# Service difficulty reports: N8659D

A list on [N8659D](https://openairdocs.org/aircraft/N8659D.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 2 · 81 reports

- [SDR SWAA2026100554194](https://openairdocs.org/sdr/SWAA2026100554194.md): Slide · detached · Sep 29, 2026 · N8659D · Boeing 7378H4 · Escape Slide
  > AFT SERVICE DOOR SLIDE FELL OUT OF THE CONTAINER. REINSTALLED R2 DOOR SLIDE IAW MT 725-61-06.
- [SDR SWAA2026021168830](https://openairdocs.org/sdr/SWAA2026021168830.md): Bulb · inoperative · Feb 8, 2026 · N8659D · Boeing 7378H4 · Emergency Lighting
  > AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN BULB INOPERATIVE. REPLACED THE BULB AND PERFORMED A GOOD TEST IAW AMM 33-51-01-960-801.
- [SDR SWAA2026021168829](https://openairdocs.org/sdr/SWAA2026021168829.md): Bulb · inoperative · Feb 8, 2026 · N8659D · Boeing 7378H4 · Emergency Lighting
  > AFT LEFT OVERWING DOOR EMERGENCY EXIT SIGN HAD TWO BULBS INOPERATIVE. REPLACED THE BULB AND PERFORMED A GOOD TEST IAW AMM 33-51-01-960-801.
- [SDR SWAA2026012964546](https://openairdocs.org/sdr/SWAA2026012964546.md): Lens · missing · Jan 26, 2026 · N8659D · Boeing 7378H4 · Emergency Lighting
  > LENS MISSING FROM CEILING LIGHT AT ROW 2 EMERGENCY LIGHT. INSTALLED THE MISSING LENS COVER IAW SIP.
- [SDR SWAA2025111033650](https://openairdocs.org/sdr/SWAA2025111033650.md): Window · failed · Nov 6, 2025 · N8659D · Boeing 7378H4 · Flight Compartment Windows
  > L1 WINDOW OUTER LAYER SHATTERED AT FL350 NO CABIN PRESSURE CHANGES. R & R L1 WINDOW PER AMM 56-11-11 AND WHCU PER AMM 30-41-11. LEAK AND OP CHECKED GOOD.
- [SDR SWAA2025010880115](https://openairdocs.org/sdr/SWAA2025010880115.md): Floorbeam · cracked · Dec 21, 2024 · N8659D · Boeing 7378H4 · Fuselage Main, Floor Beam
  > WING CENTER SECTION FLOOR SUPPORT AT STA 540 LBL1 AND RBL1 HAS CRACK STREAMER ATTACHED. DOT#P862.<[01] REMOVED AND REPLACED FLOOR SUPPORTS PN 143A5240-63 PO#0 AND 143A5240-64 PO#1109294.1 AT STA 540 LBL1 AND RBL1 IAW B737NG-SRM 51-40-02 AND BAC DWG#143A0060 RE
- [SDR SWAA2025010680117](https://openairdocs.org/sdr/SWAA2025010680117.md): Floor Panel · pulled · Dec 21, 2024 · N8659D · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231XF HAS PULLED FIBERS<[01] PREFORMED PERMEANT REPAIR TO MAIN CABIN FLOOR PANEL 231XF PEELING FIBERS IAW B737-800 SRM 53-00-50.;[02] 04 - REPAIRED PER [SRM 53-00-50-2R-0-B00275 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]
- [SDR SWAA2025010680118](https://openairdocs.org/sdr/SWAA2025010680118.md): Floor Panel · pulled · Dec 21, 2024 · N8659D · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231YF HAS PULLED FIBERS<[01] PREFORMED PERMEANT REPAIR TO MAIN CABIN FLOOR PANEL 231YF PEELING FIBERS IAW B737-800 SRM 53-00-50;[02] 04 - REPAIRED PER [SRM 53-00-50-2R-0-B00275 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]
