JASC 7110
Service difficulty reports · 2,324
Reports filed under 7110 · Engine Cowling System, 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 = '7110' 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 = '7110' 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 HALA0800458Cowling · damagedNR 1 ENG I/B CORE COWL HAS VARIOUS DEFECTS ALONG THE BOTTOM STRUCTURE. BLENDED THE DAMAGED AREA IAW SRM 54-41-02, FIG 101.SDR 08FDEA01143Web · corrodedNR 1 ENGINE WEB APPEARS TO HAVE CORROSION JUST FWD OF THE HYD FILTER BOWLS. REPAIRED WEB IN REF TO EA 8-7220-118465 .SDR SIMA200807905Cowling · openON FLIGHT 4154, CREW REPORTED ENGINE VIBRATION IN CRUISE FLIGHT. PASSENGER REPORTED HEARING A LOUD BOOM NOISE FROM THE ENGINE IN FLIGHT. UPON LANDING IN ORD, THE TOWER REPORTED THAT EAGLE SHOULD CHECK THE NR 1 ENGINE DUE TO OBVIOUS DAMAGE AS SEEN DURING TAXISDR 08FDEA00967Acoustic Panel · brokenNR 1 ENGINE INTAKE BLACK SOUND SUPPRESSION FWD LIP IS BROKE AT THE 10:30 POSITION. REMOVED PANEL IAW MM 72-23-01. REPAIRED IAW MM 72-23-01. RESTORED FINISH IAW SRM 51-21-02 VOL II. REINSTALLED SUPPRESSION PANEL IAW AMM 72-23-00.SDR WRLA2008027Nose Cowl · debondedDURING C-CHECK INSPECTION NR 3 ENGINE NOSE COWL INNER BARREL COMPOSITE DISBONDED. REF EGAT NR U02006. REPAIRED NR 3 ENGINE INLET COWL DISBONDED AREA IAW ERA 087123.SDR HALA0800372Attach Bracket · gougedNR 2 ENGINE NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKET AT 2 O'CLOCK POSITION GOUGED. DAMAGE ON NOSE COWL AFT BULKHEAD INNER RING BLENDED IAW SRM 54-11-02/1A01, FIG. 101, DETAIL 111, WITHIN SRM LIMITS.SDR DHL2008752511Skin · crackedNR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1.SDR DHL2008749015Nose Cowl · dentedDURING C CHECK, NR 1 ENGINE NOSE COWL EXTERIOR SURFACE AT 9 O'CLOCK AFT TRAILING EDGE COWL TO COWL LIP FLANGE IS BENT, DENTED, AND METAL PIECE BROKEN OFF. CUT OUT DAMAGE AREA ON NR 1 ENGINE NOSE COWL AFT TRAILING EDGE DIMENSION CUT OUT 1.75 INCH BY .5 INCH IASDR DHL2008749016Nose Cowl · crackedDURING C CHECK, NR 1 ENGINE NOSE COWL EXTERIOR SURFACE AT 9 O'CLOCK AFT TRAILING EDGE IS BENT OUT AND 1" CRACK. CUT OUT DAMAGE AREA DIMENSION 2" BY .75" IAW SRM 51-10-1. FABRICATED NEW DOUBLER REPAIR IAW SRM 51-30-5 AND 54-30-2 FIG 1. ALODINED AND PRIMED RESDR CA080131003Latch · inoperative(CAN) THE LOWER FWD COWLING HOOK AND CAM ASSY FAILING TO LATCH WITH THE UPPER COWL ASSY WHEN INSTALLING THE COWLS ON THE ENGINE. IT IS POSSIBLE TO HAVE THE ALIGNMENT MARKS INDICATE A SUCCESSFUL LATCH WHEN IN FACT THE HOOK MAY HAVE MISSED THE CAM DURING ROTATIOSDR A6WA200840036Nose Cowl · wornLT ENGINE LOWER NOSE COWL (432AB) AFT CORNER WORN THIN.. (K)SDR A6WA200840034Nose Cowl · wornLT ENGINE UPPER NOSE COWL (432AT) AFT CORNER WORN THIN. REPLACED ON LT