# Service difficulty reports: N942WN

A list on [N942WN](https://openairdocs.org/aircraft/N942WN.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 · 184 reports

- [SDR SWAA2026101473533](https://openairdocs.org/sdr/SWAA2026101473533.md): Floor Panel · cracked · Oct 10, 2026 · N942WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 120CF CRACKED. REMOVED & INSTALLED A NEW FWD CARGO FLOOR PANEL IAW AMM 25-52-10.
- [SDR SWAA2026101389481](https://openairdocs.org/sdr/SWAA2026101389481.md): Floor Panel · cracked · Oct 9, 2026 · N942WN · Boeing 7377H4 · Fuselage Floor Panel
  > GROUND CREW FOUND SMALL CRACK IN BIN C FLOOR FAULT. OK TO CONTINUE PER MEL 25-16-01 XA. REMOVED AND REPLACED THE FLOOR PANEL 120BF IAW AMM 25-52-10.
- [SDR SWAA2026072729522](https://openairdocs.org/sdr/SWAA2026072729522.md): Skirt · debonded · Jul 21, 2026 · N942WN · Boeing 7377H4 · Escape Slide
  > PASSENGER CABIN FWD SERVICE DOOR ESCAPE SLIDE SKIRT RUBBER TORN AND DISBONDED. R & R THE SLIDE IAW AMM 25-66-01.
- [SDR SWAA2026072713137](https://openairdocs.org/sdr/SWAA2026072713137.md): Battery Pack · no test · Jul 21, 2026 · N942WN · Boeing 7377H4 · Emergency Lighting
  > FWD LT EMERGENCY BATTERY PACK AT M1675 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK PER AMM 33-51-06.
- [SDR SWAA2026060308625](https://openairdocs.org/sdr/SWAA2026060308625.md): Light · faulty · Jun 1, 2026 · N942WN · Boeing 7377H4 · Emergency Lighting
  > F/O SIDE EMER EXT LIGHT FLICKERS. OK TO CONTINUE PER MEL 33-2-03 SP1B. REMOVED AND REPLACED F/O SIDE EMERGENCY EXIT SIDE WALL LIGHT IN REF TO AMM 33-21-00. OPS TEST GOOD. THIS CLEARS MEL.
- [SDR SWAA2026031679934](https://openairdocs.org/sdr/SWAA2026031679934.md): Slide · displaced · Mar 14, 2026 · N942WN · Boeing 7377H4 · Escape Slide
  > AFT RT SERVICE DOOOR SLIDE DISPLACED. REPOSITIONED SLIDE PER MT 725-61-06.
- [SDR SWAA2025102928336](https://openairdocs.org/sdr/SWAA2025102928336.md): Socket · dirty · Oct 25, 2025 · N942WN · Boeing 7377H4 · Emergency Lighting
  > FWD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED LAMP SOCKET CONTACTS AND VERIFIED NORMAL OPERATION OF FWD SERVICE DOOR EXTERIOR EMERGENCY LIGHT LAMP IAW AMM 33-51-00.