- [SDR SWAA2025010680119](https://openairdocs.org/sdr/SWAA2025010680119.md): Floor Panel · pulled · Dec 21, 2024 · N8659D · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242AF HAS PULLED FIBERS<[01] PREFORMED PERMEANT REPAIR TO MAIN CABIN FLOOR PANEL 242AF PEELING FIBERS IAW B737-800 SRM 53-00-50;[02] 04 - REPAIRED PER [SRM 53-00-50-2R-0-B00275 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]
- [SDR SWAA2025010680120](https://openairdocs.org/sdr/SWAA2025010680120.md): Floor Panel · pulled · Dec 21, 2024 · N8659D · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241AF HAS PULLED FIBERS<[01] PREFORMED PERMEANT REPAIR TO MAIN CABIN FLOOR PANEL 241AF PEELING FIBERS IAW B737-800 SRM 53-00-50;[02] 04 - REPAIRED PER [SRM 53-00-50-2R-0-B00275 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]
- [SDR SWAA2025010680121](https://openairdocs.org/sdr/SWAA2025010680121.md): Floor Panel · pulled · Dec 21, 2024 · N8659D · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241DF HAS PULLED FIBERS<[01] PREFORMED PERMEANT REPAIR TO MAIN CABIN FLOOR PANEL 241DF PEELING FIBERS IAW B737-800 SRM 53-00-50;[02] 04 - REPAIRED PER [SRM 53-00-50-2R-0-B00275 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT).
- [SDR SWAA2025010680122](https://openairdocs.org/sdr/SWAA2025010680122.md): Floor Panel · pulled · Dec 21, 2024 · N8659D · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241BF HAS PULLED FIBERS<[01] PREFORMED PERMEANT REPAIR TO MAIN CABIN FLOOR PANEL 241BF PEELING FIBERS IAW B737-800 SRM 53-00-50;[02] 04 - REPAIRED PER [SRM 53-00-50-2R-0-B00275 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]
- [SDR SWAA2025010879499](https://openairdocs.org/sdr/SWAA2025010879499.md): Bracket · cracked · Dec 20, 2024 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON R/H VAPOR BARRIER LOWER BRACKET @ STA 663.75<[01] REMOVED R/H VAPOR BARRIER ANGLE; LOCATED AND DRILLED NEW VAPOR BARRIER ANGLE; PERFORMED OPEN HOLE HFEC OF AL HOLES IN THE REPAIR AREA USING T8257F CAL DUE 13MAY25 IAW B737 NDTM PT. 6 51-00-00 PRO
- [SDR SWAA2025010879500](https://openairdocs.org/sdr/SWAA2025010879500.md): Angle · cracked · Dec 20, 2024 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > L/H VAPOR LOWER ANGLE BARRIER CRACKS (2) FOUND @ STA 663.75<[01] REMOVED L/H VAPOR BARRIER ANGLE; LOCATED AND DRILLED NEW VAPOR BARRIER ANGLE; PERFORMED OPEN HOLE HFEC OF AL HOLES IN THE REPAIR AREA USING T8257F CAL DUE 13MAY25 IAW B737 NDTM PT. 6 51-00-00 PRO
- [SDR SWAA2025010879484](https://openairdocs.org/sdr/SWAA2025010879484.md): Skin · delaminated · Dec 19, 2024 · N8659D · Boeing 7378H4 · Trailing Edge Flaps
  > R/H WING O/B AFT FLAP DELAMINATED AT THE I/B AFT CORNER.<[01] ACCOMPLISHED TASK CARD R/H WING O/B AFT FLAP DELAMINATED AT THE I/B AFT CORNER. [TTG8Q00XQKUQ].<BR>B737-800 AMM 27-51-22;[02] VERIFIED ACCOMPLISHED TASK CARD R/H WING O/B AFT FLAP DELAMINATED AT THE
- [SDR SWAA2025010879027](https://openairdocs.org/sdr/SWAA2025010879027.md): Vapor Barrier · cracked · Dec 18, 2024 · N8659D · Boeing 7378H4 · Fuselage Main, Bulkhead
  > CR --- ACCOMPLISH GVI OF L/H VAPOR BARRIER ANGLE FOR CRACKS<[01] PERFORMED GVI OF L/H VAPOR BARRIER IAW 51-10-04. CRACKS (2) FOUND AT STATION 663.75;[02] PERFORMED GVI OF L/H VAPOR BARRIER IAW 51-10-04. CRACKS (2) FOUND AT STATION 663.75
