N214UP, cancelled May 6, 2003

Service difficulty reports · 91

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N214UP' AND deregistration_id = 'N214UP-2003-05-06'
  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 UPS01237375Battery · dischargedINSPECTION TYPE:PFLT CREW ENTRANCE EMERGENCY EXIT LIGHT DOES NOT TEST. REPLACED BATTERIES, OPS CHECKED GOOD.Dec 20, 2001 · N214UP · Boeing 7272A1 · Emergency LightingSDR UPS01237193Bulkhead · corrodedINSPECTION TYPE:IN FWD SIDE OF BS 1342 NR 2 ENGINE BULKHEAD IS CORRODED AT APPROX LBL TO LBL 40 AS VIEWED LOOKING AFT STANDING ON AIRSTAIRS JUST O/B OF NR 2 ENGINE GENERATOR FEEDER CABLES NUMEROUS FASTENERS ARE CORRODED AS IS A STIFFENER. CLEANED AND TREATED Oct 30, 2001 · N214UP · Boeing 7272A1 · Fuselage Main, BulkheadSDR UPS01236767Window · crackedINSPECTION TYPE:PFLT CAPTAIN'S L1 WINDOW INNER PANE CRACKED AND ARCHING. REPLACED L1 WINDOW PER MM 56-11-11.Sep 5, 2001 · N214UP · Boeing 7272A1 · Flight Compartment WindowsSDR UPS01236152Battery · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES.Jun 19, 2001 · N214UP · Boeing 7272A1 · Emergency LightingSDR UPS01235403Terminal · damagedAMBER MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT. FOLLOWED PROCEDURES PER AOM CH 2. DIVERTED FLIGHT TO FWA. DEFERED PER MEL 52-4 AND COMPLIED WITH DMP VERIFYING THAT MAIN CARGO DOOR CLOSED AND LOCKED PRIOR TO DEPARTURE. ITEM DEFERRED M211761 PLACARD INSTLD Mar 23, 2001 · N214UP · Boeing 7272A1 · Door Warning SystemSDR UPS01235239Skin · crackedINSPECTION TYPE:C, LEFT WING I/B AFT FLAP LOWER SURFACE L/E CRACKED AT O/B CENTER ECCENTRIC ROLLER FITTING CUTOUT. REPAIRED PER SRM 57-50-4.Feb 15, 2001 · N214UP · Boeing 7272A1 · Trailing Edge FlapsSDR UPS01235023Stringer · corrodedINSPECTION TYPE:C CORROSION (C53-100-01.00-04) UNDER STRINGER 29L BETWEEN BS 1166- BS 1183 AND T-CLIP AT 1183. REMOVED CORROSION ON STRINGER 29L IN AN AREA OF 1.0 X.5 X.020 INCH FROM ORIG THICKNESS OF .090 INCH OUT OF LIMITS PER SRM 53-10-1, SRM 53-10-2 SRM 5Jan 10, 2001 · N214UP · Boeing 7272A1 · Fuselage Main, Longeron/StringerSDR UPS01235022Shear Tie · corrodedINSPECTION TYPE:C CORROSION (C53-113-01.00-01) ON FRAME SHEAR TIE, BS 600 BETWEEN STR 28R AND STR 28L. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-4, 51-10-2, 51-30-2 AND MM 51-20-151.Jan 7, 2001 · N214UP · Boeing 7272A1 · Fuselage Main, StructureSDR UPS99230991Battery Pack · dischargedINSPECTION TYPE:N/A, ENTRY DOOR EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.Oct 26, 1999 · N214UP · Boeing 7272A1 · Emergency LightingSDR UPS99230990Battery Pack · dischargedINSPECTION TYPE:N/A, COCKPIT EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.Oct 26, 1999 · N214UP · Boeing 7272A1 · Emergency LightingSDR UPS99230241Skin · corrodedINSPECTION TYPE:C WHILE WORKING CARD 973519, FOUND CORROSION ON INNER SKIN AT BS 1005, RBL 7, WL 148. REMOVED CORRODED SECTION OF SKIN AT BS 1005, RBL 7, WL 148 AND REPAIRED IAW ER NR 99-5802 AND SRM 53-30-03 FIG 3A.Jul 28, 1999 · N214UP · Boeing 7272A1 · Fuselage Main, Plate/SkinSDR UPS99230239Keel Beam · corrodedINSPECTION TYPE:C CORROSION (C53-113-01.06-02) BS 982 RT KEEL BEAM. REMOVED CORRODED KEEL BEAM SEGMENT AND REPLACED WITH NEW SEGMENT IAW ER 99-5790.Jul 28, 1999 · N214UP · Boeing 7272A1 · Fuselage Main, KeelSDR UPS99230240Stringer · corrodedINSPECTION TYPE:C WHILE WORKING CUST CARD NR 973522 FOUND CORROSION ON STR 20R STA 1153. REMOVED CORRODED STRINGER BS 1153 AND REPLACED WITH NEW STRINGER IAW SRM 51-40-03, 51-10-1, 51-30-02, DRW NR 65-16349.Jul 27, 1999 · N214UP · Boeing 7272A1 · Fuselage Main, Longeron/StringerSDR UPS99230238Clip · corrodedINSPECTION TYPE:C