# Service difficulty reports: N8645A

A list on [N8645A](https://openairdocs.org/aircraft/N8645A.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 · 145 reports

- [SDR SWAA2026102335763](https://openairdocs.org/sdr/SWAA2026102335763.md): Bolt · missing · Oct 19, 2026 · N8645A · Boeing 7378H4 · Escape Slide
  > FWD GALLEY SERVICE DOOR FWD EMERGENCY SLIDE MOUNT MISSING HARDWARE. INSTALLED BOLT AND WASHER AT FWD SVC DOOR EMERGENCY SLIDE MOUNTING BRACKET IAW AMM 20-50-11.
- [SDR SWAA2026052701097](https://openairdocs.org/sdr/SWAA2026052701097.md): Access Panel · delaminated · May 14, 2026 · N8645A · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > DELAMINATED ACCESS PANEL 193AR LOWER FUSELAGE THIS FAULT WAS RESOLVED ON FAULT TTG8Q01BU803;[02] THIS FAULT WAS RESOLVED ON FAULT TTG8Q01BU803
- [SDR SWAA2026052794700](https://openairdocs.org/sdr/SWAA2026052794700.md): Skin · delaminated · May 1, 2026 · N8645A · Boeing 7378H4 · Elevator, Plate/Skin
  > DELAMINATED ON UPPER AREA NEAR OF HINGE ELEVATOR 5 OF LT ELEVATOR. REPAIRED UPPER AREA NEAR OF HINGE ELEVATOR 5 OF LT ELEVATOR IAW SRM 55-20-01-2R-1 REPAIR 1 AND SRM 51-70-05-2R-1 REPAIR 1.
- [SDR SWAA2026052794428](https://openairdocs.org/sdr/SWAA2026052794428.md): Support Angle · cracked · Apr 30, 2026 · N8645A · Boeing 7378H4 · Passenger/Crew Doors
  > CRACK ON SUPPORT ANGLE LOCATED ACCESS PANEL 834DZ AT AFT ENTRY DOOR. REPLACED SUPPORT ANGLE LOCATED ACCESS PANEL 834DZ AT AFT ENTRY DOOR MEASURE CRACK IS:0.279? IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 411A2119 SHEET 72 REV: -.
- [SDR SWAA2026052794302](https://openairdocs.org/sdr/SWAA2026052794302.md): Support Angle · cracked · Apr 30, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 500I TO BS 520 LBL 1 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BTW BS 500I TO BS 520 LBL 1 WL 208.1 AT PASSENGER CABIN IAW BOEING 737-800 SRM-51-10-02 ITEM 9 AND DGW 143A5400 SHEET: 189 AND 190 REV-.
- [SDR SWAA2026052703510](https://openairdocs.org/sdr/SWAA2026052703510.md): Reveal · cracked · Apr 30, 2026 · N8645A · Boeing 7378H4 · Service Doors
  > CRACK ON REVEAL ASSY LOCATED ACCESS PANEL 844AW AT AFT GALLEY DOOR. REPLACED REVEAL ASSY LOCATED ACCESS PANEL 844AW AT AFT GALLEY DOOR IAW SOPM 20-50-01 REV 40 AND DWG 411A2104 REV - SHEET 30, CRACK MEASURES: 1.5070 IN.
- [SDR SWAA2026052794427](https://openairdocs.org/sdr/SWAA2026052794427.md): Support Web · cracked · Apr 30, 2026 · N8645A · Boeing 7378H4 · Nacelle/Pylon, Main Frame
  > CRACK SUPPORT WEB LOCATED OUTBOARD FAN COWL ON ENGINE 2. REPLACED SUPPORT WEB LOCATED OUTBOARD FAN COWL ON ENGINE 2 IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND CMM 71-13-30 REV 34. PAGE 10090 DETAIL P; FIGURE 3; SHEET 5.
- [SDR SWAA2026052794301](https://openairdocs.org/sdr/SWAA2026052794301.md): Support Web · cracked · Apr 30, 2026 · N8645A · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > CRACK SUPPORT WEB LOCATED INBOARD FAN COWL ON ENGINE 1. REPLACED SUPPORT WEB AND FASTENERS LOCATED ON INBOARD FAN COWL AT ENGINE 1 IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND CMM 71-13-30 PAGE 10090. MEASUREMENT OF CRACK: 1.317 INCH.
