# Service difficulty reports: N932WN

A list on [N932WN](https://openairdocs.org/aircraft/N932WN.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 · 187 reports

- [SDR SWAA2026073054497](https://openairdocs.org/sdr/SWAA2026073054497.md): Pump · faulted · Jul 28, 2026 · N932WN · Boeing 7377H4 · Engine Fuel Pump
  > NR 2 ENGINE WOULD NOT PRODUCE TAKEOFF THRUST. 87.4 N1 REQUIRED. 83.7 PRODUCED. R & R 773-11-00 FUEL PUMP PACKAGE IAW TASK (REM/INST - FUEL PUMP PACKAGE) ON TTG8Q01DECXX. REQUIRES LEAK CHECK, R & R 773-11-00 FUEL PUMP PACKAGE PER TASK (REM/INST - FUEL PUMP PACK
- [SDR SWAA2026073033178](https://openairdocs.org/sdr/SWAA2026073033178.md): Hmu · faulted · Jul 28, 2026 · N932WN · Boeing 7377H4 · Fuel Controlling System
  > NR 2 ENGINE WOULD NOT PRODUCE TAKEOFF THRUST. 87.4 N1 REQUIRED. 83.7 PRODUCED. R & R 773-11-00 FUEL PUMP PACKAGE PER TASK (REM/INST - FUEL PUMP PACKAGE) ON TTG8Q01DECXX. REQUIRES LEAK CHECK R&R 773-11-00 FUEL PUMP PACKAGE PER TASK (REM/INST - FUEL PUMP PACKAG
- [SDR SWAA2026042391075](https://openairdocs.org/sdr/SWAA2026042391075.md): Scuff Plate · cracked · Apr 19, 2026 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > R1 DOOR SCUFF PLATE CRACKED ON AFT CORNER. REMOVED R1 DOOR SCUFF PLATE IAW AMM 53-11-01. INSTALLED R1 DOOR SCUFF PLATE PER EA 26-153-01069 AND AMM 53-11-01. LEAK CHECK GOOD OF R1 SCUFF PLATE REF AMM 53-11-01.
- [SDR SWAA2026030976706](https://openairdocs.org/sdr/SWAA2026030976706.md): Support Angle · cracked · Mar 5, 2026 · N932WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LEFT WING TRAILING EDGE WEB SUPPORT ANGLE, ATTACHED TO FLAP DEFLECTION RIB AND AFT OF NR 1 ENGINE PYLON CRACKED IN RADIUS. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02.
- [SDR SWAA2025122253197](https://openairdocs.org/sdr/SWAA2025122253197.md): Rib · cracked · Dec 17, 2025 · N932WN · Boeing 7377H4 · Turbine Engine Air Inlet Section
  > #1 ENG OUTER LINER HAS ONE CRACK THAT GOES ACROSS 3 AND A HALF PANELS AT S10 (RIGHT IGNITOR). COLD SIDE INSPECTION SHOWS RIBS 4;5 AND 6 ARE CRACKED. OKAY TO CONTINUE; CIS FOR 25 CYCLES FOR ENGINE REPLACEMENT PER AMM 72-00-00-200-805-F00. REF TSR-20250010142.
- [SDR SWAA2025101323252](https://openairdocs.org/sdr/SWAA2025101323252.md): Lock · out of adjust · Oct 10, 2025 · N932WN · Boeing 7377H4 · Passenger Compartment Equipment
  > PASSENGER SEAT 11D RECLINES INTO EMERGENCY EXIT ROW. ADJUSTED HYDROLOCK PER CMM 25-21-42.
- [SDR SWAA2025100821773](https://openairdocs.org/sdr/SWAA2025100821773.md): Tab · broken · Oct 5, 2025 · N932WN · Boeing 7377H4 · Emergency Lighting
  > F/A REPORT AFT RT SERVICE DOOR, EMERGENCY EXIT SIGN COVER FELL OFF. BASE TAB BROKEN OFF. COMPLIED EA M-21-133-00720; EMERGENCY EXIT LIGHT OPS CHECK GOOD.
