# Service difficulty reports: N866AA, cancelled Apr 24, 2018

A list on [N866AA, cancelled Apr 24, 2018](https://openairdocs.org/deregistered/N866AA-2018-04-24.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 · 59 reports

- [SDR AALA20012180](https://openairdocs.org/sdr/AALA20012180.md): Light · inoperative · Dec 26, 2001 · N866AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20011602](https://openairdocs.org/sdr/AALA20011602.md): Light · damaged · Aug 6, 2001 · N866AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR PATH LIGHTING AT ROW 6 DAMAGED. REPLACED TRACK AND LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20011146](https://openairdocs.org/sdr/AALA20011146.md): Door · cracked · May 24, 2001 · N866AA · Boeing 727223 · Doors
  > TUL - FOUND DOOR SKIN CRACKED, FORWARD EDGE ABOVE LOWER HINGE. ROUTED OUT CRACK, INSTALLED DOUBLER ESO 11697 DATED 5/24/2001. (M)
- [SDR AALA20011164](https://openairdocs.org/sdr/AALA20011164.md): Stringer · corroded · May 24, 2001 · N866AA · Boeing 727223 · Fuselage Structure (General)
  > TUL - FOUND CORROSION ON OUTBOARD SIDE STRINGER 29R, DOUBLER BULGED BELOW STRINGER 29R. REMOVED CORROSION, INSTALLED SKIN DOUBLER AND STRINGER REPAIR PER SRM 53-30-3 AND 53-10-3. (M)
- [SDR AALA20011161](https://openairdocs.org/sdr/AALA20011161.md): Skin · corroded · May 24, 2001 · N866AA · Boeing 727223 · Fuselage Structure (General)
  > TUL - FOUND CORROSION AT STRINGER END FITTING STATION 1183 STRINGER 27R. INSTALLED REPAIR DOUBLER PER ESO 11697 DATED 5/24/01. (M)
- [SDR AALA20011162](https://openairdocs.org/sdr/AALA20011162.md): Web · cracked · May 23, 2001 · N866AA · Boeing 727223 · Fuselage Structure (General)
  > TUL - FOUND NR 2 CARGO DOOR FUSELAGE CUT OUT, FORWARD DOOR JAMB WEB CRACKED AT BOTTOM DOOR STOP FITTING. INSTALLED DOUBLER PER S/B 727-53A0199. (M)
- [SDR AALA20011160](https://openairdocs.org/sdr/AALA20011160.md): Skin · cracked · May 21, 2001 · N866AA · Boeing 727223 · Empennage Structure
  > TUL - FOUND ELEVATOR LOWER SKIN CRACKED FORWARD SIDE OF SKIN 28 INCHES FROM INBOARD END. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 55-20-3 PAGE 1 FIG 1. (M)
- [SDR AALA20011159](https://openairdocs.org/sdr/AALA20011159.md): Floorbeam · corroded · May 18, 2001 · N866AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - FOUND TOP FLANGE OF FLOORBEAM CORRODED AT STATION 1070 APPROX LBL 15. INSTALLED DOUBLER PER SRM 53-10-07-02 TREATED AND PRIMED. (M)
- [SDR AALA20011158](https://openairdocs.org/sdr/AALA20011158.md): Skin · May 18, 2001 · N866AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND SKIN BULGED BROKEN, PITTED, CORRODED, PUCKERED AT LONGERON 28R STATION 1050-1130. CORROSION REMOVED, DOUBLER REPAIR INSTALLED PER SRM 53-30-3 STRINGER REPAIR INSTALLED PER SRM 53-10-3. (M)
- [SDR AALA20011154](https://openairdocs.org/sdr/AALA20011154.md): Stringer · corroded · May 18, 2001 · N866AA · Boeing 727223 · Standard Practices/Structures
  > TUL - FOUND STRINGER CORRODED AND SPLIT AT THE DRAIN MAST. INSTALLED STRINGER REPAIR AS PER SRM 53-10-3. INSTALLED NEW DRAIN MAST PAN PER SRM 51-10-1. (M)
