N764AT, cancelled Jul 21, 2010
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 = 'N764AT' AND deregistration_id = 'N764AT-2010-07-21' 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 = 'N764AT' AND deregistration_id = 'N764AT-2010-07-21' 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 DHLA2000800117Cable Assy · noisyFLIGHT 935 - DURING CLIMBOUT HEARD LOUD NOISE SEEMING TO COME FROM NOSE GEAR AREA, MINUTES LATER RED DOORS LIGHT ON FWD PANEL & NOSE GEAR DOOR LIGHT ILLUM ON S/O PANEL. FELT VIBRATION. COMPLETED ABNORMAL PROCEDURE & RETURNED TO ILN. REPLACED BOTH NOSE GEAR SDR DHLA200800114Accessory Unit · failedON CLIMBOUT AT 300KIAS PASSING FL200 RED DOORS LIGHT ON FWD PANEL & NOSE GEAR DOOR LIGHT ON S/O'S PANEL ILLUMINATED. FELT HEAVY VIBRATION PERFORMED ABNORMAL PROCEDURE AFTER SLOWING TO 260KTS LIGHT WENT OUT /VIBRATION REMAINED. MX INSTRUCTED, CYCLE GEAR UPON SDR DHL2008764532Spar · crackedWHILE AT C CHECK, RT WING REAR SPAR J BEAM CRACKED WBL 126. FABRICATED AND REMOVED AND REPLACED IAW BOEING DWG 65-21655 AND ASTAR EC-00911-001.SDR DHL2008764531Spar · crackedWHILE AT C CHECK, LT WING REAR SPAR J BEAM CRACKED INDICATION WBL126. FABRICATED AND REMOVED AND REPLACED IAW BOEING DWG 65-21655 AND ASTAR EC-00910-001 MATERIAL BAC 1506-860 7075T6 DIM 81 INCH BY 5 1/2 INCH PO NR 815922.SDR DHL2008764533Attach Angle · crackedWHILE AT C CHECK, LT O/B MID FLAP I/B LOWER END CAP AND ATTACHMENT ANGLE CRACKED. REPAIRED IAW B727 SRM 51-40-2, 51-20-1, 51-30-5 AND 57-50-2 FIG 6. REPAIR ANGLE MAT.7075 T6 .071" PO NR 9006522 DIM 4 INCH BY 4 INCH AND 3 INCH BY 2 INCH.SDR DHL2008764530Rib · crackedWHILE AT C CHECK, NR 5 K-FLAP ACTUATOR SIDE MOUNTING RIBS I/B AND O/B CRACKED. REPAIRED RIBS IAW BOEING DWG 65-16269 REVC MATERIAL 2024T3 .063" DIM 7" BY 6 1/8 INCH PO NR 9006773.SDR DHL2008764529Skin · bentWHILE AT C CHECK, L1 DOOR INNER SKIN BENT FWD LOWER CORNER. REPAIRED IAW B727 SRM 51-40-2 AND ASTAR EVA B52-00073 REV1.SDR DHL2008764528Keelbeam · crackedWHILE AT C-CHECK, CRACK AT BS 874 RIGHT KEEL BEAM LWR CHORD IN APU BAY. REPAIRED IAW S/B 727 53-02-08 MATERIAL 4130 STEEL .071" PO 610176.SDR DHL2008764527Frame · dentedWHILE AT C-CHECK, DENT AT MAIN FRAME BS 580 BETWEEN STR 16 AND 17R. REPAIRED IAW SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3, 7075T6 .050 DIM 7.125" X 6.25" PO 9006742.SDR DHL2008764526Stringer · corrodedWHILE AT C-CHECK, PILLOWING AT FASTENERS AT RIGHT LWR FUSELAGE AT BS 350, 4 INCHES FWD OF NOSE JACK PAD. REPAIRED IAW SRM 53-10-3 FIG 1 DETAIL 2. MATERIAL USED P/N 95-24786-10 GUSSET / CHANNEL, REPAIR FOR 21R BAC 1496-138 DIM 11" PO 815987, CHANNEL SPLICE FRSDR DHL2008764524Skin · delaminatedWHILE AT