# Service difficulty reports: N268WN

A list on [N268WN](https://openairdocs.org/aircraft/N268WN.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 6 · 262 reports

- [SDR SWAA2026092274966](https://openairdocs.org/sdr/SWAA2026092274966.md): Cover · missing · Sep 18, 2026 · N268WN · Boeing 7377H4 · Emergency Lighting
  > AISLE OVERHEAD EXIT SIGN MISSING FORWARD FACING COVER. REPLACED AISLE FRONT FACING OVERHEAD EXIT SIGN COVER REF AMM 33-51-01-960-802. OPS CHECKS NORMAL.
- [SDR SWAA2026090870845](https://openairdocs.org/sdr/SWAA2026090870845.md): Cover · missing · Sep 3, 2026 · N268WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT ROW 14 & 15 A,B & C, COVER MISSING. INSTALLED MISSING COVER IAW AMM 33-51-03.
- [SDR SWAA2026081423387](https://openairdocs.org/sdr/SWAA2026081423387.md): Lens · detached · Aug 10, 2026 · N268WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN OVERHEAD IN CABIN FELL DOWN REINSTALLED LENS COVER REF AMM 33-51-00.
- [SDR SWAA2026080575007](https://openairdocs.org/sdr/SWAA2026080575007.md): Floor Panel · cracked · Aug 1, 2026 · N268WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL CRACKED (6, 5.5 2 SPOT) BS 500. PERFORMED A PATCH REPAIR IAW AMM 25-52-01. NO OTHER LINER AND PANEL DAMAGE NOTED.
- [SDR SWAA2026060208207](https://openairdocs.org/sdr/SWAA2026060208207.md): Floor Panel · split · May 31, 2026 · N268WN · Boeing 7377H4 · Fuselage Floor Panel
  > RAMP REPORTS AFT CARGO PIT FIBERGLASS FLOOR SPLIT. SPLIT IS IN FIBERGLASS FLOOR FROM STATION 751-768. OK TO CONT PER MEL 25-16-01. REMOVED AND REPLACED AFT CARGO FLOOR PANEL PER AMM 25-52-10.
- [SDR SWAA2026022372823](https://openairdocs.org/sdr/SWAA2026022372823.md): Cover · loose · Feb 21, 2026 · N268WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT COVER ON F/O SIDE OVERWING EXIT FELL OFF DURING FLIGHT. SECURED EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-01.
- [SDR SWAA2025082909134](https://openairdocs.org/sdr/SWAA2025082909134.md): Light · loose · Aug 28, 2025 · N268WN · Boeing 7377H4 · Emergency Lighting
  > RH PHOTO LUMINESCENT STRIP LOOSE AT FWD GALLEY MAT. SECURED RT PHOTOLUMINESCENT STRIP AT FWD GALLEY BALL MAT IN REF TO AMM 33-51-15.
- [SDR SWAA2025080697913](https://openairdocs.org/sdr/SWAA2025080697913.md): Battery Pack · inoperative · Aug 3, 2025 · N268WN · Boeing 7377H4 · Emergency Lighting
  > FOUND FRONT LEFT EMERGENCY LIGHTS OUT. R & R FWD LT BATTERY PACK PER AMM 33-51-06 OPS GOOD.
