# Service difficulty reports: N209WN

A list on [N209WN](https://openairdocs.org/aircraft/N209WN.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 6 · 296 reports

- [SDR SWAA2026101975253](https://openairdocs.org/sdr/SWAA2026101975253.md): Battery Pack · no test · Oct 15, 2026 · N209WN · Boeing 7377H4 · Emergency Lighting
  > AFT LEFT EMERGENCY BATTERY PACK M1673 FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026101999157](https://openairdocs.org/sdr/SWAA2026101999157.md): Battery Pack · no test · Oct 15, 2026 · N209WN · Boeing 7377H4 · Emergency Lighting
  > AFT RT EMERGENCY BATTERY PACK M1672 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026101923787](https://openairdocs.org/sdr/SWAA2026101923787.md): Battery Pack · no test · Oct 15, 2026 · N209WN · Boeing 7377H4 · Emergency Lighting
  > RT EMERGENCY EXIT BATTERY PACK M1669 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK PER AMM 33-51-06 INSPECTION VERIFIED CORRECTIVE ACTION TAKEN IN STEP 1.
- [SDR SWAA2026101914969](https://openairdocs.org/sdr/SWAA2026101914969.md): Battery Pack · no test · Oct 15, 2026 · N209WN · Boeing 7377H4 · Emergency Lighting
  > LEFT EMERGENCY EXIT BATTERY PACK M1668 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026092855806](https://openairdocs.org/sdr/SWAA2026092855806.md): Screw · missing · Sep 22, 2026 · N209WN · Boeing 7377H4 · Passenger Compartment Equipment
  > SEAT 15F TRAY TABLE INOPERATIVE. INSTALLED MISSING SCREW IAW AMM SIP
- [SDR SWAA2026090384922](https://openairdocs.org/sdr/SWAA2026090384922.md): Sign · missing · Aug 30, 2026 · N209WN · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY DOOR EMERGENCY EXIT SIGN MISSING. REPLACED THE FWD ENTRY DOOR EMERGENCY LIGHT ASSY IAW.AMM 33-51-04.
- [SDR SWAA2026081016905](https://openairdocs.org/sdr/SWAA2026081016905.md): Lens · missing · Aug 5, 2026 · N209WN · Boeing 7377H4 · Emergency Lighting
  > COVER FOR EMERGENCY LIGHT NEAR L1 DOOR MISSING. REPLACED MISSING EMERGENCY LENS AT L1 DOOR IAW MM 33-51-01.
- [SDR SWAA2026072039827](https://openairdocs.org/sdr/SWAA2026072039827.md): Sign · out of adjust · Jul 15, 2026 · N209WN · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY DOOR EXIT SIGN FELL OFF. REINSTALLED FWD ENTRY EXIT SIGN LENS COVER IAW AMM 33-51-01.
- [SDR SWAA2025122654860](https://openairdocs.org/sdr/SWAA2025122654860.md): Seat Back · out of adjust · Dec 22, 2025 · N209WN · Boeing 7377H4 · Passenger Compartment Equipment
  > SEAT BACK 11B RECLINES INTO EXIT ROW. ADJUSTED THE SEAT BACK IAW AMM 25-22-00.
