# Service difficulty reports: N939WN

A list on [N939WN](https://openairdocs.org/aircraft/N939WN.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 4 · 200 reports

- [SDR SWAA2026081007254](https://openairdocs.org/sdr/SWAA2026081007254.md): Girt Bar · unpacked · Aug 6, 2026 · N939WN · Boeing 7377H4 · Emergency Equipment
  > FA REPORTS L1 GIRT BAR HARD TO RELEASE. REPACKED EXCESS GIRT MATERIAL AT BOTTOM OF SLIDE AMM 25-66-01. OP CHECK GOOD
- [SDR SWAA2026072304935](https://openairdocs.org/sdr/SWAA2026072304935.md): Flashlight · inoperative · Jul 19, 2026 · N939WN · Boeing 7377H4 · Emergency Equipment
  > FWD ENTRY NR 1 EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD ENTRY NR 1 EMERGENCY FLASHLIGHT REF AMM 25-64-00.
- [SDR SWAA2026061510979](https://openairdocs.org/sdr/SWAA2026061510979.md): Seat · out of adjust · Jun 11, 2026 · N939WN · Boeing 7377H4 · Passenger Compartment Equipment
  > PASSENGER CABIN SEAT 14B, WHICH IS IN AN EMERGENCY EXIT ROW, RECLINES AND SHOULDN`T. LOCKED OUT SEAT 14B RECLINE IAW CMM 25-21-45.
- [SDR SWAA2026020566854](https://openairdocs.org/sdr/SWAA2026020566854.md): Contact · dirty · Feb 1, 2026 · N939WN · Boeing 7377H4 · Equipment/Furnishings Wiring
  > AFT FA MEGAPHONE INOPERATIVE. CLEANED BATTERY CONTACTS AND ACCOMPLISHED MEGAPHONE OPS CHECK IAW AMM 25-64-00, CHECKED NORMAL.
- [SDR SWAA2026011961926](https://openairdocs.org/sdr/SWAA2026011961926.md): Seat · out of adjust · Jan 16, 2026 · N939WN · Boeing 7377H4 · Passenger Compartment Equipment
  > PASSENGER CABIN EMERGENCY EXIT ROW SEAT 14B RECLINES. LOCKED OUT 14B SEAT RECLINE IAW CMM 25-21-42
- [SDR SWAA2025120134400](https://openairdocs.org/sdr/SWAA2025120134400.md): Fitting · cracked · Nov 11, 2025 · N939WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > RIB FITTING IS CRACKED AT STAB BL 281.81 RH SIDE. PERFOMED REPAIR IAW SRM 55-10-90-2R-1-A01330, REPAIR 1.
- [SDR SWAA2025090209425](https://openairdocs.org/sdr/SWAA2025090209425.md): Seal · cracked · Aug 29, 2025 · N939WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LH HORIZONTAL STAB UPPER FWD SLIDER SEAL IS CRACKED. REMOVED AND REPLACED SEAL PER AMM 53-31-31.
- [SDR SWAA2025090209426](https://openairdocs.org/sdr/SWAA2025090209426.md): Seal · cracked · Aug 29, 2025 · N939WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RH HORIZONTAL STAB UPPER FWD SLIDER SEAL CRACKED. REMOVED AND REPLACED SEAL PER AMM 53-31-31.;[02] C/W INSPECTION
- [SDR SWAA2025040219829](https://openairdocs.org/sdr/SWAA2025040219829.md): Web · cracked · Mar 30, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED BTW BS440 TO BS BS460 AT LEVEL S-25L FWD CARGO COMPARTMENT 2025-203869<[01] FABRICATED WEB LOCATED BTW BS440 TO BS BS460 AT LEVEL S-25L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-05; SRM 51-20-01; SRM 51-30-01 AND DWG 143A7510 REV C. SEE
- [SDR SWAA2025040709653](https://openairdocs.org/sdr/SWAA2025040709653.md): Angle · damaged · Mar 18, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE ANGLE LOCATE BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT 2025-203852<[01] REPLACED ANGLE AND LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND D
- [SDR SWAA2025040706455](https://openairdocs.org/sdr/SWAA2025040706455.md): Lens · misinstalled · Mar 17, 2025 · N939WN · Boeing 7377H4 · Emergency Lighting
  > INCORRECTLY EMERGENCY LIGHT LENS GALLEY 1 AT FWD GALLEY AREA 2025-203843<[01] REPLACED EMERGENCY LIGHT LENS GALLEY AREA 1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 STEP 2.C.(1).(A)(2) AND (3).(4);[02] JOB COMPLETED
- [SDR SWAA2025040706454](https://openairdocs.org/sdr/SWAA2025040706454.md): Lens · wrong part · Mar 17, 2025 · N939WN · Boeing 7377H4 · Emergency Lighting
