Boeing 727-27C

Service difficulty reports · 1,078

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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 = '72727C'
  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 UPS97223160Floorbeam · corrodedINSPECTION TYPE:SI, CORROSION (C53-224-01.00-03) ON FLOORBEAM AROUND BOTTOM SIDE OF NUT CLIP HOLES STA 1110 RBL 40 TO 65 WL 208. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPAIRED STA 1110 FLOORBEAM IAW SRM 53-10-8.May 27, 1997 · N914UP · Boeing 72727C · Fuselage Main, Floor BeamSDR UPS97223151Connector · chafedINSPECTION TYPE:N/A, DURING FLIGHT EXPERIENCED A TEN MINUTE PERIOD OF INTERMITTENT ILLUMINATION OF NR 1 ENG A/SS 13 FIRE DETECTION FAULT LIGHTS. REMAINED OUT FOR REST OF FLIGHT. FOUND NR 1 ENGINE FIREWALL CONNECTOR (D9511P) WIRES CHAFING TO GROUND WIRES. REMay 27, 1997 · N908UP · Boeing 72727C · Fire DetectionSDR UPS97223163Cable Drum · corrodedINSPECTION TYPE:SI, FWD CABLE DRUM FOR WFA ABOVE OUTBOARD FLAP CONTROL VALVE IS CORRODED. REMOVED AND REPLACED CABLE DRUM AND SUPPORT IAW MM 27-51-51.May 26, 1997 · N914UP · Boeing 72727C · Trailing Edge Flap Control SystemSDR UPS97223162Support Fitting · corrodedINSPECTION TYPE:SI, NR 2 FWD FLAP TRACK ATTACH FITTING CORRODED. REMOVED AND REPLACED FWD ATTACH FITTING PER SRM 51-30-4.May 25, 1997 · N914UP · Boeing 72727C · Trailing Edge FlapsSDR UPS97223166Web · crackedINSPECTION TYPE:SI, CRACK IN PRESSURE WEB BS 292 RBL 24 WL 150 (MARKED). REMOVED AND REPLACED PRESSURE WEB IAW 51-40-2, 53-10-2, 53-10-9 AND MM 51-20-00, 51-20-151.May 24, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97223165Intercostal · corrodedINSPECTION TYPE:SI, CORROSION (C53-224-01.00-02) ON PRESSURE WEB STIFFENER BS 870 TO 880 LBL 46 WL 208. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-1, 51-20-4 AND MM 51-20-151.May 24, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97223164Floorbeam · corodedINSPECTION TYPE:SI, CORROSION (C53-224-01.05-01) CORROSION ON FLOORBEAM AT BS 544 FROM LBL 60 TO RBL 14 WL 208. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-30-2, 51-10-2.May 24, 1997 · N914UP · Boeing 72727C · Fuselage Main, Floor BeamSDR UPS97223034Beam · corrodedINSPECTION TYPE:SI, CORROSION (C53-224-01.05-02) CORROSION ON STUB BEAM AT BS 824 RBL 57 WL 207. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED STUB BEAM IAW SRM 51-30-2, 51-30-5 AND MM 51-20-151.May 23, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97223035Track · corrodedINSPECTION TYPE:SI, CORROSION (C57-581-06.00-03) NR 4 FLAP TRACK FWD ATTACH LUGS HAVE FITTING CORROSION. FLAP TRACK WAS REPLACED DUE TO TIME CONSTRAINTS ON MAINTENANCE CHECK IAW MM 27-51-31.May 22, 1997 · N914UP · Boeing 72727C · Trailing Edge FlapsSDR UPS97223038Tension Tie · corrodedINSPECTION TYPE:SI, VERTICLE FIN TENSION TIE RIB ALL SIX BUSHINGS ARE LOOSE AND MIGRATING. WHILE PREPARING RIB FOR REBUSHING HOLES FOUND