# Service difficulty reports: N913WN A list on [N913WN](https://openairdocs.org/aircraft/N913WN.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 5 · 247 reports - [SDR SWAA2026070617449](https://openairdocs.org/sdr/SWAA2026070617449.md): Hydrolock · out of tolerance · Jul 1, 2026 · N913WN · Boeing 7377H4 · Passenger Compartment Equipment > PASSENGER SEAT ROW RECLINES INTO EXIT ROW 9B; 9C. ADJUSTED HYDRO-LOCKS TO THE LOCK POSITION PER AMM 25-22-00 - [SDR SWAA2025120442741](https://openairdocs.org/sdr/SWAA2025120442741.md): Apu · shutdown · Dec 4, 2025 · N913WN · Boeing 7377H4 · APU Core Engine > AT CRUISE FL 400 RECEIVED APU LOP LIGHT. APU DID AUTO SHUTDOWN NH30. PERFORMED OPERATONAL TEST OF APU AND TEST PASS IAW AMM 49-11-00. - [SDR SWAA2024122680900](https://openairdocs.org/sdr/SWAA2024122680900.md): Control Module · faulty · Dec 23, 2024 · N913WN · Boeing 7377H4 · Detection System > ENG1 OVHT; ENG2 OVHT; ENG 1&2&APU FIRE HANDLES ILLUMINATED & WHEEL WELL LIGHT ILLUMINATED ON TAKEOFF ROLL WITH ASSOCIATED FIRE WARNING BELLS ON TAKEOFF ROLL (125KT)<[01] R&R ENG & APU FIRE CONTROL PANEL IAW AMM 26-00-01;[02] PERFORMED THE FOLLOWING OPERATIONAL - [SDR SWAA2024122680732](https://openairdocs.org/sdr/SWAA2024122680732.md): Control Panel · faulty · Dec 23, 2024 · N913WN · Boeing 7377H4 · Detection System > ENG1 OVHT; ENG2 OVHT; ENG 1&2&APU FIRE HANDLES ILLUMINATED & WHEEL WELL LIGHT ILLUMINATED ON TAKEOFF ROLL WITH ASSOCIATED FIRE WARNING BELLS ON TAKEOFF ROLL (125KT)<[01] R&R ENG & APU FIRE CONTROL PANEL IAW AMM 26-00-01;[02] PERFORMED THE FOLLOWING OPERATIONAL - [SDR SWAA2024032166186](https://openairdocs.org/sdr/SWAA2024032166186.md): Battery Pack · no test · Mar 21, 2024 · N913WN · Boeing 7377H4 · Emergency Lighting > M1672 EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST<[01] REMOVED AND REPLACED M1672 EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06 - [SDR SWAA2024032166169](https://openairdocs.org/sdr/SWAA2024032166169.md): Seal · cracked · Mar 21, 2024 · N913WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED.<[01] R&R RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL. IAW AMM 53-31-31;[02] C/W INSPECTION REQUIREMENT - [SDR SWAA2024032166182](https://openairdocs.org/sdr/SWAA2024032166182.md): Seal · cracked · Mar 21, 2024 · N913WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > LH HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LH HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL PER AMM 53-31-31;[02] C/W INSPECTION - [SDR SWAA2024032166170](https://openairdocs.org/sdr/SWAA2024032166170.md): Vapor Barrier · cracked · Mar 21, 2024 · N913WN · Boeing 7377H4 · Fuselage Main, Bulkhead > WING CENTER SECTION REAR SPAR VAPOR BARRIER HAS SINGLE VERTICAL CRACK 15.8 INCH IN LONG BETWEEN STIFFENER AT LBL 45.64 & LBL 31.83.