# Service difficulty reports: N858AA, cancelled Aug 21, 2013

A list on [N858AA, cancelled Aug 21, 2013](https://openairdocs.org/deregistered/N858AA-2013-08-21.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 · 54 reports

- [SDR GAIA05005OP](https://openairdocs.org/sdr/GAIA05005OP.md): Actuator · leaking · Feb 15, 2005 · N858AA · Boeing 727223 · Leading Edge Slat Actuator
  > FLT 544 - FWA-DTW - DURING TAKEOFF THE 'A' SYSTEM HYDRAULIC FLUID QUANTITY DECREASED AND BOTH A-PUMP LOW PRESSURE LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO FWA AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED NR 2 LEADING EDGE FLAP ACTUATOR AND NR
- [SDR GAIA03080OP](https://openairdocs.org/sdr/GAIA03080OP.md): Hose · leaking · Sep 2, 2003 · N858AA · Boeing 727223 · Hydraulic System, Main
  > AFTER TAKEOFF FROM ATL AT 1000 FT AGL THE FLIGHT CREW NOTICED THAT THE 'A' SYSTEM HYDRAULIC FLUID WAS LOST. THE CREW RETURNED TO ATL MANUALLY EXTENDING THE LANDING GEAR AND FLAPS. AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED NR 1 ENGINE DRIVEN PUMP
- [SDR GAIA03020OP](https://openairdocs.org/sdr/GAIA03020OP.md): Light · inoperative · Jun 19, 2003 · N858AA · Boeing 727223 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE MAIN ENTRY EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA01296ST](https://openairdocs.org/sdr/GAIA01296ST.md): Frame · damaged · Aug 13, 2001 · N858AA · Boeing 727223 · Fuselage Structure (General)
  > DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE BS 600 FRAME WAS DAMAGED AT STRINGER S17R. REPAIRED IAW BOEING 727 SRM 51-40-3, FIGURE 1 PAGE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA01297OP](https://openairdocs.org/sdr/GAIA01297OP.md): Light · inoperative · Aug 13, 2001 · N858AA · Boeing 727223 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE L1 DOOR POSITION EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE L1 DOOR POSITION EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (
- [SDR GAIA01154OP](https://openairdocs.org/sdr/GAIA01154OP.md): Engine · vibration · Apr 20, 2001 · N858AA · Boeing 727223 · Engine (Turbine/Turboprop)
  > FLT 1804 - PHX-FWA - WHILE AT CRUISE AT 35,000 FEET, NR 2 ENGINE BEGAN VIBRATING AND MAKING NOISE AS NR 2 THROTTLE WAS RETURNED TO IDLE, AND THE EGT INCREASED. THE CREW ACCOMPLISHED A PRECAUTIONARY ENGINE SHUT DOWN, DECLARED AN EMERGENCY, AND PROCEEDED TO LAN
- [SDR GAIA00796](https://openairdocs.org/sdr/GAIA00796.md): Slat · obstructed · Dec 22, 2000 · N858AA · Boeing 727223 · Leading Edge Slat Control System
  > FLIGHT 1725, FROM FWA TO ATL, AFTER TAKE OFF NR5 SLAT WOULD NOT RETRACT. AIRCRAFT MADE AN UNEVENTFUL RETURN TO FWA.FOUND FUELING PANEL DOOR OPEN AND BADLY BENT. PANEL DOOR INTERFERES WITH NR5 SLAT RETRACTION, WHICH LED TO NR5 SLAT FROM RETRAACTING AND GIVING
- [SDR GAIA00431](https://openairdocs.org/sdr/GAIA00431.md): Hinge · worn · Jul 14, 2000 · N858AA · Boeing 727223 · Landing Gear Doors
  > DISCREPANCY: DURING A 'C' CHECK INSPECTION, FOUND LEFT GEAR STRUT DOOR, FORWARD HINGE BUSHINGS HAD MIGRATED OUT AND LOOSE. CORRECTIVE ACTION: REPAIRED LEFT GEAR DOOR FORWARD HINGE PER S/B 727-32-0340, AND TIMCO REO S00248.
