# Service difficulty reports: N816SY

A list on [N816SY](https://openairdocs.org/aircraft/N816SY.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 4 · 178 reports

- [SDR SCNA20261015432](https://openairdocs.org/sdr/SCNA20261015432.md): Latch · faulted · Oct 14, 2026 · N816SY · Boeing 7378Q8 · Escape Slide
  > L2 DOOR SLIDE BUSTLE LATCH ASSY. WILL NOT BREAK OVER AND LOCK. REMOVED AND REPLACED LATCH ASSY AT DOOR L2 IAW AMM 25-66-01.
- [SDR SCNA20260713296](https://openairdocs.org/sdr/SCNA20260713296.md): Engine · fod · Jul 12, 2026 · N816SY · Boeing 7378Q8 · Engine (Turbine/Turboprop)
  > NR 1 ENG VIB WENT TO 4.0 - RAN CHKLST, RETURNED TO MSP. DECLARED EMERGENCY BLEW OUTER MLG TIRE ON T/O. COMPLTD TIRE TREAD/BURST INSP IAW AMM 05-51-54. NO DEFECTS. NR 4 TIRE REPLACED. ENG CHANGE C/W - W/O 106195, NR00001. EVIDENCE OF TIRE INGEST FOUND, FAN S
- [SDR SCNA20260623255](https://openairdocs.org/sdr/SCNA20260623255.md): Smoke Goggles · cracked · Jun 19, 2026 · N816SY · Boeing 7378Q8 · Emergency Equipment
  > SMOKE GOOGLES HAVE CRACK ON NOSE. PRIMARY OBSERVER SMOKE GOGGLES R&R REF AMM 25-64-00 OK FOR SERVICE THIS CLEARS MEL 25-11-1 MDDR# 139614
- [SDR SCNA20260603236](https://openairdocs.org/sdr/SCNA20260603236.md): Light · unsecure · Jun 3, 2026 · N816SY · Boeing 7378Q8 · Emergency Lighting
  > PHOTOLUMINESCENT ESCAPE PATH MARKING SYSTEM ALONG FLOUR AT ROWS 13-14 STRIP IS LOSE. RESECURED PHOTOLUMINESCENT FLOOR PATH AT SEATS 13 AND 14 DEF REF AMM 33-51-16.
- [SDR SCNA20260518203](https://openairdocs.org/sdr/SCNA20260518203.md): Skin · damaged · May 15, 2026 · N816SY · Boeing 7378Q8 · Fuselage Main, Plate/Skin
  > LIGHTING STRIKE STA 243.7 STR 1L. REMOVED AND REPLACED 1 SOLID RIVET AT FUSELAGE SKIN BS 234.7 STR 1L IAW SRM 53-00-01-2R-40 REPAIR 40 PARAG 4.
- [SDR SCNA20260518201](https://openairdocs.org/sdr/SCNA20260518201.md): Not Reported · damaged · May 15, 2026 · N816SY · Boeing 7378Q8 · Standard Practices/Structures
  > LIGHTNING STRIKE TRANSFERRED TO W/O 104619 N/R-0001. COMPLETED PHASE 1 AND 2 AMM 05-51-19-210-804 AND AMM 05-51-19-210-805. ALL LIGHTING STRIKES ARE ON NON-ROUTINES W/O 104619
- [SDR SCNA20260513196](https://openairdocs.org/sdr/SCNA20260513196.md): Girt Bar · no discrepancy · May 12, 2026 · N816SY · Boeing 7378Q8 · Emergency Equipment
  > FA REPORTS DIFFICULTY WITH UNSEATING FWD ENTRY GIRT BAR FROM HANGER DURING ARMING PROCEDURE - - REMOVED AND INSTALLED GIRT BAR SMOOTH OPERATION IAW AMM 25-66-01
- [SDR SCNA20260102001](https://openairdocs.org/sdr/SCNA20260102001.md): Switch · broken · Dec 31, 2025 · N816SY · Boeing 7378Q8 · Emergency Lighting
  > EMERGENACY EXIT LIGHT SWITCH IN COCKPIT HAS BROKEN BLACK SWITCH GUARD. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH GAURD IAW AMM 33-51-00.
