# Service difficulty reports: CFM International CFM56-3B-1

A list on [CFM International CFM56-3B-1](https://openairdocs.org/engine/cfm-international-cfm56-3b-1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 11 · 540 reports

- [SDR XV6A2013081200007](https://openairdocs.org/sdr/XV6A2013081200007.md): Solenoid · malfunctioned · Aug 12, 2013 · N732VA · Boeing 7373T0 · Landing Gear Retraction/Extension System
  > LANDING GEAR LEVER HUNG UP ON GEAR RETRACTION, HAD TO USE LOCK OVERRIDE SWITCH TO BRING GEAR UP. R & R LANDING GEAR CONTROL LEVER ACTUATOR SOLENOID IAW AMM 32-31-31. OPS/FUNCTIONAL CHECKS GOOD. PN OFF: A420-060283-05, SN OFF: 3762, PN ON: A420-060283-05, SN
- [SDR SWAA2013061917352](https://openairdocs.org/sdr/SWAA2013061917352.md): Engine · leaking · Jun 16, 2013 · N397SW · Boeing 7373H4 · Engine (Turbine/Turboprop)
  > AIR TURNBACK ON INITIAL CLIMB OUT. F/A REPORT VERY STRONG ODOR IN CABIN AGAIN. FOUND INTEGRAL OIL LEAK AT NR 2 ENGINE. R & R NR 2 ENGINE IAW MT.
- [SDR SWAA105724](https://openairdocs.org/sdr/SWAA105724.md): Strap · cracked · Sep 26, 2010 · N399WN · Boeing 7373H4 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED 16Y CHECK, FOUND STRAP CRACKED AT BS 949, STR 11L. R & R STRAP IAW SRM AND MANUFACTURER DRAWING.
- [SDR SWAA105738](https://openairdocs.org/sdr/SWAA105738.md): Floor Support · cracked · Sep 26, 2010 · N664WN · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 44. REPAIRED BEAM IAW ER AND EA.
- [SDR USAA2010092292071](https://openairdocs.org/sdr/USAA2010092292071.md): Skin · cracked · Sep 22, 2010 · N334AW · Boeing 7373Y0 · Trailing Edge Flaps
  > MAJOR REPAIR - CRACK ON LT WING OTBD MID FLAP L/E SKIN BETWEEN WBL204.4 TO WBL219.4. REPAIRED LT WING OTBD MID FLAP L/E SKIN BETWEEN WBL204.4 TO WBL219.4 IAW SRM 57-53-01 REPAIR NR 8.
- [SDR SWAA095583](https://openairdocs.org/sdr/SWAA095583.md): Engine · overheated · Aug 30, 2009 · N337SW · Boeing 7373H4 · Turbine Section
  > ABORTED TAKEOFF / DECLARED EMERGENCY. ON TAKEOFF NR 1 ENG OFF EGT WAS CLIMBING THRU, 800 REDUCED POWER TO MAINTAIN LIMITS AND RETURNED TO AIRPORT. REMOVED AND REPLACED NR 1 ENGINE PER MM.
- [SDR SWAA095276](https://openairdocs.org/sdr/SWAA095276.md): Shutoff Valve · malfunctioned · Aug 15, 2009 · N650SW · Boeing 7373H4 · Fuel Controlling System
  > INFLIGHT SHUTDOWN / DECLARED EMERGENCY. FWD LOW PRESSURE LIGHT NR 1 MAIN FUEL TANK ON, FOLLOWED BY AFT LOW PRESSURE LIGHT, IN NR 1 MAIN. BOTH PUMPS TURNED OFF. FL 260, ENG RUNNING NORMAL THEN FLAMED OUT. WINDMILLING N1 & N2 NORMAL. REMOVED AND REPLACED
- [SDR SWAA075748](https://openairdocs.org/sdr/SWAA075748.md): Engine · failed · Nov 17, 2007 · N676SW · Boeing 7373A4 · Engine (Turbine/Turboprop)
  > AIR TURNBACK / DECLARED EMERGENCY. IN FLIGHT SHUTDOWN EN ROUTE AT ABOUT 25,000 FT, AIRCRAFT BEGAN VIBRATING THEN HEARD EXPLOSION. SECURED NR 2 ENGINE. NR 2 ENGINE REPLACEMENT IN PROGRESS PER MM.
