# Service difficulty reports: N941WN

A list on [N941WN](https://openairdocs.org/aircraft/N941WN.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 · 219 reports

- [SDR SWAA2026101254258](https://openairdocs.org/sdr/SWAA2026101254258.md): Scuff Plate · cracked · Oct 8, 2026 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > R1 DOOR HAD A CRACK IN LWR AFT CORNER SCUFF PLATE. REMOVED AND REPLACED THE R1 DOOR SCUFF PLATE IAW AMM 53-11-01.
- [SDR SWAA2026091162693](https://openairdocs.org/sdr/SWAA2026091162693.md): Battery Pack · discharged · Sep 10, 2026 · N941WN · Boeing 7377H4 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS INOPERATIVE. CHARGED EMERGENCY LIGHT POWER SUPPLY BATTERY PACKS IAW AMM 33-51-06. OPS CHKD GOOD.
- [SDR SWAA2025082908141](https://openairdocs.org/sdr/SWAA2025082908141.md): Battery Pack · inoperative · Aug 26, 2025 · N941WN · Boeing 7377H4 · Emergency Lighting
  > THE EXTERIOR EMERGENCY LIGHT AT THE L2 DOOR IS INOPERATIVE. REMOVED AND REPLACED LT AFT EMERGENCY LIGHTING BATTERY PACK AND POWER SUPPLY ASSEMBLY PER M/M 33-51-06.
- [SDR SWAA2025082607233](https://openairdocs.org/sdr/SWAA2025082607233.md): Bulb · inoperative · Aug 22, 2025 · N941WN · Boeing 7377H4 · Emergency Lighting
  > L2 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED L2 SERVICE DOOR EMERGENCY LIGHT BULB PER AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2025050664317](https://openairdocs.org/sdr/SWAA2025050664317.md): Fitting · worn · Apr 26, 2025 · N941WN · Boeing 7377H4 · Emergency Equipment
  > WEAR ON GIRT BAR FITTINGS ENTRY AND SERVICE DOOR HARDWARE AT FWD GALLEY AREA 2025-244014<[01] REPLACED GIRT BAR FITTINGS ENTRY AND SERVICE DOOR HARDWARE AT FWD GALLEY AREA I.A.W SOPM 20-50-01 REV.38.;[02] CORRECTED STEP 1:<BR>REPLACED GIRT BAR FITTINGS ENTRY A
- [SDR SWAA2025050757107](https://openairdocs.org/sdr/SWAA2025050757107.md): Access Panel · cracked · Apr 19, 2025 · N941WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ON ACCESS PANEL 344GB AT RT HORIZONTAL STAB. REPAIRED ACCESS PANEL 344GB AT RT HORIZONTAL STAB IAW B737-700 SRM 55-20-01-2R-4 REPAIR 4.
- [SDR SWAA2025050757101](https://openairdocs.org/sdr/SWAA2025050757101.md): Support Bracket · cracked · Apr 11, 2025 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO 3R AT PASSENGER CABIN. REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO 3R AT PASSENGER CABIN IAW SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG 146A7901 SHEET 66 REV A.
- [SDR SWAA2025050757090](https://openairdocs.org/sdr/SWAA2025050757090.md): Support Angle · cracked · Apr 10, 2025 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS807 AND BTW STR25R AND STR26R AFT CARGO COMPARTMENT 2025-244196<[01] TOOL USED ON STEP 1. ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] PERFORMED VISUAL INSPECTION ON ANGLE - SUPPORT LOCATED BS80
- [SDR SWAA2025050757093](https://openairdocs.org/sdr/SWAA2025050757093.md): Angle · cracked · Apr 10, 2025 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS867 AND BTW STR26L AND STR27L AFT CARGO COMPARTMENT 2025-244195<[01] REPLACED ANGLE LOCATED BS 867 AND BETWEEN STRINGER 26L AND STRINGER 27L AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND DW
- [SDR SWAA2025050723643](https://openairdocs.org/sdr/SWAA2025050723643.md): Support Angle · cracked · Apr 10, 2025 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - SUPPORT LOCATED BS500D AND STR28R AFT POSITION FWD CARGO COMPARTMENT. REPLACED ANGLE-CLIP LOCATED BS500D AND STR28R AFT POSITION FWD CARGO COMPARTMENT IAW SRM 51-40-02; DWG 143A7902 SHEET: 126 REV: A.
