# Service difficulty reports: N725AA, cancelled Jun 5, 2013

A list on [N725AA, cancelled Jun 5, 2013](https://openairdocs.org/deregistered/N725AA-2013-06-05.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 · 61 reports

- [SDR AALA20011691](https://openairdocs.org/sdr/AALA20011691.md): Battery Pack · discharged · Aug 24, 2001 · N725AA · Boeing 727227 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN AFT SECTION DIM. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20011300](https://openairdocs.org/sdr/AALA20011300.md): Stringer · corroded · Jun 24, 2001 · N725AA · Boeing 727227 · Standard Practices/Structures
  > TUL - FOUND STRINGER 28R IS CORRODED ON OUTBOARD SIDE. REMOVED CORRODED STRINGER AT STATION 950C PLUS 9,5 INCH AND 950 PLUS 8 INCHES. INSTALLED STRINGER FILLERS SPLICE ANGLES PER ESO 11697 DATED 6-22-2001. (M)
- [SDR AALA20011313](https://openairdocs.org/sdr/AALA20011313.md): Stiffener · corroded · Jun 21, 2001 · N725AA · Boeing 727227 · Standard Practices/Structures
  > TUL - FOUND VERTICAL STIFFENER CORRODED. REMOVED AND REPLACED STIFFENER 51-10-00. (M)
- [SDR AALA20011299](https://openairdocs.org/sdr/AALA20011299.md): Frame · cracked · Jun 21, 2001 · N725AA · Boeing 727227 · Fuselage Main, Frame
  > TUL - FOUND BELT FRAME CRACKED STATION 1110, RBL 18 TOP OF FLANGE. REPAIRED BELT FRAME BY CUTTING OUT CRACKED AREA AND INSTALLING REPAIR TO BELT FRAME PER SRM 51-40-3. (M)
- [SDR AALA20011298](https://openairdocs.org/sdr/AALA20011298.md): Stringer · corroded · Jun 21, 2001 · N725AA · Boeing 727227 · Fuselage Structure (General)
  > TUL - FOUND STRINGER 27R CORRODED AT STATION 1130 INBOARD SIDE. REMOVED DAMAGED STRINGER AND INSTALLED NEW STRINGER SECTION AND SPLICE PER SRM 53-10-3. (M)
- [SDR AALA20011297](https://openairdocs.org/sdr/AALA20011297.md): Shear Tie · corroded · Jun 21, 2001 · N725AA · Boeing 727227 · Fuselage Internal Mounting Structure
  > FOUND FORWARD SIDE OF STATION 520 SHEAR TIE HAS LIGHT CORROSION BETWEEN STRINGER 28 RL. CUT AND REMOVED CORRODED AND CRACKED FLANGE OF SHEAR TIE. FABRICATED AND INSTALLED REPAIR PART IAW SRM 53-10-4 FIG 5. (M)
- [SDR AALA20011296](https://openairdocs.org/sdr/AALA20011296.md): Shear Tie · corroded · Jun 20, 2001 · N725AA · Boeing 727227 · Fuselage Internal Mounting Structure
  > TUL - FOUND SHEAR TIE STATION 720C STRINGER 28 RIGHT CORRODED. REMOVED AND REPLACED SHEAR TIE 51-01 SRM. (M)
- [SDR AALA20011294](https://openairdocs.org/sdr/AALA20011294.md): Bulkhead · cracked · Jun 20, 2001 · N725AA · Boeing 727227 · Fuselage Main, Structure
  > TUL - FOUND CRACK IN WEB BELOW APU LOAD CONTROL VALVE, STATION 870 BULKHEAD 4 INCHES LONG. CRACK IN FS 870 BULKHEAD FORWARD SIDE AT APU CONTROL VALVE BOTTOM OUTBOARD SIDE OF CUTOUT. REPAIRED PER SRM 53-10-2 WITH DOUBLER. (M)
- [SDR AALA20011292](https://openairdocs.org/sdr/AALA20011292.md): Skin · cracked · Jun 20, 2001 · N725AA · Boeing 727227 · Fuselage Structure (General)
  > TUL - FOUND SKIN CRACKED AT RIVIT HOLE STATION 328 JUST BELOW STRINGER 206. ALSO, FOUND SKIN CRACKED AT TWO RIVITS STATION 328 JUST BELOW STRINGER 21L. CUT OUT DAMAGED SECTION OF SKIN AND INSTALLED DOUBLER PER SRM 53-30-3. (M)
- [SDR AALA20011295](https://openairdocs.org/sdr/AALA20011295.md): Light · inoperative · Jun 19, 2001 · N725AA · Boeing 727227 · Emergency Lighting
