# Service difficulty reports: N435WN

A list on [N435WN](https://openairdocs.org/aircraft/N435WN.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 7 · 311 reports

- [SDR SWAA2026101596385](https://openairdocs.org/sdr/SWAA2026101596385.md): Bulb · inoperative · Oct 11, 2026 · N435WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT 26ABC WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB AT SEAT ROW 26ABC IAW AMM 33-51-03-960-801. OPS CHKD GOOD.
- [SDR SWAA2026080515446](https://openairdocs.org/sdr/SWAA2026080515446.md): Igniter · faulted · Aug 1, 2026 · N435WN · Boeing 7377H4 · Spark Plug/Igniter
  > ABORTED NR 2 ENGINE START. IGNITION, RT N1, STALLED AT APPROX 9% TEMP 550. ENGINE STARTED OK WITH START SWITCH IN BOTH, OK TO CONTINUE IAW MEL 74-1-04, SP1. NR 2 ENG POWER SUPPLY CABLES SWAPPED AT IGNITION EXCITERS IAW MEL, R & R LT & RT IGNITER PLUGS ON N
- [SDR SWAA2026072498626](https://openairdocs.org/sdr/SWAA2026072498626.md): Cover · missing · Jul 20, 2026 · N435WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT COVER MISSING ROW 14 LEFT SIDE OVER WING REPLACED LENS COVER PER AMM 33-51-01
- [SDR SWAA2026051195709](https://openairdocs.org/sdr/SWAA2026051195709.md): Yaw Damper · faulty · May 5, 2026 · N435WN · Boeing 7377H4 · Rudder Control System
  > AT FL400; CREW NOTED THAT YOKE WAS DISPLAYED TO RIGHT 3 UNITS; CORRECTED USING RUDDER TRIM. APPROX. 1 MINUTE LATER; CREW OBSERVED UNCOMMANDED RUDDER INPUT (SHARP YAW TO THE LEFT.) OCCURRED 3 TIMES. OCCURRED A TOTAL OF 3 TIMES IN FLIGHT.<[01] INTERROGATED #1 SM
- [SDR SWAA2026051197274](https://openairdocs.org/sdr/SWAA2026051197274.md): Sensor · faulty · May 5, 2026 · N435WN · Boeing 7377H4 · Rudder Tab Control System
  > AT FL400; CREW NOTED THAT YOKE WAS DISPLAYED TO RIGHT 3 UNITS; CORRECTED USING RUDDER TRIM. APPROX. 1 MINUTE LATER; CREW OBSERVED UNCOMMANDED RUDDER INPUT (SHARP YAW TO THE LEFT.) OCCURRED 3 TIMES. OCCURRED A TOTAL OF 3 TIMES IN FLIGHT.<[01] INTERROGATED #1 SM
- [SDR SWAA2026051197275](https://openairdocs.org/sdr/SWAA2026051197275.md): Actuator · faulty · May 5, 2026 · N435WN · Boeing 7377H4 · Rudder Tab Control System
  > AT FL400; CREW NOTED THAT YOKE WAS DISPLAYED TO RIGHT 3 UNITS; CORRECTED USING RUDDER TRIM. APPROX. 1 MINUTE LATER; CREW OBSERVED UNCOMMANDED RUDDER INPUT (SHARP YAW TO THE LEFT.) OCCURRED 3 TIMES. OCCURRED A TOTAL OF 3 TIMES IN FLIGHT. INTERROGATED #1 SMYD P
- [SDR SWAA2026051197276](https://openairdocs.org/sdr/SWAA2026051197276.md): Pcu · faulty · May 5, 2026 · N435WN · Boeing 7377H4 · Rudder Tab Control System
  > AT FL400; CREW NOTED THAT YOKE WAS DISPLAYED TO RIGHT 3 UNITS; CORRECTED USING RUDDER TRIM. APPROX. 1 MINUTE LATER; CREW OBSERVED UNCOMMANDED RUDDER INPUT (SHARP YAW TO THE LEFT.) OCCURRED 3 TIMES. OCCURRED A TOTAL OF 3 TIMES IN FLIGHT. INTERROGATED #1 SMYD
- [SDR SWAA2026022372928](https://openairdocs.org/sdr/SWAA2026022372928.md): Skirt · out of position · Feb 21, 2026 · N435WN · Boeing 7377H4 · Escape Slide
  > FA STATES AFT ENTRY DOOR ESCAPE SLIDE SKIRT TOUCHES GROUND. REPOSITIONED SKIRT AT AFT ENTRY ESCAPE SLIDE. NO DEFECTS NOTED IAW MM 25-66-01.