- [SDR SWAA2025050657091](https://openairdocs.org/sdr/SWAA2025050657091.md): Cargo Track · cracked · Apr 10, 2025 · N941WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK ON CARGO TRACK RBBL 13.84 LOCATED BS767 AFT CARGO COMPARTMENT 2025-244197<[01] STEPS 5 AND 6 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 200048001; CAL DUE DATE: 28-MAY-25;[02] TOOL USED ON STEP 10. ET EQUIPMENT: P/N: NORTEC 600D; S/N: 600071
- [SDR SWAA2025050657094](https://openairdocs.org/sdr/SWAA2025050657094.md): Cargo Track · cracked · Apr 10, 2025 · N941WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK ON CARGO TRACK RBBL 13.84 LOCATED BS727E AFT CARGO COMPARTMENT 2025-244198<[01] REPAIR CARGO TRACK RBBL 13.84 LOCATED BETWEEN 727D +14? AND BSTA 767 +10?. AT AFT CARGO COMPARTMENT IS RESOLVED ON [TTG8Q00ZSUYX];[02] CORRECTED ITEM 1.<BR>REPAIR CARGO TRACK
- [SDR SWAA2025050657096](https://openairdocs.org/sdr/SWAA2025050657096.md): Stringer · cracked · Apr 10, 2025 · N941WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK ON STRINGER 23L LOCATED BS540 AT FWD CARGO COMPARTMENT 2025-244235<[01] TOOL USED ON STEP 8:EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220272712; DUE DATE: 28-JAN-26;[02] TOOLS USED TEMPERATURE CONTROLLED P/N: P3015GOES00000; S/N: 112811020; DUE DATE:
- [SDR SWAA2025050657092](https://openairdocs.org/sdr/SWAA2025050657092.md): Support · cracked · Apr 10, 2025 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON CHANNEL SUPPORT LOCATED BS727 RBL7 AREA BULKHEAD AT AFT CARGO COMPARTMENT 2025-244199<[01] REPLACED ON CHANNEL SUPPORT CHANNEL SUPPORT AND FASTENERS LOCATED BS727 RBL7 AREA BULKHEAD AT AFT CARGO COMPARTMENT COMPARTMENT IAW B737-700 SRM 51-40-02-0G; SR
- [SDR SWAA2025050757067](https://openairdocs.org/sdr/SWAA2025050757067.md): Angle · cracked · Apr 9, 2025 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - CLIP LOCATED BS500C AND LBL21 FWD POSITION FWD CARGO COMPARTMENT. REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS500C AND LBL21 FWD POSITION FWD CARGO COMPARTMENT IAW SRM 51-40-02-0G AND DRAWING 143A7505 SHEET 81 REV-.
- [SDR SWAA2025050757080](https://openairdocs.org/sdr/SWAA2025050757080.md): Scuff Plate · cracked · Apr 9, 2025 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT I.A.W. BOEING SRM 53-30-15-2R-1.
- [SDR SWAA2025050757071](https://openairdocs.org/sdr/SWAA2025050757071.md): Gusset · cracked · Apr 9, 2025 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT. REPLACED GUSSET AND FASTENERS LOCATED BS 500D AND STRINGER 19L AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG# 143A7902 SHEET 209 AND REV -.
- [SDR SWAA2025050757072](https://openairdocs.org/sdr/SWAA2025050757072.md): Gusset · cracked · Apr 9, 2025 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT. REPLACED GUSSET AND FASTENERS LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG#143A7902; SHEET:209; REV:-.
- [SDR SWAA2025050757081](https://openairdocs.org/sdr/SWAA2025050757081.md): Door Sill · corroded · Apr 9, 2025 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER SILL DOOR CUT OUT LOCATED BS827 RBL68 AND WL198 AT AFT CARGO COMPARTMENT. REPLACED WEB LOCATED UPPER SILL DOOR CUTOUT BTW BS 827 RBL 68 AND WL 198 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG# 146A8113 SHEET 11; REV -; DWG# 1
- [SDR SWAA2025050841360](https://openairdocs.org/sdr/SWAA2025050841360.md): Seat Track · elongated · Apr 8, 2025 · N941WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION ON SEAT TRACK CAPTAIN AND F/O SIDE AT COCKPIT 2025-244078<[01] REPLACED REAR SEAT TRACK CAPTAIN AND F/O SIDE AT COCKPIT (4EA) IAW B737-700 AMM 25-11-11-200-801 AND AMM 25-11-11-400-801<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED REAR SEAT TRACK C
- [SDR SWAA2025050722727](https://openairdocs.org/sdr/SWAA2025050722727.md): Access Panel · cracked · Apr 8, 2025 · N941WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK BLADE ANGLE ACCESS PANEL 343AB AT RT HORIZONTAL STAB. REPLACED BLADE ACCESS PANEL 343AB AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-01; 51-10-02 PARAGRAPH 9. REPLACED BLADE ACCESS PANEL 343AB AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02; 51-10-02 P
- [SDR SWAA2025050757028](https://openairdocs.org/sdr/SWAA2025050757028.md): Stub Frame · cracked · Apr 7, 2025 · N941WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON STUB FRAME LOCATED BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FWD GALLEY DOOR AREA(1EA). CRACK LENGTH APPROX 0.812 INCH AT PASSENGER CABIN. REPLACED STUB FRAME LOCATED BTW BS 294.5 TO BS 296 AND STRINGER 7R TO STRINGER 11R AT FWD GALLEY DOOR. IAW B7
- [SDR SWAA2025050757042](https://openairdocs.org/sdr/SWAA2025050757042.md): Scuff Plate · cracked · Apr 7, 2025 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDING WITH B737-700 SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4. B; STEPS (2 AND 4 TO 7); FIGURE 203. REFER TO BAC 5975.
