# Service difficulty reports: Boeing 737-282C

A list on [Boeing 737-282C](https://openairdocs.org/model/boeing-737-282c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 121 reports

- [SDR TSAA20130822007](https://openairdocs.org/sdr/TSAA20130822007.md): Clamp · failed · Aug 22, 2013 · N826AL · Boeing 737282C · Pneumatic Distribution System
  > DURING CLIMB, AT 3000 FT, CREW NOTICED THE LT WING TO BODY OVERHEAT WARNING LIGHT ILLUMINATED. AFTER 2 MINUTES, THE RT WING TO BODY OVERHEAT WARNING ALSO ILLUMINATED. RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED THE BLEED DUCT CLAMP AT THE KE
- [SDR TSAA20120713004](https://openairdocs.org/sdr/TSAA20120713004.md): Engine · power loss · Jul 13, 2012 · N826AL · Boeing 737282C · Engine (Turbine/Turboprop)
  > DURING TAKEOFF/CLIMB AT APPROXIMATELY 400 FEET, NR 2 ENGINE FAILURE/LOSS OF POWER WITH HEAVY VIBRATION. COMPLETED ENGINE FAILURE AND SHUTDOWN CHECKLIST. INFLIGHT EMERGENCY DECLARED. REPLACED NR 2 ENGINE. OPS AND LEAK CHECK GOOD.
- [SDR TSAA20120531002](https://openairdocs.org/sdr/TSAA20120531002.md): Frame · cracked · May 31, 2012 · N826AL · Boeing 737282C · Fuselage Main, Frame
  > CRACK APPROX 2.6250 FOUND AT BS 927, STRINGER 23L. REPAIR COMPLIED WITH IAW SRM 53-30-3, FIG 48, DETAIL XI.
- [SDR 7AHR201192030](https://openairdocs.org/sdr/7AHR201192030.md): Frame · cracked · Oct 16, 2011 · N826AL · Boeing 737282C · Fuselage Main, Frame
  > AFT PIT CRACKED, FRAME LOWER CHORD AT BS 907 AND STRINGER 26R.
- [SDR 7AHR2011092029](https://openairdocs.org/sdr/7AHR2011092029.md): Seat Track · cracked · Oct 8, 2011 · N826AL · Boeing 737282C · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK UPPER FLANGE CRACKED STATION 727B AT RBL 24.75
- [SDR 7AHR2011092028](https://openairdocs.org/sdr/7AHR2011092028.md): Floorbeam · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Floor Beam
  > UPPER FUSELAGE FLOOR STRUCTURE HEAVY AMOUNT OF CORROSION UNDER NUTLPLATE ON LOWER CHORD OF FLOORBEAM AT BS 787 AT RBL 24
- [SDR 7AHR2011092027](https://openairdocs.org/sdr/7AHR2011092027.md): Beam · elongated · Sep 23, 2011 · N826AL · Boeing 737282C · Wing, Landing Gear Attach Fittings
  > DURING THE ACCOMPLISHMENT OF ECO 3731 SB 737-57A-1266 INSPECTION OF THE MAIN LANDING GEAR BEAM TO WING ATTACH FITTINGS IT WAS DISCOVERED THAT THE MLG BEAM PIN RETAINER LOCK BOLT FITTING IS ELONGATED ON BOTH LT AND RT MLG BEAM.
- [SDR 7AHR2011092026](https://openairdocs.org/sdr/7AHR2011092026.md): Skin · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/Skin
  > AFT FUSELAGE HAS EVIDENCE PILLOWING (CORROSION) AT BODY STA 1016 AT STR 25L AND 24L AROUND FASTENERS.
- [SDR 7AHR2011092025](https://openairdocs.org/sdr/7AHR2011092025.md): Floor Support · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > AFT FUSELAGE CABIN FLOOR STURCTURE AT BODY STA 947 TO 967 AT LBL 12 HAS EVIDENCE OF CORROSION.
- [SDR 7AHR2011092024](https://openairdocs.org/sdr/7AHR2011092024.md): Floor Support · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > AFT BAGAGGE COMPARTMENT FLOOR SUPPORTS AT BODY STATION 770 AT SPLICE STRAP ATTACHED HAS SIGNS OF CORROSION
- [SDR 7AHR2011092023](https://openairdocs.org/sdr/7AHR2011092023.md): Transition Panel · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > AFT PIT TRANSITION PANEL CORRODED JUST AFT OF CARGO DOOR ON THE RT SIDE AT BODY STATION 887.
