# Service difficulty reports: N869AA, cancelled Aug 21, 2013

A list on [N869AA, cancelled Aug 21, 2013](https://openairdocs.org/deregistered/N869AA-2013-08-21.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 · 62 reports

- [SDR AALA20020170](https://openairdocs.org/sdr/AALA20020170.md): Connector · disconnected · Feb 24, 2002 · N869AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT SEAT TRACK LIGHTING SYSTEM ROW 6 THROUGH 16 INOPERATIVE. RECONNECTED EMERGENCY EXIT SEAT TRACK LIGHTING CONNECTOR AT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20011312](https://openairdocs.org/sdr/AALA20011312.md): Beam · corroded · Jun 26, 2001 · N869AA · Boeing 727223 · Standard Practices/Structures
  > TUL - FOUND STATION 265 LBL CORROSION ON FLOORBEAM. INSTALLED REPAIR PER ESO 11697 DATED 6/25/2001. (M)
- [SDR AALA20011314](https://openairdocs.org/sdr/AALA20011314.md): Web · cracked · Jun 26, 2001 · N869AA · Boeing 727223 · Fuselage Main, Structure
  > TUL - FOUND CRACK, AFT FACE OF FS 1183 PRESSURE BULKHEAD IN TAIL SKID WELL. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-2. (M)
- [SDR AALA20011307](https://openairdocs.org/sdr/AALA20011307.md): Skin · corroded · Jun 26, 2001 · N869AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON SKIN OUTBOARD STRINGER 26L. REPAIRED PER SRM 53-30-3 FIG 14. (M)
- [SDR AALA20011306](https://openairdocs.org/sdr/AALA20011306.md): Skin · corroded · Jun 26, 2001 · N869AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION 60 INCHES BY 30 INCHES, ON SKIN OUTBOARD OF STRINGER 26R. REPAIRED AREA PER SRM 53-30-3 FIG 14. (M)
- [SDR AALA20011302](https://openairdocs.org/sdr/AALA20011302.md): Stiffener · corroded · Jun 25, 2001 · N869AA · Boeing 727223 · Standard Practices/Structures
  > TUL - FOUND VERTICAL STIFFENER CORRODED OUTBOARD OF NR 2 LEADING EDGE FLAP ACTUATOR AT NR 2 TANK PRESSURE SWITCHES AT WFS 244. REPLACED STIFFENER PER SRM 51-10-1. (M)
- [SDR AALA20011305](https://openairdocs.org/sdr/AALA20011305.md): Stringer · corroded · Jun 23, 2001 · N869AA · Boeing 727223 · Fuselage Structure (General)
  > TUL - FOUND STRINGER 26L HAS HEAVY CORROSION AT STATION 683 TO 686, OUTBOARD SIDE OF STRINGER. INSTALLED STRINGER REPAIR PER SRM 53-10-03. (M)
- [SDR AALA20011303](https://openairdocs.org/sdr/AALA20011303.md): Stringer · corroded · Jun 22, 2001 · N869AA · Boeing 727223 · Fuselage Structure (General)
  > TUL - FOUND CORROSION 1 INCH BY 2 INCHES ON INSIDE OF STRINGER 27R. REMOVED CORROSION AND REPAIRED STRINGER PER SRM 53-10-3. (M)
- [SDR AALA20011304](https://openairdocs.org/sdr/AALA20011304.md): Web · Jun 20, 2001 · N869AA · Boeing 727223 · Standard Practices/Structures
  > TUL - FOUND RIGHT LOWER TORQUE BOX VERTICAL WEB ROUTED OUT AT LIGHTENING HOLE WITHOUT REPAIR. INSTALLED DOUBLER REPAIR ON WEB PER SRM 51-40-2 FIG 1, PAGE 1. (M)
