# Service difficulty reports: N8706W

A list on [N8706W](https://openairdocs.org/aircraft/N8706W.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 · 66 reports

- [SDR SWAA2026090775278](https://openairdocs.org/sdr/SWAA2026090775278.md): Battery · inoperative · Sep 3, 2026 · N8706W · Boeing 7378 · Emergency Equipment
  > TWO FLASHLIGHTS IN AFT GALLEY, INOPERATIVE. R & R THE AFT LT FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHKD GOOD.
- [SDR SWAA2026090851055](https://openairdocs.org/sdr/SWAA2026090851055.md): Flashlight · missing · Sep 2, 2026 · N8706W · Boeing 7378 · Emergency Equipment
  > FLIGHT ATTENDANT FLASHLIGHTS NOT INSTALLED IN FWD FA SEAT. INSTALLED FA FLASHLIGHTS IN FWD SEAT IAW AMM 25-64-00.
- [SDR SWAA2026090889068](https://openairdocs.org/sdr/SWAA2026090889068.md): Elec Connector · unsecure · Aug 30, 2026 · N8706W · Boeing 7378 · Light System Wiring
  > LEFT EMERGENCY LIGHT, SEAT ROW 8 ABC INOPERATIVE. SECURED THE ELECTRICAL CONNECTOR IAW AMM 33-51-03. TESTED GOOD.
- [SDR SWAA2026090418699](https://openairdocs.org/sdr/SWAA2026090418699.md): Battery Pack · inoperative · Aug 29, 2026 · N8706W · Boeing 7378 · Emergency Lighting
  > FWD EMERGENCY POWER PACK (M02816) INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ON POWER PACK AND OP'S CHECK GOOD IAW AMM 33-51-06 AND AMM 33-51-00.
- [SDR SWAA2026090222369](https://openairdocs.org/sdr/SWAA2026090222369.md): Plate · cracked · Aug 14, 2026 · N8706W · Boeing 7378 · Fuselage Miscellaneous Structure
  > FWD CARGO, FWD CORNER PLATE IS CRACKED. FWD CARGO FWD CORNER PLATE IS CRACKED. INSTALLED A NEW FWD CARGO FWD LOWER CORNER PLATE ASSY IAW AMM 53-11-02.
- [SDR SWAA2026081957296](https://openairdocs.org/sdr/SWAA2026081957296.md): Doubler · delaminated · Jul 25, 2026 · N8706W · Boeing 7378 · Fuselage Miscellaneous Structure
  > PAX CABIN RT SIDE, JUST ABOVE THE CREASE BEAMS, 10, BONDED WAFFLE DOUBLERS FACE SHEETS DELAMINATED OR COMPLETELY REMOVED. BS 360 - 500C. REPAIRED THE BONDED WAFFLE DOUBLERS IAW AMM 25-00-00.
- [SDR SWAA2026081913615](https://openairdocs.org/sdr/SWAA2026081913615.md): Doubler · delaminated · Jul 25, 2026 · N8706W · Boeing 7378 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN RT SIDE, JUST ABOVE THE CREASE BEAMS, 8 BONDED WAFFLE DOUBLERS DELAMINATED OR COMPLETELY REMOVED. BS 500C - 540. REPAIRED BONDED THE WAFFLE DOUBLERS IAW AMM 25-00-00.
- [SDR SWAA2026081976130](https://openairdocs.org/sdr/SWAA2026081976130.md): Doubler · delaminated · Jul 25, 2026 · N8706W · Boeing 7378 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN, LEFT SIDE, JUST ABOVE THE CREASE BEAMS, 8 BONDED WAFFLE DOUBLERS, DAMPING ASSY IPC 53-31-51-40. FACE SHEETS DELAMINATED OR COMPLETELY REMOVED. BS 500C - 540. REPAIRED BONDED WAFFLE DOUBLERS FROM BS 500C -540 IAW AMM 25-00-00.
- [SDR SWAA2026081934365](https://openairdocs.org/sdr/SWAA2026081934365.md): Doubler · delaminated · Jul 25, 2026 · N8706W · Boeing 7378 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN, LT SIDE, JUST ABOVE THE CREASE BEAMS, 10, BONDED WAFFLE DOUBLERS FACE SHEETS DELAMINATED OR COMPLETELY REMOVED. BS 360 - 500C. REPAIRED BONDED WAFFLE DOUBLERS FROM BS 360 - 500C IAW AMM 25-00-00.
