# Service difficulty reports: N936WN

A list on [N936WN](https://openairdocs.org/aircraft/N936WN.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 · 161 reports

- [SDR SWAA2026093026404](https://openairdocs.org/sdr/SWAA2026093026404.md): Battery Pack · inoperative · Sep 26, 2026 · N936WN · Boeing 7377H4 · Emergency Lighting
  > FWD GALLEY AND LT, FWD EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. FWD GALLEY AND LT FWD EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AT FWD ENTRY DOOR IAW AMM 33-51-06. OPS CHKD OK.
- [SDR SWAA2026081788001](https://openairdocs.org/sdr/SWAA2026081788001.md): Floor Panel · cracked · Aug 13, 2026 · N936WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL CRACKED. R & R FWD CARGO FLOOR PANEL 120BF IAW AMM 25-52-10.
- [SDR SWAA2026061712459](https://openairdocs.org/sdr/SWAA2026061712459.md): Brake · overtemp · Jun 15, 2026 · N936WN · Boeing 7377H4 · Landing Gear Brake System
  > FLIGHT FROM COS TO DEN. LONG TAXI IN COS. RIGHT MAIN BRAKE ASSEMBLY SMOKED FOR 25 MIN AFTER PARKING. NO SMOKE ON LEFT MAIN BRAKES. ON LANDING AUTO BRAKE 3 SEL UP TOP. PERFORMED GVI OF MAIN WHEEL AND BRAKE, NO LEAKS OBSERVED. RT BRAKES AT 440* AND L/H BRAKE
- [SDR SWAA2026031980173](https://openairdocs.org/sdr/SWAA2026031980173.md): Handle · no discrepancy · Mar 16, 2026 · N936WN · Boeing 7377H4 · Service Doors
  > FWD SERVICE DOOR HANDLE APPEARS TO BE LOOSE. PERFORMED GVI OF FWD SERVICE DOOR HANDLE PER AMM 52-41-00. NO DEFECTS NOTED.
- [SDR SWAA2025100822186](https://openairdocs.org/sdr/SWAA2025100822186.md): Strap · broken · Oct 6, 2025 · N936WN · Boeing 7377H4 · Emergency Equipment
  > AFTER CABIN EMERGENCY STRAP BROKEN. REPLACED STRAP NON AFT FLASHLIGHT IAW AMM 25-64-00.
- [SDR SWAA2025082105535](https://openairdocs.org/sdr/SWAA2025082105535.md): Guard · stuck · Aug 18, 2025 · N936WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT COVER STUCK IN ARM POSITION. R & R EMERGENCY LIGHT SWITCH GUARD IAW SIP.
- [SDR SWAA2025061681759](https://openairdocs.org/sdr/SWAA2025061681759.md): Skin · cracked · Jun 13, 2025 · N936WN · Boeing 7377H4 · Passenger/Crew Doors
  > L1 DOOR LOWER HINGE CUTOUT CRACKED LOWER EDGE 2 INCHES FROM THE FORWARD EDGE OF DOOR SKIN 141A6150-3M: IN DAL 1 AVAILABLE. CLEANED AND STRIPPED PAINT ON L1 DOOR HINGE CUTOUT AREA FOR REPAIR PER SOPM 20-44-04. DAMAGE REPAIRED PER EA 25-152-01580. VERIFIED T
- [SDR SWAA2025031103552](https://openairdocs.org/sdr/SWAA2025031103552.md): Laminated Hinge · inoperative · Mar 9, 2025 · N936WN · Boeing 7377H4 · Emergency Lighting
  > INOP EMERGENCY EXIT LIGHT LT AND RT BEHIND AFT WING TO BODY FAIRING 2025-152000<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT LAMP LT AND RT BEHIND AFT WING TO BODY FAIRING I.A.W B737-700 AMM 33-51-04-960-801. TEST IS OK. SEE INDIVIDUAL SIGNOFF STEP BELOW;[02
- [SDR SWAA2025031101820](https://openairdocs.org/sdr/SWAA2025031101820.md): Seal · debonded · Mar 4, 2025 · N936WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > DETERIORATED SEAL ACCESS PANEL 343AB (PLASTIC SEAL IS DEBONDED) AT RT HORIZONTAL STABILIZER (1 EA) 2025-151987<[01] REPAIRED PLASTIC SEAL ON ACCESS PANEL 343AB AT RT HORIZONTAL STABILIZER (1 EA) IAW B737-700 SOPM 20-50-12;[02] COMPLETED
- [SDR SWAA2025031199394](https://openairdocs.org/sdr/SWAA2025031199394.md): Web · cracked · Feb 24, 2025 · N936WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > CRACK WEB OUTBOARD FAN COWL ON ENGINE 2 2025-151970<[01] REPLACED WEB OUTBOARD FAN COWL ON ENGINE 2 IAW B737-700 SRM 51-40-02;[02] CERTIFIED WORK PERFORMED.