- [SDR SWAA2025060969973](https://openairdocs.org/sdr/SWAA2025060969973.md): Keelbeam · cracked · May 12, 2025 · N942WN · Boeing 7377H4 · Fuselage Main, Keel
  > CRACK INTERNAL STRUCTURE KEEL BEAM LOCATED BETWEEN BS 727 TO BS 727A AND STR 27R AT AFT CARGO COMPARTMENT 2025-310172<[01] ON STEP 7 AND 8. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 60007161486. DUE DATE: 06-SEP-25.;[02] TOOLS USED: TEMPERATURE CONTROLL
- [SDR SWAA2025060969974](https://openairdocs.org/sdr/SWAA2025060969974.md): Angle · cracked · May 12, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS907 TO BS 927 BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT 2025-310174<[01] REPLACED ANGLE AND FASTENERS LOCATED BS907 TO BS927 BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G AND DWG: 147A7221 SHEET: 28 REV: - <
- [SDR SWAA2025060969975](https://openairdocs.org/sdr/SWAA2025060969975.md): Angle · cracked · May 12, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS947.5 AND S-26L AT AFT CARGO COMPARTMENT 2025-310173<[01] REPLACED ANGLE (FITTING) AND FASTENERS LOCATED BS947.5 AND S-26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0; DWG # 149A8103 SHEET 7 REV: A.<BR>SE
- [SDR SWAA2025060970160](https://openairdocs.org/sdr/SWAA2025060970160.md): Scuff Plate · cracked · May 12, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2025-310178<[01] TOOL USED DIGITAL CALIPER P/N:500-193-30; S/N: 0000291; DUE DATE: 01-NOV-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N: 1753759; DUE DATE: 30/JUN/25;[03] REPAIRED TH
- [SDR SWAA2025060970159](https://openairdocs.org/sdr/SWAA2025060970159.md): Rib · cracked · May 12, 2025 · N942WN · Boeing 7377H4 · Vertical Stabilizer, Spar/Rib
  > CRACK RIB LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER 2025-310176<[01] TOOL USED: TEMPERATURE CONTROLLED: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26.;[02] REPLACED RIB AND FASTENERS LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER I.A.W B737
- [SDR SWAA2025060969745](https://openairdocs.org/sdr/SWAA2025060969745.md): Angle · cracked · May 11, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS400 AFT SIDE LBL 24 FWD CARGO COMPARTMENT 2025-310106<[01] INSTALLED CLIP LOCATED BS 400 AFT SIDE LBL 24 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG# 143A7505 SHEET 117 AND REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02]
- [SDR SWAA2025060969744](https://openairdocs.org/sdr/SWAA2025060969744.md): Support Channel · corroded · May 11, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION CHANNEL SUPPORT LOCATED BETWEEN BS500A AND BS500B LBL24 WL 156.5 AT FWD CARGO COMPARTMENT 2025-310101<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N 45MG S/N 232019809 DUE DATE: 08-OCT-25.;[02] REPAIRED CHANNEL SUPPORT (SUPPORT ZEE) LOCATED BETWEEN BS480 A
- [SDR SWAA2025060969746](https://openairdocs.org/sdr/SWAA2025060969746.md): Support Channel · corroded · May 11, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION CHANNEL SUPPORT LOCATED BETWEEN BS500 AND BS500A RBL24 WL 156.5 AT FWD CARGO COMPARTMENT 2025-310110<[01] REPLACED CHANNEL SUPPORT (SHIELD) AND FASTENERS LOCATED BETWEEN BS500 TO BS500A RBL 24 WL 156.5 AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM
- [SDR SWAA2025060969747](https://openairdocs.org/sdr/SWAA2025060969747.md): Access Panel · cracked · May 11, 2025 · N942WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2025-310153<[01] REPLACED BLADE ON ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0.<BR>MEASURED CRACK IS L: 0.181 INCHES; TOOL USED DIGITAL CALIPER P/N: 8647A42;
- [SDR SWAA2025060969317](https://openairdocs.org/sdr/SWAA2025060969317.md): Angle · cracked · May 9, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - CLIP LOCATED BS500B AND LBL21 FWD CARGO COMPARTMENT 2025-310010<[01] REPLACED CLIP LOCATED BS 500B AND LBL 21 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG# 143A7505 SHEET 118 AND REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLAC
- [SDR SWAA2025060969320](https://openairdocs.org/sdr/SWAA2025060969320.md): Angle · cracked · May 9, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE - CLIP LOCATED BS500C AND LBL21 FWD POSITION FWD CARGO COMPARTMENT 2025-310011<[01] REPLACED CLIP LOCATED BS 500C AND LBL 21 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG# 143A7505 SHEET 117 AND REV -. SEE INDIVIDUAL SIGN OFF BELOW
- [SDR SWAA2025060969314](https://openairdocs.org/sdr/SWAA2025060969314.md): Rib · cracked · May 9, 2025 · N942WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 28 INCH FROM FRONT SPAR LT HORIZONTAL STAB 2025-310000<[01] TOOL USED ON STEP 3: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 220272712 DUE DATE: 28-JAN-26;[02] PERFORMED REPAIR ON INSPAR RIB LOCATED STAB STA 120.30
- [SDR SWAA2025060969311](https://openairdocs.org/sdr/SWAA2025060969311.md): Rib · cracked · May 9, 2025 · N942WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOACTED STAB STA 129.50 AND 9 INCH FROM REAR SPAR LT HORIZONTAL STAB 2025-310001<[01] ON STEP 3 AND 4. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 210136503. DUE DATE: 24-JUL-25.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600
- [SDR SWAA2025060969312](https://openairdocs.org/sdr/SWAA2025060969312.md): Rib · cracked · May 9, 2025 · N942WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 9 INCH FROM REAR SPAR AT RT HORIZONTAL STABILIZER 2025-310003<[01] STEP 3 AND STEP 4. EDDY CURRENT EQUIPMENT USED P/N: NORTE 600D; S/N: 220273012 AND DUE DATE: 22-JAN-26.;[02] STEP 7. EDDY CURRENT EQUIPMENT USED P/N
- [SDR SWAA2025060969178](https://openairdocs.org/sdr/SWAA2025060969178.md): Floorbeam · cracked · May 9, 2025 · N942WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK ON BREAK PANEL LOCATED BS 540 LBL 1 AT CENTER WING BOX 2025-309994 CRACK ON BREAK PANEL LOCATED BS 540 BTW BL0 TO LBL 24.75 AT CENTER WING BOX<[01] REPLACED BREAK PANEL AND FASTENERS LOCATED BS 540 BTW BL0 TO LBL 24.75 AT CENTER WING BOX IAW B737-700 SRM
- [SDR SWAA2025060969179](https://openairdocs.org/sdr/SWAA2025060969179.md): Angle · cracked · May 9, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS 695 LBL1 AT CENTER WING BOX 2025-309996<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 29 JAN 26; TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE 28 JAN 26.;[02] REPLACED ANGLE AND FASTE
- [SDR SWAA2025060969180](https://openairdocs.org/sdr/SWAA2025060969180.md): Floorbeam · cracked · May 9, 2025 · N942WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK ON BREAK PANEL LOCATED BS 540 RBL 1 AT CENTER WING BOX 2025-309995 CRACK ON BREAK PANEL LOCATED BS 540 BTW BL0 TO RBL 24.75 AT CENTER WING BOX<[01] REPLACED BREAK PANEL AND FASTENERS LOCATED BS 540 RBL 1 AT CENTER WING BOX IAW B737-700 SRM 51-40-02-0G; B
- [SDR SWAA2025060968101](https://openairdocs.org/sdr/SWAA2025060968101.md): Handle · deteriorated · May 7, 2025 · N942WN · Boeing 7377H4 · Passenger/Crew Doors
  > DETERIORATED ASSIST HANDLE NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GALLEY AREA (4EA). REPLACED ASSIST HANDLE NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GALLEY AREA (4EA) IAW AMM 52-11-31-400-802 STEP 3.G.(4). THE INSTALLATION IS DOCUMENTED ON TTG8Q010CWF
- [SDR SWAA2025060968098](https://openairdocs.org/sdr/SWAA2025060968098.md): Light · deteriorated · May 6, 2025 · N942WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA). REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) I.A.W B737-700 AMM 33-51-15-400-802.
- [SDR SWAA2025060968093](https://openairdocs.org/sdr/SWAA2025060968093.md): Skin · cracked · May 6, 2025 · N942WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK LOWER SURFACE ACTUATOR AREA LEADING EDGE ON SLAT 6 AT RT WING. REPAIRED LOWER SURFACE ACTUATOR AREA LEADING EDGE ON SLAT 6 AT RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1.
- [SDR SWAA2025031404536](https://openairdocs.org/sdr/SWAA2025031404536.md): Girt Bar · out of adjust · Mar 12, 2025 · N942WN · Boeing 7377H4 · Emergency Equipment
  > GIRT BAR ON AFT CAPTAINS SIDE HANGING OUT TOO FAR <[01]. REINSTALLED GIRT BAR IAW MM 25-66-01.
