# Service difficulty reports: N969WN

A list on [N969WN](https://openairdocs.org/aircraft/N969WN.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 · 152 reports

- [SDR SWAA2026081483767](https://openairdocs.org/sdr/SWAA2026081483767.md): Slide · partial deploy · Aug 10, 2026 · N969WN · Boeing 7377H4 · Escape Slide
  > L1 DOOR SLIDE PARTIALLY DEPLOYED BECAUSE IT WAS NOT SECURED AT ARRIVAL_ SECURED AND REINSTALLED SLIDE PER MT 725-61-06-FE.
- [SDR SWAA2025122253820](https://openairdocs.org/sdr/SWAA2025122253820.md): Handle · loose · Dec 19, 2025 · N969WN · Boeing 7377H4 · Buffet/Galleys
  > FWD GALLEY RIGHT HAND SIDE DOOR ASSIST GRAB HANDLE LOOSE<[01] SECURED FWD GALLEY R/H SIDE ASSIST HANDLE REF AMM 25-21-35
- [SDR SWAA2025102822276](https://openairdocs.org/sdr/SWAA2025102822276.md): Plate · cracked · Oct 7, 2025 · N969WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LEFT WING AFT SPAR AREA WAFFLE PLATE JUST OTBD OF PANEL 551DB, CRACKED AT FASTENER. DRILLED AND REMOVED CRACKED WAFFLE PLATE IAW SRM 51-40-02-0G-0. INSTALLED NEW WAFFLE PLATE IAW SRM 51-40-02-0G-0, PART 115A2781-3.
- [SDR SWAA2025102822277](https://openairdocs.org/sdr/SWAA2025102822277.md): Plate · cracked · Oct 7, 2025 · N969WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING AFT SPAR AREA WAFFLE PLATE JUST OTBD OF PANEL 651DB, CRACKED AT FASTENER. DRILLED AND REMOVED CRACKED WAFFLE PLATE AT RT WING OTBD OF 651BB IAW SRM 51-40-02-0G-0, LOCATED AND DRILLED ALL FASTENER HOLES INTO NEW RT WAFFLE PLATE IAW SRM51-40-02-0G-
- [SDR SWAA2025102921985](https://openairdocs.org/sdr/SWAA2025102921985.md): Stub Frame · cracked · Oct 6, 2025 · N969WN · Boeing 7377H4 · Fuselage Main, Frame
  > BS 295; ABOVE STR 8R; STUB FRAME ABOVE R1 DOOR SEAL DEPRESSOR CRACKED. REMOVED DAMAGE PART; LOCATED; DRILL AND INSTALLED NEW PART I.A.W. SRM 51-40-02-0G-0 AND IAW AMM 51-21-73-701 DWG 141A8370 REV D, SRM 51-40-05-0G-0,
- [SDR SWAA2025102821840](https://openairdocs.org/sdr/SWAA2025102821840.md): Seat Track · worn · Oct 6, 2025 · N969WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK WORN ON UPPER CROWN AT STA 520 LBL 45 WL 208. REMOVED THE SEAT TRACK AT BS 500C+10.5' TO 520 IAW. SRM 51-40-02-0G-0, LOCATED AN DRILLED NEW SEAT TRACK IAW SRM 53-00-52-2R-4 REPAIR 4; INSTALLED NEW SEAT TRACK IAW SRM 53-00-52-2R-4, REPAIR 4,
- [SDR SWAA2025102821688](https://openairdocs.org/sdr/SWAA2025102821688.md): Seal · cracked · Oct 5, 2025 · N969WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT LOWER HORIZONTAL STAB PANEL 333AB SEAL PLATE CRACKED. REPLACED LT LOWER HORIZONTAL STAB PANEL 333AB SEAL PLATE IAW AMM 51-40-02-0G-0, STEP 4.
- [SDR SWAA2025102821481](https://openairdocs.org/sdr/SWAA2025102821481.md): Floor Panel · pulled · Oct 4, 2025 · N969WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242BF HAS UPPER SURFACE DENTED AND PULLED FIBERS. REPAIRED FLOOR PANEL 242BF UPPER SURFACE IAW SRM 53-00-50-2R-2, SRM 53-00-50-2R-0, REPAIR GENERAL, AND EA M 25-153-02385.
