# Service difficulty reports: N8623F

A list on [N8623F](https://openairdocs.org/aircraft/N8623F.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 · 194 reports

- [SDR SWAA2026082442664](https://openairdocs.org/sdr/SWAA2026082442664.md): Cover · missing · Aug 20, 2026 · N8623F · Boeing 7378H4 · Emergency Lighting
  > AFTER WINDSCREEN EMERGENCY EXIT SIGN LIGHT COVER MISSING CAPTAINS SIDE. CAPTAIN HELD OFF BOARDING. R & R AFT EMER LIGHT COVER IAW AMM 33-51-01.
- [SDR SWAA2026081046552](https://openairdocs.org/sdr/SWAA2026081046552.md): Rivet · missing · Aug 6, 2026 · N8623F · Boeing 7378H4 · Emergency Equipment
  > FA REPORTED FWD GALLEY DOOR GIRT BAR DIFFICULT TO LATCH ONTO DOOR. FOUND AFT GIRT BAR RETAINING BRACKET ON SLIDE BUSTLE RIVET MISSING. SECURED RETAINING BRACKET IAW EA M-23-125-01839. OK FOR SERVICE.
- [SDR SWAA2026071559853](https://openairdocs.org/sdr/SWAA2026071559853.md): Lens · missing · Jul 11, 2026 · N8623F · Boeing 7378H4 · Emergency Lighting
  > CABIN FWD EMERGENCY LIGHT COVER MISSING. INSTALLED NEW LENS COVER IAW AMM 33-51-03.
- [SDR SWAA2026061110084](https://openairdocs.org/sdr/SWAA2026061110084.md): Megaphone · inoperative · Jun 7, 2026 · N8623F · Boeing 7378H4 · Emergency Equipment
  > MEGAPHONE IS INOPERATIVE. R & R MEGAPHONE. OPS CHECK GOOD AT THIS TIME. R & R THE MEGAPHONE. OPS CHECK GOOD IAW AMM 25-64-00.
- [SDR SWAA2026033083815](https://openairdocs.org/sdr/SWAA2026033083815.md): Lens · missing · Mar 27, 2026 · N8623F · Boeing 7378H4 · Emergency Lighting
  > LT. FWD OVERWING EMERGENCY EXIT LOWER LIGHTED EXIT SIGN MISSING LENS.<[01] INSTALLED LOWER LIGHTED EXIT SIGN LENS ON LT. FWD EMERGENCY EXIT IAW AMM 33-51-01.
- [SDR SWAA2026032079473](https://openairdocs.org/sdr/SWAA2026032079473.md): Floor Panel · cracked · Mar 13, 2026 · N8623F · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 221GF CRACKED AT FWD LT CORNER. REPAIRED FLOOR PANEL 221GF CRACKED AT FWD L/H CORNER IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026012062751](https://openairdocs.org/sdr/SWAA2026012062751.md): Cover · dislodged · Jan 19, 2026 · N8623F · Boeing 7378H4 · Escape Slide
  > AFT LT ESCAPE SLIDE COVER DISPLACED. SECURED AFT LT SLIDE COVER IAW AMM 25-66-01. AC OK FOR SERVICE.
- [SDR SWAA2026010658252](https://openairdocs.org/sdr/SWAA2026010658252.md): Slide · unpacked · Jan 4, 2026 · N8623F · Boeing 7378H4 · Escape Slide
  > ESCAPE SLIDE FWD SERVICE DOOR NEEDS REPACKING. PERFORMED INSPECTION OF FWD GALLEY SERVICE DOOR ESCAPE SLIDE PER AMM 25-66-01. FOUND NO DEFECTS. OK FOR SERVICE.
- [SDR SWAA2025112029146](https://openairdocs.org/sdr/SWAA2025112029146.md): Angle · cracked · Oct 28, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BS 500I, STR 28R IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7902, SHEET 301, REV A.
- [SDR SWAA2025112029147](https://openairdocs.org/sdr/SWAA2025112029147.md): Angle · cracked · Oct 28, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS 500I & STR 28L AT FWD CARGO COMPARTMENT. REPLACED THE ANGLE IAW SRM 51-40-02 AND DWG 143A7902, SHEET 301, REV A.
- [SDR SWAA2025112829141](https://openairdocs.org/sdr/SWAA2025112829141.md): Rib · cracked · Oct 27, 2025 · N8623F · Boeing 7378H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK RIB LOCATED LE STA 123.85 ACCESS PANEL 341B AT RT HORIZONTAL STAB. REPLACED RIB LOCATED LE STA 123.85 ACCESS PANEL 341B AT RT HORIZONTAL STAB IAW SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG: 186A1001 SHEET: 19 REV -.