- [SDR SWAA2025010879028](https://openairdocs.org/sdr/SWAA2025010879028.md): Vapor Barrier · cracked · Dec 18, 2024 · N8659D · Boeing 7378H4 · Fuselage Main, Bulkhead
  > CR --- ACCOMPLISH GVI OF R/H VAPOR BARRIER ANGLE FOR CRACKS<[01] PERFORMED GVI OF R/H VAPOR BARRIER IAW 51-10-04. CRACK FOUND AT STATION 663.75;[02] PERFORMED GVI OF R/H VAPOR BARRIER IAW 51-10-04. CRACK FOUND AT STATION 663.75
- [SDR SWAA2024120272805](https://openairdocs.org/sdr/SWAA2024120272805.md): Sensor · inoperative · Nov 29, 2024 · N8659D · Boeing 7378H4 · Trailing Edge Flap Control System
  > FLAPS WOULDNT RETRACK TO ZERO 0. FLAPS STAYED AT TWO 2<[01] R&R RIGHT WING FLAP TORQUE TUBE SUPPORT ASSEMBLY PER AMM 27-51-59;[02] R&R #8 FLAP SKEW SENSOR PER AMM 27-59-01
- [SDR SWAA2024102953871](https://openairdocs.org/sdr/SWAA2024102953871.md): Cover · loose · Oct 26, 2024 · N8659D · Boeing 7378H4 · Emergency Lighting
  > EMER EXIT SIGN COVER LOOSE; O'WING EXIT F/O SIDE<[01] INSTALLED COVER AS PER MM 33-51-001
- [SDR SWAA2024091336665](https://openairdocs.org/sdr/SWAA2024091336665.md): Rib · cracked · Sep 12, 2024 · N8659D · Boeing 7378H4 · Wing, Rib/Bulkhead
  > UPPER TAB ON LEFT WING DEFLECTION CONTROL RIB CRACKED/SEPARATED<[01] REMOVED DAMAGE; FLAP PEENED AREA AND TREATED AND PRIMED REF 57-51-02-2R-3.;[02] ACCOMPLISHED REPAIR 3 - LEFT WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB CRACK DAMAGE REP
- [SDR SWAA2024091336664](https://openairdocs.org/sdr/SWAA2024091336664.md): Rib · cracked · Sep 12, 2024 · N8659D · Boeing 7378H4 · Wing, Rib/Bulkhead
  > LEFT WING DEFLECTION CONTROL RIB ATTACHMENT CLIP UNDER FIXED UPPER PANEL CRACKED<[01] REPLACED LEFT WING DEFLECTION CONTROL RIB ATTACHMENT CLIP UNDER FIXED UPPER PANEL PER SRM 51-40-02
- [SDR SWAA2024091336666](https://openairdocs.org/sdr/SWAA2024091336666.md): Bracket · cracked · Sep 12, 2024 · N8659D · Boeing 7378H4 · Wing Miscellaneous Structure
  > LEFT WING PANEL 551GB INBOARD AFT SUPPORT ROD BRACKET CRACKED<[01] 01 - REMOVED AND REPLACED BRACKET PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]
- [SDR SWAA2024083031005](https://openairdocs.org/sdr/SWAA2024083031005.md): Rivet · missing · Aug 27, 2024 · N8659D · Boeing 7378H4 · Emergency Equipment
  > FWD RIGHT SERVICE DOOR GIRT BAR RETAINER CLIP MISSING RIVET<[01] INSTALLED MISSING RIVET REF SRM 51-40-02
- [SDR SWAA2024081927611](https://openairdocs.org/sdr/SWAA2024081927611.md): Girt Bar · loose · Aug 18, 2024 · N8659D · Boeing 7378H4 · Emergency Equipment
  > RT FWD SERVICE DOOR. RT LOWER GRIT BAR SILVER CLIP THAT HOLDS THE GRIT BAR IS LOOSE<[01] PERFORMED REPAIR PER EA-M-23-125-01839 FOR FWD SVC GRIT BAR CLIPS
- [SDR SWAA2024080519893](https://openairdocs.org/sdr/SWAA2024080519893.md): Lens · missing · Jul 30, 2024 · N8659D · Boeing 7378H4 · Emergency Lighting
  > OVERWING EXIT SIGN MISSING COVER ON CEILING<[01] REINSTALLED EXIT LENS REF. AMM 33-51-01. LIGHT FUNCTIONS NML.
