# Service difficulty reports: N8639B

A list on [N8639B](https://openairdocs.org/aircraft/N8639B.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 3 · 130 reports

- [SDR SWAA2026051296809](https://openairdocs.org/sdr/SWAA2026051296809.md): Charger · faulted · May 8, 2026 · N8639B · Boeing 7378H4 · Emergency Lighting
  > L/H SIDE OVER WING EMERGENCY EXIT SIGN LIGHTS INOP FOR BOTH DOORS AND FWD LOWER LIGHT. LIGHTS GO OUT AFTER 1 MIN OR LESS. REMOVED AND INSTALLED BATTERY PACK (M1668) IAW AMM 33-51-06-960-805 AND REMOVED AND INSTALLED BATTERY CHARGER (M1668) IAW AMM 33-51-06-9
- [SDR SWAA2026051296808](https://openairdocs.org/sdr/SWAA2026051296808.md): Light · inoperative · May 8, 2026 · N8639B · Boeing 7378H4 · Emergency Lighting
  > RIGHT SIDE EMERGENCY EXIT FWD DOOR LOWER LIGHT INOPERATIVE. FAULT WAS CORRECTED ON CCN: TTG8Q01C39LA.
- [SDR SWAA2026051295145](https://openairdocs.org/sdr/SWAA2026051295145.md): Lamp · inoperative · May 4, 2026 · N8639B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT L1359 IS INOPERATIVE. RELAMPED AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY EXIT LIGHT L1359 IAW AMM 33-51-01-960-801.
- [SDR SWAA2026051295146](https://openairdocs.org/sdr/SWAA2026051295146.md): Power Supply · inoperative · May 4, 2026 · N8639B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS L1188 AND L1189 ARE INOPERATIVE. REMOVED AND REPLACED M1695 POWER SUPPLY AND PERFORMED GOOD FUNCTIONAL CHECK ON LIGHTS L1188 AND L1189 IAW AMM 33-51-06-960-806.;
- [SDR SWAA2026051295147](https://openairdocs.org/sdr/SWAA2026051295147.md): Power Supply · inoperative · May 4, 2026 · N8639B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS L1207 AND L1208 ARE INOPERATIVE. REMOVED AND REPLACED M1694 POWER SUPPLY AND PERFORMED GOOD FUNCTIONAL CHECK ON LIGHTS L1207 & L1208 IAW AMM 33-51-06-960-806.
- [SDR SWAA2026051295284](https://openairdocs.org/sdr/SWAA2026051295284.md): Bulb · inoperative · May 4, 2026 · N8639B · Boeing 7378H4 · Emergency Lighting
  > LEFT ESCAPE SLIDE AFT L732 INOPERATIVE. REPLACED LIGHT BULB L732 ON LEFT ESCAPE SLIDE AFT AND PERFORMED GOOD FUNCTIONAL TEST IAW 33-51-04-960-801.
- [SDR SWAA2026051292705](https://openairdocs.org/sdr/SWAA2026051292705.md): Elec Connector · broken · Apr 24, 2026 · N8639B · Boeing 7378H4 · Light System Wiring
  > FWD R/H OVERWING EXIT DOOR PANEL ABOVE HAS BROKEN CONNECTOR. REMOVED AND REPLACED R/H FWD OVERWING LIGHT ASSEMBLY M2837 PER AMM 33-21-00-960-805 STEPS 10A THROUGH 10C(6).
- [SDR SWAA2026051289434](https://openairdocs.org/sdr/SWAA2026051289434.md): Floor Panel · pulled · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 231LF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL 231LF IAW SRM 53-00-50-2R-0 AND DWG 143A5810.
- [SDR SWAA2026051289440](https://openairdocs.org/sdr/SWAA2026051289440.md): Floor Panel · pulled · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 241MF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241MF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 146A5810 ID:0456.