- [SDR SWAA2025112029148](https://openairdocs.org/sdr/SWAA2025112029148.md): Angle · cracked · Oct 27, 2025 · N8623F · Boeing 7378H4 · Service Doors
  > CRACKED ANGLE ON ACCESS PANEL 844DZ RT SIDE AFT GALLEY DOOR. REPLACED THE ANGLE IAW SRM 51-40-02, AND 51-10-02, ITEM 9.
- [SDR SWAA2025112029145](https://openairdocs.org/sdr/SWAA2025112029145.md): Angle · cracked · Oct 27, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE ON ACCESS PANEL 844DZ, LT SIDE, GALLEY DOOR. REPLACED ANGLE IAW SRM 51-40-02, AND 51-10-02, ITEM 9.
- [SDR SWAA2025112029143](https://openairdocs.org/sdr/SWAA2025112029143.md): Support Beam · cracked · Oct 27, 2025 · N8623F · Boeing 7378H4 · Service Doors
  > CRACK SUPPORT BEAM NR 4 LOCATED FWD GALLEY SERVICE DOOR. REPLACED BEAM 4 LOCATED FWD GALLEY SERVICE DOOR AT PASSENGER CABIN IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 141A6516; SHEET 142; REV -.
- [SDR SWAA2025112032981](https://openairdocs.org/sdr/SWAA2025112032981.md): Balance Arm · out of tolerance · Oct 27, 2025 · N8623F · Boeing 7378H4 · Elevator Miscellaneous Structure
  > DURING WEIGHT AND BALANCE PROCEDURE OF RT ELEVATOR FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1EA) ON BAY 2; P/N: 183A0210-14 (1EA) AND P/N: 69-53211-2 (2EA) ON BAY 3; P/N: 183A0210-15 ON BAY 4 2025-652468. TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-03767.
- [SDR SWAA2025112032980](https://openairdocs.org/sdr/SWAA2025112032980.md): Balance Arm · out of tolerance · Oct 27, 2025 · N8623F · Boeing 7378H4 · Elevator Miscellaneous Structure
  > DURING WEIGHT AND BALANCE PROCEDURE OF LT ELEVATOR FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1EA) ON BAY 2; P/N: 183A0210-14 (1EA) AND P/N: 69-53211-2 (2EA) ON BAY 3; P/N: 183A0210-15 ON BAY 4 2025-652467. TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-03766.
- [SDR SWAA2025112029022](https://openairdocs.org/sdr/SWAA2025112029022.md): Rib · cracked · Oct 27, 2025 · N8623F · Boeing 7378H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK RIB LOCATED LE HSS 105.26 LT HORIZONTAL STAB. REPLACED RIB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 186A1001, SHEET 19, REV-, DUE TO NO ALLOWABLE DAMAGE FOUND IN SRM IAW SRM 55-10-09-1A-1, ALLOWABLE DAMAGE 1. MEASUREMENT OF CRACK IS:0.5500 INCH.
- [SDR SWAA2025112028839](https://openairdocs.org/sdr/SWAA2025112028839.md): Floorbeam · cracked · Oct 26, 2025 · N8623F · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CRACK ON THE FLOORBEAM, BS 540 BTW BL 0 TO RBL 24.75, WL 208.1. REPLACED THE FLOORBEAM IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 143A0060, SHEET 64, REV-. MEASUREMENT OF CRACK IS 0.380.
- [SDR SWAA2025112828448](https://openairdocs.org/sdr/SWAA2025112828448.md): Bracket · cracked · Oct 25, 2025 · N8623F · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACK ON BRACKET TRAILING EDGE LOCATED ORSS273 AT RT WING. REPLACED THE BRACKET TRAILING EDGE LOCATED ORSS273 AT RT WING IAW SRM 51-10-02-0G; SRM 51-40-02-0G-0 AND DWG 115A6200 SHEET 17 REV A TOOK MEASURE OF CRACK IS: 1.754 INCHES.
- [SDR SWAA2025112628445](https://openairdocs.org/sdr/SWAA2025112628445.md): Support · corroded · Oct 25, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS 500E TO BS 500I LBL 22 WL 156.1AT FWD CARGO COMPARTMENT, 12 POINTS. FAULT RESOLVED ON FAULT TTG8Q016272L.
- [SDR SWAA2025112628455](https://openairdocs.org/sdr/SWAA2025112628455.md): Support · corroded · Oct 25, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS 500 TO BS 500E LBL 22 WL 156.1, AT FWD CARGO COMPARTMENT,12 POINTS. THE DAMAGE WAS REPAIRED IAW SRM 53-00-53-2R-5 AND EA M-22-153 -01550.
- [SDR SWAA2025112028452](https://openairdocs.org/sdr/SWAA2025112028452.md): Web · corroded · Oct 25, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SHIELD WEB, BTW BS 492.4 - 500A, RBL 23, WL 208.1. REPLACED SHIELD WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A0080, SHEET 39, REV-.
