N770AT, cancelled Oct 31, 2017
Service difficulty reports · 78
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 = 'N770AT' AND deregistration_id = 'N770AT-2017-10-31' 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 = 'N770AT' AND deregistration_id = 'N770AT-2017-10-31' 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 DHLA2009770AT526Frame · wornEMPENNAGE VERTICAL STABILIZER ACTUATOR RT ACCESS PANEL FRAME "T" SHAPE SUPPORT WORN AND LOOSE. REPAIRED VERTICAL STABILIZER MID SPAR CHORD RIGHT SIDE FROM FIN STA 222 TO FIN STA 235 IAW B727 SRM 55-30-6 FIG 3SDR DHLA2009770AT521Stringer · corrodedLWR FUSELAGE FWD CARGO COMPARTMENT S-28R WITH CORROSION AT BS 488. REPAIRED S-28R SECTION BETWEEN BS 480 TO BS 516.5 IAW SRM 53-10-3 FIG 1. REPLACED S-28R SECTION FROM BS 450 TO BS 480 IAW SRM 51-10-1 PARA 7A AND 53-10-3 FIG 1.SDR DHLA2009770AT517Support Channel · corrodedREF N/R 1-306 LOWER FUSELAGE INTERIOR FWD NOSE COMPARTMENT, LOWER CHORD AND SUPPORT CHANNEL WITH CORROSION AT BS 227.8 LBL2. REPAIRED FUSELAGE FWD NOSE COMPT LOWER CHORD SECTION AT BS 227.8 BTWN LBL 5.5 AND RBL 6 IAW SRM 51-40-4 FIG 1.SDR DHLA2009770AT508Frame · dentedUPPER FUSELAGE CARGO CABIN FRAME WITH DENT AT BS 580 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION BS 580 BTWN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1.SDR DHLA2009770AT524Skin Panel · corrodedLOWER FUSELAGE FWD CARGO COMPARTMENT SKIN WITH CORROSION FROM BS 486 TO BS 494 BETWEEN S-27R AND S28R. REPAIRED FUSELAGE SKIN SECTION FROM BS 481 TO BS 496.5 BETWEEN BL 0 AND S27R IAW EO-COO-2-53-500-08 DTD 12/23/08 DOCUMENTED OF FAA FORM 8110-3. DTA WITHIN SDR DHLA2009770AT520Seat Track · corrodedUPPER FUSELAGE MAIN CARGO CABIN SEAT TRACK WITH CORROSION FROM BS 480 TO BS 620 RBL 45.5 OTBD FLANGE. REPLACED SEAT TRACK FROM BS 480 TO BS 690 RBL 45.5 IAW SRM 51-10-1 PARA 7A AND IAW RIGID BARRIER INSTALLATION PARA 5.4.SDR DHLA2009770AT510Frame · dentedUPPER FUSELAGE CARGO CABIN FRAME WITH DENT AT BS 640 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION BS 640 BETWEEN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1.SDR DHLA2009770AT504Frame · dentedUPPER FUSELAGE CARGO CABIN FRAME WITH DENT AT BS 520 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION AT BS 520 BTWN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1.SDR DHLA2009770503Frame · dentedUPPER FUSELAGE CARGO CABIN FRAME WITH DENT AT BS 540 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION BS 540 BETWEEN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1.SDR DHLA2009770502Frame · dentedUPPER FUSELAGE CARGO CABIN FRAME