# Service difficulty reports: N726AA, cancelled Feb 27, 2002

A list on [N726AA, cancelled Feb 27, 2002](https://openairdocs.org/deregistered/N726AA-2002-02-27.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 · 56 reports

- [SDR AALA20011400](https://openairdocs.org/sdr/AALA20011400.md): Light · defective · Jul 11, 2001 · N726AA · Boeing 727227 · Emergency Lighting
  > TUL - FOUND FLOOR EMERGENCY ESCAPE PATH LIGHTING STRIP WEAK, DIM, FROM FORWARD GALLEY TO AFT GALLEY. INSTALLED NEW PATH LIGHT AND CLEAR LENS. OPS CHECK OK. (M)
- [SDR AALA20011409](https://openairdocs.org/sdr/AALA20011409.md): Shear Tie · corroded · Jul 9, 2001 · N726AA · Boeing 727227 · Fuselage Structure (General)
  > TUL - FOUND CORROSION ON SHEAR TIE BS 720A AT STRINGER 28. REMOVED CORROSION AND REMOVED DAMAGED AREA, AND REPAIRED PER SRM 53-10-04. (M)
- [SDR AALA20011402](https://openairdocs.org/sdr/AALA20011402.md): Skin · bulged · Jul 6, 2001 · N726AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - FOUND SKIN BULGING AT RIVETS, RIVETS DISHED ON SKIN LAP 24R STATION 343 TO 360. REPAIRED AREA PER SRM 53-30-4 FIG 16. (M)
- [SDR AALA20011403](https://openairdocs.org/sdr/AALA20011403.md): Skin · corroded · Jul 6, 2001 · N726AA · Boeing 727227 · Fuselage Structure (General)
  > TUL - FOUND SKIN BULGING IN AREA PREVIOUSLY WORKED, SKATE ANGLE (APPEARS TO BE RE-CORRODING) JUST ABOVE RIGHT NOSE GEAR STRUT DOOR.294.5 TO 335. SKIN BULGING AROUND REPAIR AREA FASTENERS, SIX INCHES ABOVE SKATE ANGLE STATION 295-333. REPAIRED AREA PER ESO 1
- [SDR AALA20011401](https://openairdocs.org/sdr/AALA20011401.md): Frame · dented · Jul 6, 2001 · N726AA · Boeing 727227 · Fuselage Main, Frame
  > TUL - FOUND BELT FRAME DENTED AT STATION 1050 OVER STRINGER 26L. CUT OUT DAMAGE AND INSTALLED BELT FRAME REPAIR PER 53-10-4 PAGE 1. (M)
- [SDR AALA20011404](https://openairdocs.org/sdr/AALA20011404.md): Stringer · corroded · Jul 5, 2001 · N726AA · Boeing 727227 · Fuselage Structure (General)
  > TUL - FOUND CORROSION IN BOTTOM OF STRINGER 26R. REPAIRED STRINGER PER SRM SB 53-10-3 AND BOTTOM WITH BOLTS, NUTS AND WASHERS THRU STRINGER CLIP AND STRINGER SIDES. (M)
- [SDR AALA20011405](https://openairdocs.org/sdr/AALA20011405.md): Beltframe · dented · Jul 5, 2001 · N726AA · Boeing 727227 · Fuselage Main, Frame
  > TUL - FOUND BELT FRAME DENTED STATION 1050 AT STRINGER 25R. INSTALLED BELT FRAME REPAIR PER SRM 51-40-3 PAGE 1. (M)
- [SDR AALA20011406](https://openairdocs.org/sdr/AALA20011406.md): Skin · cracked · Jul 4, 2001 · N726AA · Boeing 727227 · Fuselage Structure (General)
  > TUL - FOUND FUSELAGE SKIN CRACKED AT STATION 235 STRINGER 22L. REPAIRED CRACK PER SRM 53-30-3 FIG 3 SHEET 4, CLOSE TO EXISTING REPAIR DOUBLER. INCORPORATED ONE LARGE DOUBLER 16 INCHES BY 8 INCHES TO COVER BOTH AREAS. (M)
- [SDR AALA20011407](https://openairdocs.org/sdr/AALA20011407.md): Frame · cracked · Jul 4, 2001 · N726AA · Boeing 727227 · Fuselage Main, Frame
  > TUL - FOUND BELT FRAME CRACKED STATION 312 BETWEEN STRINGER 13, 14 RIGHT SIDE FORWARD LAVATORY. REMOVED DAMAGED SECTION. INSTALLED DOUBLER REPAIR PER RM 53-10-4. (M)
- [SDR AALA20011408](https://openairdocs.org/sdr/AALA20011408.md): Stringer · corroded · Jul 3, 2001 · N726AA · Boeing 727227 · Fuselage Structure (General)