- [SDR SCNA20251212483](https://openairdocs.org/sdr/SCNA20251212483.md): Light · unsecure · Dec 12, 2025 · N816SY · Boeing 7378Q8 · Emergency Lighting
  > ROW 12 ABC EMERGENCY FLOOR LIGHTING STRIP NEEDS TO BE RESECURED TO FLOOR
- [SDR SCNA20250828341](https://openairdocs.org/sdr/SCNA20250828341.md): Strip · unsecure · Aug 25, 2025 · N816SY · Boeing 7378Q8 · Fuselage Miscellaneous Structure
  > FLOOR STRIP IN FWD GALLEY BETWEEN NICKLE BOARD AND AISLE RUNNER DAMAGED, TRIP HAZARD. REPLACED STRIP BETWEEN NICKLE BOARD AND AISLE RUNNER IAW AMM25-27-15 OK FOR SVC
- [SDR SCNA20250807296](https://openairdocs.org/sdr/SCNA20250807296.md): Door · stuck · Aug 2, 2025 · N816SY · Boeing 7378Q8 · Fixed Inner Doors
  > FWD GALLEY EMERGENCY EQUIPMENT DOOR STUCK CLOSED- PUSHED IN TO FAR. UNJAMMED DOOR OPERATED NORMALLY. OK FOR SERVICE REF AMM 25-24-15
- [SDR SCNA20250618218](https://openairdocs.org/sdr/SCNA20250618218.md): Bracket · out of adjust · Jun 17, 2025 · N816SY · Boeing 7378 · Emergency Equipment
  > DEFECT 814016: GIRT BAR BRACKETS STIFF ON L1 AND R1 DOORS. ADJUSTED GIRT BAR BRACKETS AND OPS CHECKS GOOD REF AMM 25-66-01.
- [SDR SCNA20250611204](https://openairdocs.org/sdr/SCNA20250611204.md): Bracket · loose · Jun 10, 2025 · N816SY · Boeing 7378Q8 · Emergency Equipment
  > DEFECT 814002: BOTH FOWARD DOOR GIRT BAR BRACKETS LOOSE - RESOLUTION: ADJUSTED L1 AND R1 GIRT BAR BRACKETS REF AMM 25-66-01. OK FOR SERVICE
- [SDR SCNA20250423121](https://openairdocs.org/sdr/SCNA20250423121.md): Door · open · Apr 16, 2025 · N816SY · Boeing 7378Q8 · Accessory Compartment Doors
  > LOUD VIBRATION HEARD AFTER TAKEOFF SUSPECTED GROUND CREW HEADSET AUDIOPANEL DOOR WAS LEFT OPEN OR CAME OPEN. - RESOLUTION: GROUND CREW REPORTED GROUND SERVICE DOOR OPEN ON TAXI IN. INSPECTED DOOR PER AMM52-49-02 OK FOR SERVICE.
- [SDR SCNA20250408107](https://openairdocs.org/sdr/SCNA20250408107.md): Skirt · out of position · Apr 7, 2025 · N816SY · Boeing 7378Q8 · Escape Slide
  > WORK ORDER 94406, NR00009: AFT GALLEY ENTRY DOOR, ESCAPE SLIDE SKIRT EXTENDS MORE THAN 10 INCHS AT BOTTOM OF DOOR AND CATCHES ON DOOR SILL. - RESOLUTION: REPOSITIONED SKIRT PER AMM REF 25-66-00,
- [SDR SCNA20250321079](https://openairdocs.org/sdr/SCNA20250321079.md): Light · loose · Mar 21, 2025 · N816SY · Boeing 7378Q8 · Emergency Lighting
  > SCNA20250321079 DEFECT 712156 AC 816: EXIT PATH FLOOR LIGHTING IS LOOSE NEAR 2 DEF. SECURED EXIT PATH FLOOR LIGHTING AT ROW 2 DEF REF AMM 35-27-31
- [SDR SCNA20250110010](https://openairdocs.org/sdr/SCNA20250110010.md): Light · detached · Jan 10, 2025 · N816SY · Boeing 7378Q8 · Emergency Lighting
  > DEFECT 794782: AC RIGHT ROW 12 EMERGENCY TRACK LIGHTING SEPERATING FROM FLOOR. RESOLUTION: RESECURED EMER. TRACK LIGHTING REF AMM 33-51-16.
