N933UP, cancelled Aug 24, 2007
Service difficulty reports · 157
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 = 'N933UP' AND deregistration_id = 'N933UP-2007-08-24' 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.
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 = 'N933UP' AND deregistration_id = 'N933UP-2007-08-24' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UPS02238717Battery · dischargedINSPECTION TYPE:N/A EXIT LIGHT ABOVE COCKPIT ENTRANCE DOOR DOES NOT TEST. CABIN DOOR ENTRANCE LIGHT CHECKS OK BUT CHARGE STAT US IS IN-DOUBT. R/R EMERGENCY EXIT LIGHT BATTERIES IN COCKPIT ENTRANCE DOOR AND CABIN DOOR, REF UPS 727 M/M CHAP 33-50-67 OPS CHECKESDR UPS02238567Battery · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT IN COCKPIT INOP. REMOVED AND REPLACED BATTERY, OPS CHECKS GOOD.SDR UPS02237797Angle · bulgedINSPECTION TYPE:C LT AFT NOSE W/W DOOR CUTOUT HAS BULGE FASTENERS PULLING OFF BS 320 TO BS 350. REPLACED LEFT LOWER CHORD ANGLE AT NWW AREA IAW B727 SRM 51-30-2.SDR UPS02237796Skin · crackedINSPECTION TYPE:C LT FUSELAGE SKIN HAS CRACK STARTING AT FASTENER CUT OUT BS 254 STR 10L CRACK DOES NOT NEED STOP DRILL IT RUNS FROM FASTENER HOLE TO EDGE OF SKIN, INSTALLED DOUBLER REPAIR AT LT FUSELAGE. BS 254 STR 10L AS PER B727 SRM 53-30-3 MATERIAL USESDR UPS02237795Skin · bulgedINSPECTION TYPE:C UPPER FUSELAGE SKIN HAS BULGE AT BUTT JOINT BS 521 STR 3L - 4R.SDR UPS02237794Skin · canningINSPECTION TYPE:C RT FWD FUSELAGE SKIN HAS OIL CAN, PREVIOUSLY REWORKED BS 340 STR 19R.SDR UPS02237493Battery · dischargedINSPECTION TYPE:IN EMERGENCY EXIT LIGHTS OVER MAIN ENTRY DOOR INOP. REMOVED AND REPLACED BATTERIES, OPS CHECKS NORMAL.SDR UPS01237360Light · inoperativeINSPECTION TYPE:N/A BOTH EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN COCKPIT EMERGENCY LIGHTS. REPLACED EMERGENCY LIGHT ASSY OVER EXIT DOOR P/N ON AND OFF 10-0067, S/N OFF 42-11, S/N O N 27025. OPS CHECKS GOODSDR UPS01235463Windshield · failedFIRST OFFICERS WINDSHIELD SHATTERED. OLD WINDOW REMOVED NEW WINDOW PARTIALLY INSTALLED / R&R R1 WINDOW PER M/M 56-11-1 WINDOW HEAT OPS CHECK GOODSDR UPS01234968Fire Loop · inoperativeINSPECTION TYPE:IN ENG NR 3 A-LOOP WILL NOT TEST. *S/D* FOUND CONNECTOR D354J CONTAMINATED WITH DIRT AND MOISTURE. CLEANED SAME THOROUGHLY. TESTED NORMAL. M209166 CLEARED.SDR UPS00234506Structure · crackedINSPECTION TYPE:PRE NR 4 LEADING EDGE SLAT CRACKED. AWAITING LOG PAGE ENTRY.SDR UPS00233587Flap Track · corrodedINSPECTION TYPE:SI, NR 1 FLAP TRACK FWD ATTACH LUG FACES I/B AND O/B HAVE LIGHT SURFACE RUST (CORROSION C57-581-06.00-03). REMOVED CORROSION FROM NR 1 FLAP TRACK FWD ATTACH LUG FACES I/B AND O/B AND REPAIRED PER FAA FORM 8130-3 