- [SDR SWAA2026021063490](https://openairdocs.org/sdr/SWAA2026021063490.md): Pressure Blkhd · cracked · Jan 22, 2026 · N435WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > DURING 5311-I-16524-NG (AD - INSP - FUSELAGE - INSPECTION OF BS 1016 AFT PRESSURE BULKHEAD CENTER DOME APEX - GROUP 2; INDICATION OF A CRACK (HFEC) AT BL0 RIGHT LOWER FASTENER. AFTER PAINT REMOVAL USING PART 6 51-00-00 PROCEDURE 23 INDICATION OF CRACK STILL
- [SDR SWAA2025101624872](https://openairdocs.org/sdr/SWAA2025101624872.md): Battery Pack · discharged · Oct 16, 2025 · N435WN · Boeing 7377H4 · Emergency Lighting
  > AFT GALLEY BOTH RH AND LH BATTERY PACK DEAD. R & R BOTH LT AND RT AFT GALLEY BATTERY PACK AS PER AMM 33-51-06.OPS CHECK GOOD.
- [SDR SWAA2025090510739](https://openairdocs.org/sdr/SWAA2025090510739.md): Lamp · inoperative · Sep 3, 2025 · N435WN · Boeing 7377H4 · Emergency Lighting
  > LEFT AFT ENTRY EXTERNAL EMERGENCY LIGHT INOP. REMOVED AND REPLACED LEFT AFT ENTRY EXTERNAL EMERGENCY LIGHT LAMP PER AMM 33-51-04. OPS CHECKED GOOD.
- [SDR SWAA2025071188814](https://openairdocs.org/sdr/SWAA2025071188814.md): Light · inoperative · Jul 7, 2025 · N435WN · Boeing 7377H4 · Emergency Lighting
  > CEILING LIGHTS INOP AT ROWS 2 & 24.
- [SDR SWAA2025062083132](https://openairdocs.org/sdr/SWAA2025062083132.md): Seat Back · out of adjust · Jun 19, 2025 · N435WN · Boeing 7377H4 · Passenger Compartment Equipment
  > PASSENGER CABIN SEAT RECLINE IS NOT LOCKED OUT ON SEAT 11F AT R/H OVERWING EMERGENCY EXIT. LOCKED OUT SEAT 11B SEAT ACTUATOR RH EMERGENCY EXIT ROW REF CMM 25-21-42.
- [SDR SWAA2025062382902](https://openairdocs.org/sdr/SWAA2025062382902.md): Cabin Air Sys · odor · Jun 17, 2025 · N435WN · Boeing 7377H4 · Air Distribution System
  > EXPERIENCED STRONG ELECTRICAL BURNING ODOR UPON LANDING AND TAXIING TO GATE. NO VISIBLE SMOKE. <[01] CW COND. INSP PER AMM 05-51-56. NO ABNORMAL SMELLS NOTED.
