# Service difficulty reports: N461WN

A list on [N461WN](https://openairdocs.org/aircraft/N461WN.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 · 250 reports

- [SDR SWAA2026050896283](https://openairdocs.org/sdr/SWAA2026050896283.md): Slide · low pressure · May 6, 2026 · N461WN · Boeing 7377H4 · Escape Slide
  > L1 DOOR SLIDE PRESSURE IN THE RED BAND. R & R L1 DOOR SLIDE IAW MT 725-61-06-FE
- [SDR SWAA2026021068065](https://openairdocs.org/sdr/SWAA2026021068065.md): Lamp · inoperative · Feb 6, 2026 · N461WN · Boeing 7377H4 · Emergency Lighting
  > FIRST OFFICER SIDE OVERWING EXIT SIDEWALL LIGHT INOPERATIVE. R & R RT OVERWING EXIT LIGHT LAMP IAW AMM 33-21-00, OPS CHECKED GOOD.
- [SDR SWAA2025110632361](https://openairdocs.org/sdr/SWAA2025110632361.md): Unknown · odor · Nov 6, 2025 · N461WN · Boeing 7377H4 · Air Distribution System
  > FA SMELLED SOME ELECTRICAL ODOR CENTER CABIN ROW 7. C/W FUMES IN THE CABIN, NO DEFECTS NOTED IAW FIM 21-00 TASK 806. ACFT OK FOR SERVICE.
- [SDR SWAA2025102823587](https://openairdocs.org/sdr/SWAA2025102823587.md): Access Panel · damaged · Oct 10, 2025 · N461WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLE IN ACCESS PANEL 661BB AT TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB AT TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2025102822826](https://openairdocs.org/sdr/SWAA2025102822826.md): Tail Cone · delaminated · Oct 8, 2025 · N461WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > DELAMINATED TAIL CONE RIGHT SIDE ON EXTERNAL SKIN. REPAIRED TAIL CONE RIGHT SIDE ON EXTERNAL SKIN IAW SRM 51-70-04-2R-1, REPAIR 1.
- [SDR SWAA2025102822418](https://openairdocs.org/sdr/SWAA2025102822418.md): Scuff Plate · cracked · Oct 7, 2025 · N461WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON AFT CORNER SCUFF PLATE IN FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS 2 TO 7, FIGURE 203.
- [SDR SWAA2025102822295](https://openairdocs.org/sdr/SWAA2025102822295.md): Plate · cracked · Oct 7, 2025 · N461WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED CORRUGATED PLATE TRAILING EDGE IRSS 215 AT LT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02-0G-0, PARAGRAPH 9, DRAWING 115A2001, SHEET 30, REV A, & SRM 51-40-02-0G-0. MEASUREMENT OF CRACK: REMOVED: L: 0.519 INCH.
- [SDR SWAA2025102822297](https://openairdocs.org/sdr/SWAA2025102822297.md): Support Angle · cracked · Oct 7, 2025 · N461WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE, TRAILING EDGE ORSS 280 AT RT WING. EVALUATED SUPPORT ANGLE AND NOT FOUND ON ALLOWABLE DAMAGE ON SRM IAW SRM-57-51-02-1A-1 ALLOWABLE DAMAGE 1. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02 AND DWG 115A6200 SHEET 10 REV - MEASUREMENT OF CRAC
- [SDR SWAA2025102822293](https://openairdocs.org/sdr/SWAA2025102822293.md): Angle · cracked · Oct 7, 2025 · N461WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, TRAILING EDGE ORSS 271 LT WING. REPLACED THE ANGLE IAW SRM 51-40-02, AND DRAWING 115A2930, SHEET 7, REV -.
- [SDR SWAA2025102822296](https://openairdocs.org/sdr/SWAA2025102822296.md): Plate · cracked · Oct 7, 2025 · N461WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 AT RT WING. REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE ORSS 261 AT RT WING IAW SRM 51-10-02-0G-O, PARAGRAPH 9; DRAWING 115A2001 SHEET 29, REV- AND SRM 51-40-02-0G-0. MEASUREMENT OF CRACK, REMOVED: L: 0.4
- [SDR SWAA2025102822298](https://openairdocs.org/sdr/SWAA2025102822298.md): Plate · cracked · Oct 7, 2025 · N461WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE IRSS 215 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 215 AT RT WING IAW SRM 51-40-02 AND DWG 115A2001, SHEET 30; REV A.
