# Service difficulty reports: N887AA, cancelled Apr 13, 2006

A list on [N887AA, cancelled Apr 13, 2006](https://openairdocs.org/deregistered/N887AA-2006-04-13.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 · 58 reports

- [SDR AALA20012063](https://openairdocs.org/sdr/AALA20012063.md): Connector · damaged · Nov 22, 2001 · N887AA · Boeing 727223 · Emergency Lighting
  > LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT SPLICE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20011960](https://openairdocs.org/sdr/AALA20011960.md): Light · inoperative · Oct 17, 2001 · N887AA · Boeing 727223 · Emergency Lighting
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT SOCKET AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20010385](https://openairdocs.org/sdr/AALA20010385.md): Splice · damaged · Mar 7, 2001 · N887AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FIRST CLASS INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT SPLICE AT FIRST CLASS AFT SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20010375](https://openairdocs.org/sdr/AALA20010375.md): Light · damaged · Feb 26, 2001 · N887AA · Boeing 727223 · Emergency Lighting
  > TUL - FOUND LIGHTS DIM, STATION 560-1030. REPLACED DAMAGED STRIP PER MM 33-60-098-4. (M)
- [SDR AALA20010374](https://openairdocs.org/sdr/AALA20010374.md): Skin · corroded · Feb 26, 2001 · N887AA · Boeing 727223 · Wing, Plate/Skin
  > TUL - FOUND LOWER WING SKIN HAS AREA OF CORROSION ABOVE LEFT PRIMARY HEAT EXCHANGER, STATION 820, LBL 25. REMOVED CORROSION, INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3. (M)
- [SDR AALA20010373](https://openairdocs.org/sdr/AALA20010373.md): Skin · cracked · Feb 24, 2001 · N887AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND FUSELAGE SKIN CRACKED AND CORRODED STATION 1130 AT STRINGER 29R. CUT OUT 2 INCH BY 3 INCH AREA OF SKIN AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3. (M)
- [SDR AALA20001976](https://openairdocs.org/sdr/AALA20001976.md): Light · inoperative · Nov 27, 2000 · N887AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, FLOOR PROXIMITY EMERGENCY EXIT LIGHT FROM SEAT 24 TO 26 INOPERATIVE. REPLACED FLOOR PROXIMITY EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001975](https://openairdocs.org/sdr/AALA20001975.md): Splice · faulty · Nov 27, 2000 · N887AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 5, 14 AND 28 INOPERATIVE. REPLACED FLOOR PROXIMITY LIGHT STRIP SPLICES AT SEAT 5, 14, AND 28. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001974](https://openairdocs.org/sdr/AALA20001974.md): Light · inoperative · Nov 27, 2000 · N887AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, FLOOR PROXIMITY EMERGENCY EXIT FROM SEAT 17 THROUGH 24 INOPERATIVE. REPLACED FLOOR PROXIMITY EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001692](https://openairdocs.org/sdr/AALA20001692.md): Light · inoperative · Oct 10, 2000 · N887AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, FORWARD CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED FORWARD CABIN EMERGENCY EXIT FLOOR LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR 2000ZZZM272](https://openairdocs.org/sdr/2000ZZZM272.md): Engine · fod · Mar 28, 2000 · N887AA · Boeing 727223 · Engine (Turbine/Turboprop)
  > DFW - FLT 1396 - JUST AT ROTATION NR 1 ENGINE EXPERIENCED SEVERE COMPERSSOR STALL. SHUT DOWN ENGINE RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED NR 1 ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION. FOD DAMAGE FROM TREAD SEPARATION OF NR 1 MLG TIRE. (M
- [SDR AALA20000355](https://openairdocs.org/sdr/AALA20000355.md): Tire · failed · Mar 28, 2000 · N887AA · Boeing 727223 · Tire
