# Service difficulty reports: JASC 1430

A list on [JASC 1430](https://openairdocs.org/jasc/1430.md).

Reports filed under 1430 · Fasteners, newest first.

Page 1 of 15 · 705 reports

- [SDR 2VKA2024072453552](https://openairdocs.org/sdr/2VKA2024072453552.md): Washer · cracked · Jan 24, 2024 · N314SF · Bell 407
  > WHILE CHANGING TRANSMISSION ASSEMBLY, TECHNICIAN NOTICED THREE PYLON RETAINING BOLT WASHERS PN:140-007-25S22E6 CRACKED ALL THE WAY THROUGH ON ONE SIDE.
- [SDR TSAA20230606107](https://openairdocs.org/sdr/TSAA20230606107.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330
  > CA 1464/361 WHILE PERFORM CUSTOMER PROVIDE TASK CARD ECO 3531-R10 WHICH INDICATED IN SB 737-53A1240, FOUND FASTENER HAD BEEN UPSIDE. PERFORM TASK CARD ECO 3531-R10 INSP FOUND FASTENER WRONG. PERFORM PER AIRASIA EL-737-230508.
- [SDR 8HBR20230415051](https://openairdocs.org/sdr/8HBR20230415051.md): Bolt · mismanufactured · Apr 15, 2023 · N4324D · Piper PA34220T
  > BOLT, PIPER P/N 402-921 QUANTITY OF 8 WERE ORDERED FROM BOEING, 4 OF THE 8 DID NOT HAVE THE HOLE DRILLED THROUGH THE THREADS FOR THE COTTER PIN. PIPER TAGS ON BOLTS DATED: 01/07/2022. LINE LOT/BATCH:7365740436 ON THE INVOICE FROM BOEING.
- [SDR 2022FA0000485](https://openairdocs.org/sdr/2022FA0000485.md): Bolt · used · Aug 1, 2022 · N8111P · Piper PA34200T
  > LEFT LANDING GEAR SCISSOR LINK CENTER BOLT FAILED DURING TAXI
- [SDR 2022FA0000272](https://openairdocs.org/sdr/2022FA0000272.md): Cowl Fastener · broken · May 22, 2022 · N3JA · Cessna 172M
  > I DO NOT KNOW IF I OR THE MANUFACTURER NEED TO REPORT THIS. I BOUGHT A FEW COWLING FASTENERS AND THEY ALL FAILED WITHIN 30 HOURS OF INSTALLATION. FEB 2022 I BOUGHT 4 SKYBOLT SK2003-42A COWLING MOUNT FASTENERS FROM THE MANUFACTURER. 3 WERE INSTALLED ON THE
- [SDR 2022FA0000011](https://openairdocs.org/sdr/2022FA0000011.md): Bracket · cracked · Jan 11, 2022 · N750VP · Cessna 750
  > A RECENT SDR REPORT FOR A BROKEN BRACKET AND SUBSEQUENT LEAK IN A HYDRAULIC LINE ON AIRCRAFT N733FL (12508 HRS), S/N 750-0027 RESULTING IN AN EMERGENCY LANDING PROMPTED A BAKER AVIATION FLEET-WIDE INSPECTION OF THE BROKEN BRACKET. WHEN N750VP (8603 HRS) ARRIVE
- [SDR R61A2021111700902](https://openairdocs.org/sdr/R61A2021111700902.md): Skin · out of limits · Nov 7, 2021 · N219YX · Emb ERJ170200LR
  > FOUND STUCK FASTENER IN FITTING ON AILERON TORQUE TUBE SUPPORT, PERFORMED TEMPORARY REPAIR BY REAMING HOLE AND FABRICATED AND INSTALLED BUSHING ON RH LOWER WING SKIN HOLE IN ACCORDANCE WITH REF ETD2021-170-037446.
