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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DL72S960655Torque Box Web · crackedFOUND DURING B-2 LETTER CHECK, LWR LT TORQUE BOX CRACKED AT LIGHTNING HOLE AFT OF STA 1223 ADJACENT TO PREVIOUS REPAIRS. LOWER TORQUE BOX LIGHTNING HOLE ROUTED BEYOND LIP RT SIDE STA 1243 BOTH ITEMS REPAIRED PER M/M 53-11-0.Mar 25, 1996 · N534DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960690Bulkhead · crackedSTA 870 BLKHD CRACKED AT RBL 10 JUST BELOW APU BLEED VALVE ON FWD SIDE APPROX 10. REPAIRED PER SRM 53-10-9 NR 09/010.Mar 23, 1996 · N470DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S960643Bulb · failedEMERGENCY TRACK LIGHTING UNDER SEAT 31D IS OUT. RELAMPED BULB, CKS NORMAL.Mar 23, 1996 · N406DA · Boeing 727232 · Emergency LightingSDR MZZA96027Seat Track · crackedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1 INCH LONG CRACK WAS FOUND ON PASSENGER CABIN SEAT TRACK LOW PORTION AT BS 720D, RBL 45.5. THE DAMAGED SEAT TRACK FROM BS 720C TO BS 720D WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-5. HANGAR NMar 22, 1996 · N15781 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72L960642Skin · crackedA .25 INCH CRACK IN COVE SKIN LOWER ATTACH ANGLE BELOW NR 2 SLAT ACTUATOR ROD. FOUND DURING D-1 LETTER CHECK. REPAIRED PER MM 57-54-0.Mar 22, 1996 · N506DA · Boeing 727232 · Leading Edge DevicesSDR DL72L960641Rib · crackedFOUND DURING D-1 LETTER CHECK, NR 3 L/E SLAT NOSE RIB CRACKED 1 INCH ON I/B AND O/B SIDES. REPAIRED PER MM 57-54-0.Mar 22, 1996 · N506DA · Boeing 727232 · Leading Edge DevicesSDR DL72L960640Attach Fitting · crackedA .5 INCH CRACK IN NR 1 SLAT ACTUATOR I/B ATTACH FITTING. FOUND DURING D-1 LETTER CHECK. REPAIRED PER MM 57-20-21.Mar 22, 1996 · N506DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L960639Attach Fitting · crackedDURING D-1 LETTER CHECK, FOUND .5 INCH CRACK IN NR 1 SLAT ACTUATOR O/B ATTACH FITTING. REPAIRED PER MM 57-20-21.Mar 22, 1996 · N506DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L960636Actuator · failedAFTER TAKEOFF, AMBER LE FLAP LIGHT REMAINED ON AND NR 8 SLAT AMBER LIGHT ON S/O PNL. ON RETURN TO LAX LE FLAPS LIGHT STAYED ON, BUT ALL SLATS/FLAPS POS TEST SHOWS RETRACTED. RAN TEST USING TEST BOX 10M2425 PER M/M AND NR 8 SLAT ACTUATOR FAILED TEST. REPLACEMar 22, 1996 · N504DA · Boeing 727232 · Leading Edge Slat ActuatorSDR MZZA96031Support · crackedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 2 INCH LONG CRACK WAS FOUND ON PASSENGER CABIN FLOOR PANEL SUPPORT 'L' ANGLE BETWEEN BS 720A AND 720B, BL 0. THE DAMAGED FLOOR PANEL SUPPORT 'L' ANGLE FROM BS 720A TO 720B WAS REMOVED AND REPLACED WIMar 21, 1996 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA96029Seat Track · corrodedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK UPPER FLANGE AT BS 350, RBL 45.5. THE DAMAGED SEAT TRACK FROM BS 344 TO BS 380 WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-5. HANGAR NON Mar 21, 1996 · N15781 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR MZZA96028Channel · corrodedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON PASSENGER CABIN FLOOR PANEL SUPPORT 'J' CHANNEL AT BS 395, RBL 15. THE CORRODED 'J' CHANNEL FROM BS 380 TO 400 WAS REMOVED AND REPLACED WITH NEW 'J' CHANNEL. HANGAR NONMar 21, 1996 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA96023Stringer · crackedTNN - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 0.5 INCH LONG CRACK FOUND ON LEFT OUTER WING UPPER VENT STRINGER TO RIB ATTACHMENT AT S12, WS 686.5. THE CRACKED TAB WAS STOP DRILLED AND REPAIRED PER EA 5762-1050 (SB 727-57A159R5). REF: HANGAR Mar 21, 1996 · N15781 · Boeing 727232 · Wing, Longeron/StringerSDR DL72S961616Stiffener · crackedTHE INBOARD ACTUATOR ATTACH RIB STIFFENER ON THE NR 8 SLAT ACTUATOR WAS FOUND CRACKED. THE DAL MFG PART NUMBER FOR THE INBOARD AND OUTBOARD STIFFENERS IS (57-0367-002). BOTH THE INBOARD AND OUTBOARD ATTACH RIB STIFFENERS WILL BE REPLACED PER EO 4-59271-3AD. Mar 21, 1996 · N520DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S961615Bracket · misinstalledTHE NR 1, NR 2 AND NR 8 SLAT ACTUATOR MOUNT BRACKETS WERE FOUND WITH GAPS EXCEEDING THE 0.01 LIMIT SET BY SI 4-59271-12. THE GAPS AT THE MOUNT BRACKETS ARE THE SUBJECT OF S/B 727-57-0130. SHIMS WILL BE INSTALLED IN ACCORDANCE WITH THE SERVICE BULLETIN. THE Mar 21, 1996 · N520DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S960687Skin · crackedINNER SKIN CRACKED BETWEEN RIB NR 9 AND NR 10. REPAIRED PER M/M 57-54-0, FOR NR 6 L/E SLAT.Mar 21, 1996 · N515DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960650Web · crackedFROM MV-2 ATL, I/B WEB IS CRACKED ON NR 8 SLAT. FABRICATED AND INSTALLED DOUBLER PER M/M 57-54-0 FIG 814.Mar 21, 1996 · N520DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960634Angle · crackedDURING LETTER CHECK, NR 5 L/E SLAT AFT ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0 PAR 12.Mar 21, 1996 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960631Angle · crackedFOUND DURING A-1 LETTER CHECK, NR 7 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.Mar 21, 1996 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960630Angle · crackedFOUND DURING A-1 LETTER CHECK, NR 5 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.Mar 21, 1996 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960629Angle · crackedFOUND DURING A-1 LETTER CHECK, .75 INCH CRACK NR 4 KRUEGER FLAP ACTUATOR MOUNT BOX AT UPPER I/B FWD CORNER. REPAIRED PER M/M 57-20-21.Mar 21, 1996 · N499DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S960626Bulb · failedAFT GALLEY DOOR EXIT LIGHT INOP. RELAMPED, OPERATION NORMAL.Mar 21, 1996 · N544DA · Boeing 727232 · Emergency LightingSDR MZZA96030Intercostal · crackedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1 INCH LONG CRACK WAS FOUND ON PASSENGER CABIN FLOORBEAM INTERCOSTAL BETWEEN BS 950A AND 950B, BL 0. THE DAMAGED INTERCOSTAL FROM BS 950A AND 950B WAS REMOVED AND REPLACED WITH NEW CHANNEL. HANGAR NMar 20, 1996 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L960622Compressor · stalledAPPLYING TAKEOFF POWER HAD EXPERIENCED COMPRESSOR STALLS ON NR 2 ENG, WIND WAS APPROX 320 AT 17 TO 20 KTS, DEPARTED 35L DFW. AFTER TAKEOFF COMPRESSOR STALLS RETURNED ON CLIMBOUT AT 190 KTS. REPLACED PRBC AND P AND D VLV, NO HELP. ACTVATED 6TH STAGE BLEED PMar 20, 1996 · N505DA · Boeing 727232 · Turbine Engine Compressor SectionSDR DL72L960615Angle · crackedTHE NR 4 SPOILER ACTUATOR ATTACH FITTING WAS REPLACED DUE TO A CRACK FOUND IN THE O/B FITTING. ALL WORK DONE PER SRM 57-50-6.Mar 20, 1996 · N514DA · Boeing 727232 · Drag Control ActuatorSDR DL72K960621Light · inoperativeEMERGENCY LIGHT INOP ABOVE