JASC 7160
Service difficulty reports · 1,162
Reports filed under 7160 · Engine Air Intake 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 = '7160' 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 = '7160' 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 CA090119009Intake · corrodedDURING A STRUT REPAIR, THE TECH FOUND SEVERE CORROSION, LEVEL 3, ON 2 LONGERON INTAKE COWLS, PN C2TEC1001-18 AND C2TEC1001-17. BOTH PARTS WERE REPLACED.SDR UALA2009011900188Acoustic Liner · damagedNR 2 ENG ACOUSTIC LINER 8 O'CLOCK POS DAMAGED. NR 2 ENG INNER ACOUSTIC PANEL 8 O'CLOCK POSITION CRACKED 4.5 INCHES FORWARD OF LPC BLADES. REPLACED NR 2 ENG NOSE COWL.SDR DHLA200800138Nose Cowl · damagedRAMP DAMAGE TO INB D TOP SIDE OF NR 1 ENGINE NOSE COWL. ACFT STRUCK BY PORTABLE AIRSTAIRS WHILE PARKED ON RAMP. NR1 ENG COWL P/N NSL6051-533 REQUIRING REPLACEMENT.SDR C2XA08SH164Inlet · corrodedVARIOUS BOLTHOLES ON THE LT ENG AIR INLET CORRODED. REPAIRED BOLT HOLE ON LT ENG AIR INLET IAW EC 5420-01179. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR 2008FA0000927Hose · contaminatedBEGAN NORMAL LANDING CHECK LIST INCLUDING CHECKING CARB HEAT. AFTER PULLING CARB HEAT ON, ENGINE DIED. TURNED OFF CARB HEAT & ENGINE RESTARTED ON ITS OWN WITHOUT PILOT INPUTS. CONTINUED PATTERN & GRADUALLY REAPPLIED CARB HEAT ON BASE AND FINAL. ON SHORT FISDR UPS08M53916Acoustic Panel · dentedINSPECTION TYPE:1C 2 EA DENTS AT 6 O'CLOCK POSITION 6 INCHES AND 18 INCHES FROM NOSE LIP IN NR 1 ENG INLET ACOUSTIC PANEL. REMOVED DAMAGE, FABRICATED AND INSTALLED PLUGS AND APPLIED FIBERGLASS IAW MD-11 SRM 54-10-00 REPAIR 18 STEPS C-F AND G-O.SDR 08FDEA04872Nose Cowl · gougedNR V 1 NOSE COWL HAS A MINOR SCRATCH AT 10 O'CLOCK POSITION LEADING EDGE. REMOVED DAMAGED SKIN AREA IAW SRM 54-10-00 REPAIR NR 9. FABRICATED SKIN PATCH AND DOUBLER IAW SRM 54-10-00, LOCATED AND DRILLED PATCH AND DOUBLER IAW SRM 51-40-44. HEAT TREATED PATCHSDR ZESA2008020Inlet · damagedDURING A PREFLIGHT INSP, MX DISCOVERED A POPPED RIVET WITH SEVERAL OTHERS SHOWING SIGNS OF DETERIORATION. FURTHER INSP REVEALED A FAN BLADE HAD BEEN DAMAGED FROM THE RIVET HEAD. A BORESCOPE WAS ACCOMPLISHED TO ENSURE NO FURTHER DAMAGE WAS CAUSED. INLET AND SDR CA081014006Grommet · missing(CAN) DURING A DEFECT RECTIFICATION ON THE CARB AIR DOOR ON THE RT ENGINE IT WAS DISCOVERED THAT THE LT ENGINE CARB AIR DOOR LOWER SHAFT SUPPORT BUSHING PN, 453-991 AND GROMMETT WERE MISSING.SDR 