  > TUL - FOUND CORROSION ON STRINGER 23R STATION 720E. REPLACED STRINGER SECTION 720D PLUS 10 TO 720E PLUS 10 SPLICED EPR SRM 53-10-3 FIG 1. (M)
- [SDR AALA20011399](https://openairdocs.org/sdr/AALA20011399.md): Web · cracked · Jun 30, 2001 · N726AA · Boeing 727227 · Standard Practices/Structures
  > TUL - FOUND RIGHT NOSE GEAR PRESSURE DECK HAS VISUAL INDICATION OF CRACK AT RIVET ABOVE PANEL AT STATION 203. INSTALLED DOUBLER PER SRM 51-40-2 USING.063 2024 T-3 WITH.1875 INCH MS20470D RIVETS AND SIX.1875 INCH HI-LOCKS. (M)
- [SDR AALA20010195](https://openairdocs.org/sdr/AALA20010195.md): Connector · damaged · Feb 3, 2001 · N726AA · Boeing 727227 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, FLOOR PROXIMITY EMERGENCY EXIT PATH LIGHT DIM. REPAIRED FLOOR PROXIMITY EMERGENCY EXIT PATH LIGHT CONNECTION AT SEAT 5D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001909](https://openairdocs.org/sdr/AALA20001909.md): Light · defective · Nov 18, 2000 · N726AA · Boeing 727227 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT FORWARD LAVATORY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001085](https://openairdocs.org/sdr/AALA20001085.md): Skin · dented · Jun 23, 2000 · N726AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - FOUND DENT IN FUSELAGE SKIN AFT OF STATION 1342 BULKHEAD APPROX 24 INCHES ABOVE AIRSTAIR CUT OUT. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3, FIGURE NR 1. (M)
- [SDR AALA991745](https://openairdocs.org/sdr/AALA991745.md): Light · inoperative · Nov 18, 1999 · N726AA · Boeing 727227 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, FORWARD FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED FORWARD FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA991299](https://openairdocs.org/sdr/AALA991299.md): Connector · miswired · Aug 28, 1999 · N726AA · Boeing 727227 · Emergency Lighting
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRING TO EMERGENCY EXIT FLOOR PATH LIGHTING CONNECTOR THAT WAS FOUND INSTALLED WITH REVERSE POLARITY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA991284](https://openairdocs.org/sdr/AALA991284.md): Torque Box · cracked · Aug 25, 1999 · N726AA · Boeing 727227 · Fuselage Miscellaneous Structure
  > TUL - RIGHT GALLEY DOOR UPPER HINGE TORQUE BOX AT FUSE CRACKED. INSTALLED REPAIR STRAP TO UPPER HINGE TORQUE BOX PER ESO 11697, DATED 8-24-99. (M)
- [SDR AALA991282](https://openairdocs.org/sdr/AALA991282.md): Chord · corroded · Aug 25, 1999 · N726AA · Boeing 727227 · Horizontal Stabilizer Structure
  > TUL - RIGHT HORIZONTAL STABILIZER HAS AREA OF CORROSION ON T/E UPPER CHORD JUST INBOARD OF NR 2 ELEV HINGE AT EXISTING REPAIR, OUTBOARD OF STATION 190. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER ESO 11697, DATED 8-23-99 USING SRM 55-10-6 INSTAL
- [SDR AALA991283](https://openairdocs.org/sdr/AALA991283.md): Skin · corroded · Aug 24, 1999 · N726AA · Boeing 727227 · Wing, Plate/Skin
  > TUL - UPPER L/E SPAR CAP COVER STRIP AND SEALANT BULGED UP AT NR 2 SLAT. CUT OUT SECTION OF L/E SKIN TO GAIN ACCESS TO SPAR CAP. REMOVED SURFACE CORROSION FROM SPAR CAP. TREATED, PAINTED AND INSTALLED A DOUBLER REPAIR TO L/E SKIN AS PER SRM 57-30-4. (M)
