Boeing 727-2M7

Service difficulty reports · 459

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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 = '7272M7'
  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 K11A2014022472609Window Frame · corrodedCORROSION ON WINDOW FRAME BS 720C.Feb 6, 2014 · N726CK · Boeing 7272M7 · Fuselage Main, StructureSDR K11A2014022472608Window Frame · corrodedCORROSION ON WINDOW FRAME LT BS 720A.Feb 6, 2014 · N726CK · Boeing 7272M7 · Fuselage Main, StructureSDR K11A2014022472607Window Frame · corrodedCORROSION ON WINDOW FRAME, BS 720F.Feb 6, 2014 · N726CK · Boeing 7272M7 · Fuselage Main, StructureSDR K11A2014022472606Window Frame · corrodedCORROSION ON WINDOW FRAME RT BS 950E.Feb 6, 2014 · N726CK · Boeing 7272M7 · Fuselage Main, StructureSDR K11A2014022472603Stringer · corrodedSTRINGER 26L CORRODED AT BS 679.Feb 4, 2014 · N726CK · Boeing 7272M7 · Fuselage Main, Longeron/StringerSDR K11A2014022472605Stringer · corrodedSTRINGER 27L CORRODED AT BS 561.Jan 31, 2014 · N726CK · Boeing 7272M7 · Fuselage Main, Longeron/StringerSDR K11A2014022472602Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 700 BETWEEN S27-28R.Jan 31, 2014 · N726CK · Boeing 7272M7 · Fuselage Internal Mounting StructureSDR K11A2014022472604Stringer · corrodedSTRINGER 28L CORRODED AT BS 600.Jan 30, 2014 · N726CK · Boeing 7272M7 · Fuselage Main, Longeron/StringerSDR K11A2014022472601Frame · corrodedRIGHT WHEEL WELL OTBD SIDE BS 900, FWD SIDE OF VERTICAL FRAME ANGLE HAS CORROSION.Jan 30, 2014 · N726CK · Boeing 7272M7 · Fuselage Main, FrameSDR K11A2011111572601Pump · shearedENGINE NR 1 FLAME OUT DURING TAKEOFF AT 80 KNOTS, ALL PARAMETERS WERE NORMAL UNTIL FLAME OUT OCCURED. CREW ADVICED TOWER CLEARED RUNWAY AND RETURNED BACK TO BLOCKS. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP AND DISCOVERED THE SHAFT SHEARED OFF. PERFORMED LNov 15, 2011 · N726CK · Boeing 7272M7 · Engine Fuel PumpSDR K11A2011100472603Web · damagedWEB DAMAGE, L1 DOOR STA 228 LBL 60 .5X.5 INCHES.Sep 14, 2011 · N726CK · Boeing 7272M7 · Fuselage Miscellaneous StructureSDR K11A2011100372603Floor Support · corrodedE&E BAY FLOOR SUPPORT AT L1 DOOR HAS CORROSION, 1X2 INCHES.Sep 8, 2011 · N726CK · Boeing 7272M7 · Fuselage Miscellaneous StructureSDR K11A2011100372602Stringer · corrodedFWD PIT STRINGER CORROSION IN CENTER .5X3 INCHES (STA 720+10 STR 25 RT).Sep 7, 2011 · N726CK · Boeing 7272M7 · Fuselage Main, Longeron/StringerSDR K11A2011100372601Floorbeam · corrodedAFT PIT, CORROSION ON BOTTOM OF FLOORBEAM PREVIOUS REPAIR, CORROSION 2X3 INCHES.Sep 7, 2011 · N726CK · Boeing 7272M7 · Fuselage Main, Floor BeamSDR K11A2011100472604Seal Ring · corrodedAFT CARGO DOOR (FWD PRESSURE RELIEF DOOR) INNER SEAL RING CORRODED .25X2 INCHES.Sep 3, 2011 · N726CK · Boeing 7272M7 · Cargo/Baggage DoorsSDR K11A2011100472601Doubler · corrodedAFT PIT DOOR OUTER AFT SUPPORT ANGLE DOUBLER CORRODED, .5X1 INCHES.Sep 2, 2011 · N726CK · Boeing 7272M7 · Cargo/Baggage