HOLES TO BE CORRODED OUT OF LIMITS IAW EO 727-55-0071. REPLACED TENSION TIE IAW SRM 51-10-1, 51-30-2.May 21, 1997 · N914UP · Boeing 72727C · Vertical StabilizerSDR UPS97222983Doorway Frame · corrodedINSPECTION TYPE:SI UPON REMOVAL OF MAIN CARGO DOOR, FOUND UPPER DOORWAY FRAME WEB FROM STA 480 TO 620 TO HAVE CORROSION ON IT. REMOVED CORRODED WEB AND DOUBLERS, FABRICATED NEW PARTS AND INSTALLED IAW SRM 51-30-2.May 20, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222982Expansion Link · corrodedINSPECTION TYPE:SI CORROSION (C53-132-01.00-01), ON EXPANSION LINK AT BS.740 LBL 13, WL 160. REMOVED CORRODED EXPANSION LINK AND INSTALLED NEW PARTS IAW SRM 51-30-2.May 20, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222981Frame · crackedINSPECTION TYPE:SI CRACK ON FRAME AT STA 277 ABOVE STR 16 RIGHT, FRAME ALSO CRACKED ABOVE STR 15 RT. REPAIRED CRACKED FRAME AT STA 277 FROM ABOVE STRINGER 15R TO BELOW STR 16 RT IAW SRM 51-40-2 CRACK REPAIR ENCOMPASSED CRACKS FOUND ON NRC 685606.May 20, 1997 · N914UP · Boeing 72727C · Fuselage Main, FrameSDR UPS97222961Skin · delaminatedINSPECTION TYPE-SI, NR 8 SPOILER HAS A CREASED DENT ON THE UPPER SURFACE. REMOVED DAMAGED AREA APPLIED REPAIR AND REFINISHED IAW SRM 57-50-06.May 15, 1997 · N914UP · Boeing 72727C · SpoilersSDR UPS97222959Stiffener · corrodedINSPECTION TYPE-SI, AREAS OF CORROSION ON BREATHER WEB STRAP AT BS 855 BETWEEN LBL 12 AND RBL 12 WL 150. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED WEB STRAP IAW SRM 51-10-1, 51-30-2 AND 51-30-5.May 15, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222958Fitting · corrodedINSPECTION TYPE:SI CORROSION (C53-224-01.05-02), CORROSION ON 'L' SUPPORT OF CARGO TIE DOWN AT BS 849 LBL 57 WL 207. CORROSION REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED 'L' SUPPORT ANGLE AT BS 849 LBL 57 WL 207 IAW SRM 51-10-1, 51-30-May 15, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222986Intercostal · corrodedINSPECTION TYPE:SI CORROSION (C53-221-01.01-01) AROUND FASTENER HEADS AT STA 224 LBL 44 WL 227. MECHANICALLY REMOVED CORROSION, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. FABRICATED AND REPLACED INTERCOSTAL AT STA 224 LBL 44 WL 227.May 14, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222985Beam · corrodedINSPECTION TYPE:SI CORROSION ON SPANWISE BEAM VERTICAL WEB AT BS 744 LB 43 WL 154. REMOVED CORROSION FROM WEB AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-1 AND SRM 51-40-2.May 14, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222963Seat Track · corrodedINSPECTION TYPE-SI, CORROSION (4-25-02) AT NUTPLATE HOLES LBL 25, WL 208 BS 462 AND 466 AND 470 SEAT TRACK SECTION TO BE REPLACED ON CARD NR 685939.May 14, 1997 · N914UP · Boeing 72727C · Fuselage, Seat/Cargo Attach FittingsSDR UPS97222962Skin · delaminatedINSPECTION TYPE-SI, NR 1 SPOILER PANEL IS DELAMINATED ON THE UPPER SURFACE OUTBOARD FORWARD CORNER. REMOVED