N1997A
Service difficulty reports · 374
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 = 'N1997A' 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 = 'N1997A' 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 ABXR2026060400010Angle · crackedRIGHT WING L/E #9 SLAT AREA INTERNAL ANGLE CRACKED AT LOWER FWD WEB LOWER ANGLE. LES668. FABRICATED NEW ANGLE IAW B767 SRM 57-41-13 REPAIR 1SDR ABXR2026060400009Frame · corrodedCORROSION AT STA. 1219 RBL22 "J" FRAME FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-511.SDR 21GA202509030017Controller · faultedON APPROACH, RECEIVED WHEEL WELL FIRE EICAS MESSAGE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND NO EVIDENCE OF FIRE. REPLACED DETECTION CONTROL CARD.SDR 21GA20250610011Battery · inoperativeDURING SERVICE CHECK, L1 DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. REPLACED BATTERY ASSEMBLY.SDR UIEA2024112901131Pseu · malfunctionedAS FLAPS MOVED FROM 1 TO UP ON CLIMB OUT; FLAP (RED). EICAS STATUS MSG: NOSE A/G DISAGREE ALSO F/O HAD SPEED LIM ON HIS SPEED TAPE(<P>TROUBLESHOT & FOUND PSEU CARD MSG 002 AND TARGET MSG 266, TARGET MSG 266, FOUND RH MSG 002, SENSOR HARNESS 266, R/R PER AMM 3SDR UIEA2024112701117Wedge · damaged8028 - EA-1957A155 PART(3) REV(0) WINGS - LEADING EDGE DEVICES - RH WING #8 LEADING EDGE SLAT (PN 114T4105-58 /SN 000598) TRAILING EDGE WEDGE EXISTING REPAIR DELAMINATION - TIME LIMITED REPAIR(<P>PERMANENT REPAIR WAS PERFORMED IAW EA 1957A155. NO FURTHER DEFECSDR UIEA2024112601116Bear Strap · crackedLH FWD DOOR, AFT LOWER CORNER WITH CRACK INDICATION AT SECOND LOWER HOLE ON BEAR STRAP APPROX. 10 O'CLOCK.(<P>CRACK WAS REPAIRED IAW EA 6753A937. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024112601115Shear Tie · corrodedBULK CARGO COMPARTMENT, STA 1480 BTW STGR 28R-29R FRAME WITH CORROSION(<P>SHEAR TIE WAS REPLACED IAW DWG 146T1519. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024112501114Skin · scratchedTRAFFIC ALERT & COLLISION AVOIDANCE SYS HEALTH CHECK, ON TCAS UPPER ANTENNA WITH SCRATCHES ON FUSELAGE SKIN(<P>THE TCAS UPPER ANTENNA DOUBLER WAS BLEND OUT AND INSPECTION WERE PERFORMED IAW TRE 6753708. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024112501113Web · corrodedAFT CARGO, BTW STA 1263 AND DOOR FRAME, BTW STRG 32R AND 32R, CORROSION ON WEB.