Boeing 727-155C

Service difficulty reports · 153

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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 = '727155C'
  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 DHL9671546DSkin · damagedAT D-CHECK, REPAIR AT STA 530 STR 16 AND STR 17R. REPAIRED DOUBLER, PER SRM 53-30-3, 8 INCHES BY 12 INCHES.Jul 14, 1996 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL9671549DSupport · corrodedAT D-CHECK, FOUND FLOOR BOARD SUPPORT BEAM HAS CORROSION AT STA 1135 BETWEEN LBL 50 AND LBL 60. REMOVED AND REPLACED NEW SUPPORT CHANNEL PER SRM 51-10-1 AND SRM 51-30-2.Jul 13, 1996 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL9671548DWeb · crackedAT D-CHECK, REINFORCEMENT WEB AT STA 1176.9 HAS A CRACK BETWEEN RBL 17 AND RBL 26. REMOVED AND REPLACED WEB PER SRM 51-10-4.Jul 13, 1996 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL9671537DRib · crackedAT D-CHECK, LEFT INBOARD MID-FLAP RIB FLANGE CRACKED AT FORE FLAP TRACK, OUTBOARD SIDE. REPLACED RIB PER SRM 51-10-1 .Jul 13, 1996 · N715DH · Boeing 727155C · Trailing Edge FlapsSDR DHL9671536DRib · crackedAT D-CHECK, LEFT OUTBOARD MID-FLAP RIB FLANGE CRACKED AT OUTBOARD FORE FLAP TRACK. REMOVED AND REPLACED RIB PER SRM 51-10-1.Jul 13, 1996 · N715DH · Boeing 727155C · Trailing Edge FlapsSDR DHL9671528DSkin · crackedAT D-CHECK, CRACK IN FUESLAGE BS 235.8, STR 15L. CUT OUT CRACKED AREA, INSTALLED DOUBLER REPAIR, PER SRM 53-30-3, 11 INCHES BY 8 INCHES, AND FILLER, .75 INCH BY 3.375 INCHES.Jul 13, 1996 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL9671523DRib · crackedAT D-CHECK, RIGHT WING STA 629.5 LOWER FLANGE OF RIB HAS CRACK. INSTALLED DOUBLER REPAIR PER SRM 57-10-5, 8 INCHES LONG.Jul 13, 1996 · N715DH · Boeing 727155C · Wing, Rib/BulkheadSDR DHL9671520DRib · crackedAT D-CHECK, LEFT WING RIB STA 686.5 HAS CRACK .5 INCH. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 57-10-5, 8.5 INCHES BY 4.5 INCHES .Jul 13, 1996 · N715DH · Boeing 727155C · Wing, Rib/BulkheadSDR DHL9671519DRib · crackedAT D-CHECK, RIB W/S 629.5 LOWER FLANGE OF RIB HAS CRACK IN EXISTING DOUBLER REPAIR. REMOVED REPAIR, INSTALLED DOUBLER REPAIR PER SRM 57-10-5, 10 INCHES BY 5 INCHES.Jul 13, 1996 · N715DH · Boeing 727155C · Wing, Rib/BulkheadSDR DHL9671518DStringer · brokenAT D-CHECK, LEFT WING STA 629 TOP SKIN STRINGER HAS BROKEN ATTACH FLANGE. REPAIRED PER S/B 57A159, 12.5 INCHES LONG.Jul 13, 1996 · N715DH · Boeing 727155C · Wing, Longeron/StringerSDR DHL9671513DRib · crackedAT D-CHECK, RIGHT WING RIB AT STA 601.5 HAS CRACK IN RADII. STOP DRILLED CRACK AND INSTALLED RIB REPAIR PER SRM 57-10-5, 10 INCHES BY 3.5 INCHES.Jul 13, 1996 · N715DH · Boeing 727155C · Wing, Rib/BulkheadSDR DHL9671512DRib · crackedAT D-CHECK, RIGHT WING RIB HAS CRACK ON LOWER FLANGE STA 629.5. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 57-10-5, 9 INCHES BY 1 INCH BY 1 INCH .Jul 13, 1996 · N715DH · Boeing 727155C · Wing, Rib/BulkheadSDR DHL9671510DSeat Track · corrodedAT D-CHECK, SEAT TRACK CORRODED AT STA 640 - STA 740. REMOVED AND REPLACED SEAT TRACK PER SRM 51-10-1, 7 FEET BY 4 INCHES .Jul 13, 1996 · N715DH · Boeing 727155C · Fuselage, Seat/Cargo Attach FittingsSDR DHL9671509DSeat Track · corrodedAT D-CHECK, SEAT TRACK CORRODED STA 600 - STA 650. REPLACED SEAT TRACK PER SRM 51-10-1.Jul 13, 1996 · N715DH · Boeing 727155C · Fuselage, Seat/Cargo Attach FittingsSDR DHL9671559DFitting · crackedAT D-CHECK, FOUND LEFT MLG UPLOCK SUPPORT FITTING HAS DEEP CORROSION, HFEC SHOWS CRACK INDICATION. REPLACED SUPPORT FITTING PER S/B 53-103.Jul 12, 1996 · N715DH · Boeing 727155C · Landing Gear Retraction/Extension SystemSDR DHL9671556DFitting · crackedAT D-CHECK, FOUND RIGHT MAIN LANDING GEAR UPLOCK SUPPORT FITTING HAS DEEP CORROSION PITTING INSIDE BOLT HOLE AND HFEC SHOWS CRACK INDICATION. REPLACED SUPPORT FITTING PER S/B 53-103.Jul 12, 1996 · N715DH · Boeing 727155C · Landing Gear Retraction/Extension SystemSDR DHL9671561DAngle · corrodedAT D-CHECK, VERTICAL ANGLE CORRODED AT AFT SIDE OF BS 790.95 AT LEFT SIDE OF CABIN, AT FUSELAGE FRAME TO 70.5 WING RIB UPPER CHORD ATTACH AREA. REMOVED AND REPLACED ANGLE, 3 FEET BY 3 FEET BY 2 INCHES.Jul 11, 1996 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL9671550DSkin · crackedAT D-CHECK, AFT SKIN AT LOWER DOOR JAMB IS CRACKED IN TWO PLACES AT AFT CORNER AND 17 INCHES FORWARD OF AFT CORNER. CUT OUT CRACKED AREA AT STA 1108 AND INSTALLED REPAIR PER SRM 53-30-3, 33.75 INCHES BY 3.5 INCHES.Jul 11, 1996 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL9671545DFloor Beam · crackedAT D-CHECK, FOUND FLOOR BEAM CRACKED AT WEB BS 825, RBL 47. STOP DRILLED CRACK, PERFORMED HFEC, FABRICATED AND INSTALLED WEB REPAIR, PER SRM 51-30-2, 5 INCHES BY 4.5 INCHES.Jul 11, 1996 · N715DH · Boeing 727155C · Fuselage Main, Floor BeamSDR DHL9671544DSeat Track · corrodedAT D-CHECK, CABIN FLOOR SEAT TRACK HAS CORROSION UPPER SURFACE BETWEEN STA 761-784 BELOW RIGHT FWD OVERWING EXIT. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-2 .Jul 11, 1996 · N715DH · Boeing 727155C · Fuselage, Seat/Cargo Attach FittingsSDR DHL9671524DAngle · crackedAT D-CHECK, LT LEADING EDGE CAVITY WBL 92.8 SECOND VERTICAL SUPPORT ANGLE IS CRACKED AT BOTTOM FASTENER. STOP DRILLED CRACK, INSTALLED ANGLE REPAIR, 9 INCHES BY 1 INCH BY 1 INCH, PER SRM 51-40-3.Jul 11, 1996 · N715DH · Boeing 727155C · Wing Miscellaneous StructureSDR DHL9671521DAngle · crackedAT D-CHECK, LT WING LEADING EDGE CAVITY STA 130.7 LOWER SUPPORT ANGLE CRACKED AFT OF MIDDLE SUPPORT ANGLE AT ATTACH BOLT. INSTALLED SUPPORT ANGLE PER SRM 51-40-3, 9 INCHES BY 1 INCH BY 1 INCH.Jul 11, 1996 · N715DH · Boeing 727155C · Wing Miscellaneous StructureSDR DHL9671505DWeb · crackedAT D-CHECK, LOWER RT TORQUE BOX AFT AIRSTAIR AREA LOWER CASTING VERTICAL WEB HAS CRACK. INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 5 INCHES BY 8 INCHES.Jul 11, 1996 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL9671504DAngle · corrodedAT D-CHECK, FOUND VERTICAL ANGLE CORRODED AT AFT SIDE OF BS 760.95 AT LT SIDE OF CABIN AT FUSELAGE FRAME TO 70.5 WING RIB. REPLACED ANGLE PER SRM, 3 FEET BY 3 FEET BY 2 FEET.Jul 11, 1996 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL9671564DFitting · crackedAT D-CHECK, FS 870 FRAME HAS WEB SEPARATION OUTBOARD END OF LIGHTING HOLE BETWEEN STR 9 RT - 10 RT. ULTRA SONIC INSPECTED CRACK SEPARATION OF LIGHTING HOLES BELOW STR 9 RT. END OF SEPARATON STOPS ABOUT .375 INCH FROM EDGE. CUT TERMINAL FITTING PER S/B 53-1Jul 10, 1996 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL9671560DFitting · crackedAT D-CHECK, EDDY CURRENT INSPECTION SHOWS CRACK INDICATION AT ROW A, BOTTOM HOLE AT STA 950 LT, STR 9 LT. OVERSIZED HOLE, INSTALLED FASTENER PER