- [SDR 2007FA0000392](https://openairdocs.org/sdr/2007FA0000392.md): Tab · cracked · Mar 1, 2007
  > WHEN TECH WENT TO BEND THE TAB ATTACHED TO THE WASHER AT THE RADIUS OF THE BEND, THEY WOULD CRACK. (K)
- [SDR 2006FA0000421](https://openairdocs.org/sdr/2006FA0000421.md): Screw · wrong part · Apr 10, 2006 · N907JE · Beech 400A
  > DURING INSPECTION IAW MFG SB, FOUND BRAKE HYDRAULIC LINE DAMAGED BY FLOOR PANEL ATTACHING SCREW. REPAIRED TUBING AND MODIFIED FLOOR PANELS IAW SB. HAVE FOUND THIS SAME CONDITION ON OTHER AIRCRAFT. (K)
- [SDR ASAA0610173](https://openairdocs.org/sdr/ASAA0610173.md): Rivet · corroded · Feb 20, 2006 · N742AS · Boeing 737290C
  > CORROSION ON RIVETS. REPAIRED PER SRM 53 10 3 FIG 1.
- [SDR CA051208003](https://openairdocs.org/sdr/CA051208003.md): Bolt · wrong part · Nov 12, 2005 · Dhav DHC2MKI
  > WRONG BOLTS INSTALLED AT LOWER FUSELAGE STRUT TO BIRDCAGE STRUCTURE. AN6-A INSTALLED, SHOULD BE AN176-13A CLOSE TOLERANCE BOLTS, AS PER DEHAVILLAND DRAWING C2FS5123A.
- [SDR 05FDEA02608](https://openairdocs.org/sdr/05FDEA02608.md): Fastener · wrong part · Aug 24, 2005 · N556FE · Doug DC1010
  > AIR COND COMPT LT SIDE FOUND EXISTING REPAIR WITH WRONG FASTENERS (CHERRY AND BOLT) ON NLG BLKHD. REMOVED EXISTING REPAIR, TRIMMED OUT DAMAGED AREA AND REPAIRED IAW SRM.
- [SDR CA050818004](https://openairdocs.org/sdr/CA050818004.md): Bolt · broken · Aug 18, 2005 · Cessna U206G
  > (CAN) PILOT REPORT: NO BRAKE ON RT SIDE OF AIRCRAFT. BRAKE PEDDLE WAS SOLID, NO TRAVEL. INSPECTION REVEALED THAT THE OB MLG CLAMP AFT BOLT HAD SNAPPED ALLOWING THE GEAR TO COME LOOSE. THE MAIN LANDING GEAR HAD PINCH OFF THE SOLID ALUMINUM BRAKE LINE.
- [SDR CA050906003](https://openairdocs.org/sdr/CA050906003.md): Bolt · failed · Aug 4, 2005
  > (CAN) ENG TAY 16916 AFTER TEST, HAD ABNORMAL NOISE DURING ROTATION OF LP SYS. ENG WAS REJECTED AT DISPATCH AND MODULE 5 (LP TURBINE ASSY) WAS DISMANTLED FOR INVESTIGATION. DURING DISASSEMBLY IT WAS FOUND THAT 1 OFF BOLT AS21910 HAD FAILED IN 3 PIECES CAUSING
- [SDR SWAA052308](https://openairdocs.org/sdr/SWAA052308.md): Bolt · worn · Aug 2, 2005 · N396SW · Boeing 7373H4
  > DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB CONTROL PUSHROD BOLT AND HARDWARE PER MM.
- [SDR 2005FA0001089](https://openairdocs.org/sdr/2005FA0001089.md): Nut · cracked · Aug 2, 2005 · N36049 · Piper PA34200T
  > REPAIR STATION WAS REPAIRING AIRCRAFT HYD LEAK. WHEN REMOVING LOWER FORWARD WING ATTACH BOLT COVERS FOUND 10 OF THE 16 MS21042-6 NUTS CRACKED. PIPER P/N 404-532.
