# Service difficulty reports: N960WN A list on [N960WN](https://openairdocs.org/aircraft/N960WN.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 · 180 reports - [SDR SWAA2026011259295](https://openairdocs.org/sdr/SWAA2026011259295.md): Floor Support · cracked · Jan 8, 2026 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > PASSENGER DECK FLOOR SUPPORT BS 540, LT OF CENTERLINE, CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02. - [SDR SWAA2026011259290](https://openairdocs.org/sdr/SWAA2026011259290.md): Floor Support · cracked · Jan 8, 2026 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > FORWARD CARGO BAY, A/C DISTRIBUTION BAY, MAIN PASSENGER DECK FLOOR SUPPORT, BS 540 RT IS CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02. - [SDR SWAA2026011259282](https://openairdocs.org/sdr/SWAA2026011259282.md): Seal · cracked · Jan 8, 2026 · N960WN · Boeing 7377H4 · Elevator Miscellaneous Structure > RH ELEVATOR UPPER SLIDER SEAL CRACKED. R&R RH HORIZONTAL STAB UPPER FWD SLIDING SEAL IAW AMM 53-31-31. - [SDR SWAA2025102225663](https://openairdocs.org/sdr/SWAA2025102225663.md): Battery Pack · inoperative · Oct 19, 2025 · N960WN · Boeing 7377H4 · Emergency Lighting > FWD GALLEY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG. - [SDR SWAA2025061782051](https://openairdocs.org/sdr/SWAA2025061782051.md): Light · inoperative · Jun 15, 2025 · N960WN · Boeing 7377H4 · Emergency Lighting > CR RR LEFT OVER WING EMERGENCY EXIT DOOR LIGHT INOPERATIVE. VERIFIED LEFT OVER WING EMERGENCY EXIT DOOR LIGHT. OPS CHECK IS GOOD IAW SWA BOEING 737-700 AMM 33-51-04-960-802. - [SDR SWAA2025061781247](https://openairdocs.org/sdr/SWAA2025061781247.md): Battery Pack · inoperative · Jun 12, 2025 · N960WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHTS INOPERATIVE RH STOW BIN POSITION 8;11 AND 13. REMOVED AND REPLACED RH EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK IS GOOD. - [SDR SWAA2025050566533](https://openairdocs.org/sdr/SWAA2025050566533.md): Battery Pack · inoperative · May 2, 2025 · N960WN · Boeing 7377H4 · Emergency Lighting > RH OVER WING EMERGENCY EXIT LIGHTS 3EA INOP<[01] CHARGED RH OVER WING EXIT LIGHT POWER SUPPLY BATTERY PACK OPS OK IAW AMM 33-51-06 - [SDR SWAA2025050566532](https://openairdocs.org/sdr/SWAA2025050566532.md): Battery Pack · inoperative · May 2, 2025 · N960WN · Boeing 7377H4 · Emergency Lighting > LH OVER WING EMERGENCY EXIT LIGHTS 3EA INOP<[01] R&R LH OVER WING EMERGENCY EXIT LIGHT POWER SUPPLY BATTERY PACK OPS OK IAW AMM 33-51-06 - [SDR SWAA2025021896623](https://openairdocs.org/sdr/SWAA2025021896623.md): Battery Pack · inoperative · Feb 16, 2025 · N960WN · Boeing 7377H4 · Emergency Lighting > TWO EMERGENCY LIGHTS ON EXTERIOR AFT LOWER BELLY NOT WORKING<[01] REMOVED AND REPLACED THE BATTERY PACK ON STA L/H 747 FOR TWO EMERGENCY LIGHT ON EXT AFT LOWER BELLY REF AMM 33-51-06; OPS CHECK GOOD.;[02] ADDING PART REQUIREMENT DOCUMENTED ON TTG8Q00YG68X:
- [SDR SWAA2024123081569](https://openairdocs.org/sdr/SWAA2024123081569.md): Floor Panel · cracked · Dec 29, 2024 · N960WN · Boeing 7377H4 · Fuselage Floor Panel > RAMP REPORTS CRACK IN AFT CARGO FLOOR<[01] REMOVED AND REPLACED AFT CARGO PANEL 241KF IN REF TO EA M-21-153-00666 - [SDR SWAA2024112161119](https://openairdocs.org/sdr/SWAA2024112161119.md): Panel · cracked · Nov 18, 2024 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > FWD CARGO PANEL 120CF HAS CRACK ABOUT 6IN LONG.