- [SDR SWAA2025100219334](https://openairdocs.org/sdr/SWAA2025100219334.md): Cover · detached · Sep 29, 2025 · N932WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT COVER NEXT TO AFT SERVICE DOOR CAME OFF. REPLACED BROKEN LIGHT COVER IAW AMM 33-51-01.
- [SDR SWAA2025041422440](https://openairdocs.org/sdr/SWAA2025041422440.md): Lamp · inoperative · Apr 8, 2025 · N932WN · Boeing 7377H4 · Emergency Lighting
  > ROW 20 ABC EMERGECY LIGHT INOP<[01] RELAMPED EMERGENCY AISLE LIGHT AT ROW 20 ABC NO FIX. NO LIGHT ASSY IN STOCK. RELAMPED IAW AMM 33-51-03. OKAY TO CONTINUE ON MEL 33-15-02. SP1 AUTH# 246236.;[02] REPLACED LIGHT ASSY PER AMM 33-51-03. NO FIX. TS AND FOUND GROU
- [SDR SWAA2024121060849](https://openairdocs.org/sdr/SWAA2024121060849.md): Support · cracked · Nov 17, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS 727 BETWEEN S-27L TO S-27R AFT CARGO COMPARTMENT 2024-715126<[01] REPLACED ANGLE SUPPORT LOCATED BS 727 BETWEEN S-27L TO S-27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 144A2600 SHEET: 712 RE
- [SDR SWAA2024121060850](https://openairdocs.org/sdr/SWAA2024121060850.md): Battery Pack · inoperative · Nov 17, 2024 · N932WN · Boeing 7377H4 · Emergency Lighting
  > INOP BATTERY PACKS ON POSITION (M1669) (M1668) AND (M1670) AT PASSENGER CABIN (3EA) 2024-715127<[01] REMOVED AND REPLACED BATTERY PACKS ON POSITION (M1669) (M1668) AND (M1670) AT PASSENGER CABIN (3EA. IAW B737-700 AMM 33-51-06-960-805. TEST IS OK.<BR>SEE INDIV
- [SDR SWAA2024121060841](https://openairdocs.org/sdr/SWAA2024121060841.md): Strap · corroded · Nov 17, 2024 · N932WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRAP LOCATED BS 887 BETWEEN S-25R TO S-25L AFT CARGO COMPARTMENT 2024-715124<[01] REPLACED STRAP LOCATED BS 887 BETWEEN STRINGER 25R TO STRINGER 25L AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-10-02 ITEM 9; AND BOEING 737-700 DWG 146A940Q SHEET
- [SDR SWAA2024121060845](https://openairdocs.org/sdr/SWAA2024121060845.md): Angle · cracked · Nov 17, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS 907 TO BS 927 AFT POSITION BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT 2024-715121<[01] REPLACED ANGLE AND FASTENERS BETWEEN BS907 TO BS927 AFT POSITION IAW B737-700 SRM 51-40-02 AND DRAWING 147A7221 SHEET 24 REV ?.SEE INDIVIDUAL STEP S
- [SDR SWAA2024121060846](https://openairdocs.org/sdr/SWAA2024121060846.md): Angle · cracked · Nov 17, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS 867 AND S-26L AFT CARGO COMPARTMENT 2024-715120<[01] REPLACED ANGLE LOCATED BS 867 AND S-26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 149A8102 SHEET 18 REV-; DWG 149A8104 SHEET 1 REV B. MEASURE OF CRAC
- [SDR SWAA2024121060848](https://openairdocs.org/sdr/SWAA2024121060848.md): Support · corroded · Nov 17, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED 747 PLUS 10 INCH LBL 21 WL 156 AFT CARGO COMPARTMENT 2024-715115<[01] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BSTA 727 PLUS 4 INCHES TO BSTA 847 LBL 21 WL 156 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-5 FIGURE 202
- [SDR SWAA2024121060843](https://openairdocs.org/sdr/SWAA2024121060843.md): Support · cracked · Nov 17, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS947.5 AND S-26L AFT CARGO COMPARTMENT 2024-715123<[01] REPLACED ANGLE - SUPPORT AND FASTENERS LOCATED BS947.5 AND S-26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 149A8103 SHEET 7 REV A SEE INDIVIDUAL SIGN OFF BELOW