- [SDR DL76S050419](https://openairdocs.org/sdr/DL76S050419.md): Bolt · loose · Jul 30, 2005 · N130DL · Boeing 767332
  > RT ENG FIRE IND INTERMIT DURING CLM. S/D ENG AND ATB TO ATL.C/A FOUND 4 BOLTS LOOSE ON HPT NOZZLE COOLING DUCTS AT HPC CASE 230 AND 330 POSITION. TIGHTENED SAME. REINSTALLED RMVD LOOPS. CKD SECURITY OF ALL LOOPS. RAN ENG AT 90 PCT FOR 5 MIN AND 103 PCT FRO 5 M
- [SDR 05FDEA02138](https://openairdocs.org/sdr/05FDEA02138.md): Fastener · missing · Jul 29, 2005 · N651FE · Airbus A300F4605R
  > PASSING 5500FT MSL AND LEVELING AT 6000 FT, HAND FLYING USING AUTO THROTTLES, ATTEMPTED TO TRIM AIRCRAFT MANUALLY WITH TRIM BUTTON ON YOKE. DURING TRIM A VIBRATION WAS FELT ON THE A/C. NEEDED MORE TRIM TO LEVEL, AGAIN VIBRATION OCCURRED DURING TRIMMING, 250
- [SDR CA050708003](https://openairdocs.org/sdr/CA050708003.md): Collar · failed · Jul 8, 2005 · Dhav DHC8301
  > DURING HEAVY MAINTENANCE IT WAS DISCOVERED ON THE LHS WING FWD SPAR AT WS 490.0 SPLICE JOINT. 4 CRACKED LOCKBOLT COLLARS PN BACC30BK5 WERE FOUND. REQUEST HAS BEEN SENT TO BOMBARDIER TO REPLACE LOCKBOLTS AND COLLARS WITH HILOCK SUBSTITUTES. DETAILED VISUAL IN
- [SDR MWEA050047](https://openairdocs.org/sdr/MWEA050047.md): Rivet · lightning strike · Jun 7, 2005 · N903ME · Boeing 717200
  > ONE EACH RIVET AT STATION 64-83 ABOVE LONGERON 18 LEFT HAS EVIDENCE OF A LIGHTNING STRIKE. HEAT DAMAGE HAS BEEN REMOVED AND INSTALLED RIVETS.
- [SDR 2005FA0000835](https://openairdocs.org/sdr/2005FA0000835.md): Bolt · chafed · Jun 2, 2005 · N128JL · Raythn 390
  > UPON REMOVAL OF FLAP ACTUTORS FOUND NR 3 LT AND RT FLAP ACTUATORS WERE DEEPLY GOUGED, DUE TO FLAP TRACK BOLTS INSTALLED BACKWARDS. PN OF BOLT NAS6205-18D. REMOVED BOLT AND INSPECTED AND REINSTALLED IN THE CORRECT DIRECTION. (K)
- [SDR ASOA05455](https://openairdocs.org/sdr/ASOA05455.md): Fastener · missing · May 22, 2005 · N643AS · Aerosp ATR72
  > DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND DIFFICULT TO OPEN. MAINTENANCE REINSTALLED 2 FASTENERS (SCREWS) FOUND MISSING FROM THE PASSENGER DOOR COVER IN THE UPPER AFT CORNER. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)
- [SDR QXEA200500994](https://openairdocs.org/sdr/QXEA200500994.md): Fastener · loose · May 17, 2005 · N616QX · Cndair CL6002C10
  > RT WING UPPER SKIN TRAILING EDGE HAS LOOSE FASTENERS AT INBOARD OF MULTI-FUNCTION SPOILERS. REPAIRED IAW CRJ 700 SRM 51-42-07-001-001-A01 AND 51-25-01-001-001-A01.
- [SDR QXEA200501003](https://openairdocs.org/sdr/QXEA200501003.md): Fastener · loose · May 17, 2005 · N616QX · Cndair CL6002C10
  > LT WING OUTBOARD FLIGHT SPOILERS HAVE LOOSE FASTENERS, OUTBOARD AND INBOARD SIDES. REPAIRED IAW CRJ 700 SRM 51-42-07-001-001-A01 AND SRM 51-25-01-00-001-A01.