2008UALA06010Nose Cowl · damagedNR 2 ENG NOSE COWL DAMAGED BY RAMP LD-2 CONTAINER. REPLACED NOSE COWL.SDR CA081006004Grommet · missing(CAN) DURING A DEFECT RECTIFICATION ON OUR OTHER ACFT, IT WAS FOUND THAT THE LWR GROMMET AND BUSHING P/N 453-991 WAS MISSING ON THE LT ENGINE CARB HEAT BOX. THIS GROMMET SUPPORTS THE SHAFT IN THE CARB HEAT BOX. THIS PROMPTED THE INSP OF THIS ACFT, WHICH FOUND SDR 08FDEA04140Panel · damagedNR 2 ENGINE AT THE 5:00 POSITION; LIP RING PANEL LEFT FAN COWL OPEN / CLOSE IS DELAMINATED / CRACKED & GOUGED WITH LOOSE & SHEARED FASTENERS. REMOVED; FABRICATED & REPLACED THE LOWER SKIN PANEL & ANGLE IAW SRM 51-31-01, 51-35-01, 51-24-01 & 55-31-01 & DWG AJSDR 2008UALA05920Nose Cowl · delaminatedWHILE PROCESSING THE AC FOR PAINT, A DELAM INATED AREA WAS FOUND AT THE 10 O'CLOCK POSITION ON THE INBOARD SIDE OF THE NR 2 NOSE COWL. COMPLETELY UN-NOTICABLE VISUALLY FROM THE OUTSIDE. AREA IS 18 INCHES BY 18 INCHES. THERE ARE NO DEPRESSIONS, OR ANY OTHER SDR CA081117006Yoke · broken(CAN) DURING A 100 HOUR INSP, THE YOKE LT INTAKE COWL BROKE AT MACHINED LOCKING TAB EAR CUT OUT UPON INSTALLATION WHILE RIVETING, LT YOKE-INTAKE COWL WAS REPLACED.SDR C2X2008F00027Inlet · corrodedAC IS CURRENTLY IN C-CHECK AND CORROSION WAS FOUND ON THE NR 2 ENGINE INLET ATTACH FLANGE MOUNTING HOLES. MAINTENANCE REPAIRED THE NR 2 ENGINE INLET IAW EC542001146/ AC WO; BE RELEASED AT THE END OF THE CHECK. (K)SDR C2X2008F00026Inlet · corrodedAC IS CURRENTLY IN C-CHECK AND CORROSION WAS FOUND ON THE NR 1 ENGINE INLET ATTACH FLANGE MOUNTING HOLES. MAINTENANCE REPAIRED THE NR 1 ENGINE INLET IAW EC5420-01145. AC WILL BE RELEASED AT THE END OF THE CHECK. (K)SDR CA080910001Intake Duct · cracked(CAN) DURING A ROUTINE PATROL FLIGHT THE PILOT EXPERIENCED A VIBRATION IN THE AREA OF THE REAR ENGINE. HE ELECTED TO RETURN TO THE AIRPORT AND MADE AN UNSCHEDULED LANDING WITHOUT INCIDENT. UPON INSPECTION BY THE MX CREW, IT WAS DISCOVERED THAT THE FWD EDGE OF SDR 2008UALA05496Nose Cowl · damagedNR 1 ENG NOSE COWL HAS DAMAGE AT THE 5 OCLOCK POSITION. REPLACED NR 1 ENG NOSE COWL.SDR MAL2008F00029Intake Duct · damagedIN FLIGHT THE ODOR OF BURNED RUBBER FILLED THE FLIGHT DECK FOLLOWED BY ICE PROTECTION LOOK UP LIGHT AND LEFT INTAKE LIGHT. R&R LT LOWER INTAKE DUCT.SDR 2008FA0000565Intake Duct · crackedMFG SUPPLIED ENGINE INTAKE DUCT BEFORE THE AIR FILTER IS SUBJECT TO CRACKING IN MULTIPLE LOCATIONS. THIS PARTICULAR AC AND