# Service difficulty reports: N220WN

A list on [N220WN](https://openairdocs.org/aircraft/N220WN.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 8 · 358 reports

- [SDR SWAA2026062916232](https://openairdocs.org/sdr/SWAA2026062916232.md): Slide · detached · Jun 25, 2026 · N220WN · Boeing 7377H4 · Escape Slide
  > R1 DOOR SLIDE FELL OUT OF DOOR ONTO FLOOR IN GALLEY. REINSTALLED R1 SERVICE DOOR SLIDE IAW AMM 25-66-00 AND T/C 725-61-06-FS.
- [SDR SWAA2026052105173](https://openairdocs.org/sdr/SWAA2026052105173.md): Girt Bar · out of adjust · May 21, 2026 · N220WN · Boeing 7377H4 · Emergency Equipment
  > NG DOOR SLIDE COVER GIRT BAR RETAINER CLIP MISSING FASTENERS - PERMANENT REPAIR. REMOVED TEMP REPAIR AND INSTALLED FASTENER PER SRM 51-40-02 AND AIPC 25-66-00-13.
- [SDR SWAA2026051397439](https://openairdocs.org/sdr/SWAA2026051397439.md): Retainer · loose · May 11, 2026 · N220WN · Boeing 7377H4 · Emergency Equipment
  > FWD ENTRY DOOR GIRT BAR RETAINER LOOSE. C/W ALL EA M-23-125-01839.
- [SDR SWAA2026042290613](https://openairdocs.org/sdr/SWAA2026042290613.md): Hook · loose · Apr 18, 2026 · N220WN · Boeing 7377H4 · Emergency Equipment
  > FORWARD SERVICE DOOR GIRT BAR STORAGE HOOKS LOOSE. TIGHTENED GIRT BAR STORAGE HOOKS AS REQUIRED PER SIP. ACFT OK FOR SERVICE.
- [SDR SWAA2026033082923](https://openairdocs.org/sdr/SWAA2026033082923.md): Battery Pack · no indication · Mar 25, 2026 · N220WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT 20 ABC M1670. R & R EMERGENCY BATTERY PACK PER AMM 33-51-06;[02] INSPECTED PER AMM 33-51-06
- [SDR SWAA2025112438379](https://openairdocs.org/sdr/SWAA2025112438379.md): Lens · detached · Nov 20, 2025 · N220WN · Boeing 7377H4 · Emergency Lighting
  > EMER LT LENS FWD OF LH EMER EXIT DOOR FELL OFF<[01] RESECURED EMER LT LENS PER MM 33-51-01
- [SDR SWAA2025082105931](https://openairdocs.org/sdr/SWAA2025082105931.md): Retainer · fod · Aug 18, 2025 · N220WN · Boeing 7377H4 · Emergency Equipment
  > FA REPORTS FWD LEFT GIRT BAR DIFFICULT TO ARM & DISARM. CLEANED GIRT BAR RETAINER IAW SIP.
- [SDR SWAA2025042827272](https://openairdocs.org/sdr/SWAA2025042827272.md): Bulb · burned out · Apr 22, 2025 · N220WN · Boeing 7377H4 · Emergency Lighting
  > CUSTOMER REQUEST LIGHTBULBS BURNT OUT AT L1 AND R1 DOOR EMERGENCY EXIT LIGHTS. REPLACED LIGHTBULBS BURNT OUT AT L1 AND R1 DOOR EMERGENCY EXIT LIGHTS IAW AMM 33-51-01-960-801-NG TEST IS OK.
- [SDR SWAA2025042854252](https://openairdocs.org/sdr/SWAA2025042854252.md): Rib · cracked · Apr 8, 2025 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 9 INCH FROM FRONT SPAR LT HORIZONTAL STAB. REPAIRED INSPAR RIB LOCATED STAB STA 129.50 AND 9 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 PARAGRAPH 4;FIGURE 203.
- [SDR SWAA2025042820691](https://openairdocs.org/sdr/SWAA2025042820691.md): Scuff Plate · cracked · Apr 1, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SCUFF PLATE AFT CORNER LOCATED AT FWD CARGO COMPARTMENT. REPAIRED THE AFT CORNER SCUFF PLATE OF FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.
