Boeing 727-22C

Service difficulty reports · 2,328

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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 = '72722C'
  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 UPS97221883Bottle Pin · corrodedINSPECTION TYPE-D, EVIDENCE OF CORROSION ON LEFT HAND FRONT SPAR TO BODY BOTTLE PIN AND ASSOCIATED BUSHING. BOTTLE PIN REPLACED PER UPS EO B727-5310-7477 ITEM 30F. NEW BUSHING INSTALLED, BS 740 FITTING PER EO B727-5310-7477 ITEM 30D, REF NRC 502825 / MRR UPJan 9, 1997 · N945UP · Boeing 72722C · Wing Miscellaneous StructureSDR UPS97221860Door Beam · corrodedINSPECTION TYPE-D, CORROSION FOUND ON UPPER BEAM OF MAIN CARGO DOOR AT HINGE LINE UNDER WEATHER SEAL. BEAM REPLACED, NO REPLACEMENT BEAMS AVAILABLE. BEAM FABRICATED LOCALLY IN TWO SECTIONS TO FACILITATE HEAT TREAT AND SPLICED PER BOEING INSTRUCTIONS, REF UPJan 9, 1997 · N945UP · Boeing 72722C · Cargo/Baggage DoorsSDR 97FDEA00098Floorbeam · corrodedNR 0288 029, CORROSION (C53-224-01,1) ON FLOORBEAM BS 640, LBL 12, WL 208 AND BLI AROUND FLOORBOARD FASTENER HOLES. *S/D* REPAIRED BEAM AT BS 640, LBL 60 TO RBL 25. REPAIRED SEAT TRACK AT BS 630 TO BS 660, LBL 55. ACCOMPLISHED WEB REPAIR BS 600 TO BS 660, Jan 9, 1997 · N102FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 97FDEA00031Skin · corrosionNR 083 003 CORROSION (C53-100-01) AT LAP LT STA 211 TO STA 259.5 STRINGER 25. *S/D* REMOVED CORROSION FROM SKIN AT LAP STA 211 TO STA 259.5, STR 19 TO 24 LT AND FOUND OUT OF LIMITS PER FED-EX SRM 53-30-1. REPAIRED SKIN PER FED-EX SRM 53-30-3 FIG 3A AND FED-Jan 9, 1997 · N102FE · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS97221938Fitting · corrodedINSPECTION TYPE-D, NR 1 AND NR 2 FLAP TRACK ATTACH FITTINGS ON LWR SURFACE OF WING, CORROSION AT ATTACH POINT. CORROSION REMOVED PER SRM 51-10-6. HFEC C/O PER NDT PT6 51-00-00 F13, MPI CO PER BS 6072, NO CORROSION FOUND. REPAIR TO NR 2 WING MOUNTED FLAP C/OJan 8, 1997 · N945UP · Boeing 72722C · Wing, Control Surface Attach FittingsSDR UPS97221937Fitting · corrodedINSPECTION TYPE-D, NR 1 AND NR 2 FLAP TRACK ATTACH FITTINGS ON LOWER SURFACE OF WING, CORROSION AT ATTACH POINT. CORROSION REMOVED IAW SRM 51-10-6, HFEC C/O PER NDTPT6 51-00-00 F13, MPI C/O PER C/O PER BS 6072, NO CORROSION FOUND. REPAIR TO NR 1 WING MOUNTEJan 8, 1997 · N945UP · Boeing 72722C · Wing, Control Surface Attach FittingsSDR UPS97221932Track · corrodedINSPECTION TYPE-D, NR 2 FLAP TRACK FWD ATTACH POINT LUGS CORRODED, BOLT CORRODED AND BUSHINGS WORN. CORROSION REMOVED IAW SRM 51-10-6. HFEC C/O PER NDT PT6 51-00-00 F13, MPI C/O PER BS6072, NO CORROSION FOUND. REPAIR TO NR 2 FLAP TRACK FORWARD ATTACH LUGS CJan 8, 1997 · N945UP · Boeing 72722C · Trailing Edge FlapsSDR UPS97221931Track · corrodedINSPECTION TYPE-D, NR 1 FLAP TRACK FORWARD ATTACH POINT LUG CORRODED, BOLT CORRODED AND BUSHINGS WORN. CORROSION REMOVED IAW SRM 51-10-6. HFEC C/O PER NDT PT6 51-00-00 F13, MPI C/O PER BS6072, NO CORROSION FOUND. NR 1 FLAP TRACK FORWARD LUGS REPAIRED PER BOJan 8, 1997 · N945UP · Boeing 72722C · Trailing Edge FlapsSDR UPS97221930Shim · corrodedINSPECTION TYPE-D, SHIM CORRODED ON NR 3 FLAP TRACK MID ATTACH POINT. NEW SHIM (P/N 69-11179-10) FITTED PER SRM 51-20-1.Jan 8, 1997 · N945UP · Boeing 72722C · Trailing Edge