- [SDR SWAA2026081926013](https://openairdocs.org/sdr/SWAA2026081926013.md): Battery Pack · unsecure · Jul 20, 2026 · N8706W · Boeing 7378 · Emergency Lighting
  > A/C EMERGENCY EXIT LIGHT BATTERY PACK AND ATTACH STRUCTURE MOUNTED AT BS 727C-727D STR 16L NEEDS TO BE CLEANED CLEANED EMERGENCY LIGHT BATTERY PACK AND ATTACH STRUCTURE AT L/H CABIN STA.727C-727D IAW AMM 20-60-02. VERIFIED
- [SDR SWAA2026081916624](https://openairdocs.org/sdr/SWAA2026081916624.md): Battery Pack · dirty · Jul 20, 2026 · N8706W · Boeing 7378 · Emergency Lighting
  > ACFT EMERGENCY EXIT LIGHT BATTERY PACK AND ATTACH STRUCTURE MOUNTED AT BS 727C - 727D, STR 16R NEEDS TO BE CLEANED. CLEANED EMERGENCY EXIT LIGHT BATTERY PACK AND ATTACH STRUCTURE IAW AMM 20-6002.
- [SDR SWAA2026081972545](https://openairdocs.org/sdr/SWAA2026081972545.md): Seat Track · worn · Jul 16, 2026 · N8706W · Boeing 7378 · Fuselage, Seat/Cargo Attach Fittings
  > CAPT. AFT INBD SEAT TRACK UPPER SURFACE WORN. R & R THE SEAT TRACK IAW AMM 25-11-11.
- [SDR SWAA2026081929718](https://openairdocs.org/sdr/SWAA2026081929718.md): Seat Track · worn · Jul 16, 2026 · N8706W · Boeing 7378 · Fuselage, Seat/Cargo Attach Fittings
  > FIRST OFFICER AFT INBD SEAT TRACK UPPER SURFACE WORN. R & R THE SEAT TRACK IAW AMM 25-11-11.
- [SDR SWAA2026090262944](https://openairdocs.org/sdr/SWAA2026090262944.md): Floorbeam · corroded · Jul 14, 2026 · N8706W · Boeing 7378 · Fuselage Main, Floor Beam
  > STA 947 FLOOR BEAM HAS PITTING AND CORROSION AT LBL 51 REMOVED CORROSION ON STA.947 FLOOR BEAM UPPER CHORD AT LBL 51 MEASURED CORROSION REMOVAL TO BE 0.055" DEEP REMAINING THICKNESS IS 0.125" (ORIGINAL THICKNESS IS 0.180") FLOOR BEAM UPPER CHORD IS OUT OF LIMI
- [SDR SWAA2026081950712](https://openairdocs.org/sdr/SWAA2026081950712.md): Floor Support · corroded · Jul 14, 2026 · N8706W · Boeing 7378 · Fuselage Miscellaneous Structure
  > STA 948 INTERCOSTAL THAT ATTACHES AFT OF FLOORBEAM OF 947 AT LBL 51 HAS PITTING AND CORROSION. LOCATED AND DRILLED NEW INTERCOSTAL PER SRM 51-40-05 AND DRAWING 147A5650. INSTALL WILL BE COMPLETED ON TASK CARD TTG8Q01D6ER9 STEP 7. CORROSION OUT OF LIMITS PE
- [SDR SWAA2026081956254](https://openairdocs.org/sdr/SWAA2026081956254.md): Floorbeam · corroded · Jul 14, 2026 · N8706W · Boeing 7378 · Fuselage Main, Floor Beam
  > BS 947 FLOORBEAM HAS PITTING AND CORROSION AT RBL 51. REMOVED CORROSION ON THE FLOORBEAM UPPER TEE, MEASURED CORROSION REMOVAL TO BE 0.070" DEEP REMAINING THICKNESS IS 0.110" (ORIGINAL THICKNESS IS 0.180") THE FLOORBEAM UPPER TEE OUT OF LIMITS IAW SRM 53-70-5
- [SDR SWAA2026081976906](https://openairdocs.org/sdr/SWAA2026081976906.md): Floor Support · cracked · Jul 13, 2026 · N8706W · Boeing 7378 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CRACKED STA 540 AT RBL 1 REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02 AND IPC 53-42-11-66 INSPECTED AS REQUIRED CORRECTIVE ACTION #1
- [SDR SWAA2026081931464](https://openairdocs.org/sdr/SWAA2026081931464.md): Floor Support · cracked · Jul 13, 2026 · N8706W · Boeing 7378 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CRACKED BS 540 AT LBL 1, REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02 AND IPC 53-42-11-66.
