JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, newest first.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA011101006Web · cracked(CAN) FOUND CRACK ON ENGINE SUPPORT BEAM WHILE PERFORMING SB A601R-53-059. FOUND CRACKS AT THREE LOCATIONS ON LOWR WEB AT LBL 36, RBL 36 AND BL 0.SDR QXEA0101623Structure · crackedPDX-DECK CRACKED UNDER RIGHT HAND FINGERNAIL AFT ATTACH POINT. FABRICATED AND INSTALLED DECK IAW HORIZON AIR EA 6-54-23.SDR QXEA0101622Bracket · crackedPDX-RIGHT HAND FINGERNAIL DECK SUPPORT BRACKET AT AFT EXHAUST SHROUD ATTACHMENT POINT IS CRACKED. FABRICATED AND INSTALLED DECK SUPPORT BRACKET IAW HORIZON AIR EA 6-54-21.SDR QXEA0101645Structure · chafedPDX - RIGHT NACELLE AFT WHEEL WELL CHAFED AT ROCK GUARD BOTTOM TWO ATTACH POINTS. REPAIRED IAW SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-51.SDR CA011019017Web · cracked(CAN) DURING C-CHECK COMPLIED WITH SB A601R-53-059. FOUND CRACKS ON UPPER WEB AT LBL 8 (1.2IN ), RBL 8 (3.5IN) AND LOWER WEB AT LBL 8 (0.5").AREAS TO BE REPAIRED IAW REOS 601R-53-61-345 AND -366.SDR QXEA0101575Strut · corrodedPDX - NR 1 ENGINE INBOARD AFT NACELLE STRUT JUST ABOVE INBOARD IGNITOR DOOR HAS CORROSION FROM ENGINE EXHAUST. REPAIRED IAW DHC-8 SRM 51-20-36 AND HORIZON AIR EA 2-54-102.SDR CALA0100877Support · crackedINSPECTION FOUND A 1.52 INCH CRACK IN NR 1 PYLON UPPER SUPPORT ANGLE AT CANTED FRAME 1463, L17L. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5410-01555.SDR CA010912015Web · cracked(CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM UPPER WEB AT FS 640 NEAR L & R BL 9.0 (1.25 AND 1.5 INCHES LONG). ONE CRACK FOUND ON LHS OF ACCESS PANEL LANDING CORNER ON LOWER WEB NEAR LBL 36.2 (0.5 INCHES LONG). REPAIRED IN ACCORDANCE WITH REO'S 601R-53-61-366SDR ZW0A0108612Bar · wornDURING CHECK-C MAINT ON THE NUMBER 1 INBD PYLON, THE EQUALIZER BAR HOLE IN THE PYLON FWD OF AFT REVERSER MOUNT, THE FWD EDGE OF THE HOLE WAS WORN. CLEANED AND SMOOTHED OUT AREA PER SRM 54-5-01.SDR AWXA200100540Stiffener · crackedPHX - C8 CK - C - CRACK FOUND IN NR 1 PYLON, O/B SIDE VERTICAL STIFFENER, 1 INCH LONG AT PPS 153, PPWL 143. MAINTENANCE REMOVED AND REPLACED THE STIFFENER IAW B757 SRM 51-10-02, PG 2.SDR CA010912010Web · cracked(CAN) DURING COMPLETION OF ASB 601R-53-61-059 FOUND UPPER WEB OF ENGINE SUPPORT BEAM CRACKED NEAR L & RBL 9.0 AT FS 640. ALSO FOUND HOLES IN SUPPORT ANGLE CRACKED AT RBL 7.5 AND 8.5 (FOUND BY NDT). ALSO FOUND 1/2 INCH CRACK IN LOWER WEB NEAR RBL 36.20 IN THE FSDR UPS01436765Tee Chord · crackedINSPECTION TYPE:W/E NR 4 PYLON TEE CHORD CRACKED BELOW L/E. FABBED CHORD, INSTALLED TEE CHORD IAW 51-40-04 SRM .SDR PCAA0108107Rivet · missingDURING