# Service difficulty reports: N255AA, cancelled Oct 21, 2015

A list on [N255AA, cancelled Oct 21, 2015](https://openairdocs.org/deregistered/N255AA-2015-10-21.md).

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

- [SDR AALA20100214LGA01](https://openairdocs.org/sdr/AALA20100214LGA01.md): Battery Pack · discharged · Feb 13, 2010 · N255AA · Doug DC982 · Emergency Lighting
  > ESCAPE PATH LIGHTS FROM ROWS 3 THRU 20 INOPERATIVE. REPLACED BATTERY PACK FOR ESCAPE PATH LIGHTS FROM ROWS 3 THRU 20. OPS CHECKED NORMAL.
- [SDR AALA20090226TUL16](https://openairdocs.org/sdr/AALA20090226TUL16.md): Longeron · cracked · Feb 17, 2009 · N255AA · Doug DC982 · Fuselage Main, Longeron/Stringer
  > LONGERON CRACKED AFT OF STATION 1418 AT L2L, INSTALLED LONGERON SPLICE PER AARD 53-30-00-2.
- [SDR AALA20090226TUL15](https://openairdocs.org/sdr/AALA20090226TUL15.md): Frame · cracked · Feb 12, 2009 · N255AA · Doug DC982 · Fuselage Main, Frame
  > FRAME 1418 AFT STIFFENER CRACKED AT L2L, INSTALLED REPAIR DOUBLER PER ENGINEERING AUTHORITY MD80-53-005452.
- [SDR AALA2009021600139](https://openairdocs.org/sdr/AALA2009021600139.md): Angle · cracked · Feb 12, 2009 · N255AA · Doug DC982 · Fuselage Miscellaneous Structure
  > RIGHT FORWARD NOSE LANDING GEAR WHEEL WELL DOOR JAMB J ANGLE DOUBLER CRACKED. AREA OF DISCREPANCY IS 2 INCHES BY 3 INCHES. REPLACED NOSE LANDING GEAR DOOR BEAM J ANGLE PER SRM 53-10-00-4.
- [SDR AALA200803047](https://openairdocs.org/sdr/AALA200803047.md): Fuel Control · failed · Dec 6, 2008 · N255AA · Doug DC982 · Fuel Control/Turbine Engines
  > AUS INFLIGHT, CREW REPORTED ON SHORT FINAL APPROACH NR 1 ENGINE STOPPED PRODUCING THRUST. LANDED AUS WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA200802337](https://openairdocs.org/sdr/AALA200802337.md): Lamp · inoperative · Sep 10, 2008 · N255AA · Doug DC982 · Emergency Lighting
  > EMERGENCY LIGHT AT LT GALLEY AISLE INOPERATIVE. REPLACED LAMP. GROUND CHECKED NORMAL.
- [SDR AALA200802336](https://openairdocs.org/sdr/AALA200802336.md): Wire Harness · damaged · Sep 10, 2008 · N255AA · Doug DC982 · Light System Wiring
  > LGA EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPS.
- [SDR AALA200801378](https://openairdocs.org/sdr/AALA200801378.md): A/C Pack · dirty · May 24, 2008 · N255AA · Doug DC982 · Air Distribution System
  > ICT INFLIGHT T684/24MAY MCI TO DFW. CREW REPORTED SMOKE IN CABIN. LANDED ICT WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION. NO DEFECTS FOUND. PERFORMED AIR CONDITIONING PACK BURNOUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
- [SDR AALA200800199](https://openairdocs.org/sdr/AALA200800199.md): Lamp · inoperative · Jan 29, 2008 · N255AA · Doug DC982 · Emergency Lighting
  > LGA - EMERGENCY LIGHT AT OVERHEAD SEAT 16D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20072114](https://openairdocs.org/sdr/AALA20072114.md): Wire · pinched · Oct 25, 2007 · N255AA · Doug DC982 · Light System Wiring
  > TUL - EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED PINCHED WIRE AT FORWARD ESCAPE PATH LIGHTING PANEL FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20070231](https://openairdocs.org/sdr/AALA20070231.md): Strut · inoperative · Jan 31, 2007 · N255AA · Doug DC982 · Main Landing Gear Strut/Axle/Truck
  > ORD INFLIGHT T2329/31JAN - GEAR UNSAFE LIGHT ILLUMINATED DURING RETRACTION. CYCLED GEAR WITH NO HELP. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. DOWN AND LOCKED INDICATIONS WERE GOOD. REPLACED NOSE LANDING GEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERAT
- [SDR AALA20060583](https://openairdocs.org/sdr/AALA20060583.md): Battery Pack · inoperative · Aug 19, 2006 · N255AA · Doug DC982 · Emergency Lighting
