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 QXEA0201261Strut · chafedPDX - A LIGHT CHAFE EXISTS IN STRUT. REPAIRED IAW RD 8-54-036.SDR QXEA0201196Sump · crackedPDX- SUMP CRACKED AT RIGHT HAND FORWARD CORNER. REPAIRED IAW DHC8 SRM 51-40-11.SDR UPS02439176Stiffener · crackedINSPECTION TYPE:C #1 PYLON REAR ENGINE MOUNT B/H UPPER STIFFENER FOUND 2EA FASTENER HOLE CRACKED REFER ATTACHED SKETCH FOR DETAILS. #1 PYLON REAR ENGINE MOUNT B/H UPPER STIFFENER REPLACED AS PER SRM 51-10-01 PAGE 8.SDR UPS02439175Stiffener · crackedINSPECTION TYPE:C #2 PYLON REAR ENGINE MOUNT BULKHEAD UPPER STIFFENER 2EA FASTENER HOLES CRACK FOUND AT O/B SIDE OF PYLON THROUG THICKNESS REFER TO ATTACHED DRAWING FOR LOCATION. #2 PYLON REAR ENGINE B/H UPPER STIFFENER REPLACED AS PER SRM 51-10-01 PAGE 8.SDR UPS02439171Web · crackedINSPECTION TYPE:C #3 PYLON REAR MOUNT BULKHEAD FOUND CRACKED AT FWD & AFT WEB AT THREE FASTENER HOLE LOCATIONS AS PER ATTACHED FIGURE.(STA 221.9 TO 222, WL 170 TO 180). #3 PYLON REAR ENG MOUNT BULKHEAD REPAIR CARRIED OUT AS PER HX RS # R-54-53-34870.SDR UPS02439174Web · crackedINSPECTION TYPE:C #4 PYLON REAR MOUNT B/H AFT WEB FOUND CRACKS. #4 PYLON REAR ENG MOUNT BULKHEAD REPAIR CARRIED OUT AS PER HX RS # R-54-53-3487.SDR UPS02439173Web · crackedINSPECTION TYPE:C #1 PYLON REAR MOUNT B/H FWD & AFT WEB FOUND CRACKS. #1 PYLON REAR ENG MOUNT BULKHEAD REPAIR CARRIED OUT AS PER HX RS # R-54-53-34873.SDR UPS02439172Web · crackedINSPECTION TYPE:C #2 PYLON REAR MOUNT B/H. FWD. AND AFT. WEB FOUND CRACKS. #2 PYLON REAR ENG MOUNT BULKHEAD REPAIR CARRIED OUT AS PER HX RS# R-54-53-34872SDR AWXA200200790Longeron · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK THE #1 ENGINE FIXED FAIRING LOWER END "Z" ANGLE WAS FOUND CRACKED BETWEEN 1ST AND 2ND ATTACH FITTINGS FROM THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE LOWER END "Z" ANGLE ON THE #1 ENGINE FIXED FAIRING IAW B737-SDR AWXA200200789Angle · brokenMCN - MAJOR REPAIR - DURING C-18 CHECK A "T" ANGLE CLIP WAS FOUND BROKEN ON INBOARD SIDE OF THE #1 ENGINE FIXED FAIRING BETWEEN 2ND AND 3RD ATTACH FITTINGS FROM THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE "T" ANGLE CLIP ON INBOARD SIDE OF THE #1 ENGISDR AWXA200200788Angle · brokenMCN - MAJOR REPAIR - DURING C-18 CHECK A "T" ANGLE CLIP WAS FOUND BROKEN ON INBOARD SIDE OF THE #2 ENGINE FIXED FAIRING BETWEEN 2ND AND 3RD ATTACH FITTINGS FROM THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE "T" ANGLE CLIP ON INBOARD SIDE OF THE #2 ENGISDR 02FDEA00530Fitting · corrodedRIGHT PYLON THRUST AND SIDE LOAD FITTING FOUND BROWN STAIN ON TOP AND BOTTOM AREA.SDR SIMA200219807Frame · chafedDURING MBV INSPECTION MAINTENANCE FOUND LT NACELLE INBOARD FILLET AREA, CHAFED. BLENDED CHAFED AREA. PERFORMED NDT INSPECTION AND FOUND NO DEFECTS. MAINTENANCE FABRICATED AND INSTALLED AN REPAIR DOUBLER REPAIR DONE IAW SRM.SDR MALA020383Frame · crackedRT NACELLE FWD LOWER FRAME AT NS 197.00 CRACKED. R&R FRAME IAW EO S54058.SDR MALA020374Camlock · crackedRT OUTBOARD NACELLE AT FIG 8 CAMLOCK HAS HOLE AND CRACKS.REPAIRED IAW EO 54058.SDR UPS02438872Web · crackedINSPECTION TYPE:C NO.2 PYLON - LOWER SPAR BOTTOM AREA FOUND CRACK AT NAC STA 228 AS MARKED. LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 2 AND SRM 54-10-03 FIG 22.SDR QXEA0200901Rivet · loosePDX - ON WALKAROUND FOUND 3 LOOSE RIVETS ON NR 2 ENGINE NACELLE HORSE COLLAR. REINSTALLED HORSE COLLAR. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR ZW0A0206902Structure · crackedDURING CHECK-C MAINT ON RT PYLON, THE FWD OTBD SIDE LIGHTNING HOLE ON THE NUMBER 2 PYLON WAS CRACKED ABOUT 1/2 INCH LONG. CONFIRMED BY NDT. REPAIRED PER SERVICE BULLETIN 757-54-0037 AND EMLR 73125. --CLOSED--SDR JIK2002F00000Cap · wornENGINE CONTROL CABLE RUBBED THRU ON THE 90 DEGREES ANGLE FLANGE BY THE TOP OF THE LEFT NACELLE INBOARD SIDE. THIS CAP IS PART OF MAIN STRUCTURE OF THE NACELLE. FOUND AFTER UPPER NACELLE SKIN WAS REMOVED FOR REPAIR OF THE NACELLE.SDR 0201499921Rib · crackedDuring MCK in ATL, the aft portion of the lower cap, P/N 9958159-57, of the closing rib was found cracked. The crack was approximately .7" long on extends from a fastener hole 3.7" forward from the aft end of the cap.SDR UPS02438088Web · crackedINSPECTION TYPE:C #3 PYLON REAR ENGINE MOUNT B/H FOUND CRACKED AT AFT WEB FROM EDGE TO 3RD FASTENER HOLE. REFER ATTACH SKETCH FOR DETAILS. B/HEAD WEB CRACKED AREA REPAIRED AS PER RS 54-53-34781 AND UPS EO B747-5410-16695-A.SDR DHL2002726506Cowling · crackedDuring C Check "discrepancy" as follows, #3 engine upper cowling gouged/chaffed on the #12 rib O/B section.Corrective action as follows,Cut-out damaged area on #3 engine cowl upper #12 rib I.A.W. B-727 SRM 54-10-2. Fabricated repair from 7075-T6 .050 P.O.# 991SDR QXEA0200679Tail Cone · chafedPDX- RIGHT NACELLE TAIL CONE AFT SIDE HAS CHAFING ON INBOARD SIDE BY NUT PLATES. REPAIRED IAW DHC-8 SRM 51-40-11.SDR QXEA0200700Tail Cone · chafedPDX- RIGHT NACELLE INSIDE TAIL CONE THERE IS CHAFING TO THE UNDERSIDE OF DECK. REPAIRED IAW DHC-8 RD 8-54-097.SDR 200200203Structure · deterioratedNR 3 PYLON LOWER SURFACE, JUST AHEAD OF THE AFT ENGINE MOUNT ON THE LEFT SIDE FIRESHIELD DETERIORATED. FABRICATED, ALODINED, PRIMED AND INSTALLED PER B747 SRM.SDR 200200202Seal · crackedREPAIR CRACKS IN LEFT AND RIGHT LOWER SLOT SEALS. THE LOWER SLOT SEALS ARE MADE FROM THE SAME MATERIAL AS THE UPPER SLOT SEALS BUT ARE NOT COVERED BY THE 747 SRM. THIS DOCUMENT ALLOWS WELDING OF THE LOWER SLOT SEAL ASSEMBLIES PROVIDED THE REPAIR IS NOT IN THESDR 200200201Panel · delaminatedNR 3 ENGINE INTAKE NOSE COWL ACOUSTIC PANEL 5-6 OCLOCK FWD POSITION DELAMINATED. LOCATED AND DRILLED NEW ACOUSTIC PANEL, INSTALLED NEW ACOUSTIC PANEL.SDR 0201365643Torque Box · crackedDuring "H" check found crack in outboard side of pylon lower torque box upper aft corner at access panel 433AL. Repaired per EA 56-189401.SDR DL733020391Beam · corrodedCORROSION WAS FOUND ON THE CROWN BEAM LUG BORES ON THE #1 AND #2 PYLONS. THE BORES WERE OVERSIZED TO REMOVE THE CORROSION AND REPAIR BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.SDR DL757020400Fitting · crackedDURING INSPECTION THE NR 1 PYLON STRUT ATTACH MIDSPAR FITTING INBOARD FITTING OUTBOARD LUG A CRACK INDICATION WAS NOTED. THE LUG WAS OVERSIZED TO REMOVE CRACK INDICATION. REPAIRED PER ER/A 389368-14, REV A.SDR UPS02438027Frame · crackedINSPECTION TYPE:C NO.3 PYLON - REAR ENG MOUNT FTG UPPER FRAME FOUND CRACK AT O/B FWD AREA AS MARKED. REPAIR CARRIED OUT IAW REPAIR SCHEME INSTRUCTIONS REFER R-54-53-34756 FOR MAT HT REFER TO CWPS CONTROL SEQUENCE NO.SQYJ016-090 CLASSIFIED MAJOR