# Service difficulty reports: N428WN

A list on [N428WN](https://openairdocs.org/aircraft/N428WN.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 7 · 302 reports

- [SDR SWAA2026051397056](https://openairdocs.org/sdr/SWAA2026051397056.md): Slide · out of adjust · May 9, 2026 · N428WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE NEEDS REPACK. REPACKED FWD ENTRY DOOR SLIDE IAW MT 725-61-06.
- [SDR SWAA2026032080133](https://openairdocs.org/sdr/SWAA2026032080133.md): Resolver · out of adjust · Mar 16, 2026 · N428WN · Boeing 7377H4 · Engine Controls
  > ASYMETRIC THRUST WHEN SETTING TAKEOFF POWER AUTOTHROTTLE SPLIT AFTER TOGA IS PRESSED<[01] FOUND #2 TLA RESOLVER VALUE OUT OF LIMITS. ADJUSTED PER AMM 76-11-05
- [SDR SWAA2025122654756](https://openairdocs.org/sdr/SWAA2025122654756.md): Battery Pack · inoperative · Dec 22, 2025 · N428WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT AT 12ABC INOPERATIVE. R & R THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK AT BS 727C+13 IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2025120442229](https://openairdocs.org/sdr/SWAA2025120442229.md): Lens · missing · Dec 3, 2025 · N428WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT ROW LIGHT COVER IS MISSING, FO SIDE. INSTALLED THE EMERGENCY EXIT SIGN LENS IAW AMM 33-51-01. ACFT OK FOR SERVICE..
- [SDR SWAA2025110530986](https://openairdocs.org/sdr/SWAA2025110530986.md): Slide · loose · Nov 2, 2025 · N428WN · Boeing 7377H4 · Escape Slide
  > FORWARD SERVICE DOOR SLIDE RETAINING HOOK LOOSE. FWD SERVICE DOOR SLIDE RETAINING HOOK RETIGHTENED IAW SIP AND OPS CHECK GOOD.
- [SDR SWAA2025103129302](https://openairdocs.org/sdr/SWAA2025103129302.md): Lamp · inoperative · Oct 28, 2025 · N428WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT AT 14 ABC INOPERATIVE. RELAMPED EMERGENCY LIGHT AT ROW 14ABC PER AMM 33-51-03.
- [SDR SWAA2025092416966](https://openairdocs.org/sdr/SWAA2025092416966.md): Sign · damaged · Sep 22, 2025 · N428WN · Boeing 7377H4 · Emergency Lighting
  > FWD LAV EMERGENCY EXIT FORWARD OF L1 DOOR DAMAGED. REMOVED AND REPLACED PER AMM 33-51-01-960-802-NG.
- [SDR SWAA2025081403638](https://openairdocs.org/sdr/SWAA2025081403638.md): Slide · unpacked · Aug 13, 2025 · N428WN · Boeing 7377H4 · Escape Slide
  > L1 DOOR ESCAPE SLIDE GIRT REPACK REQUIRED. REPACKED L1 DOOR ESCAPE SLIDE GIRT REF AMM 25-66-01.
- [SDR SWAA2025031907151](https://openairdocs.org/sdr/SWAA2025031907151.md): Handle · broken · Mar 19, 2025 · N428WN · Boeing 7377H4 · Galley Doors
  > AFT GALLEY SERVICE DOOR ASSIST HANDLE BROKEN AND ATTACH HARDWARE CRACKED <[01] R&R AFT GALLEY SERVICE DOOR ASSIST HANDLE AND ATTACH HARDWARE IAW AMM 52-41-31.; [02] C/W INSPECTION.
- [SDR SWAA2025031907456](https://openairdocs.org/sdr/SWAA2025031907456.md): Fastener · broken · Mar 19, 2025 · N428WN · Boeing 7377H4 · Galley Doors
  > AFT GALLEY SERVICE DOOR ASSIST HANDLE BROKEN AND ATTACH HARDWARE CRACKED <[01]. R&R AFT GALLEY SERVICE DOOR ASSIST HANDLE AND ATTACH HARDWARE IAW AMM 52-41-31.; [02] C/W INSPECTION.
