# Service difficulty reports: N8635F, cancelled Jul 16, 2026

A list on [N8635F, cancelled Jul 16, 2026](https://openairdocs.org/deregistered/N8635F-2026-07-16.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 · 126 reports

- [SDR SWAA2026060194855](https://openairdocs.org/sdr/SWAA2026060194855.md): Rib · cracked · May 2, 2026 · N8635F · Boeing 7378H4 · Wing, Rib/Bulkhead
  > CRACKED TRAILING EDGE ON DEFLECTION CONTROL RIB ORSS 280 AT RT WING. PERFORMED PERMANENT REPAIR ON DEFLECTION CONTROL RIB AT RT WING IAW SRM 57-51-02-2R-3 REPAIR 3.
- [SDR SWAA2026060194856](https://openairdocs.org/sdr/SWAA2026060194856.md): Web · cracked · May 2, 2026 · N8635F · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACK WEB TRAILING EDGE LOCATED ORSS 261 TO ORSS 280 LT WING. REPLACED WEB TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 280 LT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2512 SHEET 16 REV-.
- [SDR SWAA2026060194857](https://openairdocs.org/sdr/SWAA2026060194857.md): Access Panel · cracked · May 2, 2026 · N8635F · Boeing 7378H4 · Nacelle/Pylon, Plate/Skin
  > CRACK SEAL BLADE ACCESS PANEL 441AL AT RT PYLON. REPLACED SEAL BLADE LOCATED ON ACCESS PANEL 441AL AT RT PYLON IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02.
- [SDR SWAA2026060194686](https://openairdocs.org/sdr/SWAA2026060194686.md): Angle · cracked · May 1, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BETWEEN STA380 TO STA400 AND LBL13 WL 208.1 AT PASSENGER CABIN. REPLACED ANGLE AND FASTENERS LOCATED BETWEEN STA380 TO STA400 AND LBL13 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 140 RE
- [SDR SWAA2026060194688](https://openairdocs.org/sdr/SWAA2026060194688.md): Angle · cracked · May 1, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BETWEEN BS 380 TO 400 AND LBL52 WL 208.1 AT PASSENGER CABIN. REPLACED ANGLE AND FASTENERS LOCATED BETWEEN BS 380 TO 400 AND LBL52 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET: 140 REV:-.
- [SDR SWAA2026060194290](https://openairdocs.org/sdr/SWAA2026060194290.md): Angle · cracked · Apr 30, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED BS 500H AFT SIDE AND S-26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS 500H AFT SIDE AND S-26R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505; SHEET 138; REV -.
- [SDR SWAA2026060194294](https://openairdocs.org/sdr/SWAA2026060194294.md): Angle · cracked · Apr 30, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE LOCATED BS500G FWD SIDE AND S-26L AT FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS500G FWD SIDE AND S-26L AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505; SHEET 137; REV -.
- [SDR SWAA2026060194297](https://openairdocs.org/sdr/SWAA2026060194297.md): Angle · cracked · Apr 30, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE LOCATED BS 500G FWD SIDE AND S-26R AT FWD CARGO COMPARTMENT. REPLACED REPAIR ANGLE AND FASTENERS LOCATED BS 500G FWD SIDE AND S-26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505; SHEET 139; REV-.
- [SDR SWAA2026060194298](https://openairdocs.org/sdr/SWAA2026060194298.md): Angle · cracked · Apr 30, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R AT FWD CARGO COMPARTMENT. REPLACED GUSSET ANGLE AND FASTENERS LOCATED ON BS 500I AT LEVEL STR 19R AT FWD CARGO BAY IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7902; SHEET: 256 AND 257; REV: B.
- [SDR SWAA2026060194289](https://openairdocs.org/sdr/SWAA2026060194289.md): Angle · cracked · Apr 30, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE LOCATED BS 500H FWD SIDE AND S-26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED BS 500H FWD SIDE AND S-26R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 AND DWG 143A7505, SHEET 137; REV-.
