# Service difficulty reports: N54348, cancelled Jan 24, 2018

A list on [N54348, cancelled Jan 24, 2018](https://openairdocs.org/deregistered/N54348-2018-01-24.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 · 57 reports

- [SDR FX7A200500009](https://openairdocs.org/sdr/FX7A200500009.md): Line · leaking · Oct 15, 2005 · N54348 · Boeing 727231 · Hydraulic System, Main
  > AFTER TAKEOFF, DURING FLAP RETRACTION FROM 15 DEGREES TO 5 DEGREES LOST ALL OF THE SYSTEM A HYDRAULICS. TROUBLESHOT AND FOUND A FLEX LINE AT THE LEFT PCU ELEVATOR LEAKING, REMOVED AND REPLACED HYDRAULIC LINE, IAW MM REF 27-30-81, OP CHECK AND LEAK CHECK NORMA
- [SDR FX7A200500002](https://openairdocs.org/sdr/FX7A200500002.md): Indicator · inoperative · Feb 12, 2005 · N54348 · Boeing 727231 · Integrated Flight System
  > CAPTAINS ADI INOPERATIVE.
- [SDR FX7A200500001](https://openairdocs.org/sdr/FX7A200500001.md): Actuator · leaking · Feb 9, 2005 · N54348 · Boeing 727231 · Leading Edge Slat Actuator
  > DURING TAXI HYDRAULIC QUANTITY DROPS TO ZERO.
- [SDR 2004F00382](https://openairdocs.org/sdr/2004F00382.md): Sensor · malfunctioned · Jan 5, 2004 · N54348 · Boeing 737231 · Landing Gear Retraction/Extension System
  > UNABLE TO RAISE THE GEAR AFTER TAKEOFF. AIRCRAFT RETURNED TO MIAMI WITHOUT INCIDENT. REMOVED AND REPLACED THE NLG SAFETY SENSOR PER MM 32-09 AND THE LANDING GEAR ACCESSORY UNIT FOR PRECAUTIONARY. PERFORMED OPS CHECK OF LANDING GEAR PER PER MM 32-32. AIRCRAF
- [SDR 2004F00250](https://openairdocs.org/sdr/2004F00250.md): Pin · backed out · Jan 5, 2004 · N54348 · Boeing 727231 · Landing Gear Steering System
  > LOSS OF STEERING DURING LINING UP FOR TAKEOFF RETURNED TO GATE. FOUND APEX PIN BACKED OUT OF STEERING KNUCKLE. INSTALLED APEX PIN AND OPS CHECK SYSTEM PER 32-51. INSPECTED AREA AND FOUND NO FURTHER DAMAGE A/C RETURNED TO SERVICE. (M)
- [SDR 2003F00606](https://openairdocs.org/sdr/2003F00606.md): Fuel Control · failed · Aug 10, 2003 · N54348 · Boeing 737231 · Fuel Control/Turbine Engines
  > LEVELING OFF AT 330 WHEN NR 2 ENGINE WAS THROTTLED BACK TO CRUISE POWER, THE FUEL FLOW WENT TO ZERO, AND THE EPR WENT TO 2.24 ENGINE FLAMED OUT. FUEL WAS DUMPED AND EMERGENCY DECLARED A/C LANDED WITHOUT INCIDENT. THE FUEL CONTROL WAS CHANGED PER MM 73-21 AND
- [SDR HOC2003F00017](https://openairdocs.org/sdr/HOC2003F00017.md): Stringer · cracked · Apr 29, 2003 · N54348 · Boeing 737231 · Fuselage Main, Longeron/Stringer
  > DURING A (C) CHECK, STRINGER AT 15L, STA 720B-720 WAS FOUND CRACKED.
- [SDR HOC2003F00015](https://openairdocs.org/sdr/HOC2003F00015.md): Support · corroded · Apr 29, 2003 · N54348 · Boeing 737231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK, CORROSION WAS NOTED ON AFT LAV PAN AND SUPPORT.
