N914UP, cancelled Aug 23, 2006

Service difficulty reports · 81

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 = 'N914UP' AND deregistration_id = 'N914UP-2006-08-23'
  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 UPS01237314Smoke Detector · inoperativeINSPECTION TYPE:N/A TARGET ALERT H20824 LOWER CARGO SMOKE DETECTION. LOWER CARGO SMOKE DETECTOR MX LT ILLUM. TECH RECOMMENDS: SUSPECT A-CHANNEL OF CCU FAILED. REPLACE CCU. PERFORMED ADJUSTMENT TEST PER MM 26-18-01, VERIFIED SN OF SMOKE DETECTORS. NO FURTNov 17, 2001 · N914UP · Boeing 72727C · Smoke DetectionSDR UPS01236530Battery · dischargedINSPECTION TYPE:IN ILLEGIBLE EXIT LIGHT AT MAIN ENTRY DOOR INOP. REPLACED ILLEGIBLE EXIT LIGHT BATTERY AND OPS CHECK AS PER B727 M/M 33-50-00.Aug 3, 2001 · N914UP · Boeing 72727C · Emergency LightingSDR UPS01236413Floor Support · corrodedINSPECTION TYPE:N/A LAV FLOOR SUPPORT CORRODED RBL 40 BS290 TP BS 312 REMOVED CORROSION AT LAV FLOOR SUPPORT RBL 40 BS290 TO BS 312 MATERI AL LOSS .050 FOUND OUT OF LIMITS AS PER B727 SRM 51-30-02 REPLACED F LOOR MATERIAL USE 60-8265 T ANGLE 8" TREAT AND PJul 11, 2001 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS01236411Beam · crackedINSPECTION TYPE:N/A AFT PRESSURE BULKHEAD VERTICAL BEAM LBL 17.8 WL 264.5 SHOW CRACK RUNNING FROM STOP DOOR CUT OUT TO O/B CHORD. CUT OUT DAMAGED SECTION OF VERTICAL BEAM AT W/L 249 IAW UPS EO B727-53 10-11743 APPENDIX E INSTALLED NEW SECTION AND REMOVED PARTSJul 10, 2001 · N914UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236414Pressure Panel · crackedINSPECTION TYPE:N/A NLG WW LT SIDE WALL CRACK INDICATION BETWEEN FASTENERS BS 235 AND LOWER OF FWD ACCESS. REMOVE ACCESS NR 3122 FOR ACCESS REPAIR AS PER B727SRM 51-30-02 CUT OUT DAMAGED AREA AS PER B727 SRM 51-30-02, SIZE OF CUT 2X1 INCH ACCOMPLISHED NDT ON CJul 9, 2001 · N914UP · Boeing 72727C · Fuselage Main, BulkheadSDR UPS01236412Frame · crackedINSPECTION TYPE:C LH WHEEL WELL TOP OB EXPOSED PORTION OF BS 930 FRAME IS CRACKED IB S IDE TOP INSTALL REPAIR AS PER REPAIR ORDER AVHM 233RO-1. ENGINEERING FILE NO 727-53-20023. MAT USED 310 1/2 HD .080 BOTTOM DOUBLER 15X8" TOP DOU BLER 6X6", TOP STRAP 20Jul 6, 2001 · N914UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01235631Window · out of adjCAPT L2 WINDOW UNLATCHES W/O PRESSING UNLATCH LEVER ADJUSTED LOCKING AND SERATION PLATE.Apr 20, 2001 · N914UP · Boeing 72727C · Flight Compartment WindowsSDR UPS01235588Bulb · inoperativeCARGO SMOKE DETECTOR TEST INOP. 2 BULBS INOP. R&R BULBSApr 13, 2001 · N914UP · Boeing 72727C · Detection SystemSDR UPS00234269Light · inoperativeINSPECTION TYPE:N/A, CREW ENTRY DOOR EMERGENCY EXIT DOOR LIGHTS INOP, BATTERIES CHANGED PREVIOUSLY 3 TIMES. LIGHT ASSY REPLACED.Oct 26, 2000 · N914UP · Boeing 72727C · Emergency LightingSDR UPS00234214Light · inoperativeINSPECTION TYPE:N/A, EXIT LIGHT OVER MAIN ENTRY DOOR COMES ON WHEN POWER IS REMOVED FROM AIRCRAFT. REMOVED AND REPLACED EXIT LIGHT ASSY, CKS OK.Oct 19, 2000 · N914UP · Boeing 72727C · Emergency LightingSDR UPS00234211Light · inoperativeINSPECTION TYPE:N/A, ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED 2 BATTERIES FROM LIGHT ASSY. INSTALLED AND TESTED EMERGENCY LIGHTS PER MM 33-30-01, TESTED GOOD.Oct 17, 2000 · N914UP · Boeing 72727C · Emergency LightingSDR UPS00233857Light · inoperativeINSPECTION TYPE:N/A FWD ENTRY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES LIGHTS, OPS CK OK.Oct 6, 2000 · N914UP · Boeing 72727C · Emergency LightingSDR UPS00233838Terminal · brokenINSPECTION TYPE:C, EMERGENCY LIGHT AT ENTRY DOOR, LIGHTS WEAK. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY, FOUND BATTERY TERMINAL BROKEN. LIGHT OPS CKS NORMAL. P/N OFF/ON 10-0067-9, S/N OFF 01, S/N ON UP11337.Oct 5, 2000 · N914UP · Boeing 72727C · Emergency LightingSDR UPS00232253Frame · corrodedINSPECTION TYPE:C WHILE WORKING CARD B727-5310-1371E, FOUND CORROSION ON FRAME AT BS 425 BL 0 WL 146 AROUND E & E BAY DOOR FWD LATCH FITTING. REMOVED CORROSION ON FRAME AT BS 425 IN A AREA 3 X 3 X .040 DEEP ORIG THICKNESS IS .040, FOUND TO BE OUT OF LIMITS IAApr 6, 2000 · N914UP · Boeing 72727C · Fuselage Main, FrameSDR UPS00232188Bulkhead · corrodedINSPECTION TYPE: C, CORROSION ON TOP EDGE OF STA 870 BULKHEAD AT WL 200, LBL 15 - 25 REMOVED CORROSION PER SRM 51-10-6 AND 53-10-1 2X4 INSTALLED FABRICATED DOUBLER AND STIFFNER L) ON BEADED PRESSURE WEB PER SRM 53-10-2, 53-10-9Mar 31, 2000 · N914UP · Boeing 72727C · Fuselage Main, BulkheadSDR UPS00232189Floorbeam · corrodedINSPECTION TYPE: C, CORROSION ON FWD SIDE OF FLOORBEAM AT CARGO DOOR LATCH FITTING 5.0 I/B FROM NR 3 LATCH AT BS 580, WL 207. REMOVED CORROSION ON FWD SIDE OF FLOORBEAM UPPER FLANGE, LOWER SURFACE PER SRM 51-10-6. REMOVED .029X1.0X2.5 FROM ORIGINAL THICKMar 27, 2000 · N914UP · Boeing 72727C · Fuselage Main, Floor BeamSDR UPS00232080Web · corrodedINSPECTION TYPE : C WHILE WORKING CUSTOMER CARD NR 114598 FOUND CORROSION ON WEB, BS 640, LBL 48, WL 208 FABRICATED REPAIR PART AND INSTALLED PER UPS EO NR 727-53-2234Mar 22, 2000 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00232248Skin · corrodedINSPECTION TYPE:C, BULGING SKIN AFT OF BS 740, BETWEEN STR 9L AND 10L. CUT OUT DAMAGED (BULGED) OUTER SKIN PER ER NR 00-0342 AND REPLACED SKIN SEGMENT PER ER NR 00-0342. SRM 51-10-1, SRM 51-10-7, SRM 51-20-1, SRM 53- 30-03, SRM 51-30-02, SRM 51-30-08, SRM 51Mar 18, 2000 · N914UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00232040Frame · corrodedINSPECTION TYPE:C CORROSION ON FRAME UPPER FLANGE AT BS 380 ABOVE STRINGER 20 LT SIDE. REPAIRED FRAME PER SRM 57-40-3.Mar 17, 2000 · N914UP · Boeing 72727C · Fuselage Main, FrameSDR UPS00231999Skin · crackedINSPECTION TYPE:C CRACK ON SKIN LT BS 251..6 FWD ROW WL 216 (END MARKED) IN ADDITION TO CRACK FOUND ALSO NOTED CRACKS AT BS 243.7, WL216 WL 221 AND WL 225 REFERENCE NRC NR'S 114717, 114718, 114719, 114720. ALL CRACKS MENTIONED ABOVE ARE ADDRESSED WITH THIS REMar 15, 2000 · N914UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00232247Forging · crackedINSPECTION TYPE:C 740 FORGING HAS A CRACK IN HORIZONTAL FLANGE BETWEEN STR 19L AND 3 BELOW STR 20L. REMOVED LEFT HAND 740 FORGING AND INSTALLED NEW PER EO 727-5310-7477 AND DWG 65C13724; SRM ADDENDUM.Mar 6, 2000 