# Service difficulty reports: N8629A A list on [N8629A](https://openairdocs.org/aircraft/N8629A.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 · 174 reports - [SDR SWAA2026100722692](https://openairdocs.org/sdr/SWAA2026100722692.md): Light · unsecure · Oct 3, 2026 · N8629A · Boeing 7378H4 · Emergency Lighting > EXIT ROW LIGHT STRIP PULLED UP FROM CARPET ABEAM ROW 12ABC. SECURED THE FLOOR PROXIMITY PHOTO LUMINESCENT IAW AMM 33-51-15. - [SDR SWAA2026042391053](https://openairdocs.org/sdr/SWAA2026042391053.md): Sign · loose · Apr 20, 2026 · N8629A · Boeing 7378H4 · Emergency Lighting > OVERWING EXIT ROW EXIT SIGN LOOSE. RESECURED EMER EXIT SIGN IN REF TO AMM 33-51-01. - [SDR SWAA2026040183895](https://openairdocs.org/sdr/SWAA2026040183895.md): Light · intermittent · Mar 28, 2026 · N8629A · Boeing 7378H4 · Emergency Lighting > MID-CABIN CEILING EXIT SIGNAGE LIGHT FLASHES INTERMITTENTLY. INSPECTED MID CABIN EMERGENCY EXIT LIGHT ASSY. AND FOUND OPERATION TO BE NORMAL IAW AMM 33-51-00. FLICKER FOUND TO BE FROM CEILING LIGHT ASSY AT 15 DEF. OK TO CONTINUE PER MEL 33-2-04, SP1B AUTH 31 - [SDR SWAA2026031270649](https://openairdocs.org/sdr/SWAA2026031270649.md): Handle · broken · Feb 13, 2026 · N8629A · Boeing 7378H4 · Passenger/Crew Doors > BROKEN ASSIST HANDLE DOOR LINING FWD ENTRY DOOR AT FWD GALLEY AREA 2EA. REPLACED ASSIST HANDLE DOOR LINING FWD ENTRY DOOR AT FWD GALLEY AREA 2EA IAW AMM-52-11-31-400-802, STEP 3.G. - [SDR SWAA2026031269986](https://openairdocs.org/sdr/SWAA2026031269986.md): Battery Pack · inoperative · Feb 12, 2026 · N8629A · Boeing 7378H4 · Emergency Lighting > BATTERY PACK LOCATED BETWEEN BS 559 & 578, RT SIDE IN PAX CABIN. REPLACED THE BATTERY PACK LOCATED BETWEEN BS 559 & 578 IAW AMM 33-51-06-960-805, STEP 4.E.(4) THRU (6). TESTED OK. - [SDR SWAA2026031269985](https://openairdocs.org/sdr/SWAA2026031269985.md): Battery Pack · inoperative · Feb 12, 2026 · N8629A · Boeing 7378H4 · Emergency Lighting > BATTERY PACK LOCATED BETWEEN STA 500C AND STA 500D RH SIDE IN PAX CABIN INOPERATIVE. REPLACED BATTERY PACK LOCATED BETWEEN BS 500C & 500D RT SIDE IN PAX CABIN IAW AMM 33-51-06-960-805, STEP 4.E.(4) THRU (6).TESTED OK. - [SDR SWAA2026031669862](https://openairdocs.org/sdr/SWAA2026031669862.md): Access Panel · cracked · Feb 11, 2026 · N8629A · Boeing 7378H4 · Nacelle/Pylon, Plate/Skin > CRACK SEAL PLATE ACCESS PANEL 441AT INBOARD POSITION RT PYLON. REPLACED SEAL PLATE ACCESS PANEL 441AT INBOARD POSITION RT PYLON IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9 MEASURE CRACK IS L: 0.429 INCH. - [SDR SWAA2026031269861](https://openairdocs.org/sdr/SWAA2026031269861.md): Support Angle · cracked · Feb 11, 2026 · N8629A · Boeing 7378H4 · Wing Miscellaneous Structure > CRACKED SUPPORT ANGLE, ACCESS PANEL 551FB, LT WING. REPLACED THE SUPPORT ANGLE FOR ACCESS PANEL 551FB, LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 115A2710, SHEET 9, REV A. - [SDR SWAA2026031669457](https://openairdocs.org/sdr/SWAA2026031669457.md): Support Bracket · cracked · Feb 10, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK SUPPORT BRACKET LOCATED ON PNEUMATIC DUCT BS 540, LBL 6 IN AIR CONDITIONING BAY. PERFORMED INSPECTION OF DAMAGE ON SUPPORT BRACKET LOCATED BS 540 LBL 6 AT AIR CONDITIONING BAY IAW SRM 51-10-02-0G-0, ITEM 9. - [SDR SWAA2026031669622](https://openairdocs.org/sdr/SWAA2026031669622.md): Nut Plate · corroded · Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing, Attach Fittings > CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS548 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS548 AT LT WING IAW SRM 51-40-02-0G;SRM 51-10-02-0G ITEM 9 AND DWG 112A4402 SHEET 40 REV A. - [SDR SWAA2026031669455](https://openairdocs.org/sdr/SWAA2026031669455.md): Support Angle · cracked · Feb 10, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, BS 500I, STR 28R. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02 ITEM 9; SRM 51-40-02, AND DWG 143A7902 SHEET 320, REV -. - [SDR SWAA2026031669623](https://openairdocs.org/sdr/SWAA2026031669623.md): Nut Plate · corroded · Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing, Attach Fittings > CORROSION ON RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS421 AT LT WING. REPLACED RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS421 AT LT WING IAW SRM 51-40-02-0G, SRM 51-10-02-0G, ITEM 9, AND DWG 112A4402, SHEET 40, REV A, AND PERFORMED - [SDR SWAA2026031669620](https://openairdocs.org/sdr/SWAA2026031669620.md): Nut Plate · corroded · Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing, Attach Fittings > CORROSION ON RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS541 AT LT WING. REPLACED RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS541 AT LT WING IAW SRM 51-40-02-0G, SRM 51-10-02-0G, ITEM 9, AND DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026031669618](https://openairdocs.org/sdr/SWAA2026031669618.md): Nut Plate · corroded · Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing, Attach Fittings > CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS761 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS761 AT LT WING IAW SRM 51-40-02-0G AND DWG 112A4402, SHEET 41, REV A. - [SDR SWAA2026031669624](https://openairdocs.org/sdr/SWAA2026031669624.md): Nut Plate · corroded · Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing, Attach Fittings > CORROSION ON RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS416 AT LT WING. REPLACED RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS416 AT LT WING IAW SRM 51-40-02-0G;SRM 51-10-02-0G, ITEM 9 AND DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026031669627](https://openairdocs.org/sdr/SWAA2026031669627.md): Nut Plate · corroded · Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing Miscellaneous Structure > CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS287 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS287 AT LT WING IAW B737-800 SRM 51-40-02-0G; SRM 51-10-02-0G Ï¿½TEM 9 AND DWG 112A4402 SHEET 40 REV A; AN - [SDR SWAA2026031669626](https://openairdocs.org/sdr/SWAA2026031669626.md): Nut Plate · corroded · Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing, Attach Fittings > CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS303 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS303 AT LT WING IAW SRM 51-40-02-0G; SRM 51-10-02-0G ITEM 9, AND DWG 112A4402 SHEET 40 REV A, AND PERFORMED - [SDR SWAA2026031369454](https://openairdocs.org/sdr/SWAA2026031369454.md): Support Angle · cracked · Feb 10, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 - 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A5400, SHEET 154, REV-. - [SDR SWAA2026031369625](https://openairdocs.org/sdr/SWAA2026031369625.md): Rail · corroded · Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing Miscellaneous Structure > CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS411 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE IAW SRM 51-40-02-0G, SRM 51-10-02-0G, ITEM 9 AND DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026031369621](https://openairdocs.org/sdr/SWAA2026031369621.md): Rail · corroded · Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing Miscellaneous Structure > CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE, OFSS 578, LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE IAW SRM 51-40-02-0G, & DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026031369461](https://openairdocs.org/sdr/SWAA2026031369461.md): Angle · cracked · Feb 10, 2026 · N8629A · Boeing 7378H4 · Fuselage Main, Bulkhead > CRACKED ANGLE, BS 663 RBL 36. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, AND DWG 111A1000, SHEET 331, REV A. - [SDR SWAA2026031669325](https://openairdocs.org/sdr/SWAA2026031669325.md): Plate · cracked · Feb 9, 2026 · N8629A · Boeing 7378H4 · Wing Main, Frame Structure > CRACK CORRUGATED PLATE LOCATED TRAILING EDGE IRSS 217 AT RT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS 217 AT RT WING IAW SRM 51-40-02-0G-0, SRM 51-20-02-0G-0, ITEM 9 AND DWG 115A2713, SHEET 6, REV A. - [SDR SWAA2026031669319](https://openairdocs.org/sdr/SWAA2026031669319.md): Support Bracket · cracked · Feb 9, 2026 · N8629A · Boeing 7378H4 · Wing Miscellaneous Structure > CRACK ON SUPPORT BRACKET LOCATED TRAILING EDGE ORSS 273 AT RIGHT. REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE ORSS 273 AT RT WING. IAW SRM 51-40-02, SRM-51-10-02, ITEM 9, AND DWG 115A6200, SHEET 17, REV A. - [SDR SWAA2026031369055](https://openairdocs.org/sdr/SWAA2026031369055.md): Bracket · cracked · Feb 9, 2026 · N8629A · Boeing 7378H4 · Doors > CRACKED BRACKET FOR ACCESS PANEL 834DZ, ON AFT ENTRY DOORS. REPLACED THE BRACKET IAW SRM 51-40-02, SRM 51-10-02, ITEM 9,0 & DWG 411A2119, SHEET 72, REV -. - [SDR SWAA2026031369326](https://openairdocs.org/sdr/SWAA2026031369326.md): Angle · corroded · Feb 9, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORRODED ANGLE, BS 500I, LBL 22 - RBL 22, WL156. REPLACED THE ANGLE IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, DWG 143A9481, SHEET 14, REV -, & DWG 143A7902, SHEET 209, REV-. - [SDR SWAA2026031369324](https://openairdocs.org/sdr/SWAA2026031369324.md): Tie Clip · cracked · Feb 9, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK TIE CLIP, BS 500I, STR 26R. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A1234, SHEET 14, REV A. - [SDR SWAA2026031369057](https://openairdocs.org/sdr/SWAA2026031369057.md): Rail · corroded · Feb 9, 2026 · N8629A · Boeing 7378H4 · Wing Miscellaneous Structure > CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS571 AT RT WING. RE-INSTALLED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE IAW SRM 51-40-02, & DWG 112A4402, SHEET 41, REV A. & PERFORMED GENERAL VISUAL INSPECTION ON AREA AND NO CORROSION D - [SDR SWAA2026031269322](https://openairdocs.org/sdr/SWAA2026031269322.md): Shield · corroded · Feb 9, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION SHIELD WEB LOCATED BETWEEN BS 492 - 500A, RBL 22, WL156. FWD CARGO BAY. REPLACED SHIELD WEB AND FASTENERS IAW SRM 51-40-02-0G AND DWG 143A0080 SHEET 39 REV -. - [SDR