- [SDR GAIA00397](https://openairdocs.org/sdr/GAIA00397.md): Seat Track · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK INSPECTION, FOUND CORROSION ON SEAT TRACK AT STATION 755-848, RBL 24. INSTALLED NEW SEAT TRACK PER B727 SRM 51-30-5. (M)
- [SDR GAIA00398](https://openairdocs.org/sdr/GAIA00398.md): Seat Track · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK INSPECTION, FOUND CORROSION ON SEAT TRACK AT STATION 755-838, LBL 24. INSTALLED NEW SEAT TRACK PER B727 SRM 51-30-5. (M)
- [SDR GAIA00399](https://openairdocs.org/sdr/GAIA00399.md): Shear Tie · cut · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Structure
  > DURING A C-CHECK INSPECTION, FOUND WEB AT BS 1055, WL 208 FOUND CUT. REMOVED AND REPLACED SHEAR TIE WEB PER B727 SRM 51-20-1 AND 51-30-21. (M)
- [SDR GAIA00400](https://openairdocs.org/sdr/GAIA00400.md): Stiffener · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, FOUND CORROSION UNDER LEVELING COMPOUND AT BS 330, RBL 30. REMOVED AND REPLACED STIFFENER PER 51-30-2 AND 51-30-5. (M)
- [SDR GAIA00401](https://openairdocs.org/sdr/GAIA00401.md): Skin · dented · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > DURING A C-CHECK INSPECTION, SKIN WAS FOUND DENTED AT BS 1100, STRINGER S-1. CUT OUT DAMAGE AND REPAIRED AREA PER B727 SRM 53-30-3, FIGURE 3. (M)
- [SDR GAIA00402](https://openairdocs.org/sdr/GAIA00402.md): Web · dented · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, A DENT FOUND IN THE WEB ON STRINGER 25L AT BS 950D AND 950E. REMOVED AND REPLACED WEB PER B727 SRM 51-30-2. (M)
- [SDR GAIA00403](https://openairdocs.org/sdr/GAIA00403.md): Shear Tie · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Structure
  > DURING A C-CHECK INSPECTION, A SHEAR TIE WAS FOUND CORRODED IN THE AFT PIT AREA BS 1010 BETWEEN STRINGER 29R AND STRINGER 30R. REMOVED AND REPLACED ANGLE PER B727 SRM 51-30-2 AND 51-40-3. (M)
- [SDR GAIA00404](https://openairdocs.org/sdr/GAIA00404.md): Shear Tie · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Structure
  > DURING A C-CHECK INSPECTION, A SHEAR TIE WAS FOUND CORRODED IN THE AFT PIT AREA BS 1010 BETWEEN STRINGER 29L AND STRINGER 30L. INSTALLED DOUBLER REPAIR PER B727 SRM 53-10-4, FIG 12. (M)
- [SDR GAIA00405](https://openairdocs.org/sdr/GAIA00405.md): Shear Tie · cracked · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Structure
  > DURING A C-CHECK INSPECTION, A SHEAR TIE AT BS 321, RBL 30 HAS A SMALL CRACK. REMOVED AND REPLACED SHEAR TIE PER B727 SRM 53-10-4. (M)
- [SDR GAIA00406](https://openairdocs.org/sdr/GAIA00406.md): Door Frame · cracked · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, A CRACK FOUND IN WEB FOR C-2 CARGO DOOR FRAME, FORWARD LOWER CORNER. INSTALLED REPAIR ON BS 950E, C-2 DOOR FRAME PER S/B 727-53A0199R1. (M)
- [SDR GAIA00407](https://openairdocs.org/sdr/GAIA00407.md): Seat Track · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK INSPECTION, SEAT TRACK CORRODED AT BS 480 TO 610, LBL 45. REMOVED AND REPLACED SEAT TRACK BS 480-610, LBL 45 PER B727 SRM 53-10-5. (M)
