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 CA110817010Actuator · sheared(CAN) UPON DEPARTURE THE NR 2 SLAT FAILED TO RETRACT. THE FLAPS WERE CYCLED AND SHORTLY AFTER "A" SYS HYD QTY WENT TO ZERO. AN EMERGANCY WAS DECLARED AFTER THE CHECK LISTS WERE RUN, AND LANDED WITHOUT PROBLEM. DUE TO HYD LOSS THE ACFT WAS TOWED OFF THE RUNWAug 16, 2011 · Boeing 72727C · Leading Edge Slat ActuatorSDR UPS03240006Battery · dischargedINSPECTION TYPE: PFLT. EMERGENCY EXIT LIGHT ASSEMBLIES AT CABIN ENTRY AND CREW ENTRY DOOR BATTERIES DEAD. RECHARGED BATTERIES, OPS CHECKS OKAY.Jan 9, 2003 · N909UP · Boeing 72727C · Emergency LightingSDR UPS02239857Cover · looseINSPECTION TYPE:N/A MAIN ENTRY DOOR EMERGENCY LIGHT FELL OUT OF BRACKET DURING T/O. R&R MAIN ENTRY DOOR EMERGENCY LIGHT COVER OK FOR CONTINUED SERVICE.Nov 4, 2002 · N908UP · Boeing 72727C · Emergency LightingSDR UPS02238614Slat · crackedINSPECTION TYPE:AS NR 5 SLAT CRACKED OUTBOARD OF FENCE JUST OUTBOARD OF UPSTOP. REMOVED AND REPLACED NR 5 SLAT PER MM 27-81-11, RIG AND OPS CHECK GOOD.Jun 12, 2002 · N910UP · Boeing 72727C · Leading Edge DevicesSDR UPS02237507Battery · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERIES NOT CHARGED OVER MAIN ENTRY DOOR, PARTS ON F/E'S DESK LIGHT ASSY 10-0067-9. INSTALLED NEW BATTERIES.Jan 23, 2002 · N910UP · Boeing 72727C · Emergency LightingSDR UPS02237399Light · inoperativeINSPECTION TYPE:PFLT L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM 33-50-01, OPS CHECK NORMAL.Jan 7, 2002 · N909UP · Boeing 72727C · Emergency LightingSDR UPS01237314Smoke Detector · inoperativeINSPECTION TYPE:N/A TARGET ALERT H20824 LOWER CARGO SMOKE DETECTION. LOWER CARGO SMOKE DETECTOR MX LT ILLUM. TECH RECOMMENDS: SUSPECT A-CHANNEL OF CCU FAILED. REPLACE CCU. PERFORMED ADJUSTMENT TEST PER MM 26-18-01, VERIFIED SN OF SMOKE DETECTORS. NO FURTNov 17, 2001 · N914UP · Boeing 72727C · Smoke DetectionSDR UPS01237194Battery · dischargedINSPECTION TYPE:IN CREW ENTRANCE DOOR EMERGENCY EXIT LIGHT WENT DIM SHORTLY AFTER TESTING LIGHTS. REPLACED BATTERIES WITH CHARGED UNITS. OPS CHECKED GOOD IAW MM 33-51-01 PG 104. P/N S106Oct 29, 2001 · N909UP · Boeing 72727C · Emergency LightingSDR UPS01237094Battery · dischargedINSPECTION TYPE:N/A, OVERHEAD LIGHTS ABOVE CREW ENTRY DOOR INOP. REPLACED BATTERIES IAW 33-50-00. OPS CHECKS GOOD.Oct 18, 2001 · N909UP · Boeing 72727C · Emergency LightingSDR UPS01236825Control Cable · corrodedINSPECTION TYPE:IN REF SEG CHECK NR 7 NWW DOOR ACTUATION CABLES DRY WITH EVIDENCE OF SURFACE CORROSION. CLEANED & LUBRICATED AS REQUIRED PER MM 12-20-01.Sep 16, 2001 · N911UP · Boeing 72727C · Landing Gear Door Retract SectionSDR UPS01236824Control Cable · corrodedREF SEG CHECK NR 7 NOSE GEAR MANUAL EXTENSION CABLES DRY WITH EVIDENCE OF SURFACE CORROSION. CLEANED AND LUBRICATED AS REQUIRED. OK FOR SERVICE PER MM 12-20-01.Sep 16, 2001 · N911UP · Boeing 72727C · Landing Gear Retraction/Extension SystemSDR UPS01236683Hydraulic Line · leakingINSPECTION TYPE:N/A SHORTLY AFTER TAKEOFF SYSTEM B ELECTRIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED. SYSTEM