- [SDR SWAA2025031198565](https://openairdocs.org/sdr/SWAA2025031198565.md): Angle · cracked · Feb 22, 2025 · N936WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED STA947.5 AND LBL11 AT AFT CARGO COMPARTMENT 2025-151941<[01] REPLACED ANGLE LOCATED BS 947.5 AND LBL 11 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG# 149A8103 SHEET 7 AND REV A. <BR>TOOL USED IS CALIPER P/N: 500-197-30; S/N:
- [SDR SWAA2025031198561](https://openairdocs.org/sdr/SWAA2025031198561.md): Support Angle · cracked · Feb 22, 2025 · N936WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS 907 TO BS 927 AFT POSITION BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT 2025-151935<[01] REPLACED ANGLE AND FASTENERS LOCATED BTW BSTA 907 TO BSTA 927 AND BTW STR 25R TO STR 27R. AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10
- [SDR SWAA2025031198566](https://openairdocs.org/sdr/SWAA2025031198566.md): Cargo Track · cracked · Feb 22, 2025 · N936WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK RBBL 13.84 LOCATED STA727E AT AFT CARGO COMPARTMENT 2025-151944<[01] STEPS 4 AND 5 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-SEP-25;[02] TOOL USED IN STEP 7: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 200053402;
- [SDR SWAA2025031198563](https://openairdocs.org/sdr/SWAA2025031198563.md): Shield · corroded · Feb 22, 2025 · N936WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB LOCATED STA847 TO STA867 AND RBL21 WL156 AT AFT CARGO COMPARTMENT 2025-151946<[01] REPLACED SHIELD WEB AND FASTENERS LOCATED STA847 TO STA867 AND RBL21 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING 146A0081 SHEET 37
- [SDR SWAA2025031198538](https://openairdocs.org/sdr/SWAA2025031198538.md): Shear Tie · cracked · Feb 21, 2025 · N936WN · Boeing 7377H4 · Fuselage Internal Mounting Structure
  > CRACK SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN 2025-151900<[01] REPLACED SUPPORT ANGLE LOCATED AT STA 867 AND BETWEEN STR2R AND STR3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG: 146A7901 SH
- [SDR SWAA2025031298537](https://openairdocs.org/sdr/SWAA2025031298537.md): Rib · cracked · Feb 20, 2025 · N936WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK RIB 8 ON ACCESS PANEL 321A DORSAL FIN VERTICAL STABILIZER 2025-151899 <[01]. REMOVED AND REPLACED RIB 8 AND FASTENERS LOCATED ON ACCESS PANEL 321A DORSAL FIN VERTICAL STABILIZER. IAW B737-700 SRM 51-10-02 PARAGRAPH 9. SRM 51-40-02 AND DWG# 174A1008. SHE
- [SDR SWAA2025031198126](https://openairdocs.org/sdr/SWAA2025031198126.md): Gusset · cracked · Feb 20, 2025 · N936WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2025-151871<[01] REPLACED GUSSET AND FASTENERS LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV. -<BR>SEE INDIVIDUAL SIGN O