- [SDR SWAA2025012889974](https://openairdocs.org/sdr/SWAA2025012889974.md): Battery Pack · inoperative · Jan 27, 2025 · N942WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS ABOVE ENTRY DOOR AND FWD 2 AISLE LIGHT ON RH SIDE INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1674 IN REF TO AMM 33-51-06. ALL AFFECTED EMERGENCY LIGHTS OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2024091737107](https://openairdocs.org/sdr/SWAA2024091737107.md): Attach Bracket · cracked · Sep 13, 2024 · N942WN · Boeing 7377H4 · Landing Gear Doors
  > RIGHT MAIN LANDING GEAR CENTER DOOR BOTTOM FWD ATTACH BRACKET CRACKED AT THE BARREL NUT.<[01] OK TO CONTINUE PER CDL 32-10-3; SP1B<BR>AUTHORIZATION CODE: #213893
- [SDR SWAA2024081325102](https://openairdocs.org/sdr/SWAA2024081325102.md): Handle · broken · Aug 10, 2024 · N942WN · Boeing 7377H4 · Passenger/Crew Doors
  > MAIN CABIN DOOR ASSIST HANDLE BROKEN<[01] R&R L-1 DOOR ASSIST HANDLE PER A.M.M. 25-21-31 & I.P.C. 52-11-51-12.
- [SDR SWAA2024081325061](https://openairdocs.org/sdr/SWAA2024081325061.md): Handle · broken · Aug 9, 2024 · N942WN · Boeing 7377H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR ASSIST HANDLE BROKEN.<[01] RESECURED DOOR ASSIST HANDLE IAW AMM 52-11-31.
- [SDR SWAA2024052085442](https://openairdocs.org/sdr/SWAA2024052085442.md): Sign · detached · May 14, 2024 · N942WN · Boeing 7377H4 · Emergency Lighting
  > PLASTIC EXIT SIGNS POPPED OFF HOLDER MID-CABIN<[01] INSTALLED PLASTIC EXIT SIGN COVERS IAW AMM 33-51-01. EXIT SIGN COVERS SECURITY CONFIRMED.
- [SDR SWAA2023091499302](https://openairdocs.org/sdr/SWAA2023091499302.md): Flap · delaminated · Sep 12, 2023 · N942WN · Boeing 7377H4 · Trailing Edge Flaps
  > L/H WING OUTBOARD AFT FLAP IS DELAMINATED ON UPPER INBOARD SURFACE. DELAMINATING IS 6.50 LONGITUDINALLY; 5.25 LATERALLY; 1.25 AWAY FROM TRAILING EDGE AND 1.25 AWAY FROM INBOARD EDGE.<[01] REMOVED AND REPLACED OUTBOARD AFT FLAP IAW B737 AMM 27-51-22. COMPLETE U
- [SDR SWAA2023062771129](https://openairdocs.org/sdr/SWAA2023062771129.md): Handle · loose · Jun 25, 2023 · N942WN · Boeing 7377H4 · Fixed Inner Doors
  > CUSTOMER WALK R-2 DOOR ASSIST HANDLE LOOSE<[01] SECURED R2 DOOR ASSIST HANDLE AS PER B737 AMM 52-13-31-400-802.;[02] VERIFIED AND INSPECTED STEP #; SECURED R2 DOOR ASSIST HANDLE AS PER B737 AMM 52-13-31-400-802.
- [SDR SWAA2023062770284](https://openairdocs.org/sdr/SWAA2023062770284.md): Light · inoperative · Jun 22, 2023 · N942WN · Boeing 7377H4 · Emergency Lighting
  > R2 DOOR EXTERIOR EMERGENCY LIGHT INOP.<[01] REPLACED LAMP SLIDE/OVERWING EMERGENCY LIGHT AS PER REF AMM 33-51-041-960-801 TEST PASS;[02] REPLACED LAMP SLIDE/OVERWING EMERGENCY LIGHT AS PER REF AMM 33-51-04-960-801 TEST PASS;[03] VERIFIED FINAL CORRECTIVE ACTIO
- [SDR SWAA2023062770285](https://openairdocs.org/sdr/SWAA2023062770285.md): Battery Pack · inoperative · Jun 22, 2023 · N942WN · Boeing 7377H4 · Emergency Lighting
  > L2 EMERGENCY AND AFT CENTER EXIT LIGHT INOP<[01] CLEANED BATTERY PACK AND CONNECTOR AS PER REF AMM 20-60-06-100-801 AND PERFORMED EMERGENCY LIGHT OPERATIONAL TEST AS PER REF AMM 33-51-00-710-801; TEST PASS;[02] VERIFIED FINAL CORRECTIVE ACTION.