- [SDR SWAA2025042809048](https://openairdocs.org/sdr/SWAA2025042809048.md): Support Bracket · cracked · Mar 24, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT BRACKET LOCATED INTERNAL AREA BTW BS188 TO BS203 AT LOWER NOSE COMPARTMENT. REPLACED SUPPORT BRACKET LOCATED INTERNAL AREA BTW BS188 TO BS203 AT LOWER NOSE COMPARTMENT IAW SRM 51-10-02-0G PARAGRAPH 9; SRM 51-40-02-0G AND DWG: 141A9194 SHEET:
- [SDR SWAA2025042808570](https://openairdocs.org/sdr/SWAA2025042808570.md): Support Bracket · cracked · Mar 23, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET BS 663.75 AND RBL 54 AT LOWER FUSELAGE 2025-204843<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE 29 JAN 26.;[02] TOOL USED: POWER PACK P/N FMK0007096 S/N PE0414/70786 DUE DATE 03 JUN 25; THERMOMETER P/N
- [SDR SWAA2025042854239](https://openairdocs.org/sdr/SWAA2025042854239.md): Skin Panel · cracked · Mar 23, 2025 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16.0 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.700 INCH. APPROX. 2025-204859<[01] TOOL USED ON STEP 5:EDDY CURRENT EQUIPMENT P/N: NORTEC 6
- [SDR SWAA2025042854240](https://openairdocs.org/sdr/SWAA2025042854240.md): Skin Panel · cracked · Mar 23, 2025 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16.0 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 1.00 INCH. APPROX. 2025-204860<[01] TOOL USED: ET EQUIPMENT; P/N: NORTEC600D; S/N: 210138103;
- [SDR SWAA2025042854241](https://openairdocs.org/sdr/SWAA2025042854241.md): Rib · cracked · Mar 23, 2025 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 24.0 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.350 INCH. APPROX. 2025-204861. REFER TO FAULT TTG8Q00ZF38D WHERE EA 25-155-00868 WAS ADDED
- [SDR SWAA2025042854222](https://openairdocs.org/sdr/SWAA2025042854222.md): Stringer · cracked · Mar 22, 2025 · N220WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK ON STRINGER 22L LOCATED BS540 FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 22L LOCATED BS500D AND BS540 AT FWD CARGO COMPARTMENT IAW SRM 53-00-03-2R-1 REPAIR 1.
- [SDR SWAA2025042854189](https://openairdocs.org/sdr/SWAA2025042854189.md): Intercostal · cracked · Mar 21, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL LOCATED BTW BS 685 TO BS 706 AT LEVEL STR 14R AT PASSENGER CABIN. REPLACED WEB INTERCOSTAL LOCATED BTW BS 685 TO BS 706 AT LEVEL STR 14R AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9; B737-700 SRM 51-40-02-0G-0 AND DWG
- [SDR SWAA2025042854191](https://openairdocs.org/sdr/SWAA2025042854191.md): Stringer · cracked · Mar 21, 2025 · N220WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK ON STRINGER 23L LOCATED BS540 FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 23L LOCATED BS500D AND BS540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.
- [SDR SWAA2025042808083](https://openairdocs.org/sdr/SWAA2025042808083.md): Angle · cracked · Mar 21, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS 540 AND RBL 6 AT CENTER WING BOX REPLACED ANGLE LOCATED BS 540 AND RBL 6 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND DWG 212A1101 SHEET: 3 REV: -. REMOVED EWIS PROTECTION LOCATED BS 540 AND RBL 6 AT CENTER WING BOX IAW B737-700
- [SDR SWAA2025042854188](https://openairdocs.org/sdr/SWAA2025042854188.md): Rib · cracked · Mar 21, 2025 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 28 INCH FROM FRONT SPAR LT HORIZONTAL. PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED STAB STA 129.50 AND 28 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4.
- [SDR SWAA2025042854207](https://openairdocs.org/sdr/SWAA2025042854207.md): Skin · debonded · Mar 21, 2025 · N220WN · Boeing 7377H4 · Trailing Edge Flaps
  > DEBONDED OB AFT FLAP INBOARD SIDE AT RT WING. PERFORMED INTERIM REPAIR AT OB AFT FLAP INBOARD SIDE AT RT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. AND THE REPAIR REQUIRED TAP TEST INSPECTION EVERY 6;875 CYCLES OR 30 MONTHS WHICHEVER COMES FIRST.
