80-57-031777. - [SDR AALA20131006013](https://openairdocs.org/sdr/AALA20131006013.md): Skin · cracked · Oct 6, 2013 · N558AA · Doug DC982 · Fuselage Main, Plate/Skin > FUSELAGE SKIN, CRACK AT FASTENER BELOW LONGERON 4 RT & ABOVE LONGERON 3 RT AT STATION 1437. INSTALLED EXTERNAL DOUBLER IAW EA MD80-53-031801. - [SDR AALA20131001003](https://openairdocs.org/sdr/AALA20131001003.md): Skin · cracked · Oct 1, 2013 · N558AA · Doug DC982 · Fuselage Main, Plate/Skin > FS SKIN CRACKED AT FASTENER BS 1309 ABOVE LONGERON 7 LT. INSTALLED DOUBLER IAW EA MD80-53-031001. - [SDR AALA20131001002](https://openairdocs.org/sdr/AALA20131001002.md): Rivet · cracked · Oct 1, 2013 · N558AA · Doug DC982 · Fuselage Miscellaneous Structure > FOUR EACH RIVETS HAVE CRACK INDICATIONS AT STRINGER 22 LT FROM BS 190 TO 200 BELOW AIRSTAIR CUTOUT. INSTALLED DOUBLER IAW EA MD80-53-031800. - [SDR AALA20130930016](https://openairdocs.org/sdr/AALA20130930016.md): Skin · cracked · Sep 30, 2013 · N558AA · Doug DC982 · Fuselage Main, Plate/Skin > CRACK AT FASTENER BETWEEN LONGERONS 4 & 5 LT AT BS 1437. INSTALLED REPAIR DOUBLER & FILLER IAW SRM 53-04-00 FIGURE 27 & EA MD80-53-031802. - [SDR AALA20130929007](https://openairdocs.org/sdr/AALA20130929007.md): Door Frame · cracked · Sep 26, 2013 · N558AA · Doug DC982 · Fuselage Main, Structure > CABIN SIDEWALL LT AFT OVER WING EXIT DOOR CUT OUT UPPER RADIUS IS CRACKED AFT OF DOOR UPPER STRIKER. INSTALLED DOUBLER IAW EA MD80-53-031799 & SRM 53-05 FIGURE 32. - [SDR AALA20130826018](https://openairdocs.org/sdr/AALA20130826018.md): Connector · disconnected · Aug 25, 2013 · N558AA · Doug DC982 · Light System Wiring > EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. RECONNECTED PLUG UNDER SEAT 24D FOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL. - [SDR AALA20130826003](https://openairdocs.org/sdr/AALA20130826003.md): Connector · disconnected · Aug 25, 2013 · N558AA · Doug DC982 · Light System Wiring > EMERGENCY LIGHT AT SEAT 4E INOPERATIVE. RECONNECTED PLUG UNDER SEAT 4E FOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL. - [SDR AALA20130321020](https://openairdocs.org/sdr/AALA20130321020.md): Wire · damaged · Mar 19, 2013 · N558AA · Doug DC982 · Light System Wiring > SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 21 AND AFT PLUS AFT CEILING EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED WIRE L788A016 FROM PIN 7 ON BATTERY PACK B5-103, CAPPED AND STOWED. INSTALLED JUMPER WIRE FROM PIN 7 ON B5-103 BATTERY PACK TO PIN 7 ON BATTERY PACK - [SDR AALA20120425016](https://openairdocs.org/sdr/AALA20120425016.md): Skin · cracked · Apr 25, 2012 · N558AA · Doug DC982 · Fuselage Main, Plate/Skin > FUSELAGE SKIN IS CRACKED AT 2 EACH RIVETS IN THE SHEAR TIE AT STATION 1380 LONGERON 14 RIGHT ABOVE THE ENGINE PYLON. CUT OUT DAMAGED FASTENER HOLES AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM 53-01-00. - [SDR AALA20120425015](https://openairdocs.org/sdr/AALA20120425015.md): Skin · cracked · Apr 25, 2012 · N558AA · Doug DC982 · Fuselage Main, Plate/Skin > FUSELAGE CRACKED AT FASTENER ABOVE PYLON AT STATION 1380. CUT OUT DAMAGED FASTENER HOLES AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM 53-01-00. - [SDR AALA20120420003](https://openairdocs.org/sdr/AALA20120420003.md): Frame · cracked · Apr 20, 2012 · N558AA · Doug DC982 · Fuselage Main, Frame > FRAME 1418 CRACKED ALONG RADIUS AT LONGERON 2 RIGHT AREA. INSTALLED DOUBLER PER SRM 53-03-00 FIGURE 31A. - [SDR AALA20120320008](https://openairdocs.org/sdr/AALA20120320008.md): Battery Pack · discharged · Mar 18, 2012 · N558AA · Doug DC982 · Emergency Lighting > LEFT CEILING EMERGENCY LIGHTS AT ROW 21 INOPERATIVE. REPLACED BATTERY PACK FOR LEFT CEILING EMERGENCY LIGHTS AT ROW 21. OPS CHECK NORMAL. - [SDR AALA20120320007](https://openairdocs.org/sdr/AALA20120320007.md): Battery Pack · discharged · Mar 18, 2012 · N558AA · Doug DC982 · Emergency Lighting > BOTH CEILING EMERGENCY LIGHTS AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROW 20. OPS CHECK NORMAL. - [SDR AALA20120318006](https://openairdocs.org/sdr/AALA20120318006.md): Battery Pack · discharged · Mar 18, 2012 · N558AA · Doug DC982 · Emergency Lighting > LEFT CEILING EMERGENCY LIGHTS AT ROW 18 INOPERATIVE. REPLACED BATTERY PACK FOR LEFT CEILING EMERGENCY LIGHTS AT ROW 18. OPS CHECK NORMAL. - [SDR AALA20110919GSW01](https://openairdocs.org/sdr/AALA20110919GSW01.md): Connector · dirty · Sep 19, 2011 · N558AA · Doug DC982 · Engine Oil System Wiring > CLT - INFLIGHT RDU-DFW. CREW REPORTED RIGHT ENGINE HIGH OIL TEMPERATURE INDICATION. RIGHT ENGINE SHUT DOWN (SINGLE ENGINE TIME 10 MINUTES). EMERGENCY DECLARED FLIGHT DIVERTED CLT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RESERVICED OIL AND C - [SDR AALA20110706STL01](https://openairdocs.org/sdr/AALA20110706STL01.md): Generator · failed · Jul 6, 2011 · N558AA · Doug DC982 · AC Generator-Alternator > STL INFLIGHT DFW-ORD. CREW REPORTED LEFT ENGINE GENERATOR FAILED AND AUXILIARY POWER UNIT WOULD NOT START. APU START SUCCESSFUL AT 6000 FT. EMERGENCY DECLARED FLIGHT DIVERTED STL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGIN - [SDR AALA20101017TUL05](https://openairdocs.org/sdr/AALA20101017TUL05.md): Beam · corroded · Oct 17, 2010 · N558AA · Doug DC982 · Fuselage Miscellaneous Structure > AFT CARGO DOOR BEAM HAS CORROSION FROM STATIONS 1155 TO 1212. INSTALLED DOOR BEAM / DOUBLER PER AARD 53-10-00-3 AND EA MD80-53-013563. - [SDR AALA20101017TUL04](https://openairdocs.org/sdr/AALA20101017TUL04.md): Mount · corroded · Oct 17, 2010 · N558AA · Doug DC982 · Fuselage, Equipment Attach Fittings > FORWARD GALLEY MOUNT AT STATIONS 215 TO 216 SEAT TRACK NUMBER 6 