# Service difficulty reports: N214WN
A list on [N214WN](https://openairdocs.org/aircraft/N214WN.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 7 · 305 reports
- [SDR SWAA2026082509906](https://openairdocs.org/sdr/SWAA2026082509906.md): Lamp · inoperative · Aug 21, 2026 · N214WN · Boeing 7377H4 · Emergency Lighting
> EXTERIOR EMERGENCY LIGHT ON WING EXIT DOOR RIGHT SIDE WILL NOT ILLUMINATE. R & R THE LAMP ON EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04.
- [SDR SWAA2026081478569](https://openairdocs.org/sdr/SWAA2026081478569.md): Scuff Plate · peeling · Aug 10, 2026 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> FWD CARGO DOOR CENTER SCUFF PLATE. MEL_WORKING WITH ENGINEERING, R & R FWD CARGO CENTER SCUFF PLATE IAW AMM 53-11-02.
- [SDR SWAA2026080372800](https://openairdocs.org/sdr/SWAA2026080372800.md): Bracket · loose · Jul 31, 2026 · N214WN · Boeing 7377H4 · Emergency Equipment
> FORWARD ENTRY DOOR GIRT BAR BRACKET LOOSE. SECURED THE FWD ENTRY DOOR SLIDE GIRT BAR RETAINER CLIPS IAW AMM 25-66-01.
- [SDR SWAA2026073134647](https://openairdocs.org/sdr/SWAA2026073134647.md): Strut · cracked · Jul 27, 2026 · N214WN · Boeing 7377H4 · Turbine Section
> LPT REAR FRAME HAD 2 ADDITIONAL CRACKS FOUND TOTALING 5 WHEN PERFORMING 7256-I-11716-NG. FRAME ASSEMBLY, TURBINE REAR FRAME MOUNT STRUT INSPECTION) [TTG8Q01BASK1] KNOWN FAULTS: NR 2 ENGINE TRF STRUT NR 1 AT LOCATION C1 HAS A CRACK MEASURING.200 LONG. TTG8Q01B
- [SDR SWAA2026073160152](https://openairdocs.org/sdr/SWAA2026073160152.md): Strut · cracked · Jul 27, 2026 · N214WN · Boeing 7377H4 · Turbine Section
> NR 2 ENG, LPT REAR FRAME, TRF STRUT NR 15 LOCATION C2 LARGEST CUMULATIVE CRACK LENGTH OF 0.170 INCH. TRANSFERRED TO [TTG8Q01DDT54] FOR M-21-172-00810 [TTG8Q01DDSQ9] 1300 REINSPECTION INTERVAL.
- [SDR SWAA2026043093586](https://openairdocs.org/sdr/SWAA2026043093586.md): Rivet · loose · Apr 27, 2026 · N214WN · Boeing 7377H4 · Emergency Equipment
> GIRT BAR LOOSE ON AFT ENTRY DOOR SLIDE. REPLACED GIRT BAR RIVET PER SIP.
- [SDR SWAA2026022372610](https://openairdocs.org/sdr/SWAA2026022372610.md): Lens · detached · Feb 19, 2026 · N214WN · Boeing 7377H4 · Emergency Lighting
> OVERHEAD EXIT SIGN MID CABIN FELL OFF. SECURED OVERHEAD EXIT SIGN LENS IAW AMM INTRO SIP.
- [SDR SWAA2025103130085](https://openairdocs.org/sdr/SWAA2025103130085.md): Girt Bar · out of adjust · Oct 30, 2025 · N214WN · Boeing 7377H4 · Emergency Equipment
> AFT R2 DOOR SLIDE GIRT HANGING DOWN EXCESSIVELY. AFT SIDE HOOK AND LOOP STRIP EXPOSED. SECURED AFT R2 DOOR EMERGENCY SLIDE GIRT IN REF TO SIP.