- [SDR ASOA05417](https://openairdocs.org/sdr/ASOA05417.md): Fastener · corroded · May 6, 2005 · N849AS · Cndair CL6002B19
  > DURING A C-CHECK IN MCN, THE FASTENERS UNDER THE CABIN FLOORBOARD AT FS 333 APPROXMATELY RBL 7-9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FASTENERS UNDER THE CABIN FLOORBOARD AT FS 333, APPROXIMATELY RBL 7-9 IAW CRJ S
- [SDR 2005FA0000789](https://openairdocs.org/sdr/2005FA0000789.md): Rivet · missing · May 5, 2005 · N200ZT · Beech B200
  > DURING VISUAL INSPECTION OF AFT FUSELAGE STRINGERS AT AFT PRESSURE BULKHEAD FOR COMPLIANCE WITH AD, NOTED (1) RIVET MISSING FROM NR7L STINGER CLIP AT ZEE SECTION ATTACHMENT. RIVET MISSING WAS AT FARTHEST FORWARD POSITION, REQUIRED REMOVING INSULATION AND SEAL
- [SDR AWXA200500617](https://openairdocs.org/sdr/AWXA200500617.md): Bolt · corroded · May 4, 2005 · N322AW · Boeing 7373G7
  > MCN - FLIGHT CONTROL - DURING C-14 CHECK, CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER, FWD UPPER SPAR TO CENTER ATTACH BOLT. NO CORROSION REMOVAL LIMITS WERE AVAILABLE FOR THE BOLT. MAINTENANCE REMOVED AND REPLACED THE RT HORIZONTAL STABILIZER, FWD UPPER
- [SDR QXEA200500931](https://openairdocs.org/sdr/QXEA200500931.md): Rivet · loose · Apr 29, 2005 · N611QX · Cndair CL6002C10
  > YYC - RIGHT WING INBOARD MFS AREA, TWO LOOSE RIVETS INBOARD NEAR PIE SHAPE AREA. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-25-16-001-001-A01.
- [SDR QXEA200500899](https://openairdocs.org/sdr/QXEA200500899.md): Rivet · loose · Apr 29, 2005 · N611QX · Cndair CL6002C10
  > YYC - FUSELAGE EXTERIOR HAS SMOKING RIVET AT STATION 830 AND STRINGER 7R. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.
- [SDR QXEA200500898](https://openairdocs.org/sdr/QXEA200500898.md): Rivet · loose · Apr 29, 2005 · N611QX · Cndair CL6002C10
  > YYC - FUSELAGE EXTERIOR HAS SMOKING RIVETS AT STATION 693 AND STRINGER 7R. REPAIRED IAW CRJ-700 SRM 51-42-06-001-001-A01.
- [SDR QXEA200500900](https://openairdocs.org/sdr/QXEA200500900.md): Rivet · loose · Apr 28, 2005 · N611QX · Cndair CL6002C10
  > YYC - FUSELAGE EXTERIOR HAS SMOKING RIVET AT STATION 850 AND STRINGER 10L. REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01.
- [SDR IXXA05SMN01S](https://openairdocs.org/sdr/IXXA05SMN01S.md): Screw · corroded · Apr 27, 2005 · N828BX · Doug DC871F
  > DURING ROUTINE C CHECK INSPECTION, RT WING, L/E INBD STUB WING UPPER SURFACE SCREWS OXIDIZED, XW 257.000. REMOVED OXIDIZED SCREWS IAW DC-8 SRM 51-3-0 PAGE 1. INSTALLED NEW SCREWS ON RT L/E INBD STUD WING UPPER SURFACE, XW 257.000 IAW DC-8 SRM 51-3-0 PAGE 1.
