# Service difficulty reports: JASC 5400

A list on [JASC 5400](https://openairdocs.org/jasc/5400.md).

Reports filed under 5400 · Nacelle/Pylon Structure, newest first.

Page 1 of 39 · 1,907 reports

- [SDR VNAA2026092425401](https://openairdocs.org/sdr/VNAA2026092425401.md): Door · gouged · Sep 23, 2026 · N520DC · Cndair CL6002C10
  > RIGHT UPPER COWLING LATCH BEAM GOUGED. PERFORMED REPAIR TO RT THRUST REVERSER LATCH BEAM USING STEPS AND DRAWINGS LISTED IN REO 670-54-22-171, REV A.
- [SDR CALA2026093020009](https://openairdocs.org/sdr/CALA2026093020009.md): Drag Fitting · not reported · Aug 30, 2026 · N19117 · Boeing 757224
  > GENERATING DIP FOR LH ENGINE STRUT DIAGONAL BRACE ON WING FITTING REPEAT INSPECTIONS OF REPAIR PERFORMED ON ECRA 5720-03677
- [SDR CALA2026093020007](https://openairdocs.org/sdr/CALA2026093020007.md): Drag Fitting · unknown · Aug 30, 2026 · N19117 · Boeing 757224
  > LH ENGINE STRUT DRAG FITTING TO WING SKIN HOLES. REPAIR PERFORMED ON ECRA 5720-03677. ACCOMPLISH INSPECTIONS IAW PART 2.3. OF EC5720-03677
- [SDR IPXA2026081505605](https://openairdocs.org/sdr/IPXA2026081505605.md): Fairing · cracked · Aug 15, 2026 · N157UP · Airbus A300F4622R
  > UPON FURTHER INSPECTION CRACK DEFERRED ON TASK T3F18E0097P77 HAS GROWN TO 5.5€? BEYOND SRM LIMITS ON NR 1 ENGINE LOWER AFT PYLON LOWER SKIN. C/W EO-98354-REQ3.
- [SDR IPXA2026082962661](https://openairdocs.org/sdr/IPXA2026082962661.md): Plate · damaged · Jul 8, 2026 · N144UP · Airbus A300F4622R
  > NR 2 PYLON, LT SIDE, FROM FR 5 TO FR 7, METALLIC PLATE WITH TOOL DAMAGE, MULTIPLE RIVETS DAMAGE AND HOLES WITH EVIDENCE OF BE ELONGATED. INSTALLED NEW SPRING AND NEW EXTRUSION ON NR 2 PYLON INBD SIDE FROM FR 5 TO FR 7 IAW SRM 51-40-21-001 AND 54-56-10-001.
- [SDR IPXA2026071772387](https://openairdocs.org/sdr/IPXA2026071772387.md): Duct · cracked · Jun 21, 2026 · N583UP · Boeing 7474R7F
  > CRACKED DUCT, NR 1 ENG RT CORE COWL PRECOOLER EXHAUST DUCT. IAW AMM 71-11-06-004-001-J00, REV 117, AND AMM 71-11-06-404-006-J00, REV 117, REPLACED THE CORE COWL. COMPLETED THIS JOB AND CONDITION CHECK SATISFACTORY.
