# Service difficulty reports: N406WN, cancelled Mar 13, 2025

A list on [N406WN, cancelled Mar 13, 2025](https://openairdocs.org/deregistered/N406WN-2025-03-13.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 · 307 reports

- [SDR SWAA2024012943900](https://openairdocs.org/sdr/SWAA2024012943900.md): Connector · damaged · Jan 23, 2024 · N406WN · Boeing 7377H4 · Flight Control System Wiring
  > CB POPPED; TRAILING EDGE FLAPS WOULD NOT EXTEND<[01] R&R CONNECTOR D40024P PER SWPM 20-61-11. REPAIRED WIRES W1022-2009R-20 AND W1022-2009B-20 PER SWPM 20-10-04. OPS CHECK GOOD PER AMM 27-51-00. NO OTHER DEFECTS NOTED. NO C/B POPPED.
- [SDR SWAA2024012946071](https://openairdocs.org/sdr/SWAA2024012946071.md): Wire · damaged · Jan 23, 2024 · N406WN · Boeing 7377H4 · Flight Control System Wiring
  > CB POPPED; TRAILING EDGE FLAPS WOULD NOT EXTEND<[01] R&R CONNECTOR D40024P PER SWPM 20-61-11. REPAIRED WIRES W1022-2009R-20 AND W1022-2009B-20 PER SWPM 20-10-04. OPS CHECK GOOD PER AMM 27-51-00. NO OTHER DEFECTS NOTED. NO C/B POPPED.
- [SDR SWAA2023091901730](https://openairdocs.org/sdr/SWAA2023091901730.md): Sensor · faulty · Sep 17, 2023 · N406WN · Boeing 7377H4 · Trailing Flap Position Indicating System
  > SPLIT FLAP INDICATOR AT FLAPS 25; FLAPS WOULD NOT MOVE ALTERNATE; UPON LANDING FLAPS BOTH INDICATOR 25<[01] -FSEU BITE TEST SHOWS; FLAP 4 SKEW AND MAINT MSG # 27-53253;[02] IAW FIM 27-59 TASK 804; NIL NOTED FAULT OF MEASURED DISTANCE FROM THE BALLSCREW NUT TO
- [SDR SWAA2023082191189](https://openairdocs.org/sdr/SWAA2023082191189.md): Panel · elongated · Aug 18, 2023 · N406WN · Boeing 7377H4 · Aerodynamic Fairings
  > 193B FAIRING PANEL HAS SEVERAL ELONGATED HOLES<[01] REMOVED AND REPLACED WING TO BODY FAIRING PANEL 193B IAW AMM 53-51-21.
- [SDR SWAA2023061358041](https://openairdocs.org/sdr/SWAA2023061358041.md): Power Supply · inoperative · Jun 10, 2023 · N406WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1675 INOP WHEN SELECTED ON<[01] REMOVED AND REPLACED M1675 BATTERY POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2023041124840](https://openairdocs.org/sdr/SWAA2023041124840.md): Sign · broken · Apr 8, 2023 · N406WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT SIDE OVERWING EXIT SIGN (LOWER) BROKEN<[01] R-R RIGHT SIDE OVERWING EMERGENCY EXIT SIGN & OPS GOOD PER AMM 33-51-01
- [SDR SWAA2023040724243](https://openairdocs.org/sdr/SWAA2023040724243.md): Light · inoperative · Apr 6, 2023 · N406WN · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY DOOR EXTERIOR EMERGENCY EGRESS LIGHT INOP<[01] RELAMPED PER MM 33-51-04
- [SDR SWAA2023022409520](https://openairdocs.org/sdr/SWAA2023022409520.md): Cover · loose · Feb 23, 2023 · N406WN · Boeing 7377H4 · Emergency Lighting
  > AFT GALLEY EXIT SIGN FELL APART<[01] RE-INSTALLED EXIT SIGN COVER PER AMM 33-51-01. AIRCRAFT OK FOR SERVICE.
