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 V0XD20220407003Strap · wornNUMBER 2 ENGINE UPPER COWLING AFT OUTBOARD TRAILING EDGE INTERNAL CHAF STRAP WORN. CORRECTIVE ACTION: REMOVED AND REPLACED (P/N: 2219-T81) NUMBER 2 ENGINE UPPER COWLING AFT OUTBOARD TRAILING EDGE INTERNAL CHAF STRAP IAW CRJ 900 SRM 54-23-00.SDR V0XD20220407002Strap · wornNUMBER 1 ENGINE UPPER COWLING AFT OUTBOARD TRAILING EDGE INTERNAL CHAF STRAP WORN. CORRECTIVE ACTION: REMOVED AND REPLACED (P/N: 2219-T81) NUMBER 1 ENGINE UPPER COWLING AFT OUTBOARD TRAILING EDGE INTERNAL CHAF STRAP.SDR V0XD20220407001Strap · wornNUMBER 1 ENGINE LOWER COWLING AFT OUTBOARD TRAILING EDGE INTERNAL CHAF STRAP WORN. CORRECTIVE ACTION REMOVED AND REPLACED (P/N: 2219-T81.040) NUMBER 1 ENGINE LOWER COWLING AFT OUTBOARD TRAILING EDGE INTERNAL CHAF STRAP.SDR FDEA202202100272Vane · damagedENG FAN EXIT VANES, APRX AT 9:15 TRAILING EDGE FOUND 1 VANE MISSING MATERIAL APROX (.75 X .125) INSTALLED WIRE CLOTH PATCH ON MISSING MATERIAL AT T/E APRX AT 9:15 POSITION ON #1 ENGINE FAN EXIT VANE PER AMM 72-33-01-8-2 PG4-6.SDR FDEA202202100271Vane · damaged#1 ENGINE, FAN EXIT VANE AFT EDGE HAS DAMAGE. MARK AT APPROX. TEN O'CLOCK #1 ENGINE, FAN EXIT VANE AFT EDGE MARKED AT 10 O'CLOCK PER AMM 72-33-01-8-2 REAIR 5 SUB TASK 72-33-01-350-270 PARA(B-E)& SUB TASK 72-33-01-942-271 PARA(1)PG19SDR HNAA2022022300085Not Reported · not reportedE898270 - RH ENGINE UPPER COWLING RIB GUSSET FWD OF ANTI/ICE ACCESS PANEL CORRODED .... REMOVED AND REPLACED RH ENGINE UPPER COWLING RIB GUSSET, FORWARD OF ANTI/ICE ACCESS PANEL ,IAW EMB145 SRM 51-40-02.SDR 2022F00035Cowl Door · puncturedLH ENGINE UPPER COWL DOOR DAMAGE. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ33099M1 DATED: JANUARY 10, 2022, 680A-0063 (N525QS) LEFT ENGINE UPPER COWL DOOR DAMAGE.SDR MASA20220112038None · noneTHE OUTBOARD LOWER FACING SHEET OF THE RH UPPER CORE COWL BONDMENT ASSEMBLY WAS FOUND TO HAVE ONE PUNCTURE AND FOUR DENTS. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 54-23-15, FIGURE 54-23-15-991-801, ITEM 2 (REV. 38 DATED 25/7/2020).SDR V0XD20220127003Housing · gougedR/H ENG LOWER COWLING AFT LATCH HOUSING UNDER PANEL 443 AR HAS A GOUGED. CORRECTIVE ACTION: BLENDED TO SMOOTH PROFILE GOUGED AREA AT AFT LATCH HOUSING UNDER PANEL 443 AR IAW CRJ 700 A.E # 22-C7-54-062.SDR MASA20220107014None · noneTHE OUTBOARD LOWER FACING SHEET OF THE RH UPPER CORE COWL BONDMENT ASSEMBLY WAS FOUND TO HAVE ONE PUNCTURE AND FOUR DENTS. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 54-23-15, FIGURE 54-23-15-991-801, ITEM 2, (REV. 38 DATED 25/7/2020). SDR MK1Y202201007None · noneENGINE # 2, LH CORE COWL, HAT FRAME, NAC STA 303.75, MID LOWER AREA: DURING MAINTENANCE INSOECTION AT IAI, MAINTENANCE DISCOVERED ON #2 ENGINE, LH CORE COWL HAT CHANNEL FRAME NAC STA 303.75 MID LOWER SECTION WITH CRACK AND GOUGE. PLEASE REFER TO FIGURE 2 FOR TSDR DALA2021122408040None · noneSHIP 185 FOUND NO.2 ENGINE RIGHT CORE COWL AFT LATCH FITTING CORROSION. CORRECITIVE ACTION: FOUND NO.2 ENGINE RIGHT CORE COWL AFT LATCH FITTING CORROSION. (2062331)SDR HNAA2021120600597None · nonePDIS 620 71-10 2746611 04DEC21 CLT CLOSE
EXTREME VIBRATION ON #1 ENGINE IN FLT @ 3000 FT. 00
FACT 04DEC21 15:42 CLT
FOUND #1 ENGINE OIL DOOR OPEN AND AIR START VALVE DOOR OPEN AND COWL DAMAGED. R+R #SDR REXA2022011900054Channel · bentRH ENGINE LOWER FAN COWL IS BENT AT ALIGNMENT PINS. C/A: REMOVED AND REPLACED LOWER CHANNEL IAW CRJ 900 SRM 51-21-16-001-001-A01, 51-42-06-001-001-A01 AND 51-42-12-001-001-A01SDR FDEA202111112824None · cracked#1 ENG I/B SIDE CORE COWL SPRING SEAL IS CRACKED APPROX 12"AFT OF THE FWD EDGE REMOVED AND REPLACED PER BOEING DWG # 311N3570 REV YSDR FDEA202111092801Deflector · cracked#1 ENG I/B CORE COWL LOWER LONGERON FWD EDGE SUBSTRUCTURE IS CRACKED REMOVED AND REPLACED DEFLECTOR PER BAC DWG # 314N3210 REV H AND B757 SRM 51-40-02-0GSDR SWAA2021110133159Web · cracked#2 ENGINE IB FAN COWL REINFORCEMENT WEB BELOW OIL SERVICE DOOR CRACKED / REMOVED AND REPLACED #2 ENGINE I/B FAN COWL WEB BELOW OIL SER DOOR IAW SRM 51-40-02INSP D77SDR IPXA2021102175183Bracket · brokenINSPECTION TYPE:A300#2 ENG T/R I/B AND O/B CIRCUMFERENTIAL LATCH UPPER GUIDE BRACKETS ARE BROKEN.REMOVED AND REPLACED BRACKETS IAW SRM 51-40-21.SDR IPXA2021102175182Bracket · brokenINSPECTION TYPE:A300#2 ENG T/R I/B AND O/B CIRCUMFERENTIAL LATCH UPPER GUIDE BRACKETS ARE BROKEN.REMOVED AND REPLACED BRACKETS IAW SRM 51-40-21.SDR DALA2021101806380None · noneSHIP 3260 RT ENG NOSE COWL RT SIDE AT 3 O'CLOCK POSTION SHROUD CRACKED. CORRECTIVE ACTION: FABRICATED NEW DOUBLER AND INSTALLED AT RT ENG NOSE COWL RT SIDE PER A320 CFM56-5A 54-02-00, CFM56-5A 54-10-00, ERA # 564422- 14MA, REV ORIGINAL. (1983282)SDR MK1Y20211011008None · noneENGINE #2, INLET COWL, PIN 242-2101-513BL, S/N 0242: DURING MAINTENANCE INSPECTION
AT IAI, SEVERAL CRACKS AND EXISTING REPAIRS WERE FOUND.SDR MK1Y20211011007None · noneMAINTENANCE FOUND A CRACK ON THE AFT FRAME OF ENGINE # 2 INBD CORE COWL (P/N 224-2301-521, S/N 3432001) AT 9 O’CLOCK POSITION. THE CRACK WAS FOUND BEYOND THE LIMITS OF SRM 54-45-01 REPAIR 4 NOTE C AND REPAIR 14 LIMITS.SDR 2A6R2021100861801None · chafedDURING INSPECTION FOUND THE ENGINE BRACKET CHAFED. PERFORMED A REPAIR IAW AIRBUS HELICOPTERS RDAS-EC135-71-2021-3462A