DoorsSDR K11A2011100472602Angle · crackedEVIDENCE OF A CRACK ON VERTICAL ANGLE, RT WW STA 870 BL 0 25 INCHES BELOW PRESSURE DECK. CRACK .75 INCHES.Aug 31, 2011 · N726CK · Boeing 7272M7 · Fuselage Miscellaneous StructureSDR K11A2011042072601Shaft · shearedENGINE NR 2 LOW OIL PRESSURE LIGHT CAME ON IN FLIGHT, OIL PRESSURE GAUGE ALSO INDICATED NO OIL PRESSURE, CREW PERFORMED PRECAUTIONARY ENGINE SHUTDOWN IAW PROCEDURES AND DIVERTED TO AND LANDED. R & R NR2 ENG MAIN OIL PUMP IAW MM 72-00-61-03-011 AND 72-00-61-43Apr 20, 2011 · N726CK · Boeing 7272M7 · Turbine Engine Oil SystemSDR K11A2010121372610Seat Track · corrodedSEAT TRACK FLANGE HAS CORROSION, 40 INCHES.Nov 9, 2010 · N726CK · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR K11A2010121472602Stiffener · crackedSTIFFENER CRACKED AT STA 1183 BULKHEAD. REMOVED AND REPLACED STIFFENER.Nov 7, 2010 · N726CK · Boeing 7272M7 · Fuselage Main, BulkheadSDR K11A2010121372609Seat Track · corrodedSEAT TRACK FLANGE HAS CORROSION, 2 INCHES.Oct 18, 2010 · N726CK · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR K11A2010121372608Seat Track · corrodedSEAT TRACK FLANGE HAS CORROSION, 8 INCHES.Oct 18, 2010 · N726CK · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR K11A2010121372607Seat Track · corrodedSEAT TRACK FLANGE HAS CORROSION.Oct 18, 2010 · N726CK · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR K11A2010121372606Seat Track · corrodedSEAT TRACK FLANGE HAS CORROSION, 21 INCHES.Oct 18, 2010 · N726CK · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR K11A2010121372605Seat Track · corrodedSEAT TRACK FLANGE HAS CORROSION, 10 INCHES.Oct 18, 2010 · N726CK · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR K11A2010121372604Seat Track · corrodedSEAT TRACK FLANGE HAS CORROSION, 68 INCHES.Oct 18, 2010 · N726CK · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR K11A2010121372601Seat Track · corrodedSEAT TRACK FLANGE HAS CORROSION, 100 INCHES LONG.Oct 18, 2010 · N726CK · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR K11A2010121372603Seat Track · corrodedSEAT TRACK FLANGE HAS CORROSION.Oct 16, 2010 · N726CK · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR K11A2010121372602Seat Track · corrodedSEAT TRACK FLANGE HAS CORROSION, 78 INCHES LONG.Oct 16, 2010 · N726CK · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR K11A2010121472601Rib · crackedVERTICAL STAB RIB CRACKED, LT SIDE AT STA 133.8.Oct 9, 2010 · N726CK · Boeing 7272M7 · Vertical Stabilizer, Spar/RibSDR K11A2010121372611Pin · damagedRT AFT BOTTLE PIN DAMAGED.Oct 1, 2010 · Boeing 7272M7 · Wing Miscellaneous StructureSDR DHLA200800120Light · loosePILOT REPORT, EMERGENCY EXIT LIGHTS ILLUMINATE PERIODICALLY WITH SWITCH IN THE ARMED POSITION. RESOLUTION, CONFIRMED. RESEATED COCKPIT EMERGENCY EXIT LIGHT. OPS CHECKS GOOD IAW MM 33-50-01.Nov 1, 2008 · N750DH · Boeing 7272M7 · Emergency LightingSDR DHL2008F00031Light · inoperativeL1 DOOR EMER EXIT LIGHT INOP. R&R EMER EXIT LIGHT ASSY OPS CHECK