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00232251Stiffener · corrodedINSPECTION TYPE:C, CORROSION (C53-100-01.09-02) ON STIFFENER AT BS 880, WL 199 LBL 3. REMOVED, FABRICATED AND INSTALLED STIFFENER PER SRM 51-30-2 AND 51-30-5.Mar 4, 2000 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00232250Fitting · corrodedINSPECTION TYPE:C, CORROSION ON NR 2 SPOILER ACTUATOR FITTING AROUND SPOILER PANEL HINGE BOLTS. REPLACED NR 2 SPOILER ACTUATOR FITTING PER MM 27-61-81 AND MM 27-51-131.Mar 3, 2000 · N914UP · Boeing 72727C · Drag Control ActuatorSDR UPS00232199Fitting · corrodedINSPECTION TYPE: C, CORROSION ON LT O/B AILERON, I/B CENTER HINGE FITTING AROUND FASTENER HOLES. REMOVED AND INSTALLED NEW HINGE FITTING PER SRM 51-30-2Mar 3, 2000 · N914UP · Boeing 72727C · AileronsSDR UPS00232198Floorbeam · corrodedINSPECTION TYPE: C, CORROSION ON TOP CHORD OF BS 344 FLOORBEAM RBL 6 TO LBL 16, WL 208. REPAIRED FLOOREAM PER SRM 53-10-8Mar 3, 2000 · N914UP · Boeing 72727C · Fuselage Main, Floor BeamSDR UPS00231979Hinge · corrodedINSPECTION TYPE:C, CORROSION (C57-581-01.00-01) ON LOWER SURFACE OF LEFT O/B AILERON O/B CENTER HINGE FITTING AROUND FASTENER HOLES. REMOVED AND REPLACED HINGE PER SRM 51-30-2.Mar 3, 2000 · N914UP · Boeing 72727C · Wing, Control Surface Attach FittingsSDR UPS00231978Hinge · corrodedINSPECTION TYPE:C, CORROSION (C57-581-01.00-01) ON LOWER SURFACE OF LEFT O/B AILERON O/B HINGE FITTING AROUND FASTENER HOLES. REMOVED AND REPLACED HINGE PER SRM 51-30-2.Mar 3, 2000 · N914UP · Boeing 72727C · Wing, Control Surface Attach FittingsSDR UPS99231235O2 Bottle · dischargedINSPECTION TYPE:N/A, CREW O2 BOTTLE READS LOW. REMOVED AND REPLACED BOTTLE.Dec 24, 1999 · N914UP · Boeing 72727C · Crew Oxygen SystemSDR UPS99231197Smoke Detector · inoperativeINSPECTION TYPE:N/A, LT LWR SMOKE DETECTOR INOP. RELAMPED SMOKE DETECTOR.Dec 15, 1999 · N914UP · Boeing 72727C · Smoke DetectionSDR UPS99231151Light · looseINSPECTION TYPE:N/A, COCKPIT DOOR EMERGENCY EXIT LIGHT FELL OFF ITS MOUNT DURING FLIGHT. RESECURED LIGHT, OPS CHECKS NORMAL.Nov 24, 1999 · N914UP · Boeing 72727C · Emergency LightingSDR UPS99230904Battery Pack · dischargedEMERGENCY EXIT LIGHTS ABOVE FWD DOOR COMES ON. BATTERY PACK LOW. RECHARGED EMERGENCY EXIT BATTERY PER MM 33-55-00. OPS CK GOOD.Oct 13, 1999 · N914UP · Boeing 72727C · Emergency LightingSDR UPS99230572Skin · damagedINSPECTION TYPE:N/A, RIGHT I/B FORE FLAP SKIN PEELED BACK AND CRACKED L/E NEXT TO SPRING DOOR. *S/D* REMOVED NAD REPLACED RIGHT FOREFLAP PER MM 27-51-05. (P/N 65-21 630-92) ON, (P/N 65-21630-174) OFF, (S/N BN119) ON, (S/N 126) OFF.Sep 4, 1999 · N914UP · Boeing 72727C · Trailing Edge FlapsSDR UPS98227879Web · crackedINSPECTION TYPE-C, THE AFT STAIRWELL TORQUE BOX INBOARD VERTICAL WEB IS CRACKED JUST UNDER PREVIOUS REPAIR AT BS 1266 WL 192 RBL 21. REMOVED PREVIOUS REPAIR CUT OUT DAMAGED AREA PER SRM 53-10-1. FABRICATED REPAIR DOUBLER PER SRM 51-40-2. INSTALLED DOUBLER POct 3, 1998 · N914UP · Boeing 72727C · Fuselage Main, StructureSDR UPS97223304Hinge Fitting · corrodedINSPECTION TYPE:SI WHILE WORKING CUST ID 686700 DISCOVERED LOWER RUDDER TAB CENTER