# Service difficulty reports: N8685B

A list on [N8685B](https://openairdocs.org/aircraft/N8685B.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 · 84 reports

- [SDR SWAA2026071532882](https://openairdocs.org/sdr/SWAA2026071532882.md): Megaphone · loose · Jul 12, 2026 · N8685B · Boeing 7378H4 · Emergency Equipment
  > CREW REPORTS AFT MEGAPHONE NEEDS SECURED. RESECURED AFT MEGAPHONE IAW AMM 25-64-00.
- [SDR SWAA2026020563410](https://openairdocs.org/sdr/SWAA2026020563410.md): Battery Pack · inoperative · Jan 21, 2026 · N8685B · Boeing 7378H4 · Emergency Lighting
  > FWD RIGHT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY BACK AND PERFORMED A GOOD OPS CHECK IAW AMM 33-51-06-960-805.
- [SDR SWAA2025110330315](https://openairdocs.org/sdr/SWAA2025110330315.md): Sign · unsecure · Oct 31, 2025 · N8685B · Boeing 7378H4 · Emergency Lighting
  > AFT GALLEY CEILING EXIT SIGN NEEDS TO BE SECURED. SECURED SCREWS IAW AMM 33-51-01-201-NG.
- [SDR SWAA2025061776810](https://openairdocs.org/sdr/SWAA2025061776810.md): Bulb · inoperative · Jun 1, 2025 · N8685B · Boeing 7378H4 · Emergency Lighting
  > IN THE CABIN ABOVE THE FWD ENTRY DOOR, THE EXIT LIGHT HAS ONE INOP BULB. REMOVED AND REPLACED LAMP OPS CHECK OK PER AMM 33-25-00.
- [SDR SWAA2025061176811](https://openairdocs.org/sdr/SWAA2025061176811.md): Battery Pack · inoperative · Jun 1, 2025 · N8685B · Boeing 7378H4 · Emergency Lighting
  > IN THE PASSENGER CABIN; THE EMERGENCY EXIT LIGHT FWD OF THE LEFT HAND FWD MID EXIT DOOR IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1694 PER AMM 33-51-06. ALL ASSOCIATED EMERGENCY LIGHTS OPS CHECK GOOD PER AMM 33-51-06.
- [SDR SWAA2025061176809](https://openairdocs.org/sdr/SWAA2025061176809.md): Battery Pack · inoperative · Jun 1, 2025 · N8685B · Boeing 7378H4 · Emergency Lighting
  > IN THE PASSENGER CABIN; THE EMERGENCY EXIT LIGHT FWD OF THE RIGHT HAND FWD MID EXIT DOOR IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1694 PER AMM 33-51-06. ALL ASSOCIATED EMERGENCY LIGHTS OPS CHECK GOOD PER AMM 33-51-06.
- [SDR SWAA2025061676296](https://openairdocs.org/sdr/SWAA2025061676296.md): Seal · cracked · May 29, 2025 · N8685B · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL UPPER FORWARD SLIDER SEAL IS CRACKED; TORN ON FORWARD TRACK. REMOVED LH HORIZONTAL UPPER FWD SLIDING SEAL PER AMM 53-31-31. REPLACED LH HORIZONTAL UPPER FWD SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2025061772760](https://openairdocs.org/sdr/SWAA2025061772760.md): Angle · cracked · May 20, 2025 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED I/B OF LH DEFECTION RIB (MPN 115A2156-7). REMOVED ANGLE PER SRM 51-40-02. LOCATED AND DRILLED FASTENER HOLES IN NEW ANGLE PER SRM 51-40-05. INSTALLED REPLACEMENT ANGLE PER SRM 51-40-02.
