Boeing 727-277

Service difficulty reports · 627

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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 = '727277'
  ORDER BY difficulty_date DESC"

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SDR 06FDEA04162Skin · misrepairedEXTERNAL REPAIR LOCATED AT APPROX 29 INCHES FROM AFT END AND 48" FROM BOTTOM END ON THE FWD LOWER CARGO DOOR FOUND NOT TO BE INSTALLED USING FAA APPROVED DATA. REF SNRM NR N00567 AND SRM 52-00-3 FIG 3 - FIG 4. INCORRECT FASTENER SPACING, DAMAGE REMOVAL CANNODec 2, 2006 · N244FE · Boeing 727277 · Cargo/Baggage DoorsSDR 06FDEA04160Spar · crackedRIGHT WING REAR SPAR UPPER CAP SURF STRIP HAS A CRACK AT SPOILER NR 11 STOPPED DRILLED CRACK. FABRICATED REPAIR PLATE AND REPAIR WASHERS, TREATED AND PRIMED, AND INSTALLED REPAIR IAW SRM 57-30-4, 51-10-2.Dec 2, 2006 · N245FE · Boeing 727277 · Wing SparSDR 06FDEA04156Seat Track · crackedMAIN CARGO COMPT SEAT TRACK HAS A CRACK AND CORROSION AT FASTENER HOLE, APPROX AT BS 693 LBL 24 REMOVED SEAT TRACK FROM STA 690-740 LBL24 REF SRM 51-30-2. VERIFIED MATERIAL FOR NEW SEAT TRACK REF SRM 53-10-2 PG 13. FABRICATED NEW SEAT TRACK REF DWG NR 2902 ADec 1, 2006 · N244FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04151Frame · crackedCABIN FUSELAGE FRAME AT STA 804 STR 14R, CRACKING OUT OF FASTENER HOLE AFT SIDE OF FRAME. CUTOUT AND REMOVED DAMAGED PORTION OF FRAME CHORD, HFEC INSPECTED THE CUTOUT TO VERIFY NO CRACKS. FABRICATED FILLER AND REPAIR ANGLE. INSTALLED REPAIR PARTS WET WITH SDec 1, 2006 · N244FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA04150Seat Track · corrodedLT CABIN SEAT TRACK BEAM IS CORRODED AT STA 620-628 LBL 1. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED REF SRM 51-30-02 (N00537).Dec 1, 2006 · N244FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04149Seat Track · corrodedLT FWD CABIN SEAT TRACK BEAM IS CORRODED AT STA 546 LBL 24. REMOVED SEAT TRACK AND INSTALLED NEW TRACK REF SRM 51-30-5, AND SRM 51-30-2. (N00527)Dec 1, 2006 · N244FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04148Floorbeam · corrodedLT FWD CABIN FLOORBEAM UPPER CAP CORRODED FOM STA 620 LBL 1- LBL 24. REMOVED CORROSION AND REPAIRED DAMAGED AREA REF SRM53-10-8 FIG 1 (N00533).Dec 1, 2006 · N244FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA04147Skin · misrepairedAGING A/C INSP, REPAIR LOCATED AT STA 400-420, STR 16L-17L FOUND NOT TO BE INSTALLED USING APPROVED DATA REF SNRM NR N00371 AND SRM 53-30-3 FIG 3. REPAIR ENDS ON A STRINGER. REMOVED REPAIR, FABRICATED AND INSTALLED NEW REPAIR REF SRM53-30-3 FIG 3.Dec 1, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04146Skin · misrepairedAGING A/C INSPECTION REPAIR LOCATED AT STA 1090-1110, STR 29L-29R FOUND NOT TO BE INSTALLED USING APPROVED DATA, REF SNRM