Boeing 727-108C

Service difficulty reports · 255

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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 = '727108C'
  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 UPS03240302Flap Track · corrodedINSPECTION TYPE: C&SI, NR 5 FLAP TRACK HAS CORROSION ON MOUNT HOLES C, E, F & CORROSION ON MOUNT PADS A & B. REFER TO SMRO EO 2003-008-008 & UPS EO B727-5742-0651-K FOR DETAILED SIGNOFF & RECTIFICATION. UPS ENGINEERING FILE B727-540-18418-B.Feb 18, 2003 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS03240277Flap Track · crackedINSPECTION TYPE:C&SI #6 FLAP TRACK HAS SUSPECT CRACK FROM HOLE F ON SPOILER SUPPORT BEAM PAD REPLACED #6 FLAP TRACK IAW MM 27-51-31Feb 18, 2003 · N936UP · Boeing 727108C · Trailing Edge Flap Control SystemSDR UPS03240272Hinge · corrodedINSPECTION TYPE: C+SI, LT WING O/B AILERON BEARING HINGES (4 OFF) CORRODED. LEFT O/B AILERON REPLACED IAW MM 27-10-14.Feb 18, 2003 · N936UP · Boeing 727108C · Aileron Control SystemSDR UPS03240271Carriage · corrodedINSPECTION TYPE:C+SI ON REMOVAL OF SEALANT FROM THE INNER BORE OF NO.6 FLAP TRACK CARRIAG E SPINDLE,EXCESSIVE CORROSION IS EVIDENT. NO.6 FLAP TRACK CARRIAGE REPLACED IAW OHM 57-58-02.Feb 18, 2003 · N936UP · Boeing 727108C · Trailing Edge Flap Control SystemSDR UPS03240265Carriage · corrodedINSPECTION TYPE:C&SI ON REMOVAL OF SEALANT FROM THE INNER BORE OF SPINDLE ON FLAP TRACK C ARRIAGE #5 EXCESSIVE CORROSION IS EVIDENT #5 FLAP TRACK CARRIAGE REPLACED IAW OHM 57-58-02Feb 18, 2003 · N936UP · Boeing 727108C · Trailing Edge Flap Control SystemSDR UPS03240262Aileron · corrodedINSPECTION TYPE:C&SI CORROSION ON O/B R/H AILERON HINGES 2, 3 & 4 ON INVESTIGATION OF HINGE ASSYS, HINGES FOUND TO BE CORRODED BEYOND ALLOWABLE LIMITS IAW SRM 57-50-11. INSTALLED REPLACEMENT AILERON IAW MM 27-10-14. REF. NRC 632179 FOR AILERON RIGGING & Feb 18, 2003 · N936UP · Boeing 727108C · Aileron Control SystemSDR UPS03240305Panel · delaminatedINSPECTION TYPE:C&SI DELAM ON R/H WING TE PANEL UPPER FWD OF NO 10 SPOILER PANEL REPAIRED IAW SRM 51-40-5Feb 17, 2003 · N936UP · Boeing 727108C · Wing Miscellaneous StructureSDR UPS03240304Fitting · crackedINSPECTION TYPE:C&SI 2 SUSPECT CRACKS ON R/H AFT UPPER 940 FLOORBEAM ATTACH FLANGE CRACKS OUT OF LIMITS FITTING REPLACED IAW UPS EO B727-5310-4501Feb 17, 2003 · N936UP · Boeing 727108C · Fuselage Main, StructureSDR UPS03240303Pressure Panel · crackedINSPECTION TYPE: C&SI, SUSPECT CRACK AT AFT END OF BEAD IN RIGHT MLG CEILING AT BS 940 RBL 58 APPROX. REPAIRED IN CONJUNCTION WITH 940 FITTING REPLACEMENT REF NRC 631320.Feb 17, 2003 · N936UP · Boeing 727108C · Fuselage Main, BulkheadSDR UPS03240282Skin · corrodedINSPECTION TYPE:C&SI SKIN BULGING JUST FWD OF 1183 AND BETWEEN STR 9R & 10R AREA FOUND