C-CHECK, LT WING O/B AILERON TAB LWR I/B SURFACE DELAM WBL 492. CUT OUT DELAMINATED AREA 1 INCH DIA AND APPLIED POTTING COMPOUND. FABRICATED DOUBLER 3 INCH DIA FROM.010" 2024-T3 PO 9003621. BONDED DOUBLER, CLEANED PRIMED AND SEALED IAW B727 SRM 51-SDR DHL2008764523Hinge · crackedWHILE AT C-CHECK, EXTERNAL FUSELAGE BS 650 MCD AFT HINGE SEGMENT HAS AFT 2 LOBES WITH SMALL CRACKS. REMOVED AND REPLACED MCD STA 650 AFT HINGE SEGMENT IAW AEI B727 M/M CH 52 PGS 17-20 P/N MS20001-16-7200 PO 9006913.SDR DHL2008764535Bulkhead · crackedCRACK INDICATION AT BS 870 IN RT W/WELL AT APU LOAD CONTROL VALVE CUT-OUT. TRIMMED OUT CRACKED MATERIAL, FABRICATED REPAIR PARTS, AND INSTALLED REPAIR AT BS 870 BULKHEAD PER B727 SRM 53-10-9 FIG 5, 51-10-6, 51-10-1, AND NDTM PT6, 51-00-00 FIG 23.SDR DHL2008764522Mount Bracket · crackedNR 1 K-FLAP ACTUATOR TRUNNION MOUNTING BRACKETS CRACK INDICATION WS 305. REMOVED NR 1 K-FLAP MOUNTING BRACKETS WS 305 IAW B727 SRM 51-30-2. FAB NEW BRACKETS WITH 2024-T3 .063", DIM 7.5" X 4" AND PO 9006027 IAW BOEING ENGINEERING DWG 65-16275.SDR DHL2008764521Frame · dentedDENTS ON MAIN CABIN FRAME BS 640 BETWEEN STR 16 AND 17R. CUT OUT DAMAGED AREA AT FRAME BS 640 BETWEEN STR 16 & 17 RT APPROX 7/8" X 1", FAB DOUBLER REPAIR WITH 7075-T6 .050", DIM 7" X 5" AND PO 9006742 IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1.SDR DHL2008764520Bracket · crackedNR 2 K-FLAP ACTUATOR, TRUNNION MOUNTING BRACKETS CRACK INDICATION (WS 235 APPROX). REMOVED NR 2 K-FLAP TRUNNION MOUNTING BRACKETS FROM ACTUATOR WS 235 IAW B727 SRM 51-30-2. FAB NEW BRACKETS WITH 2024-T3 .063" DIM 9" X 6.5 AND PO 9006773 IAW BOEING ENGINEERINSDR DHL2008764519Skin · damagedSKIN DAMAGE ON LT WING T/E AT NR 2 SPOILER NR 3 HINGE CUTOUT. ROUTER OUT SKIN AT LT WING T/E NR 2 SPOILER NR 3 HINGE CUTOUT FOUND OUT OF LIMITS IAW B727 SRM 51-10-1 AND 57-20-1 FIG 2. FAB DOUBLER REPAIR WITH 7075-T6. DIMENSION: 4" X 7" AND PO 9006522 IAW B72SDR DHL2008764518Flap · crackedLEFT INBOARD FORE FLAP CRACK INDICATIONS AT L/E FWD OF SEQUENCE CAR ATTACH POINTS (FITTING) WBL 124/203. STOP DRILLED AT THE END OF CRACKS AT LEFT INBOARD FORE FLAP L/E WBL 124/203 IAW B727 SRM 51-10-1. FAB DOUBLER REPAIR WITH 2024-T3 .050" AND PO 9006457 I/SDR DHL2008764534Tab · bentLT ELEV TAB INBD CORNER DAMAGED, REMOVED DAMAGED AREA, FABRICATED REPAIR, AND INSTALLED BY BONDING IAW B727 SRM 51-40-20 PGS 12 THROUGH 62 AND SRM 51-80 FIG 2. NO FURTHER ACTION REQUIRED.SDR DHL2008764517Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK BS 1110-1130 LBL 24. REMOVED SEAT TRACK FROM MAIN CABIN BS 1110-1137 LBL 24 FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3 AND SRM 51-30-2. FAB NEW SEAT TRACK