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 08FDEA00754Spar · crackedNR 2 PYLON AFT LOWER SPAR ANGLE IS CRACKED AT STA 999/RIB 19. REMOVED A54515241500 STAMPING TO ACCESS THE CRACKED ANGLE PER SRM 51-40- 21 PARA 5. REMOVED CRACKED A54515063204 ANGLE PER SRM 51-40-21; PARA 5 & 6. ORDERED AND RECEIVED NEW A54515063204 NAGLE. LSDR 08FDEA00753Frame · crackedNR 2 PYLON A-FRAME IS CRACKED AT STA 1115/RIB 21. REMOVED A5451675001 FLODED SHEET METAL SECTION & CRACKED A54521550100 TEE PER SRM 51-40-21 PARA 5. ORDERED & RECEIVED NEW A54521550100 TEE. LOCATED, DRILLED & DEBURRED FASTENER HOLES ON NEW TEE IAW SRM 51-40-4SDR 2008UALA01054Frame · wornWEAR WAS FOUND AT FRAME OF NR 1 STRUT AFT FAIRING SAF STA 362 (OUTBOARD SIDE).
SDR KCSA081202Frame · crackedNR 2 PYLON AFT ENGINE MOUNT BULKHEAD FWD O/B FRAME CRACKED 1.375 INCH LONG EXTENDING FROM FASTENER HOLE LOWER END OF CUTOUT NAC STA 221.9.SDR F3LA200800049Frame · crackedDURING C7 C CHECK AND LEAK CHECKING THE RIGHT PYLON, INSPECTION REPORTED A CRACKED FRAME ON THE TOP, RIGHT SIDE OF THE PYLON, JUST AFT OF THE PRE-COOLER. MAINTENANCE REPAIRED THE CRACK IN ACCORDANCE WITH THE REQUIREMENTS OF DRAWING D54630462, A319 SRM 54-52-1SDR F3LA200800050Frame · crackedDURING C7 C CHECK AND LEAK CHECKING OF THE LEFT PYLON, INSPECTION REPORTED A CRACKED FRAME ON THE TOP, LEFT SIDE OF THE PYLON, JUST AFT OF THE PRE-COOLER. MAINTENANCE REPAIRED THE CRACK IN ACCORDANCE WITH THE REQUIREMENTS OF DRAWING D54630462, A319 SRM 54-52-SDR S9BA20080005Frame · corrodedCPCP INSPECTION, LT NACELLE HOOPFRAME CORRODED. REMOVED AND REPLACED HOOP FRAME IAW SRM 57-30-00 PAGE 1 AND AC 43-13, PARA 4-57. AC GROUNDED, YES.SDR G60A200800023Rib · crackedFOUND LT PYLON PNL 437FL RIB CRACKED.SDR CA080212004Adapter · cracked(CAN) UPON COMPLIANCE WITH SB 6/540 (WING-FRONT SPAR ADAPTER ASSY (P/N C6WM1027-1) INSP FOR CRACKS) A CRACK WAS FOUND ON THE RT FRONT SPAR ADAPTER. REPLACED RT FRONT SPAR ADAPTER ASSY PN C6WM1027-1 WITH PN C6WM1027-3 IAW SB NO 61542. ALSO REPLACED WEB SUB ASSSDR FDKA200801045Frame · chafedTHE FOURTH RIB FROM THE FORWARD END OF THE RT LOWER COWLING IS CHAFED OUT OF LIMITS AT THE CENTER OF THE COWLING. THE DAMAGED FRAME HAS BEEN REPAIRED.SDR FDKA200801043Frame · chafedTHE AFT FRAME OF THE LT AND RT LOWER COWLING IS CHAFED OUT OF LIMITS. THE DAMAGED FRAME HAS BEEN REMOVED AND REPLACED.SDR QXEA200800149Frame · chafedPDX - C4 CHECK - THE OUTBOARD LOWER COWL ATTACH LUG ON THE RIGHT NACELLE FORWARD FRAME IS CHAFED. REPAIRED IAW -8 Q400 RD8/4-54-232 AND Q400 NDTM PT-6 51-00-01.SDR 07FDEA05096Longeron · crackedNR 1 ENG LWR COWL DOOR OB LONGERON IS CRACKED AT AFT HINGE CUT OUT. REMOVED, FABRICATED NEW INTERCOSTAL, SENT TO HEAT TREAT ON SNR NR N00829. TREATED AND PRIMED, COMPLETED INSTALLATION, REF SRM 51-30-2, 51-10-2 AND BAC DWG 65-19507.SDR FDKA200712439Rib · gougedTHE AFT FRAME ON THE RT UPPER ENGINE COWLING IS GOUGED OUT OF LIMITS. THE FRAME HAS BEEN REMOVED AND REPLACED.SDR HNAA0800078Frame · wornFRAME WORN OUT O/B SIDE OF LT NACELLE. REPLACED WORN OUT FRAME.SDR 07FDEA04845Frame · crackedDURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK) PYLON NR 3 FOUND INTERNAL SIDE FRAME BROKEN AND DEFORMED. REPLACED STRAP P/N AVB7123-3, ANGLE P/N AUB7123-5, ZEE P/N AUB7123-7, CLIP P/N AUB7124-2 FOR SRM 51-33-01 