JASC 5350
Service difficulty reports · 6,124
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 05FDEA00536Fairing · misrepairedCOMPLY WITH AGING 9 - AGING INSPECTION, REPAIR AT TAIL CONE EXHAUST AREA (PLEASE EVALUATE). REPLACED THIS FAIRING IAW AMM 52-41-18.SDR ASAA0540031Frame · damagedPAE - RT AFT WING -TO-BODY FAIRING FORMER HOLES ELONGATED. REMOVED AND INSTALLED NEW T-ANGLE IAW SRM. (K)SDR 757BJ0011Drag Angle · wornWEAR ON THE VERTICAL LEG OF THE LEFT FIN ATTACH ANGLE (DRAG ANGLE) BETWEEN BS 1164 AND BS 1720. REPAIRED PER EA 53-319.SDR 05FDEA00093Fairing · missingON ARRIVAL FOUND AFT CARGO DOOR MOVABLE FAIRING MISSING FROM AIRCRAFT. INSTALLED AFT CARGO DOOR MOVABLE FAIRING PER 727-100 MM 52-33-00-4. OPS CHECK GOOD.SDR UPS05843787Fitting · crackedINSPECTION TYPE:C1, TAIL CONE ATTACH FITTING CRACKED ON L36, STA 1875. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-1-20D, 51-1-8, 51-3-0.SDR 04FDEA03489Frame · crackedFWD TAIL CONE AFT MOST FRAME CRACKED AT 2 PLACES ABOVE & BELOW THE RIGHT TOP LATCH KEEPER ASSY CUTOUT AREA. REPAIRED AS PER SRM 53-00-01 FIG 9 VOL 2.SDR 249TR0098Support Angle · crackedLEFT INBOARD SUPPORT ANGLE CRACKED UNDER FORWARD WING TO BODY FAIRING. REPAIRED PER EA 53-341.SDR 2005FA0000393Skin · crackedDURING AN ANNUAL INSPECTION OF THE AIRCRAFT THE NOSE CONE ASSY WAS FOUND TO HAVE A CRACK IN THE TOP SKIN. PROBABLE CAUSE OF CRACKING OF THE NOSE CONE ASSY IS UNKNOWN. THE NOSE CONE WAS REPAIRED AND AIRCRAFT RETURNED TO SERVICE. (SO09200503395) (K)SDR 2005FA0000392Skin · crackedDURING AN ANNUAL INSPECTION OF THE AIRCRAFT, THE NOSE CONE ASSY WAS FOUND TO HAVE A CRAK IN THE TOP SKIN. PROBABLE CAUSE OF CRACKING OF THE NOSE CONE ASSY IS UNKNOWN. THE NOSE CONE WAS REPAIRED AND AIRCAFT RETURNED TO SERVICE. (SO09200503394) (K)SDR 2005FA0000391Skin · crackedDURING AN ANNUAL INSPECTION OF THE AIRCRAFT THE NOSE CONE ASSY WAS FOUND TO HAVE A CRACK IN THE TOP SKIN. PROBABLE CAUSE OF CRACKING OF THE NOSE CONE ASSY IS UNKNOWN. THE NOSE CONE WAS REPAIRED AND AIRCRAFT RETURNED TO SERVICE. OF 3 AIRCRAFT INSPECTED, ALL SDR SWIA200414120Radome · damagedUPON ARRIVAL AT GATE, FIRST OFFICER NOTICED SMOKE COMING FROM NOSE (TRU) BAY. REPLACED RADOME ASSY.SDR ASAA0410564Skin · damagedPAE - SCRIBE MARKS AT RT FWD UPPER AND LOWER WING TO BODY FAIRING. REPAIRED IAW EA.SDR 04FDEA03131Strap · tornTORN RESTRAINING STRAP ON TAIL CONE RAMP AT U-BAR. REPLACED STRAP ON TAIL CONE RAMP AT RESTRAINING U-BAR IAW FEDEX EA 8-5352-83938. REFERENCE NON-ROUTINE N00859.SDR 04FDEA03130Frame · crackedCRACKED/TORN DOUBLER ON TAIL CONE FRAME AT STATION YN2164, LEFT HAND UPPER DOWER PIN AREA. REMOVED EXISTING DOUBLER AND INTERCOSTAL IAW MD10 SRM 51-35-01 VOL II. STOP DRILLED CRACK IAW MD10 SRM 53-30-00 VOL I. PERFORMED HFEC TO VERIFY CRACK ENDS AT STOP DRISDR ASAA0410530Skin · damagedPAE - SCRIBE MARKS IN EXTERNAL SKIN, AT WING TO BODY FAIRING. REPAIRED SKIN IAW EA.SDR ASAA0410518Skin · damagedPAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA.SDR ASAA0410517Skin · damagedPAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA.SDR ASAA0410516Skin · damagedPAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA.SDR ASAA0410515Skin · damagedPAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA.SDR 371PA0049Drag Angle · crackedDRAG ANGLE CRACKED ABOVE RT RAM AIR DOOR. REPAIRED IAW EA 53-250.SDR ASAA0480502Radome · out of alignmentOKC - C-CHECK, RADOME FAILED GAP CHECK BETWEEN AFT EDGE OF RADOME AND FUSELAGE SKIN, STEP 17 OF T/C 244530001. RADOME TO FUSELAGE GAP ACCEPTABLE IAW EA 5350-01156.SDR 04260416Seal · looseLOUD THUMPING SOUND ON CLIMBOUT. CAUSE WAS TOP FUSELAGE NR1 FAIRING SEAL LOOSE. REBONDED SEAL.SDR P5CA0401205Fairing · delaminatedWING TO BODY FAIRING 1916L HAS DELAMINATION. CLEANED AREA & REBONDED.SDR 04FDEA02606Fairing · crackedSMIS 453 05-21 0003629 28JUN04 MC1 OPEN R WS-P 00026805 MOD TYPE H MOD NR C-CHECK REV NR PS ACCOMPLISH MAINTENANCE C-CHECK NR 002 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 28JUN04 19:47:42:3 BY:067708 S=M PLND: DATE:01AUG04 AT: LIS-VNSDR P9RA20040032Tail Cone · deployedAIRCRAFT IN MAINTENANCE-TOL. TAIL CONE WAS INADVERTENTLY DEPLOYED BY RAMP SERVICE PERSONNEL. REINSTALLED TAIL CONE IAW MM 535300. SFB MAINTENANCE ENTRY 8/27/2004. INSPECT TAIL CONE EVACUATION SLIDE FOR PROPER INSTALLATION. INSPECTED SLIDE IAW MM 256200. SDR CALA0400609Release Cable · out of rigTHE TAILCONE PULL CHECK FROM THE INTERIOR RELEASE HANDLE, FAILED. THE CABLES WERE ADJUSTED IAW MM 53-53-00.SDR P5CA0401148Panel · corrodedFUSELAGE PANEL 191OA, BOTH HAVE HEAVY CORROSION. REMOVED 2 EA SPLICE PLATES IAW 51-30-01. FOUND TO BE OUT OF LIMIT, FABRICATED NEW PLATES PER BOEING DRAWING 65B3878.SDR P5CA0401147Panel · delaminatedPANEL NR 194 LR DELAMINATED IN SEVERAL PLACES. REMOVED DAMAGE & PREP PER SRM 51-40-15.SDR P5CA0401139Fairing · damagedDAMAGED TO WING TO BODY FAIRING PANEL 192RR. REMOVED DAMAGED AREA REPAIR PER SRM 51-40-15.SDR P5CA0401155Panel · delaminatedFUSELAGE FITTED PANEL 191WL HAS DELAMINATION ON EXTERIOR SIDE. REPAIRED PANEL 191WL PER SRM 51-40-15.SDR 0408001Skin · delaminatedDURING A-CHECK INSPECTION, FOUND TAIL CONE WITH AN APPROXIMATELY 8 INCH BY 7 INCH SECTION OF DELAMINATION.SDR P5CA0401156Panel · delaminatedFUSELAGE FITTER PANEL NR 192 EER HAS DENT & DELAMINATION. REMOVED & CLEANED DAMAGED AREA PER SRM 51-40-15, APPLIED CURVED FIBERGLASS REPAIR SRM 51-40-03.SDR P5CA0401157Panel · delaminatedFUSELAGE FITTING PANEL 192CO DELAMINATED ON INTERIOR SIDE. REPAIRED PER SRM 51-40-15.SDR GTIA040697Lanyard · misroutedFLL - INSPECT TAILCONE FOR PROPER INSTALLATION DUE OT PREVIOUS