# Service difficulty reports: JASC 5415

A list on [JASC 5415](https://openairdocs.org/jasc/5415.md).

Reports filed under 5415 · Nacelle/Pylon, Attach Fittings, newest first.

Page 1 of 27 · 1,305 reports

- [SDR DALA2026101905737](https://openairdocs.org/sdr/DALA2026101905737.md): Strap · failed · Oct 19, 2026 · N430DX · Airbus A330941
  > SHIP 3430 ENGINE BOOTSTRAP FAILED. REPLACED PER ERA 637508-14 REV 0 AND 1. (1873828) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026101905736](https://openairdocs.org/sdr/DALA2026101905736.md): Fitting · damaged · Oct 18, 2026 · N430DX · Airbus A330941
  > 2 EA FITTINGS DAMAGED MPN G5451006620000 IN NBR 1 ENG PYLON. CORRECTIVE ACTION: REMOVED AND REPLACED 2 EA DAMAGED FITTINGS PER AIRBUS DRAWING G54510066. (1872237) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026101905735](https://openairdocs.org/sdr/DALA2026101905735.md): Fitting · damaged · Oct 18, 2026 · N430DX · Airbus A330941
  > FWD FITTING MPN G5451209120100 DAMAGED IN NBR 1 ENG PYLON. REPLACED FITTING MPN G5451209120100 PER AIRBUS DRAWING G54512091. (1872235) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026100705547](https://openairdocs.org/sdr/DALA2026100705547.md): Drag Brace · cracked · Oct 1, 2026 · N6703D · Boeing 757232
  > RIGHT WING L/E ABOVE NR 2 PYLON, ENGINE DRAG BRACE FITTING CLAMP, NR 13 HOLE HAS A CRACK INDICATION. REAMED HOLE NR 13 ON RT WING L/E ABOVE NR 2 PYLON ENG DRAG BRACE FITTING IAW PRI ER/A 573570-14. (1843141)(AIRCRAFT GROUNDED)
- [SDR IPXA2026092803255](https://openairdocs.org/sdr/IPXA2026092803255.md): Drag Fitting · cracked · Sep 5, 2026 · N444UP · Boeing 75724APF
  > FAULT: RIGHT WING PYLON HOLE #4 HAS 1EA CRACK AT 2 O'CLOCK AT TOP OF FITTING. COMPLIED WITH PER EO -88069-JIC11. REVIEWED
- [SDR IPXA2026092803215](https://openairdocs.org/sdr/IPXA2026092803215.md): Drag Fitting · cracked · Sep 5, 2026 · N444UP · Boeing 75724APF
  > RIGHT WING PYLON HOLE #5 HAS 2EA CRACKS AT 11 AND 4 O'CLOCK AT TOP OF FITTING AND 2EA CRACKS AT 7 AND 4 O'CLOCK AT BOTTOM OF SKIN. IAW EO -88069-JIC11 STEP # 3 AND NDT MANUAL PART 6, 51-00-16.
- [SDR HYIA20260827001](https://openairdocs.org/sdr/HYIA20260827001.md): Fitting · cracked · Aug 25, 2026 · N678JG · Cessna 402C
  > DURING MAINTENANCE, A CRACK WAS IDENTIFIED ON THE INBD LEG OF THE RT INBD NACELLE FITTING, THIS CRACK MEASURES APPROXIMATELY.144 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN MEL-54-02R2 TO SATISFY AD2017-10-0
- [SDR IXXA20260822001](https://openairdocs.org/sdr/IXXA20260822001.md): Attach Angle · cracked · Aug 22, 2026 · N337AZ · Boeing 767323
  > NR 2 PYLON OTBD AFT ATTACH ANGLE IS CRACKED.
