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 95FDEA01891Frame · dentedDENT IN FRAME AT BS 560, LBL 38, WL 162. REPAIRED DENT IN FRAME IAW FEDEX SRM 51-40-3. C/A ADDITION.Dec 12, 1995 · N498FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01879Stringer · wornVERTICAL FIN, BAY NR 9 FIN STA 180.6, STR 7R, WORN FASTENER HOLE AT THE RIB CHORD AND STR. REPAIRED WORN RIB CHORD AND STR PER FEDEX SRM 55-30-4, FIG 1 AND FEDEX EA 7-5510-26736. C/A ADDITION.Dec 12, 1995 · N498FE · Boeing 727232 · Vertical StabilizerSDR 95FDEA01801Beam · corrosionCORROSION AT BS 930 BEAM LOWER CHORD LBL 46-LBL 52, WL 201. REMOVED CORROSION AT BS 930 LOWER CHORD, LBL 46-LBL 52, WL 201. AREA WITHIN LIMITS PER BAC DRAWING 65-19872-3. C/A ADDITION.Dec 12, 1995 · N498FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 95FDEA01800Stringer · corrodedCORROSION (C53-224-01) ON STR 5R, BS 600-740. REPAIRED OUT OF LIMITS AREA IAW FEDEX EA 7-5310-26724A. C/A ADDITION.Dec 12, 1995 · N498FE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR 95FDEA01798Stringer · corrodedCORROSION (C53-224-04) ON STR 6R, BS 1133 AND BS 1139. REMOVED DAMAGED AREA AND REPAIRED STR IAW FEDEX EA 7-5310-26724.Dec 12, 1995 · N498FE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S954740Rib · crackedFOUND ON CV2 CHECK, .75 INCH CRACK PAST PREVIOUS STOP DRILL I/B NOSE RIB AT ACTUATOR ROD END ATTACH NR 4 SLAT. REPAIRED RIB PER M/M 57-54-0 PAR 4, NR 4 SLAT.Dec 11, 1995 · N531DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954730Skin · crackedFOUND ON CV2 REWRITTEN FROM N/R 1, .25 INCH CRACK ON PNEUMATIC AIR ACCESS DOOR CUTOUT AFT I/B END. REPAIRED PER M/M 53-30-0.Dec 11, 1995 · N531DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S954711Stringer · crackedFROM ATL HMV: REF OPN 8602AD HFEC INSP. RT WING OUTER UPPER STRINGER TO RIB INSP. CRACK IND. W.S. 686.50 AFT VENT BOX FWD TAB. CORRECTION: STOP DRILLED CRACK AND INSTALLED REPAIR PER MM 57-13-0, FIG 804.Dec 11, 1995 · N496DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S954704Eel Power Pack · inoperativeEMERGENCY LIGHT TRACKS BETWEEN SECTION 12A AND 19A. REPLACED EMERGENCY PACK POWER SUPPLY AND BATTERY PACK CHECKS OK.Dec 11, 1995 · N526DA · Boeing 727232 · Emergency LightingSDR 95FDEA01890Blkhd Skin · dentedWHILE WORKING 7-5310-7-2301G1, FOUND DENT IN 1342 BULKHEAD SKIN APPROX WL 258 LT. REPAIRED DENT AT BS 1342 BULKHEAD, WL 258 LT. ALL WORK DONE PER FEDEX SRM 54-30-03 AND FEDEX EA 7-5310-26290.Dec 11, 1995 · N498FE · Boeing 727232 · Fuselage Main, BulkheadSDR 95FDEA01889Frame · corrosionCORROSION (C53-100-01) ON FRAME WEB BS 219.8, LBL 19-32, RBL 16-24, WL 165. CORROSION FOUND TO BE OUT OF LIMITS PER FEDEX 53-10-1. REMOVED WEB AT BS 219.8, TRIM LBL - RBL 25, FABRICATED AND INSTALLED NEW WEB IAW FEDEX SRM 51-40-2.Dec 11, 1995 · N498FE · Boeing 727232 · Fuselage Main, FrameSDR DL72S954665Battery Pack · dischargedLT FORWARD EXT OVERWING EMERGENCY LIGHT OUT. REPLACED RACK OPS CHECK GOOD.Dec 10, 1995 · N489DA · Boeing 727232 · Emergency LightingSDR DL72S960200Baffle · crackedDURING ROUTINE SHOP INSPECTION, A CRACK WAS FOUND IN THE ANTI-ICE BAFFLE BETWEEN THE 11TH AND 12TH RIB FROM THE I/B END. BAFFLE WAS REPAIRED AS PER MM 57-57-0 FIG 8103A FOR NR 2 L/E SLAT.Dec 9, 1995 · N543DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954692Blkhd Web · crackedTHE BS 1183 BULKHEAD WEB WAS FOUND CRACKED IN TWO LOCATIONS AT RBL 18. THERE IS A 1 INCH CRACK AT WL 166.3 TO WL 167.5 AND A .1875 INCH CRACK AT WL 169. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF 0.050 INCH. THE CRACK LOCATIONS ADec 9, 1995 · N519DA · Boeing 727232 · Fuselage Main, BulkheadSDR MZZA95051Actuator · leakingAFTER TAKEOFF ON CLIMB-OUT FROM SPN, LOST ALL A-SYSTEM HYDRAULIC QUANTITY. FLIGHT CONTINUED TO GUM AND GEARS EXTENDED MANUALLY FOR LANDING. MAINTENANCE FOUND NR 5 L/E SLAT ACTUATOR LEAKING EXCESSIVELY. REMOVED AND REPLACED ACTUATOR ASSY. ALSO REPLACED BOTHDec 8, 1995 · N15781 · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S954753Skin · puncturedDURING A SHOP INSPECTION FOUND PUNCTURE DAMAGE TO RT ELEVATOR SKIN AT AT THE OUTBOARD END. REPAIR WAS INSTALLED PER SRM 55-20-3.Dec 8, 1995 · N484DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S954699Te Skin · separatingAT HMV, TRAILING EDGE OF LEFT ELEVATOR SEPARATED IN SEVERAL PLACES. REPAIRED PER MM 55-20-0 PG 801.Dec 8, 1995 · N496DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S954670Light · inoperativeDURING PREFLIGHT, COCKPIT EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. REPLACED LIGHT ASSEMBLY, OPERATION NORMAL.Dec 8, 1995 · N531DA · Boeing 727232 · Emergency LightingSDR DL72S954662Stiffener · crackedFRONT SPAR STIFFENER, NOSE RIB ATTACH BRACKET CRACKED BETWEEN TWO LOWER FASTENERS AT NR 7 SLAT INBOARD TRACK AT APPROX IWS 588. REPLACED STIFFENER PER MM 57-20-21.Dec 8, 1995 · N475DA · Boeing 727232 · Wing SparSDR DL72S954653Web · crackedA .25 INCH CRACK LT LWR TORQUE BOX VERTICAL WEB STA 1223 AT TOP ROW OF RIVETS. ALSO, .25 INCH CRACK IN LIGHTENING HOLE BELOW THE TOP ROW OF RIVETS. REPAIRED PER MM 53-11-0.Dec 8, 1995 · N519DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S954645Battery · dischargedEMERGENCY EXIT LIGHTS OVER R-1 DOOR ARE INOP. INSTALLED NEW BATTERIES, CKS GOOD.Dec 8, 1995 · N545DA · Boeing 727232 · Emergency LightingSDR DL72S954644Passenger Door · bentAC LOG ITEM Z60966002 RT CORNER OF FORWARD ENTRY DOOR IS BENT UP. REPAIRED PER MM 52-11-01 FIG 804.Dec 8, 1995 · N535DA · Boeing 727232 · Passenger/Crew DoorsSDR 95FDEA01884Beam · corrodedCORROSION WAS FOUND WHILE WORKING NR 0685 ON FLANGE OF BEAM AT BS 178, WL 184-189, LBL 16.Dec 8, 1995 · N498FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 95FDEA01883Frame · dentedDENT IN FRAME BS 720A, LBL 31-LBL 37, WL 160. REPAIRED DENT IN FRAME PER FEDEX SRM 51-40-3.Dec 8, 1995 · N498FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01882Floor Beam · corrodedCORROSION STA 360, FLOOR BEAM WL 208.1, LBL 3-8. REMOVED CORROSION FROM FLOOR BEAM STA 360, WL 208.1, LBL 3.5. AREA WAS 2.5 INCHES BY .25 INCH. ORIGINAL THICKNESS .125 INCH. REMOVED .022 INCH, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED FILLER WASDec 8, 1995 · N498FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 95FDEA01881Floor Beam · corrodedCORROSION (C53-229-01(1) FLOOR BEAM STA 344, LBL 3-58, WL 208.1, UPPER