- [SDR SWAA2022121280494](https://openairdocs.org/sdr/SWAA2022121280494.md): Sign · loose · Dec 10, 2022 · N406WN · Boeing 7377H4 · Emergency Lighting
  > FA REPORT:EMER EXIT ROW SIGN IN MIDDLE OF CABIN COVER IS LOOSE. AFT FACING SIGN COVER / [01] REINSTALLED EMER EXIT SIGN PER SIP; OK TO SERVICE
- [SDR SWAA2022120578182](https://openairdocs.org/sdr/SWAA2022120578182.md): Sensor · out of limits · Dec 3, 2022 · N406WN · Boeing 7377H4 · Trailing Flap Position Indicating System
  > WHEN SELECTING FLAPS 15 FOR LANDING FLAPS STAYED AT 5. PERFORMED QRH PROCEDURE LANDED FLAPS 15. FOUND THE NR 4 SKEW SENSOR OUT OF LIMITS. R & R THE NR 4 SKEW SENSOR IAW AMM 27-59 00. FLAPS OPS CHECKED GOOD.
- [SDR SWAA2022113075688](https://openairdocs.org/sdr/SWAA2022113075688.md): Battery Pack · inoperative · Nov 27, 2022 · N406WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN EMERGENCY BATTERY PACK AT POSITION M1670 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805. TESTED OK.
- [SDR SWAA2022113075171](https://openairdocs.org/sdr/SWAA2022113075171.md): Battery Pack · inoperative · Nov 23, 2022 · N406WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS 3DEF; 6DEF, 8DEF, 11DEF, AND RT OVERWING HATCH INOPERATIVE. REMOVED AND REPLACED BATTERY PACK M1669 IAW AMM 33-51-06-960-805. TESTED OK.
- [SDR SWAA2022113075172](https://openairdocs.org/sdr/SWAA2022113075172.md): Battery Pack · inoperative · Nov 23, 2022 · N406WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS AT POSITIONS L1 DOOR EXIT SIGN, R1 FLOOR PROXIMITY AND R1 ESCAPE SLIDE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805. TESTED OK.
- [SDR SWAA2022113072046](https://openairdocs.org/sdr/SWAA2022113072046.md): Cargo Track · corroded · Nov 15, 2022 · N406WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK, BS 947, RBL 10, CORRODED. REMOVED THE CARGO TRACK IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW CARGO TRACK IAW SRM 51-40-05-02-0G-0. TREATED AND PRIMED IAW AMM 51-21-41-370-803 AND AMM 51-21-72-370-804. INSTALLED THE NEW CARGO TRACK
- [SDR SWAA2022113070732](https://openairdocs.org/sdr/SWAA2022113070732.md): Floorbeam · cracked · Nov 12, 2022 · N406WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > FLOORBEAM CRACKED AT BS 540, LBL 1, WL 208. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-02-0G-0.
- [SDR SWAA2022113070733](https://openairdocs.org/sdr/SWAA2022113070733.md): Floor Support · cracked · Nov 12, 2022 · N406WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT CRACKED AT BS 540, RBL. 1, WL 208. REMOVED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0. LOCATED & DRILLED A NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0. INSTALLED THE NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0.
- [SDR SWAA2022101156798](https://openairdocs.org/sdr/SWAA2022101156798.md): None · missing · Oct 7, 2022 · N406WN · Boeing 7377H4 · Emergency Lighting
  > R1 DOOR LOWER EXIT SIGN IS NOT MULTI LANGUAGE. / [01] REMOVED AND REPLACED R1 DOOR LOWER EXIT SIGN PER AMM 33-51-01;[02] INSPECTED
- [SDR SWAA2022092941876](https://openairdocs.org/sdr/SWAA2022092941876.md): Slide · dislodged · Sep 27, 2022 · N406WN · Boeing 7377H4 · Escape Slide
  > LEFT AFT EMERGENCY EXIT SLIDE PARTIALLY STICKING OUT BOTTOM OF CONTAINER. / [01] SECURED LEFT AFT EMERGENCY EXIT SLIDE IAW AMM 25-66-01.
- [SDR SWAA2022070726487](https://openairdocs.org/sdr/SWAA2022070726487.md): Sensor · failed · Jul 7, 2022 · N406WN · Boeing 7377H4 · Trailing Edge Flap Control System
  > ON DEPARTURE MOVED FLAP LEVER FROM 5 TO 1 AND RECIEVED A SPLIT FLAP CONDITION ACMS SHOWS #4 SKEW SENSOR FAILED. / [01] R&R #4 FLAP SKEW SENSOR PER AMM 27-59-01 OPS CHECK GOOD AT THIS TIME AND NO FAULT NOTED.
