# Service difficulty reports: N406UA

A list on [N406UA](https://openairdocs.org/aircraft/N406UA.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 4 · 151 reports

- [SDR CALA2022050601155](https://openairdocs.org/sdr/CALA2022050601155.md): None · leaking · May 5, 2022 · N406UA · Airbus A320232 · Hydraulic Filter, Main
  > HYD B RSVR LO LVL DISPLAY ON ECAM. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V936927 SYSTEM LEVEL AND FOUND TO BE WITHIN LIMITS. PLEASE CONTACT TOMC BEFORE COMMENCING AN
- [SDR CALA2022011000100](https://openairdocs.org/sdr/CALA2022011000100.md): Slat · fault message · Jan 9, 2022 · N406UA · Airbus A300* · Leading Edge Slat Control System
  > *EMERGENCY DECLARED* F/CTL SLATS FAULT UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CALL TOMC AND FOLLOW TSM 27-81-00-810-810A REF TSM TASK 27-81-00-810-094 OPERATING WITH GREEN SYSTEM RECEIVED SLAT SYSTEM
- [SDR CALA2021062000907](https://openairdocs.org/sdr/CALA2021062000907.md): Seal · cracked · Jun 19, 2021 · N406UA · Airbus A320232 · Nacelle/Pylon Miscellaneous Structure
  > PDA 2 #2 ENG INBD SIDE PYLON TO NACELLE FLEX SEAL (SECOND FROM AFT) CRACKED AND MISSING A SEGMENT. PHOTO ADDED REF ECRA 5450-02357 REV- B FIGURE 3 ITEM 100 IS CRACKED & MISSING A SECTION. PERFORMED INTERIM REPAIR PER PART 1D AND APPLIED SPEED TAPE. ISSUE DIP T
- [SDR CALA2021020500128](https://openairdocs.org/sdr/CALA2021020500128.md): Stringer · cracked · Feb 4, 2021 · N406UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > LH STR 30L BETWEEN FR 35-36 IS CRACKED. -AD TASK A3NB-53-4-6159- GENERATED BY MECH V892442 AT HAECO LCQ. WORK GENERATED ON N/R 9292184/ 44184. INSTALLED REPAIR DOUBLER & FILLER @ L/H STR 30L BETWEEN FR35-36 PER AIRBUS REF 80875677/025 ECRA 5331-02693 AND REO-L
- [SDR CALA2021020300121](https://openairdocs.org/sdr/CALA2021020300121.md): Door Frame · cracked · Feb 1, 2021 · N406UA · Airbus A320232 · Fuselage Main, Structure
  > R2 DOOR FRAME 68 STOP #1 LOWER INBOARD HOLE IS CRACKED IN THE WE B AT 7:00 PER HAECO LCQ NON-ROUTINE 9292169 GENERATED BY V061633 REPAIRED R2 DOOR STOP FITTING #1 IAW SRM 53-41-12-300-011 FIG 008 SHEET 1 AND SHEET 2 AND SRM 53-41-12-300-008. THIS REPAIR FOUND
- [SDR CALA2021012700094](https://openairdocs.org/sdr/CALA2021012700094.md): Profile · cracked · Jan 25, 2021 · N406UA · Airbus A320232 · Fuselage Main, Structure
  > OFF-AIRCRAFT PART: LT AFT EMERGENCY EXIT HATCH FWD LOAD TRANSMITTING PROFILE CRACKED, PER HAECO LCQ NON ROUTINE 9292230. REMOVED CRACKED SEGMENT INSTALLED NEW SEGMENT, IAW A320 SRM 51-42 -11-801.
- [SDR CALA2021012700093](https://openairdocs.org/sdr/CALA2021012700093.md): Profile · cracked · Jan 25, 2021 · N406UA · Airbus A320232 · Fuselage Main, Structure
  > LT AFT EMERGENCY EXIT HATCH AFT LOAD TRANSMITTING PROFILE CRACKED OFF. AIRCRAFT PART: (A3NB-52-4-6031) PER HAECO LCQ NON ROUTINE 9292231. REMOVED CRACKED SEGMENT INSTALLED NEW SEGMENT, IAW A320 SRM 51-42 -11-801.
