# Service difficulty reports: N8618N, cancelled Jan 23, 2026

A list on [N8618N, cancelled Jan 23, 2026](https://openairdocs.org/deregistered/N8618N-2026-01-23.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 5 · 229 reports

- [SDR SWAA2025110327427](https://openairdocs.org/sdr/SWAA2025110327427.md): Skin · punctured · Oct 10, 2025 · N8618N · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > HOLE IN FUSELAGE SKIN, BS 188 STR 23-24R. FWD EDGE OF THE PART [4] STRUCTURAL FILLER IS 2.5 INCHES FROM NEAREST ROW OF STA 178 BUTT SPLICE. MINIMUM 3.00 INCHES REQUIRED IAW SRM 53-10-01-2R-8 FIGURE 202, FLAGNOTE 8. SEE STEP 15. OUTER RIVET ROWS HAVE BBAD RIV
- [SDR SWAA2025110323453](https://openairdocs.org/sdr/SWAA2025110323453.md): Lens · fogged · Oct 10, 2025 · N8618N · Boeing 7378H4 · Emergency Lighting
  > R2 DOOR EMERGENCY LIGHT LENS IS FOGGY.
- [SDR SWAA2025100619024](https://openairdocs.org/sdr/SWAA2025100619024.md): Angle · missing · Sep 28, 2025 · N8618N · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > MISSING TWO ANGLES SUPPORT ON IDG ACCESS PANEL OUTBOARD FAN COWL ENG 1. INSTALLED TWO ANGLES SUPPORT AND FASTENERS ON IDG ACCESS PANEL OUTBOARD FAN COWL ENGINE 1 IAW SRM 51-40-02 AND CMM 71-13-30 FIGURE 2 SHEET 6 DETAIL P.
- [SDR SWAA2025100614211](https://openairdocs.org/sdr/SWAA2025100614211.md): Bracket · broken · Sep 14, 2025 · N8618N · Boeing 7378H4 · Emergency Exits
  > BROKEN BRACKET ON LOWER SIDE OF EMERGENCY EXIT 832. REPLACED BRACKET ON LOWER SIDE OF EMERGENCY EXIT 832 IAW AMM 52-22-51-400-801 STEP 3.D (2) (D).
- [SDR SWAA2025100312998](https://openairdocs.org/sdr/SWAA2025100312998.md): Lens · broken · Sep 9, 2025 · N8618N · Boeing 7378H4 · Emergency Lighting
  > BROKEN SIGNAL LENS ASSY EMERGENCY DOOR LINING LH SIDE AT PASSENGER CABIN. REPLACED SIGNAL LENS ASSY EMERGENCY DOOR LINING LH SIDE AT PASSENGER CABIN I.A.W. B737-800 AMM 33-51-01-960-802 STEP 3. C. ITEM (5) (6) (7) AND (10) OPERATIONAL TEST IS OK.
- [SDR SWAA2025100313103](https://openairdocs.org/sdr/SWAA2025100313103.md): Battery Pack · inoperative · Sep 9, 2025 · N8618N · Boeing 7378H4 · Emergency Lighting
  > INOP BATTERY PACK LOCATION BTW BS 500C TO STA 500D RH SIDE AT PASSENGER CABIN (1 EA). REPLACED BATTERY PACK LOCATION BTW STA 500C TO STA 500D RH SIDE AT PASSENGER CABIN (1 EA) I.A.W. B737-800 AMM 33-51-06-960-805 STEP 4.E. ITEM (4) AND (5). PERFORMED OPERAT
- [SDR SWAA2025100213101](https://openairdocs.org/sdr/SWAA2025100213101.md): Battery Pack · inoperative · Sep 9, 2025 · N8618N · Boeing 7378H4 · Emergency Lighting
  > INOPERATIVE BATTERY PACK LOCATION BTW STA 559 TO STA 578 LT SIDE AT PASSENGER CABIN (1 EA). REPLACED BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.