- [SDR SWAA2022051206309](https://openairdocs.org/sdr/SWAA2022051206309.md): Light · loose · May 10, 2022 · N406WN · Boeing 7377H4 · Emergency Lighting
  > L-1 DOOR; EMERGENCY EXIT LIGHT LENS IS LOOSE. / [01] REPLACED L-1 DOOR; EMERGENCY EXIT LIGHT ASSEMBLY IAW AMM 33-51-01-960-802<BR>OPS CK GOOD;[02] VERIFIED STEP 1<BR>AUDIT C/W
- [SDR SWAA2022042900286](https://openairdocs.org/sdr/SWAA2022042900286.md): Battery Pack · inoperative · Apr 28, 2022 · N406WN · Boeing 7377H4 · Emergency Lighting
  > EXTERNAL AFT ENTRY EMERGENCY LIGHT INOP. / [01] RE-LAMP NO HELP; FOUND BATTERY PACK AT FAULT; R+R AFT TOP LEFT BATTERY PACK PER AMM 33-51-06; OPS CK?D GOOD.
- [SDR SWAA2022013164132](https://openairdocs.org/sdr/SWAA2022013164132.md): Panel · elongated · Jan 26, 2022 · N406WN · Boeing 7377H4 · Aerodynamic Fairings
  > 194E PANEL FWD EDGE HAS TWO HOLES ELONGATED 9 EACH TOTAL ON FWD EDGE. BOTH LH AND RH LEADING EDGE 3RD ONE BOTH SIDE COMING INDRD IF COUNTING LH TO RH 3RD HOLE AND 7TH HOLE ELONGATED MARKED PANEL; 194E PANEL FWD EDGE HAS TWO HOLES ELONGATED 9 EACH TOTAL ON FWD
- [SDR SWAA2021091516763](https://openairdocs.org/sdr/SWAA2021091516763.md): Girt Bar · out of position · Sep 11, 2021 · N406WN · Boeing 7377H4 · Emergency Equipment
  > FLIGHT ATTENDANT UNABLE TO ARM AFT GALLEY SERVICE DOOR SLIDE; / [01] INSTALLED CORRECT GIRT BAR REFERENCE B737 AMM CH 25-66-01. OPS CHECK GOOD. ENTERED FOR E143284 AFTER DEPARTURE
- [SDR SWAA2021032958843](https://openairdocs.org/sdr/SWAA2021032958843.md): Retainer · cracked · Mar 25, 2021 · N406WN · Boeing 7377H4 · Wing Main, Frame Structure
  > RIGHT WING UPPER AFT FIXED PANEL TRAILING EDGE ABOVE NACELLE STRUT FAIRING SEAL RETAINER CRACKED / REMOVED AND REPLACED NACELLE STRUT FAIRING SEAL RETAINER PER SRM 51-40-02
- [SDR SWAA2021032256653](https://openairdocs.org/sdr/SWAA2021032256653.md): Light · faulty · Mar 17, 2021 · N406WN · Boeing 7377H4 · Emergency Lighting
  > FO SIDE EMERGENCY EXIT DOOR WHITE LIGHT DIM. (OVERWING DOOR). / CLOSING DMA #0371359 RELAMPED; REF AMM 33-21-00 CLOSING # 72357
- [SDR SWAA2021021548063](https://openairdocs.org/sdr/SWAA2021021548063.md): Door · out of adjust · Feb 9, 2021 · N406WN · Boeing 7377H4 · Cargo/Baggage Doors
  > AFT CARGO COMPARTMENT DOOR HANDLE HARD TO CLOSE / PERFORMED ADJUSTMENT ON AFT CARO COMPARTMENT DOOR IAW B737-700 AMM 52-31-00-820-801 STEP 2.K(1); AND PERFORMED LUBRICATION IAW B737-700 AMM 12-25- 31-640-801 TOOL USED:CALIPER PART NUMBER:800-197-30 S/N:A181350
- [SDR SWAA2021021548062](https://openairdocs.org/sdr/SWAA2021021548062.md): Handle · out of adjust · Feb 9, 2021 · N406WN · Boeing 7377H4 · Cargo/Baggage Doors
  > FDW CARGO COMPARTMENT DOOR HANDLE HARD TO_CLOSE / PERFORMED ADJUSTMENT ON FWD CARGO COMPARTMENT DOOR IAW B737-700 AMM 52-31-00-820-801 STEP 2.K(1) TOOL USED: DIGITAL CALIPER P/N:500-197- 30 S/N:A18135097 DUE DATE:03 JAN 22; FEELER GAUGE P/N:2ZVEG S/N:AE-37272
- [SDR SWAA2021021546464](https://openairdocs.org/sdr/SWAA2021021546464.md): Scuff Plate · cracked · Jan 31, 2021 · N406WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT / REPAIRED BY WELD SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737- 700 SRM 53-60-15-2R-1; REPAIR 1 AND BAC 5975