- [SDR CALA2019042600652](https://openairdocs.org/sdr/CALA2019042600652.md): Interlock · missing · Apr 26, 2019 · N406UA · Airbus A320232 · Cargo/Baggage Doors
  > FWD/CARGO DOOR OPEN MSGIN FLT FOUND FWD CARGO DOOR INTERLOCK MECHANISM PIVOT LINK MISSING UPPER PIN AND CIRCLIP, FOUND PIN IN LOWER DOOR, REINSTALLED PIN AND CIRCLIP. OPS CHECKED DOOR SEVERAL TIMES, HANDLE STOWS FIRMLY NO ECAM MESSAGES.
- [SDR CALA2019012100140](https://openairdocs.org/sdr/CALA2019012100140.md): Valve · leaking · Jan 21, 2019 · N406UA · Airbus A320232 · Landing Gear Brake System
  > NEED TO COMPLY WITH AMM 29-00-00-280-006-A01 CHECK OF Y HYD SYS AFTER PUMP FAILURE OR OPERATION IN A POSSIBLE CAVITATION COND. FOUND PARKING BRAKE VALVE LEAKING REPLACED PER AMM 32-45-14-400 REPLACED NR 2 ENG DRIVEN PUMP DUE TO CAVITATION PER AMM 29-13-51-4 00
- [SDR CALA2018040501092](https://openairdocs.org/sdr/CALA2018040501092.md): Slide · unsecure · Apr 1, 2018 · N406UA · Airbus A320232 · Escape Slide
  > REPORTED BY PILOT AND CATERING THAT L2 DOOR SLIDE IS COMING APART AT THE BOTTOM OF THE SLIDE. REMOVED AND REPLACED L2 DOOR SLIDE AND TESTED IAW AMM 25-62-44-0 0-002Q, AND 25-62-44-400-006A. DOOR SLIDE SECURE AND TESTS PASSED.
- [SDR CALA2017121604482](https://openairdocs.org/sdr/CALA2017121604482.md): Cradle · broken · Dec 16, 2017 · N406UA · Airbus A320232 · Emergency Equipment
  > AFT RIGHT EMER FLASHLIGHT BRACKET IS BROKEN INSTALLED SERVICEABLE EMERG. FLASHLIGHT BRACKET & OPS CHECKS GOOD. ORIGINAL FLASHLIGHT WAS SERVICEABLE & RE-INSTALLED.
- [SDR CALA2017112104173](https://openairdocs.org/sdr/CALA2017112104173.md): Skin · damaged · Nov 20, 2017 · N406UA · Airbus A320232 · Rudder, Plate/Skin
  > PUNCTURE DISCOVERED ON THE UPPER RIGHT SIDE OF THE RUDDER. THE PUNCTURE WAS LOCATED 14.5 INCHES FROM TRAILING EDGE AND 9.7 INCHES FROM CAP SEAM. THE DAMAGE IS 1.1 INCHES IN WIDTH AND.8 INCH IN LENGTH.
- [SDR CALA2016101995831](https://openairdocs.org/sdr/CALA2016101995831.md): Stringer · corroded · Oct 16, 2016 · N406UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > CORROSION AROUND FASTENER HOLE STRINGER 41 RIGHT 6 INCH AFT OF FRAME 58 IN AFT CARGO. REMOVED AND REPLACED AFT CARGO STRINGER 41R FR 64 TO FR 59 IAW SRM 51-42-11.
- [SDR CALA2016101995828](https://openairdocs.org/sdr/CALA2016101995828.md): Skin · dented · Oct 15, 2016 · N406UA · Airbus A320232 · Cargo/Baggage Doors
  > AFT CARGO DOOR SKIN DENT FR55. INSTALLED DOUBLER IAW SRM 52-32-00 FIG 205.
- [SDR CALA2016101995827](https://openairdocs.org/sdr/CALA2016101995827.md): Skin · dented · Oct 15, 2016 · N406UA · Airbus A320232 · Cargo/Baggage Doors
  > AFT CARGO DOOR SKIN DENT FR54A+5. INSTALLED DOUBLER IAW SRM 52-32-00 FIG 205.