- [SDR SWAA2025061772761](https://openairdocs.org/sdr/SWAA2025061772761.md): Angle · cracked · May 20, 2025 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ANGLE ASSY CRACKED I/B OF LH DEFECTION RIB (MPN 115A2156-17). REMOVED ANGLE PER SRM 51-40-02. LOCATED AND DRILLED NEW FASTENER HOLES IN NEW ANGLE PER SRM 51-40-05. INSTALLED REPLACEMENT ANGLE PER SRM 51-40-02. INSPECTED PER SRM 51-40-02-0G-0-B00069 (GENE
- [SDR SWAA2025061171464](https://openairdocs.org/sdr/SWAA2025061171464.md): Seal · cracked · May 15, 2025 · N8685B · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED.<[01] INFO: PARTS ORDERED 5/15/25. AMM REFERENCE IS 53-31-31.;[02] INSTALLED ATTACH FITTING ON SEAL PER SRM 51-40-02.;[03] VERIFIED INSTALLED ATTACH FITTING ON SEAL PER SRM 51-40-02.;[04] INSTALLED RH HOR
- [SDR SWAA2025061170066](https://openairdocs.org/sdr/SWAA2025061170066.md): Seat Track · corroded · May 13, 2025 · N8685B · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings
  > CAPT'S FWD O/B SEAT TRACK HAS POSSIBLE CORROSION AT FWD MOUNT BOLT AREA. REMOVED CAPT. FWD. OTBD. SEAT TRACK IN REFERENCE TO SRM 51-40-02. REMOVED AND REPLACED PER [AMM 25-11-11-400-801-NG
- [SDR SWAA2025061170065](https://openairdocs.org/sdr/SWAA2025061170065.md): Seat Track · corroded · May 13, 2025 · N8685B · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings
  > CAPT'S FWD I/B SEAT TRACK HAS POSSIBLE CORROSION AT FWD MOUNT BOLT AREA. REMOVED CAPT. FWD INBD. SEAT TRACK IN REFERENCE TO SRM 51-40-02.
- [SDR SWAA2025061170064](https://openairdocs.org/sdr/SWAA2025061170064.md): Seat Track · corroded · May 13, 2025 · N8685B · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings
  > F.O.'S FWD O/B SEAT TRACK HAS POSSIBLE CORROSION AT FWD MOUNT BOLT AREA. MRKD<[01] REMOVED FO'S FWD. OTBD. SEAT TRACK IN REFERENCE TO SRM 51-40-02;[02] 01 - REMOVED AND REPLACED PER [AMM 25-11-11-400-801-NG (FLIGHT COMPARTMENT SEAT TRACKS - INSTALLATION AND AL
- [SDR SWAA2025061170063](https://openairdocs.org/sdr/SWAA2025061170063.md): Seat Track · corroded · May 13, 2025 · N8685B · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings
  > F.O.'S FWD I/B SEAT TRACK HAS POSSIBLE CORROSION AT FWD MOUNT BOLT AREA. MRKD<[01] REMOVED FO'S FWD. INBD. SEAT TRACK IN REFERENCE TO SRM 51-40-02;[02] 01 - REMOVED AND REPLACED PER [AMM 25-11-11-400-801-NG (FLIGHT COMPARTMENT SEAT TRACKS - INSTALLATION AND AL
- [SDR SWAA2025061170778](https://openairdocs.org/sdr/SWAA2025061170778.md): Attach Angle · cracked · May 13, 2025 · N8685B · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACKS FOUND AT BS 663 VAPOR BARRIER UPPER ATTACH ANGLE RBL 9 & 32.<[01] MATCH DRILLED BS 663 VAPOR BARRIER UPPER ATTACH ANGLE PER SRM 51-40-02 & DWG 111A1000. NEED OK TO INSTALL ANGLE.;[02] REMOVED 663 VAPOR BARRIER ANGLE PER SRM 51-40-02.;[03] C/W RII INSPEC
- [SDR SWAA2025061769935](https://openairdocs.org/sdr/SWAA2025061769935.md): Bracket · cracked · May 12, 2025 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > BRACKET CRACKED I/B OF RH DEFECTION RIB. REMOVED CRACKED SUPPORT ANGLE BRACKET PER SRM 51-40-02. THE CRACKED SUPPORT ANGLE BRACKET HAS BEEN VERIFIED AS BEING REMOVED AS STATED IN ITEM #1. LOCATED; DRILLED AND DEBURRED REPLACEMENT SUPPORT ANGLE BRACKET PER S