- [SDR SWAA2024120960844](https://openairdocs.org/sdr/SWAA2024120960844.md): Web · cracked · Nov 17, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BS927 TO BS 947 AND S-25R AFT CARGO COMPARTMENT 2024-715122<[01] REOLACED WEB - INTERCOSTAL LOCATED BS927 TO BS 947 AND S-25R AFT CARGO COMPARTMENT IAW B737-700 SRM 1-10-02 AND DWG 147A7500 SHEET 29 REV - SEE INDIVIDUAL SIGN OFF
- [SDR SWAA2024120960847](https://openairdocs.org/sdr/SWAA2024120960847.md): Support · corroded · Nov 17, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BS 727E PLUS 10 INCH RBL 21 WL 156 AFT CARGO COMPARTMENT 2024-715118<[01] REPLACED SUPPORT ZEE AND SPLICE SIDE PLATE (2 E/A) LOCATED BS 727C PLUS 11 INCH TO BS 767 RBL 21 WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0
- [SDR SWAA2024120975342](https://openairdocs.org/sdr/SWAA2024120975342.md): Plate · corroded · Nov 17, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BS 727E PLUS 10 INCH RBL 21 WL 156 AFT CARGO COMPARTMENT 2024-715118<[01] REPLACED SUPPORT ZEE AND SPLICE SIDE PLATE (2 E/A) LOCATED BS 727C PLUS 11 INCH TO BS 767 RBL 21 WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0
- [SDR SWAA2024121060475](https://openairdocs.org/sdr/SWAA2024121060475.md): Scuff Plate · cracked · Nov 16, 2024 · N932WN · Boeing 7377H4 · Rotorcraft Tail Boom
  > CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2024-715085<[01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A23272257; DUE DATE: 15-JAN-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N:185943; DUE DATE: 10/MAR/25;[03] TOOL USED RADI
- [SDR SWAA2024121060480](https://openairdocs.org/sdr/SWAA2024121060480.md): Angle · cracked · Nov 16, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS 500D AND S-28R FWD CARGO COMPARTMENT 2024-715102<[01] REPLACED ANGLE LOCATED BSTA 500D AND S-28R. FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9. AND DWG 143A7902 SHEET 126. REV. ?A? SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRE
- [SDR SWAA2024121060476](https://openairdocs.org/sdr/SWAA2024121060476.md): Fairing · cracked · Nov 16, 2024 · N932WN · Boeing 7377H4 · Nacelle/Pylon, Attach Fittings
  > CRACK LOCATED ON AFT PYLON AFT STRUT SUPPORT FAIRING ENGINE 2 2024-715088<[01] PLACED AFT STRUT FAIRING ASSY LOCATED ON AFT PYLON AT ENGINE 2. IAW B737-700 SRM 51-10-02 PARAGRAPH 9. SRM 51-40-02 AND DWG 313A2400 SHEET 35 REV ?A?. SEE INDIVIDUAL SIGN OFF BELOW;
- [SDR SWAA2024121060674](https://openairdocs.org/sdr/SWAA2024121060674.md): Angle · elongated · Nov 16, 2024 · N932WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > ELONGATED HOLE SUPPORT ANGLE OUTBOARD FAN COWL LOC. INTERNAL AREA ACCESS DOOR 424AR AT ENGINE 2 2024-715113<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED OUTBOARD FAN COWL LOC. INTERNAL AREA ACCESS DOOR 424AR AT ENGINE 2 I.A.W B737-700 SRM 51-10-02; SRM 51
- [SDR SWAA2024120960479](https://openairdocs.org/sdr/SWAA2024120960479.md): Web · cracked · Nov 16, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BS500D TO BS 520 AND S-28R FWD CARGO COMPARTMENT 2024-715101<[01] REPLACED WEB-INTERCOSTAL LOCATED BSTA 500D TO BSTA 520 AND S-28R. FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 PARAGRAPH 9. AND DWG 143A7902 SHEET 126. REV. ?
