# Service difficulty reports: N5227A A list on [N5227A](https://openairdocs.org/aircraft/N5227A.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SCNA20260325142](https://openairdocs.org/sdr/SCNA20260325142.md): Warning Message · illuminated · Mar 25, 2026 · N5227A · Boeing 73786N · Trailing Flap Position Indicating System > ON FLAP EXTENSION. GOT A FLAP DISAGREE <1 HANDLE AT 5. REMOVED AND REPLACED FLAP POSITION INDICATOR REF. AMM 27-58-02, OPS CHECK GOOD. REMOVED AND REPLACED FLAP POSITION TRANSMITTER PER AMM 27-58-02 OPS CHECK GOOD. - [SDR SCNA20260311120](https://openairdocs.org/sdr/SCNA20260311120.md): Window · arced · Mar 11, 2026 · N5227A · Boeing 73786N · Flight Compartment Windows > L1 WINDOW ARCING IN FLIGHT. R & R L1 WINDOW REF AMM 56-11-11 LEAK CHECK GOOD OK FOR SERVICE. R AND R L1 WINDOW HEAT CONTROL UNIT REF AMM 30-41-11. OK FOR SERVICE - [SDR SCNA20260116032](https://openairdocs.org/sdr/SCNA20260116032.md): Shim · missing · Jan 15, 2026 · N5227A · Boeing 73786N · Emergency Equipment > UPPER FUSELAGE FWD ENTRY AREA L1 DOOR INBD AND OTBD GIRT BAR FLOOR SUPPORT WITH PLASTIC SHIM MISSING. INSTALLED FWD ENTRY AREA L1 DOOR I/B AND O/B FLOOR-MOUNTED ESCAPE SLIDE BRACKET AND PLASTIC SHIM IAW AMM 25-66-02-400-8017 SATISFACTORY CONDITION - [SDR SCNA20260113024](https://openairdocs.org/sdr/SCNA20260113024.md): Retainer · loose · Jan 10, 2026 · N5227A · Boeing 73786N · Emergency Equipment > UPPER FUSELAGE FWD GALLEY DOOR, ESCAPE SLIDE COVER, RETAINER CLIP WITH LOOSE RIVETS. REPLACED SOLID RIVETS AT UPPER FUSELAGE FWD GALLEY DOOR, SCOPE SLIDE COVER IAW SRM BCF 51-40-02-06-0 PARAG 4E AND 4B REV 25 DATED 11-10-2025 AND AIPC 25-66-00-13 SHEET 002 RE - [SDR SCNA20260113023](https://openairdocs.org/sdr/SCNA20260113023.md): Retainer · loose · Jan 10, 2026 · N5227A · Boeing 73786N · Emergency Equipment > UPPER FUSELAGE FWD ENTRY DOOR, SCAPE SLIDE COVER RETAINER CLIP WITH LOOSE RIVETS. REPLACED SOLID RIVETS AT UPPER FUSELAGE FWD ENTRY DOOR, SCOPE SLIDE COVER IAW B-737-800 SRM BEF 51-40-02-06-0 PARAG 4E AND 4B REV 25 DATED 11-10-2025 AND AIPC 25-66-00-14 SHEET - [SDR SCNA20250604194](https://openairdocs.org/sdr/SCNA20250604194.md): Rib · cracked · May 29, 2025 · N5227A · Boeing 7378 · Horizontal Stabilizer, Spar/Rib > L/H HORIZONTALSTAB RIB IS CRACKED AT STAB STA 92.7 #2 STIFFENER. REMOVED DAMAGE AND REPAIRED L/H HORIZONTAL STAB RIB @ STAB STA. 92.7 #2 STIFFENER PER SRM 55-10-09-2R-4, FIG 202 - [SDR SCNA20250604193](https://openairdocs.org/sdr/SCNA20250604193.md): Skin · cracked · May 29, 2025 · N5227A · Boeing 7378 · Horizontal Stabilizer, Plate/Skin > CUSTOMER CARD #: ENG-55SCA-11150-LH FOUND CRACK AT L/H HORIZONTAL STABALIZER LOWER SKIN AT STAB STA 101.90 APROX 0.75" LONG AND 20" AFT OF LEADING EDGE. (MARKED ENDS OF CRACK) - REPAIRED L/H HORZ STAB LOWER SKIN @ STAB 101.90 PER SRM 55-10-01-2R-11, FIG. 204 - [SDR SCNA20250604195](https://openairdocs.org/sdr/SCNA20250604195.md): Rib · cracked · May 26, 2025 · N5227A · Boeing 7378 · Horizontal Stabilizer, Spar/Rib > L/H HORIZONTALSTAB RIB IS CRACKED AT STAB STA 92.7 #3 STIFFENER. REMOVED DAMAGE AND REPAIRED L/H HORIZONTAL STAB RIB @ STA. 92.7 #3 STIFFENER PER SRM 55-10-09-2R-4, FIG. 202 - [SDR UIEA2024120401165](https://openairdocs.org/sdr/UIEA2024120401165.md): Door · open · Dec 4, 2024 · N5227A · Boeing 73786N · Electrical/Electronic Compartment Doors > AIR TURN BACK, EQUIP DOOR LIGHT CAME ON @3000'. AIRCRAFT WOULDN'T PRESSURIZE.(

