# Service difficulty reports: N76503

A list on [N76503](https://openairdocs.org/aircraft/N76503.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR CALA2026062517348](https://openairdocs.org/sdr/CALA2026062517348.md): Bulb · burned out · Jun 23, 2026 · N76503 · Boeing 737824 · Trailing Flap Position Indicating System
  > LE FLAPS TRANSIT LIGHT ON AT FLAPS 10. LIGHT WENT GREEN AT FLAP S 15. PERFORMED OPS TEST REF FIM TASK 27-51 TASK 801 AND AMM TASK 27-81-00-860-801, ALSO FOUND 1 L/ E FLAP TRANSIT LIGHT BULB WAS BURNED OUT AND REPLACED CYCLE THE FLAP AND SLAT FOUND NO FAULT
- [SDR CALA2026020413544](https://openairdocs.org/sdr/CALA2026020413544.md): Access Door · missing · Jan 31, 2026 · N76503 · Boeing 737824 · Fluid Service Doors
  > FOUND WASTE SERVICE ACCESS PANEL COMPLETELY MISSING. APPLIED CDL 52D ON WASTE SERVICE PANEL. CDL 52D SDR REQUIRED INSPECTED WASTE SVC PNL AREA, NO FURTHER DAMAGE FOUND. APPLIED CDL 52D ON WASTE SVC PNL. INSTALLED PLACARD. C/W DDP INSTALLED NEW WASTE TANK SER
- [SDR CALA2026011913069](https://openairdocs.org/sdr/CALA2026011913069.md): Slide · unraveled · Jan 16, 2026 · N76503 · Boeing 737824 · Escape Slide
  > R1 DOOR SLIDE PACK FABRIC BY GIRT BAR DRAGS ON GALLEY FLOOR. REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-66-01.
- [SDR CALA2025110410872](https://openairdocs.org/sdr/CALA2025110410872.md): Slide · unraveled · Nov 3, 2025 · N76503 · Boeing 737824 · Escape Slide
  > SLIDE AT DOOR 1R SLIDE IS UNRAVELED AND BAR HANGING DOWN AND BAR HANGING DOWN CHK 1R SLIDE. GIRT FABRIC INPLACE WITH NORMAL FOLDS WITHIN LIMITS PER AMM 25-66-01. 1R DOOR OPERATES AND ARMS NORMALY, FABRIC NOT DRAGGING.AC OK TO CONTINUE.
- [SDR CALA2025090808595](https://openairdocs.org/sdr/CALA2025090808595.md): Control Lever · faulted · Sep 4, 2025 · N76503 · Boeing 737824 · Landing Gear Selector
  > LANDING GEAR HANDLE WOULD NOT MOVE FULLY TO THE UP POSITION. FIRE EXTINGUISHER FELL OFF WALL DURING PUSHBACK (PROBABLY CAUSING ALT EXT DOOR TOO POP NOT CLOSED). FOUND ALT EXT DOOR NOT CLOSED AND DEBRIS UNDER DOOR. PSEU BITE SHOWS NO CURRENT FAULTS OR FAULT
- [SDR CALA2025071006433](https://openairdocs.org/sdr/CALA2025071006433.md): Door · out of adjust · Jul 8, 2025 · N76503 · Boeing 737824 · Service Doors
  > FWD SERVICE DOOR LIGHT ILLUMINATED 5 TIMES IN FLIGT W/ASSOCIATED HANDLE MOVEMENT OF 4IN ADJUSTED R1 GALLEY SERVICE DOOR PER AMM 52-41-00-820-801 STEPS N- LATCH ADJUSTMENT, O-HORIZONTAL CONTROL ROD ADJUSTMENT, Q-STOP PIN ADJUSTMENT. ADJUSTED SOFT UNLATCHING PER
