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 95FDEA01267Frame · gougedFWD, FRAME DENTED AND GOUGED ON TOP BS 720C AT STR 23 TO 24R. GOUGE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED FRAME AT BS 720C STR 23 TO 24R, PER SRM 51-40-3.Sep 8, 1995 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01266Skin Support · corrodedFWD BAY, FOUND CORROSION WHILE WORKING NR O858 FUSELAGE 00117 SKIN SUPPORT (P/N 69-43695-1), OF BS 740 WL 145 TO 150 BETWEEN STR 28 AND 27L. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SKIN SUPPORT IAW SRM 51-10-1, 53-10-1.Sep 8, 1995 · N499FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 95FDEA01265Web · cracked1303 WEB IN BAY NR 1 AT VERTICAL FIN IS CRACKED LT LOWER CORNER. REPAIRED CRACK AT 1303 WEB IN BAY NR 1 OF VERTICAL FIN LT LOWER CORNER, PER FEDEX DRAWING SR 27-53-015.Sep 8, 1995 · N499FE · Boeing 727232 · Vertical StabilizerSDR DL72S953636Angle · crackedNR 6 SLAT, .25 INCH CRACK AT FASTENER HOLE IN ATTACH ANGLE AFT OF RIB, 6 INCHES O/B OF TAI DUCT. REPAIRED PER MM 57-54-0 FIG 805A.Sep 7, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR CAL950799Actuator · leakingCUN - FLT 0774 - THE A-HYDRAULIC SYSTEM QUANTITY BEGAN TO SLOWLY DECREASE WHILE EN ROUTE FROM IAH TO SJO. 'ABNORMAL' PROCEDURES WERE FOLLOWED AND THE A-HYDRAULIC SYSTEM WAS STABILIZED WITH BOTH A-PUMPS OFF. THE AIRCRAFT WAS DIVERTED TO CUN WHERE IT LANDED WISep 7, 1995 · N17779 · Boeing 727232 · Landing Gear Door ActuatorSDR DL72S954234Rib · crackedDURING A ROUTINE SHOP INSPECTION, NR 8596 WAS WRITTEN FOR A CRACK IN THE 3RD RIB FROM I/B EDGE OF THE NR 2 SLAT. THE CRACK WAS REPAIRED PER M/M 57-54-0 FIG 819.Sep 6, 1995 · N401DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954233Rib · crackedDURING A ROUTING SHOP INSPECTION, NR 8598 WAS WRITTEN FOR A CRACK IN THE 17TH RIB FROM I/B EDGE OF THE NR 2 SLAT. THE CRACK WAS REPAIRED PER M/M 57-54-0 FIG 819.Sep 6, 1995 · N401DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954232Rib · crackedDURING A ROUTINE SHOP INSPECTION, NR CARD 8598 WAS WRITTEN FOR A CRACK IN THE 15TH RIB FROM I/B EDGE OF THE NR 2 SLAT. THE CRACK WAS REPAIRED PER M/M 57-54-0 FIG 805.Sep 6, 1995 · N401DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953839Cowl · wornDURING HMV, NR 2 ENGINE RT AFT COWL PANEL WAS FOUND WITH TOP SIDE SKIN RIVETS ALONG LONGERON ARE SHORT OF EDGE DISTANCE. ALSO, TOP EDGE OF COWL IS WORN. REPAIRED PER SRM 54-10-3 FIG 6.Sep 6, 1995 · N544DA · Boeing 727232 · Engine Cowling SystemSDR DL72S953785Skin · crackedDURING HMV INSPECTION, FOUND NR 2 MIDFLAP WAS FOUND TO HAVE COVE SKIN CRACKED AT I/B ACTUATOR CUTOUT. REPAIRED PER M/M 57-52-0 PAGE 819.Sep 6, 1995 · N515DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S953784Doubler · crackedDURING HMV INSPECTION, THE NR 2 MIDFLAP WAS FOUND CRACKED AFT SPAR RAIL REPAIR DOUBLER AT ACTUATOR CUTOUT. REPAIRED PER M/M 57-52-0, CRACKED AT 21 INCHES AND 56 INCHES FROM I/B END.Sep 6, 1995 · N515DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S953740Skin · damagedDURING SHOP INSPECTION, NR 4 MID-FLAP WAS FOUND WITH WEAR DAMAGE TO LEADING EDGE SKIN, AT THE OUTBOARD 9 OF FLAP. REPAIRED PER MM 57-52-0, FIG 803.Sep 6, 1995 · N515DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S953669Rib · crackedNR 1 SLAT I/B TRACK I/B RIB CRACKED. DRILLED DOUBLER AND INSTALLED PER M/M 57-54-0 PG 806 AND 807.Sep 6, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953643Rib · crackedDURING SHOP INSPECTION, THE 4TH RIB FOR I/B END WAS FOUND CRACKED. THE RIB WAS REPAIRED PER SRM 57-54-00. THE LOWER COVE PANEL ATTACH ANGLE UNDERNEATH THE I/B UPSTOP WAS FOUND TO HAVE A CRACK. THE ANGLE WAS REPAIRED PER SRM 57-54-0 FIG 812, FOR NR 2 L/E SLASep 6, 1995 · N419DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953633Rib · crackedDURING HMV, FOUND NR 1 SLAT WITH CRACKED RIB AT TRACK ATTACH AREA. REPAIRED PER MM 57-40-0 PG 806 AND 807.Sep 6, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR 95FDEA01287Frame · dentedFWD BAY, FRAME DENTED AT BS 720C BETWEEN STR 25 TO 24L. REPAIRED DENTED FRAME AT BS 720C BETWEEN STR 24 TO 25L PER FEDEX SRM 51-40-3.Sep 6, 1995 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01286Frame · dentedFWD BAY, FRAME DENTED ON TOP AT BS 600 BETWEEN STR 26 TO 23L. ALSO, FACTORY SPLICE IS DENTED. REPAIRED FRAME AT BS 600 BETWEEN STR 26 TO 23L PER FEDEX SRM 51-40-3.Sep 6, 1995 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01285Clip · corrodedCORROSION STR CLIP BS 1166 STR 15L. REMOVED CORRODED STR CLIP AT BS 1166 STR 15L AND INSTALLED NEW STR CLIP AT BS 1166 STR 15L IAW FEDEX SRM 51-30-2.Sep 6, 1995 · N499FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 95FDEA01284Seat Track · corrosionFOUND CORROSION IN SEAT TRACK AT BS 480 TO 600 WL 208.5 BL 0. REMOVED CORRODED SEAT TRACK AT BS 480 TO 600 BL 0 WL 208.5. FABRICATED NEW SEAT TRACK AND INSTALLED AT BS 480 TO 600 BL 0 WL 208.5, REF FEDEX SRM 53-10-5.Sep 6, 1995 · N499FE · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA01264Frame · dentedFWD BAY, FRAME DENTED AT BS 720C BETWEEN STR 25 TO 24L. REPAIRED DENTED FRAME AT BS 720C BETWEEN STR 24 TO 25L PER FEDEX SRM 51-40-3.Sep 6, 1995 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01263Frame · dentedFWD BAY, FRAME DENTED ON TOP AT BS 600 BETWEEN STR 26 TO 23L. ALSO FACTORY SPLICE IS DENTED. REPAIRED FRAME AT BS 600 BETWEEN STR 26 TO 23L PER FEDEX SRM 51-40-3.Sep 6, 1995 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01262Clip · corrodedCORROSION STR CLIP BS 1166 STR 15L. REMOVED CORRODED STR CLIP AT BS 1166 STR 15L AND INSTALLED NEW STR CLIP, IAW FEDEX SRM 51-30-2.Sep 6, 1995 · N499FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 95FDEA01261Seat Track · corrosionFOUND CORROSION IN SEAT TRACK AT BS 480 TO 600 WL 208.5 BL 0. REMOVED CORRODED SEAT TRACK AT BS 480 TO 600 WL 208.5 BL 0. FABRICATED NEW SEAT TRACK AND INSTALLED AT BS 480 TO 600 WL 208.5 BL 0, REF FEDEX SRM 53-10-5.Sep 6, 1995 · N499FE · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S953614Angle · crackedFOUND ON A-1 LETTER CHECK, .25 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER MM 57-54-0.Sep 5, 1995 · N543DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953607Eel Battery Pack · dischargedDURING LAYOVER, RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK, OPS CKS NORMAL.Sep 5, 1995 · N519DA · Boeing 727232 · Emergency LightingSDR DL72K953620Skin · corrodedTHE SKIN BETWEEN S-28 LT AND S-28 RT AT STA 720 WAS FOUND TO BE