- [SDR CALA2016101995826](https://openairdocs.org/sdr/CALA2016101995826.md): Skin · damaged · Oct 15, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > RT FUSE AT FR35 STR 30 HOLE MARKED 3 IS OUT OF ROUND. INTERIM RPR ACP IAW ECRA5330-05797 PART1 ACP PERM RPR OF THE FASTENER HOLES AT FR35 STR 30L 30R ON OR BEFORE MARCH 26 2017.
- [SDR CALA2016101995825](https://openairdocs.org/sdr/CALA2016101995825.md): Skin · damaged · Oct 15, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > LT FUSE AT FR35 STR30 HOLE MARKED 3 IS OUT OF ROUND. INTERIM RPR ACP IAW ECRA5330-05797 PART1 ACP PERM RPR OF THE FASTENER HOLES AT FR35 STR 30L, 30R ON OR BEFORE MARCH 26 2017.
- [SDR CALA2016101995824](https://openairdocs.org/sdr/CALA2016101995824.md): Skin · damaged · Oct 15, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > LT FUSE AT FR35 STR30 HOLE MARKED AS 4 IS OUT OF ROUND. INTERIM RPR ACP IAW ECRA5330-05797 PART1 ACP PERM RPR OF THE FASTENER HOLES AT FR35 STR 30L, 30R ON OR BEFORE MARCH 26 2017.
- [SDR CALA2016101995823](https://openairdocs.org/sdr/CALA2016101995823.md): Skin · damaged · Oct 15, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > LT FUSE AT FR35 STR 30 HOLE MARKED AS 1 IS CRACKED IN SKIN AND SIDESHELL. INTERIM RP ACP IAW ECRA 5330- 05797 PART1 ACP PERM RPR OF THE FASTENER HOLES AT FR35 STR 30L, 30R ON OR BEFORE MARCH 26 2017.
- [SDR CALA2016101995822](https://openairdocs.org/sdr/CALA2016101995822.md): Skin · damaged · Oct 15, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > LT FUSE AT FR 35 STR 30 HOLE MARKED AS 2 IS CRACKED IN SIDESHELL AND FRAME FLANGE. INTERIM RPR ACP IAW ECRA 5330-05797 PART1ACP PERM RPR OF THE FASTENER HOLES AT FR 35 STR 30L, 30R ON OR BEFORE MARCH 26 2017.
- [SDR CALA2016101995820](https://openairdocs.org/sdr/CALA2016101995820.md): Skin · corroded · Oct 14, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FUSELAGE EXT SKIN AT WASTE VENT HAS MINOR CORROSION FR 69-FR 70, STR 28R. DAMAGED FOUND TO BE OUT OF LIMITS IAW SRM 53-41-11 TABLE 108. INSTALLED REPAIR DOUBLER AT FR69-FR70 STR 28R EXT SKIN AT WASTE VENT, IAW SRM 53-41-11 PARA 5 D.
- [SDR CALA2016101795806](https://openairdocs.org/sdr/CALA2016101795806.md): Angle · corroded · Oct 12, 2016 · N406UA · Airbus A320232 · Emergency Exits
  > CORROSION ON LEFT AFT EMERGENCY EXIT LOWER FRAME NEXT TO DRAIN HOLE. REMOVED AND REPLACED T-ANGLE FWD AND LEFT LOWER CORNER CURVED WEBS IAW SRM 51-42-11.
- [SDR CALA2016101395797](https://openairdocs.org/sdr/CALA2016101395797.md): Skin · dented · Oct 10, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL DENT FR3, 11" ABOVE LOWER LAP SEAM. ACCOMPLISHED REPAIR IAW SRM 53-00-11, PAR 4 W FIG 240.
- [SDR CALA2016101395802](https://openairdocs.org/sdr/CALA2016101395802.md): Cleat · corroded · Oct 9, 2016 · N406UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO FR 31 STR 43L-43R CLEAT HAS CORROSION. REMOVED AND REPLACED FWD CARGO FR31 STR 43L-43R CLEAT SRM 51-42-11.
- [SDR CALA2016093095791](https://openairdocs.org/sdr/CALA2016093095791.md): Cleat · corroded · Sep 30, 2016 · N406UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO PIT FR32 STR 40R-41R CLEAT HAS CORROSION. R&R CLEAT IAW SRM 51-42-11.
