# Service difficulty reports: N505SW, cancelled Oct 27, 2017

A list on [N505SW, cancelled Oct 27, 2017](https://openairdocs.org/deregistered/N505SW-2017-10-27.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 7 · 313 reports

- [SDR SWAA2013012411808](https://openairdocs.org/sdr/SWAA2013012411808.md): Control Unit · faulty · Jan 23, 2013 · N505SW · Boeing 7375H4 · Fire Detection
  > AIR TURNBACK, MX & SYS OK LIGHTS ON CARGO FIRE PANEL BOTH R & R UNIT IAW MM.
- [SDR SWAA2012122610854](https://openairdocs.org/sdr/SWAA2012122610854.md): Fastener · corroded · Dec 22, 2012 · N505SW · Boeing 7375H4 · Emergency Equipment
  > R1 DOOR FORWARD GIRT BAR FLOOR MOUNT HAS RUSTY MOUNTING HARDWARE. REPLACED R1 DOOR FORWARD GIRT BAR HARDWARE IAW AMM.
- [SDR SWAA2012122610853](https://openairdocs.org/sdr/SWAA2012122610853.md): Skin · cracked · Dec 21, 2012 · N505SW · Boeing 7375H4 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED ABOVE STRINGER 4R, STA 287-291. REPAIR IAW SRM.
- [SDR SWAA2012122110815](https://openairdocs.org/sdr/SWAA2012122110815.md): Support Angle · cracked · Dec 19, 2012 · N505SW · Boeing 7375H4 · Trailing Edge Flaps
  > RIGHT WING INBOARD MID FLAP FIXED WING PANEL HAS A CRACK AFT RIGHT CORNER. MARKED IN RED. REMOVE AND REPLACE SUPPORT ANGLE PER SRM 51-40-02.
- [SDR SWAA2012122110814](https://openairdocs.org/sdr/SWAA2012122110814.md): Cover · loose · Dec 19, 2012 · N505SW · Boeing 7375H4 · Emergency Lighting
  > RIGHT EMERGENCY EXIT LIGHT COVER IS LOOSE. SECURED LIGHT COVER PER AMM.
- [SDR SWAA2012062105128](https://openairdocs.org/sdr/SWAA2012062105128.md): Motor · faulty · Jun 18, 2012 · N505SW · Boeing 7375H4 · Compressor Bleed Control
  > ON CLIMBOUT UNABLE TO MAINTAIN CLIMB N1 WITHOUT EXCEEDING MAX CONT EGT TO MAINTAIN CLIMB N1 REQUIRES 920+ ON NR 1 ENG EGT. REMOVED AND REPLACED VBV MOTOR & VBV STOP INSTALLED NEW FLEX SHAFT PER MM.
- [SDR SWAA2012060604720](https://openairdocs.org/sdr/SWAA2012060604720.md): Mount · cracked · Jun 3, 2012 · N505SW · Boeing 7375H4 · Escape Slide
  > R2 DOOR EMERGENCY EVAC SLIDE FORWARD SLIDE MOUNT CRACKED. REMOVED AND REPLACED MOUNT PER AMM.
- [SDR SWAA2012051504003](https://openairdocs.org/sdr/SWAA2012051504003.md): Slide · out of position · May 14, 2012 · N505SW · Boeing 7375H4 · Escape Slide
  > R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
- [SDR SWAA2012032902712](https://openairdocs.org/sdr/SWAA2012032902712.md): Toggle · loose · Mar 29, 2012 · N505SW · Boeing 7375H4 · Trailing Edge Flaps
  > AIRCRAFT SHUTTER AND YOKE VIBRATION 210 KTS FLAPS MOVING FROM 2 TO POSITION 5, 2, TO 4 SECONDS. REMOVED AND REPLACED FLAP TOGGLES PER MM.
- [SDR SWAA2012040202764](https://openairdocs.org/sdr/SWAA2012040202764.md): Light · inoperative · Mar 28, 2012 · N505SW · Boeing 7375H4 · Emergency Lighting
  > RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 16 TO ROW 17. REPAIRED LIGHT PER MM.
- [SDR SWAA2012031902389](https://openairdocs.org/sdr/SWAA2012031902389.md): Retainer · broken · Mar 15, 2012 · N505SW · Boeing 7375H4 · Emergency Equipment
  > L1 DOOR EMERGENCY EVAC SLIDE AFT FLOOR GIRT BAR RETAINER SPRING BROKEN. REMOVED AND REPLACED RETAINER ASSY PER M/M.
- [SDR SWAA117169](https://openairdocs.org/sdr/SWAA117169.md): Cover · loose · Oct 18, 2011 · N505SW · Boeing 7375H4 · Emergency Lighting
  > RT EEPLS COVER LOOSE AT ROW 8. REMOVED AND REPLACED COVER PER MM.
- [SDR SWAA116716](https://openairdocs.org/sdr/SWAA116716.md): Light · discharged · Sep 21, 2011 · N505SW · Boeing 7375H4 · Emergency Lighting
  > DURING SCHEDULED 22Y CHECK, LT EMERGENCY EXIT LIGHTS INOP. RELAMPED PER MM.