B QTY INDICATED 0. EMERGENCY CHECKLISTS ACCOMPLISHED AND LANDING WAS UNEVENTFUL. FOUND OUTLET LINE OF NR 2 B PUMP LEAKING. PERFORMED AN INTERIM HOSE REPAIAug 23, 2001 · N907UP · Boeing 72727C · Hydraulic System, AuxiliarySDR UPS01236690Stringer · crackedINSPECTION TYPE:C SUSPECT CRACK IN CENTRE SECTION UPPER STRINGER S1 IN THE WING CENTRE TANK STRINGER REPAIRED IAW SRM 57-10-04 FIG 2Aug 16, 2001 · N908UP · Boeing 72727C · Wing Main, Frame StructureSDR UPS01236664Stringer · crackedINSPECTION TYPE:C ON INSPECTION OF FUSELAGE STRINGERS AT BS 400 WHERE ACCESSABLE, S18R AT BS 400 FOUND TO BE CRACKED. STRINGER REPAIR CARRIED IAW SRM PROCEDURESAug 15, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS01236658Stringer · crackedINSPECTION TYPE:C ON INSPECTION OF FUSELAGE STRINGERS AT BS 400 WHERE ACCESSABLE, STRI NGER 18R AT BS 400 FOUND TO BE CRACKED. STRINGER REPAIRED IAW SRM.Aug 15, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS01236689Stiffener · corrodedINSPECTION TYPE:C WING CENTRE SECTION UPPER SKIN STIFFENER LWR CHORD IS CORRODED AT BS 870 RBL0. ***CPCP*** DAMAGED SECTION REMOVED AND NEW SECTION SPLICED IAW SRMAug 13, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236686Intercostal · crackedINSPECTION TYPE:C SUSPECT CRACK AT R/H BS 1183 WL 230 OUTBD LWR CORNER OF INTERCOSTAL AT RBL 62.5 INTERCOSTAL REPLACED IAW DWG 65-16350Aug 13, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236688Terminal · crackedINSPECTION TYPE:C L/H UPPER TENSION TIE CRACKED IN TAIL SKID BAY FABRICATED TERMINAL IAW DWG 65-85208, REMOVED / INSTALLED PER SRMAug 11, 2001 · N908UP · Boeing 72727C · Auxiliary Gear (Tail Skid)SDR UPS01236679Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION S6L AT BS 400 FOUND TO BE CRACKED. DAMAGED STRINGER REPAIRED IAW SRM 53-10-3Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236678Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION S3R FOUND CRACKED AT BS 400 REPAIRED PER SRM.Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236677Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION S9R FOUND CRACKED AT BS 400 STRINGER REPAIRED IAW SRM.Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236676Stringer · crackedINSPECTION TYPE:C ON FURTHER INSP FOR ACCESS S15R AT BS 400 FOUND TO BE CRACKED REPAIRED IAW SRMAug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236675Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS S16R FOUND CRACKED AT BS 400 REPAIRED IAW SRM.Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236661Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS S15L FOUND CRACKED AT BS 400 REPAIRED IAW SRMAug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236660Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS, S16L FOUND CRACKED AT BS 400 REPAIRED IAW SRMAug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236657Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION STRINGER S6R FOUND CRACKED AT BS 400 REPAIRED PER SRMAug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236687Strap · crackedINSPECTION TYPE:C ON NDT