- [SDR SWAA074020](https://openairdocs.org/sdr/SWAA074020.md): Engine · flamed out · Aug 11, 2007 · N682SW · Boeing 7373Y0 · Engine (Turbine/Turboprop)
  > UPON LANDING AND DECELERATION IN PHX NR 2 ENGINE FLAMED OUT. REMOVED AND REPLACED NR 2 ENGINE PER MM.
- [SDR 2007FA0000704](https://openairdocs.org/sdr/2007FA0000704.md): Line · leaking · Aug 9, 2007 · N1732 · Boeing 7373T0 · Engine Fuel Distribution
  > FLOAT STICKS, CAUSING FUEL TO COME OUT OF CARBURETOR SPLIT LINE. LEAKING FUEL FROM GASKET.
- [SDR CALA0700388](https://openairdocs.org/sdr/CALA0700388.md): Fuse · inoperative · Aug 1, 2007 · N14358 · Boeing 737300 · Emergency Lighting
  > THE EMERGENCY LIGHT OVER COCKPIT DOOR WAS FOUND INOPERATIVE. THE F2 FUSE ON BATTERY PACK M1133 WAS REMOVED AND REPLACED IAW AMM 33-51-51.
- [SDR CALA0700387](https://openairdocs.org/sdr/CALA0700387.md): Stringer · corroded · Aug 1, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 28R CORRODED AT STA 294-323. THE STRINGER WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0700383](https://openairdocs.org/sdr/CALA0700383.md): Channel · cracked · Jul 30, 2007 · N63305 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN NR 1 VHF ANTENNA MOUNT CHANNEL ON BOTH ENDS AT STA 500-500A, S29R TO 29L. THE ANTENNA CHANNEL WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0700384](https://openairdocs.org/sdr/CALA0700384.md): Channel · corroded · Jul 30, 2007 · N63305 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN FLOOR CHANNEL CORRODED AT STA 727D + 8 INCHES, RBL 3. REPAIRED IAW SRM 53-00-53.
- [SDR CALA0700385](https://openairdocs.org/sdr/CALA0700385.md): Rail · cracked · Jul 30, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A 1 INCH CRACK IN AFT BAGGAGE BIN TIE DOWN RAIL AT STA 727E, S27R. THE TIE DOWN RAIL WAS REMOVED AND A NEW SECTION OF TIE DOWN RAIL WAS INSTALLED IAW SRM 53-00-53, REPAIR 2, PAGE 202.
- [SDR CA070807001](https://openairdocs.org/sdr/CA070807001.md): Lock Actuator · failed · Jul 27, 2007 · Boeing 73735B · Landing Gear Retraction/Extension System
  > (CAN) DURING APPROACH, THE NOSE LANDING GEAR DID NOT RECEIVE A DOWNLOCK INDICATION IN THE COCKPIT. IT WAS BELIEVED BY THE CREW THAT THE GEAR FAILED TO EXTEND. A SECOND ATTEMPT WAS MADE AND THE NOSE GEAR EXTENDED AND LOCKED AS NORMAL. NOTE: THE EMERGENCY EXTEN
- [SDR SB07051](https://openairdocs.org/sdr/SB07051.md): Wire · broken · Jul 7, 2007 · N592US · Boeing 737301 · Light System Wiring
  > MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 12, LT SIDE, INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT SEAT ROW 12, LT SIDE. OPERATIONAL CHECK GOOD.
- [SDR CA070312003](https://openairdocs.org/sdr/CA070312003.md): Starter · failed · Mar 12, 2007 · Boeing 73735B · APU Start/Ignition System
  > (CAN) APU SHUTDOWN ON ITS OWN AND WOULD NOT RE-START. NEW STARTER INSTALLED. NEW STARTER BLEW APART ON FIRST START ATTEMPT. SECOND STARTER INSTALLED AND OPERATED SERVICEABLE. (TC NR 20070312003)
- [SDR CALA0700054](https://openairdocs.org/sdr/CALA0700054.md): Frame · cracked · Feb 6, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN FRAME AT STA 597, S13L. THE FRAME WAS REPAIRED IAW SRM 53-00-07, PAGE 203, FIGURE 201.