- [SDR SWAA2025102821482](https://openairdocs.org/sdr/SWAA2025102821482.md): Floor Panel · damaged · Oct 4, 2025 · N969WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242AF HAS UPPER SURFACE DENTED AND PULLED FIBERS. REPAIRED THE FLOOR PANEL 242AF UPPER SURFACE IAW SRM 53-00-50-2R-2; SRM 53-00-50-2R-0, REPAIR GENERAL, AND EA M 25-153-02385.
- [SDR SWAA2025102721485](https://openairdocs.org/sdr/SWAA2025102721485.md): Floor Panel · pulled · Oct 4, 2025 · N969WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241BF HAS UPPER SURFACE DENTS AND PULLED FIBERS. REPAIRED FLOOR PANEL 241BF UPPER SURFACE IAW SRM 53-00-50-2R-2, SRM 53-00-50-2R-0, REPAIR GENERAL AND EA M-25-153-02385.
- [SDR SWAA2025102721486](https://openairdocs.org/sdr/SWAA2025102721486.md): Floor Panel · dented · Oct 4, 2025 · N969WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241AF HAS UPPER SURFACE DENTS AND PULLED FIBERS. REPAIRED FLOOR PANEL 241AF UPPER SURFACE IAW SRM 53-00-50-2R-2; SRM 53-00-50-2R-0 REPAIR GENERAL AND EA M-25-153-02385.
- [SDR SWAA2025080597542](https://openairdocs.org/sdr/SWAA2025080597542.md): Skin · delaminated · Aug 1, 2025 · N969WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT WING OB AFT FLAP LOWER FACE SHEET DELAMINATED AT IB TE 19.5' X 10'(PICS ATTACHED)<[01] R/R LEFT WING OUT BOARD AFT FLAP PER AMM 27-51-22
- [SDR SWAA2025080196800](https://openairdocs.org/sdr/SWAA2025080196800.md): Seat Back · out of adjust · Jul 31, 2025 · N969WN · Boeing 7377H4 · Passenger Compartment Equipment
  > PASSENGER SEAT 11D RECLINES INTO EMERGENCY EXIT ROW. ADJUSTED PASSENGER SEAT 11D RECLINE CABLE PER CMM 25-21-42.
- [SDR SWAA2025080196794](https://openairdocs.org/sdr/SWAA2025080196794.md): Floor Panel · cracked · Jul 31, 2025 · N969WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 140BF WORN,CRACKED AND PREVIOUSLY REPAIRED. REMOVED AND REPLACED PER AMM 25-52-10-401-NG (CARGO FLOOR PANEL - REMOVAL/INSTALLATION - PERMANENT). AFT CARGO FLOOR PANEL 140BF.
- [SDR SWAA2024100344523](https://openairdocs.org/sdr/SWAA2024100344523.md): Fire Loop · loose · Oct 1, 2024 · N969WN · Boeing 7377H4 · Fire Detection
  > WHEEL WELL FIRE LIGHT ON DURING CLIMB PART NUMBER 35460-3 NEEDED. PAR APP SUBMITTED DCN-042441. OK TO CONT PER MEL 26-4-01 SP1 SP3. UPON INSPECTION FOUND LH SIDE OF THE WHEEL WELL FIRE DETECTOR LOOP NOT SECURED AND THE NUT STRIPPED OUT. FIRE LOOP DETECTOR WI
- [SDR SWAA2024100344541](https://openairdocs.org/sdr/SWAA2024100344541.md): Nut · stripped · Oct 1, 2024 · N969WN · Boeing 7377H4 · Fire Detection
  > WHEEL WELL FIRE LIGHT ON DURING CLIMB PART NUMBER 35460-3 NEEDED. PAR APP SUBMITTED DCN-042441<[01] OK TO CONT PER MEL 26-4-01 SP1 SP3;[02] UPON INSPECTION FOUND LH SIDE OF THE WHEEL WELL FIRE DETECTOR LOOP NOT SECURED AND THE NUT STRIPPED OUT. FIRE LOOP DETEC
- [SDR SWAA2024022957113](https://openairdocs.org/sdr/SWAA2024022957113.md): Girt Bar · unknown · Feb 27, 2024 · N969WN · Boeing 7377H4 · Emergency Equipment
  > L1 AND L2 GIRT BARS VERY HARD FOR FAS TO INSERT.<[01] INSPECTED BOTH L1 AND L2 GIRT BARS. ALL CHECKS GOOD. GIRT BARS OPERATE NORMALLY IAW AMM 25-66-01.
