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 DL72S953544Stiffener · crackedFOUND ON F-1 LETTER CHECK - FRONT SPAR STIFFENERS CRACKED AT NR 4 LEADING EDGE SLAT, INBOARD TRACK ROLLER BOX. REPAIRED PER M/M 57-20-21.Aug 29, 1995 · N516DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S953538Eel Battery Pack · dischargedEMERGENCY TRACK LIGHTS INOP IN F/C CABIN, REPLACED PACK AND BATTERIES, FOUND LIGHT ASSEMBLY AT SEAT 2AB SHORTED. REMOVED LIGHT AND FWD LIGHT AT 2AB TO MCO PER MEL 33-00-17. REPLACED LIGHT ASSEMBLY AT SEAT 2AB. OPERATION NORMAL.Aug 29, 1995 · N470DA · Boeing 727232 · Emergency LightingSDR DL72S953536Skin · crackedC-2 DOOR SKIN CRACKED IN 2 PLACES AT UPPER EDGE 15 INCHES FWD OF AFT CORNER. REPAIRED PER SRM 52-00-3, FIG 3.Aug 29, 1995 · N521DA · Boeing 727232 · Cargo/Baggage DoorsSDR DL72L954783Nose Cowl · crackedCAP-FRAME CRACKED INSIDE AT ACCESS HOLE NR 2. DURING SHOP INSPECTION OF NR 3 NOSE COWL, REPAIRED PER SRM 54-10-3, FIG NR 3.Aug 29, 1995 · N508DA · Boeing 727232 · Engine Cowling SystemSDR DL72L954782Frame · crackedCAP FRAME CRACKED AT STATION 69.00, AT THE 7:00 POSITION. DURING SHOP INSPECTION OF NR 3 ENGINE NOSE COWL, REPAIRED CAP PER SRM 54-10-3.Aug 29, 1995 · N508DA · Boeing 727232 · Engine Cowling SystemSDR DL72L954775Cowling · crackedDURING SHOP INSPECTION, NR 3 ENGINE NOSE COWL WAS FOUND WITH CRACKED WEB AT STA 69.00 AT 4'CLOCK POSITION, REPAIRED PER SRM 54-00.Aug 29, 1995 · N508DA · Boeing 727232 · Engine Cowling SystemSDR DL72K953629Skin · dentedFOUND ON CV2 CHECK, SEVERAL DENTS AND GOUGES AT TOP SIDE OF RT ELEVATOR O/B END. REPAIRED PER SRM 55-20-3 FIG 4, O/B DENT ONLY. THE I/B DENTS WITHIN LIMITS PER SRM 55-20-1.Aug 29, 1995 · N410DA · Boeing 727232 · Elevator, Plate/SkinSDR CAL950769Transmission · inoperativeFLT NR 0219 - EWR - THE OUTBOARD TRAILING EDGE FLAPS FAILED TO EXTEND ON APPROACH TO EWR. USE OF FLAP ALTERNATE DRIVE SYSTEM WAS NO HELP. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE OUTBOARD NR 8 FLAP TRANSMISSION AT FAULT. THE NR 8 FLAP TRAug 29, 1995 · N523PE · Boeing 727232 · Trailing Edge Flap Control SystemSDR 95FDEA01226Skin · dentedDENT WITH CREASE FOUND IN SKIN AT BS 1243 WL 143 ON RIGHT SIDE OF A/C BETWEEN STR 22R AND 23R.Aug 29, 1995 · N499FE · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S953548Blkhd Stiffener · crackedAT CV3 IN ATL, A CRACK WAS FOUND EMANATING FROM THE BOTTOM OF THE LT FLANGE ON THE FS 1183 BULKHEAD VERTICAL STIFFENER AT RBL 8. THE CRACK WAS 1 INCH LONG. REPAIRED DAMAGE PER DL ERA 302413-14AD. AUTHORIZED BY B727-53-0175 REV. 2.Aug 28, 1995 · N521DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S953547Skin · dentedDURING CV3 IN ATL, THE FUSELAGE SKIN WAS DENTED IN TWO PLACES AT FUSELAGE STATION 1323, STR 21L. IN ACCORDANCE WITH B727 SRM 53-30-3, FIGURE 3, AN EXTERNAL REPAIR DOUBLER WAS INSTALLED.Aug 28, 1995 · N521DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S953531Angle · crackedCRACK, 25 INCHES, NR 2 SLAT INBOARD UPSTOP PAD. FOUND AT C-1 LTR CK. SLAT WAS REPLACED AND ROUTED TO SHOP.Aug 28, 1995 · N419DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953530Rib · crackedNR 6 SLAT HAS .50 INCH CRACK INBOARD OF ACTUATOR ATTACH POINT AT FORWARD RIB. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-54-0.Aug 28, 1995 · N419DA · Boeing 727232 · Leading Edge DevicesSDR 95FDEA01204Delta Beam Web · corrodedIN THE LOWER A/C BAY AT BS 790 RBL 5 WL 148 THERE IS CORROSION ON THE DELTA BEAM WEB. REMOVED DAMAGED SECTION. FABRICATED REPAIR DOUBLER & FILLER PER FEDEX SRM 51-40-02. INSTALLED DOUBLER & FILLER PER FEDEX SRM 51-30-02. APPLIED SKYDROL RESISTANT FINAug 28, 1995 · N499FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S953560Frame · misdrilledDURING HMV IN ATL, SEVERAL HOLES IN THE INBOARD FRAME FLANGE WERE OVERSIZED AT FS 760.95 AND FS 783.95, IN BOTH RT AND LT SIDE WHILE ACCOMPLISHING EO 4-61904-3AD. THE HOLES WERE AUTHORIZED OVERSIZED PER S/B 727-53-0197 REV 2.Aug 27, 1995 · N515DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S953521Eel Sign · brokenEMERGENCY EXIT LIGHT FOUND BROKEN AND HANGING ON SIDEWALL PANEL SEAT ROW 20ABC. REPLACED LIGHT ASSEMBLY, OPERATION NORMAL.Aug 27, 1995 · N532DA · Boeing 727232 · Emergency LightingSDR DL72S953520Eel Battery Pack · dischargedDURING LAYOVER, FOUND THE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOP. RELAMPED, CLEANED CONNECTIONS AND REPLACED BATTERY PACK. OPERATION NORMAL.Aug 27, 1995 · N532DA · Boeing 727232 · Emergency LightingSDR DL72S953574Angle · corrodedANGLE CORRODED, A/C BAY DOOR ATTACH TEE FROM STA 740 TO 780 CORRODED WHERE HINGES ATTACH FOR PANEL NR 3448. CORROSION WAS FOUND AT HMV, REPAIRED PER M/M 53-30-1 PG 807 AND 808.Aug 26, 1995 · N515DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S953539Angle · corrodedANGLE CORRODED, A/C BAY DOOR ATTACH TEE FROM STA 740 TO 780, CORRODED WHERE HINGES ATTACH FOR PANEL 3348L. FOUND DURING HMV AND REPAIRED PER MM 53-30-1 PG 807 TO 808.Aug 26, 1995 · N515DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S953516Skin · creasedAT HMV, FOUND RT ELEVATOR LOWER SKIN PANEL NR 4 FROM THE I/B END WITH CREASE. REPAIRED PER SRM 55-20-3 FIG 5.Aug 26, 1995 · N515DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S953513Le Rib · crackedDURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH CRACKED L/E RIB AT THE ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0 FIG 804.Aug 26, 1995 · N411DA · Boeing 727232 · Leading Edge DevicesSDR CAL950760Gpws Computer · inoperativeFLT NR 0219 - EWR - THE GPWS SOUNDED AT 300 FEET WITH FLAPS SET AT 30 DEGREES WHILE ON APPROACH TO EWR. A 'GO AROUND' WAS PERFORMED AND ON THE NEXT APPROACH THERE WAS NO GPWS WARNING WITH THE SAME CONDITIONS. THE GPWS COMPUTER WAS REMOVED AND REPLACED IAW MMAug 26, 1995 · N523PE · Boeing 727232 · Ground Proximity SystemSDR DL72S953507S-Duct · crackedFWD EDGE OF UPPER S-DUCT INNER SKIN CRACKED AT APPROX 6 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3 FIG 9.Aug 24, 1995 · N515DA · Boeing 727232 · Nacelle/Pylon StructureSDR DL72S953494Ribs · crackedDURING SHOP INSPECTION, NR 7 L/E SLAT WAS FOUND WITH NR 2 L/E RIB CRACKED IN LOWER AFT CORNER. REPAIRED PER MM 57-54-0 FIG 814.Aug 24, 1995 · N495DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953493Le Ribs · crackedDURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH SEVERAL CRACKED L/E RIBS. ACCOMPLISHED REPAIRS PER MM 57-54-0.Aug 24, 1995 · N470DA · Boeing 727232 · Leading Edge DevicesSDR DL72L953492Eel Battery Pack · dischargedDURING LAYOVER C-2, CARGO EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OPERATION NORMAL.Aug 24, 1995 · N505DA · Boeing 727232 · Emergency LightingSDR DL72S953484Attach Fitting · corrodedDURING HMV, FOUND NOSE LANDING GEAR LT PIVOT ATTACH POINTS CORRODED ON MATING FLANGES AND INSIDE OF HOLES. REPAIRED PER SRM 53-40-1.Aug 23, 1995 · N515DA · Boeing 727232 · Fuselage, Landing Gear Attach FittingsSDR DL72S953483Attach Fitting · corrodedDURING HMV, FOUND NOSE LANDING GEAR RT PIVOT ATTACH POINT FITTINGS CORRODED ON MATING FLANGES AND INSIDE OF HOLES. REPAIRED PER SRM 53-40-1.Aug 23, 1995 · N515DA · Boeing 727232 · Fuselage, Landing Gear Attach FittingsSDR DL72S953482Trunnion · crackedDURING HMV, FOUND I/B TRUNNION MOUNT BRACKET CRACKED ON NR 6 FLAP ACTUATOR. REPAIRED PER M/M 57-20-21.Aug 23, 1995 · N515DA · Boeing 727232 · Wing, Control Surface Attach FittingsSDR DL72S953481Bracket · crackedDURING HMV, FOUND I/B MOUNT BRACKET CRACKED FOR THE NR 5 L/E FLAP ACTUATOR. REPAIRED PER 57-20-21.Aug 23, 1995 · N515DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953480Trunnion · corrodedDURING HMV, FOUND RT MLG TRUNNION FITTING CORRODED INSIDE HOLES. REPAIRED PER M/M 57-43-0.Aug 23, 1995 · N515DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S953479Stringer · crackedDURING HMV, FOUND STRINGER CRACKED RT WING STA 686 FWD STRINGER. REPAIRED PER M/M 57-13-0 PG 808.Aug 23, 1995 · N515DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S953476Angle · crackedAT HMV, FOUND ANGLE CRACKED INBD LWR CORNER OF INBD GRND SPOILER MOUNT BOX. REPAIRED PER MM 57-55-0 PG 805.Aug 23, 1995 · N515DA · Boeing 727232 · SpoilersSDR CAL950746Pwr Control Unit · inoperativeFLT NR 0354 - SJU - WHILE CRUISING AT FL 280 THE AIRCRAFT BEGAN A 'FISHTAILING' MOTION. THE AIRCRAFT WAS SLOWED TO APPROXIMATELY 270 AND BOTH YAW DAMPERS WERE CYCLED OFF, BUT THIS DID NOT CORRECT THE PROBLEM. THE AIRCRAFT WAS RETURNED TO SJU. MAINTENANCE FOAug 23, 1995 · N523PE · Boeing 727232 · Rudder Control SystemSDR DL72S953886Bulkhead · fastener subWHILE ACCOMPLISHING EO 4-40130-3AD, AFT ENTRY DOORWAY AND BODY STATION 1183 BULKHEAD REINFORCEMENT, SEVERAL FASTENERS CALLED FOR BY THE DRAWING, COULD NOT BE INSTALLED DUE TO FRAME INTERFERENCE. THESE FASTENERS WILL BE SUBSTITUTED TO FACILITATE THE MODIFICATIAug 22, 1995 · N515DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S953884Frames · misdrilledDURING ACCOMPLISHMENT OF SI 4-61904-12AD, MAINTENANCE DISCOVERED THAT THE FRAMES AT STA 760.95 LT AND RT AND STA 783.95 LT AND RT HAVE OPEN PILOT HOLES IN THE WEB ABOVE STR 17. THE HOLES WHICH ARE ATTACH POINTS FOR INSULATION BLANKETS, HAVE BEEN INSPECTED ANDAug 22, 1995 · N498DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S953666Attach Lug · brokenAT HMV, FWD ENTRY DOOR UPPER GATE STOP ROD ATTACH LUG FOUND BROKEN. REPAIRED PER 52-10-2 FIG 10.Aug 22, 1995 · N499DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S953578Act Attach · crackedNR 6 L/E FLAP ACTUATOR ATTACH STRUCTURE CRACKED AT