- [SDR AALA991281](https://openairdocs.org/sdr/AALA991281.md): Skin · cracked · Aug 24, 1999 · N726AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - FOUND CRACK IN FUSELAGE SKIN BELOW CAPTAINS WINDOW C-D POST (FORWARD OF NR 2 WINDOW). INSTALLED REPAIR DOUBLR ON FUSE SKIN BELOW CAPTAINS C-D WINDOW POST (FWD OF NR 2 WINDOW). INSTALLED REPAIR DOUBLER ON FUSE SKIN BELOW CAPTAINS C-D WINDOW POST PER SRM
- [SDR AALA990906](https://openairdocs.org/sdr/AALA990906.md): Light · inoperative · Jun 19, 1999 · N726AA · Boeing 727227 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY DOOR MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD GALLEY DOOR MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA990905](https://openairdocs.org/sdr/AALA990905.md): Light · inoperative · Jun 19, 1999 · N726AA · Boeing 727227 · Emergency Lighting
  > TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON CEILING AT BOTTOM OF AFT STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT CEILING LIGHT AT BOTTOM OF AFT STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA982076](https://openairdocs.org/sdr/AALA982076.md): Turbine · failed · Nov 14, 1998 · N726AA · Boeing 727227 · Turbine Section
  > MIA - FLT 1301 - AFTER TAKEOFF MIA, NR 2 ENGINE WAS SHUT DOWN BY CREW DUE TO HIGH ENGINE EXHAUST GAS TEMPERATURE AND VIBRATION. CREW DECLARED AN EMERGENCY, RETURNED AND LANDED MIA WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENGINE. SOURCE OF HIGH EGT WAS CAUSED
- [SDR AALA981203](https://openairdocs.org/sdr/AALA981203.md): Wire · broken · Jun 20, 1998 · N726AA · Boeing 727227 · Light System Wiring
  > DFW - DURING OVERNIGHT MAINTENANCE, LOWER HALF OF AFT AIR STAIR LIGHTS INOPERATIVE. REPAIRED WIRE ON LOWER HALF OF AFT STAIR LIGHTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA981180](https://openairdocs.org/sdr/AALA981180.md): Light · inoperative · Jun 15, 1998 · N726AA · Boeing 727227 · Emergency Lighting
  > ORD - DURING OVERNIGHT INSPECTION, AFT STAIR WELL EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT IN AFT STAIR WELL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA9800877](https://openairdocs.org/sdr/AALA9800877.md): Wire · failed · May 4, 1998 · N726AA · Boeing 727227 · Light System Wiring
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FORWARD CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA971882](https://openairdocs.org/sdr/AALA971882.md): Light · defective · Oct 6, 1997 · N726AA · Boeing 727227 · Emergency Lighting
  > DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OEPRATION. (X)
- [SDR AALA971643](https://openairdocs.org/sdr/AALA971643.md): Skin · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - BULGE IN SKIN STR 17L, STA 720 - STA 720E. CUT OUT CORRODED SKIN, INSTALLED DOUBLER TO FILLER PER SRM 53-30-3, FIGURE 3. TST: 67,059. CYCLES, 43,852. (X)
- [SDR AALA971642](https://openairdocs.org/sdr/AALA971642.md): Skin · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - SKIN HAS CORROSION AT STA 660 UNDER DOUBLER THAT WAS TAKEN OFF BETWEEN 28L TO 38R. BULGE IN SKIN STA 27L - STA 26L AFT OF STA 660. REPLACED SKIN, STA 680 TO STA 650, STR 26L - STR 26R PER SRM 53-30-3. TST: 67,059. CYCLES, 43,852. (X)
- [SDR AALA971641](https://openairdocs.org/sdr/AALA971641.md): Stringer · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - 2 INCHES FORWARD OF STA 720A, STR 28L CORRODED. INSTALLED NEW FACTORY STR 28L PER B723 SRM 51-10-1. TST: 67,059. CYCLES, 43,852. (X)
