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.

SDR DHL2001727546Skin · crackedDURING C-CHECK, NR 1 ENGINE LWR COWLING, O/B SIDE, FIRST U-BOLT CUTOUT, PREVIOUS REPAIR CRACKED. REMOVED PREVIOUS REPAIR PER B-727 SRM 51-30-2 FROM THE NR 1 ENGINE LOWER COWLING O/B SIDE FIRST U-BOLT CUTOUT. MADE NEW DOUBLER PER B-727 SRM 54-10-3 INSTALLED DAug 19, 2001 · N727DH · Boeing 727200SDR DHL2001727529Gusset · crackedNR 3 ENG COWLING O/B SIDE INTERNAL GUSSET CRACKED AT 4TH U-BOLT CUTOUT. REMOVED AND REPLACED NR 3 ENG LWR COWLING O/B SIDE INTERNAL GUSSET AT NR 4 U-BOLT CUTOUT .Aug 19, 2001 · N727DH · Boeing 727228SDR DHL2001362029Channel · crackedA4 CHECK NR 2 ENG O/B REVERSER COWL, BUMPER HAT SECTION HAS A CRACK. REMOVED & REPLACED NR 2 ENG O/B REVERSER COWL, BUMPER HAT SECTION IAW A-300-SRM-51-30-30 PAGE 8Aug 12, 2001 · N362DH · Airbus A300B4203SDR DHL2001362031Cowling · chafedA4 CHECK - NR 2 ENG O/B AFT CORE COWL, CHAFFED AT 5 O'CLOCK POSITION AFT SECTION. REMOVED AND REPLACED TRAILING EDGE CLOSE OUT AT NR 2 ENGINE O/B AFT CORE COWL IAW A300 MM 71-13-00Aug 11, 2001 · N362DH · Airbus A300B4203SDR DHL2001362030Cowling · chafedA4 CHECK - NR 2 ENG I/B AFT CORE COWL, CHAFED AT 6 O'CLOCK POSITION AT AFT SECTION. REMOVED AND REPLACED THE NR 2 ENGINE I/B AFT CORE COWLING AFT SECTION STRIP PER THE A300 MM 71-13-00Aug 11, 2001 · N362DH · Airbus A300B4203SDR DLM88011280Skin · delaminatedTHE NOSE COWL ACOUSTIC BARREL BACKSKIN WAS FOUND DELAMINATED REPAIR PER ER/A .Aug 3, 2001 · N901DL · Doug MD88SDR USAA01933Nose Cowl · crackedFOUND DAMAGE TO LEFT ENGINE NOSE COWLING. DURING PILOT WALKAROUND FOUND A 12 INCH CRACK 99 INCHES FROM GROUND AND A 5 INCH CRACK 61 INCHES FROM GROUND ON LEFT SIDE OF THE LEFT ENGINE NOSE COWLING. COWLING REMOVED AND REPLACED WITH LIKE PART IAW 71-61-401 S/NAug 1, 2001 · N672UW · Airbus A330323SDR QXEA0101306Cowling · chafedPDX- NR 1 ENGINE LOWER COWL, FORWARD OUTBOARD LATCH BUTTPLATE IS CHAFED. REPAIRED IAW DHC-8 RD8-71-18 AND HORIZON AIR EA 2-71-155.Aug 1, 2001 · N349PH · Dhav DHC8202SDR 2001F00271Latch · brokenFLT 1 - FLL - ON DEPARTURE CLIMB-OUT, NR 2 ENGINE ACCESS DOOR ILLUMINATED. AIRCRAFT RETURNED TO FLL. INSPECTED AND FOUND BROKEN LATCH ON NR 2 ENGINE ACCESS DOOR. REMOVED AND REPLACED LATCH ASSEMBLY PER MM 71-10-00. OPERATION CHECKED NORMAL. AIRCRAFT RETURJul 23, 2001 · N553NA · Boeing 7272J7SDR QXEA0101203Cowling · damagedPDX - RIGHT-HAND LOWER COWL STIFFNER ON TOP DECK HAS CHAGE APPROXIMATELY 27" FORWARD OF AFT END OUTBOARD SIDE. REPAIRED IAW HORIZON AIR EA 2-71-151.Jul 23, 2001 · N375PH · Dhav DHC8202SDR QXEA0101202Cowling · chafedPDX - RIGHT-HAND LOWER COWL INTAKE FLANGE HAS A SCREW HEAD CHAFE AT THE OUTBOARD SIDE OF THE RING. CHAFE MEASURES .375 WIDE AND IS APPROXIMATELY .008" DEEP. REPAIRED IAW HORIZON AIR EA 2-71-152 AND RD 8-71-74.Jul 23, 2001 · N375PH · Dhav DHC8202SDR DHL2001366507Cowling · crackedA CHECK - NR 2 ENGINE AFT COWLING AT 7 O'CLOCK HAS A CRACK.STOP DRILLED CRACK. INSTALLED DOUBLER REPAIR AS PER A-300 SRM 54-00-00 FIGURE 708.Jul 22, 2001 · N366DH · Airbus A300B4203SDR DHL2001366019Bracket · crackedA1 CHECK - NR 1 ENG O/B COWL CENTER LATCH HAS 2 S/M ANGLE BRACKETS CRACKED (T/R DOOR CENTER)REMOVED BRACKETS (2 EACH),WELDED, AND INSTALLED BRACKETS (2 EACH) AT NR 1 ENG O/B COWL CENTER LATCH AS PER A300 M/M 71-13-00Jul 21, 2001 · N366DH · Airbus A300B4203SDR DHL2001366505Bracket · crackedA1 CHECK - NR 1 ENG O/B COWL CENTER LATCH HAS 2 S/M ANGLE BRACKETS CRACKED (T/R DOOR CENTER)REMOVED BRACKETS(2 EACH) WELDED, AND INSTALLED BRACKETS (2 EACH) AT NR 1 ENG O/B COWL CENTER LATCH AS PER A300 M/M 71-13-00Jul 21, 2001 · N366DH · Airbus A300B4203SDR 2001UALA01444Cowling · crackedNR 2 ENGINE LOWER FORWARD COWLING MATING FLANGE, FOUND 3 CRACKS, ONE 8 INCHES LONG, THE OTHERS 3.5 INCHES LONG. ALSO, THERE IS A HOLE WORN THRU COWL MATING FLANGE. REPAIRED COWL AND SPLICED IN NEW FLANGE. MAJOR REPAIR ACCOMPLISHED.Jul 20, 2001 · N7263U · Boeing 727222SDR QXEA0101170Cowling · damagedPDX - SHEET METAL DAMAGED ON INBOARD LOWER NACELLE JUST AFT OF LOWER COWL. REPAIRED IAW RD 8-54-003.Jul 12, 2001 · N830PH · Dhav DHC8102SDR RRXA11319Doubler · chafedDURING A MAINTENANCE VISIT FOUND CHAFF DAMAGE TO NR 3 ENGINE I/B FAN COWL INNER DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 71-2-8 PAR.5C.Jun 23, 2001 · N606AL · Doug DC873FSDR AUS20010639Bracket · broken(AUS) NR 1 ENGINE INBOARD THRUST REVERSER COWL V' BAND HOOK BRACKET BROKEN.Jun 17, 2001 · Boeing 767338SDR DHL2001803532Skin · crackedAT C-CK, ENGINE NR 3 HAD 1.5 INCH CRACK ON EXTERNAL SKIN OF TRANSLATING COWL LT (UPPER BORDER) AT 11 O'CLOCK.Jun 16, 2001 · N803DH · Doug DC873SDR CA010625029Hinge · cracked(CAN) DURING AN INSPECTION OF THE FLAP ASSY FOR THE OIL COOLER DOR A 1" CRACK WASFOUND DBETWEEN THE MOUNTING HOLES AND THE HINGE. NEW PART WAS INSTALLED.Jun 13, 2001 · Pilats PC1245SDR QXEA0100925Cowling · chafedPDX - LEFT-HAND LOWER COWL RIGHT-HAND CENTER CHAFE PAD CHAFED. REPAIRED IAW HORIZON AIR EA 2-71-142 AND RD 8-71-018.Jun 8, 2001 · N374PH · Dhav DHC8202SDR QXEA0100924Cowling · chafedPDX - LEFT-HAND LOWER COWL LEFT-HAND