JASC 5411
Service difficulty reports · 1,454
Reports filed under 5411 · Nacelle/Pylon, Frame/Spar/Rib, 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 = '5411' 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 = '5411' 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 KCSA061146Frame · crackedNR 4 PYLON INTERNAL RT SIDE LOWER FRAME IS CRACKED AT NAC STA 236.SDR QXEA200601157Frame · chafedPDX - INBOARD SURFACE OF HORSESHOE FRAME CHAFED BY FWD EDGE OF NACELLE PANEL 412AR. MAINTENANCE REPAIRED IAW RD 8/4-54-331 AND NDTM PART 6, 51-00-02.SDR KCSA061102Spar · chafedNR 1 PYLON HAS NUMEROUS DINGS AND CHAFE AREAS ON MIDSPAR WEB AT NAC STA 221 TO 199.SDR KCSA061060Spar · crackedNR 3 PYLON LOWER SPAR WEB CRACKED AT OUTBOARD NAC STA 229. REPAIRED WEB IAW B747 SRM 54-10-03 FIG 23.SDR KCSA061059Spar · crackedNR 3 PYLON HORIZONTAL SPAR WEB CRACKED AT NAC STA 234. REPAIRED WEB IAW B747 SRM 54-10-03 FIG 23.SDR MALA060188Frame · chafedDURING N4K CHECK IN BNA, FOUND NR 1 NACELLE, FORWARD FRAME AT NS 197 IS CHAFED OUT OF LIMITS ON THE INBOARD SIDE. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO#S54156. REF. EAMS WORK ORDER 213668 TASK 4503.SDR MALA060179Frame · chafedNR 1 NACELLE, FORWARD FRAME AT NS197 IS CHAFED ON THE IB FLANGE AND HAS BEEN REPAIRED IAW MESABA EO#S54155. REF: EAMS WORK ORDER 213644 TASK 4502.SDR UPS06446484Spar · crackedINSPECTION TYPE:C NR 2 PYLON LOWER SPAR WEB UPPER AT NAC STA 248 O/B RIVET AREA CRACKED, CRACK LENGTH 0.40". NR 2 PYLON LOWER SPAR WEB AT NAC STA 248 O/B AREA REPAIRED AS PER SRM 54-10-03 FIG 2.SDR AWXA200600426Rib · crackedPHX - MAJOR REPAIR - NR 1 ENGINE, NR 14 RIB FOUND CRACKED DURING MAINTENANCE INSPECTION. MAINTENANCE IS CURRENTLY REPAIRING.SDR UPS06146454Longeron · crackedNR 2 ENGINE PYLON STINGER FAIRING UPPER OUTBD MOUNT LONGERON HAS PIECE CRACKED OUT AT FORWARD END. REMOVED AND REPLACED O/B LONGERON PER SRM 51-40-21.SDR UPS06146451Longeron · crackedNR 1 AFT LOWER PYLON O/B ATTACH FLANGE BETWEEN RIB J3 AND RIB J4 HAS CRACK. REMOVED AND REPLACED O/B ATTACH FLANGE PER SRM 51-40-00.SDR MALA060131Frame · chafedDURING N4K BRIDGE CHECK IN BNA, FOUND AFT FORMER PN 7271115-037 ON COWLING PANEL NR 453CL IS CHAFED AND HAS BEEN REMOVED AND REPLACED IAW SRM 51-40-21. REF: EAMS WORK ORDER 213551 TASK 4508.SDR MALA060114Frame · chafedDURING N4K BRIDGE CHECK IN BNA, FOUND THE AFT FORMER PN 7271115-037 ON COWLING 463CL IS CHAFED AND HAS BEEN REMOVED AND REPLACED IAW SRM 51-40-21. REF: EAMS WORK ORDER 213551 TASK 4501SDR MALA060094Frame · crackedDURING 2Y CHECK IN BNA, FOUND RT NACELLE, OUTBOARD FRAME, AT NS203 IS CRACKED AND HAS BEEN REPAIRED IAW MESABA EO NR S54149.SDR MALA060072Frame · chafedLT NACELLE, FRAME AT NS197, INBOARD SIDE IS CHAFED OUT OF LIMITS AND HAS BEEN REPAIRED IAW MESABA EOS54148.SDR UPS06446371Frame · crackedNR 3 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT FWD AND AFT FRAME MOST O/B CRACK LENGTH 3/8" AND 1/4". NR 3 PYLON REAR MOUNT BULKHEAD BOTH SIDES FWD AND AFT FRAMES REPLACED AND REPAIRED AS PER RS R54-53-35431 DETAIL VISUAL AND HFEC INSPECTION