SYSTEM TRACKING REF NR 20235.SDR UPS00233586Flap Track · corrodedINSPECTION TYPE:SI, CORROSION (SDN C57-581-06.00-04) ON NR 7 FLAP TRACK AFT CENTER MOUNT HOLE. REMOVED CORROSION ON NR 7 FLAP TRACK AFT CENTER MOUNT HOLE AND REPAIRED PER FAA FORM 8130-3 SYSTEM TRACKING REF NR 20232.SDR UPS00233585Flap Track · corrodedINSPECTION TYPE:SI, CORROSION (SDN C57-581-06.00-04) ON NR 7 FLAP TRACK FWD ATTACH POINT I/B FLANGE AROUND BUSHING HOLE. REMOVED CORROSION ON NR 7 FLAP TRACK FWD ATTACH POINT I/B FLANGE AROUND BUSHING HOLE AND REPAIRED PER FAA FORM 8130-3 SYSTEM TRACKING REF SDR UPS00233609Web · corrodedINSPECTION TYPE:SI, CORROSION ON UPPER SURFACE OF SHEAR WEB AT BS 640, WL 208 LBL 63. SHEAR WEB REPLACED AT STA 630 - 660, LBL 45-LBL 62, WL 208 PER ER NR 00-0952.SDR UPS00233568Fitting · crackedINSPECTION TYPE:SI, STRINGER FITTING IS CRACKED AT BS 365 STR 26L. REMOVED AND REPLACED STRINGER FITTING.SDR UPS00233588Fitting · crackedINSPECTION TYPE:SI, NR 1 K-FLAP O/B ATTACH LUG FITTING ON K-FLAP UPPER O/B SIDE IS CRACKED. REMOVED AND INSTALLED NEW K-FLAP ASSY PER MM 27-81-01.SDR UPS00233540Skin · corrodedINSPECTION TYPE:C, CORROSION ON LWR RUDDER RT SKIN AT STA 120.6 IN BELOW FRONT SPAR. REPAIRED PER SRM 55-20-3 PG 1 STEP 3 & 4 AND SRM 51-40-5 PG 20 & 22 STEP 13 A-I.SDR UPS00233612Stringer · crackedINSPECTION TYPE:SI, RIGHT WING UPPER STR 17 OUTSIDE OF RIB AT WS 304 IS CRACKED. REMOVED CRACK STRINGER SECTION. FABRICATED AND INSTALLED NEW SECTION, ALL WORK DONE IAW SRM 57-10-4, 51-20-1, 51-30-2.SDR UPS00233611Flap Track · corrodedINSPECTION TYPE:SI, NR 5 FLAP TRACK IS RUSTED AT MAIN LANDING GEAR DOOR FWD FITTING ATTACH BOLTS. REMOVED AND REPLACED FLAP TRACK PER TC 57-581-04-4D.SDR UPS00233558Carriage · corrodedINSPECTION TYPE:SI, CORROSION (SDN C57-581-04.00-04) IN BORE OF SPINDLE FOR NR 6 FLAP CARRIAGE. REMOVED AND REPLACED NR 6 FLAP CARRIAGE PER MM 25-51-03.SDR UPS00233513Mount · corrodedINSPECTION TYPE:SI, CORROSION ON NR 6 FLAP TRACK AFT ATTACH MOUNT BLOCK OUT OF LIMITS IAW SRM 51-30-2. REMOVED AND REPLACED MOUNT BLOCK IAW SRM 51-30-5.SDR UPS00233512Fitting · corrodedINSPECTION TYPE:SI, NR 6 FLAP TRACK SPOILER BEAM MOUNT FITTINGS CORRODED OUT OF LIMITS IAW SRM 51-30-2 ON RT WING. FOUND WHILE WORKING NRC 178771. REMOVED CORRODED MOUNT FITTINGS AND REPLACED WITH NEW PART IAW SRM 51-30-2.SDR UPS00233557Fitting · corrodedINSPECTION TYPE:SI, MAIN DECK FLOOR WEB FITTING CORRODED (C53-224-01.00-03) BETWEEN LEFT CREASE BEAM AND DITCHING PAN, FWD OF BS 1183 BULKHEAD BS 1180 LBL 65, WL 208. REMOVED AND REPLACED FLOOR WEB FITTING IAW SRM 51-30-05, 53-10-01, 51-10-06.SDR UPS00233556Floorbeam · corrodedINSPECTION TYPE:SI, CORROSION (C53-111-01.00-03) FWD CARGO BAY BS 