# Service difficulty reports: N965WN

A list on [N965WN](https://openairdocs.org/aircraft/N965WN.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 · 175 reports

- [SDR SWAA2026092237909](https://openairdocs.org/sdr/SWAA2026092237909.md): Light · smoke · Sep 21, 2026 · N965WN · Boeing 7377H4 · Passenger Compartment Lighting
  > FA OBSERVED A BURNING ODOR IN AFT GALLEY AT GATE AFTER LANDING NEAR SERVICE DOOR. COMPLIED WITH SMOKE/FUMES IN CABIN CONDITIONAL INSP IAW MM 05-51-56 RELAMPED AFT GALLEY ENTRY LIGHT IAW MM 33-29-00. NO OTHER DEFECTS FOUNDS.
- [SDR SWAA2026081799954](https://openairdocs.org/sdr/SWAA2026081799954.md): Handle · broken · Aug 12, 2026 · N965WN · Boeing 7377H4 · Service Doors
  > AFT SERVICE DOOR ASSIST HANDLE BROKEN. R & R AFT SERVICE DOOR ASSIST HANDLE IAW AMM 52-41-31.
- [SDR SWAA2026030976661](https://openairdocs.org/sdr/SWAA2026030976661.md): Strip · worn · Mar 5, 2026 · N965WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN PHOTOLUMINESCENT STRIP WORN, RT CENTER ISLE ROW 1. R & R PHOTOLUMINESCENT STRIP IAW AMM 33-51-15.
- [SDR SWAA2026022774235](https://openairdocs.org/sdr/SWAA2026022774235.md): Door · corroded · Feb 25, 2026 · N965WN · Boeing 7377H4 · Cargo/Baggage Doors
  > WHILE WORKING AFT CARGO DOOR HANDLE FAIRING; FOUND CORROSION ON AFT CARGO DOOR INNER SKIN APPROX 2 L X 1 W. REMOVED AND REPLACED AFT CARGO DOOR THROUGH DOOR ADJUSTMENT IAW AMM 52-31-00. SYSTEM TEST AND LEAK CHECK ARE STILL REQUIRED.;[02] SEE TTG8Q01AMM8J FOR
- [SDR SWAA2025090410481](https://openairdocs.org/sdr/SWAA2025090410481.md): Hook · loose · Sep 1, 2025 · N965WN · Boeing 7377H4 · Emergency Equipment
  > FWD ENTRY DOOR GIRT BAR HOOK LOOSE. REPLACED FASTENER IAW AMM 51-40-02.
- [SDR SWAA2025082708376](https://openairdocs.org/sdr/SWAA2025082708376.md): Cover · detached · Aug 25, 2025 · N965WN · Boeing 7377H4 · Emergency Lighting
  > EXIT LIGHT COVER ON FO SIDE OVER WING EXIT FELL OFF. SECURED THE COVER IAW AMM SIP.
- [SDR SWAA2025081905556](https://openairdocs.org/sdr/SWAA2025081905556.md): Cover · detached · Aug 17, 2025 · N965WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING EXIT LIGHTED EMERGENCY EXIT COVER FELL OFF. RESECURED COVER IAW AMM 33-51-01.
- [SDR SWAA2025081998882](https://openairdocs.org/sdr/SWAA2025081998882.md): Fitting · cracked · Aug 6, 2025 · N965WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 1 ENGINE OTBD FAN COWL AFT HOLD OPEN ROD STOW PIN FIITING CRACKED. REMOVED AND REPLACED NR 1 OTBD FAN COWL AFT HOLD OPEN ROD STOW PIN FITTING PER AMM 51-40-02-0G-0. AFT HOLD OPEN ROD STOW PIN FITTING REPLACED WHEN THE FAN COWL WAS REPLACED ON SWA NON-R
- [SDR SWAA2025081998165](https://openairdocs.org/sdr/SWAA2025081998165.md): Plate · cracked · Aug 4, 2025 · N965WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT WING T/E INBD WAFFLE PLATE FOR PANEL 551EB CRACKED. REMOVED & REPLACED LT WING T/E INBD WAFFLE PLATE FOR PANEL 551EB IAW SRM 51-40-05-0G-0 & DWG115A2001 & DWG 115A2713.