- [SDR HOC2003F00014](https://openairdocs.org/sdr/HOC2003F00014.md): Support Bracket · corroded · Apr 29, 2003 · N54348 · Boeing 737231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK CORROSION WAS NOTED ON DITCHING PANEL SUPPORT BRACKET AT STA1176-1183R.
- [SDR HOC2003F00013](https://openairdocs.org/sdr/HOC2003F00013.md): Floorbeam · corroded · Apr 29, 2003 · N54348 · Boeing 727231 · Fuselage Main, Floor Beam
  > DURING A (C) CHECK CORROSION WAS NOTED ON LOWER FLANGE. COMMON TO FLOORBEAM STRAP AND INTERCOSTAL. STA 1130, LBL24.
- [SDR HOC2003F00012](https://openairdocs.org/sdr/HOC2003F00012.md): Intercostal · corroded · Apr 29, 2003 · N54348 · Boeing 737231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK CORROSION WAS NOTED ON LOWER FLANGE COMMON TO FLOORBEAM STRAP AND INTERCOSTAL. STA 1130, LBL 24.
- [SDR HOC2003F00011](https://openairdocs.org/sdr/HOC2003F00011.md): Floor Support · corroded · Apr 29, 2003 · N54348 · Boeing 737231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK, CORROSION WAS NOTED ON CABIN FLOOR SUPPORT BRACKET AT STA 1070, LEFT.
- [SDR HOC2003F00016](https://openairdocs.org/sdr/HOC2003F00016.md): Frame · corroded · Apr 28, 2003 · N54348 · Boeing 737231 · Fuselage Main, Frame
  > DURING A (C) CHECK CORROSION WAS NOTED ON LOWER FRAME, STA 1130 AT 27R.
- [SDR HOC2003F00010](https://openairdocs.org/sdr/HOC2003F00010.md): Support Bracket · corroded · Apr 28, 2003 · N54348 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK CORROSION WAS NOTED ON LEFT, OUTBOARD DITCHING PAN SUPPORT BRACKET. STA 1176-1183.
- [SDR HOC2003F00009](https://openairdocs.org/sdr/HOC2003F00009.md): Support · corroded · Apr 26, 2003 · N54348 · Boeing 737231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK, CORROSION WAS NOTED AT STA 1166, AFT BULKHEAD SUPPORT. (CENTER/ TOP).
- [SDR HOC2003F00003](https://openairdocs.org/sdr/HOC2003F00003.md): Floorbeam · corroded · Apr 25, 2003 · N54348 · Boeing 727231 · Fuselage Main, Floor Beam
  > DURING A (C) CHECK CORROSION WAS NOTED ON FLOORBEAM TOP SURFACE STA 440, 12 LBL-12 RBL.
- [SDR HOC2003F00002](https://openairdocs.org/sdr/HOC2003F00002.md): Intercostal · corroded · Apr 25, 2003 · N54348 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK CORROSION WAS NOTED ON OUTBOARD LWR INTERCOSTAL, STA 1070-STGR30, RBL 2.0.
- [SDR HOC2003F00008](https://openairdocs.org/sdr/HOC2003F00008.md): Floor Support · corroded · Apr 20, 2003 · N54348 · Boeing 737231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK, CORROSION WAS NOTED ON OUTBOARD FLOOR SUPPORT BRACKET FOR FORWARD LAV. STA 314-344, RBL 5-10.
- [SDR HOC2003F00007](https://openairdocs.org/sdr/HOC2003F00007.md): Seat Track · corroded · Apr 20, 2003 · N54348 · Boeing 737231 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A (C) CHECK CORROSION WAS NOTED ON SEAT TRACK AND FLOOR SUPPORTS AT STA 380-420, RBL 10-20.
