N928UP, cancelled Mar 26, 2013

Service difficulty reports · 128

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 = 'N928UP' AND deregistration_id = 'N928UP-2013-03-26'
  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 UPS02239022Stringer · corrodedINSPECTION TYPE:C MATERIAL LOSS INDICATION AT BS 259.5 AT STR.19 R/H. REMOVED FASTENERS IAW SRM 51-30-2. CORR NOT FOUND TO BE WITHIN LIMIT S IAW SRM 53-30-01. REPAIR CARRIED OUT AS REQUIRED IAW EO-B727-5310-1371 APPDX. E.Aug 8, 2002 · N928UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS02238980Yoke · corrodedINSPECTION TYPE:C, LT BS 940 SWING LINK REMOVAL YOKE ASSY FOUND TO BE CORRODED. YOKE ASSY REPLACED IAW MM 57-15-01.Jul 31, 2002 · N928UP · Boeing 72722C · Main Landing GearSDR UPS02239016Frame · corrodedINSPECTION TYPE:C CORROSION ON FAIRING # 3334 ON FRAME AT L/H FAN INLET DOOR AFT AREA FRAME REPAIR CARRIED OUT IAW SRM 51-40-4 L/H FAN INLET DOOR REPLACED IAW MM 21-52-51 & DOOR ACTUATING ROD REP LACED IAW MM 21-52-51Jul 30, 2002 · N928UP · Boeing 72722C · Aerodynamic FairingsSDR UPS02239021Link · damagedINSPECTION TYPE:C, LEFT MLG BEAM SWING LINK BOLT HOLE HAS MECHANICAL DAMAGE. REPAIR CARRIED OUT IAW SMRO EO 2002-040-004 UPS ENGINEERING FILE 727-57-20059.Jul 26, 2002 · N928UP · Boeing 72722C · Main Landing GearSDR UPS02239018Panel · delaminatedINSPECTION TYPE:C, ENGINE NR 3 PYLON PANEL 5508 IS DELAMINATED, INNER SURFACE FWD END. REPAIRED IAW SRM 51-40-5.Jul 25, 2002 · N928UP · Boeing 72722C · Nacelle/Pylon, Plate/SkinSDR UPS02239017Panel · delaminatedINSPECTION TYPE:C, ENGINE NR 1 PYLON PANEL 5408 IS DELAMINATED INNER, SURFACE FWD END. REPAIRED IAW SRM 51-40-5.Jul 25, 2002 · N928UP · Boeing 72722C · Nacelle/Pylon, Plate/SkinSDR UPS02238984Strap · crackedINSPECTION TYPE:C, FLOORBOARD SUPPORT STRAP CRACKED BS 850 LBL 45.5. FLOORBOARD SUPPORT STRAP REPLACED BS 850 LBL 45.5 IAW SRM 53-20-2.Jul 24, 2002 · N928UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS02239025Fitting · crackedINSPECTION TYPE:C LH WHEEL WELL BS 940 FORGING HAS A SUSPECT CRACK @ BASE OF PREVIOUS BLENDOUT FITTING REPLACED IAW UPS EO B727-5310-4501Jul 23, 2002 · N928UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02239011Channel · crackedINSPECTION TYPE:C CRACK ON CHANNEL SECTION IN LWR AFT CARGO HOLD AT BS 1060 BBL 8L REPAIRED IAW SRM 53-10-5 FIG 4Jul 23, 2002 · N928UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02239010Frame · crackedINSPECTION TYPE:C, LEFT WHEEL WELL, BS 930 FRAME IS CRACKED ON INNER FLANGE UPPER HOLE. REPAIR CARRIED OUT IAW UPS EO B727-5310-2611-B.Jul 23, 2002 · N928UP · Boeing 72722C · Fuselage Main, FrameSDR UPS02239009Stiffener · crackedINSPECTION TYPE:C, MAIN CARGO DECK COMPARTMENT BS 1183 STIFFENER TIE CRACKED AT RBL 361 UPPER TIE BETWEEN VERT BEAM AT RBL 26.83 & RBL 36.83. NEW STIFFENER INSTALLED IAW SRM 51-30-2.Jul 23, 2002 · N928UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS02239029Skin · corrodedINSPECTION TYPE:C, 15 TO 20 PERCENT MATERIAL LOSS INDICATION AT BS 1080 STR 4R. REPAIR CARRIED OUT IAW UPS EO B727-5330-1177 & SMRO EO 2002-040-005 UPS ENGINEERING FILE B727-5330-17277.Jul 22, 2002 · N928UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS02239023Skin · corrodedINSPECTION TYPE:C, MATERIAL LOSS INDICATIONS AT BS 521 AFT SKIN FROM STR 1 TO STR 2 OF 15 - 20 PERCENT AND FROM STR 3R TO STR 4R OF 20 PERCENT AND ON FWD SKIN AT BS 521 BETWEEN STR 3R AND STR 4R OF 15 PERCENT. AREA INSP AND CORROSION FOUND ON SKIN AND TEAR STJul 22, 2002 · N928UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS02239020Doubler · crackedINSPECTION TYPE:C CRACK ON R/H WINDOW POST BETWEEN R1 & R2 WINDOWS AT UPPER CORNER REPAIR DOUBLER FABRICATED IAW SRM 53-30-3 REPAIR DOUBLER INSTALLED IAW SRM 53-30-3 FIG 8 REPAIR 2Jul 22, 2002 · N928UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02239012Window Post · crackedINSPECTION TYPE:C CRACKS ON CENTER WINDOW POST ON LWR LHS & RHS COCKPIT CENTER WINDOW POST REPAIRED IAW UPS EO B727-5330-5128Jul 22, 2002 · N928UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02239013Structure · crackedINSPECTION TYPE:C PLS CARRY OUT PERMANENT REPAIR TO NR 2 L/E SLAT DENT (APPROX 1.5 FT O/B OF ACTUATOR). PERMANENT REPAIR CARRIED OUT ON NR 2 L/E SLAT IAW SRM 57-50-03 FIG 1.Jun 26, 2002 · N928UP · Boeing 72722C · Leading Edge DevicesSDR UPS01236010Pressure Panel · crackedINSPECTION TYPE:N/A, RT WHEEL WELL CRACKS. *S/D* REPAIRED PER SRM 51-1-9A.May 26, 2001 · N928UP · Boeing 72722C · Fuselage Main, BulkheadSDR UPS01235658Control Rod · lack of lubeINSPECTION TYPE:IN AILERON STIFF IN LEFT TURNS AILERON SPRING CARTRIDGE FOUND OUT OF RIG. RE-ADJUSTED I.A.W. B727 M .M.27-61-21. SPRING CARTRIDGE OPS CHECKS SERV. CONTROL WHEEL INPUTS (FORCE) THE SAME LEFT AND RIGHT NOTE: MIXER CONTROL ROD AND SPD BRK INPUApr 21, 2001 · N928UP · Boeing 72722C · Aileron Control SystemSDR UPS01234776Pitot Tube · damagedINSPECTION TYPE:IN AT FL 33.0 CAPTS ALT 33,000 FT F/OS ALT 32820 FT CAPTS A/S 296 KNOTS F/OS A/S 294.5. STANDBY ALT 33,200. TESTED CAPT AND FO ALT PER MM 34-12-05. TESTS GOOD. TESTED CAPT AND FO MACH A/S PER MM 34-12-06. TESTS GOOD F/OS PITOT TUBE DAMAGED Jan 26, 2001 · N928UP · Boeing 72722C · Pitot/Static SystemSDR UPS01234762Heat Exchanger · leakingINSPECTION TYPE:C, RT WING HYDRAULIC HEAT EXCHANGER LEAKING HYD FLUID INTO NR 3 TANK. ACCOMPLISHED RIGHT WING HYDRAULIC COOLER ANTI-ROTATION PLATE REPLACEMENT IAW AVITAS ENGINEERING REPAIR ORDER AVHM-187RO-1.Jan 17, 2001 · N928UP · Boeing 72722C · Hydraulic System, MainSDR UPS01234765Frame · crackedINSPECTION TYPE:C, LEFT WHEEL WELL CASTING FRAME BS 930 SHOWS CRACK TO LOWER END STR 18L. INSTALLED REPAIR AT BS 930 CASTING FRAME IAW UPS EO B727-5310-2611B.Jan 11, 2001 · N928UP · Boeing 72722C · Fuselage Main, FrameSDR UPS01234770Angle · crackedINSPECTION TYPE:C, RT WING NR 6 LE SLAT, I/B TRACK RECESS CUTOUT 2 ANGLES CRACKED, I/B AND O/B AT LWR END OF ANGLE. REMOVED AND REPLACED 2 ANGLES IAW SRM 57-10-2.Jan 3, 2001 · N928UP · Boeing 72722C · Leading Edge DevicesSDR UPS01234767Angle · crackedINSPECTION TYPE:C, RT WING NR 6 LE SLAT, O/B TRACK RECESS CUTOUT, I/B VERT ANGLE CRACKED AT LWR END. REMOVED AND REPLACED I/B VERT ANGLE IAW SRM 51-30-2.Jan 3, 2001 · N928UP · Boeing 72722C · Leading Edge DevicesSDR UPS01234764Skin · bulgedINSPECTION TYPE:C, MAIN CARGO DOOR OUTER SKIN BULGING AT BS 610, STR 4L. INSTALLED DOUBLER REPAIR IAW 52-30-01.Jan 3, 2001 · N928UP · Boeing 72722C · Cargo/Baggage DoorsSDR UPS01234763Skin · bulgedINSPECTION TYPE:C, MAIN CARGO DOOR OUTER SKIN BULGED AT BS 490, STR 4 LEFT. INSTALLED REPAIR AT MAIN CARGO DOOR SKIN IAW SRM 52-30-01.Jan 3, 2001 · N928UP · Boeing 72722C · Cargo/Baggage DoorsSDR UPS01234772Skin · bulgedINSPECTION TYPE:C, SKIN BULGING AT STR 2L, STA 441. ACCOMPLISHED REPAIR IAW UPS EO B727-5310-1371E.Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS01234771Skin · crackedINSPECTION TYPE:C, NOSE LANDING GEAR WHEEL WELL TOP CEILING BS 272, LBL 15 SHOWS CRACK RUNNING BETWEEN RIVETS, ABOUT 2.5 INCHES LONG. INSTALLED DOUBLER REPAIR IAW SRM 51-40-2.Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS01234766Skin · bulgedINSPECTION TYPE:C, SKIN BULGING BETWEEN STR 5R AND STR 6R AT STA 481. INSTALLED REPAIR DOUBLER IAW UPS EO B727-5310-1371E.Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS01234759Pressure Panel · crackedINSPECTION TYPE:C CK, NLG W/W RIGHT SIDEWALL BS272 LWR OF AFT ACCESS DOOR CRACK INDICATION RUNNING BETWEEN FASTENER ROW, 1.5 INCH LONG. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2.Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, BulkheadSDR UPS01234758Pressure Panel · crackedINSPECTION TYPE:C CK, NLG W/W LT SIDEWALL BS 243 TO LWR SHOWED CRACK AROUND FASTENER, ABOU T 1 INCH LONG. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2.Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, BulkheadSDR UPS01234757Pressure Panel · crackedINSPECTION TYPE:C CK, NLG W/W TOP CEILING RBL 15 AND BS 272 CRACK INDICATION ALONG FASTENER ROW ABOUT 2.5 INCHES LONG. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2.Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, BulkheadSDR UPS01234756Pressure Panel · crackedINSPECTION TYPE:C CK, NLG W/W RIGHT SIDEWALL BS 251 AFT OF FWD ACCESS DOOR, CRACK INDICATION ALONG FASTENERS ROW, ABOUT 4.5 INCHES. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2.Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, BulkheadSDR UPS01234755Pressure Panel · crackedINSPECTION TYPE:C CK, NOSE LANDING GEAR WHEEL WELL SIDEWALL RIGHT BS 290 TO LWR HAS CRACK INDICATION MIGRATING FROM PREVIOUS REPAIR ABOUT 1 INCH LONG. INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH SRM 51-40-2.Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, BulkheadSDR UPS01234761Skin · bulgedINSPECTION TYPE:C, BULGE IN SKIN AT STA 260 LEFT WL 270. REPAIRED PER UPS EO B727-5310-1371E.Dec 31, 2000 · N928UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS01234753Support Bracket · crackedINSPECTION TYPE:C CK, LEFT WHEEL WELL STA 913 UPLOCK SUPPORT ASSY, CRACK AT AFT SUPPORT FRAME. CRACK VERIFIED BY NDT. REPAIRED STA 913 SUPPORT FRAME IN ACCORDANCE WITH UPS EO B727-5310- 1896B, KIT INSTALLED. (P/N 65C-27194-25).Dec 29, 2000 · N928UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS01234760Skin · bulgedINSPECTION TYPE:C CK, FUSELAGE AFT RIGHT BS 1333 STR 8R TO STR 10R, SKIN BULGE AND FASTENERS PULLING THROUGH. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 54-30-3 FIG 7.Dec 26, 2000 · N928UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS00232079Light · inoperativeEXIT LIGHT OVER COCKPIT DOOR INOPERATIVE. CANIBALIZED EMERGENCY LIGHT ASSY FROM AIRCRAFT 907 OPS CHECKED GOOD.Mar 22, 2000 · N928UP · Boeing 72722C · Emergency LightingSDR UPS99231048Light · missingINSPECTION TYPE:N/A, FWD ENTRY DOOR EMERGENCY EXIT LIGHT ROBBED FOR ACFT 910. INSTALLED FWD ENTRY DOOR EMERGENCY EXIT LIGHT, OPS CHECK GOOD.Nov 4, 1999 · N928UP · Boeing 72722C · Emergency LightingSDR UPS99230117Duct · crackedINSPECTION TYPE:C, ENGINE NR 3 ANTI-ICE DUCT CRACKED AT BRACKET NEAR ANTI-ICE VALVE. DUCT REPAIRED PER SMRO EO 99-17-005 (UPS ENGINEERING FILE NR 727-30- 0009).Jul 9, 1999 · N928UP · Boeing 72722C · Engine Anti-Icing SystemSDR UPS99230116Skin · delaminatedINSPECTION TYPE:C, RUDDER LOWER TAB DELAMINATED AT UPPER T/E LEFT SIDE PREVIOUS REPAIR. REPAIRED IAW SRM 51-40-10 FIG 3.Jul 9, 1999 · N928UP · Boeing 72722C · Rudder, Tab StructureSDR UPS99230107Clevis · crackedINSPECTION TYPE:C, ENGINE NR 2 STRUTS ABOVE NR 2 HORIZONTAL FIRE WALL, CLEVIS CRACKED ON LOWER END OF LOWER STRUT. CLEVIS REPLACED IAW DWG 65-17553.Jul 9, 1999 · N928UP · Boeing 72722C · Nacelle/Pylon StructureSDR UPS99230120Balance Panel · corrodedINSPECTION TYPE:C, NR 5 ELEVATOR BALANCE PANEL RT HAS EVIDENCE OF CORROSION ON PANEL TO HINGE ATTACH RACK. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-6. BALANCE PANEL REPLACED AND INSTALLED IAW MM 27-30-21.Jul 8, 1999 · N928UP · Boeing 72722C · Elevator StructureSDR UPS99230106Web · corrodedINSPECTION TYPE:C, CORROSION ON SHEAR WEB LBL 24.75 STA 1130-1183. WEB REPAIRED IAW SRM 51-40-2.Jul 8, 1999 · N928UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS99230124Angle · crackedINSPECTION TYPE:C, FLOOR SUPPORT CRACKED BS 850 LBL 45.5. FLOOR SUPPORT ANGLE REPAIRED IAW SRM 57-20-1.Jul 7, 1999 · N928UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS99230119Mount · corrodedINSPECTION TYPE:C, CORROSION FOUND ON NR 1 ENG, FWD MOUNT HOLE AFT I/B HOLE ONLY (PITTING CORROSION). INVESTIGATED AND REPAIRED IAW SMRO EO 99-17-002 UPS ENGINEERING FILE NR 727-54-0088.Jul 7, 1999 · N928UP · Boeing 72722C · Engine Mount SectionSDR UPS99230118Mount · corrodedINSPECTION TYPE:C, CORROSION FOUND ON NR 3 ENG FWD MOUNT HOLES AT TRUNNION FITTING ATTACH (PITTING CORROSION). REPAIRED IAW SRMO EO 99-17-003 (UPS ENGINEERING FILE NR 727-54-0089).Jul 7, 1999 · N928UP · Boeing 72722C · Engine Mount SectionSDR UPS99230103Rib · crackedINSPECTION TYPE:C, NR 6 SLAT RIB AT IB SIDE OF ACTUATOR HAS SMALL CRACK IN FWD LOWER RADIUS. RIB REPAIRED IAW SRM 57-50-3.Jul 7, 1999 · N928UP · Boeing 72722C · Leading Edge DevicesSDR UPS99230121Firewall Web · crackedINSPECTION TYPE:C, STRUCTURE OVER NR 2 ENGINE HORIZ FIREWALL LEFT AND RIGHT WEBS AT BS 1376 ARE CRACKED. FABRICATED AND INSTALLED WEBS IAW DRG NR 65-17555.Jul 6, 1999 · N928UP · Boeing 72722C · Nacelle/Pylon, Bulkhead/FirewallSDR UPS99230110Stiffener · crackedINSPECTION TYPE:C, NR 4 SPOILER IB ATTACH VERTICAL LEG CRACKED VERTICAL STIFFENER. REPLACED IAW DWG 69-16201.Jul 6, 1999 · N928UP · Boeing 72722C · SpoilersSDR UPS99230105Support · corrodedINSPECTION TYPE:C, CORROSION FOUND ON AFT LT LAVATORY PARTITION SUPPORT ON FLOOR STRUCTURE BS 1140 LBL 24.75-LBL60. TOP HAT SECTION REPLACED IAW SRM 51-10-1.Jul 6, 1999 · N928UP · Boeing 72722C · Fuselage Miscellaneous Structure
Back to N928UP, cancelled Mar 26, 2013