- [SDR AWXA200700046](https://openairdocs.org/sdr/AWXA200700046.md): Wedge · debonded · Jan 7, 2007 · N175AW · Boeing 73733A · Leading Edge Devices
  > MAJOR REPAIR - C-21 CHECK - NR 5916465, LT WING NR 3 SLAT WEDGE UPPER AND LOWER SURFACE DEBONDED, SS 50 -SS 80. REPLACED LT WING NR 3 SLAT IAW AMM 27-81-00-5.
- [SDR 2007FA0000108](https://openairdocs.org/sdr/2007FA0000108.md): Powerplant · contaminated · Jan 1, 2007 · Boeing 737300 · Engine (Turbine/Turboprop)
  > ENGINE SUFFERED AN IFSD DUE TO POWER LOSS AND A COMMANDED ENGINE SHUTDOWN WAS CARRIED OUT. ENGINE RESTART WAS ATTEMPTED, UNSUCCESSFULLY. FURTHER INVESTIGATION REVEALED THAT NR 10 STRUT ON FAN FRAME (9 O`CLOCK STRUT AFT LOOKING FWD) WHICH RADIAL DRIVE SHAFT I
- [SDR AWXA200602116](https://openairdocs.org/sdr/AWXA200602116.md): Bulb · inoperative · Dec 21, 2006 · N154AW · Boeing 7373G7 · Engine Oil Temperature
  > FLIGHT 644: MCI - PHX - DURING CLIMB, THE CREW SHUT DOWN (IFSD) THE NR 2 ENG DUE TO HIGH ENGINE OIL TEMP THE CREW DECLARED AN EMERGENCY AND RETURNED TO MCI. EMERGENCY EQUIPMENT WAS DISPATCHED. THE PASSENGERS WERE NOT BRACED. THE LANDING WAS UNEVENTFUL AND T
- [SDR GAIA06033OP](https://openairdocs.org/sdr/GAIA06033OP.md): Csd · failed · Nov 17, 2006 · N102KH · Boeing 737306 · Alternator-Generator Drive
  > FLIGHT 453, DURING TAXI OUT, THE NR 1 GENERATOR TRIPPED OFF. MEL PROCEDURES WERE FOLLOWED AND POWER WAS TRANSFERED TO THE APU. DURING CLIMB OUT, THE APU FLAMED OUT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DEPARTURE. AN UNEVENTFUL LANDING WAS
- [SDR CALA0600444](https://openairdocs.org/sdr/CALA0600444.md): Seat Track · corroded · Oct 30, 2006 · N59302 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT OB SEAT TRACK CORRODED AT STA 897-927, RBL 45.5. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52.
- [SDR SWAA064142](https://openairdocs.org/sdr/SWAA064142.md): Battery · inoperative · Oct 27, 2006 · N346SW · Boeing 7373H4 · Emergency Lighting
  > DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW MM.
- [SDR SWAA064109](https://openairdocs.org/sdr/SWAA064109.md): Compressor · stalled · Oct 19, 2006 · N353SW · Boeing 7373H4 · Turbine Engine Compressor Section
  > CREW REPORTED LOUD BANGING SOUND ON LT SIDE OF FUSELAGE DURING DESCENT AND AFTER ADDING POWER TO ENGINES. SUSPECT NR 1 ENGINE COMPRESSOR STALL. R&R NR 1 ENGINE MEC AND FUEL PUMP PER MM. R&R CIT SENSOR PER MM.
- [SDR SWAA064020](https://openairdocs.org/sdr/SWAA064020.md): Pressure Panel · cracked · Oct 17, 2006 · N638SW · Boeing 7373H4 · Fuselage Main, Bulkhead
  > DURING SCHEDULED 10Y CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, RBL 39. REPAIRED PRESSURE WEB IAW SWA EA.