- [SDR HOC2003F00006](https://openairdocs.org/sdr/HOC2003F00006.md): Floorbeam · corroded · Apr 20, 2003 · N54348 · Boeing 737231 · Fuselage Main, Floor Beam
  > DURING A (C) CHECK CORROSION WAS NOTED ON CABIN FLOORBEAM, STA 1110, BL-0.
- [SDR HOC2003F00005](https://openairdocs.org/sdr/HOC2003F00005.md): Splice · corroded · Apr 20, 2003 · N54348 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK CORROSION WAS NOTED ON TENSION TIE FITTING AND SPLICE ANGLE AT STA 1183, STR 17R.
- [SDR HOC2003F00004](https://openairdocs.org/sdr/HOC2003F00004.md): Tie · corroded · Apr 20, 2003 · N54348 · Boeing 737231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK CORROSION WAS NOTED ON TENSION TIE FITTING AND SPLICE ANGLE AT STA 1183, STR 17R.
- [SDR HOC2003F00001](https://openairdocs.org/sdr/HOC2003F00001.md): Seat Track · corroded · Apr 20, 2003 · N54348 · Boeing 737231 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A (C) CHECK CORROSION WAS NOTED ON SEAT TRACK STA 1070-1130 LT.
- [SDR HOC2003F00000](https://openairdocs.org/sdr/HOC2003F00000.md): Floor Support · cracked · Apr 20, 2003 · N54348 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK FLOOR SUPPORT AT STA 848 BL 0, WAS FOUND CRACKED.
- [SDR 2003F00104](https://openairdocs.org/sdr/2003F00104.md): Switch · out of adjust · Nov 30, 2002 · N54348 · Boeing 727231 · Landing Gear Position and Warning
  > UPON GEAR RETRACTION OUT OF MHLM GEAR DOOR LIGHTS REMAINED ON AIRCRAFT RETURNED TO AIRPORT WITH NO INCIDENT. ADJUSTED SWITCH ON MLG DOOR OPS CHECK NORMAL PER MM 32-12-0. OPS CHECK NORMAL. A/C RETURNED TO SERVICE. (M)
- [SDR FX72002F00003](https://openairdocs.org/sdr/FX72002F00003.md): Engine · flamed out · Aug 10, 2002 · N54348 · Boeing 727231 · Engine (Turbine/Turboprop)
  > AFTER CRUISING AT FLIGHT LEVEL 33. IN ICE CONDITIONS, WITH ENGINE ANTI-ICE ON. NR 2 ENGINE EPR AND AND FUEL FLOW OSCILLATED (EPR BETWEEN 1.7 AND 1.4), (FUEL FLOW 2500-1200). AFTER 20 MINUTES OUT OF ICE CONDITIONS AND COMMENCING DESCENT AFTER POWER REDUCTION,
- [SDR 2002F00887](https://openairdocs.org/sdr/2002F00887.md): Clamp · loose · Jul 27, 2002 · N54348 · Boeing 727231 · Engine Bleed Air System
  > AFTER TAKEOFF IN MIA, NR 3 ENGINE STRUT O/H LIGHT CAME ON, WHEN REDUCING POWER LIGHT WENT OUT. FOLLOWED PROCEDURES AND RETURNED TO MIA. FOUND LOOSE 13TH STAGE MOD VALVE CLAMP AT ENGINE STRUT TIGHTENED SAME PER MM 20-80-1 AND RAN ENGINE PER MM 71-00. OPS CHE
- [SDR 2002F00888](https://openairdocs.org/sdr/2002F00888.md): B-Nut · loose · Jul 26, 2002 · N54348 · Boeing 727231 · Hydraulic System, Main
  > DURING CRUISE SYSTEM 'A' HYDRAULICS FAILED, PRESSURE WENT TO ZERO. AIRCRAFT DIVERTED TO SAP AND LANDED SAFELY, FOUND SYSTEM 'A' PRESSURE LINE B-NUT LOOSE TIGHTENED SAME SERVICED HYD AND OPS CHECK GOOD PER MM 29-11. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR FX72002F00001](https://openairdocs.org/sdr/FX72002F00001.md): Hydraulic Line · loose · Jul 26, 2002 · N54348 · Boeing 727231 · Hydraulic Power System
  > DURING CRUISE SYSTEM (A) HYDRAULICS FAILED, PRESSURE WENT TO (O) A/C DIVERTED TO SAP AND LANDED SAFELY FOUND SYSTEM (A) PRESSURE LINE (B) NUT LOOSE TIGHTENED SAME SERVICED HYDRAULIC AND OPS CHECK GOOD PER MM. AIRCRAFT RETURNED TO SERVICE.