FlapsSDR UPS97221858Skin · corrodedINSPECTION TYPE-D, CORROSION FOUND IN CROWN SKIN BS 441 TO 521 S4R TO S10L. CROWN SKIN REPLACED, NO OEM SKINS AVAILABLE. SKIN REPLACED IN SECTIONS PER BOEING INSTRUCTIONS, REF UPS ENGINEERING FILE NR 727-53-1855.Jan 8, 1997 · N945UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR 97FDEA00083Angle · double holesNR 0637 026. WHILE WORKING 7-5300-7-230YM1 PT 3, FOUND EXISTING DOUBLE HOLE IN L-ANGLE BS 925-950, LBL 63, WL 200. REMOVED L- ANGLE. FABRICATED NEW ANGLE, DRILLED, TREATED AND INSTALLED FASTENERS I.A.W. BAC DWG 65-18745, 65-18332 AND FED-EX SRM 51-10-1.Jan 8, 1997 · N102FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 97FDEA00058Frame · crackedNR 0609 012 FWD LT OVERWING EXIT LOWER WENCE FRAME, HAS A CRACK BETWEEN FASTENER HOLES AT O/B EDGE OF FRAME THAT ATTACHES TO OUTER SKIN. *S/D* REMOVED AND REPLACED FWD LT OVERWING EXIT, FWD LOWER CORNER FRAME IAW FED-EX SRM 51-30-2.Jan 8, 1997 · N102FE · Boeing 72722C · Emergency ExitsSDR 97FDEA00057Bulkhead Angle · crackedNR 0618 011 CORROSION BS 178 BULKHEAD L-ANGLE LBL 28, WL 208 TO WL 224. *S/D* REMOVED CORROSION AND FOUND CHORD L-ANGLE TO BE CRACKED. REMOVED CHORD AND REPLACED PER FED-EX SRM 51-10-1, 51-30-2.Jan 8, 1997 · N102FE · Boeing 72722C · Fuselage Main, BulkheadSDR 97FDEA00030Stringer · corrosionNR 0595 002 CORROSION (C53-224-01) ON STRINGER 4 RT BS 460 TO 360. *S/D* REMOVED DAMAGED STR 4 RT, BS 410 TO 450. FABRICATED NEW PARTS AND INSTALLED PER FED-EX 727 SRM 53-10-3.Jan 8, 1997 · N102FE · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS97221888Support · corrodedINSPECTION TYPE-D, NR 9 SPOILER SUPPORT CASTING HAS CORROSION ON PERIPHERY OF BOLT HOLE SPOILER CASTING. REPLACED PER BOEING DRAWING 65-16216.Jan 7, 1997 · N945UP · Boeing 72722C · SpoilersSDR UPS97221884Support · corrodedINSPECTION TYPE-D, NR 7 SPOILER SUPPORT CASTING HAS CORROSION ON PERIPHERY OF BOLT HOLE. SPOILER CASTING REMOVED AND REPLACED IAW BOEING DRAWING 65-16216.Jan 7, 1997 · N945UP · Boeing 72722C · SpoilersSDR UPS97221857Floor Beam · corrodedINSPECTION TYPE: D. FLOOR BEAM CORRODED AT BS 344. UPPER T-SECTION REPLACED BETWEEN RBL 70 AND LBL 70.Jan 7, 1997 · N945UP · Boeing 72722C · Fuselage Main, Floor BeamSDR UPS97221856Support · corrodedINSPECTION TYPE: D. CORROSION FOUND ON FWD LAVATORY PARTITION SUPPORT RUNNING FROM BS 310 -BS 350 AT RBL 16 APPROX FLOOR LEVEL. NEW TOP-HAT SECTION INSTALLED PER SRM 51-30-2. FABRICATED FROM BAC 15 10-335 EXTRUSION.Jan 7, 1997 · N945UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR 97FDEA00070Stringer · corrodedNR 0353 020. CORROSION (C53-224-01) ON STRINGER 2 RT BS 560-BS 520. REMOVED CORRODED STRINGER 2 RT FROM BS 510-570 AND FABRICATED AND INSTALLED REPAIR PARTS ON AIRCRAFT PER FED-EX SRM 53-10-3.Jan 7, 1997 · N102FE · Boeing 72722C · Fuselage Main, Longeron/StringerSDR 97FDEA00055Skin · corrodedNR 0356 008. CORROSION (C53-224-05) ON UPPER SURFACE OF CENTER WING TANK AT BS 757, RBL 65, WL 204. REMOVED CORROSION AND REPAIRED I.A.W. FED-EX E.A. NR 7-5710-32133.Jan 6, 1997 · N102FE · Boeing 72722C · Fuselage Main, Plate/SkinSDR 97FDEA00027Frame · corrodedNR 0367 001 CORROSION (C53-111-01, 2) ON TOP OF FRAME AT BS 680, WL 156, LBL 20.5. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. REMOVED CORRODED MATERIAL AND REPAIRED CORRODED FRAME AT BS 680, WL 156, LBL 20.5 IAW FED-EX SRM 51-40-3.Jan 6, 1997 · N102FE · Boeing 72722C · Fuselage Main, FrameSDR DHL96705002Actuator · crackedSYSTEM-A HYDRAULICS SYSTEM FAILED ON DEPARTURE, QUANTITY WAS ZERO. FOUND NR 3 L/E SLAT ACTUATOR HOUSING CRACKED. REPLACED SAME.Dec 23, 1996 · N705DH · Boeing 72722C · Leading Edge Slat ActuatorSDR RAAA96B2048Battery Pack · dischargedLT AFT OVERWING EMERGENCY EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE.Dec 17, 1996 · N832RV · Boeing 72722C · Emergency LightingSDR RAAA96B2047Battery Pack · dischargedLT FWD OVERWING EMERGENCY EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE.Dec 17, 1996 · N832RV · Boeing 72722C · Emergency LightingSDR DHL96705001Instrument Amp · failedON CLIMBOUT, CAPT ADI DISPLAYED GYRO AND STEER FLAGS. REMOVED AND REPLACED NR 1 INSTRUMENT AMP, OPS CHECK OK PER M/M 34-62-61.Dec 17, 1996 · N705DH · Boeing 72722C · Indicating/Recording SystemSDR RAAA96B2046Pbe · failedFLIGHT ATTENDANT REPORTED ROW 22 PBE RED INDICATOR PIN PROTRUDING. CHANGED PBE DUE SEAL FAILURE.Dec 16, 1996 · N832RV · Boeing 72722C · Passenger Oxygen SystemSDR UPS96221745Slat Actuator · inoperativeINSPECTION TYPE-N/A, NR 2 SLAT WOULD NOT RETRACT AFTER T/O. COMPLETED AOM PROCEDURES, DUMPED FUEL AND RETURNED TO OAK. REPLACED NR 2 SLAT ACT AS PER MM 27-81-32, SLAT OPS CHKS NORMAL ON GROUND (P/N 141095-9-2) (S/N 3997L) OFF, (S/N 01405BDJLMN) ON.Dec 12, 1996 · N929UP · Boeing 72722C · Leading Edge Slat ActuatorSDR RAAA96B2045Pbe · failedDURING SERVICE CHECK, FOUND COCKPIT PBE RED INDICATOR PIN PROTRUDING. CHANGED PBE DUE SEAL FAILURE.Dec 8, 1996 · N832RV · Boeing 72722C · Portable Oxygen SystemSDR RAAA96B2044Lamp · failedCENTER LEFT WING EXTERNAL EMERGENCY LIGHT FAILED SERVICE CHECK. REPLACED 2 LAMPS.Dec 6, 1996 · N832RV · Boeing 72722C · Emergency LightingSDR RAAA96B1027Hose · failedON GEAR RETRACTION AFTER DEPARTURE A-SYSTEM HYD QUANTITY AND PRESSURE WENT TO ZERO. RETURNED TO AKN. REPLACED FAILED LT MLG ACTUATING CYLINDER DOWN SUPPLY HOSE.Nov 15, 1996 · N831RV · Boeing 72722C · Hydraulic System, MainSDR RAAA96B2043Battery Pack · dischargedROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE.Nov 9, 1996 · N832RV · Boeing 72722C · Emergency LightingSDR RAAA96B2042Battery Pack · dischargedROW 22 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE.Nov 9, 1996 · N832RV · Boeing 72722C · Emergency LightingSDR CA961203005Duct · twisted(CAN) ON TURNAROUND CREW NOTICED TWISTED DUCT ASSEMBLY ON #5 THERMAL ANTI-ICE TELESCOPING DUCT. REPLACED.Nov 6, 1996 · Boeing 72722C · Airfoil Anti/De-ice SystemSDR UPS96221543Fitting · crackedINSPECTION TYPE-D, FUSELAGE BS 940 FITTING, HFEC SHOWS CRACK INDICATIONS IN OUTER PORTION OF FITTING BETWEEN UPPER AND LOWER FASTENER HOLES SECOND ROW FROM FRONT AND LOWER FASTENER HOLE IN THIRD ROW FROM FRONT. REPLACED RT SIDE 940 FITTING, INSTALLED REPLACEMNov 4, 1996 · N942UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS96221542Frame · corrodedINSPECTION TYPE-D, TENSION BOLTS CORRODED AT BS 360 FRAME BELOW STR 21. REPAIRED PER UPS EO B727-53-1827.Nov 4, 1996 · N942UP · Boeing 72722C · Fuselage Main, FrameSDR UPS96221540Flap Track · corrodedINSPECTION TYPE-D, LEFT I/B FLAP O/B FLAP TRACK NR 3 HAS RUST IN AREA OF