- [SDR SWAA2026052694300](https://openairdocs.org/sdr/SWAA2026052694300.md): Support Beam · cracked · Apr 30, 2026 · N8645A · Boeing 7378H4 · Fuselage Main, Structure
  > CRACKED SUPPORT BEAM NR 4 LOCATED FWD GALLEY DOOR. REPLACED SUPPORT BEAM #4 LOCATED FWD GALLEY DOOR IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 141A6516 SHEET 142 REV-.
- [SDR SWAA2026052794062](https://openairdocs.org/sdr/SWAA2026052794062.md): Support Angle · cracked · Apr 29, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 380 TO BS 400 BL 0 AND WL 208.1 AT FLOOR STRUCTURE OF PASSENGER CABIN AREA IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51
- [SDR SWAA2026052794060](https://openairdocs.org/sdr/SWAA2026052794060.md): Support Angle · cracked · Apr 29, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 380 TO BS 400 RBL 10 AND WL 208.1 AT FLOOR STRUCTURE OF PASSENGER CABIN AREA IAW B737-800 SRM 51-10-02-0G-0 PARAGR
- [SDR SWAA2026052794063](https://openairdocs.org/sdr/SWAA2026052794063.md): Floor Support · cracked · Apr 29, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 380 TO BS 400 LBL 51 AND WL 208.1 AT FLOOR STRUCTURE OF PASSENGER CABIN AREA IAW SRM 51-40-02-0G-0; DRAWING 143A54
- [SDR SWAA2026052794064](https://openairdocs.org/sdr/SWAA2026052794064.md): Floor Support · cracked · Apr 29, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 380 TO BS 400 RBL 41 AND WL 208.1 AT FLOOR STRUCTURE OF PASSENGER CABIN AREA IAW SRM 51-40-02-0G-0; DRAWING NUMBER
- [SDR SWAA2026052793950](https://openairdocs.org/sdr/SWAA2026052793950.md): Frame · cracked · Apr 29, 2026 · N8645A · 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 LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA I.A.W B737-800 EA M-22-153-01244.
- [SDR SWAA2026052693949](https://openairdocs.org/sdr/SWAA2026052693949.md): Web · cracked · Apr 29, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 22 AT AFT CARGO COMPARTMENT. TOOK MEASURE OF CRACK LOC. WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 22 AT AFT CARGO COMPARTMENT IS IS L:0.250 ?INCH. REPLACED WEB LOCATED CEILING AREA BTW BS 84
- [SDR SWAA2026052793644](https://openairdocs.org/sdr/SWAA2026052793644.md): Support Angle · cracked · Apr 28, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - SUPPORT LOCATED BS867 AND LBL11 AT AFT CARGO COMPARTMENT. REPLACED ANGLE-SUPPORT LOCATED BS867 AND LBL11 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0 DWG 149A8102 SHEET: 19 REV:A CRACK LENGTH: 0.800 INCH
- [SDR SWAA2026052793793](https://openairdocs.org/sdr/SWAA2026052793793.md): Support Angle · cracked · Apr 28, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - SUPPORT LOCATED AFT SIDE BS500I AND STR28R FWD CARGO COMPARTMENT. REPLACED ANGLE SUPPORT LOCATED AFT SIDE BS500I AND STR28R FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 143A7902 SHEET 320 REV.-.
- [SDR SWAA2026052693645](https://openairdocs.org/sdr/SWAA2026052693645.md): Intercostal · cracked · Apr 28, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947 AND RBL21 AFT CARGO COMPARTMENT. REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS927 TO BS947 AND RBL21 AFT CARGO COMPARTMENT IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A7500 SHEET: 27 REV: -.
- [SDR SWAA2026052606583](https://openairdocs.org/sdr/SWAA2026052606583.md): Intercostal · cracked · Apr 28, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947 AND RBL21 AFT CARGO COMPARTMENT. REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS927 TO BS947 AND RBL21 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A7500 SHEET: 27
- [SDR SWAA2026052693642](https://openairdocs.org/sdr/SWAA2026052693642.md): Intercostal · corroded · Apr 28, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947 WL150 AND RBL4 AFT CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947 WL150 AND RBL4 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A7500 SHEET:38
- [SDR SWAA2026052793421](https://openairdocs.org/sdr/SWAA2026052793421.md): Angle · cracked · Apr 27, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - CLIP LOCATED BS500H AND RBL21 AFT SIDE POSITION FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP LOCATED BS500H AND RBL21 AFT SIDE POSITION FWD CARGO COMPARTMENT IAW BOEING SRM-51-10-02 ITEM 9 AND DWG 143A7505; SHEET: 137 AND 138 REV:-.