CORRODED. THE DAMAGE WAS REMOVED AND A DOUBLER WAS INSTALLED PER DL ERA 302443-14AD.Sep 5, 1995 · N410DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S953615Trunnion · corrodedDURING LTR CHECK, FOUND NOSE GEAR LEFT AFT TRUNNION BOLT BORE CORRODED. OPENED HOLE TO .9385, HFEC CK OK. REAMED HOLE PER M/M 53-40-0, MACHINED BUSHINGS TO SIZE AND TREATED. TREATED, PAINTED BOLT BORES AND INSTALLED BUSHINGS PER M/M 53-40-0.Sep 4, 1995 · N519DA · Boeing 727232 · Nose/Tail Landing Gear Attach SectionSDR DL72L953596Window · brokenPREFLIGHT CHECK, FOUND LEFT FORWARD OVERWING EMERGENCY EXIT HATCH WINDOW OUTER PANE BROKEN. REPLACED WITH SERVICEABLE DOOR FOR RETURN TO SERVICE. SDR UNDER INVESTIGATION.Sep 4, 1995 · N505DA · Boeing 727232 · Door WindowsSDR DL72S953602Skin · crackedDURING HMV, NR 2 SLAT LOWER SKIN ATTACH ANGLE CRACKED UNDER I/B STOP PAD. REPAIRED PER MM 57-54-0 PG 816.Sep 3, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953626Frame · misdrilledWHILE ACCOMPLISHING EO 4-61904-3AD AT HMV IN ATL, 2 OVERSIZED HOLES WERE DISCOVERED IN THE RT OVERWING EXIT FRAME AT STA 784. THE DOUBLER WAS MODIFIED TO REMOVE THE TWO HOLES FROM THE MODIFICATION, IN ACCORDANCE WITH BACO TWX DAL-ATL-95-0883RR DTD 8-31-95.Sep 1, 1995 · N515DA · Boeing 727232 · Fuselage Main, FrameSDR DL72K953627Vert Stiffener · crackedDURING CV-2 IN TPA, THE RT TORQUE BOX VERTICAL STIFFENER ANGLE AT STA 1263 WAS FOUND CRACKED. THE VERTICAL STIFFENER ANGLE WAS REPLACED IN ACCORDANCE WITH S/B 727-53-0129 REV 4.Sep 1, 1995 · N410DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR 95FDEA01236Frame · dentedFWD BAY, FRAME DENTED ON TOP BS 660 BETWEEN STR 25 AND 22L. ALSO, FACTORY SPLICE IS DENTED. REPAIRED FRAME AT BS 660 BETWEEN STR 25 AND 22L, IAW FEDEX SRM 51-10-3.Sep 1, 1995 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01235Frame · dentedFWD BAY, FRAME DENTED AT BS 680 BETWEEN STR 25 AND 23R. REPAIRED FRAME AT BS 680 BETWEEN STR 25 AND 23R, PER SRM 51-40-3 FEDEX.Sep 1, 1995 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01234Skin · damagedFASTENERS AT BS 1333 ON SKIN HAS 11 PULLED THROUGH FASTENER WL 257, LT SIDE ON SKIN EDGE. REMOVED DAMAGED SKIN AT BS 1333 WL 257 LT, FABRICATED DOUBLER, FILLER AND TAPERED SHIM, SCOTCH BRITE, ALODINE AND PRIMED. INSTALLED AS PER FEDEX 54-30-3, 51-20-1.Sep 1, 1995 · N499FE · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S953885Beam · crackedTHE LOWER TRAILING EDGE BEAM ON THE RT HORIZONTAL STABILIZER WAS FOUND CRACKED APPROXIMATELY 2 INCHES FROM THE OUTBOARD END OF THE BEAM. ACCOMPLISHED REPAIRS PER ERA 302395-14.Aug 31, 1995 · N515DA · Boeing 727232 · Horizontal Stabilizer StructureSDR DL72S953568Pbe Mask · defectiveDURING PREFLIGHT, FWD CABIN PBE WAS FOUND PARTIALLY OPEN. REPLACED PBE ASSEMBLY.Aug 31, 1995 · N522DA · Boeing 727232 · Portable Oxygen SystemSDR DL72S953566Rib · crackedDURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH NR 6 L/E SUPPORT RIB CRACKED. REPAIRED PER MM 57-54-0 FIG 814.Aug 31, 1995 · N411DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953575Blkhd · crackedCRACK INSIDE VERTICAL STABILIZER AT STA 1303 BULKHEAD LOWER RT CORNER, VENTRAL WALL ABOVE S-DUCT HAS CRACK. CRACK WAS FOUND AT HMV, REPAIRED BY INSTALLING DOUBLER PER SRM 53-10-4 