- [SDR SWAA2025050566945](https://openairdocs.org/sdr/SWAA2025050566945.md): Fastener · loose · May 2, 2025 · N435WN · Boeing 7377H4 · Passenger/Crew Doors
  > AFT ENTRY DOOR EMERGENCY ESCAPE SLIDE BUSTLE ATTACH FASTENER IS LOOSE.<[01] CONFIRMED AFT ENTRY DOOR COVER FASTENERS SECURE PER AMM 20-50-11; AND INSTALLATION CORRECT PER AMM 25-66-01. ACFT OK FOR SERVICE.
- [SDR SWAA2025033109403](https://openairdocs.org/sdr/SWAA2025033109403.md): Battery Pack · inoperative · Mar 26, 2025 · N435WN · Boeing 7377H4 · Emergency Lighting
  > LIGHTS ASSOCIATED WITH M1674 BATTERY PACK INOP<[01] BATTERY PACK M1674 REPLACED AND RETESTED IAW AMM 33-51-06-960-805; NOT DEFECT NOTED.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025033109401](https://openairdocs.org/sdr/SWAA2025033109401.md): Bulb · inoperative · Mar 26, 2025 · N435WN · Boeing 7377H4 · Emergency Lighting
  > OVERHEAD EMERGENCY EXIT SIGN AT FWD SERVICE DOOR HAS INOP BULBS<[01] RELAMPED INOP BULBS IN OVERHEAD EMERGENCY EXIT SIGN AT FWD SERVICE DOOR AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025033109402](https://openairdocs.org/sdr/SWAA2025033109402.md): Bulb · inoperative · Mar 26, 2025 · N435WN · Boeing 7377H4 · Emergency Lighting
  > R/H OWE FWD LOCATOR SIGN HAS INOP BULBS<[01] RELAMPED INOP BULBS IN R/H OWE FWD LOCATOR SIGN AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025033104830](https://openairdocs.org/sdr/SWAA2025033104830.md): Floor Panel · delaminated · Mar 12, 2025 · N435WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASS CABIN FLOOR 231XF PREVIOUS REPAIR DELAMINATING<[01] PASS CABIN FLOOR 231XF; WITH PREVIOUS REPAIR DELAMINATION WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810 ID:0126.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025033104417](https://openairdocs.org/sdr/SWAA2025033104417.md): Stiffener · corroded · Mar 12, 2025 · N435WN · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION ON PRESSURE DECK STIFFENER AT STA 706+8; WL 200; RBL 62.<[01] REMOVAL OF CORROSION ON PRESSURE DECK STIFFENER AT STA 706+8; WL 200; RBL 62 ACCOMPLISHED ON WIP 1; EA 25-153-00668.;[02] REPAIRED PRESSURE DECK STIFFENER AT STA 706+8; WL 200; RBL 62 IAW
- [SDR SWAA2025033104419](https://openairdocs.org/sdr/SWAA2025033104419.md): Stiffener · corroded · Mar 12, 2025 · N435WN · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION ON PRESSURE DECK STIFFENER AT STA 685+12; WL 200; RBL 63.<[01] REFER TO FAULT TTG8Q00Z7MFP WHERE EA 25-153-00668 WAS ADDED AS A SUBTASK.;[02] REMOVED CORROSION ON PRESSURE DECK STIFFENER AT STA 685+12; WL 200; RBL 63 REFER TO FAULT TTG8Q00Z7MFP WHERE
- [SDR SWAA2025033104418](https://openairdocs.org/sdr/SWAA2025033104418.md): Stiffener · corroded · Mar 12, 2025 · N435WN · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION ON PRESSURE DECK STIFFENER AT STA 685+1.5; WL 200; RBL 66.<[01] REFER TO FAULT TTG8Q00Z7MFP WHERE EA 25-153-00668 WAS ADDED AS A SUBTASK.;[02] REPAIRED PRESSURE DECK STIFFENER AT STA 685+1.5; WL 200; RBL 66 IAW EA 25-153-00668. REFERENCE FAULT TTG8Q0
