N16301, cancelled Mar 21, 2013
Service difficulty reports · 89
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 = 'N16301' AND deregistration_id = 'N16301-2013-03-21' 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 = 'N16301' AND deregistration_id = 'N16301-2013-03-21' 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 CALA0800546Megaphone · defectiveA/C MEGAPHONE MISSING VOLUME KNOB AND LOW IN VOLUME. REPLACED MEGAPHONE, OPS CHECK GOOD.SDR CALA0800139Skin · crackedSTA 747 ABOVE STRINGER 24 FOUND 1.8" LONG CRACK WHILE PERFORMING C-SCAN INSPECTION. REPAIRED FUSELAGE PER SRM 53-00-01 REPAIR 31 DETAIL X.SDR CALA0700702Skin · crackedFUSE SKIN CRACK INDICATION RT SIDE 39 INCHES AFT OF AFT BIN DOOR FRAME & 30 INCHES ABOVE LAP SEAM. COMPLETED SKIN REPAIR 31 PER SRM 53-00-01 AND REPAIR DEVIATION PER ECRA 5331-01365.SDR CALA0700699Skin · crackedCRACK IN FUSELAGE SKIN 10 INCHES ABOVE LAP JOINT AND 11 INCHES AFT OF AFT UPPER BODY FAIRING RIGHT SIDE AT STATION 727A AND STRINGER S-19R. REPAIRED FUSELAGE SKIN PER SRM 53-00-01.SDR CALA0700564Reflector · contaminatedTHE L-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE EMERGENCY LIGHT REFLECTOR ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-02 AND 33-51-11.SDR CALA0700443Frame · corrodedINSPECTION FOUND FORWARD CORROSION AT ACCESS DOOR AFT FRAME IN BULKHEAD CHORD, BS 227.8 BETWEEN LBL 5.7 AND RBL 5.7. REPAIRED IAW ECRA 5311-01353.SDR CALA0700115Drag Angle · crackedLEFT UPPER WING TO BODY DRAG ANGLE CRACKED FWD OF A/C DOOR 3302L. REPAIRED IAW ECRA 5311-01300.SDR CALA0700114Frame · crackedLEFT MAIN FRAME CRACKED AT STA 639. REPAIRED IAW ECRA 5311-01299.SDR CALA0700113Web · crackedCRACKED AT WEB STA 639 ABOVE FLOOR LINE. REPAIRED IAW ECRA 5311-01299.SDR CALA0700116Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN UPPER RADIUS OF FITTING AFT OF FRAME JUST BELOW STRINGER 17L AND CREASE BEAM AT STA 616. A NEW FITTING WAS INSTALLED IAW SRM 51-10-2 AND 51-40-02.SDR CALA0700103Beam · crackedCRACKED L1 DOOR AFT SIDE OF THE THIRD FROM BOTTOM DOOR STOP CUTOUT. REPAIRED IAW ECRA 5210-01919.SDR CALA0700102Skin · crackedA 2 INCH CRACK IN R1 DOOR AT THE LOWER BOTTOM CORNER. REPAIRED IAW ECRA 5331-01291.SDR CALA0700101Skin · crackedA 3 INCH CRACK LOWER AFT FUSELAGE STA 727D AND 727E. REPAIRED IAW ECRA5331-01292.SDR CALA0700100Frame · crackedAFT CARGO COMPARTMENT CRACKED ON FWD BULKHEAD FRAME. INSTALLED STIFFENER IAW SRM 51-10-02, 51-30-01, AND 51-40-02.SDR CALA0700096Frame · corrodedAFT CARGO FLOOR FRAME AT STA 747 IS CORRODED FROM STR 26L TO 26R. REPAIRED IAW SRM 53-00-07 DETAIL 2, 51-40-02 & 51-10-02.SDR CALA0700094Keelbeam · damagedLOWER FUSE SKIN BULGED BETWEEN RIVETS ALONG STRINGER 28R STA 500C TO 500D. REPAIRED KEEL BEAM IAW SRM 53-60-12.SDR CALA0700093Keelbeam · corrodedAFT CARGO COMPARTMENT