FOUND EQUIP DOOR FULLY OPEN WITH EQUIP LIGHT ON. CLOSED AND SECURED DOOR MULTIPLE TIMES. NO DAMAGE NOTED IN LOCKING MECHANISM IAW AMM 52-48-41. COMPLETED VISUAL INSPECTION IAW AMM - [SDR UIEA2024111301087](https://openairdocs.org/sdr/UIEA2024111301087.md): Beam · unknown · Nov 14, 2024 · N5227A · Boeing 737 · Wing Main, Frame Structure > PNEU DOOR OUTBOARD LATCH INOP(

EA3857A012 COMPLIED WITH PART 1 PERMANENT REPAIR RH LWR SUPPORT BEAM ASSY NEAR 192DR HIGH PRESSURE CONNECT ACCESS DOOR. DMI 219921 CLOSED

) - [SDR UIEA2024021000075](https://openairdocs.org/sdr/UIEA2024021000075.md): Doubler · cracked · Feb 12, 2024 · N5227A · Boeing 73786N · Fuselage Main, Structure > LOWER FUSELAGE, EXTERNAL POWER RECEPTACLE CUT-OUT WITH CRACK.(

R/R INNER DOUBLER P/N: 141A3722-12 AT EXTERNAL POWER RECEPTABLE IAW B737-800 BCF SRM 51-10-02-0G-0 PARAG 9. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2023110200935](https://openairdocs.org/sdr/UIEA2023110200935.md): Proximity Sensor · unknown · Nov 2, 2023 · N5227A · Boeing 73786N · Leading Edge Slat Position Indicating System > LE FLAP TRANSIT LIGHT ILLUMINATED ON FINAL.(

TROUBLESHOT PER FIM 27-88 TASK 814 AND FOUND LH #3 FLAP PROX SENSOR FAILED. REMOVED AND REPLACED L/H #3 FLAP EXTEND PROX SENSOR IAW B 737 AMM 27-88-11. OPS CHECK GOOD AT THIS TIME. FOUND F3 PROX EXTEND CODE 27-812 - [SDR UIEA2023100600890](https://openairdocs.org/sdr/UIEA2023100600890.md): Smoke Goggles · unknown · Oct 6, 2023 · N5227A · Boeing 73786N · Emergency Equipment > CAPTAIN SMOKE GOGGLES BROKEN.(

R/R CAPTAIN SMOKE GOGGLES PER AMM 25-64-00 AND DAILY CHECK JC E-06-001-01-08. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2023090100824](https://openairdocs.org/sdr/UIEA2023090100824.md): Unknown · unknown · Sep 1, 2023 · N5227A · Boeing 73786N · Auto Flight System > AT GLIDESLOPE / LOCALIZER INTERCEPT W/ AP ENGAGED, HAD THE AIRSPEED TAPE (RED) JUMP UP 10 KTS, CAUSING AN A/S LOW MESSAGE AND STICK SHAKER. WE PERFORMED A GO-AROUND, FLAPS 40, NORMAL APPROACH & LANDING ON NEXT ATTEMPT.(

PERFORMED DFCS BITE. NO FAULTS FOUND I - [SDR UIEA2023040700337](https://openairdocs.org/sdr/UIEA2023040700337.md): Fseu · unknown · Apr 7, 2023 · N5227A · Boeing 73786N · Trailing Edge Flap Control System > LE FLAP TRANSIT LIGHT STAYED ILLUMINATED AMBER WHEN SELECTING FLAPS 5(

PERFORM FSEU BITE IAW FIM TASK 27-51 TASK 801. FOUND F3 PROX RET MESSAGE 27-81220. PERF FIM TASK 27-88 TASK 805. ALL SENSORS GAP NORMAL. DUE TO HISTORY, R/R FSEU IAW AMM 27-51-01. OPS CHK - [SDR UIEA2022072100769](https://openairdocs.org/sdr/UIEA2022072100769.md): Beam · corroded · Jul 24, 2022 · N5227A · Boeing 73786N · Wing, Control Surfaces > AGING A/C INSP - AREAS OF MINOR CORROSION ON THE RH WING T/E CLOSE OUT PANEL ATTACH ANGLE BETWEEN THE O/B FAIRINGS, MULTIPLE AREAS ALONG THE ANGLE (CORROSION FOUND IN MULTIPLE AREAS AROUND NUTPLATES MEASURING 1.0"L X 1.0" W X.015" D ALONG FULL LENGTH OF BEAM. - [SDR Q2SA20201021439](https://openairdocs.org/sdr/Q2SA20201021439.md): Actuator · inoperative · Oct 21, 2020 · N5227A · Boeing 73786N · Leading Edge Slat Actuator > AIRCRAFT GROUNDED. LEADING EDGE FLAP 1 EXTENDED INDICATION WHILE CRUISING AT FL 390. LEADING EDGE TRANSIT LIGHT ALSO ILLUMINATED. REMOVED AND REPLACED LEADING EDGE NR 1 FLAP ACTUATOR, IAW AMM 27-81-31-400-801. REMOVED LEADING EDGE LOCK OUT TOOL. OPERATION - [SDR Q2SA20201017437](https://openairdocs.org/sdr/Q2SA20201017437.md): Electronic Unit · inoperative · Oct 17, 2020 · N5227A · Boeing 73786N · Trailing Edge Flap Control System > AIRCRAFT GROUNDED. FLAPS DID NOT EXTEND WHEN SELECTED. USED ALTERNATE FLAPS. R & R FLAP/SLAT ELECTRONIC UNIT ASSEMBLY, IAW AMM 27-51-00. OPERATIONS CHECK GOOD. A/C CLEAR FOR SERVICE. ## 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 = 'N5227A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N5227A/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.