(<P>CLIP P/N 146T8081-13 SMALL AUTHORIZATION IAW CONSECUTIVE NUMBER M675498 & SRM 51-40-02-0G-0. NO FURTHER DEFECTS NOTED.CORROSION REMOVED</P>)SDR UIEA2024112401111Frame · corrodedFRAME AT STA 1480 BETWEEN STGR 27R / 29R WITH CORROSION (BULK CARGO COMPARTMENT AREA)(<P>FRAME N/P 146T1519-3 WAS MANUFACTURED IN ACCORDANCE SMAL AUTHORIZATION BY BOEING MESSAGE CMA-TLS-24-0222-01B (MXA ENGINEERING TASK CARD M6753499 ISSUED DATE NOVEMBER 19, 2SDR UIEA2024112201104Shear Tie · corrodedBULK CARGO, FLOOR LEVEL AT FRAME 1540, SHEAR TIE WITH CORROSION BTW STRG 39R AND 38R.(<P>THE SHEAR TIE WITH CORROSION WAS REMOVED. THE AREA WAS CLEANED. THE NEW SHEAR TIE WAS DRILLED AND INSTALLED CORRECTLY IAW SRM 51-40-02-0G-0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024112201103Skin · crackedRH FWD DOOR, AFT LOWER CORNER WITH CRACK INDICATION AT THIRD HOLE ON SKIN APPROX 1 O'CLOCK, AND VISUAL CRACK (CONFIRMED WITH HFEC) AT FOURTH HOLE ON SKIN AND BEAR STRAP APPROX. 2 O'CLOCK AND CONTINUE TO APPROX 7 O'CLOCK.<BR>(<P> IT WAS REPAIRED IAW EA 6753A937SDR UIEA2024112201102Support Beam · corrodedBULK CARGO DOOR, INTERNAL STRUCTURE, CORROSION BTW BEAMS 2 AND 4.(<P>THE AREA WAS CLEANED, NEW SUPPORT WAS DRILLED, SUPPORT BEAM WAS INSTALLED. THE BEAM SUPPORT WAS REPLACED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024112201101Bearing · cokedENGINE 1, BEARING #5, LH/RH SUMP PIPES WITH LEAK EVIDENCE.(<P>DURING VISUAL EXAMINATION, OIL COKE BUILD-UP WAS FOUND, COKING WAS REMOVED AND NO OIL LEAK WAS FOUND IN LH/RH SUMP PIPES IAW AMM SUBTASK 72- 50-00-216-032-H00 REV. 143 DATE: 22 AUG 2024. C/W IDLE LESDR UIEA2024112201100Splice · corrodedBULK CARGO COMPARTMENT AT STA 1502 BTW STGR 31R-32R SPLICE WITH CORROSION.(<P>A NEW SPLICE WEB WAS MANUFACTURED AND INSTALLED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024112201099Skate Angle · crackedCRACK ON LH SKATE ANGLE ON STRUT #2 (FOUND DURING SEALANT REMOVAL)(<P>A SEGMENT OF THE SKATE WITH CRACK WAS REMOVED, AND THE NEW SEGMENT WAS MANUFACTURED AND INSTALLED IAW FVCI CONTROL EO 24190-2. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024112201098Frame · corrodedBULK CARGO COMPARTMENT AT STA 1480 BTW STGR 31R-32R FRAME WITH CORROSION(<P>FRAME WAS MANUFACTURED AND REPLACED WITH THE NEW ONE. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024111901096Skin · debondedRH WING, INBOARD AILERON, LEADING EDGE DISBONDED BTW RIB 1 AND 2.(<P>RH WING, INBOARD AILERON, L/E BETWEEN RIB 1 AND 2 WAS REPAIRED AS PER B767-300 SRM 57-60-01-2R-1 FIG. 201, SHEET 4, PAG. 1-10 AND B767-300 SRM 51-70-17-0G-0 PAR. 4G, FIG. 15, PAG. 16, 17,42. SDR UIEA2024051900395Light · brokenEMERGENCY EXIT LIGHT BY L1 BOOR BROKEN(<P>RESECURED EMERGRNCY EXIT SIGN LENSE IAW 33-51-01. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023071300756Hose · unknownO2 DISCHARGED COMPLETELY THROUGH FO'S REGULATOR IN MASSIVE AND SUDDEN LEAK(<P>FOUND FO'S OXYGEN MASK BOX CONNECTION HOSE BLOWN OFF AND MASSIVELY LEAKING. REMOVED AND REPLACED CONNECTION HOSE ASSY IAW AMM 20-11-00, OPS AND LEAK CHECHED GOOD IAW AMM 35-11-00. </SDR UIEA2023040300310Pimu · unknownRH PIMU FAULT MESSAGE.(<P>R/R RH PIMU & OPS CHECK OK PER AMM 77-35-02.</P>)SDR UIEA2023040300309Lead · unknownENG #1 LOWER HIGH TENSION LEAD DAMAGED.(<P>REMOVED & REPLACED ENG #1 LOWER HIGH TENSION LEAD IAW 767-300 AMM 74-21-02. PERFORMED AUDIBLE TEST FOR ENG #1, AUDIBLE TEST OK IAW AMM 74-00-00</P>)SDR UIEA2023040300308Unknown · unknownFWD E/E CREW OXYGEN NEED SERVICE TO FULL.(<P>SERVICED FWD E&E CREW OXYGEN AS PER B767 AMM CH 12-15-08, AC 43.18-1B PAR 9-46 THRU 9-51 PGS 9-448 THRU 9-455. OPS CHECK GOOD. NO LEAKS FOUND.</P> / <P>PN: 801307-00 SN ST298851 DUE DATE 31 JUL 25 MFG DATE 31 JAN 1SDR UIEA2023040300307Controller · unknownCABIN COMPT TEMP CONTROL SYS INOP.(<P>R/R CABIN COMPT TEMP CONTROLLER M195 & ZONE TEMP CONTR. 1 SYS. OPS TEST GOOD PER AMM 21-61-03. MDDR 182947 CLEARED UP</P>)SDR UIEA2023040300306Unknown · unknownECM 2023P-168 N1997A ENG #1 ESN #702928 IS EXPERIENCING HIGH FAN VIBRATION. A TRIM BALANCE IS REQUIRED TSLV 10,240 CSLV 3,348.(<P>PERFORMED LH ENG RUN UP PER AMM 71-00-00. INCREASED N2 POWER TO 99% & FAN VIB DID NOT EXCEED 0.9. NO DISCREPANCY NOTED. OPS CHECK SDR UIEA2022122701217Lamp · inoperativeEMERGENCY LIGHT AT L1 DOOR INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED NORMAL IAW AMM 33-51-00.SDR UIEA2022053100562Pca · leakingWITH LEFT AND CENTER HYD SYS DEPRESSURIZED LEFT INBOARD AILERON FLOATS UP DURING LEVEL FLIGHT RESULTING IN HARD LEFT ROLL. FOUND LEFT INBOARD AILERON INBOARD & OUTBOARD PCA'S LEAKING AT SCRAPPER SEALS. REMOVED AND REPLACED O/B PCA IAW B767 AMM 27-11-48. STEPS SDR UIEA2022053100561Pca · erraticAIRPLANE WAS HAVING PROBLEMS MAINTAINING VNAV PTH ON THE ARRIVAL ROUTE. AFTER DISCONNECTING AUTOPILOT I FELT HEAVY RESISTANCE WITH AILERON FLIGHT CONTROLS. BOTH LEFT AND RIGHT AILERON INPUT AT AIRSPEEDS ABOVE 200 KTS. AILERON TRIM SHOWED ZERO WITH LEVEL CONTROSDR UIEA2022042000350Transducer · noneSUPERNUMERARY O2 INDICATION IS ERRATIC(<P>TRANSFERRED TO MMDR 164289 IAW MEL 35-11-03-02A, CAT C.</P> / <P>LOGPAGE 1504123 - ITEM #4: REMOVED AND REPLACED PAX O2 TRANSDUCER PER AMM 35-11-04. THIS CLEARS MDDR 164289.