- [SDR SWAA2026060194296](https://openairdocs.org/sdr/SWAA2026060194296.md): Angle · cracked · Apr 30, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE LOCATED BS 500G AFT SIDE AND S-26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED BS 500G AFT SIDE AND S-26R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505; SHEET 139; REV-.
- [SDR SWAA2026060193942](https://openairdocs.org/sdr/SWAA2026060193942.md): Stop Fitting · cracked · Apr 29, 2026 · N8635F · Boeing 7378H4 · Emergency Exits
  > CRACK ON PAD STOP FITTING AFT EMERGENCY EXIT DOOR AT PASSENGER CABIN. REPLACED PAD STOP FITTING AFT EMERGENCY EXIT DOOR LT SIDE AT PASSENGER CABIN (1 EA) IAW AMM 52-22-01-400-801.
- [SDR SWAA2026060193943](https://openairdocs.org/sdr/SWAA2026060193943.md): Intercostal · cracked · Apr 29, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FAULT RAISED TO CAPTURE RII LABOR OF CRACK ON WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 LBL 10 WL 208.1 AT FWD GALLEY AREA. REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 344 TO BS 360 LBL 10 WL 208.1 AT FWD GALLEY AREA IAW SRM 53-10-15; SRM 51-40-02 A
- [SDR SWAA2026060193754](https://openairdocs.org/sdr/SWAA2026060193754.md): Floor Panel · cracked · Apr 28, 2026 · N8635F · Boeing 7378H4 · Fuselage Floor Panel
  > CRACKED FLOOR PANEL 221BF AT FWD GALLEY AREA. REPLACED FLOOR PANEL 221BF AT FWD GALLEY AREA IAW AMM 53-21-00-400-801 STEP 12.F.(12)(13) AND INSTALLATION OF FLOOR PANEL 221BF WILL BE INSTALLED ON ANOTHER TASK SEE TTG8Q01BBYBT.
- [SDR SWAA2026060193622](https://openairdocs.org/sdr/SWAA2026060193622.md): Intercostal · corroded · Apr 28, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB - INTERCOSTAL LOCATED BS 767 TO BS 794 AND S-25R, WL 156. AFT CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL LOCATED BS 767 TO BS 794 AND S-25R WL 156 AFT CARGO COMPARTMENT IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 146A0081, SHEET 49, REV
- [SDR SWAA2026052893621](https://openairdocs.org/sdr/SWAA2026052893621.md): Support · corroded · Apr 28, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BS 767 TO BS 787 AND S-25L WL 156 AFT CARGO COMPARTMENT. PERFORMED REPAIR CATEGORY A ON SUPPORT ZEE LOC. BTW BS727G + 7? TO BS807 + 14? AND S-25L WL 156 AFT CARGO COMPARTMENT IAW B737-800 SRM 53-00-53-2R-6 REPAIR 6 AND DWG 146A7
- [SDR SWAA2026060193393](https://openairdocs.org/sdr/SWAA2026060193393.md): Tie Clip · cracked · Apr 27, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK TIE CLIP BS 277 AND STR 10R PASSENGER CABIN. REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 STR 10R AT PASSENGER CABIN IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A1110, SHEET 55, REV - AND DWG 141A8380, SHEET 21, REV -.
- [SDR SWAA2026060193394](https://openairdocs.org/sdr/SWAA2026060193394.md): Frame · cracked · Apr 27, 2026 · N8635F · Boeing 7378H4 · Fuselage Main, Frame
  > CRACK FRAME BS 312 BTW STR 5L TO STR 6L AT PASSENGER CABIN. REPAIRED FRAME BS 312 BTW STR 5L TO STR 6L AT PASSENGER CABIN IAW EA M-22-153-01244.
- [SDR SWAA2026060193395](https://openairdocs.org/sdr/SWAA2026060193395.md): Support Angle · cracked · Apr 27, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED STA867 BETWEEN STR 2R TO STR 3R AT PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED STA867 BETWEEN STR 2R TO STR 3R AT PASSENGER CABIN IAW SRM 51-10-02-0G-0, STEP 9, AND SRM 51-40-02-0G-0, DWG 146A7901, SHEET 66, REV A.
