Boeing 727-30C

Service difficulty reports · 931

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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 = '72730C'
  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 UPS98227337Seat Track · corrodedINSPECTION TYPE:SI, SEAT TRACK CORRODED BS 760-785 RBL 25. REPLACED TRACK PER SRM 53-10-5.Jul 28, 1998 · N906UP · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR UPS98227284Skin · corrodedINSPECTION TYPE-SI, DISHED RIVETS AND PILLOWED SKIN STA 1120 TO 1150 LT 3 STR TO STR 4 LT AND 3 STR RT TO 4 STR RT. REPLACED SKIN PER EO 98-2608.Jul 28, 1998 · N906UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS98227336Link · corrodedINSPECTION TYPE:SI, CORROSION ON EXPANSION LINK BS 870 RBL 25. REPLACED PER DRAWING 65-34144.Jul 27, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS98227335Floorbeam · corrodedINSPECTION TYPE:SI CORROSION ON FLANGES OF LONGITUDINAL FLOORBEAM. REPLACED PER DWG 65-34144.Jul 24, 1998 · N906UP · Boeing 72730C · Fuselage Main, Floor BeamSDR UPS98227217Floorbeam · corrodedINSPECTION TYPE:SI CORROSION (C53-224-01.05-02) AND CHAFFING ON UPPER BS 740 FLOORBEAM UPPER FLANGE, RBL 0-45, WL 208, MARKED. REMOVED COROSION FOUND TO BE OUT OF LIMITS, REPLACED CHORD AS PER SRM 51-30-2.Jul 22, 1998 · N906UP · Boeing 72730C · Fuselage Main, Floor BeamSDR UPS98227182Stiffener · corrodedINSPECTION TYPE-SI, WHILE WORKING FUSELAGE 88 CUSTOMER ID NR 832295 FOUND CORROSION ON NLG WHEEL WELL STIFFENER BS 336, LBL 14, WL 158. OUT OF LIMITS. REPAIRED PER SRM 51-10-6, 53-10-1, 53-10-2, 51-30-2, 51-20-151.Jul 17, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS98227181Track · corrodedINSPECTION TYPE-SI, CORROSION (C57-581-06.00-04) NR 7 FLAP TRACK FWD LUG HAS RUST AROUND BOLT HOLE. REMOVED FLAP TRACK AND SENT TO OUTSIDE SERVICES FOR REPAIR AND REINSTALLED AFTER REPAIR.Jul 16, 1998 · N906UP · Boeing 72730C · Trailing Edge FlapsSDR UPS98227180Track · corrodedINSPECTION TYPE-SI, NR 1 FLAP TRACK FWD MOUNT BOLT LUGS ARE CORRODED. REMOVED FLAP TRACK AND SENT TO OUTSIDE SERVICES FOR REPAIR AND REINSTALLED AFTER REPAIR.Jul 16, 1998 · N906UP · Boeing 72730C · Trailing Edge FlapsSDR UPS98227179Track · corrodedINSPECTION TYPE-SI, NR 3 FLAP TRACK CENTER MOUNT BOLT IS CORRODED ON THE AFT SIDE CORROSION (C57-581-06.00-03) AND CORROSION (C57-581-06.00-03) NR 3 FLAP TRACK IS CORRODED ON THE SPOILER BEAM MOUNT PAD. FLAP TRACK REMOVED AND SENT TO OUTSIDE SERVICES FOR REPAJul 16, 1998 · N906UP · Boeing 72730C · Trailing Edge FlapsSDR UPS98227171Light · inoperativeINSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FLIGHT DECK DOOR WILL NOT STAY IN IT'S ELECTRICAL SOCKET CAUSING IT TO STAY ON IN FLIGHT. REINSTALLED EMER EXIT LIGHT PROPERLY UNTILL LATCHES ENGAGED, EMER EXIT LIGHT, OPS CHECK GOOD.Jul 15, 1998 · N918UP · Boeing 72730C · Emergency LightingSDR UPS98227166Rib · crackedINSPECTION TYPE-SI, CRACK INDICATION NOTED ON RT WING RIB AT WS 656.5 STR 6 LOWER. REPLACED CRACKED RIB WITH NEW RIB PER EO B727-5710-1325.Jul 14, 1998 · N906UP · Boeing 72730C · Wing, Rib/BulkheadSDR UPS98227165Rib · crackedINSPECTION TYPE-SI, CRACK INDICATION NOTED ON LT WING RIB AT WS 6565 STR 6 LOWER. REMOVED CRACKED RIB REPLACED WITH NEW RIB IAW EO B727-5710-1325D.Jul 14, 1998 · N906UP · Boeing 72730C · Wing, Rib/BulkheadSDR UPS98227164Batteries · dischargedINSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FLIGHT DECK DOOR INOP. REPLACED WITH NEW BATTERIES, LIGHT OPS CHECKED OK.Jul 14, 1998 · N918UP · Boeing 72730C · Emergency LightingSDR UPS98227167Stringer · corrodedINSPECTION TYPE-SI, CORROSION (C53-221-01.00-01) ON STR 1 AT STA 291. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED AREA OF STRINGER AND FABRICATED REPAIR PARTS IAW SRM 53-10-3 SRM 53-10-4.Jul 13, 1998 · N906UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS98227288Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON NUT PLATES AT BS 740 FLOORBEAM RBL 60 TO LBL 60 WL 208. REMOVED FLOORBEAM AT BS 740 LBL 6, RBL 60, INSTALLED FABRICATED FLOORBEAM IAW SRM 51-30-2, 53-104.Jul 11, 1998 · N906UP · Boeing 72730C · Fuselage Main, Floor BeamSDR UPS98227291Angle · crackedINSPECTION TYPE-SI, POSSIBLE CRACK IN FLOORBEAM SUPPORT ANGLE BS 804, LBL 46, WL 206. FLOORBEAM SUPPORT CRACKED, VERIFIED BY NDI. REPLACED SUPPORT ANGLE PER 727 SRM 51-30-2 AND 51-10-1.Jul 10, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS98227169Angle · crackedINSPECTION TYPE-SI, POSSIBLE CRACK IN FLOORBEAM SUPPORT ANGLE BS 804, LBL 46, WL 206. FLOORBEAM SUPPORT CRACKED, VERIFIED BY NDI. REPLACED SUPPORT ANGLE PER 727 SRM 51-30-2 AND 51-10-1.Jul 10, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS98227168Seat Track · corrodedINSPECTION TYPE-SI, CORROSION ON SEAT TRACK BS 850 LBL 65 BL 208. REPLACED SEAT TRACK EXTRUSION BS 760 TO 850 LBL 65 WL 208 PER 727 SRM 51-30-2. ALSO, REFERENCE NRC 832521 REPLACED L-ANGLES PER SRM 51-20-1 AT BS 804.Jul 10, 1998 · N906UP · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR UPS98227127Floorbeam · corrodedINSPECTION TYPE:SI CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 344 FROM LBL 25 TO RBL 15. REMOVED AND REPLACED UPPER CHORD AT FLOOR BEAM IAW SRM 53-10-8.Jul 8, 1998 · N906UP · Boeing 72730C · Fuselage Main, Floor BeamSDR DHL98702002Hyd Pump · failedAT FL 330, NR 1 ENGINE OIL PRESSURE LIGHT CAME ON AND OIL QUAN DROPPED TO 1.5 . NR 1 ENGINE HAD VIBRATION. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP.Jul 8, 1998 · N702DH · Boeing 72730C · Hydraulic Pump (Electric/Engine), MainSDR DHL98702001Line · holeAT FL 330, NR 1 ENGINE OIL PRESSURE LIGHT CAME ON. OIL QUAN DROPPED TO 1.5, ENGINE HAD VIBRATION. REMOVED AND REPLACED OIL LINE FROM OIL PRESSURE TRANSMITTER.Jul 8, 1998 · N702DH · Boeing 72730C · Engine Oil PressureSDR UPS98227338Expansion Link · corrodedINSPECTION TYPE:SI, WHILE WORKING INTERIOR 140 CUST NR 832471 FOUND STA 860 RBL 45 EXPANSION LINK CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-1.Jul 6, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS98227290Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON FLANGES OF LONGITUDINAL FLOORBEAM AND NUT PLATES BS 760 TO 848, WL 208 RBL 45. REPLACED LONGITUDINAL FLOORBEAM AND SEAT TRACK (NRC 832504) BS 760 TO 848 PER SRM 51-30-2.Jul 6, 1998 · N906UP · Boeing 72730C · Fuselage Main, Floor BeamSDR UPS98227130Skin · corrodedINSPECTION TYPE:SI CORROSION (C53-111-01.01-02) ON INTERNAL SKIN SURFACE OF LWR LAP JOINT AT BS 679 ABOVE STR 19L. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AND FILLERS PER 727 SRM 53-30-3.Jul 6, 1998 · N906UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS98227129Doubler · crackedINSPECTION TYPE:SI BONDED DOUBLER ON TOP SURFACE OF NLG (DOGHOUSE) IS CRACKED AT BS 305 LBL 2 WI L181. REPLACED DOUBLER 16.5 BY 24.5 LBL 14 TO RBL 14 PER 727 SRM 51-40-2, 51-30-2, 51-40-2. BONDED PER BAC5514-551 AND 5514-5101 AND DRAWING 65-18417 AND REPLACEJul 6, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS98227128Seat Track · corrodedINSPECTION TYPE:SI CORROSION (C53-224-01.05-02) ON FLANGES OF LONGITUDINAL FLOORBEAM AND NUT PLATES BS 760-848, WL 208 RBL 