- [SDR SWAA2025031198127](https://openairdocs.org/sdr/SWAA2025031198127.md): Gusset · cracked · Feb 20, 2025 · N936WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK GUSSET LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT 2025-151872<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D AND STRINGER 21L FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND DWG 143A7902 SHEET:209;
- [SDR SWAA2025031198536](https://openairdocs.org/sdr/SWAA2025031198536.md): Access Panel · cracked · Feb 20, 2025 · N936WN · Boeing 7377H4 · Aerodynamic Fairings
  > CRACK ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR 2025-151898<[01] TOOL USED CALIPER PN: 500-464; SN: B17030933; DUE DATE: 21/DEC/25.;[02] TOOL USED HOT BONDER PN: HCS8800; SN: 01685794; DUE DATE: 25/APR/25.;[03] REPAIRED ACCESS PANEL 191D BODY FAIRING
- [SDR SWAA2025031197766](https://openairdocs.org/sdr/SWAA2025031197766.md): Stiffener · cracked · Feb 19, 2025 · N936WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK STIFFENER ASSY FLOOR STRUCTURE LOCATED STA540 AND BETWEEN RBL24.75 TO RBL45.5 PASSENGER CABIN 2025-151707<[01] REPLACED STIFFENER ASSY FLOOR STRUCTURE LOCATED STA 540 AND BETWEEN RBL 24.75 TO RBL 45.5 PASSENGER CABIN IAW BOEING 737-700 SRM 51-40-02 AND D
- [SDR SWAA2025031101615](https://openairdocs.org/sdr/SWAA2025031101615.md): Skin · debonded · Feb 19, 2025 · N936WN · Boeing 7377H4 · Trailing Edge Flaps
  > CUSTOMER REQUEST - PERFORM PERMANENT REPAIR ON O/B AFT FLAP O/B SIDE AT RT WING 2025-151782<[01] TOOL USED IN STEP 3: UT FLAW DETECTOR; P/N: EPOCH 650; S/N: 201036102; DUE DATE: 25-OCT-25;[02] TOOL USED ON STEP 16:BANDMASTER 600M; S/N:230106912; DUE DATE: 05-F
- [SDR SWAA2025031197604](https://openairdocs.org/sdr/SWAA2025031197604.md): Connector · broken · Feb 19, 2025 · N936WN · Boeing 7377H4 · Light System Wiring
  > BORKEN EMERGENCY LIGHT ELECTRICAL CONECTOR ON STA 747 RT SIDE AT PASSENGER CABIN 2025-151671<[01] REMOVED AND REPLACED EMERGENCY LIGHT ELECTRICAL CONNECTOR D11336 ON RT SIDE AT AFT PASSENGER CABIN I.A.W B737-700 WDM 33-51-14 AND SWPM 20-61-28 AND PERFORMED EME
- [SDR SWAA2025031197134](https://openairdocs.org/sdr/SWAA2025031197134.md): Handle · deteriorated · Feb 18, 2025 · N936WN · Boeing 7377H4 · Passenger/Crew Doors
  > DETERIORATED ENTRY DOOR SIDE NUT ASSISTLE HANDLE AT FWD GALLEY AREA (2 EA) 2025-151637<[01] REPLACED ENTRY DOOR SIDE NUT ASSISTLE HANDLE AT FWD GALLEY AREA (2 EA) IAW B737-700 52-11-31-400-802 STEP 3.G.(2).(B);[02] REPLACED ENTRY DOOR SIDE NUT ASSISTLE HANDLE
- [SDR SWAA2025031197138](https://openairdocs.org/sdr/SWAA2025031197138.md): Handle · deteriorated · Feb 18, 2025 · N936WN · Boeing 7377H4 · Passenger/Crew Doors