- [SDR IPXA2026052439830](https://openairdocs.org/sdr/IPXA2026052439830.md): Bushing · worn · May 12, 2026 · N394UP · Boeing 767381
  > WORN - BUSHING, NR 2 ENG R/H CORE COWL R/H SIDE PRESSURE RELIFE DOOR UPPER AND LOWER SIDE, TOTAL: 2EA..INSTALL NEW BUSHING I.A.W SRM 51-40-02-0G REV.55 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-24 REV. 50
- [SDR FDEA202605090577](https://openairdocs.org/sdr/FDEA202605090577.md): Bearing · worn · May 9, 2026 · N621FE · Doug MD11F
  > AFT SPHERICAL BEARING WORN. COMPLIED WITH EA 1-5450-T0386066 P2
- [SDR FDEA202605050546](https://openairdocs.org/sdr/FDEA202605050546.md): Nacelle · not reported · May 5, 2026 · N521FE · Doug MD11F
  > NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAGE COMPLY WITH EA 1-5450-T0386263 REV NR POS. P2 COMPLY WITH E..A. 1-5450-T0386263 REV NR PS P2 EA: 1-5450-T0386263 PT 2 COMPLLIED WITH EA 1-5450-T0386263 PT 2 REMOVING AND
- [SDR IXXA20260417003](https://openairdocs.org/sdr/IXXA20260417003.md): Angle · cracked · Apr 17, 2026 · N255CM · Boeing 767223
  > CRACK NOTED AY PYLON #1 HYDRAULLIC BAY INTERNAL AREA, I/B SIDE FWD UPPER CORNER, CLOSE TO BOOT-STRAP ENGINE REMOVAL TOOL ATTACHING POINT REFERENCE XTREME WO 014592 NRC 872
- [SDR UIEA2026031600090](https://openairdocs.org/sdr/UIEA2026031600090.md): Not Reported · not reported · Mar 15, 2026 · N431GT · Boeing 7474H6F
  > DEVIATION FOUND DURING PERFORMING SB-747-54A2245 ON BOTH SIDES ON NR 1 & 4 PYLON. PERFORM EI T2026A54M-360 REV 0. 2) ACCOMPLISH IAW EI T2026A54M-360 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)
- [SDR UIEA2025121301343](https://openairdocs.org/sdr/UIEA2025121301343.md): Structure · no discrepancy · Dec 13, 2025 · N780BA · Boeing 747409
  > NR 1 ENG STRUCK GSE ON TOW IN. MX IN WORK WHILE IN AOGD FOR NR 1 ENG COWL DAMAGE. CONDITIONAL INSPECTIONS C/W PER AMM 05-51-06-212 REV 115, NO DEFECTS NOTED. R & R ENG 1 LH FAN COWL ASSY PER AMM 71-11-04-014 REV 115 & IPC 71-11-04-01 FIG 1 ITEM 60 REV 33. LE
- [SDR COEA2025110613778](https://openairdocs.org/sdr/COEA2025110613778.md): Mechanism · cracked · Oct 17, 2025 · N778FX · Textrn 408
  > WO 271981 NR 5 MINOR REPAIR/DISCREPANCY: #1 AND #2 ENGINE SEPERATOR FWD DOOR LINK CRACKED. CORRECTIVE ACTION: REPLACED #1 AND #2 ENGINE INERTIAL SEPERATOR CONTROL MECHANISM ASSYS IAW C408 MM 30-20-16.
- [SDR NACA202510229002](https://openairdocs.org/sdr/NACA202510229002.md): Clamp · misinstalled · Sep 30, 2025 · N567NC · Boeing 76733A
  > NR 2 ENGINE IDG WIRING HARNESS CLAMPS NOT PROPERLY INSTALLED PERFORMED PROPERLY INSTALLATION OF THE CLAMPS IN THE IDG WIRE HARNESS AT #2 ENGINE IAW SWPM 20-10-12 STEP Y PG 148.
- [SDR CALA2025100309582](https://openairdocs.org/sdr/CALA2025100309582.md): Fairing · cracked · Sep 30, 2025 · N69804 · Boeing 737924ER
  > FOUND CRACK NO-2 PYLON LOWER FIXED FAIRING INTERNAL AFT SUPPORT RIB MKD DOT 022 REF AAR N/R 99957175 ESFR ENTERED. REMOVED AND REPLECED # 2 PYLON AFT FAIRING EDGE ASSY AS PER B737 SRM 51-40-02-0G-0 AND DWG'S 313A2400 AND 313A2750.
- [SDR NACA2025092600001](https://openairdocs.org/sdr/NACA2025092600001.md): Clamp · unsecure · Sep 26, 2025 · N567NC · Boeing 76733A
  > NR 2 ENGINE IDG WIRING HARNESS CLAMPS NOT PROPERLY INSTALLED. PERFORMED PROPERLY INSTALLATION OF THE CLAMPS IN THE IDG WIRE HARNESS AT #2 ENGINE IAW SWPM 20-10-12 STEP Y PG 148.