- [SDR SWAA2025042854175](https://openairdocs.org/sdr/SWAA2025042854175.md): Support Angle · cracked · Mar 20, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FLOOR STRUCTURE AFT SUPPORT ANGLE BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AT AFT CARGO COMPARTMENT. REPLACED AFT SUPPORT ANGLE (STIFFENER) BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51
- [SDR SWAA2025042854176](https://openairdocs.org/sdr/SWAA2025042854176.md): Support Angle · cracked · Mar 20, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FLOOR STRUCTURE FWD SUPPORT ANGLE BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AT AFT CARGO COMPARTMENT. REPLACED FWD SUPPORT ANGLE (STIFFENER) BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51
- [SDR SWAA2025042854179](https://openairdocs.org/sdr/SWAA2025042854179.md): Angle · cracked · Mar 20, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON CLOUSURE ANGLE LOCATED BS1016 TO BS1088 AT LEVEL ST2L AND STR3L EXTERNAL SKIN AT UPPER FUSELAGE. REPLACED CLOUSURE ANGLE AND FASTENERS LOCATED BS1016 TO BS1121+ 10 INCHES APROX AT LEVEL ST2L AND STR3L EXTERNAL SKIN UPPER FUSELAGE IAW B737-700 SRM 51
- [SDR SWAA2025042808077](https://openairdocs.org/sdr/SWAA2025042808077.md): Support · corroded · Mar 20, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE BETWEEN BS 727D TO BS 767 AND RBL 21 AFT CARGO COMPARTMENT 2025-204674<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 RBL21 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 146A7500 SHEET: 85 REV: A; DWG
- [SDR SWAA2025042854183](https://openairdocs.org/sdr/SWAA2025042854183.md): Light · broken · Mar 20, 2025 · N220WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN BASE ON EMERGENCY EXIT LIGHT ON LAV B. REPLACED BASE ON EMERGENCY EXIT LIGHT ON LAV B IAW B737-700 AMM-33-51-01-960-802 STEP 3.A TO 3.C (6) AND (7). TESTED OK.
- [SDR SWAA2025042854172](https://openairdocs.org/sdr/SWAA2025042854172.md): Support Angle · cracked · Mar 19, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - SUPPORT LOCATED BS727C AND LBL47 UPPER CEILING AREA AT AFT CARGO COMPARTMENT 2025-204643<[01] REPLACED ANGLE - SUPPORT AND FASTENERS LOCATED BTW BS727A TO 727E+10? AND LBL47 UPPER CEILING AREA AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02
- [SDR SWAA2025042854155](https://openairdocs.org/sdr/SWAA2025042854155.md): Frame · cracked · Mar 18, 2025 · N220WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON WEB FRAME LOCATED BS 259.5 BTW STR 8R TO STR 9R AT FWD GALLEY AREA 2025-204596<[01] ET EQUIPMENT USED P/N: NORTEC 600D; S/N: 240494307; DUE DATE: 27-AUG-25;[02] PERFORMED PERMANENT REPAIR ON WEB FRAME LOCATED BS 259.5 BTW STR 6R TO STR 11R AT FWD GALL
- [SDR SWAA2025042806634](https://openairdocs.org/sdr/SWAA2025042806634.md): Angle · cracked · Mar 18, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE BS663 UPPER POSITION RBL40 AT CENTER WING BOX. REPLACED ANGLE LOCATED BS 663.75 BTW RBL 5 T0 RBL 65 AT CENTER WING BOX IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; B737-700 SRM 51-40-02-0G-0 AND DRAWING 111A1000; SHEET:171; REV: -. DRAWING 111A100
- [SDR SWAA2025042806251](https://openairdocs.org/sdr/SWAA2025042806251.md): Fitting · worn · Mar 17, 2025 · N220WN · Boeing 7377H4 · Emergency Equipment
  > WEAR ON GIRT BAR FITTING HARDWARE AND PLATE ON AFT ENTRY AND SERVICE DOOR AT AFT GALLEY AREA 2025-204561<[01] REPLACED GIRT BAR FITTING HARDWARE AND PLATE ON AFT ENTRY AND SERVICE DOOR AT AFT GALLEY ARE IAW B737-700 AMM 25-66-02-000-801 AND AMM 25-66-02-400-80
- [SDR SWAA2025042854145](https://openairdocs.org/sdr/SWAA2025042854145.md): Support Angle · cracked · Mar 17, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2025-204581<[01] REPLACED ANGLE AND FASTENERS LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 PARA
- [SDR SWAA2025042806445](https://openairdocs.org/sdr/SWAA2025042806445.md): Tie Clip · cracked · Mar 17, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DWG DWG 141A1110 SHEET 18 REV.