- [SDR SWAA2025061669934](https://openairdocs.org/sdr/SWAA2025061669934.md): Skin · delaminated · May 12, 2025 · N8685B · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT WING OUTBOARD AFT FLAP HAS DELAM ON UPPER INBOARD AFT SURFACE.<[01] REMOVED R/H WING O/B AFT FLAP PER AMM 27-51-22.;[02] OK TO INSTALL RIGHT WING OTBD FLAP.;[03] INSTALLED SERVICEABLE R/H O/B AFT FLAP PER AMM 27-51-22.;[04] VERIFIED RII WORK ACCOMPLISHED
- [SDR SWAA2025061168741](https://openairdocs.org/sdr/SWAA2025061168741.md): Attach Angle · cracked · May 8, 2025 · N8685B · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACK FOUND AT L/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 9<[01] FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5. NEED OK TO INSTALL PARTS.;[02] REMOVED R/H A/C DISTRIBUTION DUCTING F.O.M.;[03] C/W RII INSPECTION OF C/A #1;[04] INSTALLED REPAIR PER SRM 5
- [SDR SWAA2025021294473](https://openairdocs.org/sdr/SWAA2025021294473.md): Unknown · fumes · Feb 8, 2025 · N8685B · Boeing 7378H4 · Air Distribution System
  > FLIGHT ATTENDANTS REPORT PLASTIC BURNING FUMES AT ROWS 2-4. RAN SMOKE; FIRE OR FUMES QRH. FUMES EXTINGUISHED. RESTORED PWR TO ALL SWITCHES NO FUMES NOTED REMAINDER OF FLIGHT WAS NORMAL<[01] ACCOMPLISHED SMOKE/FUMES IN CABIN CONDITIONAL INSPECTION REF AMM 05-51
- [SDR SWAA2024060597735](https://openairdocs.org/sdr/SWAA2024060597735.md): Seat · locked · Jun 3, 2024 · N8685B · Boeing 7378H4 · Passenger Compartment Equipment
  > PASSENGER EMERGENCY EXIT SEAT 15C; 15B RECLINE NOT LOCKED OUT<[01] LOCKED OUT EMR EXIT SEATS 15C AND 15B RFE AMM 25-22-00
- [SDR SWAA2024043077020](https://openairdocs.org/sdr/SWAA2024043077020.md): Battery Pack · inoperative · Apr 19, 2024 · N8685B · Boeing 7378H4 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS L/H FWD CABIN STA 500C BATTERY PACK INOP<[01] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06.;[02] INSPECTED WORK PERFORMED. REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06.;[03] OPS CHECKED GOOD PER AMM 33-51-06.;[04] REMOVED AND
- [SDR SWAA2024043077021](https://openairdocs.org/sdr/SWAA2024043077021.md): Battery Pack · inoperative · Apr 19, 2024 · N8685B · Boeing 7378H4 · Emergency Lighting
  > FWD CABIN R/H OVERWING EMERGENCY LIGHTS AT STA 565 BATTERY PACK IS INOP<[01] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06.;[02] OPS CHECK GOOD PER AMM 33-51-06.;[03] REMOVED AND REPLACED BATTERY CHARGER ASSY PER AMM 33-51-06. <BR>OPS CHECK GOOD PER AMM 3
- [SDR SWAA2024050275843](https://openairdocs.org/sdr/SWAA2024050275843.md): Bracket · corroded · Apr 16, 2024 · N8685B · Boeing 7378H4 · Wing Miscellaneous Structure
  > R/H WING FUELING PANEL BRACKET FOR CENTER FUEL TANK HAS CORROSION.<[01] REPLACED P15 REFUELING PANEL PLATE PER SOPM 20-50-01 AND MM 28-41-61. P15 REFUELING PANEL OPS CHECKED GOOD PER MM 28-21-00-400-801;[02] VERIFIED INSTALLATION OF P15 REFUELING PANEL PLATE P
- [SDR SWAA2024050277222](https://openairdocs.org/sdr/SWAA2024050277222.md): Angle · corroded · Apr 15, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > REPLACE LH AFT CARGO SIDE PLATE FORM STA 727H +11 TO 800 DUE TO CORROSION<LOCATED; DRILLED AND COUNTERSUNKED NEW LH SIDE PLATE FROM STA 727H + 11 TO 800 PER SRM 51-40-05; 51-40-08 AND 53-00-53-2R-6;[03] CW INSP STEP #2;- REMOVED AND REPLACED PER [SRM 51-40-02
