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 DL72K990415Battery Pack · dischargedOVERHEAD EMERGENCY EXIT SIGN WOULD NOT ILLUM WHEN TESTED. REPLACED BATTERY PACK, CKS NORMAL.Feb 28, 1999 · N526DA · Boeing 727232 · Emergency LightingSDR CALA9900198Wire · brokenINSPECTION FOUND THE LAST FIVE AISLE PATH LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE FOUND A BROKEN WIRE AT AFT BATTERY PACK. THE WIRE WAS REPAIRED AND OPERATION CHECKED GOOD.Feb 28, 1999 · N14788 · Boeing 727232 · Light System WiringSDR DL72L990412Beam · crackedWEB AND OUTER CHORD FOUND CRACKED JUST AFT OF THE FWD PRESSURE STOP FITTING. OUTER CHORD IS TO BE REPLACED. WEB SPLICE REPAIR IS TO BE ACCOMPLISHED PER ER/A.Feb 27, 1999 · N501DA · Boeing 727232 · Cargo/Baggage DoorsSDR DL72S990451Beam · crackedCRACK IN L-1 LOWER BEAM AFT CORNER HFEC TO CONFIRM CRACK MARK ENDS. FABRICATED REPAIR DOUBLER PER M/M 52-11-01 FIG 803. STOP DRILLED CRACK AT MARKED ENDS. INSTALLED PER M/M 52-11-01 FIG 803. COMPLETED INST PER M/M 52-11-01 FIG 803.Feb 26, 1999 · N531DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S990448Stringer · crackedRT WING STR-TO-RIB INSP AT WS 686.5 STRINGER 8 SHOWS CRACK INDICATION, MARKED (AFT UPPER STR). LOOSENED FUEL DUMP LINE FOR ACCESS, BEGAN DRILLING UP REPAIR PER M/M 57-13-0 FIG 802. STOP DRILLED CRACK REPAIR PER M/M 57-13-0 FIG 802. INSTALLED REPAIR PER M/M Feb 26, 1999 · N531DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S990446Stringer · crackedLT WING UPPER STR-TO-RIB HOLE INSP, SHOWS CRACK INDICATION WS 686.5 STRINGER 11. CUT ACCESS HOLE IN STRINGER, BEGAN DRILLING UP RADIUS BLOCKS. STOP DRILLED CRACK, REMOVED FUEL VENT TUBE FWD OF STRINGER 12 AT WS 686.5 TO FOM, REMOVED FUEL PROBE HARNESS STANDOFeb 26, 1999 · N531DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S990422Skin · crackedLFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTION OF THE ENTIRE PANEL CONFIRMED 7 CRACKS BETWEEN FS 400 AND 420. THE DAMAGED SECTION OF LAP SPLICE WAS CUT OUT AND REPAIRFeb 26, 1999 · N400DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990411Oil Filter · dirtyNR 3 ENGINE OIL FILTER INDICATED BYPASS IN CRUISE FL280. PRECAUTIONARY, SHUTDOWN PROCEDURE ACCOMPLISHED. REPLACED OIL FILTER, LOP SWITCH, FILTER BYPASS SWITCH, DRAINED OIL RES, PERFORMED OIL BREATHER PRESS CK TEST 'Z' PER PFHB AND OPN OK. REPLACED OIL FILTEFeb 26, 1999 · N499DA · Boeing 727232 · Turbine Engine Oil SystemSDR DL72S990410Battery Pack · dischargedFOUND ON L/O, LT AFT EMERGENCY SLIDE LIGHT INOP. REPLACED BATT PACK, CKS GOOD.Feb 26, 1999 · N540DA · Boeing 727232 · Emergency LightingSDR DL72S990408Light · inopL1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS NOW OK.Feb 26, 1999 · N536DA · Boeing 727232 · Emergency LightingSDR DL72S990407Stiffener · crackedTPA - LTR CHK C-1 02/26/99, WING LE SPAR STIFFENER CRACKED AT I/B SIDE NR 2 SLAT I/B TRACK BOX. REPLACED STIFFENER PER MM 57-20-21.Feb 26, 1999 · N401DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S990406Bracket · crackedNR 8 SLAT ACT I/B MOUNT BRACKET CRACKED AT WEB. REPAIRED PER M/M 57-20-21.Feb 26, 1999 · N401DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S990405Skin · crackedNR 7 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0.Feb 