# Service difficulty reports: N8625A, cancelled Mar 6, 2026 A list on [N8625A, cancelled Mar 6, 2026](https://openairdocs.org/deregistered/N8625A-2026-03-06.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 · 188 reports - [SDR SWAA2026021962632](https://openairdocs.org/sdr/SWAA2026021962632.md): Bulb · burned out · Jan 19, 2026 · N8625A · Boeing 7378H4 · Emergency Lighting > EXIT SIGNS AT 14ABC; 14DEF AND 15BC HAS BULBS BURNED OUT<[01] REPLACED THE EXIT SIGN LAMPS, 14ABC;14DEF AND 15BC IAW AMM 33-51-01-960-801 PERFORMED OPERATIONAL TESTED GOOD. - [SDR SWAA2026011343848](https://openairdocs.org/sdr/SWAA2026011343848.md): Angle · cracked · Dec 8, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 500H, LBL 21 IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026011343849](https://openairdocs.org/sdr/SWAA2026011343849.md): Angle · cracked · Dec 8, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 500G, RBL 21 IN FWD FWD CARGO. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, 51-40-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026011343850](https://openairdocs.org/sdr/SWAA2026011343850.md): Angle · cracked · Dec 8, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 500H, RBL 21 IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, 51-40-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026011343855](https://openairdocs.org/sdr/SWAA2026011343855.md): Angle · cracked · Dec 8, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 500H, LBL 21. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, 51-40-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026011343856](https://openairdocs.org/sdr/SWAA2026011343856.md): Angle · cracked · Dec 8, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 500H, RBL 21. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, 51-40-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026011343852](https://openairdocs.org/sdr/SWAA2026011343852.md): Angle · cracked · Dec 8, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 400, LBL 21, FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02-0G, AND DWG 143A7505, SHEET 137, REV -. - [SDR SWAA2026011343851](https://openairdocs.org/sdr/SWAA2026011343851.md): Shield · cracked · Dec 8, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK SHIELD WEB, BTW BS492.4 - 500A, RBL 21 IN THE FWD CARGO BAY. REPLACED SHIELD WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A0080, SHEET 39, REV -. - [SDR SWAA2026011243857](https://openairdocs.org/sdr/SWAA2026011243857.md): Support · corroded · Dec 8, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION SUPPORT ZEE LOCATED BTW BS 500A TO BS 500I RBL 21 AND WL 156 AT FWD CARGO COMPARTMENT, THE DAMAGE WAS REPAIR IAW SRM 53-00-53-2R-5 AND EA M-22-153-01550. - [SDR SWAA2026010943624](https://openairdocs.org/sdr/SWAA2026010943624.md): Support Bracket · cracked · Dec 7, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ON SUPPORT BRACKET PNEUMATIC DUCT LOCATED BS 540, LBL 6 IN THE AIR CONDITIONING BAY. - [SDR SWAA2026011343419](https://openairdocs.org/sdr/SWAA2026011343419.md): Support Angle · cracked · Dec 6, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE BTW BS 380 - 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 177, REV A. - [SDR SWAA2026011343429](https://openairdocs.org/sdr/SWAA2026011343429.md): Support Angle · cracked · Dec 6, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, BTW BS 380 - 400, RBL 40, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 184, REV -. - [SDR SWAA2026011343432](https://openairdocs.org/sdr/SWAA2026011343432.md): Support Angle · cracked · Dec 6, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, BTW BS 380 - 400, LBL 53, WL 208.1. REPLACED THE SUPPORT ANGLE & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 183, REV-. - [SDR SWAA2026011343427](https://openairdocs.org/sdr/SWAA2026011343427.md): Tie Clip · cracked · Dec 6, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED TIE CLIP, BS 277, S10R IN FWD GALLEY. MEASUREMENT OF CRACK: L: 0.416 INCHES. REPLACED TIE CLIP IAW SRM 51-10-02-0G, SRM 51-40-02-0G, AND DWG 141A1110, SHEET 55, REV-. - [SDR SWAA2026011343428](https://openairdocs.org/sdr/SWAA2026011343428.md): Support Angle · cracked · Dec 6, 2025 · N8625A · 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, AND DWG 143A5400, SHEET 184, REV -. - [SDR SWAA2026011343426](https://openairdocs.org/sdr/SWAA2026011343426.md): Frame · cracked · Dec 6, 2025 · N8625A · Boeing 7378H4 · Fuselage Main, Frame > CRACK ON FRAME, BS 312 BTW S5 - 6L. PERFORMED PERMANENT REPAIR TO THE FRAME IAW EA M-22-153-01244, REV B. - [SDR SWAA2026011343508](https://openairdocs.org/sdr/SWAA2026011343508.md): Support Bracket · cracked · Dec 6, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ON SUPPORT BRACKET, BS 867 BTW S2 & 3R. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 146A7901, SHEET 66, REV A. - [SDR SWAA2026011343155](https://openairdocs.org/sdr/SWAA2026011343155.md): Support Angle · corroded · Dec 5, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORRODED SUPPORT ANGLE, BTW BS 767 - 887, WL156, AND RBL 21 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 146A8123, SHEET 16, REV -. - [SDR SWAA2026011343141](https://openairdocs.org/sdr/SWAA2026011343141.md): Intercostal · cracked · Dec 5, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ON INTERCOSTAL WEB, BTW BS 344 - 360, RBL 12, WL 208.1. PERFORMED A PERMANENT REPAIR ON WEB INTERCOSTAL IAW SRM 53-10-51-2R-20, REPAIR 20. - [SDR SWAA2026011343145](https://openairdocs.org/sdr/SWAA2026011343145.md): Intercostal · cracked · Dec 5, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED INTERCOSTAL WEB, BTW BS 344 - 360, BL 0, WL 208.1. REPLACED NEW INTERCOSTAL WEB AND FASTENERS IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G, AND DRAWING 141A5400, SHEET 32, REV -. - [SDR SWAA2026011343146](https://openairdocs.org/sdr/SWAA2026011343146.md): Intercostal · cracked · Dec 5, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED INTERCOSTAL WEB, BTW BS 344 - 360, LBL 12, WL 208.1. REPLACED THE INTERCOSTAL WEB AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 141A5400, SHEET 46, REV A. - [SDR SWAA2026011343160](https://openairdocs.org/sdr/SWAA2026011343160.md): Plate · cracked · Dec 5, 2025 · N8625A · Boeing 7378H4 · Wing Main, Frame Structure > CRACKED CORRUGATED PLATE TRAILING EDGE LOCATED BETWEEN ORSS290 TO ORSS297, LT WING. REPLACED CORRUGATED PLATE AND FASTENERS TRAILING EDGE, LT WING IAW SRM 51-40-02, DWG 115A3700, SHEET 81, REV A, AND DWT 115A3712, SHEET 5, REV -. - [SDR SWAA2026011347409](https://openairdocs.org/sdr/SWAA2026011347409.md): Structure · cracked · Dec 5, 2025 · N8625A · Boeing 7378H4 · Fuselage Main, Plate/Skin > CRACK INNER CHORD LOCATED BS 303.9, S17L. REPLACED INNER CHORD BTW BS 270 - 370, S17L IAW SRM 51-40-02-0G-0, DWG 141A8110, SHEET 3, REV E, DWG 141A8110, SHEET 11, REV -, DWG 141A8110, SHEET 24, REV-, DWG 140A9810, SHEET 53, REV-, AND DWG 143A5900, SHEET 12, R - [SDR SWAA2026011343149](https://openairdocs.org/sdr/SWAA2026011343149.md): Plate · cracked · Dec 5, 2025 · N8625A · Boeing 7378H4 · Wing Main, Frame Structure > CRACK CORRUGATED PLATE TRAILING EDGE ORSS 297 RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 115A3712, SHEET 7, REV A, AND DWG 115A3700, SHEET 41, REV -. - [SDR SWAA2026011343150](https://openairdocs.org/sdr/SWAA2026011343150.md): Plate · cracked · Dec 5, 2025 · N8625A · Boeing 7378H4 · Wing Main, Frame Structure > CRACK CORRUGATED PLATE T/E IRSS 215 ON RT WING. REPLACED CORRUGATED PLATE LOCATED ON RT WING TRAILING EDGE IAW SRM 51-40-02, AND DWG 115A2001, SHEET 67, AND REV -. - [SDR SWAA2026011343148](https://openairdocs.org/sdr/SWAA2026011343148.md): Web · cracked · Dec 5, 2025 · N8625A · Boeing 7378H4 · Wing Miscellaneous Structure > CRACK WEB T/E FIXED PANEL ORSS 271 ON RT WING. REPLACED WEB IAW SRM 51-40-02, AND DWG 115A2512, SHEET 16, REV -. - [SDR SWAA2026011343142](https://openairdocs.org/sdr/SWAA2026011343142.md): Web · cracked · Dec 5, 2025 · N8625A · Boeing 7378H4 · Engine Cowling System > CRACK WEB FAN COWL INBOARD LOC. INTERNAL AREA ACCESS DOOR 414AR ON NR 1 ENGINE. REPLACED WEB FAN COWL INBD INTERNAL AREA ACCESS DOOR 414AR IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND CMM 71-13-30, REV 31, SHEETS 10092 & 10110. LENGTH OF CRACK: 0.870 IN. - [SDR SWAA2026011343151](https://openairdocs.org/sdr/SWAA2026011343151.md): Web · cracked · Dec 5, 2025 · N8625A · Boeing 7378H4 · Engine Cowling System > CRACKED OUTBOARD FAN COWL WEB, INTERNAL AREA ACCESS DOOR 424AR ON NR 2 ENGINE. REPLACED WEB LOCATED ON OTBD FAN COWL INTERNAL AREA ACCESS DOOR 424AR IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND CMM 71-13-30, REV 31, SHEETS 10092 & 10110. LENGTH OF CRACK: 0 - [SDR SWAA2026011243152](https://openairdocs.org/sdr/SWAA2026011243152.md): Intercostal · cracked · Dec 5, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ON WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947.5 AND RBL21 AFT CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947.5 AND RBL21 AFT CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG 147A7500 SHEET 37 REV-. - [SDR SWAA2026011243153](https://openairdocs.org/sdr/SWAA2026011243153.md): Support Angle · cracked · Dec 5, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ON ANGLE - SUPPORT LOCATED BS867 AND LBL 10 AFT CARGO COMPARTMENT. REPLACED ANGLE - SUPPORT LOCATED BS867 AND LBL 10 AFT CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02. MEASURE OF CRACK IS: 0.375 INCH. - [SDR SWAA2026011243154](https://openairdocs.org/sdr/SWAA2026011243154.md): Web · corroded · Dec 5, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION ON SHIELD WEB LOCATED BTW BS767 TO BS794.3 WL156 AND RBL21 AT AFT CARGO COMPARTMENT. REPLACED SHIELD WEB LOCATED BTW BS767 TO BS794.3 WL156 AND RBL21 AT AFT CARGO COMPARTMENT IAW 737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET: 49 R - [SDR SWAA2026011243156](https://openairdocs.org/sdr/SWAA2026011243156.md): Support · corroded · Dec 5, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION ON SUPPORT ZEE LOCATED BTW BS727E PLUS 10INCH TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT. REPAIRED SUPPORT ZEE LOCATED BTW 727 TO 767 AT AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-6 SRM 51-40-02 DWG 146A7500 SHEET 233 REV - AND DWG 146A7502 SHEET - [SDR SWAA2026011243159](https://openairdocs.org/sdr/SWAA2026011243159.md): Support · corroded · Dec 5, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION SUPPORT ZEE LOCATED BTW BS 727G PLUS 10INCH TO BS807 PLUS 10INCH WL156 AND LBL21 AFT CARGO COMPARTMENT. REPAIRED SUPPORT ZEE CHANNEL LOCATED BTW BS 727G - BS 807 WL156 AND LBL21 AFT CARGO COMPARTMENT IAW SRM 51-40-02 DWG 146A7500 SHEET 233 REV - AND - [SDR SWAA2026010843144](https://openairdocs.org/sdr/SWAA2026010843144.md): Frame · cracked · Dec 5, 2025 · N8625A · Boeing 7378H4 · Fuselage Main, Frame > CRACK INNER CHORD LOCATED BS 303.9 AT LEVEL OF STR 17L AT FWD GALLEY AREA. - [SDR SWAA2026011342430](https://openairdocs.org/sdr/SWAA2026011342430.md): Intercostal · corroded · Dec 4, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL BTW BS 947 - 967, LBL 50, WL 208.1. REPLACED THE INTERCOSTAL IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 147A5650, SHEET 54, REV A. - [SDR SWAA2026011342674](https://openairdocs.org/sdr/SWAA2026011342674.md): Nut Plate · corroded · Dec 4, 2025 · N8625A · Boeing 7378H4 · Wing, Attach Fittings > CORROSION OTBD FRONT SPAR RAIL NUT PLATE OFSS 548 ON LT WING. REPLACED THE SPAR RAIL NUT PLATE OFSS 548, FASTENERS IAW SRM 51-40-02, AND DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026011342675](https://openairdocs.org/sdr/SWAA2026011342675.md): Nut Plate · corroded · Dec 4, 2025 · N8625A · Boeing 7378H4 · Wing, Attach Fittings > CORROSION OTBD FRONT SPAR RAIL NUT PLATE OFSS 449 LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026011342673](https://openairdocs.org/sdr/SWAA2026011342673.md): Nut Plate · corroded · Dec 4, 2025 · N8625A · Boeing 7378H4 · Wing, Attach Fittings > CORROSION OTBD FRONT SPAR RAIL NUT PLATE OFSS 652 ON LT WING. REPLACED OTBD FRONT SPAR RAIL NUT PLATE IAW SRM 51-40-02, 51-10-02, ITEM 9, AND DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026011342676](https://openairdocs.org/sdr/SWAA2026011342676.md): Nut Plate · corroded · Dec 4, 2025 · N8625A · Boeing 7378H4 · Wing, Attach Fittings > CORROSION OTBD FRONT SPAR RAIL NUT PLATE OFSS 421 ON LT WING. REPLACED THE RAIL NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026011342677](https://openairdocs.org/sdr/SWAA2026011342677.md): Nut Plate · corroded · Dec 4, 2025 · N8625A · Boeing 7378H4 · Wing, Attach Fittings > CORROSION OTBD FRONT SPAR RAIL NUT PLATE OFSS 527 ON LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02 AND DWG: 112A4402, SHEET 40, REV A. - [SDR SWAA2026011242863](https://openairdocs.org/sdr/SWAA2026011242863.md): Support Angle · cracked · Dec 4, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK SUPPORT ANGLE AT BULKHEAD BS 663.75 AND LBL 10 CENTER SECTION. PERFORMED PERMANENT REPAIR ON ANGLE LOCATED AT BS 663 BTW LBL 6 TO LBL 25 IAW B737-800 SRM 57-10-10-2R-5. - [SDR SWAA2026011242864](https://openairdocs.org/sdr/SWAA2026011242864.md): Support Angle · cracked · Dec 4, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK SUPPORT