</P>)SDR UIEA2022032800249None · noneCORROSION IN THE AFT CARGO COMPARTMENT HORIZONTAL ATTACH FITTING BETWEEN STR,23R AND STR.24R JUST AFT OF THE BS.1065 BULKHEAD. DOT 129-097(<P><SPAN>REMOVED AND REPLACE THE RH HORIZ. FITTING, 2EA. ATTACH BRACKETS AND 1 EA. WEB AT STA. 1065-1109 STR. 23R-24R IAWSDR UIEA2022040800268None · noneCORROSION AROUND FASTENER HOLE AND UNDER ROLLER TRAY IN THE AFT CARGO COMPARTMENT FLOOR BEAM UPPER CHORD LOWER SURFACE BS.1241 LBL.43.(<P>REMOVED, FABRICATED NEW, AND INSTALLED NEW <SPAN>AFT CARGO COMPARTMENT FLOOR BEAM UPPER CHORD AT STA 1241 IAW B767 SRM 53-SDR UIEA2022040800270Fitting · noneCORROSION IN THE AFT CARGO COMPARTMENT HORIZONTAL ATTACH FITTING BETWEEN STR,23L AND STR.24L JUST AFT OF THE BS.1065 BULKHEAD(<P>REMOVED AND REPLACED THE LH HORIZ. FITTING AT STA 1065-1109 STR. 23L-24L IAW B767 SRM 51-40-02. (CORROSION LEVEL 2)</P>)SDR UIEA2022041000279Fitting · noneRH PYLON OB SIDE AFT STA 280 APPROX LWR FITTING CRACKED AT LWR END.(<P>REMOVED AND REPLACED <SPAN>RH PYLON OB SIDE AFT LWR FITTING </SPAN><SPAN>STA 280 IAW B767 SRM 51-40-02, 51-40-05.</SPAN></P>)SDR UIEA2022041400306None · noneRH WING UPPER SIDE BODY SPLICE CENTER WING WBL.95 BTWN. 1, 2 STRINGERS U 10, U7 SKIN FOUND CORRODED AREA DOT 11/ 0013(<P>REMOVED CORROSION FROM RH WING UPPER SIDE BODY SPLICE CENTER WING WBL.95 BTWN. 1, 2 STRINGERS U 10, U7 SKIN. ORIGINAL MATERIAL .200" REMAINSDR UIEA2022041800312Bottle · low pressureCREW O2 LOW AT DEPARTURE CREW O2 READ 1600 ON ARRIVAL 1220(<P>REMOVED AND REPLACED CREW O2 BOTTLE IAW AMM 12-15-08 & LEAKED CHECKED OKAY PER GMM 3.25.3. NO DEFECTS NOTED AT THIS TIME . </P>)SDR UIEA2022012300073None · noneGEAR DISAGREE EICAS AFTER SELECTING GEAR DOWN. RAN QRH PROCEDURES(<P>ON WALK AROUND FOUND TAIL SKID RETRACTED. PERFORMED FIM 32-30 FT 305. ON PSEU BITE TEST FOUND MSG '248' TAIL SKID RETRACT. PERFORMED TAIL SKID EXTEND OPS TEST PER AMM 32-71-00-715-001 OPS GOOSDR UIEA2022010500006Switch · noneEMERGENCY LIGHT KORRY SWITCH INOP(<P>REMOVED AND REPLACED EMERGENCY LIGHT KORRY SWITCH IAW AMM 33-13-00. OPS TEST GOOD.</P>)SDR UIEA2021120502445Elevator System · failedELEVATOR NOT RETURNING TO CENTER POSITION WHEN DOING FLIGHT CONTROL CHECK.(<P>PERFORMED ELEVATOR POSITION INDICATING SYSTEM OPS TEST IAW AMM 27-38-00. OPS CHECK GOOD AT THIS TIME. AC OK FOR SERVICE.</P>)SDR UIEA2021110802362None · noneFWD EQPT VAL EICAS MSG MOMENTARILY APPEARED DURING ROTATION. REPEAT WRITE UP.(<P>REF ITEM M9 LP 1431441 FOR CORRECTIVE ACTION. EQ COOLING GROUND VALVE POSITION FROM N2 SPEED CARD PER AMM 21-58-00. PERFORMED VALVE OPERATIONAL CHECK IAW AMM 21-58-00 VALVE HEALTHSDR UIEA2021110802365None · noneL ENG SPEED CARD EICAS MSG.(<P>FOUND CANNON PLUG D4978P WITH BROKEN WIRE PIN 38 TO N2 SPEED CARD. RETERMINATED IAW SWPM 70-60-02 AND WDM77-12-12. PERFORMED IDLE RUN IAW AMM 7100-00 ALL OPS CHECK GOOD.