- [SDR SWAA2024121059894](https://openairdocs.org/sdr/SWAA2024121059894.md): Angle · cracked · Nov 14, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED AFT FACE BS 695 BL 0 RT SIDE AT CENTER SECTION 2024-714996<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AFT FACE BS 695 BL 0 RT SIDE AT CENTER SECTION I.A.W B737-700 SRM 51-10-02; 51-40-02 AND DWG 273A9110 SHEET: 6; REV: A.
- [SDR SWAA2024121059898](https://openairdocs.org/sdr/SWAA2024121059898.md): Gusset · cracked · Nov 14, 2024 · N932WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2024-715028<[01] INSTALLED NEW GUSSET AND FASTENERS LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV - AND SRM 51-10-02 ITEM 9 SEE INDIVIDUAL
- [SDR SWAA2024121059897](https://openairdocs.org/sdr/SWAA2024121059897.md): Gusset · cracked · Nov 14, 2024 · N932WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2024-715029<[01] INSTALLED NEW GUSSET AND FASTENERS LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV - AND SRM 51-10-02 ITEM 9 SEE INDIVIDUAL
- [SDR SWAA2024121059895](https://openairdocs.org/sdr/SWAA2024121059895.md): Bracket · cracked · Nov 14, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-714979<[01] REPLACED BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 146A7901 SHEET 66
- [SDR SWAA2024121059896](https://openairdocs.org/sdr/SWAA2024121059896.md): Seal · broken · Nov 14, 2024 · N932WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > BROKEN SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB 2024-714994<[01] REPLACED SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] CERTIFIED CORRECTIVE ACTION.
- [SDR SWAA2024120960041](https://openairdocs.org/sdr/SWAA2024120960041.md): Web · corroded · Nov 14, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOCATED BETWEEN BS420 TO BS440; RBL21 AND WL156 AT FWD CARGO COMPARTMENT 2024-715041<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS420 TO BS440; RBL21 AND WL156 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND D
- [SDR SWAA2024120960040](https://openairdocs.org/sdr/SWAA2024120960040.md): Web · cracked · Nov 14, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BS500C AND LBL21 FWD CARGO COMPARTMENT 2024-715040<[01] REPLACED WEB-INTERCOSTAL LOCATED BSTA 500C AND LBL 21 FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02. PARAGRAPH 9. SRM 51-40-02. AND DWG 143A7505. SHEET 82. REV. ?-?. SEE
- [SDR SWAA2024121059528](https://openairdocs.org/sdr/SWAA2024121059528.md): Intercostal · cracked · Nov 13, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL LOCATED BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN 2024-714908<[01] REPLACED INTERCOSTAL LOCATED BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 46 REV. -<BR>SEE IND
- [SDR SWAA2024121059529](https://openairdocs.org/sdr/SWAA2024121059529.md): Access Panel · cracked · Nov 13, 2024 · N932WN · Boeing 7377H4 · Aerodynamic Fairings
  > CRACK ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR 2024-714909<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: B20189521 DUE DATE: 26-JAN-25.;[02] TOOL USED: SCALE PN:SPX621 SN:8340225441 DUE DATE: 02-JUL-25.;[03] REPAIRED ACCESS PANEL 191D BODY FAIRING AT
- [SDR SWAA2024120959526](https://openairdocs.org/sdr/SWAA2024120959526.md): Plate · cracked · Nov 13, 2024 · N932WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON PLATE LOCATED UPPER EDGE RT SIDE AT COCKPIT DOOR POST 2024-714900<[01] REPLACED PLATE LOCATED UPPER EDGE RT SIDE AT COCKPIT DOOR POST IAW B737-700 SRM 51-10-02.;[02] COMPLETED
