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 P5CA9600388Slot Seal · crackedCRACKED SKIN AT NR 1 ENGINE RIGHT SLOT SEAL FORWARD END. WELD REPAIRED PER BOEING SRM 51-10-01.SDR P5CA9600372Support Plate · crackedNR 2 ENGINE OUTBOARD CORE COWL, LOWER FORWARD CORNER SUPPORT PLATE IS CRACKED IN THE LIGHTENING HOLE. WELDED BRACKET AND REINSTALLED IAW SRM 51-30-02.SDR 96ZZZX4368Stud · loosePILOT REPORTED THAT COWLING STUDS WERE LOOSE WHEN FASTENED. INSPECTED AND FOUND ENGINE COWL STUDS TO BE TOO LONG. REMOVED AND INSTALLED NEW STUDS, P/N 50-007-15, AND GROMMET, P/N 50-009-2 ( 5 EACH). TWO EACH P /N 50007A26 AND P/N 50007A22.SDR P5CA9600531Nose Cowl · dentedDENT IN NR 4 ENGINE NOSE COWL 9 O'CLOCK POSITION. REPAIRED PER BOEING SRM 51-40-06 PARA 2L.SDR P5CA9600523Panel · debondedDEBONDED PANEL NR 4 ENGINE NOSE COWL 6 O'CLOCK POSITION. REPAIRED PER BOEING SRM 54-30-03 FIG 28.SDR P5CA9600521Nose Cowl · debondedDEBONDED PANEL NR 1 ENGINE NOSE COWL TOP PANEL 12 O'CLOCK POSITION. REPAIRED PANEL PER BOEING SRM 54-30-03.SDR P5CA9600517Nose Cowl · dentedDENT IN NR 1 ENGINE NOSE COWL 7 O'CLOCK POSITION. METAL FILLER REPAIRED AS PER BOEING SRM 51-40-06 PARA 2L.SDR UPS96220932Engine Ring · corrodedINSPECTION TYPE-C, STA 1352 ENGINE RING CORRODED. REMOVED AND REPLACED (P/N 65-23687-23) IAW SRM 51-30-02.SDR P5CA9600343Cowl · crackedNR 3 LEFT FAN COWL LOWER EDGE IS CRACKED BETWEEN THE AFT AND MIDDLE U-BOLTS. REPAIRED CRACK PER BOEING SRM 51-40-06.SDR P5CA9600341Channel · bentNR 1 ENGINE OUTBOARD CORE COWL LOWER EDGE CHANNEL VERY BENT, WITH PULLED RIVETS AND LOST DOUBLERS. REMOVED FABRICATED AND INSTALLED CHANNEL PER BOEING SRM 51-40-03.SDR P5CA9600332Cowl · tornNR 4 ENGINE CORE COWL FRONT LATCH AREA TORN AND DEFORMED. REMOVED, FABRICATED AND INSTALLED U-CHANNEL PER BOEING SRM 51-30-02 AND 51-10-01.SDR 97FDEA01207Stiffener · crackedSNRM NR 4225 NR 2 ENGINE NOSE COWL BLKHD STIFFENER ON D-DUCT WEB CRACKED 10:00 POS AS SEEN THROUGH PANEL 361 KL. REMOVED STIFFENER, WELDED CRACK AND REINSTALLED STIFFENER PER SRM 57-00-00, CLOSED 7/11/96.SDR P5CA9600351Channel · crackedNR 3 INBOARD CORE COWL LOWER EDGE CHANNEL CRACKED AND BENT. REMOVED CHANNEL, FABRICATED CHANNEL AND SPLICE AND INSTALLED IAW SRM 51-40-03.SDR P5CA9600324Frame · crackedNR 2 ENGINE INBOARD CORE COWL LOWER FRAME CRACKED AND TORN AT NR 5 LATCH U-BOLT, GUIDE PIN PUSHED BACK. REMOVED AND REPLACED SECTION OF FRAME IAW SRM 51-10-01 AND 51-10-02.SDR P5CA9600267Skin · crackedNR 4 OUTBOARD CORE COWL TOP AFT INSIDE SKIN CRACKED DUE TO EXCESSIVE HEAT. INSTALLED REPAIR DOUBLER IAW SRM 54-30-02.SDR PLGA9606192Cowl Door · not latchedPIT - FLT 4382 - AFTER TAKEOFF FROM PIT, THE RIGHT ENGINE FWD OUTBOARD COWLING DOOR OPENED. THE AIRCRAFT RETURNED TO PIT, LANDING WITHOUT INCIDENT. THE COWLING WAS TEMPORARILY REPAIRED AND THE AIRCRAFT THEN FERRIED TO PSM FOR PERMANENT REPAIR. (M)SDR 97ZZZX660Latch · wornHIGH PROFILE COWL LATCH WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR UPS96220559Lining · wear damageINSPECTION TYPE-C, DAMAGE TO ATTENUATION LINING ON NR 2 ENGINE (S/N 81058). REPAIRED IAW UPS EO TAY 7230-8339-A.SDR