# Service difficulty reports: N272NV

A list on [N272NV](https://openairdocs.org/aircraft/N272NV.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR WX0A2025121732672](https://openairdocs.org/sdr/WX0A2025121732672.md): Megaphone · inoperative · Dec 15, 2025 · N272NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD MEGAPHONE INOPERATIVE. REMOVED AND REPLACED THE FWD MEGAPHONE.
- [SDR WX0A2025102932617](https://openairdocs.org/sdr/WX0A2025102932617.md): Power Supply · no test · Oct 28, 2025 · N272NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) EPSU FAILED BITE CHECK. EPSU TEST PANEL SHOWS BATT FAIL ILLUMINATED. REMOVED AND REPLACED 10WL EPSU BATT PACK IAW AMMS 33-51-38-000-002-A/33-51-38-400-002-A. BITE CHECK GOOD.
- [SDR WX0A2025092232573](https://openairdocs.org/sdr/WX0A2025092232573.md): Battery · inoperative · Sep 19, 2025 · N272NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD O/B FLIGHT ATTND JUMPSEAT FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED BATTERY AT FWD F/A JUMPSEAT FLASHLIGHT IAW A320 AMM 25-65-00-00. OPS CHECK GOOD.
- [SDR WX0A2025090532556](https://openairdocs.org/sdr/WX0A2025090532556.md): Girt Bar · out of adjust · Sep 4, 2025 · N272NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FA UNABLE TO ARM THE SLIDE ON R1 DOOR, LEVER WILL NOT COME DOWN FULLY / FOUND ESCAPE SLIDE GIRT FLAP TO BE NOT ADJUSTED CORRECTLY, READJUSTED GIRT FLAP. OPS CHECK GOOD. REF AMM 25-62-44-400-802-A AND AMM 52-10-00-860-001-A. A/C OK FOR S
- [SDR WX0A2025090232552](https://openairdocs.org/sdr/WX0A2025090232552.md): Battery · discharged · Sep 1, 2025 · N272NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD MEGAPHONE BATTERY DEAD / R&R MEGAPHONE BATTERIES REF AMM 25-65-51-920-001-A"
- [SDR WX0A2025050532414](https://openairdocs.org/sdr/WX0A2025050532414.md): Battery Pack · no test · May 4, 2025 · N272NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) DURING EPSU BAT CAP TEST 13WL BATTERY FAULT. / REMOVED AND REPLACED EPSU BATTERY 13WL PER AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPERATIONAL CHECK SATISFACTORY PER 33-51-00-710-001-A AND AMM 23-73-00-740-005-B."
- [SDR EE4Y2025040822152](https://openairdocs.org/sdr/EE4Y2025040822152.md): Skin · bulged · Apr 8, 2025 · N272NV · Airbus A320214 · Wing, Plate/Skin
  > LEFT WING REAR SPAR, TOP SKIN LOWER SURFACE OVERHANG AREA BETWEEN RIB 13 AND RIB 15 SEAL PLATE BULGED. PERFORMED BLEND OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN RIB 13 AND RIB 15 IAW COOPESA EO N° COO-EO-2025-21701-R02 DATED 03/21/2025. APPR
- [SDR EE4Y2025040822151](https://openairdocs.org/sdr/EE4Y2025040822151.md): Skin · none · Apr 8, 2025 · N272NV · Airbus A320214 · Standard Practices/Structures
  > L/H WING BOX TOP SKIN PANEL 2 TRAILING EDGE OVERHANG AT RIB 10 BETWEEN FASTENER #437 AND FASTENER #455 REMOVE EXISTING EXTERNAL REPAIR PLATE. PERFORMED BLEND OUT REPAIR AT LOWER SURFACE UNDER REPAIR PLATE RIB 9 TO RIB 11 AND O/B OF THE REPAIR PLATE RIB 10 TO R
- [SDR EE4Y2025040822150](https://openairdocs.org/sdr/EE4Y2025040822150.md): Skin · corroded · Apr 8, 2025 · N272NV · Airbus A320214 · Wing, Plate/Skin
  > LH WING BOX TOP SKIN TRAILING EDGE OVERHANG AREA LOWER SURFACE EXISTING BLEND OUT WITH CORROSION AT RIB 14+400MM. PERFORMED BLEND OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE AT RIB 14+400MM (AREA 7) IAW COOPESA EO N° COO-EO-2025-21701-R02 DATED 03/21/