- [SDR SWAA2024020648261](https://openairdocs.org/sdr/SWAA2024020648261.md): Lamp · inoperative · Feb 3, 2024 · N969WN · Boeing 7377H4 · Emergency Lighting
  > AFT ENTRY DOOR SLIDE LIGHT INOP<[01] RELAMPED AFT ENTRY DOOR SLIDE LIGHT REF AMM 33-51-04 OPS CHECK GOOD.
- [SDR SWAA2023110316498](https://openairdocs.org/sdr/SWAA2023110316498.md): Sign · loose · Oct 31, 2023 · N969WN · Boeing 7377H4 · Emergency Lighting
  > OVERHEAD EXIT ROW EXIT SIGN HANGING BY WIRE<[01] SECURED O/H EXIT SIGN PER MM 33-51-01
- [SDR SWAA2023102714193](https://openairdocs.org/sdr/SWAA2023102714193.md): Light · broken · Oct 24, 2023 · N969WN · Boeing 7377H4 · Emergency Lighting
  > EXIT SIGN CENTER ISLE BROKEN<[01] RELAMPED EE LIGHT PER AMM 33-51-28
- [SDR SWAA2023102411184](https://openairdocs.org/sdr/SWAA2023102411184.md): Light · loose · Oct 16, 2023 · N969WN · Boeing 7377H4 · Emergency Lighting
  > AFT ENTRY DOORWAY; EMERGENCY EXIT LIGHT COVER LOOSE<[01] REMOVED AND REPLACED DAMAGED AFT ENTRY DOORWAY; EMERGENCY EXIT LIGHT ASSY I.A.W. AMM 3-51-01-960-802 STEPS 3. C. (1) THRU (6) (A) THRU (E) TEST IS REQUIRE;[02] REMOVED; REPLACED AND PERFORMED GOOD TEST O
- [SDR SWAA2023102411178](https://openairdocs.org/sdr/SWAA2023102411178.md): Cover · loose · Oct 16, 2023 · N969WN · Boeing 7377H4 · Emergency Lighting
  > LH EMERGENCY EXIT DOOR EXIT LIGHT COVER LOOSE.<[01] UPON FURTHER INVESTIGATION; FOUND LIGHT LENS COVER TO HAVE LOWER RETAINING SCREW LOOSE. TIGHTENED LOWER RETAINING SCREW ON L/H EMERGENCY EXIT DOOR EXIT LIGHT LENS COVER IAW SOPM 20-50-01.;[02] COMPLETED MEASU
- [SDR SWAA2023102405831](https://openairdocs.org/sdr/SWAA2023102405831.md): Intercostal · cracked · Sep 30, 2023 · N969WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CABIN FLOOR INTERCOSTAL CRACKED; BS 277 + 5; RBL 1; WL 208<[01] REMOVED AND REPLACED INTERCOSTAL BS277+5; RBL1; WL208<BR>IAW SRM 51-40-02 AND DWG 141A5400;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.