SURFACE OF TOP CHORD, RBL 0-42, WL 208, LOWER SURFACE OF TOP CHORD. TOP CHORD OF THE FLOOR BEAM AT BS 344 WAS FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-1. REPAIRED FLOOR BEAM AT BS 34Dec 8, 1995 · N498FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 95FDEA01880Skin · gougeAT BS 312, STR 24, WL 158, THERE IS ONE SHEARED FASTENER AND A GOUGE THROUGH SKIN AND FASTENER. BLENDED GOUGE AT BS 312, STR 24, WL 158, OUT OF LIMITS PER FEDEX SRM 53-30-1. REMOVED DAMAGED AREA, INSTALLED EXTERNAL REPAIR PATCH PER FEDEX SRM 53-30-3.Dec 8, 1995 · N498FE · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S954668Mask · popped indicatorDURING INSPECTION, FOUND FWD CABIN PBE WITH POPPED INDICATOR. REPLACED PBE.Dec 7, 1995 · N536DA · Boeing 727232 · Portable Oxygen SystemSDR DL72S954641Rib · crackedRIB MARKED NR 16 CRACKED. REPAIRED PER M/M 57-54-0 FOR NR 7 L/E SLAT DURING SHOP INSPECTION.Dec 7, 1995 · N489DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954640Rib · crackedRIBS MARKED NR 17 AND NR 18 CRACKED. REPAIRED PER M/M 57-54-0 FOR L/E SLAT NR 7 AT SHOP INSPECTION.Dec 7, 1995 · N489DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954639Rib · crackedRIBS MARKED NR 4 AND NR 9 CRACKED. REPAIRED PER M/M 57-54-0 FOR NR 7 L/E SLAT AT SHOP INSPECTION.Dec 7, 1995 · N489DA · Boeing 727232 · Leading Edge DevicesSDR 95FDEA01878Frame · gougedGOUGE ON FRAME BS 500 BETWEEN STR 13-14R. REPAIRED DAMAGED FRAME AT BS 500, STR 13-14R PER FEDEX SRM 53-10-4.Dec 7, 1995 · N498FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01877Stringer · corrosionCORROSION ON STR 27R AT BS 541. REPAIRED STR PER FEDEX SRM 53-10-3.Dec 7, 1995 · N498FE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR 95FDEA01874Solenoid · failedAFTER TAKEOFF FROM PHL, LANDING GEAR LEVER FAILED TO RAISE PASS THE OFF POSITION. THE LANDING GEAR LEVER LATCH FAILED TO RELEASE. CHECKLIST WAS ACCOMPLISHED. LANDING GEAR WAS SUBSEQUENTLY RETRACTED USING THE LANDING GEAR LEVER LATCH TRIGGER. SWAPPED LANDINDec 7, 1995 · N499FE · Boeing 727232 · Landing Gear SelectorSDR DL72S954636Elevator · damagedDURING SHOP INSPECTION, RT ELEVATOR WAS RESTORED PER SRM 55-20-3.Dec 6, 1995 · N484DA · Boeing 727232 · Elevator StructureSDR 95FDEA01873Skin · corrosionWHILE WORKING CARD NR 0812, DISCOVERED CORROSION ON SKIN ALONG FAIRING SEAM, BS 950F-1010, STR 21L-20L. REPAIRED DAMAGED SKIN ALONG FAIRING SEAM AT BS 750D-950F PER FEDEX SRM 53-30-3, FIG 14, ALSO REMOVED CORROSION FROM BS 950F-BS 1010 AND FOUND TO BE WITHIN Dec 6, 1995 · N498FE · Boeing 727232 · Fuselage Main, Plate/SkinSDR 95FDEA01872Beam · corrodedCORROSION (C53-224-01) FOUND ON TOP CHORD OF LONGITUDINAL BEAM AT BS 760-848, LBL 25, WL 208.1 (OUT OF LIMITS PER FEDEX SRM 53-10-01). REMOVED AND REPLACED TOP CHORD OF LONGITUDINAL BEAM AT BS 760-848, LBL 25, WL 208.1 IAW FEDEX 53-10-01 DUE TO CORROSION OUT Dec 6, 1995 · N498FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 95FDEA01871Frame · double holeDOUBLE HOLE IN FRAME AT BS 460, STR 7R. REPAIRED DOUBLE HOLE IN FRAME AT BS 460, STR 7R PER FEDEX SRM 53-10-4, FIG 2.Dec 6, 1995 · N498FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01870Skin · corrodedCORROSION ON SKIN AT BS 343-374, STR 27L-R. REMOVED CORROSION AT BS 352-360. FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-30-1. FABRICATED AND INSTALLED NEW SKIN PANEL AT BS 352-360, STR 27L-R PER FEDEX SRM 53-30-3.Dec 6, 1995 · N498FE · Boeing 727232 · Fuselage Main, Plate/SkinSDR 95FDEA01869Str Splice · corrodedCORROSION (C53-224-04) ON STR 7 SPLICE LT, BS 1015. REMOVED OLD STR SPLICE, STR 7L BS 1015 AND INSTALLED NEW STR SPLICE.Dec 6, 1995 · N498FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 95FDEA01868Floor Beam · corrosionCORROSION (C53-111-01(3)) ON BOTTOM CHORD OF FLOOR BEAM AT BS 1070, WL 200, RBL 51-LBL 42 AT NUTPLATE HOLES. REPAIRED OUT OF LIMITS FLOOR BEAM AT BS 1070, WL 200 FROM SKIN-TO-SKIN. REPAIRED AS PER FEDEX EA 7-5310-26725.Dec 6, 1995 · N498FE · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S954630Battery Pack · dischargedAFT EXIT EMERGENCY LIGHT INOP C/A REPLACED BATTERY PACK M1089. OPS CHKS GOOD.Dec 5, 1995 · N420DA · Boeing 727232 · Emergency LightingSDR DL72S954629Battery Pack · dischargedBOTH AFT SERVICE DOOR EMERGENCY LIGHTS INOP C/A REPLACED BATTERY PACK M983. OPS CHKS GOOD.Dec 5, 1995 · N420DA · Boeing 727232 · Emergency LightingSDR DL72K960333Rib · crackedDURING INSPECTION, FOUND NR 8 L/E SLAT WITH CRACKED SUPPORT RIB. REPAIRED PER MM 57-54-0.Dec 5, 1995 · N480DA · Boeing 727232 · Leading Edge DevicesSDR 95FDEA01867Frame · mis drilledINSTALLATION OF FASTENERS IN FRAME WEB BS 950F, WL 295, LBL 35 WITH IMPROPER SPACING AND FASTENERS DAMAGED. REPAIRED FRAME AT BS 950F, WL 295, LBL 35 PER FEDEX SRM 5-10-4. C/A ADDITION.Dec 5, 1995 · N498FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01864Frame · dentedDENT IN FRAME AT BS 1050 BETWEEN STR 25 AND 26 LBL 30 WL 150. REPAIRED DENT IN FRAME AT BS 1050 BETWEEN STR 25 TO 26 LBL 30 WL 150. ALL WORK DONE PER FEDEX SRM 51-40-03 FIG 1.Dec 5, 1995 · N498FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01863Floorbeam · corrodedCORROSION AROUND FASTENER HOLES ON TOP CHORD OF FLOORBEAM AT BS 720A RBL 21 LBL 10, 16 AND 21 WL 208. TOP CHORD OF FLOORBEAM AT BS 720A LBL RBL 21 WL 208, FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-1. REPAIRED FLOORBEAM AT BS 720A LBL 32 RBL 34 WL 208 IAWDec 5, 1995 · N498FE · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S954621Battery · dischargedDURING LAYOVER, FOUND AFT AIRSTAIR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK OPERATION NORMAL.Dec 4, 1995 · N523DA · Boeing 727232 · Emergency LightingSDR DL72L954625Window · arcingTOP LEFT CORNER OF L1 WINDOW AROUND SCREWS THERE WAS SPARKS AND SMOKE. WITH L1 WINDOW HEAT TURNED OFF THERE WAS NO SMOKE OR SPARKS. REPLACED WINDOW AND CONTROLLER.Dec 4, 1995 · N504DA · Boeing 727232 · Flight Compartment WindowsSDR 95FDEAO1826Web · corrodedWHILE WORKING NRO 676, FOUND CORROSION ON AFT SIDE OF WEB STATION 219.8 W/L 214 TO 222, LBL 44. UPON REMOVING CORROSION AFT SIDE OF WEB STATION 219.8 W/L 214 TO 222, LBL 44, FOUND CRACK. REPAIRED WEB IAW FEDEX SRM 51-40-2. CORROSION WAS FOUND TO BE WITHIN LDec 4, 1995 · N498FE · Boeing 727232 · Fuselage Miscellaneous Structure
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