ENG UPPER NOSE COWL (432AT) AFT CORNER IAW CMM 71-14-01-300-814-A01. (K)SDR DHL2007873505Nose Cowl · wornNR 3 ENG NOSE COWL WORN BETWEEN STA YN 147.534 AND 156.534 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN AND SPLICE IAW SRM 71-5-2 FIG 2 SHEET 1, 2,SDR CA071218002Vane · debonded(CAN) ON THE RT ENGINE COWLING INTAKE DUCT THERE IS A VANE ASSY TO REDIRECT INTAKE AIRFOW. THE VANE ASSY WAS FOUND TO HAVE DEBONDED ITSELF FROM THE ATTACH BRACKETS. THE VANE WAS ALSO CRACKED COMPLETELY ALONG THE TRAILING EDGE AND A 4 INCH CRACK LOCATED ON THE SDR CA071205005Cowling · burned(CAN) DURING START, AN ENGINE COMPARTMENT FIRE WAS NOTED. DAMAGE IS EVIDENT TO COWLING, ENGINE AND ENGINE COMPARTMENT. MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071205005)SDR 14011NOV2907Stiffener · crackedENGINE COWLING STIFFENER CRACKED AT APPROX. STA. 4960, WL 1979, BL 510. THE CRACK RUNS COMPLETELY THROUGH THE STIFFENER IN THE AREA OF THE CUTOUT FOR THE OIL BREATHER TUBE INSTALLED ONTO THE ENGINE.SDR CA071126009Cowling · broken(CAN) UPON LANDING, DURING THE OPERATION OF NR1 THRUST REVERSER THE NR 1 ENGINE UPPER FAN COWL DEPARTED THE AC. THE PILOTS DID NOT NOTICE THAT THE COWLING WAS MISSING UNTIL THEY DID THEIR POST FLIGHT WALK-AROUND. THE COWLING WAS LATER FOUND BY AIRPORT OPERATISDR 100607N409CSCowling · departedDURING FLIGHT, THE RT ENGINE LOWER COWL SEPARATED FROM THE ENGINE. DAMAGE TO THE RT HORIZONTAL STABILIZER OCCURRED CAUSED BY IMPACT DAMAGE. CREW REPORTED FEELING A SLIGHT "BUMP" DURING THE FLIGHT, HOWEVER THERE WAS NO INDICATION OR ABNORMAL FLIGHT CHARACTERISTSDR CA070821006Intake · cracked(CAN) COWL ASSY LOWER FWD P/N 101-910024-1 WAS ONCE MODIFIED. (TC NR 20070821006)SDR CA070522001Spring · broken(CAN) COMING OUT OF A MAJOR INSPECTION WHERE THE EJECTION SPRING ON ALL THE COWLS (P/N 105-62648, 105-62664, 105-62643 AND 105-62663) WERE REPLACED, SEVERAL EJECTION SPRING P/N V40GT39-1-1AA WERE BREAKING IN TWO PIECES. THIS PROBLEM HAPPENED STATICALLY AND INSDR CA070506002Nose Cowl · damaged(CAN) DURING A SCHEDULED MAINTENANCE CHECK, AFTER FAN COWL RT REMOVAL, STRUCTURAL DAMAGE WAS OBSERVED ON THE INLET COWL BY THE CAPPED 14TH STAGE BLEED AIR DUCT. DAMAGE WAS OBSERVED ON THE REMOVED FAN COWL, SAME AREA, AS WELL. MAINTENANCE PROCEED TO REPLACE THSDR CA070509004Cowling · separated(CAN) ON DESCENT, THROUGH FL280, CREW FELT SLIGHT VIBRATION TO THE AIRCRAFT. FIRST OFFICER (FO) FELT A SLIGHT SHUDDER IN THE CABIN. ON ARRIVAL, IT WAS FOUND NR 1 LOWER ENGINE COWL HAD SEPARATED FROM THE AIRCRAFT. UPON MAINTENANCE INITIAL INSPECTION, IT WASSDR ASMF200704014Cowling · bird strikeDURING TRANSIT CHECK, A BIRD STRIKE WAS DETECTED IN THE LT ENGINE NOSE COWLING. A BIRD STRIKE INSPECTION WAS PERFORMED IAW MM 05-51-48, FOUNDING