Boeing 727-30C

Service difficulty reports · 931

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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 = '72730C'
  ORDER BY difficulty_date DESC"

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SDR UPS07248886Slide · dislodgedFWD ENTRY ESCAPE SLIDE IS OUT OF CONTAINER. INSTALLED FORWARD ENTRY DOOR EVACUATION SLIDE IAW 25-60-14-2. OPS CHECK GOOD.Jan 19, 2007 · N919UP · Boeing 72730C · Escape SlideSDR UPS06248684Skin · cracked3 INCH CRACK ON FUSELAGE SKIN AT 10 O'CLOCK POSITION RUNNING FWD AND AFT AT STA 348.2, BETWEEN STRINGERS 5L & 6L. ADDITIONAL DISBONDING APPROXIMATELY 4 X 4 INCHES. C/W EO B727-5330-25585A TO FERRY A/C TO BFM 9014 D337794 ISSUED.Nov 14, 2006 · N919UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS06248513Slide · dislodgedFOUND DOOR SLIDE ON FLOOR. RE-INSTALLED ESCAPE SLIDE PER 25-60-14-2.Nov 7, 2006 · N919UP · Boeing 72730C · Escape SlideSDR UPS06248330Battery · inoperativeEMERGENCY EXIT LIGHTS ABOVE THE MAIN ENTRY DOOR AND ABOVE THE COCKPIT ENTRY DOOR ARE INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY ON MAIN ENTRY DOOR PER MM 33-50-90-2. REMOVED AND REPLACED BATTERIES ON COCKPIT ENTRY DOOR. OPS CHECK GOOD.Oct 26, 2006 · N919UP · Boeing 72730C · Emergency LightingSDR UPS06247834Light · no testINSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED C/P PORTABLE EMERGENCY LIGHT ASSY IAW MM 33-50-67-2. SYS OPS CKS OK.Aug 29, 2006 · N918UP · Boeing 72730C · Emergency LightingSDR UPS06247827Slide · dislodgedINSPECTION TYPE: NA ESCAPE SLIDE FELL OUT OF CASE ON MAIN ENTRY DOOR REPLACED ENTRY DOOR EVACUATION SLIDE IAW MM 25-60-14-2.Aug 28, 2006 · N919UP · Boeing 72730C · Escape SlideSDR UPS06247826Lamp · failedINSPECTION TYPE:NA EMERGENCY LIGHT ABOVE CREW ENTRY DOOR DIM, RELAMPED. OPS CK NORMAL IAW 25 60 00.Aug 28, 2006 · N918UP · Boeing 72730C · Emergency LightingSDR UPS06247717Battery · inoperativeINSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WITH SWITCH ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. OPS CK NORMAL.Aug 17, 2006 · N919UP · Boeing 72730C · Emergency LightingSDR UPS06247529Battery · dischargedFOUND COCKPIT DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES AS REQUIRED.Jul 31, 2006 · N919UP · Boeing 72730C · Emergency LightingSDR UPS06246808Fairing · delaminatedDELAM ON L/AFT WING TO BODY FAIRING PANEL NR 3510 JUST AFT OF HYD SYS BAY REF EO B727-5350-24306. PERFORMED INTERIM REPAIR PER EO B727-5350-24306 STEP 6. DEFERRED FOR REPEAT INSPECTION EVERY 30 DAYS AND PERM BY C-CK. NR D 325051 ASSIGNED INSTALLATION OF PANMay 8, 2006 · N919UP · Boeing 72730C · Aerodynamic FairingsSDR UPS06246793Light · inoperativeEMERGENCY EXIT LIGHT CAME OUT OF SOCKET. REINSTALLED ASSEMBLY. OPS