- [SDR CALA2025070706259](https://openairdocs.org/sdr/CALA2025070706259.md): Skin · corroded · Jul 2, 2025 · N76503 · Boeing 737824 · Fuselage Main, Plate/Skin
  > LAV PAN SERVICE PANEL SKIN STRUCTURE AROUND PAN HAS SIGNS OF CORROSION AT HYLOCK AREA, REF 002741809 FUSELAGE SKIN AT LAVATORY SERVICE PAN BS 847-867 AT S-25L REPAIRED PER ECRA -5331-03169 REF BAM N/R002731809 FOR WORKED PERFORMED AND REQUIRED INSPECTION SIGN
- [SDR CALA2025062005737](https://openairdocs.org/sdr/CALA2025062005737.md): Battery Pack · malfunctioned · Jun 20, 2025 · N76503 · Boeing 737824 · Emergency Lighting
  > 3 EMERGENCY LIGHT CIRCUIT SECTIONS FAILED TO STAY ON PAST 15 MIN FOR EMERGENCY LIGHTING FUNCTIONAL CHECK AFFIILATED WITH EMER BATTERY PACKS M1694, M1670, M1673. BATTERY PACKS M1694, M1670, M1673 FAILED DURING EMERGENCY LIGHT SYSTEM OPERATIONAL CHECK 29-3350-1-
- [SDR CALA2025070306201](https://openairdocs.org/sdr/CALA2025070306201.md): Skin · cracked · Jun 14, 2025 · N76503 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > C- SCAN INSPECTION REF NDT PART 6-55-10-01, RT HORIZONTAL FOUND CRACK ON LOWER SKIN AT STATION 175.50 AND 26" FROM FRONT SPAR REF GMM 04-20-05. REPAIRED RH STAB LOWER SKIN CRACK AT STA 175.50 PER SRM 55-10-01 -2R-11.
- [SDR CALA2025070306200](https://openairdocs.org/sdr/CALA2025070306200.md): Skin · cracked · Jun 14, 2025 · N76503 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > TWO CRACKS FOUND AT APPROXIMATED STAB STA 120.30 ON LT STAB LOWER SKIN. EXISTING REPAIR DOUBLER ON ELB 9846823 WILL BE INCORPORATED INTO THIS REPAIR DOUBLER. MAJOR REPAIR, REPAIRED LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKS AT STA 120.3 PER SRM 55-10
- [SDR CALA2025070306199](https://openairdocs.org/sdr/CALA2025070306199.md): Skin · cracked · Jun 13, 2025 · N76503 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACKS LOCATED ON RT HORIZONTAL STAB LOWER SKIN 2 CRACKS AT STAB STA 120.30,2 CRACKS AT STAB STA 129.50. REPAIR DOUBLER FROM ELB 9846818 WILL BE INCROPERATED INTO THIS REPAIR DOUBLER. MAJOR REPAIR, REPAIRED RT STAB LOWER SKIN CRACKS AT STA 120.30-STA 129.5
- [SDR CALA2025032603213](https://openairdocs.org/sdr/CALA2025032603213.md): Lamp · inoperative · Mar 25, 2025 · N76503 · Boeing 737824 · Emergency Lighting
  > R/H FORWARD SLIDE/OVERWING EMERGENCY LIGHT INOP. R/H FWD SLIDE/OVERWING EMERGENCY LIGHT LAMP REPLACED REF AMM 33-51-04-960-801; OPS CHECK GOOD.
