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 EIA2000354Frame · misdrilledEAC-MZJ - DURING C6 CHECK INSPECTION, FOUND MISDRILLED HOLES IN CIRCUMFERENTIAL FRAME ON NR 1 ENGINE LOWER COWLING. FABRICATED AND INSTALLED FREEZE PLUGS, REPAIR FILLER, ANGLES AND DOUBLER PER ECRA UNIT-71-150-2. (M)SDR 20001106SH049Frame · misdrilledMISDRILLED HOLES IN CIRCUMFERENTIAL FRAME ON NR 1 ENGINE, LOWER COWLING. (X)SDR CA000928034Cowling · separated(CAN) ITEM NR 1 P/N 745-4000-501 COWL LT ITEM NR 2 P/N 745-4000-502 COWL RT AFTER TAKE OFF NR 1 ENGINE LT AND RT FAN COWLING SEPARATED FROM AIRCRAFT. - LT SLATS 1, 2, 3 DAMAGED.- LT UPPER WING SURFACE DAMAGED.SDR DHL200072010CDoubler · brokenNR 2 ENGINE RT FWD COWL, T/E RAIN GUTTER AND DOUBLER BENT AND BROKEN. INSTALLED DOUBLER REPAIR PER 727 SRM 51-30-2, SIZE OF REPAIR 6 X 15 INCH.SDR 20001122SH004Link Rod · damagedVHHH - FLT EIA 208 - ON TAKEOFF, ATC REPORTED LOSS OF COWLING ON NR 4 ENGINE. ALL COCKPIT INDICATIONS NORMAL. DUMPED FUEL AND RETURNED TO HKG. FOUND OTBD CORE COWL AND LOWER HALF OF INBD CORE COWL MISSING. FOUND NR 4 ENGINE DAMAGED DUE TO COWL SEPARATION. SDR 20001122SH003Cowling · missingVHHH - FLT EIA 208 - ON TAKEOFF, ATC REPORTED LOSS OF COWLING ON NR 4 ENGINE. ALL COCKPIT INDICATIONS NORMAL. DUMPED FUEL AND RETURNED TO HKG. FOUND OTBD CORE COWL AND LOWER HALF OF INBD CORE COWL MISSING. FOUND NR 4 ENGINE DAMAGED DUE TO COWL SEPARATION. SDR 20001122SH002Cowl Door · missingVHHH - FLT EIA 208 - ON TAKEOFF, ATC REPORTED LOSS OF COWLING ON NR 4 ENGINE. ALL COCKPIT INDICATIONS NORMAL. DUMPED FUEL AND RETURNED TO HKG. FOUND OTBD CORE COWL AND LOWER HALF OF INBD CORE COWL MISSING. FOUND NR 4 ENGINE DAMAGED DUE TO COWL SEPARATION. SDR 20001122SH001Cowl Door · separatedVHHH - FLT EIA 208 - ON TAKEOFF, ATC REPORTED LOSS OF COWLING ON NR 4 ENGINE. ALL COCKPIT INDICATIONS NORMAL. DUMPED FUEL AND RETURNED TO HKG. FOUND OTBD CORE COWL AND LOWER HALF OF INBD CORE COWL MISSING. FOUND NR 4 ENGINE DAMAGED DUE TO COWL SEPARATION. SDR EIAA2000045Cowl Door · separatedVHHH - FLT EIA 208 - ON TAKEOFF, ATC REPORTED LOSS OF COWLING ON NR 4 ENGINE. ALL COCKPIT INDICATIONS NORMAL. DUMPED FUEL AND RETURNED TO HKG. FOUND OTBD CORE COWL AND LOWER HALF OF INBD CORE COWL MISSING. FOUND NR 4 ENGINE DAMAGED DUE TO COWL SEPARATION. SDR AU000795Cap · cracked(AUS) ENGINE COWL NOSE CAP CRACKED. CRACK LENGTH 100 M (4 INCHES). NOSE CAP HAD BEEN ILLEGALLY REPAIRED USING A FIRE EXTINGUISHER DATE PLATE, POP RIVETS AND LIQUID NAILS. UNAPPROVED REPAIR. (X)SDR RIVA0000027Nose Cowl · crackedPSM, CRACK AT NR 3 NOSE COWL AT 12 O''CLOCK POS AT NAC STA 77.5, 6 AFT OF COWL L/E. DAMAGE AREA WAS CUT OUT OF NOSE COWL AT NAC STA 77.5. THE REP PLATE WAS FAB FROM .050 2024T-3. DRILLED EXISTING (AND REPAIRED) HOLES ONTO REP