Boeing 727-232

Service difficulty reports · 6,539

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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 = '727232'
  ORDER BY difficulty_date DESC"

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SDR DL72S982053Rib · crackedINBOARD AFT CLOSE OUT RIB CRACKED AT LWR AFT CORNER. DAMAG REPAIRED PER MM 57-52-0 ON SHOP ORDER 582612.Sep 29, 1998 · N407DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982015Angle · crackedREF TPA LETTER CHECK D-1, SUPPORT ANGLE CRACKED AT LWR FWD SIDE OF NR 8 SPOILER ACTUATOR SUPPORT FITTING. INSTALLED DOUBLER PER M/M 57-20-22.Sep 29, 1998 · N540DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S982114Track · corrodedBUSH FWD ATTACH LUG AND REPAIR MLG BEAM ATTACH HOLES PER SB 727-57-0178, EXCEPT INCREASE HOLE DIA TO .847.Sep 28, 1998 · N401DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982113Track · corrodedTYPICAL CORROSION FOUND IN MLG BEAM ATTACH HOLES. REPAIRED SIMILAR TO SB 727-57-0178 EXCEPT TO OS HOLES, .838 MAX DIAMETER TO REMOVE ALL CORROSION.Sep 28, 1998 · N401DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981995Battery Pack · dischargedLT OVERWING EXIT DOOR(S), EMERGENCY LIGHTS INOP. REPLACED LT OVERWING EXIT DOOR(S) BATTERY PACK, SYSTEM OPS. NORMAL PER MM.Sep 27, 1998 · N475DA · Boeing 727232 · Emergency LightingSDR DL72S981992Power Supply · inoperativeDURING L/O, FOUND FLOOR TRACK LIGHTS FROM SEAT 27-36 INOP. REPLACED EMERGENCY LIGHTS PWR SUPPLY DAL (P/N 337701962) (S/N 0474) OFF, (S/N 1881) ON.Sep 26, 1998 · N517DA · Boeing 727232 · Emergency LightingSDR DL72S981998Pin · corrodedBORE CORRODED LEFT AFT BTL PIN IS CORRODED. CLEANED CORROSION PER SRM 53-40-1 FIG 4 DAMAGE WITHIN LIMITS OK TO TREAT. TREATED BORE PER PS 900-2-4-1 NO O2.Sep 25, 1998 · N407DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981987Frame · crackedA CRACK WAS FOUND IN THE FS 761 RT FRAME DURING ACCOMPLISHMENT OF S/B 727-53-0197. THE CRACK IS TYPICAL OF THAT SHOWN IN SUBJECT S/B AND IS DUE TO FATIGUE. REPAIRED PER ERA 332248-14AD.Sep 25, 1998 · N409DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S981976Panel · delaminatedFOUND ON A1 LETTER CK, NR 1 SPOILER PANEL DELAMINATED. REPAIRED PER SRM 57-50-6.Sep 24, 1998 · N477DA · Boeing 727232 · SpoilersSDR DL72S982218Angle · crackedDURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 21 AND 34 FR OM IB END OF FLAP. THE ANGLE WAS REPAIRED BY SPLICING IN A NE W SECTION OF ANGLEPER MM 57-52-0, FIG. 802.Sep 23, 1998 · N407DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982060Support · wornITEM: NR 2 ENG FWD COWL SUPPORT RING IS WORN AT THE 9 O'CLOCK POS LOC ON FUSELAGE. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER PER M/M 53-11-0 PG 801. OK TO INSTALL. INSTALLED REPAIR PER M/M 53-11-0 PG 801.Sep 23, 1998 · N407DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L981973Trim · out of positionA/C UNABLE TO PRESSURIZE. FOUND A PIECE OF INTERIOR TRIM BETWEEN DOOR SEAL AND A/C FRAME. REPOSITIONED TRIM, ALL OPS NORMAL.Sep 23, 1998 · N506DA · Boeing 727232 · Passenger Compartment EquipmentSDR DL72S981967Angle · crackedNR 6 L/E FLAP ACT ATTACH ANGLE CRACKED O/B LOWER RADIUS. REPAIRED PER MM 57-20-21 PG 811.Sep 22, 1998 · N517DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L982003Floorbeam · corrodedFLOORBEAM CAP CORRODED STA 344 LBL 40 TO 48. REPAIRED PER 272 SRM 53-10-8.Sep 22, 1998 · N508DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72L981978Fitting · wornFITTING WORN ON LT AFT SERVICE DOOR AFT LOWER EDGE OF DOOR. C/W MM 52-14-0 FIG 805.Sep 22, 1998 · N508DA · Boeing 727232 · Service DoorsSDR CALA9801852Fitting · corrodedINSPECTION FOUND RT WING NR 6 FLAP TRACK FORWARD ATTACH FITTING CORRODED. THE FLAP TRACK FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.Sep 22, 1998 · N14788 · Boeing 727232 · Trailing Edge FlapsSDR CALA9801851Skin · lightning strikeINSPECTION FOUND LIGHTNING STRIKE DAMAGE TO STATIC PORT SKIN ON RT FUSELAGE FORWARD OF FORWARD PIT DOOR AT STA 500. THE DAMAGE WAS REPAIRED IAW SRM 53-30-03.Sep 22, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S982321Angle · crackedDURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED 34 