- [SDR AALA20011163](https://openairdocs.org/sdr/AALA20011163.md): Shear Tie · corroded · May 17, 2001 · N866AA · Boeing 727223 · Fuselage Structure (General)
  > TUL - FOUND SHEAR TIE CORRODED FORWARD OF DRAIN MAST STATION 1148 STRINGER 29L. INSTALLED NEW SHEAR TIE PER SRM 51-10-1. (M)
- [SDR AALA20011157](https://openairdocs.org/sdr/AALA20011157.md): Web · corroded · May 17, 2001 · N866AA · Boeing 727223 · Fuselage Structure (General)
  > TUL - FOUND CORROSION 6 INCHES BY 1 INCH ON WEB AND PLATE RBL 16. INSTALLED FILLER AND DOUBLER AT STATION 1168-1174 RBL 16 PER 51-40-2. (M)
- [SDR AALA20010878](https://openairdocs.org/sdr/AALA20010878.md): Connector · inoperative · Apr 29, 2001 · N866AA · Boeing 727223 · Emergency Lighting
  > ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20010643](https://openairdocs.org/sdr/AALA20010643.md): Module · inoperative · Mar 28, 2001 · N866AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT ENTRY STAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001865](https://openairdocs.org/sdr/AALA20001865.md): Light · defective · Nov 12, 2000 · N866AA · Boeing 727233 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001163](https://openairdocs.org/sdr/AALA20001163.md): Light · broken · Jul 11, 2000 · N866AA · Boeing 727233 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT REAR ENTRY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT REAR ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20000711](https://openairdocs.org/sdr/AALA20000711.md): Skin · corroded · Apr 26, 2000 · N866AA · Boeing 727233 · Fuselage Main, Plate/Skin
  > TUL - FOUR EACH FASTENER HEADS DISHED ON FUSELAGE BETWEEN STA 1150 AND 1166. STR 25L TO STR 27L. REMOVED CORRODED SHEAR TIES AND REPLACED WITH NEW. CUT OUT CORRODED SKIN AND REMOVED CORROSION ON STR 27L. INSTALLED STR 27 STRAP REPAIR PER ESO 11097 DATED 4-1
- [SDR AALA20000710](https://openairdocs.org/sdr/AALA20000710.md): Stringer · corroded · Apr 20, 2000 · N866AA · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON STRINGER 30 STA 1070 - STA 1090. INSTALLED STRINGER REPAIR PER SRM 53-10-3 FIG1. (X)
- [SDR AALA20000050](https://openairdocs.org/sdr/AALA20000050.md): Line · leaking · Mar 28, 2000 · N866AA · Boeing 727233 · Hydraulic System, Main
  > PLS - FLT 625 - DURING DESCENT INTO PLS, SYSTEM 'B' HYDRAULIC FAILURE. CREW DECLARED EMERGENCY AND LANDED PLS WITHOUT INCIDENT. REPLACED PRESSURE LINE ON NR 2 PUMP. SYSTEM GROUND CHECK NORMAL OPERATION. REPLACED WITH TEMPORARY HOSE. (M)
- [SDR AALA991837](https://openairdocs.org/sdr/AALA991837.md): Relay · failed · Dec 1, 1999 · N866AA · Boeing 727233 · Emergency Lighting
  > TPA - FLT 811 - DURING FLIGHT WITH EMERGENCY EXIT LIGHT SWITCH IN ARM POSITION EMERGENCY EXIT FLOOR PATH LIGHTS ILLUMINATE. REPLACED EMERGENCY EXIT LIGHT RELAY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA990809](https://openairdocs.org/sdr/AALA990809.md): Frame · cracked · Jun 26, 1999 · N866AA · Boeing 727233 · Fuselage Main, Frame
  > TUL - FOUND WEB CRACKED STATION 303.9 STRINGER 16 INSIDE OF FRAME. INSTALLED NEW WEB PER SRM 51-40-2. (M)
