Boeing 727-27C

Service difficulty reports · 1,078

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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 = '72727C'
  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 UPS00232199Fitting · corrodedINSPECTION TYPE: C, CORROSION ON LT O/B AILERON, I/B CENTER HINGE FITTING AROUND FASTENER HOLES. REMOVED AND INSTALLED NEW HINGE FITTING PER SRM 51-30-2Mar 3, 2000 · N914UP · Boeing 72727C · AileronsSDR UPS00232198Floorbeam · corrodedINSPECTION TYPE: C, CORROSION ON TOP CHORD OF BS 344 FLOORBEAM RBL 6 TO LBL 16, WL 208. REPAIRED FLOOREAM PER SRM 53-10-8Mar 3, 2000 · N914UP · Boeing 72727C · Fuselage Main, Floor BeamSDR UPS00231979Hinge · corrodedINSPECTION TYPE:C, CORROSION (C57-581-01.00-01) ON LOWER SURFACE OF LEFT O/B AILERON O/B CENTER HINGE FITTING AROUND FASTENER HOLES. REMOVED AND REPLACED HINGE PER SRM 51-30-2.Mar 3, 2000 · N914UP · Boeing 72727C · Wing, Control Surface Attach FittingsSDR UPS00231978Hinge · corrodedINSPECTION TYPE:C, CORROSION (C57-581-01.00-01) ON LOWER SURFACE OF LEFT O/B AILERON O/B HINGE FITTING AROUND FASTENER HOLES. REMOVED AND REPLACED HINGE PER SRM 51-30-2.Mar 3, 2000 · N914UP · Boeing 72727C · Wing, Control Surface Attach FittingsSDR UPS00231940Stringer · corrodedINSPECTION TYPE:C&SI, STR 24R BETWEEN BS 360 AND BS 259.5 IS CORRODED AT BS 277 AND END OF STRINGER AT BS 360 HAS CRACK FROM PREVIOUS STOP DRILL HOLE. STRINGER INSTALLED IAW BOEING DRG 65-18420.Feb 29, 2000 · N908UP · Boeing 72727C · Fuselage Main, Longeron/StringerSDR UPS00231974Skin · corrodedINSPECTION TYPE:C&SI, CORROSION ON SKIN BETWEEN BS 1080 AND BS 1183 STRINGER 4 RT TO STRINGER 10 RT. SKIN REMOVED IAW SRM 51-30-2. NEW SKIN DRILLED AND TRIMMED IAW SRM 51-30-2 AND DRG 65-18382. NEW SKIN INSTALLED IAW DRG 65-18382 AND SRM 51-30-2 AND 51-30-3Feb 26, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00231932Sill · corrodedINSPECTION TYPE:C&SI, CONTROL CABIN ENTRY DOOR SILL, STA 303.9, EVIDENCE OF CORROSION ON DOOR SILL BOTH UPPER AND LWR SURFACES AND BRACKET ON RT SIDE OF SILL CORRODED. CORROSION REMOVED IAW SRM 51-10-06, CORROSION FOUND TO BE WITHIN LIMITS OF SR 53-10-1 MAX DFeb 24, 2000 · N908UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231949Lug · corrodedINSPECTION TYPE:C&SI, CRACK ON ATTACH LUG OF FLAP POSITION TRANSMITTER HOUSING LEFT I/B FLAP CORRODED DRUM CRACKED HOUSING REPLACED IAW OHM 27-54-06.Feb 23, 2000 · N908UP · Boeing 72727C · Trailing Edge FlapsSDR UPS00231880Flap Track · crackedINSPECTION TYPE:C&SI, NR 3 SLAT, O/B SLAT TRACK, O/B RIB ATTACH POINT HAS SUSPECT CRACK. REPAIR CARRIED OUT AS PER SRM 51-40-2.Feb 21, 2000 · N908UP · Boeing 72727C · Leading Edge DevicesSDR UPS00231879Bracket · crackedINSPECTION TYPE:C&SI, ENGINE NR 1 THROTTLE SHUT OFF CONTROL BRACKET ASSY IN FWD END OF PYLON IS CRACKED. BRACKET REPLACED IAW MM 76-11-21.Feb 18, 2000 · N908UP · Boeing 72727C · Nacelle/Pylon StructureSDR UPS00231878Shear Tie · crackedINSPECTION TYPE:C&SI, CRACK ON SHEAR TIE CLIP BETWEEN STIFEFNER AND UPPER CHORD AT FWD WALL OF CENTER TANK BS 740 AT LBL 45.61. CHANGED SHEAR TIE CLIP IAW EO B727-5710-4595.Feb 18, 2000 · N908UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231976Lug · damagedINSPECTION TYPE:C&SI, ULTRASONIC INSPECTION OF HORIZ STAB HINGE LUGS (ON VERT STAB) LT AND RT, I/B AND O/B DUE SUSPECT INDICATION FROM HFEC INSPECTION. ULTRASONIC INSPECTION CARRIED OUT BOTH LEFT AND RIGHT BORES REPAIRED IAW UPS EO B727-5510-2284.Feb 17, 2000 · N908UP · Boeing 72727C · Horizontal Stabilizer StructureSDR UPS00231975Lap Joint · corrodedINSPECTION TYPE:C&SI, SUSPECT CORROSION ON LAP JOINT AT BS 300 TO BS 320 STRINGER 24 RT. LAP REPAIRED IAW EO B727-5330-0509 AND SRM 53-30-15A.Feb 16, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00231939Stringer · crackINSPECTION TYPE:C&SI, CRACK INDICATION FOUND AT BS 740 FWD LWR HOLE IN LINE WITH STR 16R. REPAIR CARRIED OUT IAW SMRO EO 2000-04-008 UPS ENGINEERING FILE NO 727-53-2231.Feb 16, 2000 · N908UP · Boeing 72727C · Fuselage Main, Longeron/StringerSDR UPS00231938Floorbeam · corrodedINSPECTION TYPE:C&SI, FWD CARGO LEFT FLOOR TRACK UPPER SURFACE CORRODED AT BS 482 ALSO CORROSION EVIDENT ADJACENT ANCHOR NUTS LWR SURFACE BS 480 - BS 540. FWD CARGO BAY LEFT FLOOR TRACK REPLACED FROM BS 480 TO 680 IAW SRM 51-30-2, 7 SRM 53-10-5 FIG 8.Feb 16, 2000 · N908UP · Boeing 72727C · Fuselage Main, Floor BeamSDR UPS00231936Skin · corrodedINSPECTION TYPE:C&SI, CORROSION ON WING CENTER SECTION UPPER SKIN AT BS 865 LBL 65.5. REPAIR CARRIED OUT IAW SMRO EO 200-004-004 UPS ENGINEERING FILE NR 727-57-2145.Feb 15, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00231935Mount · corrodedINSPECTION TYPE:C&SI, ON INSPECTION OF ENG NR 3 MOUNT HOLES CORROSION FOUND IN ALL HOLES. REPAIR CARRIED OUT IAW EO B727-5440-11592-A.Feb 14, 2000 · N908UP · Boeing 72727C · Engine Mount SectionSDR UPS00231934Mount · corrodedINSPECTION TYPE:C&SI , ON INSPECTION OF ENG NR 1 MOUNT HOLES CORROSION FOUND IN ALL HOLES. REPAIR CARRIED OUT IAW EO B727-5440-11592-A.Feb 14, 2000 · N908UP · Boeing 72727C · Engine Mount SectionSDR UPS00231995Flap Track · corrodedINSPECTION TYPE:C&SI NR 4 FLAP TRACK CORROSION ON FACES OF FWD SUPPORT LUGS. REPAIR CARRIED OUT IAW SMRO EO 2000-004-10 UPS ENGINEERING FILE NR 727-57-2147.Feb 13, 2000 · N908UP · Boeing 72727C · Trailing Edge FlapsSDR UPS00231876Seat Track · corrodedINSPECTION TYPE:C&SI, CORROSION ON SEAT TRACK UPPER FLANGE