- [SDR EE4Y2025040722149](https://openairdocs.org/sdr/EE4Y2025040722149.md): Skin Panel · corroded · Apr 7, 2025 · N272NV · Airbus A320214 · Wing, Plate/Skin
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-572178-01-1-001 SECONDARY FINDING LH WING BOX TOP SKIN TEOH UPPER SURFACE WITH CORROSION BETWEEN WX= 4010,2 AND WX= 4390,2. PERFORMED BLEND OUT REPAIRON LH WING TOP SKIN PANEL 2 UPPER SURFACE BETWEEN WX 3494,5 A
- [SDR EE4Y2025040722148](https://openairdocs.org/sdr/EE4Y2025040722148.md): Skin · corroded · Apr 7, 2025 · N272NV · Airbus A320214 · Wing, Plate/Skin
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-572178-01-1-001 LEFT WING BOX TOP SKIN TRAILING EDGE OVERHANG LOWER SURFACE SKIN WITH CORROSION AT WX=3654,5. PERFORMED BLEND OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN WX 3494,5 AND WX 4010,2
- [SDR EE4Y2025040722147](https://openairdocs.org/sdr/EE4Y2025040722147.md): Skin Panel · corroded · Apr 7, 2025 · N272NV · Airbus A320214 · Wing, Plate/Skin
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-572178-01-1-001 LEFT WING TOP SKIN LOWER SURFACE OVERHANG AREA AT WX 4274 WITH CORROSION WAS FOUND. PERFORMED BLENT OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN WX 3494.5 AND WX 4490.52 (AREA 2)
- [SDR EE4Y2025040722146](https://openairdocs.org/sdr/EE4Y2025040722146.md): Skin Panel · corroded · Apr 7, 2025 · N272NV · Airbus A320214 · Wing, Plate/Skin
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-572179-01-1-001 LEFT WING REAR SPAR TOP SKIN LOWER SURFACE OVER HANG AREA 11 AND 12 SEAL PLATE BULGED WAS FOUND. PERFORMED BLEND OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN RIB 11/12 (AREA 6) I
- [SDR EE4Y2025040722145](https://openairdocs.org/sdr/EE4Y2025040722145.md): Fitting · cracked · Apr 7, 2025 · N272NV · Airbus A320214 · Fuselage Main, Structure
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT EO A32X-E5311-0013 WINDSHIELD CENTRAL NODE CONTINUTIY FITTING OINLY REPLACMENT REPAIR. PERFORMED EO E5311-0013-R00 AD 2020-17-03 WNDISHIELD CENTRAL LOWER NODE CONTINUITY FITTING ONLY REPLACMENT REPAIR.THIS REPAIR WAS DOCU
- [SDR EE4Y2025040722143](https://openairdocs.org/sdr/EE4Y2025040722143.md): Door Frame · cracked · Apr 7, 2025 · N272NV · Airbus A320214 · Fuselage Main, Structure
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-002 UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR66 LH DOOR STOP FITTING # 3 UPPER OUTBOARD HOLE WITH CRACK INDICATION WAS FOUND. PERFORMED OVERSIZE BOLTS INSTALLATION ON AFT PAX CABIN CREW ENTRY DOOR A
- [SDR EE4Y2025040722141](https://openairdocs.org/sdr/EE4Y2025040722141.md): Frame · cracked · Apr 7, 2025 · N272NV · Airbus A320214 · Fuselage, Wing Attach Fittings
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-002 UPPER FUSELAGE AFT PAX CABIN CREW ENTRY DOOR FR66 RH DOOR STOP FITTING # 5 UPPER OUTBOARD HOLE WITH CRACK WAS FOUND. PERFORMED OVERSIZE BOLTS INSTALLATION ON AFT PAX CABIN ENTRY DOOR AT FRE66 RH DOOR
- [SDR EE4Y2025040722142](https://openairdocs.org/sdr/EE4Y2025040722142.md): Frame · cracked · Apr 7, 2025 · N272NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-002 UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR66 DOOR STOP FITTING # 4 UPPER OUTBOARD HOLE WITH CRACK. PERFORMED OVERSIZE BOLTS INSTALLATION ON AFT PAX CABIN ENTRY DOOR AT FR66 RH DOOR STOP FITTING #