  > TUL - FOUND AFT SERVICE AND GALLEY DOORS AFT LIGHT ASSEMBLY FOR EACH HAS LAMP OUT IN LIGHT ASSEMBLIES FOR EMERGENCY EXIT. INSTALLED NEW LAMP ASSEMBLY AT AFT SIDE EACH DOOR. OPS CHECKED OK. (M)
- [SDR AALA20011293](https://openairdocs.org/sdr/AALA20011293.md): Stringer · corroded · Jun 19, 2001 · N725AA · Boeing 727227 · Fuselage Structure (General)
  > TUL - FOUND STRINGER SPLICE AT STATION 675 STRINGER 28R HAS CRACK AND IS BULGED, EMITTING CORROSION. REMOVED CORRODED SPLICE AND 5 INCHES OF STRINGER. FABRICATED AND INSTALLED NEW SPLICE IAW SRM 53-10-3. TREATED AND PRIMED ALL PARTS IAW MM 51-20-0. (M)
- [SDR AALA20011301](https://openairdocs.org/sdr/AALA20011301.md): Light · inoperative · Jun 14, 2001 · N725AA · Boeing 727227 · Emergency Lighting
  > TUL - FOUND EMERGENCY EXIT LIGHT INOPERATIVE. AFT VAULT DOOR OVERHEAD LIGHT. REPLACED EXIT LIGHT E58 NR 3934056, MM 33-50-101-2. (M)
- [SDR AALA20001607](https://openairdocs.org/sdr/AALA20001607.md): Light · damaged · Sep 29, 2000 · N725AA · Boeing 727227 · Emergency Lighting
  > DFW DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTING AFT CABIN AREA INOPERATIVE. REPLACED DAMAGED SECTION EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN AFT CABIN AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20000905](https://openairdocs.org/sdr/AALA20000905.md): Stringer · cracked · May 26, 2000 · N725AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER CORRODED AND CRACKED AT STATION 470 TO 474 STRINGER 19R. REMOVED CORROSION ON STRINGER AT STATION 470 TO 474 STRINGER 19R. INSTALLED STRINGER DOUBLER REPAIR PE SRM 53-10-3. (M)
- [SDR AALA20000901](https://openairdocs.org/sdr/AALA20000901.md): Stringer · corroded · May 24, 2000 · N725AA · Boeing 727227 · Fuselage Main, Frame
  > TUL - FOUND CORROSION ON STRINGER 28L BETWEEN STATION 680-690. INSTALLED NEW 12 INCH SECTION OF STRINGER IAW SRM 51-10-1 AND REINSTALLED EXISTING STRINGER SPLICES AT STATION 681 AND STATINO 693. (M)
- [SDR AALA20000902](https://openairdocs.org/sdr/AALA20000902.md): Skin · bulged · May 23, 2000 · N725AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - FOUND SKIN BULGING AT EDGE OF DOUBLER STATION 680 BETWEEN STRINGER 28L AND 28R. INSTALLED REPAIR DOUBLER AT STATION 671-690 STATION 28 LEFT PER SRM 53-30-3. (M)
- [SDR AALA20000900](https://openairdocs.org/sdr/AALA20000900.md): Frame · cracked · May 23, 2000 · N725AA · Boeing 727227 · Fuselage Main, Frame
  > TUL - FOUND 480 FRAME CRACKED STRINGER 26R. STOP DRILLED CRACK AND INSTALLED.040 301.5 DOUBLER PER SRM 51-40-2 DOUBLER CAD PLATED (4 INCH BY 6 INCH, 0.040 INCH 301.5 HARD DOUBLER WITH 2 ROWS OF.1875 1ST OVER HI-LOCKS AROUND CRACK). (M)
- [SDR AALA20000904](https://openairdocs.org/sdr/AALA20000904.md): Casting · cracked · May 22, 2000 · N725AA · Boeing 727227 · Fuselage Main, Structure
  > TUL - FOUND TOP AFT DOOR STOP CASTING CRACKED. REMOVED AND REPLACED CASTING SRM 51-10-1. (M)
- [SDR AALA20000903](https://openairdocs.org/sdr/AALA20000903.md): Keelbeam · cracked · May 19, 2000 · N725AA · Boeing 727227 · Fuselage Main, Keel
  > TUL - FOUND CRACK IN VERTICAL KEELBEAM ANGLE STATION 870 AT APU MOUNT BRACKET ATTACH. INSTALLED STRAP REPAIR PER SRM 53-10-2 FIG 1 PAGE 26. (M)
- [SDR AALA991295](https://openairdocs.org/sdr/AALA991295.md): Blade · failed · Aug 30, 1999 · N725AA · Boeing 727227 · Turbine Engine Compressor Section
