# Service difficulty reports: N416UP

A list on [N416UP](https://openairdocs.org/aircraft/N416UP.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 6 · 261 reports

- [SDR IPXA2026032266402](https://openairdocs.org/sdr/IPXA2026032266402.md): Floor Support · cracked · Mar 19, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT Z-100 STR: FLOOR STRINGER CRACKED FOUND AT AFT CARGO COMPARTMENT AT STA 1342 RBL 2.90 INSTALLED NEW STRINGER AT AFT CARGO COMPARTMENT AT STA 1342 RBL 2.90 IAW B757-200 SRM 51-40-02-OG
- [SDR IPXA2026031153938](https://openairdocs.org/sdr/IPXA2026031153938.md): Angle · cracked · Mar 6, 2026 · N416UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 2 ENG PYLON FWD LOWER PLATE CRACKED INBD-OTBD SIDE. INSTALLED ANGLE AT NR 2 ENG PYLON FWD LOWER IAW SRM 51-40-02.
- [SDR IPXA2026031939735](https://openairdocs.org/sdr/IPXA2026031939735.md): Tee Angle · corroded · Mar 5, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT-STR-ZONE 100. RH LOWER MIDDLE FUSELAGE STA 1040-1060 RBL 65 T-CHORD CORRODED. DOT 28-05 INSTALLED NEW T-CHORD AT RH LOWER MIDDLE FUSELAGE STA 1040-1060 RBL 65 IAW B757-200PF SRM 51-40-02-0G-0
- [SDR IPXA2026031919295](https://openairdocs.org/sdr/IPXA2026031919295.md): Tee Angle · corroded · Mar 4, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > LOWER HALF OF FUSELAGE TEE ANGLE BETWEEN BS 1040 & 1060, AROUND STRINGER 25R HAD CORROSION. INSTALLED A NEW TEE ANGLE BTWN BS 1040 - 1060, STRINGER 25R IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026032119365](https://openairdocs.org/sdr/IPXA2026032119365.md): Angle · corroded · Mar 4, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > LOWER HALF OF FUSELAGE RH PACK HOT AIR EXHAUST FRONT STRUCTURE ANGLE BETWEEN STR 1040 AND STR 1060 HAS CORROSION DOT 115-004. INSTALLED NEW INTERCOSTAL AND REINSTALLED COVER SUPPORT HOT AIR EXHAUST, IAW B757-200PF, SRM 51-40-02.
- [SDR IPXA2026031600239](https://openairdocs.org/sdr/IPXA2026031600239.md): Support Angle · corroded · Mar 3, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT RIGHT LOWER BULKHEAD SUPPORT AT STA.1640 SHOWS EVIDENCE OF CORROSION AND A CRACK DOT 47-11 INSTALLED 2 ANGLES IAW SRM 51-40-02.
- [SDR IPXA2026030974670](https://openairdocs.org/sdr/IPXA2026030974670.md): Floorboard · broken · Mar 2, 2026 · N416UP · Boeing 75724APF · Fuselage Floor Panel
  > MAJOR REPAIR, MCD FLOORBOARD 241XCF AFT CORNER IS BROKEN. THE FLOORBOARD FABRICATED IAW SREO-9692-REQ001, VERIFIED RII REQUIREMENT COMPLETED, IAW UPS GMM 04.02.01.15.
- [SDR IPXA2026031579385](https://openairdocs.org/sdr/IPXA2026031579385.md): Transition Panel · corroded · Mar 2, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > TRANSITION PANEL FROM AFT CARGO COMPARTMENT STA1310 TO STA 1360 R/H CORROSION AND HOLES DAMAGED. INSTALLED NEW TRANSITION PANEL AFT CARGO COMPARTMENT STA 1310 TO STA 1360 R/H IAW SRM 51-40-02-0G
- [SDR IPXA2026031784226](https://openairdocs.org/sdr/IPXA2026031784226.md): Angle · cracked · Mar 2, 2026 · N416UP · Boeing 75724APF · Nacelle/Pylon, Main Frame
  > NR 1 ENG AFT PYLON FARING SUPPORT ANGLE L BRACKET ON INBD SIDE IS CRACKED. REMOVED BRACKET ON NR 1 ENGINE AFT PYLON FARING IAW SRM 51-40-02. INSTALLED A NEW L ANGLE IAW SRM 51-40-02.
- [SDR IPXA2026032470530](https://openairdocs.org/sdr/IPXA2026032470530.md): Filler · corroded · Mar 1, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO, BS 1480 BILDGE AREA, NEAR ANTENNA LOWER SURFACE HAS CORRODED. INSTALLED NEW FILLER RADIUS IAW SRM 51-40-02-0G.