GOOD IAW MM 33-50-71. ACFT WAS GROUNDED. FLIGHT NR 820.Aug 26, 2008 · N750DH · Boeing 7272M7 · Emergency LightingSDR DHL2008F00029Skin · crackedL1 DOOR FRAME 303 9 CRACK ON INBOARD FASTENER HOLE INSIDE UPPER HINGE CUTOUT. REPAIRED L-1 DOOR FRAME BS 303.95 UPPER HINGE CUTOUT IAW EVA B253-00089 REV IR DATED 2 JULY 08 AND BOEING TELEX 1-864663355-15 WITH REPAIR SKETCH 1-864663355-12, FABRICATED CLIP ANGJul 8, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, Plate/SkinSDR DHL2008F00023Skin · corrodedLT WHEEL WELL BS 931.5 ABOVE STRINGER 18A CORROSION SPOT SKIN BLOWN WBL 70.5. INSTALLED REPAIR PARTS AT LT WHEEL WELL BS 931 5 ABOVE STRINGER 18A AREA WBL 70 5 IAW EVA B253-00083 REV 01 DATED 1 JULY 08 AND AVENGER REPORT AAS-SSR-08-017 REV B DATED JUNE 30, 20Jul 6, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, Plate/SkinSDR DHL2008F00028Skin · gougedFUSELAGE INNER SKIN BELOW UPPER HINGE IS GOUGED BS 303 STRINGER 12L TO 306.65 LT HAND. FABRICATED REPAIR AND INSTALLED IAW EVA B253-00086 REV 03 DATED 2 JULY 08 AND BOEING REPAIR SKETCH 1-364663355-12 IN CONJUNCTION WITH BOEING TELEX 1-864663355-B DATED 6-23-Jul 3, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, Plate/SkinSDR DHL2008F00015Angle · corrodedL-2 DOOR TAP INTERIOR ANGLE SUPPORT AND WEB ARE CORRODED (EXFOLIATION) BS 1040/1065. REMOVED AND REPLACED L-2 DOOR UPPER ANGLE SUPPORT WEB BEAM IAW B727 SRM 51-30-2 AND BOEING DRAWING 65-56992 REV V DATED 3/26/01. (A)Jun 26, 2008 · N750DH · Boeing 7272M7 · Passenger/Crew DoorsSDR DHL2008F00018Web · crackedL-1 DOOR LOWER FORWARD CORNER OF WEB HAS CRACK. CUT OUT DAMAGE L-1 DOOR LOWER FORWARD CORNER WEB IAW B727 SRM 51-40-3 FIG 1. FABRICATED DOUBLER REPAIR AND INSTALLED IN L-1 DOOR IAW EVA B252-00082 REV IR DATED 6/19/08. (A)Jun 25, 2008 · N750DH · Boeing 7272M7 · Passenger/Crew DoorsSDR DHL2008F00010Web · crackedL-1 DOOR LOWER FORWARD BOTTOM OF DOOR HAS CRACKED WEB. INSTALLED NEW LOWER WEB FROM L-1 DOOR WITH MATERIAL 7075-T6 .075 SIZE 37 5 X 8 AND PO 9007406 IAW B727 SRM 51-30-2 52-10-1 FIG 1 AND 51-10-1. (A)Jun 23, 2008 · N750DH · Boeing 7272M7 · Passenger/Crew DoorsSDR DHL2008F00014Keelbeam · corrodedSURFACE CORROSION FRONT LOWER CHORD CENTER OF KEEL BEAM BS 740. REMOVED AND REPLACED BS 740 LOWER CHORD T ANGLE P/N 69-4711Y2, PO 8180132 IAW B727 SRM 51-30-2. T-ANGLE ORIGINAL EVALUATED OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. (A)Jun 22, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, KeelSDR DHL2008F00021Beam · misinstalledHORIZONTAL WALKWAY BEAM LOWER CHORD LT SIDE, HAS SEVERAL FASTENERS BUCK TAIL FLAT, ALSO IMPROPER SIZE FASTENERS BETWEEN BS 312 AND BS 328. REMOVED AND REPLACED HORIZONTAL WALKWAY LOWER LT CHORD BS 312 TO 328 IAW B727 SRM 51-30-2. P/N 65-19861-7 (A)Jun 19, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, StructureSDR DHL2008F00011Shear Tie · crackedSHEAR TIE CRACKED AT HORIZONTAL WALKWAY BEAM AREA BS 328 STRINGER 26L. REPAIRED SHEAR TIE AT HORIZONTAL WALKWAY BEAM BS 328 