N138UP
Service difficulty reports · 250
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 = 'N138UP' AND registry_match = 'registration' 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 = 'N138UP' AND registry_match = 'registration' 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 IPXA11165113Floor Panel · crackedINSPECTION TYPE:10YR, MAIN DECK CARGO PANEL 252WJ IS CRACKED AND DELAMINATED. REPAIRED MAIN CABIN FLOOR PANEL NR 252WJ IAW EO A300-5320-38221-B, PARA 6A 1.SDR IPXA1165083Floor Panel · crackedINSPECTION TYPE:10YR, FLOOR PANEL, 252NM CRACKED. REPAIRED FLOOR PANEL 252NM IAW EO A300-5320-38221-B, PARA 6 (1).SDR IPXA1165082Seat Track · corrodedINSPECTION TYPE:10YR, FR79 Y450 SEAT TRACK CORRODED. REPAIRED FR79, Y450 SEAT TRACK IAW SRM 53-10-16, PARA 4, FIG 201.SDR IPXA1165432Skin · gougedINSPECTION TYPE:10YR, REPAIR SURVEY SEQUENCE NR 138-W3-01, REPAIR DOUBLER IS GOUGED AT RIB 13 TO RIB 15, STGR 2.6 TO 2.8 LT WING CTR FLAP. ACCOMPLISHED REPAIR ON LT WING CTR FLAP RIB 13 TO RIB 15, STGR 2.6 TO 2.8 IAW SRM 57-50-00, PARA 4F, FIG 206 AND EO A300SDR IPXA11165146Seat Track · corrodedINSPECTION TYPE:10YR, CORROSION FOUND AT SEAT TRACK -Y1137.1 FR 80 AT MAIN CARGO COMPT. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK AT FR -1137.1 FR 80 IAW SRM 53-10-16, FIG 201, PB 201, PARA 4.SDR IPXA1164997Skin · damagedINSP TYPE:10YR, REPAIR SURVEY SEQUENCE NR138-W3-02, REPAIR DOUBLER HAS LOOSE RIVETS AT LT INBD FLAP UPPER SURFACE RIB3 TO RIB 4, STR 2.1 TO 2.2 AND DOES NOT CORRELATE TO THE SRM. ACCOMPLISHED REPAIR ON LT INBD FLAP UPPER SURFACE IAW SRM 57-50-00, PB 201, PARASDR IPXA1164930Floorboard · delaminatedINSPECTION TYPE:10YR, FWD CARGO PIT FLOORBOARD NR 132FE IS DELAMINATING AT CORNER AND SKIN IS GOUGED. FABRICATED FWD CARGO FLOORBOARD NR 132FE IAW EO A300-5320-16407-E, APPENDIX C.SDR IPXA1165423Bullnose · chafedINSPECTION TYPE:10YR, RT WING OTBD FLAP INBD BULLNOSE IS CHAFED. ACCOMPLISHED REPAIR ON RT WING OTBD FLAP INBD BULLNOSE IAW SRM 57-50-00, PB 201, PARA 4H FIG 208.SDR IPXA1165424Skin · gougedINSPECTION TYPE:10YR, NR 1 ENG INBD T/R UPPER LONGERON SKIN GOUGED AT 12:00 POSITION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW EO A300- 7830-40521-B AND EA 300-7830-01-A2949.SDR IPXA0163613Skin · damagedREF LOG PAGE 434115 ITEM 1, REF D412751 FUSELAGE EXTERNAL REPAIR DOUBLER DMG ADJACENT TO FR85 AND L45. REPAIRED IAW EO A300-5330-35623D.SDR IPXA0163604Skin · damagedFUSELAGE SKIN DAMAGED FR 85. REPAIRED IAW EO A300-5330-35623-C.SDR IPXA10163564Solenoid Valve · inoperativeON TAKEOFF, SLAT SYS 2 FAULT LIGHT ECAM SLAT SYS 2 FAULT ILLUMINATED OVERHEAD PANEL. R & R SOLENOID VALVE ON VALVE BLOCK 26CV REF MM 27-84-33-04. FOLLOWED FIM 27-80-05, STEP 1 TO A2-6-13. ENABLE