- [SDR GAIA00408](https://openairdocs.org/sdr/GAIA00408.md): Seat Track · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK INSPECTION, SEAT TRACK CORRODED AT BS 620, LBL 25. REMOVED AND REPLACED SEAT TRACK PER B727 SRM 53-10-5. (M)
- [SDR GAIA00409](https://openairdocs.org/sdr/GAIA00409.md): Seat Track · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK INSPECTION, SEAT TRACK CORRODED AT BS 420, RBL 25. REMOVED AND REPLACED SEAT TRACK PER B727 SRM 53-10-5. (M)
- [SDR GAIA00410](https://openairdocs.org/sdr/GAIA00410.md): Seat Track · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK INSPECTION, SEAT TRACK CORRODED AT BS 740, LBL 45. REMOVED AND REPLACED SEAT TRACK PER B727 SRM 53-10-5. (M)
- [SDR GAIA00411](https://openairdocs.org/sdr/GAIA00411.md): Seat Track · damaged · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK INSPECTIN, SEAT TRACK DAMAGED AT BS 435, RBL 45. REMOVED AND REPLACED SEAT TRACK PER B727 SRM 53-10-5. (M)
- [SDR GAIA00412](https://openairdocs.org/sdr/GAIA00412.md): Seat Track · damaged · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK INSPECTION, SEAT TRACK DAMAGED AT BS 435, LBL 45. REMOVED AND REPLACED SEAT TRACK PER B727 SRM 53-10-5. (M)
- [SDR GAIA00413](https://openairdocs.org/sdr/GAIA00413.md): Seat Track · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK INSPECTION, SEAT TRACK CORRODED AT BS 720D AND 740, LBL 45. REMOVED AND REPLACED SEAT TRACK PER B727 SRM 53-10-5. (M)
- [SDR GAIA00414](https://openairdocs.org/sdr/GAIA00414.md): Seat Track · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK INSPECTION, SEAT TRACK CORRODED AT BS 580, LBL 45. REMOVED AND REPLACED SEAT TRACK PER B727 SRM 53-10-5. (M)
- [SDR GAIA00415](https://openairdocs.org/sdr/GAIA00415.md): Skin · cracked · Jul 14, 2000 · N858AA · Boeing 727223 · Leading Edge Devices
  > DURING A C-CHECK INSPECTION, RIGHT SLAT, WS 100 HAS A SKIN CRACK AT NR 5 L/E SLAT OUTBOARD TRACK CUT OUT. REPAIRED TRACK CUT OUT PER SRM 57-30-4. (M)
- [SDR GAIA00416](https://openairdocs.org/sdr/GAIA00416.md): Stringer Clip · cracked · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, STRINGER CLIP CRACKED AT BS 720B, STRINGER 7L. REMOVED AND REPLACED STRINGER CLIP PER B727 SRM 51-30-2. (M)
- [SDR GAIA00417](https://openairdocs.org/sdr/GAIA00417.md): Stringer Clip · cracked · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, STRINGER CLIP CRACKED AT BS 720A, STRINGER 7L. REMOVED AND REPLACED STRINGER CLIP PER B727 SRM 51-30-2. (M)
- [SDR GAIA00418](https://openairdocs.org/sdr/GAIA00418.md): Stringer Clip · cracked · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, STRINGER CLIP CRACKED AT BS 720, STRINGER 7L. REMOVED AND REPLACED STRINGER CLIP PER B727 SRM 51-30-2. (M)
- [SDR GAIA00419](https://openairdocs.org/sdr/GAIA00419.md): Stringer Clip · cracked · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, STRINGER CLIP CRACKED AT BS 700, STRINGER 9R. REMOVED AND REPLACED STRINGER CLIP PER B727 SRM 51-30-2. (M)