- [SDR AALA971640](https://openairdocs.org/sdr/AALA971640.md): Stringer · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - STR 30 CORRODED INSIDE CHANNEL FROM BS 1045 - BS 1090. INSTALLED NEW SECTION OF STRINGER STA 1010 - STA 1140 SPLICED PER 53-10-3, FIGURE 1. TST: 67,059. CYCLES, 43,852. (X)
- [SDR AALA971639](https://openairdocs.org/sdr/AALA971639.md): Stringer · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION IN CHANNEL AREA OF STR 29L FROM STA 1045 - STA 1090. INSTALLED NEW STRINGER SECTION PER 53-10-3. TST: 67,059. CYCLES, 43,852. (X)
- [SDR AALA971638](https://openairdocs.org/sdr/AALA971638.md): Stringer · worn · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - OBLONG RIVET HOLE IN STR 256, STA 710. CUT OUT DAMAGED AREA, INSTALLED STRINGER SPLICE REPAIR PER SRM 51-10-3, FIGURE 1. TST: 67,059. CYCLES, 43,852. (X)
- [SDR AALA971637](https://openairdocs.org/sdr/AALA971637.md): Floor Beam · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Floor Beam
  > TUL - FLOOR BEAM, STA 1130, HAS LIGHT CORROSION AROUND NUTPLATES, STA 1130, LBL 19 AND LBL 21. BLENDED OUT LIGHT CORROSION, BEYOND BLEND-OUT LIMITS THEN REPAIRED FLOOR BEAM PER ESO 11697 DATED 8-8-97. TST: 67,059. CYCLES, 43,852. (X)
- [SDR AALA971636](https://openairdocs.org/sdr/AALA971636.md): Skin · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - BULGE IN BELLY SKIN, TWO AREAS, STA 500 TO STA 520, STR 26R, AND STA 520 TO STA 540, STR 26R (ONE REPAIR INCORPORATING BOTH AREAS). CUT OUT DAMAGED SKIN AND STR 27R AT STA 500 TO STA 540 AND REPAIRED PER SRM 53-30-3, FIGURE 5, AND SRM 53-10-3. (BOTH IN
- [SDR AALA971635](https://openairdocs.org/sdr/AALA971635.md): Stringer · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - STR 27R CORRODED AND CRACKED AT STA 950. REMOVED DAMAGED AREA OF STR 27R. INSTALLED REPAIR SPLICE PER 51-40-4 PAGES 1 THROUGH 9. TST: 67,059. CYCLES, 43,852. (X)
- [SDR AALA971634](https://openairdocs.org/sdr/AALA971634.md): Stringer · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - STA 682, STR 27L CORRODED. INSTALLED NEW STRINGER SECTION PER SRM 53-10-3. TST: 67,059. CYCLES, 43,852. (X)
- [SDR AALA971633](https://openairdocs.org/sdr/AALA971633.md): Stringer · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - STA 683 INSIDE STR 27R HAS CORROSION. INSTALLED NEW STRINGER SECTION PER SRM 53-10-3. TST: 67,059. CYCLES, 43,852. (X)
- [SDR AALA971632](https://openairdocs.org/sdr/AALA971632.md): Shear Tie · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Miscellaneous Structure
  > TUL - STA 720F SHEAR TIE CORRODED BETWEEN STR 27 AND STR 26R. FABRICATED DOUBLER, TREATED AND PRIMED, INSTALLED WITH HI-LOCKS. REPAIR PER SRM 53-10-4, PAGE 43, FIGURE 11. TST: 62,059. CYCLES, 43,852. (X)
- [SDR AALA971631](https://openairdocs.org/sdr/AALA971631.md): Spar Chord · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Wing Spar
  > TUL - FRONT SPAR LOWER CHORD ANGLE CORRODED BELOW NR 6 SLAT ACTUATOR 2.50 INCH BY 6 INCH AREA. REMOVED CORRODED SECTION OF SPAR, REPAIRED IAW BSRM 57-10-6, FIGURE 2. TST: 67,059. CYCLES, 43,852. (X)
- [SDR AALA971630](https://openairdocs.org/sdr/AALA971630.md): Stringer · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - STA 688 INSIDE STR 26R HAS CORROSION. INSTALLED NEW STRINGER SECTION AND SPLICE PER SRM 53-10-3. TST: 67,059. CYCLES, 43,852. (X)
