# Service difficulty reports: N8653A A list on [N8653A](https://openairdocs.org/aircraft/N8653A.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 · 160 reports - [SDR SWAA2026092916162](https://openairdocs.org/sdr/SWAA2026092916162.md): Sign · unsecure · Sep 25, 2026 · N8653A · Boeing 7378H4 · Emergency Lighting > PASSENGER CABIN, CEILING EXIT SIGN UNSECURE. SECURED THE SIGN IAW AMM 33-51-01-960-802, STEP 3.C. (6) (E). - [SDR SWAA2026092988170](https://openairdocs.org/sdr/SWAA2026092988170.md): Battery Pack · inoperative · Sep 25, 2026 · N8653A · Boeing 7378H4 · Emergency Lighting > RIGHT AFT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, 21-23-03-000-801, & 21-23-03-400-802. - [SDR SWAA2026092907824](https://openairdocs.org/sdr/SWAA2026092907824.md): Battery Pack · inoperative · Sep 25, 2026 · N8653A · Boeing 7378H4 · Emergency Lighting > LEFT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, 21-23-03-000-801, & 21-23-03-400-802. - [SDR SWAA2026092935990](https://openairdocs.org/sdr/SWAA2026092935990.md): Light · inoperative · Sep 25, 2026 · N8653A · Boeing 7378H4 · Emergency Lighting > EMERGENCY LIGHT AFT OF RT WTB FAIRING WAS INOPERATIVE. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-00-710-801. TESTED OK. - [SDR SWAA2026092491186](https://openairdocs.org/sdr/SWAA2026092491186.md): Balance Weight · out of sequence · Sep 10, 2026 · N8653A · Boeing 7378H4 · Elevator Structure > DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR RT FOUND BALANCE, 1 EA ON BAY 2, 1 EA, 3 EA ON BAY 3, & 1 EA ON BAY 4. TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-03767. TTG8Q01E6J76 TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-03767. - [SDR SWAA2026092486702](https://openairdocs.org/sdr/SWAA2026092486702.md): Balance Weight · out of sequence · Sep 10, 2026 · N8653A · Boeing 7378H4 · Elevator Structure > DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR LT FOUND BALANCE WEIGHT 183A0210-15 (1 EA) ON BAY 4, 183A0210-14 (1 EA) AND 6953211-2 (2 EA) ON BAY 3, 183A0210-14 (1 EA) ON BAY 2. 2026-499052 TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-03766 SEE TASK TTG8Q01E6 - [SDR SWAA2026092957301](https://openairdocs.org/sdr/SWAA2026092957301.md): Intercostal · cracked · Sep 4, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED INTERCOSTAL BTWN BS 400 - 420, STR 26L. REPLACED THE INTERCOSTAL IAW SRM 51-10-02, ITEM 9, AND FASTENERS IAW SRM 51-40-02, & DWG 143A7505, SHEET 151, REV A. - [SDR SWAA2026092999840](https://openairdocs.org/sdr/SWAA2026092999840.md): Angle · corroded · Aug 27, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION ON LOWER ANGLE, BS 767 - 787, RBL 21, WL 155.3. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 146A8123, SHEET 16, REV-. - [SDR SWAA2026092440445](https://openairdocs.org/sdr/SWAA2026092440445.md): Plate · cracked · Aug 27, 2026 · N8653A · Boeing 7378H4 · Wing Main, Frame Structure > CRACKED CORRUGATED PLATE, IRSS 216 RT WING T/R. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2781, SHEET 2, REV B. - [SDR SWAA2026092488382](https://openairdocs.org/sdr/SWAA2026092488382.md): Plate · damaged · Aug 27, 2026 · N8653A · Boeing 7378H4 · Wing Main, Frame Structure > ELONGATED HOLE ON CORRUGATED PLATE LOCATED ORSS 320 TRAILING EDGE, RT WING. REPLACED CORRUGATED PLATE, DID NOT FIND ALLOWABLE DAMAGE LIMITS IN SRM 57-51-02-1A-1, ALLOWABLE DAMAGE 1, SRM 51-10-02, ITEM 9, & DWG 115A3700, SHEET 96, REV -. - [SDR SWAA2026092917117](https://openairdocs.org/sdr/SWAA2026092917117.md): Support Angle · cracked · Aug 26, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, BS 500I, STR 28L. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 320, REV-. - [SDR SWAA2026092973065](https://openairdocs.org/sdr/SWAA2026092973065.md): Web · cracked · Aug 26, 2026 · N8653A · Boeing 7378H4 · Wing Miscellaneous Structure > CRACKED WEB TRAILING EDGE PANEL, RT WING, ORSS 266. REPLACED THE WEB AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2512, SHEET 16, REV-. - [SDR SWAA2026092956153](https://openairdocs.org/sdr/SWAA2026092956153.md): Support Angle · cracked · Aug 26, 2026 · N8653A · Boeing 7378H4 · Wing Miscellaneous Structure > CRACKED SUPPORT ANGLE, RT WING, ORSS 261. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2512, SHEET 13, REV-. - [SDR SWAA2026092933487](https://openairdocs.org/sdr/SWAA2026092933487.md): Support Angle · cracked · Aug 26, 2026 · N8653A · Boeing 7378H4 · Wing Miscellaneous Structure > CRACKED SUPPORT ANGLE, ORSS 271, RT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 115A6200, SHEET 17, REV A. - [SDR SWAA2026092956067](https://openairdocs.org/sdr/SWAA2026092956067.md): Support Angle · cracked · Aug 26, 2026 · N8653A · Boeing 7378H4 · Wing Miscellaneous Structure > CRACKED SUPPORT ANGLE AT THE FIXED TRAILING EDGE PANEL, ORSS 261, LT WING. REPLACED THE SUPPORT ANGLE IAW RM 51-10-02, PARAGRAPH 9, SRM 51-40-02, DWG 115A2512, SHEET 16, REV-. - [SDR SWAA2026092959991](https://openairdocs.org/sdr/SWAA2026092959991.md): Access Panel · cracked · Aug 25, 2026 · N8653A · Boeing 7378H4 · Horizontal Stabilizer, Plate/Skin > CRACKED HORIZONTAL STAB ACCESS PANEL 343CB. REPLACED THE ACCESS PANEL IAW SRM 51-10-02, ITEM 9, 51-40-02, & DWG 185A1702, SHEET 19, REV F. - [SDR SWAA2026092431706](https://openairdocs.org/sdr/SWAA2026092431706.md): Support Angle · cracked · Aug 25, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE ON ACCESS PANELS 834DZ AT THE AFT ENTRY DOOR. REPLACED THE SUPPORT ANGLE ON ACCESS PANELS 834DZ IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DRILLED SUPPORT ANGLE IAW SRM 51-40-05, & APPLIED PROTECTIVE TREATMENT OPEN NEW HOLE IAW SRM 51-20-01 - [SDR SWAA2026092490877](https://openairdocs.org/sdr/SWAA2026092490877.md): Support Web · cracked · Aug 25, 2026 · N8653A · Boeing 7378H4 · Nacelle/Pylon, Main Frame > CRACKED SUPPORT WEB INBD FAN COWL, LT ENGINE. REPLACED FASTENERS & SUPPORT WEB ON THE INBOARD FAN COWL IAW SRM 51-40-02, SRM 51-10-02, & 71-13-30, PAGE 10094. - [SDR SWAA2026092457388](https://openairdocs.org/sdr/SWAA2026092457388.md): Plate · damaged · Aug 25, 2026 · N8653A · Boeing 7378H4 · Wing Main, Frame Structure > ELONGATED HOLE ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 282 AT LT WING. EVALUATED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 282 LT WING AND DID NOT FIND ALLOWABLE DAMAGE IN SRM 57-51-02-1A-1, AND REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 28 - [SDR SWAA2026092432884](https://openairdocs.org/sdr/SWAA2026092432884.md): Plate · damaged · Aug 25, 2026 · N8653A · Boeing 7378H4 · Wing Main, Frame Structure > ELONGATED HOLE ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 226 AT LT WING. EVALUATED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 226 AT LT WING AND NOT FOUND ALLOWABLE DAMAGE IN SRM 57-51-02-1A-1 AND REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 226 - [SDR SWAA2026092996069](https://openairdocs.org/sdr/SWAA2026092996069.md): Web · cracked · Aug 24, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SHIELD WEB, BTWN BS 767 - 787, STR 25R. REPLACED THE SHIELD WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 146A0081, SHEET 49, REV A. - [SDR SWAA2026092919174](https://openairdocs.org/sdr/SWAA2026092919174.md): Fitting · cracked · Aug 24, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED FITTING, BS 947.5, STR 26L. REPLACED THE FITTING IAW SRM 51-40-02, AND DWG 149A8103, SHEET 8, REV-. - [SDR SWAA2026092411897](https://openairdocs.org/sdr/SWAA2026092411897.md): Support Angle · cracked · Aug 24, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, BTWN BS 380 - 400, RBL 40, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A5400, SHEETS 140,& 184, REV-. - [SDR SWAA2026092434571](https://openairdocs.org/sdr/SWAA2026092434571.md): Support Angle · cracked · Aug 24, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, BTWN BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHEET 184, REV-. - [SDR SWAA2026092415163](https://openairdocs.org/sdr/SWAA2026092415163.md): Support Angle · cracked · Aug 24, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, BTWN BS 380 - 400, LBL 50, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, 51-10-02, ITEM 9, & DWG 143A5400, SHEET 182, REV-. - [SDR SWAA2026092459556](https://openairdocs.org/sdr/SWAA2026092459556.md): Support Bracket · cracked · Aug 24, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT BRACKET, BS 540 AIR CONDITIONING DUCT AT LOWER FUSELAGE LT SIDE. REPLACED THE SUPPORT BRACKET FOR AIR CONDITIONING DUCT AT LOWER FUSELAGE LT SIDE IAW DWG 212A1101 REV -, SHEET 11, & SOPM 20-50-01. - [SDR SWAA2026092974826](https://openairdocs.org/sdr/SWAA2026092974826.md): Access Panel · elongated · Aug 23, 2026 · N8653A · Boeing 7378H4 · Trailing Edge Flaps > ELONGATED HOLE ON ACCESS PANEL 542EB, FLAP SUPPORT FAIRING 3, LT WING. REPAIRED THE ACCESS PANEL 542EB ON FLAP SUPPORT FAIRING 3 IAW SRM 51-70-04-2R-9, REPAIR 9. - [SDR SWAA2026092947026](https://openairdocs.org/sdr/SWAA2026092947026.md): Web · cracked · Aug 21, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED WEB, BTWN BS 927 - 947.5, STR 26R. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 147A7500, SHEET 36, & 37, REV-. - [SDR SWAA2026092992864](https://openairdocs.org/sdr/SWAA2026092992864.md): Floorbeam · cracked · Aug 21, 2026 · N8653A · Boeing 7378H4 · Fuselage Main, Floor Beam > CRACKED FLOORBEAM, BS 270, BTWN BL 0 - LBL 1, WL 208.1. REPAIRED THE TRANSVERSAL BEAM IN THE FLT COMPARTMENT IAW EA 26-153-02313, EA 26-153-02313-WIP1, AND EA 26-153-02313-WIP2. - [SDR SWAA2026092916099](https://openairdocs.org/sdr/SWAA2026092916099.md): Support Bracket · cracked · Aug 21, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT BRACKET, BS 727, BL 0, WL 163. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 144A2600, SHEET 1084, REV-. - [SDR SWAA2026092915974](https://openairdocs.org/sdr/SWAA2026092915974.md): Tie Clip · cracked · Aug 21, 2026 · N8653A · Boeing 7378H4 · Fuselage Main, Structure > CRACKED TIE CLIP, BS 277, STR 10R. REPLACED THE TIE CLIP IAW SRM 51-40-02, AND DWG 141A1110, SHEET 55, REV -. - [SDR SWAA2026092995959](https://openairdocs.org/sdr/SWAA2026092995959.md): Support Angle · cracked · Aug 21, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ON SUPPORT ANGLE LOCATED BS 867 AT LEVEL STR 27L AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 149A8102, SHEET 19, REV A. - [SDR SWAA2026092491395](https://openairdocs.org/sdr/SWAA2026092491395.md): Access Panel · delaminated · Aug 21, 2026 · N8653A · Boeing 7378H4 · Fuselage Main, Plate/Skin > DELAMINATED EXTERNAL SKIN ACCESS PANEL 191CL. REPAIRED EXTERNAL SKIN ACCESS PANEL 191CL IAW SRM 51-70-04-2R-1 REPAIR 1. - [SDR SWAA2026092433515](https://openairdocs.org/sdr/SWAA2026092433515.md): Frame · cracked · Aug 21, 2026 · N8653A · Boeing 7378H4 · Fuselage Main, Frame > CRACKED FRAME, BS 312, BTWN STR 5L - 6L. REPAIRED THE FRAME IAW M-22-153-01244. - [SDR SWAA2026092491559](https://openairdocs.org/sdr/SWAA2026092491559.md): Support Angle · cracked · Aug 20, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, FWD FACE, BS 695, LBL 1, WL 208.1. REPLACED THE SUPPORT ANGLE LOCATED FWD FACE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 273A9111, SHEET 9, REV -. - [SDR SWAA2026092429167](https://openairdocs.org/sdr/SWAA2026092429167.md): Seat Track · corroded · Aug 20, 2026 · N8653A · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings > CORRODED SEAT TRACK, BOTTOM SURFACE, BS 727F + 13 INCHES, RBL 24.75, WL 208.1. REMOVED THE DAMAGE & EVALUATED REWORK ON SEAT TRACK IAW SRM 53-00-52-1A-1, STEP 4.A (2)(A), FIGURE 103, DETAIL A. - [SDR SWAA2026092411677](https://openairdocs.org/sdr/SWAA2026092411677.md): Floor Panel · delaminated · Aug 20, 2026 · N8653A · Boeing 7378H4 · Fuselage Floor Panel > DELAMINATION ON TOP SKIN OF FLOOR PANEL 231KF. REPAIRED THE FLOOR PANEL 231KF IAW SRM 53-00-50-2R-7, REPAIR 7. - [SDR SWAA2026092472284](https://openairdocs.org/sdr/SWAA2026092472284.md): Crossbeam · cracked · Aug 20, 2026 · N8653A · Boeing 7378H4 · Fuselage Main, Structure > CRACKED BRAKE PANEL LOCATED BS 540 BTW BL 0 - LBL 24.75, WL 208.1. REPLACED THE BRAKE PANEL IAW SRM 51-40-02, AND DWG 143A0060, SHEET 64, REV-. - [SDR SWAA2026092407246](https://openairdocs.org/sdr/SWAA2026092407246.md): Seat Track · corroded · Aug 20, 2026 · N8653A · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION SEAT TRACK LOCATED BTW BS 540 - 727B, WL 208, LBL 45.5, CROWN AREA BOTTOM SURFACE (4 E/A). REMOVED DAMAGE AND EVALUATED REWORK AREA IAW SRM 53-00-52-1A-1 STEP 4.A (2)(A), FIGURE 103, DETAIL A. - [SDR SWAA2026092476359](https://openairdocs.org/sdr/SWAA2026092476359.md): Floorbeam · corroded · Aug 20, 2026 · N8653A · Boeing 7378H4 · Fuselage Main, Floor Beam > CORRODED FLOORBEAM, BS 986.5, RBL 43, WL 208.1 IN THE AFT GALLEY AREA. REPAIRED THE FLOORBEAM, IAW SRM 53-70-51-2R-6, REPAIR 6. - [SDR SWAA2026092455644](https://openairdocs.org/sdr/SWAA2026092455644.md): Seat Track · corroded · Aug 20, 2026 · N8653A · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings > CORRODED SEAT TRACK, BOTTOM SURFACE, BS 727 + 13 