JASC 5100
Service difficulty reports · 4,244
Reports filed under 5100 · Standard Practices/Structures, 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 = '5100' 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 = '5100' 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 ASAA0954264None · noneOVERSPEED TO ACFT PAST MMO TEMPORARILY FOR 2 SECOND AT TOP OF DESCENT VNAV SPD DID NOT ENGAGE AS IT SHOULD ON THE COMMON VNAV PACKAGE. GROUNDED YES. CAPT REPORTED OVERSPEED OF APPROX 5KTS FOR 2 SEC. OVERSPEED WITHIN LIMITS PER MM 05-51-04 PARA G NO INSP REQ. SDR FDEA200901050037Line · looseNR1 PYLON LINES ARE LOOSE AT THE WING T/E. COMPLIED WITH E.A. 6-5730-123698. LEAK CHECKS GOOD IAW AMM 29-11-33-4. HYDRAULIC FIRE VALVES OPS CHECK GOOD IAW AMM 29-10-00-5.SDR HALA2008122700907Unknown · vibrationAIRFRAME VIBRATION ABOVE FL250 IN CLIMB AND LEVEL AT FL260. PERFORMED GENERAL VISUAL INSPECTION OF EXTERNAL AREAS OF AIRCRAFT. FLIGHT CONTROLS AND GEAR DOORS, FILLET PANELS ACCESS PANELS, NO DEFECTS NOTED OK FOR SERVICE.SDR ASOA200801722Unknown · damagedBIRDSTRIKE ON FINAL APPROACH, EMERGENCY DECLARED.SDR FDEA200812195229Stanchion · noneCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126252.SDR FDEA200812195228Stanchion · noneCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126251.SDR FDEA200812185221Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126245.SDR FDEA200812185220Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126246.SDR FDEA200812185218Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126248.SDR FDEA200812185217Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126249.SDR FDEA200812185216Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126250.SDR DXTA2008120903394Unknown · unknownAFTER LANDING GEAR RETRACTION 8-10 LOUD BANGS WERE HEARD & VIBRATIONS WERE FELT IN THE COCKPIT FLOOR.SDR OMKR2008-0003None · noneNEW ACFT FROM FACTORY. PERFORMED AD SEARCH DUE TO EXPORT REQUIREMENT DURING ANNUAL. FOUND NUMEROUS ADS SIGNED OFF AS COMPLIED WITH THAT WERE N/A TO ACFT. MANY LISTED PARTS THAT WERE SUPPOSEDLY CHANGED. CONTACTED CESSNA. WAS ASKED WHY WITH SO MANY NEW ACFTSDR OMKR2008-0002Unknown · unknownNEW AIRCRAFT FROM FACTORY. PERFORMED AD SEARCH DUE TO EXPORT REQUIREMENT DURING ANNUAL. FOUND CESSNA SUPPLIED AD LIST DID NOT MATCH LYCOMING SUPPLIED LIST, AND CESSNA HAD CHANGED 8 AD SIGN-OFFS FROM LYCOMING. CESSNA CONTACTED, AND SAID THEY HAD TO CHANGE LYSDR HALA2008112300870Unknown · vibrationATB - OUT OF 18000 MSL FELT VIBRATION IN AIRFRAME. FLT CONTROLS NO VIBRATION. CONTINUED TO 25 MSL THEN SLOWED IN INTENSITY. FL 320 STILL SLIGHT VIBRATION. RETURN TO LAS. INSPECTED AIRCRAFT PANELS, FOUND SECURED INSPECTED ALL DOOR SEAL AND PRESSURIZED TO 6SDR MALA080205Panel · damagedPANEL 193AL HAS COMPOSITE DAMAGE. REPAIRED IAW EO NR S51031.SDR 2008FA0000871Spar · crackedHAVE JUST HAD THE SPAR X-RAY ACCOMPLISHED IAW AD75-27-09 R2. UPON REVIEW OF THE X-RAYS IT WAS DETERMINED THAT THERE WAS A CRACK. IT SEEMS THIS CRACK OF A VERY SIMILAR ONE WAS PREVIOUSLY REPAIRED AND THAT REPAIR IS IN QUESTION AS WELL. (K)SDR 2008UALA05500Unknown · unknownLOSS OF FMGC1 & GPWS. RTFL.
