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 REXA2015030800304Structure · chafedTASK CARD 900-78-430-100, RT ENGINE CORE COWL CHAFING AT PYLON SEAL AREA. MECHANIC BLENDED CHAFED AREA, FABRICATED AND INSTALLED REPAIR AS REQUIRED IAW SRM 54-13-00-201-006-A01.SDR REXA2015030800303Structure · chafedTASK CARD 900-26-430-100 LT ENGINE CORE COWL CHAFING AT PYLON SEAL AREA. MECHANIC REPAIRED LT ENGINE COWL CHAFING AT PYLON SEAL AREA IAW SRM 54-13-00-201-006-A01.SDR SWIA201540934Latch · chafedLEFT NACELLE LATCH DOOR ASSY CHAFED. REPAIRED IAW EA.SDR REXA2015030400298Fairing · crackedTASK CARD CRJ900 C1, NR 1 ENGINE HINGE LINE FAIRING 433BT CRACKED AROUND FASTENER HOLE. MECHANIC REMOVED DAMAGED SECTION OF NR 1 ENGINE HINGE LINE FAIRING 433BT. FABRICATED AND INSTALLED DOUBLER AND SPIGOT TO HINGE LINE FAIRING IAW REO 670-78-33-998.SDR REXA2015030400297Fairing · crackedTASK CARD CRJ900 C1, NR 1 ENGINE HINGE LINE FAIRING 433BB CRACKED AROUND FASTENER HOLE. MECH REMOVED DAMAGED SECTION OF PANEL 433BB, FABRICATED REPAIR DOUBLER AND SPIGOT INSTALL ON PANEL 433BB IAW REO 670-78-33-998.SDR DALA2015022301792Rub Strip · wornINBD PYLON ACCESS 436BL INTERNAL FASTENER RUBSTRIPS WORN, SEPARATED. REPLACED DOUBLER IAW SRM 54-53-01.SDR SWIA201540824Door · dentedSEVERAL DENTS ON LT ENGINE LOWER FAN COWL DOOR. C-CHECK, ADDRESSED SEVERAL DENTS ON LT ENGINE LWR FAN COWL DOOR IAW REO.SDR DALA2015020901092Angle · crackedCRACK ON ACCESS PANEL ANGLE. ANGLE REPLACED IAW DWG 9935747, REV SRM 51-10-3, P-21-14, 51-30-2.SDR K11A2015033129001Angle · crackedNR 1 PYLON INBD CHORD ANGLE HAS CRACK INDICATION IN FWD FASTENER HOLE COMMON TO FWD ENGINE MOUNT, HOLE "A" LISTED IN SB 727-54A0010, R6, FIG 1.SDR DALA2015020100963Spar · crackedNR 2 NACELLE STRUT FWD UPPER SPAR WEB AROUND THE OTBD DRAIN HOLE FOUND CRACK. REPAIRED IAW ERA 14-530674.SDR DALA2015012900760Retainer · crackedCRACKED PYLON T/E RT RETAINER. THE RETAINER WAS REPLACED IAW SRM 54-31-0, FIG 2B AND 51-31-1.SDR HYIA01242015001Beam · crackedDURING SCHEDULED INSPECTION EVENT, THE RT NACELLE INBD ENG BEAM WAS FOUND TO BE CRACKED AT UPPER FWD INBD RADIUS IN THE AREA CORRESPONDING TO FWD INBD ENG MOUNT. A SUPPLEMENT TO THIS SDR WILL BE SUBMITTED TO ILLUSTRATE DAMAGE POINT. CORRECTIVE ACTION WILL BESDR ASAA2015011010204Panel · crackedNR 1 ENGINE FAN DUCT PANEL CRACKED AT FASTENER HOLE NR 6 PANEL. ACFT GROUNDED. R & R 1 ENG FAN DUCT PANEL 72-2302-400-801-100.SDR QXEA2015010901141Doubler · crackedFOUND CRACKED DOUBLER RT AFT NACELLE. REMOVED AND REPLACED THE DOUBLERIAW 54-35-20-02-03 AND 54-35-20, REPAIR-03.SDR DALA2015010200016Fitting · damagedDAMAGE FOUND INSIDE THE OTBD LUG ON NR 1 PYLON UPPER SPAR FITTING LUG BORES. REPAIRED CARRIED OUT IAW SRM.SDR KCSA201412311103Fireshield · damagedNR 1 ENGINE OTBD LOWER PYLON SKIRT FIRESHIELD DAMAGED AT NAC STA 210.SDR KCSA201412311102Fireshield · damagedNR 1 ENGINE OTBD LOWER PYLON SKIRT FIRESHIELD DAMAGED AT NAC STA 236.SDR KCSA201412311101Fireshield · damagedNR 