- [SDR AALA971629](https://openairdocs.org/sdr/AALA971629.md): Frame · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Frame
  > TUL - CORROSION ON FORWARD SIDE 720 FRAME AT SKIN ATTACH BETWEEN STR 28R AND STR 28L. INSTALLED DOUBLER AND ASSOCIATED PARTS PER 53-10-3. TST: 70,311. CYCLES: 48,592. (X)
- [SDR AALA971628](https://openairdocs.org/sdr/AALA971628.md): Skin · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - CORROSION ON SKIN STA 720 TO STA 725 BL ZERO UNDER BONDED DOUBLER. REPLACED WITH NEW FACTORY SKIN PANEL STA 680 - STA 740, STR 26R TO STR 26L PER SRM 51-10-1. TST: 67,052 HOURS. CYCLES: 43,852. (X)
- [SDR AALA971627](https://openairdocs.org/sdr/AALA971627.md): Stringer · corroded · Aug 27, 1997 · N726AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - BULGES IN SKIN STR 29R, STA 1070, WITH SEVERAL FASTENERS PULLED THROUGH SKIN. REMOVED AND REPLACED SECTION OF STRINGER WITH SRM STRINGER SPLICE PER CH 53-10-3 OF BOEING SRM. TST: 67,059. CYCLES: 43,852. (X)
- [SDR AALA971644](https://openairdocs.org/sdr/AALA971644.md): Fitting · corroded · Aug 1, 1997 · N726AA · Boeing 727227 · Fuselage Miscellaneous Structure
  > TUL - STA 740 STRINGER END FITTING CORRODED STR 27R. INSTALLED NEW STRINGER END FITTING, TREATED AND PRIMED AREA. TST: 67,059. CYCLES, 43,852. (X)
- [SDR AALA971686](https://openairdocs.org/sdr/AALA971686.md): Stringer · corroded · Jul 22, 1997 · N726AA · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON SPLICE STR 21R BETWEEN STA 440 - STA 420. INSTALLED NEW STRINGER SECTION - SPLICE. TST: 67,012. CYCLES, 43,827. (X)
- [SDR AALA961520](https://openairdocs.org/sdr/AALA961520.md): Beam · corroded · Oct 16, 1996 · N726AA · Boeing 727227 · Horizontal Stabilizer Structure
  > TUL - FOUND CORROSION UPPER HORIZONTAL TE BEAM 2 PLACES BEYOND LIMITS. CUT OUT AND BLENDED AREAS. TREATED AND PRIMED, REPAIRED PER ESO 11697 AND SRM 55-10-6 FIG 1. (M)
- [SDR AALA961519](https://openairdocs.org/sdr/AALA961519.md): Stringer · corroded · Oct 16, 1996 · N726AA · Boeing 727227 · Wing, Longeron/Stringer
  > TUL - FOUND STRINGER 22L HEAVILY CORRODED STATION 1166 TO 1183. REPAIRED STRINGER 22L, STATION 1166 TO 1183 PER SRM 53-10-3 AND STATION 1183, STRINGER 22L AND FITTING REPLACED. (M)
- [SDR AALA961517](https://openairdocs.org/sdr/AALA961517.md): Skin · corroded · Oct 16, 1996 · N726AA · Boeing 727227 · Fuselage Main, Plate/Skin
  > TUL - FOUND SKIN BULGING AND FASTENER HEAD SHEAR BELOW AFT LAV SERVICE DOOR. REPAIRED AFFECTED AREA PER ESO 11697 DATED 2 OCT 1996. (M)
- [SDR AALA961515](https://openairdocs.org/sdr/AALA961515.md): Skin · corroded · Oct 16, 1996 · N726AA · Boeing 727227 · Wing, Plate/Skin
  > TUL - FOUND LOWER WING SKIN CORRODED ABOVE AFT HEAT EXCHANGER INBOARD DUCT MOUNT ANGLE. CORROSION ON BOTH SIDES OF ANGLE APPROX 3 INCH DIAMETER. REMOVED CORROSION AND REPAIRED PER ESO 11697, DATED 10-8-96. (M)

Next page: https://openairdocs.org/deregistered/N726AA-2002-02-27/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 = 'N726AA' AND deregistration_id = 'N726AA-2002-02-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N726AA-2002-02-27/reports

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