# Service difficulty reports: JASC 5410

A list on [JASC 5410](https://openairdocs.org/jasc/5410.md).

Reports filed under 5410 · Nacelle/Pylon, Main Frame, newest first.

Page 1 of 82 · 4,100 reports

- [SDR CALA2026102320543](https://openairdocs.org/sdr/CALA2026102320543.md): Access Door · missing · Oct 22, 2026 · N57868 · Boeing 75733N
  > PDA 2 PANEL 443HL,HP2 DUCT CHECK VALVE ACCESS PANEL, DEPARTED A/C REF LP 3821419. UPDATED LP WITH SDR AND SFR ACCOMPLISHED ECRA 5450-03166 REF LP 3821419
- [SDR HYIA20261022001](https://openairdocs.org/sdr/HYIA20261022001.md): Beam · cracked · Oct 20, 2026 · N160PB · Cessna 402C
  > DURING SCHEDULED ENGINE BEAM REPLACEMENT, UPON REMOVAL OF ENGINE BEAM A CRACK WAS VISUALLY IDENTIFIED ON THE INBOARD FACE OF THE ENGINE BEAM. THIS CRACK IS EMANATING FROM A FASTENER LOCATION COMMON TO THE INBOARD VERTICAL CROSS OVER BEAM UPRIGHT (OEM: 5654107-
- [SDR FDEA202610201624](https://openairdocs.org/sdr/FDEA202610201624.md): Structure · corroded · Oct 20, 2026 · N923FD · Boeing 757204
  > NR 2 ENGINE PYLON STRUT, OTBD LOWER STRUCTURE NAC S 146.675 FOUND CORRODED.
- [SDR CALA2026102120486](https://openairdocs.org/sdr/CALA2026102120486.md): Access Door · missing · Oct 17, 2026 · N33103 · Boeing 757224
  > NR 1 ENG OIL FILLER ACCESS DOOR FOUND MISSING DURING WALK AROUND. THE OIL FILLER ACCESS DOOR WAS REPLACED IAW AMM 72-00-00, REV 141.
- [SDR FDEA202610151595](https://openairdocs.org/sdr/FDEA202610151595.md): Strut · corroded · Oct 15, 2026 · N923FD · Boeing 757204
  > ENG #2 PYLON STRUT INBD LOWER CHORD STA 144.425 CORROSION. THIS DISCREPANCY WAS ACCOMPLISHED ON EA # F-5430-T0389069 P1 TITLE: NACELLES / PYLONS-SKIN / PLATES / PANELS - CORROSION BLENDOUT #2 PYLON, LHS (INBD) SIDE SKIN DOUBLER INNER SURFACE, PP STA 153-16
- [SDR EE4Y2026100525064](https://openairdocs.org/sdr/EE4Y2026100525064.md): Heat Shield · cracked · Oct 5, 2026 · N306JB · Emb ERJ190100IGW
  > DURING INSPECTION, IT WAS NOTED THAT ENGINE #1 PYLON AFT FAIRING HEAT SHIELD SKIN #8 HAD AN EXISTING REPAIR AT THE AFT LOWER CORNER OF THE EXHAUST GRILL CUTOUT. ACCORDING TO PREVIOUS OPERATOR RECORDS, THIS REPAIR LACKS MATERIAL TRACEABILITY. CONSEQUENTLY, IT W
- [SDR EE4Y2026100525063](https://openairdocs.org/sdr/EE4Y2026100525063.md): Link · corroded · Oct 5, 2026 · N306JB · Emb ERJ190100IGW
  > DURING THE ACCOMPLISHMENT OF REF. A, THE PYLON LOWER LINK FITTING OUTBOARD LUG FIXED BUSHINGS WERE FOUND WITH WEAR. AFTER REMOVAL OF THE BUSHINGS FOR REPLACEMENT, LOCALIZED CORROSION WAS DETECTED BETWEEN THE LUG SURFACE AND THE PRODUCTION REINFORCEMENT ANGLE.