CK GOOD PER AMM 33-50-01-5.May 4, 2006 · N918UP · Boeing 72730C · Emergency LightingSDR 2006FA0000645Control Valve · failedNR 2 ENGINE FIRE EXTINGUISHING SELECTOR CONTROL VALVE FAILED TO OPEN DURING ROUTINE TESTING IAW UPS ROUTINE TASK CARD TC 2-221-12. THE VALVE SOLENOID HOUSING WAS NOTED AS BEING CORRODED. (K)Nov 8, 2005 · N918UP · Boeing 72730C · Extinguishing SystemSDR UPS05245823Stringer · corrodedINSPECTION TYPE:C STRINGER 24 RT FOUND CORRODED AT BS 725. PLEASE INVESTIGATE DAMAGE FOUND TO BE BEYOND LIMITS IAW SRM 53-10-3. DAMAGED SECTION OF STRINGER 24R CUT OUT AND REMOVED. AREA REPAIRED IAW 53-10-3 FIG 1 DETAIL 1 PAGE 4B.Nov 1, 2005 · N918UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS05245859Skin · crackedINSPECTION TYPE:C AFT CARGO DOOR CRACK ON INNER SKIN SECOND INSPECTION HOLE FWD EDGE AT BOTTOM. REMOVE FASTENER AND CHECK DEPTH OF CRACK TO DETERMINE REPAIR. HFEC CARRIED OUT AND CRACK FOUND CONTAINED WITHIN FASTENER HOLE. REPAIRED IAW SRM 51-40-02.Oct 25, 2005 · N918UP · Boeing 72730C · Cargo/Baggage DoorsSDR UPS05245826Intercostal · crackedINSPECTION TYPE:C STA 660, ST 29R REPAIR TO INTERCOSTAL IS CRACKED. PLEASE REPAIR IAW SRM. REPAIR BRACKET FABRICATED IAW SRM 51-20-071 FIG 7. REPAIR BRACKET REPLACED IAW SRM 51-30-02.Oct 24, 2005 · N918UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS05245861Link · crackedINSPECTION TYPE:C RT MLG UPLOCK FWD SUPPORT LINKS CRACKED. REPLACE LINKS. RT MLG UPLOCK FWD SUPPORT LINKS REPLACED IAW MM 20-80-01.Oct 18, 2005 · N918UP · Boeing 72730C · Main Landing GearSDR UPS05245851Spar · corrodedAREA OF SUSPECT CORROSION ON WING CENTER SECTION REAR SPAR LWR CHORD BS 870 RBL36 DUE TO 2 POPPED FASTENER HEADS. PLEASE INVESTIGATE AND RECTIFY AS NECESSARY. AS PER BOEING INSTRUCTIONS THE LWR CHORD WAS REPLACED. NEW CHORD WAS CUT AT RBL 9.5. REPAIR SPLICEOct 16, 2005 · N918UP · Boeing 72730C · Wing SparSDR UPS05245832Skin · corrodedEVIDENCE OF CORROSION AT BS 360 STR 22L AT FWD END OF STR AT AFT FACE OF FRAME. PLEASE INVESTIGATE AND RECTIFY. CORROSION BLENDED OUT IAW SRM 51-10-06. CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-1. REPAIR STRAP FABRICATED IAW SRM 51-20-1 FIG 7. MOct 16, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245821Skin · corrodedINSPECTION TYPE:C NDT INSPECTION HAS INDICATION OF MATERIAL LOSS AT BS 441 FWD OF CENTER LINE AT STR 8L, INVESTIGATE. CORROSION FOUND BETWEEN SKIN AND DOUBLER. CORROSION REMOVED AND FOUND BE WITHIN LIMITS, AREA REPROTECTED IAW SRM 51-30-02.Oct 16, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245836Trunnion · crackedRT TRUNNION ATTACH FITTING HAS CRACK AT OB FLANGE HOLE E RUNNING UP APPROX 2.5 INCHES. REMOVE AND REPLACE FITTING. RT TRUNNION FITTING FOUND CRACKED OUTSIDE REPAIRABLE