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 KCSA061325Frame · crackedNR 2 PYLON VERTICAL FRAME HAS .5 INCH CRACK LT SIDE AT NAC STA 265.SDR KCSA061324Frame · crackedNR 2 PYLON VERTICAL FRAME HAS CRACK 3 INCHES LONG AT NAC STA 270.SDR KCSA061323Frame · crackedNR 2 PYLON VERTICAL FRAME HAS CRACK .5 INCH LT SIDE AT NAC STA 250.SDR KCSA061322Frame · crackedNR 2 PYLON VERTICAL FRAME HAS CRACK AT U-CUTOUT AT NAC STA 180 RT SIDE.SDR HALA0600893Spar · crackedNR 1 PYLON UPPER SPAR FITTING AFT INBD HOLE HAS A CRACK INDICATION, HOLE IS O/S TO .468". REPAIRED THE NR 1 PYLON UPPER SPAR FITTING AFT I/B HOLE IAW GOODRICH ER NR 06-3462 DATED 07 NOV 06.SDR 2007UALA00316Frame · damagedNR 1 ENGINE PYLON AFT FAIRING LOWER WEBS, ADJACENT FRAMES AND STIFFENERS HAVE SUSTAINED HEAT DAMAGE. LOWER WEB INTERIM REPAIR INSTALLED. REPLACED THE PARTS PER UA-EVA-50655 REF SRM51-40-02 GENERAL, ACCOMPLISHED INSP AND GOOD, RECORD PN:313W3811-9, 313W3813-7SDR AALA20060817Fastener · looseAFW - RIGHT HAND PYLON MID SPAR FITTINGS FASTENERS ARE TURNING IN THE ENGINE UNLOADED CONDITION. REPAIRED PER MRB 767 2870. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR EIA2006213Rib · crackedFOUND CRACKED RIB NR 3 PYLON NAC STA 165. REPAIRED AS PER MM 51-10-01, 51-30-02. FABRICATED PER BOEING DRWG 35B90305.SDR KCSA061255Frame · crackedNR 2 PYLON NAC STA 221.9 FRAME CRACKED AT FWD I/B UPPER CORNER.SDR CA061002004Frame · cracked(CAN) AFT TAB WAS FOUND TO BE CRACKED UPON ROUTINE SCHEDULED INSPECTION. NEW FRAME ORDERED AND HELICOPTER WAS NOTIFIED OF THE PROBLEM. THEY HAVE SINCE RELEASED A NEW BULLETIN ADDING A CLAMP TO THE FRAME. THIS AIRCRAFT IS REGISTERED WITH MFG FOR WHEN THE CORRSDR SWIA200617032Frame · crackedLT IB NACELLE FRAME CRACKED AT POWER LEVER QUADRANT, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LT IB FRAME IAW RII 54-900-1000 AND SRM 51-10-02 PG 3 SEC 3 AND SECURED IAW 51-40-02.SDR AWXA200601397Frame · crackedMCN - FOUND BS 440 FRAME CRACKED AT STR 24R FROM STOP FITTING. MAINTENANCE REPAIRED STA 440 FRAME AT STR 24R STOP FITTING IAW AWA ER 03-5332-06210-ES2.SDR AWXA200601418Frame · crackedMCN - FOUND BS 492.5 FRAME CRACKED AT S24R FROM STOP FITTING. MAINTENANCE REPAIRED CRACKED BS 492.5 FRAME STR 24R IAW AWA ER 03-5332-06208 DF1.SDR KCSA061236Frame · crackedNR 4 PYLON NAC STA 221.9 AFT ENG MOUNT BULKHEAD JUST OB OF UPPER SPAR HAS STOP DRILLED CRACK IN HORSESHOE FRAMESDR KCSA061235Frame · crackedPYLON NR 4 AT PYLON STA 221.9 AFT ENG MOUNT BULKHEAD JUST IB OF UPPER SPAR HAS CRACKED HORSESHOE FRAME.SDR 06FDEA2652Rib · corrodedLT PYLON IB SIDE RIB 16A HAS CORROSION AROUND FAST HOLES REF N00174. REMOVED CORROSION ON RIB 16A GUSSET IAW A310 SRM 51-72-10 FOUND TO BE OUT OF LIMITS. REPLACED RIB 16A GUSSET IAW A310 SRM 51-40-21.SDR CA060720002Channel · cracked(CAN) WHILE CARRYING OUT MAINTENANCE IN THE RT LANDING GEAR AREA, A CRACK WAS FOUND IN THE IB LOWER NACELLE CHANNEL. THIS NACELLE CHANNEL IS THE ATTACH POINT FOR THE INBOARD GEAR DOOR HINGE. THE CRACK WAS LOCATED IN AFT PORTION OF THE HINGE ATTACH AREA MEASURSDR KCSA061229Spar · bulgedNR 2 