  > INCORRECTLY EMERGENCY LIGHT LENS GALLEY 4 AT AFT GALLEY AREA 2025-203844<[01] REPLACED EMERGENCY LIGHT LENS GALLEY 4 AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 STEP 2.C.(1).(A)(2) AND (3).(4);[02] JOB COMPLETED
- [SDR SWAA2025040705828](https://openairdocs.org/sdr/SWAA2025040705828.md): Support · corroded · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203782<
- [SDR SWAA2025040715603](https://openairdocs.org/sdr/SWAA2025040715603.md): Shield · corroded · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT 2025-203783<[01] REPLACED SHIELD WEB AND FASTENERS LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-0
- [SDR SWAA2025040715604](https://openairdocs.org/sdr/SWAA2025040715604.md): Support · corroded · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BETWEEN BS727C TO BS807 LBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203784<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 LBL 21 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DW
- [SDR SWAA2025040705829](https://openairdocs.org/sdr/SWAA2025040705829.md): Shield · corroded · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT 2025-203783<
- [SDR SWAA2025040705827](https://openairdocs.org/sdr/SWAA2025040705827.md): Support Angle · cracked · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED STA947.5 AND LBL11 AT AFT CARGO COMPARTMENT 2025-203797<[01] REPLACED ANGLE - SUPPORT LOCATED STA947.5 AND LBL11 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02 AND DWG # 149A8103 SHEET 7 REV:
- [SDR SWAA2025040715592](https://openairdocs.org/sdr/SWAA2025040715592.md): Pressure Deck · cracked · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 30 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH 0.250 INCH APPROXIMATELY.) 2025-203749<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138103; DUE DATE: 10-JUN-25.;[02] TOOL USED:
- [SDR SWAA2025040705528](https://openairdocs.org/sdr/SWAA2025040705528.md): Pressure Deck · cracked · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 41 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH 0.312 INCH APPROXIMATELY.) 2025-203751<[01] ON STEP 6 AND 7: TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101V022240; DUE DATE: 28 MAR 25;[0
- [SDR SWAA2025040705527](https://openairdocs.org/sdr/SWAA2025040705527.md): Pressure Deck · cracked · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 30 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH 0.250 INCH APPROXIMATELY.) 2025-203749<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138103; DUE DATE: 10-JUN-25.;[02] TOOL USED:
- [SDR SWAA2025040705833](https://openairdocs.org/sdr/SWAA2025040705833.md): Floorbeam · corroded · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ANGLE FLOOR STRUCTURE LOCATED STA947.5 AND RBL4 WL156 AT AFT CARGO COMPARTMENT 2025-203796<
- [SDR SWAA2025040705681](https://openairdocs.org/sdr/SWAA2025040705681.md): Floorbeam · cracked · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK LOWER ANGLE FLOOR STRUCTURE BS 695 AND RBL 24.75 CENTER SECTION 2025-203648<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 29-JAN-26.
- [SDR SWAA2025040705836](https://openairdocs.org/sdr/SWAA2025040705836.md): Rib · cracked · Mar 15, 2025 · N939WN · Boeing 7377H4 · Vertical Stabilizer, Spar/Rib
  > CRACK RIB 8 ON ACCESS PANEL 321A AT VERTICAL STABILIZER 2025-203809<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26.;[02] REPLACED RIB 8 AND FASTENERS LOCATED ON PANEL 312A AT VERTICAL STABILIZER IAW B737-700 S
- [SDR SWAA2025040715599](https://openairdocs.org/sdr/SWAA2025040715599.md): Angle · cracked · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK LOWER ANGLE FLOOR STRUCTURE BS 695 AND RBL 24.75 CENTER SECTION 2025-203648<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 29-JAN-26.