- [SDR CALA2024102400920](https://openairdocs.org/sdr/CALA2024102400920.md): Engine · overheated · Oct 21, 2024 · N76503 · Boeing 737824 · Engine (Turbine/Turboprop)
  > R ENG OVERHEAT ON GND BEFORE T/O SHUT DOWN ENG HAD CFR INSPECT AND TAXIED BACK. REMOVED AND REPLACED #2 ENGINE IAW 71-00-02-400-801-F00,ACCOMPLISHED 5 MINUTE ENGINE IDLE RUN ALL SYSTEMS TEST NORMAL, SERVICED ALL FLUIDS TO NORMAL LEVELPARTS USED: 57-5452-3-0
- [SDR CALA2023072802362](https://openairdocs.org/sdr/CALA2023072802362.md): Charger · faulty · Jul 25, 2023 · N76503 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT LIGHT AT DOOR 2L IS ILLUMINATED. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID V941599 MAC RELATED WORK ORDER 000000003081439 AND PRTR MILLER, DYLAN (V941599)
- [SDR CALA2022100702732](https://openairdocs.org/sdr/CALA2022100702732.md): Battery Pack · inoperative · Oct 6, 2022 · N76503 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS OP CHECK FAILED ON POSITIONS M01674, M01675, M0 1695 (REF AAR NR 99944572
- [SDR CALA2022100702731](https://openairdocs.org/sdr/CALA2022100702731.md): Battery Pack · inoperative · Oct 6, 2022 · N76503 · Boeing 737824 · Emergency Lighting
  > REMOVE AND REPLACE EMERGENCY LIGHT BATTERY PACKS, FOR SCEPTRE TR ACKING ONLY (REF AAR NR 99944576)
- [SDR CALA2022100702730](https://openairdocs.org/sdr/CALA2022100702730.md): Battery Pack · inoperative · Oct 6, 2022 · N76503 · Boeing 737824 · Emergency Lighting
  > REMOVE AND REPLACE EMERGENCY LIGHT BATTERY PACKS, FOR SCEPTRE TR ACKING ONLY (REF AAR NR 99944575)
- [SDR CALA2022091602378](https://openairdocs.org/sdr/CALA2022091602378.md): Beam · corroded · Sep 15, 2022 · N76503 · Boeing 737 · Fuselage Main, Structure
  > AFT PASSENGER COMPARTMENT WWET AREA:POSSIBLE CORROSION POINTS ON FLOOR BEAM STA. 986.5IN LBL 27,LBL35 AND LBL43 (REF AAR NR 99944 132) PERFORMED REPAIR AT STA 986.5 IAW B737-800 SRM 53-70-51-2R-4, SR M 51-10-02, SRM 51-40-02, SOPM 20-10-03, AMM 51-21-41-370-80
- [SDR CALA2022091402373](https://openairdocs.org/sdr/CALA2022091402373.md): Skin · corroded · Sep 13, 2022 · N76503 · Boeing 737 · Fuselage Structure (General)
  > WASTE TANK CUT OUT VENT HAS CORROSION (REF. AAR NR 99944029). REPAIRED WASTE TANK CUT OUT VENT IAW B737-800 SRM 53-70-01-2R RE PAIR 3 STEP 4 (WORK ACCOMPLISHED BY V940417 AND AAR QC A-76 V920 285). PER SRM 53-70-01-2R REPAIR 3 STEP PERFORM LFEC EVERY 5000FC BE
- [SDR CALA2022090902314](https://openairdocs.org/sdr/CALA2022090902314.md): Waste Tank · none · Sep 9, 2022 · N76503 · Boeing 737 · Fuselage Structure (General)
  > WASTE TANK CUT OUT VENT HAS CORROSION (REF. AAR NR 99944029). REPAIRED WASTE TANK CUT OUT VENT IAW B737-800 SRM 53-70-01-2R RE PAIR 3 STEP 4 (WORK ACCOMPLISHED BY V940417 AND AAR QC A-76 V920 285). PER SRM 53-70-01-2R REPAIR 3 STEP PERFORM LFEC EVERY 5000FC BE
- [SDR CALA2022051101201](https://openairdocs.org/sdr/CALA2022051101201.md): None · damaged · May 10, 2022 · N76503 · Boeing 737 · Lighting System