- [SDR SWAA2025010884121](https://openairdocs.org/sdr/SWAA2025010884121.md): Skin · delaminated · Jan 8, 2025 · N428WN · Boeing 7377H4 · Trailing Edge Flaps
  > LH INBOARD MAIN FLAP LOWER SKIN DELAMINATION AT AFT OUTBOARD. REMOVED AND REPLACED L/H I/B AFT FLAP O/B WEDGE PANEL PER AMM 27-51-11.
- [SDR SWAA2025010884122](https://openairdocs.org/sdr/SWAA2025010884122.md): Lamp · inoperative · Jan 8, 2025 · N428WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY AREA LIGHT AT SEAT 16DEF INOP<[01] RELAMPED EMERGENCY AREA LIGHT AT SEAT 16DEF IAW AMM 33-51-03. OP?S CHECK GOOD.
- [SDR SWAA2025010884120](https://openairdocs.org/sdr/SWAA2025010884120.md): Power Supply · inoperative · Jan 8, 2025 · N428WN · Boeing 7377H4 · Emergency Lighting
  > R2 DOOR EMERGENCY SLIDE LIGHT INOP<[01] REMOVED AND REPLACED AFT R/H EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2025010884119](https://openairdocs.org/sdr/SWAA2025010884119.md): Skin · delaminated · Jan 8, 2025 · N428WN · Boeing 7377H4 · Trailing Edge Flaps
  > RIGHT INBD MAIN FLAP LOWER SKIN O/B END OF TRAILING EDGE, AREA OF DELAMINATION. REMOVED SECTION OF DISBONDED LOWER SKIN; PREPPED AREA; APPLIED BOEGEL; BOND PRIMER; LAYED UP REPAIR PARTS AND STARTED CURE PER SRM 57-53-01-2R-7. PERMANENT REPAIR ACCOMPLISHED P
- [SDR SWAA2024082226940](https://openairdocs.org/sdr/SWAA2024082226940.md): Seat Back · misconfigured · Aug 16, 2024 · N428WN · Boeing 7377H4 · Passenger Compartment Equipment
  > ROW 10 A B & C RECLINES INTO EXIT ROW.<[01] ADJUSTED CENTER BOLT TO CORRECT BREAKOVER FORCE IN REFERENCE TO CMM 25-21-42.;[02] CORRECTION: ADJUSTED CENTER BOLT TO CORRECT BREAKOVER FORCE IN REFERENCE TO CMM 25-21-42.<BR>TOOL USED: B/C: 162016 DUE:07/11/2025.;[
- [SDR SWAA2024082322329](https://openairdocs.org/sdr/SWAA2024082322329.md): Skin · cracked · Aug 3, 2024 · N428WN · Boeing 7377H4 · Leading Edge Devices
  > R/W SLAT #5 NOSE SKIN CRACK FOUND AT FWD O/B COUNTERSUNK HOLE AT ACTUATOR FITTING<[01] FABRICATED AND INSTALLED FREEZE PLUG AT REWORKED FASTENER HOLE ON RT WING SLAT #5 NOSE SKIN PER REF. SRM 51-20-10-0G-0 AND SRM 57-42-01-2R-8; WORK ACCOMPLISHED BY SUBCONTRAC
- [SDR SWAA2024082220027](https://openairdocs.org/sdr/SWAA2024082220027.md): Connector · damaged · Jul 30, 2024 · N428WN · Boeing 7377H4 · Light System Wiring
  > EMERGENCY LIGHT L/H AFT OF WING CONNECTOR WILL NOT CORRECTLY LOCK<[01] REMOVED AND REPLACED CONNECTOR I/A/W BOEING SWPM 20-61-17 & WDM 33-51-14; OPS CHECK PERFORMED I/A/W BOEING AMM 33-51-00-710-801; OPS CHECK NORMAL;[02] VERIFIED STEP 1
- [SDR SWAA2024082220016](https://openairdocs.org/sdr/SWAA2024082220016.md): Connector · damaged · Jul 30, 2024 · N428WN · Boeing 7377H4 · Light System Wiring
  > EMERGENCY LIGHT R/H AFT OF WING CONNECTOR WILL NOT CORRECTLY LOCK<[01] REMOVED AND REPLACED CONNECTOR I/A/W BOEING SWPM 20-61-17 & WDM 33-51-14; OPS CHECK PERFORMED I/A/W BOEING AMM 33-51-00-710-801; OPS CHECK NORMAL;[02] VERIFIED STEP 1
- [SDR SWAA2024082219685](https://openairdocs.org/sdr/SWAA2024082219685.md): Floorbeam · cracked · Jul 30, 2024 · N428WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CABIN FLOOR CROSS SECTIONAL MEMBER AT LOCATION STA 537.45 LBL 45.5 TO LBL 63 WITH CRACKED CORNER.<[01] REMOVED AND REPLACED CABIN FLOOR SECTIONAL MEMBER AT LOCATION STA 537.45 LBL 45.5 TO LBL 63 PER REF. SRM 51-0-02-0G-0 AND DWG143A5240;[02] VERIFIED STEP # 1
