JASC 2510
Service difficulty reports · 1,328
Reports filed under 2510 · Flight Compartment Equipment, 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 = '2510' 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 = '2510' 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 UPS08853594Inertia Reel · inoperativeINSPECTION TYPE:N/A F/E'S INERTIAL REEL INOP, (SWAPPED WITH 1ST OBSERVERS AND DEFERRED PER MEL). REMOVED AND REPLACED 1ST OBSERVERS SEAT IAW AMM 25-11-02-2. THIS CLEARS M386600.SDR 2008FA0000892Clevis Pin · missingCLEVIS PIN THAT SUPPORTS BACK OF PILOTS SEAT WORN OVER .2500 THRU. THIS PIN SLIDES IN A CURVED PORTION OF THE LOWER FRAME OF THE SEAT. PROBLEM PARTS ARE CLEVIS PINS THAT SUPPORT THE SEAT BACK ON NR (2), (BELLCRANK). THE BELLCRANK IS WELL WORN IN THE CURVED SDR 2008FA0000659Seat · failedREAR SEAT PN 7-1500 FAILED AT THE LT HINGE POINT. THE AN3 SERIES BOLT PULLED THRU THE HINGE LUGS WHICH ARE WELDED TO THE SEAT FRAME BOTTOM. THE RT HINGE HOLES SHOW ELONGATION, BUT REMAINED INTACT. THE AC WAS DOING SPIN TRAINING AT THE TIME OF THE INCIDENT. RECSDR ABXA080232Seat · defectiveCAPTAINS ELECTRICAL SEAT UNOP. FORE AND AFT, UP AND DOWN, SEAT LOCK RELEASED WHEN APPLYING BRAKES ALLOWING SEAT TO SLIDE AFT UNCONTROLLABLY. REPLACED CAPTAINS SEAT WITH SERVICEABLE UNIT. OPS CHECK OK. IAW B767 MM 25-11-02.SDR CA080819001Cable Assy · broken(CAN) ON AUGUST 14, 2008, PILOT REPORTED "PILOT SEAT DOESN`T MOVE BACK, COULD NOT GET OUT". INVESTIGATION BY MAINT FOUND THAT THE CABLE ASSEMBLY FOR THE PILOT SEAT SECONDARY SEAT STOP HAD FAILED PREVENTING THE INERTIAL REEL FROM RELEASING TO ALLOW THE SEAT TO SDR 2008FA0000584Seat Frame · crackedUPPER CHAIR BASE ASSY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. CHAIR WAS REPAIRED IAW STO-1042WI STRUCTURAL SEAT REPAIR. (K)SDR C2XA08IA145Control Panel · shortedFLIGHT 2885 - THE FLIGHT CREW REPORTED A BURNING SMELL EMANATING FROM THE FLIGHT DIRECTOR PANEL. THE PANEL WAS REPLACED. OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. (S)SDR C2XA08IA143Holder · odorHSV - FLIGHT 2990 THE CREW REPORTED SMOKE IN THE COCKPIT WITH THE SOURCE IN THE VICINITY OF THE STEER DISCONNECT TRIGGER. THE ACFT RETURNED TO HSV WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE CAPTAIN`S CHART HOLDER ON MEL, AND THE ACFT WAS APPROVSDR CA080618002Seat Frame · interference(CAN) DURING THE INSTALLATION OF VERTICAL REFERENCE SEAT KIT, IAW STC SH06-31, IT WAS DISCOVERED THAT THE CYCLIC FLIGHT CONTROL STICK IS INTERFERED WITH DUE TO THE SEAT NOW BEING POSITIONED FURTHER FWD AND ELEVATED BECAUSE OF THE KIT INSTALLATION. AN ELEVATIONSDR U2RA290LP024Trim Panel · looseSMOKE IN THE F/O'S AREA OF THE FLIGHT DECK. FLT CREW PERFORMED QRH CHECKLIST IMMEDIATE ITEMS AND LANDED AIRCRAFT AT YIP. FOUND LOOSE VINYL FROM GLARE SHIELD ON FLOOD LIGHT. SECURED VINYL AND REPLACED BULB. OPS CHECKS GOOD IAW J/S3200 MM 33-10-00.SDR MASA200800399Track · lack of lubeASH FLT 7117 IAD - CAE - FLT ATTENDANTS JUMP SEAT HARD TO STOW. MX