- [SDR SWAA2025081596842](https://openairdocs.org/sdr/SWAA2025081596842.md): Panel · cracked · Jul 30, 2025 · N965WN · Boeing 7377H4 · Vertical Stabilizer, Plate/Skin
  > PANEL 324BL CRACKED ON EDGE NEAR FASTENER HOLE. REPAIRED VERTICAL STAB TRAILING EDGE PANEL 324BL IAW SRM 55-30-01-2R-9, SRM 51-70-04-2R-6, AND SRM 51-70-04-2R-0 REPAIR GENERAL.
- [SDR SWAA2025081595038](https://openairdocs.org/sdr/SWAA2025081595038.md): Bulkhead · cracked · Jul 25, 2025 · N965WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > LEFT SIDE VERTICAL 663 BULKHEAD LOWER VAPOR BARRIER FOUND CRACKED WITH TEMP REPAIR; CUSTOMER REQUEST TO ACCOMPLISH PERMEANT REPAIR. REPAIRED L/H VERTICAL 663 BULKHEAD LOWER VAPOR BARRIER IAW SRM 51-70-04-2R-0 AND SRM 51-70-04-2R-10.
- [SDR SWAA2025081994462](https://openairdocs.org/sdr/SWAA2025081994462.md): Fitting · cracked · Jul 23, 2025 · N965WN · Boeing 7377H4 · Trailing Edge Flaps
  > A71-40 LEFT WING TRAILING EDGE CAVITY. FIXED TRAILING EDGE SUPPORT BRACKET 10' I/B OF DEFLECTION CONTROL RIB; HAS A CRACK AT BULB SEAL ATTACH BRACKET. REMOVED LT WING T/E SUPPORT BRACKET IAW SRM 51-40-02-0G-0. DRILLED FASTENERS HOLES IAW SRM 51-40-02-0G-0 A
- [SDR SWAA2025081594679](https://openairdocs.org/sdr/SWAA2025081594679.md): Seat Track · worn · Jul 23, 2025 · N965WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN LT SEAT TRACK LBL 45 AT BS 520 UPPER SIDE OF CROWN HAS EVIDENCE OF WEAR. REMOVED DAMAGE; MATERIAL LOSS OF 0.026' IS OUT OF LIMITS IAW SRM 53-00-52-1A-1. REMOVED DAMAGED SECTION OF SEAT TRACK BETWEEN STA 500C + 10' AND BS 520 LBL 45. LOCATED AND D
- [SDR SWAA2025081594686](https://openairdocs.org/sdr/SWAA2025081594686.md): Seat Track · corroded · Jul 23, 2025 · N965WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN L/H SEAT TRACK LBL45 AT STA 685+12' TO 727+13' LOWER SIDE OF CROWN HAS EVIDENCE OF CORROSION. REPAIRED IAW SRM 53-00-52-1A-1-A00026.
- [SDR SWAA2025081494218](https://openairdocs.org/sdr/SWAA2025081494218.md): Seat Back · out of adjust · Jul 23, 2025 · N965WN · Boeing 7377H4 · Passenger Compartment Equipment
  > EMERGENCY EXIT ROW SEAT RECLINES AT 11D. ADJUSTED HYDRAULIC LOCK TO PREVENT RECLINE AT SEAT 11D IAW CMM 25-21-45, REPAIR STEPS 3.G.
- [SDR SWAA2025081494452](https://openairdocs.org/sdr/SWAA2025081494452.md): Floor Panel · deformed · Jul 23, 2025 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO FLOOR PANEL 120BF IS WAVY BETWEEN FLOORBEAMS. COMPLETED FABRICATION OF A NEW FLOOR PANEL 120BF IAW AMM 25-52-01-201-801.
- [SDR SWAA2025060977799](https://openairdocs.org/sdr/SWAA2025060977799.md): Lamp · dim · Jun 4, 2025 · N965WN · Boeing 7377H4 · Emergency Lighting
  > L/H OVERWING EMERGENCY EXIT DOOR LIGHT IS DIM. RELAMPED PER AMM 33-51-01. INSPECTED PER [AMM 33-51-01-201-NG.
- [SDR SWAA2025032508522](https://openairdocs.org/sdr/SWAA2025032508522.md): Shield · corroded · Mar 23, 2025 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > POSSIBLE CORROSION IN AFT CARGO PIT ON LOWER SCREWS HOLES FOR PANEL 142FW <[01]. REMOVED AND REPLACED AFT CARGO PIT PART CALLED A SHIELD UNDER PANEL 142FW WHICH HAD MINOR CORROSION. REPLACING THE PART REMOVED ALL AND ANY CORROSION. REF SRM 51-40-02.