- [SDR SWAA2025100213102](https://openairdocs.org/sdr/SWAA2025100213102.md): Battery Pack · inoperative · Sep 9, 2025 · N8618N · Boeing 7378H4 · Emergency Lighting
  > INOPERATIVE BATTERY PACK BTW STA 727C TO STA 727D LT SIDE AT PASSENGER CABIN (1 EA). REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805 STEP 4.E. ITEM (4) AND (5). PERFORMED OPERATIONAL TEST BATTERY PACK IAW AMM 33-51-06-960-805 STEP 4.E ITEM (6), TESTED O
- [SDR SWAA2025100311955](https://openairdocs.org/sdr/SWAA2025100311955.md): Handle · worn · Sep 6, 2025 · N8618N · Boeing 7378H4 · Service Doors
  > WORN NUT OF ASSISTANT HANDLE LOCATED ON FWD SERVICE DOOR 2 EA AND AFT SERVICE DOOR 2 EA. REPLACED NUT OF ASSISTANT HANDLE LOCATED ON FWD SERVICE DOOR 2 EA AND AFT SERVICE DOOR 2 EA IAW 737-800 AMM 52-41-31-400-802 STEP 3.F(2).
- [SDR SWAA2025100311954](https://openairdocs.org/sdr/SWAA2025100311954.md): Handle · worn · Sep 6, 2025 · N8618N · Boeing 7378H4 · Passenger/Crew Doors
  > WORN NUT OF ASSISTANT HANDLE LOCATED ON FWD ENTRY DOOR LOWER SIDE 2EA. REPLACED NUT OF ASSISTANT HANDLE LOCATED ON FWD ENTRY DOOR LOWER SIDE 2EA IAW AMM 52-11-31-400-802 STEP 3.G Ï¿½TEM (2) (D).
- [SDR SWAA2025100311957](https://openairdocs.org/sdr/SWAA2025100311957.md): Handle · worn · Sep 6, 2025 · N8618N · Boeing 7378H4 · Passenger/Crew Doors
  > WORN NUT OF ASSISTANT HANDLE LOCATED ON DOORWAY LININGS AT FWD ENTRY DOOR 4 EA AND FWD SERVICE DOOR 2 EA AT FWD GALLEY AREA. REPLACED NUT OF ASSISTANT HANDLE LOCATED ON DOORWAY LININGS AT FWD ENTRY DOOR 4 EA AND FWD SERVICE DOOR 2 EA AT FWD GALLEY AREA IAW A
- [SDR SWAA2025100311956](https://openairdocs.org/sdr/SWAA2025100311956.md): Handle · worn · Sep 6, 2025 · N8618N · Boeing 7378H4 · Passenger/Crew Doors
  > WORN NUT OF ASSISTANT HANDLE LOCATED ON DOORWAY LININGS AT AFT ENTRY DOOR 2 EA AND AFT SERVICE DOOR 2 EA AT AFT GALLEY AREA. REPLACED NUT OF ASSISTANT HANDLE LOCATED ON DOORWAY LININGS AT AFT ENTRY DOOR 2 EA AND AFT SERVICE DOOR 2 EA AT AFT GALLEY AREA IAW A
- [SDR SWAA2025100311943](https://openairdocs.org/sdr/SWAA2025100311943.md): Angle · cracked · Sep 5, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED AFT FACE BS 500I AT LEVEL STR 28R AT FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED AFT FACE BS 500I AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 301 REV A
- [SDR SWAA2025100311944](https://openairdocs.org/sdr/SWAA2025100311944.md): Angle · cracked · Sep 5, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED AFT FACE BS 500I AT LEVEL STR 28L AT FWD CARGO COMPARTMENT. REPLACED ANGLE (BRACKET) AND FASTENERS LOCATED AFT FACE BS 500I AT LEVEL STR 28L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG:143A7
- [SDR SWAA2025100611313](https://openairdocs.org/sdr/SWAA2025100611313.md): Nut Plate · corroded · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing, Attach Fittings
  > CORROSION ON RAIL NUT-PLATE LOCATED OFSS 573 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 573 INTERNAL CAVITY LEADING EDGE AT LT WING IAW IAW SRM 51-40-02 AND DRAWING 112A4402 REV:A.