STRINGER 26L IAW B727 SRM 53-10-4 FIG 15. (A)Jun 19, 2008 · N750DH · Boeing 7272M7 · Fuselage Internal Mounting StructureSDR DHL2008F00009Skin · bulgedBULGE AT BS 660 AND STRINGER 27R EXTERIOR SKIN. REMOVED FASTENERS AND SHEAR TIE, TEE AT BS 660 AND STRINGER 27R IAW B727 SRM 51-30-2. FOUND SHEAR TIE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. INSTALLED NEW PART WITH P/N 6943683-5 AND PO 8180177 IAW B727 SRMJun 16, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, Plate/SkinSDR DHL2008F00026Channel · corrodedCORROSION, NOSE GEAR TRUNNION WELL LT FORWARD C-CHANNEL BS 303. REMOVED CORROSION ON LT FORWARD C-CHANNEL BS 303 IAW B727 SRM 51-10-6. EVALUATED OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED AND REPLACED C-CHANNEL IAW B727 SRM 51-30-2. (A)Jun 13, 2008 · N750DH · Boeing 7272M7 · Fuselage Miscellaneous StructureSDR DHL2008F00027Stringer · corrodedEXFOLIATED CORROSION ON STRINGER 28L CHANNEL BETWEEN BS 620 AND BS 640. REPAIRED STRINGER BS 620-640 STRINGER 28L IAW B727 SRM 53-10-3 FIG 1 DETAIL 1. (A)Jun 12, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, Longeron/StringerSDR DHL2008F00022Stringer · crackedSTRINGER 15R IS CRACKED AT BS 720B + 5 INCHES. CUT OUT DAMAGE AREA DIMENSION .625 AT STRINGER 15R 720B IAW SRM 53-10-3 FIG 5. FABRICATED CHANNEL USING 7075-T6 040 PO 9007282 DIMENSION 5.125" X 1" X 1", RADIUS FILLER USING 7075-T6 .090 PO 9006162 DIMENSION 2.Jun 12, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, Longeron/StringerSDR DHL2008F00012Seat Track · corrodedCABIN SEAT TRACK BS 1166 TO 848 LBL 24-25 LIGHT CORROSION IN SEVERAL AREA AND MISSING PRIMER. REMOVED CORROSION ON SEAT TRACK BETWEEN BS 1050 TO 848 LBL 24.25 IAW SRM 51-10-6. AREA OF SEAT TRACK WITH ORIGINAL THICKNESS OF .300, MATERIAL LOSS .002, MATERIAL RJun 11, 2008 · N750DH · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2008F00008Skin · crackedLT WING UPPER LEADING EDGE WS 507 AFT CORNER OF HOOK CUT OUT IS CRACKED. REMOVED HOOK SEAL IAW B727 SRM 51-30-2. STOP DRILLED CRACK DIMENSION .250 IAW B727 SRM 51-10-1. CUT OUT STRAP DIMENSION 7.875" X 1.875" IAW B727 SRM 57-30-4 FIG 9. FABRICATED PLATE REJun 10, 2008 · N750DH · Boeing 7272M7 · Wing, Plate/SkinSDR DHL2008F00020Seat Track · corrodedPITTING CORROSION ON SEAT TRACK UPPERMOST SURFACE AT BS 1029 AND RBL 24. BLEND OUT AREA AT SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 3. FABRICATED NEW SECTION OF SEAT TRACK IAW SRM 53-10-5 FIG 1 AND 51-20-1 INSTALLED NEW SEAT TRACK SRM 53-10-5 FIG 1Jun 7, 2008 · N750DH · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2008F00025Hinge · crackedMAIN CARGO DOOR AFT HINGE SECTION IS CRACKED AT FUSELAGE SIDE BS 650. REMOVED AFT HINGE SECTION AT MAIN CARGO DOOR SIDE BS 650 AND INSTALLED NEW SECTION WITH MS 20001+16-7200 AND PO 9002527 DIMENSION 17 IAW BOEING 727-200 FREIGHTER MAINTENANCE MANUAL FIGURE 5Jun 6, 2008 · N750DH · Boeing 7272M7 · Fuselage, Door Hinge
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