  > DETERIORATED PLASTIC NUT ON HANDLS AT FWD ENTRY DOOR (4 EA) 2025-151647<[01] REPLACED PLASTIC NUT ON HANDLS AT FWD ENTRY DOOR (4 EA) IAW B737-700 AMM 52-11-31-400-802 STEP 3.G.(2);[02] CORRECTED STEP <BR>REPLACED PLASTIC NUT ON HANDLES AT FWD ENTRY DOOR (4 EA)
- [SDR SWAA2025031096744](https://openairdocs.org/sdr/SWAA2025031096744.md): Light · deteriorated · Feb 16, 2025 · N936WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2025-151567<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 35-51-15-400-802;[02] REPLACED STRIP PHOTOLUMINESCENT
- [SDR SWAA2024110555540](https://openairdocs.org/sdr/SWAA2024110555540.md): Floorbeam · cracked · Nov 1, 2024 · N936WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > FORWARD CARGO A/C DISTRIBUTION BAY- CRACKED FLOOR BEAM AT STATION 540 JUST RIGHT OF FLOOR CENTERLINE.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)] R&R FWD CARGO A/C BAY FLOOR
- [SDR SWAA2024110555545](https://openairdocs.org/sdr/SWAA2024110555545.md): Battery Pack · no test · Nov 1, 2024 · N936WN · Boeing 7377H4 · Emergency Lighting
  > EMX LIGHT BATTERY PACK M01675 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX LIGHT BATTERY PACK M01675 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024110555549](https://openairdocs.org/sdr/SWAA2024110555549.md): Support Beam · cracked · Nov 1, 2024 · N936WN · Boeing 7377H4 · Service Doors
  > CABIN FORWARD GALLEY SERVICE DOOR HANDLE MECHANISM LOWER SUPPORT BEAM IS CRACKED APPROXIMATELY 0.9 LONG AT RADIUS FORWARD OF INBOARD FORWARD MOUNT BOLT.<[01] VERIFIED CRACK WITH HFEC PER BOEING NDT PART 6 51-00-00 PROCEDURE 23.;[02] R&R CABIN FWD GALLEY SERVIC
- [SDR SWAA2024080823118](https://openairdocs.org/sdr/SWAA2024080823118.md): Floor Panel · cracked · Aug 6, 2024 · N936WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOOR PANEL 140EF CRACKED.<[01] 05 - OK TO CONTINUE PER [MEL 25-16-01 XB;AFT LOWER CARGO COMPT LINING PANELS & FLOOR PANELS]. WITH SP __1B_______ AND AUTHORIZATION NUMBER __208119_____;[02] PANEL 140EF IS INCORRECT. FLOOR PANEL WITH DAMAG
- [SDR SWAA2024072918173](https://openairdocs.org/sdr/SWAA2024072918173.md): Light · inoperative · Jul 27, 2024 · N936WN · Boeing 7377H4 · Emergency Lighting
  > R/H AFT EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED R/H AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04
- [SDR SWAA2024030759881](https://openairdocs.org/sdr/SWAA2024030759881.md): Handle · detached · Mar 6, 2024 · N936WN · Boeing 7377H4 · Passenger/Crew Doors
  > MAIN ENTRY DOOR ASSIT HANDLE FELL OFF DURING TURBULANCE<[01] REMOVED FWD LAVE ASSIT HANDLE AND INSTALLED ON FWD ENRTY DOOR IAW AMM 52-11-31; MISSING LAVE ASSIT HANDLE OK TO CONTINUE MEL 25-10-01 SP1B. REPLACED AFT LAV DOOR ASSIST HANDLE IAW SIP.