- [SDR SWAA2021021544458](https://openairdocs.org/sdr/SWAA2021021544458.md): Stringer Splice · cracked · Jan 16, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRUCTURE ON STRINGER SPLICE LOCATED ON BST 360 STR 28RH AT EQUIPMENT ELECTRONIC COMP / REPLACED STRINGER SPLICE LOCATED ON BS360 STR28RH AT EQUIPMENT ELECTRONIC COMPARTMENT IAW B737-700 SRM 51-40-02 MATERIAL USED PN 7075 TO +0.036' PO 2020-214270
- [SDR SWAA2021021644455](https://openairdocs.org/sdr/SWAA2021021644455.md): Stringer Splice · corroded · Jan 15, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRUCTURE ON STRINGER SPLICE BST 360 STR 27RH WL 148.5 AT EQUIPMENT ELECTRONIC COMP / REPLACED STRINGER SPLICE LOC ON BS360 STR27RH WL WL 148.5 AT EQUIPMENT ELECTRONIC COMP IAW SPM B737-700 51-40-02 AND DWG140A9101 SHEET 17 REV 51-10-02 ITEM 9 NOT FO
- [SDR SWAA2021021644456](https://openairdocs.org/sdr/SWAA2021021644456.md): Stringer Splice · corroded · Jan 15, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRUCTURE ON STRINGER SPLICE BST 360 STR 23RH WL 130 AT EQUIPMENT ELECTRONIC COMP / REPLACED STRINGER SPLICE BS 360; STR.23R WL 160.5 EQUIPMENT ELECTRONIC COMPARTMENT IAW B737-700 SRM 51-10-02 ABD DRAWING #140A9101 REV. R FABRICATED FROM 70-75-01 0.0
- [SDR SWAA2021021543526](https://openairdocs.org/sdr/SWAA2021021543526.md): Stringer · corroded · Jan 13, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRUCTURE STRINGER 23RH AT BST 360 MORE 4 INCH AT EQUIPMENT ELECTRONIC COMP WL 165.00 / EVALUATION CORROSION ON STRUCTURE STRINGER 23RH AT BS360 MORE 4 INCH AT EQUIPMENT ELECTRONIC COMPARTMENT AND FOUND OUT OF ALLOWABLE DAMAGE LIMITS I.A.W B737-700SR
- [SDR SWAA2021021644138](https://openairdocs.org/sdr/SWAA2021021644138.md): Angle · cracked · Jan 12, 2021 · N406WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS 947.5 AND STR 26L AT AFT CARGO COMPARTMENT / REPLACED ANGLE SUPPORT LOCATED BS947.5 AND STR 26L AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG #149A8103 REV.-
- [SDR SWAA2021021643523](https://openairdocs.org/sdr/SWAA2021021643523.md): Support · corroded · Jan 12, 2021 · N406WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOC BTW BS727 TO BS767 AND STR 25R WL 156.5 AFT CARGO COMPARTMENT / REPLACED SSUPORT ZEE LOCATED BTW BS 727 TO BS 767 AND STR 25-R WL 156.5 AFT CARGO COMPARTMENT DUE TO FOUND OUT LIMITS MEASURE ARE: L=1.813' W=1.404' D=0.013' TOOL USED DI
- [SDR SWAA2021021544137](https://openairdocs.org/sdr/SWAA2021021544137.md): Rivet · broken · Jan 12, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > BROKEN EXTERNAL SKIN HEAD RIVETS (6E/A) LOC S-23R BTW BS 360 MORE 5 INCH AT LOWER FUSELAGE / REPLACED RIVETS (6EA) LOC S-23R BTW BS 360 MORE 5' AT LOWER FUSELAGE IAW SRM B737-700 51-40-02. THIS WORK IS DOCUMENTED ON NRC L190893