PLATE. DEBURRED ALL EDGES ON NSDR RRXA003811Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO ENGINE INLET COWL AT 5:30 POSITION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW EO#00-196 WITH APPROVSDR MALA000530Door · crackedFOUND DURING C-CHECK, LT ENGINE COWL DOOR (P/N 727110-614) CRACKED LOWER RIB. MAINTENANCE CUT OUT DAMAGE, STOP DRILLED CRACKS ON 613 RIB. FABRICATED REPAIR DOUBLERS FROM 301 1/4HD, .032(614 RIB) & 301 1/4HD. 020(613 RIB), INSTALLED REPAIRS IAW SRM 51-40-21.SDR CALA0001209Panel · delaminatedINSPECTION FOUND NR 2 ENGINE NOSE COWL PANEL 363AL DELAMINATED. THE PANEL WAS REPLACED IAW MM 20-50-02.SDR MALA000508Skin · crackedFOUND DURING C-CHECK, RT I/B NACA SCOOP IS CRACKED AT AFT END. MAINTENANCE REMOVED DAMAGED AREA OF SCOOP, TREATED AREA WITH ALODINE 1200 IAW SRM 51-20-42, PRIMED AREA IAW SRM 51-20-43, REPAIRED DAMAGE IAW SAAB EO 72SDS2746.SDR 20001012SH023Angle · crackedFORWARD ANGLE ON LEFT NOSE CAP FOR INDUCTION AIR PLENUM ATTACHMENT CRACKED. (X)SDR MALA000505Skin · crackedFOUND DURING C-CHECK, LT O/B COWL DOOR NACA SCOOP IS CRACKED IN THE AFT CORNER. MAINTENANCE REMOVED DAMAGED AREA OF SCOOP IAW SRM 72SDS2746. TREATED AREA WITH ALODINE 1200 IAW SRM 51-20-42. REPAIRED DAMAGE.SDR 00FDEA00528Skin · crackedNR 1 ENGINE LT CORE COWL FWD SKIN FOUND CRACKED. *S/D* REMOVED AND REPLACED PER EA 1-7110-52071.SDR DHL200072146CCowling · damagedNR 1 INLET COWL AFT O/B FLANGE DAMAGED ABOVE AND BELOW O/B HORZ LATCH 8 TO 10 O''CLOCK. CUT OUT DAMAGED AREA AND REMOVED FASTENERS, FABRICATED ANGLES PER SRM 54-10-3. INSTALLED ANGLES PER SRM 54-10-3. TREATED AND PRIMED PER SRM 51-10-2. CLOSED ALL ACCESS PSDR 20001012SH022Angle · crackedFORWARD ANGLE ON LEFT NOSE CAP FOR INDUCTION AIR PLENUM ATTACHMENT CRACKED. (X)SDR MALA000491Intake Duct · crackedFOUND DURING C-CHECK, RT NACELLE OUTBOARD COWL DOOR NACA SCOOP IS CRACKED IN THE AFT CORNER. REFER TO CELSIUS TASK CARD 4524, W/O 18639 AND SAAB STATEMENT 72SDS2728. MAINTENANCE REMOVED CRACK ON RT NACELLE OUTBOARD COWL DOOR NACA SCOOP, REPAIRED.SDR MALA000488Duct · crackedFOUND DURING C-CHECK, LT ENGINE INBOARD COWL DOOR NACA DUCT IS CRACKED AT THE AFT CORNERS, REFER TO CELSIUS TASK CARD 4519, SAAB STATEMENT 72SDS2728. MAINTENANCE REMOVED CRACKS ON LT INBOARD COWL DOOR NACA SCOOP AFT CORNERS.SDR MALA000490Frame · chafedFOUND DURING C-CHECK, RT INBOARD NACELLE COWL DOOR FRAME IS CHAFED BELOW NACA SCOOP. REFER TO CELSIUS TASK CARD 4523, W/O18639. MAINTENANCE REMOVED CHAFED AREA IAW SRM 51-10-10, FABRICATED REINFORCEMENT ANGLE, INSTALLED.SDR MALA000489Duct · crackedFOUND DURING C-CHECK, RT NACELLE INBOARD COWL DOOR NACA DUCT IS CRACKED AT THE AFT CORNER. REFER TO CELSIUS TASK 4527, AND SAAB STATEMENT 72SDS2728. MAINTENANCE REMOVED CRACK ON RT NACELLE INBOARD CORNER DOOR