# Service difficulty reports: N8620H, cancelled Jan 30, 2026

A list on [N8620H, cancelled Jan 30, 2026](https://openairdocs.org/deregistered/N8620H-2026-01-30.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 3 · 148 reports

- [SDR SWAA2025121034545](https://openairdocs.org/sdr/SWAA2025121034545.md): Seat · out of adjust · Nov 12, 2025 · N8620H · Boeing 7378H4 · Passenger Compartment Equipment
  > SEAT 13D RECLINES. IT SHOULD NOTRECLINE INTO EXIT ROW. ADJUSTED PAX SEAT 13D RECLINE LOCK IAW AMM 25-22-00-525-801.
- [SDR SWAA2025121033754](https://openairdocs.org/sdr/SWAA2025121033754.md): Lens · fogged · Nov 10, 2025 · N8620H · Boeing 7378H4 · Emergency Lighting
  > R1 DOOR EMERGENCY LIGHT LENS FOGGY. REMOVED AND REPLACED THE R1 DOOR EMERGENCY LIGHT LENS IAW AMM 33-51-04-960-801, STEP F;3 D.
- [SDR SWAA2025121033763](https://openairdocs.org/sdr/SWAA2025121033763.md): Lens · cracked · Nov 10, 2025 · N8620H · Boeing 7378H4 · Emergency Lighting
  > ROW 2 CEILING EMERGENCY LIGHT LENS TRIM IS CRACKED AND IN POOR CONDITION. R & R IAW AMM35-51-03-960-803.
- [SDR SWAA2025120933757](https://openairdocs.org/sdr/SWAA2025120933757.md): Light · deteriorated · Nov 10, 2025 · N8620H · Boeing 7378H4 · Emergency Lighting
  > RIGHT FWD CABIN EMERGENCY PHOTOLUMINESCENT LIGHT STRIPS ARE DETERIORATED. REMOVED AND REPLACED RH FWD CABIN EMERGENCY PHOTOLUMINESCENT LIGHT STRIP IAW AMM 33-51-15-960-801.
- [SDR SWAA2025120933758](https://openairdocs.org/sdr/SWAA2025120933758.md): Light · deteriorated · Nov 10, 2025 · N8620H · Boeing 7378H4 · Emergency Lighting
  > LEFT FWD CABIN EMERGENCY PHOTOLUMINESCENT LIGHT STRIPS ARE DETERIORATED. REMOVED AND REPLACED LH FWD CABIN EMERGENCY PHOTOLUMINESCENT LIGHT STRIP IAW AMM 33-51-15-960-801.
- [SDR SWAA2025120933769](https://openairdocs.org/sdr/SWAA2025120933769.md): Lens · wrong part · Nov 10, 2025 · N8620H · Boeing 7378H4 · Emergency Lighting
  > AFT LAV ON THE EXTERIOR EMERGENCY EXIT LIGHT LENS IS MISSING VERBIAGE (EXIT). REMOVED AND REPLACED ATF LAV EXTERIOR EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01-960-802.
- [SDR SWAA2025110530572](https://openairdocs.org/sdr/SWAA2025110530572.md): Power Supply · inoperative · Oct 31, 2025 · N8620H · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT POWER SUPPLY M1695, BS 565, RT INOPERATIVE. REPLACED THE POWER SUPPLY IAW AMM 33-51-06-960-806. TESTED OK.
- [SDR SWAA2025110524435](https://openairdocs.org/sdr/SWAA2025110524435.md): Web · cracked · Oct 14, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED WEB, BS 500G - 500H, STRINGER 26R. REPLACED THE WEB & FASTENERS IAW SRM 51-40-02, AND DWG 143A7505, SHEET 123, REV-.
- [SDR SWAA2025110522763](https://openairdocs.org/sdr/SWAA2025110522763.md): Light · inoperative · Oct 9, 2025 · N8620H · Boeing 7378H4 · Emergency Lighting
  > INOPERATIVE EMERGENCY LIGHT, REPLACED EMERGENCY LIGHT IAW AMM 33-51-03-960-805, TESTED OK.
- [SDR SWAA2025110522764](https://openairdocs.org/sdr/SWAA2025110522764.md): Light · inoperative · Oct 9, 2025 · N8620H · Boeing 7378H4 · Emergency Lighting
  > INOPERATIVE EMERGENCY LIGHT AT ROW 16ABC. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-03-960-805, TESTED OK.