- [SDR SWAA2025050722377](https://openairdocs.org/sdr/SWAA2025050722377.md): Floorbeam · cracked · Apr 7, 2025 · N941WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK BRAKE PANEL LOCATED BS540 LBL 1 AT CENTER WING BOX. REPLACED BRAKE PANEL LOCATED BS 540 LBL 1 TO LBL 24 AT CENTER WING BOX. IAW SRM 51-10-02; SRM 51-40-02 AND DWG# 143A5240; SHEET 14 AND REV -.
- [SDR SWAA2025050757032](https://openairdocs.org/sdr/SWAA2025050757032.md): Floorbeam · cracked · Apr 7, 2025 · N941WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK BRAKE PANEL LOCATED BS540 RBL 24.75 AT CENTER WING BOX. REPLACED BRAKE PANEL LOCATED BS540 RBL 24.75 AT CENTER WING BOX IAW N B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG 143A0060 SHEET 46 REV -.
- [SDR SWAA2025050657037](https://openairdocs.org/sdr/SWAA2025050657037.md): Plate · corroded · Apr 7, 2025 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE PLATE LOCATED CARGO DOOR CUTOUT AT AFT CARGO COMPARTMENT 2025-244047<[01] REPLACED FLOOR STRUCTURE PLATE LOCATED CARGO DOOR CUTOUT AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9.;[02] COMPLETED
- [SDR SWAA2025050722204](https://openairdocs.org/sdr/SWAA2025050722204.md): Handle · deteriorated · Apr 6, 2025 · N941WN · Boeing 7377H4 · Passenger/Crew Doors
  > DETERIORATED ASSIST HANDLE AND NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GALLEY AREA (2EA) REPLACED ASSIST HANDLE AND NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GALLEY AREA (2EA) I.A.W B737-700 AMM 52-11-31-400-802 STEP 3.G (2) THE INSTALLATION WILL BE DOC
- [SDR SWAA2025050722201](https://openairdocs.org/sdr/SWAA2025050722201.md): Access Panel · cracked · Apr 6, 2025 · N941WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK AROUND HOLES ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW SRM 51-70-05-2R-6 REPAIR 6.
- [SDR SWAA2025050722023](https://openairdocs.org/sdr/SWAA2025050722023.md): Skin · debonded · Apr 5, 2025 · N941WN · Boeing 7377H4 · Trailing Edge Flaps
  > DEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE PANEL AT LT WING. PERFORMED PERMANENT REPAIR ON I/B MAIN FLAP TRAILING EDGE WEDGE PANEL LOWER SKIN AT LT WING IAW EA# 25-157-01004.
