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 ASAA0440067Bearing · defectiveGYR - FOUND NR 1 ENGINE PYLON, UPPER LINK ATTACH POINT ROTATING IN UPPER SPAR FITTING. REMOVED AND REPLACED CROWN BEAM BEARING. (M)SDR ASAA0440066Bearing · looseGYR - NR 2 PYLON, UPPER SPAR ATTACH FITTING BEARING IS LOOSE IN LUG. REMOVED AND REPLACED CROWN BEAM BEARING. (M)SDR SWIA200413081Frame · crackedLEFT NACELLE FRAME ONE IS CRACKED ON INBOARD AND OUTBOARD SIDES. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT NACELLE FRAME ONE IAW 120 SB 120-54-0036 & 120 SRM 51-10-02 PG 3 PAR 3. ACCOMPLISHED PART II OF SB 120-54-0036.SDR SWIA200413080Frame · crackedRIGHT NACELLE FRAME ONE CRACKED ON INBOARD AND OUTBOARD SIDES. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT NACELLE FRAME ONE IAW 120 SB 120-54-0036 PART II AND 120 SRM 51-10-02 PG 3 PAR 3, ACCOMPLISHED PART II OF SB 120-54-0036.SDR C2XA04SH076Structure · chafedSHV- DURING C-CHECK THE NUMBER ONE ENGINE UPPER COWLING AFT EDGE STRUCTURE WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE STRUCTURE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 2004FA0000206Spar Cap · corrodedDURING AN INSPECTION FOUND A LOT OF CORROSION IN THE REGION OF RT FIREWALL NACELLE AND THE THE UPPER FWD SPARCAP. BECAUSE OF THIS FACT HE TOOK OUT THE WING LOCKER TANK. IN THIS REGION HE FOUND A LOT OF HEAVY CORROSION.SDR UPS04441981Frame · crackedINSPECTION TYPE: C, NR 3 PYLON REAR MOUNT BULKHEAD FOUND CRACKS AT O/B FWD AND AFT FRAME WEB. FRAME WEB ATTACH PARTS REINSTALLED PER BS 54-53-34870 AND CONTINUE REPEAT INSPECTION PER RS OR UPS EO SINCE NO FURTHER CRACK PROPAGATION AFTER REPAIR PARTS REMOVED.SDR SWIA200412973Frame · crackedLEFT ENGINE FRAME NR 1 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT ENGINE FRAME NR 1 IAW EMB120 SRM 51-10-02 PG 3 SEC 3A AND S/B 120-54-0036 AND RII CARD 54-301.SDR SWIA200412972Frame · crackedLEFT MLG, OUTBOARD LOWER NACELLE FRAME CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LOWER NACELLE FRAME IAW 120 SRM 51-10-02 PG 3 SEC 3A & RII CARD 54-301.SDR SWIA200412971Frame · crackedRIGHT NACELLE (WHEEL WELL) OUTBOARD UPPER FRAME CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT NACELLE (WHEEL WELL) OUTBOARD UPPER AFT FRAME IAW EMB120 SRM 54-10-03 PAGE 202 FIG 201 SHEET 1.SDR UPS04441804Frame · crackedINSPECTION TYPE:C NR 4 PYLON - LOWER CAVITY NEAR NAC STA 211 RT VERT SUPPORT RIB CRACKED. NR 4 PYLON - LOWER CAVITY NEAR NAC 221 RT VERTICAL SUPPORT FRAME REPLACED AS PER SRM 51-10-01 PAGE 8.SDR SWIA200412958Frame · crackedCHANNEL CRACKED FORWARD OF FRAME NR 1 ON RIGHT ENGINE NACELLE AT TOP INBOARD SIDE AT UPPER NUT PLATE STRIP. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD SECTION OF CHANNEL FORWARD OF FRAME NR 1 ON RIGHT NACELLE IAW SRM 54-10-02.SDR ABXA040047Rib · crackedLEADING EDGE ASSEMBLY RIB WAS CRACKED. REPAIRED IAW DC-9 SRM K05159.SDR SWIA200412849Frame · crackedLEFT NACELLE INBOARD HALF FRAME UNDER TAILPIPE AFT MOUNT FRAME CRACK. DISCOVERED DURING C-CHECK INSPECTION. REPLACED NACELLE HALF FRAME IAW 120 SRM 51-10-02.SDR SWIA200412914Rib · crackedFS 605 RT PYLON RIB CRACKED. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 & RII 54-401. P/N: 601-37004-86.SDR UPS04441709Spar · crackedINSPECTION TYPE: C, NR 1 PYLON I/B AFT LOWER SPAR WEB FOUND CRACKED JUST AFT OF REAR ENGINE MOUNT BULKHEAD. NR 1 PYLON LOWER SPAR WEB I/B EDGE AREA REPAIRED AS PER SRM 54-10-03 FIG 23.SDR UPS04441708Spar · crackedINSPECTION TYPE: C, NR 3 PYLON I/B AFT LOWER SPAR WEB FASTENER FOUND CRACKS JUST AFT OF REAR ENGINE MOUNT BULKHEAD. NR 3 PYLON I/B AFT LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 22 AT NAC STA 221.9.SDR C2XA03SH526Rib · gougedDURING C CHECK THE AFT EDGE MEMBER WAS FOUND TO BE GOUGED AT THE SIX O'CLOCK POSITION. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR AWXA200400006Rib · crackedMCN - MINOR REPAIR - DURING C-02 CHECK A 1.25 INCH CRACK WAS FOUND ON NR 2 PYLON AFT FIXED FAIRING (RIB 12) AT OUTBOARD ANGLE. MAINTENANCE REMOVED CRACKED RIB AT NR 2 PYLON AFT FIXED FAIRING; FABRICATED A NEW REPLACEMENT RIB; INSTALLED REPAIR PART IAW A320 SRSDR SWIA200312747Frame · crackedRT NACELLE FRAME CRACKED AFT CENTER JUST BELOW JET PIPE. DISCOVERED DURING C-CHECK INSPECTION. DOUBLER REINFORCEMENT INSTALLED AT AFFECTED RT NACELLE AREA IAW EMB120 SRM 51-40-02.SDR AWXA200301531Rib · crackedDURING C-04 CHECK A .375 INCH CRACK WAS FOUND ON NR 2 ENGINE PYLON AFT FIXED FAIRING RIB 14 AT PYLON STATION 908. MAINTENANCE REMOVED AND REPLACED CRACKED NR 2 ENGINE PYLON AFT FIXED FAIRING RIB 14 AT PYLON STATION 908 IAW A319 SRM 51-42-11, FIG 2, 3, & 8, PGSDR QXEA200301529Frame · chafedFRAME CHAFED UNDER RIGHT HAND GRAVEL GUARD. REPAIRED IAW RD 8-54-1052.SDR SWIA200312679Frame · crackedRIGHT NACELLE FRAME NR 1 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT NACELLE FRAME NR 1 IAW SB 120-54-0036 PART 2. C/W CARD RII 54-301.SDR DHL2003364017Spar · corrodedDURING CLEANING OF PYLON AREA DUE TO HYD LEAKAGE FOUND POSSIBLE CORROSION BETWEEN STA 726/RIB 8 AND STA 837 RIB 12 OF PYLON NR 2. REPAIRED NR 2 PYLON LOWER SPAR PER AIRBUS DRAWING 41R54610300, REFER EADS NR 141-15082 AND LOG PAGE 358326 ITEM 1M & 2M.SDR QXEA200301402Frame · damagedPDX- NR 2 NACELLE MID FRAME ASSEMBLY HAS FRETTING DAMAGE ON RIGHT AND LEFT SIDES. REPAIRED IAW HORIZON AIR EA 6-54-278.SDR QXEA200301401Frame · damagedPDX- NR 2 NACELLE FORWARD FRAME ASSEMBLY HAS FRETTING DAMAGE ON RIGHT AND LEFT SIDES. REPAIRED IAW HORIZON AIR EA 