- [SDR SWAA2025042854147](https://openairdocs.org/sdr/SWAA2025042854147.md): Support Angle · cracked · Mar 17, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BS 294.5 BTW STR 12L TO STR 14L AT FWD GALLEY AREA. REPLACED SUPPORT ANGLE LOCATED BS 294.5 BTW STR 12L TO STR 14L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND DWG 141A1311 SHEET 1 REV C.
- [SDR SWAA2025042806247](https://openairdocs.org/sdr/SWAA2025042806247.md): Fitting · worn · Mar 17, 2025 · N220WN · Boeing 7377H4 · Emergency Equipment
  > WEAR ON GIRT BAR FITTING HARDWARE AND PLATE ON FWD ENTRY AND SERVICE DOOR AT FWD GALLEY AREA 2025-204551<[01] REPLACED GIRT BAR FITTING HARDWARE AND PLATE ON FWD ENTRY AND SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 AND INSTALLATION WILL
- [SDR SWAA2025042854121](https://openairdocs.org/sdr/SWAA2025042854121.md): Gusset · cracked · Mar 16, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2025-204510<[01] REPLACED GUSSET AND FASTENERS LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02-0G-0; DWG 143A7902 SHEET: 174 REV: - AND B737-700 SRM 51-10-02-0G-0 PARAG
- [SDR SWAA2025042854122](https://openairdocs.org/sdr/SWAA2025042854122.md): Gusset · cracked · Mar 16, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2025-204516<[01] REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02-0G AND DWG: 143A7902 SHEET: 256 REV: B; SEE INDIVIDUAL SIGN-OFF
- [SDR SWAA2025042806082](https://openairdocs.org/sdr/SWAA2025042806082.md): Angle · cracked · Mar 16, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS420 AND LBL21 FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP LOCATED BS420 AND LBL21 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG: 143A7505 SHEET: 2 REV B.
- [SDR SWAA2025042854119](https://openairdocs.org/sdr/SWAA2025042854119.md): Floorbeam · cracked · Mar 16, 2025 · N220WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED STIFFENER (PANEL BREAK) FLOOR STRUCTURE ON BS 540 BTW BL 0 AND RBL 24 AT PASSENGER CABIN. REPLACED STIFFENER FLOOR STRUCTURE ON BS 540 BTW BL 0 AND RBL 24 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 44 REV
- [SDR SWAA2025042805959](https://openairdocs.org/sdr/SWAA2025042805959.md): Access Panel · delaminated · Mar 16, 2025 · N220WN · Boeing 7377H4 · Aerodynamic Fairings
  > DELAMINATED ACCESS PANEL 194BL BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 194BL BODY FAIRING AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-10 REPAIR 10.
- [SDR SWAA2025042854123](https://openairdocs.org/sdr/SWAA2025042854123.md): Lens · broken · Mar 16, 2025 · N220WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN LENS EMERGENCY LIGHT ON BULL NOSE BIN POSITION 1 3 4 5 6 7 8 9 11 LH SIDE. REPLACED LENS EMERGENCY LIGHT ON BULL NOSE BIN POSITION 1; 3; 4; 5; 6; 7; 8; 9; 11 LH SIDE IAW B737-700 AMM 33-51-03-960-801 STEP 2.D(3) (A) AND (C).
