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 DL72L002040Frame · crackedCHANNEL WORN/DAMAGED ALONG LWR FLANGE 5 O CLOCK TO 6 O CLOCK POSITION AT NR 2 ENG FWD COWL CUTOUT. REPAIRED PER MM 53-11-0 PG 801.Oct 17, 2000 · N504DA · Boeing 727232 · Nacelle/Pylon, Main FrameSDR DL72S002030Battery · inoperativeEMERGENCY EXIT LIGHT NOT HOLDING CHARGE. REPLACED BATTERY.Oct 16, 2000 · N532DA · Boeing 727232 · Emergency LightingSDR DL72S002028Engine · bird strikeDURING TAKEOFF, A/C SUFFERED BIRD STRIKE, FODDING OUT NR 1 ENGINE. REPLACED ENGINE.Oct 16, 2000 · N407DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72L002023Beam · corrodedLT MLG BEAM LWR T/E PANEL ATTACH BORES CORRODED. HOLES 35, 29, 27, 26, 25 REAMED TO .312 PER SRM 57-40D. 28 REAMED TO .359 PER SRM 57-40D. REAMED 10 8 TO .312 PER SRM 57-40D. BHEC INSPECT OF FASTENER HOLE FOR CRACKS AND CORROSION. NO ITEM, TURNED O/D ON Oct 16, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L010887Angle · crackedDURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED ON THE MID FLAP. THE CHORD ANGLE WAS REPAIRED PER 727 M/M 57-52-0, FIG 802 BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER.Oct 13, 2000 · N508DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L002095Skin · corrodedLOWER SECTION OF BONDED DOUBLER FOUND DISBONDED BELOW THE AFT LAV SERVICE PANEL CUTOUT. 396323-14 REV A.Oct 13, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S002022Door Frame · crackedTHE INNER CHORD OF THE FWD FRAME ON THE C1 DOOR OPENING WAS FOUND WITH A .5 INCH CRACK IN THE VERTICAL FLANGE OF THE INNER CHORD JUST ABOVE THE NR 3 DOOR STOP FITTING. THE CRACK WAS ROUTED OUT OF THE FLANGE AND REPAIRED WITH TWO ALUMINUM REPAIR ANGLES IOct 13, 2000 · N515DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L002004Light · inoperativeON LAYOVER FOUND ESCAPE PATH LIGHTING INOP AT SEAT 3AB. FOUND PIN PULLED ON CABLE UNDER SEAT. RESET PIN, OPS CKS GOOD.Oct 13, 2000 · N507DA · Boeing 727232 · Emergency LightingSDR DL72S001990Isolation Valve · chafedWHILE TROUBLESHOOTING WING ANTI-ICE PROBLEM FOUND RIGHT BLEED AIR ISOLATION VALVE WIRING CHAFING ON PNUEMATIC DUCT BETWEEN THE VALVE AND THE AFT PACK VALVE. WHILE INSTALLING PNUEMATIC DUCT FOUND WIRE BUNDLE FOR LEFT BLEED ISOLATION VALVE CHAFED. REPAIRED WIROct 12, 2000 · N535DA · Boeing 727232 · Airfoil Anti/De-ice SystemSDR DL72S001983Skin · debondedFROM B-2 LTR CK N/R 63, NR 9 SPOILER PANEL UPPER SURFACE DISBONDED AT FWD I/B CORNER. REPAIRED PER SRM 57-50-6.Oct 11, 2000 · N527DA · Boeing 727232 · SpoilersSDR DL72L001972Beam · corrodedRT MLG SUPPORT BEAM BORES CORRODED. TASK: C57-581-01.01 FASTENER BORES CORRODED AT HOLES 3, 4, 5, 11, 12, 26, 27, 30, 31, 32, 36 & 38. REWORK HOLES PER DRD 57-40D. 3, 4, 5, 11, 26, 30, 31, 32, 36 REAMED TO 0.358. 