- [SDR SWAA2024121058995](https://openairdocs.org/sdr/SWAA2024121058995.md): Strip · deteriorated · Nov 12, 2024 · N932WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT STRIP (10FT) AT PASSENGER CABIN 2024-714843<[01] REPLACED PHOTOLUMINESCENT STRIP (10FT) AT PASSENGER CABIN I.A.W SOPM 20-50-12 REV. 56;[02] CERTIFIED COMPLETE TASK
- [SDR SWAA2024121058998](https://openairdocs.org/sdr/SWAA2024121058998.md): Vapor Barrier · cracked · Nov 12, 2024 · N932WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACK VAPOR BARRIER RH SIDE BS 663 RBL 42 AT MAIN WHEEL WELL COMPARTMENT 2024-714848<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189521; DUE DATE: 26-JAN-25;[02] TOOL USED: HOT BONDER PN: HCS9000B; SN: 18175469; DUE DATE: 14-AUG-25.;[03] ULTRASONIC EQUIPM
- [SDR SWAA2024081926183](https://openairdocs.org/sdr/SWAA2024081926183.md): Fairing · cracked · Aug 15, 2024 · N932WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > RIGHT # 2 ENGINE NACELLE STRUT FAIRING AFT CASTING CRACKED MARKED VERIFIED PER NDT PART 6 51-00-00 PROCEDURE 23<[01] ACCOMPLISHED TIME LIMITED REPAIR PER EA M-23-154-01884;[02] INSPECTION C/W.ACCOMPLISHED TIME LIMITED REPAIR PER EA M-23-154-01884
- [SDR SWAA2024081626035](https://openairdocs.org/sdr/SWAA2024081626035.md): Web · cracked · Aug 15, 2024 · N932WN · Boeing 7377H4 · Landing Gear Doors
  > RMLG CENTER DOOR WEB CRACKED- SEE PIC<[01] REMOVED R/H MLG CENTER AND INNER DOOR PER AMM 32-13-11 OK TO CONTINUE PER CDL 32-10-3 AUTH # 2090430
- [SDR SWAA2024070206840](https://openairdocs.org/sdr/SWAA2024070206840.md): Doubler · cracked · Jun 28, 2024 · N932WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > EGPR DOUBLER CRACKED AT DOOR CUTOUT<[01] PERFORMED REPAIR AT EGPR DOOR DOUBLER IAW SRM 53-10-15-2R-4 FIGURE 204 REPAIR 4. SEE BARCODE NUMBER TTG8Q00U2Y1K FOR MATERIAL ORDERED.
- [SDR SWAA2024061903284](https://openairdocs.org/sdr/SWAA2024061903284.md): Slide · out of adjust · Jun 19, 2024 · N932WN · Boeing 7377H4 · Escape Slide
  > AIRCRAFT LEFT AFT SLIDE APPEAR TO BE UNTUCKED<[01] TUCKED AND PERFORMED INSPECTION OF THE L/H AFT EMERGENCY DOOR SLIDE NO DEFECT NOTED REF B737NG 700 AMM 25-66-01.
- [SDR SWAA2024030457562](https://openairdocs.org/sdr/SWAA2024030457562.md): Sensor · malfunctioned · Feb 29, 2024 · N932WN · Boeing 7377H4 · Cabin Cooling System
  > BURNING SMELL NOTED AT CRUISE R/H PACK.<[01] PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION; NO DEFECTS NOTED IAW AMM 5-51-56; FIM 21-00 TASK 806. CREW ALSO REPORTED RT. RAM DOOR FULL OPEN LIGHT CYCLING IN FLIGHT. PERFORMED FIM 21-51 TASK 803; REPLAC
- [SDR SWAA2024030458807](https://openairdocs.org/sdr/SWAA2024030458807.md): A/C Pack · fumes · Feb 29, 2024 · N932WN · Boeing 7377H4 · Cabin Cooling System
  > BURNING SMELL NOTED AT CRUISE R/H PACK.<[01] PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION; NO DEFECTS NOTED IAW AMM 5-51-56; FIM 21-00 TASK 806. CREW ALSO REPORTED RT. RAM DOOR FULL OPEN LIGHT CYCLING IN FLIGHT. PERFORMED FIM 21-51 TASK 803; REPLAC
- [SDR SWAA2024020546666](https://openairdocs.org/sdr/SWAA2024020546666.md): Panel · debonded · Jan 30, 2024 · N932WN · Boeing 7377H4 · Aerodynamic Fairings
  > FUSELAGE BODY PANEL #193B IS CHAFED AND DISBONDED AROUND FASTENER HOLES<[01] LOCATE AND DRILLED A NEW PANEL 193B PER SRM 51-40-02.