SWAA2026031668956](https://openairdocs.org/sdr/SWAA2026031668956.md): Support Angle · cracked · Feb 8, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. REPLACED SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA; IAW SRM 51-40-02 AND DWG 141A8310, SHEET 33, REV-. - [SDR SWAA2026031668954](https://openairdocs.org/sdr/SWAA2026031668954.md): Frame · cracked · Feb 8, 2026 · N8629A · Boeing 7378H4 · Fuselage Main, Frame > CRACKED FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. REPAIRED THE FRAME IAW EA M-22-153-01244. - [SDR SWAA2026031368955](https://openairdocs.org/sdr/SWAA2026031368955.md): Tie Clip · cracked · Feb 8, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED TIE CLIP, BS 277, STR 10R. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, DRAWING 141A1110, SHEET 55, REV-, & DWG 141A8380, SHEET 21, REV-. - [SDR SWAA2026031369046](https://openairdocs.org/sdr/SWAA2026031369046.md): Support Angle · cracked · Feb 8, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ON SUPPORT ANGLE, BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHEET 184, REV-. - [SDR SWAA2026031369052](https://openairdocs.org/sdr/SWAA2026031369052.md): Support Angle · cracked · Feb 8, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, BS 867, LBL 10. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, & DWG 149A8102, SHEET 19, REV A. - [SDR SWAA2026031369047](https://openairdocs.org/sdr/SWAA2026031369047.md): Support Angle · cracked · Feb 8, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 - 400, LBL 52, WL 208.1. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, AND DWG 143A5400 SHEET 182 REV-. - [SDR SWAA2026031269045](https://openairdocs.org/sdr/SWAA2026031269045.md): Access Panel · cracked · Feb 8, 2026 · N8629A · Boeing 7378H4 · Wing, Plate/Skin > CRACKED ACCESS PANEL 544BB, LT WING. REPAIRED THE ACCESS PANEL 544BB IAW EA 26-157-00484. - [SDR SWAA2026031269050](https://openairdocs.org/sdr/SWAA2026031269050.md): Shield · corroded · Feb 8, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORRODED SHIELD WEB BETWEEN BS 767 - 794.3, RBL 22, WL 156. REPLACED SHIELD WEB IAW SRM 51-40-02-0G-0, & DWG 146A0081, SHEET 49, REV A.. - [SDR SWAA2026031268957](https://openairdocs.org/sdr/SWAA2026031268957.md): Support Beam · cracked · Feb 8, 2026 · N8629A · Boeing 7378H4 · Service Doors > CRACKED SUPPORT BEAM NR 4, FWD GALLEY DOOR. REPLACED SUPPORT BEAM IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DRAWING 141A6516, SHEET 142, REV-. - [SDR SWAA2026031269051](https://openairdocs.org/sdr/SWAA2026031269051.md): Support · corroded · Feb 8, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727C - 747, RBL 21, WL156 IN THE AFT CARGO BAY. REPAIRED SUPPORT ZEE IAW SRM 51-40-02, SRM 53-00-53-2R-6, REPAIR 6, FIG 203, & DWG 146A7500, SHEET 233, REV- & DWG 146A7502, SHEET 31, REV-. - [SDR SWAA2026031169049](https://openairdocs.org/sdr/SWAA2026031169049.md): Keelbeam · cracked · Feb 8, 2026 · N8629A · Boeing 7378H4 · Fuselage Main, Keel > CRACKED KEELBEAM BETWEEN BS 727 - 727A, STR 27R, AFT CARGO BAY. PERFORMED REPAIR ON KEELBEAM BTWN BS 727 - 727A, STR 27R IAW EA 26-153-00444 AND 26-153-00444 WIP 1. - [SDR SWAA2026031668572](https://openairdocs.org/sdr/SWAA2026031668572.md): Nut · corroded · Feb 7, 2026 · N8629A · Boeing 7378H4 · Wing Miscellaneous Structure > CORROSION ON RAIL NUT LOCATED OSS 146.43 BETWEEN OSS 160.30 ON LH WING. REPLACED NEW RAIL NUT