- [SDR SWAA2026060193178](https://openairdocs.org/sdr/SWAA2026060193178.md): Balance Weight · out of balance · Apr 26, 2026 · N8635F · Boeing 7378H4 · Elevator Structure
  > DURING WEIGHT AND BALANCE OF ELEVATOR LT P/N: 183A0103-21 FOUND BALANCE WEIGHTS P/N: 183A0210-15 (1EA) ON BAY 4; P/N: 183A0210-14 (1EA) ON BAY 3; P/N: 183A0210-14 (1EA) ON BAY 2 THIS BALANCE WEIGHTS. MULTI-EFFECTIVE EA M-22-155-03766 (TCO-SWA-22-0356) COMPLET
- [SDR SWAA2026060193179](https://openairdocs.org/sdr/SWAA2026060193179.md): Balance Weight · out of balance · Apr 26, 2026 · N8635F · Boeing 7378H4 · Elevator Structure
  > DURING WEIGHT AND BALANCE OF ELEVATOR RT P/N: 183A0103-26 FOUND BALANCE WEIGHTS P/N: 183A0210-15 (1EA) ON BAY 4; P/N: 183A0210-14 (1EA) ON BAY 3; P/N: 183A0210-14 (1EA) ON BAY 2 THIS BALANCE WEIGHTS. MULTI-EFFECTIVE EA M-22-155-03767 (TCO-SWA-22-0356) COMPLET
- [SDR SWAA2026060192700](https://openairdocs.org/sdr/SWAA2026060192700.md): Scuff Plate · cracked · Apr 25, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA. REPAIRED SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA IAW SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.
- [SDR SWAA2026060192697](https://openairdocs.org/sdr/SWAA2026060192697.md): Support Web · cracked · Apr 24, 2026 · N8635F · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > CRACK SUPPORT WEB LOCATED INBOARD FAN COWL ON ENGINE 1. REPLACED SUPPORT WEB LOCATED INBD FAN COWL ON ENGINE 1 IAW SRM 51-10-020-G-0 STEP 9; SRM 51-40-02-0G-0 AND CMM 71-13-30 FIG 3 SHEET 10092.
- [SDR SWAA2026060191946](https://openairdocs.org/sdr/SWAA2026060191946.md): Girt Bar · deteriorated · Apr 23, 2026 · N8635F · Boeing 7378H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT FWD GALLEY AREA. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT FWD GALLEY AREA IAW AMM 25-66-02-400-801 THE INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8R008B4KB STEP 2.A.(12).
- [SDR SWAA2026060191945](https://openairdocs.org/sdr/SWAA2026060191945.md): Girt Bar · deteriorated · Apr 22, 2026 · N8635F · Boeing 7378H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS FWD SERVICE DOOR AT FWD GALLEY AREA. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS FWD SERVICE DOOR AT FWD GALLEY AREA IAW AMM 25-66-02-400-801, THE INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8R008B4KB STEP 2.A
- [SDR SWAA2026060191943](https://openairdocs.org/sdr/SWAA2026060191943.md): Girt Bar · deteriorated · Apr 22, 2026 · N8635F · Boeing 7378H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS SERVICE DOOR AT AFT GALLEY AREA. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS SERVICE DOOR AT AFT GALLEY AREA IAW AMM 25-66-02-400-801 THE INSTALLATION WILL BE<BR>ACCOMPLISHED ON TASK CARD TTG8R008B4WB STEP 2.A. (13)
- [SDR SWAA2026060191944](https://openairdocs.org/sdr/SWAA2026060191944.md): Girt Bar · deteriorated · Apr 22, 2026 · N8635F · Boeing 7378H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT AFT GALLEY AREA. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT AFT GALLEY AREA IAW AMM 25-66-02-400-801 THE INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8R008B4WB STEP 2.A.(13).