- [SDR SWAA2025100620872](https://openairdocs.org/sdr/SWAA2025100620872.md): Cover · detached · Oct 3, 2025 · N214WN · Boeing 7377H4 · Emergency Lighting
> MID CABIN EXIT SIGN COVER FELL DOWN. SECURED EXIT SIGN COVER IAW SIP.
- [SDR SWAA2025063085513](https://openairdocs.org/sdr/SWAA2025063085513.md): Seal · cracked · Jun 26, 2025 · N214WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
> RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDER SEAL CRACKED. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER UPPER SLIDER SEAL IAW AMM 53-31-31
- [SDR SWAA2025042226087](https://openairdocs.org/sdr/SWAA2025042226087.md): Lamp · inoperative · Apr 18, 2025 · N214WN · Boeing 7377H4 · Emergency Lighting
> L2 EXTERIOR EMERGENCY LIGHT INOP<[01] REPLACED L2 EXTERIOR EMERGENCY LAMP REF AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2025021094181](https://openairdocs.org/sdr/SWAA2025021094181.md): Bulb · burned out · Feb 8, 2025 · N214WN · Boeing 7377H4 · Emergency Lighting
> BURNED ENTRY DOOR EMERGENCY LIGHT BULB ON EXTERIOR FUSELAGE AT AFT GALLEY AREA 2024-780560<[01] REPLACED ENTRY DOOR EMERGENCY LIGHT BULB ON EXTERIOR FUSELAGE AT AFT GALLEY AREA IAW B737-700 AMM 33-51-04-960-801.;[02] TASK CARD COMPLETED
REPLACED ENTRY DOOR
- [SDR SWAA2025021093069](https://openairdocs.org/sdr/SWAA2025021093069.md): Light · detached · Feb 5, 2025 · N214WN · Boeing 7377H4 · Emergency Lighting
> MISSING EMERGENCY EXIT LIGHT (2EA) FOUND DISCONNECTED AND REMOVED FROM EYE END TERMINALS BY UNDOCUMENTED MAINTENANCE ON ROW 12ABC AND 9ABC AT PASSENGER CABIN 2024-780549<[01] REMOVED AND RE-INSTALLED EMERGENCY Ï¿½REA LIGHT ROW 12ABC AND 9ABC LIGHT ASSEMBLY AT
- [SDR SWAA2025021092660](https://openairdocs.org/sdr/SWAA2025021092660.md): Plate · cracked · Feb 3, 2025 · N214WN · Boeing 7377H4 · Wing Main, Frame Structure
> CRACK CORRUGATED PLATE AT OFS 353 BTW SPOILER 3 AND 4 LT WING 2024-780547<[01] REPLACED CURRUGATED PLATE LOC OFS 353 BTW SPOILER 3 AND 4 LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 STEP 9. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED
SEE IND
- [SDR SWAA2025021086354](https://openairdocs.org/sdr/SWAA2025021086354.md): Beam · cracked · Jan 15, 2025 · N214WN · Boeing 7377H4 · Fuselage Main, Floor Beam
> CRACK INDICATION FOUND LOC. STA 663.75 LBL 45.5 I/B SIDE LOWER CHORD LONGITUDINAL BEAM AT 10 OCLOCK. 2024-780492 <[01]. TOOL USED ON STEP 2. ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25; [02] ON STEP 4: TOOL USED EDDY CURRENT EQUIP
- [SDR SWAA2025021089099](https://openairdocs.org/sdr/SWAA2025021089099.md): Support · cracked · Jan 12, 2025 · N214WN · Boeing 7377H4 · Fuselage, Equipment Attach Fittings
> CRACK ANGLE WEATHER RADAR SUPPORT STRUCTURE LOCATED BETWEEN STA188 TO STA203.8 AND RBL5 AT FWD OF NOSE WHEEL WELL 2024-780466<[01] REPLACED NEW ANGLE WEATHER RADAR SUPPORT STRUCTURE AND FASTENERS LOCATED BETWEEN STA188 TO STA203.8 AND RBL5 AT FWD OF NOSE WHEEL
- [SDR SWAA2025020585210](https://openairdocs.org/sdr/SWAA2025020585210.md): Stringer · cracked · Jan 12, 2025 · N214WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
> CRACK STRINGER 26L LOCATED STA540 FWD CARGO COMPARTMENT 2024-780464 <[01] TOOL USED P/N: 45MG; S/N: 130066401; CAL DUE: 21-OCT-25.;[02] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 60009161631 DUE DATE: 11-MAR-25;[03] REPAIRED STRINGER 26L LOCATED BS