- [SDR SWAA2024012242434](https://openairdocs.org/sdr/SWAA2024012242434.md): Indication Sys · out of limits · Jan 18, 2024 · N936WN · Boeing 7377H4 · Fuel Indicating System
  > PER QRH SUSPECTED FUEL LEAK #1 ENGINE. #1 MAIN TANK QTY DECREASED APPROX 50# PER 5 MINUTES DUE TO INFLIGHT SHUTDOWN AND EMERGENCY DIVERSION RR ALL PROBES AND COMP HANGAR REQUEST 2845<[01] PERFORMED VENTS INSP IAW AMM 71-71-00; NO DEFECTS; PERFORMED EEC BITE IA
- [SDR SWAA2023100406899](https://openairdocs.org/sdr/SWAA2023100406899.md): Start Valve · faulty · Oct 3, 2023 · N936WN · Boeing 7377H4 · Engine Start Valves/Controls
  > #2 ENINGE START VALVE LIGHT REMAINED ILLUMINATED AFTER ENGINE START. ABORTED ENGINE START AND #2 ENGINE OVERHEAT LIGHT ILLUMINATED; DISCHARGED BOTH FIRE BOTTLES.<[01] R/R START VALVE AMM 80-11-03<BR>R/R AIR TURBINE STARTER AMM 80-11-01<BR>R/R START SWITCH AMM
- [SDR SWAA2023062165995](https://openairdocs.org/sdr/SWAA2023062165995.md): Light · faulty · Jun 21, 2023 · N936WN · Boeing 7377H4 · Emergency Lighting
  > RH OVER-WING EXIT LIGHT DIM<[01] R&R CABIN OVERWING EXIT LIGHT PER AMM 33-51-01;[02] INSPECTION C/W R&R CABIN OVERWING EXIT LIGHT PER AMM 33-51-01
- [SDR SWAA2023060956533](https://openairdocs.org/sdr/SWAA2023060956533.md): Light · inoperative · Jun 6, 2023 · N936WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY EXIT DOOR WINDOW LIGHT INOP<[01] CONTINUE PER MEL 33-2-03 SP#1B AUTHRO# 138055;[02] R&R LIGHT BALLAST @ R/H OVER WING EMERGENCY EXIT DOOR WINDOW REF MM 33-21-00
- [SDR SWAA2023041124592](https://openairdocs.org/sdr/SWAA2023041124592.md): Lens · broken · Apr 7, 2023 · N936WN · Boeing 7377H4 · Emergency Lighting
  > RT O/W EXIT SIGN HAS A BROKEN LENS COVER<[01] REPLACED EXIT SIGN LENS PER M/M 33-51-01.
- [SDR SWAA2023032420020](https://openairdocs.org/sdr/SWAA2023032420020.md): Handle · loose · Mar 23, 2023 · N936WN · Boeing 7377H4 · Emergency Exits
  > *C/R* L-1 DOOR AFT ASSIST HANDLE LOOSE.<[01] SECURED AFT ASSIST HANDLE AT L-1 DOOR AS PER AMM 25-21-31-420-802;[02] VERIFIED STEP 1..
- [SDR SWAA2023032419033](https://openairdocs.org/sdr/SWAA2023032419033.md): Lens · missing · Mar 20, 2023 · N936WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT LENS MISSING AT O/H BIN BULL NOSE ROW 22 DEF<[01] EMERGENCY LIGHT LENS FOUND AND REINSTALLED AT O/H BIN BULL NOSE ROW 22 DEF AS PER B737 700 AMM 33-51-06-960-802;[02] VERIFIED STEP#1.
- [SDR SWAA2023032418572](https://openairdocs.org/sdr/SWAA2023032418572.md): Battery Pack · inoperative · Mar 19, 2023 · N936WN · Boeing 7377H4 · Emergency Lighting
  > MULTIPLE INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERABLE<[01] ALL STEPS COMPLETED.
- [SDR SWAA2023032420523](https://openairdocs.org/sdr/SWAA2023032420523.md): Charger · inoperative · Mar 19, 2023 · N936WN · Boeing 7377H4 · Emergency Lighting
  > MULTIPLE INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERABLE<[01] ALL STEPS COMPLETED.
- [SDR SWAA2023032416604](https://openairdocs.org/sdr/SWAA2023032416604.md): Doubler · defective · Mar 15, 2023 · N936WN · Boeing 7377H4 · Fuselage Structure (General)
  > C/R FOUND EXTERNAL POWER RECEPTACLE DOUBLER (P/N 284A6807-12) DEFECTIVE.<[01] REMOVED AND REPLACED EXTERNAL POWER RECEPTACLE DOUBLER (P/N 284A6807-12) AS PER B737 AMM 24-41-11-000-802-001; AMM 24-41-11-400-802-001. TEST OK.<BR><BR>TOOL USED<BR>TORQUE WRENCH B/
- [SDR SWAA2023032416605](https://openairdocs.org/sdr/SWAA2023032416605.md): Light · defective · Mar 15, 2023 · N936WN · Boeing 7377H4 · Emergency Lighting
  > OVERHEAD BIN EMERGENCY LIGHT AT SEAT 8DEF DEFECTIVE.<[01] RELAMPED OVERHEAD BIN EMERGENCY LIGHT AT SEAT 8DEF AS PER REF B737 AMM 33-51-03-960-801. TEST OK.;[02] VERIFIED STEP 1.