CORRODED OUTSIDE LIMITS IAW SRM 51-30-01. DAMAGED AREA CU T OUT IAW SRM 51-30-3 AT STR. 9.REMOVED CORROSION IAW SRM 51-20-01 F OUND WITHIN LIMITS IAW SRM 53-30-01. STRINFeb 17, 2003 · N936UP · Boeing 727108C · Fuselage Main, Plate/SkinSDR UPS03240264Skin · corrodedINSPECTION TYPE: C&SI, AREA OF LIGHT SURFACE CORROSION ON SKIN ABOVE ENG NR 2 PYLON RT SIDE AT BS 1363 AT RT COWL HINGE LINE. FASTENERS REMOVED FROM SKIN & GUTTER IAW SRM 51-30-02. NEW PANEL MADE IAW SRM 54-10-2 & 51-10-1. NEW PANEL ALODINED & PRIMED IAW SFeb 17, 2003 · N936UP · Boeing 727108C · Fuselage Main, Plate/SkinSDR UPS03240263Rib · corrodedINSPECTION TYPE: C&SI, LEFT WING, L/E CAVITY SUPPORT RIB CORRODED AT FSS 250 ADJACENT TO WIRING P-CLIP. REMOVED RIB IAW SRM 51-30-02, FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-01. REPLACED EXTRUDED TEE TO RIB IAW SRM 51-30-02. INSTALLED RIB IAW SRM 51-30-02Feb 17, 2003 · N936UP · Boeing 727108C · Wing, Rib/BulkheadSDR UPS03240306Flange · crackedINSPECTION TYPE: C&SI, LEFT MAIN WHEEL WELL BS 930 FITTING SUSPECT CRACK ON I/B VERTICAL FLANGE. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-40-04, 53-10-3, 53-10-4, 51- 10-02 & 51-40-3 & DRAWINGS 65-16336 & 65C15732.Feb 14, 2003 · N936UP · Boeing 727108C · Fuselage Main, StructureSDR UPS03240299Support Fitting · crackedINSPECTION TYPE: C&SI, CRACK FOUND AT CLEAT BETWEEN MCD SUPPORT FITTING AND FRAME AT STA 540 WL 207 CRACK START AT RIVET TO EDGE OF CLEAT .375 INCH. REPAIR CARRIED OUT IAW SRM 51-40-3.Feb 14, 2003 · N936UP · Boeing 727108C · Fuselage Main, StructureSDR UPS03240258Pressure Panel · crackedINSPECTION TYPE: C&SI, AIR LEAK COMING FROM WHAT APPEARS TO BE CRACK IN PRESSURE WEB IN NOSE W/W LEFT SIDE MIDWAY ON LT SIDE WALL. CRACKED AREA CUT OUT IAW SRM 51-40-2. DOUBLER & FILLER FABRICATED IAW SRM 51-40-2. HFEC C/O ON CUTOUT ON THE ABOVE AREA IAW NFeb 14, 2003 · N936UP · Boeing 727108C · Fuselage Main, BulkheadSDR UPS03240257Skin · crackedINSPECTION TYPE:C&SI AIR LEAK COMING FROM WHAT APPEARS TO BE CRACK IN SKIN OF NOSE W/W L/ H SIDE ABOVE DECAL FOR STRUT SERVICING. CRACKED AREA CUTOUT IAW SRM 51-40-2 DOUBLER, FILLER & SHIM FABRICATE D IAW SRM 51-40-2.. HFEC C/O AROUND CUTOU ON THE AREA - NFeb 14, 2003 · N936UP · Boeing 727108C · Fuselage Main, Plate/SkinSDR UPS01235299Support Fitting · crackedINSPECTION TYPE:HFEC REFERENCE D211423 VERTICAL SUPPORT FITTINGS AT BS 930 BETWEEN STRINGERS 14 AND 18A HAS APPROX 5 INCHES CRACK (LEFT HAND SIDE). CLEANED AREA PERFORMED HFEC INSP PER B727 NDT MANUAL PART 6-51-00-00 FIG 4 ON BS 930 FITTING LT SIDE CRACK DOESMar 16, 2001 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS01235080Door · inoperativeINSPECTION TYPE:N/A, UPON PLACING GEAR HANDLE IN OFF POSITION AFTER T/O RED DOOR LIGHT ON FROM PANEL AND RIGHT MAIN GEAR DOOR