- [SDR SWAA2025050622022](https://openairdocs.org/sdr/SWAA2025050622022.md): Skin · debonded · Apr 5, 2025 · N941WN · Boeing 7377H4 · Trailing Edge Flaps
  > DEBONDED EXTERNAL SKIN OB AFT FLAP IB EDGE AT RT WING. 2025-243970<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26.;[02] TOOL USED STEP 3: ULTRASONIC EQUIPMENT; P/N: BONDMASTER 600M; S/N: 230106912; DUE DATE: 05 FEB 2026.;[03] TOOL US
- [SDR SWAA2025050657012](https://openairdocs.org/sdr/SWAA2025050657012.md): Vapor Barrier · cracked · Apr 5, 2025 · N941WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK ON VAPOR BARRIER LOCATED BS 663 LBL 35 APROX AT MAIN WHEEL WELL COMPARTMENT 2025-243959<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: B20189571; DUE DATE: 06-JUN-25.;[02] TOOL USED. HOT BONDER P/N HCS9200B-AV; S/N 18185781; DUE DATE 22-FEB-26.;[03] TOOL
- [SDR SWAA2025050657008](https://openairdocs.org/sdr/SWAA2025050657008.md): Glowstrip · deteriorated · Apr 5, 2025 · N941WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) 2025-243963<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) IAW B737-700 AMM 33-51-15-400-802 AND DWG 33500007 SHEET 2 REV. 2;[02] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (
- [SDR SWAA2025050757002](https://openairdocs.org/sdr/SWAA2025050757002.md): Skin · cracked · Apr 4, 2025 · N941WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK LOWER SURFACE OF THE LEADING EDGE NOSE SKIN AT ACTUATOR RIB LOC. SLAT 4 LOWER SURFACE AT LT WING. INSTALLED PERMANENT REPAIR PARTS [1] DOUBLER; [2] FILLER AND FASTENERS LOCATED LEADING EDGE NOSE SKIN LOWER SURFACE SLAT 4 AT LT WING IAW SRM 57-42-01-2R
- [SDR SWAA2025031705581](https://openairdocs.org/sdr/SWAA2025031705581.md): Bonding Jumper · loose · Mar 14, 2025 · N941WN · Boeing 7377H4 · Emergency Equipment
  > L2 DOOR ESCAPE SLIDE PACK COVER BONDING JUMPER NOT SECURED <[01]. REATTACHED THE BONDING JUMPER IN PLACE PER MT 725-61-06.
- [SDR SWAA2025013191792](https://openairdocs.org/sdr/SWAA2025013191792.md): Sign · broken · Jan 31, 2025 · N941WN · Boeing 7377H4 · Emergency Lighting
  > CEILING EMERGENCY EXIT SIGN LOCATED BETWEEN OVERWING EMERGENCY EXIT HAS A BROKEN ATTACHMENT.<[01] R&R CEILING MERGENCY EXIT SIGHN LIGHT ASSY LOCATED BETWEEN OVERWING EXITS PER AMM 33-51-01 OP CHECK OK.
- [SDR SWAA2024122079319](https://openairdocs.org/sdr/SWAA2024122079319.md): Bracket · cracked · Dec 19, 2024 · N941WN · Boeing 7377H4 · Fuselage Main, Keel
  > LEFT WHEEL WELL; BRACKET CRACKED ABOVE #1 AFT FUEL BOOST PUMP<[01] REMOVED AND REPLACED LEFT WHEEL WELL BRACKET ABOVE #1 AFT FUEL BOOST PUMP IN REF SRM 51-40-02 AND SRM 51-10-02.
- [SDR SWAA2024121979326](https://openairdocs.org/sdr/SWAA2024121979326.md): Battery Pack · failed · Dec 19, 2024 · N941WN · Boeing 7377H4 · Emergency Lighting
  > M1673 AND M1672 FAILED CAPACITY CHECK<[01] R/R M1673 AND M1672 BATTERY PACKS PER AMM 33-51-06
- [SDR SWAA2024121979322](https://openairdocs.org/sdr/SWAA2024121979322.md): Battery Pack · failed · Dec 19, 2024 · N941WN · Boeing 7377H4 · Emergency Lighting
  > M1668 AND M1669 FAILED CAPACITY CHECK<[01] R/R M1668 AND M1669 BATTERY PACKS PER AMM 33-51-06
- [SDR SWAA2024121979321](https://openairdocs.org/sdr/SWAA2024121979321.md): Battery Pack · failed · Dec 19, 2024 · N941WN · Boeing 7377H4 · Emergency Lighting
  > M1675 AND M1674 FAILED CAPACITY CHECK<[01] R/R M1675 AND M1674 BATTERY PACKS PER AMM 33-51-06
- [SDR SWAA2024121979336](https://openairdocs.org/sdr/SWAA2024121979336.md): Fitting · loose · Dec 19, 2024 · N941WN · Boeing 7377H4 · Galley Doors
  > FWD SERVICE DOOR INTERNAL DOOR HANDLE ATTACH FITTING LOOSE.<[01] TIGHTENED R1 DOOR INTERNAL DOOR HANDLE ATTACH FITTING PER AMM 52-41-11.