  > SEAT MOUNTED EMERGENCY LIGHT AT 31 ABC DAMAGED. REMOVED AND REPLACED WHITE EMERGENCY LIGHT REF MM 33-51-11. OPS CK OK. VERIFIED IDT REQUIREMENTS
- [SDR CALA2021111502107](https://openairdocs.org/sdr/CALA2021111502107.md): Light · inoperative · Nov 14, 2021 · N76503 · Boeing 737824 · Lighting System
  > EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK - FLOOR PROXIMITY LIGHTS DO NOT COME ON ROWS 22 TO 38 RPL BATTERY PACK AT POSITION AFT RIGHT, AND CENTER FLOOR MOUNT PER AMM 33-51-06-960-805. RPL POWER SUPPLY AT AFT RIGHT POSITION PER AMM 33-51-06-968-806. RPL FU
- [SDR CALA2021102501957](https://openairdocs.org/sdr/CALA2021102501957.md): None · damaged · Oct 24, 2021 · N76503 · Boeing 737824 · Hydraulic Power System
  > ENG 1 LOW PRESSURE LIGHT LIGHT ON PREVIOUS WRITEUP ENG 1 EVIDENCE FOUND EDP. DAMAGED PLEASE COMPLETE SDR BEFORE UNLOCKING THIS ITEM. TOMC MGR CASEY SETTING SDR FOR IRREGULARITY. FURTHER DETAILS AWAITED. PER LP 7300051 REPLACED EDP AT ENG 1 AS PER AMM 29-11-11/
- [SDR CALA2021102501959](https://openairdocs.org/sdr/CALA2021102501959.md): Engine · none · Oct 22, 2021 · N76503 · Boeing 737824 · Powerplant System
  > REFERENCE LOG PAGE 7284669: AFTER ENGINE 1 HYD LOW PRESS INDICATION IN CRUISE, ENGINE 1 OIL FILTER BYPASS SHOWED ON THE ENGINE DISPLAY. ENGINE WAS SHUT DOWN AS PRECAUTIONARY PER QRH PROCEDURE. OIL PSI AT SHUT DOWN WAS 70. WINDMILL TIME WAS 33 MINUTES. NO OIL Q
- [SDR CALA2019052000805](https://openairdocs.org/sdr/CALA2019052000805.md): Switch · dirty · May 20, 2019 · N76503 · Boeing 737824 · Landing Gear Position and Warning
  > AFTER T/O GEAR FAILED TO RETRACT CYCLED NO RETRACT RETURNED TO LAND SEE LOG PG 3247373 FOR SWITCG CLEANING. PERFORMED LANDING GEAR INDICATION AND WARNING SYSTEM TEST AND GEAR RETRACT PER AMM 32-61-00-710-801 AMM 32-09-00-840-801 AMM 07-11-01-580-815 AND AMM 07
- [SDR CALA2017111904151](https://openairdocs.org/sdr/CALA2017111904151.md): Wire Harness · loose · Nov 19, 2017 · N76503 · Boeing 737824 · Light System Wiring
  > EMERGENCY LIGHTS INOPERATIVE AT ROWS 15, 20 AND 23. CONNECTED THE LIGHT WIRE HARNESSES. OPS CHECKED OK.
- [SDR CALA2017101603645](https://openairdocs.org/sdr/CALA2017101603645.md): Sign · detached · Oct 16, 2017 · N76503 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT SIGN IN MID-CABIN CAME LOOSE, INSTALLED THE SIGN. TESTED OK IAW AMM 33-51-01-960-802, AND 33-51-00-720-801.
- [SDR CALA2017081802742](https://openairdocs.org/sdr/CALA2017081802742.md): Light · inoperative · Aug 18, 2017 · N76503 · Boeing 737824 · Emergency Lighting
  > OVERHEAD INTERIOR EMERGENCY LIGHT INOPERATIVE, ROW 7 CBA. REPLACED LIGHT ASSY. OPS CHECKED NORMAL.
- [SDR CALA2017081402700](https://openairdocs.org/sdr/CALA2017081402700.md): Charger · inoperative · Aug 14, 2017 · N76503 · Boeing 737824 · Emergency Lighting
  > OVERHEAD INTERIOR EMERGENCY LIGHTS INOPERATIVE, ROWS 12BCA AND 11FED. REPLACED EMERGENCY LIGHT CHARGER ASSEMBLY. OPS CHECKED GOOD IAW AMM 33-51-06-960-806.