CORROSION ON SHEAR TIE T-CLIP AT BS 990, RBL 8, WL 148 BETWEEN STR 29-29 R (WHILE WORKING CARD 973519). REMOVED CORRODED T-CLIP AND REPLACED WITH NEW T-CLIP IAW 51-10-1 AND 51-30-02.Jul 26, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230172Shear Tie · corrodedINSPECTION TYPE:C WHILE WORKING 973519, FOUND CORROSION ON SHEAR TIE AT BS 970 RBL 8, WL 148 BETWEEN STRINGER 28, 29R. REPAIRED SHEAR TIE AT BS 970 RBL 8 WL 148 PER SRM 53-10-1, 51-30-2, 53-10-4, 51-10-2.Jul 25, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230171Shear Tie · corrodedINSPECTION TYPE:C CORROSION ON FRAME SHEAR TIE BS 990, RBL 4, WL 148 BETWEEN STR 29-30R. REMOVED DAMAGE SHEAR TIE AND REPAIRED IAW SRM 53-10-04 FIG 15.Jul 23, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230170Seat Track · corrodedINSPECTION TYPE:C CORROSION ON SEAT TRACK UPPER SURFACE O/B SIDE BS 950, LBL 45. REMOVED AND REPLACED SEAT TRACK FROM BS 870 TO BS 960.Jul 23, 1999 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99230156Crease Beam · crackedINSPECTION TYPE:C, LEFT I/B CREASE BEAM IS CUT AT BS 116, WL 209, LBL 64. FOUND CREASE BEAM TO BE CRACKED AT BS 1166, WL 209, LBL 64 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF CREASE BEAM FROM BS 1157 TO BS 1177, FABRICATED NEW CREASE BEAM, REPAIJul 23, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230157Splice · corrodedINSPECTION TYPE:C, WHILE WORKING CARD 973519, FOUND CORROSION AND GOUGE ON STRINGER SPLICE BS 1000, STR 29R, RBL 6, WL 148. REMOVED AND REPLACED STR SPLICE BS 1000 STR 29R, RBL 6, WL148, WITH NEW STR SPLICE.Jul 22, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230178Crease Beam · corrodedINSPECTION TYPE:C CORROSION ON CREASE BEAM I/B BS 1166, WL 209 RBL 64. CORROSION OUT OF LIMITS REPAIR WILL BE ACCOMPLISHED ON NRC 973389 DO TO OTHER DEFECTS REPAIR WILL COVER FROM 1138-1176.*Jul 12, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230177Crease Beam · corrodedINSPECTION TYPE:C CORROSION ON I/B CREASE BEAM BS 1170 WL 208 LBL 64. CORROSION OUT OF LIMITS REPAIRS WILL BE ACCOMPLISHED ON NRC 973397, WHICH ENCOMPASS THIS AREA. REPAIR GOES FROM BS 1159-1176.Jul 12, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS99230112Frame · crackedINSPECTION TYPE:C, CRACKS NOTED IN BS 1183, LBL 18 DOOR FRAME. ONE CRACK AT NR 7L DOOR STOP CUTOUT AND THE OTHER CRACK AT 2 FWD OF NR 7L DOOR STOP CUTOUT. ACCESSED AREA AT 1183 FRAME AND REPAIRED FRAME IAW SB B727-53-0210.Jul 6, 1999 · N214UP · Boeing 7272A1 · Fuselage Main, FrameSDR UPS99229972Window · shatteredINSPECTION TYPE:N/A, AIRCRAFT DIVERTED INTO TUL DUE TO L-2 WINDOW SHATTERED IN FLIGHT. *S/D* REMOVED AND REPLACED L-2 WINDOW WITH NEW PER MM 56-12-11 (P/N 5-71762-39) (S/N 1429) OFF. (P/N 5-71762-39) (S/N 84-H -3-5-116) ON. HEAT CONTROL (P/N 1231-2) (S/N 9Jun 25, 1999 · N214UP · Boeing 7272A1 · Flight Compartment WindowsSDR UPS98225724Skin · corrodedINSPECTION TYPE:SI CORROSION (C53-224-01.00-02) ON INTERIOR OF SKIN AROUND PERIMETER OF SIDELIGHT BETWEEN BS 720B PLUS 5 AND 720C LBL 73 WL 218-228 BETWEEN STR 14L AND 16L. CORROSION OUT OF LIMITS IAW SRM 53-30-3. REPAIRED SKIN AROUND PERIF OF LT SIDELIGHT IFeb 5, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Plate/SkinSDR UPS98225711Rib · corrodedINSPECTION TYPE-SI, FRETTING CORROSION ON VERTICAL STAB L/E FAIRING RIB, FWD LIP AT FIN STA 55.9. RECEIVED NEW TEE-EXTRUDED RIB AND INSTALLED WEB TO NEW RIB PER 727 SRM 51-30-2.Feb 2, 1998 · N214UP · Boeing 7272A1 · Vertical Stabilizer, Spar/RibSDR UPS98225664Bottle Pin · corrodedINSPECTION TYPE-SI, R/W REAR BOTTLE PIN IS CORRODED. ALSO, FWD AND AFT BUSHINGS ARE MISSING SECTION OF MICARTA INNER SLEEVE