  > DTW - EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT FORWARD GALLEY FOR INOPERATIVE EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20060259](https://openairdocs.org/sdr/AALA20060259.md): Wire Harness · inoperative · Apr 27, 2006 · N255AA · Doug DC982 · Light System Wiring
  > LGA - FLOOR LEVEL EMERGENCY LIGHT OPPOSITE FIRST CLASS LAVATORY INOPERATIVE. REPAIRED BROKEN WIRE FOR FLOOR LEVEL EMERGENCY LIGHT OPPOSITE FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20050769](https://openairdocs.org/sdr/AALA20050769.md): Battery Pack · inoperative · Nov 22, 2005 · N255AA · Doug DC982 · Emergency Lighting
  > SFO - EMERGENCY LIGHTS IN FORWARD CEILING AT ENTRY, SERVICE DOOR AND COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD CEILING AT ENTRY, SERVICE DOOR AND COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20050772](https://openairdocs.org/sdr/AALA20050772.md): Battery Pack · inoperative · Nov 22, 2005 · N255AA · Doug DC982 · Emergency Lighting
  > SFO - EMERGENCY LIGHT IN TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20050237](https://openairdocs.org/sdr/AALA20050237.md): Wire · damaged · Apr 4, 2005 · N255AA · Doug DC982 · Light System Wiring
  > DFW - ENTRY AISLE EMERGENCY LIGHT ASSEMBLY ON FORWARD GALLEY WALL NEAR FLOOR WITH DOUBLE ARROW IS INOPERATIVE. REPAIRED DAMAGED WIRES AT THE BASE OF THE WINDSCREEN FORWARD OF SEAT 3EF WITH ENVIRONMENTAL SPLICES FOR ENTRY AISLE EMERGENCY LIGHT ASSEMBLY ON FORW
- [SDR AALA20020502](https://openairdocs.org/sdr/AALA20020502.md): Wire · damaged · Jun 21, 2002 · N255AA · Doug DC982 · Light System Wiring
  > DFW - DURING OVERNIGHT MAINTENANCE, FOUND RIGHT AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED RIGHT AFT EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20020494](https://openairdocs.org/sdr/AALA20020494.md): Wire · damaged · Jun 21, 2002 · N255AA · Doug DC982 · Light System Wiring
  > DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED FORWARD EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA990841](https://openairdocs.org/sdr/AALA990841.md): Light · defective · Jun 8, 1999 · N255AA · Doug DC982 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA981566](https://openairdocs.org/sdr/AALA981566.md): Piston · defective · Aug 16, 1998 · N255AA · Doug DC982 · Landing Gear Position and Warning
  > DFW - FLT 1317 - AFTER TAKEOFF DFW NOSE GEAR WOULD NOT RETRACT. HAD NUMEROUS SPOILER AND FLAP WARNINGS IN FLIGHT. OUTFLOW VALVE CYCLED OPEN AND CLOSED SEVRAL TIMES. RECYCLED GEAR AND CIRCUIT BREAKER PER OPERATIONS MANUAL. RETURNED DFW AND LANDED WITHOUT IN
- [SDR AALA981474](https://openairdocs.org/sdr/AALA981474.md): Fuel Pump · failed · Aug 5, 1998 · N255AA · Doug DC982 · Engine Fuel Pump
  > ORD - FLT 1949 - DURING CRUISE, EN ROUTE DTW-DFW, UNABLE TO TRANSFER FUEL FROM CENTER TANK. PHASE B PLUS C CIRCUIT BREAKER WILL NOT RESET ON FORWARD CENTER FUEL PUMP. AIR INTERRUPTED AND LANDED ORD WITHOUT INCIDENT. REPLACED FORWARD CENTER FUEL PUMP AND HAR
- [SDR AALA960442](https://openairdocs.org/sdr/AALA960442.md): Angle · corroded · Mar 21, 1996 · N255AA · Doug DC982 · Fuselage Miscellaneous Structure
  > TUL - CORROSION ON ANGLE. REPLACED ANGLE. TST: 34,667.47 HRS. CYCLES: 19,822. (X)
- [SDR AALA960487](https://openairdocs.org/sdr/AALA960487.md): Shear Tie · cracked · Mar 20, 1996 · N255AA · Doug DC982 · Fuselage Miscellaneous Structure
  > TUL - SHEAR TIE CRACKED AT STA 1309 BETWEEN LONGERON 14L AND LONGERON 15L. STOP DRILLED CRACK AND BLENDED FRAME BEHIND SHEAR-TIE, TREATED AND PRIMED PER ESO 80559, 3-20-96. TST: 34,667.47 HRS. CYCLES: 19,822. (X)
