# Service difficulty reports: N8655D

A list on [N8655D](https://openairdocs.org/aircraft/N8655D.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 · 98 reports

- [SDR SWAA2026060809184](https://openairdocs.org/sdr/SWAA2026060809184.md): Sign · missing · Jun 3, 2026 · N8655D · Boeing 7378H4 · Emergency Lighting
  > LOWER EXIT SIGN MISSING FROM ROW 14AC. INSTALLED LOWER EXIT SIGN IAW AMM REF 33-51-01.
- [SDR SWAA2026050594624](https://openairdocs.org/sdr/SWAA2026050594624.md): Placard · missing · May 1, 2026 · N8655D · Boeing 7378H4 · Placards and Markings
  > LOWER PLACARD AT ROW 14A EMERGENCY EXIT MISSING. RESECURED LOWER PLACARD AT ROW 14A EXIT PER SIP.
- [SDR SWAA2026030976250](https://openairdocs.org/sdr/SWAA2026030976250.md): Light · unsecure · Mar 3, 2026 · N8655D · Boeing 7378H4 · Emergency Lighting
  > PHOTOLUMINESCENT FLOOR PROXIMITY LIGHT STRIP LIFTING AT 12C. SECURED WITH DOUBLE SIDED TAPE IAW AMM 33-51-15.
- [SDR SWAA2026010657914](https://openairdocs.org/sdr/SWAA2026010657914.md): Sign · loose · Jan 3, 2026 · N8655D · Boeing 7378H4 · Emergency Lighting
  > MID CABIN EXIT SIGN ON CEILING LOOSE. SECURED EXIT SIGN PER MM 33-51-01
- [SDR SWAA2025120140358](https://openairdocs.org/sdr/SWAA2025120140358.md): Stop Fitting · out of adjust · Nov 27, 2025 · N8655D · Boeing 7378H4 · Landing Gear Doors
  > AFTER TAKEOFF RAISED GEAR HANDLE TO UP POSITION, GEAR CAME UP UPON MOVING GEAR HANDLE TO OFF POSITION RECEIVED A RED NOSE GEAR LIGHT AND COULD HEAR THAT THE GEAR EXTENDED. OK CONTINUE PER MEL 32-16-01, SP1. ADJUSTED RT NLG DOOR AFT STOP IAW AMM 32-22-11-00
- [SDR SWAA2025100220471](https://openairdocs.org/sdr/SWAA2025100220471.md): Cover · unsecure · Oct 2, 2025 · N8655D · Boeing 7378H4 · Escape Slide
  > L2 DOOR SLIDE COVER WINDOW NOT SECURE. SECURED L2 DOOR SLIDE COVER IAW SOPM 20-50-12.
- [SDR SWAA2025090806020](https://openairdocs.org/sdr/SWAA2025090806020.md): Handle · loose · Aug 19, 2025 · N8655D · Boeing 7378H4 · Passenger/Crew Doors
  > L1 DOOR ASSIST HANDLES (BOTH) LOOSE. SECURED BOTH L1 DOOR ASSIST HANDLES IAW AMM 52-11-31.
- [SDR SWAA2025090406025](https://openairdocs.org/sdr/SWAA2025090406025.md): Handle · unsecure · Aug 19, 2025 · N8655D · Boeing 7378H4 · Service Doors
  > R1 DOOR ASSIST HANDLE LOOSE DOOR SIDE. SECURED R1 DOOR ASSIST HANDLE IAW B737-800 AMM 52-41-31.
- [SDR SWAA2025090406026](https://openairdocs.org/sdr/SWAA2025090406026.md): Handle · loose · Aug 19, 2025 · N8655D · Boeing 7378H4 · Service Doors
  > R2 DOOR ASSIST HANDLE LOOSE. SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 52-41-31.