- [SDR SWAA2024061300041](https://openairdocs.org/sdr/SWAA2024061300041.md): Light · loose · Jun 9, 2024 · N8659D · Boeing 7378H4 · Emergency Lighting
  > CENTER ISLE PHOTOLUMINESCENT ESCAPE PATH MARKING LOOSE CAPT SIDE BETWEEN ROW 12-13<[01] RESECURED PER AMM 33-51-15
- [SDR SWAA2024031965467](https://openairdocs.org/sdr/SWAA2024031965467.md): Skin · delaminated · Mar 19, 2024 · N8659D · Boeing 7378H4 · Trailing Edge Flaps
  > L/H O/B TRAILING EDGE FLAP REQUIRES REPLACEMENT. REMOVED LH OTBD AFT FLAP IAW AMM 27-51-22. REMOVED AND REPLACED LH OB AFT FLAP PER AMM 27-51-26.
- [SDR SWAA2024031864684](https://openairdocs.org/sdr/SWAA2024031864684.md): Skin · delaminated · Mar 17, 2024 · N8659D · Boeing 7378H4 · Trailing Edge Flaps
  > LH WING OUTBD TRAILING EDGE FLAP IS DELAMINATED AT LOWER INBD END. 17IN X 9IN<[01] CW EA 24-127-00702;[02] CW
- [SDR SWAA2023100403928](https://openairdocs.org/sdr/SWAA2023100403928.md): Slide · low pressure · Sep 25, 2023 · N8659D · Boeing 7378H4 · Escape Slide
  > AFT SERVICE DOOR SLIDE PRESSURE GAUGE OUT OF LIMITS<[01] R&R SLIDE PER AMM 25-66-01 AND TC 725-61-06-AS;[02] INSPECTED THAT SLIDE WAS R&R PER AMM 25-66-01 AND TC 725-61-06-AS
- [SDR SWAA2022120776196](https://openairdocs.org/sdr/SWAA2022120776196.md): Intercostal · out of adjust · Nov 29, 2022 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > SUPPLEMENTAL INFORMATION: REMOVED INTERCOSTAL BETWEEN STA 947 AND 967 AT RBL 51 FOR EVALUATION OF FLOOR PANEL HOLE ALIGNMENT.<[01] INSTALLED NEW INTERCOSTAL BETWEEN STA 947 AND 967 AT RBL 51 PER SRM 51-40-02 AND EA 22-153-03489-WIP1 (TTG8Q00GCT30).;[02] INSPEC
- [SDR SWAA2022120976197](https://openairdocs.org/sdr/SWAA2022120976197.md): Skin · damaged · Nov 29, 2022 · N8659D · Boeing 7378H4 · Leading Edge Devices
  > NR 3 SLAT LEADING EDGE SKIN IS WRINKLED AND BENT AROUND FASTENERS. APROX 6 IN. LONG AND COMMON TO THE INBD MAIN TRACK. REMOVED THE NR 3 LEADING EDGE SLAT AND REPLACED WITH NEW SLAT IAW AMM 27-81-21. INSPECTED THE RIG AND OPS CHECK OF THE NR 3 SLAT.