- [SDR SWAA2026051289441](https://openairdocs.org/sdr/SWAA2026051289441.md): Floor Panel · pulled · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 241RF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACEMENT FLOOR PANEL 241RF WAS FABRICATED DUE TO EXTENSIVE DAMGE TO UPPER SKIN IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026051289442](https://openairdocs.org/sdr/SWAA2026051289442.md): Floor Panel · pulled · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241UF; WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026051289435](https://openairdocs.org/sdr/SWAA2026051289435.md): Floor Panel · pulled · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 231NF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL 231NF IAW SRM 53-00-50-2R-0 AND BOEING DWG 143A5810.
- [SDR SWAA2026051289451](https://openairdocs.org/sdr/SWAA2026051289451.md): Attach Angle · cracked · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > WASTE COMPARTMENT BULKHEAD SUPPORT LOWER ATTACH ANGLE IS CRACKED AT STA 847+18.5; WL 166; LBL 10. REMOVED AND REPLACED WASTE COMPARTMENT BULKHEAD SUPPORT LOWER ATTACH ANGLE IAW B737-800 SRM 51-40-02-0G-0 AND DWG:149A8102 ID:0019 REV: A.
- [SDR SWAA2026051289455](https://openairdocs.org/sdr/SWAA2026051289455.md): Floor Panel · pulled · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221BF UPPER SKIN AT I/B AFT CORNER HAS AREA OF PULLED STRANDS. FWD FLOOR PANEL 221BF HAD PULLED STRANS ON UPPER SKIN AT I/B AFT CORNER AREA REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026051289463](https://openairdocs.org/sdr/SWAA2026051289463.md): Support Angle · corroded · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT ANGLE FROM STA 500A TO 500E+12; 500G+16; 500H+2; 500H+11; AND 500H+15; RBL 22; WL 158. REMOVED AND REPLACED ON FWD CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT IAW B737-800 SRM 51-40-02-0G-0
- [SDR SWAA2026051289622](https://openairdocs.org/sdr/SWAA2026051289622.md): Frame · cracked · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Main, Frame
  > BS 312 FRAME UPPER ANGLE CRACKED AT LBL33 BETWEEN S-5L AND S-6L. REPAIRED PER EA# M-22-153-01244.
- [SDR SWAA2026051289448](https://openairdocs.org/sdr/SWAA2026051289448.md): Threshold Web · corroded · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT DOOR CUT-OUT SUB-THRESHOLD WEB CORRODED FROM STA 787+9 TO STA 827+15; RBL 21 TO RBL 28; WL 156. REMOVED AND REPLACED SUB-THRESHOLD WEB AT BS 787+7 TO BS 847 RBL 24 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 146A8120 REV A.
- [SDR SWAA2026051289449](https://openairdocs.org/sdr/SWAA2026051289449.md): Shield · corroded · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT DOOR CUT-OUT FWD SHIELD AT STA 767+3 AND 767+7; RBL 24; WL 157. REMOVED AND REPLACED AFT CARGO COMPARTMENT DOOR CUT-OUT FWD SHIELD IAW SRM 51-40-02-0G-0 AND DWG:146A0081, REV A.
- [SDR SWAA2026051289465](https://openairdocs.org/sdr/SWAA2026051289465.md): Threshold Web · corroded · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO DOOR CUT-OUT SUB-THRESHOLD WEB FROM 440+7 TO 480+5; RBL 27 TO RBL 29; WL 156. REMOVED AND REPLACED NEW SUB THRESHOLD WEB FCB RBL 27 WL156 IAW SRM 51-40-02 AND DWG 143A8122 REV. D.
- [SDR SWAA2026051289623](https://openairdocs.org/sdr/SWAA2026051289623.md): Crossbeam · cracked · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Main, Structure
  > PANEL BREAK AT BS 540 CRACKED AT RBL2 WL208. REMOVED AND REPLACED PANEL BREAK AT PASSENGER BS540 RBL2, WL 208 IAW SRM 51-40-02 AND DWG 143A0060.
- [SDR SWAA2026051289624](https://openairdocs.org/sdr/SWAA2026051289624.md): Crossbeam · cracked · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Main, Structure
  > PANEL BREAK AT BS 540 CRACKED AT LBL2 WL208. REMOVED AND REPLACED PANEL BREAK AT PASSENGER BS 540, LBL 2 IAW SRM 51-40-02 AND DWG 143A0060.