SOLENOID VALVE HAD RESISTANCE VALVE OF 69 OHMS. OPS CK OF SYS 2SDR IPXA10162287Skin · dentedRT INBD FLAP DENTED WITH GOUGE. REPAIRED IAW EO A300-5750-35971-C.SDR IPXA0161966Warning Light · false activationWHILE PASSING THROUGH FL210 ON CLIMB OUT GOT SLIDE WARNING ON CREW DOOR (AURAL AND LIGHT) WARNING WENT OUT ON DESCENT PASSING THROUGH 13,500 AT 305 KTS AND 410 PSI. PERFORMED OPS TEST OF EMER ESCAPE SLIDE RELEASE IAW MM 52-73-00-05. AURAL AND LIGHT CHECKS GOOSDR IPXA09157978Slide · inoperativeL1 DOOR SLIDE INOP. REMOVED AND REPLACED L1 DOOR SLIDE ASSY IAW MM 25-61-21-04. OPS CHECK GOOD.SDR IPXA09157979Bottle · low pressureMAIN CREW DOOR SLIDE BOTTLE PRESSURE LOW. PLACED ON MEL 52-11-01-3. M414400 ASSIGNED. CREW DOOR EVAC SLIDE INOP. REMOVED AND REPLACED L1 DOOR SLIDE ASSY IAW MM 35-61-21-04. OPS CHECK GOOD. M414400 CLEARED.SDR IPXA09156148Jackscrew · malfunctionedINSPECTION TYPE:N/A NEITHER SLAT EXTENDED FOR LANDING. RECYCLED, NO SLATS/FLAPS 40. T/S IAW TSM 27-80-02 FOUND RT TQ LIMITER POPPED AND RT NR 3 JACKSCREW LOCKOUT TRIPPED. TOPPED OFF RT NR 3 JACKSCREW WITH 70CC IAW AMM 12-13-27. GREASED BALL NUT IAW AMM 12-SDR IPXA09154835Connector · not seatedINSPECTION TYPE:N/A EVAC SLIDE OR SLIDE RAFT RELEASE WARNING SYS LIGHT INOP. BUZZER OK. DEFERRED PER MEL 52-73-01-1 M395381. RESEATED ASPSU CONNECTOR PERFORMED TEST OF POWER SUPPLY UNIT IAW MM 52-73-00. SYSTEM OPS CHECK GOOD. THIS CLEARS M395381.SDR UPS08153223Floor Panel · damagedINSPECTION TYPE:C1 MAIN CARGO FLOOR BOARD PANEL 252WJ HAS A FIELD REPAIR. REPAIRED MAIN CARGO FLOOR PANEL 252WJ REF SRM 53-10-20 TABLE 201 PARA 8A.SDR UPS08153238Floor Panel · damagedINSPECTION TYPE:C1 MAIN CARGO FLOOR PNL 251XJ AFT HAS FIELD REPAIRS. REPAIRED MAIN CARGO FLOOR PNL 251XJ REF A300-600 SRM 51-10-20 TABLE 201 PARA 8A.SDR UPS08153237Floor Panel · damagedINSPECTION TYPE:1C MAIN CARGO FLOOR PNL 252SJ HAS FIELD REPAIRS. REPAIRED MAIN CARGO FLOOR PNL 252SJ REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.SDR UPS08153222Floor Panel · damagedINSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 251MJ FWD HAS FIELD REPAIR. REPAIRED MAIN CARGO FLOOR PANEL 251MJ REF SRM 53-10-20 TABLE 201 PARA 8A.SDR UPS08153221Floor Panel · damagedINSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 251SJ HAS FIELD REPAIR. REPAIRED MAIN CARGO FLOOR PANEL 251SJ REF SRM 53-10-20 TABLE 201 PARA 8A.SDR UPS08153220Floor Panel · damagedINSPECTION TYPE:1C MAIN CARGO FLOOR PANEL 252OJ HAS A FIELD REPAIR. REPAIRED MAIN CARGO FLOOR PANEL 252OJ REF SRM 53-10-20 TABLE 201 PARA 8A.SDR UPS08153244Skin · gougedINSPECTION TYPE:1C GOUGE 24 INCHES FWD AND 18 INCHES LEFT OF TAIL STAND BALL. FABRICATED & INSTALLED PERMANENT REPAIR IN FUSELAGE SKIN 24 INCHES FWD & 18 