27, 12, 13 REAMED TO 0.262. 38 REAMED TO 0Oct 11, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S001995Frame · chafedNR 2 ENG CUTOUT FRAME LIP WORN THROUGH 9:00 POS STA 1352. REPAIRED PER MM 53-11-0 PG 801.Oct 10, 2000 · N515DA · Boeing 727232 · Nacelle/Pylon, Main FrameSDR DL72L001975Mount · crackedROUTINE HFEC BOLT HOLE INSPECTIONS OF THE NR 3 ENGINE PYLON FWD ENGINE MOUNT SUPPORT FITTING REVEALED A CRACK INDICATION IN HOLE G. THE CRACKING IS TYPICAL OF BAC S/B 727-54A0010AND AD 97-05-08. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND A .0312 INCH INSOct 10, 2000 · N507DA · Boeing 727232 · Nacelle/Pylon, Attach FittingsSDR DL72S001974Sill · corrodedTHE LOWER DOOR SILL OF THE C2 DOOR OPENING WAS FOUND WITH CORROSION ON THE OUTER FLANGE OF THE OUTBOARD CHORD BETWEEN FS 950E & 990. CLEANUP OF THE CORROSION RESULTED IN A 4.5 INCH FLANGE TRIMOUT, A 2.5 INCH TRIMOUT AND SEVERAL BLEND LOCATIONS. THE BLENDSOct 10, 2000 · N515DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L001973Fitting · crackedROUTINE INSPECTIONS OF THE LT AND RT WING LEADING EDGE SLAT DOWNSTOP FITTINGS REVEALED A BROKEN BOLT IN A FITTING FOR THE NR 6 SLAT. THE CONDITION IS TYPICAL OF BAC S/B 727-57-171AND AD 94-07-08. THE DOWNSTOP FITTINGS OF THE NR 6 SLAT WERE MODIFIED PER THEOct 10, 2000 · N506DA · Boeing 727232 · Leading Edge DevicesSDR DL72S001967Light · inoperativeCOCKPIT EMERGENCY LIGHT WILL NOT ILLUM. REPLACED SAME.Oct 10, 2000 · N411DA · Boeing 727232 · Emergency LightingSDR DL72L002131Plate · corrodedAT HMV, THE VERT STAB TENSION TIE PLATE AFT CTR ATTACH POINTS WERE CORRODED AROUND FACE AND IN BORES. REMOVED CORR DYE PEN CK GOOD WITHIN LIMITS PER SRM 55-30-5D FIG 801D. REAMED HOLES TO .691 TI REM CIRR BHEC INSP NO ITEMS OPENED HOLES TO .737 BFEC INSP NO Oct 9, 2000 · N508DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72L002020Rib · crackedAT HMV THE NR 11 RIB FLANGE OF THE NR 3 SLAT WAS FOUND TO BE CRACKED. ROUTED OUT DAMAGE, FABRICATED REPAIR PARTS PER MM 57-54-0, REPAIRED PER MM 57-54-0.Oct 9, 2000 · N508DA · Boeing 727232 · Leading Edge DevicesSDR DL72L002021Shim · shiftedAT HMV THE SHIMS WERE FOUND MIGRATING AT NR 12 SPOILER ACTUATOR LOWER ATTACH BOLT SHIMS. REPAIRED SHIMS AND C/W MM 57-54-0.Oct 8, 2000 · N508DA · Boeing 727232 · SpoilersSDR DL72L002052Stringer · crackedAT HMV, THE FIFTH STRINGER AFT OF FRONT SPAR STA 171.5 WAS FOUND TO BE CRACKED. REMOVED DAMAGE PER SRM 57-10-5D FIG 802D. PERFORMED HFEC