- [SDR SWAA2025040705830](https://openairdocs.org/sdr/SWAA2025040705830.md): Support · corroded · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BETWEEN BS727C TO BS807 LBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203784<
- [SDR SWAA2025040405831](https://openairdocs.org/sdr/SWAA2025040405831.md): Track · cracked · Mar 15, 2025 · N939WN · Boeing 7377H4 · Cargo Compartments
  > CRACK CARGO TRACK RBBL 13.84 LOCTAED BS727E AFT CARGO COMPARTMENT 2025-203785 <[01]. STEP 5 AND 6 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATE: 27-AUG-25; [02] INSTALLED PERMANENT REPAIR PARTS [1] TRACK EXTRUSION [2] TRACK SPLICE
- [SDR SWAA2025040205832](https://openairdocs.org/sdr/SWAA2025040205832.md): Cargo Track · cracked · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK CARGO TRACK RBBL 13.84 LOCATED BS727C AFT CARGO COMPARTMENT 2025-203786<[01] STEP 4 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATE: 27-AUG-25;[02] STEP 5 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATE
- [SDR SWAA2025040205826](https://openairdocs.org/sdr/SWAA2025040205826.md): Cargo Track · cracked · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK CARGO TRACK LBBL 17.24 LOCATED BS727E AFT CARGO COMPARTMENT 2025-203789<[01] STEP 4 AND 5 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATE: 27-AUG-25;[02] REPAIRED CARGO TRACK LOCATED BS 727D + 13? TO BS 727E + 11? LBL 17.24 AT A
- [SDR SWAA2025040215605](https://openairdocs.org/sdr/SWAA2025040215605.md): Floor Support · corroded · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ANGLE FLOOR STRUCTURE LOCATED STA947.5 AND RBL4 WL156 AT AFT CARGO COMPARTMENT 2025-203796<[01] REPLACED ANGLE FLOOR STRUCTURE AND FASTENERS LOCATED STA947.5 AND RBL4 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AN
- [SDR SWAA2025040215602](https://openairdocs.org/sdr/SWAA2025040215602.md): Support · corroded · Mar 15, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203782<[01] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BETWEEN BS727 TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND S
- [SDR SWAA2025040705346](https://openairdocs.org/sdr/SWAA2025040705346.md): Shield · damaged · Mar 14, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE ON SHIELD WEB LOCATED BETWEEN STA492.4 TO STA500A AND RBL21 AT FWD CARGO COMPARTMENT 2025-203697<[01] REPLACED SHIELD WEB LOCATED BTW BS 492.4 TO BS 500A AND RBL 21 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG # 143A0080; SHEET 33
- [SDR SWAA2025040705507](https://openairdocs.org/sdr/SWAA2025040705507.md): Flashlight · inoperative · Mar 14, 2025 · N939WN · Boeing 7377H4 · Emergency Equipment
  > INOP WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) 2025-203706<[01] REPLACED WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-SWA-807 AND DWG 25600001 REV K;[02] CORRECTED ITEM 1 <BR><BR>REPLACED WINDSCREE
- [SDR SWAA2025040715570](https://openairdocs.org/sdr/SWAA2025040715570.md): Stringer Clip · cracked · Mar 14, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2025-203695<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D AND STRINGER 19L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG # 143A7902; SHEET 209; REV -.<BR>SEE
- [SDR SWAA2025040705347](https://openairdocs.org/sdr/SWAA2025040705347.md): Angle · cracked · Mar 14, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED STA440 AND STR26L FWD CARGO COMPARTMENT 2025-203694<
- [SDR SWAA2025040705348](https://openairdocs.org/sdr/SWAA2025040705348.md): Stringer Clip · cracked · Mar 14, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2025-203695<
- [SDR SWAA2025040715569](https://openairdocs.org/sdr/SWAA2025040715569.md): Angle · cracked · Mar 14, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED STA440 AND STR26L FWD CARGO COMPARTMENT 2025-203694<[01] REPLACED ANGLE CLIP LOCATED BS 440 STRINGER 26L AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG # 143A7505 SHEET 118. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED A
- [SDR SWAA2025040715571](https://openairdocs.org/sdr/SWAA2025040715571.md): Stringer · cracked · Mar 14, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 23L LOCATED STA540 FWD CARGO COMPARTMENT 2025-203705<[01] TOOL USED ON STEP 6. ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] REPAIRED STRINGER 23L LOCATED BS 500D PLUS 10 INCHES TO BS 540 IAW BOEING 737-700 SRM 5
- [SDR SWAA2025040705506](https://openairdocs.org/sdr/SWAA2025040705506.md): Stringer · cracked · Mar 14, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 23L LOCATED STA540 FWD CARGO COMPARTMENT 2025-203705<[01] TOOL USED ON STEP 6. ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] REPAIRED STRINGER 23L LOCATED BS 500D PLUS 10 INCHES TO BS 540 IAW BOEING 737-700 SRM 5
