Boeing 727-2Q9

Service difficulty reports · 830

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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 = '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 DHL9974153CChannel · crackedAT C CHECK, RT WING LOWER T/E COVE PANEL I/B SUPPORT CHANNEL CRACKED I/B OF NR 12 SPOILER ACTUATOR STA 495. REMOVED AND REPLACED SUPPORT CHANNEL PER SRM 51-30-2, N/R 2852.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Wing Miscellaneous StructureSDR DHL9974142CSeat Track · corrodedAT C CHECK, NR 1,2,3,4, AND 5 SEAT TRACKS GALLED AT STA 438. SEAT TRACKS BURNISHED, NR 5 OUT OF LIMITS PER SRM. CUT OUT DAMAGED SEAT TRACK AT STA 420 TO 480 AND REPLACED PER SRM 51-30-2, N/R 5719.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9974141CSeat Track · corrodedAT C CHECK, NR 1, 2, 3, 4 AND 5 SEAT TRACKS HAS CORRSION AND GALLED AT STA 950D. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 1 FROM 950C TO 950E AND INSTALLED NEW PER SRM 53-10-5, 40 N/R 5727.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9974137CSuport · bentAT C CHECK, FLOOR SUPPORT L CHANNEL BS 950D, RBL 16 BENT. CUT OUT DAMAGED SECTION, INSTALLED EXTRUDED ANGLE REPAIR, 11 PER SRM 51-40-4.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9974133CSeat Track · damagedAT C CHECK, NR 1 SEAT TRACK HAS LUGS BROKEN OFF GALLED AND CORRODED AT STA 852. REMOVED TRACK AND INSTALLED NEW TRACK PER SRM 51-30-2, N/R 5723.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9974132CSeat Track · galledAT C CHECK, STA 1088 NR 1 SEAT TRACK GALLED OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-5, N/R 5729.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9974128CSkin · chafedAT C CHECK, LEFT WING I/B FLAPS FORE FLAP LOWER SURFACE I/B EDGE CHAFFING. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8, 18 BY 15, N/R 1379.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL9974127CSkin · delaminatedAT C CHECK, LEFT OUTBD TRAILING EDGE FLAP HAS SKIN SEPARATING ALONG TRAILING EDGE WS 436 THROUGH 656. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8, 9 BY 6, 5 FT BY 5 AND 7 BY 4, N/R 1368.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL9974126CSkin · delamiantedAT C CHECK, LEFT OUTBD FORE FLAP TRAILING EDGE ON UNDERSIDE SEPARATING. INSTALLED FIBERGLASS OVERLAY REPAIR AT LEFT OUTBD FORE FLAP TRAILING EDGE PER SRM 51-40-8, 9 BY 6.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL9974125CHinge · crackedAT C CHECK, LEFT MLG STRUT DOOR FWD HINGE HINGED FAIRING HAS CRACKED, HINGE AT DOOR ATTTACH. REPLACED HINGE PER SRM 51-30-2, N/R 7004.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Landing Gear DoorsSDR DHL9974123CTip · gougedAT C CHECK, LEFT WING TIP LEADING EDGE THE INBD SIDE WHICH MATES NEXT TO SLAT IS GOUGED ON THE LOWER SURFACE. CUT OUT DAMAGED AREA. INSTALLED DOUBLER AND FILLER REPAIR PER SRM 51-30-2, 11 BY 8, N/R 1349.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Wing Miscellaneous StructureSDR DHL9974118CPanel · delaminatedAT C CHECK, RT WING UPPER SURFACE PANEL AT RT SIDE OF APU EXHAUST OLD REPAIR PULLING FASTENERS. REMOVED PANEL AND INSTALLED BONDING REPAIR PER SRM 51-40-6, 50 BY 6, N/R 2860.