- [SDR SWAA2023102405173](https://openairdocs.org/sdr/SWAA2023102405173.md): Web · corroded · Sep 28, 2023 · N969WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT DOOR CUT-OUT SUB-THRESHOLD WEB FROM STA787+7 TO STA 787+14; RBL 20 TO RBL 28; WL 156; STA 787+15.5; RBL 26; STA 827+18; RBL 20; WL 156.<[01] REMOVED AND REPLACED SUB-THRESHOLD WEB <BR>BS794-BS847 RBL20 WL156 <BR>IAW SRM 51-40
- [SDR SWAA2023102405176](https://openairdocs.org/sdr/SWAA2023102405176.md): Support Angle · corroded · Sep 28, 2023 · N969WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLE AT STATIONS: 767; 767+6; 767+10; WL 156; LBL 22.<[01] THIS CARD WILL BE ACCOMPLISHED ON CUSTOMER CARD NBR: TTG8Q00NPGFW;[02] VERIFIED APPLICABILITY PER SRM 53-60-53-0I-1 AND ALLOWABLE DAMAGE SR
- [SDR SWAA2023102405169](https://openairdocs.org/sdr/SWAA2023102405169.md): Shield · corroded · Sep 28, 2023 · N969WN · Boeing 7377H4 · Cargo Compartments
  > AFT CARGO BAY DOOR CUT-OUT FWD SHIELD IS CORRODED FROM STA 767+1 TO STA 767+19; RBL 20 TO 22; WL 156.<[01] REMOVED AND REPLACED ACB FWD SHIELD IAW SRM 51-40-02;[02] REMOVED AND REPLACED ACB FWD SHIELD IAW SRM 51-40-02 AND DWG # 146A0081;[03] VERIFIED MEASUREME
- [SDR SWAA2023102405171](https://openairdocs.org/sdr/SWAA2023102405171.md): Sidewall Support · corroded · Sep 28, 2023 · N969WN · Boeing 7377H4 · Cargo Compartments
  > CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT AT: STA727C+18; FROM STA727D+3 TO 727D+11; STA727D+14; STA727D+18; STA727E+2; STA727E+6; STA727E+ 18; STA747+5; STA747+10 WL156; RBL 22<[01] THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q00NPEX4
- [SDR SWAA2023102405174](https://openairdocs.org/sdr/SWAA2023102405174.md): Sidewall Support · corroded · Sep 28, 2023 · N969WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLE AT: STA 747+14 AND STA 747+14; RBL 22; WL 156.<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT RBL 22 WL156 STA 727 -STA 767 I.A.W SRM 51-40-0A-0G-0 AND DWG 146A7500.;
- [SDR SWAA2023102405175](https://openairdocs.org/sdr/SWAA2023102405175.md): Sidewall Support · corroded · Sep 28, 2023 · N969WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLE AT: STATIONS 727A+6; 727D+3; 727D+6; 727D+7.5; 727D+13; 727D+16; 727E; 727E+10; 727E+12;747+18; LBL 20-22; WL 156.<[01] REMOVED AND INSTALLED NEW AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT
- [SDR SWAA2023102405170](https://openairdocs.org/sdr/SWAA2023102405170.md): Sidewall Support · corroded · Sep 28, 2023 · N969WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLE AT: STA 727A+10; 727A+14; 727B; 727B+2; 727B+10; 727B+14; 727B+18; 727C; 727C+10; 727C+14; WL 156; RBL 22.<[01] THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q00NPEX4;[02] VERIFIED CORRECTI
- [SDR SWAA2023102404965](https://openairdocs.org/sdr/SWAA2023102404965.md): Scuff Plate · cracked · Sep 27, 2023 · N969WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB AFT CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED FCB AFT CORNER SCUFF PLATE. IAW SRM 53-30-15-2R-1<BR>THIS PART WILL BE INSTALLED ON TASK CARD NBR: TTG8Q00NFN78.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE
- [SDR SWAA2023102404217](https://openairdocs.org/sdr/SWAA2023102404217.md): Cargo Track · corroded · Sep 25, 2023 · N969WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO BAY HAS CORROSION ON RAIL AT BS 480+19; LBL 2; WL 156<[01] FWD CARGO BAY RAIL WAS REPAIRED PER REF SRM 53-00-53-1A-2;[02] VERIFIED COMPLETE
- [SDR SWAA2023102404218](https://openairdocs.org/sdr/SWAA2023102404218.md): Floor Panel · pulled · Sep 25, 2023 · N969WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CABIN FLOOR PANEL 222DF HAS PULLED STRANDS ON UPPER SURFACE.<[01] FWD CABIN FLOOR PANEL 222DF HAD PULLED STRANDS ON UPPER SURFACE REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED JOB COMPLETE AND CURE SHEETS
- [SDR SWAA2023102404213](https://openairdocs.org/sdr/SWAA2023102404213.md): Gusset · cracked · Sep 25, 2023 · N969WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY UPPER GUSSET IS CRACKED AT BS 500C+19; RBL 61; WL 194<[01] REMOVED AND REPLACED FCB UPPER GUSSET BS 500C+19; RBL 61; WL 194 IAW SRM 51-40-02 AND DWG #143A7902;[02] VERIFIED COMPLETE RII STEP 3.;[03] VERIFIED COMPLETE STEP 4; CARD COMPLETE.