WITH DENT BS 600 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION BS 600 BETWEEN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1.SDR DHLA2009770AT514Floorbeam · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 1130 RBL 45 FLOORBEAM LOWER FWD FLANGE WITH CORROSION. REPAIRED FUSELAGE FLOORBEAM LOWER CHORD SECTION BS 1130 BETWEEN RBL 20 AND RBL 56.5 IAW B727 SRM 53-10-8 FIG 10 DETAIL V.SDR DHLA2009770AT523Frame · crackedLWR FUSELAGE FWD CARGO COMPARTMENT DOOR CUTOUT BS 560 AT STOP FITTING NR 1 WEB WITH CRACK. REPAIRED FRAME WEB SECTION AT BS 560 BETWEEN S-17R AND S-22R IAW SRM 51-40-2 FIG 1.SDR DHLA2009770AT522Frame · crackedLWR FUSELAGE FWD CARGO COMPARTMENT DOOR CUTOUT BS 620 AT STOP FITTING NR 1 WEB WITH CRACK. REPAIRED FUSELAGE FRAME WEB SECTION AT BS 620 BETWEEN S-18R AND S-22R IAW B727 SRM 51-40-2 FIG 1.SDR DHLA2009770AT516Stringer · corrodedREF N/R 1-279 LWR FUSELAGE AFT CARGO COMPARTMENT AT BS 1010 S-29R WITH CORROSION. REPAIRED FUSELAGE S-29R SECTION FROM BS 1010 TO BS 1045 IAW SRM 53-10-3 FIG 1 DETAIL 1.SDR DHLA2009770AT507Stringer · corrodedLOWER FUSELAGE FWD CARGO COMPARTMENT BS 727E STRINGER END S-27R CORRODED. REPAIRED FUSELAGE S-27R SECTION FROM BS 727E TO BS 740 IAW B727 SRM 53-10-3 FIG 1 DETAIL 1.SDR DHLA2009770AT506Web · dentedLOWER FUSELAGE NOSE W/W WEB DENTED AT BS 323 WL 181 BL 0. REPAIRED NOSE W/W WEB FROM BS 320 TO BS 325.5 BETWEEN LBL4 AND RBL 5 IAW B727 SRM 51-40-2 FIG 1.SDR DHLA2009770AT512Shear Tie · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT BS 1050 BETWEEN S-26L AND S-27L SHEARTIE WITH CORROSION. REPLACED FUSELAGE SHEARTIE SECTION AT BS 1050 BETWEEN S-26L AND S-27L.SDR DHLA2009770AT509Strap · crackedLOWER FUSELAGE STABILIZER STRAP WITH CRACK AT BS 344 LBL 23 WL 201. REPAIRED STABILIZER STRAP FROM BS 324.5 TO BS 347.5 AT LBL 23 IAW B727 SRM 53-10-8 FIG 6.SDR DHLA2009770AT505Frame · damagedUPPER FUSELAGE CARGO CABIN FRAME WITH DOUBLE HOLE AT BS 1090 BETWEEN S-16L AND S-17L. REPAIRED FUSELAGE FRAME SECTION AT BS 1090 BETWEEN S-16L AND S-17L IAW B727 SRM 51-40-3 FIG 1.SDR DHLA2009770AT501Failsafe · corrodedUPPER FUSELAGE CARGO CABIN FRAME FAIL SAFE CHORD WITH CORROSION AT BS 1166 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME FAIL SAFE CHORD SECTION AT BS 1166 BETWEEN S-16R AND S-18R DUE TO CORROSION IAW B727 SRM 51-40-3 FIG 1.SDR DHLA2009770AT530Keelbeam · crackedLOWER FUSELAGE AIR CONDITIONING BAY AT BS 740 KEEL BEAM LOWER LEFT CHORD WITH CRACK. REPAIRED FUSELAGE LEFT SIDE KEEL BEAM LOWER CHORD AT HORIZONTAL FLANGE SECTION FROM BS 740 TO BS 748 LBL 7 IAW COOPESA EO-COO-2-53-503-08 DTD 