- [SDR SWAA2026081990203](https://openairdocs.org/sdr/SWAA2026081990203.md): Seal · cracked · Jul 13, 2026 · N8706W · Boeing 7378 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STAB, FWD UPPER SLIDER SEAL WAS CRACKED. REMOVED THE CRACKED RT HORIZONTAL STAB FWD UPPER SLIDER SEAL IAW AMM 53-31-31. INSTALLED A NEW SLIDER SEAL IAW AMM 53-31-31 OPS AND CLEARANCE CHECK GOOD INSTALLED NEW FWD UPPER SLIDER SEAL IAW AMM 53-
- [SDR SWAA2026081943397](https://openairdocs.org/sdr/SWAA2026081943397.md): Floor Panel · damaged · Jul 12, 2026 · N8706W · Boeing 7378 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241AF HAD AREAS OF EXPOSED FIBERS. REMOVED & REPLACED THE FLOOR PANEL IAW AMM 53-21-00.
- [SDR SWAA2026081940734](https://openairdocs.org/sdr/SWAA2026081940734.md): Floor Panel · damaged · Jul 12, 2026 · N8706W · Boeing 7378 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231XF HAS AREAS OF EXPOSED FIBERS. REMOVED & REPLACED THE FLOOR PANEL 231XF IAW AMM 53-21-00.
- [SDR SWAA2026081915057](https://openairdocs.org/sdr/SWAA2026081915057.md): Attach Angle · cracked · Jul 10, 2026 · N8706W · Boeing 7378 · Fuselage Main, Attach Fittings
  > RIGHT A/C BAY, BS 663, RBL 9 HAD A CRACK IN THE VAPOR BARRIER VERTICAL ATTACH ANGLE, REPAIRS COMPLETED ON EA M-157-01143.
- [SDR SWAA2026081969600](https://openairdocs.org/sdr/SWAA2026081969600.md): Attach Angle · cracked · Jul 10, 2026 · N8706W · Boeing 7378 · Fuselage Main, Attach Fittings
  > LEFT A/C BAY, BS 663, LBL 9 HAD A CRACK IN THE VAPOR BARRIER VERTICAL ATTACH ANGLE. REPAIRS COMPLETED ON EA M-157-01142.
- [SDR SWAA2026062916311](https://openairdocs.org/sdr/SWAA2026062916311.md): Battery · inoperative · Jun 26, 2026 · N8706W · Boeing 7378 · Emergency Equipment
  > FA REPORTS RT AFT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERY IAW AMM 25-64-00.
- [SDR SWAA2026032081279](https://openairdocs.org/sdr/SWAA2026032081279.md): Lens · missing · Mar 18, 2026 · N8706W · Boeing 7378 · Emergency Lighting
  > INSPECTED CABIN AREA, & FOUND ONE CEILING EMERGENCY LIGHT COVER MISSING IN FRONT OF THE LIFE RAFT AT SEAT ROW 21D. COMPLIED WITH EMERGENCY LIGHTS OPS TEST IAW AMM 33-51-00. LIGHTS WORKS NORMAL. DEFERRED LENS COVER. OKAY TO CONTINUE IAW MEL 25-10-014. INSTALL
- [SDR SWAA2026011661805](https://openairdocs.org/sdr/SWAA2026011661805.md): Flashlight · no test · Jan 15, 2026 · N8706W · Boeing 7378 · Emergency Equipment
  > CAPTS SIDE AFT GALLEY I BE FLASHLIGHT WILL NOT TEST. OK TO CONTINUE PER MEL 25-64-02A;EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS. WITH SP 1B & AUTHORIZATION NUMBER 302197. REMOVED AND REPLACED BATTERY PER AMM 25-64-00. OPS CHECK GOOD.
- [SDR SWAA2025080196261](https://openairdocs.org/sdr/SWAA2025080196261.md): Sensor · faulted · Jul 28, 2025 · N8706W · Boeing 7378 · APU Controls
  > APU OVERSPEED FAULT CODE 49-31014. OK TO CONT PER MEL 49-11-01. R & R APU SPEED SENSOR REF AMM 49-61-21.