- [SDR SCNA20250807302](https://openairdocs.org/sdr/SCNA20250807302.md): Rib · cracked · Nov 23, 2024 · N816SY · Boeing 7378Q8 · Horizontal Stabilizer, Spar/Rib
  > CRACKS ON RIB STAB STA= 249.10 AT RH HORIZONTAL STABILIZER. CRACKS ON RIB STAB STA= 249.10 AT RH HORIZONTAL STABILIZER WERE REPAIRED PER ETI-737-24-176 REV 4 AND ENG-55SCA-11502.
- [SDR SCNA20241125376](https://openairdocs.org/sdr/SCNA20241125376.md): Wire · arced · Nov 22, 2024 · N816SY · Boeing 7378Q8 · Window System Wiring
  > WORKORDER 80746, NON-ROUTINE 00004: INITIAL INSPECTION: SIGN OF ARCING ON BRAID WIRE UPPER EDGE OF WINDOW 1 RH AT FLIGHT COMPARTMENT.
- [SDR SCNA202405207240](https://openairdocs.org/sdr/SCNA202405207240.md): Bumper · broken · May 13, 2024 · N816SY · Boeing 7378Q8 · Escape Slide
  > DOOR 2L SLIDE BUMPER PART BROKE OFF SLIDE BUMPER. (OPEN)
- [SDR SCNA202405170236](https://openairdocs.org/sdr/SCNA202405170236.md): Bumper · broken · May 7, 2024 · N816SY · Boeing 7378Q8 · Passenger/Crew Doors
  > : DOOR 2L SLIDE BUMPER PART BROKE OFF SLIDE BUMPER - - RESOLUTION: (OPEN DEFECT)
- [SDR SCNA20240429222](https://openairdocs.org/sdr/SCNA20240429222.md): Slide · dislodged · Apr 28, 2024 · N816SY · Boeing 7378Q8 · Escape Slide
  > DOOR 1L SLIDE DROPPED OUT OF CASEING WHILE DOOR WAS BEING OPENED. REINSTALLED SLIDE PACK AND COVER 1L DOOR REF AMM 25-66-01.
- [SDR SCNA20240206029](https://openairdocs.org/sdr/SCNA20240206029.md): Bracket · out of adjust · Feb 4, 2024 · N816SY · Boeing 7378Q8 · Emergency Equipment
  > GIRT BAR ON MAIN DOOR LOOSE FALLS OUT. ADJUSTED TENSION ON GRIT BAR HOLD BRACKET REF AMM 25-66-02.
- [SDR SCNA20230202052S](https://openairdocs.org/sdr/SCNA20230202052S.md): Not Entered · not entered · Feb 1, 2023 · N816SY · Boeing · Landing Gear Retraction/Extension System
  > SCNA20230202052 SUPPLEMENT
- [SDR SCNA20230202052](https://openairdocs.org/sdr/SCNA20230202052.md): Not Entered · not entered · Feb 1, 2023 · N816SY · Boeing 7378Q8 · Landing Gear Retraction/Extension System
  > DEFECT 756124: NOSE GEAR CAME DOWN ON THE AFTER TAKEOFF CHECKLIST. NOSE GEAR LIGHT DISPLAYED RED THEN ONLY GREEN. LANDING GEAR DISAGREE CHECKLIST/QRH COMPLETE. RESOLUTION: PERFORMED FIM TASK 32-09 # PSEU BITE-NO FAULTS. JACKED A/C PERFORMED GEAR SWING RE
- [SDR SCNA20221011127](https://openairdocs.org/sdr/SCNA20221011127.md): Oven · smoke · Oct 10, 2022 · N816SY · Boeing 7378Q8 · Buffet/Galleys
  > DEFECT 725184: OVEN SMOKING WHILE COOKING SMELLS ELECTRICAL. RESOLUTION: CATERING REPLACED OVEN RACKS AND INSERT WITH CLEAN UNITS OPS CHECK GOOD IAW AMM 25-30-61 NO ELECTRIC SMELL NOTED.