INSP, CRACK INDICATION FOUND IN REINFORCING STRAP OF MID GALLEY DOOR CUTOUT FWD UPPER CORNER. REPAIR CARRIED OUT PER UPS EO B727-5330-2695 APPENDIX 8.2Aug 10, 2001 · N908UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS01236685Intercostal · crackedINSPECTION TYPE:C INTERCOSTAL CRACKED ABOVE DRAG BRACE FITTING SUPPORT INTERCOSTAL REPLACED IAW DRWG 65-18417Aug 10, 2001 · N908UP · Boeing 72727C · Standard Practices/StructuresSDR UPS01236666Frame · crackedINSPECTION TYPE:C CRACK BS 930 R/H FLANGE I/B LOWER CORNER RADIUS REPAIRED PER SRM ADDENDUM B727-5310-2611BAug 10, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236684Skin · corrodedINSPECTION TYPE:C AREA OF LIGHT SURFACE CORROSION ON SKIN AT BS660 S19R ***CPCP*** AREA REPAIRED IAW APPENDIX 8.3 OF EO B727-5330-0509Aug 9, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS01236681Skin · crackedINSPECTION TYPE:C SKIN CRACKS BS 400 BETWEEN S16R 15R REPAIRED IAW SRMAug 9, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS01236680Frame · corrodedINSPECTION TYPE:C BODY FAIRING #3430 HAS CORRODED FRAME AT R/H GND FAN LOUVRE DOOR AFT CUTOUT. FRAME FABRICATED AND INSTALLED PER SRMAug 9, 2001 · N908UP · Boeing 72727C · Aerodynamic FairingsSDR UPS01236673Skin · crackedINSPECTION TYPE:C SKIN CRACKS BS 400 BETWEEN S16L AND 15L CRACKS REPAIRED IAW SRMAug 9, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS01236530Battery · dischargedINSPECTION TYPE:IN ILLEGIBLE EXIT LIGHT AT MAIN ENTRY DOOR INOP. REPLACED ILLEGIBLE EXIT LIGHT BATTERY AND OPS CHECK AS PER B727 M/M 33-50-00.Aug 3, 2001 · N914UP · Boeing 72727C · Emergency LightingSDR UPS01236437Pressure Panel · crackedINSPECTION TYPE:C CRACK IN MLG WEB BS 938 O/B AFT CORNER ADJACENT TO STR 18A LWR FASTENER ROW IN RT MLG WW CRACK DRESSED OUT AND NDT CONFIRMED REMOVAL SRM51-10-1 WEB REPAIRED IAW SRM 51-20-02.Jul 31, 2001 · N909UP · Boeing 72727C · Fuselage Main, BulkheadSDR UPS01236444Fitting · corrodedINSPECTION TYPE:IN FRAME FOOT ANGLE AT FS 351 BETWEEN STRINGERS 24R AND 25R IS SEVERELY CORRODED. THIS IS UNDER FLOOR PANEL ON RT SIDE OF NLG WW ENCLOSURE ON THE INSIDE. R&R FRAME FOOT ASSY PER SRM 51-30-02.Jul 30, 2001 · N915UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS01236434Angle · crackedINSPECTION TYPE:N/A FRAME ANGLE CRACKED STA 351 JUST AFT OF O/B AFT CORNER OF ACCESS PANEL BEHIND NLG RT SIDE CUTOUT DAMAGED ANGLE PER SRM 51-10-01 PERFORMED HFEC INSPECTION OF CUTOUT AREA NO CRACKS NOTED REPAIRED PER B727 5330 15208.Jul 27, 2001 · N915UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS01236476Fitting · crackedINSPECTION TYPE:C TAIL SKID LT LWR TENSION TIE REAR TERMINAL FITTING CRACKED. LT LWR TENSION TIE AFT FITTING REMOVED AND NEW ONE INSTALLED IAW DRAWING 65-25992.Jul 22, 2001 · N909UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS01236400Skin · corrodedINSPECTION TYPE:N/A CORROSION AFT OF NLG WW, BELLY SKIN. REMOVED CORROSION AT BS 340 TO BS 360 BETWEEN STR 26 AND 27 RT PER SRM 51-10-01. INSTALLED LT AND RT INTERNAL DOUBLER SPLICES AND T ANGLES, INSTALLED NEW FUSELAGE SKIN IAW 727 SRM 51-30.Jul 