NACA SCOOP AFT CORNER.SDR 00FDEA00461Strut · overheatedNR 1 ENG STRUT OVERHEAT LIGHT AT TAKEOFF ROTATION FOLLOWED RED TABS. *S/D* REMOVED AND REPLACED NR 1 STRUT LOOP. CK OK PER MM 26-14-001-2. NO LEAKS FOUND. OK FOR SERVICE.SDR VNAA0007002Cowl Door · openAFTER DEPARTURE, THE FLIGHT ATTENDANT NOTIFIED THE CREW THAT THE LEFT HAND ENGINE INBOARD COWLING WAS OPEN. FLIGHT 4083 RETURNED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND SECURED THE COWLING IN ACCORDANCE WITH DORNIER MAINTENANCE SDR F3LA00135Channel · damagedDEN - DURING C-7 CHECK INSPECTION, FOUND BOTTOM CHANNEL OF NR 2 ENGINE INBOARD COWL DAMAGED AT FORWARD END. MAINTENANCE REMOVED DAMAGED SECTINO OF LOWER CHANNEL AND FABRICATED REPLACEMENT CHANNEL PER SRM 51-30-2 AND 51-30-01. (M)SDR F3LA00131Cowl Door · damagedDEN - DURING C-7 CHECK, INSPECTION FOUND NR 2 ENGINE INBOARD COWL DAMAGED, EXTERNAL SURFACE, 32 INCHES FROM AFT END AND 12 INCHES FROM TOP. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED AND INSTALLED DOUBLER AND FILLER PER SRM 54-10-3. (M)SDR 20001017SH017Cowling · wornCATCHER/CREST COWLING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR CALA0000913Skin · delaminatedINSPECTION FOUND INTERNAL SURFACE OF NR 2 ENGINE LT TRANSLATING COWL DELAMINATED. THE LT TRANSLATING COWL WAS REMOVED AND REPLACED IAW MM 78-32-17.SDR MALA000415Cowl Door · crackedFOUND DURING C-CHECK, LT I/B COWL DOOR NACA SCOUP (DUCT) CRACKED AT THE AFT END. MAINTENANCE ROUTED OUT CRACK LOWER SIDE, STOP DRILLED UPPER SIDE. NO CRACKS NOTED PAST STOP DRILL IAW FFVNDT006. FABRICATED REPAIR DOUBLER IAW SAAB DOC 372SDS52603.SDR AWXA0000396Cowling · separatedAIR TURNBACK, EMERGENCY DECLARED ENGINE COWL. NR 1 ENGINE OUTBOARD FAN COWL DEPARTED AIRCRAFT. EVALUATION AND WORK IN PROGRESS SUPPLEMENTAL DATA FORTH COMING. RECOMENDATION: IMPLEMENT ONE OF THE LISTED FAN COWL DOOR LATCHING SYSTEM IMPROVEMENTS PER AIRBUS OSDR MALA000414Cowl Door · crackedFOUND DURING C-CHECK, RIGHT O/B COWL DOOR NACA SCOUP CRACKED ON THE AFT END. MAINTENANCE BLENDED OUT DAMAGE AREA SRM 51-10-10. NO CRACKS NOTED IAW FFUNDT006. FABRICATED REPAIR DOUBLERS REF: 72SDS23603.SDR MALA000392Cowling · crackedFOUND DURING C-CHECK, ENGINE COWLING 463CL IS CRACKED AT THE AFT LOWER FRAME. MAINTENANCE STOPPED DRILLED CRACK IAW SRM 51-70-03. FABRICATED REPAIR DOUBLER IAW SRM 54-20-10, INSTALLED DOUBLER IAW SRM 54-20-10.SDR F3LA00117Cowling · damagedDEN - DURING C-7 CHECK INSPECTION, FOUND NR 1 ENGINE OUTBOARD COWL HAD A CRACK FROM RIVET HOLE, BELOW NR 2 HINGE POINT. MAINTENANCE REMOVED DAMAGED SKIN AREA AND REPAIRED PER SRM 54-10-3. (M)SDR CA000801023Cowling · elongated(CAN) SAME PROBLEM AS WITH C-GAKN. COWLING IS FALLING OFF DUE TO STRUCTURALLY INADEQUATE FIREWALL.SDR DHL200070730CCowling · wornAT C CK; NR 2 ENGINE