- [SDR 7AHR2011092022](https://openairdocs.org/sdr/7AHR2011092022.md): Skin · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/Skin
  > AFT FUISELAGE BODY STA 976.6 AT STRINGER 25L, EDGE OF WATER SERVICING DOOR HAS EVIDENCE OF CORROSION.
- [SDR 7AHR2011092021](https://openairdocs.org/sdr/7AHR2011092021.md): Stringer · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Longeron/Stringer
  > AFT BAGGAGE COMPARTMENT AT BODY STA 947.6, STRINGER 26L, HAS CORROSION OUT OF LIMITS.
- [SDR 7AHR2011092020](https://openairdocs.org/sdr/7AHR2011092020.md): Intercostal · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > AFT BAGGAGE COMPARTMENT INTERCOSTAL UPPER FLANGE CORRODED OUT OF LIMITS BETWEEN BODY STATION 767 AND 787 AT STRINGER 25R
- [SDR 7AHR2011092019](https://openairdocs.org/sdr/7AHR2011092019.md): Threshold · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > FORWARD FUSELAGE FLOOR STRUCTURE AT L1 DOOR CENTER THRESHOLD AREA HAS LIGHT CORROSION ON UPPER SURFACE STRUCTURE AND UNDER NUTPLATES
- [SDR 7AHR2011092018](https://openairdocs.org/sdr/7AHR2011092018.md): Floor Support · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > FORWARD CABIN FLOOR STRUCTURE HAS CORROSION ON FLOOR SUPPORT AT LBL 6 BETWEEN BODY STATION 294.5 AND 312.0.
- [SDR 7AHR2011092017](https://openairdocs.org/sdr/7AHR2011092017.md): Floor Support · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > AFT BAGGAGE COMPARTMENT FLOOR SUPPORT SPLICE PLATE HAS SIGNS OF CORROSION ON BOTTOM SIDE AT BODY STA 770.
- [SDR 7AHR2011092016](https://openairdocs.org/sdr/7AHR2011092016.md): Floor Support · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > CORROSION UNDER TIE DOWN AT STRINGER 26R AT SHEAR TIE FLOORBOARD SUPPORT AT BODY STATION 384.
- [SDR 7AHR2011092015](https://openairdocs.org/sdr/7AHR2011092015.md): Floorbeam · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Floor Beam
  > AFT FUSELAGE FLOOR STRUCTURE HAS CORROSION AT FLOOR SUPPORT BODY STA 957 BETWEEN RT SIDE OF SEAT TRACKS AT RBL 24 AND 45.
- [SDR 7AHR2011092014](https://openairdocs.org/sdr/7AHR2011092014.md): Floor Support · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > AFT FUSELAGE FLOOR STRUCTURE AT LT LAVATORY WALL, FLOOR IS CORRODED AT BODY STATION 947 TO 967.
- [SDR 7AHR2011092013](https://openairdocs.org/sdr/7AHR2011092013.md): Sill · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > FORWARD CABIN FLOOR STURCTURE AT BODY STATION 312 TO 344 AT MOP SILL HAS CORROSION AROUND FASTNER HOLES.
- [SDR 7AHR2011092012](https://openairdocs.org/sdr/7AHR2011092012.md): Floorbeam · corroded · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Floor Beam
  > FORWARD CABIN FLOOR STRUCTURE (FRAME) HAS CORROSION AT BODY STA 312 BETWEEN RBL 24 AND RBL 45.
- [SDR 7AHR2011092011](https://openairdocs.org/sdr/7AHR2011092011.md): Skin · cracked · Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/Skin
  > DURING THE ACCOMPLISHMENT OF ECO 3735, FORWARD ENTRY AND FORWARD GALLEY SERVICE DOORWAY UPPER AND LOWER HINGE CUTOUT INSPECTION, IT WAS DETERMINED THAT THE FORWARD ENTRY DOOR, LOWER HINGE CUTOUT HAS 1 EACH CRACKED FASTENER HOLE. CRACK IS IN THE LOWER B-5 HOLE
- [SDR 7AHR2011092010](https://openairdocs.org/sdr/7AHR2011092010.md): Skin · corroded · Sep 22, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/Skin
  > AFT PIT AT STATION 907 TO 929 AT STRINGER 26R HAS CORROSION AROUND FASTENER. FASTENERS ARE PULLING THROUGH.