CA960625016Air Scoop · missing(CAN) CAPTAIN REPORTED THAT THE RIGHT NACELLE, ZONE 2, LEFT INBOARD JETPIPE COWLING AIR SCOOP WAS MISSING. JETSTREAM ISSUED A TECHNICAL/OPERATIONAL RESPONSE ALLOWING AIRCRAFT TO REMAIN IN SERVICE FOR SEVEN DAYS.SDR P5CA9600295Skin · puncturedFOUND NR 1 OUTBOARD MAIN COWL SKIN PUNCTURED BETWEEN FIRST AND SECOND RIB. REPAIRED COWLING IAW SRM 54-30-03.SDR P5CA9600294Bracket · crackedFOUND NR 1 INBOARD ENGINE COWLING LOWER FORWARD CORNER INSIDE BRACKETS AT FORWARD FRAME STIFFENER CRACKED AND DAMAGED. REPAIRED CORNER BRACKETS AND FRAME STIFFENER IAW SRM 54-14-03.SDR P5CA9600293Chafe Strip · crackedFOUND NR 1 INBOARD COWLING LOWER AFT CORNER (INSIDE) HAS CHAFE STRIP CRACKED. REMOVED AND REPLACED CHAFE STRIP IAW SRM 51-10-01 AND SRM 51-30-02.SDR P5CA9600292Angle · crackedFOUND CRACKED BRACKET AND DAMAGED PIN AREA AT NR 1 INBOARD COWLING LOWER INSIDE CORNER AT ALIGN PIN. REPAIRED CRACKED ANGLE IAW SRM 51-40-04.SDR 97ZZZX659Latch · seizedLOW PROFILE COWL LATCH SEIZED. WILL NOT MOVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR P5CA9600237Nose Cowl · crackedFOUND NR 3 ENGINE NOSE COWL DENTED AND CRACKED AT THE 8 O'CLOCK POSITION. POTTED DENT, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-40-06.SDR P5CA9600270Core Cowl · crackedFOUND OLD REPAIR CRACKED AND BROKEN ON NR 1 ENGINE OUTBOARD CORE COWL, AFT TOP END. REMOVED OLD REPAIR, FABRICATED AND INSTALLED NEW REPAIR IAW SRM 51-30-02.SDR P5CA9600272Flange · crackedFOUND NR 2 ENGINE INBOARD CORE COWL MATING FLANGE ON T/R TRAILING EDGE CRACKED AND WORN. REMOVED AND REPLACED FLANGE IAW SRM 51-10-01.SDR AALA960834Nose Cowl · crackedSAT - DURING ROUTINE MAINTENANCE, FOUND A CRACK AT THE 6 O'CLOCK POSITION ON THE LEFT ENGINE NOSE COWL. CRACK IS LOCATED 1.5 INCHES AFT OF NOSE COWL LIP SEAM AND ABOUT 3 INCHES OUTBOARD OF NOSE COWL INSPECTION PANEL. APPLIED SPEED TAPE TO DAMAGED AREA, APPROSDR 97ZZZX674Latch · wornHIGH PROFILE COWL LATCH WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM.SDR P5CA9600271Cowl · delaminatedFOUND NR 4 ENGINE OUTBOARD FAN COWL DELAMINATED AT 2 O'CLOCK POSITION. REMOVED AND REPLACED OUTBOARD FAN COWL IAW MM 71-11-04.SDR CA960604010Fairing · missing(CAN) ON ROUTINE INSPECTION, NR 1 ENGINE GAS GENERATOR FAIRING LOWER PORTION MISSING AND ADJACENT FAIRINGS DAMAGED.SDR 96ZZZX3018Support · crackedDURING 300-HOUR ENGINE INSPECTION, A 6.5 INCH HORIZONTAL CRACK WAS FOUND IN THE FAN COWL SUPPORT AT 3 O'CLOCK POSITION. ALSO, VARIOUS BRACKETRY ATTACHED TO COWL ASSY FOUND TO HAVE SMALL CRACKS.SDR AU960710Cowling · corroded(AUS) LH AND RH ENGINE TOP COWLS BADLY CORRODED AND CRACKED - LH ENGINEOIL DIPSTICK ACCESS DOOR TORN AND ALMOST SEPARATEDSDR CA960502054Cowling Latch · cracked(CAN) ON PREPARATION FOR PAINTING, THE FOUR COWLING LATCHES REMOVED. FORWARD R.H. LATCH CRACKED ACROSS THE ATTACH HOLES.SDR 96ZZZX3510Nose Cowl · crackedNR 1 ENGINE NOSE COWL, 5 O'CLOCK POSITION SKIN IS PULLED UP 0.10 INCH BY 3 INCHES LONG, 0.5 INCH FORWARD WITH A 0.15 INCH CRACK IN UPPER EDGE. STOP DRILLED CRACK PER SRM 51-10-6. INSTALLED DOUBLER PER SRM 54-30-3 AND SRM 51-10-2.SDR 96ZZZX2928Cowl · damagedAIRCRAFT DESCENDING TO MCO AT 13,000 FEET AND 250 KNOTS. ENTERED SCATTERED HAIL. NO FLAPS DOWN, NO LANDING GEAR DOWN. DAMAGE TO NR 2 ENGINE RING COWL, UPPER 180, LEADING EDGE DAMAGE AND ALL OLD REPAIRS TORN LOOSE, WINDOW SEAL TORN BACK, UPPER BEACON BROKE, SDR 96ZZZX2099Cowl · crackedFOUND 12 INCH CRACK ON NOSE COWL REAR FRAME TO BARREL ATTACH ANGLE AT ABOUT 10 O'CLOCK POSITION LOOKING FORWARD. SUBMITTER STATED CAUSE UNKNOWN. ENGINE VIBS WELL WITHIN LIMITS. NOSE COWL HAD EXTENSIVE REPAIRS.SDR CA960412004Latch Assy · broken hook(CAN) HOOK BROKEN WHEN LATCHING COWL AFTER CHECKING OIL. SKETCH SHOWS BREAK OCCURRING ON THE HOOK PORTION OF THE ASSEMBLY.SDR GLBA96056Cowl Latch · wornLAN - DURING CLIMB-OUT, CREW OBSERVED LEFT TOP COWL WAS DETACHED FROM INBOARD LATCHES (OUTBOARD LATCHES REMAINED LATCHED). CREW ELECTED AN AIR TURN BACK AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED INBOARD, AFT COWL LATCH AND RESECURED COWL. (M)SDR CAL960609Former · crackedMAN - INSPECTION FOUND THE NR 1 ENGINE NOSE COWL FORWARD FORMER CRACKED FROM APPROXIMATELY THE 11 O'CLOCK TO 2 O'CLOCK POSITIONS ALONG INNER SEATING ANGLE. THE CRACK WAS 26 INCHES LONG. A HOLE 2 INCHES IN DIAMETER WAS ALSO FOUND IN THE AREA. THE NOSE COWL WSDR AU960301Fairing · broken(AUS) RH ENGINE COWL HINGE ASSEMBLY BROKENSDR REXA96011Cowling · bentAFTER TAKEOFF RIGHT COWLING DOOR CAME OPEN IN FLIGHT, AIR RETURN. REMOVED AND REPLACED FORWARD AND AFT COWLINGS. (M)SDR 96FDEA00421Nose Cowl · dentedNR 1 ENG NOSE COWL LIP RING EXTERNAL SKIN HAS A DENT AT APPROX 9 O'CLOCK POSITION. REMOVED NR 1 ENG NOSE COWL AND SENT OUT FOR REPAIR. INSTALLED SERVICEABLE NR 1 ENG COWL IAW FEDEX MM 71-10-21.SDR USAASB96040Cowl Latch · not latchedPIT - FLT 421 - RIGHT ENGINE COWLING LATCH CAME OPEN IN-FLIGHT, ACFT RETURNED. MAINTENANCE SECURED RIGHT ENGINE UPPER COWLING LATCH, CHECKS NORMAL. CHECKED ALL OTHER COWLING LATCHES, CHECK GOOD. (X)SDR IXXA9622Cowling · crackedDURING THE D-CHECK INSPECTION, FOUND CRACK ON THE INBOARD COWL ON ENGINE. REPAIR WAS ACCOMPLISHED PER DRAWING CF-N820BX, 10/96 DATED 1/18/96. REPAIR WAS APPROVED ON FAA FORM 8110-3 DATED 1/25/96. (M)SDR 96ZZZX1106Bracket · elongated holeWHILE INSPECTING RIGHT COWL FLAP FOR EXCESSIVE PLAY, FOUND IMPROPER BOLT USED WHICH ELONGATED HOLES ON ATTACH BRACKETS. REPLACED BRACKETS WITH NEW AND REPLACED BOLTS WITH PROPER CLEVIS PINS AND WASHERS PER PARTS BOOK.SDR P5CA9600145Nose Cowl · delaminatedFOUND NR 1 ENGINE NOSE COWL INLET ACOUSTICAL PANEL AT THE 8 O'CLOCK POSITION IS DELAMINATING AT THE CORNER OF OUTER PANEL. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 54-30-03 AND 51-10-01.SDR AU960220Cowling · bird strike(AUS) RH ENGINE UPPER INTAKE COWL DAMAGED BY BIRDSTRIKESDR CAL960236Nose Cowl · crackedSTATION 31J - INSPECTION FOUND A 1.75 INCH CRACK AT RIVET OF NR 3 ENGINE NOSE COWL SKIN. THE CRACKED AREA OF SKIN WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 54-30-3, FIGURE 8 AND ECRA 5430-01377. (M)SDR COMA9610062Cowling · damagedRT ENGINE OUTBD COWLING DOOR OPENED IN FLIGHT. REPLACED COWLING AND REPAIRED SURROUNDING DAMAGE.
Back to JASC 7110