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 CAL951096Floor Panel · corrodedTHE RIGHT FLOOR SUPPORT PANEL WAS FOUND CORRODED IN THE AFT CARGO COMPARTMENT AT BS 950-950F. THE FLOOR SUPPORT PANEL WAS REMOVED. A NEW FLOOR SUPPORT PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-6, AND 51-10-2. (M)Nov 8, 1995 · N77780 · Boeing 727232 · Fuselage Floor PanelSDR CAL951085Frame · corrodedINSPECTION FOUND AIRCRAFT BAY AFT FRAME CORRODED AT PANEL NR 3458R, BS 740. THE CORRODED SECTION OF FRAME WAS REMOVED. AN L-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M)Nov 8, 1995 · N77780 · Boeing 727232 · Fuselage Main, FrameSDR DL72S954273Battery · dischargedAFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERY, CHECKS NORMAL.Nov 7, 1995 · N419DA · Boeing 727232 · Emergency LightingSDR DL72L954359Skin · crackedFOUND ON CV2 CHECK, .25 INCH CRACK IN NR 5 SLAT COVE SKIN AT CUTOUT FOR I/B STOP PAD. REPAIRED PER SRM 57-50-3 FIG 23.Nov 7, 1995 · N509DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954453Rib · crackedDURING ACCOMPLISHMENT OF EO 4-58560-3AD, A CRACK WAS DISCOVERED IN THE VERTICAL FLANGE OF THE LBL 70.5 WING RIB CHORD. THE CRACK RAN FROM ONE OF THE UPPER FASTENERS IN THE VERTICAL FLANGE AT STA 760.95 DOWN TO THE HORIZONTAL FLANGE. THIS CRACK REQUIRES AN ALTNov 6, 1995 · N490DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S954259Angle · crackedDURING F-1 LETTER CHECK, FOUND .375 INCH CRACK AND 1 INCH CRACK, NR 7 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54-0.Nov 6, 1995 · N401DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954258Battery · dischargedFWD OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS NORMAL.Nov 6, 1995 · N489DA · Boeing 727232 · Emergency LightingSDR DL72S954257Battery · dischargedFWD BULLNOSE EMERGENCY LIGHT INOP. REPLACED RACK M1088 AND BATTERIES, ALL CKS NORMAL.Nov 6, 1995 · N489DA · Boeing 727232 · Emergency LightingSDR DL72S954255Battery · dischargedCENTER SECTION OF FLOOR EMERGENCY EXIT LIGHTS INOP. REPLACED RACK M9026 AND BATTERIES, ALL CKS NORMAL.Nov 6, 1995 · N489DA · Boeing 727232 · Emergency LightingSDR DL72S954252Actuator · crackedA-SYS HYD FAILURE AFTER GEAR SELECTED UP. A-SYS QTY WAS FLUX AT THE ZERO MARK. FOUND LT MLG DOOR ACTUATOR CRACKED. REPLACED SAME, OPERATION NORMAL.Nov 6, 1995 · N400DA · Boeing 727232 · Landing Gear ActuatorSDR DL72L954246Bulb · failedON LAYOVER, LEFT AFT OVERWING EMERGENCY LIGHT INOP. RELAMPED AND CKS NORMAL.Nov 6, 1995 · N508DA · Boeing 727232 · Emergency LightingSDR CAL951100Intercostal · corrodedINSPECTION FOUND CORROSION ON INTERCOSTAL AT BS 1130-1148, LT SIDE. THE INTERCOSTAL WAS REMOVED. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M)Nov 4, 1995 · N77780 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960426Frame · crackedDURING INSPECTION, A 2 INCH CRACK WAS FOUND EMANATING FROM THE CORNER OF THE UPPER HINGE CUTOUT ON THE FWD FRAME OF THE LT AFT SERVICE DOOR. IN ACCORDANCE WITH B727 SRM 52-40-2 FIG 4, A DOUBLER WAS INSTALLED AROUND THE DAMAGE.Nov 3, 1995 · N490DA · Boeing 727232 · Service DoorsSDR MZZA95049Actuator · brokenFLT NR 917 - GUM - ON CLIMB-OUT, LOST A-SYSTEM HYDRAULICS, CREW SHUT DOWN