- [SDR SWI2025F01593](https://openairdocs.org/sdr/SWI2025F01593.md): Fan Cowl · damaged · Aug 7, 2025 · N759EV · Cndair CL6002C10
  > RT UPPER FAN COWL HAS A DAMAGED HOLE (C-CHECK RO 11/22/2025)EVALUATED. MEASURES OF DAMAGE: LENGTH: 0.570", WIDTH: 0.398", DEPTH #1: 0.032", DEPTH#2: 0.029". NO ALLOWABLE DAMAGE REF CRJ700 SRM 54-14-00-101-001-A01. RECIEVED ENGINEERING INSTRUCTION AND PERFORM
- [SDR JR2R20250715257](https://openairdocs.org/sdr/JR2R20250715257.md): Skirt · bent · Jul 15, 2025 · N85355 · Emb ERJ170200LR
  > #2 ENG I/B FWD SKIRT SEAL BENT.
- [SDR IPXA2025072363772](https://openairdocs.org/sdr/IPXA2025072363772.md): Valve · damaged · Jul 4, 2025 · N325UP · Boeing 76734AF
  > CRACK - FLANGE, NO. 2 PYLON FAN AIR VALVE INLET. I.A.W. AMM 36-11-16-004-001-006, AND 36-11-16-404-015-006, REV.145, REPLACED THE FAN AIR VALVE OF NO.2 ENGINE. I.A.W AMM 36-11-16-404-015-006 REV.145, DID THE OPERATIONAL TEST, RESULT: NO LEAK WAS FOUND AND TEST
- [SDR HYIA20250522001](https://openairdocs.org/sdr/HYIA20250522001.md): Fitting · cracked · May 20, 2025 · N290CA · Cessna 402C
  > DURING SCHEDULED NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS NOTED ON THE RIGHT HAND OUTBOARD NACELLE FITTING P/N: 5292029-32. THE CRACK MEASURES.125 INCHES LONG AND IS CONSISTENT WITH OTHERS FOUND USING THE LIGHTED BORESCOPE INSPECTION TECHNIQUE (TE
- [SDR ERKR15050237717](https://openairdocs.org/sdr/ERKR15050237717.md): Actuator · broken · May 2, 2025 · Boeing 777F6N
  > PDOS ACTUATOR ON NUMBER 2 ENG. I/B FAN COWL BROKEN
- [SDR IPXA2025050533324](https://openairdocs.org/sdr/IPXA2025050533324.md): Skin · deformed · Apr 30, 2025 · N125UP · Airbus A300F4622R
  > #2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES (P/N A54612232200/201)DEFORMED FWD OF RIB J4. DOT# 110-99 JP-110 VERIFIED REMOVAL OF 2 EA SUPPORT ANGLES IAW-A300-SRM-51-40-21
- [SDR IPXA2025041273466](https://openairdocs.org/sdr/IPXA2025041273466.md): Bracket · cracked · Apr 7, 2025 · N151UP · Airbus A300F4622R
  > AFT FAIRING PANEL 475AL O/B SIDE HAS A CRACKED BRACKET ON AFT PART OF PANEL.REMOVED THE CRACKED BRAKET AT PANEL 475AL O/B SIDE IAW A300-600 SRM 51-40-21.LOCATED AND DRILLED BRACKET AT AFT FAIRING PANEL 475AL O/B SIDE IAW A300-600 SRM 51-40-21.INSTALLED BRACKET
- [SDR UIEA2025031900234](https://openairdocs.org/sdr/UIEA2025031900234.md): Skin · gouged · Mar 15, 2025 · N1373A · Boeing 76731K
  > ENG 1, LH SIDE, SKIN ON AFT TORQUE BOX WITH A GOUGE.(<P>ENG 1, LH SIDE, SKIN ON AFT TORQUE BOX DAMAGE WAS REPAIRED IAW TRE6754205 ISSUED DATE 01MAR25. RDR NUMBER: CMA-TLS-25-0015-03B DATE 01MAR25. NO FURTHER DEFECTS</P>)
- [SDR JR2R20250211338](https://openairdocs.org/sdr/JR2R20250211338.md): Pylon · chafed · Feb 11, 2025 · N86324 · Emb ERJ170200LR
  > RH PYLON, 429ML, CHAFED IN MULTIPLE PLACES OUT OF LIMITS REQUIRING ENGINEERING APPROVAL.