- [SDR SWAA2025020585211](https://openairdocs.org/sdr/SWAA2025020585211.md): Stringer · cracked · Jan 12, 2025 · N214WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
> CRACK STRINGER 25L LOCATED STA540 FWD CARGO COMPARTMENT 2024-780465 <[01] TOOL USED P/N: 45MG; S/N: 130066401; CAL DUE: 21-OCT-25.;[02] TOOL USED ON STEP 8: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 60007161486; DUE DATE:06-SEP-25;[03] REPAIRED STRINGER 25L LOCATE
- [SDR SWAA2025021084900](https://openairdocs.org/sdr/SWAA2025021084900.md): Support Bracket · cracked · Jan 10, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND LBL 6 AT AIR CONDITIONING BAY 2024-780405<[01] REPLACED SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND LBL 6 AT AIR CONDITIONING BAY I.A.W B737-700 SRM 51-40-02-0G-0 AND AMM 20-50-11-910-801.
SEE INDIVIDU
- [SDR SWAA2025021085018](https://openairdocs.org/sdr/SWAA2025021085018.md): Rib · cracked · Jan 10, 2025 · N214WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
> CRACK LEADING EDGE RIB ACCESS PANEL 331B LE STA 151.75 AT LT HORIZONTAL STABILIZER 2024-780411<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25.;[02] REPLACED RIB LOCATED LEADING EDGE ACCESS PANEL 331B LE STA 151.75 AT
- [SDR SWAA2025021085019](https://openairdocs.org/sdr/SWAA2025021085019.md): Rib · cracked · Jan 10, 2025 · N214WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
> CRACK LEADING EDGE RIB ACCESS PANEL 331B LE STA 161.04 AT LT HORIZONTAL STABILIZER 2024-780414<[01] REPLACED LEADING EDGE RIB ACCESS PANEL 331B LE STA 161.04 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; AND DWG 186A1001 SHEET 11 REV A.;[02] CO
- [SDR SWAA2025021084899](https://openairdocs.org/sdr/SWAA2025021084899.md): Bracket · cracked · Jan 10, 2025 · N214WN · Boeing 7377H4 · Wing Miscellaneous Structure
> CRACK SUPPORT BRACKET INBOARD FRONT SPAR IFSS 151 AT RT WING 2024-780410<[01] REPLACED SUPPORT BRACKET LOCATED INBOARD FRONT SPAR IFSS 151 AT RT WING IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGNS OF BELOW.;[02] REPLACED SUPPORT BRACKET LOCATED INBOARD FRONT
- [SDR SWAA2025020584898](https://openairdocs.org/sdr/SWAA2025020584898.md): Stringer · cracked · Jan 10, 2025 · N214WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
> CRACK STRINGER 8 INTERNAL AREA FUEL TANK LOC. BTW RIB 19 AND RIB 20 UPPER SKIN LOWER SURFACE AFT AREA AT RT WING 2024-780408 <[01]. TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25.;[02] REPAIRED STRINGER 8 INTERNAL
- [SDR SWAA2025021084797](https://openairdocs.org/sdr/SWAA2025021084797.md): Skin Panel · cracked · Jan 9, 2025 · N214WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
> CRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 1.25 INCH. APPROX. 2024-780403 <[01]. ON STEP 4; TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC
- [SDR SWAA2025020584460](https://openairdocs.org/sdr/SWAA2025020584460.md): Intercostal · cracked · Jan 8, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK WEB INTERCOSTAL LOCATED BETWEEN BS 294.5 AND BS 303.9 AND STRINGER 16L AT FWD GALLEY AREA 2024-780350<[01]. INSTALLED NEW WEB INTERCOSTAL; STRAP 1(E/A) ANGLE 1(E/A) AND FASTENERS. LOCATED BETWEEN BS 294.5 AND BS 303.9 AND STRINGER 16L AT FWD GALLEY AREA