- [SDR SWAA2025110521930](https://openairdocs.org/sdr/SWAA2025110521930.md): Lens · broken · Oct 7, 2025 · N8620H · Boeing 7378H4 · Emergency Lighting
  > BROKEN SIDEWALL PANEL 231ZLW EMERGENCY LIGHT LENS AT PASSENGER CABIN. REPLACED SIDEWALL PANEL 231ZLW EMERGENCY LIGHT LENS AT PAX CABIN IAW AMM 33-51-01-960-802, STEP 3.C.(5).(D) AND (10)
- [SDR SWAA2025110521932](https://openairdocs.org/sdr/SWAA2025110521932.md): Light · deteriorated · Oct 7, 2025 · N8620H · Boeing 7378H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH AND RH SIDE IN CABIN 10 EA. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH AND RH SIDE AT PASSENGER CABIN (10 EA) FOR INSTALLATION REFER TO TTG8Q00P2YRU;[02] CORRECTED STEP 1<BR>REPLACED PHOTOLU
- [SDR SWAA2025110521643](https://openairdocs.org/sdr/SWAA2025110521643.md): Support Angle · cracked · Oct 5, 2025 · N8620H · Boeing 7378H4 · Engine Air Intake System
  > CRACK ON SUPPORT ANGLE OTBD FAN COWL, NR 2 ENGINE. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02.
- [SDR SWAA2025110521416](https://openairdocs.org/sdr/SWAA2025110521416.md): Handle · deteriorated · Oct 4, 2025 · N8620H · Boeing 7378H4 · Service Doors
  > DETERIORATED HANDLE BOX HARDWARE, FWD SERVICE DOOR. REPLACED HANDLE BOX HARDWARE IAW AMM 52-41-11-400-801, STEP 3.F, 2J,
- [SDR SWAA2025110521056](https://openairdocs.org/sdr/SWAA2025110521056.md): Support Bracket · cracked · Oct 3, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT RT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED BS540 AT LEVEL RBL 6 AT RT AIR CONDITIONING BAY IAW SRM 51-10-02 Ï¿½TEM 9; 51-40-02 AND DWG:212A1116 SHEET:1.
- [SDR SWAA2025110520966](https://openairdocs.org/sdr/SWAA2025110520966.md): Support Bracket · cracked · Oct 3, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABINREPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO 3R AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 146A7901 SHEET:66 REV:A.
- [SDR SWAA2025110521063](https://openairdocs.org/sdr/SWAA2025110521063.md): Support Angle · cracked · Oct 3, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BODY STA 663.75 AND LBL 10 AT AIR CONDITIONING BAY. REPLACED SUPPORT ANGLE IAW SRM 51-10-02; SRM 51-40-02. AND DRAWING 111A1000; SHEET 31; REV A.
- [SDR SWAA2025110521057](https://openairdocs.org/sdr/SWAA2025110521057.md): Support Beam · cracked · Oct 3, 2025 · N8620H · Boeing 7378H4 · Service Doors
  > CRACK SUPPORT BEAM NR 4 LOCATED FWD GALLEY DOOR. REPLACED SUPPORT BEAM NR 4 AND FASTENERS IAW SRM 51-10-02; SRM 51-40-02; DWG 141A6535, SHEET 13, REV -, AND DWG 141A6516, SHEET 142, REV -.
- [SDR SWAA2025110521062](https://openairdocs.org/sdr/SWAA2025110521062.md): Support Angle · cracked · Oct 3, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BODY STA 663.75 RBL 35 AT AIR CONDITIONING BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02; SRM 51-40-02 AND DRAWING 111A1000; SHEET 31; REV A.
- [SDR SWAA2025110520967](https://openairdocs.org/sdr/SWAA2025110520967.md): Support Angle · cracked · Oct 3, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE BTW BS 380 - 400, LBL 13, WL 208.1. REPLACED SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, DWG 143A5400, SHEET 138, REV -, & DWG 143A5400, SHEET 142, REV -.