- [SDR CALA2017051201405](https://openairdocs.org/sdr/CALA2017051201405.md): Cover · loose · May 12, 2017 · N76503 · Boeing 737824 · Emergency Equipment
  > 2 OVERWING EXIT SIGN COVERS HAVE COME OFF. INSTALLED 2 EA EMERGENCY EXIT SIGN COVERS ON MID CEILING AS REQUIRED.
- [SDR CALA2017042801149](https://openairdocs.org/sdr/CALA2017042801149.md): Engine · flamed out · Apr 28, 2017 · N76503 · Boeing 737824 · Engine (Turbine/Turboprop)
  > ENGINE FLAMEOUT, ENGINE RESTART NOT ATTEMPTED. RECORD ENGINE CONDITION. ENG1 FAILED DURING TAXI IN TO GATE IN MMUN DURING ENG2 SHUTDOWN. PERFORMED EEC 1 BITE TEST PER FIM 73-00-00-810-801-F00. SHOWING FAILURE MESSAGES 73-31441, 73-31351 & 74-30971. PERFORMED A
- [SDR CALA2016081200525](https://openairdocs.org/sdr/CALA2016081200525.md): Skin · gouged · Aug 12, 2016 · N76503 · Boeing 737824 · Fuselage Main, Plate/Skin
  > A MINOR GOUGE AT BS 847 - 852 BETWEEN STRINGERS 2L AND 2R. REPAIRED IAW ECRA 5331-02126.
- [SDR CALA2016081200524](https://openairdocs.org/sdr/CALA2016081200524.md): Floorbeam · corroded · Aug 12, 2016 · N76503 · Boeing 737824 · Fuselage Main, Floor Beam
  > FLOORBEAM BS 986, RBL 41 HAS CORROSION. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01935 AND SRM 53-70-51 REP 4.
- [SDR CALA2016081200519](https://openairdocs.org/sdr/CALA2016081200519.md): Floorbeam · corroded · Aug 10, 2016 · N76503 · Boeing 737824 · Fuselage Main, Floor Beam
  > FWD WET AREA FLOORBEAM CORRODED BS 328, RBL 11. REPAIRED THE FLOORBEAM IAW EC/RA 5321-01934.
- [SDR CALA2016080900507](https://openairdocs.org/sdr/CALA2016080900507.md): Skin · dented · Aug 6, 2016 · N76503 · Boeing 737824 · Fuselage Main, Plate/Skin
  > FWD CARGO DOOR CUTOUT UPPER FWD CORNER AT BS 450 3 X 1 BY 0.100 DEEP DENT. INSTALLED DOULBER REPAIR IAW SRM 53-00-01 REPAIR 21.
- [SDR CALA2016080900504](https://openairdocs.org/sdr/CALA2016080900504.md): Skin · cracked · Aug 5, 2016 · N76503 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION ON THE LT HORIZONTAL STAB HSS 101.90. 11 INCH FWD T/E. REPAIR IAW SRM 55-10-01 REPAIR 11
- [SDR CALA2016080900503](https://openairdocs.org/sdr/CALA2016080900503.md): Skin · cracked · Aug 5, 2016 · N76503 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION ON THE LH HORIZONTAL STAB HSS 157.10. 10 INCH FWD T/E. REPAIR IAW SRM 55-10-01 REPAIR 11
- [SDR CALA2016080900502](https://openairdocs.org/sdr/CALA2016080900502.md): Skin · cracked · Aug 5, 2016 · N76503 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION ON THE RT HORIZONTAL STAB HSS 101.90, 11 INCH FWD T/E. REPAIR IAW SRM 55-10-01 REPAIR 11.
- [SDR CALA2016080900501](https://openairdocs.org/sdr/CALA2016080900501.md): Skin · cracked · Aug 4, 2016 · N76503 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION ON THE RT HORIZONTAL STAB HSS 138.70. 18 INCH FWD T/E. REPAIR IAW SRM 55-10-01 REPAIR 11.
