N315AA, cancelled Mar 8, 2016
Service difficulty reports · 112
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 = 'N315AA' AND deregistration_id = 'N315AA-2016-03-08' 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 = 'N315AA' AND deregistration_id = 'N315AA-2016-03-08' 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 ABXA20151014189Skin · corrodedCORROSION ON LT FUSELAGE SKIN, STATION 955 C/T FAILSAFE TRIM OUT AREA GOING FWD UNDER FAILSAFE STRAP. FAIL SAFE REMOVED ON EA 53500013-008. REMOVED ALL CORROSION, NDT TESTED, NO DEFECTS NOTED. COMPLIED WITH EA 53500013-004 & REA B657-61768MR. REFERENCE EASDR ABXA20151013173Skin · corrodedRIGHT STATION 18.09 PREVIOUS REPAIR DOUBLER, BETWEEN STRINGERS 9RT & 10RT. REQUEST ENGINEERING INSTRUCTIONS. REMOVED DOUBLER, CLEANED HOLES TO LEVEL 3, PERFORMED HFEC ON HOLES & AREA AROUND HOLES. PERFORMED GVI OF 22" AROUND 1809 REPAIR. FABRICATED RT DOUBSDR ABXA20151012175Frame · crackedRIGHT FRAME INNER CHORD AT STATION 883.5, RBL 89 HAS A .250 CRACK IN TRANSITION RADIUS. REPAIRED CHORD IAW EA 53000050-101. CRACKED .50, PN 691T0003-44, PART NAME CHORD RT INNER, SN N/A, FS & BS LOCATION FROM 883.5 STRINGER & WS LOCATION RBL 89. ACFT WAS GNSDR ABXA20151007190Tee Fitting · corrodedUPON CURSORY INSPECTION, FOUND CORROSION WITHIN AREA UNDER THIRD INBD HEAT SHIELD PANEL AT LOWER AFT PYLON AREA, APPROX NAC STATION 400. R & R CORRODED T FITTING IAW BCSF SRM 51-40-02 & DWG 313T1355. SDR INFO, CORRODED LEVEL 2, PN 313T1355-128, PART NAME T FSDR ABXA20151003188Failsafe · crackedLEFT STATION 955, FAIL SAFE STRAP HAS .125 CRACK APPROX 2:00 POSITION AT THE BOTTOM FASTENER HOLE. LT FAIL SAFE STRAP IS BEING REPLACED. NEW FAIL SAFE STRAP PN 145T2524U21 TO BE INSTALLED ON EA53500013-008. SDR INFO CRACKED .125", PN 145T2524, PART NAME FAISDR ABXA20151002165Stiffener · corrodedLEFT WW AFT SPAR BULKHEAD FS 955, LBL 9, INBD VERTICAL ANGLE HAS TOOLING MARKS ON INBD SIDE IN NUMEROUS PLACES. BLENDED TOOLING MARKS ON REAR SPAR STIFFENER IAW REA 66740-MR. SDR INFO CORRODED, PN 111T 1005-1, SN N/A, PART NAME STIFFENER, LOCATION FROM STATISDR ABXA20151001170Longeron · corrodedCORROSION ON UPPER SIDE OF OVERWING LONGERON IN UPPER FWD OTBD CORNER OF RT WW, AROUND FASTENERS & ON FASTENER HEADS FROM FS 975 - 985. REMOVED CORROSION ORIGINAL .080, REMOVED .012, REMAINING .068 IAW REA B653-61757-MR RFTS E-46344 REV IR DATE 9 23 15. SDR SDR ABXA20151001169Longeron · corrodedCORROSION ON UPPER SIDE OF OVERWING LONGERON IN UPPER FWD OTBD CORNER OF RT WW FROM FS 965 - 975. REMOVED CORROSION ORIGINAL .080, REMOVED .012, REMAINING .068 IAW REA B653-61757-MR RFTS E-46344 REV IR DATE 9 23 15. SDR INFO CORRODED LEVEL 2, PN 145T8800-20,SDR ABXA20150930186Skin · corrodedFOUND CORROSION AT APPROX WS 110 RT WING TE FLANGE. REMOVED CORROSION AT UPPER RT WING TE WBL110, PN 112T3101-6 IAW REA B657-61760-MR. SDR INFO, CORRODED LEVEL 2, PN 112T3101-6, SN NSN, PART NAME SKIN, FROM WS110. ACFT WAS GNDED.SDR ABXA20150929168Longeron · corrodedLEFT WW FS APPROX 980 OVERWING LONGERON TOP SIDE HAS CORRODED FASTENERS & POSSIBLY AROUND BASE OF FASTENERS. REMOVED CORROSION, ORIGINAL MATERIAL .080, REMOVED .003, REMAINING .077 IAW REA B653-61756-MR, RFTS NR E-46344 REV DATE ER 9 23 15. SDR INFO CORRODEDSDR ABXA20150928187Failsafe · crackedFOUND CRACK AT LOWER OF 3 FASTENER