- [SDR SWAA2025071590687](https://openairdocs.org/sdr/SWAA2025071590687.md): Light · inoperative · Jul 12, 2025 · N8706W · Boeing 7378 · Emergency Lighting
  > FIRST 12-14 OF FLOOR STRIP LIGHTING LEFT SIDE NOT WORKING AIRCRAFT LEFT.<[01] REPLACED PHOTOLUMINESCENT FLOOR STRIP LEFT SIDE REF AMM 33-51-15.
- [SDR SWAA2024102350789](https://openairdocs.org/sdr/SWAA2024102350789.md): Panel · delaminated · Oct 19, 2024 · N8706W · Boeing 7378 · Aerodynamic Fairings
  > PANEL 192BL IS DELAMINATED<[01] R&R PANEL 192BL PER AMM 53-51-21. REFERENCE TTG8Q00W949J
- [SDR SWAA2024102149322](https://openairdocs.org/sdr/SWAA2024102149322.md): Girt Bar · loose · Oct 16, 2024 · N8706W · Boeing 7378 · Emergency Equipment
  > GIRT BAR DROOP ON AFT ENTRY EMERGENCY SLIDE<[01] SECURED GIRT BAR IAW AMM 25-66-01. OK FOR SERVICE.
- [SDR SWAA2024080924379](https://openairdocs.org/sdr/SWAA2024080924379.md): Slide · out of adjust · Aug 8, 2024 · N8706W · Boeing 7378 · Escape Slide
  > EMERGENCY EXIT SLIDE COMING OUT OF HOUSING L2 DOOR<[01] ADJUSTED L2 DOOR SLIDE PER AMM 25-66-01 AND MT 825-PRD-01-01. A/C OK FOR SERVICE.
- [SDR SWAA2024080823467](https://openairdocs.org/sdr/SWAA2024080823467.md): Slide · out of adjust · Aug 7, 2024 · N8706W · Boeing 7378 · Escape Slide
  > AFT SLIDE CAPTAINS SIDE DIFFICULT TO DISARM<[01] REMOVED DEBRIS FROM AFT ENTRY DOOR SLIDE GIRTH BAR AS REQUIRED. NO FURTHER DEFECTS NOTED REFERENCE AMM 25?66-01.
- [SDR SWAA2024080520556](https://openairdocs.org/sdr/SWAA2024080520556.md): Power Supply · inoperative · Jul 31, 2024 · N8706W · Boeing 7378 · Emergency Lighting
  > 4 ABC EMERGENCY CEILING LIGHT AND LEFT FWD EXTERNAL OVERWING EMERGENCY LIGHT INOP DURING EMERGENCY LIGHTS TEST<[01] REMOVED AND REPLACED M2335EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK PER AMM 33-51-06
- [SDR SWAA2024080522722](https://openairdocs.org/sdr/SWAA2024080522722.md): Battery Pack · inoperative · Jul 31, 2024 · N8706W · Boeing 7378 · Emergency Lighting
  > 4 ABC EMERGENCY CEILING LIGHT AND LEFT FWD EXTERNAL OVERWING EMERGENCY LIGHT INOP DURING EMERGENCY LIGHTS TEST<[01] REMOVED AND REPLACED M2335EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK PER AMM 33-51-06
- [SDR SWAA2024020950546](https://openairdocs.org/sdr/SWAA2024020950546.md): Cover · missing · Feb 9, 2024 · N8706W · Boeing 7378 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR RETURN PANEL COVERS MISSING AT 16DEF; 19ABC AND 20DEF<[01] REPLACED SEAT TRACK AT 16DEF 19ABC AND 20DEF AS PER SA-M1023
- [SDR SWAA2023112022504](https://openairdocs.org/sdr/SWAA2023112022504.md): Light · inoperative · Nov 17, 2023 · N8706W · Boeing 7378 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AFT OF R2 DOOR IS INOP.<[01] RELAMPED EXTERIOR EMERGENCY LIGHT AFT OF R2 DOOR. IAW AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2023072179841](https://openairdocs.org/sdr/SWAA2023072179841.md): Battery Pack · inoperative · Jul 18, 2023 · N8706W · Boeing 7378 · Emergency Lighting
  > WHILE TROUBLE SHOOTING EMERGENCY EXIT LIGHTS FOUND EMERGENCY EXIT ISLE LIGHTS OUT AT SEAT ROW 10 AND 14 DEF<[01] REPLACED EMERG LIGHT BATTERY PACK AT STA 500C +7 RIGHT SIDE CABIN BEHIND DADO PANEL IAW 33-51-06-960-802. TESTS GOOD;[02] VERIFIED ITEM 1<BR>C/W
- [SDR SWAA2023072178697](https://openairdocs.org/sdr/SWAA2023072178697.md): Battery Pack · inoperative · Jul 15, 2023 · N8706W · Boeing 7378 · Emergency Lighting
  > AFT GALLEY AREA EMERGENCY EXIT LIGHTS ARE INOP AT M1672<[01] REPLACED EMERGENCY BATTERY PACK IAW AMM 33-51-06-960-802 OPS TEST GOOD FOR BATTERY PACK;[02] VERIFIED STEP 1.<BR>AUDIT C/W.