- [SDR AALA20010468](https://openairdocs.org/sdr/AALA20010468.md): Connector · damaged · Mar 12, 2001 · N869AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 17 DIM. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR AT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20010325](https://openairdocs.org/sdr/AALA20010325.md): Fan · faulty · Feb 25, 2001 · N869AA · Boeing 727223 · Air Distribution Fan
  > IAH - FLT 1791 - EN ROUTE IAH-MIA - DETECTED LIGHT SMOKE AT FLOOR VENT NEAR ROW 27 DEF. LANDED MIA WITHOUT FURTHER INCIDENT. REPLACED GROUND VENTURI FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001168](https://openairdocs.org/sdr/AALA20001168.md): Light · defective · Jul 12, 2000 · N869AA · Boeing 727223 · Emergency Lighting
  > DFW - AFT STAIR OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED AFT OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA20001042](https://openairdocs.org/sdr/AALA20001042.md): Floorbeam · corroded · Jun 20, 2000 · N869AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - FOUND CORROSION ON FLOORBEAM AT STATION 380 BETWEEN RBL 23 AND RBL 63. INSTALLED DOUBLER ON FLOORBEAM PER SRM 53-10-08 PAGE 9B. (M)
- [SDR AALA20001043](https://openairdocs.org/sdr/AALA20001043.md): Skin · cracked · Jun 17, 2000 · N869AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - LFEC AND HFEC SHOWS CRACK IND AT LOWER ROW OF RIVETS STRINGER NR 4, STATION 451, 431, 428, 448, 427. INSTALLED REPAIR DOUBLER AT STRINGER 4 LEFT STATION 421-455 IAW SRM 53-30-3 PART 1 FIG 5. (M)
- [SDR AALA20001044](https://openairdocs.org/sdr/AALA20001044.md): Frame · corroded · Jun 17, 2000 · N869AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FOUND CORROSION ON LOWER CHORD OF RBL 40.5 FRAME BETWEEN STATION 868 AND STATION 870. INSTALLED REPAIR PER SRM 51-40-4 FIG 1 SHEET 8. (M)
- [SDR AALA20001045](https://openairdocs.org/sdr/AALA20001045.md): Lap Joint · cracked · Jun 17, 2000 · N869AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND LFEC SHOWS CRACK LOWER ROW OF RIVETS IN SKIN LAP STRINGER 4R AT STATION 585. INSTALLED EXTERNAL DOUBLER AT STATION 585 STRINGER 4R PER SRM 53-30-3. (M)
- [SDR AALA20001041](https://openairdocs.org/sdr/AALA20001041.md): Spar · corroded · Jun 15, 2000 · N869AA · Boeing 727223 · Horizontal Stabilizer, Spar/Rib
  > TUL - FOUND RIGHT HORIZONTAL CORRODED ON TOP REAR SPAR CHORD 20 INCHES FROM INBOARD END. INSTALLED DOUBELR PER ESO 11697, DATED 6-13-2000. (M)
- [SDR AALA20000941](https://openairdocs.org/sdr/AALA20000941.md): Wire · loose · Jun 9, 2000 · N869AA · Boeing 727223 · Light System Wiring
  > MIA - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHTING INOPERATIVE. SECURED WIRE CONTACT ON AFT STAIR EMERGENCY EXIT LIGHTING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA991452](https://openairdocs.org/sdr/AALA991452.md): Trim Tab · defective · Sep 26, 1999 · N869AA · Boeing 727223 · Aileron Tab Control System
  > MIA - FLT 1360 - EN ROUTE MIA/DCA AT 30,000 FEET WITH AIRSPEED OF 305 KNOTS AND ECON CLIMB THERE WAS A NOTICEABLE FLUTTER IN YOKE. INSPECTED AILERON IN-FLIGHT AND NOTICED RIGHT INBOARD AILERON FLUTTER APPROXIMATELY 3 SECONDS AFTER A TURN IN EITHER DIRECTION.