- [SDR SWAA2022113075863](https://openairdocs.org/sdr/SWAA2022113075863.md): Floorbeam · damaged · Nov 27, 2022 · N8659D · Boeing 7378H4 · Fuselage Main, Floor Beam
  > FLOORBEAM HAS 5 EACH ELONGATED FASTENER HOLES ON UPPER SURFACE. BS 950, RBL 28-46. REMOVED AND REPLACED FLOORBEAM IAW EA 22-153-03502 AND SRM 51-40-02.
- [SDR SWAA2022113071981](https://openairdocs.org/sdr/SWAA2022113071981.md): Battery Pack · weak · Nov 16, 2022 · N8659D · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACKS WEAK. REPLACED THE BATTERY PACKS IAW MM 33-51-06.
- [SDR SWAA2022113069985](https://openairdocs.org/sdr/SWAA2022113069985.md): Angle · corroded · Nov 11, 2022 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BS 490-500A, RT TRANSITION ANGLE CORRODED AROUND NUT-PLATE HOLES. REMOVED SURFACE CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR SWAA2022113069987](https://openairdocs.org/sdr/SWAA2022113069987.md): Angle · corroded · Nov 11, 2022 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BS 500B-500D, RT TRANSITION ANGLE CORRODED AROUND NUT-PLATE HOLES. REMOVED SURFACE CORROSION AND FOUND TO BE OUT OF LIMITS. REPLACED THE ANGLE IAW SRM 53-00-53-1A-2.
- [SDR SWAA2022113069997](https://openairdocs.org/sdr/SWAA2022113069997.md): Angle · corroded · Nov 11, 2022 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BS 500D-500F, RT TRANSITION ANGLE CORRODED AROUND NUT-PLATE HOLES. REMOVED SURFACE CORROSION AND FOUND TO BE OUT OF LIMITS.
- [SDR SWAA2022113069999](https://openairdocs.org/sdr/SWAA2022113069999.md): Angle · corroded · Nov 11, 2022 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BS 500F-500I, RT TRANSITION ANGLE CORRODED AROUND NUT-PLATE HOLES. REMOVED SURFACE CORROSION AND FOUND TO BE OUT OF LIMITED. LOCATED AND DRILLED A NEW RH TRANSITION ANGLE IAW SRM 51-40-02. INSTALLED THE NEW TRANSITION ANGLE IAW SRM 51-40-02.
- [SDR SWAA2022120769957](https://openairdocs.org/sdr/SWAA2022120769957.md): Angle · corroded · Nov 10, 2022 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RT SIDE PLATE CHANNEL HAS CORROSION AROUND FASTENER HOLES RBL 21, BS 727G-727H. THE TRANSITION ANGLE TO BE REPLACED ON NR TTG8Q00G0A7F.
- [SDR SWAA2022120769958](https://openairdocs.org/sdr/SWAA2022120769958.md): Angle · corroded · Nov 10, 2022 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RT SIDE PLATE CHANNEL HAD CORROSION AROUND FASTENER HOLES RBL 21, BS 727H-727I. THE RT TRANSITION ANGLE TO BE REPLACED ON NR TTG8Q00G0A7F.
- [SDR SWAA2022120769959](https://openairdocs.org/sdr/SWAA2022120769959.md): Angle · corroded · Nov 10, 2022 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H SIDE PLATE CHANNEL HAS CORROSION AROUND FASTENER HOLES RBL 21; BS 727I-727J. RT TRANSITION ANGLE TO BE REPLACED ON NR TTG8Q00G0A7F.
- [SDR SWAA2022113069956](https://openairdocs.org/sdr/SWAA2022113069956.md): Channel · corroded · Nov 10, 2022 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RT CHANNEL CORRODED AROUND FASTENER HOLES, RBL 21, BS 727F-727G. CHANNEL REPAIRED IAW SRM 53-00-53-2R-5, REPAIR 5, AND EAM-22-153-01550.