- [SDR SWAA2023072178700](https://openairdocs.org/sdr/SWAA2023072178700.md): Battery Pack · inoperative · Jul 15, 2023 · N8706W · Boeing 7378 · Emergency Lighting
  > AFT GALLEY AREA EMERGENCY EXIT LIGHTS ARE INOP AT M1673<[01] REPLACED EMERGENCY BATTERY PACK IAW AMM 33-51-06-960-802 OPS TEST GOOD FOR BATTERY PACK;[02] VERIFIED STEP 1.<BR>AUDIT C/W.
- [SDR SWAA2023072178698](https://openairdocs.org/sdr/SWAA2023072178698.md): Battery Pack · inoperative · Jul 15, 2023 · N8706W · Boeing 7378 · Emergency Lighting
  > FWD LH ENTRY AREA EMERGENCY EXIT LIGHTS ARE INOP AT M1675<[01] REMOVED AND REPLACED BATTERY ON POWER SUPPLY M1675 IAW AMM 33-51-06-960-802. EMERGENCY LIGHTS FOR POWER SUPPLY M1675 CHECK GOOD.;[02] VERIFIED STEP 1.<BR>AUDIT C/W.
- [SDR SWAA2023072177057](https://openairdocs.org/sdr/SWAA2023072177057.md): Unknown · corroded · Jul 11, 2023 · N8706W · Boeing 7378 · Fuselage Structure (General)
  > AFT CARGO COMPARTMENT; FWD L/H #3 CAPSTRIP HAS CORROSION ON LOWER SURFACE AFT CARGO COMPARTMENT FWD L/H #3 CAPSTRIP HAS CORROSION ON LOWER SURFACE<[01] REMOVED AND INSTALLED NEW CAP STRIP P/N 453A2611-10 A TAG A194733 IAW SRM 51-40-02;[02] VERIFIED ITEM 1<BR>C
- [SDR SWAA2023072176388](https://openairdocs.org/sdr/SWAA2023072176388.md): Floor Panel · corroded · Jul 7, 2023 · N8706W · Boeing 7378 · Fuselage Floor Panel
  > (A204 DOT 81) AFT CARGO FLOOR PANEL 140DF HAS CORROSION ON UPPER SURFACE AROUND PERIMITER OF FLOOR PANEL<[01] EVALUATED CORROSION AREA FOUND LENGTH OF CORRODED AREA IS MORE THAN 3' MAX ALLOWABLE LIMIT IS 3' FOUND OUT OF LIMITS I.A.W BOEING SRM 53-00-53-1A-1;[0
- [SDR SWAA2023072573846](https://openairdocs.org/sdr/SWAA2023072573846.md): Angle · corroded · Jul 1, 2023 · N8706W · Boeing 7378 · Fuselage Miscellaneous Structure
  > (A204 DOT 14) AFT CARGO STA 727I+4 RBL 23; WL 161; Z-ANGLE HAS CORROSION AROUND FASTNER HOLE.<[01] REMOVED CORROSION OF Z- ANGLE AND CHECK WITH MAGNIFYING GLASS IAW SRM 51-10-02-0G-0 ITEM 14;[02] EVALUATED DAMAGE;ORIG.'T'.040 MATERIAL REMAINING.032 LOSS.008
- [SDR SWAA2023072573841](https://openairdocs.org/sdr/SWAA2023072573841.md): Doubler · corroded · Jul 1, 2023 · N8706W · Boeing 7378 · Fuselage Main, Structure
  > (A204 DOT 15) AFT ARGO STA 727I+4; RBL 23; WL 161; Z-ANGLE DOUBLER PLATE HAS CORROSION ON LOWER SURFACE.<[01] Z ANGLE DOUBLER PLATE BEEN REPLACED ON N/R TTG8Q00LZ34E I.A.W SRM 53-00-53-2R-5;[02] AUDIT C/W
- [SDR SWAA2023072573847](https://openairdocs.org/sdr/SWAA2023072573847.md): Shield · corroded · Jul 1, 2023 · N8706W · Boeing 7378 · Fuselage Miscellaneous Structure