  > DFW - FLT 1396 - JUST AT ROTATION NR 1 ENGINE EXPERIENCED SEVERE COMPERSSOR STALL. SHUT DOWN ENGINE RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED NR 1 ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION. FOD DAMAGE FROM TREAD SEPARATION OF NR 1 MLG TIRE. (M
- [SDR AALA2000204](https://openairdocs.org/sdr/AALA2000204.md): Flange · damaged · Mar 28, 2000 · N887AA · Boeing 727223 · Vertical Stabilizer
  > TUL - VERTICAL STABILIZER FIN STATION 242, STRINGER 7 RIGHT. SCREW HEAD WORN DEEP INTO FLANGE. REPAIRED STRINGER IAW ECO 11697, DATED 1-21-00. OVERSIZE HOLE TO.25 INCH. FABRICATE REPAIR STRAP 17-7 PH BY.063 THK. CONDITION TH1050. CAD PLATE, PRIME, INST
- [SDR AALA2000205](https://openairdocs.org/sdr/AALA2000205.md): Flange · damaged · Mar 28, 2000 · N887AA · Boeing 727223 · Vertical Stabilizer
  > TUL - VERTICAL STABILIZER FIN STATION 242, STRINGER 7 LEFT, SCREW HEAD WORN DEEP INTO FLANGE. REPAIRED STRINGER IAW ESO 11697 DATED 1-21-00. OVERSIZE HOLE TO.25 INC. FABRICATE REPAIR STRAP, 17-7PHX.063 THK. CONDITION TH1050. CAD PLATE AND PRIME INSTALL S
- [SDR AALA2000206](https://openairdocs.org/sdr/AALA2000206.md): Skin · corroded · Mar 28, 2000 · N887AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - CORROSION ON STRINGER 27R INBOARD SIDE STATION 677-683. REMOVED AND REPLACED STRINGER CAP IN CONJUNCTION WITH SKIN REPAIR PER SRM 53-30-3. (M)
- [SDR AALA991972](https://openairdocs.org/sdr/AALA991972.md): Wire · broken · Dec 26, 1999 · N887AA · Boeing 727223 · Light System Wiring
  > DFW - DURING OVERNIGHT MAINTENANCE, ALL EMERGENCY EXIT FLOOR PATH LIGHTS IN COACH CLASS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRING AT AFT LAVATORY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA991831](https://openairdocs.org/sdr/AALA991831.md): Light · inoperative · Dec 1, 1999 · N887AA · Boeing 727223 · Emergency Lighting
  > TUL - RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT HAS ONE LAMP INOPERATIVE. REPLACED BOTH LAMPS AND OPS CHECKED EMERGENCY LIGHTING PER MM 33-50-011-2 PAGE 201. (M)
- [SDR AALA990166](https://openairdocs.org/sdr/AALA990166.md): Mount · cracked · Feb 2, 1999 · N887AA · Boeing 727223 · Leading Edge Slat Actuator
  > TUL - FOUND NR 1 SLAT ACTUATOR OUTBOARD MOUNT CRACKED (INBOARD PIECE). INSTALLED NEW SLAT ACTUATOR OUTBOARD MOUNT. (M)
- [SDR AALA990068](https://openairdocs.org/sdr/AALA990068.md): Wire · broken · Jan 1, 1999 · N887AA · Boeing 727223 · Light System Wiring
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING BROKEN WIRE IN COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA982237](https://openairdocs.org/sdr/AALA982237.md): Light · defective · Dec 27, 1998 · N887AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT CHECK, FORWARD GALLEY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD GALLEY DOOR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA981694](https://openairdocs.org/sdr/AALA981694.md): Skin · dented · Sep 11, 1998 · N887AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FUSELAGE SKIN DENTED AND PUNCTURED AT STRINGER 26L STATION 720. INSTALLED DOUBLER PER SRM 53-30-3. (M)
- [SDR AALA981693](https://openairdocs.org/sdr/AALA981693.md): Frame · damaged · Sep 11, 1998 · N887AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - LEFT FUSELAGE LOWER FAIRING ATTACH RIB FRAME AT STATION 720 DAMAGED. INSTALLED NEW RIB/FRAME. (M)
- [SDR AALA980602](https://openairdocs.org/sdr/AALA980602.md): Light · defective · Mar 25, 1998 · N887AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA980391](https://openairdocs.org/sdr/AALA980391.md): Spar Chord · corroded · Feb 20, 1998 · N887AA · Boeing 727223 · Wing Spar
  > TUL - HEAVY CORROSION ON LOWER SPAR CHORD UNDER NR 6 SLAT AT FSS 512 - FSS 515, RT WING. INSTALLED DOUBLER REPAIR PER B727 AARD/DC 57-30-00-2. ALODINED AND PRIMED AREA PER 51-10-2 AND 51-20-14 (SRM). SEALED REPAIR PER 51-30-0 FIG 4MM. TST: 51,688 HOURS.