- [SDR IPXA2026101387189](https://openairdocs.org/sdr/IPXA2026101387189.md): Hinge · worn · Oct 4, 2026 · N364UP · Boeing 767346
  > RT AFT FAIRING DOOR NR 4 HINGE WORN, NR 2 PYLON. REPAIR DAMAGE AREA I.A.W UPS EO-98882-REQ1 REV1. 2. REPLACED NEW HINGE FITTING (P/N: 313T3325U6) I.A.W SRM 51-40-02-0G REV. 56 AND BOEING DWG NO: 313T3340 SHEET 27 REV. B.
- [SDR CALA2026100620144](https://openairdocs.org/sdr/CALA2026100620144.md): Door · damaged · Oct 3, 2026 · N786UA · Boeing 777222
  > RIGHT ENGINE NACELLE DRAIN ACCESS PANEL FOUND OPEN ON ARRIVAL. R & R DOOR ASSEMBLY IAW AMM 78-31-19. DOOR ADJUSTED AND OPS CHECK CARRIED OUT, FOUND SATISFACTORY.
- [SDR JR2R20261003051](https://openairdocs.org/sdr/JR2R20261003051.md): Heat Shield · chafed · Oct 3, 2026 · N85320 · Emb ERJ170200LL
  > LEFT AFT PYLON FAIRING HEAT SHIELD HAS EVIDENCE OF CHAFING. REPAIRED PER ETD.
- [SDR CALA2026100720169](https://openairdocs.org/sdr/CALA2026100720169.md): Fitting · cracked · Oct 2, 2026 · N17126 · Boeing 757224
  > NR 2 ENG PYLON NACELLE MID STRUCTURE BULKHEAD PP STA 174.30 RBL 9 WITH CRACK. ACCOMPISHED REPAIR ON #2 ENG PYLON MID-BULKHEAD FWD RH LOWE R-FLANGE IAW EC/RA#:5450-03163,VT EA#:757-5450-13-A4626.REF:NR#1 9168
- [SDR IPXA2026100639564](https://openairdocs.org/sdr/IPXA2026100639564.md): Panel · cracked · Oct 1, 2026 · N158UP · Airbus A300F4622R
  > AFTER REMOVAL OF SEAL, FOUND PANEL 423BL CRACKED. INSTALLED DOUBLER ON PANEL 423BL IAW SRM 54-52-51-201-C1, PARAGRAPH D.2. STEP U, FIGURE 204.
- [SDR CALA2026100520118](https://openairdocs.org/sdr/CALA2026100520118.md): Door · missing · Sep 30, 2026 · N674UA · Boeing 767322
  > PDA 2 MISSING ACCESS PANEL ON I/B NUMBER 2 ENGINE REPLACED MISSING ACCESS PANEL ON I/B ENGINE 2 REF IPC 54-53-01-17. AIRCRAFT OK TO CONTINUE PARTS USED: 76-5453-3-0047,QTY:1
- [SDR HYIA20261001001](https://openairdocs.org/sdr/HYIA20261001001.md): Beam · cracked · Sep 30, 2026 · N290CA · Cessna 402C
  > DURING HIGH TIME ENGINE BEAM REPLACEMENT, UPON REMOVAL OF ENGINE BEAM A CRACK WAS VISUALLY IDENTIFIED ON THE INBOARD FACE OF THE RH INBOARD ENGINE BEAM. THIS CRACK IS EMANATING FROM A FASTENER LOCATION COMMON TO THE INBOARD VERTICAL CROSS OVER BEAM UPRIGHT (OE
- [SDR 1Q2R2026093020063](https://openairdocs.org/sdr/1Q2R2026093020063.md): Latch · gouged · Sep 28, 2026 · N706PS · Cndair CL6002C10
  > R/H ENGINE LATCH, BEAM LATCH, STRUCTURE IS GOUGED. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-131113 REV. 0, AND REO 670-54-14-1357 REV. -.
