Boeing 727-25C

Service difficulty reports · 2,007

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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 = '72725C'
  ORDER BY difficulty_date DESC"

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SDR UPS03241070Panel · debondedINSPECTION TYPE:C NR 3 SPOILER PANEL LOWER SURFACE DISBOND AT ACTUATOR CUTOUT. REPAIR CARRIED OUT IAW SRM 51-40-05.Jul 14, 2003 · N946UP · Boeing 72725C · SpoilersSDR UPS03241067Skin · corrodedINSPECTION TYPE:C EVIDENCE OF CORROSION AT LAP JOINT BS 820 TO BS 870, S-4R REPAIR CARRIED OUT IAW UPS EO B727-5330-0509.Jul 14, 2003 · N946UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS03241066Skin · crackedINSPECTION TYPE: C, EVIDENCE OF CRACK AROUND FASTENER AT MID GALLEY DOOR CUTOUT BS 640, S-8L. REPAIR CARRIED OUT IAW SMRO EO 2003-041-004. REFERENCE UPS EO B727- 5330-19065.Jul 14, 2003 · N946UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS03241065Skin · debondedINSPECTION TYPE: C, LEFT O/B AFT FLAP - DISBOND AT UPPER SURFACE 5 TO 20 INCHES FROM O/B END. REPAIR CARRIED OUT IAW SRM 51-40-20.Jul 14, 2003 · N946UP · Boeing 72725C · Trailing Edge FlapsSDR UPS03241064Tab · contaminatedINSPECTION TYPE: C, FOLLOWING X-RAY INSPECTION OF RT ELEVATOR TAB, WATER INGRESS FOUND ON RT ELEVATOR TAB AT APPROX ELEV STA 95 TO ELEV STA 105. REPAIR CARRIED OUT IAW SRM 51-40-05.Jul 14, 2003 · N946UP · Boeing 72725C · Elevator, Tab StructureSDR UPS03241061Pressure Panel · crackedINSPECTION TYPE:C NLG WHEEL WELL RT CEILING PRESSURE PANEL HAS A CRACK FROM OUTBOARD EDGE OF PANEL TO BOLT HOLE. PANEL REPAIRED IAW 2003-041-005. REFERENCE UPS ENGINEERING FILE NR 727-53-20125.Jul 14, 2003 · N946UP · Boeing 72725C · Fuselage Main, BulkheadSDR UPS03241050Skin · crackedINSPECTION TYPE: C, LEFT I/B MIDFLAP LWR SURFACE 2 CRACKS AT FWD I/B & O/B CORNERS OF SKIN CUTOUT FOR I/B AFT FLAP ACTUATING ROD. CRACK STOP DRILLED TO .250 INCH IAW SRM 51-10-1. REPAIR CARRIED OUT IAW MRO EO 2003-041-002. UPS FILE NR 727-27-20007.Jul 14, 2003 · N946UP · Boeing 72725C · Trailing Edge FlapsSDR UPS03241049Frame · crackedINSPECTION TYPE: C, FRAME CRACKED AT BS 1070 AND ATTACH POINT FOR AFT LWR CARGO DOOR. CRACKED FRAME AT BS 1070 REMOVED AND NEW FRAME INSTALLED IAW DRAWING NR65-18622.Jul 11, 2003 · N946UP · Boeing 72725C · Fuselage Main, FrameSDR UPS03241010Fairing · crackedINSPECTION TYPE:C ENG NR 3 THRUST REV O/B FAIRING IS CRACKED NEAR FWD SUPPORT BRACKET UPPER EXISTING DOUBLER AT CRACK LOCATION REMOVED IAW SRM 51-30-02. CRACKS TOP DRILLED IAW SRM 78-30-01 0.025 HOLE. HFEC INSP CARRIED ON STOP DRILL IAW B727 NDTM PT 6 51-00-Jul 11, 2003 · N946UP · Boeing 72725C · Engine Thrust ReverserSDR UPS03241006Skin · lightning strikeINSPECTION TYPE: C, LIGHTNING STRIKE DAMAGE AT BS 590 S25R. FASTENER REMOVED AND AREA CLEANED IAW SRM 51-30-02. HFEC INSP CARRIED OUT ON DAMAGED AREA IAW B727 NDTM PT 6 FIG 4. RESULT CRACK FOUND AS MARKED ON A/C & ENDS OF CRACK MARKED. REPAIR CARRIED OUT Jul 11, 2003 · N946UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS03241005Doubler · corrodedINSPECTION TYPE: C, CORROSION ON DELTA BEAM LT WEB DOUBLER AT BS 740. REMOVED CORRODED DOUBLER IAW SRM 51-30-02. REMOVED CORROSION FOUND ON DELTA BEAM WEB & FOUND TO BE WITHIN LIMITS IAW SRM 51-10-01 & 53-1 0-2. FABRICATED REPAIR PARTS IAW SRM 53-10-2. CAJul 11, 2003 · N946UP · Boeing 72725C · Fuselage Main, StructureSDR UPS03241071Skin · crackedINSPECTION TYPE: C, SKIN CRACKS FROM FASTENER HOLES BS 255 (AFT OF NR 3 RT WINDOW CUTOUT) BETWEEN S-10R AND S-9R. REPAIR CARRIED OUT IAW SRM 53-30-03, FIGURE 29.Jul 10, 2003 · N946UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS03241009Angle · corrodedINSPECTION TYPE: C, SURFACE CORROSION ON ANGLE IN LT MLG WHEEL WELL AT BS 935 FWD OF 940 FITTING AT STR 19. REMOVED ANGLE IAW SRM 51-30-02. ANGLE FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-01. FABRICATED ANGLE IAW DRAWING 65-22419 & SRM 51-20-01 & 51-40-3. IJul 10, 2003 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS03240994Support Bracket · crackedINSPECTION TYPE: C, ENG NR 3 THRUST REVERSER OUTER FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM 78-30-01.Jul 10, 2003 · N946UP · Boeing 72725C · Engine Thrust ReverserSDR UPS03241072Skin · corrodedINSPECTION TYPE:C SKIN CRACK FOUND AT FWD CORNER CUTOUT OF FWD ENTRY DOOR S-7L. NOTE: WHEN NDT WAS CARRIED OUT IN REPAIR AREA, IT WAS FOUND THAT THERE WAS CORROSION BETWEEN THE SKIN AND BONDED DOUBLER IN THE AREA SURROUNDING THE FWD ENTRY DOOR SKIN PANEL P/N Jul 9, 2003 · N946UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR CA030729013Warning Switch · out of adjust(CAN) JUST PRIOR TO DESCENT THE MAIN CARGO DOOR WARNING LIGHT ILUMINATED. THE CAPTAIN MADE AN EMERGENCY DESCENT AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. THE MAIN CARGO DOOR WARNING SYSTEM WAS UNDER THE APPROVED MEL AT THE TIME. THE MEL HAD BEEN APPLIEJul 2, 2003 · Boeing 72725C · Door Warning SystemSDR UPS03240848Fire Detector · malfunctionedAIR TURNBACK FOR WHEEL WELL FIRE INDICATION IN FLIGHT ALL CHECKLIST COMPLIED WITH DEF M261369. INSPECTED TIRES, BRAKES, WHEEL ASSEMBLIES & ALL 3 WHEEL WELLS FOR FOR INDICATION OF FIRE. NO EVIDENCE OF FIRE OR OVERHEAT WAS FOUND REPLACED OVERHEAT DETECTION UNIJun 13, 2003 · N951UP · Boeing 72725C · Fire DetectionSDR UPS03240846Swivel · failedA-SYSTEM HYDRAULIC LOSS AFTER T/O DURING FLAP RETRACTION. AIR TURN BACK TO SDF. ALL CKLISTS ACCOMPLISHED. FOUND NR 4 SLAT ACTUATOR SWIVEL SPRING RETAINER BLOWOUT AND O-RINGS CAUSING MASSIVE LEAKAGE. REMOVED AND REPLACED NR 4 SLAT ACTUATOR PER MM 27-81-01. Jun 11, 2003 · N951UP · Boeing 72725C · Hydraulic System, MainSDR CA030327007Switch · failed(CAN) AFTER TAKE OFF FROM FLAPS SELECTED FROM 5 DEGREES TO 2 DEGRESS, AMBER LEADING EDGE LIGHT ILLUMINATED ON FWD PANEL. MAIN LEADING EDGE PANEL INDICATED NR 5 LE FLAP OUT. FUEL WAS DUMPED AND AIRCRAFT RETURNED TO AIRPORT. MAINTENANCE FOUND THE LEADING EDGEMar 27, 2003 · Boeing 72725C · Leading Edge Slat Position Indicating SystemSDR UPS03240322Rib · crackedINSPECTION TYPE:C, LEFT WING, SUSPECT CRACK AT I/B TRACK RIB ON NR 4 SLAT. CRACK STOP DRILLED IAW SRM 51-10-01.Mar 8, 2003 · N949UP · Boeing 72725C · Trailing Edge FlapsSDR UPS03240321Bracket · crackedINSPECTION TYPE:C NO.3 ENGINE THRUST REV. FAIRING MID BRACKET CRACKED. REPLACED BRACKET IAW MM 20-80-01.Mar 8, 2003 · N949UP · Boeing 72725C · Engine Thrust ReverserSDR UPS03240297Rib · crackedINSPECTION TYPE:C&SI ON REMOVAL OF WING TIP, INNER RIB FOUND TO BE CRACKED RIB REPLACED IAW SRM 51-20-1 FIG 7 & DRAWING 65-72719 SHEET 6Mar 8, 2003 · N949UP · Boeing 72725C · Wing Miscellaneous StructureSDR UPS03240295Rib · crackedINSPECTION TYPE:C&SI L/H WING SUSPECT CRACK AT I/B TRACK RIB ON 4 SLAT CRACK STOP DRILLED IAW SRM 51-10-01. HFEC C/O ON L/H WING AT I/B TR ACK RIB ON NO. 4 SLAT INSP. IAW B727 NDTM PT 6 51-00-00 RESULTS CRAC K CONTAINED BY STOP DRILLED HOLEMar 8, 2003 · N949UP · Boeing 72725C · Wing Main, Frame StructureSDR UPS03240323Spar · crackedINSPECTION TYPE: C, LT WING REAR SPAR HAS ONE CRACK AND 2 CORROSION INDICATIONS AT WS 193 TO 196. REPAIR CARRIED OUT IAW SRM 51-20-04.Mar 6, 2003 · N949UP · Boeing 72725C · Wing SparSDR UPS03240296Structure · crackedINSPECTION TYPE: C&SI, AIRSTAIRS; A CRACK IS EXTENDING FROM BENEATH REPAIR AT LIGHTENING HOLE ON RT SIDE OF AIRSTAIRS AT STEP 10 AND ONE RIVET IN THE REPAIR IS NOT SECURE. REPAIR PLATE FITTED AS PER SRM 51-40-2. RIVETED AS PER SRM 51-30-2, TREATED PER SRM 5Mar 6, 2003 · N949UP · Boeing 72725C · Entrance StairsSDR UPS03240320Bracket · crackedINSPECTION TYPE:C FWD.CARGO DOOR FUSELAGE CUTOUT AFT LWR.DOOR STOP FITTING CRACKED. FABRICATED NEW BRACKET IAW.SRM.51-20-1 REPLACED BRACKET IAW SRM 51-30-2.Mar 5, 2003 · N949UP · Boeing 72725C · Fuselage Main, StructureSDR UPS03240195Support Fitting · crackedINSPECTION TYPE:C MAIN CARGO DOOR LATCH SUPPORT FITTING @ BS 612-90 FOUND CRACKED DURI NG INSPECTION FITTING REMOVED I.A.W. SRM 51-30-03 FITTING REPLACED I.A.W. EO B727-5310-0437Feb 14, 2003 · N947UP · Boeing 72725C · Fuselage Main, StructureSDR UPS03240160Skin · crackedINSPECTION TYPE: C, SUSPECT CRACK ON NR 3 ENG TR LWR DOOR INNER UPPER SKIN. NDT PERFORMED AND TWO CRACKS DETECTED AND ENDS MARKED. CRACKED ENDS TERMINATED BY STOP DRILLING WITH .1875 INCH HOLE DIAMETER SRM SUPP 78-30-01 FIG 201 PARA 2. DAMAGED RAMP SKIN REFeb 2, 2003 · N947UP · Boeing 72725C · Engine Thrust ReverserSDR UPS03240161Doubler · corrodedINSPECTION TYPE:C SMALL AREA OF EXFOLIATION CORROSION FOUND ON FUSELAGE SKIN BS1180 JU ST ABOVE STR.6L REPAIR FILLER AND NEW DOUBLER TO INCORPORATE NEW AND EXISTING REPAIR FABRICATED IAW SRM 53-30-03 FIG.3A. REPAIR PARTS INSTALLED IAW SRM 53-30-03.Jan 29, 2003 · N947UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS03240158Skin · corrodedINSPECTION TYPE:C NDT HAVE MATERIAL LOSS INDICATION OF 15-20 PERCENT ON FUSELAGE SKIN FWD OF BUTT JOINT 360, STR 25R TO 27R. FASTENERS REMOVED FROM ABOVE AREA IAW SRM 