N77261
Service difficulty reports · 90
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 = 'N77261' 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 = 'N77261' 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 CALA2022022100469Pressure Deck · crackedINSPECTION (HFEC) OF THE CENTER WING BOX REAR SPAR VERTICAL PRESSURE DECK, SHOWS A CRACKBETWEEN LBL. 40.00 AND LBL. 31.83 INSPECTION. INITIAL INSPECTION THRESHOLD 56,000 FLIGHT CYCLES THEREAFTER 36,000 FLIGHT CYCLES PER TABLE 204 AFTER INSTALLATION. HFEC / LFESDR CALA2022022100451Frame · dentedAFT CARGO COMPARTMENT FRAME 727G @ STR23R FOUND DENTED AND REPAI RED ON FLEETCYCLE NR 9801935 PER ECRA 5311-02757. REQUIRES DIP TO ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF EC/RA 5311- 0275 ON OR BEFORE 75,000 TOTAL FLIGHT CYCLES. PLACE ON DIP TO ACCOMPSDR CALA2022021800425Frame · dentedREF FLEET CYCLE N/R 9801933 AFT PIT FRAME 727 J STRINGER 23R - 24R FRAME HAS DENT TO BE DETERMINED BY ENGENEERING REPAIR TO BE DETERMINED BY ENGENEERINGSDR CALA2022021800418Frame · dentedAFT CARGO PIT FRAME 727E STRINGER 21L FRAME HAS DENT. FLIGHT CYCLES,PART 2 ? INSPECTION REQUIREMENTS 1. TO BE THRESHOLD.PART 3 PERMANENT REPAIR1. THE REPAIR ACCOMPLISHED REPETITIVE INSPECTION REQUIRMENTS (RIR). THERE IS NO TERMINATING DETERMINED BY ENGINEERINGSDR CALA2022021800417Frame · dentedAFT PIT FRAME 727C BETWEEN STRINGERS 22L AND 23L FRAME HAS DENT. 2024" PERFORMED INTERIM REPAIR PER ECRA 5311-02755 INITIATE A DTA DIP TO READ "ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE FEB 14 , VERIFIED DIP REQUIREMENTS.SDR CALA2022020700327Pressure Blkhd · crackedINSPECTION (HFEC) OF THE CENTER WING BOX REAR SPAR VERTICAL PRESSURE DECK, SHOWS A CRACKBETWEEN LBL. 40.00 AND LBL. 31.83SDR CALA2021122202424Frame · crackedAVO9353 REV-A STEP B1-4 HFEC ACCOMPLISHED , L1 CRACK FOUND ( CRACK CONDITION #1 ) FIG12.1 FIG A. NO CRACK ON OUTER SURFACE, JUST ON WINDOW FRAME INNER EDGE AND ON THE INSIDE SURFACE OF FRAME, SEE ATTACHED PICTURE. VERIFIED FRAME SEPARATED AND CRACK CUT OUT REFSDR CALA2021122202423Frame · crackedAVO9353 REV-A STEP B1-4 HFEC ACCOMPLISHED , R1 CRACK FOUND ( CRACK CONDITION #1 )FIG. 13.1 FIG A 5/8" IN LENGTH, SEE ATTACHED PHOTO. VERIFIED FRAME SEPARATED AND CRACK CUT OUT REF AVO STEPS A&B. VERIFIED HARDWARE INSTALLATION AND SLIDING WINDOW OPERATION PER VSDR CALA2021122002419Frame · crackedAVO9353 REV-A STEP B1-4 HFEC ACCOMPLISHED , R1 CRACK FOUND ( CRACK CONDITION #1 )FIG. 13.1 FIG A 5/8" IN LENGTH, SEE ATTACHED PHOTO. VERIFIED FRAME SEPARATED AND CRACK CUT OUT REF AVO STEPS A&B. VERIFIED HARDWARE INSTALLATION AND SLIDING WINDOW OPERATION PER VSDR CALA2021122002418Frame · crackedAVO9353 REV-A STEP B1-4 HFEC ACCOMPLISHED , L1 CRACK FOUND ( CRACK CONDITION #1 ) FIG12.1 FIG A. NO CRACK ON OUTER SURFACE, JUST ON WINDOW FRAME INNER EDGE AND ON THE INSIDE SURFACE OF FRAME, SEE ATTACHED PICTURE. VERIFIED FRAME SEPARATED AND CRACK CUT OUT REFSDR CALA2019030800374Connector · shortedHF 1 RADIO