- [SDR AALA980386](https://openairdocs.org/sdr/AALA980386.md): Skin · corroded · Feb 20, 1998 · N887AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - CORROSION UNDER STR 28R AFT OF STA 480. SKIN BULGED, RIVETS POPPED. INSTALLED SKIN DOUBLER AT STRINGER SPLICE PER SRM 53-10-3 PAGE 3, 53-30-3, FIG 3, PAGE 14A. TST: 51,688 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980357](https://openairdocs.org/sdr/AALA980357.md): Shear Tie · corroded · Feb 18, 1998 · N887AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - CORROSION ON BOTTOM OF SHEAR TIE ABOVE STR 26L AT FS 950E. INSTALLED NEW SHEAR TIE PER SRM 51-10-1. TST: 51,688 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980356](https://openairdocs.org/sdr/AALA980356.md): Skin · corroded · Feb 18, 1998 · N887AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FUSELAGE SKIN CORRODED ABOVE STR 27L AFT OF STA 500 THROUGH TO EXTERIOR OF SKIN. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3. TST: 51,688 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980355](https://openairdocs.org/sdr/AALA980355.md): Spar · corroded · Feb 18, 1998 · N887AA · Boeing 727223 · Wing Spar
  > TUL - HEAVY CORROSION ON LOWER FRONT SPAR CHORD FROM FSS 358 - FSS 370 ON BOTTOM OF CHORD RT WING. REMOVED CORROSION, TREATED AND PRIMED. INSTALLED DOUBLER REPAIR PER B727 AARD/DC 57-30-00-2. TST: 51,688 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980325](https://openairdocs.org/sdr/AALA980325.md): Skin · corroded · Feb 13, 1998 · N887AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - STA 515 - STA 520, SKIN CORRODED OUTBOARD OF STR 27L UNDER LEVELING COMPOUND. INSTALLED DOUBLER REPAIR 53-30-3 PG 105. TST: 51,688 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980324](https://openairdocs.org/sdr/AALA980324.md): Stringer · cracked · Feb 13, 1998 · N887AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - STR 15L CRACKED AFT OF WING ICE LIGHT FORWARD OF BS 720. REPAIRED STR 15L PER SRM 53-10-3. TST: 51,688 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980323](https://openairdocs.org/sdr/AALA980323.md): Skin · corroded · Feb 13, 1998 · N887AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - CORROSION OUTBOARD SIDE STR 28R AFT SIDE BS 992. REMOVED CORROSION PER SRM 51-20-0, REPAIRED EXTERNAL FUSELAGE SKIN PER SRM 53-30-3 PAGE 1. TST: 51,688 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980322](https://openairdocs.org/sdr/AALA980322.md): Sill · corroded · Feb 13, 1998 · N887AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - CORROSION AROUND FASTENER HOLE OF DOOR SILL AREA OUTBOARD OF STR 27R AT FS 950E +8. REMOVED CORROSION AROUND FASTENER HOLE PER SRM 51-10-6. REPAIRED DAMAGE PER ESO 11697 DATED 2-3-98. TST: 51,688.24 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980321](https://openairdocs.org/sdr/AALA980321.md): Stringer · cracked · Feb 13, 1998 · N887AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - STRINGER CRACKED IN RADIUS STR 4R STA 560. REPAIRED STR 4R BS 560 PER SRM 53-10-3 FIG 2. TST: 51,688 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980299](https://openairdocs.org/sdr/AALA980299.md): Tie Cap · corroded · Feb 10, 1998 · N887AA · Boeing 727223 · Horizontal Stabilizer Structure