FIG 17.Aug 30, 1995 · N515DA · Boeing 727232 · Vertical StabilizerSDR DL72S953573Bulkhead · crackedINSIDE VENTRAL STABILIZER AT STA 1303, BULKHEAD LOWER VERTICAL WALL ABOVE S-DUCT HAS CRACK AT LT CORNER. CRACK WAS FOUND AT HMV, REPAIRED PER SRM 53-10-4 FIG 17.Aug 30, 1995 · N515DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S953556Stiffener · crackedDURING A-1 LETTER CHECK, O/B LEADING EDGE SPAR STIFFENER HAS 1.5 INCH CRACK AT NR 2 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21.Aug 30, 1995 · N492DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S953555Stiffener · crackedDURING A-1 LETTER CHECK, FOUND I/B SPAR STIFFENER HAS 1.5 INCH CRACK AT NR 3 SLAT I/B TRACK. O/B SPAR STIFFENER HAS 1.5 INCH CRACK AT NR 3 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21.Aug 30, 1995 · N492DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S953554Skin · crackedDURING A-1 LETTER CHECK, FOUND COVE SKIN SUPPORT ANGLE CRACKED 1 INCH FROM O/B END ON NR 4 SLAT. REPAIRED PER MM 57-54-0.Aug 30, 1995 · N492DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953553Skin · crackedDURING A-1 LETTER CHECK, FOUND COVE SKIN SUPPORT ANGLE CRACKED .3750 INCH UNDER TAI DUCT ON NR 2 SLAT. REPAIRED PER M/M 57-54-0 AND ID PER PS 900-5-1 NR 4.Aug 30, 1995 · N492DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953543Eel Socket · wornLEFT FWD DOOR SLIDE LIGHT INOP. REPLACED WORN LIGHT SOCKET, OPERATION NORMAL.Aug 30, 1995 · N493DA · Boeing 727232 · Emergency LightingSDR DL72S953542Eel Bulb · failedRT CENTER OVERWING EMERG LIGHT, AFT BULB INOP. RELAMPED, OPERATION NORMAL.Aug 30, 1995 · N493DA · Boeing 727232 · Emergency LightingSDR 95FDEA01227Stringer · crackedFOUND CRACK STRINGER AT BS 404 STR 2R. ACCOMPLISHED STR REPAIR AT BS 404 STR 2R PER FEDEX SRM 53-10-3.Aug 30, 1995 · N499FE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S961617Transverse Beam · crackedTHERE IS DAMAGE TO THE LOWER TORQUE BOX STATION 1263 TRANSVERSE BEAM FWD SIDE. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AD 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS REPLACEMENT DOES NOT TERMINATE THE REPETITIVE INSPECTION REQUIREMENTSAug 29, 1995 · N535DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S953586Stringer · crackedWING UPPER STRINGER TO RIB WS 686.5 STRINGER NR 5 IS CRACKED. STOP DRILLED CRACK PER M/M 57-13-0 PG 802. FABRICATED REPAIR PARTS AND INSTALLED PER M/M 57-13-00 PG 802.Aug 29, 1995 · N499DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S953549Beam · crackedAT A LETTER CHECK IN TPA, A .50 INCH CRACK WAS FOUND IN THE UPPER TRANSVERSE BEAM GUSSET ANGLE AT F.S. 1273. ALSO, A .75 INCH CRACK IN THE ACCOMPANYING UPPER TRANSVERSE BEAM AT F.S. 1273. THE DAMAGED PARTS WILL BE REPLACED IN ACCORDANCE WITH B727 S/B 53-0129Aug 29, 1995 · N419DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S953545Switches · dirtyON APPROACH, NOSE GEAR DOOR LIGHTS ON FORWARD PANEL AND FLIGHT ENGINEER'S PANEL TOOK EXCEPTIONALLY LONG, 30-50 SECONDS, TO EXTINGUISH. CORRECTIVE ACTION. CLEANED DEBRIS FROM NOSE LANDING GEAR DOOR SWITCHES. CKS OK. NO MRR. REJECTED. 08-31-05 GT 595.Aug 29, 1995 · N400DA · Boeing 727232 · Landing Gear Position and Warning
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