Boeing 727-2Q9

Service difficulty reports · 830

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = '7272Q9'
  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 95ZZZW380Stringer · crackedDURING D-CHECK, FORWARD CARGO COMPARTMENT STATION 500 STRINGER 23, STRINGER IS CRACKED AND DAMAGED. STOP DRILLED CRACK AS PER SRM 53-10-3 AND INSTALLED REPAIR AS PER SRM 53-10-3 12 INCHES BY 2 INCHES. TOTAL CYCLES 29,235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW379Stringer · crackedDURING D-CHECK, FORWARD CARGO COMPARTMENT STATION 500 STRINGER 25L, STRINGER IS DAMAGED AND CRACKED. STOP DRILLED CRACK AS PER SRM 53-10-3 AND INSTALLED REPAIR AS PER SRM 53-10-3 12 INCHES BY 2 INCHES. TOTAL CYCLES 29,235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW378Stringer · crackedDURING D-CHECK, FORWARD CARGO COMPARTMENT STATION 500 STRINGER 24L, STRINGER IS CRACKED. STOP DRILLED CRACK AS PER SRM 53-10-3 AND INSTALLED REPAIR AS PER SRM 53-10-3 12 INCHES BY 2 INCHES. TOTAL CYCLES 29,235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW377Stringer · crackedDURING D-CHECK, FORWARD CARGO COMPARTMENT STATION 500 STRINGER 21L, STRINGER IS CRACKED. REPLACED DAMAGE SECTION AS PER SRM 53-10-3. TOTAL CYCLES 29,235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW376Stringer · crackedDURING D-CHECK, FORWARD CARGO COMPARTMENT STATION 500 STRINGER 20L, STRINGER IS DAMAGED. STOP DRILLED CRACK AS PER SRM 53-10-3 AND INSTALLED REPAIR AS PER SRM 53-10-3 12 INCHES BY 2 INCHES. TOTAL CYCLES 29,235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW375Stringer · gougedDURING D-CHECK, FORWARD CARGO COMPARTMENT STATION 540, DAMAGED TO STRINGER 21L, GOUGED. GOUGE STOP DRILLED PER SRM 51-10-1, FABRICATED REPAIR DOUBLER CHANNEL PER SRM 53-10-3 .063 7075-T6, TREATED AND PRIMED PER SRM 51-10-2, REPAIR DOUBLER INSTALLED PER SRM 53Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW374Frame · crackedDURING D-CHECK, FRAME UPPER FLANGE CRACKED TWO PLACES BS 560 BETWEEN STRINGER 29L TO OUTBOARD OF 29R. STOP DRILLED CRACKS AS PER SRM 51-10-1. REMOVED DAMAGED AREA AS PER SRM 53-10-4. FABRICATED FILLER 7075-T6 1 INCH BY 3 INCH BY 30 INCHES AS PER SRM 53-10-Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW373Frame · crackedDURING D-CHECK, FRAME UPPER FLANGE CRACKED BS 620 BETWEEN STRINGER 28L NUMEROUS AREAS. REMOVED FASTENERS PER SRM 51-30-2. CUT OUT DAMAGED AREA (3 PLACES) PER SRM 53-10-4 FIG 1. INSTALLED FRAME AND REPAIR AND PER SRM 53-10-4 FIG 1 AND SRM 51-30-2. SIZE 24 IFeb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW372Frame · crackedDURING D-CHECK, FRAME UPPER FLANGE CRACKED BS 660 ABOVE STRINGER 28R, ALSO GUSSET NOT ATTACHED TO 'Z' ANGLE. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED DOUBLER 7075-T6 .063 8 INCHES BY 4 INCHES. INSTALLED DOUBLER PER SRM 51-40-2 AND INSTALLED FASTENERS Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW371Frame · crackedDURING D-CHECK, FRAME UPPER FLANGE CRACKED BS 700 BETWEEN STRINGER 29L AND 29R. STOP DRILLED CRACK PER SRM 51-10-1, FABRICATED REPAIR DOUBLER .063 7075-T6 PER SRM 51-40-3, TREATED AND PRIMED DOUBLER, WET PER SRM 51-40-3 AND SRM 51-20-4, SIZE 1 INCH BY 3 INCH Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW370Skin · material lossDURING D-CHECK, 10 PERCENT SKIN LOSS NOTED BS 360 RT AFT ROW OF FASTENERS BETWEEN STRINGER 4 AND STRINGER 5. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER REPAIR PER SRM 43-30-3. DOUBLER SIZE 7 INCHES BY 15 INCHES 2024-T3 .071. TOTAL CYCLES 29,235. (W)Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW369Angle · bentDURING D-CHECK, FORWARD CARGO DOOR CUT OUT STATION 590 STRINGER 26 RT SUPPORT AND 'L' ANGLE ARE BENT. DAMAGED ANGLES REMOVED PER SRM 51-10-1, FABRICATED ANGLES PER SRM 51-40-4, TREATED AND PRIMED PER SRM 51-10-2, INSTALLED ANGLES PER SRM 51-10-1 4 INCHES BY 4Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW368Angle · corrosionDURING D-CHECK, FORWARD CARGO DOOR CUT OUT, AFT BOTTOM CORNER 'L' ANGLE HAS CORROSION, LOCATED JUST ABOVE TIE DOWN STATION 620 STRINGER 26R. FABRICATED NEW 'L' ANGLE PER SRM 51-10-5 .063 2024-T3 2 INCH BY 1 INCH BY 2 INCH. TREATED AND PRIMED PER SRM 51-10-2 Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW367Frame · corrosionDURING D-CHECK, CORROSION FRAME LOWER FLANGE BS 1166 BETWEEN STRINGER 29L AND 27L. REMOVED CORROSION FOUND OUT OF LIMITS, REMOVED CLIP AND INSTALLED NEW CLIP AS PER SRM 51-10-1 PART 4. TOTAL CYCLES 29,235. (W)Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW366Support · corrosionDURING D-CHECK, VERTICAL SUPPORT BEAM FORWARD OF BS 1183 CORROSION STRESS CRACK AT BOTTOM ATTACHMENT LUG JUST INBOARD OF STRINGER 26L. REPAIR INSTALLED PER SRM 727-53-0181 AND DRAWING NR 65C33724. TOTAL CYCLES 29,235. (W)Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW365Stringer · corrosionDURING D-CHECK, AFT CARGO STATION 1175 STRINGER 22L, CORROSION ON STRINGER. REMOVED FASTENERS, REMOVED STRINGER, REMOVED CORROSION. ALODINE AND PRIMED AND INSTALLED STRINGER NEW 30.5 INCH, INSTALLED FASTENERS, PER SRM 51-30-2, 53-10-1, 51-10-6, 51-10-2, 53-1Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW364Intercostal · crackedDURING D-CHECK, AFT CARGO RT STATION 1030-1050 STRINGER 25R INTERCOSTAL IS BENT AND CRACKED. STOP DRILLED CRACK AS PER SRM 51-10-1, INSTALLED DOUBLER AS PER SRM 51-40-2 2024-T3 .050 4.5 INCH BY 5.5 INCH. TOTAL CYCLES 29,235. (W)Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW363Beam · corrosionDURNG D-CHECK, NOSE COMP RT HORIZONTAL WALKWAY BEAM CHORD HAS CORROSION STATION 294-328 RT. CLEANED CORROSION PER SRM 51-10-6. FOUND OUT OF LIMITS STATION 294 TO 299. FABRICATED REPAIR PARTS PER SRM 51-40-4, .125 INCH BY 9 INCH BY 4 INCH, 7075-T6, TREATED WFeb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW362Skin · corrosionDURING D-CHECK, CORROSION ON STRINGER 30 BETWEEN BS 1030 AND BS 1050, ALSO SKIN SURFACE ADJACENT TO STRINGER. REMOVED FASTENERS PER SRM 51-30-2. REMOVED CORROSION PER SRM 51-10-6, TREATED AND PRIMED PER SRM 51-10-2. REPLACED PARTS (FAB) PER SRM 51-10-1, SEAFeb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW361Frame · corrosionDURING D-CHECK, CORROSION ON FRAME BS 990 LOWER FLANGE AND AFT SIDE SHEER CLIPS. ALSO, STRINGERS BETWEEN 30 AND 28L. INSTALLED BETWEEN STRINGER 28L AND 30L ANGLE REPAIR AS PER SRM 51-40-3 2024-T3 .071 7.5 INCHES BY 3.5 INCHES. REPLACED CLIPS PER SRM 51-30-2Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW360Frame · corrosionDURING D-CHECK, CORROSION