  > TUL - CORROSION RT HORIZONTAL STABILIZER UPPER T/E HINGE CAP. THREE LOCATIONS ABOVE NR'S 4, 5, AND 7, ELEVATOR HINGE POINTS. REMOVED CORROSION AND REPAIRED PER ESO 11697 DATED 2-5-98. ALL THREE LOCATIONS. TST: 51,688 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980298](https://openairdocs.org/sdr/AALA980298.md): Stringer · corroded · Feb 10, 1998 · N887AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION INSIDE OF STR 28R AT BS 950E +2 INCHES. REMOVED CORROSION PER SRM 51-10-6, REPAIRED STR PER ESO 11697 DATED 2-2-98. TST: 51,688 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980297](https://openairdocs.org/sdr/AALA980297.md): Support · cracked · Feb 10, 1998 · N887AA · Boeing 727223 · Wing Miscellaneous Structure
  > TUL - CRACK IN VERTICAL STIFFENER ATTACH ANGLE AT FORWARD SPAR, STA 112 LEFT, OTBD OF FORWARD BOTTLE PIN. REPAIRED VERTICAL STIFFENER PER SRM 51-40-3, PAGE 2. TST: 51,688.24 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980289](https://openairdocs.org/sdr/AALA980289.md): Angle · cracked · Feb 9, 1998 · N887AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - BELL FRAME CRACKED AT OUTBOARD SIDE CHORD ANGLE AT RIVET ATTACH POINT TO STR 14R. REPLACED FAILSAFE CHORD ANGLE ATTACHED TO OUTBOARD SIDE OF BELL FRAME FRM STR 13R TO TOP OF FUEL TANK PER SRM 51-10-1. TST: 51,688 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980288](https://openairdocs.org/sdr/AALA980288.md): Floorbeam · corroded · Feb 9, 1998 · N887AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - CORROSION AROUND CLIP NUTS ON BOTTOM FLANGE OF FLOOR BEAM AT BS 1130 FROM ZERO BL TO LBL 45. REPAIRED FLOORBEAM STA 1130, LBL ZERO TO LBL 45 AS OUTLINED IN SRM 51-10-6 AND ESO 11697 DATED 2-6-98. ALODINED, TREATED, AND PRIMED. TST: 51,688 HOURS. CYCL
- [SDR AALA980287](https://openairdocs.org/sdr/AALA980287.md): Stringer · corroded · Feb 9, 1998 · N887AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - STR 25L CORRODED AFT OF 720F. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-10-3 PAGES 1-11. TST: 51,688 HOURS. CYCLES: 31,372. 9X)
- [SDR AALA980286](https://openairdocs.org/sdr/AALA980286.md): Floorbeam · corroded · Feb 9, 1998 · N887AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - CORROSION ON FLOORBEAM AT BS 1130 RBL 25. REMOVED CORROSION, INSTALLED REPAIR STRAP ON TOP OF FLOORBEAM PER ESO 11697 DATED 2-4-98 AND AARD 53-10-07-1. TST: 51,688 HOURS. CYCLES: 31,372. (X)
- [SDR AALA980285](https://openairdocs.org/sdr/AALA980285.md): Stringer · corroded · Feb 9, 1998 · N887AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON STR 24R AT STA 1166. REMOVED CORRODED STRINGER SECTION AND REPAIRED WITH STRINGER SPLICE AND DOUBLER PER SRM 53-10-3 PAGES 3-4B. TST: 51,688.24 HOURS. CYCLES: 31,370. (X)
- [SDR AALA980284](https://openairdocs.org/sdr/AALA980284.md): Skin · corroded · Feb 9, 1998 · N887AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - STA 1053 TO STA 1063, STR 30, SKIN BULGING (AS SEEN FROM OUTSIDE). CUT OUT EXISTING DAMAGE ON SKIN (ALL CORROSION REMOVED). REMOVED LIGHT CORROSION ON STRINGER, INSTALLED REPAIR DOUBLER PER SRM 53-30-3 PAGE 14. TST: 51,688.24 HOURS. CYCLES: 31,372.