LIGHT ON S/O PANEL ILLUMINATED. GEAR WAS CYCLED, SAME INDICATIONS AGAIN OCURRED WHEN GEAR HANDLE WAS PLACED IN OFF POSITION. *S/D* Feb 22, 2001 · N936UP · Boeing 727108C · Landing Gear Door Retract SectionSDR UPS01235033Warning Light · illuminatedINSPECTION TYPE:N/A, RT MLG DOOR WARNING ILLUM. OK TO FLY ON REVENUE TO CAE FROM PHL AS PER EO B727-1245B-DISSUED. A/C MUST FLY WITH GEAR HANDLE IN UP POSITION AT ALL TIMES NO FURTHER ACTION IS REQUIRED.Feb 22, 2001 · N936UP · Boeing 727108C · Landing Gear Position and WarningSDR UPS00234431Switch · malfunctionedINSPECTION TYPE:N/A - AIR TURNBACK, UNABLE TO RETRACT FLAPS PAST 2 DEGREES. REMOVED AND REPLACED NR 2 FLAP SWITCH.Nov 10, 2000 · N936UP · Boeing 727108C · Leading Edge Slat Control SystemSDR UPS00233024Skin · crackedINSPECTION TYPE:N/A SMALL CRACK ON LT HORIZANTAL LEADING EDGE VERIFIED CRACK WITH HFEC REPAIRED CRACK PER SRM 55-10-3. THIS EXTERNAL DOUBLER MUST BE REPLACED WITH A FLUSH REPAIR PER SRM 5501003, FIG 2 NO LATER THAN NEXT C CHECK.Jun 27, 2000 · N936UP · Boeing 727108C · Horizontal Stabilizer, Plate/SkinSDR UPS00233023Skin · crackedINSPECTION TYPE:N/A CRACK FOUND AFT LOWER FUSELAGE SIDE JUST IN FRONT OF AIRSTAIRS STOP DRILLED CRACK PER EO B727-5330-12732-A. PERFORMED HFGC NO CRACKS BEYOND STOP DRILL PERMANENT REPAIR WITHIN 15 DAYS. RCQC 15650Jun 27, 2000 · N936UP · Boeing 727108C · Fuselage Main, Plate/SkinSDR UPS00231762O2 Regulator · inoperativeF/O 02 REGULATOR INOP. REPLACED F/O REGULATOR AND MASK.Feb 22, 2000 · N936UP · Boeing 727108C · Crew Oxygen SystemSDR UPS99231182Switch · out of adjustINSPECTION TYPE:N/A, AFTER GEAR RETRACTION, RED DOORS LIGHT REMAINED ILLUMINATED, CYCLED GEAR, LIGHT WENT OUT. PERFORMED ADJ/TEST OF LANDING GEAR DOOR WARNING SWITCHES PER AMM 32- 62-11 PG 501. ALL INDICATORS LIGHTS CK GOOD PER MM REFERENCE.Dec 7, 1999 · N936UP · Boeing 727108C · Landing Gear Position and WarningSDR UPS99230329Light · inopINSPECTION TYPE:N/A COCKPIT ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERIES, LIGHTS OPS CK OK.Aug 17, 1999 · N936UP · Boeing 727108C · Emergency LightingSDR UPS99230328Light · inopINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR INOP. REPLACED BATTERIES, OPS CKS OK.Aug 17, 1999 · N936UP · Boeing 727108C · Emergency LightingSDR UPS99228745Bulb · failedINSPECTION TYPE-N/A, EMER EXIT LIGHT ABOVE COCKPIT ENTRY DOOR VERY WEAK. RELAMPED, OPS CHECKS OK.Feb 20, 1999 · N936UP · Boeing 727108C · Emergency LightingSDR UPS98228013Bearing · corrodedINSPECTION TYPE:C FWD RT MLG TRUNNION BEARING (FWD) AND SUPPORT CORRODED. BEARING AND SUPPORT REPLACED IAW MM 32-11-51 AND 32-11-72.Oct 23, 1998 · N936UP · Boeing 727108C · Main Landing Gear Attach SectionSDR UPS98227989Frame · crackedINSPECTION TYPE-C, CRACK FOUND EMINATING FROM FASTENER HOLE ON