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Wing, Plate/SkinSDR DHL9974116CFrame · crackedAT C CHECK, EVIDENCE OF CORROSION AND SMALL CRACK AT BS 950C FRAME UPPER FLANGE BETWEEN S-26 L AND STR 27 L. CUT OUT DAMAGED AREA AT UPPER FLANGE, HFEC, INSTALLED FRAME REPAIR AT BS 950C PER SRM 51-40-3, N/R 3360.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9974114CAngle · crackedAT C CHECK, LEFT WW STR 18A FWD RIB ATTACH ANGLE STA 940 FITTING IS CRACKED ON INBD END. REMOVED AND INSTALLED NEW ATTACH ANGLE PER SRM 53-10-1, 6 BY 4.5, N/R 7078.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9974111CSkin · corrodedAT C CHECK, FUS INTERIOR EVIDENCE OF CORROSION CRACK AT SKIN STA 580 AND STR 27L. CUT OUT CORRODED SKIN, INSTALLED DOUBLER REPAIR FROM STA 520 TO 610 BETWEEN STR 26L- 29L, 36.5 BY 23.5 AND 34 BY 15.5 PER AVITAS ENGINEERING ORDER 99AVHM 002RO-01, N/R 3369.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL9974110CSupport · crackedAT C CHECK, CRACKED AFT CARGO COMPARTMENT FLOOR SUPPORT U CHANNEL BS 950D, RBL 12. CUT OUT DAMAGED SECTION, 10 INSTALLED EXTRUDED ANGLE PER SRM 51-40-4, 18 LONG, N/R 3357.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9974109CAngle · crackedAT C CHECK, LEFT WING LEADING EDGE CAVITY INBD VERTICAL SUPPORT ANGLE FOR NR 2 SLAT ACTUATOR IS CRACKED. REMOVED AND REPLACED VERTICAL SUPPORT ANGLE PER SRM 51-30-2. INSTALLED STAINLESS STEEL DOUBLER ON THE SUPPORT ANGLES PER S/B 57-130, N/R 1356.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Leading Edge Slat ActuatorSDR DHL9974104CFrame · crackedAT C CHECK, CRACKED FRAME AT STA 1010 UPPER FLANGE BETWEEN STR 25R AND 26R. CUT OUT DAMAGED AREA, FABRICATED FRAME REPAIR PER SRM 51-40-3, 13.5 BY 3.5 BY 1, AND INSTALLED PER SRM 51-40-3, N/R 3352.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9974103CSkin · corrodedAT C CHECK, FUSELAGE EXTERIOR SEVERAL BROKEN FASTENERS STA 1010 TO 1025 SRT 29R. REMOVED INNER SKIN CORROSION. REMOVED BROKEN RIVETS AND INSTALLED SKIN REPAIR SPLICES FILLER AND DOUBLER PER SRM 53-30-31, 3 BY 11, N/R 3339.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL9974102CSkin · delaminatedAT C CHECK, RT WING SURF PANEL OVER MLG SUPPORT MAIN BEAM WARPED AND DELAMINATED. INSTALLED HOT BOND REPAIR PER SRM 51-20-3, 84 BY 1, N/R 2861.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Wing, Plate/SkinSDR DHL9974156CAngle · crackedAT C CHECK, RT WING UPPER L/E INTERIOR WEB AT STA 0 O/B SUPPORT ANGLE CRACKED L/E STA 349. REMOVED AND FABRICATED SUPPORT ANGLE PER SRM 51-40-3 1, 65 BY 15, 65 N/R 2826.Feb 24, 1999 · N741DH · Boeing 7272Q9 · Wing Miscellaneous StructureSDR DHL9974143CWeb · canningAT C CHECK, AFT AIRSTAIRS RT LOWER TORQUE BOX HAS VERTICAL WEB OIL CANNING AT STA 1277. REPLACED REPAIR DOUBLER PER S/B 53-129, 30 BY 17, N/R 4055.Feb 23, 1999 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9974138CWeb · crackedAT C CHECK, NOSE GEAR W/W LEFT SIDE WEB LIGHTING HOLE HAS CRACK FWD END. REMOVED WEB, INSTALLED NEW WEB PER SRM 51-40-2, N/R 7026.Feb 23, 1999 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9974119CSkin · damagedAT C CHECK, PERFORM PERMANENT REPAIR UPPER L/E SLAT NR 5. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 57-50-3, 6 BY 7, N/R 2801.Feb 19, 1999 · N741DH · Boeing 7272Q9 · Leading Edge DevicesSDR DHL99741002Transponder · inoperativeTRANSPONDER NR 1 AND NR 2 INOP AS REPORTED BY ATC DURING CLIMBOUT. REMOVED AND REPLACED TRANSPONDERS PER MM 34-45-1.Feb 17, 1999 · N741DH · Boeing 7272Q9 · ATC Transponder SystemSDR DHL9974032CIntercostal · crackedAT C CHECK, INTERCOSTAL CRACKED STRINGER 5 R, BS 360. REMOVED CRACKED INTERCOSTAL. REPLACED INTERCOSTAL WEB PER SRM 53-10-1, 20 BY 4, N/R 5744.Feb 11, 1999 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9974029CStiffener · corrodedAT C CHECK, FRONT SPAR VERTICAL STIFFENER HAS CORROSION AT LOWER LEG W/S 170. REMOVED WEB, INSTALLED ANGLE REPAIR PER SRM 51-40-4, 4 BY 6, N/R 2108.Feb 10, 1999 · N740DH · Boeing 7272Q9 · Wing Miscellaneous StructureSDR DHL9974030CStringer · corrodedAT C CHECK, CORROSION ON STR 29 STA 950 F, FOUND STR 29R CRACKED AT STA 950D TO 950F AND CORROSION OUT OF LIMITS FROM 950 TO 990. FOUND FRAME TO SKIN CLIP CRACKED AT STA 990. FOUND VERTICAL U-CHANNEL FLOOR SUPPORT CRACKED. REPLACED STRINGER 29 RT FROM STA 9Feb 9, 1999 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR DHL9974027CAngle · deterioratedAT C CHECK, NR 3 ENGINE UPPER COWL PANEL FORWARD UPPER INNER LUG FITTING ATTACH ANGLE DETERIORATED. REPLACED ANGLE PER SRM 54-10-2, 12 BY 5, N/R 6428.Feb 4, 1999 · N740DH · Boeing 7272Q9 · Engine Cowling SystemSDR DHL9974019CRib · brokenAT C CHECK, NR 3 ENGINE LOWER COWL PANEL NR 5 INNER RIB IS GOUGED. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 54-10-3, 3 BY 7, N/R 6435.Feb 4, 1999 · N740DH · Boeing 7272Q9 · Engine Cowling SystemSDR DHL9974011CFairing · crackedAT C CHECK, NR 4 FLAP TRACK FIXED FAIRING CRACKED AT FWD END. REPLACED STRAP ON FLAP TRACK PER SRM 53-50-1, 13 BY 3, N/R 1163.Feb 4, 1999 · N740DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL9974028CWeb · corrodedAT C CHECK, RT HORIZ WEB HAS CORROSION BULGING AND POPPED RIVETS AT RT INBD SIDE NEXT TO NOSE WHEEL WELL BOX STA 294 TO 360. REMOVED INTERNAL RT WEB CENTER WEB FOR REPAIR. REMOVED CHORD ANGLE. REMOVED FWD AND AFT VERTICAL STIFFENERS AND GEAR FITTING SUPPORTFeb 3, 1999 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9974025CSeat Track · wornAT C CHECK, TOP FLANGE OF SEAT TRACK WORN IN TWO SPOTS BS 935 TO 945 RBL 48. INSTALLED NEW SEAT TRACK PER SRM 53-10-5 FROM BS 870 TO 960, N/R 5733.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9974024CSeat Track · gougedAT C CHECK, TOP FLANGE OF SEAT TRACK GOUGED BS 940 RBL 24. REMOVED DAMAGED SEAT TRACK AND REPLACED PER SRM 53-10-5, 90 LONG N/R 5732.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9974023CSeat Track · brokenAT C CHECK, TOP FLANGE OF SEAT TRACK BROKEN OFF BS 710 BL 0. REMOVED DAMAGED SECTION FROM 700 TO 730 PER AE DRAWING AE 727-2-063 AND REPLACED SAME, N/R 5730.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9974022CCowl · chafedAT C CHECK, NR 1 ENGINE UPPER COWL FWD OUTBD LE CHAFF STRIP NEEDS REPLACEMENT. CUT OUT DAMAGED AREA, INSTALLED ANGLE REPAIR PER SRM 51-10-3, 3 BY 20, N/R 6332.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Engine Cowling SystemSDR DHL9974021CCowl · crackedAT C CHECK, NR 1 ENGINE LOWER COWL NR 5 RIB AFT OF OIL BREATHER HAS HOLE WORN THROUGH. INSTALLED ANGLE REPAIR PER SRM 54-10-3, 3 BY 18, N/R 6341.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Engine Cowling SystemSDR DHL9974020CTailpipe · damagedAT C CHECK, NR 2 ENGINE, HOLE ON LEADING EDGE TAIL PIPE EXTERIOR LT SIDE ABOUT 7 O'CLOCK POSITION. CUT OUT DAMAGED AREA, INSTALLED DOUBLER, 12 BY 4 PER SRM 51-40-3, N/R 6399.