660 FLOORBEAM FWD SIDE UPPER FLANGE LOWER SURFACE AT LBL 45 TO LBL 50. REMOVED CORROSION IN DESCREPANT AREA AT LBL 45 IN A 2.4 X 1.0 X .030 ORIGINAL THICKNESS .240 OUT OF LIMITS. REMOVED UPPERSDR UPS00233555Floorbeam · corrodedINSPECTION TYPE:SI, CORROSION (C53-111-01.00-02) FWD CARGO BAY STA 540 FLOORBEAM FWD SIDE, UPPER FLANGE, LWR SURFACE AT LBL 45. REMOVED CORROSION ON UPPER CHORD LOWER FLANGE IN AN AREA OF 1.0 X 2.0. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 5. CUT OFF TSDR UPS00233610Drum · corrodedINSPECTION TYPE:SI, RT MLG MANUAL EXTENSION CABLE DRUM IS CORRODED. REMOVED AND REPLACED PER MM 32-34-01.SDR UPS99228760Spar Chord · corrodedINSPECTION TYPE-C,CORROSION (C57-581-03.00E-01) ON L/W UPPER REAR SPAR CHORD AT WBL 76, INSIDE FUEL HOSE SHROUD. REPAIRED IAW ERO 99-5030.SDR UPS99228742Chord · corrosionINSPECTION TYPE:C CORROSION (C57-581-03-00E-01) ON L/W UPPER REAR SPAR CHORD AT WBL 76, INSIDE FUEL HOSE SHROUD. REPAIRED IAW ERO 99-5030.SDR UPS99228633Seat Track · crackedINSPECTION TYPE:C WHILE ACCESSING OVERWING FRAMES FOUND SEAT TRACK AT STA 760 RBL 65 WL 208 CRACKED AT O/B FLANGE. REPLACED SEAT TRACK FROM BS 760 TO BS 848 PER 727 SRM 53-10-5 AND 51-30-2.SDR UPS99228558Skin · corrodedINSPECTION TYPE-C, NR 4 K-FLAP AND BULLNOSE ARE CORRODED AT INBD LOWER BONDING JUMPER ATTACHMENT POINTS. REPLACED K-FLAP PER MM 27-81-01 AND ADJUST/TEST PER 727 MM 27-81-00.SDR UPS99228530Skin · corrodedINSPECTION TYPE-C ,CORROSION RT ELEVATOR AROUND BASE OF O/B STATIC WICK. REPLACED SKIN PER SRM 51-30-2 AND SRM 55-20-3.SDR UPS99228559Foreflap · corrodedINSPECTION TYPE-C, LEFT WING O/B FOREFLAP HAS .25 X 3.5 AREA OF DELAMINATION. TAP TESTED, FOUND ADDITIONAL DELAMINATION. FOUND CORRSION ON SPAR. REPLACED O/B FOREFLAP.SDR UPS99228674S Duct · crackedINSPECTION TYPE:C NR 2 ENGINE S DUCT HAS 5 INCH CRACK IN THE CENTER SECTION 4 RIBS FWD OF THE PRODUCTION BREAK, LT SIDE APPRX 8:00 POSITION. REMOVED DAMAGED AREA AND PERFORMED A FILLER AND DOUBLER REPAIR PER SRM 54-10-3, SRM 51-40-2 AND MM 51-20-151.SDR UPS99228538Skin · corrodedINSPECTION TYPE-C, CORROSION (C55-300-10.00-01) ON LT ELEVATOR AROUND I/B STATIC WICK BASE. REMOVED CORROSION OUT OF LIMITS, REPLACED SKIN PANEL. ALL WORK DONE PER SRM 55-20-1, 55-20-2 AND MM 23-61-00.SDR UPS98226858Control Valve · failedINSPECTION TYPE N/A, LEFT PACK TRIPPED OFF LIGHT ON LANDING ROLLOUT. LEFT PACK SWITCH DID NOT TURN OFF, WHITE SMOKE ENTERED COCKPIT. LOST CONTROL OF PACK EVEN WITH SWITCH OFF. LEFT PACK VLV STUCK OPEN, CYCLED VLV TO CLOSED POSITION AND ITEM DEFERRED PER MELSDR UPS98226177Battery Pack · dischargedINSPECTION TYPE-N/A, COCKPIT EMERGENCY EXIT LIGHT INOP. FOUND BOTH BATTERIES TO BE DEAD AND OUT OF