- [SDR SWAA2024043074100](https://openairdocs.org/sdr/SWAA2024043074100.md): Floor Support · cracked · Apr 12, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR SUPPORT CRACKED AT ATTACH FASTENER STA. 540 RBL 1.<[01] REMOVED BROKEN CABLIN FLOOR SUPPORT BRAKE ASSY AT STA. 540 RBL1;[02] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME -
- [SDR SWAA2024043074101](https://openairdocs.org/sdr/SWAA2024043074101.md): Floor Support · cracked · Apr 12, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR SUPPORT CRACKED AT ATTACH FASTENER STA.540 LBL 1.<[01] REMOVED BROKEN CABLIN FLOOR SUPPORT BRAKE ASSY AT STA. 540 LBL 1.;[02] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME
- [SDR SWAA2024050273653](https://openairdocs.org/sdr/SWAA2024050273653.md): Support Angle · corroded · Apr 11, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > WALL SUPPORT STA. 986.5 + 4 HAS CORROSION ON UPPER SURFACE I/B END<[01] CORROSION AT Z-ANGLE(WALL SUPPORT) AT APPROXIMATELY STA. 987+5'; LBL 33' IS OUT OF LIMITS PER SRM 53-70-51-1A-1. PARENT THICKNESS IS.050'. REMAINING THICKNESS IS.000'. REMOVED ANGLE PER
- [SDR SWAA2024050272575](https://openairdocs.org/sdr/SWAA2024050272575.md): Channel · corroded · Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDE PLATE CHANNEL AT LBL 21; STA 767-787+2 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED) AFT CARGO SIDE PLATE CHANNEL AT LBL 21 STA 767-787+2 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON L/H S
- [SDR SWAA2024050272576](https://openairdocs.org/sdr/SWAA2024050272576.md): Channel · corroded · Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 767-787 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] 01 - REMOVED AND REPLACED PER [SRM 51-10-02-0G-0-B00070 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)] REMOVED CORROSION ON
- [SDR SWAA2024050272569](https://openairdocs.org/sdr/SWAA2024050272569.md): Channel · corroded · Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDE PLATE CHANNEL AT LBL 21; STA 747-767 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON AFT CARGO L/H SIDE PLATE CHANNEL PER SRM 51-10-02; FOUND TO BE WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIA
- [SDR SWAA2024050272577](https://openairdocs.org/sdr/SWAA2024050272577.md): Channel · corroded · Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 747-767 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON AFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 747-767 PER SRM 51-10-02. REMANNING THICKNESS.030; FOUND TO BE OUT OF LI
- [SDR SWAA2024050272578](https://openairdocs.org/sdr/SWAA2024050272578.md): Channel · corroded · Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDE PLATE CHANNEL AT LBL 21; STA 727J-747 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON AFT CARGO L/H SIDE PLATE CHANNEL PER SRM 51-10-02; FOUND TO BE WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERI
- [SDR SWAA2024050272579](https://openairdocs.org/sdr/SWAA2024050272579.md): Channel · corroded · Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 727J-747 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON AFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 727J-747 PER SRM 51-10-02. REMANNING THICKNESS.033; FOUND TO BE OUT OF