- [SDR SWAA2025101524300](https://openairdocs.org/sdr/SWAA2025101524300.md): O-Ring · leaking · Oct 13, 2025 · N209WN · Boeing 7377H4 · Hydraulic System, Main
  > HYDRAULIC SYSTEM A WENT DOWN TO 58 % IN FLIGHT. LOST 10 % DURING THE LEG. RETURNED TO NORMAL INDICATIONS AFTER LANDING. NOTED FLUID DRIPPING OUT OF HELL HOLE DRAINS AND AREA THICK WITH VAPOR. REPLACED O-RING FROM LEAKING UNION AT ELEVATOR FEEL COMPUTER AS
- [SDR SWAA2025031204529](https://openairdocs.org/sdr/SWAA2025031204529.md): B-Nut · loose · Mar 12, 2025 · N209WN · Boeing 7377H4 · Hydraulic Power Accumulator, Main
  > EVIDENCE OF HYDRAULIC LEAK IN HELL HOLE <[01]. PERFORMED INSPECTION IN THE HELL HOLE FOUND HYDRAULIC LEAK FROM ELEVATOR FEEL COMPUTER AT B PRESSURE LINE FLARELES TUBING B- NUT WAS LOSE TIGHTENED PER AMM 20-10-51. AND HYDRAULIC LEAK CHECK DONE FOUND OK PER AMM
- [SDR SWAA2025031103592](https://openairdocs.org/sdr/SWAA2025031103592.md): Fitting · cracked · Mar 10, 2025 · N209WN · Boeing 7377H4 · Nacelle/Pylon, Attach Fittings
  > LEFT ENGINE NACELLE AFT ATTACH POINT SUPPORT FITTING CRACKED.<[01] REMOVED AFT ATTACH POINT SUPPORT FITTING IAW SRM 51-40-02.;[02] REPLACED LEFT ENGINE AFT FAIRING AFT SUPPORT FITTING PER SRM 51-40-02 REINSTALLED LEFT ENGINE AFT FAIRING ASSEMBLY PER AMM 54-52-
- [SDR SWAA2025021294193](https://openairdocs.org/sdr/SWAA2025021294193.md): Battery Pack · failed · Feb 7, 2025 · N209WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH M1674 FAIL TO LIGHT UP<[01] REMOVED AND REPLACED BATTERY PACK M1674. PERFORMED GOOD OP CHECK OF EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1674 PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025021294194](https://openairdocs.org/sdr/SWAA2025021294194.md): Battery Cable · failed · Feb 7, 2025 · N209WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH M1675 FAIL TO LIGHT UP<[01] REMOVED AND REPLACED BATTERY PACK M1675. PERFORMED GOOD OP CHECK FOR LIGHTS ASSOCIATED TO BATTERY PACK M1675. PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025021487993](https://openairdocs.org/sdr/SWAA2025021487993.md): Rib · cracked · Jan 21, 2025 · N209WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK ON RT HORIZ. STAB. LEADING EDGE RIB AT L/E STA. 86.66<[01] REMOVED AND REPLACED LE RIB AT L/E STA. 86.66 IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025021487992](https://openairdocs.org/sdr/SWAA2025021487992.md): Rib · cracked · Jan 21, 2025 · N209WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK ON RT HORIZ. STAB. LEADING EDGE RIB AT L/E STA. 95.96<[01] REMOVED AND REPLACED RIB AT R/H LE STAB STA 95.96 IAW SRM 51-40-02-0G-0 AND DWG. 186A1001-16.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025021887822](https://openairdocs.org/sdr/SWAA2025021887822.md): Floor Support · cracked · Jan 20, 2025 · N209WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > BREAKER PANEL IS CRACKED AT BS 540 LBL 1 WL208 BREAKER PANEL IS CRACKED AT BS 540 RBL1 WL208<[01] REPLACED BREAKER PANEL AT BS 540 RBL1-RBL25 WL208 PER SRM 51-40-02 AND DWG#143A0060 ID:0036 REV:A;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TAB
- [SDR SWAA2025021887321](https://openairdocs.org/sdr/SWAA2025021887321.md): Stringer Clip · cracked · Jan 18, 2025 · N209WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP S-8L BS 259.5 (MARKED)<[01] REMOVED CRACKED STRINGER CLIP S-8L BS 259.5 AND REPLACED WITH NEW FABRICATED STRINGER CLIP IAW SRM 51-40-02-0G-0.;[02] VERIFIED STEP 2;5 CORRECTION ACTION ITEM 1 MEASUREMENT FIELD COMPLETE; CARD COMPLETE
- [SDR SWAA2025021486195](https://openairdocs.org/sdr/SWAA2025021486195.md): Rib · cracked · Jan 14, 2025 · N209WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > L/H HORIZONTAL STAB #5 INSPAR RIB AT STAB STA 129.50 I/B LOWER FLANGE IS CRACKED AT FWD EDGE<[01] REPAIRED L/H HORIZONTAL STAB #5 INSPAR RIB AT STAB STA 129.50 I/B LOWER FLANGE IAW SRM 55-10-09-2R-5.;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2025021285467](https://openairdocs.org/sdr/SWAA2025021285467.md): Floor Panel · delaminated · Jan 13, 2025 · N209WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241EF HAS DENTS AND DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 241EF WITH DENTS AND DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2025021085464](https://openairdocs.org/sdr/SWAA2025021085464.md): Floor Panel · delaminated · Jan 13, 2025 · N209WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242AF HAS DELAMINATION<[01] ATTACHED (2EA) PLACARDS TO THE UPPER SURFACE USING BAC27DCA854 LOT # 1591209-1 IAW BOEING DWG: 144A5810 ID: 0189.<BR><BR>242AF FLOOR PANEL DELAMINATION DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A009
- [SDR SWAA2025021085465](https://openairdocs.org/sdr/SWAA2025021085465.md): Floor Panel · delaminated · Jan 13, 2025 · N209WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231XF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 231XF; WITH DELAMINATION; WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
- [SDR SWAA2025021085466](https://openairdocs.org/sdr/SWAA2025021085466.md): Floor Panel · delaminated · Jan 13, 2025 · N209WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241DF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 241DF WITH DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
- [SDR SWAA2025021085468](https://openairdocs.org/sdr/SWAA2025021085468.md): Floor Panel · delaminated · Jan 13, 2025 · N209WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241FF HAS DENTS AND DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 241FF WITH DENTS AND DELAMINATED WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
- [SDR SWAA2025021085469](https://openairdocs.org/sdr/SWAA2025021085469.md): Floor Panel · delaminated · Jan 13, 2025 · N209WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242CF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 242CF WITH DELAMINATION WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.;[02] JOB COMPLETE.