- [SDR AALA991205](https://openairdocs.org/sdr/AALA991205.md): Light · inoperative · Aug 30, 1999 · N869AA · Boeing 727223 · Emergency Lighting
  > TUL - FORWARD GALLEY 36 INCH LENGTH OF SEALED EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED SECTION OF LIGHT ASSEMBLY, FOUND BROKEN WIRE (E583053872). (M)
- [SDR AALA991257](https://openairdocs.org/sdr/AALA991257.md): Battery · dirty · Aug 23, 1999 · N869AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CONTACTS AT BATTERY PACK AND BATTERY CHARGER FOR AFT AIRSTAIR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA991190](https://openairdocs.org/sdr/AALA991190.md): Frame · corroded · Aug 9, 1999 · N869AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND BOTTOM OF FRAME CORRODED. REMOVED CORRODED SHEAR TIE AND LEG FROM LOWER FRAME STATION 600, STRINGER 27R-28R PER SRM 53-10-4 FIG 13. FABRICATED AND INSTALLED FRAME REPAIR FOR SHEAR TIE AND LEG PER SRM 53-10-4 FIG 13. (M)
- [SDR AALA991189](https://openairdocs.org/sdr/AALA991189.md): Frame · cracked · Aug 5, 1999 · N869AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FORWARD FROM WEB FOR DOOR CUTOUT HAS CRACK EXTENDING ON BOTH SIDES OF FLUSH RIVET HOLE JUST ABOVE UPPER DOOR STOP CASTING. STOP DRILLED CRACKS IAW SRM 51-10-1. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-40-2 FIG 1. (M)
- [SDR AALA991191](https://openairdocs.org/sdr/AALA991191.md): Stiffener · corroded · Aug 2, 1999 · N869AA · Boeing 727223 · Wing Miscellaneous Structure
  > TUL - FRONT SPAR VERT STIFFENER CORRODED AT TOP JUST OUTBOARD OF FUEL PRESS SWITCHES. REMOVED AND REPLACED STIFFENER WITH 6 EACH, STEEL HI-LOCKS HL62, 7 EACH STEEL HI-LOCKS HL62 PER SRM 51-10-1 AND SAME PART NR STIFFENER. (M)
- [SDR AALA991430](https://openairdocs.org/sdr/AALA991430.md): Light · defective · Jun 22, 1999 · N869AA · Boeing 727223 · Emergency Lighting
  > TPA - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT LIGHT ABOVE AFT ENTRY DOOR DOES NOT TEST. REPLACED EMERGENCY EXIT LIGHT ABOVE AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA990709](https://openairdocs.org/sdr/AALA990709.md): Actuator · leaking · May 14, 1999 · N869AA · Boeing 727223 · Landing Gear Retraction/Extension System
  > DFW - FLT 1654 - DURING APPROACH, UNABLE TO EXTEND NOSE GEAR ON FIRST ATTEMPT BUT, EXTENDED NORMALLY ON SECOND ATTEMPT. FLIGHT LANDED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NOSE GEAR UNLOCK ACTUATOR LEAKING. REPLACED NOSE GEAR UNLOCK ACTUATOR. LEA
- [SDR AALA980037](https://openairdocs.org/sdr/AALA980037.md): Light · inoperative · Jan 7, 1998 · N869AA · Boeing 727223 · Emergency Lighting
  > TUL - EMERGENCY EXIT LIGHT IN AFT LEFT GALLEY GOES DIM AFTER LIGHT IS TURNED TO ON POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT WITH SERVICEABLE UNIT NR LIG 5192 SN ON 4307. OPERATION CHECKS NORMAL. TST: 56,854.46 HOURS. CYCLES: 35,139. (X)
- [SDR AALA971734](https://openairdocs.org/sdr/AALA971734.md): Stringer · corroded · Sep 8, 1997 · N869AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - STR 27R CORRODED OUTBOARD FLANGE STA 562 - STA 564. STRINGER SECTION REPLACED PER 53-10-3, FIG 1. TST: 55,975 HOURS. CYCLES: 34,667. (X)