<[01] REPAIRED CRACK ON FWD CARGO PANEL 120 CF PER AMM 25-52-01. - [SDR SWAA2024072315412](https://openairdocs.org/sdr/SWAA2024072315412.md): Limiter · inoperative · Jul 22, 2024 · N960WN · Boeing 7377H4 · Trailing Edge Flap Control System > LOSS OF B SYSTEM WHEN SETTING FLAPS TO 5 FOR LANDING<[01] REMOVED AND REPLACED TRAILING EDGE FLAP FLOW LIMITER IN REF TO AMM 27-51-67.;[02] REF TTG8Q00URRTA R/R HYD PUMP. - [SDR SWAA2024072315908](https://openairdocs.org/sdr/SWAA2024072315908.md): Limiter · leaking · Jul 22, 2024 · N960WN · Boeing 7377H4 · Trailing Edge Flap Control System > LOSS OF B SYSTEM WHEN SETTING FLAPS TO 5 FOR LANDING<[01] REMOVED AND REPLACED TRAILING EDGE FLAP FLOW LIMITER IN REF TO AMM 27-51-67.;[02] REF TTG8Q00URRTA R/R HYD PUMP. - [SDR SWAA2024040570771](https://openairdocs.org/sdr/SWAA2024040570771.md): Fairing · pulled · Apr 5, 2024 · N960WN · Boeing 7377H4 · Trailing Edge Flaps > #6 FLAP SUPPORT AFT FAIRING HAS FASTENERS PULLED THRU<[01] 04 - REPAIRED PER [SRM 57-53-70-2R-2-A01234 (REPAIR 2 - FLAP SUPPORT FAIRING - NUMBERS 3 AND 6 INBOARD TRAILING EDGE FLAP - ALTERNATIVE 1 - 500 CYC DVI - INTERIM REPAIR)];[02] VERIFIED WORK PERFORMED I - [SDR SWAA2024020547507](https://openairdocs.org/sdr/SWAA2024020547507.md): Engine · failed · Feb 1, 2024 · N960WN · Boeing 7377H4 · Engine (Turbine/Turboprop) > ON CLIMB OUT #2 ENG LOUD BANG; LOSS OF THRUST ENGINE FAIL MESSAGE; NO N2 ROTATION. ON ENGINE SHUTDOWN EGT RED BOXED.<[01] R&R #2ENG PER MT 771-00-01;[02] R&R #2ENG PER MT 771-00-01. RII 67658 - [SDR SWAA2023072481290](https://openairdocs.org/sdr/SWAA2023072481290.md): Tire · damaged · Jul 21, 2023 · N960WN · Boeing 7377H4 · Tire Tube > ON CLIMB OUT AT APROX; 12.000 FEET WE FELT A POP AND SHUDDER FROM UNDERNEATH AIRCRAFT; ALL SYSTEMS AND INDICATIONS WERE NORMAL. - CONTINUE TO FAULT DESCRIPTION SECTION 15 MINUTES LATER THE MASTER CAUTION ILLUM WITH SYS A HYDRAULIC QTY LOSS. AFTER LANDING DISCO - [SDR SWAA2023062872172](https://openairdocs.org/sdr/SWAA2023062872172.md): Battery Pack · inoperative · Jun 28, 2023 · N960WN · Boeing 7377H4 · Emergency Lighting > LIGHTS ASSOCIATED WITH M1670 BATTERY INOP LIGHTS ASSOCIATED WITH M1670 BATTERY INOP. SUSPECTED BAD BATTERY CHARGER. REMOVED AND REPLACED M1670 BATTERY PACK WITH SERVICEABLE UNIT AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805. COMPLETION OF STE - [SDR SWAA2023062771029](https://openairdocs.org/sdr/SWAA2023062771029.md): Light · inoperative · Jun 25, 2023 · N960WN · Boeing 7377H4 · Emergency Lighting > FWD SERVICE DOOR SLIDE LIGHT IS INOP<[01] REPLACED LAMP FOR FWD SERVICE SLIDE LIGHT AND PERFORMED GOOD TEST PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTION ACTION ITEM 1; CARD COMPLETE. - [SDR SWAA2023062771030](https://openairdocs.org/sdr/SWAA2023062771030.md): Battery