- [SDR SWAA2025010683326](https://openairdocs.org/sdr/SWAA2025010683326.md): Battery Pack · inoperative · Jan 6, 2025 · N965WN · Boeing 7377H4 · Emergency Lighting
  > OVERHEAD BIN EMERGENCY LIGHTS AT SEAT 3DEF AND 6DEF INOP.<[01] REMOVED AND REPLACED M1674 EMERGENCY LIGHT CRADLE AND BATTERY PACK IN FWD GALLEY CEILING PANEL UNDER LIGHT. ASSY OPS CHECKED GOOD REF B737 AMM 33-51-06
- [SDR SWAA2025010683492](https://openairdocs.org/sdr/SWAA2025010683492.md): Battery Pack · inoperative · Jan 6, 2025 · N965WN · Boeing 7377H4 · Emergency Lighting
  > OVERHEAD BIN EMERGENCY LIGHTS AT SEAT 3DEF AND 6DEF INOP.<[01] REMOVED AND REPLACED M1674 EMERGENCY LIGHT CRADLE AND BATTERY PACK IN FWD GALLEY CEILING PANEL UNDER LIGHT. ASSY OPS CHECKED GOOD REF B737 AMM 33-51-06
- [SDR SWAA2025010683314](https://openairdocs.org/sdr/SWAA2025010683314.md): Vapor Barrier · cracked · Jan 6, 2025 · N965WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CENTER WING REAR SPAR VAPOR WEB IS CRACKED ON THE LEFT SIDE OF THE KEEL; JUST FORWARD OF THE HYDRAULIC FLOW REGULATOR VALVE. CENTER WING REAR SPAR VAPOR WEB IS CRACKED ON THE LEFT SIDE OF THE KEEL JUST FORWARD OF THE HYDRAULIC FLOW REGULATOR VALVE.<[01] REVIEW
- [SDR SWAA2024041774578](https://openairdocs.org/sdr/SWAA2024041774578.md): Slide · dislodged · Apr 14, 2024 · N965WN · Boeing 7377H4 · Escape Slide
  > L1 DOOR SLIDE IS NO LONGER IN PLASTIC COVER.<[01] REINSTALLED FWD ENTRY DOOR ESCAPE SLIDE PER MT 725-61-06 AND AMM 25-66-01. NO FURTHER DEFECTS NOTED. A/C OK FOR SERVICE.;[02] C/W
- [SDR SWAA2024040168991](https://openairdocs.org/sdr/SWAA2024040168991.md): Slide · dislodged · Mar 30, 2024 · N965WN · Boeing 7377H4 · Escape Slide
  > RAMP REPORTS R1 DOOR SLIDE FELL OUT OF HOLDER. REINSTALLED FWD ENTRY DOOR SLIDE PER AMM 25-66-01 AND MT 725-66-06.
- [SDR SWAA2024032868273](https://openairdocs.org/sdr/SWAA2024032868273.md): Slide · dislodged · Mar 27, 2024 · N965WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE FELL OUT OF CONTAINER<[01] REINSTALLED FWD ENTRY SLIDE PER MT 725-61-06 AND REF AMM 25-61-06
- [SDR SWAA2023113025741](https://openairdocs.org/sdr/SWAA2023113025741.md): Light · inoperative · Nov 29, 2023 · N965WN · Boeing 7377H4 · Emergency Lighting
  > AFT GALLEY CENTER AISLE ENTRANCE L/H EMERGENCY EGRESS STRIP DELAMINATED<[01] R&R CABIN PHOTOLUMINESCENT STRIP PER AMM 33-51-15
- [SDR SWAA2023080985889](https://openairdocs.org/sdr/SWAA2023080985889.md): Sign · inoperative · Aug 5, 2023 · N965WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING HATCH AFT INDICATOR SIGN HAS INOPERATIVE LAMPS.<[01] REPLACED AND PERFORMED GOOD FUNCTIONAL TEST ON THE RIGHT OVERWING HATCH AFT INDICATOR SIGN PER AMM 33-51-01-960-801.;[02] CERTIFY CORRECTIVE ACTION 1;[03] RELAMP THREE BULBS ON THE RIGHT OVERW
- [SDR SWAA2023080985890](https://openairdocs.org/sdr/SWAA2023080985890.md): Light · inoperative · Aug 5, 2023 · N965WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SLIDE LIGHT AT THE FORWARD ENTRY DOOR DOES NOT ILLUMINATE.<[01] REPLACED EMERGENCY EXIT SLIDE LIGHT AT FWD ENTRY AND PERFORMED GOOD FUNCTIONAL TEST PER AMM 33-51-04-960-801.;[02] CERTIFY CORRECTIVE ACTION 1;[03] VERIFIED CORRECTIVE ACTION #1.