INSPECTED SEAT, LUBED SEAT AND TRACKS AND CHECKED FOR PROPER OPERATION. SEAT OPERATES NORMALLY.SDR MASA200800364Track · dirtyASH FLT 2752 PHX- SBP - FA SEAT HARD TO OPEN AND CLOSE. MAINTENANCE CLEANED AND LUBED THE SEAT TRACKS, OPS NORMAL.SDR FDKA200804184Switch · shortedFDM 6169 RIC-MCO. ELECTRICAL BURN / SMOKE SMELL COMING FROM F/O'S CONTROL COLUMN (YOKE). MX INSPECTED AREA AND FOUND F/O'S YOKE CHART HOLDER SWITCH SHORTING OUT. MX REMOVED AND REPLACED CHART HOLDER.SDR MASA200800348Spring · brokenASH FLT 7230 ORD - CAE FORWARD FLIGHT ATTENDANT SEAT RETRACT SPRING BROKE. REMOVED AND REPLACED OUTBOARD SPRING, OPS NORMAL.SDR ABXA080139Seat · unlockedCAPTAIN'S SEAT BECAME UNLOCKED DURING ROTATION WHILE CAPTAIN WAS FLYING AND SLIDE TO REAR STOP. SEAT WAS VERIFIED LOCKED DURING PUSHBACK. INSPECTED CAPTAIN'S SEAT IN ALL LOCKING POSITIONS. NO DEFECTS FOUND. MOVED SEAT VIGOROUSLY IN ALL LOCKING POSITIONS ANSDR UPS08552018Shoulder Belt · tangledINSPECTION TYPE:N/A SHOULDER HARNESS INERTIA REEL AT CAPTAIN'S SEAT FAILED TO RETRACT. UNTANGLED SHOULDER STRAP GOING INTO INERTIA REEL. OPS CHECK GOOD.SDR P5CA0801555Seat Belt · missingAFTER PUSHBACK FLIGHT ENGINEER FOUND THE CROTCH SEATBELT MISSING FROM FIRST OBSERVER'S SEAT. AIRCRAFT CAME BACK TO GATE AND MAINTENANCE DEFERRED THE FIRST OBSERVER'S SEAT IAW MEL 25-23-1.SDR MASA200800300Jumpseat · lack of lubeASH FLT 2881 PHX - ELP. F/A JUMP SEAT HARD TO MOVE FROM AND TO STOW. MX LUBED THE F/A JUMP SEAT, OPS NORMAL.SDR CA080404009Cable · out of adjustFLIGHT CREW DISCREPANCY, PILOTS SEAT DOES NOT SLIDE BACK INTERMITTENTLY. SEAT REMOVED AND VISUALLY INSPECTED. REEL ASSEMBLY CABLE ADJUSTED AND SEAT FUNCTION TESTED WITH NO DEFECTS FOUND. SEVERAL AIRCRAFT IN OUR FLEET OF CESSNA 100 SERIES AIRCRAFT HAVE EXPERSDR MASA200800288Mechanism · lack of lubeASH FLT 7136 ORD-OVERNIGHT. F/A JUMP SEAT WAS DIFFICULT TO UNLATCH TO STOW. MX LUBED THE LATCH MECHANISM AND THE SEAT OP CHECKED GOOD.SDR CA080331002Cable Assy · cracked(CAN) DURING INSTALLATION OF SERVICE KIT SK210-175 - SECONDARY SEAT STOP, IT WAS FOUND THAT THE THREADS ON THE HOUSING FOR THE ADJUSTMENT CABLE WERE CRACKED. (TC NR 20080331002)SDR CA080314004Inertia Reel · binding(CAN) CO-PILOT SEAT SHOULDER HARNESS INERTIAL REEL CABLE FOUND BINDING AGAINST VERTICAL REFERENCE SEAT KIT - PLATE ASSY P/N AAL-292-031-001. FOUND TO BE COMMON PROBLEM WHEN CHECKED ON OTHER ACFT. WILL CONTACT MFG.SDR 2008FA0000235Screw · improper partMFG SB NR SEB07-3 TO CHECK THE LENGTH OF THE SCREWS IN ACCESS PLATE UNDER REAR SEAT. THE PLATE MAY HAVE HAD TOO LONG A SCREW INSTALLED WHICH COULD CAUSE A FAILURE OF THE LANDING GEAR TO OPERATE DOWN. THE SB LISTED THE PROPER SCREWS TO USE IN EACH HOLE IN THESDR MASA200800180Seat · malfunctionedASH 7409 HSV-IAD. CAPT REPORTS THE F/A SEAT WILL NOT RETRACT. CONTRACT MX WAS ABLE TO GET THE SEAT RETRACTED.SDR SWIA200819290Holder · shortedFLT 5879 - FIRST OFFICERS CHART HOLDER IS SHORTING OUT. TIGHTENED CHART HOLDER HARDWARE. OPS CHECK GOOD.