26, 1999 · N401DA · Boeing 727232 · Leading Edge DevicesSDR DL72L990420Skin · corrodedSEVERAL EXISTING SKIN DOUBLER REPAIRS WERE LOCATED ON THE BELLY SKIN PANEL BETWEEN STRINGERS 26L & 26R AND BETWEEN FS 1010 AND 1080. THE REPAIRS WERE FOR CORROSION CUTOUTS. TO IMPROVE THE CONDITION OF SKIN AND ELIMINATE ADDITIONAL CORROSION, THE SKIN WAS CUTFeb 26, 1999 · N509DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990403Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. HFEC INTERNAL INSPECTION CONFIRMED 7 CRACK LOCATIONS ALONG THE PANEL. THE ENTIRE LAP SPLICE WAS CUTOUT ALONG THE PANFeb 25, 1999 · N518DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990402Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. HFEC INTERNAL INSPECTION CONFIRMED 4 CRACKS IN TWO CONSECUTIVE FRAME BAYS. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT ALFeb 25, 1999 · N518DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990394Battery Pack · dischargedBATTERY DEAD ON EMERGENCY FLASHLIGHT AT 1L DOOR. REPLACED BATTERY AND BULB.Feb 25, 1999 · N518DA · Boeing 727232 · Emergency LightingSDR DL72S990393Light · inopMID CEILING EMER LIGHT WOULD NOT ELIMINATE WHEN CHECKING EMERGENCY LIGHTS. REPLACED LIGHT ASSY.Feb 25, 1999 · N518DA · Boeing 727232 · Emergency LightingSDR DL72S990385Skin · tornGOUGE IN SKIN AT THE AFT EDGE OF THE C-2 DOOR CUTOUT AT FS 990. DAMAGED AREA LOCATED AT 2-24R. SKIN, DOUBLER, TRIPLER AND BEAR STRAP ARE ALL DAMAGED. ACTION TAKEN, ERA 332858-14.Feb 24, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990361Frame · dentedFRAME DENTED AFT CARGO COMPT LT FRAME DENTED AT STA 950B ABOVE STR 26L. REMOVED DAMAGED PER SRM 53-10-4 FIG 27. DYE PENETRANT CHECKED PER PS 900-6-3, NO CRACKS NOTED. DRILLED NEW DUCT PER SRM 53-10-4 FIG 27. REMOVED WEB FROM STA 950A TO 950B AT STR 25L. IFeb 24, 1999 · N411DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S990360Frame · dentedFRAME DENTED LT FS 1070, STR 26L. REMOVED DAMAGED AREA, DYE CHECKED PER PS 900-6-3 NR 1. NO FURTHER DAMAGE FOUND. FABRICATED DOUBLER, INSTALLED DOUBLER PER SRM 53-10-4 FIG 27.Feb 24, 1999 · N411DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S990461Fitting · corrodedAT HMV2, FOUND CORROSION IN BORES AND MATING SEAM OF AFT RT WING AND FUS REMINAL FITTINGS. BLENDED CORROSION, CHECKED, REWORKED PER ERA 366788-14, INSTALLED BUSHNG.Feb 23, 1999 · N411DA · Boeing 727232 · Fuselage, Wing Attach FittingsSDR DL72S990398Frame · crackedOVERWING EXIT FRAME STA 761 RT, 784 LT AND 784 RT FOUND CRACKED IN I/B FLANGE. ACTION TAKEN, ERA 361976-14AD.Feb 23, 1999 · N411DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990397Skin · damagedLIGHTNING STRIKE DAMAGE AT AN EXISTING FASTENER IN THE SKIN BETWEEN S-7R AND S-8R AT STA 277. ACTION TAKEN, ERA 255827-14.Feb 23, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990367Skin · crackedLFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 460 INDICATED A SINGLE CRACK. INTERNAL HFEC INSPECTION CONFIRMED ONE CRACK ONLY AT FS 444. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAIRED PER THE B727 SRM 53-30-3, FIG 5. TEN FASTEFeb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990366Skin · crackedLFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL OF THE STRINGER 4R LAP SPLICE BETWEEN FS 360 AND 481. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL LENGTH. THE LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL LENFeb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990365Skin · crackedLFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN AT THE STRINGER 4R LAP SPLICE BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION VERIFIED 27 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG THE ENTIRE PANEL LENGTH AND RFeb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990364Skin · crackedLFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4R LAP SPLICE BETWEEN FS 481 AND 680. INTERNAL HFEC INSPECTION CONFIRMED 31 CRACKS ALONG THE PANEL LENGTH. THE LAP SPLICE WAS CUTOUT ALONG THE PANEL LENGTH AND REPAIRFeb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990363Skin · crackedLFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN AT THE STRINGER 4R LAP SPLICE BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION CONFIRMED 12 CRACKS ALONG THE LENGTH OF THE PANEL. THE LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL LEFeb 23, 1999 · N518DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990362Skin · crackedLFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 26L LAP SPLICE BETWEEN FS 480 AND 681. INTERNAL HFEC INSPECTION CONFIRMED A TOTAL OF 6 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIREFeb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990359Fire Loop · malfunctionedNR 2 ENG SHUT DOWN IN FLIGHT DUE TO FIRE WARNING. FIRST FIRE WARNING AFTER NR 2 ENGINE ANTI ICE TURNED ON. ACCOMPLISHED SHUTDOWN PROCEDURES FROM HARD CARD CHECKLIST. AFTER 1ST BOTTLE DISCHARGED LIGHT WENT OUT. LIGHT CAME ON AGAIN AFTER FIRE WARNING TEST, DFeb 23, 1999 · N539DA · Boeing 727232 · Fire DetectionSDR DL72S990357Actuator · failedSLC- AFTER T/O, LOST -A- SYSTEM HYDRAULIC SYSTEM. FOUND NR 2 L/E FLAP ACTUATOR LEAKING AND ACTUATOR BRACKET BROKEN. REPLACED SAME.Feb 23, 1999 · N495DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L990355Beacon · looseUPPER ROTATING BEACON CAME OUT OF ITS RETAINER AND FELL AND ROLLED BETWEEN CEILING PANEL AND OVERHEAD COMPARTMENT IN CABIN CAUSING A PASSENGERS BAG TO BE SCORCHED. NO OTHER DAMAGE. REINSTALLED BEACON, ALL CHECKED OK.Feb 23, 1999 · N513DA · Boeing 727232 · Exterior LightingSDR DL72S990372Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 4 CRACK INDICATIONS AT APPROX FS 1100 WITH NO OTHER CRACK INDICATIONS FOR THE ENTIRE PANEL LENGTH. THFeb 22, 1999 · N518DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990356Light · inopON LAYOVER CK, FOUND R-1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY PER M/M, CKS OK.Feb 22, 1999 · N403DA · Boeing 727232 · Emergency LightingSDR DL72S990352Switch · looseYELLOW AFT AIRSTAIR LIGHT CAME ON DURING TAKEOFF ROLL. FOUND SWITCH (P/N AN3167-1) LOOSE IN BRACKET (P/N 69-20985-6), REFERENCE IPC 52-70-00-49, ITEM 15 AND 20. TIGHTENED SWITCH, ADJUSTED SWITCH, CHECKS NORMAL.Feb 22, 1999 · N484DA · Boeing 727232 · Door Warning SystemSDR DL72S990349Wire · brokenEMERGENCY TRACK LIGHTING INOP FROM ROW 11 FWD. REPAIRED WIRES AS PER WDM 33-51-03 AND CHAP 20. FOUND POWER SUPPLY M9026 BAD. REPLD SAME, TRACK LIGHT OPN