- [SDR SWAA2025112028454](https://openairdocs.org/sdr/SWAA2025112028454.md): Support · corroded · Oct 25, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE, BTW BS 500E - 500I, RBL 22, WL 156.1. FWD CARGO COMPARTMENT. FAULT RESOLVED ON FAULT TTG8Q0161PAR.
- [SDR SWAA2025112028446](https://openairdocs.org/sdr/SWAA2025112028446.md): Support · corroded · Oct 25, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE, BTW BS 500A - 500E, RBL 22, WL 156.1. THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR5) AND EA M-22-153 -01550.
- [SDR SWAA2025112028453](https://openairdocs.org/sdr/SWAA2025112028453.md): Tie Clip · cracked · Oct 25, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON TIE CLIP, BS 500I, STRINGER 26R, WL 156.1. REPLACED THE TIE CLIP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A1234, SHEET 13, REV A.
- [SDR SWAA2025112028579](https://openairdocs.org/sdr/SWAA2025112028579.md): Support Angle · cracked · Oct 25, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE BTW BS 380 TO BS 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 138, REV -. MEASUREMENT OF THE CRACK IS 1.298
- [SDR SWAA2025112028578](https://openairdocs.org/sdr/SWAA2025112028578.md): Support Angle · cracked · Oct 25, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1. REPLACED SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 142, REV-. MEASUREMENT OF THE CRACK IS: 1.250 INCH.
- [SDR SWAA2025112028576](https://openairdocs.org/sdr/SWAA2025112028576.md): Support Angle · cracked · Oct 25, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 49 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 38, REV-. MEASUREMENT OF THE CRACK IS: 0.292 INCH.
- [SDR SWAA2025112028577](https://openairdocs.org/sdr/SWAA2025112028577.md): Support Angle · cracked · Oct 25, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE BTW BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A5400, SHEET 154, REV -, MEASUREMENT OF THE CRAK IS 0.667 INCH.
- [SDR SWAA2025112028573](https://openairdocs.org/sdr/SWAA2025112028573.md): Support Bracket · cracked · Oct 25, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT BRACKET, BS 867, BTW STR 2R TO STR 3R. REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 146A7901, SHEET 66, REV A.
- [SDR SWAA2025112028574](https://openairdocs.org/sdr/SWAA2025112028574.md): Frame · cracked · Oct 25, 2025 · N8623F · Boeing 7378H4 · Fuselage Main, Frame
  > CRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. PERFORMED PERMANENT REPAIR FRAME IAW EA M-22-153-01244.
- [SDR SWAA2025112028190](https://openairdocs.org/sdr/SWAA2025112028190.md): Intercostal · cracked · Oct 24, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BTW BS 500A - 500B, STRINGER 26R. REPLACED THE WEB - INTERCOSTAL IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV -.
- [SDR SWAA2025112028195](https://openairdocs.org/sdr/SWAA2025112028195.md): Nut · deteriorated · Oct 24, 2025 · N8623F · Boeing 7378H4 · Service Doors
  > DETERIORATED CAM NUT ON AFT GALLEY SERVICE DOOR HANDLE. REPLACED CAM NUT IAW AMM 52-41-11-400-801, STEP 3.F (5), ITEM (I) THRU 3.F (5), ITEM (N).
- [SDR SWAA2025112028188](https://openairdocs.org/sdr/SWAA2025112028188.md): Angle · cracked · Oct 24, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE AFT FACE BS 500H, STRINGER 26R. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 139, REV-. MEASUREMENT OF CRACK: L: 0.480 INCH.
- [SDR SWAA2025112028189](https://openairdocs.org/sdr/SWAA2025112028189.md): Angle · cracked · Oct 24, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE CLIP FWD FACE, BS 500H, STRINGER 26R. REPLACED THE ANGLE CLIP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505 SHEET 139, REV-. MEASUREMENT OF THE CRACK: L: 0.345 INCH.
- [SDR SWAA2025112028193](https://openairdocs.org/sdr/SWAA2025112028193.md): Angle · cracked · Oct 24, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE CLIP AFT FACE, BS 400 STRINGER 26L. MEASUREMENT OF CRACK IS L: 0.530 INCHES. REPLACED THE ANGLE CLIP IAW SRM 51-40-02-0G, SRM 51-10-02-0G, PARAGRAPH 9, AND DWG 143A7505 SHEET 137, REV-.
- [SDR SWAA2025112028194](https://openairdocs.org/sdr/SWAA2025112028194.md): Angle · cracked · Oct 24, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE CLIP FWD FACE, BS 500H, STRINGER 26L. REPLACED THE ANGLE CLIP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 139, REV-. MEASUREMENT OF CRACK IS: L: 1.905 INCH.