- [SDR GAIA00420](https://openairdocs.org/sdr/GAIA00420.md): Stringer Clip · cracked · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, STRINGER CLIP CRAKCED AT BS 680, STRINGER 7R. REMOVED AND REPLACED STRINGER CLIP PER B727 SRM 51-30-2. (M)
- [SDR GAIA00421](https://openairdocs.org/sdr/GAIA00421.md): Stringer Clip · cracked · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, STRINGER CLIP CRACKED AT BS 620, STRINGER 7R. REMOVED AND REPLACED STRINGER CLIP PER B727 SRM 51-30-2. (M)
- [SDR GAIA00422](https://openairdocs.org/sdr/GAIA00422.md): Skin · gouged · Jul 14, 2000 · N858AA · Boeing 727223 · Leading Edge Devices
  > DURING A C-CHECK INSPECTION, FOUND GOUGE AT THE UNDER SIDE WING SKIN JUST BELOW NR 5 SLAT, RIGHT WING. REPAIRED GOUGE PER B727 SRM 57-50-3. (M)
- [SDR GAIA00423](https://openairdocs.org/sdr/GAIA00423.md): Frame · cracked · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A C-CHECK INSPECTION, FOUND CRACKED FRAME AT BS 380, S5L. REPAIRED FRAME PER B727 SRM 53-10-4. (M)
- [SDR GAIA00424](https://openairdocs.org/sdr/GAIA00424.md): Floorbeam · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING A C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM, UPPER SURFACE AT BS 380, RBL 25. INSTALLED NEW FILLER PER B727 SRM 53-10-8. (M)
- [SDR GAIA00425](https://openairdocs.org/sdr/GAIA00425.md): Frame · dented · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A C-CHECK INSPECTION, FOUND DENT AT CIRCUMFERENTIAL, BS 1166, WL 215 RIGHT, JUST ABOVE PREVIOUS REPAIR. REMOVED EXISTING REPAIR TO INCLUDE EXISTING DAMAGE. REMOVED DAMAGE AREA, AND INSTALED A REPAIR TO FRAME AT BS 1166, STRINGER 14R TO A18R. (M)
- [SDR GAIA00426](https://openairdocs.org/sdr/GAIA00426.md): Frame · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A C-CHECK INSPECTION, FOUND CIRCUMFERENTIAL FRAME AT BS 1163, WL 208 CORRODED. REPAIRED PER B727 SRM 51-40-3. (M)
- [SDR GAIA00427](https://openairdocs.org/sdr/GAIA00427.md): Frame · cracked · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A C-CHECK INSPECTION, FOUND CIRCUMFERENTIAL FRAME AT BS 783.95, WL 208 CRACKED. REPAIRED PER S/B 727 53-0197, R2 AT BS 783.95, WL 216 TO WL 201. (M)
- [SDR GAIA00428](https://openairdocs.org/sdr/GAIA00428.md): Stringer Clip · damaged · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND STRINGER TIE DAMAGED AT BS 1166, STRINGER 15R. REMOVED AND REPLACED STRINGER TIE PER B727 SRM 51-20-1 AND 51-30-2. (M)
- [SDR GAIA00429](https://openairdocs.org/sdr/GAIA00429.md): Frame · corroded · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A C-CHECK INSPECTION, FOUND CORROSION ON FRAME AT BS 986, STRINGER 26R TO STRINGER 29R IN AFT PIT. REPAIRED PER B727 SRM 51-40-4. (M)
- [SDR GAIA00430](https://openairdocs.org/sdr/GAIA00430.md): Floorbeam · damaged · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING A C-CHECK INSPECTION, FOUND ELONGATED HOLE IN FLOORBEAM AT BS 720B, RBL 63. REPAIRED PER B727 SRM 53-10-8. (M)