- [SDR DALA2026071604192](https://openairdocs.org/sdr/DALA2026071604192.md): Attach Fitting · corroded · Jul 14, 2026 · N307DU · Airbus BD5001A11
  > CORROSION FOUND ON RH OUTER UPPER FORWARD PYLON ATTACH FITTINGS R7 AND R8. REMOVED AND REPLACED BEARINGS PER BOMBARDIER DWG C01627010 -B. (LP# 1700103; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026071404139](https://openairdocs.org/sdr/DALA2026071404139.md): Drag Fitting · corroded · Jul 13, 2026 · N550NW · Boeing 757251
  > IN REF CARD 5720-01100-02A STEP. 28, LT ENG DRAG FTG CLAMP, CORROSION POINTS ON FASTENER HOLE NR 2. LEVEL 2 CORROSION ON FASTENER HOLE NR 2 WAS REAMED AT FINAL DIMENSION 0.5780 PER CARD 5720-01100-02A STEP 29. INSPECTION HFEC WAS ACCOMPLISHED, NO CRACKS WERE
- [SDR JR2R20260712633](https://openairdocs.org/sdr/JR2R20260712633.md): Attach Angle · cracked · Jul 13, 2026 · N88326 · Emb ERJ170200LR
  > LH AFT PYLON FAIRING, INBOARD ANGLE OF HEAT SHIELD 3 IS CRACKED. REPLACED
- [SDR AALA202607085984](https://openairdocs.org/sdr/AALA202607085984.md): Sleeve · worn · Jul 4, 2026 · N827AW · Airbus A319132
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON AFT ATTACH FITTING UPPER POSITION SLEEVE WORN. REPALCED SLEEVE PER AMM 54-51-00-200-014-A STEP 4.A.
- [SDR AALA202607082461](https://openairdocs.org/sdr/AALA202607082461.md): Shackle · worn · Jul 4, 2026 · N827AW · Airbus A319132
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON FORWARD ATTCH FITTING / SHACKLE WORN. REPLACED SHACKLE PER AMM 54-51-00-200-009-A STEP 4.A.
- [SDR JR2R20260627851](https://openairdocs.org/sdr/JR2R20260627851.md): Fitting · chafed · Jun 27, 2026 · N85323 · Emb ERJ170200LL
  > NR 2 ENGINE PYLON INBOARD AND OUTBOARD UPPER LINK FITTINGS ARE CHAFED & GOUGED. REPAIRED PER ETD.
- [SDR UIEA2026061400478](https://openairdocs.org/sdr/UIEA2026061400478.md): Beam · cracked · Jun 15, 2026 · N485MC · Boeing 74745EF
  > RHW L/E NEAR NO.3 PYLON O/B D-BEAM UPPER CHORD FOUND CRACK(<P>UPPER CHORD REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 FIG 201.</P>)
- [SDR DALA2026060403391](https://openairdocs.org/sdr/DALA2026060403391.md): Bearing · damaged · Jun 2, 2026 · N305DU · Airbus BD5001A11
  > BEARINGS FOUND DAMAGED ON PYLON SIDE LINK UPPER ATTACHMENT FITTING. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. COMPLIED WITH ERA 634589-14, PRI REV 0, 01, 02 AND ERA 634589-14, SECTION 1: PERMANENT REPAIR REV ORIGINAL. (LP# 1626312; AIRCRAFT WAS GROUNDED)
- [SDR CALA2026052916658](https://openairdocs.org/sdr/CALA2026052916658.md): Link · corroded · May 28, 2026 · N37255 · Boeing 737824
  > NR 1 ENGINE PYLON UPPER LINK FORWARD ATTACH POINT IS CORRODED. REMOVED NR 1 PYLON UPPER LINK AND REPLACED BUSHINGS IN THE FWD ATTACH POINT IAW AMM 51-54-03 AND SOPM 20-50-03. PNEUMATIC DUCT REMOVED FOR ACCESS AND REINSTALLED IAW AMM 36-13-01.
- [SDR R61A2026031100064](https://openairdocs.org/sdr/R61A2026031100064.md): Fitting · damaged · Mar 6, 2026 · N102HQ · Emb ERJ170200LR
  > WHILE ON HEAVY CHECK - RH OUTBOARD LOWER PYLON TO WING FITTING OUTBOARD BUSHING MIGRATED.
- [SDR YENA2026030400251](https://openairdocs.org/sdr/YENA2026030400251.md): Fillet · cracked · Mar 1, 2026 · N913JB · Airbus A321231
  > DURING HEAVY MAINTENANCE: PYLONS / LH PYLON / PYLON TO WING CENTER FILLETS / OUTBD STRIP RIB 7A AND RIB 10A / CRACK AND CORROSION – PERMANENT REPAIR; REFERENCES: /1/ STS EA 160-2026-001 REV IR /2/ AIRBUS RDAF 81708168/003/2025#A /3/ REPAIR INSTRUCTIONS TD/8170
- [SDR YENA2026030400250](https://openairdocs.org/sdr/YENA2026030400250.md): Fillet · corroded · Mar 1, 2026 · N913JB · Airbus A321231
  > DURING HEAVY MAINTENANCE: LT PYLON, PYLON TO WING CENTER FILLETS, INBD STRIP RIB 7A & RIB 10A, CORRODED. EA 160-2025-011 REV IR /2/ AIRBUS RDAF 81708156/003/2025#A /3/ REPAIR INSTRUCTIONS TD/81708156/012/2025#A. DESCRIPTION: DURING CURRENT (01/2026) M1 CHE
- [SDR AALA202602094532](https://openairdocs.org/sdr/AALA202602094532.md): Attach Fitting · worn · Jan 22, 2026 · N829AW · Airbus A319132
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON AFT SHACKLE ATTACH FITTING AT RIB 10 WORN. REPLACED ATTACH FITTING PER AMM 54-51-17-400-002-A.