- [SDR SWAA2025110520965](https://openairdocs.org/sdr/SWAA2025110520965.md): Support Angle · cracked · Oct 3, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 52 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 52 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-01, DWG 143A5400, SHEET 14, REV -, & DWG 143A5400, SHEE
- [SDR SWAA2025110520968](https://openairdocs.org/sdr/SWAA2025110520968.md): Support Angle · cracked · Oct 3, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 39 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 39 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02; DWG 143A5400; SHEET 140; REV- AND DWG 143A5400, SHEE
- [SDR SWAA2025110520670](https://openairdocs.org/sdr/SWAA2025110520670.md): Support · corroded · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION LOWER SILL LOCATED BTW BS 794.3 TO BS 847 RBL 22 WL 156.1. REMOVED AND REPLACED LOWER SILL AND FASTENERS LOCATED BTW BSTA 794.3 TO BSTA 847. RBL 22 AND WL 156.1. AT AFT CARGO COMPARTMENT. IAW SRM 51-10-02 PARAGRAPH 9. SRM 51-40-02. AND DWG 146A8340
- [SDR SWAA2025110520667](https://openairdocs.org/sdr/SWAA2025110520667.md): Skin · corroded · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > CORROSION INTERNAL SKIN LOCATED BTW STA 727D TO STA 727E BTW STR 27L TO STR 27R AND WL 148.5 AT AFT CARGO. GAINED ACCESS LOCATED BTW STA 727D TO STA 727E BTW STR 27L TO STR 27R AND WL 148.5 THE CORROSION FOUND ON VHF COMMUNICATION ANTENNA #2 ONLY AT LOWER FUS
- [SDR SWAA2025110520561](https://openairdocs.org/sdr/SWAA2025110520561.md): Tie Clip · cracked · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON TIE CLIP LOCATED BS 500I AT LEVE STR 26R AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP AND FASTENERS LOCATED BS 500I ON STRINGER 26R AT FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 143A1234 SHEET 14 REV A.
- [SDR SWAA2025110520562](https://openairdocs.org/sdr/SWAA2025110520562.md): Support Angle · corroded · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ANGLE LOCATED BS 500I BTW STR26L TO STR 26R AT FWD CARGO. PERFORMED CLEAN ON AREA AND APPLIED PAINT SUPPORT ANGLE LOCATED BS 500I BTW STR26L TO STR 26R AT FWD CARGO COMPARTMENT IAW SOPM 20-30-03 AMM 51-21-99-300-801.
- [SDR SWAA2025110520676](https://openairdocs.org/sdr/SWAA2025110520676.md): Plate · corroded · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION PLATE BTW STA 827 TO STA 847, STR 25R TO STR 26R WL 156. REPLACED THE PLATE IAW SRM 51-10-02; SRM 51-40-02 AND DWG 146A8340 SHEET 28 REV -.
- [SDR SWAA2025110520672](https://openairdocs.org/sdr/SWAA2025110520672.md): Plate · corroded · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORRODED PLATE BTW STA 794.3 TO STA 807 BTW STR 25R TO STR 26R WL 156. REPLACED PLATE IAW SRM 51-10-02; SRM 51-40-02 AND DWG 146A8340 SHEET 28 REV -.
- [SDR SWAA2025110520567](https://openairdocs.org/sdr/SWAA2025110520567.md): Web · cracked · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED WEB, BS 500 - 500A, STRINGER 26L. REPLACED THE WEB IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 124, SHEET 125, REV -.
- [SDR SWAA2025110520665](https://openairdocs.org/sdr/SWAA2025110520665.md): Support · corroded · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORRODED SUPPORT ZEE, BS 727I - 807, LBL 21, WL 156.1. REPLACED SUPPORT ZEE IAW SRM-53-00-53-2R-5, REPAIR 5, SRM-51-40-02, DWG:146A7500, SHEET 233, REV-, & DWG 146A7500, SHEET 236, REV-.
- [SDR SWAA2025110520669](https://openairdocs.org/sdr/SWAA2025110520669.md): Shield · corroded · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORRODED SHIELD, BS 767 - 794.3, STRINGER 25R, WL 165. REPLACED THE SHIELD AND FASTENERS IAW SRM 51-40-02, & DWG 146A0081, SHEET 49, REV A.
- [SDR SWAA2025110520674](https://openairdocs.org/sdr/SWAA2025110520674.md): Strap · corroded · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROED STRAP, BS 767 - 787, STRINGERS 25L - 25R. REPLACED THE STRAP IAW SRM 51-10-02, ITEM 9, NO ALLOWABLE DAMAGE IN SRM.