- [SDR AALA0283](https://openairdocs.org/sdr/AALA0283.md): Stringer · corroded · Feb 9, 1998 · N887AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION INSIDE STR 25R AT FS 1145. INSTALLED STRINGER SPLICE REPAIR (STA 1140 TO STA 1158) PER SRM 53-10-3. TST: 51,688.24 HOURS. CYCLES: 31,372. (X)
- [SDR AALA970596](https://openairdocs.org/sdr/AALA970596.md): Skin · corroded · Mar 21, 1997 · N887AA · Boeing 727223 · Wing, Plate/Skin
  > TUL - LOWER WING EXTERNAL SURFACE CORRODED AT FS 840, RBL 32, BETWEEN S4C AND S5C, ABOVE RIGHT PRIMARY HEAT EXCHANGER. REMOVED CORROSION, REWORKED AREA PER ESO 11697, DATED 3/14/97. (M)
- [SDR AALA970595](https://openairdocs.org/sdr/AALA970595.md): Skin · corroded · Mar 21, 1997 · N887AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION BETWEEN FUSELAGE SKIN AND SHEAR TIE OUTBOARD SIDE OF STRINGER 29R AT STATION 950A. REMOVED CORROSION, TREATED AND PRIMED AREA, REMOVED SHEAR TIE AND INSTALLED NEW SHEAR TIE ON OUTBOARD SIDE OF STRINGER 29R AT STATION 950A. (M)
- [SDR AALA970594](https://openairdocs.org/sdr/AALA970594.md): Skin · corroded · Mar 21, 1997 · N887AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON FUSELAGE SKIN OUTBOARD OF STRINGER 27L AT STATION 686. INSTALLED DOUBLER PER SRM 53-30-03 AND SEALED DOUBLER PER SRM 51-20-04. (M)
- [SDR AALA970592](https://openairdocs.org/sdr/AALA970592.md): Skin · corroded · Mar 21, 1997 · N887AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON FUSELAGE SKIN BELOW LEVELING COMPOUND STATION 720C-720C PLUS 2 INCHES AND EXTERIOR SKIN BULGE STATION 720C, STRINGER 28L, 28R. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 PG 12-14A. (M)
- [SDR AALA970591](https://openairdocs.org/sdr/AALA970591.md): Skin · corroded · Mar 21, 1997 · N887AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON FUSELAGE SKIN AND TEAR STRIP OUTBOARD OF STRINGER 27R, STATION 683. REMOVED CORROSION STATION 683, STRINGER 27R. INSTALLED DOUBLER PER SRM 53-30-3. (M)
- [SDR AALA970590](https://openairdocs.org/sdr/AALA970590.md): Stringer · corroded · Mar 21, 1997 · N887AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION ON OUTBOARD CHORD OF STRINGER, BS 950-950A PLUS 5 INCHES, STRINGER 29RT. REPAIRED STRINGER PER ESO 11697, DATED 3/14/97. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER SRM 53-10-03, SB 727 53-0179 AND ESO 11697. (M)
- [SDR AALA970589](https://openairdocs.org/sdr/AALA970589.md): Frame · cracked · Mar 21, 1997 · N887AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FRAME WEB CRACKED AT BOTTOM INBOARD EDGE, STATION 783, LBL 63. INSTALLED FRAME REPAIR EPR S/B 727-53-0197. (M)

Next page: https://openairdocs.org/deregistered/N887AA-2006-04-13/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 = 'N887AA' AND deregistration_id = 'N887AA-2006-04-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N887AA-2006-04-13/reports

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