- [SDR JR2R20260120898](https://openairdocs.org/sdr/JR2R20260120898.md): Attach Fitting · chafed · Jan 20, 2026 · N87302 · Emb ERJ170200LL
  > #2 ENG UPPER DRAG LINK O/B FWD ATTACH FITTING CHAFED ON THE EDGE. REPAIRED
- [SDR YENA2026012100055](https://openairdocs.org/sdr/YENA2026012100055.md): Fillet · corroded · Jan 18, 2026 · N2047J · Airbus A321271NX
  > DURING HEAVY MAINTENANCE: PYLONS / LH PYLON / PYLON TO WING CENTER FILLETS / INBD STRIP RIB 7A AND RIB 10A / CORROSION – PERMANENT REPAIR; REFERENCES: /1/ STS EA 160-2025-011 REV IR /2/ AIRBUS RDAF 81708156/003/2025#A /3/ REPAIR INSTRUCTIONS TD/81708156/012/20
- [SDR YENA2026012100054](https://openairdocs.org/sdr/YENA2026012100054.md): Fillet · cracked · Jan 18, 2026 · N2047J · Airbus A321271NX
  > DURING HEAVY MAINTENANCE: PYLONS / LH PYLON / PYLON TO WING CENTER FILLETS / OUTBD STRIP RIB 7A AND RIB 10A / CRACK AND CORROSION – PERMANENT REPAIR; REFERENCES: /1/ STS EA 160-2026-001 REV IR /2/ AIRBUS RDAF 81708168/003/2025#A /3/ REPAIR INSTRUCTIONS TD/8170
- [SDR AALA202602063560](https://openairdocs.org/sdr/AALA202602063560.md): Spigot · corroded · Jan 16, 2026 · N830AW · Airbus A319132
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.
- [SDR AALA202602064323](https://openairdocs.org/sdr/AALA202602064323.md): Spigot · corroded · Jan 16, 2026 · N830AW · Airbus A319132
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.
- [SDR VNAA202501090023](https://openairdocs.org/sdr/VNAA202501090023.md): Yoke · gouged · Jan 9, 2026 · N511EA · Cndair CL6002C10
  > LEFT FWD ENGINE YOKE IS GOUGED BY LOWER PYLON MOUNTING LUG.
- [SDR 2026FA0000011](https://openairdocs.org/sdr/2026FA0000011.md): Mount Bolt · loose · Jan 5, 2026 · N89RT · Amd FALCON2000EX
  > WHILE N67RT SERIAL NUMBER 381 WAS IN FOR ITS 24-MONTH INSPECTION AT DUNCAN AVIATION IN BATTLE CREEK, MAINTENANCE DISCOVERED THE LOWER FORWARD PYLON YOKE MOUNTING BOLT WAS LOOSE ON THE NR 1 & 2 ENGINES. THE LOOSE HARDWARE WAS DISCOVERED DURING THE INSPECTION O
- [SDR FDEA202512262290](https://openairdocs.org/sdr/FDEA202512262290.md): Fitting · loose · Dec 26, 2025 · N963FD · Boeing 75728A
  > NR 1 ENGINE NACELLE STRUT R/H SIDE AFTER. HINGE FITTING BOLT HEAD BROKEN OFF. REMOVED AND REPLACED BOLT AT NO 1 ENGINE NACELLE STRUT R/H SIDE AFT. HINGE FITTING IAW SRM 51-40-02-0G AND E.A # F-5440-T0385898 P1.
- [SDR CALA2025122312344](https://openairdocs.org/sdr/CALA2025122312344.md): Drag Fitting · cracked · Dec 19, 2025 · N77865 · Boeing 75733N
  > NDT ROTO INSPECTION ON NR 1 ENG PYLON DRAG FITTING. NOTED A CRACK IN HOLE NR 8 AT TOP OF SKIN AT THE 3 O'CLOCK. ACCOMPLISHED A REPAIR IAW EA 757-5720-13-A4226, AND EC/RA 57 20-03596, PART 1 STEP 1.