FLEET INSPECTION OF NACELLES FOR LOOSE AND MISSING RIVETS, FOUND 2 MISSING AND 5 LOOSE RIVETS ON RIGHT OUTBOARD NACELLE FORWARD OF FINGERNAIL (PANEL 15). RIVETS REPLACED IN ACCORDANCE WITH CALLAHAN REPAIR SERVICES DER REPAIR REFERENCE NUMBER CAS-AAL-09SDR PCAA0108104Rivet · missingDURING FLEET INSPECTION FOR NACELLE RIVETS BEING LOOSE AND MISSING, ONE RIVET WAS FOUND MISSING ON INSPECTION PANEL ON REAR OF RIGHT NACELLE. LOOSE AND MISSING RIVETS ON INSPECTION PANEL REPLACED IN ACCORDANCE WITH DER CALLAHAN REPAIR SERVICES 8110 FORM CASAASDR PCAA0108102Rivet · looseDURING FLEET INSPECTION FOR NACELLE RIVETS BEING LOOSE AND MISSING, FOUR LOOSE RIVETS WERE FOUND ON OUTBOARD RIGHT COWLING BELOW FLAP TRACK. FOUR RIVETS WERE REPLACED ON COWLING. AIRCRAFT RETURNED TO SERVICE.SDR PCAA0108100Rivet · looseDURING FLEET INSPECTION FOR NACELLE RIVETS BEING LOOSE AND MISSING, ONE RIVET FOUND MISSING AND ONE FOUND PULLING THROUGH ON LEFT NACELLE OUTBOARD END PLATE JUST BELOW FLAP TRACK. THREE RIVETS REPLACED ON OUTBOARD LEFT NACELLE JUST BELOW FLAP TRACK IN ACCORDASDR HNAA0100052Angle · crackedNR 2 NACELLE HORSE COLLAR WAS FOUND CRACKED IN RADIUS OF FWD UPPER CLOSING ANGLE JUST ABOVE ENGINE HOIST ATTACH BRACKET. REPAIRED PER EO8-54-01-799.SDR PCAA0108097Rivet · missingBGM- DURING FLEET INSPECTION OF NACELLES FOR LOOSE AND MISSING FASTENERS FOUND 4 RIVETS MISSING FROM OUTBOARD RIGHT NACELLE AFT OF FLAP TRACK TRAILING EDGE. MAINTENANCE REPLACED RIVETS ON RIGHT OUTBOARD NACELLE AFT OF FLAP TRACK TRAILING EDGE. AIRCRAFT RETURSDR DHL2001727517Angle · corrodedNR 2 ENG LEFT TOP PANEL OF PYLON ANGLE SUPPORT IS CORRODED AND CRACK AT STA 1380. REMOVED CORRODED ANGLE AT TOP OF PYLON NR 2 ENG LEFT SIDE BS 1381.5 TO 1455 PER SRM 51-30-2. FABRICATED NEW ANGLE PER SRM 54-10-2 FIG 3. INSTALLED ANGLE PER SRM 51-30-2.SDR DHL2001727528Bracket · crackedCRACKED BRACKET AT NR 3 ENGINE PYLON AFT OF PRECOOLER SHROUD. REMOVED AND REPLACED BRACKET PER SRM 54-10-3.SDR QXEA0101351Structure · crackedPDX - RIGHT NACELLE FINGNAIL ATTACHMENT TAP CRACKED AT NUPLATE RIVET, INBOARD OF STATION XN236.20. REPAIRED IAW DHC-8 RD 8-54-163.SDR DL76G011327Fitting · crackedTHE INBOARD FITTING ON THE NR 1 PYLON WAS FOUND WITH CRACKS IN THE TYPICAL LOCATION AS SHOWN IN S/B 767-54-0081.SDR QXEA0101333Structure · crackedPDX - LEFT-HAND NACELLE DECK IS CRACKED AT STATION XN249.00. REPAIRED IAW DHC-8 SRM 51-40-11.SDR SWIA200110190Clip · crackedRIB NR 19 RIGHT WING INNER SKIN CLIPS CRACKED AT 3 PLACES ONE LOWER, THREE UPPER.REMOVED, FABRICATED AND INSTALLED SKIN CLIPS IAW SRM 51-40-02 AND 51-70-06.SDR QXEA0101317Stiffener · crackedPDX - NR 1 NACELLE PANEL 413AL , OIL SERVICE