Boeing 727-227

Service difficulty reports · 5,082

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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 = '727227'
  ORDER BY difficulty_date DESC"

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SDR 05FDEA04246Stringer Clip · gougedFWD CARGO BAY STR CLIP GOUGED AT BS 540, STR 24LT. REPLACED STRINGER CLIP PER SRM 51-30-2.Dec 12, 2005 · N490FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 05FDEA04262Frame · dentedFOUND FWD CARGO BAY FRAME IB FLANGE DENTED AT BS 720, STR 24RT. REPAIRED FRAME AT B.S. 720 STR 24R PER SRM 51-40-3.Dec 12, 2005 · N490FE · Boeing 727227 · Fuselage Main, FrameSDR 05FDEA04256Skin · damagedBS 1183 SECTION 48 RIGHT SIDE OUTER SKIN CREASED AT BS 1184 NEXT TO THE TAIL SKID. REMOVED AND REPLACED SKIN PANEL IAW SRM 51-30-2.Dec 12, 2005 · N490FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 05FDEA04248Frame · damagedFOUND STA 720E STR 7R DOUBLE HOLE IN FRAME WEB. REPAIRED FRAME AT BS 720E, STR 7R PER SRM 51-40-3 FIG 1.Dec 12, 2005 · N490FE · Boeing 727227 · Fuselage Main, FrameSDR 05FDEA04244Shear Tie · corrodedFOUND CORROSION ON SHEAR TIE AT BS 1010 RBL 3 WL 148. REPAIRED SHEAR TIE AT BS 1010 RBL 3 WL 148 IAW SRM 53-10-4 FIG 15.Dec 12, 2005 · N485FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR 05FDEA04207Seat Track · corrodedFOUND CORROSION, STA 620 - 640 BL 0 WL 208 CORROSION ON SEAT TRACK. STRINGER TO BE REPLACED ON CUST ID N00436Dec 9, 2005 · N490FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA04206Seat Track · corrodedFOUND CORROSION C53-224-01, STA 570 RBL 1 WL 208 CORROSION ON SEAT TRACK. SEAT TRACK TO BE REPLACED ON CUST ID N00436.Dec 9, 2005 · N490FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA04204Keelbeam · corrodedFOUND CORROSION ON KEELBEAM REPAIR STRAP BS 976 STR29 LT. REPLACED KEEL BEAM REPAIR STRAP PER SR DRAWING 27-53-023A.Dec 9, 2005 · N490FE · Boeing 727227 · Fuselage Main, KeelSDR 05FDEA04208Floorbeam · dentedFOUND CARGO FLOORBEAM DENTED AT BS 587 LBL 8 WL 156. REMOVED AND FABRICATED CARGO FLOORBEAM AT BS 565-610, LBL 8, W/L 156 USING BAC1517-1507 PER SRM 51-40-3 AND INSTALLED PER SRM 51-30-2.Dec 9, 2005 · N490FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA04205Floorbeam · corrodedFOUND CORROSION C53-111-01 (3) ON FLOORBEAM LOWER FLANGE BS 950D BBL0-LBL44 WL 201. REPAIRED FLOORBEAM LOWER FLANGE BS 950D, BL 0 LBL 44, WL 201 PER SRM 53-10-8, 51-10- 2.Dec 9, 2005 · N490FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA04209Floorbeam · corrodedFOUND FLOORBEAM UPPER CHORD CORRODED, BS 1130 , RBL 50, WL 208. REPAIRED FLOORBEAM UPPER CHORD PER FEDEX EA 7-5310-96828A.Dec 9, 2005 · N490FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA04203Lap Joint · damagedFOUND DOUBLER HOLE AT MCD LAP SEAM LOWER ROW BS 660 S27L. REPAIRED PER FED EX EA 7-5330-95993A.Dec 9, 2005 · N485FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005783007Connector · dirtyAFTER TAKEOFF, GEAR