- [SDR CALA2016093095790](https://openairdocs.org/sdr/CALA2016093095790.md): Cleat · corroded · Sep 30, 2016 · N406UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO PIT FR33 STR43R-43L CLEAT IS CORRODED. R&R CLEAT IAW SRM 51-42-11.
- [SDR CALA2016093095789](https://openairdocs.org/sdr/CALA2016093095789.md): Cleat · corroded · Sep 30, 2016 · N406UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO PIT FR33 STR40R-41R CORROSION ON CLEAT. R&R CLEAT IAW SRM 51-42-11.
- [SDR CALA2016093095786](https://openairdocs.org/sdr/CALA2016093095786.md): Cleat · corroded · Sep 30, 2016 · N406UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO FR33 STR 42-43R CLEAT HAS CORRSION. REMOVED AND REPLACED FWD CARGO FR33 STR 42-43R CLEAT IAW SRM51-42-11.
- [SDR CALA2016092795780](https://openairdocs.org/sdr/CALA2016092795780.md): Shear Tie · corroded · Sep 26, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO FR30 CLEATS HAVE CORROSION AT STR'S 42L - 43L AND 44 - 43R. REPLACED 2 EA CLEATS IAW A320 SRM 51-42-1 1.
- [SDR CALA2016092795779](https://openairdocs.org/sdr/CALA2016092795779.md): Shear Tie · corroded · Sep 26, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO FR28, STR 43R - 44R CLEAT HAS CORROSION. REMOVED & REPLACED IAW A320 SRM 51-42-11.
- [SDR CALA2016092795763](https://openairdocs.org/sdr/CALA2016092795763.md): Shear Tie · corroded · Sep 26, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO BAY FRAME 28 STRINGERS 41-40L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.
- [SDR CALA2016092795782](https://openairdocs.org/sdr/CALA2016092795782.md): Shear Tie · corroded · Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO BAY, FRAME 30 STRINGERS 40, 41, 42, 43R CLEATS HAVE CORROSION. REPLACED THE CLEATS IAW SRM 51-42-1 1.
- [SDR CALA2016092795781](https://openairdocs.org/sdr/CALA2016092795781.md): Shear Tie · corroded · Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO FRAME 27 STRINGERS 43L - 42L AND 43L - 43R CLEATS HAVE CORROSION. REPLACED THE CLEATS IAW SRM 51-42-1 1.
- [SDR CALA2016092795771](https://openairdocs.org/sdr/CALA2016092795771.md): Shear Tie · corroded · Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO BAY FRAME 27 STRINGERS 42-41 SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.
- [SDR CALA2016092795770](https://openairdocs.org/sdr/CALA2016092795770.md): Shear Tie · corroded · Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO BAY FRAME 34 STRINGERS 42-43L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.
- [SDR CALA2016092795769](https://openairdocs.org/sdr/CALA2016092795769.md): Shear Tie · corroded · Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO BAY FRAME 33 STRINGERS 40-41L HAS CORROSION. REMOVED AND REPLACED THE SHEART TIE IAW SRM 53-42-11.
- [SDR CALA2016092795768](https://openairdocs.org/sdr/CALA2016092795768.md): Shear Tie · corroded · Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO BAY FRAME 33 STRINGERS 42-43L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.
- [SDR CALA2016092795767](https://openairdocs.org/sdr/CALA2016092795767.md): Shear Tie · corroded · Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO BAY FRAME 28 STRINGERS 42-43R SHEAR TIE HAS CORROSION, REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.
- [SDR CALA2016092795766](https://openairdocs.org/sdr/CALA2016092795766.md): Shear Tie · corroded · Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO BAY FRAME 28 STRINGERS 41-42R SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.
- [SDR CALA2016092795765](https://openairdocs.org/sdr/CALA2016092795765.md): Shear Tie · corroded · Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO BAY FRAME 28 STRINGERS 41-42L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.
- [SDR CALA2016092795764](https://openairdocs.org/sdr/CALA2016092795764.md): Shear Tie · corroded · Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO BAY FRAME 28 STRINGERS 42-43L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.
- [SDR CALA2016092795775](https://openairdocs.org/sdr/CALA2016092795775.md): Skin · dented · Sep 22, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE SKIN HAS DENT FRAME 7 8.5 INCH ABOVE LOWER LAP SEAM. FOUND TO BE OUT OF LIMITS. CUT OUT THE DAMAGED AREA & FABRICATED A REPAIR DOUBLER AND INSTALLED IAW SRM53-00-11 FIG 239.