HINGE FITTING CORRODED UNDER BUSHING. REMOVED AND REPLACED LOWER RUDDER TAB CENTER HINGE FITTING IAW OHM 55-40-11.Jun 6, 1997 · N914UP · Boeing 72727C · Rudder/Tab, Attach FittingsSDR UPS97223214Floorbeam · corrodedINSPECTION TYPE:SI, CORROSION (SDN C53-224-04.00-01) ON FLOORBEAM AT BS 1178 LBL 45 AND LBL 60 WL 208. CORROSION REMOVAL/REWORK OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED BEAM AT BS 1178 LBL 60 TO RBL 60 IAW SRM 51-30-5, 51-30-2.May 30, 1997 · N914UP · Boeing 72727C · Fuselage Main, Floor BeamSDR UPS97223215Frame · crackedINSPECTION TYPE:SI, CRACK IN THE FUSELAGE FWD ENTRY DOORWAY FWD FRAME. STANDARD REPAIR ACCOMPLISHED IAW UPS EO B727-5310-0149G APP 8.1.May 29, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97223212Expansion Link · corrodedINSPECTION TYPE:SI, CORROSION ON SEAT TRACK EXPANSION LINK STA 850 TO 820 LBL 45 UNDER NUT PLATES AREAS MARKED. CORROSION REMOVAL OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED EXPANSION LINK IAW SRM 51-30-2, 51-30-5, 51-10-1.May 29, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97223211Link · corrodedINSPECTION TYPE:SI, CORROSION UNDER FWD BOLT OF SEAT TRACK EXPANSION LINK STA 740 RBL 25 WL 206 AREA MARKED. CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-1 ON LINK AND STIFFENER (SEAT TRACK). REMOVED AND REPLACED EXPANSION LINK AND TRACK AT STA 740 RBL 25 IAWMay 29, 1997 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97223157Seat Track · corrodedINSPECTION TYPE:SI, CORROSION (4-25-02) UNDER NUT PLATE LBL 25, WL 208, BS 345.5. REMOVED CORRODED SECTION OF SEAT TRACK, PROCURED NEW SECTION OF SEAT TRACK AND INSTALLED IAW SRM 53-10-5.May 28, 1997 · N914UP · Boeing 72727C · Fuselage, Seat/Cargo Attach FittingsSDR UPS97223156Stringer · crackedINSPECTION TYPE:SI, RWS 686.5 STRINGER 13 AND 14 (VENT STRINGER) HAS CRACKED RIB FLANGES. STANDARD REPAIR ACCOMPLISHED PER UPS EO B727-5710-0314F ON VENT STRINGER RWS 686.5.May 28, 1997 · N914UP · Boeing 72727C · Wing, Longeron/StringerSDR UPS97223155Seat Track · corrodedINSPECTION TYPE:SI, CORROSION (C53-224-04-00-01) ON SEAT TRACK AROUND FASTENER AT BS 1130 LBL 45 WL 208. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED SECTION FROM STA 1100 TO 1130 IAW SRM 53-10-5.May 28, 1997 · N914UP · Boeing 72727C · Fuselage, Seat/Cargo Attach FittingsSDR UPS97223154Seat Track · corrodedINSPECTION TYPE:SI, CORROSION ON SEAT TRACK AND UPPER CHORD OF LONGITUDINAL BEAM STA 760 TO 850 LBL 25 AREAS MARKED. REPAIRED LONGITUDINAL BEAM IAW TRAMCO/BFG EWO 97-2190 (UPS EO FILE NR 727-53-1922) CORROSION ON LONGITUDINAL BEAM WAS OUT OF LIMITS IAW SRM 53May 28, 1997 · N914UP · Boeing 72727C · Fuselage, Seat/Cargo Attach FittingsSDR UPS97223161Fitting Support · corrodedINSPECTION TYPE:SI, NR 3 FLAP TRACK FORWARD ATTACH FITTING CORRODED (C57-581-06.00-03). REPAIRED NR 3 FLAP TRACK FWD FTG IAW TRAMCO EWO 97-2197 (UPS EO FILE NR 727-57-1837).May 27, 1997 · N914UP · Boeing 72727C · Trailing Edge FlapsSDR 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 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 Structure
Back to N914UP, cancelled Aug 23, 2006