- [SDR FX72002F00002](https://openairdocs.org/sdr/FX72002F00002.md): Link · inoperative · Jul 11, 2002 · N54348 · Boeing 727231 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, GEAR HANDLE WOULD NOT MOVE BEYOND OFF POSITION AIRCRAFT RETURNED TO AIRPORT, REMOVED AND REPLACED THE GROUND SHIFT LINK IN LEFT WHEEL WELL PER MM. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVICE.
- [SDR 2002F00217](https://openairdocs.org/sdr/2002F00217.md): Pump · failed · Feb 8, 2002 · N54348 · Boeing 727231 · Hydraulic Pump (Electric/Engine), Main
  > DURING CLIMB-OUT FROM MIAMI, LOW PRESSURE LIGHT ON NR 1 ENGINE 'A' SYSTEM HYDRAULIC PUMP ILLUMINATED, ACCOMPLISHED SUPPLEMENTARY PROCEDURE, UPON ARRIVAL TO CCS MAINTENANCE TROUBLESHOT AND FOUND THE NR 1 ENGINE HYDRAULIC PUMP TO BE DEFECTIVE. OPS CHECK NORMAL,
- [SDR 2002F00216](https://openairdocs.org/sdr/2002F00216.md): Module · failed · Feb 7, 2002 · N54348 · Boeing 727231 · Hydraulic System, Main
  > DURING APPROACH AIRCRAFT HAD FULL SYSTEM 'A' HYDRAULIC FAILURE. REMOVED AND REPLACED 'A' SYSTEM HYD MODULE PER MM 29-11-61. REMOVED AND REPLACED CASE DRAIN FILTERS ON ENGINES 1/2 PER MM 29-11-41. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TWAA0014202](https://openairdocs.org/sdr/TWAA0014202.md): Pump · failed · Sep 12, 2000 · N54348 · Boeing 727231 · Hydraulic Pump (Electric/Engine), Main
  > FLIGHT EXPERIENCED A LOSS OF B HYDRAULIC SYSTEM FLUID. USED ALTERNATE SYSTEM FOR BRAKING. REPLACED THE NUMBER 2 B HYD PUMP DUE TO FAILURE. A STUD ON THE PUMP FAILED CAUSING SEAL FAILURE. CHECK-C 12-12-99 MCI.
- [SDR TWAA0013001](https://openairdocs.org/sdr/TWAA0013001.md): Light · inoperative · Aug 22, 2000 · N54348 · Boeing 727231 · Emergency Lighting
  > THE EMERGENCY EXIT LIGHT ABOVE THE AFT HOSTESS JUMP SEAT, AND AT CABIN ROW 3 WERE INOPERATIVE. REPLACED THE BATTERY PACK AND POWER SUPPLY, (P/N 50202-090), FOR THE HOSTESS SEAT, AND REPLACED THE LAMP, (P/N 1315) AT ROW 3. CHECK-C 12-12-99 MCI.
- [SDR TWAA0009103](https://openairdocs.org/sdr/TWAA0009103.md): Power Supply · inoperative · Jun 9, 2000 · N54348 · Boeing 727231 · Emergency Lighting
  > THE EMERGENCY LIGHTS AT ROW 18 EMERGENCY EXIT WERE INOPERATIVE. REPLACED THE POWER SUPPLY IN AFT AIRSTAIR. CHECK-C 12-12-99 MCI.