- [SDR 7AHR2011092009](https://openairdocs.org/sdr/7AHR2011092009.md): Floor Support · corroded · Sep 22, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > AFT FUSELAGE FLOOR STRUCTURE HAS CORROSION ON FLOOR SUPPORT AT BODY STATION 955 INBD OF SEAT TRACK AT RBL 24.
- [SDR 7AHR2011092008](https://openairdocs.org/sdr/7AHR2011092008.md): Floor Support · corroded · Sep 22, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > AFT BAGGAGE COMPARTMENT FLOOR SUPORT AT RBL 8" HAS CORROSION THAT IS OUT OF LIMITS AT SPLICE STRAP BODY STA 770.
- [SDR 7AHR2011092007](https://openairdocs.org/sdr/7AHR2011092007.md): Skin · corroded · Sep 22, 2011 · N826AL · Boeing 737282C · Wing, Plate/Skin
  > CORROSION AROUND FASTNERS AT LT LOWER SURFACE OF WING AT STATION WRL 167 BEHIND FUEL ACCESS PANEL NR 7204.
- [SDR 7AHR2011092006](https://openairdocs.org/sdr/7AHR2011092006.md): Floor Support · corroded · Sep 22, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > AFT PIT FLOOR SUPPORT AT BODY STATION 770 HAS CORROSION AND WAS FOUND TO BE OUT OF LIMITS AT SPLICE STRAP
- [SDR 7AHR2011092005](https://openairdocs.org/sdr/7AHR2011092005.md): Angle · corroded · Sep 22, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > AFT FUSELAGE FLOOR STRUCTURE AT AFT LAVATORY FORWARD WALL AS CORROSION AT ATTACH ANGLE AT INBD FASTENER HOLE.
- [SDR 7AHR2011092004](https://openairdocs.org/sdr/7AHR2011092004.md): Skin · corroded · Sep 22, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/Skin
  > PILLOWING CORROSION AROUND FASTENERS AT BODY STA 787, STRINGER 27R.
- [SDR 7AHR2011092003](https://openairdocs.org/sdr/7AHR2011092003.md): Structure · corroded · Sep 22, 2011 · N826AL · Boeing 737282C · Fuselage Main, Structure
  > CORROSION UNDER FLOORBOARD SPLICE AT STA 464 BETWEEN STRINGER 27R AND 26R IN FORWARD PIT.
- [SDR 7AHR2011092001](https://openairdocs.org/sdr/7AHR2011092001.md): Skin · corroded · Sep 21, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/Skin
  > FUSELAGE LOWER LOBE AT BODY STATION 807 TO 827 AT STRINGER 26R TO 27R HAS EVIDENCE OF PILLOWING (CORROSION).
- [SDR 7AHR2011092002](https://openairdocs.org/sdr/7AHR2011092002.md): Access Panel · corroded · Sep 21, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/Skin
  > AFT FUSELAGE AT POTABLE WATER SERVICING PANEL HAS EVIDENCE OF CORROSION AROUND PANEL.
- [SDR TSAA2011F00203](https://openairdocs.org/sdr/TSAA2011F00203.md): Skin · corroded · Sep 20, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/Skin
  > FUSELAGE LOWER LOBE BETWEEN STA 827 AND 807 AT STRINGER 27R AND 26R HAS POSSIBLE PILLOWING AROUND FASTENERS (CORROSION).
- [SDR TSAA1126004](https://openairdocs.org/sdr/TSAA1126004.md): Connector · shorted · Apr 9, 2011 · N826AL · Boeing 737282C · Fire Protection System Wiring
  > DURING CRUSE FLIGHT, THE CREW NOTED THE NR1 ENGINE OVERHEAT WARNING LIGHT ILLUMINATED. THE CONDITION WAS INTERMITTENT AND EXTINGUISHED. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MX FOUND A SHORTED CONNECTOR IN THE LOWER FIRE AND OVERHEAT DETECTOR L
- [SDR TSAA1012020](https://openairdocs.org/sdr/TSAA1012020.md): Unknown · odor · Dec 19, 2010 · N826AL · Boeing 737282C · Air Distribution System
  > NON-ETOPS CARGO FLIGHT 25. UPON ARRIVAL, AN ELECTRICAL ODOR WAS REPORTED BY THE PILOT IN THE COCKPIT. MX INSPECTED COCKPIT AND FOUND NO DEFECTS OR ODORS. MX INSPECTED THE E & E BAY AND FOUND WATER IN THE BAY. ACFT WAS TOWED TO HANGAR, DRIED OUT, AND RETURN
- [SDR TSAA1053017](https://openairdocs.org/sdr/TSAA1053017.md): Stiffener · corroded · Oct 5, 2010 · N826AL · Boeing 737282C · Fuselage Miscellaneous Structure
  > WING CTR SECTION LOWER BEAM AT RBL 40.875 IS CORRODED AT BS 612 AND BS 630. MAINTENANCE ACTION: REPLACED ANGLE IN ACCORDANCE WITH SRM 51-10-1. CLEANED AND TREATED AFFECTED AREA IN ACCORDANCE WITH SRM 51-10-6 AND FOUND WITHIN LIMITS.
