# Service difficulty reports: Boeing 727-2S2F

A list on [Boeing 727-2S2F](https://openairdocs.org/model/boeing-727-2s2f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 17 · 842 reports

- [SDR VGCA20260917001](https://openairdocs.org/sdr/VGCA20260917001.md): Engine · making metal · Sep 17, 2026 · N215WE · Boeing 7272S2F · Engine (Turbine/Turboprop)
  > ENGINE OIL BYPASS INDICATION. METAL IN OIL FILTER
- [SDR VGCA20251024009](https://openairdocs.org/sdr/VGCA20251024009.md): Skin Panel · damaged · Oct 24, 2025 · N215WE · Boeing 7272S2F · Elevator, Plate/Skin
  > R/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANEL 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21
- [SDR VGCA20251024020](https://openairdocs.org/sdr/VGCA20251024020.md): Frame · punctured · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1110 BETWEEN STRINGER 25R AND 28R.
- [SDR VGCA20251024019](https://openairdocs.org/sdr/VGCA20251024019.md): Frame · punctured · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1090 BETWEEN STRINGER 26R AND 28R
- [SDR VGCA20251024018](https://openairdocs.org/sdr/VGCA20251024018.md): Frame · dented · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME INNER CHORD DENT AT BS 1070 BETWEEN STRINGER 25R AND 29R
- [SDR VGCA20251024017](https://openairdocs.org/sdr/VGCA20251024017.md): Frame · dented · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME INNER CHORD DENT AT BS 1050 BETWEEN STRINGER 26R AND 28R
- [SDR VGCA20251024016](https://openairdocs.org/sdr/VGCA20251024016.md): Floorbeam · corroded · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Floor Beam
  > FUSELAGE FLOOR STABILIZER BEAM MULTIPLE SPOTS CORROSION AT BL 0 BETWEEN BS 449.94 AND BS 720+9.94
- [SDR VGCA20251024015](https://openairdocs.org/sdr/VGCA20251024015.md): Frame · gouged · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME INNER CHORD GOUGED AT BS 1130 BETWEEN STRINGER 26L AND 28L
- [SDR VGCA20251024014](https://openairdocs.org/sdr/VGCA20251024014.md): Frame · gouged · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME INNER CHORD GOUGED AT BS 1110 BETWEEN STRINGER 26L AND 28L
- [SDR VGCA20251024013](https://openairdocs.org/sdr/VGCA20251024013.md): Frame · punctured · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1090 BETWEEN STRINGER 26L AND 28L
- [SDR VGCA20251024012](https://openairdocs.org/sdr/VGCA20251024012.md): Skin · dented · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN GOUGE/DENT REPAIRED BELOW MCD BETWEEN BS 460 AND BS 620, AND BETWEEN STRINGER 15L-20L
- [SDR VGCA20251024011](https://openairdocs.org/sdr/VGCA20251024011.md): Frame · punctured · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1070 BETWEEN STRINGER 26L AND 29L
- [SDR VGCA20251024010](https://openairdocs.org/sdr/VGCA20251024010.md): Shear Tie · corroded · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Internal Mounting Structure
  > FUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R.
- [SDR VGC2025F00000](https://openairdocs.org/sdr/VGC2025F00000.md): Frame · corroded · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R
- [SDR VGCA202511254009](https://openairdocs.org/sdr/VGCA202511254009.md): Skin Panel · damaged · Oct 24, 2025 · N215WE · Boeing 7272S2F · Horizontal Stabilizer, Plate/Skin
  > R/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANELS 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21 REPAIRED AND INSTALLED I.A.W. V1 AEROSPACE DOC. NO. R24-02464-001, REVISION 6,DATE OCTOBER 03.2025
- [SDR VGCA202511254008](https://openairdocs.org/sdr/VGCA202511254008.md): Skin Panel · damaged · Oct 24, 2025 · N215WE · Boeing 7272S2F · Elevator, Plate/Skin
  > RIGHT HORIZONTAL STABILIZER UPPER T/E DAMAGED PANELS 65-20658-24 BETWEEN ELEV. STA. 99.79 AND 173.21 REPAIRED AND INSTALLED IAW. R24-02464-001, REVISION 6,DATE OCTOBER 03.2025.
- [SDR VGCA20251024007](https://openairdocs.org/sdr/VGCA20251024007.md): Beam · corroded · Oct 24, 2025 · N215WE · Boeing 7272S2F · Horizontal Stabilizer Miscellaneous Structure
  > R/H SIDE H-STAB. TRAILING EDGE BEAM UPPER SURFACE CORROSION REPAIRED BY REPLACEMENT OF R/H TRAILING EDGE UPPER BEAM ENTIRE LENGTH BETWEEN ELEVATOR STATION 10 AND ELEVATOR STATION 209.90 I.A.W BOEING DRAWING 65-22987, SHEET 5, REVISION C.
