Boeing 727-31C

Service difficulty reports · 885

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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 = '72731C'
  ORDER BY difficulty_date DESC"

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SDR UPS04242180Floorbeam · crackedINSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328, RBL 44. REPAIR CARRIED OUT IAW SRM 53-10-8.Apr 6, 2004 · N926UP · Boeing 72731C · Fuselage Main, Floor BeamSDR UPS04242219Drum · corrodedINSPECTION TYPE:C LEFT I/B MIDFLAP O/B AFT FLAP ACTUATING DRUM CORRODED. DRUM REPLACED IAW MM 27-51-01.Apr 5, 2004 · N926UP · Boeing 72731C · Trailing Edge Flap Control SystemSDR UPS04242179Floorbeam · crackedINSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 344 LBL 24. REPAIR CARRIED OUT IAW SRM 51-20-1 FIG 7.Apr 5, 2004 · N926UP · Boeing 72731C · Fuselage Main, Floor BeamSDR UPS04242178Floorbeam · crackedINSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328 RBL 24. REPAIR CARRIED OUT IAW SRM 53-10-8.Apr 5, 2004 · N926UP · Boeing 72731C · Fuselage Main, Floor BeamSDR UPS04242223Rib · crackedINSPECTION TYPE:C NR 3 L/E SLAT, CRACK AT ACTUATOR ATTACH RIB (O/B RIB). REPAIR CARRIED OUT IAW SRM 51-30-02, 51-30-03, 57-50-03 & MM 28-81-11 & 27-00-00.Apr 3, 2004 · N926UP · Boeing 72731C · Leading Edge DevicesSDR UPS04242220Rib · crackedINSPECTION TYPE:C NR 2 L/E SLAT CLOSURE RIB AT INBOARD END OF SLAT CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-20-1 & MM 20-10-05.Apr 3, 2004 · N926UP · Boeing 72731C · Leading Edge DevicesSDR UPS04242177Skin · crackedINSPECTION TYPE:C NR 4 K-FLAP HAS CRACK ON INNER ANTI-ICE SKIN AROUND RIVET HOLE I/B OF O/B ACTUATION LINKAGE FOR BULLNOSE. REPAIR CARRIED OUT IAW SRM 51-30-2, 57-50-3.Apr 3, 2004 · N926UP · Boeing 72731C · Leading Edge DevicesSDR UPS03241537Skin · crackedINSPECTION TYPE: C, NLG WW BS 259 SUSPECT CRACKS AT RIVETS AT RT AFT PRESSURE PANEL FWD EDGE. HFEC CONFIRMED CRACKS. AREA CUT OUT IAW SRM 51-40-2 FIG 1. HFEC CONFIRMS DEFECT FREE CUTOUT. REPAIRED CUTOUT IAW SRM 51-40-2 FIG 1.Oct 19, 2003 · N927UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS03241535Skin · crackedINSPECTION TYPE: C, NLG WW BS 263 AND BS 267 ROW OF RIVETS HAVE SUSPECT CRACKS ABOVE RT AFT PRESSURE PANEL. HFEC CONFIRMED CRACKS. AREA CUT OUT IAW SRM 51-40-2 FIG 1. HFEC NDF REPAIRED CUTOUT IAW SRM 51-40-2 FIG 1.Oct 19, 2003 · N927UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS03241534Pressure Panel · crackedINSPECTION TYPE:C NLG W/W BS 290 LBL 0 SUSPECT CRACKS IN ROW OF RIVETS AT NLG CEILING. AREA CUTOUT IAW SRM 51-40-2 FIG 1, HFEC NDF. REPAIRED CUTOUT IAW SRM 51-10-2 FIG 1.Oct 19, 2003 · N927UP · Boeing 72731C · Fuselage Main, BulkheadSDR UPS03241526Fitting · crackedINSPECTION TYPE: C, TO REMOVE RT BS 930 FITTING, PARTIAL SHELF ATTACHING BS 930 TO 940 MUST BE REMOVED, ON REMOVAL OF PARTIAL SHELF AT STR 14 BS 930-940, 3 SUSPECT