- [SDR SWAA2025042838333](https://openairdocs.org/sdr/SWAA2025042838333.md): Lens · broken · Mar 15, 2025 · N220WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN LENS EMERGENCY LIGHT ON BULL NOSE BIN POSITIONS 3 4 5 6 7 8 9 RH SIDE 2025-204479<[01] REPLACED LENS EMERGENCY LIGHT ON BULL NOSE BIN POSITIONS 3; 4; 5; 6; 7; 8; 9 RH SIDE IAW B737-700 AMM 33-51-03-960-801 STEP 2.D(3) (A) AND (C).;[02] REPLACED LENS EME
- [SDR SWAA2025042805677](https://openairdocs.org/sdr/SWAA2025042805677.md): Access Panel · elongated · Mar 15, 2025 · N220WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLE ACCESS PANEL 571 DB AT LT WING. REPAIRED ACCESS PANEL 571 DB AT LT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.
- [SDR SWAA2025042854098](https://openairdocs.org/sdr/SWAA2025042854098.md): Lens · broken · Mar 15, 2025 · N220WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN EMERGENCY EXIT LIGHT LENS UPPER CENTER POSITION AT FWD AREA GALLEY. REPLACED EMERGENCY EXIT LIGHT LENS UPPER CENTER POSITION AT FWD AREA GALLEY IAW B737-700 AMM 33-51-01-960-801 STEP 2.C(1)(A)1) AND STEP 2.C(4).
- [SDR SWAA2025042805196](https://openairdocs.org/sdr/SWAA2025042805196.md): Floor Panel · corroded · Mar 14, 2025 · N220WN · Boeing 7377H4 · Fuselage Floor Panel
  > CORROSION PLATE LOC. ON FLOOR PANEL 140CF AREA BS 794.3 RH SIDE AT AFT CARGO COMPARTMENT. 2025-204366<[01] REPLACED PLATE LOC. ON FLOOR PANEL 140CF AREA BS 794.3 RH SIDE AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 453A2600 SHE
- [SDR SWAA2025042805195](https://openairdocs.org/sdr/SWAA2025042805195.md): Plate · corroded · Mar 14, 2025 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION PLATE LOC. ON FLOOR PANEL 140CF AREA BS 847 RH SIDE AT AFT CARGO COMPARTMENT. 2025-204365<[01] REPLACED PLATE LOC. ON FLOOR PANEL 140CF AREA BS 847 RH SIDE AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 453A2600 SHEET:
- [SDR SWAA2025010382720](https://openairdocs.org/sdr/SWAA2025010382720.md): Handle · broken · Jan 2, 2025 · N220WN · Boeing 7377H4 · Passenger/Crew Doors
  > MAIN ENTRY FOR ASSIST HANDLE BROKEN<[01] R&RD FWD ENTRY DOOR ASSIST HANDLE IAW MM 52-11-31
- [SDR SWAA2024122781033](https://openairdocs.org/sdr/SWAA2024122781033.md): Light · inoperative · Dec 27, 2024 · N220WN · Boeing 7377H4 · Emergency Lighting
  > LEFT AFT ENTRY DOOR EXTERNAL EMERGENCY LIGHT INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801-NG (SLIDE/OVERWING LIGHT - LAMP REPLACEMENT - PERMANENT)]
- [SDR SWAA2024121777658](https://openairdocs.org/sdr/SWAA2024121777658.md): Water System · odor · Dec 14, 2024 · N220WN · Boeing 7377H4 · Waste Disposal System
  > FWD LAV HAS A FOWL ODOR THAT CLEANING COULD NOT FIX. NO DIRECT INDICATION OF CAUSE.<[01] R&R CREW. OPS CHECK AND FLUSH CHECK OF FWD LAV GOOD IAW MM 38-32-00. NO FOWL ODORS DETECTED.
- [SDR SWAA2024100744597](https://openairdocs.org/sdr/SWAA2024100744597.md): Battery Pack · no test · Oct 3, 2024 · N220WN · Boeing 7377H4 · Emergency Lighting
  > EMX BATTERY PACK M01675 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01675 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024100444598](https://openairdocs.org/sdr/SWAA2024100444598.md): Battery Pack · failed · Oct 3, 2024 · N220WN · Boeing 7377H4 · Emergency Lighting
  > EMX BATTERY PACK M01672 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01672 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Next page: https://openairdocs.org/aircraft/N220WN/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 = 'N220WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N220WN/reports

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