PER SRM 57-10-5D FIG 802D, NO IND. TREATED AND PAINTED PER SRM 57-10-5D FIG 802D. FABRICATED REPAIR PARTS PER SRM 57-10Oct 6, 2000 · N508DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72L002019Rib · crackedAT HMV THE NR 13 RIB OF THE NR 3 SLAT WAS FOUND TO BE CRACKED. ROUTED OUT DAMAGE FOR FABRICATED DOUBLER. REPAIRED PER MM 57-54-0.Oct 6, 2000 · N508DA · Boeing 727232 · Leading Edge DevicesSDR DL72L002018Rib · crackedAT HMV NR 7 RIB OF SLAT FOUND TO BE CRACKED. REMOVED LWR AFT SPAR REPAIR DOUBLER IN AREA, FABRICATED REPAIR DOUBLER PER MM 57-54-0, ROUTED OUT DAMAGE, INSTALLED DOUBLER AND FILLER PER MM 57-54-0, REINSTALLED SPAR DOUBLER.Oct 6, 2000 · N508DA · Boeing 727232 · Leading Edge DevicesSDR DL72L002084Web · crackedAT HMV, THE WEB ON THE VERTICAL FIN WAS FOUND CRACKED. REMOVED FASTENERS AND BEGAN FABR DOUBLER PER SRM 53-10-4D FIG 802D. STOP DRILLED CRACKS, COMPLETED FABR OF DOUBLER, DYE CKED, INSTALLED DOUBLER PER SRM 53-10-4D FIG 802D.Oct 5, 2000 · N508DA · Boeing 727232 · Vertical StabilizerSDR DL72L002083Flange · bentAT HMV, THE AFT FLANGE OF THE NR 2 INLET WAS TORN/BENT. REMOVED DAMAGE PER SRM 54-10-3D FIG 801D. DYE CKED, NO FURTHER DAMAGE NOTED. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 54-10-3D FIG 801D.Oct 5, 2000 · N508DA · Boeing 727232 · Turbine Engine Air Inlet SectionSDR DL72L001982Cowling · wornAT HMV FOUND NR 2 ENG COWL RING WORN NR 2 FWD COWL, 5 O''CLOCK TO 7 O''CLOCK NO ED FOR RIVETS. REMOVED EXISTING REPAIR, FABD NEW REPAIR PER MM 53-11-0 PG 801, INSTALLED NEW COWL RING PER MM 53-11-0 PG 801, APPLIED TEFLON COATING PER PS 900-3-1, 04.Oct 5, 2000 · N508DA · Boeing 727232 · Engine Cowling SystemSDR DL72L001981Frame · crackedAT HMV FOUND FORMER CRACKED, STA 600, LBL 10. ROUTED OUT CRACK PER SRM 53-10-4D FIG 811D, FABD REPAIR, T/P PER SRM 51-40-3, INSTALLED PER SRM 51-40-3.Oct 5, 2000 · N508DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L001963Beam · corrodedAT HMV FOUND RT MLG SUPPORT BEAM BORES CORRODED. FASTENER BORES CORRODED AT HOLES, 17/18/19/22/23/24/39/40/41/42/43/44/45/46. REWORKED CORRODED HOLES PER DRD 57-40D FIG 803D, ALL HOLES ARE 0.312, BHEC INSP OF HOLES LISTED PER DRD 57-40D, SHOWS NO ITEMS.Oct 5, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L001962Beam · corrodedAT HMV BHEC OF BEAM NR HOLE 25 ON RMLG SUPPORT BEAM SHOWS CORROSION IN HOLES. REWORK HOLE NR 25 PER DRD 57-40D FIG 803D, NR 25 0.358, BHEC INSP OF HOLE PER DRD 57-40 CKD OK, MECH AND TREATED BUSHINGS PER SRM 57-40D INSTALLED BUSHING PER SRM 57-40D PG 14, STEOOct 5, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L001941Flap Track · corrodedDURING