- [SDR SWAA2026052793414](https://openairdocs.org/sdr/SWAA2026052793414.md): Angle · cracked · Apr 27, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - CLIP LOCATED BS500G AND RBL21 FWD SIDE POSITION FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP LOCATED BS 500G AND RBL21 FWD SIDE POSITION FWD CARGO COMPARTMENT IAW BOEING SRM-51-10-02 ITEM 9 AND DWG 143A7505; SHEET: 137 AND 138 REV:-.
- [SDR SWAA2026052793416](https://openairdocs.org/sdr/SWAA2026052793416.md): Angle · cracked · Apr 27, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - CLIP LOCATED BS500G AND LBL21 AFT SIDE POSITION FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP LOCATED BS500G AND LBL21 AFT SIDE POSITION FWD CARGO COMPARTMENT IAW BOEING 737-800 SRM-51-10-02 ITEM 9 AND DWG 143A7505; SHEET: 137 AND 138 REV:-.
- [SDR SWAA2026052793417](https://openairdocs.org/sdr/SWAA2026052793417.md): Angle · cracked · Apr 27, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - CLIP LOCATED BS500H AND LBL21 FWD SIDE POSITION FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP LOCATED BS500H AND LBL21 FWD SIDE POSITION FWD CARGO COMPARTMENT IAW BOEING 737-800 SRM-51-10-02 ITEM 9 AND DWG 143A7505; SHEET: 137 AND 138 REV:-.
- [SDR SWAA2026052793418](https://openairdocs.org/sdr/SWAA2026052793418.md): Angle · cracked · Apr 27, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - CLIP LOCATED BS500H AND LBL21 AFT SIDE POSITION FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP LOCATED BS500H AND LBL21 AFT SIDE POSITION FWD CARGO COMPARTMENT IAW BOEING SRM-51-10-02 ITEM 9 AND DWG 143A7505; SHEET: 137 AND 138 REV:-.
- [SDR SWAA2026052793420](https://openairdocs.org/sdr/SWAA2026052793420.md): Angle · cracked · Apr 27, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - BS500H AND RBL21 FWD SIDE POSITION FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS500H AND RBL21 FWD SIDE POSITION FWD CARGO COMPARTMENT IAW SRM-51-10-02 ITEM 9 AND DWG 143A7505; SHEET: 137 AND 138 REV:-.
- [SDR SWAA2026052793412](https://openairdocs.org/sdr/SWAA2026052793412.md): Angle · cracked · Apr 27, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - CLIP LOCATED BS440 AND LBL21 AFT SIDE POSITION FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP LOCATED BS440 AND LBL21 AFT SIDE POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 143A7502 SHEET: 37 REV. -.
- [SDR SWAA2026052793419](https://openairdocs.org/sdr/SWAA2026052793419.md): Gusset · cracked · Apr 27, 2026 · N8645A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACK ON GUSSET ANGLE LOCATED BS500I AT LEVEL STR21L AT FWD CARGO COMPARTMENT. REPLACED GUSSET ANGLE AND FASTENERS LOCATED BS500I AT LEVEL STR21L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02-0G-0 ITEM 9 SRM 51-40-02-0G-0 AND DWG 143A7902 SHEET 256 REV
- [SDR SWAA2026052793415](https://openairdocs.org/sdr/SWAA2026052793415.md): Gusset · cracked · Apr 27, 2026 · N8645A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACK ON GUSSET ANGLE LOCATED BS500I AT LEVEL STR19R AT FWD CARGO COMPARTMENT. REPLACED GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R AT FWD CARGO COMPARTMENT. IAW SRM 51-10-02-0G-0 ITEM 9 AND DWG 143A7902 SHEET: 256 AND SHEET: 257 REV: B.
- [SDR SWAA2026052793221](https://openairdocs.org/sdr/SWAA2026052793221.md): Rail · corroded · Apr 26, 2026 · N8645A · Boeing 7378H4 · Wing Main, Frame Structure
  > CORROSION ON RAIL NUT AT LEVEL ORSS 449 LEADING EDGE AT RT WING. REPLACED RAIL NUT AT LEVEL ORSS 449 LEADING EDGE AT RT WING IAW SRM: 51-40-02-0G-0 AND DWG: 112A4402 SHEET 40 REV. A.
- [SDR SWAA2026052793219](https://openairdocs.org/sdr/SWAA2026052793219.md): Access Panel · cracked · Apr 26, 2026 · N8645A · Boeing 7378H4 · Nacelle/Pylon, Plate/Skin
  > CRACK SEAL PLATE ACCESS PANEL 431AT INBOARD SIDE LT PYLON. REPLACED SEAL PLATE LOCATED ON ACCESS PANEL 431AT ON INBOARD SIDE AT LT PYLON IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 313A2110 SHEET: 1 REV: B. MEASUREMENT OF CRACK: 405 IN.