- [SDR SWAA2026051289443](https://openairdocs.org/sdr/SWAA2026051289443.md): Sidewall Support · corroded · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON R/H FLOOR TO SIDEWALL SUPPORT AT: STA 727D+5; 727D+6. M727G+6; 727H+9; AND 727I TO 767; RBL 22; WL 156. REMOVED AND REPLACED NEW A.C.B. FLOOR TO SIDEWALL SUPPORT P/N 146A7502-52 LOT# 1583396-1 AT BS727 - BS767 RBL22 WL156 PER SRM 51-40-02 AND DW
- [SDR SWAA2026051289823](https://openairdocs.org/sdr/SWAA2026051289823.md): Floorbeam · corroded · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON BS 328 FLOORBEAM UPPER FLANGE AT NUTPLATE HOLE RBL 56, WL 208. REPAIRED BS 328 FLOORBEAM UPPER FLANGE.
- [SDR SWAA2026051189464](https://openairdocs.org/sdr/SWAA2026051189464.md): Support Angle · corroded · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT LT FLOOR TO SIDEWALL SUPPORT ANGLE FROM STA 500B+6 TO STA 500I; AND STA 400+11; LBL 22; WL 158. THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550.
- [SDR SWAA2026051189822](https://openairdocs.org/sdr/SWAA2026051189822.md): Floorbeam · corroded · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON BS328 FLOORBEAM UPPER FLANGE AT NUTPLATE HOLE RBL40; WL208. REPAIRED BS 328 FLOORBEAM UPPER FLANGE R/H SIDE ON FAULT [TTG8Q01BPT65]
- [SDR SWAA2026051189824](https://openairdocs.org/sdr/SWAA2026051189824.md): Floorbeam · corroded · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON BS328 FLOOR BEAM UPPER FLANGE AT RBL42; WL208. REPAIRED BS 328 FLOOR BEAM UPPER FLANGE R/H SIDE; APPLIED A FILLET SEAL AND CIC TO THE REPAIR AREA IAW SRM 53-10-51-2R-7 REPAIR 7.
- [SDR SWAA2026051189436](https://openairdocs.org/sdr/SWAA2026051189436.md): Floor Panel · pulled · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 231PF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL 231PF IAW SRM 53-00-50-2R-0 AND BOEING DWG 143A5810.
- [SDR SWAA2026051189437](https://openairdocs.org/sdr/SWAA2026051189437.md): Floor Panel · pulled · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 232HF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 232HF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGED.
- [SDR SWAA2026051189438](https://openairdocs.org/sdr/SWAA2026051189438.md): Floor Panel · pulled · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 231XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGED.
- [SDR SWAA2026051189439](https://openairdocs.org/sdr/SWAA2026051189439.md): Support · corroded · Apr 15, 2026 · N8639B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON L/H FLOOR TO SIDEWALL SUPPORT AT: 727D+5; 727D+8; 727E+19; 727G+13; AND 727H TO 807; LBL 22; WL 156. REMOVED AND REPLACED L/H FLOOR TO SIDEWALL SUPPORT IAW B737-800 SRM 51-40-02-0G-0 DWG: 146A7500 ID: 0001 REV: B;
- [SDR SWAA2026051289401](https://openairdocs.org/sdr/SWAA2026051289401.md): Support Angle · corroded · Apr 14, 2026 · N8639B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ZEE SUPPORT ANGLE BS986.5+5 RBL36; WL208. REMOVED AND REPLACED ZEE SUPPORT ANGLE BS986.5+5 RBL36; WL208 IAW B737-800 SRM 51-40-02-0G-0 AND DWG:147A5700 ID:0121 REV: A.;
- [SDR SWAA2026051289433](https://openairdocs.org/sdr/SWAA2026051289433.md): Light · damaged · Apr 14, 2026 · N8639B · Boeing 7378H4 · Emergency Lighting
  > PASSENGER CABIN SIDEWALL 232ZLW EMERGENCY EXIT LIGHT ASSEMBLY DAMAGED. INSTALLED PASSENGER CABIN SIDEWALL 232ZLW EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01-960-802. STEP 3. C (10);[02]
- [SDR SWAA2026051189402](https://openairdocs.org/sdr/SWAA2026051189402.md): Floorbeam · corroded · Apr 14, 2026 · N8639B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON BS 986.5 FLOORBEAM UPPER FLANGE AT NUTPLATE HOLE RBL43; WL208. REPAIRED BS 986.5 FLOORBEAM UPPER FLANGE IAW SRM 53-70-51-2R-6. REPAIR 6.