- [SDR SWAA2025033104420](https://openairdocs.org/sdr/SWAA2025033104420.md): Stiffener · corroded · Mar 12, 2025 · N435WN · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION ON PRESSURE DECK STIFFENER AT STA 708+2; FROM LBL 62 TO 70; WL 200.<[01] FABRICATED A NEW STIFFENER FROM 7075-T0 0.071' LOT 1523843-1 IAW SRM 51-30-01 AND DWG 144A7713 REV: B. REMOVED AND REPLACED THE CORROEDED STIFFENER ON PRESSURE DECK WITH THE STI
- [SDR SWAA2025033104421](https://openairdocs.org/sdr/SWAA2025033104421.md): Stiffener · corroded · Mar 12, 2025 · N435WN · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION ON PRESSURE DECK STIFFENER AT STA 706+8; FROM LBL 62 TO 70; WL 200.<[01] FABRICATED A NEW STIFFENER FROM 7075-T0 0.071' LOT 1523843-1 IAWSRM 51-30-01 AND DWG 144A7713 REV: B. REMOVED AND REPLACED THE CORROEDED STIFFENER ON THE PRESSURE DECK AT STA 70
- [SDR SWAA2025033103823](https://openairdocs.org/sdr/SWAA2025033103823.md): Skin · cracked · Mar 10, 2025 · N435WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE;.3' IN LENGTH (MARKED)<[01] REPAIRED L/H HORIZONTAL STABILIZER SKIN AT STAB STA 193.9 IAW SRM 55-10-01-2R-11 REPAIR 11; FIG. 204; DETAIL B.;[02] TASK C/W
- [SDR SWAA2025033103168](https://openairdocs.org/sdr/SWAA2025033103168.md): Skin · debonded · Mar 8, 2025 · N435WN · Boeing 7377H4 · Trailing Edge Flaps
  > RIGHT O/B T/E AFT FLAP I/B CORNER LOWER SKIN AND UPPER SKIN HAVE DISBONDS. (MARKED)<[01] REMOVED AND REPLACED RIGHT O/B T/E AFT FLAP PER AMM 27-51-22-401;[02] COMPLETED ALL STEPS
- [SDR SWAA2025033103167](https://openairdocs.org/sdr/SWAA2025033103167.md): Skin · debonded · Mar 8, 2025 · N435WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT I/B MAIN FLAP T/E LOWER SKIN IS DISBONDED. (MARKED)<[01] REMOVED AND REPLACED LEFT I/B MAIN FLAP T/E LOWER SKIN PER AMM 20-50-11-910-801 AND SRM 51-40-050G-0 AND BOEING DWG 113A2100 REV.: A.;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED CARD COMPLETE
- [SDR SWAA2024101446860](https://openairdocs.org/sdr/SWAA2024101446860.md): Handle · loose · Oct 10, 2024 · N435WN · Boeing 7377H4 · Service Doors
  > FWD SERVICE DOOR HANDLE CAM PLATE IS LOOSE<[01] SECURED HARDWARE TO FWD SERVICE DOOR HANDLE CAM PLATE IAW AMM 20-50-11.;[02] C/W INSPECTION
- [SDR SWAA2024080923898](https://openairdocs.org/sdr/SWAA2024080923898.md): Scuff Plate · cracked · Aug 8, 2024 · N435WN · Boeing 7377H4 · Service Doors
  > ON CLIMB THROUGH 7000FT;LOUD CRACK FROM FWD R/H SIDE BEHIND COCKPIT. ON DECENT F/A REPORTED RUSHING AIR SOUND FROM FWD FWD SVC DOOR. A/C HELD PRESSURE. AFTER ARRIVAL FOUND FWD SVC DOOR HANDLE LOOSE<[01] REMOVED DOOR HANDLE TO FOM. IAW AMM 52-41-31;[02] FOUND
- [SDR SWAA2024050281659](https://openairdocs.org/sdr/SWAA2024050281659.md): Bracket · loose · May 1, 2024 · N435WN · Boeing 7377H4 · Emergency Equipment
  > F/A REPORTS FWD GIRT BAR BRACKET NEEDS TO BE TIGHTENED.<[01] SECURED FWD ENTRY DOOR GIRT BAR BRACKET IAW AMM 25-66-02. OPS CHECK GOOD.