- [SDR EE4Y2025040722140](https://openairdocs.org/sdr/EE4Y2025040722140.md): Frame · cracked · Apr 7, 2025 · N272NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-003 UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR68RH DOOR STOP FITTING # 7 UPPER OUTBOARD HOLE WITH CRACK. PERFORMED FREEZE PLUG AND OVERSIZE BOLT INSTALLATION AT FR68RH DOOR STOP FITTING # 7 UPPER INB
- [SDR EE4Y2025040622139](https://openairdocs.org/sdr/EE4Y2025040622139.md): Door Frame · cracked · Apr 6, 2025 · N272NV · Airbus A320214 · Fuselage Main, Structure
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 2022-08-08-30200/2 UPPER FUSELAGE FORWARD ENTRY PASSENGER /CREW DOOR FR16 RHDOUGLE JOGGLE AREA STOP FITTING # 7 HOLE # 4 WITH CRACK INDICATION IN FRAME LAYER WAS FOUND. REPAIRED FUSELAGE FRAME AT DOUBLE JOGGLE AREA
- [SDR EE4Y2025040622138](https://openairdocs.org/sdr/EE4Y2025040622138.md): Door Frame · cracked · Apr 6, 2025 · N272NV · Airbus A320214 · Fuselage Main, Structure
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-002 UPPER FUSELAGE AFT PAX CABIN CREW ENTRY DOOR FR66 LH DOOR STOP FITTING # 1 LOWER INBOARD HOLE WITH CRACK INDICATION WAS FOUND.PERFORMED FREEZE PLUG AND OVER SIZE BOLTS INSTALLATION AT FR66LH DOOR STOP
- [SDR EE4Y2025040622137](https://openairdocs.org/sdr/EE4Y2025040622137.md): Door Frame · cracked · Apr 6, 2025 · N272NV · Airbus A320214 · Fuselage Main, Structure
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-003 UPPER FUSELAGE AFT PAX CABIN CREW ENTRY DOOR FR68 RH DOR STOP FITTING # 1 HOLE WITH CRACK WAS FOUND.PERFORMED PERMANENT REPAIR ON FUSELAGE FRAME AT FR68RH STOP FITTING #1 IAW A320 SRM TASK 53-41-12-30
- [SDR EE4Y2025040622136](https://openairdocs.org/sdr/EE4Y2025040622136.md): Door Frame · cracked · Apr 6, 2025 · N272NV · Airbus A320214 · Fuselage Main, Structure
  > DURING ALLEGAINT TASK ACCOMPLISHMENT TASK A32X-53-260-003 UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR, FR68 LH DOOR STOP FITTING # 1 LOWER INBOARD HOLE WITH CRACK WAS FOUND.PERFORMED PERMANENT REPAIR ON FUSELAGE FRAME SECTION AT FR68 LH STOP FITTING # 1 IAW A
- [SDR WX0A2025010232246](https://openairdocs.org/sdr/WX0A2025010232246.md): Plug · stripped · Jan 2, 2025 · N272NV · Airbus A320214 · Turbine Engine Compressor Section
  > (AIRCRAFT NOT GROUNDED) APPROX HALFWAY THROUGH THE FLIGHT AT FL280. THE FA'S REPORTED THAT THERE WAS A MUSTY ODOR IN THE AFT CABIN WHICH THEN CLEARED APPROX. 10 MINS LATER. REFER TO REPORT SOF-500 / REF WO 510916 TASK CARD 21-000-002. DURING TASK CARD FOUND LO
- [SDR WX0A2024102332204](https://openairdocs.org/sdr/WX0A2024102332204.md): Battery · failed · Oct 22, 2024 · N272NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD AED BATTERY FAIL WARNING MESSAGE / REMOVED & REPLACED AED BATTERY I.A.W. AMM 25-64-10-960-005A. PN OFF = 989803139301........ SN OFF = 79401P. PN ON = 989803139301......... SN ON = 04802P"
- [SDR WX0A2024080732148](https://openairdocs.org/sdr/WX0A2024080732148.md): Megaphone · inoperative · Aug 5, 2024 · N272NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FORWARD FLIGHT ATTENDENT MEGAPHONE INOP / REMOVED AND REPLACED FORWARD MEGAPHONE. OPS CHECK GOOD. REFERENCE ALLEGIANT AIR LOPA"
- [SDR WX0A2024042232019](https://openairdocs.org/sdr/WX0A2024042232019.md): Flashlight · no test · Apr 18, 2024 · N272NV · Airbus A320214 · Emergency Equipment
  > EMERGENCY FLASHLIGHT UNDER JUMPSEAT #4 IS NOT FLASHING RED TEST LIGHT / REMOVED AND RESEATED #4 FA FLASHLIGHT IAW STANDARD INDUSTRY PRACTICES. OPS CHECK GOOD. PLACARDS REMOVED. THIS CLEARS DMI 117255.