A DENT OUT OF LIMITS WITH 18 INCHES LENGTH X 8 INCHES WIDTH AND 2 INCHES DEPTH, SO AIRCRAFT WAS SENT TO THE HANGAR.SDR CA070405011Support · cracked(CAN) THE ORIGINAL PART WAS FOUND CRACKED AND WAS REPLACED LESS THAN 50 HOURS AGO. THE CRACKS ORIGINATE AT THE 4 O’CLOCK AND 8 O’CLOCK POSITIONS, AT THE END OF THE FLANGED SECTION OF THE SUPPORT. SUBMITTER SUSPECTS THAT THE PULSATING AIRFLOW FROM THE PROPELLERSDR QXEA200700479Hinge Bracket · damagedC4 PDX - 424AR RIGHT COWL DOOR HOLD OPEN ROD HINGE BRACKETS HAVE ELONGATED HOLES AT CLEVIS PIN. REPAIRED IAW SRM 51-40-11.SDR 2007FA0000287Rivet · corrodedOWNER BROUGHT COWLINGS IN FOR REPAIR BECAUSE THE THROUGH SKIN RIVETS WERE CORRODING AND SHEARING OFF AT THE MFG HEAD AS EXHIBITED BY BLISTERING PAINT AT THE RIVET LOCATIONS. INSPECTION REVEALED MOST OF THE AD TYPE RIVETS WERE SEVERELY CORRODED BECAUSE THE COWSDR A6WA200740084Cowling · departedTOP OF LT ENGINE COWLING DETACHED FROM ENGINE IN FLIGHT STRIKING VERTICAL AND HORIZONTAL STABILIZERS. REMOVED AND REPLACED UPPER NOSE COWL IAW AMM 71. (K)SDR CA070202001Cowling · damaged(CAN) AFTER TAKEOFF THE PILOTS NOTICED THAT THE TOP FRONT COWLING WAS LIFTING OFF AT THE REAR. THEY RETURNED TO THE FIELD AND DURING THE FLARE THE COWLING DEPARTED THE AIRCRAFT, STRIKING AND DAMAGING THE PROP REQUIRING ITS DISASSEMBLY AND RT WING DAMAGING THE SDR CA070202005Duct · missing(CAN) UPON ARRIVAL, MAINTENANCE NOTICED AN APPROXIMATELY 6 INCH HOLE IN NR 1 ENGINE COWL. FURTHER INVESTIGATION DETERMINED THE CAP ON THE 6TH STAGE SADDLE DUCT MISSING, LOCATED IN COWL. CAP INSTALLED AND SECURED IAW MM AND COWL REPAIRED. (TC NR 20070202005)SDR FDKA200701024Cowling · damagedFDM 6212 SYR-JFK (1824 PHX LCL). APPARENT ICE DAMAGE TO NR 2 INLET COWL FIBER GLASS IS TORN. MX CHANGED THE LOWER COWLING.SDR CA080110005Cowling · cracked(CAN) BACK WALL OF HEATED LIP ASSY FOUND CRACKED. DEFECT INTRODUCES HOT EXHAUST GASES INTO COWL ASSY, CONTAMINATING ENGINE INTAKE, CABIN PRESSURIZATION, ENGINE CONTROL, AIR. DEFECT CAUSES INCREASED CORROSION OF COWL ASSY. DEFECT IS DIFFICULT TO SEE UPON INSSDR QXEA200603228Latch · unsecureSEA - ON FLIGHT 2224, RETURNED TO GATE. ENGINE COWL NR 2 LATCH OPEN. MAINTENANCE SECURED LATCH. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR COMA0670207Inlet · dentedRIGHT ENGINE LOWER FAN COWL IS DENTED. REPAIRED RT LOWER COWL IAW REO 670-54-16-694.SDR WRLA2006097Door · missingDURING WALKAROUND FOUND MISSING PRESSURE RELIEF DOOR FROM NR 1 ENG LT HAND SIDE CORE COWL, DOOR HINGE DAMAGED AND COWLING SKIN CRACKED ABOUT .875 INCH FORWARD OF DOOR HINGE AREA; CHECKED WING FUSELAGE AND TAIL, NO DAMAGE NOTED. REPAIRED AS PE 14-121-379 BOEINSDR MWEA060209Nose Cowl · debondedDISBOND FOUND ON RIGHT ENGINE INNER NOSE COWL AT 