- [SDR SWAA2025070186477](https://openairdocs.org/sdr/SWAA2025070186477.md): Fairing · damaged · Jun 28, 2025 · N268WN · Boeing 7377H4 · Aerodynamic Fairings
  > STRUT 4 FAIRING HAS AN ENLARGED MOUNT HOLE ON TOP AFT SIDE<[01] C/W 25-172-01732
- [SDR SWAA2024103054003](https://openairdocs.org/sdr/SWAA2024103054003.md): Connector · damaged · Oct 27, 2024 · N268WN · Boeing 7377H4 · Light System Wiring
  > INOP EMERGENCY EXIT LIGHT ON CEILING PANEL AT FWD GALLEY AREA 2024-593383<[01] CONNECTED CORRECTLY ELECTRICAL CONNECTOR D3160 OF THE EMERGENCY LIGHT ON CEILING PANEL AT FORWARD GALLEY AREA IAW B737-700 WDM 33-51-12-2 AND PERFORMED EMERGENCY LIGHTS OPERATIONAL
- [SDR SWAA2024103045313](https://openairdocs.org/sdr/SWAA2024103045313.md): Web · cracked · Oct 5, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON LOWER SILL WEB LOCATED BS 294.5 AT LEVEL STR 17R FWD GALLEY AREA 2024-593316<[01] REPLACED LOWER SILL WEB (1EA) LOCATED BTW BS 291.5 TO BS 332.1 AT LEVEL STR 17R FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET: 25 REV: DWG 140A9810 SH
- [SDR SWAA2024103042819](https://openairdocs.org/sdr/SWAA2024103042819.md): Support Angle · cracked · Sep 28, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK BODY FAIRING SUPPORT T ANGLE LOCATED BS500D; BETWEEN STRINGER 18R AND STRINGER 19R AT LOWER FUSELAGE 2024-593247<[01] REPLACED SUPPORT T ANGLE LOCATED AT BS500D; BETWEEN STRINGER 18R AND STRINGER 19R AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND DWG 14
- [SDR SWAA2024103042817](https://openairdocs.org/sdr/SWAA2024103042817.md): Support Bracket · cracked · Sep 27, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO 3R AT PASSENGER CABIN 2024-593237<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO 3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 146A7901 SHEET 66 REV A.;[02] REPLACED SUPPORT BRACKET LO
- [SDR SWAA2024103041983](https://openairdocs.org/sdr/SWAA2024103041983.md): Lens · broken · Sep 26, 2024 · N268WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN LENS EMERGENCY EXIT ON LAVATORY A AT FWD GALLEY AREA 2024-593195<[01] REPLACED LENS EMERGENCY EXIT ON LAVATORY A AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3. C. (6) (A) THRU 3. C. (6) (E);[02] REPLACED LENS EMERGENCY EXIT ON LAVATORY A A
- [SDR SWAA2024103041726](https://openairdocs.org/sdr/SWAA2024103041726.md): Angle · cracked · Sep 25, 2024 · N268WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED ORSS 269 AT LT WING 2024-593185<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 269 AT LT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 SRM 51-40-02 AND DRAWING 115A2930 SHEET 7 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFI
- [SDR SWAA2024103041725](https://openairdocs.org/sdr/SWAA2024103041725.md): Angle · cracked · Sep 25, 2024 · N268WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED ORSS 269 AT RT WING 2024-593183<[01] REPLACED ANGLE AND FASTENERS TRAILING EDGE LOCATED ORSS 269 AT RT WING IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9;DWG 115A2930 SHEET 8 REV-;;[02] REPLACED ANGLE AND FASTENERS TRAILING ED
- [SDR SWAA2024103041527](https://openairdocs.org/sdr/SWAA2024103041527.md): Skin · cracked · Sep 25, 2024 · N268WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 RIB AND 8 INCH. FROM REAR SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. 2024-593167<[01] TOOL USED IN STEP 5: EDDY CURRENT EQUIPMENT P/N: NORTEC 600
- [SDR SWAA2024103041229](https://openairdocs.org/sdr/SWAA2024103041229.md): Web · cracked · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA 2024-593135<[01] REPLACED WEB LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV ?<BR>SEE INDIVIDUAL SING OFF BELOW;[02] REPLACED