- [SDR SWAA2023070358411](https://openairdocs.org/sdr/SWAA2023070358411.md): Channel · corroded · Jun 13, 2023 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MODERATE TO FLACKING LEVALS OF CORROSION FOUND ON UNDER SIDE OF RT.SIDE Z-CHANNEL FROM STA 807- STA 787 AT FASTENER HOLE LOCATIONS. ( MRKED). R/H AFT CARGO COMPARTMENT STA 727 - STA 767 CHANNEL UNDER SIDE AT FASTENER HOLES HAS CORROSION.<[01] INSTALLED NEW ZE
- [SDR SWAA2023070358413](https://openairdocs.org/sdr/SWAA2023070358413.md): Channel · corroded · Jun 13, 2023 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MODERATE TO FLACKING LEVALS OF CORROSION FOUND ON UNDER SIDE OF LT. SIDE OF THE Z-CHANNEL FROM STA 807- STA 767 AT FASTENER HOLE LOCATIONS. ( MRKED).<[01] REMOVED AND REPLACED ZEE CHANNEL ON L/H AFT CARGO COMPARTMENT PER REF. SRM 51-40-02-0G-0 AND DRAWING # 1
- [SDR SWAA2023062958410](https://openairdocs.org/sdr/SWAA2023062958410.md): Channel · corroded · Jun 13, 2023 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MODERATE TO FLACKING LEVALS OF CORROSION FOUND ON UNDER SIDE OF LT. SIDE Z-CHANNEL FROM STA 887- STA 844 AT FASTENER HOLE LOCATIONS. ( MRKED). MODERATE TO FLACKING LEVALS OF CORROSION FOUND ON UNDER SIDE OF LT. SIDE -CHANNEL FROM STA 807- STA 847 AT FASTENER
- [SDR SWAA2023062758409](https://openairdocs.org/sdr/SWAA2023062758409.md): Channel · corroded · Jun 13, 2023 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MODERATE TO FLACKING LEVALS OF CORROSION FOUND ON UNDER SIDE OF RT.SIDE Z-CHANNEL FROM STA 767- STA 747 AT FASTENER HOLE LOCATIONS. ( MRKED).<[01] REMOVED CORROSION ON R/H Z-CHANNEL FROM STA. 767 - STA. 747 PER REF. SRM 51-10-02-0G-0; AFTER FURTHER EVALUATION
- [SDR SWAA2023062758412](https://openairdocs.org/sdr/SWAA2023062758412.md): Channel · corroded · Jun 13, 2023 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MODERATE TO FLACKING LEVALS OF CORROSION FOUND ON UNDER SIDE OF LT. SIDE OF Z-CHANNEL SECTION FROM STA 807- STA 847 AT FASTENER HOLE LOCATIONS. ( MRKED).<[01] REMOVED CORROSION ON L/H Z-CHANNEL FROM STA. 807 - STA. 847 PER REF. SRM 51-10-02-0G-0; AFTER FURTHE
- [SDR SWAA2023062858776](https://openairdocs.org/sdr/SWAA2023062858776.md): Angle · cracked · Jun 12, 2023 · N942WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACK INDICATION FOUND AT L/H VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 42 HOLE. CRACK INDICATION FOUND AT L/H VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 42 HOLE.<[01] INSTALLED REPAIR AT L/H VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 42 PER REF SRM 57-10-10-2R-5 REPA
- [SDR SWAA2023070357861](https://openairdocs.org/sdr/SWAA2023070357861.md): Door · corroded · Jun 11, 2023 · N942WN · Boeing 7377H4 · Service Doors
  > CORROSION AT AFT LAV EXTERIOR SERVICE DOOR EXTERNAL SKIN FWD CORNER MKD DOT<[01] REF TASK CARD TTG8Q00LJR0Z FOR TOILET SERVICE DOOR REPLACEMENT.;[02] VERIFIED STEP #1. TRANSFER CARD.
