N278CM

Service difficulty reports not matched to an aircraft · 29

They name N278CM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 n_number = 'N278CM' AND registry_match IS NULL
  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 2023FA0000659Unknown · unknownENG #1 EXHAUST OUTER SLEEVE S/N 0468-A P/N 015T0305-10: NRC M0769 DENT WITH SHARP CREASE IN THE OUTER EXHAUST SKIN LOCATED BT 7-8 O’CLOCK AND BT NAS STA 331.47-337.32. DENT SIZE: 2.42”(A)X0.125(Y) A=2.42” Y=0.125” A/Y RATIO 19.3. Oct 22, 2023 · N278CM · Boeing 76738E · Engine Exhaust SystemSDR 2023FA0000658Unknown · unknownDURING AIRCRAFT CARGO CONVERSION FROM PASSENGER TO FREIGHTER, AIRCRAFT MAINTENANCE DISCOVERED (2 EA) DENTS IN THE OUTER SLEEVE SKIN OF THE #2 ENGINE PRIMARY EXHAUST NOZZLE LOCATED BETWEEN NAC STA 335.2 AND NAC STA 348.94 BETWEEN THE 3 TO 4 O’CLOCK POSITION. Oct 22, 2023 · N278CM · Boeing 76738E · Standard Practices/StructuresSDR 2023FA0000657Unknown · unknownDURING MAINTENANCE INSPECTION AT IAI, FOUND CRACK AND EDGE DAMAGE AT ENG #1, INBD, FWD UPPER SIDE OF THE THRUST REVERSER, RING-OUT. T/R S/N R648-624, P/N 681L272G12, RING-OUT PRESUMED P/N 491B1330003-013.Oct 22, 2023 · N278CM · Boeing 76738E · Engine Thrust ReverserSDR 2023FA0000656Unknown · unknownDURING MAINTENANCE INSPECTION AT IAI, FOUND CRACK AND EDGE DAMAGE AT ENG #1, OUTBD, FWD UPPER SIDE OF THRUST REVERSER, RING-OUT. THRUST REVERSER S/ N: R647-1020. THRUST MODEL NO: TR-CF6-F28FG10. RING-OUT PRESUMED P/N: 491B1330003-013.Oct 22, 2023 · N278CM · Boeing 76738E · Engine Thrust ReverserSDR 2023FA0000655Unknown · unknownFWD CARGO – LOWER FRAME – STA 412, LBL 34: SHOP MISTAKENLY DAMAGED LOWER LOBE FRAME WEB AT THE NOTED LOCATION. DAMAGE SIZE: 0.4”X0.6”.Oct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000654Unknown · unknownDURING MAINTENANCE INSPECTION SHOP FOUND ON ENG #1, THRUST REVERSER, AT JUNCTION OF TWO (2) PANELS, LOWER REAR PART, MISSING FILLER MATERIAL. DAMAGES DIMENSIONS: LENGTH: 2.6”, WIDTH: 1.2”.Oct 22, 2023 · N278CM · Boeing 76738E · Engine Exhaust SystemSDR 2023FA0000653Unknown · unknownDURING MAINTENANCE INSPECTION SHOP FOUND ON ENG #2, STRUT INBD SIDE (LEFT), UNDOCUMENTED DOUBLER REPAIR ON PANEL 447ELX OUTER SKIN, B/T NAC STA 296 & NAC STA 302. EXISTING REPAIR DIMENSIONS: FILLER: 1.5”X5.5”; DOUBLER: 6.7”X5”.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000652Unknown · unknownENGINE #2 INLET COWL: FOUND DENTS BEYOND OF SRM 54-12-01 LIMITS ON THE EXTERIOR NOSE LE SKIN OF THE INLET COWL. DENT NO 1 – LOCATED 12 O’CLOCK 15” FROM THE AFT LIP A=0.88”, Y=0.047”, A/Y=18; DENT NO 2Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000651Unknown · unknownDURING MAINTENANCE INSPECTION AT IAI, FOUND CRACK AND EDGE DAMAGE AT ENG#2, INBD, FWD UPPER SIDE OF THRUST REVERSER, RING-OUT. THRUST REVERSER S/N R649-112, P/N 681L269G07. RING-OUT PRESUMED P/N 491B1330003-013.Oct 22, 2023 · N278CM · Boeing 76738E · Engine Thrust ReverserSDR 2023FA0000650Unknown · unknownENGINE #2, CORE