SDR C2XA08IA055Holder · shortedIAH - FLIGHT 2292 - THE CREW REPORTED THAT THE COCKPIT READING LIGHT CIRCUIT BREAKER POPPED ON CLIMBOUT WHEN THE CHART HOLDER WAS OPENED FOLLOWED BY A LITE SMELL OF SMOKE. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED SDR CA080214011Seat Back · broken(CAN) SEAT BACK FRAME BROKEN JUST ABOVE INSERT ON THE OTBD SIDE. NOTEWORTHY ITEM: THIS SEAT DID HAVE A STEAL BAR INSTALLED IAW AD 2007-05-10. WE DO NOT KNOW WHETHER THIS WAS A CONTRIBUTING CAUSE TO THE FAILURE.SDR SIMA200802102Holder · smokeON FLIGHT 4302, CREW REPORTED SHUTDOWN ENGINE AT THE GATE. A LITTLE BIT OF SMOKE WAS SEEN FROM UNDER THE F/O'S GLARE SHIELD. AIRCRAFT REMOVED FROM SERVICE. FOUND F/O`S CHART HOLDER SHORTING OUT AGAINST CHART ASSEMBLY CAUSING CIRCUIT BREAKER NR 2 COCKPIT REASDR DL757071653Power Cable · frayedF/O SEAT ELECTRICAL ARC AND SEAT UNPOWERED. PWR CORD FRAYED. REMOVED CORD. FWD TO MCO/PLAC MEL 25.11.01A. REPLACED PWR CORD ON F/O SEATS CKS GOOD MCO/PLAC REMOVED.SDR UPS07151269Seat · defectiveINSPECTION TYPE:N/A DURING TAKEOFF ROLL IN MIAMI, CAPTS SEAT UNLATCHED AND SLID TO REAR STOP. REJECTED TAKEOFF SPEED LESS THAN 50 KTS. REMOVED AND REPLACED CAPT'S SEAT ASSY IAW A300 MM 25-11-11-04-01.SDR UPS07851280Inertia Reel · sticksCAPTAIN'S LEFT SHOULDER HARNESS INERTIAL REEL IS STICKY. REMOVED AND REPLACED CAPTAIN'S INERTIA REEL. OPS CHECK GOOD.SDR MASA200700860Seat · wornASH FLT 7230 CAE-OVERNIGHT - CREW REPORTED FA SEAT COVER WORN AND WOULD NOT RETRACT. RECOVERED AND LUBED TRACKS.SDR CA071128018Cable · broken(CAN) COMPLIED WITH SB07-5 PILOT SECONDARY SEAT STOP INSTALLATION. THE AIRCRAFT LEFT OUR SHOP SERVICABLE AND IN COMPLIANCE WITH THE SB. BROUGHT IT IN THE NEXT DAY TO DO UNSCHEDULED MAINT. LOOKING OVER THE JOB FOR A SECOND TIME FOUND THE THREADED PLASTIC END SDR HNAA0700269Master Caution · unknownDURING CREW SWAP IN CLT, ARRIVING CREW FOUND A FISH ODOR IN COCKPIT AREA. MAINTENANCE CHECKED OVERHEAD PANELS IN COCKPIT. SLIGHT ODOR WAS NOTICED COMING FROM MASTER CAUTION PANEL. REMOVED AND REPLACED CAUTION PANEL AND OPS CHECKED GOOD PER AMM 33-12-01. SMESDR MASA200700792Track · dirtyASH FLT 7364 ORD - FA FWD JUMPSEAT WILL NOT AUTO STOW. MX REMOVED GRIM TRACKS AND DEBRIS FROM AREA, SEAT STOWED NORMALLY.SDR CA071113007Doubler · cracked(CAN) DOUBLER INSTALLED ON CRACKED SEAT PAN WEB IAW SB 5PC41000-MOD1, FOUND CRACKED. NEW DOUBLER PN 5PC41301-001 INSTALLED. (TC NR 20071113007)SDR 2007FA0000968Inertia Reel · severedPILOTS SHOULDER HARNESS INERTIA REEL LOCKED UP, UPON EXAMINATION THE METAL GUIDE WHICH SURROUNDS THE FABRIC AND GUIDES IT ONTO THE REEL, HAD RUBBED AGAINST THE CENTER SHAFT OF THE REEL ITSELF. THIS OVER TIME REDUCED THE DIAMETER OF THE SHAFT UNTIL IT FAILED.SDR CA070910004Buckle · disconnected(CAN) WHILE COMPLYING WITH COMPANY CAMPAIGN NOTICE 010-25-10-011 CREW SEAT BELT BUCKLE INSPECTION, (REFER TO FAA SAIB NM-06-29)INTERFERENCE BETWEEN THE COCKPIT SEATBELT BUCKLES AND THE CONTROL