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 HEEA078289Cowling · corrodedENGINE COWL CORRODED.SDR COMA0260174Clip · brokenFLIGHT 5910 LEFT ENGINE POWER LEVER JAMMED AT 92 DEGREES. POWER COULD BE INCREASED BUT COULD NOT BE DECREASED.FOUND CORE COWL SUPPORT ROD STOW BRACKET BROKEN WHICH ALLOWED THE SUPPORT ROD TO JAM THE FUEL CONTROL LINKAGE. REPLACED BRACKET.SDR F3LA200200103Cowling · crackedDURING C-3 CHECK, INSPECTION REPORTED CRACK ON AFT LOWER CORNER OF NR 2 ENGINE OUTBOARD FIXED COWL NEXT TO FIRE SEAL. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3 AND 51-30-2.SDR DL73K020235Bullet · separatedON TAKEOFF ROLL, A LOUD THUD WAS HEARD AND AIRCRAFT PULLED SLIGHTLY TO THE LEFT. TAKEOFF WAS ABORTED. ENGINE PARAMETERS WERE NORMAL. UPON INSPECTION FOUND NR 1 ENGINE NOSE BULLET MOUNTING STUDS HAD PULLED FROM N1 TACH GEARBOX AND BULLET BECAME DISLODGED IN SDR F3LA200200090Cowling · damagedDURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE LT OUTBOARD COWL TOP EDGE DAMAGED BETWEEN SECOND AND LAST HINGE. REMOVED DAMAGE PER SRM 51-40-3. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-2, 51-40-3 AND 51-30-2.SDR USAA020073Acoustic Panel · crackedPIT - FOUND NOSE COWLING CRACKED/DISBONDED 4 FT BY 2 FT, LOWER ACOUSTICAL PANEL NOSE COWL 4 TO 8 O'CLOCK. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)SDR F3LA200200055Gusset · wornDURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE RT EXHAUST COWL INSIDE FLANGE ON BOTTOM OF THIRD RIB FROM FRONT WORN. REMOVED DAMAGED GUSSET FROM NR 1 ENGINE RT EXHAUST COWL. FABRICATED AND INSTALLED REPLACEMENT GUSSET PER SRM 51-21-171 AND 51-30-2.SDR AUS20020131Panel · debonded(AUS) NR 1 ENGINE ICE IMPACT PANEL DISBONDED.SDR IXXA0200005OCowling · departedEN ROUTE, SHORTLY AFTER TAKEOFF THE FLIGHT CREW HEARD AN ABNORMAL NOISE IN THE COCKPIT. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE NOISE WAS STILL PRESENT. THE FLIGHT RETURNED TO MCO FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH RSDR QXEA0300258Support Angle · crackedPDX - NR 1 ENGINE LOWER COWL: LEFT HAND SUPPORT ANGLE NEXT TO BYPASS DOOR CRACK AT FORWARD ATTACHMENT. REPAIRED IAW RD 8/4-71-016.SDR ASOA02074Cowling · crackedDURING HANGAR MAINTENANCE IN MCN, THE LEFT ENGINE AFT COWL HAD CRACKS. MAINTENANCE REPAIRED DAMAGE TO THE LEFT ENGINE COWL IAW SRM CHAPTER 51. CLEARANCE CHECK GOOD. (M)SDR QXEA0200095Skin · dentedPDX - DENT FOUND BETWEEN NR 1 LOWER COWL AND OIL COOLER. REPAIRED IAW RD 8-54-063.SDR 2002F00980Nose Cowl · crackedAFTER FINDING THE SAME CRACK ON SERIAL NR 17 PERFORMED AN INSPECTION AND FOUND A CRACK ON THE INNER SIDE APPROXIMATELY 3 O'CLOCK POSITION OF THE RIGHT ENGINE INLET NOSE CAP. THE CRACK WAS