- [SDR SWAA2025020584458](https://openairdocs.org/sdr/SWAA2025020584458.md): Angle · cracked · Jan 8, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK ANGLE LOCATED STA294.5 AND STR13L AT PASSENGER CABIN 2024-780338 <[01]. REPLACED ANGLE AND FASTENERS LOCATED STA294.5 AND STR13L AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A1311 SHEET 1 REV C. SEE INDIVIDUAL SIGN OFF
- [SDR SWAA2025020584461](https://openairdocs.org/sdr/SWAA2025020584461.md): Angle · cracked · Jan 8, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK ANGLE LOCATED STA294.5 AND STR17R AT FWD GALLEY AREA 2024-780353 <[01] REPLACED ANGLE AND FASTENERS LOCATED STA294.5 AND STR17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 STEP 9 AND SRM 51-40-02; AND DWG:141A8310;SHEET:25; REV:; SEE INDIVIDUAL SIGN OF
- [SDR SWAA2025020584462](https://openairdocs.org/sdr/SWAA2025020584462.md): Tie Clip · collapsed · Jan 8, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN 2024-780336 <[01]. REPLACED TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN IAW B737-700 SRM: 51-40-02 AND SRM 51-10-02 STEP 9; AND DWG: 141A8380 SHEET:15. REV:-; SEE INDIVIDUAL SIGN OFF BELOW;[02] T
- [SDR SWAA2025020583804](https://openairdocs.org/sdr/SWAA2025020583804.md): Support Angle · cracked · Jan 7, 2025 · N214WN · Boeing 7377H4 · Cargo Compartments
> CRACK ANGLE - SUPPORT BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRNGER 27R AFT CARGO COMPARTMENT 2024-780306 <[01] REPLACED ANGLE - SUPPORT LOCATED BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRNGER 27R AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02; DWG NO:
- [SDR SWAA2025020483803](https://openairdocs.org/sdr/SWAA2025020483803.md): Intercostal · cracked · Jan 7, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK WEB - INTERCOSTAL BETWEEN BS 927 TO BS 947.5 AND STRINGER 25R AFT CARGO COMPARTMENT 2024-780305<[01]. REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 927 TO BS 947.5 AND STRINGER 25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 5
- [SDR SWAA2025021083466](https://openairdocs.org/sdr/SWAA2025021083466.md): Angle · cracked · Jan 6, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK ANGLE - CLIP LOCATED STA400 AND STR26R FWD CARGO COMPARTMENT 2024-780271<[01] REPLACED ANGLE-CLIP AND FASTENERS LOC ON STA400 AND STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 STEP 9 AND SRM 51-40-02 AND DWG 143A7505 SHEET 2 REV B. SEE INDIVIDUA
- [SDR SWAA2025021083472](https://openairdocs.org/sdr/SWAA2025021083472.md): Pressure Web · cracked · Jan 6, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK INDICATION FOUND ON HORIZONTAL PRESSURE WEB UPPER SURFACE BTW STA 663 TO STA 675; AT LEVEL LBL 30. CRACK LENGTH = 0.695 INCHES APPROX. 2024-780281<[01] ON STEP 5: TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030456 DUE DATE: 14 APR 25.;
- [SDR SWAA2025020483469](https://openairdocs.org/sdr/SWAA2025020483469.md): Support · elongated · Jan 6, 2025 · N214WN · Boeing 7377H4 · Cargo Compartments