BOEING TELEX DHL MIA 960018R AND S/B 53-0196.Jul 10, 1996 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL9671552DSkin · crackedAT D-CHECK, LAP SEAM 14L HAS 3 CRACK INDICATIONS, BY HFEC BETWEEN BS 259 AND BS 277. CUT OUT CRACKED AREA AND INSTALLED DOUBLER REPAIR, 22 INCHES BY 8 INCHES, AND TAPERED FILLER, 4 INCHES BY 3 INCHES PER SRM 53-30-3.Jul 9, 1996 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL9671551DSkin · crackedAT D-CHECK, LAP SEAM 24L HAS 4 CRACK INDICATIONS BY HFEC BETWEEN BS 259 AND BS 277. CUT OUT DAMAGED TOP SKIN AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 12 INCHES BY 7 INCHES .Jul 9, 1996 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL9671522DAngle · crackedAT D-CHECK, LT WING LEADING EDGE LOWER SUPPORT ANGLE AT WS 121.5 CRACKED AT ATTACH BOLTS. STOP DRILLED AND INSTALLED ANGLE REPAIR, 4 INCHES BY 1 INCH, PER SRM 51-10-1.Jul 9, 1996 · N715DH · Boeing 727155C · Wing Miscellaneous StructureSDR DHL9671506DSkin · looseAT D-CHECK, STA 1342 RT SIDE, STR 8R HAS LOOSE SKIN AND RIVETS. CUT OUT DAMAGED SECTION, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 3 INCHES BY 7 INCHES. REMOVED AND REPLACED RIVETS PER SRM 51030-2.Jul 9, 1996 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL9671562DFrame · crackedAT D-CHECK, FUSELAGE INTERIOR FRAME CORRODED AT BS 620 INNER FLANGE ABOVE FLOOR LEVEL. REMOVED AND REPLACED SPLICE PLATE PER SRM 51-40-3 . PLATE 6 INCHES BY 7 INCHES.Jul 8, 1996 · N715DH · Boeing 727155C · Fuselage Main, FrameSDR DHL9671554DFrame · crackedAT D-CHECK, FOUND FUSELAGE INTERIOR FRAME CRACKED AT BS 600, INNER FLANGE ABOVE FLOOR LEVEL. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 53-10-4. REPAIR, 8 INCHES BY 10.5 INCHES.Jul 8, 1996 · N715DH · Boeing 727155C · Fuselage Main, FrameSDR DHL9671553DWeb · crackedAT D-CHECK, ONE CRACK IN LOWER RIGHT TORQUE TUBE BOX VERTICAL WEB AT FS 1263 BELOW AIRSTAIRS ACTUATOR. STOP DRILLED, INSTALLED DOUBLER REPAIR PER SRM 51-40-2 AND SRM 51-30-2, 6 INCHES BY 9 INCHES.Jul 8, 1996 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL9671539DFrame · dentedAT D-CHECK, FUSELAGE FRAME HAS DENTS AT STA 580 BETWEEN STR 6R AND STR 7R. INSTALLED FRAME DOUBLER REPAIR, PER SRM 53-10-4, 13 INCHES BY 2 INCHES BY 1 INCH .Jul 8, 1996 · N715DH · Boeing 727155C · Fuselage Main, FrameSDR DHL9671534DSkin · crackedAT D-CHECK, FOUND SKIN CRACKED BETWEEN STA 211.8 AND STA 219.8 AT STR 15L. CUT OUT DAMAGED AREA. INSTALLED DOUBLER, PER SRM 53-30-3, 10 INCHES BY 12 INCHES.Jul 8, 1996 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL9671533DSkin · crackedAT D-CHECK, FUSLAGE SKIN CRACKED BETWEEN STA 227 AND STA 235 AT STR 17L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 8 INCHES BY 6 INCHES .Jul 8, 1996 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL9671532DFrame · dentedAT D-CHECK, FUSELAGE INTERIOR FRAME HAS TWO DENTS ON INNER FRAME AT BS 540, STR 6R AND BELOW. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR, PER SRM 53-10-4, 14.5 INCHES BY 2 INCHES BY 1 INCH.Jul 8, 1996 · N715DH · Boeing 727155C · Fuselage Main, FrameSDR DHL9671531DFrame · dentedAT D-CHECK, FUSELAGE INTERIOR FRAME HAS DENT ON INNER FLANGE AT BS 540, STR 8 RT. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-10-4. REPAIR 10.75 INCHESBY 2 INCHES BY 1 INCH.Jul 8, 1996 · N715DH · Boeing 727155C · Fuselage Main, FrameSDR DHL9671530DFrame · dentedAT D-CHECK, FUSELAGE FRAME AT BS 560, STR 6R TO 7 RT DENTED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-10-4, 12.5 INCH BY 2.5 INCH BY 1 INCH.Jul 8, 1996 · N715DH · Boeing 727155C · Fuselage Main, FrameSDR DHL9671529DSkin · crackedAT D-CHECK, FUSELAGE CRACKED AT BS 251.6 BETWEEN STR 15L AND STR 16L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER, 8 INCHES BY 9 INCHES AND FILLER, 1.5 INCH BY .5 INCH, PER SRM 53-30-3.Jul 8, 1996 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL9671508CBulkhead Angle · chafedAT D-CHECK, AFT SIDE OF STA 1183 BULKHEAD HORIZONTAL Z-ANGLE AT RBL 22 HAS BEEN CHAFED BY VERTICAL FRAME ANGLE. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 1.25 INCHES BY 1 INCH.Jul 8, 1996 · N715DH · Boeing 727155C · Fuselage Main, BulkheadSDR DHL9671507DBulkhead Angle · chafedAT D C HECK, AFT SIDE OF 1183 BULKHEAD HORIZONTAL Z ANGLE AT LBL 22 HAS BEEN CHAFFED THROUGH BY VERTIAL DOOR FRAME ANGLE INSTALLED ANGLE REPAIR PER SRM 51-40-3 10.5 X 1.5 X 1Jul 8, 1996 · N715DH · Boeing 727155C · Fuselage Main, BulkheadSDR DHL9671567DSpar · corrodedAT D-CHECK, RIGHT WING HAS CORROSION ON REAR SPAR JUST FWD OF APU EXHAUST. REMOVED DAMAGED AREA, INSTALLED REPAIR PER SRM 57-10-6, 11 INCHES BY 5 INCHES.Jul 7, 1996 · N715DH · Boeing 727155C · Wing SparSDR DHL9671565DBeam · crackedAT D-CHECK, AFT BAGGAGE VERTICAL BEAM AT BS 1183 AND LBL 8 IS CRACKED AT LOWER END. STOP DRILL CRACK PER SRM. REPAIRED VERTICAL BEAM PER S/B 53-0175 .Jul 7, 1996 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL9671563DSpar · crackedAT D-CHECK, RIGHT WING UPPER SPAR SHOWS CRACK ON VERTICAL FLANGE OUTBD SIDE OF NR 13 SPOILER ACTUATOR MOUNT CASTING. CUT OUT DAMAGED SECTION PER S/B 57-145 , 23 INCHES BY 2 INCHES. INSTALLED REPAIR PER S/B 57-145, DRAWING 65C19647 AND AVITAS DRAWING 96PMSI1Jul 7, 1996 · N715DH · Boeing 727155C · Wing SparSDR DHL9671558DSkin · dentedAT D-CHECK, FOUND AFT CARGO DOOR HAS DEEP GOUGES, NICKS AND DENTS. BURNISHED OUT GOUGES, NICKS AND DENTS. DEEP DENT 12 INCHES BEYOND HANDLE. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 52-00-3. FILLER, 12 INCHES BY 18 INCHES, DOUBLER, 25 INCHES BY 34Jul 7, 1996 · N715DH · Boeing 727155C · Cargo/Baggage DoorsSDR DHL9671555DAngle · crackedAT D-CHECK, FOUND LEFT W/W PRESSURE DECK SUPPORT ANGLE CRACKED AT OUTBOARD AFT CORNER. CUT OUT CRACKED AREA AND INSTALLED ANGLE REPAIR PER SRM 51-40-4, 8 INCHES BY 2 INCHES.Jul 7, 1996 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL9671527DBeam · crackedAT D-CHECK, AFT BAGGAGE VERTICAL BEAM AT BS 1183 RBL 8 IS CRACKED. INSTALLED REPAIR PER S/B 53-0175.Jul 7, 1996 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL9671525DSkin · dentedAT D-CHECK, FUSELAGE EXTERNAL SKIN DENTED STA 600 RIGHT STR 21 TO STR 24. CUT OUT DAMAGED AREA AND INSTALLED DOUBLERS PER SRM 53-10-3, 2 INCHES BY 4 INCHES.Jul 3, 1996 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL96715001Position Ind · malfunctionedUPON APPROACH, WHEN FLAPS 2 WERE SELECTED INBOARD FLAPS WENT TO 2 DEGREES OUTBOARD SHOWED 0 DEGREES WORKED ALTERNATE PROCEDURE, ABNORMAL PROCEDURE AND LANDED AFTER LANDING OUTBOARD FLAPS SHOWED 2 DEGREES. TROUBLESHOT PER MM 27-51-00, FOUND FLAP POSITION INDICFeb 11, 1996 · N715DH · Boeing 727155C · Trailing Flap Position Indicating System
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