NR N00081 AND SRM 53-30-3 FIG 3 REPAIR DOES NOT HAVE REQUIRED NUMBER OF FASTENER ROWS FWD AND AFT. REMOVED PREVIOUS REPAIR, VERIFIED MATEDec 1, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04145Skin · damagedLIGHTNING STRIKE ON FWD LOWER FUSELAGE BLENDED OUT OF LIMITS REF SNRM N00292 AT STA 226 13 INCH BELOW STR 26L. CUT OUT DAMAGED AREA, VERIFIED MATERIAL. FABRICATED DOUBLER, ALODINED, PRIMED, PAINTED, EDGE SEALED DOUBLER. REF SRM 53-30-3, AND SRM 51-10-7 FIDec 1, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04144Seat Track · corrodedCABIN LT SIDE STA 990-1070 LBL 45.5 SEAT TRACK HAS CORROSION AND EXFOLIATION ON O/B FLANGE REMOVED DAMAGED SEAT TRACK AND REPLACED WITH NEW TRACK REF SRM 53-10-5 PG1-5Dec 1, 2006 · N244FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04021Flap Track · corrodedRT WING LWR SURFACE AT NR 7 FLAP TRACK HAS CORROSION AT FWD TRACK MOUNTING BRACKET. REPAIRED PER FED EX EA 7-5710-100604.Nov 16, 2006 · N241FE · Boeing 727277 · Trailing Edge FlapsSDR 06FDEA04022Shear Tie · corrodedFOUND CORROSION BETWEEN SHEAR TIE AND FRAME BS 1148, STR 28 LT - 30 LT. REPAIRED SHEAR TIE PER SRM 53-10-4 FIG 14.Nov 16, 2006 · N241FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR 06FDEA04020Fitting · corrodedWHILE WORKING CARD N00533, FOUND CORROSION ON NR 5 K-FLAP CENTER HINGE FITTING (A/C SIDE) IB LUG, I/B FACE. REPAIRED NR 5 K-FLAP CENTER HINGE FITTING IAW FED EX EA 7-5710-100605.Nov 16, 2006 · N241FE · Boeing 727277 · Trailing Edge FlapsSDR 06FDEA04014Flap Track · corrodedNR 7 FLAP TRACK HAS CORROSION AT AFT MOUNTING HOLES. REMOVED AND REPLACED NR 7 FLAP TRACK IAW FED EX W/C 27X5709-03.Nov 15, 2006 · N241FE · Boeing 727277 · Trailing Edge FlapsSDR 06FDEA03995Skin · unknownRT STAB UPPER SURFACE, STA APPROX 4" FROM I/B END T/E, EXTERNAL 3" DOUBLERS, REQUIRES EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF THE REPAIR IS IN ACCORDANCE WITH FAA, APPROVED DATA. REMOVED EXISTING REPAIR ON RT HORIZ STAB UPPER SURFACE AND RENov 13, 2006 · N241FE · Boeing 727277 · Horizontal Stabilizer, Plate/SkinSDR 06FDEA03994Angle · corrodedFOUND CORROSION ON UPPER SPOILER BEAM ANGLE FROM NR 5 TO NR 6 SPOILER ACTUATORS. REMOVED DAMAGE ON UPPER SPOILER BEAM ANGLE FROM NR 5 TO NR 6 SPOILER ACTUATORS AND REPAIRED IAW SRM 51-40-4.Nov 13, 2006 · N241FE · Boeing 727277 · SpoilersSDR 06FDEA03986Seat Track · corrodedEXPANSION LINK, BS 740-760, LBL 45 CORRODED AROUND FWD ATTACH BOLT. REMOVED AND REPLACED EXPANSION LINK BS 740-760 LBL 45 IAW SRM 53-10-1.Nov 13, 2006 · N241FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03940Depressor · damagedAFT NR 2 CARGO DOOR LWR CENTER SEAL DEPRESSOR CHAFED. REMOVED AND REPLACED AFT NO. 2 CARGO DOOR CNTR SEAL DEPRESSORE IAW SRM 51-30-5.Nov 10, 2006 · N241FE · Boeing 727277 · Cargo/Baggage DoorsSDR 