- [SDR IPXA2026030970913](https://openairdocs.org/sdr/IPXA2026030970913.md): Floor Panel · damaged · Mar 1, 2026 · N416UP · Boeing 75724APF · Fuselage Floor Panel
  > MAJOR REPAIR, FLOOR PANEL 241XDF IS DAMAGED IN A CORNER. DOT 23-027 INSPECTION FABRICATION OF FLOOR PANEL,VERIFIED RII REQUIREMENT COMPLETED, IAW UPS GMM 04.02.01.15.
- [SDR IPXA2026031770646](https://openairdocs.org/sdr/IPXA2026031770646.md): Panel · corroded · Mar 1, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO STA 1540 ON LH SIDE FLOOR ANCHOR POINT HAS CORROSION AROUND FASTENER. INSTALLED NEW REPAIR DOUBLER, NEW SIDE PANEL IAW B757-200PF, SRM 51-40-02.
- [SDR IPXA2026031763179](https://openairdocs.org/sdr/IPXA2026031763179.md): Support Channel · cracked · Mar 1, 2026 · N416UP · Boeing 75724APF · Fuselage Main, Structure
  > LEFT MLG WW, TANG DOOR FWD CUTOUT, BRACKET SUPPORT AT LOWER SIDE HAS A CRACK. REMOVED DAMAGED BRACKET SUPPORT IAW SRM 51-40-02. INSTALLED PANEL 197DL, IAW AMM 53-36-02-404-006.
- [SDR IPXA2026032658517](https://openairdocs.org/sdr/IPXA2026032658517.md): Skin · damaged · Feb 28, 2026 · N416UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, TAIL EXTERNAL FUSELAGE, BTWN BS 1896.2 - 1992.8, 11 O'CLOCK POSITION, HAS 11EA POINTS WITH LIGHTNING STRIKE DAMAGE. BONDED REPAIR DOUBLER IAW SRM 51-70-10-2R-2A.
- [SDR IPXA2026032458260](https://openairdocs.org/sdr/IPXA2026032458260.md): Rivet · sheared · Feb 28, 2026 · N416UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR. EXTERNAL LOWER FUSELAGE, BS 1460, S29R HAD A SHEAR RIVET, EVIDENCE OF CORROSION INSIDE. VERIFIED REPAIR ACCOMPLISHED PER EO-96803-REQ1 AND VT-MAE EA 757-5360-27-A4377 REV-, PRIOR TO FURTHER FLIGHT.
- [SDR IPXA2026032153766](https://openairdocs.org/sdr/IPXA2026032153766.md): Strap · corroded · Feb 28, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, APU INLET DOOR CUTOUT AFT STRAP HAS EVIDENCE OF CORROSION INSTALLED ALL PARTS OF REPAIR: FILLER MIDDLE STRAP [3], FILLER SHEAR TIE [4], STRAP [2], STRAP [1] (DOUBLER METAL) I.A.W. B757-200 SRM 53-80-15-2R-1 AND SRM 51-40-02-0G-0
- [SDR IPXA2026032054456](https://openairdocs.org/sdr/IPXA2026032054456.md): Tee Fitting · corroded · Feb 28, 2026 · N416UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > LOWER FUSELAGE, STA 1040 T-CHORD RBL 6 TO RBL 25 HAS EVIDENCE OF CORROSION AND BARE METAL INSTALLED NEW T-CHORD ON, LOWER FUSELAGE, STA 1040, IAW B757-200PF, SRM 51-40-02.