- [SDR SWAA2023102404214](https://openairdocs.org/sdr/SWAA2023102404214.md): Gusset · cracked · Sep 25, 2023 · N969WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY UPPER GUSSET IS CRACKED AT BS 500C+19; LBL 61; WL 194<[01] INSTALLED NEW FCB UPPER GUSSET BS 500C+19; LBL 61; WL 194 IAW SRM 51-40-02 AND DWG #143A7902;[02] REMOVED AND REPLACED FCB UPPER GUSSET BS 500C+19; LBL 61; WL 194 IAW SRM 51-40-02 AND DWG
- [SDR SWAA2023102402678](https://openairdocs.org/sdr/SWAA2023102402678.md): Seal · cracked · Sep 21, 2023 · N969WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LT HORIZ STAB GAP COVER 333AT BLADE SEAL IS CRACKED<[01] REMOVED AND REPLACED LT HORIZ STAB PANEL 333AT BLADE SEAL IAW SRM 51-40-02; STEP 4. AND MM 20-50-11.<BR><BR>SCREWGUN<BR>ATS1482<BR>CAL DUE 10/23;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.
- [SDR SWAA2023102402664](https://openairdocs.org/sdr/SWAA2023102402664.md): Floorbeam · corroded · Sep 20, 2023 · N969WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON 986 FLOOR BEAM AT AFT WET AREA RBL43 WL208.<[01] REPAIRED IAW SRM 53-70-51-2R-6; REPAIR 6; FIG 205;<BR>FLOOR BEAM BS986; RBL43; WL208;[02] VERIFIED CORRECTIVE ACTION COMPLETE
- [SDR SWAA2023102402660](https://openairdocs.org/sdr/SWAA2023102402660.md): Stringer · cracked · Sep 20, 2023 · N969WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > AREA AFT OF FWD CARGO BAY HAS A CRACKED STR; STR R25; BS 520+19<[01] REMOVED AND REINSTALLED AND PERFORMED GOOD OPERATIONAL TEST OF RETRACTABLE LANDING LIGHT ASSEMBLY. IAW AMM 33-42-02-960-802.;[02] CERTIFIED ACTION 1.;[03] COMPLETED STEPS 6 AND 10;[04] CERTIF
- [SDR SWAA2023102502239](https://openairdocs.org/sdr/SWAA2023102502239.md): Skin · corroded · Sep 19, 2023 · N969WN · Boeing 7377H4 · Aerodynamic Fairings
  > EXTERNAL RADOME AND ADAPTER RING - ROW 44 WI-FI - AIRCRAFT SKIN HAS SPOTS CORROSION ON SURROUND RIVETS BS 727E+10 TO BS 747+17 BETWEEN LBL 13 TO RBL (MARKED) STC LARGE EXTERNAL DOUBLER ROW 44 WI-FI -HAS SPOTS CORROSION ON SURROUND RIVETS BS 727E+4 TO BS 747+10
- [SDR SWAA2023102502238](https://openairdocs.org/sdr/SWAA2023102502238.md): Skin · corroded · Sep 19, 2023 · N969WN · Boeing 7377H4 · Aerodynamic Fairings
  > EXTERNAL RADOME AND ADAPTER RING - ROW 44 WI-FI - AIRCRAFT SKIN HAS SPOTS CORROSION ON SURROUND RIVETS BS 727B+15 TO BS 727C+14 BETWEEN LBL 10 TO RBL 10 APPROX. 53 EA (MARKED)<[01] 'REFER TO FAULT TTG8Q00NJ6Y7 WHERE EA 23-153-02981 WAS ADDED AS A SUBTASK.';[02
- [SDR SWAA2023102401030](https://openairdocs.org/sdr/SWAA2023102401030.md): Tail Cone · debonded · Sep 16, 2023 · N969WN · Boeing 7377H4 · Aerodynamic Fairings
  > TAILCONE FAIRING DISBONDED SKIN AT LOWER RH SIDE 9' FROM FWD EDGE<[01] TAILCONE FAIRING DISBONDED SKIN AT LOWER RH SIDE 9' FROM FWD EDGE WAS REPAIRED IAW SRM 51-70-04-2R-2.;[02] VERIFIED THE REPAIR OF THE TAILCONE FAIRING DISBONDED SKIN AT LOWER RH SIDE 9' FRO
- [SDR SWAA2023062060976](https://openairdocs.org/sdr/SWAA2023062060976.md): Floor Panel · damaged · Jun 20, 2023 · N969WN · Boeing 7377H4 · Cargo Compartments
  > FWD CARGO COMPARTMENT AFT FLOORBOARD IS WTL.<[01] REMOVED AND REPLACED FWD CARGO AFT FLOORBOARD REF. AMM 25-52-10
- [SDR SWAA2023062060977](https://openairdocs.org/sdr/SWAA2023062060977.md): Floor Panel · damaged · Jun 20, 2023 · N969WN · Boeing 7377H4 · Cargo Compartments
  > AFT CARGO CARGO COMPARTMENT FLOORBOARD 140BF IS WTL<[01] REMOVED FLOOR BOARD REF AMM 20-50-11. FABRICATED AND INSTALLED FLOORBOARD PANEL PER M/M 25-52-01 & 25-52-10.;[03] VERIFIED FABRICATION AND INSTALLATION OF FLOORBOARD PANEL PER M/M 25-52-01 & 25-52-10.