- [SDR SWAA2026060191932](https://openairdocs.org/sdr/SWAA2026060191932.md): Web · cracked · Apr 22, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 BL 0 WL 208.1 AT FWD GALLEY AREA. REPLACED WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 BL 0 WL 208.1 AT FWD GALLEY AREA IAW SRM 51-40-02 AND DWG 141A5400; SHEET: 32 AND REV-.
- [SDR SWAA2026060191931](https://openairdocs.org/sdr/SWAA2026060191931.md): Web · cracked · Apr 22, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 RBL 51 WL 208.1 AT FWD GALLEY AREA. REPLACED WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 RBL 51 WL 208.1 AT FWD GALLEY AREA IAW B737-800 SRM 51-10-02-0G-0 STEP 9; 51-40-02-0G-0 AND DWG 141A5400 SHEET 14 R
- [SDR SWAA2026060191934](https://openairdocs.org/sdr/SWAA2026060191934.md): Structure · cracked · Apr 22, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON INNER CHORD LOCATED BS 303.9 LBL 54 WL 208.1 AT FWD GALLEY AREA. REPLACED INNER CHORD LOCATED BTW STA 270 TO STA 360 LBL 54 WL 208.1 AT FWD GALLEY AREA IAW SRM 51-40-02; DWG 142A0050 SHEET 15 REV- AND DWG 141A8110 SHEET 11 REV-.
- [SDR SWAA2026060191933](https://openairdocs.org/sdr/SWAA2026060191933.md): Intercostal · cracked · Apr 22, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 LBL 10 WL 208.1 AT FWD GALLEY AREA. REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS 344 TO BS 360 LBL 10 WL 208.1 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DWG 141A5400 SHE
- [SDR SWAA2026060191929](https://openairdocs.org/sdr/SWAA2026060191929.md): Web · cracked · Apr 22, 2026 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED BTW BS 312 TO BS 328 RBL 32 WL 208.1 AT FWD GALLEY AREA. REPLACED WEB AND FASTENERS LOCATED BTW BS 312 TO BS 328 RBL 32 WL 208.1 AT FWD GALLEY AREA IAW SRM 51-40-02; SRM 51-10-02, ITEM 9, AND DWG 141A5400, SHEET 39, REV -.
- [SDR SWAA2026060191137](https://openairdocs.org/sdr/SWAA2026060191137.md): Battery Pack · inoperative · Apr 20, 2026 · N8635F · Boeing 7378H4 · Emergency Lighting
  > INOPERATIVE LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA. REPLACED LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA (2 EA) IAW AMM 33-51-06-960-805 TEST OK;
- [SDR SWAA2026060190522](https://openairdocs.org/sdr/SWAA2026060190522.md): Skin · debonded · Apr 17, 2026 · N8635F · Boeing 7378H4 · Trailing Edge Flaps
  > DEBONDED LOWER SKIN LOCATED IB SIDE OF OB AFT FLAP AT RT WING. PERFORMED PERMANENT REPAIR ON RH WING T/E OUTBD AFT FLAP WEDGE PANEL ON UPPER AND LOWER SKIN IAW SWA EA 26-157-01292-WIP2.
- [SDR SWAA2026060190521](https://openairdocs.org/sdr/SWAA2026060190521.md): Skin · delaminated · Apr 17, 2026 · N8635F · Boeing 7378H4 · Trailing Edge Flaps
  > DELAMINATED AFT FLAP LOCATED INBOARD EDGE OF OUTBOARD FLAP AT LT WING. PERFORMED PERMANENT REPAIR ON LT WING T/E OUTBD AFT FLAP WEDGE PANEL ON UPPER AND LOWER SKIN IAW SWA EA# 26-157-01295-WIP1.
- [SDR SWAA2026012864544](https://openairdocs.org/sdr/SWAA2026012864544.md): Slide · dislodged · Jan 26, 2026 · N8635F · Boeing 7378H4 · Escape Slide
  > RAMP REPORTED FWD ENTRY DOOR SLIDE FELL OUT OF IT`S COVER. REPACKED THE FWD ENTRY DOOR ESCAPE SLIDE IAW MT 725-61-06.