HOLES INSPECTED. CRACK PLAINLY VISIBLE. REPAIRED AREA IAW DOCUMENT 470080RD06 & EA 53500014-003. SDR, CRACKED, LENGTH : 1.7 INCHES, PN 14T9524-22, PART NAME FAIL SAFE, SN NSN, FS & BS LOCATION SM 955, STRINGER & WS LOCATIOSDR ABXA20150924191Angle · corrodedUPON CURSORY INSPECTION FOUND CORROSION WITHIN AREA UNDER FWD HEAT SHIELD PANEL AT LOWER AFT PYLON AREA, JUST ABOVE AFT EDGE OF EXHAUST NOZZLE, APPROX NAC STATION 350. R & R CORRODED ANGLE INSIDE OF FWD HEAT SHIELD PANEL AREA IAW SRM 51-40-02. SDR INFO, CORRSDR ABXA20150918171Spar · corrodedCORROSION UNDER NUTPLATE ON UPPER CHORD OF WING REAR SPAR TO TE BEAM AT WING STATION 434, OTBD SIDE AS SEEN THRU PANEL 561AB. R & R UPPER CHORD OF WING REAR SPAR IAW SRM BCSF 51-40-02 PARA 7 D. SDR INFO CORRODED LEVEL 2, PN 113T1510-33, SN NSN, PART NAME CHOSDR ABXA20150914185Support Fitting · corrodedFLAP SUPPORT NR 1, TENSION BOLT HOLE NR 1 HAS A DEFECT INDICATION, REFERENCE JC EA5750006-001. REAMED HOLE TO .672, NO FURTHER DEFECTS NOTED, REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-43, PART NAME, FLAP SUPPORT FITTING NR 1, SDR ABXA20150914184Support Fitting · corrodedFLAP SUPPORT NR 2, TENSION BOLT HOLE NR 3 HAS A DEFECT INDICATION, REFERENCE JC A57500018-001. REAMED FASTENER HOLE TO .8285, NO DEFECTS NOTED REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-48, PART NAME, FLAP SUPPORT FITTING NR 2,SDR ABXA20150914183Support Fitting · corrodedFLAP SUPPORT NR 2, TENSION BOLT HOLE NR 2 HAS A DEFECT INDICATION, REFERENCE JC A57500018-001. REAMED HOLE TO .829, NO DEFECTS NOTED REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-48, PART NAME, FLAP SUPPORT FITTING NR 2, WS LOCATISDR ABXA20150914182Support Fitting · corrodedFLAP SUPPORT NR 2, TENSION BOLT HOLE NR 1 HAS DEFECT INDICATION, REFERENCE JC EA57500018-001. REAMED FASTENER HOLE TO .8285, NO FURTHER DEFECTS, REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-48, PART NAME, FLAP SUPPORT FITTING NR SDR ABXA20150914181Support Fitting · corrodedFLAP SUPPORT NR 7, TENSION BOLT HOLE NR 4 HAS DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO .7985, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO, CORRODED LEVEL 2, PN 113T1345-47, PART NAME FLAP SUPPORT FITTING NR 7, WS LOCSDR ABXA20150914180Support Fitting · corrodedFLAP SUPPORT NR 7 TENSION BOLT HOLE NR 2 HAS A DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO .7985, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-47, PART NAME FLAP SUPPORT FITTING NR 7, WS LOCSDR ABXA20150914179Support Fitting · corrodedFLAP SUPPORT NR 7 TENSION BOLT HOLE 1 HAS A DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO .7985, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO, CORRODED LEVEL 2, PN 113T1345-47, PART NAME FLAP SUPPORT FITTING 7, WS LOCATIOSDR ABXA20150914178Support Fitting · corrodedFLAP SUPPORT 8 TENSION BOLT HOLE 4 HAS DEFECT INDICATION. REFERENCE JC EA57500017-001. REAMED FASTENER HOLE TO .875, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO, CORRODED LEVEL 2, PN 113T1345-44, PART NAME FLAP SUPPORT FITTING 8, WS LOCATION 798 SDR ABXA20150914177Support Fitting · corrodedNUMBER 8 FLAP SUPPORT TENSION BOLT HOLE 3 HAS A DEFECT INDICATION. REFERENCE JC EA57500017-001. REAMED FASTENER HOLE TO .672, NO DEFECTS NOTED IAW REA B657-61078-MR REV A. SDR INFO, CORRODED LEVEL 