- [SDR SWAA2023032415376](https://openairdocs.org/sdr/SWAA2023032415376.md): Bracket · cracked · Mar 12, 2023 · N936WN · Boeing 7377H4 · Aerodynamic Fairings
  > FOUND PANEL SUPPORT BRACKET CRACKED AT STA 500L BEHIND PANEL 191AR<[01] REMOVED PANEL 191AR FOR ACCESS TO BRACKET REF B737-700 SRM 51-40-02-0G-0;[02] REMOVED R/H SUPPORT BRACKED AT STA 500L IN REF TO B737 AMM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW SUPPORT
- [SDR SWAA2023032414367](https://openairdocs.org/sdr/SWAA2023032414367.md): Rib · cracked · Mar 9, 2023 · N936WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > AFTER REMOVAL OF RIB #5; AT RT HOR STAB; FOUND RIB UPPER CHORD CRACKED AT AFT SPAR<[01] ATTACHED TO AIRCRAFT EA # 23-155-00885;[02] C/W.
- [SDR SWAA2023032413588](https://openairdocs.org/sdr/SWAA2023032413588.md): Retainer · cracked · Mar 7, 2023 · N936WN · Boeing 7377H4 · Vertical Stabilizer
  > VERTICAL FIN PANEL ASSEMBLY 323CL - RETAINER IS CRACKED AS MARKED. 124-048 CRACKED RETAINER IS ON 324AL<[01] REMOVED AND REPLACED VERTICAL FIN PANEL ASSEMBLY 324AL RETAINER REF B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1. R/R VERICAL FIN PANEL 324AL RETAIN
- [SDR SWAA2023032412919](https://openairdocs.org/sdr/SWAA2023032412919.md): Skin · cracked · Mar 6, 2023 · N936WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90; 16' FROM FRONT SPAR;I/B ROW. CRACK LENGTH -1'. CRACK FOUND AT RIGHT HORIONTAL STABILIER LOWER SKIN STAB STA 193.90 16&#34; FROM FRONT SPAR I/B ROW. CRACK LENGTH -1&#34;.<[01] TREATED AND P
- [SDR SWAA2023032412920](https://openairdocs.org/sdr/SWAA2023032412920.md): Skin · cracked · Mar 6, 2023 · N936WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90; 23' FROM FRONT SPAR;I/B ROW. CRACK LENGTH -1' CRACK FOUND AT RIGHT HORIONTAL STABILIER LOWER SKIN STAB STA 193.90 23&#34; FROM FRONT SPAR I/B ROW. CRACK LENGTH -1&#34;<[01] TREATED AND PRI
- [SDR SWAA2023032413109](https://openairdocs.org/sdr/SWAA2023032413109.md): Stiffener · cracked · Mar 6, 2023 · N936WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > RT HORIZONTAL STABILIZER INSPAR RIB #5 - STIFFENER #2 IS CRACKED.<[01] PERFORMED HFEC ON SUSPECTED CRACK ON STIFFENER #2 OF RIB #5 OF RH HORIZONTAL STABILIZER. CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23.<BR>[NORTEC 600; B/C 166316; CALIB.DUE-10/2
- [SDR SWAA2023032413112](https://openairdocs.org/sdr/SWAA2023032413112.md): Stiffener · cracked · Mar 6, 2023 · N936WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STABILIZER INSPAR RIB #5 - STIFFENER #4 HAS A POSSIBLE CRACK.<[01] PERFORMED HFEC ON SUSPECTED CRACK ON STIFFENER #4 OF RIB #5 OF RH HORIZONTAL STABILIZER. CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23.<BR>[NORTEC 600; B/C 166316; CALI
- [SDR SWAA2022111469552](https://openairdocs.org/sdr/SWAA2022111469552.md): Support Fitting · cracked · Nov 10, 2022 · N936WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PANEL 192E RH FWD SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING REF SRM 51-40-02

Next page: https://openairdocs.org/aircraft/N936WN/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 = 'N936WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N936WN/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.