- [SDR VGCA20251024006](https://openairdocs.org/sdr/VGCA20251024006.md): Floorbeam · corroded · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Floor Beam
  > FUSELAGE TRANSVERSE FLOOR BEAM UPPER FLANGE CORROSION DAMAGE AT BS 740 BETWEEN LBL 45 AND LBL 62
- [SDR VGCA20251024005](https://openairdocs.org/sdr/VGCA20251024005.md): Frame · dented · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME INNER CHORD DENTED AT BS 1050 BETWEEN STRINGER 25L AND 28L
- [SDR VGCA20251024004](https://openairdocs.org/sdr/VGCA20251024004.md): Frame · cracked · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME INNER CHORD CRACK AT BS 660 BETWEEN STRINGER 27L AND 27R
- [SDR VGCA20251024003](https://openairdocs.org/sdr/VGCA20251024003.md): Frame · cracked · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME INNER CHORD CRACK AT BS 640 BETWEEN STRINGER 28L AND 27R
- [SDR VGCA20251024002](https://openairdocs.org/sdr/VGCA20251024002.md): Frame · dented · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME INNER CHORD DENT AT BS 1148 BETWEEN STRINGER 25R AND 28R
- [SDR VGCA20251024001](https://openairdocs.org/sdr/VGCA20251024001.md): Frame · dented · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame
  > FUSELAGE FRAME INNER CHORD DENTS AT BS 1130 BETWEEN STRINGER 24R AND 28R
- [SDR VGCA20250805029](https://openairdocs.org/sdr/VGCA20250805029.md): Spar Web · elongated · Aug 5, 2025 · N216WE · Boeing 7272S2F · Wing Spar
  > ELONGATED HOLE ON VERTICAL STIFFENER WEB IN CENTER FUEL TANK FRONT SPAR AT LBL40
- [SDR VGCA20250805028](https://openairdocs.org/sdr/VGCA20250805028.md): Skin · cracked · Aug 5, 2025 · N216WE · Boeing 7272S2F · Wing, Plate/Skin
  > CRACKED AT THE SLAT HOOK CUT-OUT IN THE AFT CORNER. AT WS 519 ON THE RIGHT WING
- [SDR VGCA20250805027](https://openairdocs.org/sdr/VGCA20250805027.md): Bear Strap · corroded · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > CORROSION ON BEAR STRAP, DOUBLER, AND FUSLAGE EXTERNAL SKIN AT AFT CONER OF AFT CARGO DOOR FROM FS965 TO FS1010 AND STR S-21R TO S-29L
- [SDR VGCA20250805026](https://openairdocs.org/sdr/VGCA20250805026.md): Beam · corroded · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Structure
  > RIGHT OTBD END OF THE SIDELOAD BEAM CORRODED. CENTER FUSELAGE BULKHEAD SIDELOAD BEAM CORRODED AT BS740 FROM LBL30 TO RBL30
- [SDR VGCA20250815025](https://openairdocs.org/sdr/VGCA20250815025.md): Floorbeam · corroded · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Floor Beam
  > FORWARD UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER AND LOWER CHORDS CORROSION AT BS720 FROM LBL65-RBL50
- [SDR VGCA20250815024](https://openairdocs.org/sdr/VGCA20250815024.md): Fastener · wrong part · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Frame
  > NONPRODUCTION FASTENER INSTALLED @ AFT LOWER FUSELAGE FRAME REPAIRED AT BS1166 FROM S-25L TO S-28L
- [SDR VGCA20250805023](https://openairdocs.org/sdr/VGCA20250805023.md): Frame · misrepaired · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Frame
  > NON-PRODUCTION FASTENERS INSTALLED.AFT LOWER FUSELAGE FRAME REPAIRED AT BS1050 FROM S-25L TO S-28L
- [SDR VGCA20250805022](https://openairdocs.org/sdr/VGCA20250805022.md): Floorbeam · corroded · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Floor Beam
  > AFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORRODED AT BS1030 FROM LBL10 TO LBL20.
- [SDR VGCA20250805021](https://openairdocs.org/sdr/VGCA20250805021.md): Vertical Beam · corroded · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Bulkhead
  > VERTICAL BEAM CORRODED AT LOWER END. REPAIRED AT BL 0 BS 1183.
- [SDR VGCA20250805020](https://openairdocs.org/sdr/VGCA20250805020.md): Frame · punctured · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Frame
  > AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1148 FROM S-25R TO S-28R.
