N930UP, cancelled Nov 21, 2007

Service difficulty reports · 175

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 = 'N930UP' AND deregistration_id = 'N930UP-2007-11-21'
  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 UPS01235799Support · corrodedINSPECTION TYPE:C, NR 7 SPOILER, I/B END HINGE SUPPORT ATTACHED TO SPOILER SUPPORT BEAM I S CORRODED BEYOND LIMITS. /BEND HINGE REPLACED IAW SRM 51-30-02Apr 20, 2001 · N930UP · Boeing 72722C · SpoilersSDR UPS01235798Rib · corrodedINSPECTION TYPE:C, NR 7 SPOILER, SUPPORT RIB ON I/B SIDE ATACHED TO MLG BEAM IS CORRODED BEYOND LIMITS. REPLACED SUPPORT RIB IAW SRM 51-30-2Apr 20, 2001 · N930UP · Boeing 72722C · SpoilersSDR UPS01235790Casting · corrodedINSPECTION TYPE:C, NR 7 SPOILER SUPPORT CASTING IS CORRODED BEYOND LIMITS. NR 7 SPOILER CASTING REMOVED & REPLACED IAW DRW 65-16216 & IAW SRM 51- 10-2Apr 20, 2001 · N930UP · Boeing 72722C · SpoilersSDR UPS01235775Skin · crackedINSPECTION TYPE: C, ON HFEC INSPECTION CRACKS FOUND ON FUSELAGE SKIN AT BS 235.8 BETWEEN SL 223 & 225 LT. SKIN REPAIR CARRIED OUT IAW SRM 530 FIG 3Apr 20, 2001 · N930UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS01235780Web · corrodedINSPECTION TYPE: C, SURFACE CORROSION FOUND ON LOWER SURFACE OF HORIZONTAL WEB S18A RT, BETWEEN BS 880 & 950. ALL REPAIRS CARRIED OUT IAW SRM 51-10-6, 51-10-1, 51-10-2, 51-30-2 & SMRO EO 2001-013-001 UPS ENGINEERING FILE NO 727-53-20015Apr 19, 2001 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS01235808Stringer · corrodedINSPECTION TYPE:C CORROSION FOUND ON S18A LT AT BS 890 TO 940 HORIZ. FLANGE AT BODY F AIRING SUPPORT. REPAIR CARRIED OUT IAW SRM 51-30-2 51-30-6 & SMRO EO 2001-013-002 UPS ENGINEERING FILE NO 727-53-20016Apr 18, 2001 · N930UP · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS01235807Stringer · corrodedINSPECTION TYPE: C, CORROSION FOUND AT BS 870 LT ON S18A LWR AFT ATTACH BOLT LOCATION. REPAIR CARRIED OUT IAW SRM 51-10-6 & SHANNON MRO EO 2001-013-002 UPS ENGINEERING FILE NO 727-53-20016Apr 18, 2001 · N930UP · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS01235777Housing · corrodedINSPECTION TYPE: C, CORROSION ON OPERATING HANDLE HOUSING ON AFT RT EMERGENCY EXIT. OPERATING HOUSING REPLACED IAW SRM 51-30-2 & PER DRW 50-7978Apr 18, 2001 · N930UP · Boeing 72722C · Emergency ExitsSDR UPS99230921Bracket · crackedINSPECTION TYPE:C, LT AND RT ELEVATOR POSITION SENSOR BRACKETS CRACKED. LT AND RT ELEVATOR POSITION SENSOR BRACKETS REPLACED IAW MM 20- 80-01.Oct 11, 1999 · N930UP · Boeing 72722C · Elevator Control SystemSDR UPS99230925Seat Track · crackedINSPECTION TYPE:C, SEAT TRACK CRACKED AT BS 560 RT SIDE. REPAIRED IAW SRM 53-10-5 FIG 5.Oct 9, 1999 · N930UP · Boeing 72722C · Fuselage, Seat/Cargo Attach FittingsSDR UPS99230924Stringer · corrodedINSPECTION TYPE:C, STRINGER CORRODED AT BS 480 STR 28L. STRINGER SPLICE SECTION REPAIRED IAW SRM 51-20-1 FIG 7.Oct 9, 1999 · N930UP · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS99230947Panel · crackedINSPECTION TYPE:C, RT OUTBOARD AILERON LOWER SURFACE ACCESS PANEL T/E EXTRUSION CRACKED. EXTRUSION REPLACED IAW SRM 51-30-02.Oct 8, 1999 · N930UP · Boeing 72722C · AileronsSDR UPS99230930Web · crackedINSPECTION TYPE:C, NOSE WHEEL WELL, CEILING WEB HAD SUSPECT CRACK AT BS 277 APPROX AND RBL 14. DAMAGED AREA TRIMMED OUT IAW SRM 51-40-2, ALL EXISTING FASTENER HOLES IN PERIMETER ROW OF DOUBLER ZERO-TIMED PER SRM 51-10-1. WEB REPAIRED IAW SRM 51-40-02.Oct 7, 1999 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS99230928Skin · nickedINSPECTION TYPE:C, FWD CARGO DOOR LWR AFT CORNER SKIN NICKED. NICKED SKIN FOUND TO BE OUT OF LIMITS IAW SRM 52-00-2. SKIN BLENDED OUT LIMITS IAW SRM 52-00-2 FIG 1. FWD CARGO DOOR REPAIRED IAW B727 NDT MANUAL PART 6, 51-00-00 FIG 4.Oct 7, 1999 · N930UP · Boeing 72722C · Cargo/Baggage DoorsSDR UPS99230927Beam · corrodedINSPECTION TYPE:C, ON REMOVAL OF ACCORDION SEAL, CORROSION FOUND ON UPPER BEAM OF MAIN CARGO DOOR. CORROSION REMOVED FROM UPPER BEAM, LIMITS CHECKED AND FOUND OUTSIDE REF SRM 51-10-6. BEAM REPLACED IAW SRM 51-30-2, WITH REF TO BOEING DWG NR 65-25337. ALL AROct 6, 1999 · N930UP · Boeing 72722C · Cargo/Baggage DoorsSDR UPS99230923Intercostal · crackedINSPECTION TYPE:C, WEB CRACKED ON LWR LEG AFT OF BS 1148 LBL 3 INTERCOSTAL. INTERCOSTAL REPAIRED IAW SRM 51-40-03 FIG 1.Oct 6, 1999 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS99230942Web · crackedINSPECTION TYPE:C, CRACK ON WEB AT FWD LOWER LIGHTNING HOLE RT TORQUE BOX AFT AIRSTAIRS. REPAIRED AREAS IAW SRM 51-40-3.Oct 5, 1999 · N930UP · Boeing 72722C · Entrance StairsSDR UPS99230933Web · crackedINSPECTION TYPE:C, CRACK ON WEB AT LIGHTNING HOLE (UPPER ROW 2ND FROM AFT) RT TORQUE BOX AFT AIRSTAIRS. CRACK STOP DRILLED IAW SRM 51-10-1, REPAIRED AREA IAW SRM 51-40-2.Oct 5, 1999 · N930UP · Boeing 72722C · Entrance StairsSDR UPS99230931Bracket · crackedINSPECTION TYPE:C, AFT CARGO DOOR AFT HINGE AFT BRACKET CRACKED. REPLACED AFT CARGO AFT HINGE BRACKET IAW DRAWING NR 65-18625.Oct 5, 1999 · N930UP · Boeing 72722C · Cargo/Baggage DoorsSDR UPS99230926Casting · crackedINSPECTION TYPE:C, SUSPECT CRACK ON NR 3 L/E FLAP I/B ATTACH CASTING. NR 3 L/E FLAP REPLACED IAW MM 27-81-01.Oct 5, 1999 · N930UP · Boeing 72722C · Trailing Edge FlapsSDR UPS99230920Hinge · crackedINSPECTION TYPE:C, RT OUTBOARD AILERON OUTBOARD HINGE SUPPORT CRACKED. REPLACED AILERON HINGE CASTING IAW DWG NR 65-19277.Oct 5, 1999 · N930UP · Boeing 72722C · AileronsSDR UPS99230932Angle · crackedINSPECTION TYPE:C, CRACK IN AFT CARGO DOOR FWD HINGE FWD ANGLE. REPLACED ANGLE IAW DRAWING NR 65-18625.Oct 4, 1999 · N930UP · Boeing 72722C · Cargo/Baggage DoorsSDR UPS99230929Fitting · crackedINSPECTION TYPE:C, CRACK FOUND ON 940 FRAME FITTING UPPER FWD FLANGE BELOW FLOOR LEVEL NDT. COFIRMED CRACK, REPAIRED PER EO B727-5310-3787.Oct 4, 1999 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS99229548Fitting · crackedINSPECTION TYPE:AD, DURING NDT INSPECTION OF MAIN CARGO DOOR CAM SUPPORT FITTINGS. CRACK FOUND ON FITTING AT BS 520. FITTING BS 520 REPLACED IAW UPS EO B727-5230-0005 APPENDIX B.May 4, 1999 · N930UP · Boeing 72722C · Cargo/Baggage DoorsSDR UPS99228723Tr Unit · malfunctionedINSPECTION TYPE-N/A, ON CLIMBOUT NR 3 THRUST LEVER RAPIDLY RETARD TO IDLE A/C YAWED, T/R WARNING LIGHT CAME ON, PERFORMED APPROPRIATE CHECKLIST AND SECURED THE ENGINE. PERFORMED E/O