- [SDR CALA2016092795774](https://openairdocs.org/sdr/CALA2016092795774.md): Skin · contaminated · Sep 22, 2016 · N406UA · Airbus A320232 · Horizontal Stabilizer Structure
  > RIGHT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATIONS 186" FROM INBOARD, 9" FROM TE, 4 X 5.5 DIA A ND 150" FROM INBOARD, 14" FROM TE, 4.5 X 6.0 DIA. REPAIRED IAW SRM 55-21-11 PAR. 5.N.
- [SDR CALA2016092795773](https://openairdocs.org/sdr/CALA2016092795773.md): Skin · contaminated · Sep 22, 2016 · N406UA · Airbus A320232 · Horizontal Stabilizer, Plate/Skin
  > LEFT ELEVATOR UPPER SKIN PANEL HAS A TRAPPED WATER INDICATION, 47.5" FROM INBOARD, 5" FROM TE, 3 X 2.5 DIA. REPAIRED IAW SRM 55-21-11 PAR. 5.E.
- [SDR CALA2016082695685](https://openairdocs.org/sdr/CALA2016082695685.md): Engine · stalled · Aug 25, 2016 · N406UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > AT FL 360, ECAM INDICATION LEFT ENGINE STALLED. DIVERTED, ENGINE DISPLAYED STALL INDICATIONS TWICE AT ALTITUDE BUT PERFORMED NORMAL REST OF FLIGHT. TROUBLESHOOT IAWTSM. REPLACED EEC AS A PRECAUTION. LEAK CHECK AND PURGE OF PB SENSE LINE, INSPECTED FOR DE
- [SDR CALA2016050495331](https://openairdocs.org/sdr/CALA2016050495331.md): Battery · discharged · May 2, 2016 · N406UA · Airbus A320232 · Emergency Lighting
  > AFTER REPLACEMENT OF 1R SLIDE, FOUND SEVERAL LIGHTS OUT FROM CTR BATTERY PACK WITH A-C POWER OFF. REPLACED CTR BATTERY PACK WITH SERVICEABLE UNIT. TESTED SUCCESSFUL.
- [SDR CALA2015081194189](https://openairdocs.org/sdr/CALA2015081194189.md): Slide · activated · Aug 7, 2015 · N406UA · Airbus A320232 · Escape Slide
  > DOOR 2L SLIDE INFLATED DURING CLEANING. REMOVED INFLATED SLIDE FROM DOOR 2L IAW AMM 25-62-44-000-011-A.
- [SDR CALA2015020293061](https://openairdocs.org/sdr/CALA2015020293061.md): Skin · damaged · Jan 30, 2015 · N406UA · Airbus A320232 · Wing, Plate/Skin
  > RIGHT WING TANK ACCESS PLATE 640PB HAS DAMAGED FASTENER HOLE ON LANDING. HOLE WAS REPAIRED IAW HAECO REO-L187 08 & CONSIDERED CAT B REPAIR IAW -B RDAS 80022401-003-2015. HOLE WAS OVERSIZED & BUSHING WAS INSTALLED. IAW CRA THRESHOLD SUPPLEMENTAL INSPECTIONS T
- [SDR CALA2015020293054](https://openairdocs.org/sdr/CALA2015020293054.md): Skin · damaged · Jan 29, 2015 · N406UA · Airbus A320232 · Wing, Plate/Skin
  > RIGHT FUEL TANK ACCESS LANDING, TWO EACH HOLES HAS ELONGATION 640HB. R & R BUSHING HOLE 565 & INSTALLED BUS HINGE HOLE 562 IAW A320. SRM 57-21-11 PG 210-216 PAR B.
- [SDR CALA2015012793033](https://openairdocs.org/sdr/CALA2015012793033.md): Door Sill · corroded · Jan 26, 2015 · N406UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL BEAM HAS CORROSION ON PREVIOUS REPAIR & FRAME 68, JUST FWD OF THE AFT GIRT BAR FITTING PLATE. R & R DOOR SILL IAW SRM 51-42-11.

Next page: https://openairdocs.org/aircraft/N406UA/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 = 'N406UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N406UA/reports

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