- [SDR SWAA2021021543525](https://openairdocs.org/sdr/SWAA2021021543525.md): Stringer · corroded · Jan 12, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER LOCATED BS 360 TO BS 380 STR 28R WL 148.5 AT EQUIPMENT ELECTRONIC COMP / PERFORMED PERMANENT REPAIR ON STRINGER LOCATED BS 360 TO BS 400 STR 28R WL 148.5 AT EQUIPMENT ELECTRONIC COMPARTMENT I.A.W EA #21-153-00190 REV. IR AND 53-0023-21 REV 0
- [SDR SWAA2021021543522](https://openairdocs.org/sdr/SWAA2021021543522.md): Support · corroded · Jan 12, 2021 · N406WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOC BS727 TO BS847 STR 25L WL 156.5 AFT CARGO COMPARTMENT / EVALUATED SUPPORT ZEE LOC BS 727 TO BS847 STR25L WL 156.5 AFT CARGO COMPARTMENT AND FOUND OUT LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 STEP 4A(2)(A) FIGURE 103 DE
- [SDR SWAA2021021543524](https://openairdocs.org/sdr/SWAA2021021543524.md): Stringer · corroded · Jan 12, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER LOCATED BS 360 TO BS 380 STR 27R WL 148.5 AT EQUIPMENT ELECTRONIC COMP / PERFORMED PERMANENT REPAIR ON STRINGER 27R BS 360 TO BS 380 W/148.5 AT EQUIPMENT ELECTRONIC COMP IAW SRM B737-700 53-00-03-2R REPAIR 1 FIG 206 MATERIAL USED ON STRINGER
- [SDR SWAA2021021545074](https://openairdocs.org/sdr/SWAA2021021545074.md): Seat Track · worn · Jan 12, 2021 · N406WN · Boeing 7377H4 · Buffet/Galleys
  > WEAR ON TRACK RAIL-ASSY FIRST OFFICER RAIL AFT LT AND RT SIDE AT COCKPIT (2 EA) / REPLACED TRACK RAIL-ASSY FIRST OFFICER RAIL AFT LT AND RT SIDE AT COCKPIT (2EA) IAW B737-700 AMM 25-11-11-400-801
- [SDR SWAA2021021545075](https://openairdocs.org/sdr/SWAA2021021545075.md): Seat Track · worn · Jan 12, 2021 · N406WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > WEAR ON TRACK RAIL-ASSY CAPTAIN RAIL AFT LT SIDE AT COCKPIT (1 EA) / REPLACED TRACK RAIL-ASSY CAPTAIN RAIL AFT LT SIDE AT COCKPIT (1EA) IAW B737-700 AMM 25-11-11-400-801
- [SDR SWAA2021042345628](https://openairdocs.org/sdr/SWAA2021042345628.md): Panel · cracked · Jan 10, 2021 · N406WN · Boeing 7377H4 · APU Core Engine
  > CRACK AIR INLET PLENUM I/B PANEL ASSEMBLY ON APU COMPARTMENT (1 EA) / REPLACED ANGLE LOC. ON AIR INLET PLENUM I/B PANEL ASSEMBLY ON APU COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DRAWING #353A2010 REV. 'B' PART NUMBER USED 353A2010-18 PO #20
- [SDR SWAA2021021544125](https://openairdocs.org/sdr/SWAA2021021544125.md): Support Angle · cracked · Jan 10, 2021 · N406WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT BS 500 D AT LEVEL STRINGER 28L FWD CARGO COMPARTMENT / REPLACED SUPPORT ANGLE LOC. BS 500D AT LEVEL STRINGER 28L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 REV.A FABRICATED FROM ALUMINUM SHEET 2024T3.040
- [SDR SWAA2021021544393](https://openairdocs.org/sdr/SWAA2021021544393.md): Stringer · cracked · Jan 10, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 23L BS 540 FWD CARGO COMPARTMENT / PERFORMED PERMANENT REPAIR ON STRINGER 23L BS540 FWD CARGO COMPARTMENT BTW 500D TO BS 540 IAW B737- 700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED ON STRINGER SECTION (-7) 7075-T6 0.040' CHANNEL (-2) 7