WITH BAC1520-792-7178-T6 DIM, 2'3" AND PO 9003797 IAW B727 SRM 5SDR DHL2008764516Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK BS 1110-1130 LBL 45. REMOVED CORRODED SEAT TRACK FROM BS1110 TO 1137 LBL 45 FOUND OUT OF LIMITS IAW B727 SRM 51-30-2 ZND 53-10-1 FIG 3. FAB NEW SECTION WITH BAC 1520-792-7178-T6 DIM. 2'3" AND P.O. 6295113 IAW B727 SRM 53-1SDR DHL2008764515Rib · crackedNR 6 K-FLAP ACTUATOR SUPPORT SIDE I/B AND O/B RIBS CRACKED WS 304. REMOVED INBOARD AND OUTBOARD RIBS AND FAB NEW RIBS WITH 2024-T3-.063 INCH DIM 7 1/2 INCH BY 4 INCH AND PO 9006773 IAW BOEING ENGINEER DWG NR 65-16275.SDR DHL2008764514Flap · crackedL/WING I/B MIDFLAP T/E CHORD CRACKED AT I/B CABLE DRUM, 2 PLACES. REMOVED DAMAGED AREA AT T/E CHORD ABOUT 51 INCHES. FABRICATED NEW SECTION WITH P/N 604754 7075-T6 DIM 51 INCH AND PO 815986 IAW B727 SRM 57-50-2 FIG 5 AND 51-40-1 FIG 1.SDR DHL2008765513Seat Track · corrodedCORRODED SEAT TRACK RBL 45 BS 1110-1135. SEAT TRACK AT RBL 45 BS 950 TO 1183 CORRODED OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. FAB NEW SECTION OF SEAT TRACK WITH BAC 1520-792-7178-T6 DIM 15'7 INCH AND PO 9006864 AND TWO ANGLES FOR SPLICES WITH BAC 1503-1001SDR DHL2008764512Seat Track · corrodedCORRODED SEAT TRACK RBL 24 BS 1110-1135. SEAT TRACK CORRODED FROM RBL 24 FROM BS 1070 TO 1136 IAW B727 SRM 51-30-2 AND 53-10-1 FIG 3. FAB NEW SECTION WITH BAC 1520-792-7178-T6 DIM 5'6" AND PO 9006020 IAW B727 SRM 53-10-5 FIG 1.SDR DHL2008764511Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK BS 480-600 LBL 45. SEAT TRACK CORRODED OUT OF LIMITS STA 480-590 IAW B727 SRM 51-20-2 FIG 21 AND 53-10-1 FIG 3. FAB NEW SECTION OF SEAT TRACK WITH BAC 1520-792-7178-T6511 DIM 9'2 INCH PO 9006020 IAW B727 SRM 53-10-2 FIG 1 ASDR DHL2008764510Shear Web · dentedDENT AND PUNCTURE HOLE ON MAIN CABIN SHEAR WEB BS 1140 RBL 24. CUT OUT DAMAGED AREA AT SHEAR WEB RBL 24 BS 1140 (2 EACH ) 3/4 INCH BY 3/4 INCH AND 1 INCH BY 1 INCH IAW B727 SRM 51-40-2 FIG 1. FAB DOUBLER REPAIR WITH 7075-T6 .071 INCH SIZE: 9 INCH BY 7 INCH ASDR DHL2008764509Floorbeam · corrodedCORROSION ON BS 1110 FLOORBEAM LBL 24 - LBL 45. CORROSION ON FLOORBEAM LBL 24-LBL 45 BS 111O FOUND OUT OF LIMITS AT LBL 33 IAW B727 SRM 51-10-6 AND 53-10-1 FIG 5. CUT OUT DAMAGED AREA, FAB ONE FILLER WITH 7075-T6 .125 INCH DIM 2 INCH BY 1 INCH PO 7371263. TSDR DHL2008764507Frame · gougedWHILE AT C CHECK REF N/R 097896, 4 EACH TOOLING MARKS/GOUGES ON MAIN CABIN FRAME BS 700 BETWEEN S7-8L. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MATERIAL 7075-O PO NR 9006027 HEAT TREATED FROM 7075-O TO 7075-T6 IAW FAS ENGINEERING REPORT NR 2-3715SDR DHL2008764506Frame · dentedWHILE AT C CHECK REF N/R 098177, DENT ON MAIN CABIN FRAME BS 600 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MATERIAL 7075-T6 .050 INCH DIMENSION 7 INCH BY 5 1/4 INCH PO NR 9006153.SDR DHL2008764505Frame · dentedWHILE AT C CHECK REF N/R 098175, DENT ON MAIN CABIN FRAME BS 540 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MATERIAL 7075-T6 .050 INCH DIM 7 1/8 INCH BY 6 INCH PO NR 9006742.SDR DHL2008764508Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK BS 480-620 RBL 45. SEAT TRACK CORRODED OUT OF LIMITS IAW B727 SRM 51-20-2 FIG 21 AND 53-10-1 FIG 3. FAB NEW SECTION WITH BAC 1520-792-7178T6 DIM 12'6 3/8 INCH AND PO 9006020 IAW B727 SRM 53-10-5 FIG 1 AND VENTURA AEROSPACE SDR DHL2008764504Frame · dentedWHILE AT C CHECK REF N/R 098180, DENT AT MAIN CABIN FRAME BS 680 BETWEEN STR 16 AND 17R. FABRICATED REPAIR IAW B727 SRM 51-40-3 FIG1 AND 53-10-2 FIG3 MATERIAL 7075-T6 .050 INCH DIM 7 1/8 INCH BY 5 1/4 INCH PO NR 9006742.SDR DHL2008764503Frame · dentedWHILE AT C CHECK REF N/R098179, DENT AT MAIN CABIN FRAME BS 660 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 DOUBLER MATERIAL 7075-T6 .050 DIM 7 1/8 INCH BY 5 1/4 INCH PO NR 9006742.SDR DHL2008764502Frame · dentedWHILE AT C CHECK REF N/R 098174, DENT AT MAIN CABIN FRAME AT BS 520 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MAT, 7075-T6 .050" DIM 5 1/8 INCH BY 8 1/4 INCH PO NR 9006742.SDR DHL2008764501Frame · dentedWHILE AT C CHECK REF N/R 098173, DENT AT RT MAIN CABIN FRAME BS 480 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG1 AND 53-10-2 FIG3 MATERIAL DOUBLER 7075-T6 .050 INCH DIM 7 1/4 INCH BY 5 3/4 INCH PO NR 9006742.SDR DHL2008764500Skin · crackedWHILE AT C CHECK REF N/R 097599, RT I/B AFT FLAP LOWER SKIN WBL 203 CRACKED AT MOUNTING FITTING. REPAIRED IAW B727 SRM 57-50-4 FIG 11, SPLICE 2024T3 .050 DIM 5.5 INCH BY 11 INCH PO NR 9006742. FABBED FILLER 2024T3 .040 DIM 9 INCH BY 14 INCH PO NR 9006587.SDR DHL2006764003Light · inoperativeSECURITY CHECK COCKPIT EMERG EXIT LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERG EXIT LIGHT ASSY IAW B727 M/M 33-50-101. OPS CHECK GOOD.SDR DHL2006764007Skin · damagedREF. ASTAR LOG PAGE 098862 ITEM 1P. BELT LOADER STRUCK A/C AFT OF FWD BELLY LEFT 17 INCH GASH. C/W ASTAR JC EA53100140-001-B REPAIR SKIN (FS680-690). ACCOMPLISHED ASTAR JC EA53100140-001-B WO 600017273 REPAIR SKIN (FS680-690) EXT. B727 AND DWG NR 53100140-001SDR DHL2006764004Skin · damagedCREASE IN SKIN STA 660 STR 26R-27R IAW ITEM 1P LP 098862. CUTOUT DAMAGE AREA DIM. 3 INCH X 1 INCH, FAB. DOUBLER MAT. USED 2024T3 .063 PO NR 9003898 DIM. 11.3750 INCH X 9.7500 INCH. FAB TRIPLER MAT USED 2024T3 .071 PO NR 9003866 DIM. 12.1250 INCH X 10 INCH. SDR