- [SDR YENA2026092500902](https://openairdocs.org/sdr/YENA2026092500902.md): Rub Strip · damaged · Sep 24, 2026 · N4080J · Airbus A321271NX
  > FLT 1621, LHR-BOS. (ETOPS) "DAMAGE FOUND ON ENG 2 FAN CASE RUB STRIP. DAMAGE OUT OF LIMITS PER AMM 72-21-01-220-802-A. DENT 1 IS.43 X.43 DENT 2 IS.43 IN LENGTH.125 IN W AREA IS LIMIT; PERFORMED REPAIR OF ENG #2 FAN CASE RUB STRIP @ 7 0'CLOCK POSITION I
- [SDR R61A2026092800289](https://openairdocs.org/sdr/R61A2026092800289.md): Panel · missing · Sep 23, 2026 · N402YX · Emb ERJ170200LR
  > NR 1 PYLON PANEL MISSING UPON ARRIVAL. INSTALLED PYLON SIDE FAIRING PANEL
- [SDR DALA2026092305313](https://openairdocs.org/sdr/DALA2026092305313.md): Bearing · damaged · Sep 22, 2026 · N415DX · Airbus A330941
  > NR 2 PYLON SPIGOT BEARING DAMAGE. REPAIRED PER ERA 636951-14. (1826757) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026092305312](https://openairdocs.org/sdr/DALA2026092305312.md): Bearing · damaged · Sep 22, 2026 · N415DX · Airbus A330941
  > NR 1 PYLON SPIGOT BEARING DAMAGE. REPAIRED PER ERA 636950-14. (1826456) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026092305310](https://openairdocs.org/sdr/DALA2026092305310.md): Fitting · corroded · Sep 22, 2026 · N415DX · Airbus A330941
  > NR 1 PYLON, AFT SPIGOT FITTING TOP SURFACE HAS POWDERY SUBSTANCE RESEMBLING CORROSION. COMPLIED WITH ERA 636950-14 REV ORIGINAL. (1826790) AIRCRAFT WAS GROUNDED.
- [SDR CALA2026092519801](https://openairdocs.org/sdr/CALA2026092519801.md): Panel · missing · Sep 21, 2026 · N818UA · Airbus A319131
  > FOUND NR 1 PYLON SECTION PANEL MISSING, REF IPC 54-57-22-07A, ITEM 90, DETERMINED TO BE CATEGORY 2 50.75 SQ-IN R & R THE PYLON TO NACELLE PROFILE PANEL INBD IAW AMM 54-57-22.
- [SDR YENA2026092300868](https://openairdocs.org/sdr/YENA2026092300868.md): Spigot · corroded · Sep 21, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, RT PYLOHN RECEPTACLE FITTING AND SPIGOT BALL JOINT CORRODED. REMOVED AND REPLACED RECEPTACLE FITTING (SPIGOT LOWER FITTING) IAW SRM 54-51-12-300-002, STEP 2.A AND PERFORMED VISUAL INSPECTION ON SPIGOT BALL JOINT, IAW AMM 54-51-41-400
- [SDR YENA2026092300867](https://openairdocs.org/sdr/YENA2026092300867.md): Ball Joint · rusted · Sep 21, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, CORROSION RECEPTACLE FITTING AND SPIGOT BALL JOINT LT PYLON. REMOVED AND REPLACED RECEPTACLE FITTING (SPIGOT LOWER FITTING) IAW SRM 54-51-12-300-002, STEP 2.A AND PERFORMED VISUAL INSPECTION ON SPIGOT BALL JOINT IAW AMM 54--51-41-40
- [SDR IPXA2026101834137](https://openairdocs.org/sdr/IPXA2026101834137.md): Plate · damaged · Sep 19, 2026 · N146UP · Airbus A300F4622R
  > PANEL 485AL FWD INNER AREA, LH UPPER LONGERON HAS WEAR DAMAGE WITH MATERIAL LOSS. REPLACED FAIRING ATTACH PLATE ON PANEL 485AL FWD INNER AREA, LT UPPER, IAW SRM 54-55-51, AND 51-40-21.