SDR 2008UALA05482Unknown · unknownMECHANICAL PROBLEM INCURRED. FLIGHT DIVERTED.SDR FPI2008F00000Cable · brokenMFG SERVICE KIT PN SK210174, CABLE ASSY BROKE AT THREADED END AFTER THE STOP NUT SEVEN WEEKS AFTER INSTALLATION APPEARS THREAD WALL IS TOO THIN LEADING TO FATIGUE. (K)SDR 2008FA0000581Vernatherm · failedTHIS VERNATHERM HAD A SHAFT AND NUT ASSY THAT WAS SECURED WITH A ROLL PIN. THE SHAFT FAILED AT ROLLPIN. THE NUT, SHAFT PIECE AT ROLLPIN TRAVELED THRU THE OIL GALLY AND LODGED AT A FITTING. HIGH OIL TEMP ALERTED US TO THIS FAILURE, OIL PRESSURE WAS NORMAL.(KSDR GUU2008F00050Unknown · leakingDURING FLIGHT, STRONG FUEL ODOR IN CABIN, MADE PASSENGER SICK. REMOVED AND CLEANED OLD SEALANT AT SUSPECTED FUEL LEAK AREA AND RESEALED. NO LEAKS NOTED. (K)SDR VNAA0808005None · noneCREW REPORTED A BIRD STRIKE ABOVE THE WINDSHIELD ON TAKEOFF ROLL. CREW ELECTED TO ABORT THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS OR DAMAGE. ACFT WAS RELEASED FOR SERVICE. (S)SDR DXTA200808073218Unknown · unknownWHILE CRUISING AT FL 340, ENTERED VIS MOISTURE. RAT* WAS APPROX-10* AND THE SAT * -30* , TURNED ON ENG/ STAB HEAT AND WING ANTI-ICE. APPROX 5 MINUTES LATER, ACFT HAD SLOWED TO MACH .69 AND THE " ENGINE FAULT" RT, THEN LT CAS MESSAGES ILLUMINATED THESE MESDR SWIA200819918None · nonePOSSIBLE TAIL STIKE ON LANDING. (FLIGHT NR 4125) PERFORMED TAIL STRIKE INSPECTION IAW 32-71-00. NO DISCREPENCIES NOTED.SDR QXEA200800885Fastener · missingPDX C4 CHECK 2 MISSING FASTENERS AT BL 9R, FS281 AND FS283. INSTALLED FASTENERS IAW CRJ SRM 51-42-13.SDR 08FDEA03026None · noneMAIN CABIN EXISTING ANGLE REPAIR ON TEE FLOOR SUPPORT.SDR 08FDEA03013None · noneFWD CARGO COMPARTMENT STRUT SUPPORT BEAM NOT IN CONFIGURATION.SDR 08FDEA03012None · noneFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.SDR 08FDEA03011None · noneFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.SDR 08FDEA03010None · noneFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.SDR 08FDEA03009None · noneFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.SDR VNAA0807011None · noneCREW REPORTED A BIRD STRIKE ON NOSE OF AIRCRAFT. CREW ELECTED TO RETURN TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND INSPECTED AIRCRAFT. NO DAMAGE WAS NOTED AND AIRCRAFT WAS RELEASED TO SERVICE. (A) [NOT AN SDR]SDR 08FDEA02968None · noneFOUND AT SLAT NR 1 RIB 2A, PLUGGED HOLES, MOST LIKELY FROM PRODUCTION OF SLAT. REPAIR PERFORMED BY LEAVE IT AS IT IS AND TOPCOAT THE AREA IAW RAS/FOK/149/2008 ISS A, APPROVED BY EA 6-5742-120081.SDR 08FDEA02967None · noneFOUND OLD REPAIR AT SLAT NR 1 RT INBOARD ARM BASE, RIB 2 A, WITH REFENCE TO RAS/FOK/054/2004. REPAIR DEVIATES FROM RAS REPAIR RENEWED (SKIN INSERT ) IAW RAS/FOK/148/2008 ISS A, APPROVED BY EA 6-5742-120081.SDR VNAA0807009None · noneCREW REPORTED THE PDF SHOWED FLAPS EXTENDED TO 2 DEG UNCOMMANDED AT 30,000FT WITH NO AURAL WARNING AT CRUISE. THE CREW DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS. AIRCRAFT WAS RETURNED TO SERVICE. (SDR VNAA0807006None · noneCREW REPORTED A LOUD NOISE ON RT SIDE OF AIRCRAFT AND ELECTED TO RETURN TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE OXYGEN SERVICE DOOR LEFT OPEN. MAINTENANCE SECURED THE DOOR CLOSED. AIRCRAFT WAS RELEASED FOR SERVICE. (A)SDR 08FDEA02857None · noneFOUND OLD DOUBLER REPAIR ON LT KRUEGER FLAP INNER SKIN WITHOUT ANY OLD DOCUMENTATION. REPAIR PERFORMED BY REPLACEMENT OF KRUEGER FLAP IAW AMM 278711 PAGE 401.SDR VNAA0807004None · noneCREW REPORTED A COMMUNICATION DOOR LEFT OPEN. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. MAINTENANCE SECURED THE DOOR CLOSED. AIRCRAFT WAS RELEASED FOR SERVICE. (A)SDR ANC2008F00000Unknown · unknownPILOT REPORT 4274013-1: DURING SINGLE ENG TAXI WHILE APPLYING THRUST RT ENGINE STALLED THEN AFTER THE LT ENG WAS STARTED, IT ALSO STALLED LT ENG LIMITER COME ON AT THE EICAS. LT BVCU SHOWS CODE 07, IAW FIM 75-32-00 TABLE 102 GEN DEDICATED CONTROL UNIT "B" WASSDR VNAA0807003None · noneCREW REPORTED A GROUND POWER DOOR LEFT OPEN. CREW RETURNED TO HSV AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. MAINTENANCE SECURED THE DOOR CLOSED. AIRCRAFT WAS RELEASED FOR SERVICE. (A)SDR 08FDEA02813Unknown · unknownON CLIMB-OUT, L INR PUMPS HOWEVER, LFT INR ISOLATION VALVE WAS AMBER, NO FUEL WAS BEING BURNED. GRAVITY FED FUEL MANUALLY TO BALANCE. LANDED W/ 28.8 ON LT AND 24.8 ON RT. LANDED OVER MAX LANDING WT. 200 FPM DESCENT ON LANDING. LANDING WT 276.1 AND MAX LANDSDR KCS2008F00003None · noneAT ABOUT 2:52 A.M. EDT ON JULY 7, THE CARGO AIRCRAFT (N714CK), CRASHED SHORTLY AFTER TAKEOFF FROM EL DORADO INTERNATIONAL AIRPORT, BOGOTA, COLOMBIA. (A) [THIS IS AN ACCIDENT(AP)]SDR WRL2008F00003None · noneDURING 1C + 12A CHECK REQUIRED UPGRADE EXISTING REPAIR DOUBLER ON RT WING FIXED L/E UPPER SKIN AT WING STA XS 261. PERFORM EJ NR W2008A578-613 REV 00. REPAIR ON RT WING FIXED L/E UPPER SKIN AT XIS 261, COND CHECK NML AND JOB COMPLETED. (K)SDR VNA2008F00000None · noneCREW REPORTED MULTIPLE BIRD STRIKES ON TAKEOFF. MAINT INSPECTED AND FOUND NO DEFECTS. AC WAS RELEASED FOR SERVICE. (K)SDR 08FDEA02606None · noneFOUND OLD SPLICE REPAIR IN FWD CARGO COMPARTMENT AT UPPER FLANGE C 38.2 RT WITHOUT ANY OLD DOCUMENTATION. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10 AND DRAWING R537B1760.SDR 08FDEA02602None · noneFOUND OLD FILLER REPAIR ON CROSSBEAM C 57.2 LT BETWEEN Y-140 AND Y-1470 WITHOUT ANY OLD DOCUMENTATION. REPAIR PERFORMED IAW SRM 53-10-15 FIG 208.SDR 08FDEA02596None · noneFOUND OLD SPLICE REPAIR IN AFT CARGO COMPARTMENT AT C 63 LT, BETWEEN Y 805 AND Y 1470 WITHOUT ANY OLD DOCUMENTATION. NEW SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG.207SDR EHA2008F00001Chip Detector · activatedCHIP LIGHT ILLUMINATED, PILOT LANDED AIRCRAFT IMMEDIATELY. INSPECTION FOUND TINY SLIVER ON CHIP PLUG, NO FURTHER FINDINGS. FOLLOWED MANY PROCEDURES. NO FURTHER PORBLEMS NOTED. (K)SDR 08FDEA02492None · noneNR 2 PYLON REPAIR INSTALLED ON PRECOOLER WEB DOES NOT MEET REQUIREMENTS PER SRM. REMOVED THE ORIGINAL REPAIR PART PER SRM 51-40-21. DRILLED CRACK STOP HOLES (4.8MM) PER SRM 54-52-31. FABRICATED REPAIR PART PER SRM 54-52-31. DRILLED FASTENER HOLES TO THE RE
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