- [SDR SCNA20220926110](https://openairdocs.org/sdr/SCNA20220926110.md): Hmu · faulted · Sep 22, 2022 · N816SY · Boeing 7378Q8 · Fuel Controlling System
  > NR 2 ENGINE HIGH VIB (MORE THAN 4.0) AND MOMENTARY SURGE. PERFORMED BORESCOPE OF #2 ENGINE BOOSTER SECTION AND LPT BLADES REF. AMM 72-00-00-200-803-F00, AND AMM 72-00-00-200-808-F00. NO DEFECTS FOUND. REMOVED #2 ENG SPINNER CONES PER AMM 72-21-01, AND RE
- [SDR SCNA20221003112](https://openairdocs.org/sdr/SCNA20221003112.md): Battery · inoperative · Jun 1, 2022 · N816SY · Boeing 7378 · Emergency Lighting
  > DEFECT WORK ORDER N/R-00016: EMERGENCY BATTERY AT M1694 INOP RESOLUTION: REMOVED, REPLACED AND TESTED EMERGENCY BATTERY AT M1694 IAW AMM B737 33-51-06-960-805, TEST GOOD. 59705C 08JUN22
- [SDR SCNA20220414026](https://openairdocs.org/sdr/SCNA20220414026.md): None · none · Mar 17, 2022 · N816SY · Boeing 737 · Emergency Lighting
  > DEFECT: AT ROWS 10 AND 11, LUMINESCENT LIGHT STRIP IS LOOSE RESOLUTION: REINSTALLED EMERGENCY FLOOR PATH STRIP REF. AMM 33-51-16.
- [SDR SCNA20220427040](https://openairdocs.org/sdr/SCNA20220427040.md): Girt Bar · loose · Feb 25, 2022 · N816SY · Boeing 7378Q8 · Escape Slide
  > L2 GIRT BAR HOLDER LOOSE. RESOLUTION: ADJUSTED HOLDER REF AMM 25-66-00
- [SDR SCNA202217003](https://openairdocs.org/sdr/SCNA202217003.md): None · none · Feb 12, 2022 · N816SY · Boeing 7378Q8 · Fuselage Structure (General)
  > DEFECT SECTION 43 FUSELAGE SKIN GOUGED FROM BS414 TO BS438 AT S-20R. RESOLUTION: DAMAGE WAS TRIMMED OUT FROM BS414 TO BS438 AT STRINGER 20R. STRINGER 20R WAS FOUND CRAKCED ATHE THE AFT THREE FASTENER HOLES WHICH WAS TRIMMED AND REPAIRED. A REPLACEMENT STRING
- [SDR SCNA20220217001](https://openairdocs.org/sdr/SCNA20220217001.md): None · none · Feb 12, 2022 · N816SY · Boeing 7378Q8 · Fuselage Main, Plate/Skin
  > TASK: TEMPORARY SKIN REPAIR INSTALLED STA 420 STR 20R. RESOLUTION: REMOVED TEMPORARY SKIN REPAIR AT BS 420 STR 20 AND INSTALLED 1 DOUBLER 2024-T3.063", -2 TRIPLER 2020-T3.063" AND -3 FILLER 2024-T3.090" IAW SUN COUNTRY ENGINEERING TASK CARD ENG-53SCA-1091
- [SDR SCNA20211208099SU](https://openairdocs.org/sdr/SCNA20211208099SU.md): Wire · chafed · Dec 5, 2021 · N816SY · Boeing 7378 · Flight Control System Wiring
  > VERIFY THE WIRE INTEGRITY AT THE BELOW LISTED CONNECTORS AND MEGGER THE WIRING LOOKING FOR SHORTS. WHILE USING THE MEGGER METER. FOUND 3 TWISTED SHIELDED PAIR WIRES AFFECTED. JUST INBD FROM #4 CANOE ON RT WING. WIRES THAT WHERE CHAFFED WHERE W1032-2006-R2, W1
- [SDR SCNA20211208099](https://openairdocs.org/sdr/SCNA20211208099.md): Sensor · faulted · Dec 5, 2021 · N816SY · Boeing 7378 · Leading Edge Slat Position Indicating System
  > DEFECT: HAD TRAILING EDGE FLAP DISAGREE ON APPROACH AFTER VECTORS INDICATED 0 WHEN LEVER SAET AT 15 RAN QRH THEN RECEIVED ASYMETRY RAN QRH AND LANDED RESOLUTION: PERFORMED FIM 27-51 TASK 801. FOUND FAULT 27-53280 R28VAC EXC INV. FOUND RT SKEW AND IND BREAKER
- [SDR SCNA20211208098](https://openairdocs.org/sdr/SCNA20211208098.md): Sensor · faulted · Nov 24, 2021 · N816SY · Boeing 7378 · Trailing Flap Position Indicating System