- [SDR SWAA2025011686730](https://openairdocs.org/sdr/SWAA2025011686730.md): Battery · no test · Jan 16, 2025 · N8655D · Boeing 7378H4 · Emergency Equipment
  > FWD FA FLASHLIGHT INOP<[01] R & R FWD F.A. FLASHLIGHT BATTERY. OPS CK GOOD PER AMM 25-64-00
- [SDR SWAA2024112659891](https://openairdocs.org/sdr/SWAA2024112659891.md): Power Supply · inoperative · Nov 14, 2024 · N8655D · Boeing 7378H4 · Emergency Lighting
  > FWD L/H ENTRY EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED FWD L/H EMERGENCY POWER SUPPLY AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-805;[02] REMOVED AND REPLACED FWD L/H EMERGENCY POWER SUPPLY AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-805
- [SDR SWAA2024112657022](https://openairdocs.org/sdr/SWAA2024112657022.md): Flap · delaminated · Nov 6, 2024 · N8655D · Boeing 7378H4 · Trailing Edge Flaps
  > R/H O/B AFT FLAP HAS SIGN OF DELAMINATION AT THE I/B AFT CORNER AREA. R/H O/B AFT FLAP HAS SIGNS OF DEMLAMINTION AT THE I/B AFT CORNER AREA.<[01] R/H O/B AFT FLAP REMOVED AND REPLACED IAW B737-800 AMM 27-51-22;[02] VERIFIED R/H O/B AFT FLAP REMOVED AND REPLACE
- [SDR SWAA2024112656915](https://openairdocs.org/sdr/SWAA2024112656915.md): Bracket · cracked · Nov 5, 2024 · N8655D · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT WING TRAILING EDGE WEB AT AFT PYLON AREA HAS A CRACKED BRACKET. STREAMERED<[01] REMOVED AND REPLACED BRACKET 115A6260-2 PO#1084100.3 IAW B737-800 SRM 51-40-02 AND BAC DWG#115A6200 REV.A;[02] REMOVED AND REPLACED BRACKET 115A6260-2 PO#1084100.3 IAW B737-8
- [SDR SWAA2024112656917](https://openairdocs.org/sdr/SWAA2024112656917.md): Bracket · cracked · Nov 5, 2024 · N8655D · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT WING TRAILING EDGE WEB AT AFT PYLON AREA HAS A CRACKED BRACKET OUTBOARD END OF WEB.<[01] REMOVED AND REPLACED BRACKET 115A6260-1 PO#110490.1 IAW B737-800 SRM 51-40-02 AND BAC DWG#115A6200 REV.A;[02] REMOVED AND REPLACED BRACKET 115A6260-1 PO#110490.1 IAW
- [SDR SWAA2024112157016](https://openairdocs.org/sdr/SWAA2024112157016.md): Floor Panel · delaminated · Nov 5, 2024 · N8655D · Boeing 7378H4 · Fuselage Floor Panel
  > CR: (MH) FLOOR PANEL 232JF DELAM REQ. REMOVE AND REPLACE<[01] C/W T/C REMOVED AND REPLACED FLOOR PANEL 232JF;[02] REMOVED AND REPLACED NEW FLOOR PNL 232JF IAW B737-800 AMM 53-21-00-401;[03] VERIFIED REMOVED AND REPLACED NEW FLOOR PNL 232JF IAW B737-800 AMM 53-
- [SDR SWAA2024112157017](https://openairdocs.org/sdr/SWAA2024112157017.md): Floor Panel · delaminated · Nov 5, 2024 · N8655D · Boeing 7378H4 · Fuselage Floor Panel
  > CR: (MH) FLOOR PANEL 241RF DELAM REQ. REMOVE AND REPLACE<[01] REMOVED AND REPLACED PANEL 241RF IAW B737NG AMM 53-21-00-401;[02] REMOVED AND REPLACED PANEL 241RF IAW B737NG AMM 53-21-00-401