COLUMN WOULD UNLATCH THE SEATBELT BUCKLE WHEN THE YOKE WAS MOVED THSDR HNAA0700175Mechanism · lack of lubeDURING TAKEOFF ROLL, THE CAPTAINS SEAT BECAME DISLODGED AND FELL FROM THE TRACKS TO THE FLOOR. MTX LUBED VERTICAL ADJUSTMENT LOCK MECHANISM.SDR UIEA200700334Pan · crackedCOCKPIT 2ND OBSERVER SEAT PAN CRACKED. REPAIRED IAW BOEING MESSAGE NR 1-497681686-1.SDR CA070823003Lock · broken(CAN) RT SEAT LOCKING PIN SHEATH FOUND BROKEN AT THE SEAT LEG ATTACH POINT. THE LOCKING PIN WOULD RETRACT BUT NOT ENGAGE ON THAT SIDE. THE SEAT LOCK MECHANISM COMPRISES OF A SPRING LOADED HANDLE , WITH TWO CABLES ATTACHED AND TWO SHEATHS SECURED TO THE SEAT LESDR 07FDEA02832Motor · burnedUPON TAKING RUNWAY, FUMES NOTICED IN THE COCKPIT. TAXIED CLEAR BACK TO THE RAMP. FUMES INCREASED, DECLARED EMERGENCY, EVACUATED THE AIRCRAFT. UPON FURTHER INSPECTION, FOUND S/O'S SEAT CONTROL C/B POPPED, AND STRONG ODOR FROM SEAT MOTOR. UPON FURTHER INSPECSDR AALA20071467Mask · leakingANC INFLIGHT T169/08AUG - CREW FOUND OXYGEN TEST BUTTON STUCK. CREW OXYGEN BOTTLE HAS LOW PRESSURE. LANDED ANC WITHOUT INCIDENT. FOUND FIRST OBSERVER MASK LEAK. REPLACED FIRST OBSERVER MASK ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AC2A116707Seat Back · crackedSEAT BACK FRAME CRACKED.SDR QXEA200701150Lock Pin · dirtySEA - ON FLIGHT 2490, RETURNED TO FIELD CAPTAINS SEAT WILL NOT LOCK IN PLACE. MAINTENANCE CLEANED AND LUBED SEAT LOCKING PINS. OPERATIONAL CHECK GOOD, NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.SDR CA070711005Seat · cracked(CAN) DEFECT REPORTED IN THE JOURNEY LOG BOOK THAT RT SEAT WOULD NOT ADJUST. REMOVED SEAT, INSPECTED, AND FOUND THE SEAT BOTTOM FRAME CRACKED COMPLETELY IN (2) PIECES. AREA IS DIFFICULT TO INSPECT BECAUSE OF UPHOLSTERY INSTALLATION. LOWEST TIME IN THE FLEETSDR YENA2007038Printer · odorFLT 145, BUF-JFK, ELECTRICAL ODOR EMANATING FROM RMP2, ACP2, ATC AREA. FOUND EVIDENCE OF BURNING IN PRINTER PAPER. REMOVED & REPLACED PRINTER PER MM 31-35-22, OPS CHECK NORMAL. ALSO CHECKED RMP'S 1 & 2, ACP'S 1 & 2, ATC AREA, NO EVIDENCE OF BURNING IN THIS SDR 2007FA0000479Seat · crackedSEAT PAN WAS FOUND CRACKED AT THE FORWARD END OF PILOTS OB SEAT RAIL STIFFENER, APPROXIMATELY 1 NR LONG ACROSS SCREW HOLES. STIFFENER PN 0411546-1 WAS ALSO CRACKED AT CUTOUT FOR FUEL LINE. TOTAL AIRFRAME TIME UNKNOWN, BUT GREATER THAN 1300 HOURS. THESE CRACKS SDR SIMA200712704Holder · burnedCAPTAIN CHART HOLDER SMOKING ON POWER UP, SMOKE STOPPED AFTER HOLDER LIGHTS TURNED OFF. REMOVED AND REPLACED CHART HOLDER IAW EMB AMM 25-12-11. FUNCTIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.SDR CA070423006Seat · cracked(CAN) WHILE PERFORMING AD CF87-15R2 A CRACK WAS NOTED IN THE RADIUS OF THE MACHINED FORK AT THE LT FRONT LOCATION. THE FORK IS MADE OF RATHER THIN RECTANGULAR ALUMINUM TUBING AND IS SUBJECT TO SOME FLEXING AS OCCUPANTS ENTER OR EXIT THE AIRCRAFT. (TC NR 200704
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