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0 FIG 802.Sep 21, 1998 · N409DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982320Angle · crackedDURING SHOP INSP, THE AFT CHORD ANGLE WAS FOUND CRACKED 33 INCHES FROM IB END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 809 BY INSTALLING A DOUBLER.Sep 21, 1998 · N409DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982319Angle · crackedDURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED 33 INCHES FROM O/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A DOUBLER.Sep 21, 1998 · N409DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L981963Wire · brokenWHEN LANDING GEAR WAS LOWERED THE RLG GREEN DOWN AND LOCKED DIDN'T ILUMINATE. LIGHT DIDN'T PRESS TO TEST. CHANGED BULBS, NO HELP. WENT TO BRIGHT ON BRIGHT/DIM SWITCH AND INDICATION WERE NORMAL. SECURED WIRE ON BACK OF BRIGHT/DIM SWITCH, OPS CHECK NORMAL.Sep 21, 1998 · N510DA · Boeing 727232 · Landing Gear System WiringSDR CALA9801847Floorbeam · corrodedINSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT BS 1166, RBL 50 TO RBL 66. THE CORROSION WAS REMOVED AND A REPAIR STRAP WAS INSTALLED IAW SRM 51-30-5, 51-10-2, 51-30-2, AND ECRA 5321-01029.Sep 21, 1998 · N14788 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9801846Wire · brokenINSPECTION FOUND R-1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE AT LIGHT ASSEMBLY.Sep 21, 1998 · N15790 · Boeing 727232 · Light System WiringSDR CALA9801845Skin · corrodedINSPECTION FOUND THE RT WING INBOARD MIDFLAP CORRODED AROUND TWO RIVETS ON UPPER SURFACE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-1.Sep 21, 1998 · N15790 · Boeing 727232 · Trailing Edge FlapsSDR CALA9801844Skin · corrodedINSPECTION FOUND NR 5 SPOILER CORRODED ALONG TOP EDGES. THE NR 5 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.Sep 21, 1998 · N15790 · Boeing 727232 · SpoilersSDR CALA9801843Skin · delaminatedINSPECTION FOUND THE NR 2 SPOILER DELAMINATED AFT OF INBOARD HINGE. THE NR 2 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.Sep 21, 1998 · N15790 · Boeing 727232 · SpoilersSDR CALA9801842Skin · delaminatedINSPECTION FOUND RT WING INBOARD TRAILING EDGE AFT FLAP DELAMINATED AT OUTBOARD AND INBOARD TRAILING EDGE CORNER. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-1.Sep 21, 1998 · N15790 · Boeing 727232 · Trailing Edge FlapsSDR CALA9801841Skin · delaminatedINSPECTION FOUND NR 7 SPOILER DELAMINATED AT LOWER OUTBOARD AFT TRAILING EDGE. THE NR 7 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.Sep 21, 1998 · N15790 · Boeing 727232 · SpoilersSDR CALA9801840Skin · delaminatedINSPECTION FOUND LT OUTBOARD AFT FLAP OUTBOARD LOWER CORNER DELAMINATED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-61-12.Sep 21, 1998 · N15790 · Boeing 727232 · Trailing Edge FlapsSDR CALA9801839Skin · corrodedINSPECTION FOUND NR 1 SPOILER CORRODED ALONG OUTBOARD EDGE AND DELAMINATED ON TOP. THE NR 1 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.Sep 21, 1998 · N15790 · Boeing 727232 · SpoilersSDR CALA9801835Angle · corrodedINSPECTION FOUND NOSE RADOME AREA LOWER L-ANGLE CORRODED AT FS 178, LBL 6 TO RBL 6. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2 AND MM 51-20-0.Sep 21, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801834Splice · corrodedINSPECTION FOUND LT FORWARD CARGO BUTT SPLICE NR 6 AND BUTT SPLICE AT BS 720 TO 730 CORRODED. NEW BUTT SPLICES WERE INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-10-2, MM 51-20-11.Sep 20, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801833Seat Track · corrodedINSPECTION FOUND RT SEAT TRACK CORRODED AT STA 1132-113 TO , RBL 48. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-5, FIGURE 7, 51-30-5, 51-10-2, 53-10-4, AND MM 51-20-11.Sep 20, 1998 · N14788 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801832Angle · corrodedINSPECTION FOUND ANGLE CORRODED BELOW FORWARD FLIGHT ATTENDANT'S SEAT AT STA 303.9 FROM LBL 12 TO LBL 50. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-30-5, 53-10-2, AND MM 51-20-11.Sep 20, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801830Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING NR 5 SLAT INBOARD AND OUTBOARD RIBS AT ACTUATOR ROD END ATTACH POINT. BOTH THE INBOARD AND OUTBOARD RIBS WERE REMOVED AND REPLACED IAW SRM 51-30-2.Sep 19, 1998 · N14788 · Boeing 727232 · Leading Edge DevicesSDR CALA9801829Floor · corrodedINSPECTION FOUND COCKPIT LT SIDE FLOOR PANEL CORRODED. A NEW FLOOR PANEL WAS INSTALLED IAW SRM ECRA 5320-01448.Sep 19, 1998 · N14788 · Boeing 727232 · Fuselage Floor PanelSDR CALA9801827Frame · crackedINSPECTION FOUND C-3 CARGO DOOR CUTOUT FORWARD FRAME LOWER CORNER CRACKED OUT OF BOTTOM STOP FITTING UPPER INBOARD BOLT HOLE AND LOWER PART OF FRAME WAS CORRODED. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-3. THE CRACK WAS 1.Sep 19, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801826Fitting · corrodedINSPECTION FOUND TOP OF VERTICAL STABILIZER LT HORIZONTAL HINGE ATTACH FITTINGS CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-4, AND ECRA 5550-01033.Sep 19, 1998 · N14788 · Boeing 727232 · Vertical StabilizerSDR CALA9801825Stringer · crackedINSPECTION FOUND A 4 INCH CRACK IN STRINGER 14L AT STA 900. THE CRACKED SECTION OF STRINGER WAS REPLACED IAW SRM 51-30-2.Sep 19, 1998 · N14788 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9801824Web · corrodedINSPECTION FOUND RT AFT LAV FLOOR WEB CORRODED VANITY PLUMBING FITTING. THE FLOOR WEB WAS REMOVED, A NEW LAV FLOOR WEB, DOUBLER, AND FILLER WERE INSTALLED IAW SRM 51-40-2, 51-30-2, 51-10-2 AND MM 51-20-11.Sep 19, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S982135Spar · crackedLWR AFT SPAR RAIL CRACKED TWO PLACES AT I/B DRIVE ROD CUTOUT. REPAIRED PER MM 57-52-0 FIG 802.Sep 18, 1998 · N409DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981959Skin · crackedTHE R1 DOOR SURROUND SKIN ASSY WAS FOUND WITH A 2.25 INCH TYPICAL CRACK IN THE BEAR STRAP AT THE UPPER HINGE CUTOUT. THE CRACK WAS REPAIRED PER BAC S/B 727-53-0136, REV 3. THE REPAIR WAS DOCUMENTED PER ER/A 365667-14. NOTE: THE BEAR STRAP HAD THE S/B 53-01Sep 18, 1998 · N499DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9801823Press Panel · crackedINSPECTION FOUND A .1875 INCH CRACK IN NLG RT SIDE PRESSURE PANEL OUT OF FASTENER HOLE AT BS 271, WL 185. THE EXISTING DOUBLER WAS REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 6A. A DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-2Sep 18, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801822Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1130, RBL 26 TO RBL 34 AND LBL 62. THE FLOORBEAM AREAS WERE REPAIRED IAW ECRA 5321-01028 AND ECRA 5321-01027.Sep 18, 1998 · N14788 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9801821Frame · corrodedINSPECTION FOUND SIDE WALL SUPPORT FRAME CORRODED AT STA 720D ABOVE STRINGER 26R. THE CORRODED SECTION OF SUPPORT FRAME WAS REMOVED. A REPAIR ANGLE AND DOUBLER WERE INSTALLED IAW SRM 51-40-3, 51-10-2, 51-50-2 AND MM 51-20-11.Sep 18, 1998 · N14788 · Boeing 727232 · Fuselage Main, FrameSDR CALA9801820Channel · crackedINSPECTION FOUND C-1 CARGO DOOR UNDER LOWER LIGHT HAD A PIECE OF PAN CRACKED OUT. THE PAN CHANNEL WAS REMOVED, A REPAIR WAS INSTALLED IAW SRM 52-30-1, 51-10-2, 51-30-2 AND MM 51-20-12.Sep 18, 1998 · N14788 · Boeing 727232 · Cargo/Baggage DoorsSDR CALA9801819Angle · crackedINSPECTION FOUND 8 INCH CRACK IN L-ANGLE AT STA 1166, STRINGER 26L TO 26R. THE ANGLE WAS REMOVED, A REPAIR ANGLE, NUT PLATES, AND RADIUS BLOCK WERE INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2 AND MM 51-20-11.Sep 18, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801818Panel · crackedINSPECTION FOUND A .5 INCH CRACK IN PANEL NR 3338. THE CRACKED AREA WAS CUT OUT, A WEB AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-20-1, 51-30-2, 51-10-2 AND MM 51-20-11.Sep 18, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9801817Chord · corrodedINSPECTION FOUND LT UPPER CHORD CORRODED INSIDE NOSE WHEEL WELL AT STA 292, LBL 20. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-30-2.Sep 18, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801816Stiffener · crackedINSPECTION FOUND A .5 INCH CRACK IN NOSE WHEEL WELL STIFFENER AT STA 234, LBL 20. THE STIFFENER WAS REPAIRED IAW SRM 51-10-2.Sep 18, 1998 · N15790 · Boeing 727232 · Fuselage Miscellaneous Structure
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