CORRODED AT KEEL BEAM STA 727, LBL 6. REPAIRED IAW ECRA 5311-01293 AND 5311-01296.SDR CALA0700092Pan · crackedC2 DOOR FWD SIDE PAN CRACKED AT SPLICE POINT. INSTALLED NEW PAN IAW SRM 52-30-02.SDR CALA0700091Pan · crackedUPPER FWD PAN CRACKED AT FWD SPLICE. INSTALLED SERVICEABLE PAN.SDR CALA0700089Bulkhead · corrodedFWD APB LOWER CENTER SECTION WEB CORRODED. REPAIRED IAW ECRA 5311-01298.SDR CALA0700088Structure · bulgedFWD BAG BIN BULGED ALONG S28L FROM STA 500D 6 INCHES. REPAIRED IAW SRM 53-30-12.SDR CALA0700090Support Angle · crackedSUPPORT ANGLE CRACKED AT 360 AND STRINGER S11L. REPAIRED IAW ECRA 5311-01297.SDR CALA0700083Frame · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT FLOOR FRAME CORRODED AT STA 847 BETWEEN STRINGERS 27L AND 27R, LBL 8 TO RBL 8. THE CORRODED SECTION OF FLOOR FRAME WAS REMOVED AT FLOOR FRAME ATTACH AND A SHEAR TIE REPAIR WAS INSTALLED IAW SRM 53-00-07.SDR CALA0700082Stringer · corrodedINSPECTION FOUND LIGHT SURFACE CORROSION DOWN CENTER OF STRINGER 26L IN FORWARD BAGGAGE BIN AT STA 500D-520. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.SDR CALA0700081Skin · crackedINSPECTION FOUND A 0.75 INCH CRACK IN FUSELAGE SKIN AT R-2 DOOR FORWARD LOWER RADIUS, STA 947.5, S14R. A DOUBLER WAS INSTALLED IAW SRM 53-60-01, FIGURE 201.SDR CALA0700075Frame · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT CENTER FLOOR AREA, STA 867, S28L TO S28R. THE CORRODED SECTION OF FRAME WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 201.SDR CALA0700067Stiffener · corrodedINSPECTION FOUND TWO CHANNEL STIFFENERS CORRODED ON FORWARD FACE OF APB LOWER SECTION. THE STIFFENERS WERE REMOVED AND NEW SECTIONS WERE SPLICED IN IAW BOEING DRAWING 65C28106.SDR CALA0700066Stringer · corrodedINSPECTION FOUND CENTER OF STRINGER 27L CORRODED AROUND NUT PLATE IN FORWARD BAGGAGE BIN AT STA 500D. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.SDR CALA0700062Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 947, RBL 6 TO LBL 6. A FLOORBEAM REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 201.SDR CALA0700061Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN RT MAIN FRAME AT STA 616 BELOW FLOOR LINE. THE CRACKED AREA OF FRAME WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED IAW ECRA 5311-01158.SDR CALA0700060Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT NUT PLATES ON TOP AND BOTTOM, STA 1016, LBL 6 TO LBL 34. THE FLOORBEAM CHORD WAS REMOVED AND REPLACED IAW ECRA 5310-03851.SDR CALA0700059Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN LT FRAME AT STA 616, S17L TO S18L BELOW FLOOR LINE. THE CRACKED AREA OF FRAME WAS REMOVED AND A REPAIR ANGLE AND FILLER WAS INSTALLED IAW ECRA 5311-01158.SDR CALA0700054Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FRAME AT STA 597, S13L. THE FRAME WAS REPAIRED IAW SRM 53-00-07, PAGE 203, FIGURE 201.SDR CALA0600511Skin · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 727A-727B, S22R TO S25R. REPAIRED IAW ECRA 5331-01283.SDR CALA0600225Frame · corrodedINSPECTION FOUND AFT CARGO DOOR FORWARD FRAME CORRODED. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-80-02.SDR CALA0500132Panel · crackedFUSELAGE SKIN CRACKED AT STA 727D, STRINGER 23R. REPLACED PANEL PER ECRA 5331-01178A.SDR CALA0500076Skin · crackedINSPECTION FOUND A 1.7 INCH CRACK IN FUSELAGE SKIN THREE INCHES AFT OF STA 727D JUST BELOW S23R ON BONDED DOUBLER LINE. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5331-01178.SDR CALA0500066Stiffener · crackedINSPECTION FOUND 8 INCH CRACK IN STIFFENER FOR NR 3 VHF ANTENNA BETWEEN STA 727D AND 727E. A NEW STIFFENER WAS INSTALLED IAW SRM 51-40-2.SDR CALA0300165Skin · crackedINSPECTION FOUND A 0.4 INCH CRACK IN SKIN AT UPPER FORWARD CORNER OF PILOT'S WINDOW CD POST AT BS 205, WL 238. REPAIRED IAW SRM 53-10-01, FIGURE 210.SDR CALA0300164Floorbeam · corrodedINSPECTION FOUND TOP SURFACE OF TOP CAP OF LATERAL FLOORBEAM AT STA 1016 CORRODED AT LT SIDE AREA UNDER LAV TANK. REPAIRED IAW ECRA 5310-03851.SDR CALA0300163Skin · dentedINSPECTION FOUND R-2 DOOR EXTERNAL SKIN DENTED AT FORWARD LOWER CORNER. REPAIRED IAW SRM 52-00-01.SDR CALA0300162Bulkhead · crackedINSPECTION FOUND TWO 0.1 INCH CRACKS AT RIVET HOLES IN AFT PRESSURE BULKHEAD BETWEEN S6L AND S7L AT BS 1016. REPAIRED IAW SRM 53-80-08, FIGURE 202 AND 207.SDR CALA0300161Stringer · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT STRINGER 26R CORRODED AT BS 1010. REPAIRED IAW SRM 51-40-02 AND B737-300 AMM 20-50-11.SDR CALA0300157Frame · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT LOWER LOBE INTERIOR FRAME CORRODED AT BS 847 BETWEEN S28L AND S28R. REPAIRED IAW SRM 53-00-07, FIGURE 208.SDR CALA0300156Floorbeam · corrodedINSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 312 AND 320, R-1 DOOR THRESHOLD. REPAIRED WITH REPLACEMENT PART IAW SRM 51-40-02.SDR CALA0300155Skin · tornINSPECTION FOUND FORWARD CARGO DOOR SKIN CUTOUT TORN AT BS 440, S24R. THE SKIN WAS REPAIRED IAW ECRA 5330-03222.SDR CALA0300154Skin · gougedINSPECTION FOUND LT HORIZONTAL STABILIZER LEADING EDGE SKIN GOUGED AT STA 176.50. REPAIRED IAW ECRA 5515-01008.SDR CALA0300153Skin · dentedINSPECTION FOUND VERTICAL STABILIZER LEADING EDGE SKIN DENTED AT L/E STA 132.92 + 6 AND AT 226.54 + 1.3. THE DENTED AREAS WERE REPAIRED IAW SRM 55-30-01, FIGURE 203.SDR CALA0300152Stringer · puncturedINSPECTION FOUND STRINGER 24R PUNCTURED AT BS 363. REPAIRED IAW SRM 53-00-03, FIGURE 201.SDR CALA0300151Stringer · corrodedINSPECTION FOUND STRINGER 25R CORRODED AT BS 364 AND S24R WAS CORRODED AT BS 360. REPAIRED IAW SRM 53-00-03, FIGURE 201.
Back to N16301, cancelled Mar 21, 2013