VOL II.SDR 07FDEA04746Spar Cap · crackedNR 2 PYLON LEFT UPPER SPAR CAP OF THE TAIL PYLON CRACKED. REPAIRED AS PER E.A. 1-5410-117046, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR DALA1161550674Spar · crackedNR 2 PYLON FWD UPPER SPAR CHORD CRACK REPAIRED IAW ERA 452272-14.SDR ABXR070397Spar · crackedRIGHT AFT PYLON SPAR WEB CRACKED FORWARD SIDE. REPAIRED CRACKED WEB IAW DC9 SRM 54-01.SDR KCSA071441Frame · corrodedNR 2 PYLON INBOARD REAR ENGINE MOUNT BULKHEAD FRAME IS CORRODED AROUND A FASTENER AT NAC STA 221.90.SDR UIEA200700421Frame · crackedNR 3 ENGINE RT CORE COWL FORWARD FRAME HAS A HOLE AND CRACK. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-20-01 FIG 4 AND SRM 51-40-03 FIG 1. ALSO, REFERENCE ATLAS AIR XEO NR 71-092807.SDR USAA920070907Spar · crackedMAJOR REPAIR - C-04 CHECK - NR 5989697, RIGHT PYLON OUTBOARD SPAR CRACKED, RIB 6. REPAIRED RIGHT PYLON OUTBOARD SPAR, RIB 6 IAW A320 SRM 54-52-12 FIGURE 203.SDR KCSA071400Frame · crackedNR 1 PYLON NAC STA 235 I/B FRAME CRACKED FWD OF ACCESS PANEL.SDR KCSA071396Spar · crackedNR 2 PYLON NAC STA 194 LOWER SPAR WEB CRACKED .75 INCH.SDR KCSA071394Flange · wornNR 2 PYLON LOWER AFT FLANGE WORN FROM PNUEMATIC DUCT ANTI-ROTATION CLIPS NAC STA 240.SDR 07FDEA04206Spar · corrodedFOUND AT LT PYLON SPAR RIB 18 AT PYLON TO WING FITTING CORROSION. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5440-70338 AND RAS 027276/007/2003.SDR WRLA2007092Spar · crackedDURING C-5 CHECK, FOUND CRACK FROM NR 3 PYLON LOWER SPAR LT SIDE BESIDE FAN AIR DUCT FEED THROUGH. REF NR 64879. 10-12-07 REPAIRED PER DC10 SRM VOL.1 54-20-00.SDR FDKA200709502Frame · chafedRT LOWER ENGINE COWLING AFT FRAME IS CHAFED BEYOND LIMITS. REMOVED AND REPLACED DAMAGED FRAME.SDR QXEA200701473Frame · damagedC5 PDX - NR 2 NACELLE, FRAME FITTING FOR FORWARD MAIN LANDING GEAR DOOR, AFT HINGE ARM SUPPORT RIB HAS ONE FASTENER HOLE BLOWN OUT. REPAIRED IAW SRM 51-40-11.SDR FDKA200709491Frame · chafedRT LOWER ENGINE COWLING, THIRD FRAME FROM THE AFT END, IS CHAFED OUT OF LIMITS. REPAIRED THE DAMAGE.SDR FDKA200709487Frame · chafedTHE AFT FRAME ON THE LOWER ENGINE COWLING IS CHAFED OUT OF LIMITS. REMOVED AND REPLACED DAMAGED FRAME.SDR F3LA200700212Support Angle · crackedDURING C4/S1 CHECK, INSPECTION REPORTED RT ENGINE PYLON SUPPORT ANGLE THAT ATTACHES PYLON PANELS 423DL AND 424CR AT RIB 5 CRACKED (AREA AROUND AFT SCREW HOLE). REMOVED AND FABRICATED REPLACEMENT SUPPORT ANGLE IAW SRM'S 54-52-12, P28, 51-31-00, P44,51-44-11, 5SDR KCSA071326Frame · crackedNR 4 PYLON I/B FRAME CRACKED APPROX 10 INCHES ABOVE LOWER SPAR AT NAC STA 236.SDR UPS07450581Rib · crackedINSPECTION TYPE:C NR 3 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O/B & I/B SIDE RIB ANGLE FOUND CRACKED (NAC STA 227.4) FWD SIDE (CRACK LENGTH .375 INCH & 1 INCH). NR 3 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT ENG SDR UPS07450580Rib · crackedINSPECTION TYPE:C NR 2 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O/B AND I/B SIDE RIB ANGLE FOUND CRACKED (NAC STA 277-4) FWD SIDE (CRACK LENGTH 1 INCH APPROX). NR 2 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O/B AND I/B SIDE RIB SDR UPS07450565Rib · crackedINSPECTION TYPE:C NR 1 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O/B SIDE RIB ANGLE FOUND CRACKED FWD SIDE, CRACK