FRAME 760.95 RT OVERSIZE HOLE. FRAME 760.95 RT REPAIRED IAW APPENDIX C OF EO B727-5310-5474.Oct 14, 1998 · N936UP · Boeing 727108C · Fuselage Main, FrameSDR UPS98228011Support · corrodedINSPECTION TYPE:C SUPPORT ASSY CORRODED FOR RT I/B FLAP I/B TRACK AT ATTACH HOLE FOR MLG FITTING BOLT. SUPPORT ASSY REPLACED IAW MM 32-11-51.Oct 13, 1998 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS98228009Support Rod · shearedINSPECTION TYPE:C NR 8 SPOILER I/B HINGE SUPPORT ROD SHEARED. SUPPORT ROD REMOVED AND REPLACED IAW MM SRM 51-30-2.Oct 12, 1998 · N936UP · Boeing 727108C · Drag Control SystemSDR UPS98227988Bracket · crackedINSPECTION TYPE-C, RT ELEVATOR AT REAR SPAR AND ELEV STA 66.5 BRACKET CRACKED. REPLACED BRACKET IAW DRAWING NR 69-19144 AND DRAWING NR 65-25635.Oct 12, 1998 · N936UP · Boeing 727108C · Elevator StructureSDR UPS98227987Fitting · corrodedINSPECTION TYPE-C, CORROSION FOUND ON RT LANDING GEAR SUPPPORT FITTING ON WING REAR SPAR STA 224.5. FITTING REPLACED IAW DRAWING 65-84405.Oct 11, 1998 · N936UP · Boeing 727108C · Wing Miscellaneous StructureSDR UPS98228008Bracket · crackedINSPECTION TYPE:C ENGINE NR 3 ENGINE CONTROLS DRUM INSTALLATION, SUPPORT BRACKET HAS SUSPECT CRACK. REPAIRED BRACKET, REINSTALLED AS PER MM CHP 76-11-21.Oct 9, 1998 · N936UP · Boeing 727108C · Power LeverSDR UPS98227986Channel · crackedINSPECTION TYPE-C, SUSPECT CRACK AT BS 351-2 LOCK ACTUATOR SUPPORT CHANNEL LT SIDE UPPER BOLT HOLE. REPLACED CHANNEL IAW DRAWING NR 69-19122.Oct 9, 1998 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS98228035Fitting · corrodedINSPECTION TYPE-C, CORROSION ON 870 FRAME RT AT FLOORBEAM ATTACH RBL 62.5. FITTING REPLACED IAW EO B727-5310-3056.Oct 8, 1998 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS98228034Frame · crackedINSPECTION TYPE-C, SUSPECT CRACK OUTBOARD FLANGE RADIUS BS 910 LT BETWEEN STRINGER 18A SILL AND WHEEL WELL CEILING LT WHEEL WELL. REPAIR CARRIED OUT IAW SRM ADDENDUM EO B727-5310-1896.Oct 8, 1998 · N936UP · Boeing 727108C · Fuselage Main, FrameSDR UPS98228010Casting · corrodedINSPECTION TYPE:C ON REMOVAL OF LT INB AILERON TURNAROUND PULLEY, PULLEY CASTING FOUND CORRODED AT LWR LUG. REPLACED LT I/B TURNAROUND CASTING IAW SRM 51-30-02 AND MM 20-10-20.Oct 8, 1998 · N936UP · Boeing 727108C · Aileron Control SystemSDR UPS98227985Frame · damagedINSPECTION TYPE-C, DURING INSP OF FRAME 848.95 LT FOURTH FASTENER HOLE ABOVE FLOOR FOUND TO BE .3125 WITH MECHANICAL DAMAGE AFTER MAX OVERSIZE. FRAME 848.95 LT REPAIRED IAW APPENDIX C OF EO B727-5310-5474.Oct 8, 1998 · N936UP · Boeing 727108C · Fuselage Main, FrameSDR UPS98227984Flange · crackedINSPECTION TYPE-C, SUSPECT CRACK O/B FLANGE RADIUS BS 910 RT BETWEEN STR 18A SILL AND W/WELL CEILING IN RT W/WELL. REPAIR CARRIED OUT IAW SRM ADDENDUM EO B 