HANDLE TO OFF, DOORS LIGHT ON FWD PANEL AND RT DOOR LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE, RESTORED NORMAL OPERATIONS. CLEANED AND RESEATED CONNECTOR ON RT MLG DOOR SWITCH AND OPS CHECKED GOOD IAW MM 32-62-11.Dec 7, 2005 · N783DH · Boeing 727227 · Landing Gear System WiringSDR 05FDEA04160Frame · corrodedN01022, CORROSION (C53-113-01(2)) ON LOWER CHORD AROUND NUTPLATE HOLE BS 1130 RBL 24 WL 201. REMOVED CORROSION ON LOWER CHORD BS 1130 RBL 24, WL 201, FOUND TO BE OUT OF LIMITS, REPAIRED LOWER CHORD IAW SRM 53-10-8 FIG 10.Dec 6, 2005 · N485FE · Boeing 727227 · Fuselage Main, FrameSDR 05FDEA04158Floorbeam · gougedCORROSION BS 304, WL 280, LBL 14 GOUGE ON TOP FLANGE, FLOORBEAM. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-30-2 AND SRM 51-10-2.Dec 6, 2005 · N490FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA04156Floor Support · corrodedCORROSION BS 297-304, WL 208, LBL 12-14. UPPER FLANGE OF FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT BS 294-BS312 IAW SRM 51-30-2, SRM 51-10-2.Dec 6, 2005 · N490FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 05FDEA04155Floorbeam · corrodedCABIN FLOORBEAM UPPER TEE CAP CORRODED AT STA BS 344 BETWEEN LBL24 AND RBL24. CUT OUT CORRODED SECTION OF TEE CAP FROM LBL45 TO RBL24 IAW SRM 53-10-8 FIGURE 9. FABRICATED NEW TEE SECTION AND SPLICE ANGLES IAW SRM 53-10-8 FIGURE 9. ALODINED AND PRIMED REPADec 6, 2005 · N486FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA04154Beam · corrodedSEAT TRACK ATTACH TEE CAP HAS CORROSION OUT OF LIMITS AT LBL45 FROM STA BS760 TO STA BS850. REMOVED SEAT TRACK FROM BS 740 TO BS850 AT LBL45 IAW SRM 51-30-2. REMOVED, REPLACED AND INSTALLED NEW UPPER CHORD FROM STA BS 760 TO STA BS850 AT LBL45 IAW BAC DRADec 6, 2005 · N486FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 05FDEA04153Hinge Fitting · wornRT HORIZONTAL STABILIZER IB NR1 ELEVATOR HINGE FITTING ON HORIZONTAL STABILIZER HAS IB FACE OF FITTING WORN. REMOVED BUSHING, SPOTTED FACE, HFEC INSPECTED LUG BORE FABRICATED AND INSTALLED REPAIR WASHER AND NEW BUSHING ALL IAW EA NR 7-5510-91317. THIDec 6, 2005 · N486FE · Boeing 727227 · Horizontal Stabilizer Miscellaneous StructureSDR 05FDEA04152Floorbeam · gougedMAIN DECK TOP SIDE OF FLOORBEAM GOUGED AT STA BS680 LBL47 TO LBL57. REMOVED DAMAGED, FABRICATED REPAIR ANGLES FROM 17-7PH CRES STEEL .063 INCH, FABRICATED FILLER AND INSTALLED REPAIR ANGLES AND FILLER IAW SRM SR27-53-034 REV E. INSTALLED SEAT TRACK AT LBL65Dec 6, 2005 · N486FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA04141Skin · gougedLEFT OUTBOARD MID FLAP OUTBOARD LEADING EDGE HAS 2 EACH GOUGES. REPAIRED FLAP LEADING EDGE IAW FEDEX EA7-5750-92591. WINGS - LEFT WING OUTBOARD MID FLAP LEADING EDGE SKIN HAS GOUGES. THIS IS A MINOR REPAIR BY TIMCO MECH 7153 AND QC303.Dec 5, 2005 · N486FE · Boeing 727227 · Trailing Edge FlapsSDR 05FDEA04131Skin · corrodedMAIN CABIN, CENTER WING BOX UPPER SURFACE, SKIN IS CORRODED AT STA BS 820 