Boeing 727-232

Service difficulty reports · 6,539

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Query with SQL
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 CALA9900289Bolt · corrodedINSPECTION FOUND BOTH HORIZONTAL STABILIZER HINGE PIN BOLTS CORRODED. BOTH HINGE PINS WERE REPLACED IAW MM 55-00.Mar 18, 1999 · N77780 · Boeing 727232 · Horizontal Stabilizer StructureSDR CALA9900288Wire · brokenINSPECTION FOUND EXIT IDENTIFIER LIGHT AT R-2 DOOR INOPERATIVE. MAINTENANCE FOUND EXIT LIGHT WIRE BROKEN. THE WIRE WAS REPAIRED IAW MM 33-51-00, PAGE 903 AND OPERATION WAS RESTORED.Mar 18, 1999 · N77780 · Boeing 727232 · Light System WiringSDR CALA9900287Wire · brokenINSPECTION FOUND THE EXIT IDENTIFIER LIGHT AT L-2 DOOR INOPERATIVE. MAINTENANCE FOUND A BROKEN GROUND WIRE. THE WIRE WAS REPAIRED IAW MM 33-51-00, PAGE 903 AND OPERATION WAS RESTORED.Mar 18, 1999 · N77780 · Boeing 727232 · Light System WiringSDR CALA9900286Wire · looseINSPECTION FOUND EXIT IDENTIFIER LIGHT AT LEFT AFT LAV WALL INOPERATIVE. MAINTENANCE FOUND A LOOSE GROUND WIRE. THE WIRE WAS SECURED IAW MM 33-51-00, PAGE 903 AND OPERATION WAS RESTORED.Mar 18, 1999 · N77780 · Boeing 727232 · Light System WiringSDR CALA9900285Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN LEFT ELEVATOR LOWER SKIN JUST I/B AND AFT OF PANEL NR 9311. THE CRACK WAS STOP DRILLED IAW SRM 55-20-3. A DOUBLER WAS INSTALLED IAW SRM 55-20-3, 51-10-2, AND 51-30. A CALCULATED BALANCE WAS PERFORMED IAW SRM 51-80-7 AND WAMar 18, 1999 · N77780 · Boeing 727232 · Elevator, Spar/RibSDR CALA9900284Skin · crackedINSPECTION FOUND TWO .5 INCH CRACKS COMING FROM SCREW HOLE TO RIVETS AT RT WING NR 7 SLAT UPPER TRAILING EDGE WHERE O/B HOOK MOUNTS. REMOVED FASTENERS IAW SRM 51-30-2. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-20-3.Mar 18, 1999 · N77780 · Boeing 727232 · Leading Edge DevicesSDR CALA9900283Skin · crackedINSPECTION FOUND A .1875 INCH CRACK AT RT WING UPPER TRAILING EDGE AT CUTOUT FOR NR 13 SPOILER SECOND FROM O/B HINGE CUTOUT. THE CRACK WAS STOP DRILLED. A REPAIR WAS INSTALLED AND EDGES WERE SEALED IAW SRM 51-10-1 AND 51-10-3, PAGE 4.Mar 18, 1999 · N77780 · Boeing 727232 · SpoilersSDR DL72S990610Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 19 CRACK INDICATIONS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE Mar 17, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990609Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 85 CRACKS INCLUDING A 15 INCH LONG CRACK LINK UP BETWEEN FS 640 AND 660. THE ENTIRE SKIMar 17, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990593Frame · crackedDURING ACCOMPLISHMENT OF INSPECTIONS PER SI 4-61904-12AD, A CRACK WAS NOTED IN THE 2ND FAST HOLE ABOVE THE FLOORLINE. ALSO, THE 4TH FASTENER HOLE ABOVE THE FLOORLINE FELL OUT IN THE RADIUS OF THE REPAIR ANGLE. REPAIRED PER 332907-14AD.Mar 17, 1999 · N482DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S990559Skin · crackedPERFORMING INSPECTIONS PER SI 4-74176-12AD, 12 CRACK INDICATIONS WERE FOUND BETWEEN BS 380 TO 460 IN THE SKIN LAP JOINT AT S4L. REPAIRED PER ERA 332914-14AD.Mar 17, 1999 · N482DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990558Skin · crackedPERFORMING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S4R LAP JOINT BETWEEN BS 560 TO 580. THE CRACK INDICATION WAS LOCATED AT FASTENER ROW 8 AS IDENTIFIED IN FIGURE 6 OF THE SI. REPAIRED PER ERA 332910-14AD.Mar 17, 1999 · N482DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990557Skin · crackedPERFORMING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATIONS WAS NOTED IN THE S4R LAP JOINT BETWEEN BS 620 AND 640. THE INDICATION WAS LOCATED IN FASTENER ROW NR 11 AS IDENTIFIED IN FIGURE 6 OF THE SI. REPAIRED PER ERA 332909-14AD.Mar 17, 1999 · N482DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9900282Angle · crackedINSPECTION FOUND A .125 INCH CRACK IN RT WING NR 7 SLAT LOWER SPANWISE CHORD ANGLE AT CUTOUT FOR I/B TRACK AND A .3125 INCH CRACK AT STOP PAD AREA SIX INCHES INBOARD. THE ANGLE WAS REMOVED. AN ANGLE AND REPAIR SPLICE WERE INSTALLED IAW SRM 51-40-3, 51-10-2, Mar 17, 1999 · N77780 · Boeing 727232 · Leading Edge DevicesSDR CALA9900281Skin · crackedINSPECTION FOUND A 1.25 INCH CRACK IN RT O/B FOREFLAP LEADING EDGE. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW SRM 57-50-4 AND 51-30-2, PAGE 7.Mar 17, 1999 · N77780 · Boeing 727232 · Trailing Edge FlapsSDR CALA9900280Skin · debondedINSPECTION FOUND TWO SMALL DEBONDED AREAS IN RT O/B AILERON TAB TRAILING EDGE. THE RT O/B AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41.Mar 17, 1999 · N77780 · Boeing 727232 · Aileron TabsSDR CALA9900279Skin · tornINSPECTION FOUND RT I/B FOREFLAP INBOARD MOST END UPPER LEADING EDGE SKIN TORN FORWARD OF SPRING DOOR. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-3.Mar 17, 1999 · N77780 · Boeing 727232 · Trailing Edge FlapsSDR CALA9900278Skin · crackedINSPECTION FOUND A .3125 INCH CRACK AT RT I/B MIDFLAP LOWER TRAILING EDGE. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW SRM 51-40-2 AND 51-30-2.Mar 17, 1999 · N77780 · Boeing 727232 · Trailing Edge FlapsSDR CALA9900277Skin · disbondedINSPECTION FOUND LT TRAILING EDGE I/B FOREFLAP DISBONDED AT UPPER AND LOWER SURFACE. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-4.Mar 17, 1999 · N77780 · Boeing 727232 · Trailing Edge FlapsSDR CALA9900276Skin · gougedINSPECTION FOUND LT HORIZONTAL STABILIZER I/B LEADING EDGE AREA GOUGED. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-6 AND 51-30-2, PAGE 4.Mar 17, 1999 · N77780 · Boeing 727232 · Horizontal Stabilizer, Plate/SkinSDR CALA9900275Skin · separatedINSPECTION FOUND LT ELEVATOR CONTROL TAB TRAILING EDGE SKIN SEPARATING IN TWO PLACES. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW 55-20-2.Mar 17, 1999 · N77780 · Boeing 727232 · Elevator, Tab StructureSDR CALA9900274Wire · brokenINSPECTION FOUND EMERGENCY PATH SEAT MOUNTED LIGHTING INOPERATIVE FROM ROW 23 TO 30. REPAIRED WIRING AND OPERATIONAL CHECK WAS GOOD IAW MM 33-50-00, PAGE 201.Mar 17, 1999 · N77780 · Boeing 727232 · Light System WiringSDR CALA9900273Battery Pack · dischargedINSPECTION FOUND EMERGENCY PATH LIGHTING IN FORWARD SECTION OF FIRST CLASS CABIN INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-00, PAGE 201.Mar 17, 1999 · N77780 · Boeing 727232 · Emergency LightingSDR DL72S990608Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS BETWEEN FS 440 AND 460. THE CRACKED AREA OF SKIN LAP SPLICE WAS CUTOUT AND REMar 16, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990577Skin · crackedWHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON THE S26L LAP JOINT, CRACK INDICATIONS WERE NOTED BETWEEN BS 480 AND BS 681. HFEC INSPECTIONS CONFIRMED 4 CRACK INDICATIONS. ADDITIONALLY, A 2.5 INCH CRACK RUNNING FWD/AFT WAS NOTED AT S25L AT BS 540Mar 16, 1999 · N531DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990570Skin · crackedLFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 2 CRACKS BETWEEN FS 460 AND 480. THE CRACKS WERE ROUTED OUT AND REPAIRED PER B72Mar 16, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990553Keel Beam · crackedKEEL BEAM LT LWR CHORD WAS FOUND CRACKED IN THE UPPER FLANGE TYPICAL OF THAT DESCRIBED BY SB 727-53-0208, REV 1. REPAIRED PER ERA 332906-14.Mar 16, 1999 · N482DA · Boeing 727232 · Fuselage Main, KeelSDR DL72S990552Rib · crackedTHE UPPER CHORD ANGLE OF THE LEFT WING RIB AT WS 171.5 WAS FOUND CRACKED. THE CRACK WAS LOCATED AT A FASTENER HOLE ON THE HORIZONTAL FLANGE OF THE CHORD ANGLE UNDER S16. REPAIRED PER ERA 332872-14, REV B.Mar 16, 1999 · N531DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S990616Flap Track · corrodedDURING OUTSIDE REPAIR, OVERHAUL PER CMM AND MOD PER SB 727-57-0178, TYPICAL CORROSION WAS FOUND TO THE FWD ATTACH LUGS AND THE MLG BEAM AND SPOILER BEAM ATTACH PADS AND HOLES. AUTHORIZED BUSHING REPAIR FOR FWD ATTACH LUG AND OVERSIZED SPOILER BEAM ATTACH HMar 15, 1999 · N411DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S990615Flap Track · corrodedDURING OUTSIDE REPAIR OF COMPONENT AND OVERHAUL PER CMM AND MOD PER SB 727-57-0178, TYPICAL CORROSION WAS FOUND ON THE MLG BEAM AND SPOILER BEAM ATTACH PAD AND HOLES. AUTHORIZED OVERSIZED FASTENERS, BUSHING REPAIR AND LEAVING THE OVERSIZED MLG BEAM ATTACH HOLMar 15, 1999 · N411DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S990588Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG THE PANEL LENGTH AND REMar 15, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990571Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED ONE CRACK BETWEEN FS 580 AND 600. THE CRACK WAS ROUTED OUT AND REPAIRED PER B727 SRM Mar 15, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K990551Skin · crackedWHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON THE S4R LAP JOINT, TWO CRACK INDICATIONS WERE FOUND BETWEEN BS 360 AND BS 481. HFEC INSPECTION VERIFIED THE TWO CRACK INDICAITONS, BETWEEN BS 360 AND BS 380. THE CRACKS WERE IN THE LWR ROW FASTENERSMar 15, 1999 · N491DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990572Skin · 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. INTERNAL HFEC INSPECTION CONFIRMED 15 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTMar 13, 1999 · N404DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990561Skin · crackedLFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 21 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE LENGTMar 13, 1999 · N404DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990546Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 360 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 500 AND 520. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP AND REPAIRMar 13, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990545Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 86 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANELMar 13, 1999 · N404DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990535Battery · dischargedROW 13 OVERHEAD EMERGENCY EXIT LIGHT DIM. REPLACED BATTERY.Mar 13, 1999 · N546DA · Boeing 727232 · Emergency LightingSDR DL72S990534Battery · dischargedR1 DOOR EMERGENCY EXIT LIGHTS LOW. REPLACED BATTERY.Mar 13, 1999 · N546DA · Boeing 727232 · Emergency LightingSDR CALA9900250Wire · brokenINSPECTION FOUND LT EMERGENCY PATH LIGHT ON SEAT AT ROW 11 INOPERATIVE. INSPECTION FOUND PATH LIGHT WIRE BROKEN. THE WIRE WAS REPAIRED AND STOWED. OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-00, PAGE 102.Mar 13, 1999 · N77780 · Boeing 727232 · Light System WiringSDR DL72S990569Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A CRACK BETWEEN FS 520 AND 540. THE CRACK WAS ROUTED OUT AND REPAIRED PER B727 SRM 53Mar 12, 1999 · N404DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990531Web · crackedRT SIDE TORQUE BOX WEB HAS .125 INCH CRACK PROTRUDING PAST. ROUTE OUT REPAIR AT STA 1283 LOWER HOLE M/M 53-11-0 PG 832.Mar 12, 1999 · N543DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990529Skin · corrodedCORROSION WAS FOUND UNDER S28L AT BS 1010 AT THE SKIN BUTT JOINT. REPAIRED PER ERA 332920-14.Mar 12, 1999 · N531DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990528Stringer · crackedFUSELAGE STRINGER 29R WAS FOUND CRACKED 2 FWD OF BS 950E. ADDITIONALLY, CORROSION WAS NOTED 2 AFT OF BS 950D. A SECTION OF STRINGER FROM BS 950D+10 TO BS 950E+10 WILL BE CUT OUT AND REPLACED. REPAIRED PER ERA 332882-14.Mar 12, 1999 · N531DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S990527Frame · wornSTATION 1148 FRAME WAS FOUND WORN ON THE I/B HORIZ FLANGE AT S22L DUE TO CONTACT WITH A HYD LINE. REPAIRED PER ERA 332918-14.Mar 12, 1999 · N531DA · Boeing 727232 · Fuselage Main, FrameSDR CALA9900246Accessory Unit · inopBOTH RT MLG RED AND GREEN ANNUNCIATOR LIGHTS ILLUMINATED DURING DESCENT. THE GEAR HANDLE WAS CYCLED FROM UP TO OFF AND THE GEAR DOOR LIGHT CAME ON. WHEN GEAR WAS SELECTED TO DOWN, GOT THREE GREEN AND LANDING WAS NORMAL. THE LANDING GEAR AND DOORS WERE INSPEMar 12, 1999 · N15781 · Boeing 727232 · Landing Gear Position and WarningSDR DL72S990568Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT ALONG ITS ENTIRE LENGTH AMar 11, 1999 · N499DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990567Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED A CRACK IN LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION OF THE ENTIRE PANEL CONFIRMED A SINGLE CRACK BETWEEN FS 560 AND 580. THE CRACK WAS ROUTED OUT ANDMar 11, 1999 · N404DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990566Skin · crackedLFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 400 AND 420. THE CRACKS WERE CUT OUT AND REPAIRED PER B727 SRM 53-30-3Mar 11, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990565Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 TO 740 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 720 AND 720A. THE CRACKED AREA WAS ROUTED OUT AND REPAIRED PEMar 11, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/Skin
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