4 PYLON OTBD FIRESHIELD DAMAGED AT NAC STA 236.SDR KCSA201412311100Fireshield · damagedNR 4 PYLON, OTBD FIRE SHIELD DAMAGED AT NAC STA 225.SDR KCSA201412311099Fireshield · damagedNR 4 PYLON INBD FIRE SHIELD DAMAGED AT NAC STA 212.SDR KCSA201412311097Fireshield · damagedNR 2 ENGINE INBD PYLON SKIRT, LOWER, FIRE SHIELD DAMAGED FROM NAC STA 179 TO STA 218.SDR KCSA201412311096Fireshield · damagedNR 4 ENGINE INBD PYLON SKIRT, LOWER FIRE SHIELD DAMAGED AT NAC. STA 235,SDR REXA2014122001225Hinge · wornLOWER BLOWOUT DOOR HAS WORN HINGE AND LATCH PLATE. MECH REPAIRED LT LWR COWL HINGE BODY IAW EA. R & R LEVER ARM IAW SRM 51-41-02-001-001-A01. R & R LATCH PLATE IAW SRM 51-42-10-001-001-A01, FIG 51-42-10-991-804 AND SRM 51-42-06-001-001-A01.SDR DALA2014122006920Spar Web · crackedNR 2 PYLON MID SPAR WEB FOUND CRACKED APPROXIMATELY 0.410 INCH LONG ON THE AFT MIDSPAR WEB LT CORNER AREA. REPAIRED ERA 524557-14AD.SDR REXA2014121801220Structure · wornNR 1 ENGINE AFT CORE COWL SHOWS WEAR AT PYLON INTERFACE AREA. MECH REMOVED DAMAGE AT PYLON INTERFACE AREA, FABRICATED RUB STRIPS PERFORMED NDT AND INSTALLED RUB STRIPS IAW SRM 54-13-00-201-006-A01 AND NDTM PART 1 51-20-006-250-A01 AND SRM 51-42-06-001-001-A01SDR DALA2014121806918Spar · crackedNR 1 PYLON FOUND CRACKED ON THE FWD UPPER SPAR WEB AT NAC STA 156. REPAIRED IAW ERA 530659-14.SDR ASOA2015011312043Skin · dentedLEFT NOSE INLET COWL HAS A DENT JUST FWD OF FADEC ACCESS PANEL. COMPLIED WITH PERMANENT REPAIR IAW SRM 54-11-01. CLEANED AREA OF DENT AND MEASURE DAMAGE 2.0" LONG X 1.6" WIDE X 0.075" DEEP FOUND DENT OUT OF LIMITS IAW SRM 54-11-01-101-001-A01.SDR QXEA2014121501062Fastener · backed outRIVETS BACKING OUT LT NACELLE JUST AFT OF INBD TEE PANEL. REPLACED RIVETS IAW SRM 51-42-45 STEP 6G, AND DWG 85414612.SDR DALA2014121106508Shackle · wornDURING INSPECTION, FOUND RT PYLON AFT SHACKLE, FWD, FWD FACE HAS WEAR MARK AROUND ALL THREE SLEEVE HOLES. REMOVED DAMAGE IAW SRM 51-73-00. FOUND OUT OF LIMITS IAW ER/A 507720-14MA. INSTALL NEW SHACKLE.SDR SWIA201440221Fairing · chafedRT ENGINE LOWER HINGE LINE FAIRING 443BB IS CHAFED . REPAIRED FAIRING IAW EA.SDR SWIA201440220Fairing · chafedLT ENGINE LOWER HINGE LINE FAIRING 433BB CHAFED. REPAIRED FAIRING IAW EA.SDR CA141126003Strap · corroded(CAN) FOLLOWING REMOVAL OF THE FOUR (4) ENGINE NACELLE INLET DEICE BOOTS, MISSING AND CORRODED RIVET HEADS WERE DISCOVERED ON THE FIBERGLASS INLET LIPS. FURTHER CORROSION WAS FOUND ON THE FOUR (4) ENGINE NACELLE STRAPS BENEATH THE FIBERGLASS INLET LIPS. MAISDR SWIA201440219Door · damagedLEFT NACELLE DAMAGED TO COWL WHEN COWLS WERE OPENED. REPAIRED IAW REO. OPS CHECKED GOOD.SDR SWIA201440218Door · damagedDAMAGE TO COWL WHEN COWLS WERE OPENED. REPAIRED IAW REO. OPS CHECK GOOD.SDR SWIA201440319Slider · gougedRIGHT OTBD TRANSLATING COWL SLIDER GOUGED AT FORWARD END OF SLIDER. MARKED, C-CHECK, RO 12/6/14, REMOVED DAMAGE FROM RT OTBD TRANSLATING COWL SLIDER AT FORWARD END. ORIGINAL MATERIAL THICKNESS .152", REMAINING