- [SDR DALA2025121909259](https://openairdocs.org/sdr/DALA2025121909259.md): Mount · out of alignment · Dec 18, 2025 · N318NB · Airbus A319114
  > FORWARD PYLON MOUNT ALIGNMENT FWD HOLE HAS DAMAGE. BLENDED TO REMOVE DAMAGE TO WITHIN ALLOWABLE LIMITS IAW SRM 54-51-18. (1356895).
- [SDR DALA2025121909253](https://openairdocs.org/sdr/DALA2025121909253.md): Mount · damaged · Dec 18, 2025 · N318NB · Airbus A319114
  > FORWARD PYLON MOUNT ALIGNMENT AFT HOLE HAS DAMAGE. BLENDED TO REMOVE DAMAGE TO WITHIN LIMITS IAW SRM 54-51-18. (1356909).
- [SDR DALA2025121009026](https://openairdocs.org/sdr/DALA2025121009026.md): Drag Fitting · loose · Dec 10, 2025 · N822DX · Boeing 75726D
  > DURING INSPECTION BY STEP 15 AND 16, LOOSE FASTENERS NBR: #3, #4, #5, #7, #8 #13, #14 AND 18 WERE FOUND AT RH DRAG FITTING.( FOLLOWING INSTRUCTION OF STEP #26 AND NOTE #2). LOOSE FASTENERS NBR: #3, #4, #5, #7, #8 #13, #14 AND 18 WERE REPAIRED PER PRI 583
- [SDR DALA2025121009025](https://openairdocs.org/sdr/DALA2025121009025.md): Drag Fitting · damaged · Dec 10, 2025 · N822DX · Boeing 75726D
  > DAMAGE WAS FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #3 CORROSION ON FITTING AT 4 O CLOCK POSITION, IN REF. CARD 5720-01100-02B. JOB # 101-0001 STEP 30.: HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #3 WAS
- [SDR DALA2025111908470](https://openairdocs.org/sdr/DALA2025111908470.md): Link · galled · Nov 18, 2025 · N557NW · Boeing 757251
  > NR 1 PYLON DRAG LINK FITTING HOLE 1 HAS GALLING IN HOLE. #1 PYLON DRAG LINK FITTING NO. 1 FASTENER HOLE DISCREPANCY HAS BEEN COMPLIED WITH PER ERA 584851-14AD REV F REMOVED AND INSTALLED IB DRAG FITTING AND REMOVED + INSTALLED NEW SERVICABLE OB DRAG FITTING
- [SDR HYIA20251107001](https://openairdocs.org/sdr/HYIA20251107001.md): Fitting · cracked · Nov 5, 2025 · N26156 · Cessna 402C
  > DURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE LEFT HAND INBOARD NACELLE FITTING. (P/N: 5292029-21) THIS CRACK MEASURES APPROXIMATELY.100 INCHES LONG ON THE INBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACKS F
- [SDR AALA202510088165](https://openairdocs.org/sdr/AALA202510088165.md): Attach Fitting · corroded · Oct 7, 2025 · N184US · Airbus A321211
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON FORWARD ATTACH FITTING (SHACKLE) RIGHT HAND POSITION AT RIB 4. REPLACED PYLON ATTACH FITTING PER AMM 54-51-17-400-001-A
- [SDR AALA202510064841](https://openairdocs.org/sdr/AALA202510064841.md): Attach Fitting · corroded · Oct 4, 2025 · N184US · Airbus A321211
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON FORWARD ATTACH FITTING (SHACKLE) OUTBOARD ON PYLON OUTBOARD SIDE. REPLACED PYLON ATTACH FITTING PER AMM 54-51-17-000-001-A AND AMM 54-51-17-400-001-A.
- [SDR AALA202510065770](https://openairdocs.org/sdr/AALA202510065770.md): Attach Fitting · corroded · Oct 4, 2025 · N184US · Airbus A321211
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON FORWARD ATTACH FITTING (SHACKLE) OUTBOARD ON PYLON INBOARD SIDE. REPLACED PYLON ATTACH FITTING PER AMM 54-51-17-000-001-A AND AMM 54-51-17-400-001-A.
- [SDR AALA202510068379](https://openairdocs.org/sdr/AALA202510068379.md): Attach Fitting · corroded · Oct 4, 2025 · N184US · Airbus A321211
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON FORWARD ATTACH FITTING (SHACKLE) INBOARD ON PYLON OUTBOARD SIDE. REPLACED PYLON ATTACH FITTING PER AMM 54-51-17-000-001-A AND AMM 54-51-17-400-001-A
- [SDR AALA202509262401](https://openairdocs.org/sdr/AALA202509262401.md): Attach Fitting · corroded · Sep 22, 2025 · N663AW · Airbus A320232
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT ATTACH FITTING AFT POSITION ON LT PYLON MEASURE CORROSION ARE L=0.73 INCH W=0.41 INCH D=0.011 INCH. MAINTENANCE REPLACED AFT ATTACH FITTING AFT POSITION ON LH PYLON.