DHL2006764006Web · damagedWEB DAMAGED BELOW STR 27R BETWEEN STA 680-700 REF. ITEM 1P LP 098862. REMOVED DAMAGED WEB, FABRICATED PO NR 900245 DIM. 18.1250 INCH X 7.1250 INCH, INSTALLED, PRIMED AND TREATED IAW SRM 51-30-2 & 51-10-2 AT STA 680-700 BELOW STR 27R.SDR DHL2006764005Skin · damagedSTRINGERS 28R AND 27R DAMAGED BETWEEN STA 680-700. REF. ITEM 1P LP 098862. CUTOUT DAMAGED SECTIONS STR 27R 26.5 INCH AND STR 28R 7.5 INCH. FAB. NEW FROM BAC1498-144. SPLICE FROM BAC1498-132 STR 27R 12INCH AND STR 28R 22.5 INCH PO INCH 623185 AND PO INCH 423185SDR DHL2006764002Battery · dischargedCOCKPIT EMERGENCY EXIT LIGHT WILL NOT ILLUM. DURING SBY PWR CHECK. R&R EMERGENCY EXIT LIGHT BATTERIES 2 EACH P/N38931-002. INSTALLED, OPS CHECK SERVICEABLE PER B-727 M/M 33-50-00.SDR DHL2006764001Light · looseEMERGENCY EXIT LIGHT IN COCKPIT LOOSE AND REMAINS ILLUMINATED IN FLIGHT. RESECURED COCKPIT EMERGENCY EXIT LIGHT PACK. OPS CHECK GOOD IAW MM 33-50-71.SDR DHL2006764517Tab · dentedDENT ON R/WING OB AILERON TAB UPPER SURFACE. CUT OUT DENTED AREA ON RT OB AILERON TAB APPROX 1 INCH DIA FABRICATED FILLER APPROX 1 INCH DIA AND DOUBLER APPROX 3.7500 INCHES X 4 INCHES FROM 2024-T3 .010 PO NR 9912184CLEANED, PREPPED PRIMED, BONDED CLEANED TREATSDR DHL2006764516Skin · dentedNR 016062 LT WING IB AILERON UPPER SKIN HAS NUMEROUS DENTS. REMOVED AND REINSTALLED LH IB AILERON AND TAB IAW MM 27-10-01 AND MM 27-10-11. FABRICATED NEW SKIN USING MAT 2024T3 .040 PO NR 9003189 DIM 41 .2500 X 22.2500 INCH IAW SRM 57-50-2 FIG7 AND SRM 51-30-5SDR DHL2006764519Stiffener · crackedLT WING FRONT SPAR VERTICAL STIFFENER AT WS 90 SHOWS CRACK FROM BOTTOM END. REMOVED FASTENERS FOR ACCESS IAW SRM 51-30-2 HFEC AT ANGLE MARKED END OF CRACK NDT MAN PART6 51-00-00 FIG23 STOP DRILLED .250 END OF CRACK IAW SRM51-10-1 FAB REPAIR MAT USED 7075 T6 .SDR DHL2006764506Attach Fitting · crackedL/WING INSIDE NR 4 SLAT LE ACTUATOR ATTACH POINT FOUND CRACK ON INNER SKIN AT WS 410. CUTOUT AREA AT L/WING INSIDE NR 4 SLAT LE ON INNER SKIN AT WS 410 DIM 10.5"X 5.250" IAW B727 SRM 57-30-4 FIG 3. FABRICATED FILLER MAT USED 2024T3 .040 PO# 9002787 AND DIM. SDR DHL2006764515Rib · crackedREF ASTAR N/R 015815 DISCREPANCY: NR 6 SLAT OB ACT ROD END MOUNT RIB CRACKED REMOVED AND REPLACED RIB NR 6 SLAT OB ACT ROD END MOUNT PO NR 619549 P/N 65-17294-14 IAW B727 SRM 51-30-2.SDR DHL2006764512Attach Bracket · crackedLT WING INSIDE NR 4 SLAT LE ACTUATOR ATTACHED POINT IB AND OB RIB CRACKED. REMOVED RIBS AT LT WING NR 4 SLAT IB AND OB ACTUATOR ATTACHED POINT AND 1 CHANNEL IAW B727 SRM 51-30-5. TREATED AND PRIMED HOLES AND AREA IAW B727 SRM 51-10-2. INSTALED RIBS P/N 65-1
Back to N764AT, cancelled Jul 21, 2010