- [SDR SWAA2026051288728](https://openairdocs.org/sdr/SWAA2026051288728.md): Door · out of adjust · Apr 13, 2026 · N8639B · Boeing 7378H4 · Passenger/Crew Doors
  > FED REQUIRES ADJUSTMENTS. PERFORMED AND VERIFIED FED ADJUSTMENT; WARNING AND SYSTEM TEST IAW AMM 52-11-00-820-801; AMM 52-11-00-700-804 AND AMM 52-71-11-820-801. SATISFACTORY ADJUSTMENT AND TEST.
- [SDR SWAA2026051289001](https://openairdocs.org/sdr/SWAA2026051289001.md): Panel · delaminated · Apr 13, 2026 · N8639B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PANEL 194CL HAS DELAMINATION DAMAGE. REPAIRED IAW SRM 51-70-05-2R-2-B00319, REPAIR 2. REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE.
- [SDR SWAA2026051289002](https://openairdocs.org/sdr/SWAA2026051289002.md): Floor Panel · delaminated · Apr 13, 2026 · N8639B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 194CR HAS DELAMINATION DAMAGE. REPAIRED IAW SRM 51-70-05-2R-2-B00319, REPAIR 2. REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE.
- [SDR SWAA2026051288539](https://openairdocs.org/sdr/SWAA2026051288539.md): Tail Cone · cracked · Apr 12, 2026 · N8639B · Boeing 7378H4 · Trailing Edge Flaps
  > NUMBER 3 FLAP TRACK FAIRING TAILCONE 542EB TIP IS CRACKED. DUE TO THE EXTENT OF DAMAGE; REPLACED #3 FLAP TRACK FAIRING TAILCONE 542EB IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 27-51-18-01 ITEM 430.
- [SDR SWAA2026051288257](https://openairdocs.org/sdr/SWAA2026051288257.md): Nonskid · deteriorated · Apr 11, 2026 · N8639B · Boeing 7378H4 · Wing Structure
  > LEFT WING EMERGENCY EXIT WALKWAY REQUIRES TOUCH UP PAINT. APPLIED THE OVERWING EMERGENCY WALKWAY COATING TO LEFT WING EMERGENCY EXIT WALKWAY. IAW AMM 51-21-97-370-802.
- [SDR SWAA2026051288258](https://openairdocs.org/sdr/SWAA2026051288258.md): Nonskid · deteriorated · Apr 11, 2026 · N8639B · Boeing 7378H4 · Wing Structure
  > RIGHT WING EMERGENCY EXIT WALKWAY REQUIRES TOUCH UP PAINT. APPLIED THE OVERWING EMERGENCY WALKWAY COATING TO RIGHT WING EMERGENCY EXIT WALKWAY. IAW AMM 51-21-97-370-802.
- [SDR SWAA2026051289397](https://openairdocs.org/sdr/SWAA2026051289397.md): Scuff Plate · cracked · Apr 11, 2026 · N8639B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ACD AFT CORNER SCUFF PLATE CRACKED. REMOVED AFT CORNER SCUFF PLATE IAW AMM 53-11-02-020-801. REMOVED AND REINSTALLED ACD AFT CORNER SCUFF PLATE IAW AMM 53-11-02-020-801 AND AMM 53-11-02-420-801.
- [SDR SWAA2026031177431](https://openairdocs.org/sdr/SWAA2026031177431.md): Lens · loose · Mar 7, 2026 · N8639B · Boeing 7378H4 · Emergency Lighting
  > LEFT AFT EMERGENCY LIGHT COVER LOOSE. REMOVED AND REPLACED THE LT OVERWING EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01.