- [SDR AALA990816](https://openairdocs.org/sdr/AALA990816.md): Skin · corroded · Jun 2, 1999 · N866AA · Boeing 727233 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON INTERIOR BELLY SKIN AND ON INTERCOSTAL STATION 593, STRINGER 28R AND STRINGER 27R. INSTALLED NEW INTERCOSTAL AND REPAIR DOUBLER TO SKIN PER ESO 11697 DATED 5-27-99. (M)
- [SDR AALA990808](https://openairdocs.org/sdr/AALA990808.md): Skin · corroded · Jun 2, 1999 · N866AA · Boeing 727233 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON INTERIOR BELLY SKIN BELOW INTERCOSTAL. INSTALLED REPAIR AS PER ESO 11697 DATED 5/27/99. (M)
- [SDR AALA990807](https://openairdocs.org/sdr/AALA990807.md): Skin · corroded · Jun 1, 1999 · N866AA · Boeing 727233 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON INTERIOR OF BELLY SKIN OF FORWARD CARGO OUTBOARD STRINGER 27L STATION 685. CUT OUT CORRODED SKIN TO SKIN SPLICE AND REPAIRED WITH DOUBLER PER SRM 53-30-3 FIG 12. (M)
- [SDR AALA990806](https://openairdocs.org/sdr/AALA990806.md): Keel Beam · corroded · Jun 1, 1999 · N866AA · Boeing 727233 · Fuselage Main, Keel
  > TUL - FOUND CORROSION AROUND DOM NUT ON KEEL BEAM EXTENSION STATION 720B. REMOVED CORROSION AND INSTALLED REPAIR STRAP PER ESO 11697 DATED 5/27/99. (M)
- [SDR AALA990805](https://openairdocs.org/sdr/AALA990805.md): Stringer · corroded · Jun 1, 1999 · N866AA · Boeing 727233 · Standard Practices/Structures
  > TUL - FOUND CORROSION ON STRINGER 28L AT STATION 720 PLUS 15 INCHES. REMOVED CORROSION INSTALLED REPAIR STRAP PER ESO 11697 DATED 5-27-99. (M)
- [SDR AALA990804](https://openairdocs.org/sdr/AALA990804.md): Skin · corroded · Jun 1, 1999 · N866AA · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION ON FUSE INTERIOR SKIN STATION 685, OUTBOARD STRINGER 27R. CUT OUT CORRODED SKIN TO SPLICE AND REPAIRED WITH DOUBLERS PER SRM 53-30-3. (M)
- [SDR AALA990802](https://openairdocs.org/sdr/AALA990802.md): Stringer · corroded · Jun 1, 1999 · N866AA · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION IN STRINGER 26 LEFT, STATION 690. CUT OUT DAMAGED SECTION OF STRINGER 2. INSTALLED NEW SECTION PER SRM 53-10-3 FIGURE 1. (M)
- [SDR AALA990800](https://openairdocs.org/sdr/AALA990800.md): Skin · dented · Jun 1, 1999 · N866AA · Boeing 727233 · Fuselage Main, Plate/Skin
  > TUL - FOUND DENT IN SKIN AT SECOND FRAME FROM TOP, 6 INCHES FORWARD OF AFT EDGE OF RIGHT SERVICE DOOR. CUTOUT DAMAGE AND REPAIRED PER SRM 52-00-3 FIGURE 4 BY INSTALLATION OF DOUBLER. (M)
- [SDR AALA990801](https://openairdocs.org/sdr/AALA990801.md): Stringer · corroded · May 31, 1999 · N866AA · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION AROUND RIVETS ALONG BOTTOM OF STRINGER STATION 660-700. REPAIRED PER SRM 51-10-3 FIG 1. (M)
- [SDR AALA99803](https://openairdocs.org/sdr/AALA99803.md): Stringer · corroded · May 28, 1999 · N866AA · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION IN STRINGER 27 RIGHT STATION 500-520. INSTALLED STRINGER REPAIR IAW SRM 53-10-3 FIG 1. (M)