OF THE BULKHEAD LWSDR UPS06446225Rib · crackedINSPECTION TYPE:C NR 2 PYLON, RT INTERIOR RIB CRACKED AT NAC STA 210 BELOW MID SPAR, CRACK LENGTH 2.5". NR 2 PYLON RT INTERIOR RIB AT NAC STA 210 BELOW MID SPAR AREA REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.SDR MALA060048Frame · crackedDURING 4K CHECK IN BNA FOUND FRAME ON RT O/B NACELLE, AT NS203 IS CRACKED AND HAS BEEN REPAIRED IAW MESABA EO S54145.SDR CALA0600031Frame · crackedINSPECTION FOUND A 0.626 INCH CRACK IN NR 1 PYLON I/B FRAME CHORD AT NAC STA 285. THE FRAME CHORD WAS REPLACED IAW ECRA 5420-01447.SDR QXEA200600163Frame · chafedPDX: RT NACELLE FRAME CHAFED FWD OF EXTERNAL AIRCRAFT POWER RECEPTABLE BACK COVER. MAINTENANCE REPAIRED IAW Q400 SRM 51-14-00, NDTM PART 6, 51-00-02, SRM 51-21-10, SRM 51-24-45 AND SRM 51-25-25.SDR UPS06846071Rib · wornINSPECTION TYPE:C1 5TH RIB ON NR 1 PYLON WORN" CHECK LIMITS". BLENDED OUT WORN AREA. FABRICATED AND INSTALLED REPAIR STRAP IAW DC-8 SRM 54-3-1 FIG 3, 51-1-8,51-1-21 AND 51-1-20D.SDR 06FDEA0094Frame · wornNR 2 ENGINE, LEFT CORE COWL INTERIOR FRAME (5TH FROM FORWARD) FOUND EXISTING REPAIR STRIP AND FRAME WORN. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL.II.SDR CALA0600003Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN LT PYLON NAC STA 285.4 AREA I/B FRAME CHORD. THE FRAME CHORD WAS REPLACED IAW ECRA 5420-01445.SDR CALA0600010Frame · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 2 PYLON NACELLE STRUT FRAME CHORD AT NAC STA 285.45, I/B AREA. THE FRAME CHORD WAS REPLACED IAW ECRA 5420-01444.SDR 2005UALA01448Bushing · looseNR 2 PYLON OUTBOARD MIDSPAR FITTING, INBOARD LUG BUSHING MOVES IN BORE. NR 2 PYLON OUTBD MIDSPAR FITTING, INBD LUG BUSHING MOVED IN THE BORE. BUSHING MIGRATION CAUSE IS UNKNOWN. IT WAS REPLACED WITH AN OVERSIZED BUSHING PER SRM 54-53-90SDR CA051219001Frame · cracked(CAN) DURING NOV 26/04 SB 5/316 INSPECTION 4 CRACKS WERE FOUND, 1 CRACK RT OB, 2 CRACKS LT OB AND 1 CRACK LT IB FRAMES AT STA 123.10 IN THE NACELLE. RD5-54-017 WAS INCORPORATED TO ALL 3 AFFECTED AREAS. DURING DEC 11/05 SB 5/316 INSPECTION THE NR OF CRACKS HASDR AWXA200600251Rib · damagedPHX - DURING ROUTINE MAINTENANCE THE LT PYLON NUMBER 5-RIB, LINE ATTACHMENT CLEATS (PN'S D463072820000 & D54610270200) WERE FOUND WORN AND ELONGATED AT SEVERAL LINE ATTACHMENT POINTS. MAINTENANCE REMOVED DISCREPANT PARTS FROM THE LT PYLON. WELDED DISCREPANT SDR 0501559869Rib · crackedDURING INSPECTION, FOUND CRACK IN LOWER SURFACE OF LT PYLON CLOSING RIB AND ANGLE BEHIND THE AFT ENGINE MOUNT. REPAIRED PER EA 98-205378.SDR CA050928002Longeron · cracked(CAN) WHILE CARRYING OUT THE LOWER LONGERON INSPECTION IAW AD CF 81-07R4 AND SB 6/509, THE LT IB LONGERON ON THE RT NACELLE WAS FOUND CRACKED LATERALLY ACROSS THE WEB. THE CRACK WAS JUST AFT OF THE ENGINE MOUNT.SDR UPS05445463Rib · damagedL/T SIDE OF THE NR 2 PYLON, DAMAGED RIBS REPAIR. SHOW EVIDENCE OF CRACK INSIDE PYLON OPPOSITE PREVIOUS REPAIR. 