- [SDR SWAA2025112028191](https://openairdocs.org/sdr/SWAA2025112028191.md): Angle · cracked · Oct 24, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK GUSSET ANGLE, BS 500I, STRINGER 21L. REPLACED THE GUSSET ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7902, SHEET 256, REV B. REJECTED REPLACEMENT DUE TO BAD AND WRONG SEALANT APPLICATION AROUND GUSSET, APPLIED SEALANT ON GUSS
- [SDR SWAA2025112028187](https://openairdocs.org/sdr/SWAA2025112028187.md): Angle · cracked · Oct 24, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED GUSSET ANGLE, BS 500I, STRINGER 19R IN THE FWD CARGO BAY. MEASUREMENT OF THE CRACK IS L: 0.9235 INCHES.. REPLACED GUSSET ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG: 143A7902, SHEETS 256 AND 257, REV B.
- [SDR SWAA2025112028192](https://openairdocs.org/sdr/SWAA2025112028192.md): Angle · cracked · Oct 24, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON THE ANGLE LOCATED AFT FACE BS 500H, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEP 9, SRM 51-40-02, AND DWG 143A7505, SHEET 139, REV-.
- [SDR SWAA2025112028186](https://openairdocs.org/sdr/SWAA2025112028186.md): Access Panel · cracked · Oct 24, 2025 · N8623F · Boeing 7378H4 · Horizontal Stabilizer, Plate/Skin
  > CRACKED SEAL - BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER. REPLACED BLADE LOCATED ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER IAW SRM 51-40-02.
- [SDR SWAA2025112027629](https://openairdocs.org/sdr/SWAA2025112027629.md): Web · corroded · Oct 23, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB - INTERCOSTAL BTW BS 747 - 767, STR 25R, WL 156.4. REPLACED THE WEB - INTERCOSTAL IAW 51-40-02, AND DWG 146A7502, SHEET 50, REV-.
- [SDR SWAA2025112027440](https://openairdocs.org/sdr/SWAA2025112027440.md): Web · cracked · Oct 23, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB BTW BS 927 TO BS 947.5, STRINGER 25R. REPLACED THE WEB IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G, AND DWG 147A7500, SHEET 20, REV -.
- [SDR SWAA2025112027447](https://openairdocs.org/sdr/SWAA2025112027447.md): Support Angle · corroded · Oct 23, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ANGLE, BTW BS 767 - 792, RBL 21, WL 156.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 146A8123, SHEET 16, REV -.
- [SDR SWAA2025112027446](https://openairdocs.org/sdr/SWAA2025112027446.md): Web · corroded · Oct 23, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON THE SHIELD WEB BS 767 - 792, RBL 21, WL 156.1. REPLACED THE SHIELD WEB IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 146A0081, SHEET 49, REV A.
- [SDR SWAA2025112027178](https://openairdocs.org/sdr/SWAA2025112027178.md): Fitting · deteriorated · Oct 23, 2025 · N8623F · Boeing 7378H4 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTINGS HARDWARE AND SHIMS ENTRY AND SERVICE DOOR. REPLACED GIRT BAR FITTINGS HARDWARE AND SHIMS ENTRY AND SERVICE DOOR AT AFT GALLEY AREA IAW AMM 25-66-02-400-801,
- [SDR SWAA2025112027177](https://openairdocs.org/sdr/SWAA2025112027177.md): Fitting · deteriorated · Oct 23, 2025 · N8623F · Boeing 7378H4 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTING HARDWARE AND SHIMS FWD ENTRY AND SERVICE DOOR. REPLACED GIRT BAR FITTING HARDWARE AND SHIMS. INSTALLATION WILL BE ACCOMPLISHED ON TTG8R008CEXW STEP 13.
- [SDR SWAA2025112027438](https://openairdocs.org/sdr/SWAA2025112027438.md): Angle · cracked · Oct 23, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED BS 867, STRINGER 26L, WL 156.1. REPLACED THE ANGLE IAW SRM 51-10-02-0G, SRM 51-40-02-0G-0, AND DWG 149A8102, SHEET 19, REV A. MEASURE OF CRACK: 0.833 INCHES.
- [SDR SWAA2025112027638](https://openairdocs.org/sdr/SWAA2025112027638.md): Support · corroded · Oct 23, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE, BTW BS 727F - 767, STRINGER 25R, WL 156.4. REPLACED SUPPORT ZEE IAW SRM 51-10-02-0G, ITEM 9, SRM 51-40-02-0G, SRM 53-00-53-2R-6, REPAIR 6, DWG 146A7500, SHEET 233, REV-, DWG 146A7502, SHEET 50, REV-.
- [SDR SWAA2025112027172](https://openairdocs.org/sdr/SWAA2025112027172.md): Scuff Plate · cracked · Oct 23, 2025 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON FWD CORNER OF SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.

Next page: https://openairdocs.org/aircraft/N8623F/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 = 'N8623F' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8623F/reports

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