Boeing 727-225

Service difficulty reports · 4,226

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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 = '727225'
  ORDER BY difficulty_date DESC"

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SDR 05FDEA03182Floorbeam · corrodedUPPER CHORD FLOORBEAM AT FS 344 LBL 22.5 TO RBL 22.5 CORRODED. REMOVED, FABRICATED AND INSTALLED CHORD AND HAT-CHANNEL IAW FED-EX DRAWING SR-27-53-007 AND B727 SRM 51-30-2.Oct 1, 2005 · N462FE · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL2005742508Support Angle · corrodedAFT PIT BS 1163 WL 25 LBL 25 TO RBL 25 FRAME HAS EXFOLIATED CORROSION. SUPPORT ANGLE FOUND BEYOND LIMITS IAW B727 SRM 53-10-1 FIG 1, 100 PERCENT MATERIAL LOSS. REMOVED SUPPORT ANGLE, FABRICATED AND INSTALLED SUPPORT ANGLE 81 - .375 INCH FROM AND10133-1401 IASep 30, 2005 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR 05FDEA03181Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA. 344 FROM BL 12 L TO BL 12 R. REMOVED CORROSION FROM FLOOORBEAM UPPER CAP IAW FED-EX SRM 53-10- 1. REMOVED, FABRICATED AND INSTALLED SPLICES AND FLOORBEAM IAW SRDM SR27-53-007, B727 SRM 51-10-2,51-30-2.Sep 30, 2005 · N465FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 05FDEA03178Seat Track · corrodedSEAT TRACK LBL 24 HAS 2 SPLICES AND CORROSION STA 380 - STA 480. REMOVED CORROSION, MATERIAL LOSS FOUND OUT OF LIMITS, ORIGINAL THICKNESS .085 MATERIAL REMOVED .029 RAMAINING .056, REMOVED SEAT TRACK. FABRICATED, DRILLED TO FIT, ALODINED, PRIMED AND INSTALLESep 30, 2005 · N465FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 724000012Frame · dentedDENT ON FUSELAGE FRAME FLANGE.Sep 29, 2005 · N724CK · Boeing 727225 · Fuselage Main, FrameSDR 724000011Frame · crackedCRACK IN FUSELAGE FRAME SUPPORT.Sep 29, 2005 · N724CK · Boeing 727225 · Fuselage Main, FrameSDR 724000010Stringer · crackedCRACKS ON STRINGER RIB ATTACHMENT.Sep 29, 2005 · N724CK · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 72400009Stringer · crackedCRACKS ON STRINGER RIB FLANGE.Sep 29, 2005 · N724CK · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 72400008Stringer · crackedCRACKS ON STRINGER RIB ATTACHMENT.Sep 29, 2005 · N724CK · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 05FDEA03146Floorbeam · corrodedCORRODED FLOORBEAM FS 620 FROM LBL 24 - LBL 45 THREE HEAVY AREAS. REMOVED, FABRICATED, ALODINED, PRIMED, HEAT TREATED, CAD PLATED AND INSTALLED FLOORBEAM REPAIR AT STA 620 FROM LBL24-45 ALL IAW FX DWG SR27-53-034E REPAIR NR 4 B727SRM 51-10-2,BAC5619H AND ASep 27, 2005 · N465FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 05FDEA03080Skin · tornLEFT WING OUTBORD FORE FLAP UPPER SKIN SECTION MISSING (HONEYCOMB EXPOSED) REFERENCE FEDEX NSRM N00007. ORDERED AND RECEIVED LEFT OUTBORD FORE FLAP. INSTALLATION, ADJUSTMENT AND OPERATIONAL CHECK WAS ACCOMPLISHED ON FEDEX NSRM N00079 IAW B727-200 MM 27-51-0Sep 24, 2005 · N464FE · Boeing 727225 · Trailing Edge