I/B AT BS 740 RBL 24.75. CORROSION REMOVED, LIMITS CHECKED AND FOUND OUTSIDE REF SRM 51-10-6. REPAIR CARRIED OUT IAW SRM 53-10-5.Feb 12, 2000 · N908UP · Boeing 72727C · Fuselage, Seat/Cargo Attach FittingsSDR UPS00231931Carriage · corrodedINSPECTION TYPE:C&SI, FLAP CARRIAGE NR 2 PITTING CORROSION IN BORE OF SPINDLE. CARRIAGE REPLACED IAW OHM 57-52-11..Feb 11, 2000 · N908UP · Boeing 72727C · Wing, Control SurfacesSDR UPS00231875Flap Track · crackedINSPECTION TYPE:C&SI, NR 2 SLAT, I/B TRACK ATTACH POINT HAS SUSPECT CRACK. REPAIR CARRIED IAW SRM 51-40-2.Feb 11, 2000 · N908UP · Boeing 72727C · Leading Edge DevicesSDR UPS00231873Skin · corrodedINSPECTION TYPE:C&SI, SUSPECT CORROSION BETWEEN SKIN AND DOUBLER AT BS 1120 - BS 1140 BETWEEN STR 3R AND STR 4R. REPAIR CARRIED OUT IAW B727 NDM PT6 51-00-00 FIG 4 AND 5.Feb 11, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00231943Pin · corrodedINSPECTION TYPE:C&SI, LEFT WING REAR SPAR TO BODY BOTTLE PIN HAS PITTING CORROSION ON FLANGE THAT SITS AGAINST SPAR TO BODY FITTING. BOTTLE PIN REPLACED IAW MM 57-41-01.Feb 10, 2000 · N908UP · Boeing 72727C · Wing Miscellaneous StructureSDR UPS00231872Sill · crackedINSPECTION TYPE:C&SI, SUSPECT CRACK ON MAIN CARGO DOOR SILL SKIN LWR SURFACE AT BS 488. MAIN CARGO DOOR SILL SKIN REPAIRED IAW SRM 51-40-2 FIG 1.Feb 10, 2000 · N908UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231871Skin · corrodedINSPECTION TYPE:C&SI, SUSPECT CORROSION BETWEEN SKIN AND DOUBLER AT BS 1120 - BS 1140, BETWEEN STR 3R AND 4R. REPAIR CARRIED OUT IAW SRM 51-00-00.Feb 10, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00231767Frame · corrodedINSPECTION TYPE:C, RIGHT MID CHORD IS CORRODED BS 300-306 WL 170 RBL 18, ACCESS RT MID CHORD. INSTALLED NEW MID CHORD REPLACED ACCESSED STRUCTURE PER SRM.*Feb 9, 2000 · N909UP · Boeing 72727C · Fuselage Main, FrameSDR UPS00231625Shear Tie · corrodedINSPECTION TYPE:C WHILE WORKING CUST ID NR 113675 FOUND CORROSION ON SHEAR TIE AT BS 312 BELOW STR RT SHEAR TIE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED SHEAR TIE WITH NEW ITEM PER SRM 51-40-2 AND 51-30-2.Feb 9, 2000 · N909UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231598Seat Track · corrodedINSPECTION TYPE:C CORROSION IN FWD CARGO BAY ON SEAT TRACK IN 3 AREAS AT RBL 14 BS 577, BS 585, AND BS 591 ON UPPER AND LOWER SURFACE. REMOVED CORROSION FROM OUTBOARD FLANGE ROM BS 577 TO BS 593 RBL 14. REMOVED .020 FROM ORIG .070, FOUND TO BE OUT OF LIMITS.Feb 9, 2000 · N909UP · Boeing 72727C · Fuselage, Seat/Cargo Attach FittingsSDR UPS00231996Fitting · crackedINSPECTION TYPE:C&SI RT BS 740 FITTING CRACKED BEYOND LIMITS. RT BS 740 FITTING REPLACED IAW EO B727-5310-7477-E.Feb 8, 2000 · N908UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231877Support · crackedINSPECTION TYPE:C&SI, AFT CARGO BAY FLOOR SUPPORT CRACKED AT BS 1070 RBL 12. AFT CARGO BAY FLOOR SUPPORT BEAM REPLACED IAW SRM 53-10-5.Feb 8, 2000 · N908UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231511Conduit · damagedINSPECTION TYPE:MOD, NR 2 ENGINE FUEL SOV CONDUIT WAS DAMAGED AT FWD END AND WIRING INSULATOR WAS PEELED OFF. INSTALLED NEW CONDUIT PER EO 00-0148. INSTALLED NEW WIRE IAW MM 28-22-11.Feb 5, 2000 · N909UP · Boeing 72727C · Engine Fuel DistributionSDR UPS00231600Angle · corrodedINSPECTION TYPE:C CORROSION (C53-100-01.00-02) ON L/GANGLE AT BS 949, WL 198, LBL 39. REMOVED, FABRICATED AND INSTALLED NEW L ANGLE. WORK DONE IAW SRM'S 51-30-2, 53-10-1 AND 51-30-5.Jan 31, 2000 · N909UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231599Angle · corrodedINSPECTION TYPE:C CORROSION (C53-100-01.00-02) ON L/ANGLE AT BS 949, WL 198, LBL 29.5. REMOVED, FABRICATED AND INSTALLED NEW L ANGLE. WORK DONE IAW SRM'S 53-10-1, 51-30-5 AND 51-30-2.Jan 31, 2000 · N909UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231510Gimbal · crackedINSPECTION TYPE:C, RIGHT I/B TRAILING EDGE FLAP, GIMBAL ELECTRIC ASSY, CRACKED AT NR 5 FLAP TRANSMISSION ATTACH POINT. GIMBAL REPLACED IAW MM 27-51-251, ADJUST/TEST CARRIED OUT IAW MM 27-51-22.Jan 28, 2000 · N910UP · Boeing 72727C · Trailing Edge Flap Control SystemSDR UPS00231508Skin · corrodedINSPECTION TYPE:C, BS 470 AT STR 7L RIVET PULLED RIVET TAIL. REMOVED IAW SRM 51-30-2. EVIDENCE OF CORROSION BETWEEN SKIN AND INTERNAL DOUBLER. FUSELAGE SKIN REPAIRED BETWEEN BS 440 AND BS 507 STR 2L TO 7L IAW SMRO EO NR 2000-002-05. UPS ENGINEERING FILE NR Jan 25, 2000 · N910UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00231504Stop · crackedINSPECTION TYPE:C, NR 5 FWD STOP ON AFT CARGO DOOR FOUND CRACKED. PART REPLACED IAW B727-5230-0032.Jan 25, 2000 · N910UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231509Rib · crackedINSPECTION TYPE:C, RIGHT O/B AILERON L/E NOSE RIB NR 2 I/B OF TAB ACTUATING MECHANISM CRACKED. REPAIR CARRIED OUT IAW SRM 51-40-3, FASTENERS INSTALLED IAW SRM 51-30-2.Jan 21, 2000 · N910UP · Boeing 72727C · AileronsSDR UPS00231503Stop · crackedINSPECTION TYPE:C, SUSPECT CRACK ON NR 4 STOP FORWARD ON AFT CARGO DOOR (INTERNAL). HFEC INSPECTION CARRIED OUT IAW B727 NDTM PT 6, 51-00-00 FIG 4, CRACK CONFIRMED. NR 4 STOP REPLACED IAW EO B727-5230-0032, APPENDIX C.Jan 20, 2000 · N910UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231502Support · corrodedINSPECTION TYPE:C, SURFACE CORROSION ON UPPER SIDE OF TOILET PARTITION SUPPORT BS 330 APPROX RBL 20. CORROSION ON THE TOILET PARTITION SUPPORT REMOVED AND FOUND MUCH DEEPER AND OUTSIDE