- [SDR TWAA0005206](https://openairdocs.org/sdr/TWAA0005206.md): Light · inoperative · Apr 4, 2000 · N54348 · Boeing 727231 · Emergency Lighting
  > THE RT SIDE AFT CABIN DOOR SLIDE LIGHT WAS INOPERATIVE. CORRECTION WAS DEFERRED PER MEL. ON LAYOVER AT STL CORROSION WAS REMOVED AT THE LIGHT SOCKET AND THE LAMP WAS REPLACED. CHECK-C 12-12-99 MCI.
- [SDR TWAA0005205](https://openairdocs.org/sdr/TWAA0005205.md): Light · inoperative · Apr 4, 2000 · N54348 · Boeing 727231 · Emergency Lighting
  > THE LT SIDE AFT CABIN DOOR EMERGENCY SLIDE LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 12-12-99 MCI.
- [SDR TWAA0005204](https://openairdocs.org/sdr/TWAA0005204.md): Battery Pack · inoperative · Apr 4, 2000 · N54348 · Boeing 727231 · Emergency Lighting
  > THE EMERGENCY LIGHT AT ROW 3 WOULD NOT SHUT OFF WHEN POWER WAS REMOVED AND THE LIGHT SWITCH WAS OFF. REPLACED THE BATTERY PACK. CHECK-C 12-12-99 MCI.
- [SDR TWAA0004101](https://openairdocs.org/sdr/TWAA0004101.md): Battery Pack · malfunctioned · Mar 13, 2000 · N54348 · Boeing 727231 · Emergency Lighting
  > THE LEFT SIDE NUMBER 1 AND NUMBER 2 CABIN DOOR EMERGENCY LIGHTS REMAINED ON AFTER SHUT DOWN. AT THE L1 DOOR REPLACED THE BATTERY PACK, (P/N 9008-3), AND AT THE L2 DOOR REPLACED THE LIGHT ASSEMBLY, (P/N 10-0067-9). CHECK-C 12-12-99 MCI.
- [SDR TWAA0000406](https://openairdocs.org/sdr/TWAA0000406.md): Stringer · corroded · Dec 5, 1999 · N54348 · Boeing 727231 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT, FOUND CORROSION ON LOWER OTBD EDGE OF STRINGER 29R AT STA 1111. REPLACED S29R FROM STA 1110 TO 1130 PER SRM 53-10-3.
- [SDR TWAA9916705](https://openairdocs.org/sdr/TWAA9916705.md): Skin · cracked · Nov 30, 1999 · N54348 · Boeing 727231 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT, THE FORWARD LEFT CABIN ENTRY DOOR, UPPER HINGE CUTOUT WAS CRACKED, GOING FORWARD 1.375 INCH LONG IN FUSELAGE SKIN. ACCOMP HIGH FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED CRACK 0.250 INCH PER SRM 51-10-1, PAGE 6 TO 8. INSTA
- [SDR TWAA9916704](https://openairdocs.org/sdr/TWAA9916704.md): Skin · cracked · Nov 30, 1999 · N54348 · Boeing 727231 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT, THE FORWARD LT CABIN ENTRY DOOR, LOWER HINGE CUTOUT WAS CRACKED GOING FORWARD, 1.5 INCHES LONG IN FUSELAGE SKIN. ACCOMP HIGH FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED 0.250 IN PER SRM 51-10-1, PAGE 6. INSTALLED REPAIR DOUB
- [SDR TWAA0000701](https://openairdocs.org/sdr/TWAA0000701.md): Skin · cracked · Nov 30, 1999 · N54348 · Boeing 727231 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT, THE FWD ENTRY DOOR LOWER HINGE CUT OUT WAS CRACKED, FWD 1 1/2 INCHES IN FUSELAGE SKIN. ACCOMP HIGH FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED 0.250 IN PER SRM 51-10-01, PAGE 6. INSTALLED REPAIR DOUBLER PER SSRM 53-10-219,
- [SDR TWAA0000417](https://openairdocs.org/sdr/TWAA0000417.md): Skin · cracked · Nov 30, 1999 · N54348 · Boeing 727231 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, THE FWD ENTRY DOOR LOWER HINGE CUT-OUT WAS CRACKED OUT, FWD 1.5 IN LONG IN FUSELAGE SKIN. ACCOMP HIGH FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED 0.250 IN PER SRM 51-10-1, PAGE 6. INSTALLED REPAIR DOUBLER PER SSRM 53-10
- [SDR TWAA9910401](https://openairdocs.org/sdr/TWAA9910401.md): Plug · failed · Jul 21, 1999 · N54348 · Boeing 727231 · Drag Control Actuator
  > ABOUT 15 MINUTES INTO FLIGHT LOST B HYDRAULIC SYSTEM FLUID. RETURNED TO STL. THE NUMBER 5 SPOILER PLUG BLEW OUT OF THE ACTUATOR. REPLACED THE PLUG. CHECK-C 12-13-98 MCI.