CKS NORMAL.Feb 22, 1999 · N539DA · Boeing 727232 · Light System WiringSDR DL72L990353Light · inopL2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS CHKS GOOD.Feb 22, 1999 · N511DA · Boeing 727232 · Emergency LightingSDR DL72K990383Stringer · crackedRT UPPER WING STRINGERS 13 AND 14 AT WS 629. CRACKED STRINGER TO RIB TAB. ACTION TAKEN, ERA 332815-14AD.Feb 22, 1999 · N417DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72K990382Stringer · crackedSTRINGER 29R CRACKED INCHES AFT OF STA 950E. DAMAGED STRINGER WILL BE TRIMMED OUT AND A NEW SECTION SPLICED IN. ACTION TAKEN, ERA 332797-14.Feb 22, 1999 · N417DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72K990381Skin · gougedFUSELAGE SKIN GOUGED JUST FWD OF L1 DOOR AT THE STRINGER 10L LAP SPLICE. GOUGE MEASURED 1 X 1. ACTION TAKEN, ERA 332816-14.Feb 22, 1999 · N417DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9900189Skin · crackedINSPECTION FOUND A 3.75 INCH CRACK IN RT ELEVATOR LOWER SKIN. REPAIRED IAW ECRA 5520-01207.Feb 22, 1999 · N511PE · Boeing 727232 · Elevator, Plate/SkinSDR DL72S990348Pump · failedB-SYSTEM HYD WENT TO 0, FOLLOWED PROCEDURES. WHEN GEAR EXTENDED HYD PRESS WENT TO 1700 PSI. OPERATED BRAKE INTERCONNECT, USED PNEUMATIC BRAKES TO STOP. TOWED ACFT TO GATE FROM RUNWAY. FOUND NR 2 B-HYD PUMP LEAKING. REPLACED SAME AND FITTINGS, LEAK CKS OK.Feb 21, 1999 · N407DA · Boeing 727232 · Hydraulic Pump (Electric/Engine), MainSDR DL72L990338Valve · inopAT FL250 ALTITUDE WARNING HORN WENT OFF WITH CABIN ALT AT 12,000 FT. CREW WENT ON 02, OUTFLOW VALVE SHOWED CLOSED. CARGO VALVE CLOSED, LT PACK OFF, DUE TO PREVIOUS WRITE UP. FOUND LT PACK VALVE INOP AND LT ACM NOT TURNING. REPLACED LT PACK VALVE AND ACM CFeb 19, 1999 · N503DA · Boeing 727232 · Cabin Cooling SystemSDR DL72K990333Vent Box · crackedFWD VENT BOX CRACKED AT AFT EAR TO RIB STA 686.5 ATTACH PT. CUT OUT ACCESS HOLE PER MM 57-13-0, FIG 803. DRILLED AFT AND FWD ANGLE ASSY AND RADIUS FILLER. HFEC CRACK, FOUND CRACK, RUNS FROM BOLT HOLE AFT AND OUTWARD TO EDGE OF FLANGE. DRILLED RADIUS FILLERFeb 19, 1999 · N417DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S990332Web · crackedRT INBOARD VERT TORQUE BOX WEB CRACKED AT UPPER FASTENER STA 1248 AND 1236. REPAIRED PER MM 53-11-0.Feb 18, 1999 · N405DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990751Skin · wornLOWER L/E SKIN WORN O/B END OF FLAP APPROX 6 INCHES LONG. REPAIRED PER MM 57-52-0 FIG 803.Feb 17, 1999 · N411DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S991362Spar · damagedAFT SPAR RAIL DAMAGED AT 2ND FROM I/B AFT FLAP TRACK CUT OUT. REPAIRED PER M/M 57-52-0 FIG 802.Feb 16, 1999 · N411DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S990313Battery Pack · dischargedOVERHEAD EXIT SIGN EMERGENCY LIGHT INOP ON TEST AT OVERWING EXITS. REPLACED M1094 RACK AND BATTERY PACK OP CKS OK. PARTS BORROWED FROM AMERICA WEST PACK LOCATED ABOVE ROW 19 RT SIDE OF CTR DUCT.Feb 16, 1999 · N419DA · Boeing 727232 · Emergency LightingSDR DL72S990312Battery Pack · dischargedLEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT MOST FWD INOP. REPLACED RACK AND BATTERY PACK, OP CKS OK.Feb 16, 1999 · N419DA · Boeing 727232 · Emergency Lighting
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