- [SDR GAIA00432](https://openairdocs.org/sdr/GAIA00432.md): Skin · cracked · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > DURING A C-CHECK INSPECTION, FOUND CRACK AT NR 1 CARGO DOOR CUT OUT, BS 620, STRINGER 25R IN FRAME WEB. REPAIRED PER B727 SRM 51-40-2 AND 53-10-2. (M)
- [SDR GAIA00433](https://openairdocs.org/sdr/GAIA00433.md): Bulkhead · cracked · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Bulkhead
  > DURING A C-CHECK INSPECTION, FOUND CRACK AT AFT PRESSURE BULKHEAD WEB, LBL 18, WL 265. REPAIRED PER TIMCO REO SOO242. (M)
- [SDR GAIA00434](https://openairdocs.org/sdr/GAIA00434.md): Floorbeam · damaged · Jul 14, 2000 · N858AA · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING A C-CHECK INSPECTION, FOUND ELONGATED HOLE IN FLOORBEAM AT BS 460, RBL 61. REPAIRED FLOORBEAM PER B727 SRM 53-10-8. (M)
- [SDR GAIA0038](https://openairdocs.org/sdr/GAIA0038.md): Warning Light · illuminated · Jan 21, 2000 · N858AA · Boeing 727223 · Smoke Detection
  > DURING CLIMB-OUT FWA-SEA, THE CREW INDICATED THAT THERE WAS A SMOKE INDICATION IN THE CARGO AREA. THE AIRCRAFT RETURNED TO FWA AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. INSPECTED UPPER AND LOWER CARGO AREAS FOR FIRE OR SMOKE EVIDENCE AND NONE WAS NOTED.
- [SDR GAIA0002](https://openairdocs.org/sdr/GAIA0002.md): Battery Pack · discharged · Jan 5, 2000 · N858AA · Boeing 727223 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE IN CLT, IT WAS DISCOVERED THAT THE EMERGENCY LIGHT AT THE L1 DOOR WOULD NOT TEST. REMOVED AND REPLACED BATTERY PACK AT L1 DOOR. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA99150](https://openairdocs.org/sdr/GAIA99150.md): Beam · corroded · Oct 5, 1999 · N858AA · Boeing 727223 · Wing Miscellaneous Structure
  > PHX - DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED DURING FUEL CELL REPAIR THAT THE LOWER TRAILING EDGE PANEL ATTACHMENT TO THE LEFT MLG BEAM HAD CORROSION DAMAGE. REPAIRS WERE COMPLETED IAW FVI DRAWING NUMBER 57-99515-1 AND 8110 DATED OCTOBER 4, 1999. THE
- [SDR GAIA99140](https://openairdocs.org/sdr/GAIA99140.md): Overheat Loop · intermittent · Sep 14, 1999 · N858AA · Boeing 727223 · Overheat Detection
  > ORD-TOL - FLT 713 - ON CLIMB-OUT, NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. PERFORMED STRUT OVERHEAT CHECKLIST. THE LIGHT EXTINGUISHED WHEN THE RIGHT PACK AND NR 3 BLEED SWITCHES WERE CLOSED. THE AIRCRAFT CONTINUED TO TOL AND LANDED SAFELY WITHOUT FURTHER DIFF
- [SDR GAIA99133](https://openairdocs.org/sdr/GAIA99133.md): Duct · leaking · Sep 9, 1999 · N858AA · Boeing 727223 · Pneumatic Distribution System
  > FLT 727 - MKE-TOL - ENCOUNTERED DURING CRUISE AN OVERHAT DETECTION ON NR 3 PYLON. THE LIGHT EXTINGUISHED WHEN THE THROTTLE WAS RETURNED TO IDLE. THE AIRCRAFT CONTINUED TO TOL AND LANDED SAFELY WITHOUT FURTHER DIFFICULTIES. REMOVED AND REPLACED THE HIGH PRES

Next page: https://openairdocs.org/deregistered/N858AA-2013-08-21/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 = 'N858AA' AND deregistration_id = 'N858AA-2013-08-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N858AA-2013-08-21/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.