N908UP, cancelled Aug 23, 2006

Service difficulty reports · 145

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 = 'N908UP' AND deregistration_id = 'N908UP-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 UPS02239857Cover · looseINSPECTION TYPE:N/A MAIN ENTRY DOOR EMERGENCY LIGHT FELL OUT OF BRACKET DURING T/O. R&R MAIN ENTRY DOOR EMERGENCY LIGHT COVER OK FOR CONTINUED SERVICE.Nov 4, 2002 · N908UP · Boeing 72727C · Emergency LightingSDR UPS01236690Stringer · crackedINSPECTION TYPE:C SUSPECT CRACK IN CENTRE SECTION UPPER STRINGER S1 IN THE WING CENTRE TANK STRINGER REPAIRED IAW SRM 57-10-04 FIG 2Aug 16, 2001 · N908UP · Boeing 72727C · Wing Main, Frame StructureSDR UPS01236664Stringer · crackedINSPECTION TYPE:C ON INSPECTION OF FUSELAGE STRINGERS AT BS 400 WHERE ACCESSABLE, S18R AT BS 400 FOUND TO BE CRACKED. STRINGER REPAIR CARRIED IAW SRM PROCEDURESAug 15, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS01236658Stringer · crackedINSPECTION TYPE:C ON INSPECTION OF FUSELAGE STRINGERS AT BS 400 WHERE ACCESSABLE, STRI NGER 18R AT BS 400 FOUND TO BE CRACKED. STRINGER REPAIRED IAW SRM.Aug 15, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS01236689Stiffener · corrodedINSPECTION TYPE:C WING CENTRE SECTION UPPER SKIN STIFFENER LWR CHORD IS CORRODED AT BS 870 RBL0. ***CPCP*** DAMAGED SECTION REMOVED AND NEW SECTION SPLICED IAW SRMAug 13, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236686Intercostal · crackedINSPECTION TYPE:C SUSPECT CRACK AT R/H BS 1183 WL 230 OUTBD LWR CORNER OF INTERCOSTAL AT RBL 62.5 INTERCOSTAL REPLACED IAW DWG 65-16350Aug 13, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236688Terminal · crackedINSPECTION TYPE:C L/H UPPER TENSION TIE CRACKED IN TAIL SKID BAY FABRICATED TERMINAL IAW DWG 65-85208, REMOVED / INSTALLED PER SRMAug 11, 2001 · N908UP · Boeing 72727C · Auxiliary Gear (Tail Skid)SDR UPS01236679Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION S6L AT BS 400 FOUND TO BE CRACKED. DAMAGED STRINGER REPAIRED IAW SRM 53-10-3Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236678Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION S3R FOUND CRACKED AT BS 400 REPAIRED PER SRM.Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236677Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION S9R FOUND CRACKED AT BS 400 STRINGER REPAIRED IAW SRM.Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236676Stringer · crackedINSPECTION TYPE:C ON FURTHER INSP FOR ACCESS S15R AT BS 400 FOUND TO BE CRACKED REPAIRED IAW SRMAug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236675Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS S16R FOUND CRACKED AT BS 400 REPAIRED IAW SRM.Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236661Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS S15L FOUND CRACKED AT BS 400 REPAIRED IAW SRMAug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236660Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS, S16L FOUND CRACKED AT BS 400 REPAIRED IAW SRMAug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236657Stringer · crackedINSPECTION TYPE:C ON FURTHER INSPECTION STRINGER S6R FOUND CRACKED AT BS 400 REPAIRED PER SRMAug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236687Strap · crackedINSPECTION TYPE:C ON NDT INSP, CRACK INDICATION FOUND IN REINFORCING STRAP OF MID GALLEY DOOR CUTOUT FWD UPPER CORNER. REPAIR CARRIED OUT PER UPS EO B727-5330-2695 APPENDIX 8.2Aug 10, 2001 · N908UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS01236685Intercostal · crackedINSPECTION TYPE:C INTERCOSTAL CRACKED ABOVE DRAG BRACE FITTING SUPPORT INTERCOSTAL REPLACED IAW DRWG 65-18417Aug 10, 2001 · N908UP · Boeing 72727C · Standard Practices/StructuresSDR UPS01236666Frame · crackedINSPECTION TYPE:C CRACK BS 930 R/H FLANGE I/B LOWER CORNER RADIUS REPAIRED PER SRM ADDENDUM B727-5310-2611BAug 10, 2001 · N908UP · Boeing 72727C · Fuselage Main, StructureSDR UPS01236684Skin · corrodedINSPECTION TYPE:C AREA OF LIGHT SURFACE CORROSION ON SKIN AT BS660 S19R ***CPCP*** AREA REPAIRED IAW APPENDIX 8.3 OF EO B727-5330-0509Aug 9, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS01236681Skin · crackedINSPECTION TYPE:C SKIN CRACKS BS 400 BETWEEN S16R 15R REPAIRED IAW SRMAug 9, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS01236680Frame · corrodedINSPECTION TYPE:C BODY FAIRING #3430 HAS CORRODED FRAME AT R/H GND FAN LOUVRE DOOR AFT CUTOUT. FRAME FABRICATED AND INSTALLED PER SRMAug 9, 2001 · N908UP · Boeing 72727C · Aerodynamic FairingsSDR UPS01236673Skin · crackedINSPECTION TYPE:C SKIN CRACKS BS 400 BETWEEN S16L AND 15L CRACKS REPAIRED IAW SRMAug 9, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS01235633Light · inoperativeEMERG EXIT LIGHT INOP. REPLACED BULB OP CHECKS GOODApr 18, 2001 · N908UP · Boeing 72727C · Emergency LightingSDR UPS01235096Light · malfunctionedINSPECTION TYPE:AS-E INFLIGHT, EMERGENCY EXIT LIGHTS ILLUMINATED FOR APPROX 2 MINUTES, THEN EXTINGUISHED. SWITCH WAS CHECKED TO BE IN ARMED THE ENTIRE TIME. UNABLE TO DUPLICATE PROBLEM. TESTED NORMAL PER MM 33-50-101.Feb 27, 2001 · N908UP · Boeing 72727C · Emergency LightingSDR UPS01234802Skin · crackedINSPECTION TYPE:N/A, LT OUTBOARD AILERON HAS DELAMINATION AND .25 INCH CRACK AILERON REMOVED WD 66470 INSTALLED LT OUTBOARD AILERON TO STEP D (4) MM 27-10-31. OK FOR SERVICE.Jan 30, 2001 · N908UP · Boeing 72727C · AileronsSDR UPS01234586Battery · failedINSPECTION TYPE:N/A EMERGENCY LIGHT AT ENTRY DOOR INOP LIGHT SWITCH LEFT ON. REPLACED BATTERIES. OPS CK OKJan 3, 2001 · N908UP · Boeing 72727C · Emergency LightingSDR UPS00234560Transmitter · inoperativeINSPECTION TYPE:N/A DURING APPROACH INTO SDF FLAP EXTENSION OTBD FLAPS EXTENDED ASYMETRI CALLY RT AT APROX 1 DEG AND LT APROX 5 DEGS. RAN APPROPRIATE CK LIST AND LANDED. ***SUPPLEMENTAL*** REMOVED & REPLACED OTBD FLAP POS XMTR. CYCLED FLA P THRU FULL RANGDec 21, 2000 · N908UP · Boeing 72727C · Trailing Flap Position Indicating SystemSDR UPS00232881Flap · malfunctionedINSPECTION TYPE:N/A, OUTBOARD FLAPS VERY SLOW TO RETRACT OUT OF CAE WOULD NOT EXTEND PAST 