  > IAH - FLT 1428 - AFTER TAKEOFF IAH/ORD, NR 2 ENGINE N1 DECREASED TO 50 PERCENT AND EGT INCREASED TO 600 DEGREES. VIBRATION FELT THROUGHOUT AIRCRAFT. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE. PERFOR
- [SDR AALA991081](https://openairdocs.org/sdr/AALA991081.md): Spar · corroded · Jul 21, 1999 · N725AA · Boeing 727227 · Wing Spar
  > TUL - FOUND LEFT WING, FORWARD LOWER SPAR CHORD HAS CORROSION AT WS 546 WITH PREVIOUS BLEND. INSTALLED DOUBLER PER AARD 53-30-00-02 AND ESO DATED 7/20/99. (M)
- [SDR AALA991082](https://openairdocs.org/sdr/AALA991082.md): Spar · corroded · Jul 20, 1999 · N725AA · Boeing 727227 · Wing Spar
  > TUL - LEFT FRONT SPAR HAS CORROSION ON LOWER CHORD ANGLE VERTICAL LEG. INSTALLED SPAR CHORD REPAIR DOUBLERS PER SRM 57-10-6. (M)
- [SDR AALA991080](https://openairdocs.org/sdr/AALA991080.md): Shear Tie · corroded · Jul 20, 1999 · N725AA · Boeing 727227 · Fuselage Miscellaneous Structure
  > TUL - SHEAR TIE CORRODED STATION 720A, STRINGER 28L. INSTALLED REPAIR PER SRM 53-10-4. (M)
- [SDR AALA991079](https://openairdocs.org/sdr/AALA991079.md): Casting · corroded · Jul 20, 1999 · N725AA · Boeing 727227 · Fuselage Miscellaneous Structure
  > TUL - FOUND LEFT 940 CASTING AFT FACE CORRODED. REMOVED CORROSION HFEC'D, REWORKED AREA PER ESO 11697 DATED 7-19-99 ON BACK OF E58-3048964. (M)
- [SDR AALA991078](https://openairdocs.org/sdr/AALA991078.md): Casting · corroded · Jul 20, 1999 · N725AA · Boeing 727227 · Fuselage Miscellaneous Structure
  > TUL - FOUND 940 CASTING HAS CORROSION ON FORWARD FACE AND IN BORE. REMOVED CORROSION HFEC'D, REWORKED AREA PER ESO 11697 DATED 7-19-99 OR BACK OF E58-3048962. (M)
- [SDR AALA981452](https://openairdocs.org/sdr/AALA981452.md): Web · cracked · Jul 29, 1998 · N725AA · Boeing 727227 · Fuselage Miscellaneous Structure
  > TUL - FOUND CRACK IN WEB OF CENTER WING TANK RIGHT WALL STATION 830 APPROX RBL, ABOUT 16 INCHES ABOVE FLOOR, INSIDE 3RD COMPT OF TANK. INSTALLED DOUBLER REPAIR PER ESO 11697, DATED 7/19/98. (M)
- [SDR AALA981237](https://openairdocs.org/sdr/AALA981237.md): Frame · dented · Jun 19, 1998 · N725AA · Boeing 727227 · Fuselage Main, Frame
  > TUL - BELL FRAME HAD 2 DEEP DENTS AT STATION 540 BETWEEN STRINGER 25L AND STRINGER 24L. CUTOUT DAMAGE, INSTALLED DOUBLER PER SRM 53-10-4. (M)
- [SDR AALA980365](https://openairdocs.org/sdr/AALA980365.md): Light · loose · Feb 18, 1998 · N725AA · Boeing 727227 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS OVER AFT SERVICE DOOR INOPERATIVE. RESECURED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS OVER AFT SERVICE DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA980364](https://openairdocs.org/sdr/AALA980364.md): Light · loose · Feb 18, 1998 · N725AA · Boeing 727227 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS OVER FORWARD GALLEY DOOR INOPERATIVE. RESEATED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS OVER FORWARD GALLEY DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA971735](https://openairdocs.org/sdr/AALA971735.md): Skin · damaged · Sep 8, 1997 · N725AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - FUSELAGE SKIN DAMAGED 3 AREAS. DENT, STA 950B - STA 950E STR 26R - STR 28R, APPROXIMATELY 60 INCHES LONG AND 1.375 INCHES DEEP, 6 INCHES WIDE. DENT AND GOUGE, STR 29R - STR 28R STA 950E - STA 970. FABRICATED AND INSTALLED DOUBLER PER ESO 11697 DATED 9