- [SDR SWAA2026012662672](https://openairdocs.org/sdr/SWAA2026012662672.md): Bulb · inoperative · Jan 19, 2026 · N8639B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT POS LOCATOR ON G1 HAS INOPERATIVE BULBS. REPLACED THE BULBS. PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.
- [SDR SWAA2025121752194](https://openairdocs.org/sdr/SWAA2025121752194.md): Cover · missing · Dec 14, 2025 · N8639B · Boeing 7378H4 · Emergency Lighting
  > FORWARD CEILING EMERGENCY LIGHT COVER MISSING. INSTALLED FWD EMERGENCY LIGHT COVER IAW AMM 33-51-03
- [SDR SWAA2025081399954](https://openairdocs.org/sdr/SWAA2025081399954.md): Stop · missing · Aug 9, 2025 · N8639B · Boeing 7378H4 · Emergency Equipment
  > FWD ENTRY DOOR GIRT BAR STOP MISSING. INSTALLED FWD ENTRY DOOR SCAPE SLIDE GIRT BAR STOP IAW AMM 25-66-01.
- [SDR SWAA2024112060698](https://openairdocs.org/sdr/SWAA2024112060698.md): Girt Bar · out of adjust · Nov 17, 2024 · N8639B · Boeing 7378H4 · Escape Slide
  > FORWARD ENTRY DOOR ESCAPE SLIDE; BOTH GIRT BAR RETAINING CLIPS LOOSE<[01] RESECURED AND REPLACED MISSING AND LOOSE HARDWARE ON FWD ENTRY DOOR ESCAPE SLIDE GIRT BAR RETAINING CLIPS PER SRM 51-40-02.
- [SDR SWAA2024090935770](https://openairdocs.org/sdr/SWAA2024090935770.md): Gcu · faulted · Sep 4, 2024 · N8639B · Boeing 7378H4 · AC Generator-Alternator
  > DURING CRUISE #2 ENGINE DRIVE LIGHT ILLUMINATED<[01] R&R #2 ENG GCU IAW AMM 24-21-81
- [SDR SWAA2024071911809](https://openairdocs.org/sdr/SWAA2024071911809.md): Battery Pack · inoperative · Jul 12, 2024 · N8639B · Boeing 7378H4 · Emergency Lighting
  > FORWARD ENTRY DOOR EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED FORWARD ENTRY DOOR EMERGENCY LIGHT BATTERY PACK PER MM 33-51-06. OPS CHECKS GOOD PER MM 33-51-00;[02] INSPECTED WORK PERFORMED
- [SDR SWAA2024071911453](https://openairdocs.org/sdr/SWAA2024071911453.md): Panel · cracked · Jul 11, 2024 · N8639B · Boeing 7378H4 · Wing, Plate/Skin
  > L/H WING T.E. FIXED UPPER PANEL ATTACH WEB INBD. OF DEFLECTION CONTROL RIB IS CRACKED.<[01] INSTALLED UPPER AND LOWER FASTENERS IN WEB PER SRM 51-40-02.;[02] VERIFIED INSTALLED UPPER AND LOWER FASTENERS IN WEB PER SRM 51-40-02.;[03] REMOVED AND REPLACED RIB IA
- [SDR SWAA2024071910146](https://openairdocs.org/sdr/SWAA2024071910146.md): Fairing · damaged · Jul 7, 2024 · N8639B · Boeing 7378H4 · Trailing Edge Flaps
  > #6 INBOARD FLAP SUPPORT AFT FAIRING TAIL CONE HAS PULLED FASTENER<[01] REMOVED AND INSTALLED SERVICEABLE RIGHT WING #6 AFT SUPPORT FAIRING TAIL CONE PER. M.M. 27-51-18
- [SDR SWAA2024072209867](https://openairdocs.org/sdr/SWAA2024072209867.md): Plate · corroded · Jul 6, 2024 · N8639B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H SIDEPLATE UPPER SURFACE HAS CORROSION AT N/P HOLES FROM STA 767 TO 787; RBL 21 WL 155.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.035' REMAINING THICKNESS). SIDE PLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED R/H SIDE PLATE STA 7

Next page: https://openairdocs.org/aircraft/N8639B/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 = 'N8639B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8639B/reports

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