06FDEA03943Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER CHORD BS 380 RBL 50 WL 208. REMOVED DAMAGE AREA OF UPPER CHORDS AT BS 380 RBL 50 AND REPAIRED IAW SRM 53-10-8.Nov 10, 2006 · N241FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA03942Skin · bulgedAFT NR 2 CARGO DOOR SKIN BULGING AROUND 8 CUPPED FASTENERS 1-2 INCHES FROM AFT EDGE 8-10 INCHES FROM BOTTOM. CUT OUT DAMAGE AREA LWR AFT CORNER, FABRICATED SKIN DOUBLER AND FILLER INSTALLED REPAIR ALODINED & PRIMED. REINSTALLED LEVELING COMPOUND PER SRM 52-Nov 10, 2006 · N241FE · Boeing 727277 · Cargo/Baggage DoorsSDR 06FDEA03939Skin · misrepairedNR 2 CARGO DOOR, EXTERNAL SKIN, FWD LWR CORNER, DOUBLER REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF THE REPAIR IS IN ACCORDANCE WITH FAA, APPROVED DATA. COMING DOUBLER REPAIR ON NR 2 CARGO DOOR SKIN WAS NOT IN COMPLIANCE WITNov 10, 2006 · N241FE · Boeing 727277 · Cargo/Baggage DoorsSDR 06FDEA03938Frame · dentedFOUND DENT IN FRAME STA 600 BETWEEN STR 24L - 25L. REMOVED DAMAGE IN FRAME STA 600 BETWEEN STR 24L - 25L AND REPAIRED IAW SRM 51-30-2.Nov 10, 2006 · N241FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA03936Frame · damagedFWD CARGO COMPARTMENT, DAMAGE TO STA 520 FRAME BETWEEN STR 22L AND 25L. REMOVED DAMAGE ON FRAME BS 520 BETWEEN STR 22L AND 25L AND REPAIRED IAW SRM 53- 10-1.Nov 9, 2006 · N241FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA03931Frame · dentedFRAME FLANGE DENTED STA 680 STR 23L - 25L. REMOVED DAMAGE ON FRAME BS 680 STR 23L-25L AND IAW SRM 51-40-3.Nov 9, 2006 · N241FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA03935Floorbeam · damagedDRILL START IN UPPER CHORD OF BS 870 FLOORBEAM AT LBL 50, WL 208. REPAIRED BS 870 FLOORBEAM AT LBL 50, WL 208 IAW FED EX EA 7-5310- 105909.Nov 9, 2006 · N241FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA03934Shear Tie · corrodedAFT CARGO BAY CORROSION ON SHEAR TIE BS 1148 LBL 3. REMOVED AND REPLACED SHEAR TIE BS 1148 LBL 3 IAW SRM 53-10-4.Nov 9, 2006 · N241FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR 06FDEA03933Shear Tie · corrodedAFT CARGO BAY CORROSION ON SHEAR TIE BS 1148 LBL 10. REMOVED AND REPLACED SHEAR TIE BS 1148 LBL 10 IAW SRM 53-10-4.Nov 9, 2006 · N241FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR 06FDEA03932Shear Tie · corrodedAFT CARGO BAY CORROSION ON SHEAR TIE BS 1148 LBL 16. REMOVED AND REPLACED SHEAR TIE AT BS 1148 LBL 16 IAW SRM 53-10-4.Nov 9, 2006 · N241FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR 06FDEA03923Shear Web · damagedWHILE WORKING N01197 FOUND LT SHEAR WEB AT BS 1130 - 1176, LBL 25 - LBL 65, WL 208 TO HAVE NUMEROUS MISDRILLED AND DOUBLE HOLES. REMOVED AND REPLACED LEFT SHEAR WEB AT BS 1130 - BS 1176, LBL 25 - LBL 65 WL 208 PER SRM 51-30-2.Nov 8, 2006 · N241FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR 06FDEA03920Crease Beam · corrodedFOUND CORROSION ON CREASE BEAM WEB AT BS 720C PLUS 11" AND 720C PLUS 18", LBL 65, WL 208. REMOVED DAMAGE ON CREASE BEAM AT 720C PLUS 11 TO 720C PLUS 18, LBL 65, WL 208 AND REPAIRED IAW SRM 51-30-2.Nov 8, 2006 · N241FE · Boeing 727277 · Fuselage Main, StructureSDR 06FDEA03926Crease Beam · damagedFOUND CREASE BEAM TO BE MISDRILLED AT BS 720F AND 720E LBL 63, WL 208. REMOVED DAMAGE CREASE BEAM AT BS 720F TO 720E LBL 63 WL 208 AND REPAIRED IAW SRM 51-30-5, 51-30-6, AND 51-30-8.Nov 8, 2006 · N241FE · Boeing 727277 · Fuselage Main, StructureSDR 06FDEA03924Spar · damagedSHEARED FASTENER HEAD IN RT WING UPPER REAR SPAR VERTICAL FLANGE AT WS 212. REPAIRED PER FED EX EA 7-5710-100602.Nov 8, 2006 · N241FE · Boeing 727277 · Wing SparSDR 06FDEA03922Shear Web · crackedWHILE WORKING 1176 CHORD, FOUND AFT CENTER SHEAR WEB FROM BS 1148 - BS 1176, LBL 25 - RBL 25, WL 208 TO HAVE NUMEROUS DOUBLE HOLES AND TO BE CRACKED. FABRICATED NEW WEB PER SRM 51-0-2.Nov 8, 2006 · N241FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR 06FDEA03921Shear Web · dentedFOUND DENT IN SHEAR WEB AT BS 1137, RBL 26, WL 208. REPAIRED PER SRM 51-40-2 FIG 1.Nov 8, 2006 · N241FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR 06FDEA03911Crease Beam · corrodedFOUND CORROSION ON CREASE BEAM WEB BS 720D - BS 720E, STR 17L. REMOVED DAMAGED CREASE BEAM WEB BS 720D-720E, STR 17L AND REPAIRED IAW SRM 51-10-2.Nov 7, 2006 · N241FE · Boeing 727277 · Fuselage Main, StructureSDR 06FDEA03910Skin · damagedE/E BAY DOOR OUTER SKIN DAMAGED ALL AROUND OUTER EDGE, AFT LT, OUT OF LIMITS. REMOVED AN AREA APX 3" BY 16" FROM AFT LT EDGE SKIN OF E/E BAY DOOR. FABRICATED FILLER FROM 2024-T3 .040, LOT 707522 AND PATCH FROM 2024-T3, 050, LOT NR 715012 PER SRM 52-00-3, FIGNov 7, 2006 · N241FE · Boeing 727277 · Electrical/Electronic Compartment DoorsSDR 06FDEA03913Frame · crackedOUTER CHORD OF FRAME CRACKED STA 804.5 STR 14R. REMOVED AND REPLACED OUTER CHORD OF FRAME 804.5 STR 14R IAW SRM 51-30-5, 51-30-2.Nov 7, 2006 · N241FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA03912Frame · dentedFRAME FLANGE DENTED STA 660 STR 23L - 25L. DENT ON FRAME FLANGE BS 660 STR 23L - 25L FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE OF FRAME LOCATED DRILLED NEW FRAME SECTION ALODINED, PRIMED AND INSTALLED SRM 53-10-1, SRM 51-40-3.Nov 7, 2006 · N241FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA03909Stiffener · corrodedWHILE WORKING ON THE L/W UPPER SKIN CORROSION AT THE FRONT SPAR WING LBL 348, FOUND THE TEE CLIP COMMON TO THE UPPER SPAR CHORD AND WSTA 357 RIB FWD STIFFENER CRACKED. REMOVED AND REPLACED TEE CLIP AT L/W STE 357 IAW SRM 51-30-5, 51-30-6, 51-30-2.Nov 7, 2006 · N241FE · Boeing 727277 · Wing Miscellaneous StructureSDR 06FDEA03908Stiffener · corrodedWHILE WORKING ON THE L/W UPPER SKIN CORROSION AT THE FRONT SPAR WING LBL 348, FOUND THE TEE CLIP COMMON TO THE UPPER SPAR CHORD AND WSTA 410 RIB FD STIFFENER CORRODED. REMOVED AND REPLACED TEE CLIP AT L/W STA 410 IAW SRM 51-30-5, 561-30-6, 51-30-2.Nov 7, 2006 · N241FE · Boeing 727277 · Wing Miscellaneous StructureSDR 06FDEA03907Stringer · crackedFOUND STR 16L IS CRACKED AT BS 644. REMOVED DAMAGED AREA, LOCATED AND DRILLED REPAIR PARTS AND INSTALLED IAW SRM 53-10-3.Nov 7, 2006 · N241FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR 06FDEA03899Shear Tie · corrodedFOUND CORROSION C53-111-01, ON FRAME SHEAR TIE STA 720A BETWEEN STR 27L - 28L. REMOVED SHEAR TIE FABRICATED NEW SHEAR TIE ALODINIED AND PAINTED PARTS INSTALLED WET WITH SEALANT PER SRM 51-10-1, SRM 53-10-4, SRM 51-30-2, SRM 51-20-4 AT STA 720A BETWEEN STR 27LNov 6, 2006 · N241FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR 06FDEA03854Frame · dentedFOUND DENT ON FRAME AT BS 520 STR 126R.Nov 2, 2006 · N241FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA03852Frame · misrepairedLT INTERIOR FUSELAGE, FRAME REPAIR STA 950F, STRINGER 5L, REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF THE REPAIR IS IN ACCORDANCE WITH FAA, APPROVED DATA. EVALUATED REPAIR ON FRAME BS 750F STR 5L REPAIR DOES NOT COMPLY WITH Nov 2, 2006 · N241FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA03853Floorbeam · damagedWHILE WORKING N01184 , FOUND TOP CHORD OF FLOORBEAM TO BE MISDRILLED AT BS 720F, LBL 63, WL 208. ACCESSED CREASE BEAM STIFFNER, SEAT TRACK BS 720B TO 740 LBL 25 - LBL 65 AND FLOORBEAM WEB IAW SRM 51-30-2 AND REINSTALLED UPON COMPLETION OF REPAIR IAW SRM 51-30Nov 2, 2006 · N241FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA03851Skin · corrodedFOUND WING UPPER CENTER SKIN AT STA 760 , RBL 45-51, WL 204 CORRODED. REPAIRED PER FED EX EA 7-5710-100612.Nov 2, 2006 · N241FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA03803Floorbeam · corrodedFOUND CORROSION ON BS 1110 FLOORBEAM UPPER FLANGE LBL 6-23 WL 208. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND REPAIRED IAW SRM 53-10-8 FIG 5.Oct 27, 2006 · N241FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA03802Frame · damagedFOUND FWD CARGO COMPARTMENT, DAMAGE TO STA 580 FRAME BETWEEN STR 22L AND 25L. REMOVED DAMAGE ON FRAME BS 580 STR 22L TO 25L AND REPAIRED IAW SRM 53-10-1, 51-40-3.Oct 27, 2006 · N241FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA03801Crease Beam · corrodedFOUND CORROSION ON CREASE BEAM WEB BS 720E PLUS 2" TO 720F LBL 65 TO 70. REMOVED AND REPLACED CREASE BEAM WEB STA 720E TO 720F LBL 65 TO 70 PER SRM 51-30- 2, 51-30-5, 51-30-6, 51-10-2 AND MM 51-20-151-7.Oct 27, 2006 · N241FE · Boeing 727277 · Fuselage Main, Structure
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