JASC 5412
Service difficulty reports · 1,087
Reports filed under 5412 · Nacelle/Pylon, Bulkhead/Firewall, 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 = '5412' 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 = '5412' 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 QXEA200301600Firewall · crackedCRACK IN RIGHT FIRE WALL ON RIVET SIDE OF NACELLE ABOVE FIRE LOOP BRACKET ON OUTBOARD NACELLE. REPAIRED IAW DHC-8 RD 8-54-806, RD 8-54-109 AND RD 8-54-800.SDR ENHA200320002Bulkhead · crackedRT NACELLE WAS WEARING AND CRACKING AT CONTACT WITH RT AFT LOWER COWL. REPLACED BULKHEAD.SDR AMWA89Firewall · crackedFOUND LEFT ENGINE FIREWALL CRACKED. REPAIRED CRACK IN FIREWALL IN ACCORDANCE WITH SRM 54-90-01 BY INSTALLING DOUBLER.SDR AUS20031229Firewall · distorted(AUS) RT FIREWALL BUCKLED DUE TO ASSYMETRIC WASTER CONTACT DURING TAKEOFF IN GUSTY CONDITIONS. AIRCRAFT IS CONFIGURED AS AN AMPHIBIAN.SDR AWXA200301483Firewall · crackedLCQ - MAJOR REPAIR - DURING C-14 CHECK 5 EACH CRACKS WERE FOUND ON NR 1 ENGINE PYLON FORWARD FIREWALL. MAINTENANCE PERFORMED WELD REPAIR ON FORWARD FIREWALL PAN ASSEMBLY IAW AWA ER 15-5412-03322-SS1.SDR 03FDEA01809Bulkhead · damagedMX REPORTED FINDING HYDRAULIC FLUID ACCUMULATED INSIDE OF THE NR 1 ENGINE PYLON DUE TO THE LEAK AT AUK7617-5001 HYDRAULIC LINE. HYDRAULIC LEAK WAS FIXED AND PYLON VISUALLY INSPECTED FOR INTEGRITY/SECURITY PRIOR TO ANC/LAX LEG. A FOLLOW UP CONDITIONAL INSPECTSDR QXEA200301360Firewall · crackedCRACK IN NR 2 ENGINE FIREWALL AT 10 O'CLOCK POSITION. REPAIRED IAW DHC-8 RD 8-54-806.SDR UPS03441513Bulkhead · crackedINSPECTION TYPE: C, NR 3 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT FWD AND AFT WEB (NAC 221 TO 221). NR 3 PYLON REAR ENG MOUNT BULKHEAD LWR ASSY FRAME WEB INTERIM REPAIR ACCOMPLISHED AS PER RS R54-53-35090 & UPS AUTH 747-54-20043.SDR QXEA200301274Firewall · crackedCRACK ON TOP RIGHT HAND SIDE OF FIRE WALL. REPAIRED IAW DHC-8 RD 8-54-806.SDR UPS03441502Bulkhead · crackedINSPECTION TYPE: C, NR 4 PYLON REAR ENGINE MOUNT BULKHEAD FOUND CRACK AT FWD AND AFT WEB APPROX 2 X 1 INCH RESPECTIVELY. NR 4 PYLON REAR ENGINE MOUNT BULKHEAD FWD AND AFT WEB REPAIRED AS PER RS R54-53-35087 AND UPS ENGINEERING FILE 747-54-20042.SDR QXEA200301211Angle · crackedNR 1 ENGINE FIREWALL ANGLE IS CRACKED AT BOTH ENDS JUST BELOW AFT TOP HEAT SHIELD. REPAIRED IAW DHC-8 SRM 51-40-11.SDR C2XA03SH353Firewall · crackedSHV-DURING C CHECK THE APU FIREWALL WAS FOUND TO CRACKED AT THE TOP VERTICAL REINFORCEMENT. MAINTENACE REMOVED THE DAMAGED AREA AND PERFORMED A PATCH AND DOUBLER REPIAR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA03405Firewall · crackedDURING HANGAR MAINTENANCE IN MCN, THE RT ENGINE NACELLE UPPER AFT FIREWALL WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT ENGINE NACELLE UPPER AFT FIREWALL IAW SRM 51-00. (M)SDR QXEA200301091Firewall · crackedTWO CRACKS IN THE UNDERLYING STRUCTURE OF THE LT HAND NACELLE FIREWALL COMING OUT OF RIVET HOLES. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-54-180.SDR QXEA200301088Firewall · crackedFIREWALL HAS A CRACK ALONG INBOARD SIDE OF EXHAUST APERTURE UNDER INBOARD CLIP. REPAIRED IAW HORIZON AIR EA 2-54-180.SDR QXEA200301086Firewall · crackedFIREWALL HAS A CRACK ALONG INBOARD SIDE OF EXHAUST APERATURE AT STATION YN12. REPAIRED IAW HORIZON AIR EA 2-54-180.SDR QXEA200301093Firewall · crackedCRACK ON FIREWALL OF NR 1 NACELLE INBOARD SIDE. REPAIRED IAW DHC-8 RD 8-54-1840 AND HORIZON AIR EA 2-54-180.SDR QXEA200301032Firewall · crackedPDX- FIREWALL FOR LEFT NACELLE IS CRACKED AT THE 10 O'CLOCK POSITION OF THE EXHAUST APERTURE ABOVE THE NUT PLATE HOLE. REPAIRED IAW DHC-8 SRM 51-40-11, 51-00-06 AND RD 8-54-651.SDR DL757030754Bulkhead · damagedOVERSIZE HOLE REPAIR WHILE ACCOMPLISHING THE PYLON MODIFICATION REQUIRED BY AD 2000-20-09, SEVERAL HOLES IN THE NAC STA 203 BULKHEAD COMMON TO THE MIDSPAR ATTACH FITTING WERE DAMAGED. THE HOLES WERE OVERSIZED, HFEC INSPECTED, AND LARGER DIAMETER FASTENERS INSSDR QXEA200300986Firewall · crackedPDX- RIGHT MAIN LANDING GEAR WHEEL BAY FORWARD AT TWO OCLOCK FIREWALL IS CRACKED. REPAIRED IAW DHC-8 RD 8-54-109 AND SRM 51-00-06.SDR UPS03441097Bulkhead · crackedINSPECTION TYPE:C NR 1 PYLON REAR MOUNT BULKHEAD CRACK FOUND AT I/B FWD WEB EDGE NAS 221. NR 1 PYLON REAR MOUNT BULKHEAD REPAIRED IAW HX RS R54-53-35042 AND UPS ENGINEERING FILE NUMBER 747-54-20038.SDR CA030703009Bulkhead · cracked(CAN) NACELLE BULKHEAD CRACKED FROM LOWER RT BOLT HOLE TO EDGE OF BULKHEAD. NEW BULKHEAD INSTALLED ON BOTH NACELLES. PROBLEM ATTRIBUTED TO AIRCRAFT AGE AND NUMBER OFCYCLES.SDR 0301096719Frame · crackedDURING H-CHECK CRACKS WERE FOUND ON FORWARD FRAME WEB OF NR 1 PYLON REAR ENGINE MOUNT BULKHEAD. REPAIRED PER EA 67-165068.SDR P5CA0300883Bulkhead · crackedCRACKS FOUND ON AFT TORQUE BULKHEAD ON NR 1 & 4 PYLONS. REPAIRED PER SB 54-2201 BOEING PAO R11-03-00004H.SDR CA040604005Bulkhead · damaged(CAN) DURING A SCHEDULED ENGINE CHANGE THE LT CANTED BULKHEAD ASSEMBLY ENGINE MOUNT STRUCTURE WAS FOUND TO HAVE BEEN DAMAGED BY EXHAUST GASES. THE INDIVIDUAL PARTS REQUIRING REPLACEMENT ARE AS FOLLOWS. 0851500-47 CAP0851500-39 CHANNEL 0851601-201 WEB FORWARD SDR SWIA200312121Firewall · crackedLEFT NACELLE FIREWALL HAS SMALL CRACK. FOUND DURING C-CHECK INSPECTION. REPAIR APPLIED TO AREA MENTIONED IAW SRM 120 51-10-02.SDR SWIA200312120Firewall · crackedRIGHT NACELLE FIREWALL HAS SMALL CRACK. FOUND DURING C-CHECK INSPECTION. APPLIED DOUBLER IAW 120 SRM 51-10-02.SDR ABXA030180Bulkhead · crackedLEFT FORWARD PYLON BULKHEAD WEB HAD CRACK AT ATTACH FASTENER 20 INCHES FROM FLOOR, LEFT BUTT LINE 54. REPAIRED IAW DC-9 SRM 53-01.SDR C2XA03TY065Firewall · crackedTYS, DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND CRACKED. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED A DOUBLER AND INSTALLED IAW EC5330-01250. THE REPAIR IS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.SDR UPS03440831Bulkhead · crackedINSPECTION TYPE: C, NR 2 PYLON REAR ENGINE MOUNT BULKHEAD 5EA FASTENER HOLE CRACKED AT FRAME WEB. NR 2 PYLON REAR ENGINE MOUNT BULKHEAD FRAME WEB REPAIRED AS PER HX RS R54-53-35022 AND UPS EO B747-5410-17055-B.SDR 0300946632Bulkhead · crackedDURING H-CHECK FOUND CRACK IN NR 4 PYLON REAR MOUNT BULKHEAD WEB AT NACELLE STATION 221. REPAIRED PER EA 66-165066.SDR 0300936632Bulkhead · crackedDURING H-CHECK, FOUND CRACK IN NR 3 PYLON REAR MOUNT BULKHEAD WEB AT NACELLE STATION 227. REPAIRED PER EA 66-165065.SDR ABXA030175Fitting · crackedAFT LOWER INBOARD FITTING CRACKED FS 965 PYLON BULKHEAD RIGHT SIDE. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.SDR 2003FA0000420Structure · crackedDURING INSPECTION THE UPPER HORITONTAL (Z) ON THE FIREWALL WAS FOUND CRACKED. THIS IS THE LATER REINFORCED VERSION REV. 4. THE CRACK WAS LOCATED FROM THE HOLE WHERE THE NOSE GEAR STRUT COMES THROUGH TO THE OUTSIDE FORWARD EDGE.THE PLASTIC STOP UNDER THE (Z) WASDR 2003FA0000419Structure · crackedDURING INSPECTION THE UPPER HORITONTAL (Z) ON THE FIREWALL WAS FOUND CRACKED. THIS IS THE LATER REINFORCED VERSION REV. 4. THE CRACK WAS LOCATED FROM THE HOLE WHERE THE NOSE GEAR STRUT COMES THROUGH TO THE OUTSIDE FORWARD EDGE.THE PLASTIC STOP UNDER THE (Z) WASDR GTIA030322Fire Seal · crackedNR ENGINE APRON UPPER 6TH FROM FORWARD FIRE SEAL CRACKED. REMOVED CRACKED FIRE SEAL. FABRICATED NEW FIRE SEAL. INSTALL NEW FIRE SEAL.SDR GTIA030304Fireseal · crackedNR 2 ENGINE APRON UPPER 4TH FROM FORWARD FIRESEAL CRACKED. REMOVED CRACKED FIRESEAL. FABRICATED NEW FIRESEAL. INSTALLED NEW FIRESEAL.SDR P5CA0300861Bulkhead · gougedNR 1 PYLON BULKHEAD NAC STA 222 AFT FACE DOUBLER AT WL 174 ON LT SIDE OF THE WEB PER REF 1. REPAIRED PER SRM 54-14-03. PAO - SIN 03-0014M, PAO - SIN 03-00015F.SDR UPS03440611Bulkhead · crackedINSPECTION TYPE: C, NR 3 PYLON REAR ENGINE MOUNT BULKHEAD AFT FRAME FOUND CRACKED AT 4 O/C POSITION ( LOOKING FORWARD ). NR 3 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER HX RS R54-53-35008 AND UPS REPAIR AUTHORIZATION 747-54-20034 DVI AND HFEC INSPECSDR CH1A200395012Firewall · crackedNR 2 ENGINE FIREWALL FIRE BOX CRACKED 2 PLACESSDR ASOA03088Firewall · crackedDURING HANGER MAINTENANCE IN MCN, THE LEFT NACELLE UPPER FIREWALL WAS FOUND TO BE CRACKED WITH MATERIAL FALLING OUT. MAINTENANCE REPAIRED THE CRACKED NACELLE FIREWALL BY INSTALLING A DOUBLER IAW SRM.SDR 0300536744Web · crackedDuring "H" check found cracks in frame webs of #3 pylon rear engine mount bulkhead. Repaired per EA 67-165041.SDR 0300346744Web · crackedDuring "H" check found cracks in #4 pylon rear engine mount outboard forward and aft frame webs. Repaired per EA 67-165042.SDR 0300336744Bulkhead · crackedDuring "H" check found crack in #4 pylon aft torque bulkhead chord at the top fastener hole common to the lower spar fitting. Repaired per EA 67-165046.SDR ASOA03067Firewall · crackedFLT 4250 - THE LEFT PYLON FIREWALL AT FRAME STATION 659.75 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT PYLON FIREWALL AT FRAME STATION 659.75 IAW ASA EO 600-54-0010 AND REO 801R-54-51-004. (M)SDR 0300166718Bulkhead · crackedDuring "L" check found crack on #4 pylon rear engine mount bulkhead. Repaired per EA 67-165031.SDR 0300176718Bulkhead · crackedDuring "L" Check found crack on #2 pylon rear engine mount bulkhead. Repaired per EA 67-165032.SDR BAQA084034Firewall · crackedFIREWALL CRACKED ON LOWER CORNER. REPLACED WITH SERVICEABLE UNIT.SDR PA03005Bulkhead · crackedTHE LT ENGINE NACELLE AFT BULKHEAD IS CRACKED AT THE 6 O`CLOCK POSITION. PROBABLE CAUSE IS VIBRATION.(K)SDR QXEA0300154Firewall · crackedPDX- NR 2 NACELLE OUTBOARD FIREWALL IS CRACKED AT THE BEND ABOVE FIRE LOOP BRACKET. REPAIRED IAW DHC-8 RD 8-54-806.
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