- [SDR SWAA2024082221618](https://openairdocs.org/sdr/SWAA2024082221618.md): Console · cracked · Jul 29, 2024 · N428WN · Boeing 7377H4 · Fuselage Main, Structure
  > FLIGHT COMPARTMENT RIGHT SIDE CONSOLE PANEL#212FW LOWER SURFACE HAS EVIDENCE OF A CRACK.<[01] APPLIED REPAIR ON PANEL #212FW AT DAMAGED AREA PER B737 AMM 25-00-00-340-801 PARAGRAPH 8.E.(3). MATERIALS USED RESIN P/O#2039827; CLOTH P/O#1738579;[02] VERIFIED STEP
- [SDR SWAA2024082218509](https://openairdocs.org/sdr/SWAA2024082218509.md): Strut · cracked · Jul 28, 2024 · N428WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN CUSP WEB INNER CHORD CRACKED AT STA. 616 AND LBL 63<[01] REMOVED AND REPLACED MAIN CABIN CUSP INNER CHORD BETWEEN STA 688 TO STA 540 AND LBL 63 IN REF BOEING DRAWING 144A5901 AND SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED MAIN CABIN CUSP INNER CHO
- [SDR SWAA2024082218510](https://openairdocs.org/sdr/SWAA2024082218510.md): Cusp Web · cracked · Jul 28, 2024 · N428WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN CUSP WEB INNER CHORD CRACKED AT STA. 639 AND LBL 63<[01] REPLACEMENT OF INNER CHORD WILL BE ACCOMPLISHED ON (TTG8Q00UVUNH);[02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2024082318157](https://openairdocs.org/sdr/SWAA2024082318157.md): Retainer · cracked · Jul 27, 2024 · N428WN · Boeing 7377H4 · Spoilers
  > LEFT WING OF#6 SPOILER UNDER FIXED T/E PANEL SEAL RETAINER CRACKED<[01] REMOVED AND REPLACED BRACKET AT LT. WING T/E PANEL PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 1
- [SDR SWAA2024082218160](https://openairdocs.org/sdr/SWAA2024082218160.md): Floor Panel · frayed · Jul 27, 2024 · N428WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PNL 242CF UPPER SURFACE FIBERS FRAYED AND PNL PUNCTURED<[01] REPLACED CABIN FLOOR PANEL 242CF WORK TO BE COMPLETED ON CUSTOMER WORK CARD TTG8Q00TTZWE;[02] REMOVED AND REPLACED CABIN FLOOR PANEL 242CF ASPER AMM 53-21-00-000-801 AND AMM 53-21-00-400-
- [SDR SWAA2024082218161](https://openairdocs.org/sdr/SWAA2024082218161.md): Floor Panel · damaged · Jul 27, 2024 · N428WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241DF UPPER SURFACE FIBERS FRAYED<[01] RECEIVED; LOCATED MATERAL PN.4417A4400001CC-10 AD FABRICATED NEW FLOR PANEL 241DF. REF. DWG. 144A5810;[02] RECEIVED; LOCATED AND DRILLED BOARD PN.4417A4400001CC-10 AND FABRICATED NEW FLOOR PANEL 241DF. R
- [SDR SWAA2024082218150](https://openairdocs.org/sdr/SWAA2024082218150.md): Floor Panel · deformed · Jul 26, 2024 · N428WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOOR PANEL 140AF IS WAVY. DOT 102-008<[01] FABRICATED AFT CARGO COMPARTMENT FLOOR PANEL 140AF;PER REF AMM25-52-01-201-801;[02] VERIFIED STEP#1
- [SDR SWAA2024082218151](https://openairdocs.org/sdr/SWAA2024082218151.md): Floor Panel · deformed · Jul 26, 2024 · N428WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOOR PANEL 140BF IS WAVY. DOT 102-009<[01] FABRICATED NEW AFT CARGO COMP. FLOOR PANEL 140BF PER REF. AMM 25-52-01-201-801.;[02] VERIFIED FLOOR PANEL FABRICATION.