COWL, BETWEEN NAC STA 293.25 – NAC STA 298.75: DURING AIRCRAFT CONVERSION MAINTENANCE INSPECTIONS, FOUND AN EXISTING UNDOCUMENTED DOUBLER REPAIR ON THE INBOARD SIDE OF THE #2 ENGINE, CORE COWL AT THE TITANIUM FAIRING CUTOUT AREA. THE DOUBLER REOct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000649Unknown · unknownDURING AIRCRAFT MAINTENANCE INSPECTION, SHOP FOUND THREE UNDOCUMENTED EXISTING FILLER REPAIRS AND MULTIPLE NEW DENTS ON #1 INLET COWL ACOUSTIC PANELS.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000648Unknown · unknownSEC #46, STA 1197+124 – 1197+134, STR 1L-2L: DURING AIRCRAFT SURVEY AN EXISTING REPAIR WAS FOUND PER DOCUMENTATION THE REPAIR SHOULD BE LOCATED AT STA 1197+110, STR 1L-2L, HOWEVER THE ACTUAL LOCATION OF THE REPAIR IS BETWEEN STA 1197+124 TO STA 1197+134, STR-1Oct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000647Unknown · unknownSTRUT #1, OUTB’D SIDE, NAC STA 304.54 NWL 134: DURING AIRCRAFT SURVEY SHOP FOUND UNDOCUMENTED REPEIR OF 3.2”X1.2” IN AFT FAIRING PANEL.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000646Unknown · unknownDURING MAINTENANCE INSPECTION SHOP FOUND ON ENG #1, THRUST REVERSER, AT JUCTION OF BOTH SIDE OF C-DUCT, LOWER REAR PARTS, MISSING FILLER MATERIAL. DAMAGES DIMENSIONS: LENGTH: 3”, WIDTH: 1”.Oct 22, 2023 · N278CM · Boeing 76738E · Engine Exhaust SystemSDR 2023FA0000645Unknown · unknown: INLET COWL – ACOUSTIC DYNAROHR PANEL: DURING MAINTENANCE ON AIRCRAFT, IAI’S SHOP FOUND A DENT AT INLET COWL – INNER BARREL ACOUSTIC PANEL OF ENG #2, RIGHT HAND, UPPER SEGMENT, BETWEEN 3-4 O’CLOCK. THE DENT LOCATED 7” FROM PANEL EDGE. DENT SIZE: Y=0.013”, A/Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000644Unknown · unknownDURING MAINTENANCE INSPECTION AT IAI, FOUND DOCUMENTED REPAIR AT SEC 48, STA 1725.5, STR 6R-8R. THE REPAIR WAS REMOVED TO REPLACE PARTS. SHOP HAS FOUND THE REPAIR ISN’T PER SRM 53-80-01, REPAIR5, DETAIL III AS ACCLAIMED AT THE DOCUMENT. THE CUTOUTS PREFORMED WOct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000643Unknown · unknownRFTA 02937-0229; FVCI SERVICE REQUEST; BOEING 767-300 SRM 54-52-70 IDENTIFICATION; BOEING 767-300 SRM 54-52-70 ALLOWABLE DAMAGE 1; BOEING 767-300 SRM 54-52-70 REPAIR4; DWG 313T2381; FVCI EO 23149-26 REV. “IR” DATE: 09/13/2023.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000642Unknown · unknownDURING CONVERSION AT IAI, SHOP MISTAKENLY PEELED WEB OF LOWER FWD CARGO FRAME AT STA 412, RBL 25. DAMAGE SIZE: 0.6”X1.1”. SINCE THERE IS NO APPLICABLE REPAIR FOR THE REPORTED DAMAGE IN BOEING SRM, IAI ENGINEERING ASSESSED FVCI FOR REPAIR INSTRUCTIONS.Oct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000641Unknown · unknownDURING AIRCRAFT CARGO CONVERSION FROM PASSENGER TO FREIGHTER, AIRCRAFT MAINTENANCE DISCOVERED AN EXISTING UNDOCUMENTED FUSELAGE SKIN REPAIR LOCATED BETWEEN APPROXIMATE STATIONS 1583 AND 1629, BETWEEN S29L AND S34L, MEASURING APPROXIMATELY 46.7”X19.3”, AS NOTEDOct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000640Unknown · unknownSTRUT #1, OUTBD SIDE, NAC STA 296-302, NWL 145: DURING AIRCRAFT SURVEY SHOP FOUND TWO (2) UNDOCUMENTED DOUBLER REPAIRS IN ACCESS PANEL 437ELX.