APPROXIMATELY .75 OF AN INCH IN LENGTH RUNNING FROM THE EDGE OF THE METSDR CALA0200021Nose Cowl · delaminatedINSPECTION FOUND #1 ENGINE NOSE COWL DELAMINATED. THE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-11-01.SDR QXEA0200522Plate · damagedPDX - BUTT PLATES ON RT LOWER COWL ALIGNMENT HOLES ON INBOARD AND OUTBOARD SIDES ARE ELONGATED AND OUT OF LIMITS. REPAIRED IAW DHC-8 SRM 51-20-11.SDR GTIA020216Cowling · damagedFTW - FOUND P/N 11-N-00304 LEFT ENGINE NOSE COWL ACCOUSTIC LINER IS FASTENERS AT 3 O'CLOCK POSITION AND 1 FASTENER AT 9 O'CLOCK ARE PULLED THROUGH. P/N 11-N-00316, REMOVE NR 1 ENGINE NOSE COWL TO SEND OSV, REINSTALL AFTER SERVICE. INSTALLED SERVICEABLE NOSE SDR GTIA020215Cowling · damagedFTW - RT ENGNE NOSE COWL ACCOUSTIC LINING HAS APPROX 48 FASTENERS PULLED THROUGH, RIGHT ENGINE NOSE COWL ACCOUSTIC LINING HAS BAD REPAIR AT 6 O'CLOCK POSITION. RT ENGINE NOSE COWL ACCOUSTIC LINING HAS THREE BAD REPAIRS FROM 12-10 O'CLOCK POSITIONS. RIGHT ENSDR GTIA012095Doubler · crackedFTW - NR 2 ENGINE NOSE COWL 2ND INTERNAL RIB (FROM AFT) 6 O'CLOCK POSITION REPAIR DOUBLER CRACKED. REMOVED DOUBLER REPAIR CRACKED. FORMED NEW SPLICE DOUBLER, INSTALLED NEW REPAIR IAW DC9 SRM 51-30-5. (M)SDR GTIA012156Web · crackedFTW - RIGHT NOSE COWL INBOARD AREA AT 6 O'CLOCK POSITION DOUBLER CRACKED. REMOVED CRACKED DOUBLER. AFTER FURTHER EVALUATION FOUND WEB ALSO CRACKED. CUT DAMAGED AREA (ON WEB). FABRICATED DRILLED AND LOCATED REPAIR PARTS FILLED DOUBLER. INSTALLED REPAIR PARSDR GTIA012157Structure · damagedFTW - NR 2 ENGINE NOSE COWL INLET REPAIR NOT IAW SRM (4 O'CLOCK). REMOVED OLD FILLERS AND DOUBLERS REPAIR. FORMED DOUBLERS. INSTALLED DOUBLERS IAW MD80 SRM 51-30-8. (M)SDR FXG2002F00000Cowling · failedWHILE IN FLIGHT THE LEFT SIDE OF THE UPPER ENGINE COWLING CAME LOOSE. THIS CAUSED THE COWLING TO RISE UP AND RIP OUT THE FORWARD PINS. A LARGE SECTION OF THE LEFT SIDE WAS TORN AWAY AND LOST. NO DEFECTS OR REPAIRS WERE NOTED ON THIS COWLING PRIOR TO FAILURSDR AUS20011313Cowling · corroded(AUS) INLET COWL ACOUSTIC PANELS CORRODED. SUSPECT CAUSED BY LACK OF DRAINAGE.SDR OYG2002F00000Cowling · crackedSEVERAL CRACKS WERE FOUND ON THE INSIDE OF THE AIR INLET COWL (HOT LIP) THESE CRACKS RUN HORIZONTALLY AND VERTICALLY ALONG THE WELD THE POSSIBLE CAUSE MIGHT BE THE HARMONICS OF THE VIBRATIONS FROM THE ENGINE AND PROPELLER. POSSIBLY GOING TO A THICKER GAUGE OFSDR A6WA200100065Service Door · openOIL SERVICE DOOR ON COWL 422BL OPENED INFLIGHT. MAINTENANCE SECURED DOOR CLOSED. INSPECTED COWL, NO DAMAGE NOTED.SDR GTIA011142Web · crackedFOUND NR 1 ENGINE COWLING WEB CRACKED AT 3 O'CLOCK POSITION. REPAIRED DAMAGED WEB IAW DC9/MD80 SRM 54-01. (M)SDR ABXA010627Frame · damagedENGINE NR 2 RIGHT CORE COWL FRAME NAC STA 304.60, NAC WL 75, FOUND DAMAGE ON FRAME. FABRICATED REPAIR PARTS, INSTALLED AND REPAIRED AREA IAW REA B671-42172MR.SDR F3LA200100125Doubler · tornDURING C-1 CHECK, INSPECTION REPORTED NR 2 ENGINE OTBD ENGINE COWL DOUBLER METAL TORN AT LATCH CUTOUT, 5TH LATCH FROM AFT. FABRICATED AND INSTALLED DOUBLER AND STRIKER PLATE PER SRM 51-40-2.SDR F3LA200100119Nose Cowl · wornDURING C-1 CHECK, INSPECTION REPORTED NR 1 ENGINE NOSE COWL AT 2 O'CLOCK POSITION MATING SURFACE WORN. CUT AWAY DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 54-10-03, 51-20-1 AND MM 51-21-99.SDR AUS20011209Panel · missing(AUS) NR 1 ENGINE MANUAL STARTER ACCESS PANEL MISSING. TRANSLATING SLEEVE CONTAINED A 63.5MM BY 38.1MM (2.5IN BY 1.5IN) HOLE.SDR 01FDEA00986Cowling · missingNR 3 T/R OUTBOARD SIDE TRANSLATING COWL MISSING.SDR GTIA012149Skin · crackedFTW - FOUND RIGHT ENGINE NOSE COWL, CRACK IN INNER LIP SKIN AT 6:00 POSITION. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR PARTS PER DC9 SRM 51-30-2. (M)SDR GTIA012102Web · crackedFTW - FOUND LEFT POWER PLANT NOSE COWL AFT INNER SECTION CRACK. REMOVED CRACKED WEB DOUBLER FROM NOSE COWL. FABRICATED NEW DOUBLER AND WEB. INSTALLED DOUBLER ON WEB. INSTALLED WEB PER DC9 SRM 51-30-2. (M)SDR AUS20011184Cowling · separated(AUS) LH ENGINE FORWARD UPPER COWL ASSEMBLY SEPARATED IN FLIGHT. PILOTHAD RECENTLY PERFORMED MAINTENANCE ON THE COWL. MINOR DAMAGE TO COWLS AND LEADING EDGE CAUSED BY COWL SEPARATION. PERSONNEL/MAINTENANCE ERROR.SDR GTIA011096Web · damagedFTW - NR 1 ENGINE NOSE COWL AFT WEBBING DENTED AND DAMAGED AT 9 O'CLOCK POSITION. CUT DAMAGE AREA PER SRM MD80 54-01. FABRICATED SECTION AND SPLICES TWO PER SRM MD80 54-01. INSTALLED SPLICES AND WEB IAW MD80 SRM 51-30-2 AND 51-30-1. (M)SDR GTIA011094Skin · delaminatedFTW - NOSE COWL AT 6 O'CLOCK POSITION O/B SURFACE HAS DELAMINATION. REMOVED DAMAGED PLIES OF CARBON SKIN IAW DC9/MD80 SRM 51-90-0. REPAIRED DELAMINATION AREA IN NOSE COWL AT 6 O'CLOCK POSITION IAW DC9 MD80 SRM 51-90-0. (M)SDR DHL2001742519Skin · crackedAT C-CHECK, ENG NR 3 UPPER COWL, UPPER LATCH CUTOUT AT STA 175.70 HAS SKIN CRACK.SDR TIM2001F00010Bulkhead · crackedTHE RIGHT ENGINE COWLING BULKHEAD AT STATION 238.18 THAT THE LOWER FRONT ENGINE COWLING ATTACHES TO WAS CRACKED ON THE RIGHT LOWER SIDE. THIS LOCATION IS WERE ONE OF THE FOUR BOLTS SECURE THE LOWER COWL TO THE BULKHEAD. (PICTURES INCLUDED)SDR TIM2001F00009Bulkhead · crackedTHE LEFT COWLING BULKHEAD AT STATION 238.18 THAT THE LOWER FRONT ENGINE COWLING ATTACHES TO WAS BROKEN OUT ON THE RIGHT LOWER SIDE. THE LOCATION IS WHERE ONE OF THE FOUR BOLTS SECURE THE COWL TO THE BULKHEAD. PICTURES INCLUDED.SDR