12/24/08 AND BOEING MESSAGE 1-11SDR DHLA 2009770AT527Skin Panel · crackedRIGHT WING FRONT SPAR SECTION LEADING EDGE SKIN CRACKED AT WS 491. REPAIRED RIGHT WING FIXED LEADING EDGE SKIN SECTION FROM LE STA 151.40 TO LE STA 195.65 IAW COOPESA EO COO-2-57-461-08 DTD 12/19/08.SDR DHLA2009770AT513Floorbeam · corrodedUPPER FUSELAGE CARGO CABIN AT BS 1130 BETWEEN RBL 25 AND RBL 45 FLOORBEAM UPPER AND LOWER FACE WITH CORROSION. REPAIRED FUSELAGE FLOORBEAM UPPER CHORD SECTION AT BS 1130 BETWEEN RBL 37 AND RBL 47.5 IAW B727 SRM 53-10-8 FIG 10.SDR DHLA2009770AT529Frame · corrodedLOWER FUSELAGE AT BS 740 BTWN S-27L AND S-28L FRAME WITH CORROSION. REPLACED FUSELAGE CHORD SECTION AT BS 740 BTWN S-27L AND S-28L IAW B727 SRM 51-10-1 PARA 7A.SDR DHLA2009770AT528Frame · wornEMPENNAGE VERTICAL STABILIZER ACTUATOR LT ACCESS PANEL FRAME "T" SHAPE SUPPORT WORN AND LOOSE. REPAIRED VERTICAL STABILIZER MID SPAR CHORD SECTION FROM FIN STA 222 TO FIN STA 241 IAW COOPESA EO COO-2-55-499-08 DTD 12/22/08 DOCUMENTED ON FAA FORM 8110-3.SDR DHLA2009770AT525Skin Panel · corrodedLOWER FUSELAGE FWD CARGO COMPARTMENT FROM BS 560 TO BS 570 RBL 11 WL 148 SKIN WITH CORROSION. REPAIRED FUSELAGE SKIN SECTION FROM BS 557 TO BS 579 BTWN S-26R AND S-28L IAW EO COO-2-53-474-08 DTD 12/18/08.SDR DHLA2009770AT518Skin Panel · dentedLWR FUSELAGE AT BS 509.5 BTWN S-20R AND S-21R WITH DENTS. REPAIRED FUSELAGE SKIN FROM BS 501 TO BS 512 BTWN S-19R AND S-21R IAW SRM 53-30-3 FIG 2.SDR DHLA2009770AT515Skin · dentedLOWER FUSELAGE FWD CARGO COMPARTMENT DOOR OUTER SKIN WITH DENT AT BS 617.5 BETWEEN BEAM 2 AND BEAM 3. REPAIRED FWD CARGO COMPARTMENT DOOR OUTER SKIN SECTION AT BS 615.5 TO620 BETWEEN BEAMS 2 AND 3 IAW B727 SRM 52-00-3 FIG 3.SDR DHLA2009770AT519Skin Panel · crackedLOWER FUSELAGE AT BS 1218.5 RBL 10.25 SKIN CRACKED. REPLACED SKIN SECTION FROM BS 1204.25 TO BS 1232.25 BTWN BL 0 AND RBL 21 IAW SRM 51-10-01 PAR 7A.SDR DHLA2009770AT511Skin Panel · dentedLOWER FUSELAGE AT BS 316 BETWEEN S-22R AND S-23R SKIN WITH DENT. REPAIRED FUSELAGE SKIN SECTION FROM BS 309.25 TO BS 323 BETWEEN S-21R AND S-24R IAW B727 SRM 53-30-3 FIG 1.SDR DHLA200800089Fire Warning · false activationFLT 549 - DURING CRUISE FLIGHT AT FL360, WHEEL WELL FIRE RED LIGHT ILLUMINATED FAINTLY FOR 1 SECOND ACCOMPANIED BY 1 DING OF THE FIRE BELL. INSPECTED AND TESTED SYSTEM PER MM CH 26-12-0. NO DEFECTS FOUND. SYSTEM OP CHECKS GOOD. ACFT WAS GROUNDED.SDR DHL2007770Skin · delaminatedRT WING UPPER SURFACE HAS PANEL O/B OF APU EXH WITH 2 LARGE AREAS OF DELAMINATION APPROX W/S 224 TO 330. TWO AREAS EQUAL TO ABOUT 120 SQ IN.SDR DHLA200700059Transmitter · malfunctionedNR 2 ENG OIL TEMP GAGE REDUCED TO 0 DEG ENG OIL PRESS REDUCED TO 20 PSI OIL QUALITY GOOD COMPLETED APPROPRIATE PRECAUTIONARY ENG SHUT DOWN ENG OIL PRESSURE LIGHT FORWARD PANEL DID NOT ILLUMINATE. CK WIRING ON NR 2 ENG OIL TEMP AND OIL PRESSURE, CK WIRING FROMSDR DHLA200700051Engine · malfunctionedREJECTED T/O ELP DUE TO NR 1 ENG PARAMETERS OUT OF NORMAL RANGE VS NR 2 AND NR 3 ENGS GW=147.9, SPEED EST .50 KNOTS, TEMP 29 DEGREES C PA 3950 REVERSE THRUST USED RAN NR 1 AND NR 3 ENG'S AND VERIFIED N1 AND N2 MATCHED. DEFERRED NR 1 ENG EPR GAUGE PER MEL 77-1SDR DHLA200700036Battery Pack · dischargedEMERGENCY EXIT LIGHTS (BOTH) WOULD NOT WORK DURING STBY TEST. REMOVED AND REPLACED BATTERIES IAW B727 MM 33-50-71, OPS CHECK GOOD.SDR DHLA200700033Battery · inoperativeDURING STBY PWR CHECK, THE EXIT LIGHTS WOULD NOT ILLUMINATE. REMOVED AND REPLACED FLIGHT COMPT AND MAIN ENTRY DOOR EMERGENCY LIGHT BATTERIES. OPS CHECKS OK IAW 727MM 33-50-71 PN OFF AND ON 37067-001.SDR DHL2006770517Stringer · corrodedBS 950F, STR 29R, OB STR CLIP HAS CORROSION. REMOVED FASTENERS FOR CORROSION REMOVAL IAW SRM 51-30-2. AFTER CORROSION REMOVAL IAW SRM 51-10-6 ON STR CLIP FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED DAMAGED STR CLIP IAW SRM 51-30-2. FAB PART FROM 60-SDR DHL2006770519Tab · delaminatedLT WING, IB AILERON, TAB HAS T/E DAMAGE LWR IB SURFACE. REMOVED TAB IAW MM 27-10-11. CUT OUT DAMAGED AREA ON LWR SURFACE OF AILERON TAB APPOX 4.25 INCH BY 4.25 INCH IAW SRM 51-40-20 AND 51-30-2. FAB FILLER, 4.25 INCH BY 4.25 INCH AND DOUBLER 5.85 INCH BY 6 INSDR DHL2006770514Stringer Splice · corrodedAFT CARGO COMPARTMENT, BS 1138, STR 30, STRINGER CORROSION AT ATTACHMENT POINT C/T SHEAR TIE ANGLE. REMOVED CORROSION ON STR 30 IAW BOEING SRM 51-10-6. STR REMOVAL FOUND TO BE OUT OF LIMITS IAW BOEING SRM 53-10-1 FIG 1. CUT OUT DAMAGED STRINGER IAW BOEING SSDR DHL2006770518Stringer · gougedBS 334, STR 4L HAS DEEP GOUGE ON STRINGER, ABOVE AND AFT OF L1 DOOR EXIT LIGHT. CUT OUT DAMAGED AREA APPROX SIZE 2" LENGTH IAW B727 SRM 53-10-3 FIG 1. FAB REPAIR FILLER FROM BAC 1498-108, PO NR 6408112, APPROX 11 LONG IAW B727 SRM 53-10-3 FIG 1 AND 53-10-2 FSDR DHL2006770513Stringer · gougedBS 334, STR 4L HAS DEEP GOUGE ON STRINGER, ABOVE AND AFT OF L1 DOOR EXIT LIGHT. CUT OUT DAMAGED AREA APPOX SIZE 2 INCHES LENGTH IAW SRM 53-10-3 FIG.1. FAB REPAIR FILLER FROM BAC 1498-108, PO NR 6408112, APPOX 1 LONG IAW SRM 53-10-3 FIG.1 AND 53-10-2 FIG.9. SDR DHL2006513Stringer · gougedASTAR NR 111564, DISCREPANCY: BS 334, STR 4L HAS DEEP GOUGE ON STRINGER, ABOVE AND AFT OF L1 