- [SDR AALA971732](https://openairdocs.org/sdr/AALA971732.md): Shear Tie · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - SHEAR TIES ON BOTH SIDES OF BELT FRAME STA 700 OUTBOARD STR 28R CORRODED. REMOVED AND REPLACED SHEAR TIE. TST: 55,973 HOURS. CYCLES: 34,656. (X)
- [SDR AALA971731](https://openairdocs.org/sdr/AALA971731.md): Stringer · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION ON STRINGE R27R AND STRINGER TIE CLIP AT STATION 560 FORWARD SIDE. REPLACED STRINGER SECTION PER SRM 53-10-3. INSTALLED NEW STRINGER TIE CLIP. (M)
- [SDR AALA971730](https://openairdocs.org/sdr/AALA971730.md): Skin · fuel leak · Sep 5, 1997 · N869AA · Boeing 727223 · Wing, Plate/Skin
  > TUL - FUEL LEAKING AT FASTENER IN REPAIR ABOVE THE LEFT AFT HEAT EXCHANGER STATION 810 ACM DOOR 32156. REMOVED FASTENER AND OVERSIZED TO ESO 11697 DTD 8-11-97 INSTALLED NEW FASTENER. (M)
- [SDR AALA971729](https://openairdocs.org/sdr/AALA971729.md): Stringer · broken · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER 5R BROKEN TOP AND BOTTOM FLANGE AT STATION 343. REPAIRED STRINGER 5R PER SRM 53-10-3. (M)
- [SDR AALA971728](https://openairdocs.org/sdr/AALA971728.md): Stringer · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION UNDER NUT PLATE. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-10-3 FIG PG 3-4B. (M)
- [SDR AALA971727](https://openairdocs.org/sdr/AALA971727.md): Skin · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION COMING OUT OF THE SEALANT RIGHT SIDE STRINGER 30 STATION 950E PLUS 2, STRINGER AND SKIN CORRODED. INSTALLED REPAIR IAW SRM 53-30-3 PAGE 13-14A. (M)
- [SDR AALA971726](https://openairdocs.org/sdr/AALA971726.md): Frame · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - BOTTOM FORWARD LEG, 950F, FRAME CORRODED OUTBOARD SIDE STRINGER 29R, AREA PREVIOUSLY REWORKED. REPLACED SHEAR TIE PER SRM 53-10-4. (M)
- [SDR AALA971725](https://openairdocs.org/sdr/AALA971725.md): Stringer · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION REPAIR STRINGER 29R CORRODED OUTBOARD LEFT FROM STATION 950D PLUS 17 TO 950E PLUS 3. ROUND OUT CORROSION MANUFACTURED DOUBLER IAW ESO 11697. (M)
- [SDR AALA971724](https://openairdocs.org/sdr/AALA971724.md): Stringer · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER 27R CORRODED INSIDE STATION 700-720. INSTALLED NEW SECTION OF STRINGER AND SPLICE PER SRM 53-10-3 FIG 1. (M)
- [SDR AALA971723](https://openairdocs.org/sdr/AALA971723.md): Beam · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - INTERGRANULAR CORROSION ON 1176 CHORD ANGLE RIGHT AFT LAV FLOOR AT CABLE TIE DOWN RB46. REPAIRED CHORD ANGLE 1176 PER ESO 11697 DATED 8/11/97 AT RBL 46. (M)
- [SDR AALA971722](https://openairdocs.org/sdr/AALA971722.md): Frame · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FRAME BENT DOWN AND BULGED OUT FORE AND AFT SIDES. CUT OUT DAMAGED AREA FABRICATED REPAIR DOULER IAW SRM 53-10-4 PAGE 3-6. (M)
- [SDR AALA971721](https://openairdocs.org/sdr/AALA971721.md): Keel Beam · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Keel
  > TUL - OUTBOARD STRINGER 29L AT STATION 950A PLUS 3 CORRODED. INSTALLED REPAIR IAW BOEING SB 727-53-0179 DATED JULY 13, 1989 NOTE PAGE 45. (M)
