JASC 7810
Service difficulty reports · 1,900
Reports filed under 7810 · Engine Collector/Tailpipe/Nozzle, 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 = '7810' 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 = '7810' 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 SWIA201439807Vane · looseRIGHT ACM EXHAUST DUCT HAS A LOOSE VANE. C-CHECK, REBONDED LOOSE VAIN IN RT ACM EXHAUST DUCT IAW REO.SDR REXA2014091300975Nozzle · gougedTASK CARD 900-26-440-100 NR 2 ENG EXHAUST NOZZLE PYLON INTERFACE GOUGED & NEEDS TYPICAL REPAIR. REPAIRED NR 2 ENG EXHAUST NOZZLE IAW SRM 54-13-00-201-006-A01.SDR CA140911004Bracket · broken(CAN) DURING ACCOMPLISHMENT OF ROUTINE TASKS DH4-000-05-410-302 (LT) AND DH4-000-05-420-302 (RT), BOTH THE LT AND RT EXHAUST TRUNION BRACKETS WERE FOUND BROKEN OFF OF THE JET PIPE. SEE ATTACHED PHOTOS. THESE TASKS ARE 4000 HOUR TASKSSDR A6WA201441943Bracket · crackedLEFT EXHAUST FAIRING STANDOFF BRACKET IS CRACKED.SDR QXEA2014090900747Bracket · brokenRT ENGINE FORWARD EXHAUST ASSY HAS A BROKEN BRACKET. TRIMMED AWAY CRACKED AND DAMAGE AREA IAW SRM 54-45-25, REPAIR-26, PROCEDURE 7, STEP A. C/W LPI ON REWORKED AREA REF NDTM PT1 51-00-08. NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR FILLER IAW SRM 54-SDR CA140724008Shroud · worn(CAN) DURING A ROUTINE MAINTENANCE INSPECTION, DAMAGE WAS FOUND ON THE INBD SIDE OF THE RT EXHAUST SHROUD. THE DAMAGE IS IN THE FORM OF A HOLE WORN THROUGH THE SHROUD. IT APPEARS THAT THE JET PIPE INSULATING BLANKET WAS WEARING AGAINST THE INSIDE OF THE SHROSDR A6WA201441838Plate · crackedRT ENG EXHAUST FAIRING ACCESS PANEL 446BB CUT OUT SUPPORT PLATE CRACKED.SDR A6WA201441847Doubler · crackedLEFT EXHAUST FAIRING LOWER MOUNT BOLT ACCESS CUT OUT DOUBLER CRACKED.SDR 9SUA201407180002Exhaust Duct · crackedTURBINE EXHAUST COWL ASSY CRACKED ON NR1 ENGINE. REMOVED TURBINE EXHAUST COWL ASSY, PN 35C4655-01, DUE TO CRACK. INSTALLED NEW TURBINE EXHAUST COWL ASSY, PN 35C4655-01. ALL WORK PERFORMED IAW MM PN 3072162, REV NR 11, DATED MAY 17, 2014. WORK PERFORMED BY SDR 2014FA0000492Clamp · failedFAILURE OF THE CLAMP AND OR EXHAUST GASKET WHICH CAUSED EXCESSIVE HEAT DAMAGE TO THE UPPER COWLING AND ASSOCIATED WIRING LOCATED IN THE VICINITY OF THE EXHAUST LEAK. THE OCCURANCE HAPPEDED DURING THE TAKEOFF AT FULL POWER SETTING OF 2700 RPM AND 35" MAP. GASSDR A6WA201441628Fairing · crackedLT TAIL PIPE FAIRING SECOND RING CRACKED ON INBD LOWER SIDE. REPAIRED LT TAIL PIPE FAIRING IAW CMM 