- [SDR SWAA2024050272580](https://openairdocs.org/sdr/SWAA2024050272580.md): Channel · corroded · Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 727I-727J HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON AFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 727I-727J PER SRM 51-10-02. REMANNING THICKNESS.033; FOUND TO BE OUT O
- [SDR SWAA2024050272571](https://openairdocs.org/sdr/SWAA2024050272571.md): Channel · corroded · Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDE PLATE CHANNEL AT LBL 21; STA 727H-727I HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON L/H SIDE PLATE FROM STA 727I-727J LBL21 PER SRM 51-10-02; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 MATERIAL
- [SDR SWAA2024050272586](https://openairdocs.org/sdr/SWAA2024050272586.md): Channel · corroded · Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 727D-727E HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON AFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 727D-727E PER SRM 51-10-02. REMAINING THICKNESS.035'. FOUND TO BE OUT
- [SDR SWAA2024050272596](https://openairdocs.org/sdr/SWAA2024050272596.md): Web · corroded · Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR LOWER SILL THRESHOLD WEB HAS CORROSION.<[01] REMOVED CORROSION MATERIAL LOSS.005 AND FOUND TO BE OUT OF LIMITS. REMAINING THICKNESS.040. PER SRM 53-00-53. REMOVED FORWARD CARGO THRESHOLD WEB FOR REPLACEMENT PER SRM 51-40-02.;[02] VERIFIED WEB
- [SDR SWAA2024050272964](https://openairdocs.org/sdr/SWAA2024050272964.md): Floorbeam · corroded · Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > STA 986.5 FLOOR BEAM UPPER FLANGE HAS CORROSION AROUND FLOOR PANEL ATTACH HOLE AT LBL 30.5.<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ORIGINAL THICKNESS=.150?; REMAINING THICKNESS=.125?.;[02] BLEND
- [SDR SWAA2024050272963](https://openairdocs.org/sdr/SWAA2024050272963.md): Floorbeam · corroded · Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > STA 986.5 FLOOR BEAM UPPER FLANGE HAS CORROSION AROUND NUTPLATE HOLE AT LBL 43.<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF
- [SDR SWAA2024050272966](https://openairdocs.org/sdr/SWAA2024050272966.md): Fitting · corroded · Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage, Equipment Attach Fittings
  > AFT GALLEY LAV E O/B AND AFT TIE DOWN FITTING POSSIBLE CORROSION UNDER FITTING. (MARKED)<BLENDED CORROSION PER SRM 51-10-02. MAX MATERIAL REMOVED 0.075?. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1;REMOVED DAMAGED SECTION OF FLOOR BEAM UPPER FLANGE P
- [SDR SWAA2024043072965](https://openairdocs.org/sdr/SWAA2024043072965.md): Skin · delaminated · Apr 9, 2024 · N8685B · Boeing 7378H4 · Trailing Edge Flaps
  > L/H O/B AFT FLAP DELAMINATED LOWER I/B CORNER LOWER SURFACE<[01] REMOVED L/H O/B AFT FLAP IAW AMM 27-51-22;[02] OK TO INSTALL;[03] INSTALLED L/H OB AFT FLAP PER AMM 27-51-22 THROUGH STEP 3.(5)(G).;[04] C/W RII INSPECTION OF OUTBD FLAP INSTALL;[05] REMOVED AND
- [SDR SWAA2024043072601](https://openairdocs.org/sdr/SWAA2024043072601.md): Handle · loose · Apr 9, 2024 · N8685B · Boeing 7378H4 · Galley Doors
  > AFT GALLEY SERVICE DOOR (R2) HANDLE CAM PLATE LOOSE<[01] SECURED CAM PLATE ATTACHING HARDWARE PER M/M REF 52-41-11;[02] SECURED CAM PLATE ATTACHING HARDWARE PER M/M REF 52-41-11