- [SDR SWAA2024112157018](https://openairdocs.org/sdr/SWAA2024112157018.md): Floor Panel · delaminated · Nov 5, 2024 · N8655D · Boeing 7378H4 · Fuselage Floor Panel
  > CR: (MH) FLOOR PANEL 231LF DELAM/ PUNCTURE REQ. REMOVE AND REPLACE<[01] REMOVED AND REINSTALLED FLOOR PANEL 231LF IAW B737 AMM 53-21-00<BR>TOOL: T03830-22<BR>DUE: 23/JAN/25;[02] REMOVED AND REINSTALLED FLOOR PANEL 231LF IAW B737 AMM 53-21-00<BR>TOOL: T03830-22
- [SDR SWAA2024112156648](https://openairdocs.org/sdr/SWAA2024112156648.md): Panel · delaminated · Nov 4, 2024 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT AFT BULKHEAD PANEL 121HW HAS 2EA DELAMINATED MARKS (DOT K049)<[01] REPAIRED PANEL 121HW OF 2 PUNCTURES IAW B737-800 AMM 25-00-00-300-801;[02] 02 - INSPECTED PER [AMM 25-00-00-300-801-NG (CRUSHED-CORE AND SANDWICH PANEL REPAIR - PERMANENT)
- [SDR SWAA2024112156313](https://openairdocs.org/sdr/SWAA2024112156313.md): Doubler · cracked · Nov 4, 2024 · N8655D · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER CRACKED<[01] ACCOMPLISHED REPAIR OF EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER IAW B737-800 SRM 53-10-15-2R-4;[02] VERIFIED ACCOMPLISHED REPAIR OF EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER IAW B737-800 SRM 53-10-15-2R-4;[0
- [SDR SWAA2024112656227](https://openairdocs.org/sdr/SWAA2024112656227.md): Vapor Barrier · cracked · Nov 3, 2024 · N8655D · Boeing 7378H4 · Wing Main, Frame Structure
  > L/H VAPOR BARRIER ANGLE CRACKED AT APPROX LBL 8.<[01] REMOVED DAMAGE; FORMED PARTS; ALODINED; PRIMED AND INSTALLED REPAIR PARTS AT VAPOR BARRIER ATTACH ANGLE L/H. STA LBL 5 TO LBL20 APROX. IAW B737-800 SRM 57-10-10-5-2R. ACCOMP. HFEC CUT EDGES; IAW B737 NDT MA
- [SDR SWAA2024112656228](https://openairdocs.org/sdr/SWAA2024112656228.md): Vapor Barrier · cracked · Nov 3, 2024 · N8655D · Boeing 7378H4 · Wing Main, Frame Structure
  > R/H VAPOR BARRIER ANGLE CRACKED AT APPROX RBL 8<[01] REMOVED; LOCATED; DRILLED; AND INSTALLED NEW VAPOR BARRIER ATTACH ANGLE; CHANNEL; STIFENER AND FITTING AT WING SECTION REAR SPART R/H FROM STA RBL 5 TO RBL 65 IAW B737-800 SRM 57-10-10-2R-5 ACCOMPLISHED A OP
- [SDR SWAA2024102852586](https://openairdocs.org/sdr/SWAA2024102852586.md): Cover · missing · Oct 24, 2024 · N8655D · Boeing 7378H4 · Emergency Lighting
  > LEFT AFT EMERGENCY EXIT SIDEWALL; EMERGENCY EXIT LIGHT LENS MISSING.(PHOTO ATTACHED.)<[01] INSTALLED REPLACEMENT EMERGENCY EXIT LIGHT LENS COVER PER SIP.
- [SDR SWAA2024102552560](https://openairdocs.org/sdr/SWAA2024102552560.md): Seat · loose · Oct 24, 2024 · N8655D · Boeing 7378H4 · Passenger Compartment Equipment
  > CABIN SEAT ROW LOOSE IN FLOOR TRACK 12DEF; 2DEF; 3DEF<[01] RE-SECURED PASSENGER SEAT ROWS AT 3DEF; 12DEF; AND 2DEF PER AMM 25-22-00.