- [SDR AALA990424](https://openairdocs.org/sdr/AALA990424.md): Wire · grounded · Mar 25, 1999 · N866AA · Boeing 727233 · Light System Wiring
  > ORD - DURING OVERNIGHT MAINTENANCE, FOUND THE LEFT AND RIGHT AFT SERVICE DOOR EMERGENCY SLIDE LIGHTS INOPERATIVE. MAINTENANCE FOUND THE RIGHT AFT EMERGENCY EXIT LIGHT RECEPTACLE WITH A WIRE GROUNDING. REPOSITIONED WIRE WHAT WAS GROUNDED. SYSTEM GROUND CHECK
- [SDR AALA980514](https://openairdocs.org/sdr/AALA980514.md): Light · defective · Mar 17, 1998 · N866AA · Boeing 727233 · Emergency Lighting
  > DFW - DURING OVERNIGHT CHECK, AFT STAIRWAY EMERGENCY LIGHT ASSEMBLY WAS INOPERATIVE. REPLACED AFT STAIRWAY EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA980013](https://openairdocs.org/sdr/AALA980013.md): Wire · broken · Jan 4, 1998 · N866AA · Boeing 727233 · Light System Wiring
  > IAH - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT FLOOR LIGHTS IN CABIN NOT OPERATING PROPERLY. REPAIRED BROKEN EMERGENCY EXIT FLOOR LIGHT WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA971248](https://openairdocs.org/sdr/AALA971248.md): Skin · corroded · Jul 10, 1997 · N866AA · Boeing 727233 · Wing, Plate/Skin
  > TUL - OUTER SKIN OF NR 2 TANK CORRODED ABOVE PRIMARY HEAT EXCHANGE LT A/C BAY, 2 EACH PLACES. REMOVED CORROSION, INSTALLED REPAIR DOUBLER PER SRM 57-30-03. TST: 55,772 HOURS. CYCLES: 34,468. (X)
- [SDR AALA971247](https://openairdocs.org/sdr/AALA971247.md): Skin · corroded · Jul 10, 1997 · N866AA · Boeing 727233 · Wing, Plate/Skin
  > TUL - OUTER SKIN OF NR 2 TANK CORRODED ABOVE PRIMARY HEAT EXCHANGE RIGHT A/C BAY IN PREVIOUSLY REWORKED AREA. REMOVED CORROSION, INSTALLED REPAIR DOUBLER PER SRM 57-30-03. TST: 55,772. CYCLES: 34,468. (X)
- [SDR AALA971246](https://openairdocs.org/sdr/AALA971246.md): Stringer · cracked · Jul 10, 1997 · N866AA · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > TUL - STRINGER CRACKED STA 344, STR 5R. REPAIRED STRINGER IAW SRM 53-10-3, FIG 3, PAGES 5, 6, 7, AND 8. TST: 55,772 HOURS. CYCLES: 34,468. (X)
- [SDR AALA971245](https://openairdocs.org/sdr/AALA971245.md): Skin · gouged · Jul 10, 1997 · N866AA · Boeing 727233 · Fuselage Main, Plate/Skin
  > TUL - GOUGE IN SKIN STA 498 ABOVE STR 27L. INSTALLED REPAIR PER SRM 53-30-3. DOUBLER, TRIPLER, INCLUDING PREVIOUS REPAIR. TST: 55,772 HOURS. CYCLES: 34,468. (X)
- [SDR AALA971244](https://openairdocs.org/sdr/AALA971244.md): Skin · cracked · Jul 10, 1997 · N866AA · Boeing 727233 · Fuselage Main, Plate/Skin
  > TUL - THREE SMALL CRACKS IN FUSELAGE SKIN COMING OUT OF RIVET HOLE AT FS 1090 AND STR 1. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER SB 727-53A0204 REV 3 DATED AUG 15, 1991. TST: 55,772 HOURS. CYCLES: 34,468. (X)
- [SDR AALA971243](https://openairdocs.org/sdr/AALA971243.md): Stringer · cracked · Jul 10, 1997 · N866AA · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > TUL - BOTH ENDS OF STR 15L BUTTING UP TO ICE LIGHT CRACKED AT FASTENER BETWEEN BS 720B AND BS 720C. BOTH ENDS CRACKED PAST FIRST FASTENER. REMOVED ENDS OF STR 15L AT ICE LIGHT AND SPLICED IN NEW STRINGERS IAW SRM 53-10-3, FIG 1, PAGE 4B. TST: 55,772 HOURS.