INCHES LEFT OF TAIL STAND BALL REF SRM 53-10-12 FIG 216, SRM 53-19-12 FIG 2, EO A300-5100-20876-B AND EO SDR UPS08151791Liner · looseCREW ENTRY DOOR SLIDE WARNING SOUNDING IN FLIGHT. FOUND GUIDE ARM LINING LOOSE AND MISSING HARDWARE. LINING WAS INTERFERING WITH DOOR CLOSING. INSTALLED HARDWARE AND LINING IAW 52-10-13-04. PRESS A/C IAW 21-31-00-5. NO DEFECTS NOTED. PERFORMED TEST OF MAIN ESDR UPS08151408Door · unsecureATB - CREW ENTRY DOOR ECAM MESSAGE. A/C WAS SLOWLY LOSING PRESSURIZATION AND CREW WAS HEARING A LOUD SQUEAL. FLIGHT LANDED WITH NO FURTHER INCIDENT. PERFORMED MAINTENANCE CHECK PER AMM A300-05-53-00-00. NO FAULTS NOTED.SDR UPS07151269Seat · defectiveINSPECTION TYPE:N/A DURING TAKEOFF ROLL IN MIAMI, CAPTS SEAT UNLATCHED AND SLID TO REAR STOP. REJECTED TAKEOFF SPEED LESS THAN 50 KTS. REMOVED AND REPLACED CAPT'S SEAT ASSY IAW A300 MM 25-11-11-04-01.SDR UPS07151074Light · inoperativeINSPECTION TYPE:N/A EVACUATION SLIDE WARNING SYSTEM LIGHTS DO NOT ILLUMINATE WHEN TESTED M361512. FOUND ASPSU IN MAINTENANCE CYCLE. RESET ASPSU CB 3WN AND TESTED ASPSU IAW MM 52-73-00-05. RESIDUAL PRESSURE WARNING SYSTEM ALL TESTED NORMAL. THIS CLEARS M361SDR UPS07151003Wire Harness · unknownINSPECTION TYPE:N/A ATB - IFSD - NR 2 ENGINE SHUT DOWN TO LOW OIL PRESSURE. *S/D* REMOVED AND REPLACED OIL PRESSURE TRANSMITTER HARNESS, WIRES 072057, 072056, 072055 FROM CONNECTOR DT583 & D4952P REF P&W CMM 71-51-01. REF LP 651061 REMOVED AND REPLACED NR 2SDR UPS07150557Indicator · fluctuatesINSPECTION TYPE:N/A DURING CLIMBOUT RIGHT ENGINE OIL PRESSURE INDICATION WENT TO XX ON BOTH ECAM & GAUGE, AFTER A COUPLE OF MINUTES INDICATION CAME BACK BUT WAS FLUCUATING, CREW REDUCED ENGINE POWER BUT DID NOT SHUTDOWN ENGINE, ON DESCENT EVERYTHING RETURNED TSDR UPS07150496Floor Panel · puncturedINSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL BETWEEN 10R AT 11R PUNCTURED 1 INCH. ACCOMPLISHED PERMANENT REPAIR PER SRM 53-10-20. OPS CHECK OK.SDR UPS06147624Smoke Detector · inoperativeTURNING BASE, LEG TO BUD AIRPORT, RW31L MASTER CAUTION AND ECAM SMOKE, AVIONICS IND ILLUMINATED, A/C LANDED ASAP. AVIONICS SMOKE PROCEDURE ACCOMPLISHED. INDICATION CONTINUES INTERMITTENTLY. EMERGENCY DECLARED T/S PERFORMED IAW TSM 26-15-00 PG 101 FIG 10SDR UPS06146475Lamp · inoperativeFOUND LAV EMERG LIGHT INOP. RELAMPED WORKED OK.SDR UPS06146433Connector · not seatedRED WARNINGS LIGHT ON ESCAPE SLIDE DOES NOT ILLUMINATE WHEN TEST BUTTON IS DEPRESSED. RESEATED CONNECTOR ON THE ASPSU. WARNING LIGHT AND BUZZER OP CKS GOOD. OK FOR CONTINUED SERVICESDR UPS06146197Angle · crackedINSPECTION TYPE:5YR, NR 1 ENG STRINGER FAIRING, 2ND STIFFENER FWD FROM TRAILING EDGE, OUTBD SIDE IS CRACKED THROUGH RIVET AT BOTTOM END. REMOVED & REPLACED