- [SDR AALA202510144984](https://openairdocs.org/sdr/AALA202510144984.md): Shackle · corroded · Sep 8, 2025 · N663AW · Airbus A320232
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT ATTACH FITTING (SHACKLES) FWD POSITION ON LH PYLON. MEASURES ARE L=0.520 INCH, W=0.37 INCH AND D=0.012 INCH. MAINTENANCE REPLACED SHACKLE ATTACH FITTING ASSY IAW JC D5463008400000.
- [SDR AALA202510155351](https://openairdocs.org/sdr/AALA202510155351.md): Shackle · corroded · Sep 7, 2025 · N663AW · Airbus A320232
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SHACKLES AFT ON RH PYLON. MEASURE CORROSION ARE L=0.020 INCH W=0.020 INCH D=0.001 INCH. MAINTENANCE REPLACED SHACKLE FITTING ASSY IAW JC 26C42554028.
- [SDR AALA202510147260](https://openairdocs.org/sdr/AALA202510147260.md): Shackle · corroded · Sep 7, 2025 · N663AW · Airbus A320232
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SHACKLES AFT ON RH PYLON MEASURE CORROSION ARE L=0.020 INCH W=0.025 INCH D=0.001. MAINTENANCE REPLACED SHACKLES FITTING ASSY WITH IDENTIACAL PART IAW JOB CARD 26C42554028.
- [SDR AALA202510149455](https://openairdocs.org/sdr/AALA202510149455.md): Shackle · corroded · Sep 7, 2025 · N663AW · Airbus A320232
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SHACKLES FWD INB SIDE ON RH PYLON (CPCP 545116-01) MEASURE CORROSION ARE L=0.024 INCH W=0.020 INCH D=0.001 INCH. MAINTENANCE REPLACED SHACKLE FITTING ASSY WITH IDENTICAL PART.
- [SDR SWAA2025091507045](https://openairdocs.org/sdr/SWAA2025091507045.md): Fitting · cracked · Aug 21, 2025 · N964WN · Boeing 7377H4
  > NUMBER 1 PYLON FITTING LOCATED 13 INCH AFT OF AFT ENG MOUNT FITTING IS GOUGED AND CRACKED. REMOVED PYLON FITTING AND PANELS 431CL;431CR; 433AL; 433AR; 431ER;431EL; 433DT 511BT IAW SRM 51-40-02-0G-0, INSTALLED A NEW PYLON FITTING AND PANELS 431CL;431CR; 433A
- [SDR AALA202508126563](https://openairdocs.org/sdr/AALA202508126563.md): Sleeve · damaged · Aug 9, 2025 · N768US · Airbus A319112
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON LEFT HAND SIDE FORWARD UPPER ATTACH FITTING SLEEVE (PIN) HAS DAMAGED THREADS. REPLACED SLEEVE (PIN) PER TASK CARD 26C42554028.
- [SDR AALA202508226150](https://openairdocs.org/sdr/AALA202508226150.md): Fitting · worn · Aug 4, 2025 · N186US · Airbus A321211
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON OUTBOARD AFT ATTACHMENT FITTING FOR THE THRUST REVERSER, BEARING HAS MIGRATED. REPLACED FITTING PER AMM 54-57-17.
- [SDR AALA202508091691](https://openairdocs.org/sdr/AALA202508091691.md): Fitting · corroded · Jul 10, 2025 · N826AW · Airbus A319132
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON MEASURE OF CORROSION ARE: L=13.600 INCH, W:1.345 INCH, D:0.009 INCH. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON IAW A319 SRM 54-51-12-300-002.
- [SDR IPXA2025080138044](https://openairdocs.org/sdr/IPXA2025080138044.md): Attach Angle · cracked · Jul 9, 2025 · N138UP · Airbus A300F4622R
  > NR 1 PYLON-INSIDE 475AL 4TH STIFFENER FROM AFT END ON I/B SIDE HAS UPPER ATTACH ANGLE BROKEN-109-VWV-91195430 VERIFIED INSTALLATION OF NEW ANGLE.

Next page: https://openairdocs.org/jasc/5415/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 = '5415'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5415/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.