  > DEFECT: ON DEPARTURE THE FLAPS WOULD NOT RETRACT, PER QRH ALTERNATE FLAP EXTENSION WAS ATTEMPTED IMEDIATELY A TRAILING EDGE ASSYMETRY DEVELOPED ALT FLAP EXTENSION WAS STOPPED FLIGHT LANDED FLAPS 5 NOTIFIED MC RESOLUTION: PERFORMED FIM 27-59 TASK 807. FOUND #
- [SDR SCNA20211124097](https://openairdocs.org/sdr/SCNA20211124097.md): Circuit Breaker · tripped · Nov 24, 2021 · N816SY · Boeing 7378 · Trailing Edge Flap Control System
  > ON ARRIVAL FLAPS FAILED TO EXTEND. PER THE QRH ALETERNATE FLAP EXTENISON WAS ATTEMPTED. LEADING EDGE DEVICES EXTENTED BUT TRAILING EDGE FLAPS DID NOT. NOTIFIED MC SR 8092. PERFORMED FIM 27-51 TASK 801 FOUND FAULT 27-53280 AND FOUND C/B P6-2 (A11) POPPED RES
- [SDR SCNA20211018084](https://openairdocs.org/sdr/SCNA20211018084.md): None · none · Oct 14, 2021 · N816SY · Boeing 7378Q8 · Landing Gear Door Retract Section
  > DEFECT: LANDING GEAR LEVER WILL NOT MOVE UP AFTER TAKEOFF RESOLUTION: FOUND GROUND SPOILER INTERLOCK VALVE LOWER SLIDER ASSY. DISCONNECTED. CONEECTED LOWER SLIDER ASSY SLEEVE AND SAFTIED IAW AMM 27-62-51. ADJUSTMENT AND FUNCTIONAL CHECK GOOD. ACCOMPLISHED G
- [SDR SCNA2020031911013](https://openairdocs.org/sdr/SCNA2020031911013.md): Crease Beam · corroded · Mar 11, 2020 · N816SY · Boeing 7378BK · Fuselage Main, Structure
  > CORROSION ON SEVERAL POINTS AT LH CREASE BEAM WL 208 FROM STA 968 TO STA 1016 REMOVED AND REPLACED ON BS 1016 TO 900 LH CREASE BEAM PER B737-800 SRM 51-40-02.
- [SDR SCNA2020031903012](https://openairdocs.org/sdr/SCNA2020031903012.md): Floorbeam · corroded · Mar 8, 2020 · N816SY · Boeing 7378BK · Fuselage Main, Floor Beam
  > CORROSION ON TCAP AT STA 986.5 FROM BL 0 TO BL 45L.REMOVED CORROSION ON T CAP BS986BL0TO BL45L FOUND TO BE OUT OFF LIMITS REPLACED T CAP PER WORK ORDERR 3500849/2400/0002
- [SDR SCNA2020031916003](https://openairdocs.org/sdr/SCNA2020031916003.md): Stringer · corroded · Feb 16, 2020 · N816SY · Boeing 7378Q8 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND AT AFT CARGO, AFT BULKHEAD UNDER WATER TANK.REPAIRED STRINGER CORROSION IN AFT CARGO UNDER WATER TANK PER B737-800 SRM 53-00-03 FIG 201 REINSTALLED WATER TANK IAW AMM 38-11-01-400-801.
- [SDR SCNA2020031915042](https://openairdocs.org/sdr/SCNA2020031915042.md): Rib · damaged · Feb 15, 2020 · N816SY · Boeing 7378BK · Wing, Rib/Bulkhead
  > LEFT WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB TURNBUCKLE LUG DAMAGED REPAIRED L/H WING I/B FIXED F/E DEFLECTION CONTROL RIB PER B737-800 SRM 57-51-02-2R REP 2
- [SDR SCNA2020031914018](https://openairdocs.org/sdr/SCNA2020031914018.md): Crease Beam · corroded · Feb 14, 2020 · N816SY · Boeing 7378BK · Fuselage Main, Structure
  > CORROSION ON SEVERAL POINTS AT R1 DOOR CREASE BEAM BTW STA 328 TO STA 291.5REMOVED AND REPLACED R1 DOOR CREASE BEAM AT STA 328 TO STA 291.5 ALL WORK DONE IAW B737-800 SRM 51-70-02, SRM 51-40-02 SRM 51-40-05 AND AMM 53-11-01
- [SDR SCNA2020031914004](https://openairdocs.org/sdr/SCNA2020031914004.md): Counterbalance · corroded · Feb 14, 2020 · N816SY · Boeing 7378Q8 · Rudder Structure
  > RUDDER COUNTER BALANCE HAS EVIDENCE OF CORROSION.REMOVED AND REPLACED RUDDER COUNTER BALANCE WEIGHT IAW B737 SRM 51-40-02 REFER TO NR 3500849/3000/0009 FOR BALANEC REQUIREMENTS.
