# Service difficulty reports: N868AA, cancelled Aug 21, 2012

A list on [N868AA, cancelled Aug 21, 2012](https://openairdocs.org/deregistered/N868AA-2012-08-21.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 · 53 reports

- [SDR AALA20012161](https://openairdocs.org/sdr/AALA20012161.md): Light · inoperative · Dec 14, 2001 · N868AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT AFT AIR STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20010804](https://openairdocs.org/sdr/AALA20010804.md): Module · inoperative · Apr 18, 2001 · N868AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 8 DIM. REPLACED EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA20010805](https://openairdocs.org/sdr/AALA20010805.md): Module · inoperative · Apr 18, 2001 · N868AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR DIM. REPLACED EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20010806](https://openairdocs.org/sdr/AALA20010806.md): Module · inoperative · Apr 18, 2001 · N868AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT DIM. REPLACED OVERHEAD EMERGENCY OVERHEAD EXIT LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20010644](https://openairdocs.org/sdr/AALA20010644.md): Module · inoperative · Mar 28, 2001 · N868AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN ABOVE AFT AIRSTAIR DIM. REPLACED EMERGENCY EXIT LIGHT MODULE AT AFT AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20010625](https://openairdocs.org/sdr/AALA20010625.md): Light · defective · Mar 26, 2001 · N868AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 25 DIM. REPLACED EMERGENCY EXIT LIGHT STRIP AT ROWS 25. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20010655](https://openairdocs.org/sdr/AALA20010655.md): Stringer · corroded · Mar 23, 2001 · N868AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION UNDER STRINGER 28R STATION 950F TO 970 RIVET HEADS BROKEN AND SKIN BULGING ON EXTERIOR SIDE. INSTALLED REPAIR DOUBLER IAW ESO 11697 DATED 3/20/01 AT 950F-970 STRINGER 28 RT. (M)
- [SDR AALA20010619](https://openairdocs.org/sdr/AALA20010619.md): Skin · dented · Mar 21, 2001 · N868AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND DENT AT FUSELAGE SKIN ABOVE STRINGER 24R AT STATION 340. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER SRM 53-30-3 PART 1. (M)
- [SDR AALA20010617](https://openairdocs.org/sdr/AALA20010617.md): Skin · corroded · Mar 19, 2001 · N868AA · Boeing 727223 · Wing, Plate/Skin
  > TUL - FOUND CORROSION ON LOWER CENTER SECTION WING SKIN ABOVE RIGHT PRIMARY HEAT EXCHANGER (LOWER SKIN). REMOVED CORROSION AND INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3. (M)
- [SDR AALA20010618](https://openairdocs.org/sdr/AALA20010618.md): Stringer · corroded · Mar 16, 2001 · N868AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION ON STRINGER 28R OUTBOARD SIDE STATION 677. REMOVED CORRODED SECTION OF STRINGER. INSTALLED STRINGER REPAIR PER SRM 53-10-3, AND MM 51-20-0. (M)
- [SDR AALA20001255](https://openairdocs.org/sdr/AALA20001255.md): Light · inoperative · Jul 30, 2000 · N868AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWELL EMERGENCY LIGHT INOPERATIVE. REPLACED AFT STAIRWELL EMERGENCY LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA20000596](https://openairdocs.org/sdr/AALA20000596.md): Light · inoperative · Apr 4, 2000 · N868AA · Boeing 727223 · Emergency Lighting