OVERHAUL AT BFGOODRICH, SEVERAL AREAS OF THE I/B FLAP, NR 4 I/B TRACK WERE FOUND WITH CORROSION/WEAR WHICH WERE BEYOND ALLOWABLE LIMITS. AFFECTED AREAS INCLUDE THE MLG BEAM ATTACH HOLES AND SPOTFACE, THE SPOILER BEAM ATTACH HOLES, THE MLG DOOR AFT HINGOct 5, 2000 · N508DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L001940Flap Track · corrodedDURING OVERHAUL OF THE I/B FLAP, I/B TRACK ASSY, TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS, AND WEAR AT THE FWD ATTACH LUGS, MLG DOOR HINGE FITTING ATTACH HOLES, SPACER BLOCK ATTACH HOLES, AND CLIP ASSY ATTACH HOLES, AT THE MLG BOct 5, 2000 · N508DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L001980Bolt · looseAT HMV FOUND LW NR 4 SPOILER ACTUATOR MOUNT HAS LOOSE BOLTS ON BOTTOM OF WING SPAR TO MOUNT BOLTS. TIGHTENED NUT.Oct 4, 2000 · N508DA · Boeing 727232 · SpoilersSDR DL72L001965Actuator · looseAT HMV THE NR 3 SPOILER ACTUATOR WAS FOUND TO HAVE LOOSE MOUNT BOLTS ON BOTTOM ATTACHED TO REAR SPAR. REPAIRED PER MM 57-42-0.Oct 4, 2000 · N508DA · Boeing 727232 · Drag Control ActuatorSDR DL72L001945Mount · looseAT HMV FOUND NR 1 SPOILER MOUNT BOX ATTACHED TO REPAIR SPAR IS LOOSE AT BOTTOM BOLTS. REPAIRED PER MM 57-42-0.Oct 4, 2000 · N508DA · Boeing 727232 · SpoilersSDR DL72S001931Door Frame · crackedTHE FWD FRAME OF THE C1 DOOR CUTOUT WAS FOUND WITH TWO SMALL CRACKS IN THE WEB AND ONE CRACK IN THE INNER CHORD. A .375 INCH CRACK WAS FOUND IN THE WEB BETWEEN STOPS 1 & 2. A .75 INCH CRACK WAS FOUND IN THE WEB JUST BELOW STOP NR 6. A .5 INCH CRACK WAS FOUNOct 2, 2000 · N515DA · Boeing 727232 · Fuselage Main, StructureSDR DL72L001927Battery Pack · dischargedDURING MORNING EMERGENCY LIGHTS TEST, WHEN SELECTED ON, LIGHTS ILLUMINATED THEN WENT DIM AND FINALLY OFF. REPLACED BATTERY PACKS. S/N OFF 73729, 32333, 24513, 10662, 12950, YA8852, 4671, 72867, 3467, 7428, 65522, 9956. MAN P/N OF AOct 2, 2000 · N509DA · Boeing 727232 · Emergency LightingSDR DL72L001925Oxygen Mask · disconnectedS/O OXYGEN MASK HEAD PIECE DISCONNECTED FROM HOSE. REPLACED O2 MASK ASSY, OPS CHECK OK.Oct 2, 2000 · N510DA · Boeing 727232 · Crew Oxygen SystemSDR DL72K001908Battery · dischargedFLASHLIGHT BATTERY DEAD.Sep 30, 2000 · N414DA · Boeing 727232 · Emergency EquipmentSDR DL72S001905Light · inoperativeCENTER AISLE EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT, CHECKS GOOD.Sep 29, 2000 · N540DA · Boeing 727232 · Emergency LightingSDR DL72S001903Warning System · false indicationDISCONTINUED T/O AFTER LEFT BOTTLE DISCHARGE LIGHT CAME ON. VERIFIED BOTH ENG FIRE EXT BOTTLE PRESSURES ALL NORMAL. LIGHT WENT OUT DURING LIGHT TEST. REPLACED