- [SDR JR2R20250211339](https://openairdocs.org/sdr/JR2R20250211339.md): Pylon · chafed · Feb 11, 2025 · N86324 · Emb ERJ170200LR
  > LH PYLON, 419ML, CHAFED IN MULTIPLE PLACES OUT OF LIMITS REQUIRING ENGINEERING APPROVAL.
- [SDR JR2R20250211346](https://openairdocs.org/sdr/JR2R20250211346.md): Pylon · chafed · Feb 11, 2025 · N86324 · Emb ERJ170200LL
  > LH PYLON PANEL, 419NR, CHAFED IN MULTIPLE PLACES OUT OF LIMITS REQUIRING ENGINEERING APPROVAL.
- [SDR IPXA2025021446485](https://openairdocs.org/sdr/IPXA2025021446485.md): Fairing · damaged · Feb 8, 2025 · N150UP · Airbus A300F4622R
  > FAIRING # 485 AL HAS CRACK AT LH SIDE AFT SECTION. 89-29. INSTALLED MISSING BLIND RIVET ON AFT LOWER EXTERNAL SKIN AT RIGHT SIDE AND LEFT SIDE OF THE #2 ENGINE PYLON PANEL #485AL IAW SRM 51-40-21.
- [SDR IPXA2025011407643](https://openairdocs.org/sdr/IPXA2025011407643.md): Angle · damaged · Jan 9, 2025 · N153UP · Airbus A300F4622R
  > STR-T3F18EOO3UPV4-LEFT LOWER AFT FAIRING HAS 9 EA CLIPS WITH DAMAGE ON OB SIDE REVIEWED.TREATED AND PRIMED (9EA) CLIPS IAW SRM 51-21-10
- [SDR R61A2025010400015](https://openairdocs.org/sdr/R61A2025010400015.md): Fitting · cracked · Jan 5, 2025 · N747YX · Emb ERJ170100LR
  > DURING HEAVY CHECK L/H PYLON INBD AFT LUG FITTING CRACKED. I/B AFT LUG REPLACED AS PER REPUBLIC AIRWAYS RO-030956-2024
- [SDR SWAA2024121978631](https://openairdocs.org/sdr/SWAA2024121978631.md): Web · cracked · Dec 18, 2024 · N8550Q · Boeing 7378H4
  > #2 ENGINE AFT STRUT FAIRING AFT WEDGE FWD WEB HAS CRACK PROTRUDING FROM LAP AND EXTENDING INBOARD BEYOND THE RADIUS. CRACK MEASURES 1.3 INCHES.<[01] VERIFIED CRACK PER NDT 51-00-00 PROCEDURE 23.;[02] C/W EA M-23-154-01884-REPREF.
- [SDR IPXA2024121372254](https://openairdocs.org/sdr/IPXA2024121372254.md): Inlet · cracked · Dec 12, 2024 · N329UP · Boeing 76734AF
  > R/H ENGINE INLET, INNER LIP, AT APPROXIMATE 12 O€™CLOCK POSITION, HAS 6 INCH CRACK SPANNING SEVERAL FASTENERS. REMOVED R/H ENGINE INLET COWL ASSEMBLY IN REF TO AMM TASK 71-11-01-004-002-H00
- [SDR DALA2024120311419](https://openairdocs.org/sdr/DALA2024120311419.md): Fastener · elongated · Dec 3, 2024 · N806NW · Airbus A330323
  > SHIP 3306 LH ENG LAPF IB FASTENER HOLE ELONGATED. CORRECTIVE ACTION: REMOVED OLD DOUBLER AND REAMED THE WORN HOLE, APPLIED FREEZE PLUG AND DOUBLER REPAIR WITH MATERIAL: 2024-0-0.071" AS PER PRI 622696-14 REV.0. (0690405)
- [SDR HALA20241108317](https://openairdocs.org/sdr/HALA20241108317.md): Ramp · damaged · Nov 7, 2024 · N202HA · Airbus A321271N