51-30-2. TO FACILITATE CORROSION CLEAN UP EXISTING DOUBLER ABOVE STR 25R DE-RIVETED BETWEENJan 28, 2003 · N947UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS03240156Fitting · crackedINSPECTION TYPE:C R/H LWR. TERMINAL FITTING IN TAIL SKID BAY CRACKED. REMOVED FITTING IAW SRM 51-30-02. FABRICATED NEW FITTING IAW DRAWING NO.65-85208 INSTALLED FABRICATED FITTING IAW DRAWING NO.65-25992Jan 28, 2003 · N947UP · Boeing 72725C · Fuselage Main, StructureSDR UPS03240140Fitting · crackedINSPECTION TYPE:C, RT UPPER TERMINAL FITTING IN TAIL SKID BAY CRACKED. REMOVED RT UPPER TERMINAL FITTING IAW SRM 51-30-02. NEW FITTING INSTALLED IAW DRAWING 65-25992.Jan 28, 2003 · N947UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS03240139Fitting · crackedINSPECTION TYPE:C, LT LOWER TERMINAL FITTING IN TAIL SKID BAY CRACKED. REMOVED LWR TERMINAL FITTING IAW SRM 51-30-02. NEW FITTING INSTALLED IAW DRAWING 65-25992.Jan 28, 2003 · N947UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS03240159Rib · crackedINSPECTION TYPE:C DURING EDDY CURRENT INSP.OF R/H BS870 FORGING 2 CRACKS WERE FOUND ON FWD INTEGRAL RIB AT S11. REF EO.B727-5310-3057 APPDX.D FOR PARTIAL REPLACEMENT OF TERMINAL F ITTING S9 TO S12 AND APPDX.C STEP 1.Jan 27, 2003 · N947UP · Boeing 72725C · Fuselage Main, StructureSDR UPS03240157Fitting · damagedINSPECTION TYPE: C, TO FACILITATE REPAIR TO BE 870 RT FITTING REMOVE FASTENERS X 20 BELOW PROPOSED CUT LINE AT S12 AND CARRY OUT NDT ON OPEN HOLES. FASTENERS REMOVED BELOW PROPOSED CUT LINE IAW SRM 51-30-02. FASTENER HOLE NDT INSP IAW NDTM H6 51-00-00 FIG 1Jan 27, 2003 · N947UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR CA030117007Uplock Switch · failed(CAN) ON FINIAL APPROACH INTO YYC WHEN GEAR DOWN SELECTED, NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. GEAR CYCLED, NO CHANGE. AFTER 2 MIN DELAY GREEN LIGHT ILLUMINATED. MANUAL EXTENDION INDICATION ALIGNMENT MARKS CONFIRMS GEAR DOWN AND LOCKED. SYSTEM COULD NOT Jan 17, 2003 · Boeing 72725C · Landing Gear Position and WarningSDR UPS03240021Relay · inoperativeDURING LANDING ROLLOUT & T/R APPLICATION A PWR LOSS TO THE FLT & ENGINE INSTRUMENTS WAS NOTED. THE COCKPIT WENT MOMENTARILY DARK. APPLIED T/R DURING TAXI IN AND NOTED KW NR 1 JUMPED TO 35 WHILE THE KWNR 2 DROPPED TO ZERO. REMOVED AND REPLACED R58S POWER RELJan 16, 2003 · N937UP · Boeing 72725C · AC Generation SystemSDR UPS02239930Skin · crackedINSPECTION TYPE:N/A RIGHT INBD AFT FLAP HAS DAMAGE (DENT WITH CRACKED SKIN) JUST OUTBOARD OF INBD CANOE FAIRING. REMOVED DAMAGED SKIN AND CORE, REMOVED INBD AFT FLAP SECTION, REPAIRED FLAP IAW SRM 51-40-20.Nov 21, 2002 · N937UP · Boeing 72725C · Trailing Edge FlapsSDR UPS02239932Floorbeam · corrodedINSPECTION TYPE:C MAIN ENTRY DOOR FLOORBEAM T ANGLE SUPPORT SHOWS EVIDENCE OF CORROSION BETWEEN FS 312 AND FS 344. REMOVED AND REPLACED T ANGLE SUPPORT.Nov 12, 2002 · N948UP · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS02239931Floor Panel · corrodedINSPECTION TYPE:C