  > (A204 DOT 16) AFT CARGO STA 767 TO 787+6; RBL 23; WL 161; SPLASH SHIELD HAS CORROSION ON UPPER AND LOWER SURFACE.<[01] EVALUATED SHOELD NO ALLOAWBLE LIMITS FOUND IN SRM 53-60-15-1A-1;[02] REMOVED SHIELD I.A.W SRM 51-40-02-0G-0;[03] VERIFIED ITEMS 1;2;[04] VERI
- [SDR SWAA2023072573842](https://openairdocs.org/sdr/SWAA2023072573842.md): Attach Angle · corroded · Jul 1, 2023 · N8706W · Boeing 7378 · Fuselage Main, Attach Fittings
  > (A204 DOT 17) AFT CARGO STA 767 TO 787; RBL 23; WL 161; SPLACE SHIELD ATTACH ANGLE HAS CORROSION ON LOWER SURFACE COMMON TO NUT PLATES.<[01] EVALUATED ANGLE FOUND MATERIAL LOSE IS MORE THAN 90% OF MATERIAL THICKNESS OUT OF LIMITS I.A.W SRM 51-10-02-0G-0;[02] R
- [SDR SWAA2023072573848](https://openairdocs.org/sdr/SWAA2023072573848.md): Attach Angle · cracked · Jul 1, 2023 · N8706W · Boeing 7378 · Fuselage Main, Attach Fittings
  > (A204 DOT 18) AFT CARGO; STA 867; LBL 10; JUST BELOW CARGO FLOOR LINE. ATTACHE ANGLE CRACKED FROM LONGITUDINAL FLOOR SUPPORT TO ANGLED FLOOR SUPPORT (LAV VACUUM COMPARTMENT STRUCTURE)<[01] REMOVED ANGLE ON AFT CARGO; STA 867; LBL 10; JUST BELOW CARGO FLOOR LIN
- [SDR SWAA2023072573843](https://openairdocs.org/sdr/SWAA2023072573843.md): Splice Plate · corroded · Jul 1, 2023 · N8706W · Boeing 7378 · Fuselage Miscellaneous Structure
  > (A204 DOT 19) AFT CARGO. STA 887; BL0 TO RBL 16; WL 165; FLOOR PANEL SPLICE PLATE HAS CORROSION ON UPPER SURFACE.<[01] EVALUATED SPLICE PLATE NO ALLOWABLE LIMITS FOUND IN SRM;[02] VERIFIED STEP 1;[03] SPLICED REMOVED FROM STA 887 BL 0 WL 165 IAW SRM 51-40-05;[
- [SDR SWAA2023072573849](https://openairdocs.org/sdr/SWAA2023072573849.md): Shield · corroded · Jul 1, 2023 · N8706W · Boeing 7378 · Fuselage Miscellaneous Structure
  > (A204 DOT 20) AFT CARGO STA 847+6; RBL 23; WL 162; SPLASH SHIELD HAS CORROSION AROUND NUT PLATE HOLE.<[01] EVALUATED CORRODED SHIELD NO ALLOWABLE LIMIT FOUND IN SRM 53-00-53-1A-2;[02] VERIFIED STEP 1;[03] REMOVED SHIELD IAW SRM 51-40-02-0G-0;[04] VERIFIED REPL
- [SDR SWAA2023072573851](https://openairdocs.org/sdr/SWAA2023072573851.md): Panel · cracked · Jul 1, 2023 · N8706W · Boeing 7378 · Horizontal Stabilizer Structure
  > LH HORIZONTAL STAB ELEVATOR BALANCE BY SEAL PANEL 334CB BULB SEAL IS CRACKED AT ELEVATOR STA. 149.12 P/N 183A2433-3<[01] REPLACED L/H HORIZONTAL STAB ELEVATOR BALANCE SEAL PANEL 334CB PLATE I/A/W SRM 51-40-02-0G-0 AND BOEING DWG 183A0300 REV A;[02] C/W;[03] VE

Next page: https://openairdocs.org/aircraft/N8706W/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 = 'N8706W' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8706W/reports

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