SYSTEM A-PUMPS PRIOR TO COMPLETE HYDRAULIC FLUID LOSS. AIRCRAFT DIVERTED BACK TO GUAM. MAINTENANCE FOUND NR 1 LED SLAT ACTUATOR LEAKING FLUID AND REPLACED ACTUATOR PER MM 27-81-04. SYNov 2, 1995 · N15790 · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S954498Doubler · crackedDURING HMV SHOP INSP, NR 3 MIDFLAP AFT SPAR CHORD DOUBLER CRACKED AT I/B AFT FLAP TRACK. REPAIRED PER MM 57-52-0 PAGE 807.Nov 2, 1995 · N516DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S954497Spar · crackedDURING HMV INSP, NR 3 MIDFLAP WAS FOUND WITH AFT SPAR CHORD CRACKED AT I/B QUADRANT CUTOUT. REPAIRD PER MM 57-52-0 PAGE 807.Nov 2, 1995 · N516DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S954220Eel Module · brokenEMERGENCY FLOOR TRACK MISSING IN FLOOR TRACK AT SEAT 10 C. REPLACED EMERGENCY PATH LIGHT HOLDER MODULE AND BULB, OPERATION NORMAL.Nov 2, 1995 · N520DA · Boeing 727232 · Emergency LightingSDR DL72K961608Transverse Beam · crackedCRACKS ON THE LOWER TORQUE BOX AT FS 1263. THE CRACKS ARE ON THE FORWARD RT SIDE TRANSVERSE BEAM AND THE RT VERTICAL WEB. THE RT VERTICAL WEB HAS A 1 INCH CRACK AT THE FUEL LINE CUTOUT. NORMALLY, THE FUEL LINE IS REMOVED AND THE REPAIR DOUBLER (65-17517-31,Nov 2, 1995 · N474DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K954265Skin · corrodedAT LETTER CHECK IN TPA, CORROSION WAS DISCOVERED ON THE UPPER SKIN AT THE S-24R LAP JOINT THAT WARRANTED A 12.5 INCH BY 3 INCH CUT OUT, BETWEEN STA 294.5 AND STA 312 BY MTC. THIS ER/A WILL REPAIR THE DAMAGED AREA PER SRM 53-30-3 FIG 14 DETAIL 4 WITH THE VARIANov 2, 1995 · N474DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K954264Side Wall · crackedDURING LETTER CHECK AT TPA, TWO .25 CRACKS WERE DISCOVERED IN THE .040 2024-T3 CLAD RIGHT SIDE WALL OF THE NOSE LANDING GEAR WHEEL WELL APPROX STA 277.0. THIS ER/A PROVIDES REPAIR OF CRACK DAMAGE AND INSTALLATION OF A MOD STRAP AT DAMAGE LOCATION, AD 90-06-09Nov 2, 1995 · N474DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL951041Splice · corrodedINSPECTION FOUND STRINGER SPLICE CORRODED AT BS 965 IN AFT BAGGAGE BIN. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW STRINGER SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3. (X)Nov 2, 1995 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL951040Lap Seam · corrodedINSPECTION FOUND CORROSION ON SKIN AT LAP SEAM AT BS 660 AND STR 30. THE CORROSION WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X)Nov 2, 1995 · N10791 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CAL951039Skin · corrodedINSPECTION FOUND CORROSION ON SKIN AT LAP SEAM FORWARD OF CARGO DOOR, STA 540. THE CORRODED SECTION WAS CUT OUT. A FILLER AND DOUBLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 53-30-3. (X)Nov 2, 1995 · N10791 · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S954493Doubler · crackedNR 2 MIDFLAP WAS FOUND TO HAVE CRACKED DOUBLER AT AFT LOWER SPAR ANGLE REPAIR AT I/B QUADRANT CUTOUT. REPAIR WAS PERFORMED PER M/M 57-52-0 FIG 802. FOUND DURING SHOP MTC VISIT.Nov 1, 1995 · N490DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S954216Battery · dischargedAFT AIRSTAIR EMER LIGHT INOP. REPLACED BATTERY, OPERATION NORMAL.Nov 1, 1995 · N418DA · Boeing 727232 · Emergency LightingSDR DL72L954215Battery Pack · dischargedMID CABIN CENTER AISLE AND RT OVERWING EMERGENCY EXIT, EMERGENCY LIGHTS INOP. REPLACED BATTERIES, OPERATION NORMAL.Nov 1, 1995 · N506DA · Boeing 727232 · Emergency LightingSDR DL72K954219Skin · crackedFOUND ON A2 LETTER CK, 1 INCH CRACK AT FASTENER NUMBER 2 ENGINE INLET OUTER SKIN LT SIDE FWD OF SADDLE PANEL. REPAIRED PER MM 54-30-0.Nov 1, 1995 · N474DA · Boeing 727232 · Nacelle/Pylon, Plate/SkinSDR DL72K954218Web · crackedFOUND ON A2 LETTER CK, 1 INCH CRACK IN TORQUE BOX WEB LT SIDE FWD END ALONG UPPER ROW OF RIVETS. REPAIRED PER MM 53-11-0.Nov 1, 1995 · N474DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K954217Angle · crackedFOUND ON A2 LETTER CK, .25 INCH CRACK NR 2 SLAT TAI DUCT CUTOUT. REPAIRED PER MM 57-54-0.Nov 1, 1995 · N474DA · Boeing 727232 · Leading Edge DevicesSDR CAL951103Skin · corrodedINSPECTION FOUND CORROSION ON SKIN AT BS 294, RBL 16, STRINGER 22R. THE SKIN WAS REPAIRED IAW SRM 51-10-6, 51-10-2, AND 51-30-2. (M)Nov 1, 1995 · N77780 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CAL951097Intercostal · corrodedINSPECTION FOUND THE INTERCOSTAL CORRODED AT BS 680-700 AND STRINGER 27R. THE INTERCOSTAL WAS REMOVED AND THE CORROSION WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M)Nov 1, 1995 · N77780 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL951088Threshold · corrodedINSPECTION FOUND CORROSION AT FORWARD CARGO DOOR THRESHOLD, STATION 560. THE CORROSION WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M)Nov 1, 1995 · N77780 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K954156Battery · dischargedR1 DR OVERHEAD E-PATH LIGHT INOP. REPLACED BATTERIES. CKS NORMAL.Oct 31, 1995 · N481DA · Boeing 727232 · Emergency LightingSDR CAL951104Doubler · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RIB DOUBLER WS 656.50, NR 3 FUEL TANK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-10-5. (M)Oct 31, 1995 · N77780 · Boeing 727232 · Wing Miscellaneous StructureSDR CAL951099Stringer · corrodedINSPECTION FOUND CORROSION ON FLOOR SUPPORT STRINGER NR 9 AT BS 1030-1166. THE CORRODED SECTIONS WERE REMOVED. L-ANGLES AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2. (M)Oct 31, 1995 · N77780 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL951093Frame · corrodedCORROSION WAS FOUND AT STATION 1130 FRAME DURING INSPECTION ON RIGHT FUSELAGE WALL. THE CORROSION EXTENDED ABOVE AND BELOW FLOOR LEVEL. THE CORRODED SECTION WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51-10-2, AND 53-10-4. (M)Oct 31, 1995 · N77780 · Boeing 727232 · Fuselage Main, FrameSDR CAL951090Doubler · crackedINSPECTION FOUND A 1 INCH CRACK IN DOUBLER ON AFT SIDE OF BS 826 LATERAL FLOOR BEAM WEB, LBL 54. THE CRACK WAS STOP DRILLED. A WEB REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M)Oct 31, 1995 · N77780 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL951087L-Angle · crackedINSPECTION FOUND A .75 INCH CRACK IN ATTACH L-ANGLE AT LEFT BS 804 LATERAL FLOOR BEAM WEB TO LBL 46 LONGITUDINAL FLOOR BEAM WEB. THE CRACK WAS LOCATED AT THE LIGHTENING HOLE ON AFT SIDE. THE CRACK ANGLE WAS REMOVED. A NEW L-ANGLE