<[01] REPAIRED WING CENTER SECTION REAR SPAR VAPOR BARRIER VERTICAL CRACK 15.8 INCH IN LONG BETWEEN STIFFENER AT LBL 45.64 & LBL - [SDR SWAA2023080479629](https://openairdocs.org/sdr/SWAA2023080479629.md): Gusset · cracked · Jul 17, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2023-431323<[01] TOOL USED CALIPER P/N: 500-196-30; S/N: A20231842; DUE DATE: 21-FEB-24;[02] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 - [SDR SWAA2023080478249](https://openairdocs.org/sdr/SWAA2023080478249.md): Floor Support · cracked · Jul 14, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK WEB - INTERCOSTAL BTW BS847 TO BS867 WL208 FLOOR LEVEL AT AFT CARGO COMPARTMENT 2023-431308<[01] OPEN FAULT HAS AN ERROR AND IS BEING CORRECTED BY RAISING A NEW FAULT; SEE [TTG8Q00M7MDZ];[02] CORRECTED STEP 1:FAULT SOLVED IN OTHER FAULT DUE TO REPLACED P - [SDR SWAA2023080478569](https://openairdocs.org/sdr/SWAA2023080478569.md): Support Angle · cracked · Jul 14, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK SUPPORT ANGLE LOC. BS 847 BETWEEN BS867 LBL 21 AT AFT GALLEY AREA AT PASSENGER CABIN 2023-431309<[01] REPLACED SUPPORT ANGLE LOC. BS 847 BETWEEN BS867 LBL 21 AT AFT GALLEY AREA AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG - [SDR SWAA2023080476966](https://openairdocs.org/sdr/SWAA2023080476966.md): Angle · cracked · Jul 10, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND BL 0 WL 208 AT FWD GALLEY AREA 2023-431290<[01] REPLACED ANGLE INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND BL 0 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DW - [SDR SWAA2023080476691](https://openairdocs.org/sdr/SWAA2023080476691.md): Stringer · corroded · Jul 9, 2023 · N913WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CORROSION STRINGER 23R LOCATED BS540 WL164.1 AT FWD CARGO COMPARTMENT 2023-431283<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 200048001; CAL DUE DATE: 01-MAY-24;[ - [SDR SWAA2023080476695](https://openairdocs.org/sdr/SWAA2023080476695.md): Stringer · corroded · Jul 9, 2023 · N913WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CORROSION STRINGER 27R LOCATED BS540 WL150.1 AT FWD CARGO COMPARTMENT 2023-431285<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220272712; CAL DUE DATE: 17-DEC-23;[ - [SDR SWAA2023080476690](https://openairdocs.org/sdr/SWAA2023080476690.md): Rib · cracked · Jul 9, 2023 · N913WN · Boeing 7377H4 · Vertical Stabilizer, Spar/Rib > CRACK RIB 8 ON ACCESS PANEL 321A AT VERTICAL STABILIZER 2023-431281<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED RIB 8 LOCATED ON ACCESS PANEL 321A AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-10 - [SDR SWAA2023080276692](https://openairdocs.org/sdr/SWAA2023080276692.md): Stringer · corroded · Jul 9, 2023 · N913WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CORROSION STRINGER 25R LOCATED BS540 WL155.3 AT FWD CARGO COMPARTMENT 2023-431287<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TE - [SDR SWAA2023080276681](https://openairdocs.org/sdr/SWAA2023080276681.md): Fitting · cracked · Jul 8, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK FLOOR STRUCTURE FITTING LOCATED BS947.5 AND STR26R AT AFT CARGO COMPARTMENT 2023-431262<[01] REPLACED FITTING AND FASTENERS LOCATED BS947.5 AND STR26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 