Pack · inoperative · Jun 25, 2023 · N960WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1672 ARE INOP<[01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1672 AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-06-960-805.;[02] CERTIFIED ACTION 1;[03] FOR PARTS REQUIREMENTS.;[04] VERIFIED CORRECTIVE - [SDR SWAA2023062771034](https://openairdocs.org/sdr/SWAA2023062771034.md): Battery Pack · inoperative · Jun 25, 2023 · N960WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1673 ARE INOP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1673 IAW AMM 33-51-06-960-805. PERFORMED GOOD CONTINUITY CHECK ON CONNECTOR D11330 AND AISLE LAMPS ON BS 720, WL 274, LBL 30, & AISLE LIGHT BS 850 - [SDR SWAA2023062870253](https://openairdocs.org/sdr/SWAA2023062870253.md): Sign · broken · Jun 21, 2023 · N960WN · Boeing 7377H4 · Emergency Lighting > LAV B EXIT INDICATOR IS BROKEN<[01] REPLACED LAV B EXIT INDICATOR IAW AMM 33-51-01-960-801. OPS CHECK REQUIRED;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] VERIFIED CORRECTIVE ACTION 1.;[04] FAULT CORRECTION DOCUMENTED ON TTG8Q00LV2LC.
PERFORMED GOOD OPS TE - [SDR SWAA2023062961090](https://openairdocs.org/sdr/SWAA2023062961090.md): Light · broken · Jun 20, 2023 · N960WN · Boeing 7377H4 · Emergency Lighting > EXIT LIGHT FOR OVERWING EXIT'S ATTACHED TO OVERHEAD DIFFUSER IS BROKEN.<[01] REMOVED AND REPLACED EXIT LIGHT HOUSING ASSY FOR OVER WING EXITS PER AMM 33-51-01-960-802.;[02] CERTIFIED CORRECTIVE ACTION 1;[03] VERIFIED ALL STEPS COMPLETED. - [SDR SWAA2023062957824](https://openairdocs.org/sdr/SWAA2023062957824.md): Seat Track · cracked · Jun 10, 2023 · N960WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > BS 727B; LBL 45.5 SEAT TRACK FASTENER LOCATION B CRACK NOTED IN FLOOR BEAM LAYER<[01] UPSIZED HOLE 1/32 IAW SRM 51-40-05. REQUIRES NDI TO VERIFY CRACK FREE CONDITION.;[02] CERTIFIED CORRECTIVE ACTION 1;[03] ACCOMPLISHED HFEC INSPECTION OF FASTENER HOLE INDICAT - [SDR SWAA2023062956973](https://openairdocs.org/sdr/SWAA2023062956973.md): Seat Track · cracked · Jun 7, 2023 · N960WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CRACKED SEAT TRACK FASTENER AT PASSENGER CABIN BS727B LBL45 WL208. FWD FASTENER.<[01] UPDATED MEASUREMENTS TABLE AND STEP 1.;[02] CERTIFIED CORRECTIVE ACTION 1 AND STEP 1 PARTIAL;[03] UPDATED MEASUREMENTS TABLE;[04] VERIFIED MEASUREMENT TABLE;[05] REMOVED CABI - [SDR SWAA2023062954606](https://openairdocs.org/sdr/SWAA2023062954606.md): Floor Panel · pulled · Jun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 232RF UPPER SKIN HAS PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 232RF USING BMS 4-23TY2 LOT#1525675-1. INSTALLED INSERTS USING BMS 5-107 LOT#AK2KP8383K-1; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2023; APPLIED - [SDR SWAA2023062954982](https://openairdocs.org/sdr/SWAA2023062954982.md): Angle · cracked · Jun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED INTERCOSTAL AT PASSENGER CABIN BS500D+6 BL0 WL208.<[01] REMOVED PASSENGER CABIN UPPER ANGLE INTERCOSTAL FROM BS500D - BS420; BL 0; PER SRM 51-40-02-0G-0.