*NOT FOUND IN AIRFLEETSSDR DALA2021100606102None · noneSHIP 3305 MULTIPLE LIGHTNING STRIKE DAMAGE #1 LT FWD FAN COWL 6 INCHES AFT OF FWD EDGE. CORRECTIVE ACTION: REPAIRED FAN COWL DAMAGE PER A330 SRM 51-77-12. (1973800)SDR IPXA2021101374913Panel · crackedINSPECTION TYPE:A300#1 ENG I/B T/R FAN DUCT LATCHES FWD CLOSING PANEL HAS CRACK.REMOVED AND REPLACED IAW SRM 51-40-21.SDR COEA2021092103960Cowling · openFLIGHT 8657, ENROUTE SEA-CLM AIR TURNBACK/DISCREPANCY: RIGHT COWLING OPENED IN FLIGHT RIGHT AFTER TAKEOFF. AIRCRAFT WAS RETURNED TO SEA. NO EMERGENCY DECLARED. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE FOUND R/H UPPER ENGINE LATCH UNLATSDR SWAA2021100418636Duct · cracked#1 ENGINE INLET COWL LOWER TAI EXHAUST LOUVER DUCT IS CRACKED AT WELD. / [01] REMOVAL AND REPLACEMENT #1 ENGINE TAI EXHAUST LOUVER DUCT TO BE ACCOMPLISHED ON CARD #TTG8Q006GUZN; CARD IS FOR PART TRACKING ONLY.SDR QR9R20210614001Gas Cylinder · unreliableGAS SPRING HAS INSUFFICIENT FORCE TO HOLD COWLING DOOR OPEN.SDR MDGA092506112021Cowl Door · tornRIGHT ENGINE OIL SERVICE DOOR DEPARTED THE AIRCRAFT AND TORE A SECTION OF THE LOWER ENGINE COWL.SDR MK1Y01292021003Cowling · unknownUNDOCUMENTED REPAIR DOUBLERS FOUND AT LT ENGINE ON OUTBOARD CORE COWL OUTER SKIN.SDR IPXA2021012865016Crank Assy · crackedINSPECTION TYPE: A300 NR 2 ENGINE NOSE INLET COWL HAS POSSIBLE CRACK AT 9 O'CLOCK POSITION ON AFT AREA GROUND ELBOW FITTING. REPAIR IAW SRM 54-10-00 REPAIR NR 14.SDR IPXA2021012865015Cowling · crackedINSPECTION TYPE: A300 NR 2 ENGINE NOSE INLET COWL HAS POSSIBLE CRACK AT 3 O'CLOCK POSITION ON AFT AREA GROUND ELBOW FITTING. REPAIRED IAW SRM 54-10-00 REPAIR NR 14.SDR HALA2020122900226Fairing · crackedCRACKS, FOUND 2 CRACKS ON TOP LPT FAIRING. REPLACED TOP LPT FAIRING, PER AMM 72-03-03/401. SECURITY CHECK OKAY.SDR 120B2020071600104Support Bracket · cutNR 2 ENGINE NOSE COWL, AFT WEB, OTBD LOWER SUPPORT BRACKET IS CUT.SDR 120B2020071500089Frame · chafedNR 1 ENGINE OTBD CORE COWL INTERIOR 2ND FRAME IS CHAFFED (REPAIRED).SDR UATA202007157107Support Bracket · crackedLT ENGINE COWL INERTIAL SEPARATOR INLET SUPPORT BRACKET FOUND CRACKED UPON ROUTINE ENGINE INSPECTION.SDR IPXA2020070357291Panel · damagedINSPECTION TYPE:SEG PANEL 413BL HAS (2) ELONGATED HOLES IN ATTACH FLANGE. RECEIVED NEW PNL ASSY INSTALLED ON ACCESS M10 IAW SRM 51-40-21.SDR MK1Y20200701001Cowling · corrodedDURING MAINTENANCE MULTIPLE CORROSION DAMAGES ON THE BACKSHEET'S INNER BARREL OF INLET COWL.SDR IPXA2020070157190Bracket · chafedINSPECTION