Ï¿½TEM 9 AND DWG 149A8103 SH - [SDR SWAA2023080276684](https://openairdocs.org/sdr/SWAA2023080276684.md): Support Bracket · cracked · Jul 8, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK FLOOR STRUCTURE SUPPORT BRACKET LOCATED BTW BS907 TO BS927 AND STR26L AT AFT CARGO COMPARTMENT 2023-431264<[01] REPLACED SUPPORT BRACKET LOCATED BTW BS907 TO BS927 AND STR26L AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02; SRM 51-10-02 ITEM 9 AND DRA - [SDR SWAA2023080276685](https://openairdocs.org/sdr/SWAA2023080276685.md): Support Bracket · cracked · Jul 8, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK FLOOR STRUCTURE LOCATED BS867 AND STR26L AT AFT CARGO COMPARTMENT 2023-431270<[01] REPLACED BRACKET AND FASTENERS LOCATED FLOOR STRUCTURE BS867 AND STR26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 149A8102 REV:-
SEE INDIVIDUAL S - [SDR SWAA2023080276683](https://openairdocs.org/sdr/SWAA2023080276683.md): Support Bracket · cracked · Jul 8, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK FLOOR STRUCTURE SUPPORT BRACKET LOCATED BS827 AND STR25R AT AFT CARGO COMPARTMENT 2023-431271<[01] REPLACED FLOOR STRUCTURE SUPPORT BRACKET LOCATED BS827 AND STR25R AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 146A8 - [SDR SWAA2023080276686](https://openairdocs.org/sdr/SWAA2023080276686.md): Support Bracket · cracked · Jul 8, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK FLOOR STRUCTURE SUPPORT BRACKET LOCATED BS807 AND STR25R AT AFT CARGO COMPARTMENT 2023-431272<[01] REPLACED SUPPORT BRACKET LOCATED FLOOR STRUCTURE BS807 AND STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DRAWING 146 - [SDR SWAA2023080276687](https://openairdocs.org/sdr/SWAA2023080276687.md): Cargo Track · cracked · Jul 8, 2023 · N913WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CRACK TRACK RBBL 13.84 LOCATED BS727E AFT CARGO COMPARTMENT 2023-431273<[01] REFER TO FAULT TTG8Q00M3RDR WHERE EA 23-153-02226 WAS ADDED AS A SUBTASK.;[02] REFER TO FAULT TTG8Q00M3RDR WHERE EA 23-153-02226 WAS ADDED AS A SUBTASK. - [SDR SWAA2023080276688](https://openairdocs.org/sdr/SWAA2023080276688.md): Cargo Track · cracked · Jul 8, 2023 · N913WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CRACK TRACK RBBL 13.84 LOCATED BS727C AFT CARGO COMPARTMENT 2023-431274<[01] REPAIRED TRACK AT RBL 13.84 AND BSTA 727B & BSTA 767 AFT CARGO COMPARTMENT IAW EA 23-153-02226 REV1 AND EA 23-153-02226-WIP1 REV2 SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1 CRACK ON FRAME LOCATED BS 312AT LEVEL STR 5LAT FWD GALLEY AREA 2023-431241<[01] PERFORMED REPAIR ON BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L IAW EA M-22-153-01244
SEE TASK CARD: TTG8Q00M3J6Z;[02] PERFORMED REPAIR ON BS 312 FRAM - [SDR SWAA2023080376424](https://openairdocs.org/sdr/SWAA2023080376424.md): Floor Panel · cracked · Jul 7, 2023 · N913WN · Boeing 7377H4 · Fuselage Floor Panel > CRACK FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2023-431239<[01] REPLACED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 453A2610 REV: E;[02] CORRECTED STEP 1.