- [SDR SWAA2025021085462](https://openairdocs.org/sdr/SWAA2025021085462.md): Floor Panel · delaminated · Jan 13, 2025 · N209WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242DF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 242DF WITH DELAMINATION WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.;[02] JOB COMPLETE.
- [SDR SWAA2025021785215](https://openairdocs.org/sdr/SWAA2025021785215.md): Scuff Plate · cracked · Jan 11, 2025 · N209WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FSD SCUFF PLATE; AFT EDGE IS CRACKED.<[01] REPAIRED FSD SCUFF PLATE PER SRM 53-10-15-2R-1 PARA 4.B.(3)-(6) AND (8). WILL BE REINSTALLED ON TASK TTG8Q003D32V STEP 10;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025021884802](https://openairdocs.org/sdr/SWAA2025021884802.md): Former · cracked · Jan 10, 2025 · N209WN · Boeing 7377H4 · Aerodynamic Fairings
  > R/H WING TO BODY FAIRING FORMER IS CRACKED BS 500D STRINGER 19 R/H<[01] FAIRING FORMER R/H IS CRACKED AT BS 500D IN L=2' NOT FOUND ALLOWABLE LIMITS ON SRM WILL BE REPAIRED BY REPLACEMENT OF PART PER SRM 51-10-02. PAR 9.;[02] VERIFIED CORRECTIVE ACTION 1;[03] R
- [SDR SWAA2025021484913](https://openairdocs.org/sdr/SWAA2025021484913.md): Skin · cracked · Jan 10, 2025 · N209WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 184.70; 26.5' FROM FWD EDGE; 0.9' IN LENGTH (MARKED)<[01] ACCOMPLISHED REPAIR OF CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 184.70; 26.5' FROM FWD EDGE<BR>PER SWA EA #25-155-00108;[02] VE
- [SDR SWAA2025021484804](https://openairdocs.org/sdr/SWAA2025021484804.md): Nut Plate · damaged · Jan 10, 2025 · N209WN · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR GIRT BAR FLOOR BRACKET SCREW NUT PLATE IS DAMAGED AT THE FWD SIDE FWD SCREW;<[01] REPLACED FWD SERVICE DOOR FWD GIRT BAR FLOOR BRACKET FWD SCREW NUT PLATE PER DWG#140A1005 ID:1 REV:J;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025021884799](https://openairdocs.org/sdr/SWAA2025021884799.md): Doubler · cracked · Jan 9, 2025 · N209WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > EGPR SURROUND DOUBLER IS CRACKED BS233 WL175 8' ABOVE S-24R MARKED<[01] REPAIRED EGPR SURROUND DOUBLER AT BS233 WL175 8' ABOVE S-24R IAW SRM 53-10-15-2R-4 REPAIR 4 PARG 4(A-M) FIG. 204 SHT.(3-4);[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABL
- [SDR SWAA2025021784503](https://openairdocs.org/sdr/SWAA2025021784503.md): Panel · debonded · Jan 9, 2025 · N209WN · Boeing 7377H4 · Fuselage Structure (General)
  > PANEL 192E INNER SKIN IS DISBONDED. (MARKED)<[01] PANEL 192E; INNER SKIN WITH DISBOND; WAS REPAIRED IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025021484800](https://openairdocs.org/sdr/SWAA2025021484800.md): Stiffener · cracked · Jan 9, 2025 · N209WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LH HORIZONTAL STABILIZER #5 INSPAR RIB; AT STABILIZER STATION 129.50; 2ND VERTICAL STIFFENER IS CRACKED.<[01] REPAIRED LH HORIZONTAL STABILIZER #5 INSPAR RIB; AT STABILIZER STATION 129.50; 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4 REPAIR 4;[02] VERIFIED COM