DOOR, CENTER STIFFENER CRACKED. REPAIRED IAW DHC-8 RD 8-71-213.SDR 0104549922Spar · corrodedDuring an Mck in ATL, Corrosion was found in the left and right upper beaver tails. The Beaver tails were removed to accomplish corrosion removal. After the beaver tail removal it was noted that 11 fasteners common to the pylon spar were elongated. Repaired peSDR QXEA0101204Structure · corrodedPDX-RIGHT SIDE MAIN LANDING GEAR "H" MEMBER ACTUATOR ATTACH POINT HAS SURFACE CORROSION. REPAIRED IAW HORIZON AIR EA 2-54-88.SDR USAA010841Fitting · gougedCLT - FOUND BULKHEAD FITTING .75 INCH GOUGE, NACELLE STATION 254.525, NR 2 PYLON. BLENDOUT AND ROTO-PEEN. (M)SDR 0105009922Rib · crackedDuring Mck in ATL, the aft portion of the lower cap of the pylon closing rib was found cracked. The crack is .6" long and extends from a fasterner hole 3.7" forward from the aft end of the cap. Repaired per EA 99-181307.SDR 0104419958Rib · crackedDuring Mck in ATL, The aft portion of the lower cap of the pylon closing rib was found cracked. The crack is approximately .7" long and extends from a hole 3.7" from the end of the cap. Material TI-6AI-4V. Repaired per EA. 99-181307.SDR DL72S011098Fitting · crackedDURING INSPECTIONS PER AD 97-05-08, CRACKS WERE FOUND IN THE#1 FORWARD ENGINE MOUNT AT HOLES C AND D. THE HOLES WERE OVERSIZED, INSPECTED AND NEW FASTENERS INSTALLED PER ERA 397735-14AD AT HMV.SDR MALA010548Structure · chafedFOUND DURING 4K-CHECK IN CWA, RT NACELLE LOWER I/B CHAFED AT STA 227. REPAIRED IAW SAAB STATEMENT 340 SDS002027, EO S54055. MAINTENANCE REPAIRED CHAFED AREA IAW SAAB STATEMENT.SDR QXEA0101117Strut · chafedPDX - NR 1 ENGINE NACELLE LOWER OUTBOARD FORWARD STRUT CHAFED .002 DEEP, 1 1/2 TO 3 INCHES AFT OF FORWARD FIREWALL. REPAIRED IAW HORIZON AIR EA 2-54-77.SDR MWEA010941Angle · crackedSTATION 980 ANGLE ON THE TOP OF RIGHT PYLON IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE AND REPAIR STRAPS, INSTALLED REPAIR PARTS.SDR MWEA010935Web · crackedRIGHT PYLON WEB IS CRACKED APPROXIMATELY 6 INCHES BELOW FIRE EXTINGUISHER DISCHARGE TUBE. FABRICATED AND INSTALLED REPAIR DOUBLERS.SDR MWEA010914Angle · crackedLT PYLON INTERCOSTAL AFT OF APRON HAS A CRACKED ATTACH BRACKET AT TOP END. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE.SDR MWEA010913Clip · crackedRT PYLON AFT SPAR, TOP SUPPORT CLIP HAS A CRACK, LOCATED INBOARD OF AFT ISOLATOR. REMOVED CLIP, FABRICATED AND INSTALLED SUPPORT CLIP.SDR ABXA010319Angle · crackedNR 4 PYLON INTERIOR INBOARD VERTICAL ANGLE STATION YN 298 UNDER UPPER SPAR WEB CRACKED.SDR ASAA0140085Structure · damagedSEA - DURING C-CHECK, FOUND RIGHT ENGINE STRUT PYLON NR 2 CROWN BEAM AFT BEARING BORE