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 95FDEA01484Skin · mismfgAFT CARGO BELLY SKIN AT STA 1150, STA 29 - 2 EA HOLES HAVE 2 FASTENERS IN ONE HOLE. REMOVED DAMAGED FASTENERS, INSTALLED DOUBLER ON SKIN PER SRM 53-30-3.Sep 26, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 95FDEA01483Skin · mismfgTWO FASTENERS INSTALLED IN ONE HOLE, THROUGH SHEAR TIE STA 1130, O/B OF STR 29L. REMOVED DAMAGE FROM FASTENERS AT STA 1130 O/B OF STR 29L. INSTALLED DOUBLER OF AFT FUSE BELLY SKIN PER SRM 53-30-3.Sep 26, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 95FDEA01431Floor Beam · corrodedCORROSION OF FLOOR TRACK AT LBL 45 AT BS 360, 400-420 AND 380. REMOVED SECTION OF FLOOR BEAM STATION 360 - 420 AND INSTALLED NEW FLOOR TRACK FROM STA 360-420 PER SRM 51-10-5.Sep 26, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01481Floor Beam · corrodedSTA 640, RBL 5 UPPER FLANGE OF FLOOR BEAM HAS EXFOLIATION CORROSION PILLOWED AND BLOWN OUT - REMOVED CORROSION AND INSTALLED DOUBLER REPAIR WITH 7075-T6 EXTRUSIONS AND A 15-5 STAINLESS STEEL STRAP, CAD PLOTED AND HEAT TREATED TO 180-200 RSI, TREATED AND PRIMEDSep 25, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01480Floor Beam · corrodedCORROSION BOTTOM OF FLOOR BEAM JUST I/B OF RBL 25 SEAT TRACK STA 480. REMOVED PORTION OF CORRODED BEAM - FABRICATED AND INSTALLED DOUBLER PER 53-10-8 FIG 5 OF SRM.Sep 25, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01460Floorbeam · corrodedUPPER LOBE FLOOR, CORROSION ON UNDERSIDE OF FLOORBEAM LT STA 480 BETWEEN BL 0 AND LBL 24. CORROSION REMOVAL WAS BEYOND LIMITS. INSTALLED REPAIR IAW 53-10-8 FIG 5 AND 51-40-2.Sep 25, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01459Flange · corrodedUPPER MAIN CARGO, CORROSION ON BOTTOM SIDE OF THE FWD FLANGE STA 480 RBL 5. REMOVED CORROSION AT LOCATIONS PER SRM 51-10-01, INSTALLED REPAIR IAW SRM 53-10-8 FIG 5 AND 51-40-2.Sep 25, 1995 · N135FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 95FDEA01477Spar · corrodedRIVET HEAD POPPED AND CORROSION ON OUTSIDE OF CENTER TANK REAR SPAR JUST FWD OF STA 870 RT, RBL 50. REMOVED CORR - MATERIAL THICKNESS BEYOND MM LIMIT. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER AA ESO 11782. AWAITING FEDEX EA.Sep 21, 1995 · N135FE · Boeing 72725C · Wing SparSDR 95FDEA01398Floor Beam · corrodedON NR 0234, CORROSION ON FLOOR BEAM IN MAIN CARGO STA 420 RBL 20. CORROSION REMOVED BEYOND LIMITS. CUT OUT AREA AND INSTALLED .090 INCH DOUBLERS AND FILLER PER SRM 53-11-8, FIG 8.Sep 19, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01397Rib · crackedUPPER RUDDER THRUST HINGE, LOWER LT SIDE. RIB IS CRACKED BETWEEN FASTENERS. REMOVED 6 EACH FASTENERS - HFEC CHECKED. VERIFIED CRACK FROM HOLE-TO-HOLE, AFT ROW. INSTALLED DOUBLER PER FEDEX EA 7-5510-25773 DATED 9-15-95. PAINTED ALL AREAS EFFECTED FOR WATER-Sep 18, 1995 · N135FE · Boeing 72725C · Rudder, Spar/RibSDR 95FDEA01387Aft Trunnion · damagedLEFT WING FRONT SPAR FORWARD TERMINAL PIN JOINT HOLE CRACKED AFT FORWARD. LEVELED AND SHORED A/C IAW SRM 51-50-1. CUT LOWER CHORD ANGLE AND WEB IAW BOEING