- [SDR SWAA2025021484801](https://openairdocs.org/sdr/SWAA2025021484801.md): Stiffener · cracked · Jan 9, 2025 · N209WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RH HORIZONTAL STABILIZER #9 INSPAR RIB; AT STABILIZER STATION 166.30; 3RD VERTICAL STIFFENER IS CRACKED.<[01] REPAIRED RH HORIZONTAL STABILIZER #9 INSPAR RIB; AT STABILIZER STATION 166.30; 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4 REPAIR 4.;[02] VERIFIED CO
- [SDR SWAA2025021084496](https://openairdocs.org/sdr/SWAA2025021084496.md): Sidewall Support · corroded · Jan 8, 2025 · N209WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] ' THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550'.;[02] COMPLETE
- [SDR SWAA2025021084497](https://openairdocs.org/sdr/SWAA2025021084497.md): Sidewall Support · corroded · Jan 8, 2025 · N209WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] ' THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550'.;[02] COMPLETE
- [SDR SWAA2025021883828](https://openairdocs.org/sdr/SWAA2025021883828.md): Skin · cracked · Jan 7, 2025 · N209WN · Boeing 7377H4 · Leading Edge Devices
  > CRACKED LOWER SURFACE OF THE LEADING-EDGE # 3 SLAT NOSE SKIN AT ACTUATOR RIBS - LEFT WING (MARKED)<[01] REPAIRED LOWER SURFACE OF THE LEADING-EDGE # 3 SLAT NOSE SKIN AT ACTUATOR RIBS - LEFT WING IAW SRM 57-42-01-2R-8.
- [SDR SWAA2025021883831](https://openairdocs.org/sdr/SWAA2025021883831.md): Skin · cracked · Jan 7, 2025 · N209WN · Boeing 7377H4 · Leading Edge Devices
  > CRACKED LOWER SURFACE OF THE LEADING-EDGE # 5 SLAT NOSE SKIN AT ACTUATOR RIBS - RIGHT WING (MARKED)<[01] REPAIRED LOWER SURFACE OF THE LEADING-EDGE #5 SLAT NOSE SKIN AT ACTUATOR RIBS - RIGHT WING IAW SRM 57-42-01-2R-8.;[02] VERIFIED CORRECTIVE ACTION 1;[03] VE
- [SDR SWAA2024071110882](https://openairdocs.org/sdr/SWAA2024071110882.md): Isolation Mount · cracked · Jul 10, 2024 · N209WN · Boeing 7377H4 · Escape Slide
  > AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2024071110875](https://openairdocs.org/sdr/SWAA2024071110875.md): Isolation Mount · cracked · Jul 10, 2024 · N209WN · Boeing 7377H4 · Escape Slide
  > FWD GALLEY SERVICE DOOR AFT SLIDE MOUNT ISOLATOR CRACKED<[01] R&R FWD GALLEY SERVICE DOOR AFT SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2023062671226](https://openairdocs.org/sdr/SWAA2023062671226.md): Bracket · cracked · Jun 24, 2023 · N209WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING UPPER PANEL SUPPORT FWD ATTACH POINT BRACKET IS CRACKED. (Z BRACKET)<[01] REMOVED AND REPLACED RIGHT WING UPPER PANEL SUPPORT FWD ATTACH POINT BRACKET PER SRM 51-40-02.