- [SDR SWAA2025102822294](https://openairdocs.org/sdr/SWAA2025102822294.md): Support Bracket · cracked · Oct 7, 2025 · N461WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACKED SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-O2, & SRM 51-10-02, ITEM 9. MEASUREMENT OF CRACK IS 0.200".
- [SDR SWAA2025102822036](https://openairdocs.org/sdr/SWAA2025102822036.md): Access Panel · delaminated · Oct 6, 2025 · N461WN · Boeing 7377H4 · Nacelle/Pylon, Plate/Skin
  > DELAMINATED ACCESS PANEL 431AT AT RT PYLON. PERFORMED VISUAL INSPECTION ON ACCESS PANEL 431AT AT RT PYLON AND NOT FOUND DAMAGE ON FIBER SKIN ONLY WAS FOUND SURFACE PROTECTION DETERIORATED IAW B737-700 NDT PART 1. 51-05-01 PARAGRAPH 3 AND RESTORED SURFACE PRO
- [SDR SWAA2025102721851](https://openairdocs.org/sdr/SWAA2025102721851.md): Support Angle · cracked · Oct 6, 2025 · N461WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND RBL 1 PASSENGER CABIN. INSTALLED SUPPORT ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE BS 695 AND RBL 1 PASSENGER CABIN IAW SRM 51-40-0G AND DRAWING 273A9110 SHEET 6 REV A.
- [SDR SWAA2025102821531](https://openairdocs.org/sdr/SWAA2025102821531.md): Light · broken · Oct 5, 2025 · N461WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA). REPLACED PHOTOLUMINESCENT STRIPS IAW DWG 33500007, REV 2, & SOPM 20-50-12, REV 58.
- [SDR SWAA2025102821534](https://openairdocs.org/sdr/SWAA2025102821534.md): Access Panel · cracked · Oct 5, 2025 · N461WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACKED ACCESS PANEL 661BB AT TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB AT TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2025102821703](https://openairdocs.org/sdr/SWAA2025102821703.md): Access Panel · cracked · Oct 5, 2025 · N461WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK HOLE ACCESS PANEL 561BB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2025102821533](https://openairdocs.org/sdr/SWAA2025102821533.md): Bracket · corroded · Oct 5, 2025 · N461WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CORROSION ON BRACKET FUEL BOOST PUMP REA LOCATED IRSS147 AT RT WING (2 E/A). REPLACED BRACKET FUEL BOOST PUMP AREA LOCATED IRSS147 AT RT WING IAW AMM 28-22-41-000-801 AND AMM 28-22-41-400-801.
- [SDR SWAA2025102821706](https://openairdocs.org/sdr/SWAA2025102821706.md): Pressure Deck · cracked · Oct 5, 2025 · N461WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT RBL 43 BETWEEN STA 663 TO STA 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.312 IN. APPROX. PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK WEB AT RBL 43 BETWEEN BS 663 - 675 AT MAIN WHEEL
- [SDR SWAA2025102721704](https://openairdocs.org/sdr/SWAA2025102721704.md): Floor Panel · delaminated · Oct 5, 2025 · N461WN · Boeing 7377H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 241EF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 241EF AT PASSENGER CABIN IAW SRM 53-00-50-2R-1 REPAIR 1.
- [SDR SWAA2025072494896](https://openairdocs.org/sdr/SWAA2025072494896.md): Lamp · inoperative · Jul 24, 2025 · N461WN · Boeing 7377H4 · Emergency Lighting
  > AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-03.
- [SDR SWAA2025071791508](https://openairdocs.org/sdr/SWAA2025071791508.md): Hook · loose · Jul 15, 2025 · N461WN · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR GIRT BAR HOOKS ARE REPORTED LOOSE. ADJUSTED FORWARD SERVICE DOOR GIRT BAR HOOKS IN REFERENCE TO AIRCRAFT MAINTENANCE MANUAL 25-66-00-201-NG
- [SDR SWAA2025031404422](https://openairdocs.org/sdr/SWAA2025031404422.md): Frame · pulled · Mar 12, 2025 · N461WN · Boeing 7377H4 · Nacelle/Pylon, Frame/Spar/Rib
  > #1 ENG AFT STRUT FAIRING O/B SIDE FWD STIFFENER HAS PULLED THRU HILOCS <[01]. REPLACED FRAME SECTION AS REQUIRED REF SRM 51-40-05 AND DWG313A2700.