FlapsSDR DHL2005742528Hinge · nickedRT AILERON O/B HINGE FITTING O/B SIDE (ON WING) FITTING NICKED AND GOUGED AROUND BUSHING. BLENDED GOUGE FOUND OUT OF LIMITS IAW BOEING DRAWING 65-19259-8. DRILLED, DEBURRED AND INSTALLED NEW FITTING, P/N 65-19259-6 IAW B727 SRM 51-30-2.Sep 23, 2005 · N742DH · Boeing 727225 · AileronsSDR 05FDEA03078Doubler · corrodedCORRSION FWD PIT BETWEEN STA 720D AND STA 720E INTERIOR SKIN BETWEEN STR 29L AND STR 29R. REMOVED CORROSION ORIG MAT .100 MAT REM .053 FAB PARTS, LOCATED AND DRILL ALODINE AND PRIME PARTS IAW B727 SRM 53-30-1, 51-10-6, 53-30-3, 53-30-2, 51-10-2, 51-20-1, FIG Sep 23, 2005 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 05FDEA03077Doubler · corrodedCORRSION FWD PIT BETWEEN STA 720D AND STA720E INTERIOR SKIN BETWEEN STR 29L AND STR 29R. REMOVED CORROSION ORIG MAT .100 MAT REM .053 FAB PARTS, LOCATED AND DRILL ALODINE AND PRIME PARTS IAW B727 SRM 53-30-1, 51-10-6, 53-30-3, 53-30-2, 51-10-2, 51-20-1, FIG 2Sep 23, 2005 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 05FDEA03066Doubler · corrodedCORROSION FWD PIT BETWEEN STA 720E AND STA 720F INTERIOR SKIN BETWEEN STRINGER 29R AND STRINGER 28R. REMOVED CORROSION FOUND OUT OF LIMITS ORIG MAT .100 MAT. REMAINING .038, REMOVED DAMAGE, FABBED REPAIR DBLR. LOCATED AND DRILLED, ALODINED, PRIMED, INSTALLSep 22, 2005 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 05FDEA03065Intercostal · crackedAFT PIT INTERCOSTAL AT STA 950B STRINGER 28R IS CRACKED. REMOVED AND REPLACED INTERCOSTAL AT FS 950B, STRINGER 28R, IAW B727 SRM 51-30-2, IAW B727 MM 51-20-013-7.Sep 22, 2005 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 05FDEA03064Skin · misrepairedEXTERNAL SKIN DOUBLER AT STA 950B STRINGER 28R REQUIRES EVALUATION. REMOVED IMPROPERLY INSTALLED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW B727 SRM 53-30-3, 51-10-2, 51-30-2, 53-30-2.Sep 22, 2005 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 05FDEA03063Seat Track · corrodedSEAT TRACK INBOARD FLANGE HAS CORROSION BS 700 TO BS 740 LBL 24.Sep 22, 2005 · N465FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03062Skin · misrepairedEXTERNAL SKIN DOUBLER AT STA 715-720A AND STRINGER 28R REQUIRES EVALUATION. DOUBLER FOUND TO NOT CONFORM TO SRM STANDARDS. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW DOUBLER AT STA 715 TO 720A BEWEEN STRINGERS 27R AND 28R ALL C/W IAW FX B727 SSep 22, 2005 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 72400005Frame · crackedA 1 INCH CRACK ON FUSELAGE FRAME.Sep 21, 2005 · N724CK · Boeing 727225 · Fuselage Main, FrameSDR 72400004Structure · corrodedCORROSION ON DOOR OPENING REINFORCEMENT.Sep 20, 2005 · N724CK · Boeing 727225 · Passenger/Crew DoorsSDR DHL2005742527Seat Track · gougedSEAT TRACK GOUGED AT BS 1018 LBL 45 (OUTBD TRACK). REMOVED GOUGED SECTION OF TRACK, FABRICATED AND INSTALLED SEAT TRACK 80" FROM 7178T6511 IAW B727 SRM 51-10-6, 51-10-01, 51-30-2, 53-10-5 FIG 1 DRAWING 66-1573.Sep 18, 