- [SDR TSAA1026012](https://openairdocs.org/sdr/TSAA1026012.md): Circuit Breaker · failed · Jun 15, 2010 · N826AL · Boeing 737282C · DC Power Distribution System
  > DURING CLIMB, THE CREW NOTED THE NR 2 TRANSFER BUS CIRCUIT BREAKER POPPED. CREW ATTEMPTED TO RESET WITHOUT SUCCESS. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX R & R THE NR 2 TRANSFER BUS CIRCUIT BREAKER (C821) AND OPERATIONALLY CHECKED SATISFACT
- [SDR TSAA1026011](https://openairdocs.org/sdr/TSAA1026011.md): Relay · failed · Jun 14, 2010 · N826AL · Boeing 737282C · DC Power Distribution System
  > NON-ETOPS CARGO FLIGHT 16. DURING CLIMB THE ACFT EXPERIENCED A NR2 BUS POWER FAILURE CAUSING THE LOSS OF USE OF ALL INSTRUMENTS AND SYS POWERED BY THE NR 2 BUS. CREW ACCOMPLISHED APPROPRIATE CHECK LISTS LANDED WITHOUT FURTHER INCIDENT. MX R & R THE NR2 TRAN
- [SDR TSAA0953011](https://openairdocs.org/sdr/TSAA0953011.md): Skin · cracked · Nov 23, 2009 · N841AL · Boeing 737282C · Fuselage Main, Plate/Skin
  > DURING SCHEDULED INSP A 3" CRACK WAS DISCOVERED AT BS 440, 450, S-16R FUSELAGE SKIN. REPAIRED SKIN BY REMOVING CRACK DEFECT, CONDUCTED HFEC INSP, ENLARGED TRIM BY 0.040" INSURANCE CUT, INSTALLED DOUBLER/ TRIPLER, MAINTAINED A 0.5" MIN. CORNER RADIUS, MAINTAIN
- [SDR TSAA0977007](https://openairdocs.org/sdr/TSAA0977007.md): Transmitter · defective · Jul 21, 2009 · N826AL · Boeing 737282C · Engine Pressure Ratio (EPR)
  > ON TAKEOFF, NR 1 EPR FROZE AT 1.14 WHILE SETTING TAKEOFF POWER. OTHER NR 1 INDICATIONS NORMAL. ABORTED TAKEOFF AT 70 KTS. RETURNED TO RAMP. MX: REMOVED AND REPLACED EPR INDICATOR, DID NOT FIX. REMOVED AND REPLACED EPR TRANSMITTER IAW AMM 77-11-21. OPS CH
- [SDR TSAA0932003](https://openairdocs.org/sdr/TSAA0932003.md): Uplock Sensor · dirty · Apr 16, 2009 · N826AL · Boeing 737282C · Landing Gear Position and Warning
  > FLT 11, HNL- LIH - NOSE GEAR RED LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO HNL. ALL THREE GREEN LIGHTS ILLUMINATED WHEN LANDING GEAR EXTENDED. FLIGHT TERMINATED UNEVENTFUL. CLEANED UPLOCK SENSOR. TEST IAW 32-61-41. OPERATIONAL CHECK/GEAR SWING OKAY.