- [SDR SWAA2025061080096](https://openairdocs.org/sdr/SWAA2025061080096.md): Tray · broken · Jun 6, 2025 · N8635F · Boeing 7378H4 · Passenger Compartment Equipment
  > 15C 14D TRAY TABLES BROKEN. REMOVED AND REPLACED ROW 14D AND 15C TRAY TABLES PER SIP.
- [SDR SWAA2025042964957](https://openairdocs.org/sdr/SWAA2025042964957.md): Transmission · faulted · Apr 27, 2025 · N8635F · Boeing 7378H4 · Trailing Edge Flap Control System
  > TRAILING EDGE FLAP DISAGREE ON FINAL<[01] DRAINED & SERVICED TRAILING EDGE FLAP TRANSMISSION N0.1 AND N0.8. PERFORMED OPS CK. OPS CK OK REF AMM 12-22-51
- [SDR SWAA2024112772224](https://openairdocs.org/sdr/SWAA2024112772224.md): Fuse · inoperative · Nov 27, 2024 · N8635F · Boeing 7378H4 · Emergency Lighting
  > R/H AFT FUSELAGE EMERGENCY EXIT LIGHT ADJACENT TO R2 DOOR. R & R POWER SUPPLY FUSE IAW AMM 33-51-06; OPS CHK OK.
- [SDR SWAA2024071813902](https://openairdocs.org/sdr/SWAA2024071813902.md): Indicator · tripped · Jul 18, 2024 · N8635F · Boeing 7378H4 · Trailing Flap Position Indicating System
  > FLAP WERE SELECTED 5-FLAP INDICATION REMAINED AT ZERO -GAUGE NO LEADING EDGE DEVICES EXTENDED; USE ALT FLAP EXTENSION TO EXTEND FLAP TO 15. THIS DROVE LEADING EDGE DEVICES NORMALLY<[01] FOUND #8 T/E FLAPP TRANSMISSION TORQUE IND. EXTENDED; RESETEDAND SERVICE
- [SDR SWAA2024070307054](https://openairdocs.org/sdr/SWAA2024070307054.md): Skin · delaminated · Jun 28, 2024 · N8635F · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > FUSELAGE PANEL 191D DELAMINATED AROUND PREVIOUS REPAIR.<[01] REMOVED DAMAGE PER SRM 51-70-05-2R-2.;[02] REPAIRED PANEL PER SRM 51-70-0502R-2.;[03] REQUIRES FINISH TOPCOAT.;[04] 1. DANIEL BATES (TECHNICIAN); 28-JUN-2024 17:56 UTC<BR>REMOVED DAMAGE PER SRM 51-70
- [SDR SWAA2024070306187](https://openairdocs.org/sdr/SWAA2024070306187.md): Battery Pack · inoperative · Jun 27, 2024 · N8635F · Boeing 7378H4 · Emergency Lighting
  > LH OVERWING EMERGENCY EXIT LIGHT INOP<[01] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-6. NO FAULTS NOTED.;[02] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06. NO FAULTS NOTED. INSPECTION C/W.
- [SDR SWAA2024070305929](https://openairdocs.org/sdr/SWAA2024070305929.md): Battery Pack · inoperative · Jun 26, 2024 · N8635F · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ON O/H BIN BULLNOSE INOP AT BS649.<[01] REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK PER AMM 33-51-06. NO FAULTS NOTED.;[02] REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK PER AMM 33-51-06. NO FAULTS NOTED. INSPECTION C/W.