CORROSION (C53-100-05.00-04). REMOVED AND REPLACED R/W AFT BOTTLE PIN ON NRC 657574 IAW MM 57-41-01, BUSHING REPLACED ON AOG (BOEING) Jan 27, 1998 · N214UP · Boeing 7272A1 · Wing, Fuselage Attach FittingsSDR UPS98225663Rear Spar · crackedINSPECTION TYPE-SI, L/W STRINGER 2ND FROM REAR SPAR ON UPPER SKIN AT WING STATION 686.5 IS CRACKED AT STRINGER 5 TO 10. REPAIRED L/W STRINGER 2ND FROM REAR SPAR (STR 10) AT STA 686.5 IAW UPS EO B727-5710-0314.Jan 27, 1998 · N214UP · Boeing 7272A1 · Wing SparSDR UPS98225709Support · corrodedINSPECTION TYPE-SI, NR 7 FLAP TRACK FWD ATTACH FITTING IS CORRODED AT AFT BOLT HOLES FLAP TRACK FWD ATTACH POINT BUSHING HAS MIGRATED. ALSO, FWD HARDWARE REQUIRES REPLACEMENT I/B AND O/B AT RADIUS BLOCKS. REPLACED NR 7 FLAP TRACK FITTING IAW SRM 51-10-1 WILLJan 22, 1998 · N214UP · Boeing 7272A1 · Trailing Edge FlapsSDR UPS98225710Support · corrodedINSPECTION TYPE-SI, NR 4 FLAP TRACK FWD ATTACH FITTING IS CORRODED AT FLAP TRACK FWD ATTACH LUG I/B SIDE. REMOVED AND REPLACED NR 4 FLAP TRACK FWD FITTING IAW MM 32-11-51.Jan 18, 1998 · N214UP · Boeing 7272A1 · Trailing Edge FlapsSDR UPS98225496Sill · crackedINSPECTION TYPE-SI, MOPSILL CRACKED LBL 54 STA 294 TO 304 WL 208. REPLACED MOPSILL AT LBL 54 STA 294 TO 304 WL 208 IAW SRM 51-30-2.Jan 16, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS98225497Beam · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON LONGITUDINAL BEAM ST 760 TO 848 LBL 45 WL 208. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPLACED LONGITUDINAL BEAM IAW SRM 51-10-1, 51-30-2.Jan 15, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS98225495Stringer · crackedINSPECTION TYPE-SI, DISCOVERED END OF STR 15L TO BE CRACKED AT BS 720+5. AREA OF DAMAGE REMOVED AND STRINGER END REPAIRED PER SRM 53-10-3 AND SRM 51-30-2.Jan 14, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Longeron/StringerSDR UPS98225478Skin · corrodedINSPECTION TYPE-SI, WHILE CLOSING FLOOR ON CARD 656802 FOUND CORROSION ON SKIN AT BS 1090 AT STR 28R. REMOVED CORROSION IAW SRM 51-10-6 REWORK OUT OF LIMITS IAW SRM 53-30-1. REPAIRED SKIN AT STA 1090 STR 28R IAW SRM 53-30-3.Jan 14, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Plate/SkinSDR UPS98225477Chord · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-03) ON NUT PLATE AND FLOORBEAM AT STA 1166, LBL 10, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REPAIRED FLOORBEAM PER SRM 53-10-8.Jan 14, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS98225473Angle · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AT MOP SILL AT BOTTOM OF RT ENTRY DOOR BS 380 TO 410 RBL 63 WL 208 TOP AND BOTTOM SURFACES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ON LWR SUPPORT ANGLE IAW 51-10-06, 53-10-1. REMOVED AND REPLACED ANGLE IAJan 14, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS98225472Seat Track · corrodedINSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK FLANGE BETWEEN BS 720D TO 720F LBL 25. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED SEAT TRACK BS 720D TO BS 720F LBL 25 IAW SRM 53-10-5.Jan 13, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS98225470Frame · crackedINSPECTION TYPE-SI, CRACK INDICATION NOTED AT FASTENER HOLE IN FRAME AT BS 783.95 APPROX WL 207 APPROX LBL 65. REPAIRED CRACK IN FRAME STA 783.95 LBL 65 WL 207 IAW UPS EO B727-5310-5474.Jan 13, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, FrameSDR UPS98225469Seat Track · corrodedINSPECTION TYPE-SI, CORROSION (4-25-02) AND MECHANICAL DAMAGE ON SEAT TRACK WELL AND TOOTH BETWEEN BS 980 TO 1010 LBL 25. CORROSION REWORK OUT OF LIMTS IAW SRM 53-10-1. MECHANICAL DAMAGE WITHIN LIMITS IAW SRM 53-10-1. SEAT TRACK WAS REMOVED AND REPLACED IAWJan 13, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS98225468Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON TOP OF FLOORBEAM 950 RBL 25 TO 65. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPAIRED 950 FLOORBEAM RBL 25 TO 65 IAW TRAMCO/BFG EWO 98-2012 (UPS FILE 727-53-1983).Jan 13, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor BeamSDR UPS98225467Lug · corrodedINSPECTION TYPE-SI, NR 4 K-FLAP HAS CORROSION ON O/B UPPER LUG WHERE BONDING JUMPER ATTACHES. REMOVED AND REPLACED NR 4 K-FLAP IAW OHM 57-51-21 AND MM 27-81-01.Jan 12, 1998 · N214UP · Boeing 7272A1 · Leading Edge DevicesSDR UPS98225466Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION AT BS 380 RBL 45 TO 63 WL 208 ON UPPER SURFACE OF FLOORBEAM AND BOTTOM SURFACE AT FASTENER HOLES (C53-224-01.05-01). CORROSION REMOVED IAW SRM 51-10-6 OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FLOORBEAM IAW SRM 53-10-8.Jan 12, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor BeamSDR UPS98225465Seat Track · corrodedINSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK AT BS 720C TO BS 745 RBL 25, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED CORRODED SEAT TRACK, FABRICATED, INSTALLED REPAIR SEAT TRACK IAW SRM 53-10-5.Jan 12, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS98225464Seat Track · corrodedINSPECTION TYPE-SI, CORROSION (2-224-01) GOUGES AND BARE METAL ON SEAT TRACK AT BS 520 BS 610, LBL 60, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-05, 51-30-08, MM 51-20-31, OHM 20-50-01Jan 12, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS98225463Link · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.00-02) ON EXPANSION LINK AT BS 740 TO 755 LBL 45. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED LINK PER SRM 51-20-1, 51-10-1, 51-30-2.Jan 12, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS98225404Frame · corrodedINSPECTION TYPE-SI, CORROSION ON FRAME BS 720D STR 10 TO 13 RT. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3.Jan 9, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, FrameSDR UPS98225403Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION AFT CARGO BAY ON FLOORBEAM, FWD LOWER FLANGE UNDER NUT PLATES BS 1070, BL 0 TO LBL 10 WL 200. REMOVED DAMAGED SECTION AND REPAIRED LOWER FLANGE IAW SRM 53-10-8.Jan 9, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor BeamSDR UPS98225462Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AT BS 480 LBL 45 RBL 63 WL 208 ON UPPER SURFACE OF FLOORBEAM AS MARKED. CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-8.Jan 8, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor BeamSDR UPS98225461Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON TOP CHORD OF FLOORBEAM AT BS 620 RBL 10 WL 208. CORROSION ON CHORD FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS PER SRM 53-10-8.Jan 8, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor BeamSDR UPS98225460Seat Track · dentedINSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK AT BS 484 TO BS 570 BL 0 WL 208. CORROSION ON SEAT TRACK WAS FOUND TO BE WITHIN LIMITS AFTER CLEAN UP. HOWEVER, DENTS WERE FOUND ON BS 490 AND BS 571 WHICH WERE OUT OF LIMITS. SEAT TRACK WAS REPLACED FROJan 8, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS98225397Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION AFT CARGO BAY ON FLOORBEAM, FWD LOWER FLANGE AT NUT PLATE BS 950F, LBL 12, WL 200. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER AND TRIPLER ANGLE AND FILLER IAW SRM 53-10-8.Jan 8, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor Beam
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