Boeing 727-29

Service difficulty reports · 229

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 = '72729'
  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 DHL9771251DAngle · crackedAT D-CHECK, PER X-RAY CRACK INDICATION ON LEFT ELEVATOR INBD FWD 6 FROM FRONT SPAR. NDT TO VERIFY CRACK, REMOVED AND REPLACED ANGLE PER SRM 51-40-3, 18 BY .625 BY .875 BY .312 .Feb 18, 1997 · N712DH · Boeing 72729 · Elevator StructureSDR DHL9771237DFrame · corrodedAT D-CHECK, CORROSION ON LOWER SIDE OF FRAME BS 570 STR 25R. CUT OUT DAMAGED AREA, INSTALLED FRAME REPAIR PER SRM 53-10-4, DOUBLER 16 BY 4, FILLER 6 BY 4.Feb 18, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771236DFrame · req'd repairAT D-CHECK, TEMPORARY REPAIR ON FRAME BS 570 RBL 29. REMOVED REPAIR, INSTALLED REPAIR PER SRM 53-10-4, 16 BY 4.Feb 18, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771202DSkin · puncturedAT D-CHECK, SKIN PUNCTURE NEAR BS 630, 2 INCH ABOVE STRINGER 23L. CUT OUT DAMAGED AREA AT SKIN .5 INCH DIAMETER. INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 3 DOUBLER.Feb 18, 1997 · N712DH · Boeing 72729 · Fuselage Main, Plate/SkinSDR DHL9771290DJamb · crackedDURING D-CHECK, THE LOWER AFT JAMB AT THE MAIN CARGO DOOR CUTOUT WAS FOUND CRACKED. ROUTED OUT CRACK AND INSTALLED DOUBLER 4 BY 2 PER BOEING SRM 51-40-2.Feb 17, 1997 · N712DH · Boeing 72729 · Fuselage Miscellaneous StructureSDR DHL9771247DSkin · disbondedAT D-CHECK, TWO SMALL DISBONDED AREAS AT BS 259 AFT PANEL AT STR 3R AND STR 6R. REMOVED FASTENERS, TRIMMED DISBONDED PANELS, INSTALLED SPLICE DOUBLER PER BOEING EO 69-62161 AND S/B 53-0084, 9 BY 14.5. CUTOUT DISBONDED SECTION OF SKIN AFT PANEL STR 3, INSTALLFeb 17, 1997 · N712DH · Boeing 72729 · Fuselage Main, Plate/SkinSDR DHL9771244DFrame · corrsoionAT D-CHECK, AFT PIT FUSELAGE CUTOUT FRAME WEB HAS CORROSION ON UNDER SIDE SURFACE STA 1113 BETWEEN STA 27R TO 25R. CUT OUT DAMAGED AREA, INSTALLED WEB REPAIR PER SRM 51-40-2, 4.125 BY 7.625.Feb 17, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771242DFrame · crackedAT D-CHECK, FRAME INBOARD FLANGE HAS HOLE DRILLED AT EDGE BS 804 AND STR 14 RT. BLENDED OUT DAMAGED FRAME FLANGE EDGE AND INSTALLED FRAME REPAIR PER SRM 53-10-4.Feb 17, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771208DFloorbeam · corrodedAT D-CHECK, CORROSION OF FLOORBEAM UPPER SURFACE BS 1030 LBL 45-64. CUT OUT UPPER FLANGE AT STA 1030, INSTALLED FLOORBEAM UPPER CHORD REPAIR PER SRM 53-10-8. REPAIR 19.Feb 17, 1997 · N712DH · Boeing 72729 · Fuselage Main, Floor BeamSDR DHL9771228DFitting · corrodedAT D-CHECK, CORROSION AT FUSELAGE FRAMES 761 LEFT AT FLOORBEAM AND SKIN 70.5 LEFT. REMOVED AND REPLACED T-FITTING PER SRM 51-10-1 AND 51-30-2.Feb 16, 1997 · N712DH · Boeing 72729 · Fuselage Miscellaneous StructureSDR DHL9771231DFitting · corrodedAT D-CHECK, CORROSION ON LEFT HAND ALT EMERGENCY EXIT HANDLE CUT OUT IN FRAME INNER MATING SURFACE. REMOVED FITTING, REPLACED FITTING PER SRM 51-30-2.Feb 15, 1997 · N712DH · Boeing 72729 · Fuselage Miscellaneous StructureSDR DHL9771230DFloorbeam · corrodedAT D-CHECK, CORROSION CABIN FLOORBEAM STA 1110 RBL 48 TO RBL 60. CUT DAMAGED SECTION OF FLOORBEAM BS 110 FROM RBL 36 TO O/B END PER SRM 53-10-8, INSTALLED REPAIR PER SRM 53-10-8.Feb 15, 1997 · N712DH · Boeing 72729 · Fuselage Main, Floor BeamSDR DHL9771227DFloorbeam · corrodedAT D-CHECK, CORROSION ON FLOORBEAM BS 111, RBL 32. CUT OUT DAMAGED SECTION ON UPPER SURFACE OF FLOORBEAM FROM RBL 36 TO O/B END, INSTALLED REPAIR PER SRM 53-10-8.Feb 15, 1997 · N712DH · Boeing 72729 · Fuselage Main, Floor BeamSDR DHL9771226DSeat Track · corrodedAT D-CHECK, CORROSION ON SEAT TRACK FLANGE, BS 1060 TO 1080, RBL 45. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-5 FROM 1050-1130.Feb 15, 1997 · N712DH · Boeing 72729 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9771215DSeat Track · corrodedAT D-CHECK, CORROSION ON SEAT TRACK AND ATTACH FASTENER BS 480 RBL 25. INSTALLED NEW TRACK PER SRM 51-30-2.Feb 15, 1997 · N712DH · Boeing 72729 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9771214DSeat Track · corrosionAT D-CHECK, CORROSION ON SEAT TRACK BS 470 TO 480 LBL 46. INSTALLED NEW SEAT TRACK PER SRM 51-30-2.Feb 15, 1997 · N712DH · Boeing 72729 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9771213DSeat Track · corrodedAT D-CHECK, CORROSION OF SEAT TRACK BS 510 TO 540 LBL 25. SPLICED IN SECTION OF SEAT TRACK PER SRM 53-10-5.Feb 15, 1997 · N712DH · Boeing 72729 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9771212DSeat Track · corrodedAT D-CHECK, CORROSION OF SEAT TRACK BS 470 TO 490 LBL 25. INSTALLED NEW SECTION OF SEAT TRACK FROM BS 470 TO 490 LBL 25 PER SRM 53-10-5.Feb 15, 1997 · N712DH · Boeing 72729 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9771209DFloorbeam · corrodedAT D-CHECK, FLOORBEAM HAS CORROSION AT STA 640 RBL 24-63. CUT OUT DAMAGED AREA, INSTALLED CABIN FLOORBEAM REPAIR. RBL 24 TO 36 PER SRM 53-10-8, REMOVE CORROSION ON UPPER SURFACE FROM RBL 36 TO 63, MATERIAL LOSS WITHIN LIMITS PER SRM 53-10-1.Feb 15, 1997 · N712DH · Boeing 72729 · Fuselage Main, Floor BeamSDR DHL9771249DFrame · damagedAT D-CHECK, DAMAGE ON AFT EDGE OF FRAME BS 1070 LT WW 210 TO 212 RIGHT HAND. INSTALLED DOUBLER AT FRAME BS 1070, 9 BY 4.Feb 14, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771241DFrame · corrodedAT D-CHECK, CORROSION ON FRAME STA 660 RBL 25. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER SRM 51-40-3, 14 BY 4.Feb 14, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771234DSeat Track · corrodedAT D-CHECK, CORROSION ON SEAT TRACK, BS 480 LBL 18. REPLACED SECTION OF SEAT TRACK PER SRM 53-10-5 FROM BS 480 TO 540.Feb 14, 1997 · N712DH · Boeing 72729 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9771220DSeat Track · corrodedAT D-CHECK, CABIN SEAT TRACK HAS CORROSION ON FLANGE AND INSIDE CHANNEL STA 620 TO 740 RBL 46. REPLACED SECTION OF SEAT TRACK PER SRM 53-10-5.Feb 14, 1997 · N712DH · Boeing 72729 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9771211DSeat Track · corrodedAT D-CHECK, SEAT TRACK CORRODED BS 355 TO 400 LBL 46. REPLACED DAMAGED SEAT TRACK PER SRM 53-10-5.Feb 14, 1997 · N712DH · Boeing 72729 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9771210DSeat Track · corrodedAT D-CHECK, CABIN SEAT TRACK AT RBL 46 AT STA 715 HAS CORROSION. REPLACED SECTION OF SEAT TRACK PER SRM 53-10-5 FROM STA 620 TO 740 RBL 46 .Feb 14, 1997 · N712DH · Boeing 72729 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9771205DFrame · holeAT D-CHECK, HOLE IN FRAME I/B FLANGE RADIUS BS 400 STR 16R. INSTALLED DOUBLER REPAIR PER SRM 53-10-4, 9 BY 9.Feb 14, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771253DSkin · crackedAT D-CHECK, NR 4 SLAT NR 2 RIB FROM OUTBOARD END IS CRACKED. STOP DRILLED CRACK, HFEC CRACK, INSTALLED RIB REPAIR PER SRM 57-50-3, 4.5 BY 3.Feb 13, 1997 · N712DH · Boeing 72729 · Leading Edge DevicesSDR DHL9771252DSkin · dentedAT D-CHECK, PERFORM PERMANENT REPAIR TO DENT O/B L/E NR 8 SLAT. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 57-50-3. REPAIR 6 BY 6.Feb 13, 1997 · N712DH · Boeing 72729 · Leading Edge DevicesSDR DHL9771240DFrame · corrodedAT D-CHECK, CORROSION ON FRAME AT NUT PLATE BS 640 RBL 25. CUT OUT DAMAGED AREA, INSTALLED FRAME REPAIR PER SRM 51-40-3, 14 BY 4.Feb 13, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771239DFrame · damagedAT D-CHECK, HOLE IN FRAME AT FASTENER HOLE BS 620 RBL 25. CUT OUT DAMAGED AREA, INSTALLED FRAME REPAIR PER SRM 51040-3, 14 BY 4.Feb 13, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771238DFrame · crackedAT D-CHECK, FRAME CRACKED AT FASTENER HOLE BS 600 RBL 25. CUT OUT DAMAGED AREA, INSTALLED FRAME REPAIR PER SRM 51-40-3, DOUBLER 13 BY 4.Feb 13, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771233DSeat Track · corrodedAT D-CHECK, CORRODED FASTENERS, NUT PLATES ON PREVIOUS SEAT TRACK FLANGE REPAIR, BS 520 TO 540 LB 20. REMOVED AND INSTALLED NEW SECTION OF SEAT TRACK PER SRM 51-30-2 FROM 480 TO 540.Feb 13, 1997 · N712DH · Boeing 72729 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9771229DClip · crackedAT D-CHECK, CRACK IN STRINGER TO FRAME CLIP, BS 970 STR 6L. REMOVED AND REPLACED CLIP PER SRM 51-10-1. REPAIR 3 BY 3 BY 2.Feb 13, 1997 · N712DH · Boeing 72729 · Fuselage Miscellaneous StructureSDR DHL9771218DFrame · open holesAT D-CHECK, FRAME I/B FLANGE HAS SIX OPEN HOLES WITHIN 4 AT BS 400 BETWEEN S10L AND 11L. INSTALLED FRAME REPAIR PER SRM 53-10-4, 11 BY 2.25 BY 1.25.Feb 13, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771257DRib · crackedAT D-CHECK, NR 6 SLAT INBOARD TRACK, OUTBOARD RIB IS CRACKED. REPLACED RIB PER SRM 51-10-1.Feb 12, 1997 · N712DH · Boeing 72729 · Leading Edge DevicesSDR DHL9771250DRib · crackedAT D-CHECK, NR 4 SLAT NR 3 RIB FROM OUTBOARD END CRACKED. REMOVED DAMAGED AREA AND INSTALLED RIB REPAIR PER SRM 57-50-3, DOUBLER 4.375 BY 3.Feb 12, 1997 · N712DH · Boeing 72729 · Leading Edge DevicesSDR DHL9771248DFrame · crackedAT D-CHECK, FUSELAGE FRAME CRACKED AT I/B RADIUS STA 930 NEAR STR 14 LT. STOP DRILLED CRACK, ACCOMPLISHED HFEC, INSTALLED FRAME REPAIR PER SRM 53-10-4, 11 BY 4.Feb 12, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771219DFrame · misdrilledAT D-CHECK, FASTENER INSTALLED ON FRAME RADIUS AT BS 440 BETWEEN STR 6L AND 7L. INSTALLED FRAME REPAIR PER SRM 53-10-4, 10 BY 2.33 BY 1.25.Feb 12, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771243DFrame · corrosionAT D-CHECK, AFT PIT FUSELAGE CUTOUT FRAME WEB HAS CORROSION ON NUT PLATE HOLE UNDERSIDE STA 1053 STR 27R TO 25R. REPLACED FRAME WEB PER SRM 51-40-2, 4 BY 10.Feb 11, 1997 · N712DH · Boeing 72729 · Fuselage Main, FrameSDR DHL9771275DBulkhead Plate · corrodedAT D-CHECK, 9G BULKHEAD SHEAR PLATE AT BS 360 TO 344 HAS CORROSION BEYOND LIMITS. REPLACED SHEAR PLATE 128 X 38 PER SRM 51-10-1.Feb 9, 1997 · N712DH · Boeing 72729 · Fuselage Main, BulkheadSDR DHL9771224DSeat Track · corrodedAT D-CHECK, CORROSION ON CABIN SEAT TRACK NR 6 RBL 48 FROM STA 730 TO 793. REPLACED SEAT TRACK PER SRM 53-10-5 FROM BS 600 TO 740.Feb 8, 1997 · N712DH · Boeing 72729 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9771268DRib · crackedAT D-CHECK, NR 3 SLAT THIRD RIB FROM OUTBOARD END CRACKED. INSTALLED REPAIR PER SRM 57-50-3.Feb 6, 1997 · N712DH · Boeing 72729 · Leading Edge DevicesSDR DHL9771216DFloorbeam · corrodedAT D-CHECK, CABIN FLOORBEAM BS 344 RBL 64 TO BL 64 CORRODED. REMOVED AND REPLACED T-CAP PER SRM 51-30-2.Jan 19, 1997 · N712DH · Boeing 72729 · Fuselage Main, Floor BeamSDR DHL96712005Radome · poppedDURING TAKEOFF ROLL IMMEDIATELY PRIOR TO ROTATION, CREW HEARD A POP, F/O FELT AND IMPACT UNDER HIS FEET. BURNED RUBBER SMELL IN COCKPIT LASTED 5 MINUTES AND GEAR RETRACTION WAS NORMAL. NO GEAR WARNING OR OTHER ABNORMAL INDICATIONS WERE NOTED. PERFORMED ABNONov 13, 1996 · N712DH · Boeing 72729 · Aerodynamic FairingsSDR DHL96712004Pitot Tube · pluggedFIRST OFFICERS AIRSPEED INDICATOR FAILED, TAPPED GAUGE AND HAD NO EFFECT. BLEW FIRST OFFICERS PITOT TUBE OUT WITH HIGH PSI AIR AND TEST FIRST OFFICERS AIRSPEED INDICATOR WITH PITOT STATIC TEST BOX PER MM 34-11-0.Oct 15, 1996 · N712DH · Boeing 72729 · Pitot/Static SystemSDR DHL95712002Access Panels · not securedAFTER TAKEOFF AT 230 KTS, NOSE GEAR DOOR LIGHT ILLUMINATED ON S/O PANEL AND RED NOSE GEAR DOOR LIGHT ILLUMINATED ON FWD PANEL. AIRCRAFT FAILED TO PRESSURIZE IN AUTO, PERFORMED ALTERNATE PROCEDURES AND COULD NOT PRESSURIZE IN MANUAL. SECURED NOSE GEAR ACCESS Nov 19, 1995 · N712DH · Boeing 72729 · Fuselage Miscellaneous StructureSDR 96ZZZM479Skin · dentsDURING C-CHECK, FOUND NR 2 CARGO DOOR EXTERIOR STATION 1070 ABOVE HANDLE HAS DENTS AND GOUGES. CUT OUT DAMAGED 5 INCH BY 7 INCH APPROX, FABRICATED AND INSTALLED DOUBLER 7075-T6 .050 12 INCH BY 15 INCH APPROX AS PER SRM 52-00-3 FIG 3. SEALED EDGE WITH PRC PERSep 16, 1995 · N712DH · Boeing 72729 · Cargo/Baggage DoorsSDR 96ZZZM471Floor Web · crackDURING C-CHECK, FOUND AFT CABIN, CURVED FLOOR WEB BETWEEN FS 1176.9 CHORD AND FS 1183 BULKHEAD IS CRACKED AROUND LIGHTENING HOLE AT LBL 60. INSTALLED DOUBLER CRACKED FLOOR WEB BETWEEN FS 1176.9 CHORD AND FS 1183 PER SRM 51-40-2, 5 INCHES BY 6 INCHES 2024-T3 .Sep 16, 1995 · N712DH · Boeing 72729 · Fuselage Miscellaneous StructureSDR 96ZZZM488Doubler · crackedDURING C-CHECK, FOUND CRACK INDICATION ON WINDSHIELD CENTER POST, OUTSIDE DOUBLER ON LOWER END. COMPLIED WITH BOEING SERVICE BULLETIN NR 727-53-160 AND REPLACED SKIN PANEL.May 16, 1995 · N712DH · Boeing 72729 · Fuselage Miscellaneous StructureSDR 96ZZZM487Keel Beam · crackedDURING C-CHECK, FOUND RIGHT W/W KEEL BEAM WEB CRACKED TWO PLACES FORWARD OF APU CUTOUT BS 872. CUT OUT DAMAGE AREA AND INSTALLED WEB REPAIR AS PER SRM 51-40-2 .063 7075-T6 3 INCH BY 13 INCH.May 16, 1995 · N712DH · Boeing 72729 · Fuselage Main, Keel
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