- [SDR SWAA2024103041519](https://openairdocs.org/sdr/SWAA2024103041519.md): Angle · cracked · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE AFT POSITION LOCATED BTW STA 907 TO STA 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT 2024-593151<[01] REPLACED ANGLE LOCATED AFT POSITION BTW STA 907 TO STA 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-0
- [SDR SWAA2024103041230](https://openairdocs.org/sdr/SWAA2024103041230.md): Web · cracked · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA 2024-593132<[01] REPLACED WEB LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV ?<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACE
- [SDR SWAA2024103041226](https://openairdocs.org/sdr/SWAA2024103041226.md): Plate · corroded · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON PLATE LOCATED BS 1006 PLUS 23 INCHES RBL 3 WL 208.1 AT AFT GALLEY AREA 2024-593121<[01] TOOL USED CALIPER P/N: 500-752-20; S/N:B12037208; DUE DATE: 17-APR-25.;[02] REPLACED PLATE AND FASTENERS LOCATED BS 1006 TO BS 1040 RBL 3 WL 208.1 AT AFT GALLE
- [SDR SWAA2024103041512](https://openairdocs.org/sdr/SWAA2024103041512.md): Fitting · corroded · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION INNER CHORD LOCATED BTW BS 303.9 TO BS 328 LBL 54 WL 208.1 AT FWD GALLEY AREA 2024-593138<[01] TOOL USED ULTRASONIC EQUIPMENT PN: 45MG SN 130061901; DUE DATE. 12-JUN-25;[02] REPLACED INNER CHORD AND FASTENERS LOCATED BTW BS 303.9 TO BS 360 LBL 54 WL
- [SDR SWAA2024103041520](https://openairdocs.org/sdr/SWAA2024103041520.md): Frame · cracked · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-593152<[01] TRIM OUT BS 312 FRAME UPPER CHORD AT LBL 33 BETWEEN S-5L AND S-6L IAW EA# M-22-153-01244 [TTG8Q00W585E] SEE INDIVIDUAL SIGN OFF BELOW.;[02] TRIM OUT BS 312 FRAME UPPER CHORD
- [SDR SWAA2024103041522](https://openairdocs.org/sdr/SWAA2024103041522.md): Angle · cracked · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED FWD FACE BS 294.5 AT LEVEL STR 13L AT FWD GALLEY 2024-593153<[01] REPLACED ANGLE LOCATED ON FWD FACE BS 294.5 AT LEVEL STR 13L AT FWD GALLEY IAW B737-700 SRM 51-10-02 51-40-02 AND DRAWING 141A1311 SHEET 1 REV C MATERIAL USED BAC 1489-360
- [SDR SWAA2024103041513](https://openairdocs.org/sdr/SWAA2024103041513.md): Support Angle · cracked · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 AT PASSENGER CABIN 2024-593140<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 13 AT PASSENGER CABIN. I.A.W. B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #
- [SDR SWAA2024103041515](https://openairdocs.org/sdr/SWAA2024103041515.md): Support Angle · cracked · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN 2024-593142<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN. I.A.W. B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #
- [SDR SWAA2024103041516](https://openairdocs.org/sdr/SWAA2024103041516.md): Support Angle · cracked · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN 2024-593144<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN. I.A.W. B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #
- [SDR SWAA2024103041517](https://openairdocs.org/sdr/SWAA2024103041517.md): Plate · corroded · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON PLATE LOCATED BS 312 LBL 54 WL 208.1 AT FWD GALLEY AREA 2024-593146<[01] REPLACED PLATE LOCATED BS312 LBL54 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 DUE NOT FOUND AN ALLOWABLE DAMAGE APPLICABLE TO THIS PART IN B737-700 SRM 53-30-51-1A
- [SDR SWAA2024103041526](https://openairdocs.org/sdr/SWAA2024103041526.md): Skin · cracked · Sep 24, 2024 · N268WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 RIB AND 8 INCH. FROM REAR SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. 2024-593165<[01] STEP 5 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S
- [SDR SWAA2024103041514](https://openairdocs.org/sdr/SWAA2024103041514.md): Support · cracked · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ZEE LOCATED BTW STA 727D TO STA 727E AT LEVEL STR 25R AT AFT CARGO COMPARTMENT 2024-593141<[01] REPLACED SUPPORT ZEE SECTION;AND FASTENERS LOCATED ON BS 727B PLUS 10 INCH AND BS 767 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40