LIMITS IN UPS EO B727-5740-20666C. REPLACED IAW UPS AUTHORIZATION B727-5740-23046-B.Oct 15, 2005 · N918UP · Boeing 72730C · Fuselage, Landing Gear Attach FittingsSDR UPS05245831Skin · corrodedSURFACE CORROSION ON LAP JOINT BETWEEN S-4L AND 5L AT LOCATIONS BETWEEN BS 852 AND 1011. CORROSION REMOVED IAW SRM 51-10-2 (.002") AND FOUND WITHIN LIMITS IAW SRM 51-20-4.Oct 14, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245824Support · corrodedINSPECTION TYPE:C RT MLG TRUNNION BUTTERFLY FITTING HAS CORROSION. PLS REPLACE. SUPPORT REPLACED IAW DRW 65-19296.Oct 14, 2005 · N918UP · Boeing 72730C · Fuselage, Landing Gear Attach FittingsSDR UPS05245860Bushing · crackedINSPECTION TYPE:C ENGINE NR 3 AFT MOUNT FITTING HAS CORROSION ON INNER SURFACE OF UPPER USHING. REPLACE BUSHING. REPLACED BUSHING IAW OHM 20-50-03.Oct 13, 2005 · N918UP · Boeing 72730C · Engine Mount SectionSDR UPS05245827Mount · corrodedINSPECTION TYPE:C ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION ON BOTH OUTBOARD HOLES. REPAIR. REPAIRED IAW EO B727-5540-11592-A.Oct 13, 2005 · N918UP · Boeing 72730C · Engine Mount SectionSDR UPS05245833Skin · corrodedAREA OF SUSPECT CORROSION ON CROWN SKIN BS 521 TO BS 515 BETWEEN STR 2L AND 3L. PLEASE PAINT STRIP AREA, REMOVE FASTENERS IF REQUIRED, REINSPECT AND RECTIFY AS NECESSARY. REPAIRED IAW UPS AUTHORIZATION B727-5330-23323-AOct 12, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245822Support Fitting · crackedRT WING FRONT SPAR TO BODY FITTING HAS SUSPECT CRACK ON OUTBD SIDE OF BOTTLE PIN. FITTING REPLACED IAW DWG 65C13724 AND UPS EO B727-5310-7477.Oct 12, 2005 · N918UP · Boeing 72730C · Wing, Attach FittingsSDR UPS05245835Trunnion · crackedLT MLG SUPPORT FITTING HAS CRACK INDICATION IN HOLE B & C ON INB FLANGE AND HOLES E IN COUNTERSINKS. REPAIR AND REPLACE FITTING LT MLG TRUNNION REMOVED AND FOUND CRACKED OUTSIDE REPAIRABLE LIMITS IN UPS EO B727-5740-20666C. TRUNNION REPAIRED IAW UPS AUTHORIZOct 11, 2005 · N918UP · Boeing 72730C · Fuselage, Landing Gear Attach FittingsSDR UPS05245829Skin · crackedINSPECTION TYPE:C NDT INDICATES 2 CRACKS EMINATING FROM FASTENERS " BS235.8 STR16L-17L. PLEASE REPAIR IAW SRM 53-30-3 FIG 3. FASTENERS REMOVED FROM AFFECTED AREA IAW SRM 51-80-02. AFFECTED AREA CUTOUT IAW SRM 53-30-3. HFEC CARRIED OUT AROUND CUTOUT AND ON Oct 11, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245828Skin · crackedINSPECTION TYPE:C SUSPECT SKIN CRACKS AT UPPER FWD CORNER OF FWD ENTRY DOOR CUT OUT BETWEEN STR 7L AND 8L. PLEASE CARRY OUT NDI AND RECTIFY AS NECESSARY IAW SRM ADDENDUM. HFEC CARRIED OUT IAW NDTM 51-00-00 PT6 FIG 4. TWO CRACKS FOUND. DAMAGE REMOVED IAW EOOct 11, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245834Skin · crackedFOUND SKIN CRACK