- [SDR SWAA2023042530501](https://openairdocs.org/sdr/SWAA2023042530501.md): Lens · missing · Apr 22, 2023 · N435WN · Boeing 7377H4 · Emergency Lighting
  > ROW 12 ABC EMERG. LT. OVERHEAD LENS MISSING<[01] INSTALLED LENS PER M/M 33-51-03
- [SDR SWAA2023041928506](https://openairdocs.org/sdr/SWAA2023041928506.md): Handle · loose · Apr 18, 2023 · N435WN · Boeing 7377H4 · Galley Doors
  > CUSTOMER WALK R-2 AND L-1 DOOR ASSIST HANDLES ARE LOOSE.<[01] ADJUSTED R-2 AND L-1 DOOR ASSIST HANDLES. REF. BOEING 737-700 AMM 52-11-31-400-802.;[02] VERIFIED REPLACEMENT
- [SDR SWAA2023041928505](https://openairdocs.org/sdr/SWAA2023041928505.md): Light · inoperative · Apr 18, 2023 · N435WN · Boeing 7377H4 · Emergency Lighting
  > CUSTOMER REQUEST. R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED REPLACEMENT
- [SDR SWAA2023042028184](https://openairdocs.org/sdr/SWAA2023042028184.md): Bracket · cracked · Apr 16, 2023 · N435WN · Boeing 7377H4 · Trailing Edge Flaps
  > L/H WING DEFLECTION CONTROL PANEL FWD SEAL BRACKET CRACK.<[01] CORRECTION FOR STEP #1 TO READ REMOVED LEFT WING DEFLECTION CONTROL PANEL FORWARD SEAL BRACKET AS PER B 737-700 SRM 51-40-02-0G-0;[02] *** ENTRY 1 WAS ENTERED IN ERROR ***;[03] REMOVED AND REPLACED
- [SDR SWAA2023042024890](https://openairdocs.org/sdr/SWAA2023042024890.md): Girt Bar · dragging · Apr 8, 2023 · N435WN · Boeing 7377H4 · Escape Slide
  > L2 DOOR SLIDE GIRT DRAGGING<[01] REPOSITIONED L2 DOOR SLIDE GIRT PER B737 AMM 25-66-01-400-803-NG;[02] VERIFIED STEP 1
- [SDR SWAA2023042023391](https://openairdocs.org/sdr/SWAA2023042023391.md): Panel · delaminated · Apr 4, 2023 · N435WN · Boeing 7377H4 · Aerodynamic Fairings
  > PANEL 193AL HAS DELAMINATION AT ONE SIDE<[01] APPLIED THE GLASS FABRIC REPAIR PLIES AT DAMAGED AREA ON ACCESS PANEL 193AL. REF B737 SRM 51-70-04-2R-10 REPAIR 10 PARAGRAPH 4. MATERIAL USED GLASS FABRIC PLIES PO#:1690463 AND RESIN EY3804AB PO#: 1800550.;[02] VER
- [SDR SWAA2023041923389](https://openairdocs.org/sdr/SWAA2023041923389.md): Panel · delaminated · Mar 30, 2023 · N435WN · Boeing 7377H4 · Wing, Control Surfaces
  > L/T WING I/B LOWER FAIRING ACEESS PANEL # 194CL HAS SEVERALS FASTENER HOLES BULGING/CRACKED<[01] PREPARED PANEL #194CL FOR REPAIR PER B737 SRM 51-70-06-2R-9 PARA 4.D<BR>APPLIED REPAIR IN DAMAGED AREA AT ACEESS PANEL # 194CL AROUND FASTENER HOLES. AS PER REF B7
- [SDR SWAA2023042022885](https://openairdocs.org/sdr/SWAA2023042022885.md): Panel · cracked · Mar 24, 2023 · N435WN · Boeing 7377H4 · Wing, Control Surfaces