DATE. REMOVED AND REPLACED TWO BATTERIES PER MM33-50-10. SYSTEM GROUND CHECKS GOOD.SDR UPS98226176Light · inoperativeINSPECTION TYPE-N/A, FOWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY.SDR UPS97225318Light · inoperativeINSPECTION TYPE-N/A, EMERGENCY LIGHT WOULD NOT TEST, BATTERIES OK. REPLACED LIGHT ASSY.SDR UPS97225089Line · crackedINSPECTION TYPE-N/A, ON GEAR RETRACTION RIGHT MAIN GEAR DID NOT RETRACT, A HYDRAULIC SYSTEM LOW PRESSURE LIGHTS ILLUMINATED. A PRESSURE WAS ZERO AND QUANTITY WAS ZERO. EXTENDED GEAR MANUALLY IN ACCORDANCE WITH AOM. FOUND RT MLG HYDRAULIC DOOR UP LINE CRACKESDR UPS97224364Skin · delaminatedINSPECTION TYPE-C, NR 7 SPOILER HAS A 4 BY 5 AREA OF DELAMINATION ON LOWER SURFACE O/B FWD CORNER. REPAIRED DELAMINATION IAW SRM 57-50-06 FIG 5.SDR UPS97224403Seat Track · crackedINSPECTION TYPE:C SEAT TRACK CRACKED AT BS 660 LBL 65. REMOVED AND REPLACED SEAT TRACK AT BS 660 LBL 65.SDR UPS97224365Skin · corrodedINSPECTION TYPE-C, NR 4 K-FLAP O/B BONDING JUMPER HOLE HAS CORROSION AROUND OLD BONDING JUMPER LOCATION. CORROSION REWORK OUT OF LIMITS IAW UPS EO B727-5740-3980 (SRM ADDENDOM) REPAIRED NR 4 K-FLAP AT OLD BONDING JUMPER LOCATION IAW SRM 57-50-3.SDR UPS97224367Frame · crackedINSPECTION TYPE-C, WHILE WORKING EO B727-5310-5596A (940 FRAME INSP) FOUND LT 930 FRAME CRACKED AT WL 228. REPAIRED FRAME IAW EO B727-5310-2580 AND BOEING DRAWING 65C10084.SDR UPS97224366Rib · crackedINSPECTION TYPE-C, NR 5 K-FLAP I/B LOWER BONDING JUMPER ON K-FLAP HAS CRACK EMANATING FROM HOLE. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR PARTS ON NR 5 K-FLAP I/B RIB AT BONDING JUMPER PER SRM 57-50-3.SDR UPS97224368Frame · crackedINSPECTION TYPE-C, WHILE WORKING EO B727-5310-5596A (940 FRAME INSP) FOUND RT 930 FRAME CRACKED AT WL 228. REPAIRED CRACKED FRAME IAW EO B727-5310-2580 AND BOEING DRAWING 65C10084.SDR UPS97224405Fitting · corrodedINSPECTION TYPE:C CORROSION ON UNDERSIDE OF HORIZONTAL FLANGE OF BS 740 BODY FITTING LBL 65 WL 207. BODY FITTING REPAIRED IN ACCORDANCE WITH BFG ER 97-2479 AND UPS ENGINEERING FILE DOCUMENT 727-53-1959.SDR UPS97222567Battery · dischargedINSPECTION TYPE P/F, EMERGENCY LIGHTS DID NOT COME ON WHEN TESTED AT COCKPIT DOOR. REPLACED BATTERIES ON EMERGENCY BAT PACK LIGHT (S/N 39810).SDR UPS96205974Support Fitting · misdrilledWHILE IN FOR C-CHECK, MAINTENANCE REPORTED DOUBLE HOLE IN HOR FLANGE OF RT MLG SUPPORT FITTING BS 940 RBL 66 WL 208. REMOVED DAMAGED AREA AND REPAIRED PER EO 727-53-1754.SDR UPS96205973Bullnose · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 1 BULLNOSE I/B LUG CORRODED. REMOVED AND REPLACED NR 1 K-FLAP BULLNOSE IAW MM 27-81-0 AND OHM 57-51-01.
Back to N933UP, cancelled Aug 24, 2007