  > IAH - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA2000363](https://openairdocs.org/sdr/AALA2000363.md): Frame · cracked · Feb 18, 2000 · N868AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - STATION 480 FRAME CRACKED AT STRINGER 26R, CRACK IN STRINGER CUT OUT RADIUS. INSTALLED.063 INCH 7075-T6 DOUBLER 9 INCHES LONG USING TOTAL OF 34 FASTENERS PER SRM 51-40-3. (M)
- [SDR AALA2000362](https://openairdocs.org/sdr/AALA2000362.md): Stringer · corroded · Feb 18, 2000 · N868AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - SKIN AT SKIN LAP BULGED AND 2 RIVET HEADS SHEARED STATION 480 STRINGER 26R. REMOVED CORRODED SECTION OF STRINGER. INSTALLED NEW SECTION OF STRINGER AND SPLICED. INSTALLED ALL FASTENERS PER SRM 53-10-3 FIG 1. (M)
- [SDR AALA2000361](https://openairdocs.org/sdr/AALA2000361.md): Stringer · cracked · Feb 17, 2000 · N868AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER 25 RIGHT, 6 INCHES AFT OF STATION 480 CRACKED. REPAIRED STRINGER 25 RIGHT STATION 480 PER SRM 53-10-3 FIGURE 2 DETAIL II. (M)
- [SDR AALA2000360](https://openairdocs.org/sdr/AALA2000360.md): Beam · corroded · Feb 15, 2000 · N868AA · Boeing 727223 · Horizontal Stabilizer Structure
  > TUL - FOUND CORROSION ON TOP OF T/E BEAM RIGHT HORIZ STAB 2ND FROM OUTBOARD ELEV HINGE. INSTALLED DOUBLER REPAIR PER ESO 11697, DATED 2-14-00. (M)
- [SDR AALA990553](https://openairdocs.org/sdr/AALA990553.md): Panel · corroded · Apr 21, 1999 · N868AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - AFT LAVATORY SERVICE PANEL BULGING AT BOTTOM. REPAIRED SECTION OF SKIN DOUBLER PER SRM 53-30-3. INSTALLED NEW LAVATORY PAN TRIPLER. REINSTALLED LAVATORY PAN DUMP LINE, FILL LINES AND CABLES. (M)
- [SDR AALA990551](https://openairdocs.org/sdr/AALA990551.md): Shear Tie · corroded · Apr 21, 1999 · N868AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND CORRODED SHEAR TIE STATION 1148 STRIGNER 26L. REPLACED SHEAR TIE. (M)
- [SDR AALA990552](https://openairdocs.org/sdr/AALA990552.md): Stringer · corroded · Apr 16, 1999 · N868AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION ON STRINGER 28L AT BS 525, REMOVED CORROSION MADE STRINGER OUT OF LIMITS. INSTALLED STRINGER REPAIR AS PER SRM 53-10-3 FIG 1. (M)
- [SDR AALA981926](https://openairdocs.org/sdr/AALA981926.md): Nlg · lack of lube · Oct 22, 1998 · N868AA · Boeing 727223 · Landing Gear Retraction/Extension System
  > DFW - FLT 1607 - DURING APPROACH DFW, NOSE LANDING GEAR HUNG UP MOMENTARILY BEFORE EXTENDING NORMALLY. FLIGHT LANDED DFW WITHOUT FURTHER INCIDENT. NOSE LANDING GEAR WAS INSPECTED, LUBRICATED, AND SWUNG SEVERAL TIMES WITH NORMAL OPERATION. SYSTEM GROUND CHEC
- [SDR AALA981118](https://openairdocs.org/sdr/AALA981118.md): Seal · stuck · Jun 3, 1998 · N868AA · Boeing 727223 · Landing Gear Doors
  > ORD - FLT 1523 - DURING APPROACH, WHEN GEAR HANDLE MOVED TO DOWN POSITION BOTH MAIN LANDING GEARS EXTENDED NORMALLY. NOSE GEAR REMAINED RETRACTED FOR SEVERAL SECONDS MORE FOLLOWED BY A LOUD BANG AND THEN NORMAL NOSE GEAR EXTENSION. LANDED ORD WITHOUT INCIDEN