- [SDR SWAA2025011586251](https://openairdocs.org/sdr/SWAA2025011586251.md): Slide · dislodged · Jan 14, 2025 · N461WN · Boeing 7377H4 · Escape Slide
  > LEFT AFT ENTRY DOOR SLIDE FELL OUT OF CONTAINER<[01] INSTALLED SLIDE PER M/M 25-66-01;AND MT#725-61-06-AE.NO DEFECTS NOTED.
- [SDR SWAA2024091335844](https://openairdocs.org/sdr/SWAA2024091335844.md): Skin · delaminated · Sep 10, 2024 · N461WN · Boeing 7377H4 · Trailing Edge Flaps
  > L/H OUTBOARD AFT FLAP IS DELAMINATED ON INBD SIDE.<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22.;[02] C/W INSP. REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22.
- [SDR SWAA2024080722805](https://openairdocs.org/sdr/SWAA2024080722805.md): Cover · displaced · Aug 5, 2024 · N461WN · Boeing 7377H4 · Emergency Lighting
  > SEAT 12F EMERGENCY EXIT LIGHT COVER DISPLACED<[01] RE SECURED EMERGENCY EXIT LIGHT COVER AT SEAT 12F; REF STANDARD INDUSTRY PRACTICES.
- [SDR SWAA2024080520930](https://openairdocs.org/sdr/SWAA2024080520930.md): Floor Panel · cracked · Aug 1, 2024 · N461WN · Boeing 7377H4 · Cargo Compartments
  > FORWARD CARGO BIN HAS A CRACK IN BIN FLOOR<[01] OK TO CONTINUE PER MEL 25-16-01 SP1<BR>FWD BAG PIT UNUSABLE;[02] R&R FWD CGO COMPARTMENT FLOOR PANEL PER AMM 25-52-10.
- [SDR SWAA2024010225669](https://openairdocs.org/sdr/SWAA2024010225669.md): Light · inoperative · Nov 28, 2023 · N461WN · Boeing 7377H4 · Emergency Lighting
  > AFT SERVICE DOOR UPPER EMERGENCY EXIT LIGHT HAS BURNT OUT BULB 2023-652353<[01] REPLACED AFT SERVICE DOOR UPPER EMERGENCY EXIT LIGHT IAW: B737-700 SWPM 20-84-13 AND PERFORMED OPERATIONAL TEST AMM 33-51-00-720-801 TEST IS OK.;[02] REPLACED AFT SERVICE DOOR UPPE
- [SDR SWAA2024010225670](https://openairdocs.org/sdr/SWAA2024010225670.md): Bulb · inoperative · Nov 28, 2023 · N461WN · Boeing 7377H4 · Emergency Lighting
  > FSD UPPER EMERGENCY EXIT FWD BULB IS BURNT OUT 2023-652354<[01] REPLACED UPPER EMERGENCY EXIT FWD BULB IAW: B737-700 SWPM 20-84-13 AND PERFORMED OPERATIONAL TEST AMM 33-51-00-720-801 TEST IS OK.;[02] REPLACED UPPER EMERGENCY EXIT FWD BULB IAW: B737-700 SWPM 20
- [SDR SWAA2024010315558](https://openairdocs.org/sdr/SWAA2024010315558.md): Slat Track · cracked · Oct 27, 2023 · N461WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ANGLE SLAT 1 INBOARD AUXILIARY SLAT TRACK AT LT WING 2023-652285<[01] REPLACED ANGLE SLAT 1 INBOARD AUXILIARY SLAT TRACK AT LT WING IAW B737-700 SRM 51-40-02;[02] REPLACED ANGLE SLAT 1 INBOARD AUXILIARY SLAT TRACK AT LT WING IAW B737-700 SRM 51-40-02
- [SDR SWAA2024010315557](https://openairdocs.org/sdr/SWAA2024010315557.md): Nut Plate · corroded · Oct 27, 2023 · N461WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CORROSION RAIL NUT INTERNAL CAVITY LEADING EDGE OFSS 292 AT RT WING 2023-652286<[01] REPLACED RAIL NUT INTERNAL CAVITY LEADING EDGE OFSS 292 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 112A4402 SHEET 8 REV.B;[02] REPLACED RAIL NUT INTERN
- [SDR SWAA2024010215250](https://openairdocs.org/sdr/SWAA2024010215250.md): Stringer · cracked · Oct 26, 2023 · N461WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK ON STRINGER 15L LOCATED AT BS 294.5 MORE 4 INCH AT FWD GALLEY AREA 2023-652267<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE: 15-FEB-24 WAS USED.;[02] REPAIRED STRINGER 15L LOCATED AT BS 294.5 MORE 4 INCH AT FWD GALLEY AREA IAW B737-700 SRM 53-00