- [SDR WX0A1900010031960](https://openairdocs.org/sdr/WX0A1900010031960.md): Pressure Switch · faulted · Jan 25, 2024 · N272NV · Airbus A320214 · APU Oil System
  > APU AUTO SHUTDOWN INFLIGHT / PER TSM 49-00-81-810-819-A, REPLACED LOW OIL PRESSURE SWITCH PER AMM 49-94-14-000-003-A AND LEAK CHECKED, NO LEAKS NOTED AND SERVICED APU OIL PER AMM 49-90-00-600-007-A (REASON FOR DELAYED REPORT: REGULATORY INTERPRETATION REEVALUA
- [SDR WX0A2024012231949](https://openairdocs.org/sdr/WX0A2024012231949.md): Megaphone · inoperative · Jan 20, 2024 · N272NV · Airbus A320214 · Emergency Equipment
  > FWD MEGAPHONE INOP / FWD CABIN MEGAPHONE REPLACED IAW DWG A2250020L03 REV 01."
- [SDR WX0A2023092531850](https://openairdocs.org/sdr/WX0A2023092531850.md): Unknown · unknown · Sep 22, 2023 · N272NV · Airbus A320214 · Emergency Equipment
  > REAR AND FRONT MEGAPHONE CHANGE BELOW 50% (NO GREEN LIGHT) / REPLACED FWD AND AFT MEGAPHONE BATTERIES IAW AMM 25-65-51 PB 201.A.C OK FOR SERVICE"
- [SDR WX0A2023090531828](https://openairdocs.org/sdr/WX0A2023090531828.md): Megaphone · unknown · Sep 4, 2023 · N272NV · Airbus A320214 · Emergency Equipment
  > FWD MEGAPHONE TIME EXPIRED. / REMOVED AND INSTALLED AFT MEGAPHONE PER L.O.P.A. PERFORMED OPS CHECKS PER AMM 25-65-51-710-002. OPS CHECKS GOOD."
- [SDR WX0A2023090531827](https://openairdocs.org/sdr/WX0A2023090531827.md): Megaphone · unknown · Sep 2, 2023 · N272NV · Airbus A320214 · Emergency Equipment
  > FOUND AFT MEGAPHONE EXPIRED. / REMOVED AND INSTALLED AFT MEGAPHONE PER AMM 25-65-51-920-001-A. PERFORMED OPS CHECKS PER AMM 25-65-51-710-002. OPS CHECKS GOOD."
- [SDR WX0A2022113031667](https://openairdocs.org/sdr/WX0A2022113031667.md): Battery Pack · faulted · Nov 30, 2022 · N272NV · Airbus A320214 · Emergency Lighting
  > DURING TC 33-51-00-710-003-A EPSU BATTERY 12WL FAULTED. REMOVED AND REPLACED THE EPSU BATTERY 12WL IAW AMM 33-51-38-400-002-A.
- [SDR WX0A2022090674229](https://openairdocs.org/sdr/WX0A2022090674229.md): Megaphone · none · Sep 5, 2022 · N272NV · Airbus A320214 · Escape Slide
  > DURING WEEKLY CHECK FOUND AFT MEGAPHONE INOP / REMOVED AND REPLACED BATTERIES IAW AMM 25-65-51, NO HELP. REMOVED AND REPLACED MEGAPHONE IAW LOPA DRAWING# A2250011L03, OPS CHECKS GOOD."
- [SDR WX0A2022090674228](https://openairdocs.org/sdr/WX0A2022090674228.md): Epsu · none · Sep 5, 2022 · N272NV · Airbus A320214 · Emergency Lighting
  > DURING WEEKLY CHECK, PERFORMED OPS TEST OF EMERGENCY LIGHTS. FOUND 10WL EPSU DISPLAYING UNIT FAULT RED LIGHT. / PER TSM 33-51-00-810-822-A REMOVED AND REPLACED ESPU (10WL) IAW AMM 33-51-38."
- [SDR WX0A2022090674227](https://openairdocs.org/sdr/WX0A2022090674227.md): Epsu · none · Sep 5, 2022 · N272NV · Airbus A320214 · Lighting System
  > DURING WEEKLY CHECK FOUND EPSU (12WL) EMER R FAILING. / REMOVED AND REPLACED 12WL BATTERY WITH INSPECTED BATTERY IAW AMM 33-51-38-000-002-A. OPS CHECK GOOD FOR EMER R."