HAS PITTING ON INNER SURFACE. REPAIRED IAW ENGINEERING AUTHORIZATION. (M)SDR MALA010622StiffenerFound during C-Check, #1 Engine nose Cowl Fwd Bulkhead has one stiffenrer cracked (32). Maintenance replaced #32 Stiffener PN HC716H9025-000, #1 Engine Nose Cowl IAW BAe SRM 54-10-11.SDR AALA20011150BracketTUL - FOUND THROTTLE CONTROL DRUM MOUNT BRACKET CRACKED UPPER END, NR 3 ENGINE. REPAIRED CRACK IN CONTROL DRUM MOUNT BRACKET PER ESO 11697 DATED 5-21-01 AND SRM 54-10-3 PAGE 42A. (M)SDR DHL2001364001Angle · crackedON A-5 CHECK- NR 2 ENGINE PYLON HEAT EXCHANGER ACCESS, I/B AFT CORNER SUPPORT ANGLE CRACKED. REPLACED FORMED ANGLE AT NR 2 ENGINE PYLON HEAT EXCHANGER ACCESS CORNER IAW A-300 SRM 78-32-11 MATERIAL USED 2 INCH X 3 INCH OF 321-.032 LOT 68859082, PO 8314616.SDR AWXA0001678Bushing · out of positionNR 2 ENGINE PYLON O/B MID SPAR BUSHING HAS MIGRATED .095 INCHES. REPLACED BUSHINGS IAW SB 54-1037 PARAGRAPH 1D, AWA ER 03-5410-0111D-JS1. P/N: 311A1151-12, 311A1151-13.SDR C2XA01BT087Channel · crackedYUL---DURING 4C INSPECTION MAINTENANCE FOUND RT LOWER NACELLE IS CRACKED IN LT FORWARD CHANNEL. MAINTENANCE FABRICATED NEW EDGING AND INSTALLED IAW ATR42 SRM 54-12-61 AND ATR42 SRM 51-25-03. AIRCRAFT OK FOR SERVICE.SDR MWEA010640Angle · crackedRIGHT PYLON WEB ATTACH ANGLE CRACKED AT STATION 1038 JUST INBOARD OF AFT ENGINE MOUNT. FABRICATED AND INSTALLED ATTACH ANGLE.SDR UPS01435671Frame · crackedINSPECTION TYPE:C3 NR 4 PYLON PYLON AFT TORQUE BULKHEAD O/B VERTICAL CHORD, CRACK FOUND AT 2ND FASTENER HOLE (FROM LOWER) RUNNING O/B APPROX. 0.100 INCH LONG. NR 4 PYLON AFT TORQUE BULKHEAD O/B VERTICAL CHORD CRACKED HOLE O/SIZE FASTENER INSTALLED WITH FREESDR 2001UALA00469Web · crackedNR 2 PYLON WEB IS CRACKED OUT OF THE FORWARD RIGHT HAND CUTOUT, ABOVE THE FORWARD MOUNT, AT THE ONE OCLOCK POSITION. MANUFACTURED AND INSTALLED DOUBLERS. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00465Web · crackedNR 1 PYLON WEB CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLERS TO THE AFFECTED AREA. MAJOR REPAIR ACCOMPLISHED.SDR DL76S010599Brace · corrodedTHE BUSHINGS IN THE FORWARD AND AFT LUGS OF THE NR 1 AND 2 PYLON DIAGONAL BRACES WERE FOUND ROTATED / MIGRATED. THIS CONDITION WAS FOUND DURING REMOVAL/INSTALLATION OF THE PYLON WHICH HAD BEEN REMOVED FOR OTHER REWORK. REMOVAL OF THE BUSHINGS REVEALED MINOR SDR C2XA01BT054Channel · crackedDURING C-CHECK INSPECTION FOUND RIGHTHAND ENGINE HALF MOON COWL (446AT) HAS LEFTHAND CHANNEL CRACKED. MAINTENANCE REMOVED THE DAMAGED CHANNEL AND NEW CHANNEL FABRICATED IAW ATR42 SRM 54-12-61 FIGURE 101. INSTALLED IAW ATR42 SRM 51-25-01.
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