- [SDR SWAA2023101108845](https://openairdocs.org/sdr/SWAA2023101108845.md): Megaphone · corroded · Oct 9, 2023 · N932WN · Boeing 7377H4 · Emergency Equipment
  > FWD MEGAPHONE REQ INSP BY DEC 2023<[01] FOUND CORROSION IN BATTERY COMPARTMENT OF FWD MEGAPHONE. REMOVED AND REPLACED FWD MEGAPHONE IAW AMM 25-64-00. OPS CK GOOD. NEW EXP IS OCT 2024
- [SDR SWAA2023100908394](https://openairdocs.org/sdr/SWAA2023100908394.md): Slide · low pressure · Oct 6, 2023 · N932WN · Boeing 7377H4 · Escape Slide
  > CA SIDE AFT EVACUATION SLIDE LOW PRESSURE<[01] R&R AFT ENTRY DOOR SLIDE IAW MT# 725-240-00-00.
- [SDR SWAA2023041126036](https://openairdocs.org/sdr/SWAA2023041126036.md): Megaphone · inoperative · Apr 10, 2023 · N932WN · Boeing 7377H4 · Emergency Equipment
  > CREW REPORTED FWD MEGAPHONE INOP<[01] REMOVED AND REPLACED FWD MEGAPHONE AND BATTERIES REF AMM 25-64-00.
- [SDR SWAA2023021402006](https://openairdocs.org/sdr/SWAA2023021402006.md): Lens · out of adjust · Feb 11, 2023 · N932WN · Boeing 7377H4 · Emergency Lighting
  > ROW 12ABC EMER AISLE LT LENS FELL OFF. SECURED W/ TAPE ON EDGES<[01] OK TO CONTINUE PER MEL 33-15-02 SP1;[02] REINSTALLED ROW 12ABC LIGHT ASSY IAW AMM 33-51-03.
- [SDR SWAA2023010486273](https://openairdocs.org/sdr/SWAA2023010486273.md): Light · inoperative · Dec 30, 2022 · N932WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY AISLE LIGHT BY ROWS 12ABC AND 14 ABC ARE INOP.<[01] RELAMPED EMERGENCY AISLE LIGHT AT ROWS 12ABC AND 14ABC AS PER REF. B737 AMM 33-51-03-960-801. TEST OK;[02] VERIFIED STEP 1.
- [SDR SWAA2023010486012](https://openairdocs.org/sdr/SWAA2023010486012.md): Battery Pack · inoperative · Dec 28, 2022 · N932WN · Boeing 7377H4 · Emergency Lighting
  > BATTERY PACK POSITION M1673 (AFT GALLEY LEFT SIDE INOP) EMERGENCY LIGHT BATTERY PACK POSITION M1673 INOP. REPLACED BATTERY PACK POSITION M1673 PER REFERENCE AMM 33-51-06-960-805. BATTERY PACK M1673 TEST NORMAL PER AMM 33-51-06-960-805.
- [SDR SWAA2023010486014](https://openairdocs.org/sdr/SWAA2023010486014.md): Battery Pack · inoperative · Dec 28, 2022 · N932WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK POSITION M1670 INOP. REPLACED EMERGENCY LIGHT BATTERY PACK POSITION M1670 PER REFERENCE AMM 33-51-06-960-805. BATTERY PACK M1670 TEST NORMAL PER AMM 33-51-06-960-805.

Next page: https://openairdocs.org/aircraft/N932WN/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 = 'N932WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N932WN/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.