TYPE:SV NR 2 ENGINE BRIDGE ASSY BOX RIB 2ND FROM O/B ON RT SIDE HAS A CHAFED BOLT HOLE. REMOVED AND REPLACED NR 2 ENGINE BRIDGE ASSY BOX RIB 2ND FROM O/B IAW SRM 51-33-01. (MINOR)SDR IPXA2020070157196Channel · damagedINSPECTION TYPE:SV LT FAN COWL LANGING FRAME IS DAMAGED(MID-SPAN). REPAIRED FAN COWL FRAME IAW SRM 54-00-00 FIG 208. (MINOR)SDR IPXA2020070157195Channel · damagedINSPECTION TYPE:SV NR 2 PYLON RT FAN COWL LANDING HAT CHANNEL IS DAMAGED. REPAIRED DAMAGED HAT CHANNEL IAW SRM 54-00-00 FIG 208. (MINOR)SDR IPXA2020070157226Channel · damagedINSPECTION TYPE:SV NR 2 ENG LT FAN COWL SKIN PANEL LANDING HAT CHANNEL IS DAMAGED. REPAIRED HAT CHANNEL IAW SRM 54-00-00 FIG 208. (MINOR)SDR IPXA2020070157188Skin · chafedINSPECTION TYPE:SV NR 2 LT FAN COWL CLOSE OUT (DOOR JAMB) SKIN IS CHAFED THROUGH. REMOVED AND REPLACED CHAFED NR 2 LT FAN COWL CLOSE OUT (DOOR JAMB) SKIN IAW SRM 51-35-01. (MINOR)SDR IPXA2020070157187Skin · chafedINSPECTION TYPE:SV NR 2 RT FAN COWL CLOSE OUT SKIN (DOOR JAMB) SKIN IS CHAFED THROUGH. REMOVED AND REPLACED CHAFED NR 2 RT FAN COWL CLOSE OUT (DOOR JAMB) SKIN IAW SRM 51-35-01. (MINOR)SDR QMLA2020062220028Wire · unsecureAC EQUIPPED WITH AN FDC IBF SYSTEM, WHICH INVOLVES AN ADDITIONAL COWLING ACROSS THE FORWARD PART OF THE TRANSMISSION DECK. THIS COWLING INCLUDES, ON EACH SIDE, TWO PIECES OF HARD PLASTIC DUCTING CONNECTED BY A PIECE OF FLEXIBLE ORANGE DUCTING WITH A METAL WIRSDR IPXA2020061356527Bracket · brokenINSPECTION TYPE:SEG NR 1 ENGINE NOSE COWL LOWER LT SIDE BRACKET BROKEN. REMOVED AND REPLACED NR 1 ENG NOSE COWL LT SIDE BRACKET IAW AMM 71-11-00-0401.SDR IPXA2020061556481Bulkhead · crackedINSPECTION TYPE:A300 NR 2 ENGINE INLET AFT BULKHEAD HAS A CRACK ON LT SIDE NEAR SENSE LINE AT ABOUT 9 O'CLOCK POSITION. REPAIR WEB IAW SRM 54-10-00 REPAIR NR 14.SDR IPXA2020060856206Pin · wornINSPECTION TYPE:C NR 2 ENGINE I/B ALIGNMENT PIN AND RECEIVER WORN. REMOVED AND REPLACED ALIGNMENT PIN AND RECEIVER.SDR HALA2020060100118Cowling · scratchedSCRATCH FOUND ON NR 2 ENGINE INLET COWL, AROUND 7 O'CLOCK POSITION. DAMAGE ASSESSMENT CARRIED OUT IAW SRM 54-10-01. REFER TO ATTACHED FOR DETAILS. COMPOSITE REPAIR ON NR 2 ENGINE INLET COWL AROUND 7 O'CLOCK POSITION 03 OFF AREAS. CARRIED OUT AS IAW TV NO 2SDR IXXA20200609024Skin · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VISIT. UPON ACCOMPLISHMENT OF ATI-71-834-00-01. EXTERNAL - ZONAL GV CORE COWL PANELS - ENG 1 AND 2. PERFORM EXTERNAL GENERAL VISUAL INSPECTION OF ZONE, THE FOLLOWING FINDINGS WERE NOTED: I/B CORE COWL OUTER SKIN CRACKED
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