- [SDR SWAA2023032721178](https://openairdocs.org/sdr/SWAA2023032721178.md): Cover · missing · Mar 26, 2023 · N969WN · Boeing 7377H4 · Emergency Lighting
  > CAPT SIDE O/W EXIT LIGHTED EXIT/SALIDA SIGN COVER MISSING<[01] INSTALLED LH EMERG EXIT LIGHTED SIGN COVER PER AMM 33-51-01. A/C OK FOR SERVICE.
- [SDR SWAA2023010587376](https://openairdocs.org/sdr/SWAA2023010587376.md): Container · loose · Jan 3, 2023 · N969WN · Boeing 7377H4 · Escape Slide
  > CREW REPORTS R2 DOOR SLIDE CONTAINER LOOSE. SECURED DOOR SLIDE CONTAINER MOUNTING HARDWARE PER AMM 25-66-01
- [SDR SWAA2022111068812](https://openairdocs.org/sdr/SWAA2022111068812.md): Light · inoperative · Nov 8, 2022 · N969WN · Boeing 7377H4 · Emergency Lighting
  > L/H OVERWING EXIT EMERGENCY EXIT SIGN; FWD LIGHT INOP / [01] R&R EMERGENCY EXIT LIGHT PER AMM 33-51-00
- [SDR SWAA2022101356938](https://openairdocs.org/sdr/SWAA2022101356938.md): None · missing · Oct 6, 2022 · N969WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > EXTERNAL POWER DOOR CUTOUT LOWER FLANGE HAS AREA MISSING / [01] REMOVED THE INITIAL RUBBING BLOCK AND TRIMMED OUT DAMAGED AREA OF EGPR SURROUND DOUBLER IAW SRM 53-10-15-2R-4 ZONE 2 ALT. 2;[02] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 23. NO DEFECTS NOTED. TOOL#
- [SDR SWAA2022080135892](https://openairdocs.org/sdr/SWAA2022080135892.md): Hook · loose · Jul 29, 2022 · N969WN · Boeing 7377H4 · Escape Slide
  > L1 DOOR SLIDE COVER BOTH GIRT BART HOOKS HARDWARE LOOSE. / [01] SECURED L1 DOOR SLIDE COVER GIRT BART HOOKS PER SRM 51-40-02;[02] SECURED L1 DOOR SLIDE GIRT BART HOOK PER SRM 51-40-02
- [SDR SWAA2021110233952](https://openairdocs.org/sdr/SWAA2021110233952.md): Light · inoperative · Oct 27, 2021 · N969WN · Boeing 737* · Emergency Lighting
  > R/H GROUND ILLUMINATION EMERGENCY LIGHT IS INOP; RH GROND ILLMINATION EMERGENCY LIGHT IS INOP / [07] REPLACED FUSE FOR R/H GROUND ILLUMINATION EMERGENCY LIGHT PER AMM 33-51-06-960-804 STEPS 3.D.(1) THRU (4). PERFORMED GOOD EMERGENCY LIGHTS OPERATIONAL TEST PE
- [SDR SWAA2021110232346](https://openairdocs.org/sdr/SWAA2021110232346.md): Scuff Plate · cracked · Oct 21, 2021 · N969WN · Boeing 737* · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED; / [01] WELDED CRACK ON RADIUS OF ACB; AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4).<BR>WELDING MACHINE CAL I.D. E10583; S/N; KJ256554 12/2021; [02] VERIF

Next page: https://openairdocs.org/aircraft/N969WN/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 = 'N969WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N969WN/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.