- [SDR SWAA2024070305395](https://openairdocs.org/sdr/SWAA2024070305395.md): Skin · delaminated · Jun 24, 2024 · N8635F · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT OUTBOARD AFT FLAP HAS DELAMINATION ON INBOARD UPPER SKIN AT LOWER CORNER(MARKED).<[01] REMOVED R/H O/B AFT FLAP PER MM 27-51-22.;[02] OK TO INSTALL R/H OUTBOARD AFTFLAP.;[03] REPLACED R/H OUTBOARD AFT FLAP PER MM 27-51-22.;[04] VERIFIED REPLACED R/H OUTB
- [SDR SWAA2024070505011](https://openairdocs.org/sdr/SWAA2024070505011.md): Retainer · cracked · Jun 23, 2024 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > L/H LANDING GEAR CENTER DOOR SEAL RETAINER CRACKED ON AFT END. MARKED SEE ATTACHED IMAGE.<[01] R&R RETAINER ASSEMBLY PER SRM 51-40-02.;[02] INSPECTION C/W
- [SDR SWAA2024070300726](https://openairdocs.org/sdr/SWAA2024070300726.md): Floor Support · cracked · Jun 12, 2024 · N8635F · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CABIN FLOOR SUPPORT INTERCOSTAL CRACKED STA-540 LBL-2-23<[01] REMOVED THE OLD INTERCOASTAL AND LOCATED AND DRILLED A NEW FLOOR SUPPORT INTERCOASTAL PER SRM 51-40-02.;[02] VERIFIED WORK IN CA#1.....REMOVED THE OLD INTERCOASTAL AND LOCATED AND DRILLED A NEW FLO
- [SDR SWAA2024070300727](https://openairdocs.org/sdr/SWAA2024070300727.md): Floorbeam · cracked · Jun 12, 2024 · N8635F · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CABIN FLOOR SUPPORT INTERCOSTAL CRACKED STA-540 RBL-2-23<[01] REMOVED CABIN FLOOR SUPPORT INTERCOSTAL STA.540 RBL 2-23 PER SRM 51-40-02.;[02] REPLACED INTERCOSTAL PER SRM 51-40-02.;[03] 02 - INSPECTED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLAT
- [SDR SWAA2024070300592](https://openairdocs.org/sdr/SWAA2024070300592.md): Vapor Barrier · cracked · Jun 11, 2024 · N8635F · Boeing 7378H4 · Fuselage Main, Bulkhead
  > RH AC BAY VAPOR BARRIER SUPPORT L-ANGLE AT STA 663; RBL 38 CRACKED.<[01] INSTALLED REPAIR PARTS PER SRM 51-40-02 AND EA# 24-157-01738.;[02] INSTALLED REPAIR PARTS PER SRM 51-40-02 AND EA# 24-157-01738 & BOEING DRAWING 111A1000;[03] SEE CARD TTG8Q00TUXKC FOR RH
- [SDR SWAA2024070399821](https://openairdocs.org/sdr/SWAA2024070399821.md): Angle · cracked · Jun 9, 2024 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > POSSIBLE CRACK L ANGLE R/H A/C BAY AFT WALL (STA 663) UPPER INBOARD CORNER.<[01] VERIFIED CRACKS 2EA.; PICTURE ATTACHED;[02] REMOVED CRACKED ANGLE PER SRM 51-10-02.;[03] MATCH DRILLED & DEBURRED ANGLE PER SRM 51-40-02.;[04] INSPECTED WORK IN C/A #3 MATCH DRILL
- [SDR SWAA2024070399837](https://openairdocs.org/sdr/SWAA2024070399837.md): Angle · cracked · Jun 9, 2024 · N8635F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > POSSIBLE CRACK L ANGLE L/H A/C BAY AFT WALL (STA 663) UPPER INBOARD CORNER.<[01] VERIFIED CRACK 1EA.; PICTURE ATTACHED;[02] REMOVED FASTENERS IN VERTICAL LEG OF REPAIR AREA PER SRM 57-10-10-2R-5.;[03] CUT AND REMOVED DAMAGE SECTION OF VAPOR BARRIER ATTACH ANGL

Next page: https://openairdocs.org/deregistered/N8635F-2026-07-16/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 = 'N8635F' AND deregistration_id = 'N8635F-2026-07-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8635F-2026-07-16/reports

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