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000639Unknown · unknownBETWEEN NAC STA 304.6 – NAC STA 310.6: DURING MAINTENANCE INSPECTIONS ON DATUM AIRCRAFT FOUND EXISTING REPAIR ON THE OUTER SKIN PANEL LOCATED ON THE OUTBOARD SIDE OF STRUT # 2. THE SIZE OF THE REPAIR IS 6.1”X5”. NO DOCUMENTATION WAS FOUND FOR THIS REPAIR.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000638Unknown · unknownBETWEEN NAC STA 304.6 – NAC STA 310.6: DURING MAINTENANCE INSPECTIONS ON DATUM AIRCRAFT FOUND EXISTING REPAIR ON THE OUTER SKIN PANEL LOCATED ON THE OUTBOARD SIDE OF STRUT # 2. THE SIZE OF THE REPAIR IS 6.1”X5”. NO DOCUMENTATION WAS FOUND FOR THIS REPAIR.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000637Unknown · unknownSEC # 41, STA 287, WL 135, RBL 6: DURING AIRCRAFT SURVEY SHOP FOUND A CRACK IN VERTICAL STIFFENER, NOSE WHEEL WELL STRUCTURE.Oct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000636Unknown · unknownENGINE #1 RH FAN COWL AT IAI IN TLV, MAINTENANCE FOUND AN EXISTING DOUBLER REPAIR ON THE OIL TANK ACCESS DOOR AROUND THE LATCH LOCATED ON THE FAN COWL SKIN OUTBD ENG #2 BT NAC STA 159-161.8 AT 3 O’CLOCK. REPAIR SIZE: 2.8”X2.8”. FAN COWL S/N:Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000635Unknown · unknownENGINE #1 RH FAN COWL, OIL ACCESS DOOR LATCH: DURING CONVERSION AT IAI IN TLV, MAINTENANCE FOUND AN EXISTING DOUBLER REPAIR ON THE OIL TANK ACCESS DOOR AROUND THE LATCH LOCATED ON THE FAN COWL SKIN INBD ENG#1 BT NAC STA 159-161.8 AT 3 O’CLOCK. REPAIR SIZE: 2.8Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000634Unknown · unknownDURING MAINTENANCE INSPECTION AT IAI, FOUND EXISTING DOCUMENTED (FL 1267 30372) DOUBLER REPAIR AT STA 303 BETWEEN STR 22R-24R. THERE IS A MISMATCH BETWEEN THE DOCUMENT AND THE POSITION OF THE DOUBLER ON A/C. ACCORDING TO FL 1267 30372, THE DOUBLER LOCATION IS Oct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000633Unknown · unknownSTRUT #2 BETWEEN NAC STA 294.2 TO NAC STA 304.5: DURING MAINTENANCE INSPECTION, FOUND TWO DOUBLER REPAIRS ON ACCESS PANEL 446CL LOCATED ON THE INBOARD SIDE OF STRUT #2 IN THE OUTER SKIN PANEL’S LOWER AND UPPER EDGES. Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000632Unknown · unknownDURING MAINTENANCE INSPECTION AT IAI, FOUND EXISTING DOUBLER REPAIR AT ENG #2, THRUST REVERSER SKIN (ON TRACK FAIRING), OUTBD SIDE, NAC STA 201.5 – 214.5, 1 (ONE) O’CLOCK. THRUSTOct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000631Unknown · unknownFUSELAGE SKIN – STA 1219, BETWEEN S-5R AND S-7R: DURING AIRCRAFT INSPECTION, SHOP FOUND AN EXISTING FASTENER REPAIR LOCATED 0.294” FROM BUTT SPLICE AT STA 1219. THE FASTENER WAS REMOVED. HOLE DIAMETER: 0.265”.Oct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)
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