B727-7100-10130 C/W, NO DEFECTS FOUND.Feb 10, 1999 · N930UP · Boeing 72722C · Engine Thrust ReverserSDR UPS98227017Bulb · failedINSPECTION TYPE-N/A, COCKPIT EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY F/C OK (P/N 10-0067-9), (S/N 14867) ON, (S/N 32U) OFF.Jun 23, 1998 · N930UP · Boeing 72722C · Emergency LightingSDR UPS98226473Skin · crackedINSPECTION TYPE-C, LT ELEVATOR TRAILING EDGE FASTENER HOLES FOUND CRACKED AND DAMAGED. DAMAGE BLENDED OUT AND REPAIR CARRIED OUT IAW SRM 55-20-3, FIG 2.Apr 16, 1998 · N930UP · Boeing 72722C · Elevator, Plate/SkinSDR UPS98226435Fitting · damagedINSPECTION TYPE-C, NR 3 TRUNNION FITTING FOUND TO HAVE A SURFACE IRREGULARITY DURING NDT PROCESS (FLUORESCENT DYE PENETRANT). NR 3 TRUNNION FITTING REPLACED IAW MM 71-21-01.Apr 15, 1998 · N930UP · Boeing 72722C · Main Landing Gear Attach SectionSDR UPS98226433Hinge · crackedINSPECTION TYPE-C, RT OUTBD AILERON HINGE IS CRACKED, SECOND FROM INBD HINGE FITTING. REPLACED IAW 65-19275.Apr 15, 1998 · N930UP · Boeing 72722C · Aileron Control SystemSDR UPS98226444Sill · crackedINSPECTION TYPE-C, TO AID IN CORROSION REMOVAL PLEASE DISPLACE DOOR SILL WEB BS 480 TO 600 DOOR SILL WEB DERIVETED, INSPECTED AND FOUND CRACKED AND CORRODED. NEW WEB FABRICATED IN TWO SECTIONS IAW SRM 53-10-2, FIG 3 AND SPLICED AT BS 525 IAW SRM 51-40-2 FApr 10, 1998 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS98226434Skin · scratchedINSPECTION TYPE-C, FOUND SCRATCH 3 INCHES LONG NEAR OF FWD CARGO COMPARTMENT, RT SIDE STN 530 WL 188 SECTION 43. REMOVED SCRATCH AND REPAIRED IAW SRM 53-30-3, FIG 3.Apr 10, 1998 · N930UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS98226431Skin · crackedINSPECTION TYPE-C, CRACK FOUND ON FUSELAGE SKIN BS 251.6, WL 221.5. SKIN REPAIRED IAW SRM 53-30-3 FIG 3.Apr 10, 1998 · N930UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS98226430Angle · crackedINSPECTION TYPE-C, NR 2 SPOILER ACTUATOR SUPPORT CASTING, ATTACH ANGLE ON REAR SPAR I/B CRACKED. ATTACH ANGLE REPLACED IAW SRM 51-30-2.Apr 10, 1998 · N930UP · Boeing 72722C · Drag Control ActuatorSDR UPS98226455Fitting · crackedINSPECTION TYPE-C, ON REMOVAL OF MAIN CARGO DOOR LATCH SUPPORT FITTING, FITTING FOUND CRACKED. NEW MAIN CARGO DOOR FITTING REPLACED IAW EO B727-5310-0437.Apr 9, 1998 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS98226447Frame · crackedINSPECTION TYPE-C, CRACK FOUND ON FUSELAGE FRAME AT BS 481 AT SEAT TRACK ATTACH HOLE LBL 62. CRACK REMOVED PER SRM 51-10-6 AND REPAIR CARRIED OUT IAW SRS EO 98-10-007.Apr 9, 1998 · N930UP · Boeing 72722C · Fuselage Main, FrameSDR UPS98226454Fitting · corrodedINSPECTION TYPE-C, ON REMOVAL OF BS 487 MAIN CARGO DOOR LATCH SUPPORT FITTING, CORROSION FOUND ON FITTING. NEW MAIN CARGO DOOR LATCH SUPPORT FITTING REAPLACED IAW EO B727-5310 -0437 APPENDIX 8.6 AND 8.7.Apr 8, 1998 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS98226452Web · crackedINSPECTION TYPE-C, CRACK FOUND ON RT WHEEL WELL, FWD WALL BS 870. REPAIR CARRIED OUT IAW SRM 51-40-2.Apr 8, 1998 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS98226448Frame · crackedINSPECTION TYPE-C, TOE ON FRAME AT BS 490 FWD SIDE CRACKED AT LATCH SUPPORT FITTING OF MAIN