ANOTHER IDENTICAL MODEL AC THIS FACILITY MAINTAINS, HAVE BEEN CONVERTED TO ANOTHER ENGINE AFTER THE STC CONVERSION. CRACKING PROBLEM HASDR 2008FA0000554Intake Duct · crackedMANUFACTURER SUPPLIED ENG INTAKE DUCT BEFORE THE AIR FILTER IS SUBJECT TO CRACKING IN MULTIPLE LOCATIONS. THIS PARTICULAR ACFT AND ANOTHER IDENTICAL MODEL ACFT THIS FACILITY MAINTAINS HAVE BEEN CONVERTED TO AN IO-550-F ENG. AFTER THE STC CONVERSION, THE CRACSDR 08FDEA03385Actuator · failedNR 1 ENG COMPRESSOR STALL BEGINNING DESCENT FROM FL350 ENG WOULD NOT RESTART. WINDMILLING WITHOUT OIL PRESSURE WAS 15 MINUTES. REMOVED AND REPLACED THE STATOR VANE ACTUATOR .SDR 08FDEA03315Skin · damagedNR 1 ENGINE NOSE COWL SKIN DAMAGED AT 9 O'CLOCK POSITION CUT OUT DAMAGE AREA DIM 4 3/4 BY 3 1/2 IAW B727 SRM 54-30-3 FIG 5. CUT OUT ACCESS HOLE DIM 5 IN ABOVE DAMAGE IAW B727 SRM 54-30-3 FIG 3. FABRICATED DOUBLER REPAIRS FROM 2024T3, 0.040 INCH AND FILLER FRSDR COEA0803816Flange · corrodedLEVEL 2 CORROSION: LT WING FUEL OVERFLOW/VENT TANK NACA DUCT (AIR INTAKE DUCT) FLANGE HAS AREAS OF SURFACE CORROSION. CORROSION BLENDOUT TO MATTING SURFACE OF FLANGE WAS BLENDED BEYOND SRM LIMITS. REMOVED & REPLACED DUCT ASSEMBLY. (S)SDR 2008FA0000533Skin · crackedREPORTED RT ENG INLET CRACKED AT 9:00 POSITION. THE INLET WAS REMOVED AND REPAIRED AND REINSTALLED ON THE AC. (K)SDR DJFA2008063Inlet · crackedREPORTED RT ENGINE INLET CRACKED AT 9:00 POSITION. OPEN. (S)SDR CA080807006Seal · damaged(CAN) CONVERTED LAST FEB, AT THE SAME TIME INSTALLED AN FDC ENGINE AIR FILTER. JULY 1ST 2008 THE PILOT WAS STARTING THE ENGINE GOT TO AROUND 60 PERCENT TORQUE WHEN COMPRESSOR STALLS OCCURRED. HE SHUTDOWN. UPON INSP FOR COMPRESSOR STALLS IT WAS FOUND THE COMPRESDR DJFA2008056Skin · crackedDURING A ROUTINE SERVICE CHECK IT WAS NOTED THAT THE LT ENGINE INLET INNER SKIN WAS CRACKED AT THE 9 O’CLOCK POSITION. THE INLET WAS REMOVED, REPAIRED BY INTEGRITY AERO AND REINSTALLED. (A)SDR DJF2008F00000Skin · crackedDURING A ROUTINE SERVICE CHECK IT WAS NOTED THAT THE LT ENGINE INLET INNER SKIN WAS CRACKED AT THE 9 O’CLOCK POSITION. THE SDR WILL BE UPDATED UPON COMPLETION OF THE C/A. (K)SDR WXOA070210Inlet · dentedFLIGHT CREW REPORTED DURING THE WALKAROUND INSPECTION A LARGE DENT ON THE RIGHT WING SLAT 0 AND THE RIGHT ENGINE INLET NACELLE. MAINTENANCE DEPARTMENT PERSONNEL REPLACED THE 0 SLAT AND WITH THE ASSISTANCE OF BOEING THE INLET COWL WAS INSPECTED AT THE END OF ESDR