- [SDR AALA971720](https://openairdocs.org/sdr/AALA971720.md): Shear Tie · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - OUTBOARD OF STRINGER 28L STATION 500 SHEAR TIE ON FWD SIDE OF FRAME CORRODED FROM STRINGER 28L AND STRIGNER 27L. REPAIRED SHEAR TIE PER SRM 53-10-4. (M)
- [SDR AALA971719](https://openairdocs.org/sdr/AALA971719.md): Shear Tie · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON SHEAR TIE STATION 500, FORWARD SIDE OF FRAME OUTBOARD OF STRINGER 28R TO 27R. SHEAR TIE REPAIRED PER SRM 53-10-4. (M)
- [SDR AALA971718](https://openairdocs.org/sdr/AALA971718.md): Angle · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - STATION 950 CHORD ANGLE HAS HEAVY CORROSION JUST OUTBOARD OF RT STRINGER 29 KEEL BEAM EXT. REMOVED AND REPLACED RIGHT STATION 950 LOWER CHORD ANGLE PER SRM 51-10-1 PAGE 4. (M)
- [SDR AALA971717](https://openairdocs.org/sdr/AALA971717.md): Stringer · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - INSIDE OF STRINGER 28R CORRODED AT END OF SPLICE FS 488. REPAIRED STRINGER PER SRM 53-10-3. (M)
- [SDR AALA971716](https://openairdocs.org/sdr/AALA971716.md): Angle · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON CHORD ANGLE AND SPLICE RIGHT SIDE UNDER STEP 5 FROM TOP STATION 1212. REMOVED CORROSION ON CHORD ANGLE AND REMOVED AND INSTALLED FABRICATED ANGLE SPLICE RIGHT PER SRM 51-10-1. (M)
- [SDR AALA971715](https://openairdocs.org/sdr/AALA971715.md): Skin · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND SKIN BULGED, RIVET HEADS DISHED. REMOVED AND REPLACED SHEAR TIE. (M)
- [SDR AALA971714](https://openairdocs.org/sdr/AALA971714.md): Stringer · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION ON OUTBOARD SIDE OF STRINGER 26R AFT SIDE OF STATION 720D. CUT OUT DAMAGED SECTION OF STRINGER FABRICATED NEW SECTION AND INSTALLED REPAIR SPLICES PER SRM 53-10-3 FIG 1 DETAIL 1. (M)
- [SDR AALA971713](https://openairdocs.org/sdr/AALA971713.md): Skin · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON LOWER BELLY SKIN AT STATION 660-666 BETWEEN STATION 28R AND 28L. REMOVED SECTION OF SKIN AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3 FIG 1. (M)
- [SDR AALA971712](https://openairdocs.org/sdr/AALA971712.md): Floorbeam · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - FOUND CORROSION ON TOP OF FLOORBEAM STATION 380 RBL 33-38. INSTALLED DOUBLER AND FILLER PER SRM 53-10-8 PAGES C-D AT STATION 380 RBL 33-38. (M)
- [SDR AALA971711](https://openairdocs.org/sdr/AALA971711.md): Frame · corroded · Sep 5, 1997 · N869AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FOUND STATION 500 FORWARD SIDE OF FRAME BETWEEN STRINGER 27L AND 28L FRAME CORRODED, ALSO CORROSION BETWEEN STRINGER 27L AND INTERCOSTAL BETWEEN STR 27L AND 28L. REPAIRED FRAME STATION 500 FWD, STRINGER 27L - 28L PER SRM 53-10-4, REPAIRED SKIN AT INTERC

Next page: https://openairdocs.org/deregistered/N869AA-2013-08-21/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 = 'N869AA' AND deregistration_id = 'N869AA-2013-08-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N869AA-2013-08-21/reports

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