- [SDR AALA980958](https://openairdocs.org/sdr/AALA980958.md): Floorbeam · corroded · May 11, 1998 · N868AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - FOUND CORROSION ON CABIN FLOORBEAM LOWER FLANGE, WHERE CEILING PANEL OF CARGO COMP IS SECURED. REMOVED CORROSION, ALODINED AND PAINTED, INSTALLED SUPPORT ANGLES AND STRAP PER SRM 53-10-8 ON LOWER FLOORBEAM AT STATION 1070, BL 0 TO LBL 48. (M)
- [SDR AALA971450](https://openairdocs.org/sdr/AALA971450.md): Switch · defective · Aug 11, 1997 · N868AA · Boeing 727223 · Landing Gear Position and Warning
  > DFW - FLT 781 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR INDICATED UNSAFE WITH NORMAL NOSE GEAR DOOR INDICATION. RECYCLED LANDING GEAR AND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT LANDED DFW WITHOUT INCIDENT. LUBRICATED LANDI
- [SDR AALA971125](https://openairdocs.org/sdr/AALA971125.md): Angle · corroded · Jun 20, 1997 · N868AA · Boeing 727223 · Leading Edge Devices
  > TUL - NR 5 SLAT ACTUATOR INBOARD AND OUTBOARD ATTACH ANGLES CORRODED. REMOVED AND REPLACED BOTH ANGLES. TST: 55,431 HOURS. CYCLES: 34,330. (X)
- [SDR AALA971118](https://openairdocs.org/sdr/AALA971118.md): Firewall · cracked · Jun 19, 1997 · N868AA · Boeing 727223 · Nacelle/Pylon, Bulkhead/Firewall
  > TUL - FIREWALL CRACKED 2 INCHES LONG FORWARD FLANGE FORWARD ENGINE MOUNT. INSTALLED REPAIR PER ESO 11697 DATED 5-22-97. TST: 55,431 HOURS. 34,330. (X)
- [SDR AALA971117](https://openairdocs.org/sdr/AALA971117.md): Gear Beam · corroded · Jun 19, 1997 · N868AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - CORROSION ON AFT SIDE OF GEAR BEAM AFT BORE AT THE H-LINK ATTACH PIN HOLE. LOCALLY BLENDED HOLE, REMOVED CORROSION, COUNTERSUNK THE BORE AND MF6D BUSHING. INSTALLED WET PER ESO 11697 STD 5-29-97 AND BOEING M56 AAL TUL 93-0603TR AND 0660RR. TST: 55,43
- [SDR AALA971115](https://openairdocs.org/sdr/AALA971115.md): Casting · corroded · Jun 19, 1997 · N868AA · Boeing 727223 · Ailerons
  > TUL - WEB BULGING INBOARD OF INBOARD AILERON QUADRANT ATTACH CASTING. REMOVED AND INSTALLED SERVICEABLE AILERON QUAD CASTING. TST: 55,431 HOURS. CYCLES, 34,330. (X)
- [SDR AALA971114](https://openairdocs.org/sdr/AALA971114.md): Stringer · cracked · Jun 19, 1997 · N868AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - NR 1 TANK STRINGER CRACKED WS 629 TOP SECOND FROM AFT WEB. NR 1 TANK STRINGER CRACKED WS 629 THIRD FROM AFT WEB. STOP DRILLED CRACK AND INSTALLED REPAIR PER SB 727-57A159. CRACK ENDED AT FASTENER HOLE. INSTALLED REPAIR PER SB 727-57A159. TST: 55,43
- [SDR AALA971113](https://openairdocs.org/sdr/AALA971113.md): Skin · dented · Jun 19, 1997 · N868AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL -.5 INCH BY.042 INCH DENT AT FS 360 BETWEEN STR 5 AND STR 6 RIGHT ABOVE AND AFT OF FORWARD ENTRY DOOR. INSTALLED PERMANENT REPAIR PER SRM 53-30-3, FIG 1. TST: 55,431 HOURS. CYCLES, 34,330. (X)
- [SDR AALA971112](https://openairdocs.org/sdr/AALA971112.md): Trunnion Sleeve · corroded · Jun 19, 1997 · N868AA · Boeing 727223 · Fuselage, Landing Gear Attach Fittings