78-11-00.SDR A6WA201441626Ring · crackedRT ENG EXHAUST FAIRING RIB RING CRACKED. REPAIRED RT ENG EXHAUST FAIRING FWD RIB RING IAW CMM 78-11-00.SDR A6WA201441581Stiffener · crackedRT EXHAUST FAIRING INNER STIFFENER AT XN214 IS CRACKED. REPAIRED STIFFENER IAW CMM 78-11-00 REPAIR NR SRS042.SDR A6WA201441585Doubler · cracked54600-4000-0030 RT EXHAUST FAIRING INBD MOUNT BOLT ACCESS PANEL CUT OUT LANDING DOUBLER IS CRACKED. R & R PANEL LANDING DOUBLER WITH SERVICEABLE PART IAW CMM 20-40-11 & 20-42-06.SDR SWIA201438034Exhaust Duct · crackedCRACK NOTED BY NDT IN UPPER FWD STIFFENER OF THE RT EXHAUST NOZZLE FAIRING. REPLACE STIFFENER. C-CHECK, R & R RT EXHAUST NOZZLE FAIRING UPPER FWD STIFFENER AND RESTORED FINISH IAW SRM.SDR HLXR2014FA0000370Heat Shield · departedFOUND IMPACT DAMAGE ON THE TAIL ROTOR BLADE DUE TO HEAT SHIELD DEPARTING AIRCRAFT. DURING INSPECTION, IT WAS DETERMINED THAT THE BLADE WAS CRACKED. INSTALLED, TRACKED AND BALANCED NEW BLADE. REPAIRED HEAT SHIELD.SDR CA140505017Exhaust Duct · broken(CAN) AFTER TOUCHDOWN PILOTS NOTICE ERRATIC ENGINE INDICATIONS. DURING THEIR COCKPIT MANAGEMENT THE STUDENT NOTICE SMOKE FROM THE COWLING. THE PILOTS NOTIFIED TOWER AND EVACUATED THE ACFT AT WHICH TIME THEY SAW FLAMES FROM THE BOTTOM COWLING. THE PORTABLE EXSDR CALA2014050690955Skin · crackedNR 2 ENG CHANGE, EXHAUST CONE SKIN HAS A CRACK EXCEEDING SIX INCHES AT THE 530 POSITION. REPLACED IAW MM-78-11-12- 400-010-A13.SDR CALA2014050690954Rivet · damagedRIVET HEAD MISSING INSIDE ENG 2 TAILPIPE AT APPROXIMATELY 1230 POSITION. R & R BAD RIVET IAW SRM 51-40 & CMM 78-11-11.SDR A6WA201441437Channel · crackedLEFT TAIL PIPE FAIRING FIRE LOOP CHANNEL IS CRACKED. R & R CRACKED CHANNEL WITH NEW SERVICEABLE CHANNEL IAW CMM 78-11-00-440-001-A01.SDR A6WA201441409Splice · crackedRIGHT EXHAUST NOZZLE SPLICE CRACKED. REMOVED CRACKED SPLICE & INSTALLED SERVICEABLE SPLICE IAW SRM 51-21-11, 51-40-11 & 51-42-06 SPLICE.SDR A6WA201441408Skin · puncturedRIGHT JET PIPE FAIRING OUTER SKIN NEAR UPPER INBD MOUNT IS PUNCTURED. REPAIRED DAMAGE AREA NEAR UPPER INBD MOUNT ACCESS PANEL IAW CMM 78-11-00 REPAIR SRS 062.SDR ASAA2014040807483Flange · crackedNR 2 ENGINE REAR FLANGE APPEARS TO BE CRACKED. ACFT GROUNDED. VERIFIED CRACKS WITH BOROSCOPE. R & R NR 2 ENG REAR FLANGE, REF AMM TASK 72-56-00-000-802-F00 AND TASK 78-11-02-000-801-F00, TASK 78-11-01-400-802-F00, TASK 78-11-01-000-802-F00 AND TASK 78-11-02SDR A6WA201441395Rib · crackedRIGHT ENG EXHAUST FAIRING INNER