DJFA2008051Intake · crackedDURING ROUTINE MAINTENANCE THE LT INLET SKIN AT THE INLET TEMPERATURE PROBE WAS FOUND CRACKED. THE LT INLET WAS REPLACED. (A)SDR YEN2008F00004Duct · looseAIR RETURN TO DEPARTURE DUE SOUND IN COCKPIT AS IF N1 OR NX SYNC WAS OFF. ENG INDICATIONS NORMAL. FOUND AIR INTAKE FOR BOTH RT AND LT DUCT ON 191FL LOOSE, TIGHTENED CLAMPS AND SECURED, OPS CHECK OK. (K)SDR 08FDEA01882Cowling · damagedNR 3 ENGINE INBD FAN COWL HAS A SMALL PUNCTURE. REPAIRED DAMAGED AREA BY FABRICATING AND BONDING A FILLER AND DOUBLER IAW DC/MD-10 SRM 54-00-01, FIG 4, VOL I. RESTORED THE SURFACE FINISH IAW DC/MD-10 SRM 51-21-01, VOL II, 51-21-01; VOL II AND 51-41-01, VOL SDR 08FDEA01506Skin · chafedNR 2 ENGINE INBD FAN COWL INNER SKIN DOUBLER IS WORN AND CHAFED. REMOVED AND REPLACED DAMAGED CHAFE PLATE ITEM 9 IAW SRM 54-02-01 & 54-20-00. RESTORED THE SURFACE FINISH IAW SRM 54-20-00.SDR 08FDEA01505Skin · delaminatedNR 2 ENGINE INBD FAN COWL INNER SKIN IS DELAMINATED. REMOVED DAMAGED INNER SKIN AND REPAIRED IAW SRM 54-20-00. RESTORED FINISH IAW SRM 54-20-00 & SRM 51-75-10.SDR 08FDEA01504Cowling · dentedNR 2 ENGINE INBD FAN COWL IS DENTED. REMOVED DAMAGE, PREPED FOR THE APPLICATION OF FILLER MATERIAL. APPLIED FILLER, CURED, SANDED & PREPPED FOR PRIMER. APPLIED PRIMER & PAINTED IAW SRM 54-10-00, 54-20-00 & 51-75-10.SDR 08FDEA01503Nose Cowl · dentedNR 2 ENGINE INBD FAN COWL IS DENTED. REMOVED DAMAGE, PREPPED FOR THE APPLICATION OF FILLER MATERIAL. APPLIED FILLER, CURED, SANDED & PREPPED FOR PRIMER. APPLIED PRIMER & PAINTED IAW SRM 54-10-00, SRM 54-20-00 & SRM 51-75-10.SDR 08FDEA01502Nose Cowl · delaminatedNR 1 ENGINE NOSE COWL IS DELAMINATED AT THE FWD LOWER END. REMOVED & REPLACED THE NR 1 NOSE COWL IAW AMM 71-11-00-4. FAN COWL DOORS TO BE ADJUSTED & CLOSED ON THE NR 1 ENGINE INSTALLATION W/C 64T0700-1.SDR 2008FA0000301Muff · failedAFTER A FLIGHT, IT WAS NOTED THAT A PORTION OF SCAT HOSE WAS HANGING FROM THE BOTTOM OF COWLING OPENING. UPON INSPECTION IT WAS FOUND THAT THE CARBURETOR HEAT FLANGE HAD SEPARATED WITH THE SCAT HOSE ATTACHED WITH CLAMP FRO THE IB HALF OF THE RT CARB HEAT MUFFSDR 08FDEA00966Intake · damagedNR 1 ENGINE INTAKE AT THE 8:30 POSITION; ABLATIVE COATING IS MISSING. REMOVED DAMAGE, APPLIED SEALANT TO REPAIR & CURED IAW ENGINE MANUAL 72-22-01 REPAIR 10.SDR 2008FA0000234Valve · brokenTHE ENG AUTOMATIC ALTERNATE INDUCTION AIR VALVE THAT IS PARTIALLY LOCATED INSIDE THE CYLINDRICAL