- [SDR SWAA063981](https://openairdocs.org/sdr/SWAA063981.md): Shaft · broken · Oct 14, 2006 · N388SW · Boeing 7373H4 · Compressor Bleed Control
  > WHILE CLIMBING OUT OF PHX ABOVE FL 250, NR 1 ENGINE WAS UNABLE TO REACH CLIMB N1 POWER SETTING WITH PMC OFF. THROTTLE WAS ALL THE WAY TO FWD STOP. REMOVED AND REPLACED BROKEN VBV MOTOR MAIN SHAFT PER MM.
- [SDR SWAA063856](https://openairdocs.org/sdr/SWAA063856.md): Stringer Clip · cracked · Oct 8, 2006 · N320SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2L. REMOVED AND REPLACED STRINGER CLIP IAW SRM.
- [SDR SWAA063857](https://openairdocs.org/sdr/SWAA063857.md): Stringer Clip · cracked · Oct 8, 2006 · N320SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP IAW SRM.
- [SDR SWAA063858](https://openairdocs.org/sdr/SWAA063858.md): Stringer Clip · cracked · Oct 8, 2006 · N320SW · Boeing 7373H4 · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R AND STR 2L. REMOVED AND REPLACED STRINGER CLIP IAW SRM.
- [SDR SWAA063859](https://openairdocs.org/sdr/SWAA063859.md): Stringer Clip · cracked · Oct 8, 2006 · N320SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED STRINGER CLIP IAW SRM.
- [SDR SWAA063860](https://openairdocs.org/sdr/SWAA063860.md): Stringer Clip · cracked · Oct 8, 2006 · N320SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L AND STR 3R. REMOVED AND REPLACED STRINGER CLIP IAW SRM.
- [SDR SWAA063861](https://openairdocs.org/sdr/SWAA063861.md): Stringer Clip · cracked · Oct 8, 2006 · N320SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L AND STR 4R. REMOVED AND REPLACED STRINGER CLIP IAW SRM.
- [SDR SWAA063862](https://openairdocs.org/sdr/SWAA063862.md): Stringer Clip · cracked · Oct 8, 2006 · N320SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP IAW SRM.
- [SDR SWAA063863](https://openairdocs.org/sdr/SWAA063863.md): Stringer Clip · cracked · Oct 8, 2006 · N320SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP IAW SRM.
- [SDR SWAA063864](https://openairdocs.org/sdr/SWAA063864.md): Stringer Clip · cracked · Oct 8, 2006 · N320SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP IAW SRM.
- [SDR AWXA200601717](https://openairdocs.org/sdr/AWXA200601717.md): Socket · corroded · Oct 6, 2006 · N156AW · Boeing 7373G7 · Emergency Lighting
  > PHX - EEL - DURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT THE L-1 DOOR EXTERNAL EMERGENCY EXIT LIGHT BASE ASSY HAS CORRODED NUTPLATES AND NEEDS REPLACED. MX REPLACED THE EXTERNAL EMERGENCY EXIT LIGHT. OPS CHECK WAS GOOD.
- [SDR SWAA064021](https://openairdocs.org/sdr/SWAA064021.md): O-Ring · burned · Oct 2, 2006 · N399WN · Boeing 7373H4 · Flight Compartment Windows
  > AIR TURNBACK, PASSING FL 200 CAPTAINS L1 WINDOW UPPER LT CORNER CAUGHT FIRE. TURNED OFF WINDOW HEAT SWITCH FIRE EXTINGUISHED. REMOVED AND REPLACED L1 WINDOW O-RINGS IAW MM.
- [SDR CALA0600373](https://openairdocs.org/sdr/CALA0600373.md): Frame · cracked · Sep 28, 2006 · N14341 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP FITTING, STA 794.3. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 51-10-2.
- [SDR SB06090](https://openairdocs.org/sdr/SB06090.md): Splice · damaged · Sep 13, 2006 · N591US · Boeing 737301 · Light System Wiring
  > CLT - ROW 5ABC EMERGENCY SEAT LIGHT INOPERATIVE. MAINTENANCE FOUND WIRE PULLED OUT OF BUTT SPLICE. REPLACED SPLICE.