- [SDR SWAA2023080982164](https://openairdocs.org/sdr/SWAA2023080982164.md): Support Channel · cracked · Jul 25, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FWD BULKHEAD R/H LOWER SUPPORT CHANNEL CRACKED.<[01] RECEIVED NEW SUPPORT CHANNEL<BR>ITEM#: 144A9401U20<BR>PO#: 869550/1;[02] REMOVED AND REPLACED AFT CARGO BAY FWD BULKHEAD R/H LOWER SUPPORT CHANNEL IAW SRM 51-40-02-0G-0 AND DWG 144A2600 ID:09
- [SDR SWAA2023080978184](https://openairdocs.org/sdr/SWAA2023080978184.md): Attach Angle · cracked · Jul 13, 2023 · N965WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > O2 BOTTLE FWD SUPPORT BRACKET; LOWER ATTACH ANGLE IS CRACKED AT O/B FASTENER; BS 360+2; LBL 18; WL 164<[01] ENTERED MEASUREMENTS;[02] REMOVED DAMAGED CREW OXYGEN SUPPORT RING IAW SOPM 20-50-01.<BR>RECEIVED NEW SUPPORT RING FROM STORES. REF: PO 929464.<BR>INSTA
- [SDR SWAA2023081077915](https://openairdocs.org/sdr/SWAA2023081077915.md): Bracket · cracked · Jul 12, 2023 · N965WN · Boeing 7377H4 · Aerodynamic Fairings
  > LEFT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET (212A1116) ACCESS PANEL 192CL BS540+6 LBL8.<[01] REMOVED AND REPLACED ECS BAY DUCT SUPPORT BRACKET 212A1116 IAW SOPM 20-50-01;[02] VERIFIED PARTS REQUIREMENTS.;[03] VERIFIED CORRECTION ACTION 1;2 AND MEASUREMENT TA
- [SDR SWAA2023081077466](https://openairdocs.org/sdr/SWAA2023081077466.md): Frame · cracked · Jul 12, 2023 · N965WN · Boeing 7377H4 · Fuselage Main, Frame
  > STA 312 FRAME INNER RADIUS IS CRACKED JUST ABOVE L1 DOOR CUT-OUT.<[01] UPDATED MEASURMENTS;[02] CARD WILL BE WORK ON CARD TTG8Q00M68NT.;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLE
- [SDR SWAA2023080977907](https://openairdocs.org/sdr/SWAA2023080977907.md): Panel · cracked · Jul 12, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor Panel
  > WING BOX CENTER SECTION BREAK PANEL CRACKED AT BS 540; RBL 1; WL 207<[01] UPDATED PARTS TABLE;[02] REMOVED BREAK PANEL AT BS 540; RBL 1 WL 208 IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW BREAK PANEL IAW SRM 51-40-05-0G-0.;[03] OK TO INSTALL.;[04] LOCATED AN
- [SDR SWAA2023080977908](https://openairdocs.org/sdr/SWAA2023080977908.md): Panel · cracked · Jul 12, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor Panel
  > AREA ABOVE WING BOX CENTER SECTION BREAK PANEL CRACKED AT BS 540; LBL 1; WL 207<[01] UPDATED REFERENCE TABLE;[02] REMOVED BREAK PANEL AT BS 540; LBL 1 IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW BREAK PANEL IAW SRM 51-40-05-0G-0.;[03] OK TO INSTALL;[04] LOC
- [SDR SWAA2023080977905](https://openairdocs.org/sdr/SWAA2023080977905.md): Skin · chafed · Jul 12, 2023 · N965WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CHAFING ON INNER FUSELAGE SKIN AT FWD CABIN BS277+5; 3'OB OF S-2L LBL10.<[01] UPDATED MEASUREMENT TABLE.<BR>VERIFIED SRM 53-00-01-2R-38 IS APPLICABLE TO REPAIR SMALL DAMAGE IN FUSELAGE SKIN.<BR>DRILLED OUT DAMAGE TO A.125 DIAMETER PER SRM 53-00-01-2R-38 PARA.