RECEIVED FROM TOOL ROOM NEW INTERCOSTAL UPPER ANGLE P/N 143A5410-170; LOCATED AND DRILL PER SRM - [SDR SWAA2023062954980](https://openairdocs.org/sdr/SWAA2023062954980.md): Intercostal · cracked · Jun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED INTERCOSTAL AT PASSENGER CABIN BS380+14 LBL13 WL208.<[01] DRILLED FASTENERS AND REMOVED INTERCOSTAL IAW SRM 51-40-02;[02] CERTIFY;[03] UPDATED MEASUREMENT TABLE;[04] RECEIVED NEW ANGLE PER CUSTOMER RO: N923207-SWA;[05] VERIFIED CORRECTIVE ACTION 4;[06] - [SDR SWAA2023062954983](https://openairdocs.org/sdr/SWAA2023062954983.md): Intercostal · cracked · Jun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED INTERCOSTAL AT PASSENGER CABIN BS380+14 BL0 WL208.<[01] REMOVED PASSENGER CABIN UPPER ANGLE INTERCOSTAL FROM BS380 - BS400; BL 0; PER SRM 51-40-02-0G-0
RECEIVED FROM TOOL ROOM NEW INTERCOSTAL UPPER ANGLE P/N 143A5410-170; LOCATED AND DRILL PER SRM 5 - [SDR SWAA2023062955086](https://openairdocs.org/sdr/SWAA2023062955086.md): Scuff Plate · cracked · Jun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON AFT CARGO DOOR FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B. (2) AND (4)
EQUIP USED: WELDING MACHINE E10583; CAL DUE 01/20 - [SDR SWAA2023062955087](https://openairdocs.org/sdr/SWAA2023062955087.md): Scuff Plate · cracked · Jun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON AFT CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B. (2) AND (4)
EQUIP USED: WELDING MACHINE E10583; CAL DUE 01/202 - [SDR SWAA2023062954981](https://openairdocs.org/sdr/SWAA2023062954981.md): Intercostal · cracked · Jun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED INTERCOSTAL AT PASSENGER CABIN BS380+10 RBL40 WL208.<[01] RECEIVED NEW ANGLE PER CUSTOMER RO: N923207-SWA;[02] VERIFIED CORRECTIVE ACTION 1;[03] REMOVED CRACKED INTERCOSTAL AT PASSENGER CABIN BS380+10 RBL40 WL208 IAW SRM 51-40-02;[04] LOCATED AND DRILL - [SDR SWAA2023062954100](https://openairdocs.org/sdr/SWAA2023062954100.md): Sidewall Support · damaged · May 31, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS DISBONDED NUTPLATE AT STA 727D+8; WL 155.5; LBL 21.<[01] WORK TO BE COMPLETED BY CUST SYSTEM ID: TTG8Q00LC60R
THIS FLOOR TO SIDEWALL SUPPORT IS REPAIRED BY REPLACEMENT;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2023070353513](https://openairdocs.org/sdr/SWAA2023070353513.md): Bracket · cracked · May 30, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO COMPARTMENT AT THE 727 BULKHEAD HAS BROKEN BRACKET AT STA: 727; WL:14.5; BL:3.5 CORRECTION WL: 163 RBL:3.5<[01] MEASURMENT UPDATE; NO ALLOWABLE DAMAGE LIMIT FOUND IN SRM. PART TO BE REPAIRED BY REPLACMENT;[02] REMOVED CRACKED 727 BULKHEAD BRACKET AT - [SDR SWAA2023070354094](https://openairdocs.org/sdr/SWAA2023070354094.md): Supercharger · corroded · May 30, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO RIGHT FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT: STA:727B+14; 727C+14; 727C+6; 727D+3; 727D+8; 727D+11; 727D+14; 727D+18; 727E+2; 727E+6 WL: 156; RBL:20 T0 22<[01] VERIFIED APPLICABILITY OF SRM 53-60-53-01-2 IDENTIFICATION 2 AND SRM 53-00-53-1A-2 AL - [SDR SWAA2023070354095](https://openairdocs.org/sdr/SWAA2023070354095.md): Support · corroded · May 30, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO COMPARTMENT RIGHT FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT STA: 727E+10; 727E+14; 727E+18; 747+2; 747+6; 747+10; 747+15; 747+18 WL:156; RBL: 20 TO 24<[01] VERIFIED APPLICABILITY OF SRM 53-60-53-01-2 IDENTIFICATION 2 AND SRM 53-00-53-1A-2 ALLOWABLE - [SDR SWAA2023070354092](https://openairdocs.org/sdr/SWAA2023070354092.md): Support · corroded · May 30, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO COMPARTMENT LEFT FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT STA: 727+6; 727E+6;747; 747+2; 747+10; 747+14; 767; 767+3; 767+4.5; 787. WL 156: LBL 20 TO 24<[01] REMOVED CORROSION ABOUT 1' X 1' AT
STA 727+6 0.005'(OUT OF LIMIT)
STA 727E+6 0.002'< - [SDR SWAA2023070354096](https://openairdocs.org/sdr/SWAA2023070354096.md): Shield · corroded · May 30, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO COMPARTMENT CARGO BAY FWD SHIELD HAS CORROSION FROM STA:767+3 THRU RBL:787+4; RBL:26; WL:156<[01] NO ALLOWABLE DAMAGE FOUND FOR THIS PART IN B737-700 SRM 53-00-53-1A-2 AFT CARGO FLOOR STRUCTURE ALLOWABLE DAMAGE.
REPAIR BY REPLACEMENT IAW SRM 51-10 - [SDR SWAA2023062954093](https://openairdocs.org/sdr/SWAA2023062954093.md): Bracket · broken · May 30, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO COMPARTMENT AT THE 727 BULKHEAD HAS BROKEN BRACKET AT STA: 727; WL:163; RBL:3.5<[01] TRANSFERED MEASUREMENTS FROM FAULT TTG8Q00LBLDX.;[02] INSTALLED NEW ACB BULKHEAD BRACKET AT BS 727; WL 163; RBL 3.5 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG - [SDR SWAA2023070352620](https://openairdocs.org/sdr/SWAA2023070352620.md): Bracket · cracked · May 25, 2023 · N960WN · Boeing 7377H4 · Wing, Center Box > RIGHT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET (212A1116) ACCESS PANEL 192CR BS540+6 RBL8. MARKED<[01] REMOVED CRACKED R/H ECS BAY DUCT SUPPORT BRACKET AT BS540+6 RBL 8 AND REPLACED WITH NEW BRACKET PER SRM 51-40-02-0G-0 AND AIPC 36-13-01-01;[02] VERIFIED CORR - [SDR SWAA2023070352136](https://openairdocs.org/sdr/SWAA2023070352136.md): Structure · corroded · May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON L1 DOOR MOP SILL AT STA 328+6; +7.5; & +14.5; WL 208.1; LBL 60.<[01] PART REPLACED ON FAULT TTG8Q00L8VCT;[02] VERIFIED MEASUREMENT TABLE

VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2023070352623](https://openairdocs.org/sdr/SWAA2023070352623.md): Shield · corroded · May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > FWD CARGO BAY SHIELD HAS CORROSION BS 500+13; RBL 26; WL 156<[01] PART HAS NO LIMIT FOR DAMAGE. BLEND IS 1'L X 1'W REMOVED 0.010. PART IS FOUND TO BE (OUT LIMITS) REPAIR BY REPLACEMENT. IAW SRM 51-10-02;[02] REMOVED AFT SHIELD FROM FWD CARGO IAW SRM 51-40-02;[ - [SDR SWAA2023070352635](https://openairdocs.org/sdr/SWAA2023070352635.md): Seat Track · corroded · May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Internal Mounting Structure > CORROSION ON PASSENGER CABIN SEAT TRACK RBL45 BS410;440;473 WL208.