- [SDR SWAA2025100611321](https://openairdocs.org/sdr/SWAA2025100611321.md): Nut Plate · corroded · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing, Attach Fittings
  > CORROSION ON RAIL NUT-PLATE LOCATED OFSS 632 INTERNAL CAVITY LEADING EDGE AT LT WING REPLACED RAIL NUT-PLATE LOCATED OFSS 632 INTERNAL CAVITY LEADING EDGE AT LT WING IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 112A4402 SHEET:40 REV:A.
- [SDR SWAA2025100611323](https://openairdocs.org/sdr/SWAA2025100611323.md): Nut Plate · corroded · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing, Attach Fittings
  > CORROSION ON RAIL NUT-PLATE LOCATED OFSS 573 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 573 INTERNAL CAVITY LEADING EDGE AT LT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 112A4402 SHEET 40 REV A.
- [SDR SWAA2025100611563](https://openairdocs.org/sdr/SWAA2025100611563.md): Nut Plate · corroded · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing, Attach Fittings
  > CORROSION ON RAIL NUT-PLATE LOCATED OFSS 491 INTERNAL CAVITY LEADING EDGE RT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 491 INTERNAL CAVITY LEADING EDGE AT RT WING AND APPLIED PROTECTIVE TREATMENT ON FASTENERS. IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 8;
- [SDR SWAA2025100611564](https://openairdocs.org/sdr/SWAA2025100611564.md): Support Bracket · cracked · Sep 4, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY IAW B737-800 SRM 51-10-2-0G-0 ITEM 9 AND SRM 51-40-02-0G-0. MEASURES OF CRACK IS: L=0.818.
- [SDR SWAA2025100611557](https://openairdocs.org/sdr/SWAA2025100611557.md): Channel · cracked · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACK CHANNEL OB FIXED LEADING EDGE BTW OFSS 564 AND OFSS 580 AT RT WING. REPLACED CHANNEL OB FIXED LEADING EDGE BTW OFSS 564 AND OFSS 580 AT RT WING IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG:112A4402; SHEET:41; REV A. MEASURE OF CRACK IS L: 0.
- [SDR SWAA2025100611554](https://openairdocs.org/sdr/SWAA2025100611554.md): Strap · corroded · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing Miscellaneous Structure
  > CORROSION STRAP O/B FIXED LEADING EDGE AT LEVEL OFSS 584 AT RT WING. REFER TO FAULT TT8Q014Z6U7 WHERE 25-157-02455 WAS ADDED AS A SUBTASK.
- [SDR SWAA2025100611326](https://openairdocs.org/sdr/SWAA2025100611326.md): Strap · corroded · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing Miscellaneous Structure
  > CORROSION ON STRAP O/B FIXED LEADING EDGE AT LEVEL OFSS 456 AT RT WING. PERFORMED REPAIR ON STRAP O/B FIXED LEADING EDGE AT LEVEL OFSS 456 OR ( OSS 227-95) AND OFSS 584 OR ( OSS 349.91) AT RT WING IAW EA 25-157-02455 AND EA 25-157-02455 WIP 1.
- [SDR SWAA2025100611325](https://openairdocs.org/sdr/SWAA2025100611325.md): Strap · corroded · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing Miscellaneous Structure
  > CORROSION ON STRAP OTBD FIXED LEADING EDGE AT LEVEL OFSS 456 AT RT WING. REFER TO FAULT TTG8Q014Z6U7 WHERE 25-154-02455 WAS ADDED AS A SUBTASK. LOC. OFSS 456 (OSS 227.95);[03] FAULT RESOLVED ON OTHER FAULT.
- [SDR SWAA2025100611311](https://openairdocs.org/sdr/SWAA2025100611311.md): Web · cracked · Sep 4, 2025 · N8618N · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > CRACK WEB ON OUTBOART FAN COWL ENGINE 2. REPLACED WEB LOCATED ON OUTBOARD FAN COWL OF ENGINE 2 IAW CMM 71-13-30, PAGE 10088, FIGURE 3, SHEET 1, DETAIL P, TABLE OF PAGE 10105, AND SRM 51-40-02-0G-0. MEASUREMENTS OF CRACK IS: 1.025 INCH.