</P>)SDR UIEA2021110502349None · noneDURING TAXI OUT CAPTS PFD & UPPER EICAS SCREENS WENT BLANK.(<P>CAPT'S ADI AND UPPER EICAS CAME BACK AFTER SHUTDOWN. SUPPLIED AIR FOR HOT/HUMID WEATHER CONDITIONS IAW B767AMM 21-00-00-862-068.</P>)SDR UIEA2021110802370None · noneL ENG SPEED CARD STATUS MSG REPEAT WRITE UP.(<P>R/R N2 SPEED CARD ON L/H ENG. FAULT CLEARED. FOUND CONNECTOR ON D10064 TO HAVE DAMAGED THREADED INSERTS CAUSING SPEED CARD NOT TO STAY SECURED. SEE LP 1440560 ITEM 6 FOR CORRECTION REF B767 73-21-54. N2 SPEED CARSDR UIEA2021110502351None · noneREPEAT WRITE UP LEFT ENG SPEED CARD STATUS MESSAGE AFTER ENG START(<P>PERFORMED ENG N2 SPEED CARD TEST AS PER B767 AMM TASK 73-21-54-705-005-H00 TEST OK.</P>)SDR UIEA2021110402347None · noneL ENG SPEED CARD STATUS MESSAGE AFTER START ...REPEAT WRITE UP(<P>PERFORMED FIM 73-21 TASK TT#871 BLOCK #21 FOUND L END SPEED CARD DISPLAYED. REMOVED/REPLACED M1083 N2 SPEED CARD, PERFORMED ADJUSTMENT/TEST IAW AMM 73-21-54-705-005-H00, MESSAGE CLEARED OPS TESTSDR UIEA2021110402344None · noneL. ENG SPEED CARD STATUS MESSAGE AFTER START(<P><SPAN>T/S PER B767 AMM 73-21-54-705-005-HOO AND B767 FIM 73-21 FAULT TREE 871. TEST PASSED NORMAL. MESSAGE CLEARED. COULD NOT DUPLICATE ON GROUND AT THIS TIME. MCC ADVISED</SPAN></P>)SDR UIEA2021110302331None · noneLEFT / #1 ENGINE "VIB" INDICATION BETWEEN 1 AND 4 ON STATUS PAGE DURING DEPARTURE. FLUCTUATIONS WERE ALSO SLIGHTLY FELT.(<P>RAN #1 ENGINE HIGH POWER RUN VIBRATION SURVEY PER B767 AMM 71-00-00-735-370-H03. AT IDLE. VIBE 0.7, EGT 319, FF 1.3 AT MAX POWER SETTINGSDR UIEA2021100202163Radome · damagedBIRD STRIKE ON RADOME. INSPECTED NOSE RADOME FOUND DAMAGE ON THE EXTERNAL SIDE SURFACE WAS OUT OF LIMITS IAW AMM 05-51-18 & SRM 53-10-72.LP 1401419, ITEM M6: REMOVED AND REPLACED NOSE RADOME IAW AMM 53-12-01, ADJUSTED AND SAFETIED NOSE RADOME IAW AMM 53-12-01-SDR UIEA2021082501877Valve · faultedAPU PNEUMATICS INOP ( AUXILIARY POWER UNIT, PNEUMATIC FUNCTION )(<P>TRANSCRIBED TO MEL LIST MDDR 152437 DMI # 49-11-01-01 DUE 03SEP21, CAT C. MAINT ACTIONS C/W PER 152437. PLACARDS APPLIED.</P> / <P>25AUG21 - 1397821 - ITEM# 5 - CVG - REMOVED FLOW SENSING MODUSDR UIEA2021082401862Control Valve · faultedAFT CABIN COMPARTMENT SHOWS 7D EVENT THOUGH AFT CABIN TEMPERATURE CONTROLLER IS SET TO WARM DURING CRUISE FLIGHT(<P>PERFORMED BITE CHECK ON DECK SYSTEM IAW FIM. REMOVED AND REPLACED LEFT PACK TEMP CTRL VALVE IAW AMM 21-51-12. OPS CK GOOD AT THIS TIME.</P>)
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