- [SDR SWAA2025110520675](https://openairdocs.org/sdr/SWAA2025110520675.md): Web · cracked · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED WEB, BS 927 - 947.5, RBL 21. REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02, AND DWG 147A7500, SHEET 37, REV -.
- [SDR SWAA2025110520663](https://openairdocs.org/sdr/SWAA2025110520663.md): Angle · cracked · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BS 867 BTW STRINGERS 26L - 27L. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, AND DRAWING 149A8102, SHEET 19, REV A.
- [SDR SWAA2025110520673](https://openairdocs.org/sdr/SWAA2025110520673.md): Angle · corroded · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORRODED ANGLE BTW BS 767 - 787, STRINGER 25R, WL 165. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02, AND DWG 146A8123, SHEET 16, REV-.
- [SDR SWAA2025110420560](https://openairdocs.org/sdr/SWAA2025110420560.md): Shield · corroded · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORRODED SHIELD WEB LOCATED BTW BS 492.4 - 500A, RBL 22, WL 208.1. REPLACED SHIELD WEB IAW SRM 51-10-02; B737-800 SRM 51-40-02 AND DRAWING 143A0080 SHEET: 39 REV: A.
- [SDR SWAA2025110420563](https://openairdocs.org/sdr/SWAA2025110420563.md): Support · corroded · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS 500F - 500I, RBL 22, FWD CARGO BAY. REMOVED DAMAGE AND EVALUATED REWORK AREA ON SUPPORT ZEE IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 PARAGRAPH 4.A(2)(A); FIGURE 103 DETAIL D.
- [SDR SWAA2025110420566](https://openairdocs.org/sdr/SWAA2025110420566.md): Support · corroded · Oct 2, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS 500A TO 500F, RBL 22, WL 208.1 IN THE FWD CARGO BAY. REMOVED DAMAGE AND EVALUATED REWORK AREA ON SUPPORT ZEE LOCATED BTW BS 500A TO 500F, RBL 22, WL 208.1 IAW SRM 53-00-53-1A-2, ALLOWABLE DAMAGE 2, PARAGRAPH 4 A, 2 A,
- [SDR SWAA2025110520293](https://openairdocs.org/sdr/SWAA2025110520293.md): Nut Plate · cracked · Oct 1, 2025 · N8620H · Boeing 7378H4 · Wing, Attach Fittings
  > CRACK OUTBOARD FRONT SPAR RAIL NUT PLATE OFSS 573 AT LT WING. REPLACED RAIL NUT PLATE LOCATED OUTBOARD FRONT SPAR OFSS 573 AT LT WING IAW B737-800 SRM 51-40-02-0G; SRM 51-10-02-0G-0 ITEM 9 AND DWG 112A4402 SHEET: 41 REV: A. MEASUREMENT OF CRACK IS L: 0.392 I
- [SDR SWAA2025110520295](https://openairdocs.org/sdr/SWAA2025110520295.md): Nut Plate · cracked · Oct 1, 2025 · N8620H · Boeing 7378H4 · Wing, Attach Fittings
  > CRACK OUTBOARD FRONT SPAR RAIL NUT PLATE OFSS 491 AT LT WING. REPLACED RAIL NUT PLATE LOCATED OUTBOARD FRONT SPAR OFSS 491 AT LT WING IAW B737-800 SRM 51-40-02-0G; SRM 51-10-02-0G-0 ITEM 9 AND DWG 112A4402 SHEET: 40 REV: A. MEASUREMENT OF CRACK IS L: 0.254 I
- [SDR SWAA2025110520187](https://openairdocs.org/sdr/SWAA2025110520187.md): Tie Clip · cracked · Oct 1, 2025 · N8620H · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACK TIE CLIP FRAME ON BS 277 AND STR10R AT FWD GALLEY AREA. REPLACED TIE CLIP LOCATED ON BS 277 AND STR 10R AT FWD GALLEY AREA. IAW SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG: 141A1150 SHEET: 55 REV -.