- [SDR CALA2026092219662](https://openairdocs.org/sdr/CALA2026092219662.md): Seal · cracked · Sep 19, 2026 · N836UA · Airbus A319131
  > RIGHT PYLON FWD INBD BLADE SEAL CRACKED. REMOVED AND REPLACED BLADE SEAL AT RT PYLON FWD INBD IAW SRM 51-42-11.
- [SDR YENA2026092100858](https://openairdocs.org/sdr/YENA2026092100858.md): Tie Rod · excess play · Sep 19, 2026 · N4064J · Airbus A321271NX
  > FLT 2220, LHR-JFK. (ETOPS) DURING T/C A320-29-10-00-220-004A ON W/O 1524471 FOUND LOWER HYDRAULIC INTER. TIE ROD ON ENG NR 2 TO HAVE AXIAL PLAY OUT OF LIMITS, R & R ENG NR 2 PYLON/ ENGINE INTERFACE TIE ROD (LOWER) IAW AMM 29-15-61.
- [SDR YENA2026092100857](https://openairdocs.org/sdr/YENA2026092100857.md): Tie Rod · excess play · Sep 19, 2026 · N4064J · Airbus A321271NX
  > FLT 2220, LHR-JFK. (ETOPS) DURING T/C A320-29-10-00-220-004A ON W/O 1524471, FOUND UPPER HYDRAULIC INTER. TIE ROD ON ENG NR 2 TO HAVE AXIAL PLAY OUT OF LIMITS. R & R THE ENG NR 2 PYLON/ ENGINE INTERFACE TIE ROD (UPPER) IAW AMM 29-15-61.
- [SDR IPXA2026100102772](https://openairdocs.org/sdr/IPXA2026100102772.md): Panel · cracked · Sep 17, 2026 · N158UP · Airbus A300F4622R
  > PANEL 423BL LOWER AREA WITH 2 CRACKS. REMOVED (IEA) SEAL AND SEAL RETAINER AT PANEL 423BL IAW SRM 51-40-21. REINSTALLED SEAL AND SEAL RETAINER AT PANEL 423BL IAW SRM 51-40-21.
- [SDR IPXA2026092286713](https://openairdocs.org/sdr/IPXA2026092286713.md): Cowling · cracked · Sep 17, 2026 · N355UP · Boeing 76734AF
  > CRACKED SKIN, NR 1 ENG RT CORE COWL LOWER FWD SKIN NEAR NO.1 LATCH. PERFORM REPAIR I.A.W UPS EO-98690-REQ1 REV.1.
- [SDR IPXA2026092289443](https://openairdocs.org/sdr/IPXA2026092289443.md): Nose Cowl · dented · Sep 17, 2026 · N355UP · Boeing 76734AF
  > DENTED NR 1 NOSE COWL INLET AT 7 O'CLOCK POSITION. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2026092290656](https://openairdocs.org/sdr/IPXA2026092290656.md): Nose Cowl · dented · Sep 17, 2026 · N355UP · Boeing 76734AF
  > DENTED NR 1 ENG NOSE COWL INLET AT 5 O'CLOCK POSITION. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2026092290813](https://openairdocs.org/sdr/IPXA2026092290813.md): Nose Cowl · dented · Sep 17, 2026 · N355UP · Boeing 76734AF
  > DENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL NEAR 2:00 TO 6:00 POS. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SAT
- [SDR IPXA2026092290842](https://openairdocs.org/sdr/IPXA2026092290842.md): Nose Cowl · dented · Sep 17, 2026 · N355UP · Boeing 76734AF
  > DENTED NR 1 ENGINE NOSE COWL INLET AT 6 O'CLOCK POSITION. UT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( ‘ DIA: 0.2", 27" FROM FWD EDGE, 31.5" FROM UPPER EDGE ‘¡ DIA: 0.4", 32.4" FROM FWD EDGE, 31" FROM UPPER EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF
- [SDR IPXA2026102245620](https://openairdocs.org/sdr/IPXA2026102245620.md): Fan Cowl · corroded · Sep 15, 2026 · N146UP · Airbus A300F4622R
  > NR 1 ENG.I/B FAN COWL INNER EDGE SEAL FAN COWL HAS SURFACE CORROSIONS AND DEEP WEAR. VERIFIED REMOVAL OF RUB STRIP (INNER SEAL) ON THE #1 ENG.I/B FAN COWL IAW A300 SRM 51-40-21.