- [SDR SWAA2025100311315](https://openairdocs.org/sdr/SWAA2025100311315.md): Rail · corroded · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing Main, Frame Structure
  > CORROSION ON RAIL NUT-PLATE LOCATED OFSS 449 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE AND FASTENERS LOCATED OFSS 449 INTERNAL CAVITY LEADING EDGE AT LT WING IAW B373-800 SRM 51-40-02 AND 51-10-02 APPLIED PROTECTIVE TREATMENT ON NEW FA
- [SDR SWAA2025100311316](https://openairdocs.org/sdr/SWAA2025100311316.md): Rail · corroded · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing Main, Frame Structure
  > CORROSION ON RAIL NUT-PLATE LOCATED OFSS 332 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE AND FASTENERS LOCATED OFSS 332 INTERNAL CAVITY LEADING EDGE AT LT WING IAW B373-800 SRM 51-40-02 AND 51-10-02 ITEM 9. APPLIED PROTECTIVE TREATMENT O
- [SDR SWAA2025100311550](https://openairdocs.org/sdr/SWAA2025100311550.md): Rail · corroded · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing Miscellaneous Structure
  > CORROSION ON RAIL NUT-PLATE LOCATED OFSS 286 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE AND FASTENERS LOCATED ON OFSS 286 AT INTERNAL CAVITY OF LEADING EDGE OF LT WING IAW SRM 51-40-02-0G-0 AND DRAWING NUMBER: 112A4402; SHEET: 41; REV: A
- [SDR SWAA2025100311330](https://openairdocs.org/sdr/SWAA2025100311330.md): Rail · cracked · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACK ON RAIL NUT-PLATE LOCATED OFSS 385 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE AND FASTENERS LOCATED OFSS 385 INTERNAL CAVITY LEADING EDGE AT LT WING I.A.W B737-800 SRM 51-40-02 AND DWG 112A4402 SHEET 41 REV A.
- [SDR SWAA2025100311322](https://openairdocs.org/sdr/SWAA2025100311322.md): Rail · cracked · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing Main, Frame Structure
  > CRACK ON RAIL NUT-PLATE LOCATED OFSS 604 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE AND FASTENERS LOCATED ON OFSS 604 AT INTERNAL CAVITY OF LEADING EDGE OF LT WING IAW B737-800 SRM 51-40-02-0G-0 AND DRAWING 112A4402; SHEET: 41; REV: A.
- [SDR SWAA2025100311331](https://openairdocs.org/sdr/SWAA2025100311331.md): Rail · corroded · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing Main, Frame Structure
  > CORROSION ON RAIL NUT-PLATE LOCATED OFSS 308 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE AND FASTENERS LOCATED OFSS 308 INTERNAL CAVITY LEADING EDGE AT LT WING IAW SRM 51-40-02 AND DWG 112A4402 SHEET 40 REV A.
- [SDR SWAA2025100311565](https://openairdocs.org/sdr/SWAA2025100311565.md): Angle · cracked · Sep 4, 2025 · N8618N · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACK ON ANGLE LOCATED AUXILIARY TRACK LOWER POSITION SLAT 7 AT RT WING. REPLACED ANGLE LOCATED AUXILIARY TRACK LOWER POSITION SLAT 7 AT RT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.
- [SDR SWAA2025100211566](https://openairdocs.org/sdr/SWAA2025100211566.md): Support Angle · cracked · Sep 4, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK CARGO LINER SUPPORT ANGLE LOCATED STA 727B AND BTW STR 17L TO STR 18L AT AFT CARGO COMPARTMENT. PERFORMED REPAIR SUPPORT ANGLE LOCATED STA 727B AND BTW STR 17L TO STR 18L AT AFT CARGO COMPARTMENT IAW SRM 51-70-11-2R-0.