ITEM 262316-1. FOUND KEVLAR LANYARD IMPROPERLY ROUTED, RE-ROUTED TAILCONE KEVLAR LANYARD AND INSPECTED TAILCONE INSTALLATION. (M)SDR WLDA200486Skin · scratchedDURING 4C CHECK IN TPE, WHILE PERFORMING J/C D929720 FOUND DAMAGE ON EXTENDED TAIL CONE LEFT LOWER SKIN AT BS STA 2176. PERFORMED REPAIR TO THE EXTENDED TAIL CONE LEFT LOWER SKIN PER EGAT EI W2004A53B. CONDITION CHECK SATISFACTORY.SDR UPS04242973Fairing · delaminatedINSPECTION TYPE:C, VERTICAL STAB TIP FAIRING (TAIL CONE) DELAMINATED AT BOTTOM NEAR WEDGE. REPAIR CARRIED OUT IAW SRM 51-40-9 & 51-30-2.SDR 04FDEA02167Frame · crackedFORWARD TAIL CONE FORWARD FRAME CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II.SDR 04FDEA02169Skin · crackedFORWARD TAIL CONE RIGHT HAND FORWARD LOWER SKIN CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II.SDR USAA040438Fairing · crackedPIT - FOUND FAIRING COVER CRACKED 1 INCH, LEFT SIDE NUTTED FAIRING, NR 1 HINGE COVER. REMOVED CRACKED MATERIAL, INSTALLED DOUBLER PER EA 78848 AND SRM 51-60-00. (M)SDR 04FDEA02161Frame · crackedEMP - FORWARD TAIL CONE FRAME CRACKED.SDR 04FDEA02034Bracket · crackedTAIL CONE RIGHT FWD FRAME MIDDLE GUIDE PIN BRACKET IS CRACKED. REMOVED AND REPLACED GUIDE PIN BRACKET IAW SRM 51-31-01 & SRM 51-35-01 AT MAE.SDR MWEA040115Structure · oversizedDURING TAILCONE DROP TEST, AFT CABIN DOOR ARMING PIN WOULD NOT ENGAGE DUE TO PIN HITTING COVER ABOVE DOOR. TRIMMED SLOT LONGER.SDR SWIA200413532Radome · crackedTHE F/O SIDE WINDSHIELD CRACKED. REMOVED AND REPLACED F/O'S SIDE WINDSHIELD IAW CRJ MM 56-12-01. OPERATIONAL CHECK GOOD. P/N OFF 601R33033-12, S/N OFF 03099H1509.SDR 04FDEA01910Angle · wornFUSE TAIL CONE CENTER PLATFORM LT ANGLE SUPPORT WORN. REMOVED AND REPLACED ANGLE IAW SRM 51-31-01 AT MAE.SDR 04FDEA01909Guide · wornRIGHT TAIL CONE GUIDE CAM WORN. REMOVED AND REPLACED GUIDE IAW 51-33-01 AT MAE.SDR 04FDEA01898Guide · wornLEFT TAILCONE GUIDE CAM WORN. REMOVED AND REPLACED GUIDE IAW SRM 51-33-01 AT MAE.SDR 04FDEA01883Bracket · damagedBOTH LEFT AND RIGHT FWD SUPPORT PIN BRACKETS HAVE ELONGATED HOLES ON TAIL CONE WORK PLATFORM. REMOVED AND REPLACED BRACKETS IAW SRM 51-35-01 AT MAE.SDR IXXA060219SPanel · dentedDURING ROUTINE C-CHECK FOUND WING FILLET PANEL NUMBER 162C DENTED. REPLACED OUTER SKIN AND HONEYCOMB SECTION PER COOPESA EO COO-CMP-8-53-260-04 DATED 07/14/2004.SDR 04FDEA01655Panel · corrodedAFT FUSE LEFT SIDE BANANA PANEL HAS CORROSION. REMOVED AND REPLACED PANEL IAW SRM 51-31-01.SDR VNAA0406016Tail Cone · failedUPON LANDING AT GSO, IT WAS FOUND THAT THE APU ACCESS DOOR HAD OPENED IN FLIGHT. MAINTENANCE WAS SENT TO GSO AND REPLACED THE APU TAIL CONE ASSMEBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 53-00-00. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.
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