- [SDR AALA971241](https://openairdocs.org/sdr/AALA971241.md): Beam · corroded · Jul 10, 1997 · N866AA · Boeing 727233 · Fuselage Miscellaneous Structure
  > TUL - VERTICAL BEAM AT FS 1183, LBL 36, INBOARD SIDE, HAS.50 INCH CRACK IN AFT RADIUS AT WL 235. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SB 727-53-0192, REV 1, DATED MAY 30, 1991. TST: 55,772. CYCLES: 34,468. (X)`
- [SDR AALA971240](https://openairdocs.org/sdr/AALA971240.md): Stringer · cracked · Jul 10, 1997 · N866AA · Boeing 727233 · Wing, Longeron/Stringer
  > TUL - TOP 5TH, 6TH, AND 7TH AFT STRINGER TABS CRACKED AT THE BULKHEAD ATTACH BOLTS. STOP DRILLED AND REPAIRED PER BOEING SB 727-57A 159, 3 EACH PLACES. TST: 66,772 HOURS. CYCLES: 34,468. (X)
- [SDR AALA971239](https://openairdocs.org/sdr/AALA971239.md): Skin · corroded · Jul 10, 1997 · N866AA · Boeing 727233 · Fuselage Main, Plate/Skin
  > TUL - WEB CORRODED AT TORQUE BOX OUTBOARD ATTACH POINT CASTING, LT SIDE WEB STA 289. INSTALLED DOUBLER PER SRM 53-10-9. TST: 56,772 HOURS. CYCLES: 34,468. (X)
- [SDR AALA971238](https://openairdocs.org/sdr/AALA971238.md): Casting · corroded · Jul 10, 1997 · N866AA · Boeing 727233 · Wing, Control Surface Attach Fittings
  > TUL - INBOARD AILERON QUADRANT CASTING CORRODED AROUND LOWER BUSHING. BOTH UPPER AND LOWER. REMOVED AND REPLACED QUADRANT. CORROSION BEYOND MANUAL LIMITS. TST: 56,772 HOURS. CYCLES: 34,468. (X)
- [SDR AALA971237](https://openairdocs.org/sdr/AALA971237.md): Casting · corroded · Jul 10, 1997 · N866AA · Boeing 727233 · Fuselage Miscellaneous Structure
  > TUL - CASTING CORRODED LEFT SIDE OF STR 30 AT STA 950 ATTACH. REMOVED AND REPLACED CASTING, 51-10-1.
- [SDR AALA971235](https://openairdocs.org/sdr/AALA971235.md): Splice Plate · corroded · Jul 10, 1997 · N866AA · Boeing 727233 · Wing, Plate/Skin
  > TUL - LEFT AFT WING SPLICE PLATE AT STA 870 HAS CORROSION IN 2 OUTER HOLES OF PLATE AND LOWER WING SKIN. REPLACED SPLICE PLATE AND RE-WORKED HOLES IN LOWER WING SKIN PER ESO 11697 DATED 6-24-97. TST: 55,772 HOURS. CYCLES: 34,468. (X)
- [SDR AALA971234](https://openairdocs.org/sdr/AALA971234.md): Stringer · corroded · Jul 10, 1997 · N866AA · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON STR 22R INSULATION TIE DOWN STAND-OFF IN FRONT OF STA 720C. CUT OUT DAMAGED SECTION OF STRINGER AND INSTALLED STRINGER REPAIR PER SRM 53-10-3. TST: 55,772 HOURS. CYCLES: 34,468. (X)
- [SDR AALA971233](https://openairdocs.org/sdr/AALA971233.md): Stringer · corroded · Jul 10, 1997 · N866AA · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > TUL - STR 26R SHEAR TIES AND STRINGER CLIP CORRODED AT STA 1148. REMOVED DAMAGED AREA OF STRINGER AND SHEAR TIE, AND CLIPS. INSTALLED STRINGER REPAIR PER SRM 53-10-3, PAGE 4B. TST: 55,772 HOURS. CYCLES, 34,468. (X)
- [SDR AALA971232](https://openairdocs.org/sdr/AALA971232.md): Floor Beam · corroded · Jul 10, 1997 · N866AA · Boeing 727233 · Fuselage Main, Floor Beam
  > TUL - FLOOR BEAM CORRODED AROUND FASTENER HOLES, BOTTOM SIDE OF TOP FLANGE, STA 1110, LBL 21 INCHES TO BL ZERO INCH. REMOVED CORROSION, STA 1110 LBL 21, AND REPAIRED FLOOR BEAM IAW SRM 53-10-8, FIG 1. TREATED AND PRIMED. (X)
- [SDR AALA971231](https://openairdocs.org/sdr/AALA971231.md): Frame · corroded · Jul 10, 1997 · N866AA · Boeing 727233 · Fuselage Main, Frame
  > TUL - LOWER 3 INCHES OF BELL FRAME CORRODED STA 372 INBOARD OF STR 17R (JUST FORWARD OF FORWARD GALLEY DOOR). REMOVED CORROSION AND REPAIRED PER SRM 51-40-4, LOWER 3 INCHES OF BELL FRAME ST STA 372, STR 17R. TST: 55,772 HOURS. CYCLES, 34,468. (X)

Next page: https://openairdocs.org/deregistered/N866AA-2018-04-24/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 = 'N866AA' AND deregistration_id = 'N866AA-2018-04-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N866AA-2018-04-24/reports

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