MAIN ENTRY DOOR FLOOR PANEL CORRODED BETWEEN FS 312 AND 344. REMOVED AND REPLACED FLOOR PANEL.Nov 12, 2002 · N948UP · Boeing 72725C · Fuselage Floor PanelSDR UPS02239863Panel · crackedINSPECTION TYPE:C&SI CRACK SUSPECT ON NLG BAY R/H SIDE PANEL @ BS 249.3 BETWEEN FASTENERS AFT OF R/H FWD PRESSURE PANEL CUTOUT REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1Oct 27, 2002 · N932UP · Boeing 72725C · Fuselage Main, StructureSDR UPS02239900Beam · crackedINSPECTION TYPE: C & SI, WHILE REMOVING RT BS 870 FITTING CRACK FOUND IN SIDE LOAD BEAM AT R BBL 54.50 REPAIRED IAW SMRO EO 2002-055-009. UPS ENGINEERING FILE NO. 727-53-2 0084Oct 26, 2002 · N932UP · Boeing 72725C · Fuselage Main, StructureSDR UPS02239908Frame · corrodedINSPECTION TYPE: C &SI, APU EXHAUST, SUSPECT CORROSION ON AFT WING FRAME UNDER TADPOLE SEAL OF UPPER EXHAUST. FRAME CORRODED BEYOND LIMITS. NEW FRAME FABRICATED AND INSTALLED IAW DRAWING 65-31997.Oct 24, 2002 · N932UP · Boeing 72725C · Wing SparSDR UPS02239904Seat Track · corrodedINSPECTION TYPE: C & SI, AFT CARGO BAY, SEAT TRACK HAS LIGHT SURFACE CORROSION AT BS 1110 R/H SIDE CORROSION REMOVED IAW SRM 51-10-06 AND FOUND TO BE OUTSIDE LIMITS IA W SRM 53-10-01 FIG 3. SEAT TRACK REPAIRED IAW SRM 53-10-01.Oct 23, 2002 · N932UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS02239866Seat Track · corrodedINSPECTION TYPE:C&SI AFT CARGO BAY, SEAT TRACK HAS LIGHT SURFACE CORROSION AT 2 AREAS AT BS 1027 LT & BS 1008 RT. CORROSION REMOVED AND FOUND OUTSIDE LIMITS IAW SRM 51-10-06 SEAT TRACK REPAIRED IAW SRM 53-10-5 FIG 8.Oct 23, 2002 · N932UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS02239865Frame · crackedINSPECTION TYPE:C&SI SUSPECT CRACK AT FUSELAGE FRAME ATTACH POINT AT BS 990 STR. 29L IN A FT CARGO BAY REPAIRED FRAME AS PER SRM 53-10-4 FIG 11Oct 23, 2002 · N932UP · Boeing 72725C · Fuselage Main, StructureSDR UPS02239911Bracket · crackedINSPECTION TYPE:C&SI NO. 13 SPOILER SUPPORT CASTING, I/B SUPPORT BRACKET IS CRACKED AT LW R ATTACH HOLE BRACKET REPLACED IAW SB 57-84 & DRAWING 65-17351Oct 22, 2002 · N932UP · Boeing 72725C · Drag Control SystemSDR UPS02239896Pin · corrodedINSPECTION TYPE: C & SI, RT WING REAR SPAR TO BODY FITTING TERMINAL BOTTLE PIN AT BS 870 HAS EVIDENCE OF PITTING CORROSION. CORROSION OUT OF LIMITS, BOTTLE PIN REPLACED IAW MM 57-41-01.Oct 22, 2002 · N932UP · Boeing 72725C · Wing, Fuselage Attach FittingsSDR UPS02239909Bracket · crackedINSPECTION TYPE:C&SI NO. 2 SPOILER SUPPORT CASTING, I/B REAR SPAR ATTACH BRACKET IS CRACK ED AT LWR ATTACH HOLE BRACKET REPLACED IAW SB 57-84 & DRAWING 65-17351Oct 21, 2002 · N932UP · Boeing 72725C · Drag Control SystemSDR UPS02239898Skin · corrodedINSPECTION TYPE: C & SI, CORROSION ON OUTER SURFACE OF NR 6 RISER SKIN OF AFT AIR STAIRS CORROSION REMOVED IAW SRM 51-10-06, FOUND TO BE OUT OF LIMITS IAW SR M 52-00-2. REPAIRED IAW EO B727-5260-7551-AOct 21, 2002 · N932UP · Boeing 72725C · Entrance Stairs
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