PAPER INDUCTION AIR FILTER CAME APART AND SOME OF ITS PART (2 INCH LONG, .2500 INCH DIAMETER BOLT. 2 INCH LONG SPIRAL SPRING WASHER, AND COTTER PIN) WERE INGESTEDSDR CA080318001Bracket · detached(CAN) DURING ROUTINE INSP TECH NOTICED NO CARB HEAT DROP ON IN-COMING RUN-UP. TECH DISCOVERED THAT ONE OF THE 2 CARB AIR BOX BUTTERFLY VALVE BRACKETS HAD BECOME DETACHED FROM SHAFT AND VALVE WAS NOT OPENING OR CLOSING PROPERLY.SDR 08FDEA00756Nose Cowl · corrodedNR 1 ENGINE NOSE SECTION HAS CORROSION ON THE INNER SKIN OF THE INTAKE AT THE 4:00 O'CLOCK POSITION; ACCESS 434BR. REMOVED AND REPLACED NR 1 ENGINE NOSE COWL IAW MM 71-11-00-4.SDR P5CA0801547Inlet · damagedDURING THE OIL SERVICING OF THE NR 3 ENGINE DAMAGE OCCURRED TO THE RIGHT SIDE OF THE INLET COWLING AT THE 3 O'CLOCK POSITION. ACCOMPLISHED INTERIM REPAIR PER EO NR 4471A012 PART 1 PER SRM 54-15-01.SDR DHL2008752609Skin · crackedNR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1.SDR 08FDEA00374Inlet · looseNR 2 ENGINE INLET JUST FWD OF THE ENGINE FAN BLADES HAS NUMEROUS LOOSE FASTENERS AT THE 12:00, 9:00, AND 3:00 O'CLOCK POSITION (REFERENCE MD 11 IPC 55-32-01-01, CIRCLED ITEM K). REMOVED AND REPLACED LOOSE FASTENERS INSIDE INLET PER AMM 20-00-00.SDR CA080208006Nose Bullet · separated(CAN) FOLLOWING DEPARTURE, THE CREW REPORTED COMPRESSOR STALLING OF THE NR 1 ENG AT CLIMB PWR. THE ENGINE PWR WAS REDUCED AND COMPRESSOR STALLS STOPPED. THE AC RETURNED TO DEPARTURE WITH NO FURTHER INCIDENT. INSP OF THE ENGINE IDENTIFIED THAT THE NR 1 ENGINE NSDR DHL2007793022Nose Cowl · dentedNR 3 ENGINE NOSE COWL HAS DENTS ON INBOARD SIDE 3 O'CLOCK POSITION NAC STATION 99.3. CUT OUT DAMAGE AREA AT NR 3 ENGINE NOSE COWL INBOARD SIDE AT 3 O'CLOCK POSITION. FABRICATED DOUBLER OUT 2024-T3 0.040" IAW B-727 SRM 54-30-3 AND 54-30-2. FABRICATED FILLER SDR QXEA200701790Actuator · malfunctionedSEA- FLIGHT 2287 - ENGINE INTAKE SWITCH ON THE NR 2 SIDE FLICKERING ON AND OFF WHILE SWITCH IS IN CLOSED POSITION. RETURNED TO THE GATE. MAINTENANCE REPLACED THE INTAKE BYPASS DOOR ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR VNAA0711012Inlet · damagedCREW REPORTED MULTIPLE BIRD STRIKES TO THE FUSELAGE, WING AND BOTH ENGINES. MAINTENANCE INSPECTED FOUND DAMAGE TO THE LEFT ENGINE INLET, FORWARD EQUIPMENT BAY DOOR AND BULKHEAD, AND THE RIGHT WING LEADING EDGE. MAINTENANCE REMOVED AND REPLACED THE DAMAGED LE
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