TRANSMISSION PROBLEM AT ALL STATIONS UNABLE TO XMIT RCVD LONG TUNING TONE THEN NOTHING CAN RCV VOICE/ SELCAL TOMC APPROVES BOTH HF''S ON MEL 2311E DISPATCH DESK: 59 DATE: 05-MAR-19- OC DESK: 737 DATE: 05-MAR-19- DEFERRED DIRECTLY BY TOMC REMOVED & RSDR CALA2019020100198Skin · crackedRH HORIZONTAL STABILIZER SKIN AT STAB STATION 140, 24" AFT OF FRONT STAB I/B FASTENER ROW OPPOSITE OF DRAIN HOLE 1" CRACK BETW EEN FASTNERS(MARKED). FOUND ON SMB C-CHECK WRITE UP 9646070. REP AIR PER SRM 55-10-01 REPAIR 11. RH LOWER HORZ. STAB CRACK REPAIRED PSDR CALA2017102303746Unknown · odorSHORTLY AFTER RESETTING IFE POWER, F/A REPORTED SMELL OF ELEC SMOKE R23 -24. LASTED ABOUT 3 MINUTES. PERFORMED ELECTRICAL ODOR SYSTEM INTEGRITY CHECK IAW AMM 44-20-3 6. COULD NOT DETECT ANY SMELLS AND FOUND NO DAMAGED ELECTRICAL COMPONENTS OR WIRES, OPS CHK GOSDR CALA2017051201402Cover · missingEMERG EXIT SIGN MISSING LITTLE ONE DOWN LOW. INSTALLED MISSING COVER AND OPS CKS OK.SDR CALA2017010100005Battery Pack · dischargedEMERGENCY LIGHTS INOP ABOVE RIGHT SIDE EXIT ROWS. R&R EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD.SDR CALA2016090900644Bulkhead Web · crackedTHERE IS A .50 CRACK IN THE REAR SPAR VERTICAL PRESSURE WEB AT WL 195.6 AND RBL 41.5. REPAIRED IAW SRM 57-10-10 REP 3 ALT 2.SDR CALA2016082400572Frame · dentedFWD CARGO BAY FUSELAGE FRAME AT BS 500D STRINGER 25L HAS A DENT ON INNER STRUCTURE. REPAIRED IAW EC/RA53 10-06786.SDR CALA2016061500364Door Frame · corrodedFWD LOWER SIDE F/O R2 DOOR CUTOUT, BS 952, FRAME AND WEB HAVE CORROSION. FRAME REPAIRED IAW EC/RA5310-06785. WEB REPLACED.SDR CALA2016030300141Skin · crackedLEFT HORIZONTAL STAB CRACK AT STATION 138.70, 19" FWD OF AFT SPAR. REPAIRED IAW SRM 55-10-01 REPAIR 11.SDR CALA2016030300140Skin · crackedLEFT HORIZONTAL STAB CRACKED AT STATION 138.70, 8" AFT OF FWD SPAR. REPAIRED IAW SRM 55-10-0 REPAIR 11.SDR CALA2016030300139Skin · crackedLEFT HORIZONTAL STAB FOUND A CRACK AT STATION 129.50, 6" AFT OF REAR SPAR. REPAIRED IAW SRM 55-10-01 REPAIR 11. INITIATED A DIP TO PERFORM INSPECTION IAW SRM 55-10-01 REPAIR 11 STEP 5 TABLE 204.SDR CALA2016010400002Sign · missingROW 21DEF MISSING EXIT SIGN. REPLACED EXIT LIGHT MODULE. OPERATIONS CHECKED GOOD AMM 33-51-01.SDR CALA2015091400754Display · failedCAPTAINS INBD DU FAILED. REPLACED CAPTAINS INBD DU IAW MM 31-62-11. ACCOMPLISHED OPERATIONS TEST IAW MM 31-62-00-210-801. OPERATES NORMAL.SDR CALA2015033000211Wire · chafedFOUND WIRE NUMBER W9002-001-FDD20 CHAFED AT FRAME STATION 259. INSTALLED SPLICE PN D435 ON WIRE W9002-001-FDD20 BETWEEN CONNECTORS D11128P & D11130P AT STATION 259 BEHIND PANEL 113AC NOSE WW IAW B737NG SWPM 20-30-12 AND PERFORMED OPERATIONS CHECKED N ENHANCEDSDR CALA2015032500206Seat Track · crackedSEAT TRACK FLANGE AT LBL 45.50 HAS CRACK ON RT SIDE FWD HOLE. DISCREPANCY CIRCLED ON FLANGE WITH INDELIBLE MARKER. REPAIRED SEAT TRACK FLANGE AT STATION 727B & LBL 45.50 IAW ECRA 5320-02441 REV ORIGINAL.SDR CALA2015032500205Seat Track · crackedSEAT