LOCATED OSS 146.43 BETWEEN OSS 160.30 ON LH WING. - [SDR SWAA2026031668573](https://openairdocs.org/sdr/SWAA2026031668573.md): Nut · corroded · Feb 7, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION ON RAIL NUT LOCATED OSS 126.72 BETWEEN OSS 140.92 AT LH WING. REPLACED NEW RAIL NUT IAW SRM 51-40-02-0G. - [SDR SWAA2026031668579](https://openairdocs.org/sdr/SWAA2026031668579.md): Nut Plate · corroded · Feb 7, 2026 · N8629A · Boeing 7378H4 · Wing, Attach Fittings > CORROSION ON RAIL NUT LOC OSS 93.30 BETWEEN OSS 106.65, LT WING. REPLACED NEW RAIL NUT LOC APROX OSS 93.30 BETWEEN OSS 106.65 ON LH WING SEE TTG8Q01A8AB5 STEP 5 ITEM 9. IAW SRM 51-40-02-0G. - [SDR SWAA2026031668580](https://openairdocs.org/sdr/SWAA2026031668580.md): Nut Plate · corroded · Feb 7, 2026 · N8629A · Boeing 7378H4 · Wing, Attach Fittings > CORROSION ON RAIL NUT LOCATED OSS113.18 BETWEEN OSS 118.65 AT LT WING. REPLACED NEW RAIL NUT LOCATED OSS113.18 BETWEEN OSS 118.65 AT LH. WING SEE TTG8Q01A8AB5. - [SDR SWAA2026031668753](https://openairdocs.org/sdr/SWAA2026031668753.md): Web · cracked · Feb 7, 2026 · N8629A · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure > CRACK ON WEB INBD FAN COWL ON ENGINE 1 2026-112370<[01] REPLACED WEB ON INBD FAN COWL ON ENGINE 1 IAW SRM 51-40-02-0G-0 AND CMM 71-13-30, REV 32, PAGE 10092. - [SDR SWAA2026031268587](https://openairdocs.org/sdr/SWAA2026031268587.md): Scuff Plate · cracked · Feb 7, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED FWD CORNER SCUFF PLATE, IN THE AFT CARGO BAY. REPAIRED THE FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975. - [SDR SWAA2026031268586](https://openairdocs.org/sdr/SWAA2026031268586.md): Scuff Plate · cracked · Feb 7, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ON AFT CORNER SCUFF PLATE LOC AFT CARGO BAY. REPAIRED THE AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975. - [SDR SWAA2026031668561](https://openairdocs.org/sdr/SWAA2026031668561.md): Crossbeam · cracked · Feb 6, 2026 · N8629A · Boeing 7378H4 · Fuselage Main, Structure > CRACK ON BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM- 51-40-02 AND DRAWING 143A0060 SHEET 64 REV -. - [SDR SWAA2026031668560](https://openairdocs.org/sdr/SWAA2026031668560.md): Crossbeam · cracked · Feb 6, 2026 · N8629A · Boeing 7378H4 · Fuselage Main, Structure > CRACK ON BRAKE PANEL LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN IAW SRM- 51-40-02 AND DRAWING 143A0060 SHEET 64 REV -. - [SDR SWAA2026031668427](https://openairdocs.org/sdr/SWAA2026031668427.md): Floorbeam · corroded · Feb 6, 2026 · N8629A · Boeing 7378H4 · Fuselage Main, Floor Beam > CORROSION ON FLOOR BEAM, BS 947.5 LBL 24 WL 208.1. REPAIRED IAW SRM 53-70-51-2R-5, REPAIR 5, AND EA 26-153-00448 AND EA M-24-153-02022. - [SDR SWAA2026031668205](https://openairdocs.org/sdr/SWAA2026031668205.md): Seat Track · cracked · Feb 6, 2026 · N8629A · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings > CRACK ON SEAT TRACK FWD INBOARD OF CAPTAIN SEAT IN COCKPIT. REPLACED SEAT TRACK FWD INBOARD OF CAPTAIN SEAT IN COCKPIT IAW AMM 25-11-11-400-801 INSTALLATION WILL BE PERFORMED ON SWA TASK CARD TTG8R008A8XR STEP 12. Next page: https://openairdocs.org/aircraft/N8629A/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 = 'N8629A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N8629A/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.