- [SDR SWAA2023080977911](https://openairdocs.org/sdr/SWAA2023080977911.md): Intercostal · cracked · Jul 12, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT PASSENGER CABIN BS380+14 BL0 WL208.<[01] FOUND CRACK ONLY AT UPPER ANGLE OF INTERCOSTAL. SRM DOES NOT HAVE ALLOWABLE DAMAGE LIMITS FOR CRACKED ANGLE. OUT OF LIMITS. REMOVE AND REPLACE IAW SRM 51-10-02-0G-0 STEP #9.;[02] REMOVED ANGLE FRO
- [SDR SWAA2023080977909](https://openairdocs.org/sdr/SWAA2023080977909.md): Intercostal · cracked · Jul 12, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT PASSENGER CABIN BS380+14 RBL9 WL208.<[01] FOUND CRACK ONLY AT UPPER ANGLE OF INTERCOSTAL. SRM DOES NOT HAVE ALLOWABLE DAMAGE LIMITS FOR CRACKED ANGLE. OUT OF LIMITS. REMOVE AND REPLACE IAW SRM 51-10-02-0G-0 STEP #9.;[02] REMOVED ANGLE FR
- [SDR SWAA2023080977078](https://openairdocs.org/sdr/SWAA2023080977078.md): Seat Track · corroded · Jul 10, 2023 · N965WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK IS CORRODED AT BS 380+19; 420+14; LBL 45; WL 208<[01] VERIFIED APPLICABILITY FOR 737-700 SRM 53-00-52-1A-1.;[02] REMOVED CORROSION FROM PASSENGER CABIN SEAT TRACK AT LBL 45 WL 208 BS 380+19 L: 3' W:.90' D:.051' FOUND SEAT TRACK TO BE OUT LIMI
- [SDR SWAA2023080977904](https://openairdocs.org/sdr/SWAA2023080977904.md): Attach Angle · cracked · Jul 8, 2023 · N965WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > AFT CARGO BAY FWD SHIELD ATTACH ANGLE CRACKED BS 787- BS 794 RBL 21<[01] ADDED MEASUREMENTS;[02] REMOVED AFT CARGO FWD SHIELD ATTACH ANGLE. IAW SRM 51-40-02;[03] RECEIVED REPLACEMENT PART. CUSTOMER RO NO. 928460-SWA. JOB NUMBER 561649.;[04] VERIFIED CORRECTIVE
- [SDR SWAA2023080976655](https://openairdocs.org/sdr/SWAA2023080976655.md): Attach Angle · cracked · Jul 8, 2023 · N965WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > AFT CARGO BAY FWD SHIELD ATTACH ANGLE CRACKED BS 767 - BS 787 RBL 21<[01] REMOVED AFT CARGO BAY FWD ATTACH ANGLE BS 767-BS 787 RBL 21 IAW SRM 51-40-02-0G-0.;[02] RECEIVED NEW ANGLE P/N:146A8125-53 LOT:1527393-1. LOCATED; DRILLED AND ATTACHED NUTPLATES ON NEW A
- [SDR SWAA2023080976653](https://openairdocs.org/sdr/SWAA2023080976653.md): Floor Panel · pulled · Jul 8, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CABIN FLOOR PANEL 221BF HAS PULLED STRANDS ON UPPER SURFACE<[01] VERIFIED STEP 9;[02] FWD CABIN FLOOR PANEL 221BF WITH PULLED STRANDS ON UPPER SURFACE WAS REPAIRED PER SRM 53-00-50-2R-1.;[03] VERIFIED ALL STEPS COMPLETE;[04] VERIFIED ALL STEPS COMPLETE AND
- [SDR SWAA2023080976404](https://openairdocs.org/sdr/SWAA2023080976404.md): Support Angle · cracked · Jul 7, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE FOR CHANNEL; BS 692.5 - 694 RBL 24 WL 203<[01] UPDATED MEASUREMENTS TABLE;[02] REMOVED DAMAGED SUPPORT ANGLE FOR CHANNEL FROM BS 692.5 TO BS 694; RBL 24; WL 203 IAW SRM 51-40-02-0G-0;[03] CERTIFY;[04] SRM DOESN'T HAVE ALLOWABLE DAMAGE/REP
- [SDR SWAA2023081076097](https://openairdocs.org/sdr/SWAA2023081076097.md): Intercostal · cracked · Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD CABIN BS344+5 RBL50 WL208.<[01] REQUEST HFEC INSPECTION OF SUSPECTED CRACK AREA.;[02] HFEC INSPECTED SUSPECTED CRACK AREA IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23.<BR>.3' CRACK NOTED. MARKED LOCATION<BR>EQUIP USED:<BR>-NORTEC 600 I