- [SDR SWAA116715](https://openairdocs.org/sdr/SWAA116715.md): Frame · cracked · Sep 21, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Frame
  > DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 947.5, STR 19L. REPAIRED FRAME IAW ER AND EA.
- [SDR SWAA116714](https://openairdocs.org/sdr/SWAA116714.md): Light · inoperative · Sep 21, 2011 · N505SW · Boeing 7375H4 · Emergency Lighting
  > DURING SCHEDULED 22Y CHECK, RT EMERGENCY EXIT LIGHTS INOP. RELAMPED PER MM.
- [SDR SWAA116713](https://openairdocs.org/sdr/SWAA116713.md): Frame · cracked · Sep 21, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Frame
  > DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 296.5, STR 7R. REPAIRED FRAME IAW EA ER.
- [SDR SWAA116712](https://openairdocs.org/sdr/SWAA116712.md): Skin · cracked · Sep 21, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, BS 329, STR 8R. REPAIRED SKIN IAW ER AND EA.
- [SDR SWAA116711](https://openairdocs.org/sdr/SWAA116711.md): Frame · cracked · Sep 21, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Frame
  > DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 639, STR 16L. REPAIRED FRAME IAW ER AND EA.
- [SDR SWAA116710](https://openairdocs.org/sdr/SWAA116710.md): Skin · cracked · Sep 21, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 22Y CHECK, FOUND SKIN CACKED AT BS 727A+6, STR 21L. REPAIRED SKIN IAW ER AND EA.
- [SDR SWAA116680](https://openairdocs.org/sdr/SWAA116680.md): Bulkhead · cracked · Sep 20, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Bulkhead
  > DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD LOWER CHORD HORIZONTAL FLANGE CRACKED AT BS 540, BETWEEN STR 21L TO STR 22L. REPAIRED FLANGE PER ER.
- [SDR SWAA116679](https://openairdocs.org/sdr/SWAA116679.md): Bulkhead · cracked · Sep 20, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Bulkhead
  > DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD LOWER CHORD HORIZONTAL FLANGE CRACKED AT BS 540, STR 25L. REPAIRED FLANGE PER ER.
- [SDR SWAA116678](https://openairdocs.org/sdr/SWAA116678.md): Skin · cracked · Sep 20, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO DOOR SKIN CUTOUT CRACKED. REPAIRED SKIN IAW ER AND EA.
- [SDR SWAA116677](https://openairdocs.org/sdr/SWAA116677.md): Floorbeam · cracked · Sep 20, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Floor Beam
  > DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 661, BBL 0. REPAIRED BEAM IAW ER AND EA.
- [SDR SWAA116676](https://openairdocs.org/sdr/SWAA116676.md): Skin · cracked · Sep 20, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR FUSELAGE SKIN CRACKED AT BS 327, WL 210. REPAIRED SKIN IAW EA AND ER.
- [SDR SWAA116601](https://openairdocs.org/sdr/SWAA116601.md): Frame · cracked · Sep 19, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Frame
  > DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 332.1, STR 8R. REMOVED AND REPLACED FRAME IAW SRM.
- [SDR SWAA116600](https://openairdocs.org/sdr/SWAA116600.md): Frame · cracked · Sep 19, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Frame
  > DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 482, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW ATS ER.
- [SDR SWAA116599](https://openairdocs.org/sdr/SWAA116599.md): Web · cracked · Sep 19, 2011 · N505SW · Boeing 7375H4 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED 22Y CHECK, FOUND SUPPORT WEB CRACKED AT BS 344, STR 11R. REPAIRED WEB IAW ER AND EA.
- [SDR SWAA116490](https://openairdocs.org/sdr/SWAA116490.md): Floorbeam · cracked · Sep 12, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Floor Beam
  > DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 659 TO BS 669, LBL 24.5. REPAIRED CHORD PER EA AND ER.
- [SDR SWAA116489](https://openairdocs.org/sdr/SWAA116489.md): Floor Support · corroded · Sep 12, 2011 · N505SW · Boeing 7375H4 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS 772, LBL 17. REPAIRED SUPPORT PER EA.
- [SDR SWAA116488](https://openairdocs.org/sdr/SWAA116488.md): Shear Tie · corroded · Sep 12, 2011 · N505SW · Boeing 7375H4 · Fuselage Internal Mounting Structure
  > DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482A, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED FRAME PER SRM.
- [SDR SWAA116487](https://openairdocs.org/sdr/SWAA116487.md): Shear Tie · corroded · Sep 12, 2011 · N505SW · Boeing 7375H4 · Fuselage Internal Mounting Structure
  > DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482A, BETWEEN STR 28R TO STR 28L. REMOVED AND REPLACED FRAME PER SRM.
- [SDR SWAA116550](https://openairdocs.org/sdr/SWAA116550.md): Frame · corroded · Sep 9, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Frame
  > DURING SCHEDULED 22Y CHECK FOUND, SHEAR TIE CORRODED AT BS 482A, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED FRAME PER SRM AND DWG.