6-54-278.SDR C2XA03SH417Structure · chafedSHV- DURING C-CHECK THE LEFT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 145 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR QXEA200301312Frame · chafedPDX - NR 1 ENGINE FORWARD HORSE SHOCK MOUNT FRAME HAS CHAFED AREA AT ONE O'CLOCK POSITION ON AFT EDGE OF FRAME. REPAIRED IAW HORIZON AIR EA 6-54-275.SDR F3LA200300150Frame · crackedDURING C-5 CHECK, INSPECTION REPORTED AFT LOWER END OF NR 1 ENGINE PYLON AT STA. 363 CRACKED. REPLACED NR 1 ENGINE AFT LOWER END "A" FRAME IAW SRM 51-40-02.SDR C2XA03SH399Rib · dentedDURING C-CHECK THE NR 1 ENGINE LOWER COWLING AFT RIB WAS FOUND TO BE DENTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 54-10-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR UPS03441501Frame · crackedINSPECTION TYPE: C, NR 3 PYLON NACELLE REAR ENGINE MOUNT BULKHEAD FRAME CRACK IS FOUND AT FWD AND REAR O/B SIDE. FOUR EACH MOUNTING FRAME REPAIRED AS PER RS R54-53-35086 AT NR 3 PYLON NACELLE REAR ENGINE MOUNT BULKHEAD AND UPS ENGINEERING FILE 747-54-20042.SDR AWXA200301261Rib · crackedDURING C-03 CHECK 2 EACH 1 INCH CRACKS WERE FOUND ON LOWER END OF RIB NR 14, ON NR 2 PYLON AT AFT FIXED FAIRING. MAINTENANCE REMOVED NR 14 RIB AT AFT FIXED FAIRING, NR 2 PYLON; RECEIVED A NEW REPLACEMENT RIB; INSTALLED NEW RIB IAW 54-54-11, PG. 4, FIG. 1.SDR AWXA200301260Rib · crackedDURING C-03 CHECK A 1.1250 INCH CRACK WAS FOUND LOWER END OF RIB NR 13 ON NR 2 PYLON AT AFT FIXED FAIRING. MAINTENANCE REMOVED NR 13 RIB AT AFT FIXED FAIRING, NR 2 PYLON; FABRICATED A NEW REPLACEMENT RIB IAW DWG D54530034200; INSTALLED REPAIR PART IAW 54-5SDR 0302039153Rib · crackedDURING L-CHECK FOUND CRACK IN PYLON CLOSING RIB AT STATION YN 165 LT. REPAIRED PER EA 91-196348.SDR C2XA03SH345Rib · chafedSHV-DURING C CHECK A NR 1 ENGINE LOWER COWLING INBOARD RIB 8 INCHES FORWARD OF AFT RIB WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH344Rib · chafedDURING C CHECK MAINTENANCE FOUND THE NR 1 LOWER ENGINE COWLING CENTER RIB TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 51-21-04 AND 51-21-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR AWXA200301107Rib · crackedMCN - MAJOR REPAIR - DURING C-07 CHECK A .25 INCH CRACK WAS FOUND ON NR 1 ENGINE PYLON AFT FIXED FAIRING RIB 13. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE PYLON AFT FIXED FAIRING RIB IAW A320 SRM 51-42-11 PG 21-22 FIG 8, AND SRM 51-42-11 PG 7-12 FIG 2 SDR AWXA200301101Angle · crackedDURING C-07 CHECK A 1.0625 INCH CRACK WAS FOUND ON NR 2 ENGINE PYLON INBOARD ANGLE AT RIB 7. MAINTENANCE CUTOUT CRACK ON NR 2 ENGINE PYLON INBOARD ANGLE AT RIB 7; FABRICATED A REPAIR SPLICE, FILLER AND SHIM; INSTALLED REPAIR PARTS IAW A320 SRM 54-52-12, PG. 2SDR ARWA20030908Spar Cap · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 4 PYLON LT LOWER SPAR CAP WITH CRACK STA YOP 251 BY ACCESS DOOR NR 411.SDR ARWA20030906Spar Cap · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 2 PYLON LT CENTER SPAR CAP WITH CRACK STA YIP 235.SDR QXEA200301065Stringer · chafedMIDDLE STRINGER ON UPPER DECK OF NR 2 ENGINE COWL IS CHAFED. REPAIRED IAW DHC-8 SRM 51-40-11.SDR SWIA200312487Door Frame · crackedLEFT GEAR, FORWARD OUTBOARD DOOR NACELLE FRAME CHANNEL DENTED AND CRACKED BY DOOR TENSIONER. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT GEAR, FORWARD OUTBOARD DOOR NACELLE FRAME CHANNEL BY DOOR TENSIONER WITH A SERVICEABLE UNIT IAW SRM 5SDR UPS03441266Frame · crackedINSPECTION TYPE:C NR 4 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT OB FORWARD FRAME WEB. FRAME WEBS REPLACED AND REPAIRED AS IAW RS R-54-53-35064 INSPECTIONS TO CONTINUE IAW UPS EO B747-5410-13908 ( UPS ENGINEERING FILE NR 747-54 -20040 RAISED).SDR UPS03441265Frame · crackedINSPECTION TYPE: C, NR 1 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT FWD FRAME WEB. DETAILS PLS REFER ATTACHED FIGURE. FRAME WEBS REPLACED AND REPAIRED AS IAW RS NR R-54-53-35064 INSPECTIONS TO CONTINUE PER UPS EO B747-5410-13908 ( UPS ENGINEERING FILE NR 7SDR ARWA20030907Spar Cap · damagedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 4 PYLON INTERIOR STA YOP 225 LT LOWER SPAR CAP WITH STACK, BY ACCESS DOOR NR 426.SDR 2003FA0000885Clamp · brokenON AIRCRAFT ENGINE TRUSS ADEL CLAMPS FROM 3 O'CLOCK POSITION TO 9 O'CLOCK ARE SEVERLY BRITTLE AND ARE BREAKING, AND CORRODING THE ASSEMBLY DUE TO THE HIGH HEAT BEING GENERATED FROM THE ENGINE.SDR AWXA200301007Rib · crackedDURING C-03 CHECK A 1.5 INCH CRACK WAS FOUND ON NR 1 PYLON LOWER AFT FIXED FAIRING RIB 14. MAINTENANCE REMOVED CRACKED NR 1 PYLON LOWER AFT FIXED FAIRING RIB; FABRICATED A NEW REPLACEMENT RIB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 7-12, 10, 12, ANDSDR C2XA03SH239Structure · chafedSHV DURING C-CHECK, THE RIGHT HAND LOWER COWLING AFT EDGE MEMBER WAS FOUND TO HAVE CHAFING MARKS. MAINTENANCE REMOVED AND REPLACED AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR DL76G030696Spar · crackedPYLON, NR 1 FWD UPPER SPAR WEB, POWER FEEDER CABLE CUTOUT CRACKS. TWO CRACKS WERE FOUND IN THE UPPER SPAR WEB FROM THE POWER FEEDER CUTOUT TO THE NUTPLATE ATTACH HOLES. ERA INSTALLED REPAIR DOUBLER AND FILLER PER S/B 767-54-0090._ERA 385462-14 REVISION ORIGISDR UPS03441098Frame · crackedINSPECTION TYPE: C, NR 2 PYLON REAR MOUNT BULKHEAD FOUND CRACKED AT FORWARD AND AFT FRAME WEB AT STA 221. NR 2 PYLON REAR MOUNT BULKHEAD REPAIRED PER HX RS R54-53-35045 AND UPS ENGINEERING FILE NUMBER 747-54-20039.
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