- [SDR AALA971378](https://openairdocs.org/sdr/AALA971378.md): Skin · corroded · Jul 30, 1997 · N725AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - FOUND SKIN BULGES AT STATION 1148 BETWEEN STRINGER 24R AND STRINGER 25R. INSTALLED REPAIR PER SRM 53-30-3 FIG 3. (M)
- [SDR AALA971377](https://openairdocs.org/sdr/AALA971377.md): Skin · corroded · Jul 30, 1997 · N725AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - FOUND FUSELAGE SKIN HAS CORROSION AT AFT SIDE OF STATION 660. REPAIRED PER SRM 53-30-3 FIG 3, EXTERNAL DOUBLER. (M)
- [SDR AALA971376](https://openairdocs.org/sdr/AALA971376.md): Beam · corroded · Jul 30, 1997 · N725AA · Boeing 727227 · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION AROUND FASTENERS ON THE BOTTOM SIDE OF BEAM STATION 790-800. INSTALLED REPAIR DOUBLER PER SRM 51-40-2. (M)
- [SDR AALA971375](https://openairdocs.org/sdr/AALA971375.md): Splice · corroded · Jul 30, 1997 · N725AA · Boeing 727227 · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON OUTBOARD AND INBOARD SIDE OF STRINGER 30 SPLICE STATION 1010. INSTALLED NEW STRINGER SPLICE. (M)
- [SDR AALA971362](https://openairdocs.org/sdr/AALA971362.md): Door Frame · corroded · Jul 29, 1997 · N725AA · Boeing 727227 · Fuselage Miscellaneous Structure
  > TUL - CORROSION ON CARGO DOOR STUB FRAME JUST AFT OF STA 950E BETWEEN STR 30 - STR 29R. REMOVED AND REPLACED CARGO DOOR STUB FRAME IAW SRM 51-10-1. TST: 66,905 HOURS. CYCLES, 43,822. (X)
- [SDR AALA971361](https://openairdocs.org/sdr/AALA971361.md): Clip · corroded · Jul 29, 1997 · N725AA · Boeing 727227 · Fuselage Miscellaneous Structure
  > TUL - TRIANGLE SHAPED CLIP AT BOTTOM FORWARD FACE OF 880 STUB FRAME HAS HEAVY CORROSION. INCLUDES TWO SMALL AREAS OF CORROSION ON 880 STUB FRAME. REMOVED AND INSTALLED REPLACEMENT CLIP AT BOTTOM FORWARD FACE OF 880 STUB FRAME, BLENDED OUT CORROSION ON 880 ST
- [SDR AALA971359](https://openairdocs.org/sdr/AALA971359.md): S Duct Skin · corroded · Jul 29, 1997 · N725AA · Boeing 727227 · Nacelle/Pylon, Plate/Skin
  > TUL - SKIN BULGING AND SEVERAL RIVET HEADS POPPED IN 1.50 INCH BY 8 INCH AREA OF LOWER S-DUCT SKIN, LEFT SIDE FORWARD OF VORTEX GENERATORS. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 54-10-3, PAGE 41B. TST: 66,905 HOURS. CYCLES, 43,822. (X)
- [SDR AALA971354](https://openairdocs.org/sdr/AALA971354.md): Frame · corroded · Jul 29, 1997 · N725AA · Boeing 727227 · Fuselage Main, Frame
  > TUL - CORROSION ON FRAME (RIGHT) INBOARD FLANGE ABOVE FLOORBOARD SUPPORT ANGLE AT FS 377. APPLIED DOUBLER IAW SRM 51-40-3, PAGES 1, 3, FIGURE 1, AND SRM 51-20-1, FIGURE 2A, PAGE 12A. TST: 66,905 HOURS. CYCLES, 43,822. (X)
- [SDR AALA971374](https://openairdocs.org/sdr/AALA971374.md): Skin · corroded · Jul 25, 1997 · N725AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - FOUND BULGED AT STATION 227, STRINGER 24L. REMOVED CORRODED SKIN. INSTALLED DOUBLER PER SRM 53-30-3 PAGE 20-23. (M)
- [SDR AALA971373](https://openairdocs.org/sdr/AALA971373.md): Stringer · corroded · Jul 25, 1997 · N725AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER 28L CORRODED AT NUT PLATE STATION 700. INSTALLED STRINGER REPAIR PER SRM 53-10-3 FIG 1. (M)
- [SDR AALA971372](https://openairdocs.org/sdr/AALA971372.md): Stringer · corroded · Jul 25, 1997 · N725AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER 28R HAS CORROSION INSIDE AT NUT PLATE STATION 700. CUT OUT CORRODED SECTION OF STRINGER AND INSTALLED SPLICE REPAIRED PER SRM 53-10-5 FIG 2. (M)