  > TUL - LEFT AND RIGHT GEAR AFT TRUNNION SLEEVES CORRODED. REMOVED BOTH SLEEVES, CLEANED AND TREATED THE GEAR BEAM BORES, AND INSTALLED NEW SLEEVES PER AAMPSM PAGES 16-21 AND PAGES 33 AND 34. TST: 55,431 HOURS. CYCLES, 34,330. (X)
- [SDR AALA971111](https://openairdocs.org/sdr/AALA971111.md): Bulkhead Beam · cracked · Jun 19, 1997 · N868AA · Boeing 727223 · Fuselage Main, Bulkhead
  > TUL - RIGHT AFT PRESSURE BULKHEAD CENTER SUPPORT BEAM CRACKED AT THE FASTENER HOLES 28 INCHES ABOVE THE FLOOR. STOP DRILLED THE CRACKS AND INSTALLED DOUBLER KIT PER SB 727-53-0192, IT NR 65C34406-13. TST: 55,431 HOURS. CYCLES, 34,330. (X)
- [SDR AALA971110](https://openairdocs.org/sdr/AALA971110.md): Skin · cracked · Jun 19, 1997 · N868AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - SKIN CRACKED AT FS 1097 LT AND RT RIVETS STR 1. CUT OUT DAMAGED SKIN AND REPAIRED PER SB 727-53A0204. TST: 55,431 HOURS. CYCLES, 34,330. (X)
- [SDR AALA971109](https://openairdocs.org/sdr/AALA971109.md): Stiffener · cracked · Jun 19, 1997 · N868AA · Boeing 727223 · Wing Miscellaneous Structure
  > TUL - UPPER SPAR STIFFENER NR 9 CRACKED, STA 656.50, LEFT WING. CRACK ENDED IN FASTENER HOLE. INSTALLED REPAIR PER BOEING SB 727-57A 159. TST: 55,431 HOURS. CYCLES, 34,330. (X)
- [SDR AALA971108](https://openairdocs.org/sdr/AALA971108.md): Shear Tie · corroded · Jun 19, 1997 · N868AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - SHEAR TIE CORRODED STA 700 BETWEEN STR 25L AND STR 26L. REMOVED AND REPLACED SHEAR TIE PER 53-10-4. TST: 55,431 HOURS. CYCLES, 34,330. (X)
- [SDR AALA971107](https://openairdocs.org/sdr/AALA971107.md): Stringer · corroded · Jun 19, 1997 · N868AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - STA 562 INSIDE STR 27L CORRODED. INSTALLED STRINGER REPAIR PER SRM 53-10-3, FIG 1. TST: 55,431 HOURS. CYCLES, 34,330. (X)
- [SDR AALA971106](https://openairdocs.org/sdr/AALA971106.md): Floor Beam · corroded · Jun 19, 1997 · N868AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - CORROSION ON FLOOR BEAM STA 380 RBL 14 TO RBL 64. REMOVED CORROSION, INSTALLED REPAIR PER SRM 53-10-8. TST: 55,431 HOURS. CYCLES, 34,330. (X)
- [SDR AALA971102](https://openairdocs.org/sdr/AALA971102.md): Floor Beam · corroded · Jun 19, 1997 · N868AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - FLOOR BEAM CORRODED BETWEEN LT INBOARD AND CENTER GALLEY TRACKS AT STA 1130 TOP LAND OF BEAM, FORWARD LIP. ACCOMPLISHED FLOOR BEAM REPAIR PER SRM 53-10-8. TST: 66,431. CYCLES: 34,330. (X)
- [SDR AALA971101](https://openairdocs.org/sdr/AALA971101.md): Flap Track · pitted · Jun 19, 1997 · N868AA · Boeing 727223 · Trailing Edge Flaps
  > TUL - NR 4 FLAP TRACK PITTED OUTBOARD SIDE UNDER THE TOP ROLLER INBOARD RADIUS. REMOVED AND REPLACED TRACK PER PATTERN CARD 8703. TST: 55,431 HOURS. CYCLES: 34,330. (X)
- [SDR AALA971104](https://openairdocs.org/sdr/AALA971104.md): Stringer · corroded · Jun 5, 1997 · N868AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - STA 488 INSIDE STR 28L CORRODED. REMOVED CORROSION PER 51-10-1 (OUT OF LIMITS). INSTALLED DOUBLER PER SRM 53-10-3. (X)