  > LEFT WING LOWER MID T/E ACCESS PANEL # 561BB HAS BULGING/CRACKED AROUND FASTENER HOLES<[01] REPAIRED DAMAGED AREA AT LEFT WING LOWER MID T/E ACCESS PANEL # 561BB REF B737 SRM 51-70-04-2R-9-A00753 (REPAIR 9);[02] VERIFIED ALL STEPS
- [SDR SWAA2023042022086](https://openairdocs.org/sdr/SWAA2023042022086.md): Panel · cracked · Mar 24, 2023 · N435WN · Boeing 7377H4 · Wing, Control Surfaces
  > LEFT WING LOWER L/E ACCESS PANEL # 521UB CRACKED/EXPOSED COMPOSITE<[01] REMOVED DAMAGE AREA PANEL 521 UB. AS PER B737 SRM 51-70-06-2R-9 REPARED AREA AND FABRIC REPAIR PANEL 521UB; AS PER B737 SRM 51-70-06-2R-9 REPAIRED PANEL 521UB; AS PER B737 SRM 51-70-06-2R
- [SDR SWAA2023041920586](https://openairdocs.org/sdr/SWAA2023041920586.md): Panel · elongated · Mar 24, 2023 · N435WN · Boeing 7377H4 · Ventral Structure
  > LEFT VERTICAL STABILIZER ACCESS PANEL # 322A HAS 2 EA ELONGATED FASTENER HOLES<[01] RECEIVED; LOCATED AND DRILLED NEW L/E PANEL (322A) AT VERTICAL STABILIZER PER B737-700 PER SRM 51-40-05-0G-0.;[02] VERIFIED ALL STEPS
- [SDR SWAA2023041922885](https://openairdocs.org/sdr/SWAA2023041922885.md): Panel · cracked · Mar 24, 2023 · N435WN · Boeing 7377H4 · Wing, Control Surfaces
  > LEFT WING LOWER MID T/E ACCESS PANEL # 561BB HAS BULGING/CRACKED AROUND FASTENER HOLES<[01] REPAIRED DAMAGED AREA AT LEFT WING LOWER MID T/E ACCESS PANEL # 561BB REF B737 SRM 51-70-04-2R-9-A00753 (REPAIR 9);[02] VERIFIED ALL STEPS
- [SDR SWAA2023041924744](https://openairdocs.org/sdr/SWAA2023041924744.md): Panel · cracked · Mar 24, 2023 · N435WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > LOWER FUSELAGE CENTER AFT ACCESS PANEL # 194E HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] ACCOMPLISHED REPAIR OF PANEL 194E; REF: B737 SRM 51-70-06-2R-9;[02] VERIFIED REPAIR
- [SDR SWAA2023042020454](https://openairdocs.org/sdr/SWAA2023042020454.md): Panel · elongated · Mar 23, 2023 · N435WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > R/T HORIZONTAL STAB. UPPER ACCESS PANELN # 343AT HAS 2 EACH RUBBER SEALS WITH ELONGATED HOLES<[01] REMOVED AND REPLACED R/T HORIZONTAL STAB. UPPER ACCESS PANELN # 343AT SEAL AS PER 51-40-02-0G-0.;[02] VERIFIED STEP 1.
- [SDR SWAA2023042020455](https://openairdocs.org/sdr/SWAA2023042020455.md): Panel · elongated · Mar 23, 2023 · N435WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB. T/E LOWER ACCESS PANEL # 333AB HAS RUBBER SEAL WITH ELONGATED HOLES<[01] REMOVED AND REPLACED LEFT HORIZONTAL STAB. T/E LOWER ACCESS PANEL # 333AB SEAL AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.