RIB CRACKED. R & R RIB AT XN214 PN 228-50181-849 IAW CMM 20-40-11 & 20-42-06.SDR A6WA201441419Ring · crackedRIGHT TAIL PIPE FAIRING SECOND RING CRACKED. REPAIRED SECOND RING IAW CMM 78-11-00.SDR ASOA2014041410345Skin · damagedSTANG FAIRING IS BROKEN 434BT. REMOVED OLD SKIN IAW SRM 51-42-13 & 51-42-06, LOCATED & DRILLED NEW SKIN IAW SRM 51-40-11. INSTALLED SKIN IAW SRM 51-42-06 & 51-42-13. RESTORED FINISH IAW SRM 51-25-06 & 51-25-01.SDR U2RA201403170002Liner · crackedON POST FLIGHT INSPECTION, FOUND CRACK ON NR 4 ENGINE EXHAUST NOZZLE INNER LINER AFT RING WELD AT 1 O'CLOCK POSITION.SDR U2RA201403170001Liner · crackedON POST FLIGHT INSPECTION, FOUND CRACK ON NR 2 ENGINE EXHAUST INNER LINER AFT RING WELD AT 7 O'CLOCK POSITION.SDR 9JNR20140307002Tailpipe · undersizeWHILE PERFORMING AD 2013-10-04 TO PREVENT POSSIBILITY OF AN IN-FLIGHT POWER PLANT FIRE DUE TO AN EXHAUST SYSTEM FAILURE ON N1188V A PA-31-350, THE RT ENGINE TURBO EXHAUST CLAMP FAILED THE VISUAL INSPECTION ON CLEARANCES. WHEN THE CLAMP WAS REPLACED WITH NEW CSDR CA140224026Duct · cracked(CAN) DURING A NON-SCHEDULED HOT SECTION INSPECTION, THE LARGE EXIT DUCT WAS FOUND CRACKED ALONG THE OUTER SEAM. THE TTSN OF THE LED IS 1073.8 HRS. THIS OPERATOR HAS HAD NUMEROUS PREVIOUS INSTANCES OF CRACKED LEDS.SDR CA140225007Riser · cracked(CAN) PILOTS REPORTED A STRONG SMELL OF EXHAUST IN THE COCKPIT. MAINTENANCE FOUND THAT THE NR 2 CYLINDER EXHAUST RISER WAS CRACKED .333 OF THE WAY AROUND THE FLANGE. THE NR 3 CYLINDER EXHAUST RISER WAS CRACKED COMPLETELY AND SEPARATED FORM THE FLANGE. THERE SDR A6WA201441085Plate · crackedLEFT EXHAUST FAIRING INBD NUTPLATE MOUNT PLATE CRACKED. R & R PN 228-50181-833 IAW CMM 20-42-06.SDR A6WA201441092Stiffener · crackedLEFT EXHAUST FAIRING STIFFENER IS CRACKED, 2ND FROM FRONT. REPAIRED STIFFENER IAW CMM 78-11-00-300-810-A01.SDR CA140116005Duct · cracked(CAN) DURING A HOT SECTION INSPECTION, THE LARGE EXIT DUCT WAS FOUND CRACKED ALONG THE OUTER SEAM. THE TTSN OF THE ENGINE AND LED IS 546.5 HOURS. THIS OPERATOR HAS HAD SEVERAL PREVIOUS INSTANCES OF CRACKED LED`S.SDR CALA2014010290009Tail Cone · crackedENG 2 EXHAUST TAIL CONE IS CRACKED AT FWD PORTION BETWEEN 2 & 5 O'CLOCK. APPROXIMATELY 7 TO 9 INCHES LONG. IAW AMM78-11-12 601 FOR EXHAUST CONE PCN 115-0004 ALLOWABLE DAMAGE LIMITS. REPORTED 9.0 INCH CRACK BETWEEN 2 & 5'0 CLK. IN ZONE 1, BEYOND ALLOWABLE LISDR CALA2014010290006Seal · unsecureLT SIDE OF BOTH ENGS CNA OUTER DUCT SEALS HANGING OUT. SECURED