727-5310-1896.Oct 8, 1998 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS98228033Skin · corrodedINSPECTION TYPE-C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 310 BETWEEN STR 9L AND S8L. REPAIR CARRIED OUT IAW SRS EO 98-30-003 AND 98-30-003 REVISION 1, REFERENCE UPS ENGINEERING FILE NUMBER 5330-2084.Oct 7, 1998 · N936UP · Boeing 727108C · Fuselage Main, Plate/SkinSDR UPS98228014Skin · corrosionINSPECTION TYPE:C SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 1130 JUST ABOVE STR 4 R. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 5.Oct 7, 1998 · N936UP · Boeing 727108C · Fuselage Main, Plate/SkinSDR UPS98227983Flange · crackedINSPECTION TYPE-C, SUSPECT CRACK O/B FLANGE RADIUS OF BS 913-5 BETWEEN STR 18A SILL AND W/WELL CEILING LT W/WELL. REPAIR CARRIED OUT IAW SRS EO B727-5310-1896.Oct 7, 1998 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS98227981Seat Track · corrodedINSPECTION TYPE-C, WHILE INSPECTION UNDER FWD LAV LOWER FLANGE OF SEAT TRACK AT BS 34.4 RBL 24.75 FOUND CORRODED SECTION OF SEAT TRACK. REPLACED BS 344 TO 400 RBL 24.75 TRACK FABRICATED FROM EXTRUSION BAC1520-1432 IAW SRM 53-10-5 FIG 1.Oct 7, 1998 · N936UP · Boeing 727108C · Fuselage, Seat/Cargo Attach FittingsSDR UPS98227951Skin · corrodedINSPECTION TYPE-C, LIGHT SURFACE CORROSION ON SKIN BS 1180 BETWEEN S6L AND S7L. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1. REPAIRED IAW SRM 53-30-3 FIG 9.Oct 7, 1998 · N936UP · Boeing 727108C · Fuselage Main, Plate/SkinSDR UPS98227950Skin · corrodedINSPECTION TYPE-C, LIGHT SURFACE CORROSION ON SKIN BS 1850 ABOVE NR 2 ENGINE RT COWL AFT HINGE POINT. SKIN REPAIRED AT BS 1850 RT PER SRM 54-30-2 FIG 4.Oct 7, 1998 · N936UP · Boeing 727108C · Fuselage Main, Plate/SkinSDR UPS98227947Seat Track · brokenINSPECTION TYPE:C SEAT TRACK FLANGE BROKEN AT BS 870 RBL 24.75. SEAT TRACK SECTION REPLACED IAW SRM 53-10-5 FIG 1.Oct 7, 1998 · N936UP · Boeing 727108C · Fuselage, Seat/Cargo Attach FittingsSDR UPS98227943Web · crackedINSPECTION TYPE:C WEB OVER NR 2 ENGINE CRACKED AT BS 1376 RT. NEW WEB FABRICATED AND INSTALLLED IAW DRAWING 65-17555.Oct 7, 1998 · N936UP · Boeing 727108C · Nacelle/Pylon StructureSDR UPS98228036Stringer · corrodedINSPECTION TYPE-C, CORROSION ON LOWER FLANGE OF STRINGER 18A LEFT HAND BETWEEN BS 870 AND 850. REPAIR CARRIED OUT IAW SRS EO 98-30-004, REF UPS ENGINEERING FILE NUMBER 727-53-2086.Oct 6, 1998 · N936UP · Boeing 727108C · Fuselage Main, Longeron/StringerSDR UPS98227982Skin · corrodedINSPECTION TYPE-C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 1075 S18R AREA AT BS 1071 TO BS 1080 STR 18R TO STR 19R. REPAIRED PER SRS EO 98-30-001 ENGINEERING FILE NR 5330-2085.Oct 6, 1998 · N936UP · Boeing 727108C · Fuselage Main, Plate/Skin
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