REPAIR.SDR UPS02438026Frame · crackedINSPECTION TYPE:C NO.3 PYLON - REAR ENG MOUNT FTG UPPER FRAME FOUND CRACK AT O/B AFT PORTION AS MARKED. REPAIR CARRIED OUT IAW REPAIR SCHEME INSTRUCTION REFER R-54-53-34756 FOR MATERIAL HEAT TREATMENT REFER TO COMPONENT WORK PROCESS CARD CONTROL SEQUENCE NSDR C1HA200288009Angle · crackedNR1 PYLON LOWER FWD LEADING EDGE SUPPORT ANGLE IS CRACKED OUT AT A FASTENER HOLE. REMOVED DAMAGED ANGLE FABBED AND INSTALLED.SDR C1HA200288008Angle · crackedANGLE IS CRACKED IN RADIUS INSIDE NR 1 PYLON AT APPROX FS 1160 IN ACCESS AREA FOR THROTTLE QUADRANT. REMOVED DAMAGED ANGLE, FABRICATED AND INSTALLED.SDR 0200759865Rib · crackedDuring MCK in ATL, the upper cap of the closing rib was found cracked at YN 146. The crack was stop drilled at 2 ends and a repair angle was installed. Repaired per EA 98-188393.SDR 0200742002Rib · crackedDuring MCK in ATL, the aft end of the 99158159-57 lower cap of the pylon closing rib was completely severed by a crack. This EA 98-188392 provides the means for repair of the rib.SDR 2002F00863Angle · crackedANGLE LOCATED ABOVE THE ICE DOOR HINGE, THIS ANGLE HOLDS THE LOWER FIRE SEAL BULKHEAD. WHEN THIS ANGLE CRACKS, IT ALLOWS THE OUTSIDE COWL RIVETS TO WORK LOOSE, AND THIS CAUSES THE COWL SIDE SKIN TO CRACK. (M)SDR TIM2002F00010Angle · brokenANGLE LOCATED ABOVE THE ICE DOOR HINGE. THIS ANGLE HOLDS THE LOWER FIRE SEAL BULK HEAD WHEN THIS ANGLE CRACKS, IT ALLOWS THE OUTSIDE COWL RIVETS TO WORK LOOSE, AND THIS CAUSES THE COWL SIDE SKIN TO CRACK.SDR MWEA020112Fitting · crackedFITTING IS CRACKED, LOCATED AT FUSELAGE STATION 1038 UPPER INBOARD CORNER. -- FABRICATED AND INSTALLED FITTING.SDR MALA020152Seal · chafedDURING E-CHECK MAINTENANCE FOUND LT I/B NACELLE CHAFE IS OUT OF LIMITS IAW SAAB SRM 54-10-10. CAUSED BY LEADING EDGE FILLET FAIRING SEAL. MAINTENANCE REPAIRED NACELLE DAMAGE IAW MAL EO 54053.SDR MWEA020070Angle · oversizedPYLON WEB ANGLE HAS AN OVERSIZED HOLE. -- FABRICATED AND INSTALLED ANGLE.SDR MWEA020068Angle · oversizedREMOVED RIGHT PYLON AFT SPAR WEB ANGLE TO FACILITATE OTHER MAINTENANCE. (UPPER FASTENER HOLE OVERSIZED.) -- FABRICATED AND INSTALLED "L" ANGLE ON NEW WEB.SDR MWEA020120Angle · oversizedRIGHT PYLON AFT SPAR ANGLE HAS OVERSIZED FASTENER H0LE. -- FABRICATED AND INSTALLED ANGLE.SDR MWEA020119Fitting · oversizedRIGHT PYLON FITTING HAS OVERSIZE HOLE. -- FABRICATED AND INSTALLED FITTING AND RADIUS BLOCKS.SDR MWEA020118Angle · oversizedRIGHT SPAR AFT UPPER ANGLE HAS OVERSIZED HOLES. -- FABRICATED AND INSTALLED ANGLE.SDR MWEA020115Angle · oversizedRIGHT PYLON AFT SPAR UPPER ANGLE HAS OVERSIZE HOLES. -- FABRICATED AND INSTALLED ANGLE.SDR MWEA020114Angle · oversizedRIGHT PYLON AFT SPAR ANGLE HAS OVERSIZE HOLE. -- FABRICATED AND INSTALLED ANGLE.SDR HN62002F00009Bracket · wornHYDRAULIC LINE SUPPORT CLAMP BOLT IS LOOSE AND CHAFFING AGAINST FUEL LINE UNDER PANEL NR 611KT. CAUSE: WORN BRACKET. DISPOSITION:REPLACED FUEL LINE AND BRACKET.SDR DL733020059Beam · corrodedCORROSION WAS FOUND ON THE CROWN BEAM LUG BORES OF THE NR 1 AND NR 2 PYLONS. THE BORES WERE OVERSIZED AND REPAIR BUSHINGS INSTALLED. THE DAMAGE WAS FOUND DURING INSPECTION AT HMV.SDR QXEA0200108Barrel · crackedPDX - LT FINGERNAIL HAS A TWO PRONG CRACK IN BARREL. REPAIRED IAW DHC-8 RD 8-54-240 AND SRM 51-40-00.
Back to JASC 5410