- [SDR SWAA063129](https://openairdocs.org/sdr/SWAA063129.md): Cable · worn · Aug 23, 2006 · N334SW · Boeing 7373H4 · Compressor Bleed Control
  > NR 2 ENGINE SLOW TO SPOOL UP ON ADVANCING TO TAKEOFF THRUST, APPROX 5 TO 8 SECONDS. ON LANDING AGAIN TOOK 5 TO 8 SECONDS TO SPOOL UP AND CAUSED DIRECTIONAL CONTROL PROBLEMS. REMOVED AND REPLACED NR 2 ENGINE VSV FEEDBACK CABLE PER MM.
- [SDR 2006FA0000342](https://openairdocs.org/sdr/2006FA0000342.md): Cable · misrouted · Mar 15, 2006 · N370WL · Boeing 7373G7 · Passenger Oxygen System
  > (REF: ATC0662) THE ACTUATING CABLE TO THE CHEMICAL OXYGEN GENERATORS ON PASSENGER SERVICE UNITS WERE FOUND INCORRECTLY ROUTED. IE: IT WAS UNDER THE PIN AND RESTING ON THE PLASTIC MOULDING. DEFECT RAISED AS AN (IORS) INTERNAL OCCURRENCIES REPORT AND UPGRADED
- [SDR AWXA200600348](https://openairdocs.org/sdr/AWXA200600348.md): Bleed Valve · failed · Feb 17, 2006 · N303AW · Boeing 7373G7 · Compressor Bleed Valve
  > CREW REPORTED THAT AFTER TAKEOFF, FROM PHX EN ROUTE TO OAK, THE RT ENGINE BLEED VALVE REMAINED CLOSED AND THE CIRCUIT BREAKER POPPED. CREW DIVERTED TO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE RT ENG BLEED AIR REGULATOR IAW B
- [SDR GAIA06001](https://openairdocs.org/sdr/GAIA06001.md): Slide · deployed · Feb 7, 2006 · N111KH · Boeing 737375 · Escape Slide
  > R1 ESCAPE SLIDE ACCIDENTALLY DEPLOYED BY MAINTENANCE. DIFFERED R1 DOOR SLIDE IAW MEL. UPON ARRIVAL AT THE NEXT STATION, REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE. OPERATIONAL CHECK OK. (DMI CLEARED). AIRCRAFT RETURNED TO SERVICE. (K)
- [SDR SWAA060318](https://openairdocs.org/sdr/SWAA060318.md): Turbine Blades · damaged · Jan 25, 2006 · N609SW · Boeing 7373H4 · Turbine Section
  > DURING SCHEDULED C4 CHECK, NR 2 ENGINE FAILED BOROSCOPE. FOUND 11 INCH BY 11 INCH HOLE IN HPT SHROUD. ALL HPT BLADES WORN TO CAP SHELF. FOUND 10 LPT BLADES DAMAGED BEYOND LIMITS. REMOVED AND REPLACED NR 2 ENGINE PER MM.
- [SDR SWAA060077](https://openairdocs.org/sdr/SWAA060077.md): Slide · activated · Jan 8, 2006 · N344SW · Boeing 7373H4 · Escape Slide
  > R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE IAW MM.
- [SDR SWAA060088](https://openairdocs.org/sdr/SWAA060088.md): Skin · cracked · Jan 8, 2006 · N665WN · Boeing 7373Y0 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT, FWD UPPER CORNER. REPAIRED SKIN IAW SWA EA AND SRM.
- [SDR SWAA060089](https://openairdocs.org/sdr/SWAA060089.md): Skin · cracked · Jan 8, 2006 · N665WN · Boeing 7373Y0 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, BETWEEN STR 19R TO STR 20R. REPAIRED SKIN IAW EA AND SRM.
- [SDR SWAA060090](https://openairdocs.org/sdr/SWAA060090.md): Skin · cracked · Jan 8, 2006 · N665WN · Boeing 7373Y0 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 24L. REPAIRED SKIN PER SWA EA.

Next page: https://openairdocs.org/engine/cfm-international-cfm56-3b-1/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 engine_model_key = 'CFM563B1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/cfm-international-cfm56-3b-1/reports

---
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