- [SDR SWAA2024102350780](https://openairdocs.org/sdr/SWAA2024102350780.md): Light · inoperative · Oct 19, 2024 · N8655D · Boeing 7378H4 · Emergency Lighting
  > L1 DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] REVAMPED L1 EMERGENCY DOOR LIGHT IAW AMM 33-51-04 OPS CHECK GOOD
- [SDR SWAA2024070509037](https://openairdocs.org/sdr/SWAA2024070509037.md): Handle · unsecure · Jul 4, 2024 · N8655D · Boeing 7378H4 · Passenger/Crew Doors
  > AFT ENTRY DOOR INBOARD DOOR HANDLE CAM HOUSING SAFETY WIRE BROKEN.<[01] RE-SECURED AFT ENTRY DOOR INBOARD DOOR HANDLE CAM HOUSING W SAFETY WIRE REF AMM 52-13-00.
- [SDR SWAA2024070509040](https://openairdocs.org/sdr/SWAA2024070509040.md): Floorbeam · cracked · Jul 4, 2024 · N8655D · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CABIN FLOOR BOARD PANEL BREAK ASSEMBLY AT STA. 540 CRACKED AT INBOARD END L/H OF CENTER IN A/C DISTRIBUTION BAY.<[01] REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240.;[02] IS: REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51
- [SDR SWAA2024070509041](https://openairdocs.org/sdr/SWAA2024070509041.md): Floorbeam · cracked · Jul 4, 2024 · N8655D · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CABIN FLOOR BOARD PANEL BREAK ASSEMBLY AT STA. 540 CRACKED AT INBOARD END RIGHT OF CENTER IN A/C DISTRIBUTION BAY.<[01] REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240.;[02] IS: REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM
- [SDR SWAA2024031362344](https://openairdocs.org/sdr/SWAA2024031362344.md): Connector · disconnected · Mar 12, 2024 · N8655D · Boeing 7378H4 · Landing Gear System Wiring
  > ANTI-SKID INOP LIGHT ILLUMINATED ON TAKEOFF.<[01] FOUND #3 WHEEL SPIN TRANSDUCER CONNECTOR NOT INSTALLED. SECURED PER AMM 20-61-13. OPS CK GOOD PER AMM 32-42-00
- [SDR SWAA2023122735424](https://openairdocs.org/sdr/SWAA2023122735424.md): Sign · inoperative · Dec 26, 2023 · N8655D · Boeing 7378H4 · Emergency Lighting
  > OVERWING EXIT CEILING EMERGENCY EXIT SIGN INOP<[01] REMOVED AND REPLACED OVERWING AISLE CEILING EMERGENCY EXIT SIGN. OPS CHECK GOOD. REF AMM 33-51-03
- [SDR SWAA2023113025469](https://openairdocs.org/sdr/SWAA2023113025469.md): Light · inoperative · Nov 28, 2023 · N8655D · Boeing 7378H4 · Emergency Lighting
  > AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP.<[01] RELAMPED AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK NORMAL.
- [SDR SWAA2023112224033](https://openairdocs.org/sdr/SWAA2023112224033.md): Sign · out of adjust · Nov 20, 2023 · N8655D · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN CAME OFF.<[01] RESECURED EXIT ROW SIGN. OPS CHECK GOOD. REF AMM 11-32-01.