- [SDR TSAA0932002](https://openairdocs.org/sdr/TSAA0932002.md): Control Cable · out of adjust · Apr 2, 2009 · N826AL · Boeing 737282C · Landing Gear Retraction/Extension System
  > FLT 320: TEST FLIGHT, LANDING GEAR LEVER WOULD NOT GO UP AFTER TAKEOFF. WARNING HORN ON AFTER FLAP RETRACT. RETURNED TO SJO, UNEVENTFUL LANDING. PERFORMED ADJUSTMENT AND TEST FOR THE GROUND SPOILER INTERLOCK VALVE CABLE AS PER MM 27-62-51, PAR 2 AND 3. PER
- [SDR TSAA0952001](https://openairdocs.org/sdr/TSAA0952001.md): Switch · obstructed · Jan 21, 2009 · N826AL · Boeing 737282C · Door Warning System
  > FLT 952, HNL-ITO -ON TAKEOFF, THE AFT CARGO LIGHT CAME ON. RETURNED TO HNL, NO EMERGENCY. MAINTENANCE FOUND A STRAP LODGED BETWEEN THE DOOR AND SWITCH. REPOSITIONED THE STRAP, VERIFIED DOORS OPS CHECK OK. NO PRESSURE PROBLEMS NOTED. AIRCRAFT RETURNED TO S
- [SDR TSAA0827019](https://openairdocs.org/sdr/TSAA0827019.md): Indicator · failed · Apr 8, 2008 · N826AL · Boeing 737282C · Trailing Flap Position Indicating System
  > CARGO FLIGHT 940 HNL-KOA, ON DESCENT TO KOA, THE CREW WAS ONLY ABLE TO EXTEND THE FLAPS TO 8 UNITS. THE CREW DECLARED AN EMERGENCY AND RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR AND OPERATIONALLY CH
- [SDR TSAA0877012](https://openairdocs.org/sdr/TSAA0877012.md): Indicator · failed · Mar 4, 2008 · N826AL · Boeing 737282C · Engine EGT/TIT Indicating System
  > FLIGHT 269 HNL-LIH - AT TAKEOFF, THE CREW NOTED THE NR 1 EGT READ LOW AT APPROXIMATELY 250 DEGREES AND ELECTED TO ABORT THE TAKEOFF AT 90 KTS AIRSPEED. THE AIRCRAFT WAS TAXIED BACK TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR
- [SDR TSAA0829008](https://openairdocs.org/sdr/TSAA0829008.md): Hose · failed · Feb 15, 2008 · N826AL · Boeing 737282C · Hydraulic System, Main
  > NON-ETOPS FLIGHT 215 HNL-LIH, DURING CRUISE FLIGHT, THE CREW NOTED THE HYDRAULIC QUANTITY GAUGE DROPPED TO ZERO. CREW COMPLETED THE HYDRAULIC SYSTEM A FAILURE CHECKLIST AND DECLARED AN EMERGENCY. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANC
- [SDR TSAA0734055](https://openairdocs.org/sdr/TSAA0734055.md): Dadc · failed · Oct 5, 2007 · N826AL · Boeing 737282C · Air Data Computer
  > NON-ETOPS CARGO FLIGHT 946 HNL-KOA - DURING CLIMB, THE CREW NOTED WARNING FLAGS IN THE FIRST OFFICER’S AIRSPEED INDICATOR, ALTIMETER AND VERTICAL SPEED INDICATOR. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE DIGITAL
- [SDR TSAA0753052](https://openairdocs.org/sdr/TSAA0753052.md): Skin · cracked · Sep 20, 2007 · N826AL · Boeing 737282C · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING VISUAL INSPECTION DURING SERVICE CHECK, A CRACK WAS DISCOVERED AT BS 306 AT STR 18. MAINTENANCE ALONG WITH ENGINEERING IS RESEARCHING THE REPAIR. ECO 3673 REPAIRED CRACKED. 8100-9 WAS RECEIVED FROM BOEING. AIRCRAFT WAS RETURNED TO SERVI
- [SDR TSAA0731036](https://openairdocs.org/sdr/TSAA0731036.md): Accessory Unit · failed · Jun 25, 2007 · N826AL · Boeing 737282C · Leading Edge Slat Control System
  > NON-ETOPS FLIGHT 226 HNL-OGG - WHEN THE CREW APPLIED TAKEOFF POWER, THE CONFIGURATION WARNING HORN SOUNDED. CREW ABORTED TAKE OFF AT 60 KNOTS INDICATED AIRSPEED. CREW RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP SLAT

Next page: https://openairdocs.org/model/boeing-737-282c/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 aircraft_model_key = '737282C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-282c/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.