> ELONGATED HOLE ON SUPPORT ZEE LOCATED BETWEEN STA500 TO STA500A AFT CARGO COMPARTMENT 2024-780276 ELONGATED HOLE ON SUPPORT ZEE LOCATED BETWEEN STA500 TO STA500A AND LBL22 FWD CARGO COMPARTMENT<[01] REPLACED SUPPORT ZEE (1E/A) AND STRAP SPLICE (1E/A) LOCATED B
- [SDR SWAA2025020483470](https://openairdocs.org/sdr/SWAA2025020483470.md): Intercostal · cracked · Jan 6, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK WEB - INTERCOSTAL LOCATED BETWEEN STA500 TO STA500A AND LBL22 FWD CARGO COMPARTMENT 2024-780277<[01]. REPLACED WEB - INTERCOSTAL LOCATED BETWEEN STA500 TO STA500A AND LBL22 FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG
- [SDR SWAA2025020583158](https://openairdocs.org/sdr/SWAA2025020583158.md): Support Angle · cracked · Jan 5, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND BL 0 AT PASSENGER CABIN 2024-780190<[01]. STEP 1. EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 240494307 AND DUE DATE: 27-AUG-25.;[02] PERFORMED NDT INSPECTION AND NOT CRACK FOUND IAW 737 NDT MANUAL PART 6
- [SDR SWAA2025020583159](https://openairdocs.org/sdr/SWAA2025020583159.md): Panel · cracked · Jan 5, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 AND RBL 24.75 AT PASSENGER CABIN 2024-780232 <[01]. REPLACED BRAKE PANEL (INTERCOSTAL) AND FASTENERS LOCATED BS 540 BETWEEN BL 0 AND RBL 24.75 AT PASSENGER CABIN. IAW B737-700 SRM: 51-40-02 AND DWG: 143A00
- [SDR SWAA2025020583164](https://openairdocs.org/sdr/SWAA2025020583164.md): Panel · cracked · Jan 5, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 AND LBL 24.75 AT PASSENGER CABIN 2024-780225<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 AND LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 143A0060; SHEET:44;REV:A
- [SDR SWAA2025020583163](https://openairdocs.org/sdr/SWAA2025020583163.md): Support Angle · cracked · Jan 5, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK LOWER SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND LBL 24.75 AT PASSENGER CABIN 2024-780204 <[01]. TOOL USED: TEMPE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE 23 JAN 25.;[0
- [SDR SWAA2025020583347](https://openairdocs.org/sdr/SWAA2025020583347.md): Panel · cracked · Jan 5, 2025 · N214WN · Boeing 7377H4 · Aerodynamic Fairings
> CRACK ON HOLES ACCESS PANEL 191CL BODY FAIRING AT FUSELAGE EXTERIOR 2024-780250 <[01] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 16122983 DUE DATE: 15-FEB-25;[02] UT EQUIPMENT USED P/N: EPOCH 600; S/N: 120357005; DUE DATE: 10-JUN-25;[03] REPAIRED ACCESS PANEL 19
- [SDR SWAA2025020483344](https://openairdocs.org/sdr/SWAA2025020483344.md): Light · broken · Jan 5, 2025 · N214WN · Boeing 7377H4 · Emergency Lighting
> BROKEN FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA) 2024-780243<[01] INSTALLED FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802;[02] CORRECTED STEP 1. REPLACED FLOOR PRO
- [SDR SWAA2025020483161](https://openairdocs.org/sdr/SWAA2025020483161.md): Gusset · cracked · Jan 5, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK GUSSET LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT 2024-780157 <[01]. REPLACED NEW GUSSET AND FASTENERS LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; AND DWG 143A7902 SHEET:147 REV:- SEE INDIVIDUAL SIGNS OFF BELOW; [02]