PYLON UPPER SPAR WEB AT NAC STA 221 I/B AFT SIDE OF BULKHEAD LOWER UPPER SPAR WEB SURFACE BULGED.SDR KCSA061228Spar · buckledNR 1 PYLON MID SPAR WEB AREA BUCKLED NAC STA 221 AFT SIDE OF BULKHEAD LOWER I/B SURFACE.SDR UPS06547554Bulkhead · chafedINSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD I/B & O/B LOWER CORNER ARE CHAFED. COMPLIED WITH EA 757-5453-27-A1489.SDR UPS06447404Frame · crackedNR3 PYLON O/B SUPPORT FRAME LOWER PORTION FOUND CRACK AT NAC STA 252 AS MARKED, CRACK LENGTH 3/4". NR 3 PYLON NAC STA252 O/B SUPPORT FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.SDR MALA060457Frame · chafedLT NACELLE, AT NS197, INBOARD SIDE OF FRAME, IS CHAFED OUT OF LIMITS. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO#S54166. REF: EAMS WORK ORDER 214134 TASK 4516.SDR UPS06547553Bulkhead · gougedINSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD (LWR) LT AND RT OUTER SURFACES HAVE GOUGES. COMPLIED WITH EA 757-5453-27-A1489.SDR KCSA061188Frame · crackedNR 1 PYLON AT NAC STA 221.90, REAR ENG MOUNT BULKHEAD FRAME CRACKED AT TOP O/B SIDE.SDR KCSA061187Frame · crackedNR 2 PYLON AT NAC STA 221.90, REAR ENG MOUNT BULKHEAD FRAME CRACKED AT TOP O/B SIDE.SDR EIA2006117Rib · crackedNR 3 PYLON INTERIOR RIB FOUND CRACKED AT LWR PORTION AT NAC STA 210 RHS. RIB FABRICATED FROM T7075 T6511X 0.063. REMOVED AND REPLACED PER SRM B747 51-30-02 AND DRWG NR 65B90407-8HT.SDR SWIA200616831Rib · crackedCRACK FOUND AT LEFT NACELLE INBOARD UPPER RIB BELOW EXHAUST MOUNT. REPLACED LEFT NACELLE INBOARD UPPER RIB IAW SRM 120 51-10-02 PG 3 SEC 3A.SDR DL76S060501Fitting · damagedAN ELONGATED HOLE WAS FOUND ON THE INBOARD MID SPAR FITTING. THE HOLE WAS OVERSIZED TO CLEAN UP THE DAMAGE.SDR QXEA200602366Frame · crackedYYC: LT NACELLE, FRAME FOR COMPOSITE NACELLE STRUCTURE IS CRACKED JUST ABOVE THE CENTER AREA OF THE NUMBER 3 FLAP TRACK. MAINTENANCE REPAIRED IAW RD 8/4-54-155.SDR 2006UALA01013Frame · out of limitsFOUND HEAT DAMAGE. THE READING OF THE WEB AND THE BULKHEAD FRAME AT SAF STA 3.62 WERE OUT OF LIMITS. DURING THE ACCOMPLISHMENT OF COA 208490, CONDUCTIVITY TEST FOUND HEAT DAMAGE. THE READING OF THE WEB, 313W3811-13, AND BULKHD, 313W3812-4, AT SAF STA 3.62 WESDR EIA2006231Skin · crackedNR 3 PYLON, NAC STA. 247, NR 3 STIFFENER AND SKIN CRACKED. FABBED AND INSTALLED REPAIRS IAW ECRA 489-54-007-2 (MZJ).SDR QXEA200601353Frame · chafedPDX: C3. RH ENGINE NACELLE FWD FRAME TOP SIDE WHERE CHAFE STRIP WAS REMOVED HAS LIGHT CHAFE DAMAGE FROM CHAFE STRIP, 2 EACH SPOTS - ONE LEFT, ONE RIGHT OF CENTER. MAINTENANCE REPAIRED IAW NDTM TASK 51-00-02-250-801, Q400 SRM 51-14-00-350-804, RD 8/4-54-345 ANDSDR USAA060704Bushing · corrodedNR 2 PYLON LOWER SPAR FITTING BUSHING CORRODED. REPLACED BUSHING PER EA 97272, SRM 54-52-90, DEFECT SIZE: .050"L X .050"W X .002"D.SDR QXEA200601352Lug · chafedPDX: C3. FWD FRAME NR 2 ENGINE NACELLE OB LUG FOR LOWER COWL HAS A CHAFE. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02, HORIZON EA 6-54-408 AND RD 8/4-54-342.SDR QXEA200601339Lug · chafedPDX: C3. NR 1 ENGINE FWD FRAME INBOARD LUG FOR LOWER COWL MOUNT HAS A CHAFE BY HOLE. MAINTENANCE REPAIRED IAW Q400 NDTM PART 6, 51-00-01 AND HORIZON EA 6-54-409.SDR DU4R2006444Frame · misdrilledNR 2 PYLON INBOARD LOWER CHORD FROM PPS 128 TO PPS 138 HAS 8 EACH DRILL MARKS BESIDE FASTENER HOLES. REPAIRED FASTENER HOLES BY FABRICATING AND INSTALLING FREEZE PLUGS 1 EACH .391 X .225 INCH AND 2 EACH .405 X .225 INCH FROM 15-5 PH IAW DELTA ERA 455398-14 RESDR UPS06446970Attach Angle · crackedINSPECTION TYPE:C NR 4 PYLON NAC STA 221.9 REAR ENG MOUNT B/H UPPER OF MID SPAR WEB ATT T-ANGLE FOUND CRACKED JUST AT O/B SIDE. CRACK LENGTH 1.75 INCH. NR 4 PYLON NAC STA 221.9 REAR ENG MOUNT B/H UPPER OF MID SPAR WEB ATT T-ANGLE REPAIRED AS PER SRM 51-40-04SDR 061162Rib · crackedNR 3 PYLON INTERNAL RT SIDE RIB FRAME IS CRACKED AND GOUGED AT NAC STA 192, 7 INCHES ABOVE LOWER SPAR.SDR DHL2006364504Tee Fitting · crackedPERFORM EDDY CURRENT INSPECTION OF NR 1 PYLON RIB NR 4 I/B SIDE TEE BRACKET TO VERIFY PREVIOSLY ID CRACK AS PER SB A300-54-068. REMOVED AND REPLACED "T" BRACKET AND RIB NR 4 AT NR 1 PYLON I/B AREA AS PER SRM 51-10-40.SDR 061161Rib · crackedNR 4 PYLON INTERNAL UPPER RIB FRAME IS CRACKED AT NAC STA 221.SDR 061160Rib · crackedNR 2 PYLON INTERNAL UPPER RIB FRAME IS CRACKED AT NAC STA 221.SDR UPS06447026Frame · crackedINSPECTION TYPE:C NR 3 PYLON REAR MOUNT BULKHEAD FOUND CRACKS AT BOTH SIDES FWD AND AFT FRAME WEB. CRACK LENGTH 1 INCH TO 3.5 INCH. NR 3 PYLON REAR MOUNT BULKHEAD FWD AND AFT BOTH SIDES FRAME WEB REPLACED AND REPAIRED AS PER RS R54-53-35482 AND ENGINEERING FSDR UPS06446966Attach Angle · crackedINSPECTION TYPE:C NR 4 PYLON NAC STA 221.9 REAR ENG MOUNT B/H LOWER OF MID SPAR WEB LHS I/B AREA T-ANGLE CRACKED. CRACK LENGTH .5 INCH. NR 4 PYLON NAC STA 221.9 REAR ENG MOUNT B/H LOWER OF MID SPAR WEB ATTACH T-ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-0SDR EIA2006097Skin · crackedNR 4 PYLON UPPER SKIN AND SIDE FRAMES CRACKED. REMOVED DAMAGE, HFEC THE AREA, FABBED AND INSTALLED REPAIR PER ECRA 489-54-003-2.SDR MALA060298Frame · chafedDURING 2YEAR CHECK IN BNA, FOUND RT NACELLE, FRAME AT NS197, OUTBOARD SIDE, IS CHAFED OUT OF LIMITS AND HAS BEEN REPAIRED IAW MESABA EO#S54160. REF: EAMS WORK ORDER 213786 TASK 4506.SDR MALA060297Frame · chafedDURING 2 YEAR CHECK IN BNA FOUND LT NACELLE, FRAME AT NS197, INBOARD SIDE, IS CHAFED OUT OF LIMITS AND HAS BEEN REPAIRED IAW MESABA EO#S54159. REF: EAMS WORK ORDER 213786 TASK 4503.SDR DL757060356Spar · damagedTHE NR 2 PYLON INBOARD MID SPAR CHORD HAS 3 ELONGATED HOLES. HOLES WERE OVERSIZED TO CLEAN UP THE DAMAGE AND BUSHED TO ORIGINAL SIZE AND LOCATION.SDR UPS06547038Bulkhead · chafedINSPECTION TYPE:N/A NR 1 PYLON MIDSPAR BULKHEAD LOWER O/B CORNER IS HEAVILY CHAFED. COMPLIED WITH EA757-5453-A1439 AND UPS EO B757-5410-24414.SDR QXEA200601200Stringer · crackedPDX - C4 LEFT NACELLE FINGERNAIL DECK STRINGERS CRACKED BOTTOM SIDE AND FORWARD. REPAIRED IAW DHC-8-200 SRM 51-40-11.SDR CALA06136Frame · crackedNR 2 PYLON NACELLE O/B FRAME CRACKED AT STA 285.45. REPLACE CHORD PER SRM 51-10-02 & 51-40-02.
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