- [SDR TWAA9905201](https://openairdocs.org/sdr/TWAA9905201.md): Actuator · cracked · Apr 8, 1999 · N54348 · Boeing 727231 · Landing Gear Retraction/Extension System
  > HAD HYDRAULIC SYSTEM FAILURE AND WAS NECESSARY TO MANUALLY EXTEND THE NOSE LANDING GEAR. FOUND THE NOSE LANDING GEAR DOWN LOCK CYLINDER SPLIT. REPLACED THE NLG DOWN LOCK ACTUATOR. CHECK-C 12-13-98 MCI.
- [SDR TWAA9807603](https://openairdocs.org/sdr/TWAA9807603.md): Tire · failed · May 10, 1998 · N54348 · Boeing 727231 · Tire
  > SLC - FLT 342 - DURING TAKEOFF FROM SLT, THE LEFT INBOARD TIRE CAME APART AND WAS DIGESTED INTO THE NR 1 ENGINE. SHUT DOWN NR 1 ENGINE. FLT PROCEEDED TO HOLDING AREA TO DUMP FUEL, THEN RETURNED TO SLC. REPLACED WHEEL, REPAIRED DAMAGE TO TE FLAP, AND REPLACE
- [SDR TWAA9760003](https://openairdocs.org/sdr/TWAA9760003.md): O-Ring · split · May 15, 1997 · N54348 · Boeing 727231 · Drag Control Actuator
  > MCI - FLT 117 - DURING DESCENT LOST 'B' SYSTEM HYDRAULIC QTY. REMOVED AND REPLACED SPLIT O-RING AT NR 5 SPOILER ACTUATOR PLUG. OPS CHECK NORMAL. (M)
- [SDR TWAA9715002](https://openairdocs.org/sdr/TWAA9715002.md): Engine · failed · Jan 29, 1997 · N54348 · Boeing 727231 · Engine (Turbine/Turboprop)
  > BNA - DURING CRUISE, SHUT DOWN NR 2 ENGINE, S/N 1504, DUE TO VIBRATION. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE. ENGINE OPERATION THEN CHECKED NORMAL. (M)
- [SDR TWAA9700103](https://openairdocs.org/sdr/TWAA9700103.md): Position Sw · failed · Jan 1, 1997 · N54348 · Boeing 727231 · Leading Edge Slat Position Indicating System
  > STL - FLT 475 - DURING CLIMB, NR 1 LEADING EDGE FLAP GREEN LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED LEADING EDGE FLAP POSITION SWITCH, MFG P/N H10-1026-1. OPERATIONAL CHECK NORMAL. (M)

Next page: https://openairdocs.org/deregistered/N54348-2018-01-24/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 = 'N54348' AND deregistration_id = 'N54348-2018-01-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N54348-2018-01-24/reports

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