WAS FABRICATED AND INSTALLEOct 31, 1995 · N77780 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL951086Floor Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN LATERAL FLOOR BEAM WEB AT CABLE PASS THROUGH, BS 840, LBL 54. THE CRACK WAS STOP DRILLED. A WEB REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M)Oct 31, 1995 · N77780 · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S954145Stringer · crackedFOUND DURING HMV, RT OUTER WING UPPER STRINGER TO RIB SHOWS CRACK INDICATION ON FASTENER HOLE AT W.S. 656.5, STRINGER 10. MANUFACTURED REPAIR DOUBLER PER M/M 57-13-0 AND INSTALLED DOUBLER PER M/M 57-13-0, PG. 801.Oct 30, 1995 · N490DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S954143Rib · crackedFOUND ON HMV, RIGHT WING STRINGER TO RIB FASTENER HOLE HAS CRACK INDICATION AT STA. 629, 3RD STRINGER FWD FROM AFT SPAR. STOP DRILLED CRACK PER M/M 57-13-0.Oct 30, 1995 · N490DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S954134Skin · puncturedDURING INSPECTION, C-3 CARGO DOOR WAS FOUND WITH INNER SKIN PUNCTURED, REPAIRED PER SRM 52-00-3.Oct 30, 1995 · N490DA · Boeing 727232 · Cargo/Baggage DoorsSDR DL72K954150Battery Pack · dischargedLEFT LOWER AFT BODY FAIRING E-PATH LIGHT INOP. REPLACED BATTERY PACK AT APPROX ROW 23ABC. E-PATH LIGHT CKS NORMAL.Oct 30, 1995 · N474DA · Boeing 727232 · Emergency LightingSDR CAL951105Door Frame · crackedINSPECTION FOUND A 6 INCH CRACK IN AFT ENTRY DOOR FRAME ON LEFT SIDE BETWEEN THIRD AND FOURTH DOOR STOP FROM BOTTOM. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M)Oct 30, 1995 · N77780 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL951095Stringer · crackedINSPECTION FOUND A 2 INCH IN THE STRINGER FLANGE AT LT WS 629. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-4, 51-10-2, AND 51-20-4. (M)Oct 30, 1995 · N77780 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CAL951094Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN LEFT WING STRINGER FLANGE AT WS 656.5. THE CRACK WAS STOP DRILLED. REPAIR CHANNELS WERE FABRICATED AND INSTALLED IAW SRM 57-10-4, 51-10-2, AND 51-20-4. (M)Oct 30, 1995 · N77780 · Boeing 727232 · Wing, Longeron/StringerSDR DL72S954268Skin · corrosionCORROSION AT AN EXISTING EXTERNAL REPAIR DOUBLER ON THE LOWER FUSELAGE SKIN PANEL, BETWEEN BS 259.5 AND BS312, AT STRINGER 20R. REMOVAL OF THE DOUBLER REVEALED EXTENSIVE CORROSION DAMAGE. THE SKIN WAS TRIMMED TO REMOVE CORROSION DAMAGE BELOW THE FORWARD LAVAOct 29, 1995 · N484DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S954129Skin · dentedDURING INSPECTION, FOUND LEFT OUTBOARD AILERON WITH DENTS IN UPPER SKIN. ACCOMPLISHED REPAIRS PER SRM 57-50 -5.Oct 29, 1995 · N490DA · Boeing 727232 · AileronsSDR DL72L954319Eel Charger · malfunctionedON PREFLIGHT, EMERGENCY EXIT LIGHTING BATTERY CHARGER POPS CIRCUIT BREAKER. T/S SYS REPLACED BATT CHARGER C/B AND SPLICE SM17 WDM 33-51-02 PG 5, OPERATION NORMAL.Oct 29, 1995 · N505DA · Boeing 727232 · Emergency LightingSDR DL72L954131Battery · dischargedAFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERIES. CKS NORMAL.Oct 29, 1995 · N502DA · Boeing 727232 · Emergency Lighting
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