<[01] VERIFIED APPLCABILITY PER SRM 53-00-52-1A-1. REMOVED CORROSION FROM CABIN SEAT TRACK AT BS 440 RBL45 W208 L:3' W:.45' D:.25' ON CROWN FOUND SEAT TRCK TO BE OUT OF LIMIT PER SRM 53-00-52-1A - [SDR SWAA2023070352621](https://openairdocs.org/sdr/SWAA2023070352621.md): Stringer · corroded · May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > AREA AFT OF FWD CARGO BAY STR 23 IS CORRODED AT THE AFT FASTENER; STR 23; RBL 45<[01] REMOVED CORROSION ON FCB STRINGER 23R BS 539 L=0.500'X W=0.500'D=0.036' FROM ORIGINAL THICKNESS 0.036' DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL B.[05] - [SDR SWAA2023070352637](https://openairdocs.org/sdr/SWAA2023070352637.md): Seat Track · corroded · May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Internal Mounting Structure > CORROSION ON PASSENGER CABIN SEAT TRACK RBL45 BS500+4; BS500C+9 WL208.<[01] VERIFIED APPLCABILITY PER SRM 53-00-52-1A-1. REMOVED CORROSION FROM CABIN SEAT TRACK AT BS500+4 RBL45 W208 L:3' W:.45' D:.22' ON CROWN; FOUND SEAT TRACK TO BE OUT OF LIMIT PER SRM 53-0 - [SDR SWAA2023070352626](https://openairdocs.org/sdr/SWAA2023070352626.md): Track · corroded · May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON PASSENGER CABIN SEAT TRACK RBL45 BS727C+16; 727E+8; 787+9 WL208.<[01] VERIFIED APPLCABILITY PER SRM 53-00-52-1A-1. REMOVED CORROSION FROM CABIN SEAT TRACK AT BS727C+16 RBL45 W208 L:3' W:.45' D:.25' ON CROWN; FOUND SEAT TRACK TO BE OUT OF LIMIT PER - [SDR SWAA2023070352641](https://openairdocs.org/sdr/SWAA2023070352641.md): Seat · corroded · May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON PASSENGER CABIN SEAT TRACK LBL25 BS371 WL208.<[01] VERIFIED APPLICABILITY FOR 737-700 SRM 53-00-52-1A-1.
REMOVED CORROSION FROM PASSENGER CABIN SEAT TRACK AT LBL 25 WL 208 BS371 L: 2' W:.90' D:.060' ON WELL; FOUND SEAT TRACK TO BE OUT LIMITS P - [SDR SWAA2023070352642](https://openairdocs.org/sdr/SWAA2023070352642.md): Track · corroded · May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON PASSENGER CABIN SEAT TRACK LBL45 BS380; 473 WL208.<[01] VERIFIED APPLICABILITY FOR 737-700 SRM 53-00-52-1A-1.
REMOVED CORROSION FROM PASSENGER CABIN SEAT TRACK AT LBL 45 WL 208 BS 380 L: 1' W:.90' D:.050' ON WELL; FOUND SEAT TRACK TO BE OUT LI - [SDR SWAA2023062952125](https://openairdocs.org/sdr/SWAA2023062952125.md): Floor Panel · pulled · May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL WITH BMS4-23 TYPE II LOT 1525675-1 AND BMS5-107 CLASS 1 LOT AK2KP8383K-1 RESIN; CURED RESIN UNDER A HEAT LAMP USING THERMOME - [SDR SWAA2023062952126](https://openairdocs.org/sdr/SWAA2023062952126.md): Floor Panel · pulled · May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL WITH BMS4-23 TYPE II LOT 1525675-1 AND BMS5-107 CLASS 1 LOT AK2KP8383K-1 RESIN; CURED RESIN UNDER A HEAT LAMP USING THERMOME - [SDR SWAA2023062952127](https://openairdocs.org/sdr/SWAA2023062952127.md): Floor Panel · pulled · May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 242BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 242BF FLOOR PANEL FROM BMS4-17 TYPE 6 LOT#1526676-1; LOCATED AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING HEAT LAMP AND THERMOMETER A Next page: https://openairdocs.org/aircraft/N960WN/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 = 'N960WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N960WN/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.