STIFFENER PER A300 SRM 51-40-00.SDR UPS06146134Bracket · crackedAFT CARGO FWD BULKHEAD SUPPORT BRACKET CRACKED STA 3354 CTR. REMOVED AND REPLACED BRACKET PER A300 SRM 51-40-00.SDR UPS06146133Bracket · crackedAFT CARGO FWD BULKHEAD SUPPORT BRACKET CRACKED STA 3354. REMOVED AND REPLACED BRACKET PER A300 SRM 51-40-00.SDR UPS06146234Support Angle · crackedINSPECTION TYPE:5YR, NR 2 PYLON LOWER AFT OTBD SUPPORT ANGLE CRACKED AT JOGGLE INTERIOR SIDE. REMOVED AND REPLACED SUPPORT ANGLE PER A300 SRM 51-40-21.SDR UPS06146233Support Angle · crackedINSPECTION TYPE:5YR, NR 2 PYLON LOWER AFT INBD SUPPORT ANGLE CRACKED AT JOGGLE INTERIOR SIDE. REMOVED AND REPLACED SUPPORT ANGLE PER A300 SRM 51-40-21.SDR UPS06146231Support · crackedINSPECTION TYPE:5YR, NR 2 PYLON LOWER AFT END SUPPORT MEMBER CRACKED AT INBD SIDE JUST ABOVE GANG DRAIN EXIT OF PYLON. REMOVED AND REPLACED MEMBER PER A300 SRM 51-40-21 AND 51-40-00.SDR UPS06146193Angle · crackedINSPECTION TYPE:5YR, NR 1 ENG AFT PYLON OTBD MEMBER SECTION ANGLE IS CRACKED AT JOGGLE. REMOVED AND REPLACED ANGLE PER A300 SRM 51-40-21.SDR UPS06146192Structure · crackedINSPECTION TYPE:5YR, NR 1 ENG AFT LOWER PYLON MEMBER SECTION IS CRACKED AT THRU HOLE FOR PNEUMATIC LINE. REMOVED AND REPLACED MEMBER SECTION PER A300 SRM 51-40-21.SDR UPS06146195Rib · crackedINSPECTION TYPE:5YR LT WING KRUEGER BOX AREA CURVED DOUBLER ON 2ND RIB FROM FUSELAGE HAS A CRACK. REMOVED AND REPLACED DOUBLER PER A300 SRM 51-40-00.SDR UPS06146132Rib · crackedRT WING KRUEGER FLAP WELL HAS RIB CRACKED APPROX 1.5" IN LOWER RADIUS. REMOVED AND REPLACED RIB PER A300 SRM 51-40-00.SDR UPS06146131Shear Plate · crackedLT AFT MAIN CARGO COMPT FS 79 LBL64.00 SHEAR PLATE CRACKED 1.5"L AT FWD INBD AREA AT LIGHTENING HOLE AT STR 25. REMOVED AND REPLACED SHEAR PLATE PER A300 SRM 51-40-21.SDR UPS06146130Shear Plate · crackedINSPECTION TYPE:5YR RT AFT MAIN CARGO COMPT FS 79 RBL64.00 SHEAR PLATE CRACKED 1.5" LONG AT INBD FWD AREA AT LIGHTENING HOLE AT STR 25R. REMOVED AND REPLACED SHEAR PLATE PER A300 SRM 51-40-21.SDR UPS04141853Smoke Detector · intermittentINSPECTION TYPE:N/A AVIONICS SMOKE INTERMITTENTLY. REMOVED AND REPLACED MAIN BAY SMOKE DETECTOR 11 IAW 26-15-124, OPS CHECK GOOD.SDR UPS04141677Light · inoperativeINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS, DISARM LIGHT INOP. REPLACED DISARM LIGHT ASSY IAW ESPM 20-45-11. OPS CHECK GOOD.SDR UPS03141152Skin · gougedINSPECTION TYPE: C1, LT WING INBD FLAP TOP SURFACE IS GOUGED OUTBOARD END, BLENDED AREA IAW A300 SRM 57-50-00. ORIGINAL THICKNESS OF .032 REMAINING MATERIAL .025 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE IAW A300 SRM 51-50-00 INSTALLED REPAIR DOUBLER IAW A3
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