AFT AIRSTAIR. REPLACED LIGHT ASSY PER MAINTENANCE MANUAL, OPS TESTS OK.Mar 20, 1996 · N491DA · Boeing 727232 · Emergency LightingSDR DL72S960637Actuator Bolts · looseAT MV-2 VISIT, FOUND NR 13 SPOILER ACT LUGS LOOSE RT WING. REPAIRED MOUNT BOLTS WHERE THEY ATTACH TO VERTICAL ANGLES ON REAR SPAR PER MM 57-42-0.Mar 19, 1996 · N520DA · Boeing 727232 · Wing, Control Surface Attach FittingsSDR DL72L960614Power Supply · inoperativeDURING EMERGENCY LIGHTING CHECK, MAINT FOUND TRACK LIGHTING BETWEEN ROWS 12 AND 19 INOP. REPLACED POWER SUPPLY, OPERATION NORMAL.Mar 19, 1996 · N505DA · Boeing 727232 · Emergency LightingSDR 96ZZZM1096Seat Track · corrodedAFT MAIN CABIN HAS LEVEL 2 CORROSION ON SEAT TRACK RBL 24 INCHES STATION 1050 TO 1110. REMOVED CORROSION PER SRM 51-10-16 AND REPLACED SEAT TRACK FROM STATION 1070 TO 1132 PER SRM 53-10-5.Mar 19, 1996 · N17789 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR MZZA96032Gusset · crackedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1.5 INCH LONG CRACK WAS FOUND ON BS 823 FRAME FORWARD GUSSET AT RBL 62.5. THE CRACK WAS STOP DRILLED AND REPAIRED PER SRM 51-40-3. HANGAR NON ROUTINE REPAIR ITEM CARD NR 818598. (M)Mar 18, 1996 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960605Angle · crackedFOUND ON A1 LETTER CHECK - REWRITE FROM N/R 50 - ANGLE CRACKED .50 INCH AT NR 7 SLAT ANTI-ICE 'T' DUCT CUTOUT - REPAIR, INSTALL DOUBLER PER M/M 57-54-0, PG 807.Mar 18, 1996 · N515DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960604Rib · crackedFOUND ON F1 LETTER CK, 1 INCH CRACK AT NR 2 L/E SLAT INBOARD NOSE RIB AT ACTUATOR ROD END ATTACH. REPAIRED PER MM 57-54-0.Mar 18, 1996 · N400DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960603Angle · crackedNR 7 SPOILER LOWER WING ATTACH ANGLE CRACKED INBOARD END. FOUND DURING F-1 LTR CK TPAMM. REPAIRED PER 57-20-22.Mar 18, 1996 · N400DA · Boeing 727232 · SpoilersSDR DL72S960602Stiffner · crackedWING FRONT SPAR VERTICAL STIFFENER CRACKED AT NR 3 SLAT INBOARD TRACK, OUTBOARD SIDE (ON WING). FOUND DURING F-1 LTR CK TPA 3/18/96. REPAIRED PER 57-20-21.Mar 18, 1996 · N400DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L960653Skin · damagedLAX REPORTED DAMAGE TO THE SKIN, STRINGERS AND FRAMES BETWEEN STA 340 TO STA 400 AND STR 22R TO S-24R. SEVERAL REPAIRS HAVE BEEN INSTALLED PER THE B727 SRM. DUE TO LIMITED ACCESS BLIND FASTENERS WILL BE INSTALLED IN SEVERAL LOCATIONS ON A TIME LIMITED BASIS,Mar 18, 1996 · N503DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K960623Rib · crackedFOUND ON MV1 CHECK, NR 2 SLAT (S/N BN1110) HAS .5 CRACKS IN INBD AND OUTBD NOSE RIBS ADJACENT TO ACTUATOR ROD END. REPAIRED PER M/M 57-54-0 PG 805.Mar 18, 1996 · N412DA · Boeing 727232 · Leading Edge DevicesSDR DL72K960612Attach Angle · crackedFOUND ON MV-1 CHECK, .3750 INCH CRACK IN COVE SKIN ATTACH ANGLE BELOW TIA DUCT OF NR 2 L/E SLAT. REPAIR: REPAIRED PER M/M 57-54-0, PG 807A.Mar 18, 1996 · N412DA · Boeing 727232 · Leading Edge DevicesSDR MZZA96025Spar · corrodedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON RIGHT WING FRONT SPAR LOWER CHORD PLATE BELOW NR 5 SLAT ACTUATOR. THE CORRODED CHORD PLATE WAS CLEAN UP AND REPAIRED PER B727 51-10-6 AND 51-40-4. HANGAR NON ROUTINE REMar 17, 1996 · N15781 · Boeing 727232 · Wing SparSDR MZZA96034Inboard Web · oil canningTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON AFT AIRSTAIR RT/LT TORQUE BOX INBOARD WEB AT THE FOLLOWING AREAS; RT SIDE BETWEEN BS 1213 AND 1223. RT SIDE BETWEEN BS 1243 AND 1253. RT SIDE BETWEEN BS 1263 AND 1273. RT SMar 15, 1996 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA96033Inboard Web · crackedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACKS WERE FOUND ON AFT AIRSTAIR TORQUE BOX INBOARD WEB LIGHTENING HOLE CUTOUT, AT THE FOLLOWING AREA; 1 INCH LONG CRACK AT BS 1238 LEFT SIDE, 2 INCHES LONG CRACK AT BS 1218 RIGHT SIDE, 4 INCHES LONGMar 15, 1996 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L960681Pump · failedNUMBER 2 ENGINE FLAMED OUT AT FL 310 NO INDICATIONS OF STALLS OR OTHER ENGINE DAMAGE. REPLACED FUEL PUMP AND FUEL CONTROL, OPERATION NORMAL.Mar 15, 1996 · N513DA · Boeing 727232 · Engine Fuel PumpSDR DL72S960586Skin · damagedDURING SHOP INSPECTION, RIGHT ELEVATOR WAS REPAIRED FOR SKIN DAMAGE PER SRM 55-20-3, REF DL ERA 303316-14.Mar 14, 1996 · N540DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S960577Vert Beam · crackedVISIBLE CRACK, 1.50 INCHES, IN VERT BEAM, STA 1183, RBL 8 AT WL 182. FOUND DURING E-2 LTR CK TPAMM. REPAIRED PER M/M 53-11-0.Mar 14, 1996 · N409DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR 96ZZZM877Stringer · corrodedFORWARD CARGO STATION 560 LEFT STRINGER 18 LEVEL 2 CORROSION ON STRINGER. REMOVED CORROSION PER SRM 51-10-6 MATERIAL LOSS OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED STRINGER SECTION, FABRICATED 1 REPAIR STATION AND 4 FILLERS PER SRM 53-10-3, FIGURE 1, INMar 14, 1996 · N17789 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S960680Angle · crackedA CRACK WAS FOUND 32.5 FROM I/B END ON LOWER AFT COVE SKIN ATTACH ANGLE BELOW ANTI-ICE DUCT. REPAIRED AS PER MM 57-54-0 FIG 805A, FOR NR 8 L/E SLAT.Mar 13, 1996 · N532DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960668Skin · corrosionTHE SKIN BETWEEN STA 480 TO 500 AND STR 27R TO 28R WAS FOUND CORRODED. THE DAMAGED SECTION WAS TRIMMED OUT LEAVING A CUTOUT DIMENSION OF 19.5 INCH BY 8.5 INCH. ER/A WILL INSTALL AN EXTERNAL DOUBLER AND TRIPLER FOR THE DAMAGE. REV A DETAILS ADDITIONAL CORROSMar 13, 1996 · N546DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960567Web · crackedFOUND ON B2 LETTER CHECK, LOWER RT TORQUE BOX LIGHTENING HOLE WEB CRACKED FS 1243. REPAIRED PER MM 53-11-0.Mar 13, 1996 · N532DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL960307Brake · bearing damagedEWR - FLT 0700 - THE NR 3 MAIN WHEEL BRAKE CHATTERED ON LANDING ROLL-OUT WHILE TAXIING TO GATE IN EWR. MAINTENANCE REMOVED NR 3 TIRE AND FOUND INNER BEARING DAMAGED. THE NR 3 TIRE AND BRAKE WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (X)Mar 13, 1996 · N45793 · Boeing 727232 · BrakeSDR DL72S960666Rib · crackedMTC DISCOVERED CRACKS IN THE LT AND RT WING RIB CHORD DURING MV-2 IN ATL. THE CRACK WAS REMOVED BY OVERSIZING THE HOLES TO .628 INCH IN THE LT RIB CHORD. IN THE RT RIB CHORD THE CRACK WAS REMOVED BY OVERSIZING THE UPPER HOLE TO .6435 INCH AND THE LOWER HOLE Mar 12, 1996 · N546DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S960563Bracket · crackedFOUND ON E1 LETTER CHECK, NR 1 SLAT ACTUATOR MOUNT BRACKET CRACKED ON O/B SIDE. REPAIRED PER M/M 57-20-21.Mar 12, 1996 · N478DA · Boeing 727232 · Leading Edge Slat Actuator
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