- [SDR SWAA2024010313849](https://openairdocs.org/sdr/SWAA2024010313849.md): Support Angle · cracked · Oct 23, 2023 · N461WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS867 AND BETWEEN STR2R/STR3R AT PASSENGER CABIN 2023-652137<[01] REPLACED SUPPORT ANGLE LOCATED BS867 AND BETWEEN STR2R/STR3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND #DWG:146A7901 SHEET: 58 REV:-.;[
- [SDR SWAA2024010313489](https://openairdocs.org/sdr/SWAA2024010313489.md): Stringer · cracked · Oct 22, 2023 · N461WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 23L BS 540 FWD CARGO COMPARTMENT 2023-652103<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] TOOLS USED: TEMPERATURE CONTROL
- [SDR SWAA2024010313488](https://openairdocs.org/sdr/SWAA2024010313488.md): Stringer · cracked · Oct 22, 2023 · N461WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 26L BS 540 FWD CARGO COMPARTMENT 2023-652104<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] TOOLS USED: TEMPERATURE CONTROL
- [SDR SWAA2024010313490](https://openairdocs.org/sdr/SWAA2024010313490.md): Stringer · cracked · Oct 22, 2023 · N461WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 23R BS 540 FWD CARGO COMPARTMENT 2023-652105<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] TOOLS USED: TEMPERATURE CONTROL
- [SDR SWAA2024010313491](https://openairdocs.org/sdr/SWAA2024010313491.md): Stringer · cracked · Oct 22, 2023 · N461WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 25R BS 540 FWD CARGO COMPARTMENT 2023-652106<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] TOOLS USED: TEMPERATURE CONTROL
- [SDR SWAA2024010313492](https://openairdocs.org/sdr/SWAA2024010313492.md): Stringer · cracked · Oct 22, 2023 · N461WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 26R BS 540 FWD CARGO COMPARTMENT 2023-652107<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] TOOLS USED: TEMPERATURE CONTROL
- [SDR SWAA2024010313196](https://openairdocs.org/sdr/SWAA2024010313196.md): Stiffener · cracked · Oct 22, 2023 · N461WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK STIFFENER FLOOR STRUCTURE LOCATED BS947.5 AND STR26L AT AFT CARGO COMPARTMENT 2023-652097<[01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS947.5 AND STR26L AT AFT CARGO IWA B737-700 #DWG:186A8103 SHEET: 9 REV:- AND SRM 51-40-02 AND 51-10-02 Ï¿½TEM 9.<BR
- [SDR SWAA2024010313195](https://openairdocs.org/sdr/SWAA2024010313195.md): Web · corroded · Oct 22, 2023 · N461WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOCATED BTW BS727A TO BS727B AND RBL3.0 WL148.5 AT AFT CARGO COMPARTMENT 2023-652092<[01] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 221859911; DUE DATE: 07-NOV-23.;[02] EVALUATED REWORK AREA WEB LOCATED BTW BS727A TO BS727B AND RBL3.0 WL148.5 AT A
- [SDR SWAA2024010213668](https://openairdocs.org/sdr/SWAA2024010213668.md): Frame · cracked · Oct 22, 2023 · N461WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME BS 259.5 AND STRINGER 8R AT PASSENGER CABIN 2023-652122<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC600D; S/N: 220273012; DUE DATE: 17-DEC-23.;[02] REPAIRED FRAME BS 259.5 AND BTW STR 8R TO STR 12R AT PASSENGER CABIN IAW EA 23-153-03257 AND 23-153-03257
- [SDR SWAA2024010313178](https://openairdocs.org/sdr/SWAA2024010313178.md): Frame · cracked · Oct 21, 2023 · N461WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME LOCATED BS 727D BTW STRINGER 8L TO STRINGER 9L AT PASSENGER CABIN 2023-652063<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23.;[02] PERFORMED VISUAL INSPECTION ON AREA AND FOUND ONLY DIRTY AND PERFO