RT/AFT COWLING WORN AT LOWER SIDE OF NR 7 RIB. CUTOUT WORN AREA AT NR 2 ENGINE RT AFT COWLING AT RIB NR 7, 6 INCH X 1&1/8 INCH PER B727 SRM 51-30-2, FABRICATED AND INSTALLED DOUBLER REPAIR PER B727 SRM 54-10-3. REF: N/R 6142.SDR CALA0000765Cowl Door · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 1 ENGINE NOSE COWL EXHAUST OUTLET. THE OUTLET WAS REMOVED AND A NEW OUTLET WAS INSTALLED IAW SRM 51-30-7 AND 51-10-4.SDR DHL200070702CRivet · looseNR 1 ENG, LWR COWLING SHOWS 8 WORKING RIVETS AT LOWER MID AREA. CUT OUT DAMAGED AREA 13.5 IN X 2.5 IN PER SRM 54-10-3 FIG 5. CLEANED, ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PARTS PER SRM 54-10-3 FIG 5.SDR MALA000338Latch · unlatchedNR 2 ENGINE EXHAUST CONE LATCH CAME OPEN IN FLIGHT. MX FOUND LATCH NR 2 JET PIPE PARTIALLY DEPLOYED. ADJUSTED JET PIPE LATCHES. SECURITY CHECKS GOOD.SDR DL72S001020Cowling · wornAT HMV, THE NR 2 FIREWALL COWL LANDING WAS FOUND TO BE WORN. IT WAS REPAIRED PER MM 53-11-0 PG 801.SDR MALA000322Rib · chafedDURING C-CHECK, ENGINE COWL 453DR 2ND RIB FROM AFT IS CHAFED, REFER CELSIUS TASK CARD 4531.SDR MALA000321Frame · chafedFOUND DURING C-CHECK, AFT FRAME LEFT EXHAUST COWL 454 AT CHAFED RT 10:00 POSITION. REFER CELSIUS TASK CARD 4535.SDR DLM90000867Cowl Door · missingON ARRIVAL FOUND FWD REVERSER COWL DOOR MISSING. WILL RERIG PER NEW PROCESS WHEN APPROVED.SDR DL72K000827Angle · bentAT HMV THE NBR 2 ENG FWD RT COWL CONTACT ANGLE WAS BENT AT THE 5 O''CLOCK POS AT STA 1351. TRIMMED WORN CAP FLANGE, FABRICATED REPAIR ANGLE PER 53-11-0, VERIFIED 2024-T4 HARDNESS TEST, INSTALLED REPAIR PER 53-11-0.SDR DLM90000814Door · separatedON CLIMBOUT FROM SAN, NR 1 THRUST REVERSER PRESSURE RELIEF DOOR OPENED & DEPARTED AIRCRAFT STRIKING THE L/E OF THE LEFT HAND HORIZONTIAL STABLIZER DAMAGING IT AND THE ANTI ICE TUBE.SDR RRXA002018Cowl Door · damagedDURING A MAINTENANCE VISIT FOUND A LARGE SCRATCH AND CREASE ACROSS RT FWD COWL DOOR LWR SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-055 WITH APPROVED 8110-3 DSDR DHL200072626CCowling · brokenNR 1 ENG NOSE COWL AFT AREA APPROX 9 O''''CLOCK POSITION HAS A PIECE OF SKIN BROKEN. REMOVED EXISTING REPAIR PER SRM 51-30-2. FABRICATED AND INSTALLED NEW REPAIR PER SRM 51-10-2.SDR DHL200072621CSkin · crackedNR 1 ENG UPPER COWL I/B SIDE FWD LATCH AREA WORN SKIN CRACKED. REMOVED DOUBLER REPAIR AT NR 1 ENG UPPER COWL FWD LATCH AREA PER SRM 51-30-2. FABRICATED NEW DOUBLER REPAIR PER SRM 54-10-3 FIG 5. ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PER SRM SDR DHL200072620CSkin · crackedNR 1 ENG LOWER COWL EXT SKIN I/B SIDE FWD HINGE AREA CRACKED. REMOVED EXISTING REPAIR AND INSTALLED DOUBLER REPAIR PER SRM 54-10-3 FIG 5. ALODINED AND PRIMED PER SRM 51-10-7.
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