- [SDR SWAA2023042018867](https://openairdocs.org/sdr/SWAA2023042018867.md): Angle · cracked · Mar 20, 2023 · N435WN · Boeing 7377H4 · Wing Main, Frame Structure
  > R/H VAPOR BARRIER UPPER CHORD SUPPORT ANGLE CRACKED @ APPROXIMATELY RBL-7 STA 663.75 MKD DOT<[01] ACCOMPLISHED WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR AT RBL 7 AR PER SRM 57-10-10-2R-5.;[02] VERIFIED ALL STEPS COMPLETED
- [SDR SWAA2023042018225](https://openairdocs.org/sdr/SWAA2023042018225.md): Channel · corroded · Mar 18, 2023 · N435WN · Boeing 7377H4 · Fuselage Structure (General)
  > CORROSION FOUND AFT CARGO LH ZEE CHANNEL FROM STA 727 TO STA 807 LBL 21 WL 155.5 HAS SPOTS OF CORROSION.<[01] REMOVED CORROSION AT AFT CARGO LH ZEE CHANNEL FROM STA 727 TO STA 807 AS PER B737-700 SRM 51-10-02-0G-0 FOUND EXFOLIATED CORROSION THROUGH OUT THE THI
- [SDR SWAA2023042018226](https://openairdocs.org/sdr/SWAA2023042018226.md): Channel · corroded · Mar 18, 2023 · N435WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AFT CARGO RH ZEE CHANNEL FROM STA 727 TO STA 767 HAS SPOTS OF CORROSION RBL 21 WL 155.5.<[01] REMOVED CORROSION AT AFT CARGO RH ZEE CHANNEL FROM STA 727 TO STA 767 AS PER B737-700 SRM 51-10-02-0G-0 FOUND EXFOLIATED CORROSION THROUGH OUT THE THI
- [SDR SWAA2023042017019](https://openairdocs.org/sdr/SWAA2023042017019.md): Bracket · cracked · Mar 15, 2023 · N435WN · Boeing 7377H4 · Fuselage Main, Keel
  > LEFT A/C BAY PNEUMATIC CROSS OVER DUCT MOUNTED ON KEEL BEAM CRACKED AT B.S. 546 LBL. 6'.(51-010) PNEUMATIC DUCT SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED LEFT A/C BAY PNEUMATIC CROSS OVER DUCT SUPPORT BRACKET MOUNTED ON KEEL BEAM B.S. 546 LBL. 6' IN RE
- [SDR SWAA2023042017319](https://openairdocs.org/sdr/SWAA2023042017319.md): Nut Plate · missing · Mar 15, 2023 · N435WN · Boeing 7377H4 · Escape Slide
  > L2 DOOR FWD GIRT BAR FITTING LOWER BRACKET HAS FASTENERS MISSING<[01] REMOVED AND REPLACED MISSING NUT PLATE IN REFERENCE SRM 51-40-02-0G-0.;[02] VERIFIED INSTALLATION;[03] CORRECTION TO FAULT NAME: NUT PLATE MISSING; NOT FASTENER
- [SDR SWAA2023042017018](https://openairdocs.org/sdr/SWAA2023042017018.md): Bracket · cracked · Mar 15, 2023 · N435WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > RIGHT A/C BAY PNEUMATIC CROSS OVER DUCT SUPPORT BRACKET MOUNTED ON KEEL BEAM CRACKED B.S. 546 RBL. 6'. (51-009)<[01] REMOVED AND REPLACED RIGHT A/C BAY PNEUMATIC CROSS OVER DUCT SUPPORT BRACKET MOUNTED ON KEEL BEAM B.S. 546 RBL. 6' IN REF B737 SRM 51-40-02-0G-

Next page: https://openairdocs.org/aircraft/N435WN/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 = 'N435WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N435WN/reports

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