LOWER I/B CORNER. REPAIRED PER M/M 57-20-21 PG 811.Aug 22, 1995 · N499DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S953475Bushing · misalignedAT HMV, FOUND LT FITTING FOR NR 4 FLAP TRACK MISALIGNED. REPLACED BUSHING PER MM 57-42-0 PG 814.Aug 22, 1995 · N515DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S953462Blkhd Doubler · trimmmedDURING ACCOMPLISHMENT OF BACO S/B 727-53-0055, R9, REINFORCEMENT OF THE BS 1183 BULKHEAD AS MANDATED BY AD 90-06-09. WHILE ACCOMPLISHING MODIFICATION TO THE BS 1183 LT AFT DOOR FRAME, THE DOUBLER WAS TRIMMED INADVERTENTLY. IN ACCORDANCE WITH BACO TWX-DAL-ATLAug 22, 1995 · N493DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72K954262Skin · corrodedAT CV2 IN TPA, THE FUSELAGE SKIN AT STA 540 BETWEEN S-26R AND S-27R, JUST BELOW THE LAP SPLICE HAS BEEN TRIMMED TO REMOVE CORROSION. THE CUT OUT MEASURES 5 INCH BY 11 INCH. THIS ER/A REPAIRS THE AREA BY ADDING A .090 2024-T3 CLAD FILLER, .050 2024-T3 CLAD DOAug 22, 1995 · N466DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S953855Spar · crackedDURING SHOP INSPECTION, NR 2 MIDFLAP HAS A CRACKED AFT SPAR CHORD 22 FT AND 53 FROM I/B END OF FLAP AND A CRACK AT I/B ACTUATOR CUTOUT. SPLICED IN NEW SECTIONS OF AFT SPAR CHORD AND INSTALLED DOUBLERS, PER MM 57-52-00 PG 807.Aug 21, 1995 · N499DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S953639Skin · crackedNR 5 SLAT SKIN WORN ON UPPER SURFACE AT FENCE ATTACHMENT. BURNISHED WORN AREA AND DYE PENETRANT INSP SHOWS CRACKS AT 3 FENCE ATTACH HOLES. ROUTED DAMAGE AT ATTACH HOLES, FABRICATED AND DRILLED DOUBLER PER M/M 57-54-0.Aug 21, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953577Act Attach · crackedNR 5 L/E FLAP ACTUATOR ATTACH STRUCTURE CRACKED AT LWR O/B CORNER. REPAIRED PER M/M 57-20-21 PG 811. CRACK WAS FOUND AT HMV.Aug 21, 1995 · N499DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S953668Rib · crackedDURING HMV, FOUND NR 7 SLAT RIB CRACKED AT FASTENER HOLE, I/B OF I/B STOP PAD. FABRICATED REPAIR PER M/M 57-54-0 PG 807 AND INSTALLED REPAIR PER MM 57-54-0 PG 807.Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953649Web · crackedDURING HMV, FOUND WEB CRACKED NR 5 SLAT. REPAIRED WEB PER MM 57-54-0 FIG 805.Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953637Skin · wornNR 6 SLAT SKIN WORN AND CHAFED INBD OF INBD TRACK FAIRING AND BELOW SLAT ACTUATOR ON LWR TRAILING EDGE. TRIMMED AWAY DAMAGED PORTION OF TAB AND FABRICATED DOUBLER AND FILLER PER MM 57-54-0 PG 820.Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953632Angle · crackedUPON HMV, FOUND .25 INCH CRACK AT FASTENER HOLE IN ATTACH ANGLE AFT OF RIB 6 OUTBD OF T.A.I. DUCT. REPAIRED PER M/M 51-54-0, FIG 805A.Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953610Rib · crackedDURING HMV, FOUND NR 4 SLAT RIB CRACKED .5 INCH, ON O/B SIDE OF O/B TRACK FITTING. REPAIRED RIB PER MM 57-45-0 FIG 814.Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953591Rib · crackedDURING HMV, NR 8 L/E SLAT WAS FOUND WITH CRACKED INTERNAL SUPPORT RIB. REPAIRED PER MM 57-54-0 PG 814.Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge Devices
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