CENTER CHAFE PAD CHAGED. REPAIRED IAW HORIZON AIR EA 2-71-142. AND RD 8-71-018.Jun 8, 2001 · N374PH · Dhav DHC8202SDR QXEA0100913Cowling · chafedPDX - RIGHT-HAND LOWER COWL, INBOARD DOOR 423AL FORWARD APERTURE FLANGE ON LOWER COWL STRUCTURE IS CHAFED .625 INCHES LENGTH, .187 INCHES WIDE AND .025 DEEP, LOCATED APPROXIMATELY 3.5" BELOW UPPER LATCH CUT-OUT. REPAIRED IAW DHC-8 SRM 51-40-00 AND HORIZON AIR Jun 6, 2001 · N374PH · Dhav DHC8202SDR RRXA11226Doubler · puncturedDURING A MAINTENANCE VISIT FOUND PUNCTURE DAMAGE TO NR 4 ENGINE O/B T/R COWL INNER HEAT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DC-8 MM 78-31-10 FIG.80Jun 5, 2001 · N606AL · Doug DC873FSDR ASAA0140083Cowling · damagedPAE - DURING C-CHECK, FOUND RIGHT ENGINE INLET COWL OUTSIDE RIGHT SURFACE DAMAGED AT 4 O'CLOCK AND 6 INCHES FORWARD OF AFT FLANGE. REPAIRED IAW ENGINEERING AUTHORIZATION. (M)Jun 4, 2001 · N755AS · Boeing 7374Q8SDR QXEA0100914Pan · crackedPDX - RIGHT-HAND LOWER COWL, FORWARD LEFT-HAND CORNER OF SUMP PAN IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-11.Jun 4, 2001 · N374PH · Dhav DHC8202SDR MALA010623Stiffener · crackedFOUND DURING C-CHECK IN CVG, NR 4 ENGINE NOSE COWL FWD BULKHEAD HAS FOUR STIFFENERS CRACKED (3, 19, 32, 33). MAINTENANCE REMOVED AND REPLACED 4 EACH 3, 9, 32, 33 STIFFENERS P/N HC716H9025-000 IAW SRM 54-10-11.May 31, 2001 · N505XJ · Bac AVRO146RJ85ASDR MALA010621Stiffener · crackedDURING C-CHECK IN CVG, NR 2 COWL FWD BULKHEAD HAS ELEVEN CRACKED STIFFENERS, (3, 12, 13, 14, 16, 17, 19, 27, 28, 29, 32). MAINTENANCE REMOVED AND REPLACED 11 CRACKED STIFFENERS IN NR 2 NOSE COWL FWD BULKHEAD NR 3, 12, 13, 14, 16, 17, 19, 27, 28, 29, 32 WITH BMay 31, 2001 · N505XJ · Bac AVRO146RJ85ASDR MALA010620Stiffener · crackedFOUND DURING C-CHECK IN CVG, NR 3 NOSE COWL HAS FWD BULKHEAD STIFFENERS CRACKED FIVE TOTAL (4, 6, 17, 22, 33). MAINTENANCE REMOVED STIFFENER'S 4, 6, 17, 22, 33, IAW SRM 54-10-11. FABRICATED STIFFENER'S 4, 6, 17, 22, 33 AND REPLACED STIFFENERS 4, 6, 17, 22, 3May 31, 2001 · N505XJ · Bac AVRO146RJ85ASDR QXEA0100946Cowling · damagedYYC - LEFT-HAND UPPER FIXED COWL HAS PROTRUSION ON FRAME 2948. REPAIRED IAW HORIZON AIR EA 4-71-234 AND FOKKER SRM 51-70-01, PAGE 1.May 27, 2001 · N481US · Fokker F28MK4000SDR DL72S010821Door · missingPANEL NR 3 ENGINE OIL SERVICE DOOR MISSING. REPLACED NR 3 OIL SERVICE DOOR.May 22, 2001 · N519DA · Boeing 727232SDR AUS20010502Panel · separated(AUS) RH ENGINE BULLNOSE SECTION LOCATED AFT OF THE ACOUSTIC PANELMISSING FROM AREA BETWEEN NO4 AND NO7 BLOCKER DOORS. THE