- [SDR SWAA2026052793218](https://openairdocs.org/sdr/SWAA2026052793218.md): Web · cracked · Apr 26, 2026 · N8645A · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACK ON WEB LOCATED AT LEVEL ORSS 261 DEFLECTION CONTROL RIB AREA AT TRAILING EDGE RT WING. REPLACED WEB LOCATED AT LEVEL ORSS 261 DEFLECTION CONTROL RIB AREA AT TRAILING EDGE RT WING IAW SRM-51-10-02 ITEM 9 AND DWG: 115A2512; SHEET: 8; REV C.
- [SDR SWAA2026052793220](https://openairdocs.org/sdr/SWAA2026052793220.md): Plate · cracked · Apr 26, 2026 · N8645A · Boeing 7378H4 · Wing Main, Frame Structure
  > CRACK ON CORRUGATED PLATE LOCATED AT LEVEL IRSS 210 TRAILING EDGE RT WING. REPLACED CORRUGATED PLATE LOCATED AT LEVEL OF IRSS 210 TRAILING EDGE RT WING IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02-0G-0.
- [SDR SWAA2026052793090](https://openairdocs.org/sdr/SWAA2026052793090.md): Access Panel · cracked · Apr 26, 2026 · N8645A · Boeing 7378H4 · Wing, Plate/Skin
  > CRACK BRACKET ACCESS PANEL 551FB AT LT WING. REPLACED BRACKET LOCATED ON ACCESS PANEL 551FB AT LT WING IAW SRM 51-40-02-0G-0 AND DWG: 115A2710; SHEET: 9; REV: A. MEASURES OF CRACK: 1.143 INCH.
- [SDR SWAA2026052792907](https://openairdocs.org/sdr/SWAA2026052792907.md): Light · deteriorated · Apr 25, 2026 · N8645A · Boeing 7378H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINISCENT STRIP ALONG PAX CABIN. REPLACED PHOTOLUMINISCENT STRIP ALONG PAX CABIN IAW AMM 33-51-15-400-802 THE INSTALLATION WILL BE PERFORM ON MT 753-400-00-01Y SEE TTG8R007KHSP STEP 126.
- [SDR SWAA2026052792909](https://openairdocs.org/sdr/SWAA2026052792909.md): Light · broken · Apr 25, 2026 · N8645A · Boeing 7378H4 · Emergency Lighting
  > BROKEN EMERGENCY EXIT LIGHT ON SIDEWALL PANEL POSITION 231ZKW AT PASSENGER CABIN. REPLACED EMERGENCY EXIT LIGHT ON SIDEWALL PANEL POSITION 231ZKW AT PASSENGER CABIN IAW AMM 33-51-01-960-801, OPS TESTED OK.
- [SDR SWAA2026052792906](https://openairdocs.org/sdr/SWAA2026052792906.md): Crossbeam · cracked · Apr 25, 2026 · N8645A · Boeing 7378H4 · Fuselage Main, Structure
  > CRACK BRAKE PANEL LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL AND FASTENERS LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02-0G-0; SRM 51-10-02 PARAGRAPH 9 AND DWG 143A0060
- [SDR SWAA2026052792916](https://openairdocs.org/sdr/SWAA2026052792916.md): Support Angle · cracked · Apr 25, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BS 695 BL 0 WL 208.1 AT PASSENGER CABIN RT SIDE. REPLACED SUPPORT ANGLE LOCATED BS 695 BL 0 WL 208.1 AT PASSENGER CABIN RT SIDE IAW SRM 51-40-02 AND DRAWING 273A9110 SHEET: 6 REV. A.
- [SDR SWAA2026052792905](https://openairdocs.org/sdr/SWAA2026052792905.md): Crossbeam · cracked · Apr 25, 2026 · N8645A · Boeing 7378H4 · Fuselage Main, Structure
  > CRACKED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL AND FASTENERS LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02-0G-0; SRM 51-10-02 AND DWG 143A0060 SHEET 64
- [SDR SWAA2026052792720](https://openairdocs.org/sdr/SWAA2026052792720.md): Floor Support · cracked · Apr 24, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 AT FWD GALLEY AREA. REPLACED INTERCOSTAL LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING 141A5400 SHEET 46 REV A.