45. REPLACED LONGITUDINAL FLOORBEAM AND SEAT TRACK (NRC 832504) BS 700 TO 848 PER SRM 51-30-2.Jul 6, 1998 · N906UP · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR UPS98227136Stringer · corrodedINSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 21R BS 312. REPLACED STRINGER CHANNEL FROM BS 292 TO 315 IAW SRM 51-10-7, 53-10-1 AND 53-10-3.Jul 3, 1998 · N906UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS98227135Floorbeam · corrodedINSPECTION TYPE:SI CORROSION (C53-224-01.05-02) ON FLANGES OF LONGITUDINAL FLOORBEAM AND NUT PLATES BS 760-848 LBL 25 WL 208. REPLACED LONG FLOORBEAM BS 760 TO 840 LBL 25 WL 208 AND EXPANSION LINK FROM 850 TO BS 870 PER 727 SRM 53-10-1 AND 51-30-2 EXPANSION LJul 3, 1998 · N906UP · Boeing 72730C · Fuselage Main, Floor BeamSDR UPS98227134Fitting · crackedINSPECTION TYPE:SI CRACK IN LT INBOARD 3A BOLT FITTING BS 1183 STRINGER 3A LT INBRD FITTING FWD FITTING. REPLACED FITTING 65-25591-9 PER SRM 51-10-1 AND MM 51-20-31.Jul 3, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS98227133Floor Track · corrodedINSPECTION TYPE:SI SEAT TRACK HAS CORROSION UNDER NUT CLIPS BS 568-582 LBL 25 WL 208. REPLACED SEAT TRACK EXTRUSION FROM 540 TO 615 PER SRM 53-10-5, 53-10-2, 51-20-151, 51-30-2.Jul 3, 1998 · N906UP · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR UPS98227132Seat Track · corrosionINSPECTION TYPE:SI SEAT TRACK HAS CORROSION BS 599 TO 607 LBL 25 WL 208. REPLACED SEAT TRACK BS 540 TO 615 LBL 25 PER 727 SRM 53-10-5, 51-30-2, 53-10-1.Jul 3, 1998 · N906UP · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR UPS98227131Stringer · corrodedINSPECTION TYPE:SI CORROSION (C53-111-01.00-02) ON STR 22R BS 480-500. REPLACED 22R STR CHANNEL BS 480 TO 500 PER 727 SRM 53-10-3.Jul 3, 1998 · N906UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS98227282Frame · corrodedINSPECTION TYPE-SI, CORROSION (C53-221-01.00-01) ON FRAME AT STA 294 LBL 57 WL 236 TO 239. REMOVED CORROSION FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PART IAW SRM 51-40-3.Jun 30, 1998 · N906UP · Boeing 72730C · Fuselage Main, FrameSDR UPS98227095Frame · corrodedINSPECTION TYPE:SI CORROSION (C53-221-01.00-01) ON FRAME AT STA 294 LBL 57 WL 236-239. REMOVED CORROSION FOUND OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR PART IAW SRM 51-40-3.Jun 30, 1998 · N906UP · Boeing 72730C · Fuselage Main, FrameSDR UPS98227100Stringer · corrodedINSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 24F BS 474. REPLACED STRINGER FROM BS 470 TO BS 490. INSTALLED STRINGER SECTION AND SPLICE PLATES PER 727 SRM 53-10-1, 53-10-3.Jun 26, 1998 · N906UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS98227137Fitting · corrodedINSPECTION TYPE:SI RIGHT WING REAR SPARS BOTTLE PIN AND BODY SIDE ARE DAMAGED (CORROSION C53-100-05-4B). REMOVED BUSHING FOUND CORROSION OUT OF LIMITS IAW SRM 53-40-1 AND HAD BOEING REPAIR IAW DRAWING 65C36301 AND BOEING AGREEMENT NR 6-1171-TA954.Jun 21, 1998 · N906UP · Boeing 72730C · Wing, Fuselage Attach FittingsSDR UPS98227292Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON UPPER CHORD OF FLOORBEAM AT FASTENER HOLE BS 312, LBL 3, WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-8, 51-30-5, 51-30-2, AND MM 51-20-151.Jun 18, 1998 · N906UP · Boeing 72730C · Fuselage Main, Floor BeamSDR UPS98227099Floorbeam · corrodedINSPECTION TYPE:SI CORROSION (C53-224-01.05-01) ON UPPER CHORD OF FLOORBEAM AT BS 328 LBL 45. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGE FROM BEAM AND INSTALLED STANDARD REPAIR PER SRM 53-10-8, 53-10-2 AND 51-30-2.Jun 18, 1998 · N906UP · Boeing 72730C · Fuselage Main, Floor BeamSDR UPS98227096Floorbeam · corrodedINSPECTION TYPE:SI CORROSION (C53-224-01.05-01) ON UPPER CHORD OF FLOORBEAM AT FASTENER HOLE BS 312, LBL 3, WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-8, 51-30-5, 51-30-2 AND MM 51-20-151.Jun 18, 1998 · N906UP · Boeing 72730C · Fuselage Main, Floor BeamSDR UPS98227287Bracket · corrodedINSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON NOSE COMPARTMENT DOOR STOP BRACKET, FWD SIDE OF BS 203.8 BRACKET, LBL 8. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. NEW FITTING INSTALLED IAW SRM 52-40-21 AND SRM 51-30-2.Jun 17, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS98227286Splice · corrodedINSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STR 25R SPLICE AT BS 443. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW SPLICE PER SRM 51-30-5, 51-30-2, AND MM 51-30-00.Jun 17, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS98227285Splice · corrodedINSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STR 25L SPLICE AT BS 442, BS 436. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW SPLICE PER SRM 51-30-2, 51-30-5, AND SRM 51-30-6.Jun 17, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS98227098Splice · corrodedINSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 25L SPLICE AT BS 442, BS 436. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, INSTALLED NEW SPLICE PER SRM 51-30-2, 51-30-5 AND SRM 51-30-6.Jun 17, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS98227097Splice · corrodedINSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 25R SPLICE AT BS 443. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW SPLICE PER SRM 51-30-5, 51-30-2 AND MM 51-30-00.Jun 17, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS97225364Light · looseINSPECTION TYPE-N/A, UPON LANDING EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR FLICKERED NUMEROUS TIMES. FOUND EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY, OPS CHECK GOOD.Dec 26, 1997 · N917UP · Boeing 72730C · Emergency LightingSDR DHL97701003Bulkhead · crackedAFT 1183 BULKHEAD DOOR FRAME ON RT SIDE NEAR 2ND FROM TOP STOP HAS POSSIBLE CRACK INDICATION. CRACK 1.45, VERIFIED WITH NDT METHODS. INSTALLED TEMPORARY REPAIR PER AVITAS ENGINEERING ORDER 97PMSI 184D-1 PAGES 1, 2 AND 3.Dec 20, 1997 · N701DH · Boeing 72730C · Fuselage Main, BulkheadSDR DHL97701002Boss · leakingOIL QUANTITY DECREASED TO ZERO DURING FLIGHT. LOCATED LEAK, LPS BOSS ON GEARBOX. REPAIRED DAMAGED BOSS THREADS PER PWA ENGINE MANUAL 72-61-01, LEAK CHECK GOOD.Nov 21, 1997 · N701DH · Boeing 72730C · Turbine Engine Accessory DriveSDR DHL97703001Adi · malfunctionedCAPT ADI DOES NOT DISPLAY PITCH INFORMATION. AFTER TAKEOFF ATTITUDE FLAG APPEARED. RESET C/B DID NOT HELP. FLAG RETRACTED ON ITS OWN AFTER 10 MIN. AFTER LANDING, ATTITUDE INDICATOR DOES NOT TEST NORMALLY. CHECKED CAPT ADI, WOULD NOT TEST. REMOVED AND REOct 14, 1997 · N703DH · Boeing 72730C · Integrated Flight SystemSDR UPS97224499Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY, BOTH BATTERY PACK WITH SERVICEABLE PACKS ROBBED FROM A/C 907.Sep 21, 1997 · N906UP · Boeing 72730C · Emergency LightingSDR DHL9770391DFrame · corrodedD-CHECK, CORROSION ON TOP OF FLOOR FRAME BS 312 LBL36. CUTOUT DAMAGED AREA 9.5 PER SRM 51-40-4 AT BS 312, LBL36. FABRICATED AND INSTALLED T ANGLE 11 IN LENGTH. FABRICATED AND INSTALLED L ANGLE 19 IN LENGTH PER SRM 53-10-8.Jul 18, 1997 · N703DH · Boeing 72730C · Fuselage Main, Frame
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