  > ETOPS - FIRELOOP RAMP ASSY-PYLON DAMAGED #2 ENGINE. REMOVED AND REPLACED RAMP ASSY COMPLETE WITH DETECTORS #2 ENG PER AMM 26-12-16.OPS CHECK GOOD OK FOR SERVICE
- [SDR CALA2024101800854](https://openairdocs.org/sdr/CALA2024101800854.md): Structure · damaged · Oct 16, 2024 · N25982 · Boeing 7879
  > L ENG EVIDENCE OF BIRDSTRIKE ON ARRIVALREFERENCE AMM 05-51-18-00A-280A ACCOMPLISHED INSPECTION AROUND BIRD STRIKE AREA OF NO.1 ENGINE FOUND NO DAMAGE AROUND AND BEHIND NO.1 ENGINE. ACCOMPLISHED INSPECTION FOR BIRD STRIKE NO.1 ENGINE PER AMM G71-00-00-29A-280C
- [SDR SWAA2024100737737](https://openairdocs.org/sdr/SWAA2024100737737.md): Web · cracked · Sep 14, 2024 · N8651A · Boeing 7378H4
  > RIGHT WING TRANSVERSE WEB ABOVE THE #2 PYLON AFT TIP IS CRACKED AT O/B UPPER END<[01] REMOVED; REPLACED; AND INSTALLED A NEW TRANSVERSE WEB (LOT#1569586-1) AT R/W ABOVE THE #2 PYLON AFT TIP IAW SRM 51-40-02 AND BOEING DWG 115A2512 SH 4.;[02] VERIFIED CORRECTIV
- [SDR DALA2024091609073](https://openairdocs.org/sdr/DALA2024091609073.md): Screw · missing · Sep 11, 2024 · N370NB · Airbus A319114
  > SHIP 3170 SCREW MISSING ON #2 ENGINE PYLON. CORRECTIVE ACTION: INSTALLED MISSING PYLON SCREW ON #2 ENG REF A320 AIPC 54-52. A/C OK FOR SVC. (6048663)
- [SDR SWAA2024091636197](https://openairdocs.org/sdr/SWAA2024091636197.md): Bracket · separated · Sep 10, 2024 · N7745A · Boeing 7377BD
  > L/H ENGINE LOW PRESSURE TURBINE CASE COOLING TUBE SUPPORT ANGLE BRACKET; AT 4 OCLOCK POSITION; FORWARD FLANGE IS SEPARATED (SHEARED) FROM BRACKET. REMOVED AND REPLACED L/H ENGINE LOW PRESSURE TURBINE CASE COOLING TUBE SUPPORT ANGLE BRACKET; AT 4 O?CLOCK POSIT
- [SDR SWIA2024091200819](https://openairdocs.org/sdr/SWIA2024091200819.md): Structure · bent · Aug 19, 2024 · N453SW · Cndair CL6002B19
  > LH LEADING EDGE 530JL HAS SLIGHT BEND NEAR TRAILING EDGE INBOARD SIDE. APPROX 1.25" FROM TRAILING EDGE, AND 5.75" LONG STARTING FROM INBOARD EDGE. (FILED OPEN) REMOVED LEADING EDGE 530JL INBOARD RIB AND REWORKED DENT NEAR TRAILING EDGE INBOARD SIDE. APPR
- [SDR VNAA202408070029](https://openairdocs.org/sdr/VNAA202408070029.md): Transcowl · cracked · Aug 7, 2024 · N719PS · Cndair CL6002C10
  > UPON REMOVAL OF THE RH UPPER TRANSCOWL LATCH COAMING, FOUND THE UNDERLYING STRUCTURE TO BE CRACKED. REPAIRED R/H UPPER TRANSCOWL FWD DISHING IAW MHIRJ REO 670-54-21-1647 REV. A DATED 2024-06-17.
- [SDR FXTA20240802001](https://openairdocs.org/sdr/FXTA20240802001.md): Rod End · broken · Aug 1, 2024 · N408BA · Textrn 408
  > RH INERTIAL SEPARATOR INOPERATIVE. AFTER LANDING MAINTENANCE FOUND ROD END BROKEN THAT CONNECTS THE ELECTRIC ACTUATOR TO THE FIRE WALL.