DOOR EXIT LIGHT. CUT OUT DAMAGED AREA APPOX SIZE 2 INCH LENGTH IAW SRM 53-10-3 FIG.1. FAB REPAIR FILLER FROM BAC 1498-108, PO NR 6408112, APPOX 1 LONG IAW SRM 53-10-SDR DHL2006770507Frame · dentedAFT CARGO COMPARTMENT, BS 1130 OVER STR 26R HAS FRAME WITH UPPER CHORD DENTED IN. CUT OUT DAMAGED AREA APPROX SIZE 1.875" BY 1.0" IAW B727 SRM 51-40-3 FIG 1. FAB DOUBLER REPAIR WITH 7075-0, .071, SIZE 8" BY 4", PO NR 9003817 IAW B727 SRM 53-10-2 FIG 3 AND 51SDR DHL2006770508Frame · corrodedAFT CARGO COMPARTMENT, BS 970, BETWEEN STR 28R AND 29R, FRAME LWR FLANGE BLOWN-UP WITH CORROSION. REMOVED FLOOR SUPPORT, VERTICAL STIFFENERS AND ANGLES FOR ACCESS IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA AT LWR FRAME FLANGE IAW B727 SRM 53-10-4 FIG 11. FASDR DHL2006770511Stringer · corrodedDISCREPANCY: FORWARD CARGO COMPARTMENT, BS 660, STR 28L, CORROSION ON STR 28L. REMOVED CORROSION AT STR, MATERIAL LOSS IS .022, ORIGINAL MATERIAL THICKNESS .063 AND MATERIAL REMAINING .041. FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG.1. CUT OUT DAMAGED SDR DHL2006770506Frame · dentedFORWARD CARGO COMPARTMENT, BS 720C, STR 26R, DENT IN FRAME RADIUS. CUT OUT DAMAGED AREA SIZE 1.50 INCH BY 1.50 INCH IAW SRM 51-40-3 FIG 1. FAB DOUBLER WITH 7075-0, .071, SIZE 15 INCHES BY 4 INCHES, PO NR 9003817 IAW SRM 53-10-2 FIG.3 AND 51-40-3 FIG.1. HEAT TSDR DHL2006770504Frame · dentedFORWARD CARGO COMPARTMENT, BS 660, STR 27R, DENT IN FRAME RADIUS. CUT OUT DAMAGED AREA SIZE 1.25" BY 1.625" IAW B727 SRM 51-40-3 FIG 1. FAB DOUBLER WITH 7075-0, .071, SIZE 15" BY 4", PO NR 9003817 IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. HEAT TREATED DSDR DHL2006770510Frame · dentedFORWARD CARGO COMPARTMENT BS 680, STR 26R, DENT IN FRAME RADIUS. CUT OUT DAMAGED AREA IAW SRM 51-40-3 FIG.1. FABRICATED DOUBLER IAW SRM 53-10-2 FIG.3 AND 51-40-3 FIG.1. HEAT TREATED DOUBLER IAW ENGINEERING REPORT NR 2-37153-801 REV.IR. INSTALLED REPAIR PARTS SDR DHL2006770505Stringer · corrodedFORWARD CARGO COMPARTMENT, BS 660, STR 28L, CORROSION ON STR 28L. REMOVED CORROSION AT STR, MATERIAL LOSS IS .022, ORIGINAL MATERIAL THICKNESS .063 AND MATERIAL REMAINING .041. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG.1. CUT OUT DAMAGED APPOX 16 INCHES. SDR DHL2006770503Frame · dentedFORWARD CARGO COMPARTMENT BS 680, STR 26R, DENT IN FRAME RADIUS. CUT OUT DAMAGED AREA IAW B727 SRM 51-40-3 FIG 1. FAB DOUBLER WITH 7075-0, .071, SIZE 15 INCHES BY 4 INCHES, PO 9003817 IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. HEAT TREATED DOUBLER FROM 7
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