- [SDR DAT2005F00004](https://openairdocs.org/sdr/DAT2005F00004.md): Attach Bolt · loose · Apr 27, 2005 · N938MA · Stbros SD330
  > DURING SCHEDULED MAINTENANCE OF COMPLYING WITH AD (PROP TORQUE) ON THE RT PROPELLER IN ACC`S HANGAR, (3) PROP ATTACH BOLTS WERE FOUND LOOSE, BUT NOT BROKEN. AD STATES WHEN LOOSE BOLTS ARE FOUND THE PROPELLER IS TO BE REMOVED AND INSPECTED, THE FLANGE MATING S
- [SDR 2005FA0000653](https://openairdocs.org/sdr/2005FA0000653.md): Screw · wrong part · Apr 22, 2005 · N768WT · Beech B300
  > DURING SCHEDULED INSPECTION FOUND SCREWS ATTACHING AFT LOWER EDGES OF FORWARD WING ROOT FAIRINGS TO UNDERSIDE WING ROOT FAIRINGS TO BE OF EXCESSIVE LENGTH. SCREW TIPS HAD GOUGED LT AND RT LOWER FUSELAGE SKINS AT THE APPROXIMATE FS 166.300 LOCATION TO 0.020 IN
- [SDR 05FDEA01040](https://openairdocs.org/sdr/05FDEA01040.md): Fastener · wrong part · Apr 18, 2005 · N583FE · Doug MD11
  > RT WING, DURING ACCOMPLISHMENT OF EO 1-5750-7-5004 PART 2, SEVEN (7) EACH COUNTERSUNK LOCK FASTENERS COMMON TO TENSION STRAP SUPPORT AND LOWER REAR SPAR CAP, FOUND DIFFERENT WITH HEAD SIZE FROM THE SPECIFIED LOCK FASTENERS. LOCATION IS BY XORS 570.00. INSTA
- [SDR 05FDEA01039](https://openairdocs.org/sdr/05FDEA01039.md): Fastener · wrong part · Apr 18, 2005 · N583FE · Doug MD11
  > LT WING, DURING ACCOMPLISHMENT OF EO 1-5750-7-5004 PART 1, SEVEN (7) EACH COUNTERSUNK LOCK FASTENERS COMMON TO TENSION STRAP SUPPORT AND LOWER REAR SPAR CAP, FOUND DIFFERENT WITH HEAD SIZE FROM THE SPECIFIED LOCK FASTENER. LOCATION IS BY XORS= 570.00. INSTAL
- [SDR QXEA200500687](https://openairdocs.org/sdr/QXEA200500687.md): Rivet · loose · Apr 13, 2005 · N346PH · Dhav DHC8202
  > PDX - FOUR RIVETS SMOKING/PULLING THROUGH SKIN UNDER WING FAIRING, APPROXIMATELY X424, LEFT SIDE WHERE LOWER END OF FAIRING MEETS FUSELAGE. REPAIRED IAW DHC-8 200 SRM 51-40-00, PAGE 1-6.
- [SDR QXEA200500747](https://openairdocs.org/sdr/QXEA200500747.md): Rivet · loose · Apr 12, 2005 · N614QX · Cndair CL6002C10
  > YYC - LOWER FUSELAGE STATION 1098 TO 1108 STRINGER 18 TO 19 RT SKIN HAS FOUR LOOSE RIVETS SMOKING. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01, SRM 51-23-00-001-00-A01 AND SRM 51-42-06-001-001-401.
- [SDR QXEA200500812](https://openairdocs.org/sdr/QXEA200500812.md): Rivet · loose · Apr 11, 2005 · N614QX · Cndair CL6002C10
  > YYC - VERTICAL STABILIZER, RIGHT SIDE, BOTTOM AFT SKIN HAS NINE SMOKING RIVETS. REPLACED IAW CRJ7000 SRM 51-42-13-001-001-A01.
- [SDR SIMA200510103](https://openairdocs.org/sdr/SIMA200510103.md): Rivet · damaged · Apr 1, 2005 · N689EC · Emb EMB145LR
  > SAW - LIGHTNING STRIKE DAMAGE ON SEVERAL RIVETS ON LEFT WING FUEL CELL. MAINTENANCE REPLACED RIVETS IAW SRM 51-40-02 AND 51-20-04. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR QXEA200500638](https://openairdocs.org/sdr/QXEA200500638.md): Fastener · loose · Mar 29, 2005 · N612QX · Cndair CL6002C10
  > YYC - HORIZONTAL STABILIZER CENTERING TRACK ALL ATTACHED FASTENERS LOOSE. REPAIRED IAW HORIZON AIR EA R-55-32A AND REO 670-55-31-004.