- [SDR SWAA2023080976091](https://openairdocs.org/sdr/SWAA2023080976091.md): Stub Frame · cracked · Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Main, Structure
  > FWD CABIN SERVICE DOOR SURROUND LOWER STUB FRAME CRACKED BS294 RBL54 WL209.<[01] VERIFIED SRM 53-10-15-1A-2 IS APPLICABLE FOR ALLOWABLE DAMAGE TO FSD SURROUND STRUCTURE.;[02] CONCUR WITH APPLICABILITY OF SRM 53-10-15-1A-2.;[03] REMOVED CLIP P/N 141A8312-3 PER
- [SDR SWAA2023080976092](https://openairdocs.org/sdr/SWAA2023080976092.md): Intercostal · cracked · Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD CABIN BS291 BL0 WL208.<[01] VERIFIED APPLICABILITY FOR SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1.;[02] CRACK FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1; PAR. 4.B.(1).(A). FIG. 105; DETAIL A.<BR>REMOVED INTERCOSTAL FROM BS277 - BS294;
- [SDR SWAA2023080976093](https://openairdocs.org/sdr/SWAA2023080976093.md): Intercostal · cracked · Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD CABIN BS312+5 RBL30 WL208.<[01] VERIFIED APPLICABILITY FOR SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1;[02] CRACK FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1 PAR. 4.B.(1).(A). FIG 105; DETAIL A.<BR>REMOVED INTERCOSTAL FROM BS312 - BS328
- [SDR SWAA2023080976094](https://openairdocs.org/sdr/SWAA2023080976094.md): Intercostal · cracked · Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD CABIN BS328+7 LBL46 WL208.<[01] UPDATED MEASUREMENT TABLE;[02] REMOVED DAMAGED INTERCOSTAL IAW SRM 51-40-02-0G-0;[03] LOCATED; DRILLED NEW INTERCOSTAL AT BS 328 - 344 LBL 46 IAW SRM 51-40-05-0G-0. OK TO INSTALL.;[04] VERIFIED CORRECT
- [SDR SWAA2023080976095](https://openairdocs.org/sdr/SWAA2023080976095.md): Intercostal · cracked · Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD CABIN BS344+5 RBL12 WL208.<[01] UPDATED MEASUREMENT TABLE;[02] REMOVED INTERCOSTAL AT BS 344- BS360 RBL 12; WL 208 IAW SRM 51-40-02-0G-0;[03] REMOVED INTERCOSTAL AT BS 344- BS 360 BL0 FOR ACCESS ONLY IAW SRM 51-40-02-0G-0;[04] LOCATE
- [SDR SWAA2023080976096](https://openairdocs.org/sdr/SWAA2023080976096.md): Intercostal · cracked · Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD CABIN BS344+9 LBL12 WL208.<[01] REMOVED INTERCOSTAL AT FWD CABIN BS 344+9 LBL12 WL208 IAW SRM 51-40-02;[02] UPDATED MEASUREMENT TABLE;[03] CERTIFY ACTION #1;[04] SRM DOES NOT HAVE REPAIR LIMITS FOR CRACKED INTERCOSTALS. OUT OF LIMITS
- [SDR SWAA2023080975577](https://openairdocs.org/sdr/SWAA2023080975577.md): Floor Panel · pulled · Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED FLOOR PANEL 231DF IAW SRM 53-00-50-2R-0 AND BAC DWG 143A5810-513;[02] UPDATED MEASUREMENTS TABLE;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2
- [SDR SWAA2023080975578](https://openairdocs.org/sdr/SWAA2023080975578.md): Floor Panel · pulled · Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231GF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED FLOOR PANEL 231GF IAW SRM 53-00-50-2R-0 AND BAC DWG 143A5810-575;[02] UPDATED MEASUREMENTS TABLE;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2<BR><BR>VERIFIED MEASUREMENTS TABLE

Next page: https://openairdocs.org/aircraft/N965WN/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 = 'N965WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N965WN/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.