MISSINGPIECE WAS APPROXIMATELY 2 METERS (6FT) IN LENGTH. DAMAGE CAUSED TO THREE BLOCKER DOORS, COMBUSTOR FAIRING AND BLISTER FAIRING.May 17, 2001 · Boeing 767*SDR AUS20010503Liner · missing(AUS) NR 1 ENGINE LOW POWER. INVESTIGATION FOUND ONE SECTION OF FRONTFAN ACOUSTIC LINING BETWEEN 2 O'CLOCK AND 4 O'CLOCK AREAS MISSING AND ONE AREA OF ICE IMPACT PANEL BETWEEN 1 O'CLOCK AND 5 O'CLOCKAREAS MISSING WITH LOOSE MATERIAL STILL TRAPPED BY THEENGINE.May 15, 2001 · Boeing 747238BSDR MALA010616Stiffener · crackedFOUND DURING C-CHECK IN CVG, NR 4 ENGINE NOSE COWL FWD BULKHEAD HAS THREE STIFFENERS CRACKED (3, 27, 32). MAINTENANCE REPLACED 3 STIFFENERS P/N BAEREF-000025461 IAW BAB SRM 54-10-11 201 IAW SRM 51-42-00.May 11, 2001 · N506XJ · Bac AVRO146RJ85ASDR MALA010615Stiffener · crackedFOUND DURING C-CHECK IN CVG, NR 3 ENGINE NOSE COWL FWD BULKHEAD HAS FOURTEEN CRACKED STIFFENERS. (4, 5, 6, 7, 10, 12, 16, 19, 26, 27, 28, 29, 31, 33). MAINTENANCE REPAIRED STIFFENERS IAW SRM 51-42-00, AND INSTALLED FASTENERS P/N HC716H9025-000 IAW SRM 51-43-0May 11, 2001 · N506XJ · Bac AVRO146RJ85ASDR MALA010614Stiffener · crackedFOUND DURING C-CHECK IN CVG, NR 2 ENGINE NOSE COWL FWD BULKHEAD HAS NINE CRACKED STIFFENERS (3, 4, 7, 10, 19, 27, 28, 32, 33). MAINTENANCE INSTALLED NEW STIFFENERS IAW SRM 54-10-11 201.May 11, 2001 · N506XJ · Bac AVRO146RJ85ASDR MALA010613Stiffener · crackedFOUND DURING C-CHECK IN CVG, NR 1 ENGINE NOSE COWL FWD BULKHEAD HAS FOUR CRACKED STIFFENERS (4, 16, 17, 32). MAINTENANCE REPLACED STIFFENERS IAW SRM 51-42-00 AND INSTALLED NEW FASTENERS P/N HC716H9025-000, IAW SRM 51-43-00.May 11, 2001 · N506XJ · Bac AVRO146RJ85ASDR AUS20010476Panel · separated(AUS) NR 3 ENGINE OGV INFILL PANELS MISSING BETWEEN 4 O'CLOCK AND 6O'CLOCK POSITIONS. DAMAGE TO LH COMPRESSOR CORE PANEL, IP COMPRESSOR BLEED VALVE CONTROL UNIT AIR SENSE PROBE, THRUST REVERSER CORONA AND NO5 AND NO6 THRUST REVERSER BLISTER FAIRINGS.May 11, 2001 · Boeing 747438SDR QXEA0100688Door · dentedPDX- RT ENGINE OUTBOARD AFT COWL DOOR 426AR IS DENTED AND BUCKLED AT LOWER EDGE OF DOOR. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-71-136.May 5, 2001 · N345PH · Dhav DHC8202SDR AUS20010473Fairing · missing(AUS) NR 2 ENGINE LT A' FRAME TO FAN CASE AFT LOWER FAIRING MISSING.May 4, 2001 · Boeing 767*SDR C2XA01BT089Channel · crackedYUL---DURING 4C INSPECTION MAINTENANCE FOUND RT ENGINE TOP COWL TO BE CRACKED IN LT FORWARD CHANNEL. MAINTENANCE REPAIRED COWLING IAW ATR42 SRM 54-12-61 FIGURE 101. AIRCRAFT OK FOR SERVICE.May 2, 2001 · N14825 · Aerosp