2005 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005742515Seat Track · gougedS/O 284002 N/R 037550 SEAT TRACK GOUGED AT BS 878 LBL 45. REMOVED FLOOR PANELS AT BS 870 - 950 LBL 24 - 60 IAW SRM 51-30-2. REMOVED GOUGED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK 91.00 INCHES X 1.80 INCH FROM 7178-T6511 IAW SRM 53-10-1 FIG. 3 AND 5Sep 18, 2005 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005742505Seat Track · gougedSEAT TRACK GOUGED AT BS 720B + 15 LBL 45. REMOVED SEAT TRACK, FABRICATED AND INSTALLED SEAT TRACK 130 - .5 INCH FABRICATED FROM 7178-T6511 IAW B727 SRM 51-30-2.Sep 18, 2005 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005742504Seat Track · gougedSEAT TRACK GOUGED AT BS 804 LBL 45 (O/B TRACK). REMOVED SEAT TRACK, FABRICATED AND INSTALLED SEAT TRACK 130 - .5 INCH FABRICATED FROM 7178-T6511 IAW B727 SRM 51-30-2.Sep 18, 2005 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005742503Seat Track · gougedSEAT TRACK GOUGED AT BS 950E+5 LBL 45 (O/B TRACK). REMOVED SEAT TRACK, FABRICATED AND INSTALLED SEAT TRACK 130 -.875 INCH FROM 7178-T6511 IAW B727 SRM 51-30-2.Sep 18, 2005 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005742513Shear Tie · corrodedS/O 284002 N/R 037490 FWD PIT FUSELAGE FRAME AT BS 720 BETWEEN STR 28L AND STR 28R HAS AN (L) ANGLE WHICH ATTACHES TO THE FUSELAGE SKIN CORRODED IN MULTIPLE AREAS. REMOVED CORROSION BETWEEN STR 28L AND 28R BS 720. FOUND SHEAR TIE TO BE OUT OF LIMITS IAW SRM 5Sep 17, 2005 · N742DH · Boeing 727225 · Fuselage Internal Mounting StructureSDR DHL2005742516Frame · corrodedBS 1070 LBL 65 WL 255 FRAME JUST AFT OF L-2 DOOR HAS A CORROSION BULGE. CUT OUT CORROSION ON FORMED WEB ANGLE ATTACHED TO FRAME AT BS 1070 LBL 65 AFT DOOR CUT OUT AT L-2 DOOR IAW SRM 51-40-3 FIG. 1. REMOVED (T) ANGLE, FABRICATED AND INSTALLED NEW ANGLE 2.75 ISep 17, 2005 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2005742507Web · crackedRT BL 65 WEB CRACKED BEHIND GILL LINER BS 720D + 10. REMOVED GILL LINER SUPPORT ANGLE, FABRICATED AND INSTALLED 2 EACH REPAIR ANGLES 32 INCHES AND 33 INCHES AND 1 EACH DOUBLER 36 - .5 X 16 INCHES FROM 2024-T3 .025 IAW B727 SRM 51-40-2 AND 51-30-2.Sep 17, 2005 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR 05FDEA02981Fairing · corrodedRIGHT WING TO BODY FAIRING NR 3437 HAS CORROSION (EXFOLIATED). REMOVED ANGLE IAW B727 SRM 51-30-2. FABRICATED ANGLE IAW BAC DRAWING 65-25582. ALODINED AND PRIMED ANGLE IAW B727 SRM 51-10-2. INSTALLED ANGLE IAW B727 SRM 51-30-2. REMOVED TEE CHORD IAW B727 Sep 17, 2005 · N464FE · Boeing 727225 · Aerodynamic FairingsSDR DHL2005742526Skin · chafedRT WING O/B MID FLAP CHAFFED EXISTING REPAIR I/B TOP. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED FORMED ANGLE REPAIR 7" BY 2.30" BY .75" FROM 2024-T3 .063 IAW B727 SRM 57-20-2 FIG 5, 51-20-1 PARA 7, 51-30-6 FIG 3 51-10-2, 51-40-3 FIG 1 AND 51-30-2 PARSep 16, 2005 · N742DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005742525Shear Tie · corrodedCORROSION ON BS 1130 BETWEEN STR. 27L - STR. 26R. FABRICATED AND INSTALLED SHEAR TIE 5-1/2" BY 3" FROM 7075-T6 .080 IAW B727 SRM 51-10-2, AND 51-30-2.Sep 16, 2005 · N742DH · Boeing 727225 · Fuselage Internal Mounting StructureSDR DHL2005742524Skin · debondedLT I/B AFT FLAP HAS AREA OF DISBOND NEAR I/B END. FABRICATED AND INSTALLED DOUBLER REPAIRS 8.2" BY 7.5" AND 5.2" BY 4.5" FROM 2024-T3 .016 AND 5.1" BY 4.4" FROM BMS 4.4 HONEYCOMB IAW B727 SRM 51-40-20, 51-40-23 AND 57-50-2 NOTE G.Sep 16, 2005 · N742DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005742523Skin · dentedLT I/B FORE FLAP L/E NEAR CENTER HAS DENTS IN SKIN. REMOVED DENTED SKIN. FABRICATED AND INSTALLED REPAIR SKIN 8" BY 8" FROM 2024-T3 .040 IAW B727 SRM 51-10-1 AND 51-30-2.Sep 16, 2005 · N742DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005742522Skin · chafedLT O/B MID FLAP I/B END L/E CUT AND CHAFED. REMOVED DOUBLER IAW B727 SRM 51-10-1 AND 51-30-2. FABRICATED AND INSTALLED DOUBLER REPAIR 7" BY 6.0" BY 3.2" FROM 2024-T3 .040 IAW B727 SRM 51-10-2, 57-50-4.Sep 16, 2005 · N742DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005742512Nut Plate · misinstalledNUT PLATES IMPROPERLY INSTALLED ON FLOOR SUPPORT BETWEEN BS 1070 - BS 1130 STR. 30 (ABOVE) REMOVED DAMAGED FLOOR SUPPORT BETWEEN BS 1070 - 1130. CUT AND FABRICATED NEW SUPPORT 13INCHES FROM BAC1490-2583 AND SPLICES 12 INCHES X 1INCH X 1INCH FROM AND10133-0702Sep 16, 2005 · N742DH · Boeing 727225 · Fuselage Main, Attach FittingsSDR DHL2005742514Skin · gougedRT OB FORE FLAP LEADING EDGE HAS 2 EACH GOUGES ABOUT 12 INCHES OB OF IB EDGE. FABRICATED AND INSTALLED REPAIR DOUBLER 8 INCHES X 3 INCHES FROM 024-T3 .050 FOR RT OB FORE FLAP LEADING EDGE IAW 57-50-4, 51-30-2 AND 51-10-2.Sep 16, 2005 · N742DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005742501Skin · damagedLEFT O/B FLAP I/B END LEADING EDGE GROOVED AND CHAFED. FABRICATED EXTERNAL REPAIR 4 X 4 INCHES FROM 2024-T3 .050. LOCATED, DRILLED, DEBURRED IAW B727 SRM 57-50-4, ALODINED AND PRIMED REPAIR IAW B727 SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2 Sep 16, 2005 · N742DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005748752Channel · looseNR 1 SLAT HAS PLAY AT ACTUATOR TO SLAT ATTACH POINT. REMOVED CHANNEL AND BUSHINGS IAW B727 SRM 51-30-2. LOCATED AND DRILLED NEW CHANNEL P/N 65-17327-7 PO NR 5070637 IAW B727 SRM 51-40-5. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED NEW CHANNEL Sep 16, 2005 · N748DH · Boeing 727225 · Leading Edge DevicesSDR 05FDEA02930Stringer Clip · corrodedCORROSION FWD PIT A/C PLENUM AREA FRAME STA 720E BILGE AREA BETWEEN STRINGER 29R AND STRINGER 28R. REMOVED CORROSION IAW FX B727 SRM 51-10-6. FOUND BEYOND LIMITS IAW FX B727 SRM 53-10-1. REMOVED DAMAGED SECTION IAW FX B727 SRM 51-40-3. FAB REPAIR ANGLE IAWSep 15, 2005 · N464FE · Boeing 727225 · Fuselage Main, Attach FittingsSDR DHL2005742520Window Frame · crackedPILOT'S NR 2 WINDOW