REPLACED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW - [SDR SWAA2023080775892](https://openairdocs.org/sdr/SWAA2023080775892.md): Panel · cracked · Jul 6, 2023 · N913WN · Boeing 7377H4 · Wing, Control Surfaces > CRACK ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2023-431181<[01] TOOL USED CALIPER P/N 500-197-30 S/N:B20189527 DUE DATE 26 DEC23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18196126; DUE DATE: 26-MAR-24.;[03] TOOL USED HOT BONDER P/N: HCS9200B-AV S/N - [SDR SWAA2023080775895](https://openairdocs.org/sdr/SWAA2023080775895.md): Panel · cracked · Jul 6, 2023 · N913WN · Boeing 7377H4 · Wing, Control Surfaces > CRACK ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2023-431184<[01] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18196126; DUE DATE: 26-MAR-24.;[02] TOOL USED HOT; BONDER P/N: HCS9200B-AV S/N: 18196126 DUE DATE: 26-MAR-24;[03] TOOL USED: SCALE: P/N:CR5200 S/N:8 - [SDR SWAA2023080475893](https://openairdocs.org/sdr/SWAA2023080475893.md): Support Angle · cracked · Jul 6, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON SUPPORT ANGLE LOCATED BS 500D BTW STR 18R AND STR 19R WING-TO-BODY FAIRING SUPPORT STRUCTURE 2023-431183<[01] REPLACED SUPPORT ANGLE LOCATED BS 500D BTW STR 18R AND STR 19R WING-TO-BODY FAIRING SUPPORT STRUCTURE IAW B737-700 SRM 51-10-02; SRM 51-40-02 - [SDR SWAA2023080476187](https://openairdocs.org/sdr/SWAA2023080476187.md): Support Angle · cracked · Jul 6, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON SUPPORT ANGLE LOCATED BS 500D BTW STR 18L AND STR 19L WING-TO-BODY FAIRING SUPPORT STRUCTURE 2023-431193<[01] REPLACED SUPPORT ANGLE LOCATED BS 500D BTW STR 18L AND STR 19L WING-TO-BODY FAIRING SUPPORT STRUCTURE IAW B737-700 SRM 51-10-02; SRM 51-40-02 - [SDR SWAA2023080775397](https://openairdocs.org/sdr/SWAA2023080775397.md): Flap · debonded · Jul 5, 2023 · N913WN · Boeing 7377H4 · Trailing Edge Flaps > CUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT RT WING 2023-431125<[01] TOOL USED CALIPER P/N 500-197-30 S/N 15120589 DUE DATE 13 FEB 24;[02] THE DAMAGE WAS REPAIRED PER 737-700 SRM-57-53-01-2R-18 REPAIR 18 WITH A DEVIATION DUE TO THE RE - [SDR SWAA2023080475386](https://openairdocs.org/sdr/SWAA2023080475386.md): Intercostal · cracked · Jul 5, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON INTERCOSTAL LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO RBL 24.75 AT CENTER SECTION 2023-431107<[01] INSTALLED NEW INTERCOSTAL AND FASTENERS LOC.FLOOR STRUCTURE BS 540 BTW BL 0 TO RBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM - [SDR SWAA2023080475382](https://openairdocs.org/sdr/SWAA2023080475382.md): Intercostal · cracked · Jul 5, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON INTERCOSTAL LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO LBL 24.75 AT CENTER SECTION 2023-431108<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO LBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10- - [SDR SWAA2023080475393](https://openairdocs.org/sdr/SWAA2023080475393.md): Intercostal · cracked · Jul 5, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON INTERCOSTAL LOCATED FLOOR STRUCTURE BS 540 BTW RBL 24.75 TO RBL 45.5 AT CENTER SECTION 2023-431113<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BS 540 BTW RBL 24.75 TO RBL 45.5 AT CENTER SECTION IAW B737-700 SRM 