- [SDR SWAA2023062957860](https://openairdocs.org/sdr/SWAA2023062957860.md): Stiffener · cracked · Jun 11, 2023 · N942WN · Boeing 7377H4 · Fuselage Main, Structure
  > LOWER FUSELAGE CENTER WING STIFFENER CRACKED AT R/H VAPOR BARRIER O/B A/C AIR EXIT EXHAUST DUCT RBL 25 STA 663.75<[01] REMOVED DAMAGE STIFFENER AND INSTALLED NEW STIFFENER ON R/H VAPOR BARRIER STA. 663.75 RBL 25; PER REF. SRM 51-40-02-0G-0 AND DRAWING # 111A10
- [SDR SWAA2023062957859](https://openairdocs.org/sdr/SWAA2023062957859.md): Stiffener · cracked · Jun 11, 2023 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE CENTER WING STIFFENER CRACKED AT L/H VAPOR BARRIER O/B A/C AIR EXIT EXHAUST DUCT LBL 25 STA 663.75<[01] REMOVED AND REPLACED STIFFENER AT LOWER FUSELAGE CENTER WING L/H VAPOR BARRIER O/B A/C AIR EXHAUST DUCT LBL 25 STA 663.75 REF.737-700-SRM 51-
- [SDR SWAA2023062858775](https://openairdocs.org/sdr/SWAA2023062858775.md): Angle · cracked · Jun 11, 2023 · N942WN · Boeing 7377H4 · Wing Main, Frame Structure
  > LOWER FUSELAGE CENTER WING R/H VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED @ RBL 7 STA 663.75 MKD DOT LOWER FUSELAGE CENTER WING R/H VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED @ RBL 9.25 STA 663.75 MKD DOT<[01] ACCOMPLISHED REPAIR AT RT. VAPOR BARRI
- [SDR SWAA2023070360058](https://openairdocs.org/sdr/SWAA2023070360058.md): Balance Weight · eroded · Jun 10, 2023 · N942WN · Boeing 7377H4 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STAB. T/E RUDDER BALANCE WEIGHT AT CENTER POSITION HAS SEVERAL EROSION. VERTICAL STAB. T/E RUDDER BALANCE WEIGHT AT CENTER POSITION HAS SEVERAL CORROSION.<[01] REMOVED RUDDER BALANCE WEIGHT IN REFERENCE CMM 55-40-09. AND INSTALLED RUDDER BALANCE WEIGH
- [SDR SWAA2023070357465](https://openairdocs.org/sdr/SWAA2023070357465.md): Skin · cracked · Jun 9, 2023 · N942WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90; 17' FROM FRONT SPAR;I/B ROW. CRACK LENGTH: 1.468' CRACK FOUND AT LEFT HORIONTAL STABILIER LOWER SKIN AT STAB STA 193.90 17&#34; FROM FRONT SPAR I/B ROW. CRACK LENGTH: 1.468&#34;<[01] INS
- [SDR SWAA2023062957471](https://openairdocs.org/sdr/SWAA2023062957471.md): Vapor Barrier · cracked · Jun 9, 2023 · N942WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > LEFT VAPOR BARRIER SIGNS OF CRACKS.<[01] STEPS # 4 & 5 WERE CHANGED TO COMPLETE FOR COMPLETION OF ALL WORK STEPS ON THIS COARD ARE NOW COMPLETED.;[02] VERIFIED ALL WORK STEPS HAVE BEEN ACCOMPLISHED AS REQUIERD PER WORK INSTRUCTIONS ON JOB CARD.

Next page: https://openairdocs.org/aircraft/N942WN/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 = 'N942WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N942WN/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.