- [SDR SWAA2025020483160](https://openairdocs.org/sdr/SWAA2025020483160.md): Gusset · cracked · Jan 5, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK GUSSET LOCATED STA500D AND STR19L FWD CARGO COMPARTMENT 2024-780148<[01] REPLACED GUSSET AND FASTENER LOCATED STA500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 174 REV: ? SEE INDIVIDUAL SIGN OFFS BELOW;[02]
- [SDR SWAA2025020483153](https://openairdocs.org/sdr/SWAA2025020483153.md): Angle · cracked · Jan 5, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK ANGLE - CLIP LOCATED STA400 AND STR26L FWD CARGO COMPARTMENT 2024-780136<[01] REPLACED ANGLE - CLIP LOCATED STA400 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 51-40-02 AND DWG 143A7505 SHEET 2 REV: B SEE INDIVIDUAL SIGN OFF BELOW; [02] REPLACED ANGLE -
- [SDR SWAA2025020483162](https://openairdocs.org/sdr/SWAA2025020483162.md): Angle · cracked · Jan 5, 2025 · N214WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
> CRACK ANGLE - CLIP LOCATED STA500C AND STR26R FWD CARGO COMPARTMENT 2024-780168<[01] REPLACED ANGLE - CLIP LOCATED ON STA500C AND STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7505 SHEET: 6 REV D;
- [SDR SWAA2025021083142](https://openairdocs.org/sdr/SWAA2025021083142.md): Access Panel · cracked · Jan 4, 2025 · N214WN · Boeing 7377H4 · Wing, Plate/Skin
> CRACK ON HOLES ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2024-780050<[01] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 16122983 DUE DATE: 15-FEB-25;[02] TOOL USED: HOT BONDER PN: HCS9200B SN: 16122983 DUE DATE: 15/FEB/25.;[03] TOOL USED: ULTRASONIC FLAW DETECTOR
- [SDR SWAA2024112161801](https://openairdocs.org/sdr/SWAA2024112161801.md): Battery Pack · inoperative · Nov 20, 2024 · N214WN · Boeing 7377H4 · Emergency Lighting
> MID CABIN RIGHT SIDE 3 AISLE AND OVERWING EMERGENCY EXIT LIGHTS INOP<[01] T/S PER FIM 33-50 TASK 801; REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK (M1669) PER AMM 33-51-06. ALL E-LIGHTS OPS CHECK GOOD.
- [SDR SWAA2024100444540](https://openairdocs.org/sdr/SWAA2024100444540.md): Cover · detached · Oct 2, 2024 · N214WN · Boeing 7377H4 · Emergency Lighting
> EXIT ROW SIGN AT MID CABIN FELL OFF THE CEILING<[01] REINSTALLED COVER PER AMM 33-51-03.
- [SDR SWAA2024062103854](https://openairdocs.org/sdr/SWAA2024062103854.md): Handle · loose · Jun 19, 2024 · N214WN · Boeing 7377H4 · Emergency Equipment
> CREW REPORTS MEGAPHONE HANDLE IS LOOSE<[01] R & R MEGAPHONE IAW SIP OPS CHECKS GOOD
- [SDR SWAA2024030156710](https://openairdocs.org/sdr/SWAA2024030156710.md): Counter · smoke · Feb 26, 2024 · N214WN · Boeing 7377H4 · Indicating/Recording System
> FO TRIP COUNTER HAD SMOKE COMING FROM LIGHT<[01] INSPECTED YOKE AREA; NO DAMAGE FOUND
R/R TRIP COUNTER PER AMM 33-11-00
- [SDR SWAA2023073183551](https://openairdocs.org/sdr/SWAA2023073183551.md): Fairing · delaminated · Jul 29, 2023 · N214WN · Boeing 7377H4 · Aerodynamic Fairings
> FAIRING 194FR REQUIRE REPLACEMENT REF TTG8Q00M0SWV FOR 194FR<[01] REPLACED 194FR PANEL PER AMM 53-51-21.
Next page: https://openairdocs.org/aircraft/N214WN/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 = 'N214WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```
This list as a web page: https://openairdocs.org/aircraft/N214WN/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.