DELAMINATION, REPAIRED AREA AND REFINISHED IAW SRM 57-50-6.May 14, 1997 · N914UP · Boeing 72727C · SpoilersSDR UPS97222960Skin · crackedINSPECTION TYPE-SI, LINEAR INDICATION NOTED ON RT ELEVATOR X-RAY VIEW 3, 2 INCHES FROM I/B EDGE AND 13 INCHES FROM T/E OF ELEVATOR (INTERNAL). REPAIRED CRACK 2 INCHES FROM I/B EDGE 13 INCHES FROM T/E OF RT ELEVATOR IAW SRM 55-20-3 AND 51-80-7 ELEVATOR MOMENT May 13, 1997 · N914UP · Boeing 72727C · Elevator, Plate/SkinSDR UPS97223303Frame · crackedINSPECTION TYPE:SI, CORROSION (C53-113-01.00-01) AND CRACKED FOUND ON BS 680 FRAME RT SIDE IN FWD CARGO PIT DISCREPANCIES FOUND WHILE WORKING CUSTOMER CARD NR 685843. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED FRAME PERMay 12, 1997 · N914UP · Boeing 72727C · Fuselage Main, FrameSDR UPS97223301Floorbeam · corrodedINSPECTION TYPE:SI, WHILE ACCESSING ON NRC 685905 INTERIOR 124 FOUND 880 FLOORBEAM LWR FLANGE TO BE CORRODED AT RBL 45 RBL 46 WL 201. REMOVED AND REPLACED 880 FLOORBEAM PER UPS ENGINEERING FILE NR B727-53-1427 INSTALLED FUEL FEED LINES AND SHROUD PER MM 28-22May 12, 1997 · N914UP · Boeing 72727C · Fuselage Main, Floor BeamSDR UPS97223159Attach Fitting · corrodedINSPECTION TYPE:SI, NR 7 FLAP TRACK FWD ATTACH FITTING IS CORRODED AT FWD MOUNT LUG. REPLACED FITTING IAW TRAMCO EWO 97-2224 UNDER FILE NUMBER 727-57-1838 AND MM 27-51-31.May 8, 1997 · N914UP · Boeing 72727C · Trailing Edge FlapsSDR UPS97223300Beam · corrodedINSPECTION TYPE:SI, WHILE PERFORMING TC NR 2231 (VERTICAL TAIL TIE BEAM SPLICE INSPECTION UPPER SPLICE) DISCOVERED SPLICE TO BE CORRODED AROUND BUSHING AREAS. REMOVED VERTICAL TAIL BEAM SPLICE FABRICATED AND INSTALLED NEW BUSHINGS PER MM 27-20-141.May 7, 1997 · N914UP · Boeing 72727C · Vertical StabilizerSDR UPS97223213Web · corrodedINSPECTION TYPE:SI, CORROSION (4-25-02) AROUND FASTENERS UNDER SEAT TRACK ON VENT WEB AT BS 620 TO 646 RBL 65, WL 207. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 51-10-6. FABRICATED AND INSTALLED WEB PER SRM 53-10-1, 51-10-2 AND SRM 51-30-2.May 7, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97223158Stringer · corrodedINSPECTION TYPE:SI, CORROSION (C53-224-01.00-03) ON FLANGE OF STRINGERS RIGHT STA 1140 TO 1150. REMOVED DAMAGED SECTION OF STRINGER FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-10-3.May 7, 1997 · N914UP · Boeing 72727C · Fuselage Main, Longeron/StringerSDR UPS97223039Tab Hinge · corrodedINSPECTION TYPE:SI, LEFT WING I/B AILERON TAB HINGES ARE CORRODED OR CRACKED ON AILERON. REMOVED CORRODED HINGES AND INSTALLED NEW HINGES IAW SRM 51-30-2.May 6, 1997 · N914UP · Boeing 72727C · Aileron TabsSDR UPS97223037Track · corrodedINSPECTION TYPE:SI, CORROSION (C57-581-06.00-03) NR 3 FLAP TRACK HAS PITTING CORROSION ON AFT MOUNT PAD. NR 3 FLAP TRACK WILL BE REPLACED DUE TO OVERHAUL TIME CONSTRAINTS ON MAINTENANCE CHECK.May 6, 1997 · N914UP · Boeing 72727C · Trailing Edge FlapsSDR UPS97223036Track · corrodedINSPECTION TYPE:SI, CORROSION (C57-581-06.00-03) NR 3 FLAP TRACK FWD ATTACH LUGS HAVE PITTING CORROSION. TRACK WILL BE REPLACED DUE TO OVERHAUL TIME CONSTRAINTS ON MAINTENANCE CHECK ON CUST CARD NR 686449 IAW MM 27-51-31.May 6, 1997 · N914UP · Boeing 72727C · Trailing Edge FlapsSDR UPS97222984Bracket · corrodedINSPECTION TYPE:SI BS 740 EXPANSION LINK BRACKETS ARE CORRODED AT RBL 36 WL 160. REMOVED AND REPLACED EXPANSION LINK BRACKET IAW SRM 51-10-1 AND SRM 51-30-2.May 6, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222980Track · corrodedINSPECTION TYPE:SI (CORROSION C57-581-06.00-03), NR 4 FLAP TRACK RADIUS BLOCKS AT FWD MOUNT PAD BORES ARE CORRODED. FLAP TRACK WILL BE REPLACED ON CARD NR 686454 DUE TO OVERHAUL TIME CONSTRAINTS ON MAINTENANCE SCHEDULE.May 6, 1997 · N914UP · Boeing 72727C · Trailing Edge FlapsSDR UPS97222979Track · corrodedINSPECTION TYPE:SI CORROSION (C57-581-06.00-03), NR 4 FLAP TRACK BEARING SURFACES HAVE PITTING CORROSION AND PLATING IS WORN. FLAP TRACK WILL BE REPLACED ON CARD NR 686454 DUE TO OVERHAUL TIME CONSTRAINTS ON MAINTENANCE SCHEDULE.May 6, 1997 · N914UP · Boeing 72727C · Trailing Edge FlapsSDR CA970506003Hose · ruptured(CAN) ON DEPARTURE LOST 'A' SYSTEM HYDRAULIC SYSTEM. MAIN LANDING GEAR INBOARD DOOR-CLOSE LINE FAILED. REPLACED.Apr 25, 1997 · Boeing 72727C · Hydraulic System, MainSDR UPS97222642Light · brokenFLT DECK EMERG EXIT LIGHT FELL OFF AND BROKE DURING LANDING (NOT DUE TO HARD LANDING). REINSTALLED LIGHT ASSY.Apr 18, 1997 · N908UP · Boeing 72727C · Emergency LightingSDR UPS97222643Spar Chord · corrodedINSPECTION TYPE:SI, CENTER SECTION UPPER REAR CHORD HAS EVIDENCE OF CORROSION SEPARATED FROM WEB LBL 6-36 WL 190. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED AND REPLACED REAR SPAR UPPER CHORD, SPLICE AND WEB ALL WORK DONE PER EWO NR 97-2109, UPS FILE NR 72Apr 17, 1997 · N909UP · Boeing 72727C · Wing SparSDR CA970429005Line · failed(CAN) ON DEPARTURE AIRCRAFT EXPERIENCED A HYDRAULIC SYSTEM DEPLETION DURING GEAR RETRACTION. AIRCRAFT RETURNED. R/H MAIN LANDING GEAR SEQUENCE VALVE "UC" PORT LINE FAILED, REPLACEDApr 17, 1997 · Boeing 72727C · Hydraulic System, MainSDR UPS97222638Sill · corrodedINSPECTION TYPE-SI, SSID (F-12) HFEC INSP OF UPPER SURFACE OF INNER SILL CHORD OF MAIN CARGO DOOR AT LBL 70 WL 208 BODY STATIONS 488, 501, 510 TO 520 525, 535, 550, 570, 580, 590 AND 600 EXHIBITS CORROSION INDICATIONS. REMOVED CORROSION FROM SILL AND INSTALLEApr 16, 1997 · N909UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222627Spar · corrodedINSPECTION TYPE-SI, CORROSION LT FIN MID SPAR CHORD (S-7) IS CHAFED AND FRETTING AT FS 225.7. REPAIRED PER EWO NR 97-2111, UPS FILE NR 727-55-0347.Apr 16, 1997 · N909UP · Boeing 72727C · Vertical Stabilizer, Spar/RibSDR UPS97222621Beam · damagedINSPECTION TYPE-SI, WHILE WORKING CUST ID C57-581-04-30 DISCOVERED O/B HOLE ON MLG BEAM COMMON TO NR 4 FLAP TRACK O/B