- [SDR SWAA2023051849152](https://openairdocs.org/sdr/SWAA2023051849152.md): Lens · missing · May 16, 2023 · N8655D · Boeing 7378H4 · Emergency Lighting
  > OVERWING EXIT SIGN LENS MISSING<[01] INSTALLED EMERGENCY EXIT SIGN LENS AS PER REF AMM 33-51-01
- [SDR SWAA2023051748801](https://openairdocs.org/sdr/SWAA2023051748801.md): Seat Back · out of position · May 14, 2023 · N8655D · Boeing 7378H4 · Passenger Compartment Equipment
  > 14D SEAT RECLINES INTO EXIT ROW<[01] SECURED SEAT RECLINE AT 14D PER CMM 25-22-46
- [SDR SWAA2023022710192](https://openairdocs.org/sdr/SWAA2023022710192.md): Slide · out of limits · Feb 25, 2023 · N8655D · Boeing 7378H4 · Escape Slide
  > AFT ENTRY DOOR SLIDE PRESSURE IN RED<[01] REMOVED AND INSTALLED SLIDE PER AMM 25-66-01
- [SDR SWAA2022110767383](https://openairdocs.org/sdr/SWAA2022110767383.md): Sign · cracked · Nov 2, 2022 · N8655D · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY 'EXIT' LIGHT; R/H LOWER SIDE FWD GALLEY LENS IS CRACKED. / [01] REMOVED AND REPLACED EXIT SIGN - LIGHT ASSEMBLY ON R/H LOWER FWD GALLEY PER AMM 33-51-01. EXIT SIGN OPS CHECKED GOOD PER AMM 33-51-00.;[02] VERIFIED DANIEL LEBLANC (TECHNICIAN); 03-NOV-2
- [SDR SWAA2022110760543](https://openairdocs.org/sdr/SWAA2022110760543.md): Angle · corroded · Oct 16, 2022 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT LH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 490 TO 500 (MARKED) (REF. TTG8Q00FFPCA) / [01] DUE TO OTHER DAMAGE THAT IS OUT OF LIMITS PER SRM 53-00-53-1A-2; THIS SECTION OF TRANSITION ANGLE FROM STA 480+10' TO STA 50
- [SDR SWAA2022110759700](https://openairdocs.org/sdr/SWAA2022110759700.md): Angle · corroded · Oct 14, 2022 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT R/H TRANSITION ANGLE HAS NUMEROUS AREAS OF CORROSION FROM STA 727H+12 TO 767 / [01] REMOVED CORROSION PER SRM. 51-10-02 MATERIAL FOUNDED OUT OF LIMITS PER SRM. 53-00-53-1A-02;;[02] REMOVE EXITING TRANSITION ANGLE FROM STA.727 H +10 TO STA. 767 L
- [SDR SWAA2022110759944](https://openairdocs.org/sdr/SWAA2022110759944.md): Intercostal · corroded · Oct 14, 2022 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT WET AREA INTERCOSTAL LOCATED BETWEEN STA 947.5-967; RBL 50 HAS CORROSION ON UPPER SURFACE AT LAV MOUNT BASE. / [01] BLENDED CORROSION ON MACHINED INTERCOSTAL P/N 147A5660-22 PER SRM 51-10-02. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-
- [SDR SWAA2022110759998](https://openairdocs.org/sdr/SWAA2022110759998.md): Dome Nut · corroded · Oct 14, 2022 · N8655D · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > DOME NUT HAS CORROSION INSIDE OF HOLE AT AFT WET AREA STA. 986.5 RBL 43. / [01] REMOVED DOME NUT AT RBL 43 TO FOM PER SRM 51-40-02. ATTEMPTED TO REMOVE CORROSION FROM HOLE PER SRM 51-10-02. CORROSION IS STILL PRESENT IN HOLE. CONTACTED ENGINEERING FOR FURTHER
- [SDR SWAA2022110759999](https://openairdocs.org/sdr/SWAA2022110759999.md): Angle · corroded · Oct 14, 2022 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500B-500C REFERENCE [TTG8Q00FFPBL] / [01] REMOVED DAMAGE PER SRM 51-10-02. REMOVED.001 INCH OF MATERIAL AT STATIONS 500B+2 AND 500B+7. REMAINING MATERIAL AT THOSE LOCATIO
- [SDR SWAA2022110760000](https://openairdocs.org/sdr/SWAA2022110760000.md): Angle · corroded · Oct 14, 2022 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500C-500D REFERENCE [TTG8Q00FFPBL] / [01] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT LIMITS DAMAGE AT OTHER LOCATIONS ON ANGLE.