SEAL IAW AMM.SDR CALA2013121693727Seal · tornTHE NR 1 ENG INBD LOWER EXHAUST NOZZLE SEAL IS TORN. R & R SEAL, ACFT OK FOR SERVICE.SDR CALA2013121393676Cone · cracked8 INCH CRACK IN NR 2 ENG EXHAUST CONE ALONG A PREVIOUS WELD. REPLACED EXHAUST CONE.SDR CALA2013120993568Rivet · missingENG 1 EXHAUST TAIL CONE UPPER PYLON HAS NINE MISSING RIVETS, SEVEN 7 ON RT SIDE TWO ON LT SIDE.SDR CALA2013120993553Exhaust Duct · damagedAFT BURNER SECTION OF THE 2 ENG SEPARATING. IAW MT 78-005 DAMAGE IS IN C DUCT NOT HOT SECTION AT 3 O'CLOCK AS VIEWED FROM REAR IAW TEP 2 C 2. REMOVED DAMAGE 15 X 1 & TAPED, OK TO CONTINUE.SDR A6WA201311244438Mount Bracket · crackedLEFT ENG JET PIPE INBD & OTBD MOUNT NUTPLATE BRACKETS ARE CRACKED. R & R CRACKED NUTPLATE BRACKETS IAW CRJ 200 SRM 51-42-06.SDR A6WA201311204402Nut Plate · crackedRIGHT EXHAUST NOZZLE FAIRING ATTACH POINT NUTPLATE CLIP AT 6 O`CLOCK POSITION IS CRACKED. REMOVED UNSERVICEABLE NUTPLATE CLIP & REPLACED WITH A NEW SERVICEABLE ONE.SDR CALA2013111993052Cone · crackedNR 1 ENG EXHAUST CONE CRACKED. IAW MM 78-11-12-200-011-B FOR ALLOWABLE LIMITS. HAS MULTIPLE EXTENDING PASSED PREVIOUS STOP DRILLS HAVE CRACK EXCEEDING 6IN ZONE 1 REJECTING TAIL CONE. REPLACED TAIL CONE IAW MM.SDR A6WA201311074358Stiffener · gougedRIGHT EXHAUST FAIRING FWD UPPER STIFFENER IS GOUGED. R & R DAMAGED STIFFENER.SDR CALA2013110792723Rivet · missingTHREE RIVETS MISSING ENG 2 TAIL CONE LOWER VERTICAL SUPPORT UPPER FLARED SHEET METAL 2 ON LT, 1 ON RT. RIVETS MISSING AT 6 O’CLOCK POSITION LOWER STRUT FAIRING WILL REQUIRE RECHECK.SDR CALA2013110792728Tail Cone · crackedCRACK ON TOP OF RT ENG TAIL CONE. CRACK MEASURES 3.75" & RUNS LENGTHWISE ADJACENT TO PREVIOUS WELD. ACCEPTABLE AS IS WITHOUT REPAIR IAW V2500 SRM 54-40.SDR CALA2013110592671Rivet · missingENG 1 EXHAUST TAIL CONE LOWER FIXED VERTICAL FAIRING INBD SIDE MISSING ONE RIVET. REPLACED FASTENER WITH CR3524-5 FASTENER IAW MT 78-001.STEP O.2.SDR CA131101009Panel · detached(CAN) FOUND MISSING ACCESS PANEL OF THE EXHAUST NOZZLE, PN 228 & 8722, 50181 & 8722, 911 ACCESS PANEL FOUND IN ANOTHER TOWN ON THE RUNWAY.SDR R61A201310311112Structure · crackedDURING HEAVY CHECK, FOUND RT FWD JET PIPE LT MOUNTING PIN ATTACH STRUCTURE CRACKED. MX REMOVED AND WELDED IAW SRM 54-45-25.SDR TSAA20131031007Structure · crackedRT UPPER SHROUD CRACKED AT FWD CIRCUMFERENTIAL FLANGE BEYOND LIMITS. REPAIRED IAW REPAIR STATEMENT 340SDS034475.
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