LIMITS. PARTITION SUPPORT REPLACED. FABRICATED FROM EXTRUSION BAC 1510-3Jan 20, 2000 · N910UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231467Skin · delaminatedINSPECTION TYPE:C, LT O/B AILERON DELAM ON UPPER AND LWR SKIN AT T/E O/B OF TAB. REPAIRED IAW SRM 51-40-6 FIG 39.Jan 20, 2000 · N910UP · Boeing 72727C · AileronsSDR UPS00231466Bracket · crackedINSPECTION TYPE:C, SUSPECT CRACK ON NLG MANUAL GEAR EXTENSION JACKSCREW LWR SUPPORT BRACKET ON RT SIDE OF W/W. REPLACED NLG MANUAL EXTENSION JACKSCREW LWR SUPPORT BRACKET ON RT SIDE OF W/W IAW SRM 51-30-2 AND DRAWING NR 65-21947.Jan 19, 2000 · N910UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231465Channel · crackedINSPECTION TYPE:C, NLG LOCK ACTUATOR BULKHEAD CHANNEL SUPPORT CRACKED. REPAIRED NLG LOCK ACTUATOR CHANNEL SUPPORT IAW SRM 51-30-2 AND DRAWING NR 69-18194.Jan 19, 2000 · N910UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231277Battery Pack · dischargedEMERGENCY EXIT LIGHT IN COCKPIT AND MAIN ENTRY DOOR INDICATE LOW BATTERY. REMOVED AND REPLACED EMERGENCY LT BATTERIES.Jan 11, 2000 · N908UP · Boeing 72727C · Emergency LightingSDR UPS00231267Skin · corrodedCORROSION FOUND ON FUSELAGE COMPLY WITH D185003 CORROSION AT STA 118 3 LEFT SIDE. CUT OUT DAMAGED SECTION AT STR 9 LT BS1181 TO 1175 PER SRM 51-10-1. PERFORMED HFEC INSP OF CUTOUT PER NDT PART 6 51-10-1 FIG 4 AND NO CRACKS NOTED. COMPLETED REPAIR PER SRM 51Jan 11, 2000 · N915UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS99231235O2 Bottle · dischargedINSPECTION TYPE:N/A, CREW O2 BOTTLE READS LOW. REMOVED AND REPLACED BOTTLE.Dec 24, 1999 · N914UP · Boeing 72727C · Crew Oxygen SystemSDR UPS99231197Smoke Detector · inoperativeINSPECTION TYPE:N/A, LT LWR SMOKE DETECTOR INOP. RELAMPED SMOKE DETECTOR.Dec 15, 1999 · N914UP · Boeing 72727C · Smoke DetectionSDR UPS99231151Light · looseINSPECTION TYPE:N/A, COCKPIT DOOR EMERGENCY EXIT LIGHT FELL OFF ITS MOUNT DURING FLIGHT. RESECURED LIGHT, OPS CHECKS NORMAL.Nov 24, 1999 · N914UP · Boeing 72727C · Emergency LightingSDR UPS99231121Indicator · inopINSPECTION TYPE: N/A, ON FLAP SELECTION NO O/B FLAP MOVEMENT, SPLIT FLAP COND. PERFORMED SPLIT FLAP AND ALT USE FLAP EXTENTION CHECKLIST. NORMAL LANDING. REMOVED AND REPLACED O/B FLAP POSITION INDICATOR PER MM 27-52-21 AND ADJUSTED RIGHT O/B FLAP POSITION TNov 16, 1999 · N939UP · Boeing 72727C · Trailing Flap Position Indicating SystemSDR UPS99231118Light · inopINSPECTION TYPE: N/A, EMERGENCY EXIT LIGHT FWD ENTRY DOOR INTERMIT (REPEAT ITEM). ACCOMPLISHED VOLTAGE CHECK IAW MM 33-50-01, OPS CHECK GOOD. REPLACED LIGHT MOUNT, DISCOVERED A POOR CONTACT.Nov 15, 1999 · N909UP · Boeing 72727C · Emergency Lighting
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