- [SDR SWAA2024120273023](https://openairdocs.org/sdr/SWAA2024120273023.md): Lamp · inoperative · Dec 1, 2024 · N941WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT @ RH ROW #6 INOP<[01] REMOVED AND REPLACED EMERGENCY EXIT AREA LIGHT LAMP AT ROW #6. OPS CHECK GOOD. ALL WORK PERFORMED PER AMM 33-51-03.
- [SDR SWAA2024042979791](https://openairdocs.org/sdr/SWAA2024042979791.md): Cowling · cracked · Apr 27, 2024 · N941WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > #1 ENGINE INBOARD FAN COWL CRACKED<[01] R/R FAN COWL PER AMM 71-11-02
- [SDR SWAA2024032868095](https://openairdocs.org/sdr/SWAA2024032868095.md): Web · cracked · Mar 27, 2024 · N941WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > LH ENGINE; INBOARD FAN COWL WEB AFT OF THE OIL SERVICE DOOR CRACKED. LH ENGINE INBOARD FAN COWL WEB AFT OF THE OIL SERVICE DOOR CRACKED.<[01] CRACK MEASURES 1 INCH. ENGINEERING NOTIFIED.;[02] ACCOMPLISHED EA 24-154-00815;[03] ACCOMPLISHED EA 24-154-00815
- [SDR SWAA2024010336970](https://openairdocs.org/sdr/SWAA2024010336970.md): Light · out of adjust · Jan 2, 2024 · N941WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING EXIT EMERGENCY LIGHT OUT<[01] RELAMPED RIGHT OVERWING EXIT EMERGENCY LIGHT PER AMM 33-51-04; OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2023121430700](https://openairdocs.org/sdr/SWAA2023121430700.md): Cover · wrong part · Dec 12, 2023 · N941WN · Boeing 7377H4 · Emergency Lighting
  > L1 DOOR LOWER EMERGENCY EXIT SIGN MISSING DIRECTIONAL ARROW.<[01] REMOVED AND REPLACED COVER IAW AMM 33-51-01
- [SDR SWAA2023061357260](https://openairdocs.org/sdr/SWAA2023061357260.md): Strip · loose · Jun 8, 2023 · N941WN · Boeing 7377H4 · Emergency Lighting
  > E PATH LIGHT STRIP LOOSE AT L/H AFT WINDSCREEN<[01] ATTACHED CORRECTLY EMERGENCY PATH LIGHT STRIP AT L/H AFT WINDSCREEN IAW B737-700 AMM 33-51-15-400-802.;[02] VERIFIED STEP 1
- [SDR SWAA2023061357253](https://openairdocs.org/sdr/SWAA2023061357253.md): Light · inoperative · Jun 8, 2023 · N941WN · Boeing 7377H4 · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT INOP<[01] REPLACED EMERGENCY LIGHT; BATTERY PACK ON TTG8Q00LHS71 PER REF. AMM 33-51-06-960-805. PERFORMED OPERATIONAL TEST FOUND NORMAL.;[02] VERIFIED STEP 1.
- [SDR SWAA2023061358610](https://openairdocs.org/sdr/SWAA2023061358610.md): Battery Pack · inoperative · Jun 8, 2023 · N941WN · Boeing 7377H4 · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT INOP<[01] REPLACED EMERGENCY LIGHT; BATTERY PACK ON TTG8Q00LHS71 PER REF. AMM 33-51-06-960-805. PERFORMED OPERATIONAL TEST FOUND NORMAL.;[02] VERIFIED STEP 1.
- [SDR SWAA2023061357254](https://openairdocs.org/sdr/SWAA2023061357254.md): Lens · loose · Jun 8, 2023 · N941WN · Boeing 7377H4 · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT LENS LOOSE IN HOUSING<[01] RESECURED L1 EXTERIOR DOOR EMERGENCY LIGHT LENS IN REF WITH B737 AMM 33-51-04-960-801;[02] VERIFIED STEP 1.
- [SDR SWAA2023061357259](https://openairdocs.org/sdr/SWAA2023061357259.md): Light · inoperative · Jun 8, 2023 · N941WN · Boeing 7377H4 · Emergency Lighting
  > ROW 1 AND 4 EMERGENCY LIGHTS INTERMITTENTLY INOP<[01] REPLACED EMERGENCY LIGHT; BATTERY PACK PER REF. AMM 33-51-06-960-805. PERFORMED OPERATIONAL TEST FOUND NORMAL.;[02] VERIFIED BATTERY PACK REPLACEMENT; OPS CHECK NORMAL.

Next page: https://openairdocs.org/aircraft/N941WN/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 = 'N941WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N941WN/reports

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