15 DEGREES AT ROA WITH NORMAL HYD FLAPS OPERATED NORMAL INTO CAE. A/C DID NOT LAND AT ROA, AIR TURNBACK TO CAE. REPAIRS IN PROGRESS AT CAE.Jun 13, 2000 · N908UP · Boeing 72727C · Trailing Edge Flap Control SystemSDR UPS00231940Stringer · corrodedINSPECTION TYPE:C&SI, STR 24R BETWEEN BS 360 AND BS 259.5 IS CORRODED AT BS 277 AND END OF STRINGER AT BS 360 HAS CRACK FROM PREVIOUS STOP DRILL HOLE. STRINGER INSTALLED IAW BOEING DRG 65-18420.Feb 29, 2000 · N908UP · Boeing 72727C · Fuselage Main, Longeron/StringerSDR UPS00231974Skin · corrodedINSPECTION TYPE:C&SI, CORROSION ON SKIN BETWEEN BS 1080 AND BS 1183 STRINGER 4 RT TO STRINGER 10 RT. SKIN REMOVED IAW SRM 51-30-2. NEW SKIN DRILLED AND TRIMMED IAW SRM 51-30-2 AND DRG 65-18382. NEW SKIN INSTALLED IAW DRG 65-18382 AND SRM 51-30-2 AND 51-30-3Feb 26, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00231932Sill · corrodedINSPECTION TYPE:C&SI, CONTROL CABIN ENTRY DOOR SILL, STA 303.9, EVIDENCE OF CORROSION ON DOOR SILL BOTH UPPER AND LWR SURFACES AND BRACKET ON RT SIDE OF SILL CORRODED. CORROSION REMOVED IAW SRM 51-10-06, CORROSION FOUND TO BE WITHIN LIMITS OF SR 53-10-1 MAX DFeb 24, 2000 · N908UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231949Lug · corrodedINSPECTION TYPE:C&SI, CRACK ON ATTACH LUG OF FLAP POSITION TRANSMITTER HOUSING LEFT I/B FLAP CORRODED DRUM CRACKED HOUSING REPLACED IAW OHM 27-54-06.Feb 23, 2000 · N908UP · Boeing 72727C · Trailing Edge FlapsSDR UPS00231880Flap Track · crackedINSPECTION TYPE:C&SI, NR 3 SLAT, O/B SLAT TRACK, O/B RIB ATTACH POINT HAS SUSPECT CRACK. REPAIR CARRIED OUT AS PER SRM 51-40-2.Feb 21, 2000 · N908UP · Boeing 72727C · Leading Edge DevicesSDR UPS00231879Bracket · crackedINSPECTION TYPE:C&SI, ENGINE NR 1 THROTTLE SHUT OFF CONTROL BRACKET ASSY IN FWD END OF PYLON IS CRACKED. BRACKET REPLACED IAW MM 76-11-21.Feb 18, 2000 · N908UP · Boeing 72727C · Nacelle/Pylon StructureSDR UPS00231878Shear Tie · crackedINSPECTION TYPE:C&SI, CRACK ON SHEAR TIE CLIP BETWEEN STIFEFNER AND UPPER CHORD AT FWD WALL OF CENTER TANK BS 740 AT LBL 45.61. CHANGED SHEAR TIE CLIP IAW EO B727-5710-4595.Feb 18, 2000 · N908UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231976Lug · damagedINSPECTION TYPE:C&SI, ULTRASONIC INSPECTION OF HORIZ STAB HINGE LUGS (ON VERT STAB) LT AND RT, I/B AND O/B DUE SUSPECT INDICATION FROM HFEC INSPECTION. ULTRASONIC INSPECTION CARRIED OUT BOTH LEFT AND RIGHT BORES REPAIRED IAW UPS EO B727-5510-2284.Feb 17, 2000 · N908UP · Boeing 72727C · Horizontal Stabilizer StructureSDR UPS00231975Lap Joint · corrodedINSPECTION TYPE:C&SI, SUSPECT CORROSION ON LAP JOINT AT BS 300 TO BS 320 STRINGER 24 RT. LAP REPAIRED IAW EO B727-5330-0509 AND SRM 53-30-15A.Feb 16, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00231939Stringer · crackINSPECTION TYPE:C&SI, CRACK INDICATION FOUND AT BS 740 FWD LWR HOLE IN LINE WITH STR 16R. REPAIR CARRIED OUT IAW SMRO EO 2000-04-008 UPS ENGINEERING FILE NO 727-53-2231.Feb 16, 2000 · N908UP · Boeing 72727C · Fuselage Main, Longeron/StringerSDR UPS00231938Floorbeam · corrodedINSPECTION TYPE:C&SI, FWD CARGO LEFT FLOOR TRACK UPPER SURFACE CORRODED AT BS 482 ALSO CORROSION EVIDENT ADJACENT ANCHOR NUTS LWR SURFACE BS 480 - BS 540. FWD CARGO BAY LEFT FLOOR TRACK REPLACED FROM BS 480 TO 680 IAW SRM 51-30-2, 7 SRM 53-10-5 FIG 8.Feb 16, 2000 · N908UP · Boeing 72727C · Fuselage Main, Floor BeamSDR UPS00231936Skin · corrodedINSPECTION TYPE:C&SI, CORROSION ON WING CENTER SECTION UPPER SKIN AT BS 865 LBL 65.5. REPAIR CARRIED OUT IAW SMRO EO 200-004-004 UPS ENGINEERING FILE NR 727-57-2145.Feb 15, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00231935Mount · corrodedINSPECTION TYPE:C&SI, ON INSPECTION OF ENG NR 3 MOUNT HOLES CORROSION FOUND IN ALL HOLES. REPAIR CARRIED OUT IAW EO B727-5440-11592-A.Feb 14, 2000 · N908UP · Boeing 72727C · Engine Mount SectionSDR UPS00231934Mount · corrodedINSPECTION TYPE:C&SI , ON INSPECTION OF ENG NR 1 MOUNT HOLES CORROSION FOUND IN ALL HOLES. REPAIR CARRIED OUT IAW EO B727-5440-11592-A.Feb 14, 2000 · N908UP · Boeing 72727C · Engine Mount SectionSDR UPS00231995Flap Track · corrodedINSPECTION TYPE:C&SI NR 4 FLAP TRACK CORROSION ON FACES OF FWD SUPPORT LUGS. REPAIR CARRIED OUT IAW SMRO EO 2000-004-10 UPS ENGINEERING FILE NR 727-57-2147.Feb 13, 2000 · N908UP · Boeing 72727C · Trailing Edge FlapsSDR UPS00231876Seat Track · corrodedINSPECTION TYPE:C&SI, CORROSION ON SEAT TRACK UPPER FLANGE I/B AT BS 740 RBL 24.75. CORROSION REMOVED, LIMITS CHECKED AND FOUND OUTSIDE REF SRM 51-10-6. REPAIR CARRIED OUT IAW SRM 53-10-5.Feb 12, 2000 · N908UP · Boeing 72727C · Fuselage, Seat/Cargo Attach FittingsSDR UPS00231931Carriage · corrodedINSPECTION TYPE:C&SI, FLAP CARRIAGE NR 2 PITTING CORROSION IN BORE OF SPINDLE. CARRIAGE REPLACED IAW OHM 57-52-11..Feb 11, 2000 · N908UP · Boeing 72727C · Wing, Control SurfacesSDR UPS00231875Flap Track · crackedINSPECTION TYPE:C&SI, NR 2 SLAT, I/B TRACK ATTACH POINT HAS SUSPECT CRACK. REPAIR CARRIED IAW SRM 51-40-2.Feb 11, 2000 · N908UP · Boeing 72727C · Leading Edge DevicesSDR UPS00231873Skin · corrodedINSPECTION TYPE:C&SI, SUSPECT CORROSION BETWEEN SKIN AND DOUBLER AT BS 1120 - BS 1140 BETWEEN STR 3R AND STR 4R. REPAIR CARRIED OUT IAW B727 NDM PT6 51-00-00 FIG 4 AND 5.Feb 11, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00231943Pin · corrodedINSPECTION TYPE:C&SI, LEFT WING REAR SPAR TO BODY BOTTLE PIN HAS PITTING CORROSION ON FLANGE THAT SITS AGAINST SPAR TO BODY FITTING. BOTTLE PIN REPLACED IAW MM 57-41-01.Feb 10, 2000 · N908UP · Boeing 72727C · Wing Miscellaneous StructureSDR UPS00231872Sill · crackedINSPECTION TYPE:C&SI, SUSPECT CRACK ON MAIN CARGO DOOR SILL SKIN LWR SURFACE AT BS 488. MAIN CARGO DOOR SILL SKIN REPAIRED IAW SRM 51-40-2 FIG 1.Feb 10, 2000 · N908UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00231871Skin · corrodedINSPECTION TYPE:C&SI, SUSPECT CORROSION BETWEEN SKIN AND DOUBLER AT BS 1120 - BS 1140, BETWEEN STR 3R AND 4R. REPAIR CARRIED OUT IAW SRM 51-00-00.Feb 10, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
Back to N908UP, cancelled Aug 23, 2006