IS BLENDED OUT OF LIMITS. INSTALLED NEW G2 GALLEY MOUNT ON FORWARD END OF NUMBER 6 SEAT TRACK AS PER SRM 51-30-02. - [SDR AALA20101015TUL11](https://openairdocs.org/sdr/AALA20101015TUL11.md): Floorbeam · damaged · Oct 15, 2010 · N558AA · Doug DC982 · Fuselage Main, Floor Beam > FLOOR BEAM, STATION 160 RIGHT BUTTLINE 52 AT OUTBOARD G-1 GALLEY MOUNT LOCATION HAS A.5 INCH HOLE IN AFT SIDE OF TOP TEE. INSTALLED REPAIR STRAP AT FLOORBEAM TOP TEE CAP STATION 160 RIGHT BUTTLINE 48 TO RIGHT BUTTLINE 56 PER EA MD-53-013532. - [SDR AALA20101015TUL08](https://openairdocs.org/sdr/AALA20101015TUL08.md): Diaphragm · corroded · Oct 15, 2010 · N558AA · Doug DC982 · Fuselage Miscellaneous Structure > SUB-FLOOR CORRODED STATIONS 160 TO 200 RIGHT BUTTLINES 44 TO 57. REMOVED DAMAGED AREA, INSTALLED CUSP DIAPHGRAM REPAIR, AND INSTALLED NEW FACTORY DOUBLER PER AARD 53-20-00-16. - [SDR AALA20101015TUL07](https://openairdocs.org/sdr/AALA20101015TUL07.md): Frame · cracked · Oct 15, 2010 · N558AA · Doug DC982 · Fuselage Main, Frame > STATION 1418 FRAME CRACK FORWARD SIDE AT LONGERON 2 LONG. INSTALLED DOUBLER REPAIR AND RADIUS BLOCK ON FORWARD SIDE OF STATION 1418 FRAME AT LONGERON 2 LEFT PER EA NUMBER MD80-53-011672 AND SRM 53-03-00. - [SDR AALA20101015TUL06](https://openairdocs.org/sdr/AALA20101015TUL06.md): Fitting · corroded · Oct 15, 2010 · N558AA · Doug DC982 · Fuselage, Equipment Attach Fittings > G-1 GALLEY OUTBOARD TIE-DOWN FITTING CORRODED. INSTALLED NEW TIE-DOWN FITTING PER SRM 51-30-05. - [SDR AALA20101015TUL05](https://openairdocs.org/sdr/AALA20101015TUL05.md): Fitting · corroded · Oct 15, 2010 · N558AA · Doug DC982 · Fuselage, Equipment Attach Fittings > CORROSION ON G-1 GALLEY TIE-DOWN FITTING. INSTALLED NEW TIE-DOWN FITTING PER SRM 51-30-02 AND 51-30-05. - [SDR AALA20101015TUL01](https://openairdocs.org/sdr/AALA20101015TUL01.md): Fitting · corroded · Oct 15, 2010 · N558AA · Doug DC982 · Fuselage, Equipment Attach Fittings > HEAVY CABIN CORROSION ON NUMBER 1 GALLEY TIE-DOWN FITTING NUMBER 2 OUTBOARD. INSTALLED G-1 GALLEY TIE-DOWN FITTING NUMBER 2 OUTBOARD PER SRM 51-30 05. - [SDR AALA20101014TUL06](https://openairdocs.org/sdr/AALA20101014TUL06.md): Cusp Web · cracked · Oct 14, 2010 · N558AA · Doug DC982 · Fuselage Miscellaneous Structure > CRACK IN RIGHT CUSP SHEET AT STATION 219 OUTBOARD OF NUMBER 5 SEAT TRACK. INSTALLED DOUBLER AND FILLER PER AARD 53-20-00-16. - [SDR AALA20101014TUL05](https://openairdocs.org/sdr/AALA20101014TUL05.md): Support · cracked · Oct 14, 2010 · N558AA · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK SUPPORT BELOW NUMBER 3 SEAT TRACK AT STATION 927 IS CRACKED AT BOTTOM. FABRICATED DOUBLER AND FILLER, IAW EA MD80-53-013492. INSTALLED FILLER AND DOUBLER IAW EA MD80-53-013492 AND SRM 51-30-05. - [SDR AALA20101014TUL04](https://openairdocs.org/sdr/AALA20101014TUL04.md): Pan · cracked · Oct 14, 2010 · N558AA · Doug DC982 · Cargo/Baggage Doors > AFT CARGO DOOR HAS CRACK ON LOWER INNER PAN AT LOWER STOP PAD CUTOUT. REPLACED LOWER INNER PAN PER ESO 80174. - [SDR AALA20101014TUL03](https://openairdocs.org/sdr/AALA20101014TUL03.md): Cusp Web · damaged · Oct 14, 2010 · N558AA · Doug DC982 · Fuselage Miscellaneous Structure > RIGHT CUSP CORRODED AT STATION 463. INSTALLED REPAIR DOUBLER AT STATION 463 RIGHT PER AARD 53-20-00-16. - [SDR AALA20101013TUL11](https://openairdocs.org/sdr/AALA20101013TUL11.md): Pan · cracked · Oct 13, 2010 · N558AA · Doug DC982 · Fuselage Main, Structure > CRACK IN UPPER AFT CORNER OF WINDOW PAN AT STATION 1041 LEFT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25. - [SDR AALA20101013TUL10](https://openairdocs.org/sdr/AALA20101013TUL10.md): Pan · cracked · Oct 13, 2010 · N558AA · Doug DC982 · Fuselage Main, Structure > CRACK IN LOWER FORWARD CORNER OF WINDOW PAN AT STATION 1060 RIGHT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25. - [SDR AALA20101013TUL09](https://openairdocs.org/sdr/AALA20101013TUL09.md): Pan · cracked · Oct 13, 2010 · N558AA · Doug DC982 · Fuselage Main, Structure > UPPER AFT CORNER OF WINDOW PAN CRACKED AT STATION 1250 RIGHT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25. - [SDR AALA20101013TUL08](https://openairdocs.org/sdr/AALA20101013TUL08.md): Seat Track · corroded · Oct 13, 2010 · N558AA · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON NUMBER 2 SEAT TRACK AT STATION 1201 OUT OF LIMITS. BLENDED TO REMOVE CORROSION AND INSTALLED SEAT TRACK PLUG REPAIR PER AARD 53-20-00-10. - [SDR AALA20101013TUL01](https://openairdocs.org/sdr/AALA20101013TUL01.md): Cusp Web · cracked · Oct 13, 2010 · N558AA · Doug DC982 · Fuselage Miscellaneous Structure > CABIN LEFT CUSP CRACKED STATION 671. INSTALLED DOUBLER PER AARD 53-20-00-16. - [SDR AALA20101012TUL04](https://openairdocs.org/sdr/AALA20101012TUL04.md): Pan · cracked · Oct 12, 2010 · N558AA · Doug DC982 · Fuselage Main, Structure > FORWARD LOWER CORNER OF WINDOW PAN CRACKED STATION 1136 RIGHT SIDE. CUT OUT CRACKED AREA. FABRICATED DOUBLER, TREATED, PRIMED, AND INSTALLED DOUBLER PER AARD 53-10-00-25. - [SDR AALA20101012TUL03](https://openairdocs.org/sdr/AALA20101012TUL03.md): Seat Track · corroded · Oct 11, 2010 · N558AA · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > CORROSION IN SEAT TRACK NUMBER THREE (3) AT STATION 1201. SEAT TRACK PLUG REPAIR INSTALLED PER AARD 53-20-00-10. - [SDR AALA20101012TUL02](https://openairdocs.org/sdr/AALA20101012TUL02.md): Seat Track · corroded · Oct 11, 2010 · N558AA · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > CORROSION IN SEAT TRACK NUMBER THREE(3) STATION 1175. SEAT TRACK PLUG REPAIR INSTALLED PER AARD 53-20-00-10. - [SDR AALA20101012TUL01](https://openairdocs.org/sdr/AALA20101012TUL01.md): Pan · cracked · Oct 11, 2010 · N558AA · Doug DC982 · Fuselage Main, Structure > FORWARD LOWER CORNER OF WINDOW PANE CRACKED AT STATION 160 RIGHT SIDE. DOUBLER INSTALLED PER AARD 53-10-00-25. - [SDR AALA20101011TUL19](https://openairdocs.org/sdr/AALA20101011TUL19.md): Pan · cracked · Oct 11, 2010 · N558AA · Doug DC982 · Fuselage Main, Structure > FORWARD LOWER CORNER OF WINDOW PAN CRACKED AT STATION 1136 RIGHT SIDE. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-25. - [SDR AALA20101011TUL18](https://openairdocs.org/sdr/AALA20101011TUL18.md): Attach Fitting · cracked · Oct 11, 2010 · N558AA · Doug DC982 · Leading Edge Devices > RIGHT NUMBER 5 SLAT OUTBOARD TRACK ATTACH BRACKET CRACKED. RIGHT NUMBER 5 SLAT REMOVED OUTBOARD ATTACH FITTING, LOCATED, DRILLED AND INSTALLED NEW ATTACH FITTING PER ESO 80117. - [SDR AALA20101011TUL17](https://openairdocs.org/sdr/AALA20101011TUL17.md): Attach Fitting · cracked · Oct 11, 2010 · N558AA · Doug DC982 · Leading Edge Devices > RIGHT NUMBER 5 SLAT 2ND FROM OUTBOARD TRACK ATTACH BRACKET CRACKED. RIGHT NUMBER 5 SLAT REMOVED 2ND FROM OUTBOARD END ATTACH FITTING, LOCATED, DRILLED AND INSTALLED NEW ATTACH FITTING PER ESO 80117. - [SDR AALA20101011TUL04](https://openairdocs.org/sdr/AALA20101011TUL04.md): Pan · cracked · Oct 11, 2010 · N558AA · Doug DC982 · Fuselage Main, Structure > UPPER AFT CORNER OF WINDOW PAN CRACKED AT STATION 886 LEFT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25. - [SDR AALA20101010TUL02](https://openairdocs.org/sdr/AALA20101010TUL02.md): Pan · cracked · Oct 10, 2010 · N558AA · Doug DC982 · Fuselage Main, Structure > CRACK IN UPPER FORWARD CORNER OF WINDOW PAN AT STATION 769 RIGHT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25. - [SDR AALA20101010TUL01](https://openairdocs.org/sdr/AALA20101010TUL01.md): Pan · cracked · Oct 10, 2010 · N558AA · Doug DC982 · Fuselage Main, Structure > CRACK IN FORWARD LOWER CORNER OF WINDOW PAN AT STATION 1079 RIGHT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25. - [SDR AALA20101009TUL08](https://openairdocs.org/sdr/AALA20101009TUL08.md): Pan · cracked · Oct 9, 2010 · N558AA · Doug DC982 · Fuselage Main, Structure > CRACK IN LOWER FORWARD CORNER OF WINDOW PAN AT STATION 1040 LEFT SIDE. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25. - [SDR AALA20101009TUL07](https://openairdocs.org/sdr/AALA20101009TUL07.md): Window Frame · cracked · Oct 9, 2010 · N558AA · Doug DC982 · Fuselage Main, Structure > CRACK IN UPPER AFT CORNER OF WINDOW FRAME AT STATION 886 LEFT SIDE. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25. Next page: https://openairdocs.org/aircraft/N558AA/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 = 'N558AA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N558AA/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.