THICKNESS .106". MATERIAL LOSS OF .046" WITHIN LSDR SWIA201440318Slider · gougedRIGHT ENGINE INBD TRANSLATING COWL SLIDER, FORWARD END OF SLIDER GOUGED. REMOVED DAMAGE FROM RT INBD TRANSLATING COWL SLIDER AT FORWARD END. ORIGINAL MATERIAL THICKNESS .152", REMAINING THICKNESS .128". MATERIAL LOSS OF .024" WITHIN LIMITS. TUC5271 DUE 31 ASDR SWIA201440317Slider · gougedRIGHT ENGINE INBD TRANSLATING COWL SLIDER GOUGED AT FORWARD PART OF SLIDER. REMOVED DAMAGE FROM RT INBD TRANSLATING COWL SLIDER AT FORWARD END. ORIGINAL MATERIAL THICKNESS .152", REMAINING THICKNESS .138". MATERIAL LOSS OF .014" WITHIN LIMITS. TUC5271 DUE 31SDR SWIA201440160Louver · bentLEFT ENGINE PDU ACCESS PANEL LOUVERS SLIGHTLY BENT. REPAIRED IAW REO. ACFT GOOD TO CONTINUE SERVICE.SDR EE4Y2014122000276Fairing · corrodedENGINES NR 1 AND 2, STRUT FAIRING SKIN CORRODED. THE STRUT FAIRINGS WERE REPAIRED IAW MESSAGE NR COO-FJA-14-0001-10B, DTD 26, NOV 2014, UNDER NON RUTINE WO: A1C260,SUBJOB 4 ITEMS 1,2 & 3.SDR 2014FA0000664Crossbeam · chafedDURING 50 HR, 30 DAY VISUAL INSPECTION, TECH NOTICED RESIDUE ON CROSSMEMBER UNDER NR 2 ENGINE DECK. ON FURTHER INSPECTION, FOUND WEAR HOLE IN NR 2 ENGINE DECK FOUND TO BE CHAFED THROUGH BY ENGINE FIRE SUPPRESSANT DISTRIBUTION TUBE.SDR SWIA201440130Structure · bentRIGHT UPPER FAN COWL INBD LOWER AFT CORNER BENT. REPAIRED RT UPPER FAN COWL DOOR IAW REO. OPS CHECKED GOOD AT THIS TIME.SDR SWIA201440128Skin · dentedRT ENGINE UPPER TRANSCOWL INBD FWD CORNER DENTED. REPAIRED RT ENGINE UPPER TRANSCOWL INBD FWD CORNER DENT IAW REO TESTED GOOD.SDR EE4Y201411060265Angle · crackedNR 1 ENGINE FAN COWL RT INNER OIL SERVICE DOOR WITH ANGLE CRACKED.SDR SWIA201439989Bushing · wornBUSHINGS WORN AND MIGRATED ON RT ENGINE PYLON HINGE ATTACHMENTS. R & R THE BUSHINGS ON THE RT ENGINE PYLON TIE BAR IAW REO.SDR SWIA201440156Door · damagedDAMAGE FOUND ON RT ENGINE FAN COWL DOOR. REPAIRED IAW REO.SDR SWIA201439750Drain Mast · crackedCORE COWL 445AB DRAIN MAST CRACKED. C-CHECK, REPAIRED CRACK IN DRAIN MAST ON PANEL 445AB IAW EA.SDR FDEA201410223334Hinge · crackedPANEL 362CR UPPER AFT HINGE LOBE IS BROKEN ON ACFT SIDE. REPAIR OF THE NACELLES, PYLON FILLETS FAIRINGS PANEL 362CR UPPER HINGE BROKEN LOBE. SPLICE REPAIR HAS BEEN ACCOMPLISHED IAW EA 8-5480-T0312263P1, WRI 54809675 STEPS 1 - 14, MAJOR REPAIR.SDR SWIA201440059Door · dentedLEFT LOWER FAN COWL HAS TWO DENTS. REMOVED AND INSTALLED LOWER FAN COWL DOOR IAW AMM AND REPAIRED DENTS IAW REO.SDR DALA2014102105694Hinge · delaminatedDELAMINATION ON INBOUND FLT NR 1 OTBD ENGINE PYLON HINGE PANEL. C/W ERA 529948-14, REV ORIGINAL INSTALLED PERMANENT REPAIR IAW SRM 51-70.SDR CA141015004Clamp · torn(CAN) AFTER DEPARTURE AND GEAR UP THE NO 2A HYD PUMP CAUTION LIGHT CAME ON AND SYSTEM QTY WENT TO 0% MAINTENANCE FOUND LEAK AT FLEXIBLE LINE (REF IPC 29-17-06, FIG. 1C, ITEM 128) FROM IB AFT NR 2 PYLON DOWN TO THE HYDRAULIC DAMPENER. THE SADDLE CLAMP P/N BBDRE
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