QXEA0101681Cowl Door · chafedPDX - NR 2 ENGINE FORWARD COWL DOOR ON THE OUTBOARD SIDE IS CHAFED AT RAIN GUTTER. REPAIRED IAW HORIZON AIR EA 6-71-16.SDR QXEA0101682Cowl Door · chafedPDX - NR 1 ENGINE FORWARD COWL DOOR, 412AR, IS CHAFED ON THE COMPOSITE RAIN GUTTER. REPAIRED IAW HORIZON AIR EA 6-71-16.SDR DHL2001742516Skin · corrodedAT C-CHECK, NR 2 ENG, FWD LT COWL FWD LOWER CORNER, SKIN EDGE AND INTERIOR ANGLE DOUBLER IS CORRODED.SDR GTIA012074Acoustic Panel · separatedFTW - NR 2 ENGINE AT 3:00 POSITION LE OF ACOUSTICAL PANEL SEPARATED 1.4 INCHES SPAN INLET COWL. REPAIR ACOUSTICAL PANEL PER MD80 SRM WITH EA 934 IAW MD80 SRM 54-04. (M)SDR PCAA0109109Rivet · looseDURING FLEET INSPECTION OF NACELLES FOR LOOSE AND MISSING RIVETS SEVERAL RIVETS FOUND LOOSE ON RIGHT COWLING OUTBOARD END UNDER FLAP TRACK. RIVETS REPLACED ON RIGHT ENGINE COWL IN ACCORDANCE WITH DER CALLAHAN REPAIR SERVICES 8110 FORM CAS-AAL-09 REVISION B. SDR C2XA01TY107Flange · scratchedTYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ENGINE INLET UPPER COWL MOUNT FLANGE AT THE 12 O'CLOCK POSITION WAS FOUND TO BE SCRATCHED. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB GST-3097/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RESDR PCAA0108099Rivet · looseDURING FLEET INSPECTION SEVERAL RIVETS FOUND LOOSE ON LEFT COWLING OUTBOARD END JUST BELOW FLAP TRACK. RIVETS REPLACED IN ACCORDANCE WITH CALLAHAN REPAIR SERVICES DER AUTHORIZATION CAS-AAL-09. AIRCRAFT RETURNED TO SERVICE.SDR PCAA0109106Rivet · looseDURING FLEET INSPECTION FOR NACELLE RIVETS BEING LOOSE AND MISSING, RIGHT OUTBOARD ENGINE COWL JUST BELOW FLAP TRACKS FOUND TO HAVE LOOSE RIVETS. RIVETS REPLACED IN ACCORDANCE WITH DER CALLAHAN REPAIR SERVICES 8110 FORM CAS-AAL09-REV B. AIRCRAFT RETURNED TO SDR GTIA010934Nose Cowl · erodedFTW - RIGHT NOSE COWL 12 O'CLOCK POSITION HAS DENT AND ERODED BETWEEN 10 AND 2 O'CLOCK. DENT MEASURES 3.50 INCH SPAN BY 1.8 INCH CHORD TO .140 INCH OUT OF LIMITS PER MD80 SRM 54.04A. RIGHT ENGINE NOSE COWL REPLACED WITH SERVICEABLE P/N SQ30645-5093N001919 CHSDR CA011031004Hook · failed(CAN) DURING ROUTINE MAINT, RIGHT ENGINE UPPER FWD COWL HAD BEEN REMOVED. DURING CLOSE UP, ENGINEER RESPONSIBLE FOR CLOSURE OF COWL INADVERTENTLY SECURED EACH OF 4 CAM-HOOK ASSY TOWARDS RELEASED POS. SHORTLY AFTER TAKEOFF, COWL SEPARATED FROM ENGINE, STRUCK RTSDR DHL2001727623Skin · crackedON "C" CHECK DISCREPANCY------- NR 3 ENGINE LOWER COWLING , O/B SIDE, OUTER SKIN CRACKED/ BENT AROUND 3RD U-BOLT CUT-OUT.SDR DHL2001727598Cowling · crackedON "C" CHECK DISCREPANCY-------NR 3 ENGINE, LOWER. COWLING, O/B SIDE, CLOSING ASSIST HALE, SKIN CRACKED.
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