- [SDR SWAA2024010313194](https://openairdocs.org/sdr/SWAA2024010313194.md): Web · corroded · Oct 21, 2023 · N461WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOCATED BTW BS727A TO BS727B AND LBL3.0 WL148.5 AT AFT CARGO COMPARTMENT 2023-652091<[01] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 221859911; DUE DATE: 07-NOV-23.;[02] EVALUATED REWORK AREA WEB LOCATED BTW BS727A TO BS727B AND LBL3.0 WL148.5 AT A
- [SDR SWAA2024010213167](https://openairdocs.org/sdr/SWAA2024010213167.md): Battery Pack · inoperative · Oct 21, 2023 · N461WN · Boeing 7377H4 · Emergency Lighting
  > INOP LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA (2 EA) 2023-651813<[01] REPLACED LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA (2 EA) IAW: B737-700 AMM 33-51-06-960-805 TEST IS OK;[02] REPLACED LOWERED CEILING PANEL BATTERY PACK AT FWD GALLE
- [SDR SWAA2024010213188](https://openairdocs.org/sdr/SWAA2024010213188.md): Support Angle · cracked · Oct 21, 2023 · N461WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 7 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT 2023-652085<[01] REPLACED ANGLE LOCATED BS907 PLUS 7 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 1
- [SDR SWAA2024010213191](https://openairdocs.org/sdr/SWAA2024010213191.md): Support Angle · cracked · Oct 21, 2023 · N461WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 11 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT 2023-652086<[01] REPLACED ANGLE LOCATED BS907 PLUS 11 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG
- [SDR SWAA2024010213192](https://openairdocs.org/sdr/SWAA2024010213192.md): Frame · cracked · Oct 21, 2023 · N461WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME ON BS 907 BTW STR25R AND STR26R AFT CARGO COMPARTMENT 2023-652087<[01] REPLACED FRAME LOC. ON BS 907 BTW STR25R AND STR25L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A1007 SHEET 55 REV.-; 147A1007 SHEET 42 REV.D
- [SDR SWAA2024010213193](https://openairdocs.org/sdr/SWAA2024010213193.md): Support Angle · cracked · Oct 21, 2023 · N461WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS867 AND BTW STR26L / STR27L AFT CARGO COMPARTMENT 2023-652088<[01] REPLACED ANGLE - SUPPORT LOCATED BS867 AND BTW STR26L / STR27L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 <BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[02] CERTIFIED
- [SDR SWAA2024010213189](https://openairdocs.org/sdr/SWAA2024010213189.md): Cargo Track · cracked · Oct 21, 2023 · N461WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK RBBL 13.84 LOCATED BS727E AFT CARGO COMPARTMENT 2023-652089<[01] REPAIRED CARGO TRACK RBBL 13.84 LOCATED BS727E AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4. SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED ACTION 1<BR> REP
- [SDR SWAA2024010213190](https://openairdocs.org/sdr/SWAA2024010213190.md): Cargo Track · cracked · Oct 21, 2023 · N461WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK ON TRACK LBL 17.24 LOCATED BS727E AT AFT CARGO COMPARTMENT 2023-652090<[01] REPAIRED CARGO TRACK LOCATED AT LBL 17.24 BETWEEN STA 727D TO STA 767 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4. SEE INDIVIDUAL SIGN OFF BELOW;[02

Next page: https://openairdocs.org/aircraft/N461WN/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 = 'N461WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N461WN/reports

---
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.