- [SDR AALA971371](https://openairdocs.org/sdr/AALA971371.md): Web · corroded · Jul 25, 1997 · N725AA · Boeing 727227 · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON WEB STATION 351, STRINGER 29 B/L CENTER. MADE DOUBLER 7075-T6 PER SRM 53-10-2 FIG 3 ALODINED, PRIMED AND INSTALLED DOUBLER PER SRM 51-40-2 FIG 1. (M)
- [SDR AALA971370](https://openairdocs.org/sdr/AALA971370.md): Stringer · corroded · Jul 25, 1997 · N725AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION AT STRINGER 28L, STATION 680. INSTALLED REPAIR IAW SRM 53-10-3 PAGE 3-5. (M)
- [SDR AALA971369](https://openairdocs.org/sdr/AALA971369.md): Stringer · corroded · Jul 25, 1997 · N725AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER 27R HAS CORROSION ON OUTBOARD SIDE BETWEEN STRINGER AND AIR DUCT. CUT OUT CORRODED SECTION OF STRINGER 27R AND INSTALLED SPLICE AND DOUBLER PER SRM 53-10-3 FIG 1. (M)
- [SDR AALA971368](https://openairdocs.org/sdr/AALA971368.md): Bell Frame · corroded · Jul 25, 1997 · N725AA · Boeing 727227 · Fuselage Main, Frame
  > TUL - FOUND CORROSION ON BELL FRAME STATION 720F AT STRINGER 27R FORWARD SIDE, ALSO A CRACK WAS FOUND DURING CLEAN UP. REMOVED CORROSION PER SRM 51-10-6 AND INSTALLED DOUBLER PER SRM 53-10-4 FIG 15 CRACK ENDED IN FASTENER. (M)
- [SDR AALA971367](https://openairdocs.org/sdr/AALA971367.md): Stringer · corroded · Jul 25, 1997 · N725AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER 27R HAS HOLE CORRODED IN IT AT STATION 740. CUT OUT CORRODED SECTION OF STRINGER AND SPLICED WITH REPAIR PER SRM 53-10-3 FIG 1. (M)
- [SDR AALA971366](https://openairdocs.org/sdr/AALA971366.md): Skin · corroded · Jul 25, 1997 · N725AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - SKIN BULGED BETWEEN STA 640 - STA 660 ALONG STR 28L. REMOVED CORRODED SECTION OF STRINGER AND SPLICED IN NEW SECTION PER SRM 53-10-3, FIGURE 1. TST: 66,905 HOURS. CYCLES, 43,822. (X)
- [SDR AALA971365](https://openairdocs.org/sdr/AALA971365.md): Skin · corroded · Jul 25, 1997 · N725AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - SKIN AND STRINGER HAVE CORROSION AT STA 720A, STR 14R. CLEANED AND TREATED STRINGER AND INSTALLED SKIN DOUBLER PER SRM 53-30-3, FIGURE 14. TST: 66,905 HOURS. CYCLES, 43,822. (X)
- [SDR AALA971364](https://openairdocs.org/sdr/AALA971364.md): Shear Tie · corroded · Jul 25, 1997 · N725AA · Boeing 727227 · Fuselage Miscellaneous Structure
  > TUL - CORROSION ON SHEAR TIE AFT SIDE FRAME STA 1130, STR 26R - STR 27R. REMOVED AND REPLACED SHEAR TIE, TREATED AND PRIMED PER 51-20-11. TST: 66,905 HOURS. CYCLES, 43,822. (X)
- [SDR AALA971363](https://openairdocs.org/sdr/AALA971363.md): Stringer · corroded · Jul 25, 1997 · N725AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION IN STR 28R JUST AFT OF STA 990. CUT OUT DAMAGED SECTION OF STR 28R. SPLICED IN NEW SECTION PER ESO 11697, DATED 7-7-97. TST: 66,905 HOURS. CYCLES, 43,822. (X)

Next page: https://openairdocs.org/deregistered/N725AA-2013-06-05/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 = 'N725AA' AND deregistration_id = 'N725AA-2013-06-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N725AA-2013-06-05/reports

---
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