DWG 65C29064. REMOVED FS 740 AFT TRUNNION AND REPLACED WITH NEW AFT TRUNNION. SPLICED WEB AND LOWER CSep 18, 1995 · N135FE · Boeing 72725C · Fuselage, Landing Gear Attach FittingsSDR 95FDEA01366Floor · damagedUNAUTHORIZED REPAIR INSTALL ON FLOOR, BS 344 LBL 38. REMOVED AND REPLACED REPAIR PER DRAWING NR SR27-53-007, NR O857.Sep 18, 1995 · N135FE · Boeing 72725C · Fuselage Floor PanelSDR 95FDEA01369Floorbeam · corrodedCORROSION ON MAIN CABIN FLOORBEAM STA 400 AT LBL 35.Sep 16, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01396Skin · damagedSTR 9R HAD HOLE AND CRACK AND ONE FAST HOLE WITH EXISTING MISDRILL CAUSED DAMAGE IN FUSELAGE SKIN (A/C CAME IN WITH THIS COND). STR DAMAGE AND FUSELAGE SKIN DAMAGE WAS CUT OUT AND STR SPLICE 9 .050 INCH DOUBLER ON SKIN WAS INSTALLED, PER SRM 53-30-3, FIG 9, NSep 15, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 95FDEA01368Skin · corrodedOUTSIDE FUSELAGE STA 440 STR 17R THERE IS A BULGE IN THE SKIN NR 00073. LFEC SHOWS CORROSION IN EXCESS OF 20 PERCENT MATERIAL LOSS. REMOVED CORROSION AND FABRICATED DOUBLER PER SRM 53-30-3.Sep 15, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 95FDEA01367Skin · damagedHOLE IN STR 9R AND CRACKED AT STA 1138, CUT OUT DAMAGED PART OF STR 9R AND FUSE SKIN THAT WAS DAMAGED ALONG WITH STR. INSTALLED FLUSH DOUBLER AND STR REPAIR PER 53-30-8. ARRIVED IN TUL IN THIS CONDITION.Sep 15, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 95FDEA01370Casting · corrodedCORROSION ON MAIN CARGO DOOR CASTING, 7 PLACES LOCATED BETWEEN 6TH AND 7TH LATCHES.Sep 14, 1995 · N135FE · Boeing 72725C · Cargo/Baggage DoorsSDR UPS204428Actuator · malfunctionedPILOT REPORTED, THAT RIGHT MAIN GEAR DOOR LIGHT CAME ON WHEN GEAR HANDLE WAS PLACED IN OFF. LANDING GEAR RECYCLED WITH NO EFFECT. MAINTENANCE REPLACED THE RIGHT MAIN DOOR ACTUATOR.Sep 13, 1995 · N937UP · Boeing 72725C · Landing Gear Door ActuatorSDR UPS204376Skin · delaminatedWHILE ON GROUND, MAINTENANCE FOUND LEFT MIDFLAP DELAMINATED MIDDLE TRAILING EDGE 2 PLACES O/B FLAP. DEFERRED PER D-98013 INTERM REPAIR PER 57-50-1.Sep 9, 1995 · N949UP · Boeing 72725C · Trailing Edge FlapsSDR UPS204334Le Skin · crackedWHILE ON GROUND, MAINTENANCE FOUND REF D97427 LT ELEVATOR L/E 2 CRACKED. REPAIRED LT REV IAW 55-20-3 FIG 4. CALCULATED REPAIR WEIGHT TO BE 20 GRAMS AT O MOMENT, REPAIR WEIGHT WITHIN SRM 57-80-7.Aug 24, 1995 · N932UP · Boeing 72725C · Elevator, Plate/SkinSDR UPS204286Eel · malfunctionPILOT REPORTED DURING TAKEOFF ROLL, ENCOUNTERED SEVERAL HARD BUMPS, EMERGENCY LIGHTS ILLUMINATED AND REMAINED ILLUMINATED IN ARMED POSITION. CHECKED OPERATION OF EMERGENCY LIGHTS AND FOUND OPERATION NORMAL AT PRESENT.Aug 18, 1995 · N946UP · Boeing 72725C · Emergency LightingSDR UPS803879Eel Battery · dischargedWHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK EMERGENCY EXIT LIGHT FAILS TEST. REPLACED BATTERIES, OPS CHECK OK.Jul 16, 1995 · N946UP · Boeing 72725C · Emergency LightingSDR UPS203875Eel · inoperableWHILE ON GROUND IN CLEVELAND, MAINTENANCE FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECK NORMAL.Jul 11, 