- [SDR SWAA2023033021358](https://openairdocs.org/sdr/SWAA2023033021358.md): Rib · cracked · Mar 28, 2023 · N209WN · Boeing 7377H4 · Trailing Edge Flaps
  > RIGHT WING UPPER INBOARD FIXED TRAILING EDGE SEAL RIB CRACKED AND BROKEN<[01] REMOVED AND REPLACED RIGHT WING UPPER INBOARD FIXED TRAILING EDGE SEAL RIB PER SRM 51-40-02
- [SDR SWAA2023020698639](https://openairdocs.org/sdr/SWAA2023020698639.md): Light · inoperative · Feb 3, 2023 · N209WN · Boeing 7377H4 · Emergency Lighting
  > RH INTERIOR EMERGENCY LIGHT INOP AT RH SEAT ROW 18.<[01] FOUND FUSE IN EMERGENCY LIGHT POWER SUPPLY M1672 THAT POWERS AISLE LIGHTS AT ROWS 16ABC AND 18ABC BLOWN. REPLACED FUSE AND LIGHTS WERE STILL INOP AND FOUND THE FUSE BLOWN AGAIN. REMOVED LAMPS FROM THE AF
- [SDR SWAA2023020696817](https://openairdocs.org/sdr/SWAA2023020696817.md): Bulb · inoperative · Jan 31, 2023 · N209WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LOCATOR LIGHT OVER FWD L/H DOOR HAS INOP BULBS<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF FWD L/H DOOR'S EMERGENCY EXIT LOCATOR IAW AMM 33-51-01-960-801.<BR><BR>NO ADDITIONAL FAULTS OBSERVED.;[02] VERIFIED CORRECTIVE ACTION #1.
- [SDR SWAA2023020696814](https://openairdocs.org/sdr/SWAA2023020696814.md): Light · inoperative · Jan 31, 2023 · N209WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT L/H FWD ENTRY DOOR SLIDE LIGHT INOP EMERGENCY EXIT L/H FWD ENTRY DOOR SLIDE LIGHT INOP (EXTERIOR LIGHT)<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF L/H FWD DOOR'S EXTERIOR SLIDE LIGHT IAW AMM 33-51-04-960-801.<BR><BR>NO ADDITIONAL FAUL
- [SDR SWAA2023020795281](https://openairdocs.org/sdr/SWAA2023020795281.md): Scuff Plate · cracked · Jan 26, 2023 · N209WN · Boeing 7377H4 · Fuselage Main, Structure
  > FORWARD CARGO COMPARTMENT AFT SCUFF PLATE IS CRACKED.<[01] WELDED CRACKED RADIUS OF FWD CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARAGRAPH 4.B. (2) AND (4)<BR>EQUIP USED. WELDING MACHINE E10583 CAL DUE D
- [SDR SWAA2023020792786](https://openairdocs.org/sdr/SWAA2023020792786.md): Intercostal · cracked · Jan 18, 2023 · N209WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON PASSENGER CABIN FLOOR INTERCOSTAL AT BS 500D+10 BL 0.(MARKED)<[01] DAMAGE FOUND AT PASSENGER CABIN FLOOR INTERCOSTAL UPPER ANGLE FOUND TO BE OUT OFF LIMIT DUE TO NO LIMIT ON SRM PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-40-02-0G-0. PAR. 9C;[02]
- [SDR SWAA2023020891365](https://openairdocs.org/sdr/SWAA2023020891365.md): Panel · delaminated · Jan 13, 2023 · N209WN · Boeing 7377H4 · Wing, Control Surfaces
  > PANEL 561BB DELAMINATED IN SEVERAL LOCATIONS ON OUTER SURFACE<[01] FOUND PANEL TO HAVE AREAS OF DISBOND. THESE AREAS OF DISBOND ARE BEYOND ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARAGRAPH 4.A.(5)(A)<BR><BR>DAMAGED AREAS WILL BE REPAIRED IAW SRM 51-70-05-2R-1 A
- [SDR SWAA2023020890443](https://openairdocs.org/sdr/SWAA2023020890443.md): Support Bracket · cracked · Jan 10, 2023 · N209WN · Boeing 7377H4 · Wing, Center Box
  > LEFT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET (212A1116) ACCESS PANEL 192CL BS540+6 LBL8.<[01] REMOVED LEFT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET BS540+6 LBL8 IAW AMM TASK 20-50-11-910-801.;[02] REPLACED AND INSTALLED NEW DUCT SUPPORT BRACKET (212A1116) ACC
- [SDR SWAA2023020890447](https://openairdocs.org/sdr/SWAA2023020890447.md): Support Bracket · cracked · Jan 10, 2023 · N209WN · Boeing 7377H4 · Wing, Center Box
  > RIGHT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET (212A1116) ACCESS PANEL 192CR BS540+6 RBL8.<[01] REMOVED RIGHT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET BS540+6 RBL8 IAW AMM TASK 20-50-11-910-801.;[02] REPLACED AND INSTALLED NEW DUCT SUPPORT BRACKET (212A1116) A

Next page: https://openairdocs.org/aircraft/N209WN/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 = 'N209WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N209WN/reports

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