AT FASTENER HOLE IN MID GALLEY DOOR CUT OUT, UPPER FWD CORNER. PLEASE CONFIRM WITH NDI AND RECTIFY AS NECESSARY HFEC CARRIED OUT ON FASTENER HOLES COMMON TO REPAIR IAW 727NDTM 51-00- 00 PT6 FIG 16. THREE CRACKS FOUND. REPAIR CARRIED OUT IAWOct 9, 2005 · N918UP · Boeing 72730C · Service DoorsSDR UPS05245266Skin · corrodedINSPECTION TYPE: C, NR 2 ENG UPPER HORIZ FIREWALL SURFACE TO VERT FIN, LT, ANGLE HAS EVIDENCE OF CORROSION ON INNER SURFACE OF VERT FIN SKIN BETWEEN STA 1385 AND 1425 APPROX. SKIN REMOVED AND FOUND CORRODED O/S LIMITS, CHORD BETWEEN BS 1384 AND 1484 FOUND CORAug 6, 2005 · N919UP · Boeing 72730C · Vertical Stabilizer, Plate/SkinSDR UPS05245265Stiffener · corrodedLT MLG W/W, EVIDENCE OF CORROSION ON BS 870 VERTICAL STIFFENER AND ATTACH CLIP AT LB 145. CEILING AREA. REPAIR CARRIED OUT IAW SRM 51-30-2 & 51-10-2, 51-10-1.Aug 5, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS05245262Stiffener · corrodedRT MLG W/W, EVIDENCE OF CORROSION ON VERTICAL STIFFENER CEILING AREA BS 870 RBL 45. REPAIR CARRIED OUT IAW SRM 51-40-4.Aug 4, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS05245263Floorbeam · corrodedFLOORBEAM TOP CHORD CORROSION OUTSIDE LIMITS BS 328 RBL 12. REPAIR CARRIED OUT IAW SRM 53-10-8 & 51-10-2.Aug 3, 2005 · N919UP · Boeing 72730C · Fuselage Main, Floor BeamSDR UPS05245207Intercostal · corrodedINSPECTION TYPE:C, CORROSION ON INTERCOSTAL BS 294.5 - BS 312 LBL 33. INTERCOSTAL REPLACED IAW BOEING DWG 65-17593 AND SRM 51-30-02.Aug 3, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS05245205Support · corrodedINSPECTION TYPE:C FWD LAV PARTITION SUPPORT STRUCTURAL EXTRUSION CORRODED BS 302 - 344 DOOR THRESHOLD AREA. PARTITION SUPPORT STRUCTURE EXTRUSION REPLACED IAW SRM 51-10-2, 51-20- 2 & 51-30-2.Aug 2, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS05245261Skin · corrodedAREA OF CORROSION ON SKIN BS 355, BETWEEN STR 8 AND 10 LT. PAINT STRIP AREA IF REQUIRED, REMOVE CORROSION AND RECTIFY. REPAIR CARRIED OUT IAW SRM 51-10-1, 53-30-1 MM 25-21-2 AND AAAE EO 200 5-077-001 UPS ENGINEERING FILE NO. B727-5330-22744-A.Aug 1, 2005 · N919UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245264Attach Angle · corrodedRT SIDE AFT OF BS 294.5 FWD ATTACHMENT ANGLE OF NWW BOX HAS EVIDENCE OF CORROSION. WEB REPAIRED IAW SRM 51-40-2.Jul 31, 2005 · N919UP · Boeing 72730C · Fuselage Main, Attach FittingsSDR UPS05245206Web · corrodedINSPECTION TYPE:C RT SIDE AFT OF RT 294.5 FWD ATTACHMENT ANGLE OF NWW BOX AND RT HAS EVIDENCE OF CORROSION. REPAIR CARRIED OUT IAW SRM 51-10-6, 53-10-1 & 51-40-2.Jul 31, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS05243629Light · inoperativeL1 DOOR EMERGENCY LIGHT INOP. RESEATED BULB, OPS CHECK GOOD.Jan 6, 2005 · N919UP · Boeing 72730C · Emergency LightingSDR UPS04242069Fitting · crackedINSPECTION TYPE:C ON REMOVAL OF STR END FITTING AT BS 360 S17L FOUND STR END FITTING CRACKED & CORRODED. REPLACED STR END FITTING IAW SRM 51-30-02 & DRAWING 65-18420.Mar 17, 2004 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS04242070Fitting · crackedINSPECTION TYPE:C ON REMOVAL OF LOWER SKIN BETWEEN BS 259.5 - BS 360 S22 24L STRINGER END FITTING FOUND CRACKED AT BS 360 S22L. REPLACED STRINGER END FITTING IAW SRM 51-30-02 & DRAWING 65-18420.Mar 12, 2004 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS04242058Stringer · corrodedINSPECTION TYPE: C, ON REMOVAL OF FASTENER AT BS 340 APPROX S25R STRINGER FOUND TO BE CORRODED. REPAIR CARRIED OUT IAW SRM 53-10-3.Mar 11, 2004 · N919UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS04242073Skin · corrodedINSPECTION TYPE:C ON REMOVAL OF SKIN PANEL AT BS 295.5 & BS 360 S19L - 24L UPPER SKIN UNDER FWD ENTRY DOOR FOUND TO BE EXCESSIVELY CORRODED. REPAIR CARRIED OUT IAW SRMO EO 2004-024-002 UPS ENG.Mar 10, 2004 · N919UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS04242072Door Frame · corrodedINSPECTION TYPE:C TAIL SKID DOOR RIGHT LWR FRAME IS CORRODED ON INNER SURFACE. REPLACED TAIL SKID DOOR IAW MM 32-71-61.Mar 9, 2004 · N919UP · Boeing 72730C · Landing Gear DoorsSDR UPS04242060Cargo Track · crackedINSPECTION TYPE: C, LEFT CARGO TRACK RAIL IN AFT CARGO BAY, VERY FWD SECTION TO BS 950 IS CRACKED. REF CPT 2643 FOR FABRICATION OF CARGO TRACK. REPAIRED CARGO TRACK IAW SRM 53-10-5 FIG 8.Mar 9, 2004 · N919UP · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR UPS04242075Support · corrodedINSPECTION TYPE:C NR 12 SPOILER ACTUATOR SUPPORT CASTING HAS PITTING AND CORROSION UNDERNEATH THE BOLT HEADS. NR 12 SPOILER ACTUATOR SUPPORT CASTING REPLACED IAW MM 27-61-81, 27-61-01.Mar 8, 2004 · N919UP · Boeing 72730C · Drag Control ActuatorSDR UPS04242059Mount · corrodedINSPECTION TYPE: C, ENGINE NR 1 PYLON FWD MOUNT FITTING, BOTH FWD AFT LARGE AND AFT SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX A.Mar 5, 2004 · N919UP · Boeing 72730C · Engine Mount SectionSDR UPS04242057Mount · corrodedINSPECTION TYPE: C, ENGINE NR 3 PYLON FWD MOUNT FITTING, BOTH FWD AND AFT LARGE AND FWD SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX B.Mar 5, 2004 · N919UP · Boeing 72730C · Engine Mount SectionSDR UPS04242056Skin · bulgedINSPECTION TYPE:C SUSPECT CORROSION (SKIN BULGING) BETWEEN SKIN & FRAME AT BS 260 FROM STR 18L - S19L. REF N/R 740347, LOW FREQ EDDY CURRENT INSP CARRIED OUT AT BS 260 FR STR 18L TO 19L IN ACCORDANCE W/B727 NDT MAN 51-00-00 PART 6 FIG 5. SUSPECT MATERIAL LOSMar 4, 2004 · N919UP · Boeing 72730C · Fuselage Main, Plate/Skin
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