1995 · N933UP · Boeing 72725C · Emergency LightingSDR UPS203746Frame · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND 2 CRACKS ON FRAME AT B.S. 930, RBL 64 AND 67, WL 199 RT WHEELWELL. REPAIRED IAW E.O. B727-5310-7167-A.Jul 5, 1995 · N947UP · Boeing 72725C · Fuselage Main, FrameSDR UPS203744Skin · delaminatedWHILE IN FOR C-CHECK, MAINTENANCE FOUND DELAMINATED SPOILER AT UPPER I/B CORNER 4 INCH BY 4.5 INCH ON THE NR 5. REPAIRED IAW SRM 51-40-06.Jul 3, 1995 · N947UP · Boeing 72725C · SpoilersSDR UPS203743Skin · delaminatedWHILE IN FOR C-CHECK, MAINTENANCE FOUND DELAMINATED SPOILER AT UPPER I/B CORNER, 4 INCH BY 4.5 INCH ON THE NR 9. REPAIRED IAW SRM 51-40-06.Jul 3, 1995 · N947UP · Boeing 72725C · SpoilersSDR UPS203742Web · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED WEB AT STA 294 TO 312, RBL 40, WL 207. REPAIRED IAW SRM 51-30-2, 51-20-1, M/M 51-20-151.Jul 3, 1995 · N947UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203741Tee · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TEE AT FS 760, RBL 70.5, WL 200 ON THE I/B FLANGE. REPAIRED IAW SRM 51-10-1, 51-30-2.Jul 3, 1995 · N932UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203740Tee · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TEE AT FS 760, LBL 70.5, WL 200. REPAIRED IAW SRM 51-10-1, 51-30-2.Jul 3, 1995 · N932UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203739Web · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SHEAR WEB AT STA 1175, AT RBL 40. REPAIRED IAW SRM 51-40-2, 51-30-2.Jul 3, 1995 · N932UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203738Intercostal · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED INTERCOSTAL AT STR 15L, FS 303. REPAIRED IAW SRM 51-40-3, 51-30-2.Jul 3, 1995 · N932UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203737Shear Tie · damagedWHILE IN FOR C-CHECK, MAINTENANCE FOUND BROKEN SHEAR TIE FS 294, STR 9 TO 10L. REPAIRED IAW SRM 51-40-3, 51-30-2.Jul 3, 1995 · N932UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203736Web · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED WEB AT STA 277 AT STR 14L AND 16L. REPAIRED IAW SRM 51-40-3, 51-30-2.Jul 3, 1995 · N932UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203735Shear Tie · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED SHEAR TIE AT FS 294, STA 8 TO 9L. REPAIRED IAW SRM 51-40-3, 51-30-2, B727-5310-1259.Jul 3, 1995 · N932UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203734Intercostal · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED INTERCOSTAL AT STA 303, STR 16L. REPAIRED IAW SRM 51-40-3, 51-30-2.Jul 3, 1995 · N932UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203733Shear Tie · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED SHEAR TIE AT FS 294 BETWEEN STRINGER 10L AND 11L. REPAIRED IAW SRM 51-30-2.Jul 3, 1995 · N932UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203732Seat Track · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LWR CARGO RT SEAT TRACK AT FS 580 TO 680. REPAIRED IAW SRM 51-10-1, 51-30-2.Jul 3, 1995 · N932UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS203731Flap · delaminatedWHILE IN FOR C-CHECK, MAINTENANCE FOUND DELAMINATION OF I/B RT AFT FLAP ON THE O/B CORNER. REPAIRED IAW SRM 51-40-6, M/M 51-20-151.Jul 3, 1995 · N947UP · Boeing 72725C · Trailing Edge FlapsSDR UPS203730Expansion Link · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK AT STA 740 TO 760 AT RBL 25, WL 208. REPAIRED IAW SRM 53-10-1, 51-30-8, OHM 20-50-03, 20-50-02, 20-50-1.Jul 3, 1995 · N947UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203729Support · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT STA 302 TO 312. REPAIRED IAW SRM 51-10-6, 51-30-6, 51-20-1, 51-30-5, 51-30-02.Jul 3, 1995 · N947UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203728Chord · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LT UPPER NOSE CHORD BS 340 TO 348, LBL 15, WL 170. REPAIRED IAW SRM 53-10-1, 51-10-1, 51-30-5, 51-20-4, 51-30-2.Jul 3, 1995 · N947UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR 95FDEA00865Seat Track · corrodedSEAT TRACK WL 208, LBL 45, STA 560, HAS CORROSION IN WELL. REMOVED AND REPLACED SEAT TRACK.Jul 1, 1995 · N127FE · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00864Skin · corrodedCORROSION (75C002-00) NR 1 K-FLAP DATA PLATE. REPAIRED CORROSION DAMAGE AT NR 1 K-FLAP DATA PLATE AND RELOCATED DATA PLATE IAW FEDEX SRM 57-50-3 AND SRM 27-57-010.Jul 1, 1995 · N127FE · Boeing 72725C · Leading Edge DevicesSDR UPS203682Skin · delaminatedWHILE ON GROUND, MAINTENANCE FOUND FLAP DELAMINATED AT RT, O/B TRAILING EDGE. REPAIRED IAW B727-5750-3081C.Jun 23, 1995 · N949UP · Boeing 72725C · Trailing Edge FlapsSDR 95FDEA00852Casting · crackedLIGHT CORROSION ON HEAVY CARGO DOOR CASTING STA 620 ON UNDERSIDE OF LEG, AFT SIDE OF 620 INCLUDING CORRODED GOUGE. HFEC'D AREA, APPROXIMATELY A 1.50 INCH CRACK, RUNS INTO RADIUS MARKED ENDS. INSTALLED DOUBLER REPAIR PER ESO 11782. INSTALLED DOUBLER PER FEDJun 21, 1995 · N134FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 95FDEA00855Floorbeam · corrodedFS 344 LBL 6-14 CORROSION ON TOP LEG OF FLOORBEAM. INSTALLED FLOORBEAM CAP PER 53-10-8.Jun 20, 1995 · N134FE · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS203614Tab · corrosionWHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON L/W O/B AILERON TAB, I/B TAB CORRODED. INSTALLED TAB IAW SRM 51-10-1, M/M 27-10-4.Jun 16, 1995 · N950UP · Boeing 72725C · Aileron TabsSDR UPS203598Skin · delaminatedWHILE IN FOR C-CHECK MAINTENANCE, FOUND DELAMINATION ON L/W I/B FLAP. REPAIRED IAW SRM 51-40-6, M/M 51-20-0.Jun 16, 1995 · N950UP · Boeing 72725C · Trailing Edge FlapsSDR UPS203597Door · corrodedWHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON MAIN CARGO DOOR AFT LIFT ACTUATOR LOWER CUTOUT. REPAIRED IAW EO B727-52-0153.Jun 16, 1995 · N950UP · Boeing 72725C · Cargo/Baggage DoorsSDR UPS203596Spar · corrodedWHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON UPPER CHORD OF LEFT WING REAR SPAR AT WS 198.0. REPAIRED IAW SRM 57-10-6, 51-30-2, M/M 28-11-0.Jun 16, 1995 · N950UP · Boeing 72725C · Wing Spar
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