- [SDR SWAA2024082218149](https://openairdocs.org/sdr/SWAA2024082218149.md): Floor Panel · delaminated · Jul 26, 2024 · N428WN · Boeing 7377H4 · Fuselage Floor Panel
  > MID CABIN FLOOR PNL 241AF SURFACE LAMINATED DAMAGED<[01] FABRICATED MAIN CABIN FLOORBOARD 241AF PER SRM DWG 144A5810 AND SRM 51-40-05-0G-0;[02] VERIFIED STEP 1
- [SDR SWAA2024082317426](https://openairdocs.org/sdr/SWAA2024082317426.md): Skin · pulled · Jul 25, 2024 · N428WN · Boeing 7377H4 · Leading Edge Devices
  > RIGHT WING # 8 SLAT ACTUATOR LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR HAS FOUR FASTENERS( 04)PULLED IN;EVIDENCE OF NICKS AROUND HOLE EDGE.<[01] REMOVED AND REPLACED RIGHT WING L/E # 8 SLAT IN REFERENCE AMM 27-81-21-000-801 AND AMM 27-81-21-400-801.;
- [SDR SWAA2024082316791](https://openairdocs.org/sdr/SWAA2024082316791.md): Skin · pulled · Jul 25, 2024 · N428WN · Boeing 7377H4 · Leading Edge Devices
  > LEFT WING # 1 SLAT ACTUATOR;LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR HAS SIX(06) FASTENERS PULLED IN.<[01] REMOVED AND REPLACED LEFT WING #1 L/E SLAT IN REFERENCE AMM 27-81-21-000-801 AND AMM 27-81-21-400-801.;[02] VERIFIED STEP # 1
- [SDR SWAA2024082317424](https://openairdocs.org/sdr/SWAA2024082317424.md): Doubler · pulled · Jul 25, 2024 · N428WN · Boeing 7377H4 · Leading Edge Devices
  > RIGHT WING # 5 SLAT ACTUATOR;LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR HAS FOUR(04) FASTENERS PULLED IN.<[01] INSTALLED EXTERNAL DOUBLER REPAIR AT#5 SLAT LOWER SURFACE L/E NOSE SKIN ACTUATOR ATTACHING AREA. REF SRM 57-42-01-2R-8 FIG 202.;[02] VERIFI
- [SDR SWAA2024082217425](https://openairdocs.org/sdr/SWAA2024082217425.md): Skin · pulled · Jul 25, 2024 · N428WN · Boeing 7377H4 · Leading Edge Devices
  > RIGHT WING # 6 SLAT ACTUATOR;LOWER SURFACE OF THE L/E NOSE SKIN AT ACTUATOR HAS FOUR(4) FASTENERS PULLED IN AND ONE(1) PULLED OUT.<[01] CUT AND REMOVED DAMAGED AT SLAT NOSE SKIN FABRICATED REPAIRS PARTS DOUBLER AND FILLER MATERIAL USEDLER FOR DOUBLER 7075 T62
- [SDR SWAA2024070106021](https://openairdocs.org/sdr/SWAA2024070106021.md): Flap Track · excess play · Jun 27, 2024 · N428WN · Boeing 7377H4 · Trailing Edge Flaps
  > L/H WING I/B FLAP O/B AFT FLAP TRACK HAS EXCESSIVE PLAY<[01] 01 - REMOVED AND REPLACED INBD AFT FLAP OUTBD TRACK PER [AMM 27-51-16-401-NG (INBOARD AFT FLAP TRACKS - REMOVAL/INSTALLATION - PERMANENT)]
- [SDR SWAA2024062706015](https://openairdocs.org/sdr/SWAA2024062706015.md): Battery Pack · no test · Jun 27, 2024 · N428WN · Boeing 7377H4 · Emergency Lighting
  > EMX BATTERY PACK M01673 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01673 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024062706009](https://openairdocs.org/sdr/SWAA2024062706009.md): Battery Pack · no test · Jun 27, 2024 · N428WN · Boeing 7377H4 · Emergency Lighting
  > EMX BATTERY PACK M01674 FAILS CAPACITANCE CHECK. REMOVED AND REPLACED EMX BATTERY PACK M01674 PER AMM 33-51-06-960-805-NG