ATR42320SDR C2XA01BT088Skin · crackedYUL---DURING 4C INSPECTION MAINTENANCE FOUND LT TOP COWLING CRACKED IN LT CORNER. MAINTENANCE REPAIRED COWLING BY FABRICATING EDGING IAW ATR42 SRM 54-12-61 FIGURE 101 AND INSTALLED IAW ATR42 SRM 51-25-01. AIRCRAFT OK FOR SERVICE.May 2, 2001 · N14825 · Aerosp ATR42320SDR AUS20010400Panel · separated(AUS) NR 1 ENGINE ACOUSTIC PANEL TRAILING EDGE SECTION SEPARATED FROMTHE AIRCRAFT. NR 5 BLOCKER DOOR REPLACED DUE TO DAMAGE. NR 7, NR 8 AND NR 9 BLOCKER DOORS HAD MINOR SKIN DAMAGE. NR 7 DEFLECTOR BOX CASCADE VANE DAMAGED.May 1, 2001 · Boeing 767338SDR QXEA0100687Seal · missingPDX- RT ENGINE OUTBOARD FORWARD COWL DOOR 424AR IS MISSING 2 SECTIONS OF RED RUBBER SEAL ON THE INSIDE OF THE DOOR. REPLACED MISSING RED RUBBER SEAL.May 1, 2001 · N345PH · Dhav DHC8202SDR AUS20010406Panel · separated(AUS) NO4 ENGINE VIGV CONTROLLER ACCESS PANEL SEPARATED. DAMAGE CAUSEDTO THE REAR FAN CASE ACOUSTIC LINER.Apr 30, 2001 · Boeing 747238BSDR MALA010424Cowling · looseDURING FLIGHT 2737 OUT OF MSP, LT ENGINE COWLING CAME LOOSE INFLIGHT. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED UPPER FAIRING P/N 7254501-88 AND PROP IAW SAAB 340 JOB CARD 6110-303. REINSTALLED FIGURE 8 COWL AS REQUIRED. RE-SCUFFED METAL, PRIMED Apr 26, 2001 · N106XJ · Saab SF340ASDR AUS20010394Fairing · separated(AUS) NR 3 ENGINE LT AND RT GAS GENERATOR FAIRINGS PNO UL26237 AND PNO UL23239 SEPARATED FROM ENGINE. DAMAGE TO NR 3 ENGINE INTEGRATEDNOZZLE AREA AND RT C' FLAP.Apr 24, 2001 · Boeing 747438SDR DHL2001705506Doubler · damagedAT C-CHECK, NR 3 ENG, LWR COWL INTERNAL SURFACE, RIGHT AFTER 2ND U-BOLT, STRINGER PREVIOUS DOUBLER REPAIR SHOWS BIG HOLE (8 O''CLOCK POS APPROX). REMOVED DAMAGED EXISTING DOUBLER IAW B727 SRM 51-30-2. FABRICATED DOUBLER 8 X 12 2024-0 .050 LOT 471153 PO 83196Apr 18, 2001 · N705DH · Boeing 72722CSDR CA010626020Access Door · missing(CAN) AFTER AIRCRAFT LANDED AT CHICAGO O'HARE, IT WAS NOTICED T HAT THE NOSE COWL LOWER ACCESS PANEL (228-50081-142) WAS ON THE RUNWAY. OTHER DAMAGED PARTS WERE NOSE COWL UPPER ACCESS PANEL 228-50080-158 AND COVER ASSEMBLY 228-50793-120. PRIOR TO THIS EVENT THApr 17, 2001 · Cndair CL6002B19SDR DHL2001705503Angle · crackedAT C-CHECK, NR 2 ENG LT AFT COWL HAS LOWER FWD COENER WITH CRACK ANGLE. REMOVED AND REPLACED NR 2 LT AFT CORNER ANGLE. MATERIAL USED 2024T3 .050 MATERIAL SIZE 12 X 2.5 PO 83112359 LOT 35803 AS PER B727 SRM 51-30-202. TREATED AND PRIMED AREA AS PER B727 SRMApr 17, 2001 · N705DH · Boeing 72722C
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