51-40-02 SRM 51-10-0 - [SDR SWAA2023080475394](https://openairdocs.org/sdr/SWAA2023080475394.md): Angle · cracked · Jul 5, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 CENTER SECTION 2023-431116<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112811019; DUE DATE: 25-JAN-24 AND - [SDR SWAA2023080475381](https://openairdocs.org/sdr/SWAA2023080475381.md): Floor Support · cracked · Jul 5, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON INTERCOSTAL LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO RBL 24.75 AT CENTER 2023-431106<[01] OPEN FAULT HAS AN ERROR AND IS BEING CORRECTED BY RAISING A NEW FAULT; SEE TTG8Q00M1CBD;[02] TASK CARD COMPLETED
FAULT HAS AN ERROR AND IS BEING CORRECTED - [SDR SWAA2023080475387](https://openairdocs.org/sdr/SWAA2023080475387.md): Stiffener · cracked · Jul 5, 2023 · N913WN · Boeing 7377H4 · Horizontal Stabilizer Structure > CRACK STIFFENER 2 INSPAR RIB 129.50 AT LT HORIZONTAL STABILIZER 2023-431111<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 210138103; CAL DUE DATE: 02-MAY-24;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X1693P030456; DUE DA - [SDR SWAA2023080475388](https://openairdocs.org/sdr/SWAA2023080475388.md): Stiffener · cracked · Jul 5, 2023 · N913WN · Boeing 7377H4 · Horizontal Stabilizer Structure > CRACK INSPAR RIB STIFFENER 2 STAB STA 129.50 AT RT HORIZONTAL STABILIZER 2023-431114<[01] TOOL USED P/N NORTEC 600D S/N 60009161631 DUE DATE 31/JAN/24;[02] TOOL USED EDDY CURRENT EQUIPMENT PN:NORTEC 600D; SN:210138103; DUE DATE:02-MAY-24;[03] TOOL USED EDDY CU - [SDR SWAA2023080777740](https://openairdocs.org/sdr/SWAA2023080777740.md): Frame · cracked · Jul 4, 2023 · N913WN · Boeing 7377H4 · Fuselage Main, Frame > CUSTOMER REQUEST CRACK ON CUT OUT OF EXTERNAL GROUND SERVICE DOOR 114AR LOWER FUSELAGE 2023-431020<[01] ET TOOL USED PN NORTEC 600D; SN 210138203; DUE DATE 09-JUN-24;[02] REPAIRED CUT OUT OF EXTERNAL GROUND SERVICE DOOR 114AR LOWER FUSELAGE IAW B737-700 SRM 53 - [SDR SWAA2023080774876](https://openairdocs.org/sdr/SWAA2023080774876.md): Slat · cracked · Jul 4, 2023 · N913WN · Boeing 7377H4 · Leading Edge Devices > CRACK LOWER SURFACE SLAT 5 LOCATED SLAT STATION 85.19 RT WING 2023-431043<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138203 AND DUE DATE: 09-JUN-24.;[02] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 6OOD; S/N:210138003 AND DUE DATE: 27-MAR-24.;[03] - [SDR SWAA2023080774877](https://openairdocs.org/sdr/SWAA2023080774877.md): Slat · cracked · Jul 4, 2023 · N913WN · Boeing 7377H4 · Leading Edge Devices > CRACK LOWER SURFACE SLAT 8 LOCATED SLAT STATION 451.97 RT WING 2023-431044<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X1693P030456; DUE DATE: 12 MAR 24.;[02] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022237; DUE DATE: 26-J - [SDR SWAA2023080474871](https://openairdocs.org/sdr/SWAA2023080474871.md): Vapor Barrier · cracked · Jul 4, 2023 · N913WN · Boeing 7377H4 · Fuselage Main, Bulkhead > CUSTOMER REQUEST EVALUATE CRACK ON VAPOR BARRIER LH SIDE BSTA 663 2023-431016<[01] TOOL USED CALIPER P/N 500-197-30 S/N B20189527 DUE DATE 26/DEC/23.;[02] TOOL USED: HOTBONDER: P/N:HCS9200B-AV S/N:18175478 DUE DATE:24-SEP-23;[03] TOOL USED: SCALE: P/N:CR5200 S - [SDR SWAA2023080281881](https://openairdocs.org/sdr/SWAA2023080281881.md): Door · cracked · Jul 4, 2023 · N913WN · Boeing 7377H4 · Landing Gear Doors > CUSTOMER REQUEST CRACK ON INTERNAL SURFACE OF CENTER MLG DOOR RT SIDE. 2023-431015<[01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X11290U021704; DUE DATE: 12 MAR 24;[02] TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N: A21125526; DUE DATE: 05-NOV- - [SDR SWAA2023062671526](https://openairdocs.org/sdr/SWAA2023062671526.md): Fuse · inoperative · Jun 24, 2023 · N913WN · Boeing 7377H4 · Emergency Lighting > LEFT AFT EMERGENCY EXTERIOR GROUND ILLUMINATION LIGHT INOP<[01] R&R FUSE AND CONTACT ON LH AFT EMERGENCY LIGHT REF AMM 33-51-00. OPS CHKS GOOD - [SDR SWAA2023062671736](https://openairdocs.org/sdr/SWAA2023062671736.md): Contact · inoperative · Jun 24, 2023 · N913WN · Boeing 7377H4 · Emergency Lighting > LEFT AFT EMERGENCY EXTERIOR GROUND ILLUMINATION LIGHT INOP<[01] R&R FUSE AND CONTACT ON LH AFT EMERGENCY LIGHT REF AMM 33-51-00. OPS CHKS GOOD - [SDR SWAA2023041425921](https://openairdocs.org/sdr/SWAA2023041425921.md): Cover · out of adjust · Apr 11, 2023 · N913WN · Boeing 7377H4 · Galley Doors > R1 DOOR LINER AND SLIDE COVER STAINED<[01] CLEANED R1 DOOR LINER & SLIDE COVER IAW AMM 25-00-00.;[02] C/W - [SDR SWAA2023031314229](https://openairdocs.org/sdr/SWAA2023031314229.md): Plate · cracked · Mar 9, 2023 · N913WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO AFT CORNER THRESHOLD PLATE CRACKED NEEDS TO BE REPLACED<[01] REMOVED COATINGS AND WELDED SCUFF PLATE REF DWG146A8341 AND SRM 53-00-01;[02] 1. CHAD BLOTSKE (TECHNICIAN); 09-MAR-2023 15:04 UTC
REMOVED COATINGS AND WELDED SCUFF PLATE REF DWG146A8341 - [SDR SWAA2023031314228](https://openairdocs.org/sdr/SWAA2023031314228.md): Scuff Plate · cracked · Mar 9, 2023 · N913WN · Boeing 7377H4 · Cargo/Baggage Doors > AFT CARGO FORWARD THRESHOLD CORNER PLATE CRACKED NEEDS TO BE REPLACED AFT CARGO FORWARD THRESHOLD PLATE CRACKED NEEDS TO BE REPLACED<[01] AFT CARGO FORWARD THRESHOLD CORNER PLATE REPLACED REF AMM 53-11-02 - [SDR SWAA2022121681325](https://openairdocs.org/sdr/SWAA2022121681325.md): Vapor Barrier · cracked · Dec 14, 2022 · N913WN · Boeing 7377H4 · Fuselage Main, Bulkhead > CENTER WING REAR SPAR VAPOR BARRIER HAS A 3 INCH CRACK LOCATED IN L/H WHEEL WELL FWD WALL BETWEEN LBL 24.92 AND 31.83 STARTING APPROXIMATELY 16 INCHES FROM BOTTOM ON WHEEL WELL. APPLIED INTERIM SEAL TO FORWARD SIDE OF CRACK IAW 37.7-0602 PAGE 101 AND SRM 57 - [SDR SWAA2022011861889](https://openairdocs.org/sdr/SWAA2022011861889.md): Light · loose · Jan 16, 2022 · N913WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT GLOW STRIP NOT SECURED TO FLOOR AT GALLEY AREA; / [01] RESECURED EMERGENCY LIGHT GLOW STRIP PER SWA DRAWING #33500007.SAF-T-GLO PHOTOLUM INSTALL; [02] C/W; [03] C\W - [SDR SWAA2021072695942](https://openairdocs.org/sdr/SWAA2021072695942.md): Wire · damaged · Jul 17, 2021 · N913WN · Boeing 7377H4 · Light System Wiring > R/H OVERWING EMERGENCY EXIT LIGHT (FWD LOWER ASSY.) INOP; / [01] REPAIRED JIFFY SPLICE ON LIGHT ASSY. AS PER SWPM 20-30-12 AND PERFORMED GOOD FUNCTIONAL AS PER AMM 33-51-01-960-801 STEP 2.(2)
TERM KIT:
ID: T800-004
S/N: E-3166; [02] VERIFIED REPAIRED Next page: https://openairdocs.org/aircraft/N913WN/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 = 'N913WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N913WN/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.