- [SDR JR2R20240727523](https://openairdocs.org/sdr/JR2R20240727523.md): Ground Stud · corroded · Jul 27, 2024 · N84307 · Emb ERJ170200LR
  > LH WING IDG GROUNDING BRACKET CORRODE O/B AND AFT OF #1 PYLON. REPAIRED
- [SDR JR2R202407276316](https://openairdocs.org/sdr/JR2R202407276316.md): Ground Stud · corroded · Jul 27, 2024 · N84307 · Emb ERJ170200LR
  > #2 ENGINE IDG GROUNDING BRACKET LOCATED IN THE TRAILING EDGE CAVITY O/B OF THE #2 PYLON CORRODED. REPAIRED
- [SDR IPXA2024072392472](https://openairdocs.org/sdr/IPXA2024072392472.md): Structure · damaged · Jul 19, 2024 · N264UP · Doug MD11F
  > *SUPPLEMENTAL SDR* #1 ENGINE PYLON DAMAGED. REMOVED AND REPLACED #1 ENG WING PYLON AFT LOWER FAIRING PER AMM 54-81-01 AND SRM 51-31-01.
- [SDR YENA2024062100891](https://openairdocs.org/sdr/YENA2024062100891.md): Door · no test · Jun 17, 2024 · N3132J · Airbus BD5001A11
  > FLT#1530, RSW-JFK. ' R ENG PCE DOOR OPEN ON DESCENT DURING ICE TEST; ACCOMPLISHED T/R PRES RELIEF DOOR OPEN INSP PER AMP 05-51-25 NO DEFECTS NOTED CLOSED PER AMP 78-36-04 A/C OK TO CONT IN SVC.'
- [SDR CALA2024060701712](https://openairdocs.org/sdr/CALA2024060701712.md): Stiffener · buckled · Jun 5, 2024 · N17104 · Boeing 757224
  > REF AMES NON ROUTINE 171415-0400-0044. GENERATING ITEM:ZONE 430 OPEN.FEED BACK CABLE COVER PLATE IS BENT AND CRACKED TAG#6936. REPAIRED NO.1 ENGINE O/B T/R FEEDBACK CABLE SUPPORT STIFFENER P/ N LJ70309 IAW AMES DOCUMENT 47618REA03, DATED 6/4/2024 UNITED EC /RA
- [SDR CALA2024060401690](https://openairdocs.org/sdr/CALA2024060401690.md): Drain · blocked · Jun 3, 2024 · N661UA · Boeing 767322
  > NO. 1 ENGINE CENTER DRAIN AND RACEWAY DRAIN LINES INSPECTION {B767-71-3-0006} - HEAVY DEPOSITS FOUND IN INBOARD SIDE OF CENTRE RACEWAY DRAIN BLOCKAGE ON ITEMS 725,740 AND 107 FURTHER IVESTIGATION REQUIRED FOR ITEMS 70,97,90. BLOCKAGE CLEARED ON DRAIN RACEWAY
- [SDR MK1Y20240602003](https://openairdocs.org/sdr/MK1Y20240602003.md): Strut · not reported · Jun 2, 2024 · N447CM · Boeing 767330
  > REPAIR - STRUT #2 AFT FIXED FAIRING, INBD SKIN PANEL.
- [SDR COEA2024080730738](https://openairdocs.org/sdr/COEA2024080730738.md): Mount · cracked · May 28, 2024 · N738FX · Textrn 408
  > WO 258209 NR 2 DISCREPANCY: R/H COWL, NACELLE, INERTIAL SEPARATOR MOUNTING STRUCTURE HAS CRACKS. CORRECTIVE ACTION: REPAIRED PER SR-408-ATA54-42396.
- [SDR UIEA2024052500446](https://openairdocs.org/sdr/UIEA2024052500446.md): Panel · damaged · May 27, 2024 · N418MC · Boeing 74747UF
  > NO.4 PYLON 482EL SCREW HOLE FOUND ELONGATED.(<P>#4 PYLON PANEL 482EL FABRICATED IAW RI NO: RI-54-51-16889 REV A. HFEC INSPECTION C/W PER NTM PART 6 51-00-00 PROCEDURE 23 REV 176 ON BEND RAD11 AREA, NO CRACK FOUND</P>)

Next page: https://openairdocs.org/jasc/5400/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 jasc_code = '5400'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5400/reports

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