LEFT ENGINE FIRE BOTTLE.Sep 29, 2000 · N527DA · Boeing 727232 · Extinguishing SystemSDR DL72S001994Angle · corrodedSKIN SUPPORT ANGLE CORRODED FS 740 STR 27R. REPAIRED PER MM 53-11-0 PG 859.Sep 28, 2000 · N515DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S001878Compressor · stalledAFTER T/O, THE NR 3 ENGINE COMPRESSOR STALLED FOLLOWED BY AN ELECTRICAL SMELL IN CABIN. INSPECTED AND RAN ENGINE, NO TROUBLE FOUND.Sep 26, 2000 · N542DA · Boeing 727232 · Turbine Engine Compressor SectionSDR DL72S001870Rib · crackedA 1 INCH CRACK AT NR 3 SLAT I/B NOSE RIB AT SLAT ACTUATOR ROD END BOLT. REPAIR PER M/M 57-54-0 FIG 814.Sep 26, 2000 · N515DA · Boeing 727232 · Leading Edge DevicesSDR DL72S001844Battery Pack · inoperative1L DOOR LIGHT WILL NOT DISARM. REPLACED LIGHT ASSY/BATTERY PACK. OPS CKS GOOD.Sep 22, 2000 · N420DA · Boeing 727232 · Emergency LightingSDR DL72S001856Bulb · failedR-1 DOOR AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED R-1 AFT EXTERIOR LIGHT, OPS CKS GOOD.Sep 21, 2000 · N499DA · Boeing 727232 · Exterior LightingSDR DL72S001796Transmitter · inoperativeOUTBOARD FLAP INDICATIONS SPLIT AT 15 DEG CAUSING A LOCKOUT. ALT FLAP EXTEND USED. INDICATORS BOUNCE BETWEEN SPLIT AND EQUAL SETTINGS. NO ROLL TENDENCIES WERE FELT WHEN FLAPS WERE EXTENDED. REPLACED LEFT OUTBOARD FLAP TRANSMITTER PER M/M. FLAP IND AND OPESep 17, 2000 · N406DA · Boeing 727232 · Trailing Flap Position Indicating SystemSDR DL72L001795Battery · dischargedAFT CABIN FLASHLIGHT IS NOT BLINKING. REPLACED BATTERY, CK OK.Sep 17, 2000 · N501DA · Boeing 727232 · Emergency EquipmentSDR DL72S001794Fuse · failedWHILE TESTING EMERGENCY LIGHTS FOUND FIRST CLASS LIGHTS NOT WORKING. FOUND FUSE BAD IN F/C BATTERY PACK. REPLACED FUSE, CKS OK.Sep 17, 2000 · N402DA · Boeing 727232 · Emergency LightingSDR DL72S001793Light · inoperativeEMERGENCY LIGHT AT 22D INOP. LIGHTS DISCONNECTED UNDER SEAT. RECONNECTED AFT MODULE PULLED AWAY FROM SEAT. INSTALLED NEW MODULE. CKS OK.Sep 17, 2000 · N402DA · Boeing 727232 · Emergency LightingSDR DL72K001789Battery Pack · malfunctionedDOOR 2R EMERGENCY EXIT LIGHT FLASHED WHEN TESTED. REPLACED BATTERY PACK, OPS CKS NML.Sep 15, 2000 · N525DA · Boeing 727232 · Emergency LightingSDR DL72K001788Helicoil · backed outNR 1 ENG WAS SHUT DOWN DURING CRUISE DUE TO ZERO OIL QTY AND LOW OIL PRESSURE. OCCURRED AT FL 200 WHEN WE LEVELED OFF. FOUND BUSHING/HELICOIL PULLED OUT OF GEARBOX AT LP6 DRAIN TUBE ABOVE OIL FILTER. REPLACED SAME, RAN ENGINE PER PFHB CKS GOOD.Sep 15, 2000 · N417DA · Boeing 727232 · Turbine Engine Reduction Gear
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