- [SDR AALA202609182187](https://openairdocs.org/sdr/AALA202609182187.md): Hinge Fitting · worn · Sep 15, 2026 · N901AA · Airbus A321231
  > AIRCRAFT IN BASE MAINTENANCE: ENGINE 1 INBOARD FAN COWL FORWARD HINGE WORN - REPLACED HINGE FITTING PER CMM 71-13-00
- [SDR SWAA2026091706067](https://openairdocs.org/sdr/SWAA2026091706067.md): Inlet · cracked · Sep 13, 2026 · N8632A · Boeing 7378H4
  > OTS-#2 ENGINE INLET COWL CRACKED_ VERIFIED CRACK AND MARKED ENDS. CRACK MEASURES 3.0IN LONG. REF NDT PART 6 51-00-00. PROCEDURE 23. REMOVED AND REPLACED #2 ENG INLET COWL PER 7111-E-17634-NG (AD - REP - INLET COWL AND CRUSHABLE WEAR SPACERS) TTG8Q01EKLT2 OPS
- [SDR SWAA2026091483658](https://openairdocs.org/sdr/SWAA2026091483658.md): Fairing · cracked · Sep 10, 2026 · N8736J · Boeing 7378
  > NR 1 ENGINE AFT FAIRING PLUME SUPPRESSOR CRACK, C/W EA 26-154-02465
- [SDR WX0A2026090932951](https://openairdocs.org/sdr/WX0A2026090932951.md): Hinge · corroded · Sep 9, 2026 · N206NV · Airbus A320214
  > (AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 4000-0010: 1205-06 ENGINE NR 2 PYLON OVERPRESSURE PANEL 481CR HINGE CORRODED. ENGINE NR 2 PYLON OVERPRESSURE PANEL 481CR HINGE REPLACED IAW SRM 51-42-11 REV.159.
- [SDR SWAA2026091182854](https://openairdocs.org/sdr/SWAA2026091182854.md): Skin · peeling · Sep 7, 2026 · N901WN · Boeing 7377H4
  > FOUND ENG 1 OUTBOARD T/R INNER DUCT SKIN PEELING DAMAGE EXCEEDS ALLOWABLE LIMITS IAW SRM 54-30-01A-3. C/W PERMANENT REPAIR ON ENG#1 O/B T/R INNER DUCT SKIN REF SRM 54-30-01-2R-3.
- [SDR SWAA2026092374661](https://openairdocs.org/sdr/SWAA2026092374661.md): Fan Cowl · damaged · Sep 5, 2026 · N259WN · Boeing 7377H4
  > ELONGATED HOLE LOCATED ON OUTBOARD FAN COWL 0.500 INCH FROM FWD EDGE AND 3.375 INCH FROM LOWER EDGE AT ENGINE 1. EVALUATED HOLE LOCATED ON OTBD FAN COWL 0.500 INCH FROM FWD EDGE AND 3.375 INCH FROM LOWER EDGE AT ENGINE AND FOUND WITHIN LIMITS IAW CMM 71-13-3
- [SDR SWAA2026090889890](https://openairdocs.org/sdr/SWAA2026090889890.md): Strut · cracked · Sep 3, 2026 · N449WN · Boeing 7377H4
  > NR 1 ENGINE TRF NR 2 STRUT HAS A CRACK ON C2 MEASURING.400 AND A CRACK ON C1 MEASURING.800. OK TO CONTINUE ON 350 CYCLE REINSPCECT INTERVAL IAW M-25-172-01664 TRIGGERING TRF MOUNT INSPECTION 7256-I-11716-E FOR LARGEST CUMULATED CRACK FINDINGS FROM 0.79 INC
- [SDR IPXA2026092823749](https://openairdocs.org/sdr/IPXA2026092823749.md): Fairing · cracked · Sep 1, 2026 · N158UP · Airbus A300F4622R
  > CRACK ON #1 ENG AFT LWR PYLON FAIRING, LOWER SKIN. LOWER AFT FAIRING REMOVED AND INSTALLED ON MPC 400 T3F18E007EGD6.