- [SDR SWAA2025110520296](https://openairdocs.org/sdr/SWAA2025110520296.md): Nut Plate · cracked · Oct 1, 2025 · N8620H · Boeing 7378H4 · Wing, Attach Fittings
  > CRACK OTBD FRONT SPAR RAIL NUT PLATE OFSS 333 AT LT WING. REPLACED THE NUT PLATE LOCATED OTBD FRONT SPAR OFSS 333 IAW SRM 51-40-02-0G; SRM 51-10-02-0G-0, ITEM 9, AND DWG 112A4402 SHEET: 40 REV: A. MEASUREMENT OF CRACK L: 0.232.
- [SDR SWAA2025110520292](https://openairdocs.org/sdr/SWAA2025110520292.md): Nut Plate · cracked · Oct 1, 2025 · N8620H · Boeing 7378H4 · Wing, Attach Fittings
  > CRACK ON RAIL NUT PLATE FRONT SPAR OFSS 604 AT LT WING. REPLACED THE NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 112A4402, SHEET 41, REV A.
- [SDR SWAA2025110520294](https://openairdocs.org/sdr/SWAA2025110520294.md): Nut Plate · cracked · Oct 1, 2025 · N8620H · Boeing 7378H4 · Wing, Attach Fittings
  > CRACK OUTBOARD FRONT SPAR RAIL NUT PLATE OFSS 506 AT LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G, & DWG 112A4402, SHEET 40, REV A. MEASUREMENT OF CRACK IS L: 0.168 INCHES.
- [SDR SWAA2025110519729](https://openairdocs.org/sdr/SWAA2025110519729.md): Seat Track · deteriorated · Sep 30, 2025 · N8620H · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings
  > DETERIORATED SEAT TRACK SEAT ROWS 3(INB) AND 20(OUT) AT PASSENGER CABIN. REPLACED SEAT TRACK IAW CMM 25-22-46-3500 REV. 8 PAGE 3015 DISASSEMBLY STEP 3.AA.(5) AND PAGE 7003 ASSEMBLY STEP 3.B.(3).
- [SDR SWAA2025110519408](https://openairdocs.org/sdr/SWAA2025110519408.md): Floorbeam · corroded · Sep 29, 2025 · N8620H · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM LOCATED BS 986.5 RBL 42 WL 208.1. REPAIRED FLOORBEAM IAW SRM 53-70-51-2R-6 REPAIR 6.
- [SDR SWAA2025110519259](https://openairdocs.org/sdr/SWAA2025110519259.md): Support Angle · corroded · Sep 29, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ANGLE - SUPPORT LOCATED STA 500I BTW STR 24L TO STR 26L AND WL 156 AT FWD CARGO. REMOVED DAMAGE AND EVALUATED REWORK AREA (3 EA) ON ANGLE - SUPPORT LOCATED STA 500I BTW STR 24L TO STR 26L AND WL 156 IAW SRM 53-30-08-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH
- [SDR SWAA2025110519250](https://openairdocs.org/sdr/SWAA2025110519250.md): Access Panel · cracked · Sep 29, 2025 · N8620H · Boeing 7378H4 · Aerodynamic Fairings
  > CRACK ANTENNA ACCESS PANEL 192F WING TO BODY FAIRING AT FUSELAGE EXTERIOR. REMOVED AND REPLACED MARKER BEACON ANTENNA ON ACCESS PANEL 192F WING TO BODY FAIRING AT FUSELAGE EXTERIOR IAW AMM 34-32-11-400-802 TESTED OK.
- [SDR SWAA2025110519254](https://openairdocs.org/sdr/SWAA2025110519254.md): Floorbeam · cracked · Sep 29, 2025 · N8620H · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CRACKED FLOORBEAM, BS 540, BL 0 - LBL 24.75, WL 208.1. REPLACED THE FLOORBEAM IAW SRM 51-10-02 ITEM 9, SRM 51-40-02-0G, & DWG143A0060, SHEET 64, REV-.
- [SDR SWAA2025110519413](https://openairdocs.org/sdr/SWAA2025110519413.md): Support Angle · cracked · Sep 29, 2025 · N8620H · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK CARGO LINER SUPPORT ANGLE, CEILING AREA, BS 727J, LBL 50. REPAIRED THE SUPPORT ANGLE IAW SRM 51-70-11-2R-0.

Next page: https://openairdocs.org/deregistered/N8620H-2026-01-30/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 = 'N8620H' AND deregistration_id = 'N8620H-2026-01-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8620H-2026-01-30/reports

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