FOUND ON FORWARD SIDE OF FRAME AND LOWER FLANGE FROM STRINGER 27L TO STRINGER 28R BS 970. REMOVED FASTENERS FROM STRINGER 27L TO STRINGER 28R BS 970 PER SRM 51-30-2. REMOVED CORROSION AS PER SRM 51-10-6, OUT OF LIMITS, CLIP FROM STRFeb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW359Support · corrosionDURING D-CHECK, CORROSION ON DOOR CUTOUT SUPPORT JUST AFT OF BS 950E BETWEEN STRINGER 30 AND 27R. REMOVED FASTENERS FOR ACCESS, REMOVED CORROSION AS PER SRM 51-10-6, BEYOND LIMITS, CUT OUT DAMAGE AREA AS PER SRM 53-10-4 AND INSTALLED REPAIR 3 INCH BY 5 INCH AFeb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW358Frame · corrosionDURING D-CHECK, CORROSION ON FORWARD SIDE OF FRAME BS 480 BETWEEN STRINGER 28L AND 29L. REMOVED CORROSION PER SRM 51-10-06, OUT OF LIMITS. REMOVED DAMAGE AREA AS PER SRM 51-40-3. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 1 INCH BY 1 INCH BY 6 INCHES 2024-T3 .Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW357Stringer · crackedDURING D-CHECK, LOWER NOSE COMP STATION 328 STRINGER 22R CORROSION AND CRACK ON STRINGER. CUT DAMAGE AREA AND REPAIRED WITH SPLICE REPAIR AS PER SRM 53-10-3. REPLACED 14.5 INCHES OF STRINGER WITH TWO SPLICES OF 10 INCHES EACH. TOTAL CYCLES 29,235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW356Angle · corrosionDURING D-CHECK, RT CHORD ANGLE BULGING AT STATION 350 NOSE W/W AREA. REMOVED CHORD ANGLE AND CLEAN AREA PER SRM 51-50-1, TREATED AREA PER SRM 51-10-2, INSTALLED CHORD ANGLE PER SRM 51-10-1. TOTAL CYCLES 29,235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW355Floor Beam · corrodedDURING D-CHECK, FLOOR BEAM UPPER FLANGE CORRODED BS 1130 LBL 24. CORROSION CLEANED, FOUND OUT OF LIMITS, REPAIRED AS PER SRM 51-40-4 1 INCH BY 1 INCH BY 12 INCH 7075-T6 .125. TOTAL CYCLES 29,235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW354Stringer · corrosionDURING D-CHECK, CORROSION ON STRINGER 29R AFT OF BS 950E. REMOVED CORROSION AS PER SRM 51-10-6. FOUND CORROSION CRACK, STOP DRILLED AS PER SRM 51-10-1. ALODINED AND PRIMED AS PER SRM 51-10-2. INSTALLED REPAIR AS PER SRM 51-40-4 2 INCHES BY 2 INCHES 14 INCHFeb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW353Chord · corrosionDURING D-CHECK, CORROSION AT UPPER T/E CHORD LOWER SIDE OUTBOARD END (LT STABILIZER). REMOVED CORROSION PER SRM 51-10-06, ALODINE AND PRIMED PER SRM 51-10-2, CORROSION OUT OF LIMITS, INSTALLED DOUBLER REPAIR PER SRM 5-10-6, REPAIR 2 INCHES BY 33 INCHES 2024-TFeb 20, 1995 · N741DH · Boeing 7272Q9 · Horizontal Stabilizer StructureSDR 95ZZZW417Spar · corrosionDURING D-CHECK, THE LT WING SPAR LOWER CHORD CORRODED FROM FS 188 TO 203. REMOVED CORROSION PER SRM 51-10-6. INSTALLED DOUBLER REPAIR PER SRM 51-40-4 FIG 1. REPAIR SIZE 2 INCHES BY 14 INCHES. TOTAL CYCLES 29235.Feb 2, 1995 · N741DH · Boeing 7272Q9 · Wing SparSDR 95ZZZW399Angle · corrosionDURING D-CHECK, FLOOR BOARD ATTACHMENT ANGLE RBL 64 BS 380 TO BS 420 HAS CORROSION TOP AND BOTTOM SIDES. REMOVED ANGLE PER SRM 51-30-2. REMOVED CORROSION AROUND ANGLE AREA PER SRM 51-10-6. MATERIAL LOSS 0.002, FABRICATED ANGLE PER SRM 51-10-1 2024-T3 .063. Feb 2, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous Structure
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