6 O'CLOCK POSITION 19" AFT OF FORWARD EDGE.SDR MWEA060208Nose Cowl · debondedDEBONDED AREA FOUND ON RT ENGINE INNER NOSE COWL AT 6 O'CLOCK POSITION 11.5 AFT OF FORWARD EDGE.SDR MWEA060207Nose Cowl · debondedDISBOND FOUND ON RIGHT END INNER NOSE COWL AT 6 O'CLOCK POSITION 28.5" AFT OF FORWARD EDGE.SDR ABXA060233Door · missingNR 4 ENGINE RIGHT COWL DOOR BLOWOUT PANEL MISSING. REPLACED NR 4 ENGINE RIGHT COWL BLOWOUT PANEL AND DOOR FORWARD DOOR LATCH IAW DC8 MM 71-10 AND DC8 MM CHAPTER 20. OPS CHECKED GOOD.SDR QXEA200602071Cowl Door · openPDX FLIGHT 2149 COWL DOOR OPEN. MAINTENANCE CLOSED THE COWL DOOR. OPERATION CHECK GOOD, NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR PIDA06086Cowling · delaminatedNR 2 ENGINE FAN COWLING DELAMINATED. REPAIRED IAW EA 71-218.SDR PIDAO6O86Cowling · delaminatedNR 2 ENGINE FAN COWLING DELAMINATED. REPAIRED IAW EA 71-218.SDR MASA200601981Access Door · damagedASH 6185 ICT - NR 1 LWR FAN COWL ACCESS DOOR MISSING LOUVERS. MAINTENANCE REMOVED AND REPLACED NOSE DOOR PANEL AND ACCESS.SDR QXEA200601771Retainer · chafedPDX - C4 NR 2 ENGINE INTAKE SEAL RETAINER CHAFED ON RIGHT HAND SIDE. REPLACED INTAKE SEAL OUTBOARD RETAINER RING.SDR CA060619004Channel · cracked(CAN) THE P/N 109-910053-15 AND -16 COWL SUPPORT CHANNELS WERE FOUND CRACKED IN THE LOWER FLANGE AREA, AND SUBSEQUENTLY REPAIRED. MANY OF THE REPAIRS HAVE ALSO FAILED. IT APPEARS THAT A SUBSTANTIAL AMOUNT OF COWLING WEIGHT RESTS ON THESE CHANNELS. THE REPEAT DSDR TRAX200600360Skin · corrodedRANRC 168. RIGHT NOSE INLET HAS CORROSION DAMAGE ON COMPOSITE SKIN JUST AFT OF LIPSKIN.SDR HALA0600435Cowling · crackedAPPROX 3 INCH LONG CRACK ON LT UPPER COWL ATA FAN AIR OUTLET. REMOVED & REPLACED TOP COWL ASSY PER AMM71-12-01. P/N 715-4010-509, S/N ON 279001, OFF 247001.SDR CA060515001Panel · missing(CAN) DURING FLT NR 1 ENG NOSE COWL LWR ACCESS PNL DEPARTED AC (ACCESS PNL). FLIGHT EXPERIENCED A SLIGHT BUFFET DURING FLT. UPON LANDING, FLT CREW DISCOVERED NOSE COWL LWR ACCESS PNL WAS MISSING. DAMAGE TO TRANSLATING COWL, UPPER NOSE COWL ACCESS PNL, CAUSED SDR F3LA200600049Bracket · wornDURING C-4 CHECK, INSPECTION REPORTED NR 1 ENGINE IB FWD COWL BRACE BRACKET WORN INTO THE ENGINE CASE. INSTALLED NEW BRACKETS AND HARDWARE ON NR 1 ENGINE CASE FOR THE FAN COWL HOLD OPEN ROD PER EA A9-72R-11428 AND CREATED RW 0000808.SDR QXEA200601319Cowl Door · chafedYYC - C4 RIGHT NACELLE OUTBOARD COWL DOOR 424AR HAS CHAFING DAMAGE THROUGH THE BOTTOM EDGE CHANNEL. REPAIRED IAW RD8-71-0507 AND EA 2-71-302.SDR THMN4113SQ115Bracket · crackedRIGHT INBOARD ENGINE COWL AFT SEAL BRACKET CRACKED AT TOP SIDE. ACCOMPLISHED AIRWORTHY REPAIR IAW DASSAULT FALCON KET 20 SRM 54-20-43 AND SRM 51-10-22.
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