ANGLE AT BULKHEAD BS 663.75 AND RBL 10 CENTER SECTION. PERFORMED PERMANENT REPAIR ON ANGLE LOCATED AT BS 663 BTW RBL 6 TO RBL 25 IAW SRM 57-10-10-2R-5. - [SDR SWAA2026011342262](https://openairdocs.org/sdr/SWAA2026011342262.md): Angle · cracked · Dec 3, 2025 · N8625A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED GUSSET ANGLE, BS 500I, S19R. REPLACED THE GUSSET ANGLE AND FASTENERS IAW SRM 51-40-02-0G, & DWG 143A7902, SHEET 256, REV B. - [SDR SWAA2026011242260](https://openairdocs.org/sdr/SWAA2026011242260.md): Balance Weight · out of balance · Dec 3, 2025 · N8625A · Boeing 7378H4 · Elevator Structure > DURING WEIGHT AND BALANCE PROCEDURE OF RT ELEVATOR FOUND BALANCE WEIGHTS (1EA) ON BAY 2; P/N: 183A0210-14 (1EA) AND P/N: 69-53211-2 (2EA) ON BAY 3; P/N: 183A0210-15 2025-733159<[01] TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-03767;[02] TASK CARD ACCOMPLISHED - [SDR SWAA2026011241571](https://openairdocs.org/sdr/SWAA2026011241571.md): Floor Panel · damaged · Dec 2, 2025 · N8625A · Boeing 7378H4 · Fuselage Floor Panel > ELONGATED HOLES ON FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT. REPLACED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW SRM 51-10-02 TEM 9 AND DWG 453A2610, SHEET 26, REV E. - [SDR SWAA2026011341570](https://openairdocs.org/sdr/SWAA2026011341570.md): Stub Frame · cracked · Dec 1, 2025 · N8625A · Boeing 7378H4 · Fuselage Main, Frame > CRACK INDICATION ON STUB FRAME BTWN BS 294.5 - 296.5, S8-9R. CRACK LENGTH: 0.375 IN. REPLACED THE STUB FRAME IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 141A8370, SHEET 9, REV D. - [SDR SWAA2026011341328](https://openairdocs.org/sdr/SWAA2026011341328.md): Support Angle · cracked · Dec 1, 2025 · N8625A · Boeing 7378H4 · Aerodynamic Fairings > CRACK ON SUPPORT ANGLE LOCATED BS 500I, S19R BELLY FAIRING. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG 116A3110, SHEET 8, REV -, AND DWG 149A7101, SHEET 11, REV -. - [SDR SWAA2026011341330](https://openairdocs.org/sdr/SWAA2026011341330.md): Access Panel · elongated · Dec 1, 2025 · N8625A · Boeing 7378H4 · Wing, Plate/Skin > ELONGATED HOLES ON ACCESS PANEL 661CB T/E, RT WING. REPAIRED THE ACCESS PANEL 661CB IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2026011341029](https://openairdocs.org/sdr/SWAA2026011341029.md): Adapter · deteriorated · Nov 30, 2025 · N8625A · Boeing 7378H4 · Emergency Equipment > DETERIORATED ADAPTER PLATE AND SHIM ON GIRT BAR FITTING, FWD ENTRY, & SERVICE DOORS. REPLACED THE ADAPTER PLATE AND SHIM IAW AMM 25-66-02-400-801, STEP 3 D, 1, A, B,J, AND WILL BE INSTALLED ON TASK CARD 725-025-00-01Y TTG8Q0194LLX,STEP 13. - [SDR SWAA2026011341036](https://openairdocs.org/sdr/SWAA2026011341036.md): Adapter · deteriorated · Nov 30, 2025 · N8625A · Boeing 7378H4 · Emergency Equipment > DETERIORATED ADAPTER PLATE AND SHIM ON THE GIRT BAR FITTING ON THE AFT ENTRY AND SERVICE DOORS. REPLACED THE ADAPTER PLATE AND SHIM IAW AMM 25-66-02-400-801, STEP 3.D, 1 A, B, J, & WILL BE INSTALLED ON TASK CARD 725-025-00-02Y TTG8R008CU1R STEP 13. Next page: https://openairdocs.org/deregistered/N8625A-2026-03-06/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 = 'N8625A' AND deregistration_id = 'N8625A-2026-03-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N8625A-2026-03-06/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.