CRACKS WERE DETECTED ON MOST UPPER HORIZONTAL FLANGE (FWD SIDE) ON BS 940 FITTING. REPAIR CARROct 18, 2003 · N927UP · Boeing 72731C · Fuselage Main, Attach FittingsSDR UPS03241533Skin · corrodedINSPECTION TYPE:C AREA OF SURFACE CORROSION ON SKIN AT BS 1090 S12L. AREA REPAIRED IAW SMRO EO 2003-055-002 AND UPS FILE 727-53-20131.Oct 16, 2003 · N927UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS03241532Support Bracket · crackedINSPECTION TYPE:C RT WING I/B MID FLAP GUIDE ROLLER SUPPORT BRACKET CRACKED AT UPPER CHORD REAR SPAR JUST O/B OF NR 6 FLAP TRANSMISSION. ROLLER SUPPORT REPLACED IAW SRM 51-30-02 AND BOEING DRG 65-16201.Oct 15, 2003 · N927UP · Boeing 72731C · Trailing Edge FlapsSDR UPS03241529Skin · crackedINSPECTION TYPE: C, SUSPECT CRACK AT NR 3 RT COCKPIT WINDOW CUTOUT AFT LWR CORNER. REPAIR CARRIED OUT IAW SRM 51-30-02, 53-30-03, 51-10-02 & 51-20-04.Oct 14, 2003 · N927UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS03241527Fitting · crackedINSPECTION TYPE: C, RT 930 FITTING HS SUSPECT CRACK AT AFT O/B FLANGE AT FLOOR LEVEL. REPAIR & REPLACEMENT OF BS 930 FITTING & ASSOCIATED STURCTURAL ITEMS CARRIED OUT IAW SMRO EO 2003-055-001 UPS ENGINEERING FILE 727-53-20 130.Oct 11, 2003 · N927UP · Boeing 72731C · Fuselage Main, Attach FittingsSDR UPS03241518Skin · crackedINSPECTION TYPE: C, CABIN AIR PRESS LEAK FROM NR 1 VHF ANTENNA CUTOUT (AFT). ON INVESTIGATION A SUSPECT CRACK FOUND AT ANTENNA CUTOUT. HFEC INSPECTION CARRIED OUT ON SUSPECT CRACK IAW B727 NDTM PT 6 51-00-00 FIG 4. CRACKEDCONFIRMED & MARKED. REPAIR CARRIEOct 11, 2003 · N927UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS03241538Fitting · crackedINSPECTION TYPE:C SUSPECT CRACK ON ACTUATOR FITTING I/B LUG I/B FACE BELOW BOLT HOLE AIRSTAIRS ACTUATOR. HFEC CONFIRMED CRACK. REMOVED AND REPLACED FITTING IAW SRM 51-30-02 AND DRAWING 65C13874. BOLT ALSO FOUND WORN, REPLACED IAW 52-62-71. OPS CHECKED SATIOct 10, 2003 · N927UP · Boeing 72731C · Fuselage Main, Attach FittingsSDR UPS03241536Skin · crackedINSPECTION TYPE: C, NLG WW BS 243 ROW OF RIVETS BELOW RT FWD PRESSURE PANEL HAVE CRACKS. HFEC CORFIRMED CRACKS, AREA CUT OUT IAW SRM 51-40-2 FIG 1. HFEC COFIRMS NDF ON CUTOUT, REPAIRED IAW SRM 51-40-2 FIG 1.Oct 10, 2003 · N927UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS03241517Panel · crackedINSPECTION TYPE: C, DURING PRESSURE LEAKAGE CHECK IN NLG WW A 3 INCH CRACK WAS FOUND ON RT CEILING. DAMAGED PART OF WEB CUTOUT REMOVED IAW SRM 51-40-2. DE-RIVETED IAW SRM 51-30-02. HFEC INSPECTION CARRIED OUT AROUND CUTOUT IN NWW ON RT CEILING IAW B727 NDTOct 10, 2003 · N927UP · Boeing 72731C · Fuselage Main, BulkheadSDR UPS03241528Fitting · damagedINSPECTION TYPE: C, REPLACED NLG DRAG BRACE FITTING AS PER EO B727-5340-0167.Oct 3, 2003 · N927UP · Boeing 72731C · Nose/Tail Landing GearSDR UPS03240253Structure · gougedINSPECTION TYPE: ASV, LEFT O/B TRAILING EDGE FLAP HAS A GOUGE AT