- [SDR CALA2016072100433](https://openairdocs.org/sdr/CALA2016072100433.md): Floorbeam · corroded · Jul 21, 2016 · N76503 · Boeing 737824 · Fuselage Main, Floor Beam
  > FOUND CORROSION AT FLOORBEAM BS 344 RBL 1. REPAIRED IAW SRM 53-00-53 REPAIR 1.
- [SDR CALA2014012200096](https://openairdocs.org/sdr/CALA2014012200096.md): Skin · cracked · Jan 21, 2014 · N76503 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STAB LOWER SKIN HAS A CRACK AT STATION 129.50 APPROXIMATELY 33 INCHES AFT FROM LE FRONT SPAR. CUT OUT DAMAGE, FABRICATED DOUBLER & INSTALLED REPAIR IAW SRM 55-10-01 REPAIR 11.
- [SDR CALA2013100400725](https://openairdocs.org/sdr/CALA2013100400725.md): Structure · damaged · Oct 2, 2013 · N76503 · Boeing 737824 · Fuselage Miscellaneous Structure
  > STRUCTURE UNDER LATCH PLATE FOR PNEUMATIC ACCESS DOOR 192DR OTBD FWD IS DAMAGED. REPAIRED IAW ECRA 5350-02119.
- [SDR CALA2013081900580](https://openairdocs.org/sdr/CALA2013081900580.md): Pump · failed · Aug 18, 2013 · N76503 · Boeing 737824 · Hydraulic Pump (Electric/Engine), Main
  > DURING CRUSE, SYS A ENG DRIVEN HYD LOW PRESSURE LIGHT ILLUMINATED COMPLIED WITH QRH. FOUND NR 1 ENGINE EDP FAILED. R & R 1 ENG EDP IAW 29-11-11.
- [SDR CALA2011080100524](https://openairdocs.org/sdr/CALA2011080100524.md): Skin · dented · Aug 1, 2011 · N76503 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > SUPPORT TASK - LEFT HORIZONTAL STABILIZER LEADING EDGE HAS MULTIPLE ABRASIONS, TOOLING MARKS, AND SMALL DENTS BETWEEN STA 271 AND 281. REMOVED AND REPLACED LEFT HORZ STAB L/E SKIN BETWEEN STA 271 AND 281 REF SRM 51-40-02.
- [SDR CALA2011072800518](https://openairdocs.org/sdr/CALA2011072800518.md): Intercostal · cracked · Jul 28, 2011 · N76503 · Boeing 737824 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED FWD CABIN FLOOR STRUCTURE BETWEEN STA 344-360 AT BL 0. REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 344-360 AT BL 0 REF SRM 51-40-02.
- [SDR CALA0700251](https://openairdocs.org/sdr/CALA0700251.md): Bulkhead · cracked · May 7, 2007 · N76503 · Boeing 737824 · Wing, Rib/Bulkhead
  > INSPECTION FOUND THE RIGHT WHEEL WELL FORWARD BULKHEAD (WING CENTER SECTION AFT SPAR VAPOR BARRIER) CRACKED. THERE WERE TWO CRACKS MEASURING 12.75 INCHES AND 8 INCHES. THE VAPOR BARRIER WAS REMOVED AND REPLACED IAW ECRA 5710-02116.
- [SDR CALA0700250](https://openairdocs.org/sdr/CALA0700250.md): Vapor Barrier · cracked · May 7, 2007 · N76503 · Boeing 737824 · Wing Main, Frame Structure
  > INSPECTION FOUND THE LEFT WHEEL WELL FORWARD BULKHEAD (WING CENTER SECTION AFT SPAR VAPOR BARRIER) CRACKED. THREE CRACKS WERE FOUND MEASURING 7 INCHES, 19.5 INCHES, AND 4 INCHES. THE VAPOR BARRIER WAS REMOVED AND REPLACED IAW ECRA 5710-02116.

## 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 = 'N76503' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N76503/reports

---
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