- [SDR SWAA2023101109062](https://openairdocs.org/sdr/SWAA2023101109062.md): Light · loose · Oct 8, 2023 · N428WN · Boeing 7377H4 · Emergency Lighting
  > HALF OF ROW 15 IN THE ISLE EMERGENCY EXIT SIGN FELL TO THE GROUND DURING LANDING<[01] REINSTALLED MID CABIN EXIT LIGHT ASSY REF AMM 33-51-01. OPS CHECKS GOOD AC OFK FOR SERVICE
- [SDR SWAA2023072581705](https://openairdocs.org/sdr/SWAA2023072581705.md): Sign · out of adjust · Jul 24, 2023 · N428WN · Boeing 7377H4 · Emergency Lighting
  > LIGHTED EXIT SIGN NEXT TO FWD FA JUMPSEAT COVER FELL OFF<[01] INSTALLED NEW EMERGENCY EXIT SIGN COVER NEXT TO FWD FA JUMPSEAT. WORK DONE PER AMM 33-51-01. OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2023050443449](https://openairdocs.org/sdr/SWAA2023050443449.md): Slide · out of adjust · Apr 30, 2023 · N428WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE COMING OUT ON BOTTOM<[01] PERFORMED GVI OF FWD ENTRY DOOR SLIDE. NO DEFECTS NOTED PER AMM 25-66-00
- [SDR SWAA2023031313990](https://openairdocs.org/sdr/SWAA2023031313990.md): Seal · cracked · Mar 9, 2023 · N428WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LT LOWER HORZ. STAB SLIDER SEAL CRACKED<[01] REMOVED AND REPLACED SLIDING SEAL PER AMM 53-31-31.;[02] REMOVED AND REPLACED SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2022111570455](https://openairdocs.org/sdr/SWAA2022111570455.md): Lens · missing · Nov 12, 2022 · N428WN · Boeing 7377H4 · Emergency Lighting
  > R/H OVERWING EXIT LIGHT MISSING LENS / [01] INSTALLED A NEW EXIT LIGHT LENS ON THE R/H OVERWING EXIT REF AMM 33-51-01
- [SDR SWAA2022102061446](https://openairdocs.org/sdr/SWAA2022102061446.md): Battery · inoperative · Oct 19, 2022 · N428WN · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY EMERGENCY SLIDE LIGHT INOP / [01] R AND R M1675 CHARGING BASE AND BATTERY PACK AND OPS CK OK REF AMM 33-51-06
- [SDR SWAA2022072931996](https://openairdocs.org/sdr/SWAA2022072931996.md): Fuse · defective · Jul 21, 2022 · N428WN · Boeing 7377H4 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOP THROUGH OUT CABIN AREA. / [01] RELAMPED AREA LIGHT AT SEAT 9 DEF AS PER REF. AMM 33-51-03-960-803. PERFORMED OPS CHECK AND FOUND NORMAL;[02] DURING TROUBLESHOOTING FOUND DEFECTIVE BATTERY PACK POS. M1674 AND BATTERY PACK AND CHARG
- [SDR SWAA2022072830652](https://openairdocs.org/sdr/SWAA2022072830652.md): Light · broken · Jul 18, 2022 · N428WN · Boeing 7377H4 · Passenger Compartment Equipment
  > EMERGENCY EXIT DOOR EXIT SIGN INDICATOR BROKEN AT R/H SIDE. / [01] REPLACED EMERGENCY EXIT DOOR EXIT SIGN INDICATOR AT R/H SIDE IN REF B737-700 AMM 33-51-01-960-802;[02] VERIFIED REPLACEMENT AND TEST
- [SDR SWAA2022072928610](https://openairdocs.org/sdr/SWAA2022072928610.md): Light · broken · Jul 13, 2022 · N428WN · Boeing 7377H4 · Emergency Lighting
  > R-2 DOOR HEADER PANEL EXIT SIGN ASSY BROKEN / [01] REMOVED AND REPLACED EXIT SIGN LIGHT ASSEMBLY AT R-2 DOOR HEADER PANEL. REF. BOEING 737-700 AMM 33-51-01-960-802.;[02] TRANSITION PART ONLY;[03] VERIFIED STEPS: 1 AND 2.