- [SDR SWAA2021021544394](https://openairdocs.org/sdr/SWAA2021021544394.md): Stringer · cracked · Jan 10, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 25L AT BS 540 FWD CARGO COMPARTMENT / PERFORMED PERMANENT REPAIR ON STRINGER 25L AT BS 540 FWD CARGO COMPARTMENT BTW BS 500D TO BS 540 IAW B737-700 SRM 53-00-03-2R REPAIR 1 FIGURE 206 MATERIAL USED ON STRINGER SECTION (-7) 7075-T6 0.045' CHANNEL
- [SDR SWAA2021021544395](https://openairdocs.org/sdr/SWAA2021021544395.md): Stringer · cracked · Jan 10, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 26L AT BS 540 FWD CARGO COMPARTMENT / EVALUATED ALLOWABLE DAMAGE LIMITS ON STR 26L BS 540 FWD CARGO COMPARTMENT AND FOUND OUT LIMITS DUE TO CRACK IAW SRM B737-700 53-00-03-1A-1 AND PERFORMED PERMANENT REPAIR ON STRINGER 26L BTW BS500D TO BS 540
- [SDR SWAA2021021544979](https://openairdocs.org/sdr/SWAA2021021544979.md): Sidewall Panel · scratched · Jan 10, 2021 · N406WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > SCRATCH ON INNER PANE SIDEWALL PANEL 241 YAW (1EA) AND 241 YEW (2EA) AT PASSENGER CABIN (3 EA) / PERFORMED PERMANENT REPAIR ON STRINGER 25R BTW BS500L TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIG 206 MATERIAL USED ON STRINGER SECTION (-7) 7075-T6 0.040
- [SDR SWAA2021021543169](https://openairdocs.org/sdr/SWAA2021021543169.md): Stringer Clip · cracked · Jan 9, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACK TIE CLIP LOCATED ON STA277 AND STR10R AT PASSENGER CABIN / EVALUATED ALLOWABLE DAMAGE LIMITS OF TIE CLIP LOCATED ON STA STA277 AND STR 10R AT PASSENGER CABIN AND NO FOUND ALLOWABLE FOR CRACK ON SRM MADE TIE CLIP FROM BAC/493-852 P/N 2016 557447 IAW DWG 1
- [SDR SWAA2021021543362](https://openairdocs.org/sdr/SWAA2021021543362.md): Frame · cracked · Jan 9, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME LOCATED ON STA312 AND STR5L AT PASSENGER CABIN / PERFORMED REPAIR ON FRAME LOCATED ON STA 312 AND STR 5L AT PASSENGER CABIN IAW SRM B737-700 53-10-07-2R-1 REPAIR 1. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700 ANGLE FABRICATED FROM 7075-T0 -0.
- [SDR SWAA2021021543171](https://openairdocs.org/sdr/SWAA2021021543171.md): Frame · cracked · Jan 9, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME LOCATED ON BS827 BETWEEN STR8L AND STR9L AT PASSENGER CABIN / REPAIRED FRAME LOCATED ON BS827 BETWEEN STR 8L TO STR 9L AT PASSENGER CABIN IAW EA # 1-A53-12114 REV 5 PARTS NUMBER USED SWA 53100010-003 PO # SW202000865
- [SDR SWAA2021021543170](https://openairdocs.org/sdr/SWAA2021021543170.md): Frame · cracked · Jan 9, 2021 · N406WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME LOCATED ON BS867 BETWEEN STR8R AND STR9R AT PASSENGER CABIN / REPAIRED FRAME LOCATED ON BS 867 AND BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN IAW EA # 1-A53-12114 REV 5 PARTS NUMBER USED SWA 53100010-003 PO # 2020 -136748 AND SWA 53100010-006 PO#

Next page: https://openairdocs.org/deregistered/N406WN-2025-03-13/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 = 'N406WN' AND deregistration_id = 'N406WN-2025-03-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N406WN-2025-03-13/reports

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