CARGO DOOR. FRAME REPAIRED IAW SRM 53-10-4.Apr 8, 1998 · N930UP · Boeing 72722C · Fuselage Main, FrameSDR UPS98226446Bracket · crackedINSPECTION TYPE-C, RT ELEVATOR TRAILING EDGE CAVITY BRACKET CRACKED A FS 60 (ABOVE TAB ROD). BRACKET REPLACED IAW DRAWING NR 69-19144.Apr 8, 1998 · N930UP · Boeing 72722C · Elevator Control SystemSDR UPS98226475Rib · crackedINSPECTION TYPE-C, RESULTS OF X-RAY INSPECTION ON LT ELEVATOR SHOWS CRACK IN LOWER RIB REPAIR AREA BETWEEN ES 66.79 AND 69.79 AT 23 INCHES FWD OF TRAILING EDGE. DAMAGED AREA OF RIB TRIMMED OUT AND REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-10-006, UPS ENApr 7, 1998 · N930UP · Boeing 72722C · Elevator, Spar/RibSDR UPS98226472Rib · crackedINSPECTION TYPE-C, RESULTS OF X-RAY ON LT ELEVATOR SHOWS CRACK IN LOWER RIB AREA BETWEEN ES 66.79 AND ES 71.79, 23 INCHES FWD OF TRAILING EDGE. DAMAGE TRIMMED OUT IAW SRM 55-20-1 AND REPAIR CARRIED IAW SRS ENGINEERING ORDER 98-10-006, REF UPS ENGINEERING FILEApr 7, 1998 · N930UP · Boeing 72722C · Elevator, Spar/RibSDR UPS98226445Skin · delaminatedINSPECTION TYPE-C, LT INBD AFT FLAP HAS DELAMINATION OUTBD LOWER SURFACE. REPAIRED IAW SRM 51-40-9.Apr 7, 1998 · N930UP · Boeing 72722C · Trailing Edge FlapsSDR UPS98226432Web · crackedINSPECTION TYPE-C, SUSPECT CRACK ON WEB ABOVE NR 2 ENGINE HORIZONTAL FIREWALL RT SIDE AT BS 1380. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.Apr 7, 1998 · N930UP · Boeing 72722C · Nacelle/Pylon StructureSDR UPS98226474Frame · crackedINSPECTION TYPE-C, CRACK IN TOE OF FRAME AT BS 500 LT AT LATCH SUPPORT FITTING. FRAME REPAIRED IAW SRM 53-10-4, FIG 11.Apr 6, 1998 · N930UP · Boeing 72722C · Fuselage Main, FrameSDR UPS98226451Frame · crackedINSPECTION TYPE-C, CRACK IN TOE OF FRAME AT STATION 490 LT AT LATCH SUPPORT FITTING. FRAME REPAIRED IAW SRM 53-10-4 FIGURE 11.Apr 6, 1998 · N930UP · Boeing 72722C · Fuselage Main, FrameSDR UPS98226449Frame · crackedINSPECTION TYPE-C, CRACK IN TOE OF FRAME AT BS 580 LEFT HAND AT LATCH SUPPORT FITTING. FRAME REPAIRED IAW SRM 53-10-4 FIGURE 11.Apr 6, 1998 · N930UP · Boeing 72722C · Fuselage Main, FrameSDR UPS98226471Pressure Web · crackedINSPECTION TYPE-C, CRACK DETECTED IN CEILING OF LT WHEEL WELL AT BS 938 LBL 55. CRACK STOP DRILLED IAW SRM 51-10-1 AND REPAIR CARRIED OUT IAW EO B72 7-5310-0460, APPENDIX C.Apr 4, 1998 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS98226470Pressure Web · crackedINSPECTION TYPE-C, CRACK DETECTED IN CEILING OF RT WHEEL WELL AT BS 938 RBL 36. CRACK STOP DRILLED IAW SRM 51-10-1 AND REPAIR COMPLETED PER EO B727-5 310-0460-L.Apr 4, 1998 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS98226450Extrusion · corrodedINSPECTION TYPE-C, CORROSION UNDER REMOVED TEFLON STRIP. ALL CORROSION REMOVED IAW SRM 51-10-6, ALL AREAS INSPECTED AND REPAIRED IAW SRS ENGINEERING ORDER 98-10-005, UPS FILE NUMBER 727-53-2017.Apr 4, 1998 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS98226458Casting · corrodedINSPECTION TYPE-C, RT INBD AILERON TURNAROUND PULLEY CASTING HAS CORROSION ON LUG FOR TURNAROUND PULLEY. CASTING REPLACED IAW SRM 51-30-2.Apr 1, 1998 · N930UP · Boeing 72722C · Aileron Control System
Back to N930UP, cancelled Nov 21, 2007