- [SDR SCNA2020031913041](https://openairdocs.org/sdr/SCNA2020031913041.md): Channel · corroded · Feb 13, 2020 · N816SY · Boeing 7378BK · Fuselage Miscellaneous Structure
  > RAIL CHANNELS AT ST 767 LBL 3.0, LBL 8.1, LBL 12.5 AND LBL 17.24 HAVE SURFACE CORROSION AFT CARGO BAY REPAIRED RAIL CHANNELS AT ST 767, LBL 3.0, LBL 8-1, LBL 12.5 AND LBL 17-24, ALL WORK DONE IAW B737-800 SRM 51-10-02 STEP 15, SRM 53-00-53 REP 3 TABLE 202 ALTE
- [SDR SCNA2020031913038](https://openairdocs.org/sdr/SCNA2020031913038.md): Frame · corroded · Feb 13, 2020 · N816SY · Boeing 7378BK · Fuselage Main, Frame
  > SURFACE CORROSION ON 3 EA FRAME ON COMPARTMENT FLOOR AT ST 767 REPAIRED 3EA CHANNEL FRAMES ON AFT COMPARTMENT AT S-1 767 ALL WORK DONE IAW B737-800 SRM 51-10-02, STEP 15, SRM 53-00-53 REP 3 TABLE 202 ALTERNATIVE 3, SRM 53-00-53 ALLOWABLE DAMAGE 2 AMM 51-21-41
- [SDR SCNA2020031913006](https://openairdocs.org/sdr/SCNA2020031913006.md): Channel · corroded · Feb 13, 2020 · N816SY · Boeing 7378BK · Fuselage Miscellaneous Structure
  > CORROSION ON Z CHANNEL BTW STA 986.5 AND STA 1006 AT BL 40R WL 208.REMOVED AND REPLACED Z CHANNEL ON BS986.5 AND 1006. AT BL 40 WLZ08. PER B737-800 SRM 51-40-02.
- [SDR SCNA2020031913005](https://openairdocs.org/sdr/SCNA2020031913005.md): Floorbeam · corroded · Feb 13, 2020 · N816SY · Boeing 7378Q8 · Fuselage Main, Floor Beam
  > CORROSION ON TCAP OF BEAM STA 986.5 FROM BL 0 TO BL 45R WL 208 REMOVED AND REPLACED TCAP ON BS 986.TO RBL 45 TO LBL 45, PER B7374 800 SRM 53-10-51 REP 4.
- [SDR SCNA2020031909023](https://openairdocs.org/sdr/SCNA2020031909023.md): Insert · damaged · Feb 9, 2020 · N816SY · Boeing 7378BK · Fuselage Floor Panel
  > MULTIPLE CORRODED INSERTS ON FLOOR PANEL 242 UF REMOVED AND REPLACED INSERTS ON FLOOR PANEL 242UF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2) SEE ARR-ASR FORM SHOP TRAVELLER FOR WORK PERFORMED.
- [SDR SCNA2020031908040](https://openairdocs.org/sdr/SCNA2020031908040.md): Door Frame · cracked · Feb 8, 2020 · N816SY · Boeing 7378BK · Fuselage Main, Structure
  > R1 DOOR CUT OUT FRAME LOWER SIDE FWD IS CRACK. REMOVED AND INSTALLED R1 DOOR FRAME IAW B737-800 SRM 51-40-02 STEP 4 AND 7.
- [SDR SCNA2020031908039](https://openairdocs.org/sdr/SCNA2020031908039.md): Scuff Plate · cracked · Feb 8, 2020 · N816SY · Boeing 7378BK · Fuselage Miscellaneous Structure
  > R1 SCUFF PLATE HAS A CRACK ON THE PLATE.R1 SCUFF PLATE P/N 141A8431-1 REPAIRED ON REPAIR ORDER 412614 IAW BAC5975 REV (N) DATED 12 SEP 2019 8130-3 FORM TRACKING 201076

Next page: https://openairdocs.org/aircraft/N816SY/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 = 'N816SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N816SY/reports

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