- [SDR SWAA2024043071858](https://openairdocs.org/sdr/SWAA2024043071858.md): Intercostal · cracked · Apr 8, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > BETWEEN STATION 380 AND 400; THE INTERCOSTAL AT LBL 14 HAS EVIDENCE OF CRACKS AT BOTH THE FASTENER HOLES AND THE UPPER ANGLE INNER RADIUS.<[01] REMOVED AND REPLACED UPPER ANGLE PER SRM 51-40-02.;[02] RII C/W INSPECTION AS REQUIRED
- [SDR SWAA2024050271685](https://openairdocs.org/sdr/SWAA2024050271685.md): Plate · corroded · Apr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO FLOOR STRUCTURE SIDE PLATE HAS LIGHT CORROSION AROUND FASTENER HOLES FROM STA 500 TO 500A RBL 24.<[01] BLENDED AREAS; REMOVED.030' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED AND REPLACED SHIELD PER SRM 51-40-02.;[03] 02
- [SDR SWAA2024050271668](https://openairdocs.org/sdr/SWAA2024050271668.md): Plate · corroded · Apr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO FLOOR STRUCTURE SIDE PLATE HAS LIGHT CORROSION AROUND FASTENER HOLES FROM STA 500A TO 500D LBL 24.<[01] BLENDED AREAS; REMOVED.008' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] BLENDED AREAS; REMOVED.008' MATERIAL. FOUND TO BE OUT
- [SDR SWAA2024050271688](https://openairdocs.org/sdr/SWAA2024050271688.md): Plate · corroded · Apr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO FLOOR STRUCTURE SIDE PLATE HAS LIGHT CORROSION AROUND FASTENER HOLES FROM STA 500D TO 500F LBL 24.<[01] THIS SECTION TO BE REPLACED FROM STA 500B + 10 TO 500I ON NR # TTG8Q00SLBEU;[02] BLENDED AREAS; REMOVED.009' MATERIAL FOUND TO BE OUT OF LIMITS P
- [SDR SWAA2024050271690](https://openairdocs.org/sdr/SWAA2024050271690.md): Plate · corroded · Apr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO FLOOR STRUCTURE SIDE PLATE HAS LIGHT CORROSION AROUND FASTENER HOLES FROM STA 500F TO 500I LBL 24.<[01] BLENDED AREAS; REMOVED.005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED FROM STA 500B + 10 TO 500I ON
- [SDR SWAA2024050171842](https://openairdocs.org/sdr/SWAA2024050171842.md): Floorbeam · corroded · Apr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT WET AREA- CORROSION ON FLOOR BEAM AT STA 947 +4; LBL +25. BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. BLENDING WAS DONE ON INTERCOSTAL WHICH IS OUT OF LIMITS. REMOVED DAMAGED INTERCOSTAL FROM STA
- [SDR SWAA2024050171841](https://openairdocs.org/sdr/SWAA2024050171841.md): Web · corroded · Apr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT WET AREA- CORROSION ON FLOOR PAN WEB AT STA 1006 +8; LBL +38. DRILLED UP NEW WEB PER SRM 51-40-02. BLENDED CORROSION ON FLOOR PAN WEB AT STA. 1006+8'; LBL 38' PER SRM 51-10-02. REMOVED.008' OF MATERIAL. REMAINING THICKNESS IS.032. DAMAGE REMOVAL OUT
- [SDR SWAA2024050171840](https://openairdocs.org/sdr/SWAA2024050171840.md): Web · corroded · Apr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT WET AREA- CORROSION ON FLOOR PAN WEB AT STA 1006 +3; LBL +38. DRILLED UP NEW WEB PER SRM 51-40-02.;[02] BLENDED CORROSION ON FLOOR PAN WEB AT STA. 1006+3'; LBL 38' IAW SRM 51-10-02. REMOVED.012' OF MATERIAL. REMAINING THICKNESS IS.028. DAMAGE REMOVAL OU

Next page: https://openairdocs.org/aircraft/N8685B/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 = 'N8685B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8685B/reports

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