- [SDR SWAA2022110760001](https://openairdocs.org/sdr/SWAA2022110760001.md): Angle · corroded · Oct 14, 2022 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500D-500E REFERENCE [TTG8Q00FFPBL] / [01] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT OF LIMITS DAMAGE AT OTHER LOCATIONS ON ANG
- [SDR SWAA2022110760002](https://openairdocs.org/sdr/SWAA2022110760002.md): Angle · corroded · Oct 14, 2022 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500E-500F REFERENCE [TTG8Q00FFPBL] / [01] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT OF LIMITS DAMAGE AT OTHER LOCATIONS.;[02]
- [SDR SWAA2022110760004](https://openairdocs.org/sdr/SWAA2022110760004.md): Angle · corroded · Oct 14, 2022 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500G-500H REFERENCE [TTG8Q00FFPBL] / [01] SECTION OF TRANSITION ANGLE UP TO STATION 500G+9 WILL BE REPLACED AS NOTED ON CARD TTG8Q00FGJJX DUE TO OUT OF LIMITS DAMAGE AT OT
- [SDR SWAA2022110760003](https://openairdocs.org/sdr/SWAA2022110760003.md): Angle · corroded · Oct 14, 2022 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500F-500G REFERENCE [TTG8Q00FFPBL] / [01] REMOVED DAMAGE AT STATION 500F+11. REMOVED.023 INCH OR MATERIAL. REMAINING MATERIAL THICKNESS IS.017 INCH AND IS OUT OF LIMITS
- [SDR SWAA2022110759611](https://openairdocs.org/sdr/SWAA2022110759611.md): Intercostal · corroded · Oct 13, 2022 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT LAV. LH; AFT RH MOUNT (INBD); MOUNT HAS CORROSION. AROUND BASE. / [01] BLENDED CORROSION ON MACHINED INTERCOSTAL P/N 147A5660-3 PER SRM 51-10-02. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ORIGINAL THICKNESS =.200?; REMAINING THICK
- [SDR SWAA2022110759468](https://openairdocs.org/sdr/SWAA2022110759468.md): Beam · corroded · Oct 13, 2022 · N8655D · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT WET AREA; RH LAV. AFT MOUNT OUTBD; HAS CORROSION AROUND BASE. / [01] BLENDED CORRODED AREA PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ORIGINAL PART THICKNESS =.180?; REMAINING THICKNESS AFTER BLEND OUT =.089?. CORRO
- [SDR SWAA2022110758741](https://openairdocs.org/sdr/SWAA2022110758741.md): Seal · cracked · Oct 11, 2022 · N8655D · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > R/H HORIZONTAL STAB. AFT UPPER SLIDING SEAL FWD TRACK CRACKED / [01] R&R'D TRACK PER SOPM 20-50-01;[02] VERIFIED C/A #1.
- [SDR SWAA2022110758017](https://openairdocs.org/sdr/SWAA2022110758017.md): Floor Panel · warped · Oct 9, 2022 · N8655D · Boeing 7378H4 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 140BF HAS MULTIPLE DENTS AND WAVINESS BETWEEN FLOOR SUPPORTS. / [01] FABRICATED FLOOR PANEL AFT. CARGO #140BF PER BOEING DRAWING #453A2610;[02] C/W INSPECTION.
- [SDR SWAA2022110457641](https://openairdocs.org/sdr/SWAA2022110457641.md): Battery Pack · inoperative · Oct 9, 2022 · N8655D · Boeing 7378H4 · Emergency Lighting
  > WITH THE EMERGENCY LIGHTS IN TEST MODE; NONE OF THE EMERGENCY LIGHTING IN THE FWD GALLEY AREA OPERATE. / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT STA 310;317L;500CL;500CR;565L;565R;727R AND STA 952R PER MM 33-51-06;[02] VERIFIED 1. CHRISTOPHE

Next page: https://openairdocs.org/aircraft/N8655D/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 = 'N8655D' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8655D/reports

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