- [SDR SWAA2022072928611](https://openairdocs.org/sdr/SWAA2022072928611.md): Sign · broken · Jul 13, 2022 · N428WN · Boeing 7377H4 · Emergency Lighting
  > L-2 DOOR HEADER PANEL EXIT SIGN ASSY BROKEN / [01] REPLACED L-2 DOOR HEADER PANEL EXIT SIGN ASSY IN REF B 737-700 AMM 33-51-01-960-802;[02] ACCOMPLISHED PART TRANSACTION;[03] VERIFIED REPLACEMENT AND TEST
- [SDR SWAA2022072928609](https://openairdocs.org/sdr/SWAA2022072928609.md): Light · broken · Jul 13, 2022 · N428WN · Boeing 7377H4 · Emergency Lighting
  > AFT CABIN LOWERED CEILING PANELS EXIT SIGN ASSY BROKEN. / [01] REMOVED AND REPLACED EXIT SIGN LIGHT ASSEMBLY AT AFT CABIN LOWERED CEILING PANEL. REF. BOEING 737-700 AMM 33-51-01-960-802.;[02] VERIFIED STEP 1.
- [SDR SWAA2022072924961](https://openairdocs.org/sdr/SWAA2022072924961.md): Rib · cracked · Jul 1, 2022 · N428WN · Boeing 7377H4 · Vertical Stabilizer, Spar/Rib
  > VERTICAL FIN LEADING EDGE RIB #15 CRACKED / [01] EVALUATED CRACK AT VERTICAL FIN L/E RIB #15 FOUND OUT OF LIMITS NO CRACKS ALLOWED IAW B 737-7 SRM 55-30-09-1A-1;[02] FABRICATED NEW VERTICAL FIN RIB IAW B 737-7 SRM 55-30-09-01-1 DWG.176A1410 ID 0002 REV:D;[03]
- [SDR SWAA2022072924039](https://openairdocs.org/sdr/SWAA2022072924039.md): Rib · cracked · Jun 28, 2022 · N428WN · Boeing 7377H4 · Wing, Rib/Bulkhead
  > LH L/E #3 RIB - CRACKED AT BOTH ENDS BY FASTENER HOLE / [01] REMOVED #3 RIB AT L/H L/E IAW B737 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW RIB AT L/H L/E IAW B737 SRM 51-40-05-0G-0.;[03] VERIFIED AMT STEPS 1 AND 2 OK TO INSTALL.;[04] INSTALLED #3 RIB AT L
- [SDR SWAA2022072922423](https://openairdocs.org/sdr/SWAA2022072922423.md): Floor Panel · elongated · Jun 24, 2022 · N428WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOOR PANEL 140AF HAS ELONGATED HOLES / [01] REPLACE FLOOR PANEL 140AF AS PER B737-700 AMM 25-52-01-201.;[02] VERIFIED STEP 1
- [SDR SWAA2022072922424](https://openairdocs.org/sdr/SWAA2022072922424.md): Floor Panel · elongated · Jun 24, 2022 · N428WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOOR PANEL 140DF HAS ELONGATED HOLES / [01] REPLACE FLOOR PANEL 140 DF AS PER B737-700 AMM 25-52-01-201.;[02] VERIFIED STEP 1

Next page: https://openairdocs.org/aircraft/N428WN/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 = 'N428WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N428WN/reports

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