HOLE TO HAVE THE UPPER SURFACE DAMAGED. REPAIRED PER EWO 97-2153 AND ENGINEERING FILE NR 727-57-1817 UPS.Apr 16, 1997 · N909UP · Boeing 72727C · Wing Miscellaneous StructureSDR UPS97222623Frame · corrodedINSPECTION TYPE-SI, CORROSION AROUND HANDLE HOUSING ON LT AFT EMERGENCY EXIT. REMOVED CORRODED FRAME PROCURED NEW FRAME AND INSTALLED IAW SRM 51-30-2.Apr 15, 1997 · N909UP · Boeing 72727C · Emergency ExitsSDR UPS97222622Frame · corrodedINSPECTION TYPE-SI, RT FWD EMERGENCY EXIT HAS CORROSION ON ITS HANDLE HOUSING. REMOVED CORRODED FRAME PROCURED NEW FRAME AND INSTALLED IAW SRM 51-30-2.Apr 15, 1997 · N909UP · Boeing 72727C · Emergency ExitsSDR UPS97222620Skin · corrodedINSPECTION TYPE-SI, LEFT WING LOWER SKIN CORRODED AT FLAP TRACK ATTACH POINT. REPAIRED PER EWO 97-2100 AND UPS ENG FILE NR 727-57-1803.Apr 15, 1997 · N909UP · Boeing 72727C · Wing, Plate/SkinSDR UPS97222618Spar Chord · chafedINSPECTION TYPE-SI, CORROSION RT FIN MID SPAR CHORD (S-7) IS CHAFED AND FRETTING AT FS 225.7. REPAIRED PER EWO 97-2111 AND UPS ENG FILE NR 727-55-0347.Apr 15, 1997 · N909UP · Boeing 72727C · Vertical Stabilizer, Spar/RibSDR UPS97222586Skin · corrodedINSPECTION TYPE-SI, WHILE WORKING CUST CARD NR 510847 FUSE 152 FOUND UPPER SIDE OF LOWER CENTER WING SKIN TO BE CORRODED AT STA 870 RBL 56. REMOVED CORROSION AND REWORKED SKIN IAW EWO 97-2132 UNDER FILE NR 727-57-1811.Apr 14, 1997 · N909UP · Boeing 72727C · Wing, Plate/SkinSDR UPS97222583Fitting · crackedINSPECTION TYPE-SI, CRACK INDICATIONS ON RT 950 BODY FORGING FORWARD O/B FLANGE AFT ROW BETWEEN STR 10R AND 11R. REPAIRED RT 950 BODY FORGING PER UPS EO B727-5310-3012.Apr 11, 1997 · N909UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222579Support Ftg · corrodedINSPECTION TYPE-SI, NR 11 SPOILER ACTUATOR FITTING LOWER MOUNT BOLT HOLES CORRODED. REMOVED AND REPLACED NR 11 SPOILER ACTUATOR SUPPORT FITTING IAW MM 27-51-131 MM 27-61-81 MM 27-61-01 AND SRM 51-30-2.Apr 11, 1997 · N909UP · Boeing 72727C · Drag Control ActuatorSDR UPS97222578Actuator Ftg · corrodedINSPECTION TYPE-SI, NR 4 SPOILER SUPPORT FITTING LOWER MOUNT HOLES CORRODED. REMOVED AND REPLACED NR 4 SPOILER ACTUATOR FITTING IAW MM 27-61-01, MM 27-51-131, MM 27-61-81 AND SRM 51-30-2.Apr 11, 1997 · N909UP · Boeing 72727C · Drag Control ActuatorSDR UPS97222626Spar Chord · corrodedINSPECTION TYPE-SI, WHILE WORKING CUSTOMER CARD 510847, FOUND THE LOWER CENTER SPAR CHORD TO BE CORRODED. REMOVED CORRODED SPAR CHORD PROCURED NEW SPAR CHORD AND INSTALLED IAW EWO 97-2136 UNDER FILE NR 727-57-1812.Apr 10, 1997 · N909UP · Boeing 72727C · Wing SparSDR UPS97222576Actuator Ftg · corrodedINSPECTION TYPE-SI, NR 12 SPOILER ACTUATOR FITTING LOWER MOUNT BOLTS CORRODED. REMOVED NR 12 SPOILER FITTING FOUND TO BE OUT OF LIMITS. REPLACED NR 12 SPOILER FITTING PER MM 27-61-81.Apr 10, 1997 · N909UP · Boeing 72727C · Drag Control Actuator
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