- [SDR 2005FA0000493](https://openairdocs.org/sdr/2005FA0000493.md): Screw · fractured · Mar 29, 2005 · N9563Z · Boeing B17G
  > (7) OF THE (10) FRONT COVER RETAINING SCREWS WERE FRACTURED, ALL AT THE SAME LOCATION- (3) THREADS FROM SHANK. ALL (7) HAD WORKED THEIR WAY OUT, (3) HAD STARTED TO CONTACT THE PROPELLER HUB. NR 4 ENGINE AWAITING TEARDOWN REPORT OF NOSE SECTION. (GL132005062
- [SDR QXEA200500628](https://openairdocs.org/sdr/QXEA200500628.md): Fastener · corroded · Mar 24, 2005 · N612QX · Cndair CL6002C10
  > YYC - RIGHTHAND WING LOWER SURFACE INBOARD MAIN LANDING GEAR DOUBLER PLATE ATTACHMENT FASTENERS ARE RUSTY. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01 AND SRM 51-25-00-001-001-A01.
- [SDR QXEA200500615](https://openairdocs.org/sdr/QXEA200500615.md): Rivet · smoke · Mar 23, 2005 · N612QX · Cndair CL6002C10
  > YYC - FUSELAGE EXTERIOR HAS FOUR SMOKING RIVETS AT STATION 745 AND STRINGER 16R. REPLACED RIVETS IAW CRJ7800 SRM 51-42-06-001-001-A01.
- [SDR QXEA200500623](https://openairdocs.org/sdr/QXEA200500623.md): Screw · loose · Mar 22, 2005 · N612QX · Cndair CL6002C10
  > YYC - RIGHTHAND WINGLET INBOARD AND OUTBOARD SURFACES HAVE MANY LOOSE SCREWS. RETORQUED IAW CRJ700 MM 57-30-84, PAGE 422/425.
- [SDR QXEA200500621](https://openairdocs.org/sdr/QXEA200500621.md): Rivet · loose · Mar 20, 2005 · N612QX · Cndair CL6002C10
  > YYC - FUSELAGE UPPER EXTERIOR HAS SEVERAL SMOKING RIVETS AT STRINGER 3L AND BETWEEN FUSELAGE STATION 345 TO 379. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-25-01-001-001-A01.
- [SDR QXEA200500620](https://openairdocs.org/sdr/QXEA200500620.md): Rivet · loose · Mar 20, 2005 · N612QX · Cndair CL6002C10
  > YYC - FUSELAGE UPPER EXTERIOR HAS SEVERAL SMOKING RIVETS AT STRINGER 7L, BETWEEN FUSELAGE STATION 893 TO 939. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-25-01-001-001-A01.
- [SDR QXEA200500622](https://openairdocs.org/sdr/QXEA200500622.md): Rivet · smoke · Mar 20, 2005 · N612QX · Cndair CL6002C10
  > YYC - FUSELAGE EXTERIOR HAS SEVERAL SMOKING RIVETS AT FUSELAGE STATION 677, STRINGER 3L TO STRINGER 6L. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-25-01-001-001-A01.
- [SDR QXEA200500543](https://openairdocs.org/sdr/QXEA200500543.md): Rivet · smoke · Mar 20, 2005 · N612QX · Cndair CL6002C10
  > YYC - FUSELAGE EXTERIOR HAS SMOKING RIVET AT FUSELAGE STATION 485. REPAIRED IAW CRJ700 SRM 51-25-001-001-A01.
- [SDR QXEA200500560](https://openairdocs.org/sdr/QXEA200500560.md): Rivet · pulled · Mar 19, 2005 · N612QX · Cndair CL6002C10
  > YYC - CENTER FUSELAGE AT STATION 770.0, WL 725, RBL 9.0-17.0 HAS RIVETS PULLED ON FLAT STRAP. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Next page: https://openairdocs.org/jasc/1430/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 = '1430'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/1430/reports

---
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