LBL10. REPAIR CENTER WING BOX UPPER SURFACE OF SKIN IAW FEDEX EA7 5710-92595. "WINGS UPPER SKIN PANEL, CENTER TANK CORRODED, REPAIR ". ALODINED AND PRIMED BARE METAL IAW B727 SRM 51Dec 5, 2005 · N486FE · Boeing 727227 · Wing, Plate/SkinSDR 05FDEA04085Flap Track · corrodedLEFT WING INBOARD FLAP OUTBOARD TRACK FORWARD MOUNT HOLES (BORES) HAVE CORROSION. REMOVED CORROSION BY REAMING BORES C, D AND E. MAGNETIC PAR- TICLE INSPECTION AND FABRICATED BUSHINGS FOR BORES C, D AND E IAW FEDEX EA NR 7-5710-92592. ALSO, HEAT TREATED, Dec 3, 2005 · N486FE · Boeing 727227 · Trailing Edge FlapsSDR 05FDEA04073Floorbeam · corrodedFOUND MAIN DECK FLOORBEAM HAS CORROSION AT STA BS 720A BETWEEN RBL4 AND RBL20. CLEANED AREA IAW B727 SRM 51-10-6, AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. REMOVED DAMAGED UPPER CHORD IAW B727 SRM 53-10-8 FIGURE 4. FABRICATED UPPER CHORD, SUPPORDec 2, 2005 · N486FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA04072Skin · dentedREWORK OF FEDEX SNRM N00215 DUE TO WRONG MATERIAL USED. "FORWARD LOWER CARGO DOOR EXTERIOR SKIN IS DENTED". REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER IAW SRM 52-00-3 FIGURE 3. ALODINED AND PRIMED REPAIR DOUBLER IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUDec 2, 2005 · N486FE · Boeing 727227 · Cargo/Baggage DoorsSDR 05FDEA04050Repair · unknownTEMPORARY REPAIR INSTALLED ON AIR STAIR DOOR EXTERNAL ON AIR STAIR DOOR EXTERNAL SKIN LT FWD CORNER. REPAIRED DOOR PER SRM 51-30-2.Dec 1, 2005 · N485FE · Boeing 727227 · Entrance StairsSDR 05FDEA04049Structure · damagedUPON REMOVAL OF REPAIR ON AFT AIRSTAIR (FEDEX CARD 30956, N01070) FOUND CHORD TO BE DAMAGED. REPAIRED CHORD PER SRM 51-30-2.Dec 1, 2005 · N485FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 05FDEA04024Skin · dentedGOODRICH RESPONSIBILITY. FOUND WHILE WORKING N00409, DENTED FWD CARGO DOOR SKIN 4.5" AFT FROM FWD EDGE AND 3" UP FROM LOWER EDGE. REPAIRED PER SRM 52-00-3.Nov 29, 2005 · N485FE · Boeing 727227 · Cargo/Baggage DoorsSDR 05FDEA04020Floorbeam · corrodedFOUND CABIN FLOORBEAM UPPER TEE CAP CORRODED AT STA BS400 BETWEEN BL 0 AND LBL 12. DAMAGE FOUND TO BE BEYOND LIMITS IAW B727 SRM 53-10-1 FIGURE 5. REMOVED DAMAGED UPPER CHORD IAW B727 SRM 53-10-8 FIGURE 3. FABRICATED REPAIR PARTS IAW B727 SRM 53-10-8 FIGURENov 29, 2005 · N486FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA04019Floorbeam · corrodedCABIN FLOORBEAM UPPER TEE CAP CORRODED AT STA BS 380 BETWEEN LBL24 AND LBL36. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW P-FSRM (ER 01-049) 53-10-1 FIGURE 4A. REMOVED DAMAGED AREA AND OBTAINED MATERIAL ID FOR UPPER CHORD AND REPAIR PARTS IAW B727 SRNov 29, 2005 · N486FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA04015Repair · improperREPAIR LOCATED AT STA 1148 STR 30 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA ITEM NR 17. ORIGINAL DOUBLER WAS NOT DONE USING THE B727 SRM 53-30-3 FIGURE 1. REMOVED DOUBLER IAW B727 SRM 51-30-2. Nov 29, 2005 · N486FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 05FDEA04014Floorbeam · corrodedMAIN DECK FLOORBEAM CORRODED AT STA BS 720D FROM LBL27 TO LBL44. DAMAGE FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIGURE 5. REMOVED STANCHION AND INTERCOSTAL BETWEEN STA BS 720D AND STA BS 720E TO FOM IAW B727 SRM 51-30-2. FABRICATED UPPER CHORD REPAIRNov 29, 2005 · N486FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA04011Floorbeam · corrodedFORWARD CARGO COMPARTMENT STA BS 560, BOTTOM OF FLOORBEAM HAS CORROSION BETWEEN RBL10 AND LBL40. REMOVED DAMAGE, FABRICATED 2 EACH REPAIR ANGLES, AND 1 EACH FILLER, AND 1 EACH LOWER STRAP IAW B727 SRM 53-10-8 FIGURE 2 ALODINED AND PRIMED REPAIR PARTS IAW B7Nov 29, 2005 · N486FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA04008Flap Track · corrodedLEFT WING INBOARD FLAP OUTBOARD TRACK AFT MOUNT BOLT HOLES (BORES) HAVE CORROSION. REMOVED CORROSION BY REAMING FROM BORES G AND F WITH FINAL DIAMETER OF .3765 INCH FOR HOLE F AND .3765 INCH FOR HOLE G. FABRICATED REPAIR BUSHINGS FROM 15-5 PH STEEL PO 453539Nov 29, 2005 · N486FE · Boeing 727227 · Trailing Edge FlapsSDR 05FDEA04007Floorbeam · corrodedCABIN FLOORBEAM, UPPER T-CAP CORRODED AT STA BS 440 BL 0 - RBL 24. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIGURE 5. REMOVED DAMAGED T-CAP FROM RBL-8 TO LBL 8 STA BS 440 IAW SRM 53-10-8 FIGURE 3. REMOVED CORROSION FROM RBL 8 TO RBL 24 IAW SRM 51-10Nov 29, 2005 · N486FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA03988Frame · corrodedFORWARD CARGO COMPARTMENT, FRAME AT STA BS 720E BETWEEN STRINGER STR 26-R AND STR 25-R IS CORRODED. REMOVED DAMAGE AREA OF FRAME IAW SRM 53-10-4. FABRICATED INNER AND OUTER REPAIR DOUBLER AND FILLER IAW SRM 51-40-3 FIGURE 1. FABRICATED FRAME SECTION IAW MFGNov 28, 2005 · N486FE · Boeing 727227 · Fuselage Main, FrameSDR 05FDEA03986Skin · corrodedCORROSION AT LOWER FUSELAGE STA BS 480 STRINGER STR 29-L. REMOVED CORROSION IAW SRM 51-10-6. SKIN ORIGINAL THICKNESS .090 MATERIAL LOSS .022 MATERIAL REMAINING .068 FOUND OUT OF LIMITS IAW SRM 53-30-1 UT GAGE T8253C. DOUBLER AND FILLER MATERIAL ID 7075-T6 .Nov 28, 2005 · N486FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 05FDEA03983Repair · improperREPAIR LOCATED AT STA BS 251.6 TO BS 259 STRINGER STR 20-R REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FABRICATED DOUBLER IAW B727 SRM 53-30-2 FIGURE 1. ALODINED DOUBLER IAW B727 SRM 51-10-2. PNov 28, 2005 · N486FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 05FDEA03946Skin · dentedRIGHT FUSELAGE EXTERNAL SKIN HAS A DENT AT STA BS 414 ON STRINGER STR 25-R. CHECKED DENT AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGE IAW B727 SRM 53-30-3. FABRICATED DOUBLER AND FILLERS IAW B727 SRM 53-30-3. ALODINED AND PRIMED REPAINov 23, 2005 · N486FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 05FDEA03945Web · gougedFOUND L-1 DOOR CUTOUT UPPER WEB IS GOUGED STA 341, WL 282, LBL 50. REPAIRED L1 DOOR CUTOUT