LENGTH 1" BY 1/2". NR 1 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O/B SIDE RIB ANGLE REPAIRED AS PER HX RS NR R54-51SDR UPS07450563Rib · crackedINSPECTION TYPE:C NR 1 PYLON DRY BAY UPPER LINK STRUT BEAM O/B SIDE ATTACHMENT RIB ANGLE FOUND CRACKED AS MARKED NAC STA 223 (AFT SIDE) , CRACK LENGTH 5/8" APPROX NR 1 PYLON DRY BAY UPPER LINK STRUT BEAM O/B SIDE ATTACHMENT RIB ANGLE REPAIRED AS PER HX RS NR RSDR TAMF20070008SFrame · damagedDURING INSPECTION OF C-CHECK (MFG TASK CARD 06-091-01-2) WAS FOUND CORE COWL P/N: 224-2301-541 S/N: 0217 WITH ELONGATED HOLE AT FRAME STA NAC 294 - CF6-80C2 ENGINE NR 2. DAMAGED AREA WILL BE REPAIRED IAW CV07-1678-01 AND EWO 767-54-015.SDR UPS07M50862Rib · crackedINSPECTION TYPE:C NR 1 ENG PYLON, (LT SIDE) AFT OF BULKHEAD 286, FWD LT & RT UPPER SUPPORT RIB FOUND CRACKED UPPER AREA APPROX .75 INCH AS MARKED. SUPPORT RIB CRACKED AREAS TRIM OUT PER EN1497-07. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK. 04 EA REPAIRSDR KCSA071253Frame · crackedNR 4 PYLON NAC STA 221 BULKHEAD O/B FRAME CRACKED.SDR KCSA071252Frame · crackedNR 4 PYLON NAC STA 221 BULKHEAD I/B FRAME CRACKED.SDR 07FDEA02552Rib · crackedLT AFT FUSELAGE UNDER REMOVED CENTER ENG SUPPORT EXT SKIN PANEL, TRIANGULAR RIB WEB IS CRACKED AT UPP IB CORNER ATTACHED TO OB SIDE OF VERT STAB SKIN BS 1360. (MKD) REMOVED RIB ASSEMBLY, DISASSEMBLED, FABRICATED AND HEAT TREATED NEW WEB, DRILLED UP NEW WEB, ASDR DJFA2007073Rib · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A RIB IN THE RT PYLON, CRACKED. THE RIB WAS CRACKED AT THE UPPER AND LOWER FLANGES. BOTH CRACKS WERE APPROX 2 INCHES LONG. THE RIB WAS REPLACED.SDR DJFA2007074Rib · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A RIB IN THE LT PYLON CRACKED. THE RIB WAS CRACKED AT THE UPPER AND LOWER FLANGES. BOTH CRACKS WERE APPROX. 2 INCHES LONG. THE RIB WAS REPLACED.SDR 07FDEA02407Frame · crackedNR 2 ENG FWD LT COWL FWD END LWR CORNER CLOSURE COVER ANGLE CRACKED AT OUTER RADIUS. REMOVED DAMAGED CLOSURE COVER ANGLE REF SRM 51-30-2. FABRICATED NEW CLOSURE COVER ANGLE REF SRM 51-30-2 AND DWG 65-19645-199 AND INSTALLED NEW PART REF SRM 51-30-2.SDR DHL2007803543Frame · wornNR 3 ENG T/R FIXED STRUCTURE AND FWD FRAME WORN STA YN 202.000 AT 5 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3- DATED 06-08-07, DWG NR AD42-78-110 REV IR DATED 05-30-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION SDR 07FDEA02104Frame · crackedPYLON NR 1 AT AFT T/E LOWER SECTION LOWER FARING INNER INNER (A)-FRAME UPPER AND LOWER PORTION SUPPORT HAS CRACK BETWEEN RIB 19 AND 20 AND VISIBLE THRU OPEN ACCESS NR 474CR AND LIGHTING HOLE REMOVED AND REPLACED A FRAME IAW SRM 51-40-21.SDR C2XA07TY028Rib · dentedLEFT LWR COWL DENTED. REMOVED AND REPLACED DAMAGED RIB IN CENTER SECTION OF COWL, RECON TOURED DENTS AT OIL SERVICE DOOR, FABRICATED AND INSTALLED EXTERNAL DOUBLER, ALODINED, PRIMED AND PAINTED IAW EC 5430-01059. AIRCRAFT STILL IN C-CHECK.SDR 2007UALA01708Fitting · damagedNR 1 PYLON AT NAC STA 201, INBOARD MID SPAR FITTING, LOWER TANG, FASTENER HOLE ELONGATED. MAJOR REPAIR ACCOMPLISHED: CLEANED UP DAMAGE. FABRICATED & INSTALLED A FREEZE PLUG.SDR ASAA0741704Shear Tie · crackedNR 2 ENGINE PYLON RIGHT SIDE END PANEL SUPPORT BRACKET IS CRACKED. BRACKET REPLACED WITH NEW PART.
Back to JASC 5411