- [SDR IPXA2026032453721](https://openairdocs.org/sdr/IPXA2026032453721.md): Strap · corroded · Feb 28, 2026 · N416UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors
  > APU INLET DOOR CUTOUT FWD STRAP HAS EVIDENCE OF CORROSION INSTALLED FWD STRAP IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026031653968](https://openairdocs.org/sdr/IPXA2026031653968.md): Support Angle · corroded · Feb 28, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR CUTOUT LOWER CORNER ANGLE BRACKET HAS EVIDENCE OF CORROSION INSTALLED LOWER CORNER ANGLE I.A.W. B757-200 SRM 51-40-02-0G-0
- [SDR IPXA2026031753310](https://openairdocs.org/sdr/IPXA2026031753310.md): Support Angle · corroded · Feb 28, 2026 · N416UP · Boeing 75724APF · APU Cowling/Containment
  > APU INLET DOOR CUTOUT LOWER ANGLE SUPPORT HAS CORROSION INSTALLED 1EA NEW ANGLE IAW SRM 51-40-02-0G-0
- [SDR IPXA2026031753605](https://openairdocs.org/sdr/IPXA2026031753605.md): Support Angle · corroded · Feb 28, 2026 · N416UP · Boeing 75724APF · APU Cowling/Containment
  > APU INLET DOOR CUTOUT UPPER ANGLE SUPPORT HAS EVIDENCE OF CORROSION INSTALLED 1EA NEW UPPER ANGLE I.A.W. B757-200PF SRM 51-40-02-0G-0
- [SDR IPXA2026031653872](https://openairdocs.org/sdr/IPXA2026031653872.md): Support Angle · corroded · Feb 28, 2026 · N416UP · Boeing 75724APF · APU Cowling/Containment
  > APU INLET DOOR CUTOUT UPPER CORNER ANGLE BRACKET HAS EVIDENCE OF CORROSION INSTALLED ANGLE SUPPORT IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026032144661](https://openairdocs.org/sdr/IPXA2026032144661.md): Rib · corroded · Feb 27, 2026 · N416UP · Boeing 75724APF · Wing, Rib/Bulkhead
  > LH WING THROUGH ACCESS PANEL 561HB AILERON SUPPORT WITH CORROSION, INSTALLED NEW RIB IAW B757-200PF SRM 51-40-02.
- [SDR IPXA2026031844220](https://openairdocs.org/sdr/IPXA2026031844220.md): Floor Panel · damaged · Feb 27, 2026 · N416UP · Boeing 75724APF · Fuselage Floor Panel
  > MAJOR REPAIR, TAIL COMPARTMENT WORK PLATFORM STA 1743-1768 ANTI-SKID MATERIAL DEGRADED/DISBONDING. INSTALLED NEW FLOOBOARD IAW B757-200 SRM 51-40-02.
- [SDR IPXA2026031344908](https://openairdocs.org/sdr/IPXA2026031344908.md): Plate · cracked · Feb 27, 2026 · N416UP · Boeing 75724APF · Wing Main, Frame Structure
  > LH WING REAR SPAR AT PYLON #1 HAVE RIVETS CUT AND BRACKET BROKEN. REMOVED 2 EA BROKEN BRACKETS FROM LH WING REAR SPAR AT PYLON #1 IAW B757-200PF SRM-51-40-02-0G-0. INSTALLED NEW PART(10EA) IAW SRM 51-40-02-0G.
- [SDR IPXA2024050453307](https://openairdocs.org/sdr/IPXA2024050453307.md): Deck Plate · corroded · Apr 24, 2024 · N416UP · Boeing 75724APF · Fuselage Main, Structure
  > AFT DECK PLATE STA 1681 HAS CORROSION BETWEEN LBL 10 AND LBL 15. VERIFIED INSTALLED DOUBLER AND FILLER OK TO APPLY CIC INSP ONLY. APPLIED CIC I.A.W AMM 51-00-59-112-001.
- [SDR IPXA2024050353295](https://openairdocs.org/sdr/IPXA2024050353295.md): Deck Plate · corroded · Apr 24, 2024 · N416UP · Boeing 75724APF · Fuselage Main, Structure
  > AFT DECK PLATE STA 1681 HAS CORROSION BETWEEN RBL 10 AND RBL 15. INSTALLED DOUBLER AND FILLER I.A.W SRM 53-60-51-2R-8 PARAGRAPH 4. M TO O.VERIFIED INSTALLED DOUBLER AND FILLER OK TO APPLY CIC INSP ONLY. APPLIED CIC I.A.W AMM 51-00-59-112-001.
- [SDR IPXA2024042453307](https://openairdocs.org/sdr/IPXA2024042453307.md): Deck Plate · corroded · Apr 24, 2024 · N416UP · Boeing 75724APF · Fuselage Main, Structure
  > AFT DECK PLATE STA 1681 HAS CORROSION BETWEEN LBL 10 AND LBL 15. OPEN
- [SDR IPXA2024042453295](https://openairdocs.org/sdr/IPXA2024042453295.md): Deck Plate · corroded · Apr 24, 2024 · N416UP · Boeing 75724APF · Fuselage Main, Structure
  > AFT DECK PLATE STA 1681 HAS CORROSION BETWEEN RBL 10 AND RBL 15. OPEN
- [SDR IPXA2024051089534](https://openairdocs.org/sdr/IPXA2024051089534.md): Nut Plate · corroded · Apr 19, 2024 · N416UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > ONE EA NUTPLATE STRAP WITH CORROSION AT STA 1720 BETWEEN LBL 33.10 AND LBL 39.50 VERIFIED: INSTALLED AFT DRAIN PAN IAW B757 SRM 51-40-02-0G. VERIFIED JOB COMPLETE. REVIEWED.