- [SDR SWAA2024103041511](https://openairdocs.org/sdr/SWAA2024103041511.md): Stub Frame · cracked · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON STUB FRAME LOCATED 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-593136<[01] STEPS 6 AND 7 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210138503; CAL DUE DATE: 05-AUG-25;[02] PERFORMED PERMANENT REPAIR ON STUB FRAME LOCATED 294.5 AT LEVEL
- [SDR SWAA2024103041521](https://openairdocs.org/sdr/SWAA2024103041521.md): Stringer · cracked · Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK ON STRINGER 16L LOCATED BTW BS 294.5 TO BS 303.9 AT FWD GALLEY AREA 2024-593150<[01] ON STEP 3; TOOL USED ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130064101; DUE DATE: 13/DEC/24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631
- [SDR SWAA2024103040716](https://openairdocs.org/sdr/SWAA2024103040716.md): Web · cracked · Sep 23, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT WEB LOCATED BTW STA 847 TO STR 867 AT LEVEL LBL 24.82 CEILING AREA AT AFT CARGO COMPARTMENT 2024-593041<[01] REPLACED SUPPORT WEB AND FASTENERS LOCATED BTW STA 847 TO STA 867 AT LEVEL LBL 24.82 CEILING AREA AT AFT CARGO COMPARTMENT IAW B737-700 S
- [SDR SWAA2024103040953](https://openairdocs.org/sdr/SWAA2024103040953.md): Connector · broken · Sep 23, 2024 · N268WN · Boeing 7377H4 · Equipment/Furnishings Wiring
  > BROKEN CONNECTOR OF THE OVERWING SCAPE LOCATED BTW STA 747 TO STA 767 AND BTW STR 21L TO STR 22L AT AFT CARGO COMPARTMENT 2024-593054<[01] REPLACED CONNECTOR OF THE OVERWING SCAPE LOCATED BTW STA 747 TO STA 767 AND BTW STR 21L TO STR 22L AT AFT CARGO COMPARTME
- [SDR SWAA2024103040962](https://openairdocs.org/sdr/SWAA2024103040962.md): Web · cracked · Sep 23, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA 2024-593092<[01] REPLACED WEB LOCATED BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 32 REV ?<BR>SEE INDIVIDUAL SING OFF BELOW;[02] CER
- [SDR SWAA2024103040721](https://openairdocs.org/sdr/SWAA2024103040721.md): Angle · cracked · Sep 23, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED STA 927 AT LEVEL STR 18R AT AFT CARGO COMPARTMENT 2024-593042<[01] REPAIRED ANGLE LOCATED BTW STA 900 TO STA 927 AT LEVEL STR 18R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-70-11-2R-0 FIG 201;SHEET 2.SEE INDIVIDUAL SIGN OFF BELOW;[02] CE
- [SDR SWAA2024103040954](https://openairdocs.org/sdr/SWAA2024103040954.md): Floorbeam · corroded · Sep 23, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION LOCATED ON FLOOR BEAM 986.5 RBL 42 WL 208.1 AT AFT GALLEY AREA 2024-593056<[01] PERFORMED PERMANENT REPAIR CAT A LOCATED ON FLOOR BEAM 986.5; LBL13 TO RBL50 WL 208.1 AT AFT GALLEY AREA. I.A.W. B737-700 SRM 53-70-51-2R-4 REPAIR 4 AND 24-153-02746-WIP2
- [SDR SWAA2024103040955](https://openairdocs.org/sdr/SWAA2024103040955.md): Floorbeam · corroded · Sep 23, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION LOCATED ON FLOOR BEAM 986.5 LBL 42 WL 208.1 AT AFT GALLEY AREA 2024_593057<[01] ET TOOL USED PN: MIZ-21C; SN:769680; DUE DATE: 28-AUG-25;[02] TOOL USED ON STEP 12:ET EQUIPMENT; P/N: NORTEC 600D; S/N:210138003; DUE DATE: 11/JUN/25;[03] PERFORMED PERMA
- [SDR SWAA2024103040189](https://openairdocs.org/sdr/SWAA2024103040189.md): Scuff Plate · cracked · Sep 22, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2024-592934<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30;S/N:B23272676;DUE DATE:17-MAR-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N:1998072; DUE DATE: 23/JAN/25;[03] REPAIRED BY WELDI
- [SDR SWAA2024103040179](https://openairdocs.org/sdr/SWAA2024103040179.md): Strip · cracked · Sep 21, 2024 · N268WN · Boeing 7377H4 · Emergency Lighting
  > CRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE CENTER SECTION (8 EA) 2024-592911<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE CENTER SECTION (8 EA) IAW B737-700 AMM-33-51-15-400-802;[02] REPLACED STRIP PHOTOLUMINESCENT F
- [SDR SWAA2024103040180](https://openairdocs.org/sdr/SWAA2024103040180.md): Light · cracked · Sep 21, 2024 · N268WN · Boeing 7377H4 · Emergency Lighting
  > CRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE CENTER SECTION (8 EA) 2024-592912<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE CENTER SECTION (8 EA) IAW B737-700 AMM-33-51-15-400-802-NG;[02] REPLACED STRIP PHOTOLUMINESCEN
- [SDR SWAA2024103040169](https://openairdocs.org/sdr/SWAA2024103040169.md): Panel · debonded · Sep 21, 2024 · N268WN · Boeing 7377H4 · Trailing Edge Flaps
  > CUSTOMER REQUEST - DEBONDED IB MAIN FLAP TRAILING EDGE WEDGE PANEL AT RH WING LOWER SURFACE 2024-592880<[01] TOOL USED CALIPER PN: 500-196-30; SN: A193117217; DUE DATE: 16/MAY/25.;[02] TOOL USED ON ITEM 2: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 650; S/N: 2010361
- [SDR SWAA2024103039504](https://openairdocs.org/sdr/SWAA2024103039504.md): Skin · cracked · Sep 19, 2024 · N268WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK SLAT 2 LOWER SKIN AROUND THE FASTENER THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 322.71 AT LT WING 2024-592769<[01] TOOL USED ON STEP 3: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 09-JAN-25.;[02] REPLACED L/E SLAT 2 LT WING
- [SDR SWAA2024103039505](https://openairdocs.org/sdr/SWAA2024103039505.md): Vapor Barrier · cracked · Sep 19, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CUSTOMER REQUEST CRACK VAPOR BARRIER LH SIDE BS663 AT MAIN WHEEL WELL COMPARTMENTS 2024-592759<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: B20189443; DUE DATE: 06-MAR-25;[02] TOOL USED SCALE P/N SPX222 S/N C410738991 DUE DATE 05/AUG/25;[03] HOT BONDER P/N: HC
- [SDR SWAA2024103039503](https://openairdocs.org/sdr/SWAA2024103039503.md): Vapor Barrier · cracked · Sep 19, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CUSTOMER REQUEST CRACK VAPOR BARRIER RH SIDE BS663 AT MAIN WHEEL WELL COMPARTMENT 2024-592758<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: A18229508; DUE DATE: 14-JAN-25.;[02] TOOL USED: HOTBONDER: P/N:HCS9200B-AV S/N:18196126 DUE DATE:03-APR-25;[03] TOOL USED
- [SDR SWAA2024060397128](https://openairdocs.org/sdr/SWAA2024060397128.md): Tire · blown · May 31, 2024 · N268WN · Boeing 7377H4 · Tire
  > #2 MLG TIRE BLEW ON TAXI IN<[01] REMOVED AND REPLACED #1 AND #2 MAIN TIRE AND WHEEL ASSY?S PER AMM 34-45-11
- [SDR SWAA2024060397804](https://openairdocs.org/sdr/SWAA2024060397804.md): Tire · blown · May 31, 2024 · N268WN · Boeing 7377H4 · Tire
  > #2 MLG TIRE BLEW ON TAXI IN<[01] REMOVED AND REPLACED #1 AND #2 MAIN TIRE AND WHEEL ASSY?S PER AMM 34-45-11
- [SDR SWAA2024020247465](https://openairdocs.org/sdr/SWAA2024020247465.md): Wire · broken · Feb 1, 2024 · N268WN · Boeing 7377H4 · Light System Wiring
  > LOWER LEFT EMERGENCY LIGHT ON FWD LAV INOP<[01] FOUND BROKEN WIRE ON FOR EMERGENCY LIGHT ASSY. REPAIRED WIRE IAW SWPM 20-30-12. OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2024013046004](https://openairdocs.org/sdr/SWAA2024013046004.md): Cover · detached · Jan 28, 2024 · N268WN · Boeing 7377H4 · Emergency Lighting
  > OVER WING EXIT SIGN COVER KNOCKED OFF FWD SIDE<[01] RESECURED EMERGENCY EXIT SIGN COVER AS REQUIRED PER SIP
- [SDR SWAA2023110919384](https://openairdocs.org/sdr/SWAA2023110919384.md): Battery Pack · failed · Nov 8, 2023 · N268WN · Boeing 7377H4 · Emergency Lighting
  > EMX BATT PACK M01670 FAILS CAPACITANCE CHECK / [01] REMOVED AND REPLACED EMX BATT PACK M01670 PER AMM 33-51-06

Next page: https://openairdocs.org/aircraft/N268WN/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 = 'N268WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N268WN/reports

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