- [SDR SWAA2025100611123](https://openairdocs.org/sdr/SWAA2025100611123.md): Support · corroded · Sep 3, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ANGLE - SUPPORT LOCATED STA 907 AND BTW STR 26L TO STR 27L WL 152 AT AFT CARGO COMPARTMENT. REPLACED ANGLE - SUPPORT LOCATED STA 907 AND BTW STR 26L TO STR 27L WL 152 AT AFT CARGO COMPARTMENT IAW SRM 51-10-02; SRM 51-40-02 AND DWG: 147A1007; SHEET:
- [SDR SWAA2025100611109](https://openairdocs.org/sdr/SWAA2025100611109.md): Strap · missing · Sep 3, 2025 · N8618N · Boeing 7378H4 · Emergency Equipment
  > MISSING RETAINER OF ESCAPE STRAP ON EMERGENCY EXIT RH SIDE AT PASSENGER CABIN. INSTALLED RETAINER OF ESCAPE STRAP ON EMERGENCY EXIT RH SIDE AT PASSENGER CABIN (1 EA) IAW SOPM 20-50-12 REV.58.
- [SDR SWAA2025100611111](https://openairdocs.org/sdr/SWAA2025100611111.md): Support Bracket · corroded · Sep 3, 2025 · N8618N · Boeing 7378H4 · Wing Miscellaneous Structure
  > CORROSION SUPPORT BRACKET LOCATED BTW ORSS 395 AND BTW ORSS 411 TRAILING EDGE AREA AT RT WING. REPLACED SUPPORT BRACKET LOCATED BETWEEN ORSS 395 TO ORSS 411 ON TRAILING EDGE AREA AT RT WING IAW B737-800 SRM 51-40-02-0G-0 AND DRAWING NUMBER: 115A3500 SHEET: 3
- [SDR SWAA2025100610927](https://openairdocs.org/sdr/SWAA2025100610927.md): Access Panel · cracked · Sep 3, 2025 · N8618N · Boeing 7378H4 · Wing, Plate/Skin
  > CRACK ON AFT INBOARD RETAINER SEAL ACCESS PANEL 543BB AT LT WING. MEASUREMENTS OF CRACK IS: L= 0.858. REPLACED AFT INBD RETAINER SEAL ACCESS PANEL 543BB AT LT WING IAW SRM 51-40-02-0G AND SRM 51-40-04-0G.
- [SDR SWAA2025100610925](https://openairdocs.org/sdr/SWAA2025100610925.md): Access Panel · cracked · Sep 3, 2025 · N8618N · Boeing 7378H4 · Wing, Plate/Skin
  > CRACK ON INTERNAL AREA ACCESS PANEL 542BB AT LT WING 2025-541768<[01] ACCOMPLISHED M-21-157-01063 (COMPONENT - SWA - REPAIR - #3/6 FLAP TRACK SUPPORT AFT (CANOE) FAIRING AND TAILCONE TYPICAL 350 DEGREE CURE VACUUM BAG REPAIR) ON ACCESS PANEL 542BB AT LT WING A
- [SDR SWAA2025100610926](https://openairdocs.org/sdr/SWAA2025100610926.md): Access Panel · damaged · Sep 3, 2025 · N8618N · Boeing 7378H4 · Wing, Plate/Skin
  > ELONGATED HOLE ON ACCESS PANEL 542EB AT LT WING. REPAIRED ACCESS PANEL 542EB IAW 25-157-02593-WIP1 AND 25-157-02593-WIP2.
- [SDR SWAA2025100311122](https://openairdocs.org/sdr/SWAA2025100311122.md): Angle · cracked · Sep 3, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA REPLACED ANGLE AND FASTENERS LOCATED ON FORWARD GALLEY AREA BETWEEN BS 291.5 TO BS 294.5 AT LEVEL OF STR 17R IAW SRM 51-40-02-0G-0 AND DRAWING NUMBER: 141A8310 SHEET: 33 REV.
- [SDR SWAA2025100311120](https://openairdocs.org/sdr/SWAA2025100311120.md): Tie Clip · cracked · Sep 3, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. I.A.W 737-800 DWG:141A1110;SHEET:54;REV:-, DWG:141A8380. SHEET 21, REV-, AND SRM:51-40-02-0G.