TRACK FLANGE AT 45.50 RBL HAS CRACK ON LT SIDE AFT HOLE. DISCREPANCY MARKED ON FLANGE BY INDELIBLE MARKER WITH CIRCLE. REPAIRED SEAT TRACK FLANGE AT STATION 727B & RBL 45.50 IAW ECRA 5320-02441REV ORIGINAL.SDR CALA2015031300163Wire · brokenW9665-900-22-CAL BROKEN AT STATION 394 BEHIND E2-1 SHELF IN FWD CARGO. REPAIR BROKEN WIRE W9665-900-22-CAL WITH A SPLICE AT STATION 394, LBL 53 & WL 202 IAW SWPM 20-30-12 & WDM 23-30-12. OPERATIONS CHECK WILL BE PERFORMED ON EA 2525-01562 REV A OPS 10 STEP 3SDR CALA2014031000300Bracket · looseA/C WOULD NOT PRESSURIZE AFTER TAKEOFF, FOUND FWD ENTRY DOOR L1 PARTIALLY GAPPED. FOUND GUIDE ARM BRACKET LOOSE, TIGHTENED & CHECKED RIG OF DOOR IAW AMM 52-11-00- 820-801.SDR CALA2011050400342Bulkhead · canningAFT PRESSURE BULKHEAD OIL CANNED BETWEEN STR 7 LT AND BL 0 INSTALLED REPAIR PER ECRA 5311-01526 PART 1 NEED TO REINSPECT PER ECRA 5311-01526 PART 2 BEFORE THE ACCUMULATION OF 46734 TOTAL A/C FLT CYCLES PLANNING TO CONTACT ENGINEERING AFTER 42000 FLT CYCLES BUTSDR CALA2011042800322Floorbeam · corrodedFLOORBEAM STA 328 UPPER SURFACE AREA HAS CORROSION AT RBL 10 FWD FLANGE. REPAIRED FLOORBEAM PER SRM 53-00-51 FIG 203 PAGE 208. SHIMMED PANEL BREAK AT RBL 11 STA 312 TO 328 PER ECRA 5321-01756.SDR CALA2011042800321Skin · crackedLT HORIZ STAB LOWER SKIN CRACKED STA 129.5 AND 17.5 IN FROM FRONT SPAR EA 5510-01843 OP 01. REPAIRED CRACK PER SRM 55-10-01 REPAIR 11.SDR CALA2011042800320Skin · crackedLT HORIZ STAB LOWER SKIN HAS A CRACK AT STA 129.5 AND 25.5 IN FROM FRONT SPAR. EA 5510-01843 OP 01 REPAIRED CRACK PER SRM 55-10-01 REPAIR 11.SDR CALA2011042800319Floorbeam · corrodedFLOORBEAM STA 328 UPPER SURFACE AREA HAS CORROSION AT LBL 11 TRIMMED UPPER FLANGE OF FLOORBEAM AND INSTALLED REPAIR DOUBLERS AND FILLER PER SRM 53-00-51 FIG 203. SHIMMED PANEL BREAK AT LBL 11 PER ECRA 5321-01755.SDR CALA2011042600308Skin · gougedE&E DOOR EXTERIOR SKIN GOUGED APPROX 6 INCHES FROM R/T AFT EDGE. REPAIRED EXTERIOR SKIN PER SRM 52-00-01.SDR CALA2011041900298Floorbeam · corrodedFLOORBEAM STA 986.5 AND RBL 42 HAS CORROSION AT FASTENER HOLE. INSTALLED REPAIR ANGLES PER EC/RA 5321-01429 REV B.SDR CALA2011041800296Floorbeam · corrodedFLOORBEAM STA 986.5 AND RBL 28 HAS CORROSION AT FASTNER HOLE. INSTALLED REPAIR ANGLES PER ECRA 5321-01429.
SDR CALA2011041800295Frame · crackedSUPPORT TASK - PAX CABIN HAS CRACKS ON NR 727B FRAME BETWEEN STR 8R AND 9R. REPAIRED FRAME AT STA 727 B BETWEEN STR 8 R AND 9 R REF EA 5310-04716 REV C.SDR CALA2011041800294Frame · crackedSUPPORT TASK - PAX CABIN HAS CRACKS ON FRAME NR 440 BETWEEN STR 8R AND 9R. REPAIRED FRAME PER EA 5310-04716 REV-C.SDR CALA2011041800293Frame · crackedSUPPORT TASK PZX CABIN HAS CRACKED 380 FRAME BETWEEN STR 8R & 9R. REPAIRED FRAME PER EA 5310-04716 REV C.SDR CALA2009113000696Battery Pack · dischargedEMERGENCY LIGHTS ARE INOP IN AFT CABIN SEATS. REMOVED AND REPLACED BATTERY PACK ASSY M1672 PER AMM 33-51-06, AC OK TO CONTINUE.
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