- [SDR VGCA20250805019](https://openairdocs.org/sdr/VGCA20250805019.md): Window Frame · corroded · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Structure
  > AFT UPPER FUSELAGE WINDOW FRAMES CORROSION FROM BS950A-950C AND S-10R TO S-14R
- [SDR VGCA20250805018](https://openairdocs.org/sdr/VGCA20250805018.md): Structure · corroded · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Structure
  > CORROSION AT MULTIPLE LOCATIONS AT A-NUT ATTACHMENTS. FORWARD LOWER FUSELAGE LONGITUDINAL STABILIZER LOWER CHORD REPAIRED AT BL0 FROM BS450-660
- [SDR VGCA20250805017](https://openairdocs.org/sdr/VGCA20250805017.md): Floorbeam · corroded · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Floor Beam
  > AFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORROSION AT BS1148 FROM LBL45 TO LBL55
- [SDR VGCA20250805016](https://openairdocs.org/sdr/VGCA20250805016.md): None · none · Aug 5, 2025 · N216WE · Boeing 7272S2F · Standard Practices/Structures
  > BMS3-27 IS NO LONGER PROCURABLE. BOEING SR KFC-GUC-24-0105-09B APPROVED THE USE OF BMS3-38 AS AN ALTERNATE.
- [SDR VGCA20250805015](https://openairdocs.org/sdr/VGCA20250805015.md): Spar · corroded · Aug 5, 2025 · N216WE · Boeing 7272S2F · Horizontal Stabilizer, Spar/Rib
  > CORROSION ON RH HORIZONTAL STAB REAR SPAR UPPER CHORD AT STAB STATION 104.25 THRU 123.25 AND 141.5 THRU 160.5
- [SDR VGCA20250805014](https://openairdocs.org/sdr/VGCA20250805014.md): Skin · corroded · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN AT BS1028 TO 1055 AND S-29L TO S-29R
- [SDR VGCA20250808013](https://openairdocs.org/sdr/VGCA20250808013.md): Keelbeam · corroded · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Keel
  > KEEL BEAM BREATHER WEB CORRODED AT SEVERAL LOCATIONS ON THE UPPER SURFACE FROM BS740 TO 795 AND LBL13 TO RBL13
- [SDR VGCA20250805012](https://openairdocs.org/sdr/VGCA20250805012.md): Frame · dented · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Frame
  > AFT LOWER FUSELAGE FRAME INNER CHORD DENTED AT BS1110 FROM S-24L TO S-28L
- [SDR VGCA20250805011](https://openairdocs.org/sdr/VGCA20250805011.md): Frame · punctured · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Frame
  > AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1090 FROM S-24L TO S-28L
- [SDR VGCA20250805010](https://openairdocs.org/sdr/VGCA20250805010.md): Frame · punctured · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Frame
  > FRAME INNER CHORD PUNCTURE AT BS 1090 BETWEEN S26R AND S28R.
- [SDR VGCA20250805009](https://openairdocs.org/sdr/VGCA20250805009.md): Frame · punctured · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Frame
  > AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1130 FROM S-25L TO S-29L.
- [SDR VGCA20250805008](https://openairdocs.org/sdr/VGCA20250805008.md): Frame · cracked · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Frame
  > FT LOWER FUSELAGE FRAME CRACKED AT BS1070 FROM S-26R TO S-28R
- [SDR VGCA20250805007](https://openairdocs.org/sdr/VGCA20250805007.md): Frame · cracked · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Frame
  > FORWARD LOWER FUSELAGE FRAME UPPER CHORD CRACKED AT BS700 FROM S-28L TO S-28R
- [SDR VGCA20250805006](https://openairdocs.org/sdr/VGCA20250805006.md): Skin Panel · corroded · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > AFT LOWER FUSELAGE SKIN CORROSION FROM BS990-1010 AT S-26L
- [SDR VGCA20250805005](https://openairdocs.org/sdr/VGCA20250805005.md): Shear Web · cracked · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > AFT UPPER FUSELAGE FLOOR SHEAR WEB CRACK NEAR BS1166-1176.9 AND RBL8 TO RBL17.87
- [SDR VGCA20250805004](https://openairdocs.org/sdr/VGCA20250805004.md): Spar · corroded · Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Frame
  > WING CENTER BOX FRONT SPAR CORRODED IN MULTIPLE PLACES ON VERTICAL AND HORIZONTAL CHORD FLANGES AT BS740 FROM LBL70.5 TO RBL70.5
- [SDR VGCA20250805003](https://openairdocs.org/sdr/VGCA20250805003.md): Flap Track · cracked · Aug 5, 2025 · N216WE · Boeing 7272S2F · Trailing Edge Flaps
  > CRACK FOUND ON LEFT WING OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP TRACK. CRACK WAS IN UPPER FLANGE INBOARD FLANGE.

Next page: https://openairdocs.org/model/boeing-727-2s2f/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 aircraft_model_key = '7272S2F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-2s2f/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.