- [SDR AALA960427](https://openairdocs.org/sdr/AALA960427.md): Angle · corroded · Mar 20, 1996 · N255AA · Doug DC982 · Fuselage Miscellaneous Structure
  > TUL - CORROSION AROUND NUT CLIP HOLE AT LONGERON 18L T-ANGLE AT STA 1336. REMOVED CORROSION, MADE DOUBLER AND INSTALLED PER SRM 53-01, PAGE 8, WHICH ALSO REPLACED ATTACH CLIP TO FLOORBEAM AT STA 1338. TST: 34,667.47 HRS. CYCLES: 19,822. (X)
- [SDR AALA960428](https://openairdocs.org/sdr/AALA960428.md): Shear Tie · corroded · Mar 19, 1996 · N255AA · Doug DC982 · Fuselage Miscellaneous Structure
  > TUL - INBOARD END OF SHEAR TIE CORRODED BETWEEN 29L AND 30L AT FS 1322. TRIM SHEAR TIE PER ESO 80559, TREATED AND PRIMED AREA ESO DATED 3-19-96. TST: 34,667.47 HRS. CYCLES: 19,822. (X)
- [SDR AALA960421](https://openairdocs.org/sdr/AALA960421.md): Tie Dn Track · corroded · Mar 19, 1996 · N255AA · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > TUL - CORROSION AT EACH FRAME ATTACH FASTENER THE FULL LENGTH OF TRACK, RIGHT SIDE. INSTALLED NEW TRACK, FORWARD RIGHT SECTION, STA 1003 - STA 1155. TST: 34,667.47 HRS. CYCLES: 19,822. (X)
- [SDR AALA960420](https://openairdocs.org/sdr/AALA960420.md): Tie Dn Track · corroded · Mar 19, 1996 · N255AA · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > TUL - CORROSION ON TIE-DOWN TRACK, STA 1060 TO STA 1174. INSTALLED NEW TRACK FORWARD LEFT SECTION, STA 1003 - STA 1222. TST: 34,667.47 HRS. CYCLES: 19,822. (X)
- [SDR AALA960419](https://openairdocs.org/sdr/AALA960419.md): Bell Frame · corroded · Mar 19, 1996 · N255AA · Doug DC982 · Fuselage Main, Frame
  > TUL - CORROSION ON BELL FRAME FORWARD SIDE LOWER LIP AT LONGERON 30. CUT OUT DAMAGE (CORRODED AREA) ON LOWER J-ANGLE (FRAME) INSTALLED REPAIR SPLICE AND DOUBLER PER SRM 53-03, FIGURE 2A, SHEETS 3-5, PAGES 4E-4J. TST: 34,667.47 HRS. CYCLES: 19,822. (X)
- [SDR AALA960418](https://openairdocs.org/sdr/AALA960418.md): Floor Beam · corroded · Mar 19, 1996 · N255AA · Doug DC982 · Fuselage Main, Floor Beam
  > TUL - CORROSION AROUND NUT CLIP HOLE IN FLOORBEAM. CUT OUT CORRODED AREA, INSTALLED FILLER AND DOUBLER PER SRM 53-05, FIGURE 20A. TST: 34,667.47 HRS. CYCLES: 19,822. (X)
- [SDR AALA960446](https://openairdocs.org/sdr/AALA960446.md): Floor Beam · corroded · Mar 18, 1996 · N255AA · Doug DC982 · Fuselage Main, Floor Beam
  > TUL - CORROSION AROUND NUT CLIP HOLE 2.50 FEET OUTBOARD OF INBOARD WALL, STA 1322, FLOOR BEAM RIGHT. REMOVED CORROSION AND INSTALLED STAINLESS STRAP ON FLOOR BEAM, STA 1322 PER SRM 53-05, FIGURE 20. TST: 34,667.47 HRS. CYCLES: 19,822. (X)
- [SDR AALA960412](https://openairdocs.org/sdr/AALA960412.md): Fitting · corroded · Mar 18, 1996 · N255AA · Doug DC982 · Fuselage Miscellaneous Structure
  > TUL - MID-CARGO LOWER DOOR BEAM FORWARD ANGLE FITTING CORRODED. INSTALLED NEW FORWARD ANGLE FITTING IN MID-CARGO DOORWAY. TST: 34,667.47 HRS. CYCLES: 19,822. (X)
- [SDR AALA960411](https://openairdocs.org/sdr/AALA960411.md): Fitting · corroded · Mar 18, 1996 · N255AA · Doug DC982 · Fuselage Miscellaneous Structure
  > TUL - MID-CARGO LOWER DOOR BEAM AFT ANGLE FITTING CORRODED. INSTALLED NEW ANGLE AFT END OF CARGO DOOR BEAM. TST: 34,667.47 HRS. CYCLES: 19,822. (X)
- [SDR AALA960401](https://openairdocs.org/sdr/AALA960401.md): Seat Track · corroded · Mar 14, 1996 · N255AA · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > TUL - CORROSION ON NR 3 SEAT TRACK AT STA 1307. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00. TST: 34,667.47 HRS. CYCLES: 19,822. (X)

## 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 = 'N255AA' AND deregistration_id = 'N255AA-2015-10-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N255AA-2015-10-21/reports

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