- [SDR SWAA2025040415572](https://openairdocs.org/sdr/SWAA2025040415572.md): Flashlight · inoperative · Mar 14, 2025 · N939WN · Boeing 7377H4 · Emergency Equipment
  > INOP WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) 2025-203706 <[01]. REPLACED WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-SWA-807 AND DWG 25600001 REV K; [02] CORRECTED ITEM 1. REPLACED WINDSCREEN
- [SDR SWAA2025040705002](https://openairdocs.org/sdr/SWAA2025040705002.md): Stub Frame · cracked · Mar 13, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.375 IN. APROX.AT PASSENGER CABIN 2025-203649<[01] REPLACED STUB FRAME AND FASTENERS LOC. BETWEEN STR7R TO STR11R AT FWD GALLEY AREA IAW B737-700 SRM 51-1
- [SDR SWAA2025040715564](https://openairdocs.org/sdr/SWAA2025040715564.md): Stub Frame · cracked · Mar 13, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.375 IN. APROX.AT PASSENGER CABIN 2025-203649<[01] REPLACED STUB FRAME AND FASTENERS LOC. BETWEEN STR7R TO STR11R AT FWD GALLEY AREA IAW B737-700 SRM 51-1
- [SDR SWAA2025040705001](https://openairdocs.org/sdr/SWAA2025040705001.md): Floorbeam · cracked · Mar 13, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN LBL 24.75 TO LBL 45.5 AT PASSENGER CABIN 2025-203646<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN LBL 24.75 TO LBL 45.5 AT PASSENGER CABIN B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG 1
- [SDR SWAA2025040705003](https://openairdocs.org/sdr/SWAA2025040705003.md): Floorbeam · cracked · Mar 13, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN RBL 24.75 TO RBL 45.5 AT PASSENGER CABIN 2025-203647<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN RBL 24.75 TO RBL 45.5 AT PASSENGER CABIN. B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG
- [SDR SWAA2025040715563](https://openairdocs.org/sdr/SWAA2025040715563.md): Floorbeam · cracked · Mar 13, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN 2025-203644<[01] REPLACED FLOOR STRUCTURE BRAKE PANEL AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM-51-40-02-0G; B737-700 SRM-
- [SDR SWAA2025040715565](https://openairdocs.org/sdr/SWAA2025040715565.md): Floorbeam · cracked · Mar 13, 2025 · N939WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN RBL 24.75 TO RBL 45.5 AT PASSENGER CABIN 2025-203647<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN RBL 24.75 TO RBL 45.5 AT PASSENGER CABIN. B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG
- [SDR SWAA2025040705197](https://openairdocs.org/sdr/SWAA2025040705197.md): Support · cracked · Mar 13, 2025 · N939WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK BLADE SUPPORT STRUCTURE OF THE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER 2025-203656<[01] REPLEACED BLADE SUPPORT STRUCTURE OF THE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] CORREDTED STEP 1 REP
- [SDR SWAA2025040404999](https://openairdocs.org/sdr/SWAA2025040404999.md): Panel · cracked · Mar 13, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN 2025-203644 <[01]. REPLACED FLOOR STRUCTURE BRAKE PANEL AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM-51-40-02-0G; B737-700 S
- [SDR SWAA2025040405000](https://openairdocs.org/sdr/SWAA2025040405000.md): Panel · cracked · Mar 13, 2025 · N939WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN 2025-203645 <[01]. REPLACED FLOOR STRUCTURE BRAKE PANEL AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM-51-40-02-0G; B737-700 S
- [SDR SWAA2025040715555](https://openairdocs.org/sdr/SWAA2025040715555.md): Access Panel · cracked · Mar 12, 2025 · N939WN · Boeing 7377H4 · Aerodynamic Fairings
  > CRACK ACCESS PANEL 191D AT LOWER FUSELAGE 2025-203626<[01] TOOL USED CALIPER PN: 8647A43; SN: B22440130; DUE DATE: 20/SEP/25.;[02] TOOL USED; HOT BONDER PN: HCS9200B; SN: 16122983; DUE DATE: 22-FEB-26.;[03] TOOL USED; SCALE PN: SCA-301; SN: AE-412135; DUE DATE
- [SDR SWAA2025040704618](https://openairdocs.org/sdr/SWAA2025040704618.md): Access Panel · cracked · Mar 12, 2025 · N939WN · Boeing 7377H4 · Aerodynamic Fairings
  > CRACK ACCESS PANEL 191D AT LOWER FUSELAGE 2025-203626<[01] TOOL USED CALIPER PN: 8647A43; SN: B22440130; DUE DATE: 20/SEP/25.;[02] TOOL USED; HOT BONDER PN: HCS9200B; SN: 16122983; DUE DATE: 22-FEB-26.;[03] TOOL USED; SCALE PN: SCA-301; SN: AE-412135; DUE DATE

Next page: https://openairdocs.org/aircraft/N939WN/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 = 'N939WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N939WN/reports

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