- [SDR SWAA116430](https://openairdocs.org/sdr/SWAA116430.md): Frame · cracked · Sep 7, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Frame
  > DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 277, STR 16L. REPAIRED WEB IAW SRM.
- [SDR SWAA116429](https://openairdocs.org/sdr/SWAA116429.md): Channel · cracked · Sep 7, 2011 · N505SW · Boeing 7375H4 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED 22Y CHECK, FOUND CHANNEL CRACKED AT BS 360, STR 4R. REPAIRED CHANNEL IAW EA.
- [SDR SWAA116428](https://openairdocs.org/sdr/SWAA116428.md): Floorbeam · corroded · Sep 7, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Floor Beam
  > DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, STR 16L. REPAIRED BEAM IAW ER.
- [SDR SWAA116427](https://openairdocs.org/sdr/SWAA116427.md): Frame · cracked · Sep 7, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Frame
  > DURING SCHEDULED 22Y CHECK, FOUND FRAME OUTER CHORD CRACKED AT BS 639, STR 16L. REPAIRED CHORD IAW EA.
- [SDR SWAA116426](https://openairdocs.org/sdr/SWAA116426.md): Shear Tie · corroded · Sep 7, 2011 · N505SW · Boeing 7375H4 · Fuselage Internal Mounting Structure
  > DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT S 747, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE IAW SRM.
- [SDR SWAA116355](https://openairdocs.org/sdr/SWAA116355.md): Skin · cracked · Sep 6, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 375, STR 17R. REPAIRED SKIN IAW ER.
- [SDR SWAA116354](https://openairdocs.org/sdr/SWAA116354.md): Frame · cracked · Sep 6, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Frame
  > DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 947, STR 19R. REPAIRED FRAME IAW SRM AND DWG.
- [SDR SWAA116353](https://openairdocs.org/sdr/SWAA116353.md): Shear Tie · corroded · Sep 6, 2011 · N505SW · Boeing 7375H4 · Fuselage Internal Mounting Structure
  > DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.
- [SDR SWAA116352](https://openairdocs.org/sdr/SWAA116352.md): Frame · cracked · Sep 6, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Frame
  > DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 967, BETWEEN STR 6L TO STR 7L. REMOVED AND REPLACED FRAME IAW SRM.
- [SDR SWAA116263](https://openairdocs.org/sdr/SWAA116263.md): Floorbeam · cracked · Aug 31, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Floor Beam
  > DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45. REPAIRED CHORD PER ER AND ER.
- [SDR SWAA116262](https://openairdocs.org/sdr/SWAA116262.md): Skin · cracked · Aug 31, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 273, STR 16L. REPAIRED SKIN IAW SRM.
- [SDR SWAA116236](https://openairdocs.org/sdr/SWAA116236.md): Frame · cracked · Aug 31, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Frame
  > DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 986.5, STR 20R. REMOVED AND REPLACED WEB IAW SRM.
- [SDR SWAA116235](https://openairdocs.org/sdr/SWAA116235.md): Floor Support · corroded · Aug 31, 2011 · N505SW · Boeing 7375H4 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED 22Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 859, RBL 3. REPAIRED SUPPORT IAW EA.
- [SDR SWAA116234](https://openairdocs.org/sdr/SWAA116234.md): Floor Support · corroded · Aug 31, 2011 · N505SW · Boeing 7375H4 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED 22Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 772, LBL 8. REPAIRED SUPPORT IAW EA.
- [SDR SWAA116206](https://openairdocs.org/sdr/SWAA116206.md): Floor Support · corroded · Aug 30, 2011 · N505SW · Boeing 7375H4 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS 772, LBL 12. REPAIRED SUPPORT IAW EA.
- [SDR SWAA116031](https://openairdocs.org/sdr/SWAA116031.md): Pressure Panel · cracked · Aug 24, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Bulkhead
  > DURING SCHEDULED 22Y CHECK, FOUND PRESSURE DECK WEB CRACKED BETWEEN BS 665 TO BS 675, BETWEEN RBL 35 TO RBL 45. REMOVED AND REPLACED WEB PER SRM.
- [SDR SWAA115866](https://openairdocs.org/sdr/SWAA115866.md): Stringer · cracked · Aug 15, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 400, STR 15R. REMOVED AND REPLACED STRINGER SECTION IAW SRM.
- [SDR SWAA115865](https://openairdocs.org/sdr/SWAA115865.md): Floorbeam · corroded · Aug 15, 2011 · N505SW · Boeing 7375H4 · Fuselage Main, Floor Beam
  > DURING SCHEDULED 22Y CHECK, FOUND FLOOR BEAM CORRODED AT BS 967, LBL 5. REPAIRED BEAM IAW SRM.

Next page: https://openairdocs.org/deregistered/N505SW-2017-10-27/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 = 'N505SW' AND deregistration_id = 'N505SW-2017-10-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N505SW-2017-10-27/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.