- [SDR UIEA2026083000826](https://openairdocs.org/sdr/UIEA2026083000826.md): Fairing · damaged · Sep 1, 2026 · N489MC · Boeing 747412F
  > NR 2 PYLON AFT FAIRING FWD LWR FIXED FAIRING DRAIN INBD AND OTBD AREA FOUND SEVERAL RIVETS LOOSE. NR PYLON AFT FAIRING DRAIN REPAIRED IAW RI-54-50-18444, REV.A. NO FURTHER DEFECTS NOTED.
- [SDR VNAA2026083145](https://openairdocs.org/sdr/VNAA2026083145.md): Hinge · bent · Aug 31, 2026 · N705PS · Cndair CL6002C10
  > LEFT ENGINE COWLING IS UNABLE TO BE OPENED DUE TO A DENTED HINGE LINE THAT WAS BENT UPON ARRIVAL. REPAIRED IAW REO 670-53--31-1226, REV-.
- [SDR SWAA2026090180716](https://openairdocs.org/sdr/SWAA2026090180716.md): Fairing · cracked · Aug 31, 2026 · N8733M · Boeing 7378
  > NR 1 ENGINE AFT FAIRING HEAT SHIELD PLUME SUPPRESSOR HAS A FIVE INCH CRACK 28 INCHES FORWARD OF AFT TIP. PERFORMED TIME LIMITED REPAIR IAW EA 26-154-02358. AIRCRAFT OKAY FOR CONTINUED SERVICE.
- [SDR SWIA2026082977229](https://openairdocs.org/sdr/SWIA2026082977229.md): Frame · chafed · Aug 29, 2026 · N280SY · Emb ERJ170200LL
  > CHAFING ON INBD OF FR 1 OF RT AFT PYLON FAIRING. REMOVED AND REPLACED RT AFT PYLON FR1 IAW SRM 51-40-02, & 51-40-08.
- [SDR FDEA202608281248](https://openairdocs.org/sdr/FDEA202608281248.md): Strut · cracked · Aug 28, 2026 · N993FD · Boeing 7572Q8
  > NR 2 NACELLE STRUT, RIGHT SIDE SKIN, THROUGH ACCESS 443AR, SHOWS A CRACK WITH NO VISIBLE STOP HOLE. THIS ITEM HAS BEEN ACCOMPLISHED ON EA F-5430-T0388382 P1.
- [SDR IXXA2026082800002](https://openairdocs.org/sdr/IXXA2026082800002.md): Cowling · out of tolerance · Aug 28, 2026 · N761CX · Boeing 767223
  > NR 1 ENGINE INBD CORE COWL GAPS ARE OUT OF LIMITS ON TRAILING EDGE IAW AMM
- [SDR IXXA2026082800001](https://openairdocs.org/sdr/IXXA2026082800001.md): Cowling · out of tolerance · Aug 28, 2026 · N761CX · Boeing 767223
  > NR 1 ENGINE OTBD CORE COWL GAPS ARE OUT OF LIMITS ON TRAILING EDGE IAW AMM.
- [SDR IXXA20260919NKJ01](https://openairdocs.org/sdr/IXXA20260919NKJ01.md): Cowling · cracked · Aug 27, 2026 · N233AZ · Boeing 767323
  > NUMBER 2 ENGINE OUTBOARD CORE COWL INTERNAL AREA #5 RIB/FRAME HAS CHAFING/WEAR MARKS (IS CRACKED)

Next page: https://openairdocs.org/jasc/5410/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 = '5410'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5410/reports

---
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