AFT LOWER INTERNAL CORNER ANGLE CRACKED AND CORRODED. REMOVED FITTING P/N 69-367305, FABRICATED SHIMS IAW EA NR AA15-53-1 REV. IR, DRILLED UP FITTING IAW SRM 51-30-2. INSTALLED FITTING IAW SRM 51-30-2, HEAT CHECK IAW MM 56-12-11 STEP.Sep 14, 2005 · N742DH · Boeing 727225 · Fuselage Main, StructureSDR 05FDEA02896Stringer · dentedFABRICATE AND INSTALL STRINGER REPAIR AT BODY STATION 500 AND S21R. REMOVED, FABRICATED AND INSTALLED STRINGER CHANNEL IAW FX B727-200 SRM 53-10-3. ALODINED AND PRIMED IAW FX B727-200 SRM 51-10-2.Sep 14, 2005 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 05FDEA02894Skin · dentedFUSELAGE SKIN DENTED BS 370 BETWEEN STR 3-R AND STR 6-R.Sep 14, 2005 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 05FDEA02890Door Frame · crackedL1 DOOR CUT-OUT UPPER HINGE CAVITY, FRAME IS CRACKED AROUND HOLE.Sep 14, 2005 · N464FE · Boeing 727225 · Fuselage Main, StructureSDR 05FDEA02889Skin · crackedPREVIOUS REPAIR,SKIN CUT-OUT APPEARS TO HAVE CRACK STA 500 S20R AND S21R. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS IAW B727 SRM 51-30-2, 53-30-30 FIG 3.Sep 14, 2005 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 05FDEA02885Stringer · puncturedSTA 480 SR20R HAS PUNCTURE ON LOWER SIDE. REMOVED DAMAGE ON STRINGER/DYE PENETRANT INSPECTION IAW B727 SRM 53-10-3 FIG 2, NO CRACKS NOTED. FABRICATED AND INSTALLED 3 EACH STRINGER TIES IAW B727 SRM 51-30-2 AND BAC DRAWING NR 66-11809. REMOVED AND REINSTALLESep 14, 2005 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2005742511Skin · dentedRIGHT FWD LOWER HALF OF FUSELAGE EXTERIOR SKIN HAS DENT STA 947 BELOW STRINGER 27R. FOUND A=1.100 Y + .028 = 39 NOT IN LIMITS IAW B727 SRM 53-30-1. REMOVED WEB, CUT OUT DENT, FABRICATED AND INSTALLED REPAIR DOUBLER 9.5 X 7.5 INCHES FROM 20240-T3 .050 IAW B72Sep 13, 2005 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2005748751Floorbeam · corrodedFLOORBEAM AT BS 1166 RBL 36 HAS HEAVY EXFOLIATION ON UPPER FLANGE. CUT OUT DAMAGED AREA OF TOP AFT FLANGE OF FLOORBEAM 4.6 BY 1.0 AT STA 1166 RBL 36 IAW B727 SRM 53-10-8 FIG 8. FAB REPAIR SUPPORT ANGLES FROM 7075T6 PO NR 9001487 22.0 BY 6.0 AND 15.2 BY 6.0 ISep 10, 2005 · N748DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL2005748750Skin · dentedL/WING I/B AFT FLAP HAS DENT ON UPPER SURFACE I/B END. CUT OUT DENTED AREA ON LT IMB AFT FLAP APPROX 2" DIA FAB FILLER APPROX 2" DIA AND DOUBLER APPROX 5" DIA FROM .012 2024 T3 PO NR 900534 BONDED FILLER AND DOUBLER CURED CLEANED PRIMED AND EALED IAW B727 SRMSep 8, 2005 · N748DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005748748Frame · damagedBENT FRAME ABOVE STR 17R AT BS 0. CUT OUT DAMAGED AREA OF FRAME 1 BY 1.5 FAB REPAIR CHANNEL 8 1/2 X 2 1/2 7075 T6 PO 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 51-10-2. INSTALLED NEW CHANNEL FRAME REPAIR B727 SRM 53-10Sep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, Frame
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