- [SDR SWAA2022113069960](https://openairdocs.org/sdr/SWAA2022113069960.md): Channel · corroded · Nov 10, 2022 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RT CHANNEL CORRODED AROUND FASTENER HOLES, RBL 21, BS 747-767. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM.53-00-53-1A-1. LOCATED AND DRILLED A NEW CHANNEL IAW SRM. 53-00-53-2R-5. TREATED AND PRIMED IAW SRM. 51-20-02. INSTALLED THE N
- [SDR SWAA2022113069966](https://openairdocs.org/sdr/SWAA2022113069966.md): Channel · corroded · Nov 10, 2022 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RT CHANNEL CORRODED AROUND FASTENER HOLES, RBL 21, BS 767-787. REMOVED THE CHANNEL DUE TO OUT OF LIMITS IAW SRM 51-40-02. LOCATED AND DRILLED, AND INSTALLED THE NEW CHANNEL IAW SRM 51-10-02.
- [SDR SWAA2022113069943](https://openairdocs.org/sdr/SWAA2022113069943.md): Channel · corroded · Nov 10, 2022 · N8659D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H SIDE PLATE CHANNEL HAS CORROSION AROUND FASTENER HOLES RBL 21; STA 727J-747. RT TRANSITION CHANNEL REPLACED ON NR TTG8Q00G0A7F.
- [SDR SWAA2022113069562](https://openairdocs.org/sdr/SWAA2022113069562.md): Floorbeam · damaged · Nov 9, 2022 · N8659D · Boeing 7378H4 · Fuselage Main, Floor Beam
  > FLOORBEAM BS 967 HAS ELONGATED FASTENER HOLES AT THE THREE MOST O/B HOLES ON R/H SIDE ON UPPER SURFACE.
- [SDR SWAA2022113069556](https://openairdocs.org/sdr/SWAA2022113069556.md): Floorbeam · damaged · Nov 9, 2022 · N8659D · Boeing 7378H4 · Fuselage Main, Floor Beam
  > FLOORBEAM HAS 5 EACH ELONGATED FASTENER HOLES ON UPPER SURFACE, BS 950, RBL 28 - 46. REMOVED FLOORBEAM IAW SRM 51-40-02. LOCATED AND DRILLED A NEW FLOORBEAM IAW SRM 51-40-05. INSTALLED THE NEW FLOORBEAM IAW SRM 51-40-02.
- [SDR SWAA2022120769206](https://openairdocs.org/sdr/SWAA2022120769206.md): Handle · loose · Nov 8, 2022 · N8659D · Boeing 7378H4 · Service Doors
  > AFT SERVICE DOOR HANDLE LOOSE AT CAM PLATE SHAFT. SECURED THE HANDLE IAW AMM 20-10-44, AND AMM 52-41-11.
- [SDR SWAA2022113069208](https://openairdocs.org/sdr/SWAA2022113069208.md): Seal · cracked · Nov 8, 2022 · N8659D · Boeing 7378H4 · Horizontal Stabilizer Structure
  > LT. STAB FWD UPPER SLIDING SEAL WORN AND CRACKED. R & R THE SEAL IAW MM 53-31-31.
- [SDR SWAA2022113069207](https://openairdocs.org/sdr/SWAA2022113069207.md): Seal · cracked · Nov 8, 2022 · N8659D · Boeing 7378H4 · Horizontal Stabilizer Structure
  > RT. STAB FWD UPPER SLIDING SEAL CRACKED. MATCH DRILLED AND RIVETED BRACKETS ON NEW SLIDER IAW SRM 51-40-02. REMOVED AND REPLACED R/H UPPER SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2022100552469](https://openairdocs.org/sdr/SWAA2022100552469.md): None · inoperative · Oct 4, 2022 · N8659D · Boeing 7378H4 · Emergency Lighting
  > FWD LH EMERGENCY LIGHTS INOP. / [01] REPLACED FWD LH EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.

Next page: https://openairdocs.org/aircraft/N8659D/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 = 'N8659D' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8659D/reports

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