- [SDR IPXA2024050289556](https://openairdocs.org/sdr/IPXA2024050289556.md): Floorbeam · corroded · Apr 19, 2024 · N416UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN CARGO DECK - FLOOR BEAM WITH CORROSION AT STA 1200 RBL 5. INSTALLED 4EA REPAIR PARTS IAW SRM 53-00-51-2R-6 AND SRM 51-40-02-0G-0. REVIEWED.
- [SDR IPXA2024042289534](https://openairdocs.org/sdr/IPXA2024042289534.md): Nut Plate · corroded · Apr 19, 2024 · N416UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > **SDR FILED OPEN** FAULT: 1 EA NUTPLATE STRAP WITH CORROSION AT STA 1720 BETWEEN LBL 33.10 AND LBL 39.50 APPROVED.
- [SDR IPXA2024042289556](https://openairdocs.org/sdr/IPXA2024042289556.md): Floorbeam · corroded · Apr 19, 2024 · N416UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > **SDR FILED OPEN** FAULT: MAIN CARGO DECK - FLOOR BEAM WITH CORROSION AT STA 1200 RBL 5 VERIFIED OUT OF LIMITS
- [SDR IPXA2024041966153](https://openairdocs.org/sdr/IPXA2024041966153.md): Frame · dented · Apr 18, 2024 · N416UP · Boeing 75724APF · Fuselage Main, Frame
  > FWD CARGO PIT FRAME STA 720 RH HAS A DENT ON INBOARD CHORD BETWEEN STR 24R/25R APPROVED. OPEN
- [SDR IPXA2024041966275](https://openairdocs.org/sdr/IPXA2024041966275.md): Frame · dented · Apr 18, 2024 · N416UP · Boeing 75724APF · Fuselage Main, Frame
  > **SDR FILED OPEN**FAULT: FWD CARGO PIT FRAME STA 820 LH HAS A DENT ON INBOARD CHORD BETWEEN STR 24L/25L APPROVED.
- [SDR IPXA2024041966665](https://openairdocs.org/sdr/IPXA2024041966665.md): Frame · dented · Apr 18, 2024 · N416UP · Boeing 75724APF · Fuselage Main, Frame
  > FWD CARGO PIT FRAME STA 800 LH HAS A DENT ON INBOARD CHORD BETWEEN STR 24/25L APPROVED. OPEN
- [SDR IPXA2024041966254](https://openairdocs.org/sdr/IPXA2024041966254.md): Frame · dented · Apr 18, 2024 · N416UP · Boeing 75724APF · Fuselage Main, Frame
  > FWD CARGO PIT FRAME STA 780 RH HAS A DENT ON INBOARD CHORD AT STR 24R APPROVED. OPEN
- [SDR IPXA2024050429715](https://openairdocs.org/sdr/IPXA2024050429715.md): Frame · dented · Apr 16, 2024 · N416UP · Boeing 75724APF · Fuselage Main, Frame
  > AFT CARGO PIT - FRAME STA 1500 RH SIDE HAS A DENT ON TOP OF AN EXISTING REPAIR. REF STEP 65. INSPECTED AND VERIFIED ACCOMPLISHED EA# 757-5360-27-A3576 STEP 24 PRELIM 1. INSP ONLY. FRAME BS 1500 RT SIDE HAS A DENT ON TOP OF AN EXISTING REPAIR. JOB ACCOMPLISH
- [SDR IPXA2023111605008](https://openairdocs.org/sdr/IPXA2023111605008.md): Light · inoperative · Nov 15, 2023 · N416UP · Boeing 75724APF · Emergency Lighting
  > FAULT: MXP-5067-JIC--L1 DOOR EMERGENCY LIGHT INOP INSTALLED L1 DOOR BATTERY IAW MM 33-51-01. OPS CHECKED GOOD IAW MM 33-51-01-962-001. AUDIT COMPLETE
- [SDR IPXA2022042381417](https://openairdocs.org/sdr/IPXA2022042381417.md): Structure · corroded · Apr 23, 2022 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SEG2WING TO BODY STRUCTURE AT FS 1180-1240 RBL 57.5 HAS INTERGRANULAR CORROSION.REMOVED CORRODED T CHORD SECTION AND INSTALLED REPLACEMENT T CHORD SECTION USING BAC1505-100403 PER TRAVELER# T22/1612520 AND SRM 51-40-02-0G
- [SDR IPXA2022042681493](https://openairdocs.org/sdr/IPXA2022042681493.md): Bracket · cracked · Apr 18, 2022 · N416UP · Boeing 75724APF · Engine (Turbine/Turboprop)