LEADING EDGE O/B ATTACH POINT (I/B OF ATTACH POINT). INSTALLED REPAIR DOUBLER PER SRM 57-50-4 FIG 9. REMOVED AND REINSTALLED LEFT O/B TRAILING EDGE AFT FLAP TO FACILITATE REPAIR IAW MM 27-51-1Mar 3, 2003 · N922UP · Boeing 72731C · Trailing Edge FlapsSDR UPS02239958Door · out of rigNOISE FROM NLG AREA DURING FLIGHT, WITH RED DOOR WARNING INDICATION. LEVEL AT FL260, MACH 0.82, 342 KIAS. HEARD LOUD THUMPING FROM FRONT OF AIRCRAFT WITH ASSCOCIATED RED 'DOORS' ANNUNCIATOR, SLOWED TO MACH 0.80 AND CONDITION WENT AWAY. PERFORMED NLG DOOR RIDec 4, 2002 · N925UP · Boeing 72731C · Landing Gear Door Retract SectionSDR UPS02239194Stiffener · corrodedINSPECTION TYPE:C LOWER END OF STIFFENER AT WS 210, R/H WING REAR SPAR, IS CORRODED STIFFENER REPLACED IAW SMRO EO 2002-044-006, REF. UPS ENGINEERING FI LE NO. 727-57-20060.Aug 17, 2002 · N926UP · Boeing 72731C · Wing Main, Frame StructureSDR UPS02239191Web · crackedINSPECTION TYPE:C CRACK FOUND IN NLG FWD L/H PRESSURE WEB AT BS 235 APPROX. CRACK REMOVED IAW SRM 51-40-2. HFEC INSPECTION CONFIRMED CRACK REMOV AL. REPAIR PARTS FABRICATED AND REPAIR INSTALLED IAW SRM 51-40-2, FI G. 1.Aug 15, 2002 · N926UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02239120Pressure Panel · crackedINSPECTION TYPE:C SUSPECT CRACK IN NLG FWD LT PRESS WEB AT BS 243.7. CRACKED AREA REMOVED IAW SRM 51-40-2 FIG 1. HFEC C/O ON THE ABOVE AREA INSP CARRIED OUT IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT CRACK REMOVED BY CUT OUT, FABRICATED DOUBLER & FILLER IAW Aug 15, 2002 · N926UP · Boeing 72731C · Fuselage Main, BulkheadSDR UPS02239168Skin · crackedINSPECTION TYPE:C CRACK IN ANTI-ICE SKIN AT 5TH BAY O/B ON NO.4 KRUEGER FLAP. ANTI-ICE SKIN FOUND TO BE OUT OF LIMITS IAW SRM ADDENDIUM EO NO. B72 7-5750-3082-D. ANTI ICE SKIN REPLACED IAW DRAWING NO.65-16225 + SRM 51-30-02.Aug 14, 2002 · N926UP · Boeing 72731C · Leading Edge DevicesSDR UPS02239166Skin · crackedINSPECTION TYPE:C #3 LE FLAP ANTI-ICE SKIN CRACKED AT MIDDLE O/B RIVET 3RD BAY FROM O/ B REPAIR CARRIED OUT IAW SRM ADDENDUM EO # B727-5750-3082Aug 14, 2002 · N926UP · Boeing 72731C · Leading Edge DevicesSDR UPS02239165Skin · crackedINSPECTION TYPE:C RIVET PULLED THROUGH ANTI-ICE SKIN AT #4 KRUEGER FLAP AT 8TH BAY O/B SKIN REPAIRED IAW SRM ADDENDUM EO # B727-5750-3082Aug 14, 2002 · N926UP · Boeing 72731C · Leading Edge DevicesSDR UPS02239199Spar · corrodedINSPECTION TYPE:C SUSPECT CRACK ON RT WING REAR SPAR UPPER CHORD AT APPROX WS 198 AND WS 194. UPPER CHORD HORIZONTAL FLANGE BLENDED TO REMOVE DAMAGE AT WS 196, WS 201 AND WS 205 IAW SRM 51-10-6. ADDITIONAL CORROSION FOUND AT 3 FASTENER LOCATION BETWEEN WS 17Aug 14, 2002 · N926UP · Boeing 72731C · Wing SparSDR UPS02239119Web · crackedINSPECTION TYPE:C LIGHTENING HOLE IN AFT AIRSTAIR TORQUE BOX AT BS 1243 RHS IS CRACKED WEB REPAIR CARRIED OUT IAW SRM 51-10-4Aug 14, 2002 · N926UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02239167Doubler · crackedINSPECTION TYPE:C SUSPECT CRACK AT FASTNER BESIDE REPAIR AT NLG WHEEL WELL LEFT FWD PR ESS WEB AT BS 269.5 REPAIR DOUBLER REMOVED IAW SRM 51-30-2 NDT CARRIED OUT CRACK CONFIRM ED & END OF CRACK MARKED. DOUBLER AND FILLERS FABRICATED AND INSTALL ED IAW SRM Aug 13, 2002 · N926UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02239197Web · crackedINSPECTION TYPE:C CRACKS FOUND IN NLG W/WELL PRESSURE WEB AT BS 269.5, 4" BELOW THE CE ILING ON THE R/H PRESSURE WEB AREA. NEW WEB AND DOUBLERS FABRICATED AND INSTALLED IAW DRAWING 65-18414Aug 13, 2002 · N926UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02239190Skin · corrodedINSPECTION TYPE:C CORROSION FOUND AT LAP JOINT S4L. LFEC INSPECTION CARRIED OUT FROM B S 360 TO BS 440. MATERIAL LOSS INDICATION FROM BS 440 TO BS 411 APPR OX. 20% - 30%. CORRODED INTERNAL DOUBLER ALSO FOUND TO BE DISBONDED. DOUBLER REMOVED IAW SRM 51-30-2. Aug 13, 2002 · N926UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS02239187Stiffener · crackedINSPECTION TYPE:C SUSPECT CRACK ON AFT PRESSURE BULKHEAD VERTICAL BEAM LT AT W/L 264 APPROX LBL 26.83. HFEC INSPECTION CONFIRMED CRACK. CRACK STOP DRILLED IAW EO B727-5311-0631 STEP 3. HEFC INSPECTION CONFIRMED CRACK CONTAINED. AREA REPAIRED IAW B727-5311-Aug 13, 2002 · N926UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS02239115Stiffener · crackedINSPECTION TYPE:C WING TO BODY FAIRING 3409 HAS A CRACKED FWD FRAME STIFFENER ANGLE. FABRICATED AND INSTALLED NEW STIFFENER IAW SRM 53-50-1 FIG 4 AND SRM 51-2 0-1 FIG 7.Aug 13, 2002 · N926UP · Boeing 72731C · Aerodynamic FairingsSDR UPS02239198Skin · corrodedINSPECTION TYPE:C CORROSION FOUND ON FUSELAGE SKIN AT BS 1181, BETWEEN S-5L AND S-6L. TO REMOVE CORROSION COMPLETELY, SKIN CUT-OUT WAS MADE FROM BS 1145 T O BS 1180, BETWEEN S-5L AND S-10L. REPAIR WAS CARRIWED OUT IAW SMRO EO 2002-044-002 R2. REF. UPS EO BAug 12, 2002 · N926UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02239164Seat Track · crackedINSPECTION TYPE:C CRACK ON SEAT TRACK IN LWR AFT CARGO COMP AT BS 960 BBL 18L. REPAIR CARRIED OUT IAW SRM 53-10-5 FIG 5.Aug 12, 2002 · N926UP · Boeing 72731C · Fuselage, Seat/Cargo Attach FittingsSDR UPS02239121Intercostal · crackedINSPECTION TYPE:C CRACK ON INTERCOSTAL AT BS 1130 BBL 6 R INTERCOSTAL REMOVED IAW SRM 51-30-02 INTERCOSTAL FABRICATED IAW SRM 51-20-1 FIG 7 AND INSTALLED IAW SRM 51-30-2Aug 12, 2002 · N926UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02239118Support · crackedINSPECTION TYPE:C ON REMOVAL OF FAIRING 3610, CRACK FOUND ON FAIRING 3608 SUPPORT FRAME AT BS 1010 STR 25 RBL 64. HFEC CARRIED OUT POST CUT OUT IAW B727 NDTM PT 6 51-00-00 FIG 4. SUPPORT FRAME REPAIRED IAW SRM 51-40-3 FIG 1 & SRM 53-50-1 FIG 9.Aug 12, 2002 · N926UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS02239169Wedge · delaminatedINSPECTION TYPE:C R/H I/B MIDFLAP DISBOND UPPER SURFACE