AFT MOUNT PAD AND ON MOUNT PAD ON FALSE SPAR. REMOVED CORROSION PER EO B727-57-0178.Nov 4, 1996 · N942UP · Boeing 72722C · Trailing Edge FlapsSDR UPS96221539Stringer · crackedINSPECTION TYPE-D, FUSELAGE STR 18A, RT SIDE CRACKED IN OUTER FLANGE AT BRACKET ATTACH HOLE AT BS 940. REPAIRED STRINGER PER UPS EO B727-53-1830.Nov 4, 1996 · N942UP · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS96221538Flap Carriage · corrodedINSPECTION TYPE-D, RUST ON EXTERNAL SURFACES OF LEFT O/B FLAP, I/B CARRIAGE NR 2. REPLACED WITH OVERHAULED CARRIAGE IAW MM 27-51-13.Nov 4, 1996 · N942UP · Boeing 72722C · Trailing Edge FlapsSDR UPS96221537Floorbeam · corrodedINSPECTION TYPE-D, STA 334 FLOORBEAM UPPER CHORD HAS CORROSION FROM LBL 65 TO RBL 24. REPLACED DAMAGED SECTION OF FLOORBEAM PER SRM 51-10-1, 51-30-2.Nov 4, 1996 · N942UP · Boeing 72722C · Fuselage Main, Floor BeamSDR UPS96221536Carriage · corrodedINSPECTION TYPE-D, RUST ON EXTERNAL SURFACE OF LEFT I/B FLAP, O/B CARRIAGE. REPLACED WITH OVERHAULED CARRIAGE PER MM 27-51-03.Nov 4, 1996 · N942UP · Boeing 72722C · Trailing Edge FlapsSDR UPS96221535Flap Carriage · corrodedINSPECTION TYPE-D, RUST ON EXTERNAL SURFACE AND ON SPINDLE OF I/B FLAP I/B CARRIAGE. REMOVED AND REPLACED WITH OVERHAULED CARRIAGE MM 27-51-03.Nov 4, 1996 · N942UP · Boeing 72722C · Trailing Edge FlapsSDR UPS96221534Flap Carriage · corrodedINSPECTION TYPE-D, RIGHT O/B FLAP I/B CARRIAGE, NR 7, HAS RUST AROUND SPINDLE. REMOVED AND REPLACED WITH OVERHAULED CARRIAGE PER MM 27-51-13.Nov 4, 1996 · N942UP · Boeing 72722C · Trailing Edge FlapsSDR UPS96221533Skin · corrodedINSPECTION TYPE-D, LFEC INSPECTION SHOWS MATERIAL LOSS OF 10 PERCENT AT BS 259.5 AFT PANEL FROM STR 6L TO STR 10L. FABRICATED AND INSTALLED REPAIR PER UPS EO B727-5310-1371E.Nov 4, 1996 · N942UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS96221532Skin · corrodedINSPECTION TYPE-D, LFEC INSPECTION SHOWS MATERIAL LOSS OF 10 PERCENT AT BS 259.5 FWD PANEL, FROM STR 19L TO STR 24L. FABRICATED AND INSTALLED REPAIR PER UPS EO B727-5310-1371E.Nov 4, 1996 · N942UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS96221531Skin · corrodedINSPECTION TYPE-D, LFEC INSPECTION SHOWS MATERIAL LOSS OF 10 PERCENT AT BS 259, FWD PANEL, FROM STR 19R TO 24R. FABRICATED AND INSTALLED REPAIR PER UPS EO B727-5310-1371E.Nov 4, 1996 · N942UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR RAAA96B1026Battery Pack · dischargedRIGHT SERVICE DOOR EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE.Nov 1, 1996 · N831RV · Boeing 72722C · Emergency LightingSDR RAAA96B1025Battery Pack · dischargedRIGHT AFT OVERWING EMERGENCY EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE.Nov 1, 1996 · N831RV · Boeing 72722C · Emergency LightingSDR RAAA96B1024Battery Pack · dischargedRIGHT FWD OVERWING EMERGENCY EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE.Nov 1, 1996 · N831RV · Boeing 72722C · Emergency LightingSDR RAAA96B1023Battery Pack · dischargedROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE.Nov 1, 1996 · N831RV · Boeing 72722C · Emergency LightingSDR RAAA96B1022Battery Pack · dischargedROW 22 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE.Nov 1, 1996 · N831RV · Boeing 72722C · Emergency Lighting
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