  > INSPECTION TYPE:C#1 ENGINE L/H PYLON O/B MID SPAR LOWER ATTACHMENT BRACKET IS CRACKED IN THE RADIUS CORNER 2.35" LONGREMOVED CRACKED BRACKET AND INSTALLED REPLACEMENT 311N3570-84 BATCH NUMBER 3940996 PER SRM 51-40-02
- [SDR IPXA2022042681494](https://openairdocs.org/sdr/IPXA2022042681494.md): Structure · corroded · Apr 14, 2022 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:CWING TO BODY SUPPORT STRUCTURE AT FS 1200 FROM WL 208 TO 133 RBL 70 HAS EXFOLIATED CORROSIONREMOVED AND REPLACED WITH TO BODY LOWER T CHORD SEGMENT PER SRM 51-40-02-0G
- [SDR IPXA2022042681497](https://openairdocs.org/sdr/IPXA2022042681497.md): Structure · corroded · Apr 13, 2022 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:CWING TO BODY SUPPORT STRUCTURE LOWER T CHORD AT FS 1180-1240 LBL 57.5 IS EXFOLIATEDREMOVED AND REPLACED WING TO BODY LOWER T CHORD SEGMENT PER SRM 51-40-02-0G
- [SDR IPXA2022042881539](https://openairdocs.org/sdr/IPXA2022042881539.md): Structure · corroded · Apr 12, 2022 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:CWING TO BODY STRUCTURE LOWER T CHORD AT FS 1180 TO FS 1240 RBL 50 LOWER FLANGE WAS EXFOLIATEDREMOVED AND REPLACED LOWER T CHORD PER SRM 51-40-02-0G
- [SDR IPXA2022042881538](https://openairdocs.org/sdr/IPXA2022042881538.md): Structure · corroded · Apr 11, 2022 · N416UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:CWING TO BODY STRUCTURE LOWER T CHORD AT FS 1180 FROM BL 0 TO RBL 70 IS EXFOLIATED ON UPPER FLANGE.REMOVED AND REPLACED LOWER T CHORD PER SRM 51-40-02-0G
- [SDR IPXA2022042681498](https://openairdocs.org/sdr/IPXA2022042681498.md): Bracket · cracked · Apr 11, 2022 · N416UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE:C#2 ENGINE PYLON AFT FAIRING FWD LOWER CORNER THE 313N3052-17 BRACKET IS CRACKEDREMOVED AND REPLACED BRACKET PER SRM 51-40-02-0G
- [SDR IPXA2022042581448](https://openairdocs.org/sdr/IPXA2022042581448.md): Frame · dented · Apr 11, 2022 · N416UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:CAFT LOWER CARGO PIT FRAME AT FS 1520 BETWEEN STR 25R TO 26R HAS A DENT ON UPPER FLANGE OF FRAMEREPAIRED FRAME 1520 PER SRM 53-00-07-2R-5
- [SDR IPXA2022050581792](https://openairdocs.org/sdr/IPXA2022050581792.md): Frame · damaged · Apr 9, 2022 · N416UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:CNEEDED ALTERNATIVE METHOD TO INSPECT FRAME 1600 RH PER EO# B757-5310-73926-AMODIFIED REPAIR AT FR 1600 RH STR 26R PER EA# 757-5360-27-A2897
- [SDR IPXA2022050581791](https://openairdocs.org/sdr/IPXA2022050581791.md): Frame · damaged · Apr 9, 2022 · N416UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:CNEEDED ALTERNATIVE METHOD TO INSPECT FRAME 1560 LH PER EO# B757-5310-73926-AMODIFIED REPAIR AT FR 1560 STR 26L PER EA# 757-5360-27-A2892
- [SDR IPXA2022050581790](https://openairdocs.org/sdr/IPXA2022050581790.md): Frame · damaged · Apr 9, 2022 · N416UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:CNEEDED ALTERNATIVE METHOD TO INSPECT FRAME 1300 LH PER EO# B757-5310-73926-AMODIFIED REPAIR AT FR 1300 STR 26L PER EA# 757-5360-27-A2901-A

Next page: https://openairdocs.org/aircraft/N416UP/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 = 'N416UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N416UP/reports

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