- [SDR SWAA2025100311125](https://openairdocs.org/sdr/SWAA2025100311125.md): Strap · corroded · Sep 3, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION STRAP LOCATED BTW STA 794.3 TO STA 807 AND BTW STR 25R TO STR 26R WL 156 AT AFT CARGO COMPARTMENT. REPLACED STRAP AND FASTENERS LOCATED BTW STA 794.3 TO STA 807 AND BTW STR 25R TO STR 26R WL 156 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02-0G-0; SRM 5
- [SDR SWAA2025100211115](https://openairdocs.org/sdr/SWAA2025100211115.md): Support · corroded · Sep 3, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW STA 727C TO STA 747 STR 25L WL 156 (12 POINTS) AT AFT CARGO COMPARTMENT. REPAIRED SUPPORT ZEE AND FASTENERS LOC. BTW BS727 TO BS847 STR 25L AND WL 156 AT AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-6, REPAIR 6, PARAGRAPH 4.L,
- [SDR SWAA2025100210930](https://openairdocs.org/sdr/SWAA2025100210930.md): Support · corroded · Sep 3, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW STA 727J TO STA 847 STR 25L AND WL 156 AT AFT CARGO COMPARTMENT (7 POINTS). REPAIRED SUPPORT ZEE AND FASTENERS LOC. BTW BS727 TO BS847 STR 25L AND WL 156 AT AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-6 REPAIR 6 PARAGRAPH 4.L,
- [SDR SWAA2025100210933](https://openairdocs.org/sdr/SWAA2025100210933.md): Cargo Track · cracked · Sep 3, 2025 · N8618N · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK CARGO TRACK RBL 13.84 AND STA 747 AFT CARGO COMPARTMENT. REPAIRED CARGO TRACK LOCATED RBL 13.84 BWT BS 727J TO BS767 AFT CARGO COMPARTMENT IAW B737-800 SRM 53-00-53-2R-3 REPAIR 3 AND SRM 51-40-02.
- [SDR SWAA2025100210932](https://openairdocs.org/sdr/SWAA2025100210932.md): Web · corroded · Sep 3, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB LOCATED STA 767 TO STA 794.3 STR 25R WL 156 AT AFT CARGO COMPARTMENT. REPLACED THE SHIELD WEB LOCATED STA 767 TO STA 794.3 STR 25R WL 156 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02.
- [SDR SWAA2025100211119](https://openairdocs.org/sdr/SWAA2025100211119.md): Web · corroded · Sep 3, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOCATED BTW STA 767 TO STA 787 STR 25R AND WL 156 AT AFT CARGO COMPARTMENT. REPLACED WEB LOCATED BTW STA 767 TO STA 787 STR 25R AND WL 156 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 ITEM 9 AND 146A0081 SHEET 49 REV A.
- [SDR SWAA2025100610717](https://openairdocs.org/sdr/SWAA2025100610717.md): Web · corroded · Sep 2, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOCATED BTW BS 492.4 TO 500A, S26R, WL 152, FWD CARGO COMPARTMENT. REPLACED WEB LOCATED BTW STA 492.4 TO STA 500A STR 26R WL 152 AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 143A0080 SHEET 39 REV-.
- [SDR SWAA2025100610722](https://openairdocs.org/sdr/SWAA2025100610722.md): Support Angle · cracked · Sep 2, 2025 · N8618N · 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 LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN IAW SRM-51-40-02, SRM 51-10-02, ITEM 9, DWG 143A5400, SHEET 154, REV -, AND DWG 143A5400
- [SDR SWAA2025100610723](https://openairdocs.org/sdr/SWAA2025100610723.md): Support Angle · cracked · Sep 2, 2025 · N8618N · 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 LOCATED BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN IAW SRM-51-40-02, SRM 51-01-02, ITEM 9 AND DWG 143A5400, SHEET 142, REV -, DWG 143A
- [SDR SWAA2025100610727](https://openairdocs.org/sdr/SWAA2025100610727.md): Support Angle · cracked · Sep 2, 2025 · N8618N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 50 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 50 WL 208.1 AT PASSENGER CABIN IAW SRM 51-10-02; SRM 51-40-02 AND DWG 143A5400 SHEET 141 REV -.

Next page: https://openairdocs.org/deregistered/N8618N-2026-01-23/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 = 'N8618N' AND deregistration_id = 'N8618N-2026-01-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8618N-2026-01-23/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.