11' FROM SLOT SEAL OPENIN G AND 8' FROM BOTTOM EDGE. ACCOMPLISED HI-FREQUENCY EDDY CURRENT SUSPECT AREA NO CRACKS DETECTEDSDR SWIA200515616Rib · crackedRT PYLON, RIB CRACKED ON LOWER FLANGE AT FS605, ITEM FOUND AT C-CHECK INSPECTION. RIB REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 .SDR MALA050661Rib · chafedDURING 4Y/2Y INSPECTION IN BNA, FOUND RT NACELLE RIB NR 2 IS CHAFED AT NS203, LOWER SIDE. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#$54127. REF: EAMS WORK ORDER 212631 TASK 4540.SDR ABXA050200Spar · crackedRIGHT AFT PYLON SPAR WEB WAS CRACKED AT LIGHTNING HOLE, LONGERON 13 RIGHT. REPAIRED CRACK IAW DC-9 SRM 53-01.SDR 05FDEA02234Spar · crackedNR 1 PYLON INSIDE PNL 411CL UPPER SPAR WEB HAS CRACK.SDR 2005UALA00721Frame · crackedNR 2 PYLON INSIDE PNL 444DL, CENTER LOWER FRAME IS CRACKED. PYLON FITTING WAS REPLACED DUE TO A STRESS RELATED CRACK.SDR UPS05445065Frame · crackedNR 4 PYLON NAC STA 240 I/B SIDE FWD OF ACCESS PANEL CUTOUT 483EL VERT FRAME LIGHTEN HOLE CRACKED, CRACK LENGTH 2". NR 4 PYLON NAC STA 240 I/B SIDE VERTICAL FRAME REPLACED AS PER SRM 51-10-01 PG 9.SDR SWIA200515412Frame · crackedRIGHT FRAME 1 OUTBOARD SIDE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED RIGHT FRAME NR 1 IAW SB 120-54-0036 "REV 02".SDR 05FDEA01655Frame · crackedNR 1 ENG FIXED COWL UPPER FRAME CRACKED BETWEEN NR 2 AND NR 3 LATCHES. REMOVED AND REPLACED COWL PANEL IAW SRM 51-30-2.SDR UPS05144745Angle · crackedNR 2 AFT LOWER PYLON AT RIB 18 HAS CRACK APPROX .75 L AT RIB SECTION MEMBER INBD. MEMBER 2 PLACES ABOVE AND BELOW NUTPLATE. REMOVED AND REPLACED L-ANGLE ON THE NR 2 PYLON IAW A300 SRM 51-40-00.SDR QXEA200500920Rib · scratchedYYC - LEFT PYLON AFT ENGINE MOUNT SUPPORT RIB HAS SCRATCHES ON LOWER SIDE OF MOUNT. REPAIRED IAW HORIZON AIR EA R-54-93 AND REO 670-54-51-006.SDR UPS05444426Frame · crackedNR 1 PYLON AFT BULKHEAD I/B FRAME ADJ TO UPPER SPAR FTG CRACKED APPROX .1875 RUNNING I/B AND O/B, CRACK LENGTH .1875. NR 1 PYLON AFT BULKHEAD I/B FRAME REPAIRED AS PER HX RS R54-53-35295 AND UPS EA ENGINEERING FILE NR 747-54-20051.SDR UPS05444422Frame · crackedNR 1 PYLON AFT BULKHEAD O/B FRAME ADJ TO UPPER SPAR FITTING FOUND CRACKED RUNNING I/B TO EDGE AND RUNNING O/B .9375 INCH LONG, (CRACK LENGTH .9375 ). NR 1 PYLON AFT BULKHEAD O/B FRAME REPAIRED AS PER HX RS NR R54-53-35295 AND UPS ENGINEERING FILE NR 747-54-20SDR MALA050445Stringer · crackedDURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL.SDR MALA050444Stringer · crackedDURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL.SDR MALA050443Stringer · crackedDURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL.SDR MALA050442Stringer · crackedDURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL.SDR MALA050440Stringer · crackedDURING C2 INSPECTION, FOUND 1 CRACKED STRINGERS NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL.SDR MALA050438Stringer · crackedDURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL.SDR MALA050437Stringer · crackedDURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL.SDR MALA050441Stringer · crackedDURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL.
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