- [SDR WX0A2022020473952](https://openairdocs.org/sdr/WX0A2022020473952.md): Megaphone · inoperative · Feb 3, 2022 · N272NV · Airbus A320214 · Escape Slide
  > FWD MEGAPHONE INOP / REMOVED AND REPLACED MEGAPHONE IAW AMM 25-65-51. OPS CHECK GOOD."
- [SDR WX0A1900010073985](https://openairdocs.org/sdr/WX0A1900010073985.md): Skin · corroded · Feb 1, 2022 · N272NV · Airbus A320214 · Wing, Plate/Skin
  > NRC 5000-0011: ( 2062-08) L/H WING UPPER SURFACE, FWD OF SPOILER #1 CORROSION FOUND / LH WING UPPER SURFACE, FWD OF SPOILER #1 CORROSION REMOVED AND FOUND STRUCTURALLY ACCEPTABLE IAW AIRBUS DOSSIER # 80111252 AND COMPLY IAW REPAIR DRAWING R572-58616 ISSUE K A
- [SDR WX0A2021120873886](https://openairdocs.org/sdr/WX0A2021120873886.md): Epsu · failed · Dec 7, 2021 · N272NV · Airbus A320214 · Emergency Lighting
  > EPSU BATTERY FAIL DURING CAP CHECK TC / REMOVED AND REPLACED EPSU BATTERY, FIN 11WL, IAW AMM 31-51-38. OPS CHECK GOOD."
- [SDR WX0A2021051273713](https://openairdocs.org/sdr/WX0A2021051273713.md): Megaphone · inoperative · May 10, 2021 · N272NV · Airbus A320214 · Emergency Equipment
  > CABIN EMERGENCY MEGAPHONE INOP / REPLACED MEGAPHONE BATTERIES IAW AMM 25-65-51-920-001-A OPS CK GOOD."
- [SDR WX0A2020080373541](https://openairdocs.org/sdr/WX0A2020080373541.md): Battery Pack · no test · Aug 1, 2020 · N272NV · Airbus A320214 · Emergency Lighting
  > EPSU BATTERY (12WL) FAILED BATTERY CAP TEST. / REMOVED AND REPLACED BATTERY IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK GOOD."
- [SDR WX0A2020071373526](https://openairdocs.org/sdr/WX0A2020071373526.md): Battery Pack · no test · Jul 10, 2020 · N272NV · Airbus A320214 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED, REPLACED THE BATTERY AT 10WL IAW MM 33-51-38-000-002-A AND MM 33-51-38-400-02-A. OPS CHECKED GOOD IAW MM 33-51-00-710-001-A.
- [SDR DU4R20180412005](https://openairdocs.org/sdr/DU4R20180412005.md): Skin Panel · corroded · Apr 12, 2018 · N272NV · Airbus A320216 · Wing, Plate/Skin
  > DURING SCHEDULED C CHECK FOUND CORROSION BETWEEN RIB 19 - 20 AT BONDING SPIGOT ON LT WING, TOP SKIN, PANEL 2, UPPER SURFACE.
- [SDR DU4R20180409004](https://openairdocs.org/sdr/DU4R20180409004.md): Skin · corroded · Apr 9, 2018 · N272NV · Airbus A320214 · Wing, Plate/Skin
  > DURING C-CHECK CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LT NR 1 SKIN PANEL BETWEEN RIBS 1 AND 2 AT THE FRONT SPAR. CORROSION REMOVAL EXCEEDED SRM LIMITS.
- [SDR DU4R20180313003](https://openairdocs.org/sdr/DU4R20180313003.md): Attach Fitting · gouged · Mar 7, 2018 · N272NV · Airbus A320214 · Elevator Structure
  > RIGHT OUTBOARD ELEVATOR ACTUATOR ATTACH FITTING GOUGED.
- [SDR DU4R20180301002](https://openairdocs.org/sdr/DU4R20180301002.md): Door Sill · corroded · Mar 1, 2018 · N272NV · Airbus A320214 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL HAS CORROSION ON UPPER SURFACE AT FASTENER HOLE FRAME 68, STRINGER 23L.
- [SDR DU4R20180301001](https://openairdocs.org/sdr/DU4R20180301001.md): Door Sill · corroded · Mar 1, 2018 · N272NV · Airbus A320214 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL FASTENER HOLE HAS CORROSION ON UPPER SURFACE FRAME 67 + 14, STRINGER 23R.

## 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 = 'N272NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N272NV/reports

---
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