20, 2001 · N915UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS01236438Frame · damagedINSPECTION TYPE:C FRAME DAMAGED AT BS 320 STR22R STR27R (HOLES DAMAGED) FRAME REPLACED IAW SRM 51-30-02 AND DRWG 65-18420Jul 20, 2001 · N909UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236439Bracket · crackedINSPECTION TYPE:C CRACK ON EDGE OF FLOOR PANEL SUPPORT BRACKET AT STA 755 LBL 50. NEW BRACKET FITTED IAW SRM 51-30-02.Jul 18, 2001 · N909UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS01236440Skin · corrodedINSPECTION TYPE:C CORROSION ON LAP S24R BS 295 CPCP NEAR REPAIR REQUIRED SKIN REPLACEMENT WHICH ENCOMPASSED THIS DAMAGE , SKIN REPLACED.Jul 17, 2001 · N909UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS01236436Fitting · crackedINSPECTION TYPE:C SUSPECT CRACK AT TAIL SKID COMPT, RT UPPER TENSION TIE END FITTING CRACK CONFIRMED BY NDT, FITTING REPLACED IAW DRAWING.Jul 17, 2001 · N909UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS01236460Hinge · crackedINSPECTION TYPE:C MAIN CARGO DOOR FWD AND AFT HINGES CRACKED. ON INVESTIGATION HINGES FOUND CORRODED BEYOND LIMITS, HINGES REPLACED IAW OHM 20-50-01Jul 16, 2001 · N909UP · Boeing 72727C · Cargo/Baggage DoorsSDR UPS01236413Floor Support · corrodedINSPECTION TYPE:N/A LAV FLOOR SUPPORT CORRODED RBL 40 BS290 TP BS 312 REMOVED CORROSION AT LAV FLOOR SUPPORT RBL 40 BS290 TO BS 312 MATERI AL LOSS .050 FOUND OUT OF LIMITS AS PER B727 SRM 51-30-02 REPLACED F LOOR MATERIAL USE 60-8265 T ANGLE 8" TREAT AND PJul 11, 2001 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS01236411Beam · crackedINSPECTION TYPE:N/A AFT PRESSURE BULKHEAD VERTICAL BEAM LBL 17.8 WL 264.5 SHOW CRACK RUNNING FROM STOP DOOR CUT OUT TO O/B CHORD. CUT OUT DAMAGED SECTION OF VERTICAL BEAM AT W/L 249 IAW UPS EO B727-53 10-11743 APPENDIX E INSTALLED NEW SECTION AND REMOVED PARTSJul 10, 2001 · N914UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236414Pressure Panel · crackedINSPECTION TYPE:N/A NLG WW LT SIDE WALL CRACK INDICATION BETWEEN FASTENERS BS 235 AND LOWER OF FWD ACCESS. REMOVE ACCESS NR 3122 FOR ACCESS REPAIR AS PER B727SRM 51-30-02 CUT OUT DAMAGED AREA AS PER B727 SRM 51-30-02, SIZE OF CUT 2X1 INCH ACCOMPLISHED NDT ON CJul 9, 2001 · N914UP · Boeing 72727C · Fuselage Main, BulkheadSDR UPS01236392Stringer · crackedINSPECTION TYPE:C END OF STRINGER 15 @ BS 676 LH IS CRACKED. REPAIR CARRIED OUT IAW 51-30-2 & 53-10-3Jul 9, 2001 · N910UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236314Stringer · crackedINSPECTION TYPE:C END OF STRINGER 15 @ BS 676 LH IS CRACKED REPAIR CARRIED OUT IAW 51-30-2 & 53-10-3Jul 9, 2001 · N909UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236412Frame · crackedINSPECTION TYPE:C LH WHEEL WELL TOP OB EXPOSED PORTION OF BS 930 FRAME IS CRACKED IB S IDE TOP INSTALL REPAIR AS PER REPAIR ORDER AVHM 233RO-1. ENGINEERING FILE NO 727-53-20023. MAT USED 310 1/2 HD .080 BOTTOM DOUBLER 15X8" TOP DOU BLER 6X6", TOP STRAP 20Jul 6, 2001 · N914UP · Boeing 72727C · Fuselage Main, Structure
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