- [SDR SWAA2026052792721](https://openairdocs.org/sdr/SWAA2026052792721.md): Web · cracked · Apr 24, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED WEB LOCATED BTW BS 312 TO BS 328 RBL 31 WL 208.1 AT FWD GALLEY AREA. REPLACED WEB LOCATED BTW BS 312 TO BS 328 RBL 31 WL 208.1 AT FWD GALLEY AREA IAW SRM 51-10-02 ITEM 9 AND DWG 141A5410 SHEET 126 REV-.
- [SDR SWAA2026052792188](https://openairdocs.org/sdr/SWAA2026052792188.md): Access Panel · delaminated · Apr 23, 2026 · N8645A · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > DELAMINATED ACCESS PANEL 193AR LOWER FUSELAGE. REPAIRED ACCESS PANEL 193AR LOWER FUSELAGE IAW B737-800 SRM 51-70-05-2R-10 REPAIR 10.
- [SDR SWAA2026052791990](https://openairdocs.org/sdr/SWAA2026052791990.md): Access Panel · damaged · Apr 22, 2026 · N8645A · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > ELONGATED HOLE ACCESS PANEL 193D AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 193D AT LOWER FUSELAGE IAW SRM 51-70-05-2R-10 REPAIR 10.
- [SDR SWAA2026052791826](https://openairdocs.org/sdr/SWAA2026052791826.md): Access Panel · damaged · Apr 22, 2026 · N8645A · Boeing 7378H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 561AB AT LT WING. REPAIRED ACCESS PANEL 561AB AT LT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2026052791636](https://openairdocs.org/sdr/SWAA2026052791636.md): Strap · corroded · Apr 21, 2026 · N8645A · Boeing 7378H4 · Wing Miscellaneous Structure
  > CORROSION ON STRAP LOCATED APROX OSS 60 LEADING EDGE AT LT WING. PERFORMED REPAIR ON STRAP LOCATED BTW OSS 26.92 TO OSS 109.69 LEADING EDGE AT LT WING IAW EA 26-157-01100-WIP1 AND 26-157-01100-WIP2 AND B737-800 SRM 57-20-01-2R-3 REPAIR 3.
- [SDR SWAA2026040284458](https://openairdocs.org/sdr/SWAA2026040284458.md): Battery Pack · inoperative · Mar 30, 2026 · N8645A · Boeing 7378H4 · Emergency Lighting
  > RIGHT OVER WING EMERGENCY LIGHT PARTIALLY INOPERATIVE. REMOVED AND REPLACED RT OVER WING EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06;OPS CHECK GOOD.
- [SDR SWAA2025102724834](https://openairdocs.org/sdr/SWAA2025102724834.md): Light · damaged · Oct 15, 2025 · N8645A · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT LENS HOUSING LOCATED MID CABIN UPPER CEILINGS IS DAMAGED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY HOUSING; MID CABIN CEILING AND PERFORMED A GOOD OPS CHECKED IAW AMM 33-51-01-960-802 STEPS 3. C; (4) (C) (6) (7) (11) (12).
- [SDR SWAA2025100822224](https://openairdocs.org/sdr/SWAA2025100822224.md): Cover · missing · Oct 7, 2025 · N8645A · Boeing 7378H4 · Emergency Equipment
  > VELCRO COVER FOR MANUAL INFLATION HANDLE ON SLIDE FWD SERVICE DOOR IS MISSING. REPOSITIONED SLIDE AND INSTALLED MANUAL DEPLOY FLAP IAW AMM 25-66-01.
- [SDR SWAA2025062382930](https://openairdocs.org/sdr/SWAA2025062382930.md): Check Valve · inoperative · Jun 17, 2025 · N8645A · Boeing 7378H4 · Cabin Pressure Control System
  > @APPROX FL190 CABIN ALT ALERT SOUNDED IMMEDIATELY STARTED DECENT TO 10000 FT. CABIN MASKS AUTO DEPLOYED WHILE CREW DOWNING OXYGEN. COMPLETED DECENT W/ QRC & QRH PROCEDURES AND RETURNED TO ORIGIN JAX<[01] DURING INITIAL PACK CONFIDENCE CHECK FOUND GROUND AIR CO
- [SDR SWAA2025042862974](https://openairdocs.org/sdr/SWAA2025042862974.md): Power Supply · inoperative · Apr 24, 2025 · N8645A · Boeing 7378H4 · Emergency Lighting
  > FORWARD EXTERIOR EMERGENCY EXIT LIGHT BY R1 DOOR INOP.<[01] REMOVED AND REPLACED FWD OVERHEAD (M2816) POWER SUPPLY IAW AMM 33-51-06. OPS CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N8645A/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 = 'N8645A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8645A/reports

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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.