- [SDR AALA971103](https://openairdocs.org/sdr/AALA971103.md): Skin · corroded · Jun 5, 1997 · N868AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - SKIN CORRODED ALONG THE INTERCOSTAL WHERE THE SEALING COMPOUND WAS REMOVED. INSTALLED DOUBLER PER SRM 53-30-3, FIG 24. TST: 55,431 HOURS. CYCLES: 34,330. (X)
- [SDR AALA971105](https://openairdocs.org/sdr/AALA971105.md): Skin · corroded · Jun 3, 1997 · N868AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - SKIN CORRODED FROM STA 480 TO STA 500 UNDER AND OUTBOARD OF STR 28L. INSTALLED DOUBLER PER SRM 53-30-3, FIG 3A. TST: 55,431 HOURS. CYCLES, 34,330. (X)
- [SDR AALA970322](https://openairdocs.org/sdr/AALA970322.md): Skin · corroded · Mar 2, 1997 · N868AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > AFW - FOUND CORROSION ON SKIN, UNDER PODDING COMP. REMOVED CORROSION, INSTALLED DOUBLER AS PER SRM 53-30-3. (M)
- [SDR AALA970321](https://openairdocs.org/sdr/AALA970321.md): Flap Track · corroded · Feb 7, 1997 · N868AA · Boeing 727223 · Trailing Edge Flaps
  > AFW - FOUND CORROSION AT MOUNTS. REMOVED AND REPLACED TRACK WITH SERVICEABLE TRACK. (M)
- [SDR AALA970319](https://openairdocs.org/sdr/AALA970319.md): Flap Track · rusted · Feb 7, 1997 · N868AA · Boeing 727223 · Trailing Edge Flaps
  > AFW - RUST AT MOUNTING POINTS. REPLACED WITH SHOP TRACK. (M)
- [SDR AALA970320](https://openairdocs.org/sdr/AALA970320.md): Stringer · corroded · Feb 5, 1997 · N868AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > AFW - FOUND CORROSION ON STRINGER 27L. INSTALLED REPAIR IAW SRM 53-10-3. (M)
- [SDR AALA961222](https://openairdocs.org/sdr/AALA961222.md): Light · inoperative · Aug 16, 1996 · N868AA · Boeing 727223 · Emergency Lighting
  > ATL - DURING OVERNIGHT MAINTENANCE, FOUND THE FORWARD LEFT EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED THE M982 MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA960884](https://openairdocs.org/sdr/AALA960884.md): Skin · cracked · Jun 12, 1996 · N868AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND FUSELAGE SKIN HAS.5 INCH CRACK AT FORWARD END OF FUEL ENTRY DOOR LOWER HINGE CUTOUT. ROUTED OUT CRACK, INSTALLED DOUBLER PER SB 727-53-0198. (M)
- [SDR AALA960883](https://openairdocs.org/sdr/AALA960883.md): Skin · cracked · Jun 12, 1996 · N868AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND SKIN BULGED, CRACKED AT FASTENER HOLE STATION 380 STRINGER 21 TO 22R. REMOVED CRACKED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 PAGE 5-8. (M)
- [SDR AALA960403](https://openairdocs.org/sdr/AALA960403.md): Connector · broken · Mar 15, 1996 · N868AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA952135](https://openairdocs.org/sdr/AALA952135.md): Light · defective · Dec 23, 1995 · N868AA · Boeing 727223 · Emergency Lighting
  > BWI - FLT NR 1736 - DURING OVERNIGHT CHECK, COCKPIT DOOR EMERGENCY EXIT SIGN/LIGHT INOPERATIVE. REPLACED COCKPIT DOOR EMERGENCY EXIT SIGN/LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Next page: https://openairdocs.org/deregistered/N868AA-2012-08-21/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 = 'N868AA' AND deregistration_id = 'N868AA-2012-08-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N868AA-2012-08-21/reports

---
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