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Engine Collector/Tailpipe/NozzleSDR DHL9974018CSkin · delaminatedAT C CHECK, RT ELEVATOR I/B END T/E SEPARATING AND HAS BROKEN FASTENER O/B TAB CUT OUT. APPLIED BONDING REPAIR PER SRM 51-30-3, 8 BY 1, N/R 4330.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Elevator, Plate/SkinSDR DHL9974017CSkin · delaminatedAT C CHECK, RT ELEVATOR T/E SEPARATING AND SPONGY AT O/B AREA OF TAB CUTOUT. APPLIED BONDING REPAIR PER SRM 51-20-3, 8 BY 1, N/R 4332.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Elevator, Plate/SkinSDR DHL9974013CSkin · delaminatedAT C CHECK, RT OUTBD AFT FLAP TRAILING EDGE IS DELAMINATING 78 FROM OUTBD SIDE. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8 8 BY 5, N/R 2088.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL9974012CAngle · crackedAT C CHECK, INNER STRUCTURE SUPPORT ANGLE IS CRACKED AT NR 2 L/E SLAT INNER NOSE BETWEEN L/E SLAT ACTUATOR AND ANTI-ICE DUCT. STOP DRILLED CRACK, HFEC STOP DRILL. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 1 BY 1 BY 17.5, N/R 1090.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Leading Edge DevicesSDR DHL9974009CFence · erodedAT C CHECK, NR 5 SLAT AERODYNAMIC FENCE ERODED IN SEVERAL AREAS. INSTALLED FILLER REPAIR PER SRM 51-40-1, 9 BY 3, N/R 2030.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Leading Edge DevicesSDR DHL9974008CShield · delaminatedAT C CHECK, NR 5 SLAT AERODYNAMIC FENCE LEADING EDGE METAL SHIELD DELAMINATING. INSTALLED BONDING REPAIR PER SRM 51-20-3, 6 BY 3, N/R 2029.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Leading Edge DevicesSDR DHL9974007CSkin · delaminatedAT C CHECK, L/W OUTBD AILERON UPPER SURFACE AT OUTSIDE UPPER SURFACE TRAILING EDGE DELAMINATED. INSTALLED BONDED REPAIR PER SRM 51-40-6, NO BALANCE REQUIRED PER SRM 51-80-4, 7 BY 2 N/R 1108.Feb 3, 1999 · N740DH · Boeing 7272Q9 · AileronsSDR DHL9974006CSkin · damagedAT C CHECK, LEFT WING COVE PANEL OUTBD OF NR 4 FLAP TRACK LOWER SKIN DAMAGED. INSTALLED FILLER REPAIR PER SRM 51-40-1, 9 BY 8, N/R 1248.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Wing, Plate/SkinSDR DHL9974005CAngle · corrodedAT C CHECK, ANGLE CRACKED AT LT WING 32 L/E SLAT WELL. REMOVED CRACKED ANGLE AND REPLACED PER SRM 51-30-2, 10 BY 5, N/R 1097.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Wing Miscellaneous StructureSDR DHL9974004CAngle · crackedAT C CHECK, RT WING FIXED LEADING EDGE CAVITY LOWER OUTBD SUPPORT ANGLE AT FS 130.7 IS CRACKED. REMOVED AND REPLACED ANGLE PER SRM 51-40-3, 18 BY 1 BY 1, N/R 2072.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Wing Miscellaneous StructureSDR DHL9974002CAngle · corrodedAT C CHECK, CORRSION AFT CARGO FRAME 1050 AT RIGHT FLOOR SUPPORT. FABRICATED FRAME REPAIR PER SRM 51-40-3, 10.5 BY 3.5, N/R 3161.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9974001CAngle · crackedAT C CHECK, RT FIXED LEADING EDGE CAVITY LOWER INBD SUPPORT ANGLE FSS 130.7 IS CRACKED. CUT OUT ANGLE, INSTALLED NEW SUPPORT ANGLE PER SRM 51-40-3, 9.5 BY 1 BY 1, N/R 2911.Feb 3, 1999 · N740DH · Boeing 7272Q9 · Wing Miscellaneous Structure
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