UPPER WEB PER SRM 53-10-1.Nov 23, 2005 · N485FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 05FDEA03944Crease Beam · misdrilledCREASE BEAM IB CHORD HAS DOUBLE HOLES BS 848-870 RBL 63 WL 208. REPAIRED CREASE BEAM I/B CHORD AT BS 848-870 RBL 63, WL 208 PER SRM 51-30-2.Nov 23, 2005 · N485FE · Boeing 727227 · Fuselage Main, StructureSDR 05FDEA03943Skin · dentedFOUND BS 423, STR 22-23L, CREASED DENT IN SKIN. REPAIRED SKIN AT BS 423, STR 22-23L PER SRM 53-30-3.Nov 23, 2005 · N485FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR XN0A1278Wire · looseSPEED BRAKE/ FLAP WARNING WILL NOT TEST IN TAXI OUT AND T/O WARNING HORN. SECURED LOOSE WIRE ON AURAL WARN CB. CHECKS GOOD ON GROUND.Nov 23, 2005 · N73751 · Boeing 727227 · Flight Control System WiringSDR 05FDEA03941Skin · corrodedAFT PIT AT STA BS 1012 AT LBL 29 HAS CORROSION ON SKIN. REMOVED EXISTING REPAIR AND DAMAGED SKIN IAW B727 SRM 53-30-3 FIGURE 3A. FABRICATED NEW REPAIR IAW B727 SRM 53-30-3 FIGURE 3A. ALODINED AND PRIMED IAW B727 SRM 51-10-2; AND INSTALLED NEW REPAIR IAW B72Nov 22, 2005 · N486FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 05FDEA03937Flap Track · corrodedRIGHT WING O/B FLAR I/B TRACK AFT MOUNT CENTER BOLT HOLE HAS CORROSION. REPAIRED HOLE IAW BOEING OHM 57-40-01. REMOVED CORROSION FROM BORE IAW BOEING OHM 57-40-01. MAG PARTICLE INSPECTION OF BORE IAW BOEING OHM57-40-01. FABRICATED AND INSTALLED BUSHING INov 22, 2005 · N486FE · Boeing 727227 · Trailing Edge FlapsSDR 05FDEA03936Flap Track · corrodedRIGHT WING INBOARD FLAP OUTBOARD TRACK FORWARD MOUNTING BOLT HOLES, BORES HAVE CORROSION. REAMED HOLES 2 EACH TO REMOVE CORROSION WITHIN LIMITS IAW. BAC OHM 57-40-01 NO CORROSION NOTED. FABRICATED AND CAD PLATED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW OHM Nov 22, 2005 · N486FE · Boeing 727227 · Trailing Edge FlapsSDR 05FDEA03935Flap Track · corrodedLEFT WING INBOARD FLAP TRACK FORWARD AND AFT MOUNTING FLANGES HAVE CORROSION. MACHINED FWD MOUNT PAD TO .250 REMOVING .020 TO REMOVE CORROSION. AFT PAD TO .260 REMOVING .015 TO REMOVE CORROSION IAW BAC OHM 57-40-01 PAGE 411 FIGURE 402. PERFORMED MAG PARTNov 22, 2005 · N486FE · Boeing 727227 · Trailing Edge FlapsSDR 05FDEA03932Frame · dentedFOUND FRAME DENT AT BS 560 ABOVE STR 24L. REPAIRED FRAME AT BS 560 STR 24L IAW SRM 51-40-3.Nov 21, 2005 · N485FE · Boeing 727227 · Fuselage Main, FrameSDR 05FDEA03931Frame · dentedFRAME DENT AT BS 500, ABOVE STR 23L. TRIMED DAMAGE, FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-3.Nov 21, 2005 · N485FE · Boeing 727227 · Fuselage Main, FrameSDR 05FDEA03923Frame · corrodedCORROSION AT FRAME STA BS 480 AT LBL 12, TOP OF FRAME. REMOVED DAMAGED SECTION OF BEAM. FABRICATED "T" CAP REPAIR SECTION, SUPPORT ANGLES, AND REINFORCEMENT STRAPS IAW B727 SRM 53-10-8 FIGURE 3. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALNov 20, 2005 · N496FE · Boeing 727227 · Fuselage Main, Frame
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