INCHES, RBL 24.75, WL 208.1. REMOVED DAMAGE AND EVALUATED REWORK AREA BOTTOM SURFACE LOCATED BS 727 + 13 INCHES, RBL 24.75, WL 208.1 IAW SRM 53-00-52-1A-1, STEP 4.A (2)(A), FIGURE 103, DETAIL A. - [SDR SWAA2026092415985](https://openairdocs.org/sdr/SWAA2026092415985.md): Seat Track · corroded · Aug 20, 2026 · N8653A · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings > CORRODED SEAT TRACK BTW BS 727B - 887, WL 208, RBL45.5 CROWN AREA BOTTOM SURFACE, (5 EA). REMOVED DAMAGE AND EVALUATED SEAT TRACK LOCATED BTW BS 727B - 887, WL 208, RBL45.5, FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1, PARAGRAPH 4.A.(2(A), FIGURE 103, DETAIL - [SDR SWAA2026092416069](https://openairdocs.org/sdr/SWAA2026092416069.md): Seat Track · corroded · Aug 20, 2026 · N8653A · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON SEAT TRACK BOTTOM SURFACE LOCATED BS 500F PLUS 10 INCHES RBL 24.75 WL 208.1 AT PASSENGER CABIN. REMOVED DAMAGE AND EVALUATED REWORK AREA BOTTOM SURFACE LOCATED BS 500F PLUS 10 INCHES RBL 24.75 WL 208.1 AT PASSENGER CABIN IAW SRM 53-00-52-1A-1 STE - [SDR SWAA2026092916176](https://openairdocs.org/sdr/SWAA2026092916176.md): Angle · cracked · Aug 19, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 440, STR 26L. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7505, SHEET 152, REV-. - [SDR SWAA2026092935972](https://openairdocs.org/sdr/SWAA2026092935972.md): Angle · cracked · Aug 19, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 400, STR 26L. REPLACED THE ANGLE & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DRAWING 143A7505, SHEET 151, REV A. - [SDR SWAA2026092451667](https://openairdocs.org/sdr/SWAA2026092451667.md): Access Panel · elongated · Aug 19, 2026 · N8653A · Boeing 7378H4 · Wing, Plate/Skin > ELONGATED HOLES ON ACCESS PANEL 561BB, LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2026092411625](https://openairdocs.org/sdr/SWAA2026092411625.md): Skin · cracked · Aug 19, 2026 · N8653A · Boeing 7378H4 · Fuselage Main, Plate/Skin > CRACKED INNER CHORD, BS 303.9, STR 17L. REPLACED BTWN BS 270 - 360, STR 17L IAW SRM 51-10-02, ITEM 9, INSTALLED FASTENERS IAW SRM 51-40-02 & DWG 142A0050, SHEET 15, REV -. - [SDR SWAA2026092451051](https://openairdocs.org/sdr/SWAA2026092451051.md): Support Angle · cracked · Aug 19, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, BTWN BS 291.5 - 294.5, STR 17R IN FWD GALLEY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND 141A8310, SHEET 33, REV-. - [SDR SWAA2026092472212](https://openairdocs.org/sdr/SWAA2026092472212.md): Access Panel · damaged · Aug 19, 2026 · N8653A · Boeing 7378H4 · Wing, Plate/Skin > ELONGATED HOLES ON ACCESS PANEL 661CB T / E, RT WING. REMOVED AND REPLACED THE ACCESS PANEL 661CB IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2026092471077](https://openairdocs.org/sdr/SWAA2026092471077.md): Panel · damaged · Aug 19, 2026 · N8653A · Boeing 7378H4 · Wing Main, Frame Structure > ELONGATED HOLES ON ACCESS PANEL 561AB AT LT WING. REPAIRED THE ACCESS PANEL 561AB IAW SRM 51-70-04-2R-10, REPAIR 10. Next page: https://openairdocs.org/aircraft/N8653A/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 = 'N8653A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N8653A/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.