T-EDGE WEDGE 10 INCHES FROM EN D APPROX. REPAIRED IAW SRM 51-40-20Aug 9, 2002 · N926UP · Boeing 72731C · Trailing Edge FlapsSDR UPS02239114Stiffener · corrodedINSPECTION TYPE:C, RT WHEEL WELL BS 870 BULKHEAD VERT STIFFENER CORRODED AT UPPER END AT RBL 50 APPROX JUST FWD OF L/E CONTROL VALVE. NEW VERT STIFFENER FABRICATED IAW DRAWING 65-16330, VERT STIFFENER INSTALLED IAW DRAWING 65-16330 & SMRO EO 2002-044-005 UPS Aug 8, 2002 · N926UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS02238875Battery · dischargedINSPECTION TYPE:PFLT FORWARD ENTRY EMERGENCY EXIT LIGHT INOP. FORWARD ENTRY EMERGENCY EXIT LIGHT BATTERIES REPLACED. INSPECTED/TESTED SERVICEABLE IAW B727 MM 33-50-01.Jul 22, 2002 · N922UP · Boeing 72731C · Emergency LightingSDR UPS02238550Beam · crackedINSPECTION TYPE:C CRACK INDICATION AT BS 1183 BEAM RBL 26.83 WL 250 APPROX. REPAIR CARRIED OUT IAW EO B727-5311-0631 APPENDIX DMay 31, 2002 · N927UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02238548Beam · crackedINSPECTION TYPE:C CRACK INDICATING AT BS 1183 BEAM LBL 26.83 WL AT 250 APPROX REPAIR CARRIED OUT IAW EO B727-5311-0631 APPENDIX DMay 30, 2002 · N927UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02238549Floorbeam · corrodedINSPECTION TYPE:C, CORROSION ON CHORD AT FLOOR LEVEL AT BS 1177 RT O/B. CHORD REPLACED IAW SRM 51-30-02 AND DRAWING 65-19606.May 28, 2002 · N927UP · Boeing 72731C · Fuselage Main, Floor BeamSDR UPS02238551Rib · crackedINSPECTION TYPE:C RIB CRACKED ON LE SLAT #3, RIB LOCATED I/B OF O/B TRACK #3 SLAT REMOVED TO CARRY OUT REPAIR ON CRACKED RIB IAW MM 27-81-11 CRACKED RIB REPAIRED IAW SRM 57-50-3 FIG 9 #3 SLAT INSTALLED AFTER REPAIR COMPLETED IAW MM 27-81-11May 27, 2002 · N927UP · Boeing 72731C · Leading Edge Slat Control SystemSDR UPS02238547Skin · corrodedINSPECTION TYPE:C, SURFACE CORROSION ON FUSELAGE SKIN INTERNAL AT BS 254.5 BETWEEN STR 5L & 6L. REPAIR CARRIED OUT IAW DRAWING 692161 & UPS EO B727-5310-1371 APPENDIX E.May 27, 2002 · N927UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS02238518Seat Track · corrodedINSPECTION TYPE:C CORROSION ON SEAT TRACK AT BS 660 AND BS 680 LBL 62.5 SEAT TRACK REPLACED BS 655 BS 710 LBL 62.5 IAW SRM 53-10-5 FIGURE 1May 27, 2002 · N927UP · Boeing 72731C · Cabin Equipment/FurnishingsSDR UPS02238556Skin · crackedINSPECTION TYPE:C CRACK IN SECTION 41 FUSELAGE SKIN AT BS 211.8 R/H AT WL 197.5 REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3 USING 0.063" DOULER IAW EO B727-5330-0795-GMay 23, 2002 · N927UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS02238555Skin · corrodedINSPECTION TYPE:C CORROSION BETWEEN SKIN & INTERNAL DOUBLER AT BS 1180 BETWEEN S10L & 9L. REPAIR CARRIED OUT IAW SRM 51-10-6 & 53-30-3, DAMAGE CUT OUT IAW 51- 10-6. REPAIRED IAW 51-10-2 AND 53-30-3 FIG 1 STEP 4.May 22, 2002 · N927UP · Boeing 72731C · Fuselage Main, Plate/Skin
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