2, PN 113T1345-44, PART NAME FLAP SUPPORT FITTING 8, WS LOCASDR ABXA20150914176Support Fitting · corrodedNUMBER 8 FLAP SUPPORT TENSION BOLT HOLE NR 1, HAS DEFECT INDICATION. REFERENCE JC EA57500017-001. REAMED FASTENER HOLE TO .672, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-44, PART NAME, FLAP SUPPORT FITTING NR 8, WSSDR ABXA20150910172Beam · crackedNUMBER 2 STRUT INSIDE PANEL 447BR, LOWER BEAM IS CHAFED & CRACKED AT THIRD HOLE FROM THE FWD END. R & R LOWER BEAM INSIDE NR 2 PYLON PANEL 447BR IAW SRM 54-51-71 & DWG 313T2380. SDR INFO, PN 313T2380-29, PART NAME, BEAM, SN NSN, CRACKED .5 INCHES, EXACT FS &SDR ABXA20140915293Inverter · damagedCREW REPORTED EICAS MESSAGE STBY INVERTER DISPLAYED, SMOKE IN THE CABIN & A STRONG ELEC BURNING ODOR. THE FLIGHT WAS DIVERTED TO NEAREST SUITABLE AIRPORT. THE STATIC INVERTER WAS REPLACED IAW AMM. 767 FAULT ISOLATION MANUAL PROCEDURES 24-33-807 808 WERE ACCSDR ABXA20140910291Engine · bird ingestionON ROTATION, BIRD STRIKE TO THE LT ENG. CREW HEARD LOUD NOISE & FELT AIRFRAME VIBRATION. LT ENG VIBRATION INDICATED OVER 4.5 & LT THRUST LEVER BEGAN REDUCING TO IDLE. LT ENG WAS SHUTDOWN & CREW PERFORMED AIR TURN BACK. PERFORMED BIRD STRIKE INSPECTION. RESDR ABXA20131213659Power Supply · shortedDURING EXTENDED GROUND TAXI, LT FLIGHT MANAGEMENT COMPUTER FAILED MESSAGE DISPLAYED, FOLLOWED BY SMOKE FROM THE LT CDU & THE LT CDU CIRCUIT BREAKER TRIPPED OPEN. THE CDU WAS REMOVED FOR INSPECTION & NO DAMAGE TO THE WIRING OR CONNECTORS ASSOCIATED WITH THE CDSDR ABXA20131106643Rib · crackedLEFT WING MAIN TRACK RIB AT OSS 1094 IS CRACKED WHERE TRACK BEARING ATTACHES. REMOVED DAMAGE IAW BCSF 767-200 57-41-09 FIG 101 & COMPLIED WITH RGA NR B657 - 60775 MR. CRACKED 1/2 INCH, LOC AT OSS 1094, PN 114T2118-7, PN RIB, SN NA. AIRCRAFT WAS GROUNDED.SDR ABXA20131106634Fairing · crackedVERTICAL STABILIZER AFT AT BASE UNDER 324AL METAL CHAFED & KNIFE EDGED. SRM 51-40-02 APPLIED TOP COAT IAW BOE 767 SRM 51-20-00. CRACKED CHAFED 4 INCHES, LOC FROM 1746 TO 1767, PN 148T7501017, PN FAIRING, SN NA. AIRCRAFT WAS GROUNDED.SDR ABXA20131105644Rib · crackedLEFT WING MAIN TRACK RIB AT OSS 1097 IS CRACKED WHERE THE TRACK BEARING ATTACHES. R & R IAW B767-200 SR SRM 51-40-02, REPAIRED 21E1 IAW REA NR B657-60774 MR. PN 114T2119-1 SN NSN CRACKED LENGTH .125, PN ASSEMBLY RIB STR & WS LOCATION AT OSS 1097. AIRCRAFT WSDR ABXA20131105635Stringer Clip · crackedCLIP ON STRINGER 2 RT AT STATION 1678 CRACKED. R & R CLIP IAW DRAWING 148T1121 & SRM 51-20- 02. PN 148T1303-1 SN NA CRACKED 1/4 INCH, PN CLIP FS & BS LOCATION 1678 TO 1678 STRINGER & WS LOCATION R2 TO R2. AIRCRAFT WAS GROUNDED.SDR ABXA20131104641Intercostal · corrodedFORWARD LOWER CARGO FUSELAGE STATION 549 RBL 6 THE STRUCTURE FOR THE LATERAL GUIDE NUTPLATES IS CORRODED. R & R 452T2704-1 INTERCOSTAL IAW DRAWING 451T2501 & SRM 51-40-02. R & R WEB FLOOR FS 522 - 549 RBL12 - LBL12 & INSTALLED LATERAL GUIDE AT FS 549 RBL 6 IASDR ABXA20131104627Structure · corrodedFORWARD LOWER CARGO FUSELAGE STATION 412 LBL 46 LOWER SIDE OF UPPER CHORD, BELOW CARGO FLOOR, IS SPLIT WITH INTERNAL CORROSION AT NUTPLATE LOCATION. REMOVED PDU L1 & L2, REMOVED ROLLER TRAYS. R & R DRILLED & INSTALLED CORD PT STATION 412, REINSTALLED ROLLER SDR ABXA20131102642Plate · crackedUPPER CARGO FLOOR PANEL MOUNTING PLATE UNDER CARGO LOCK MOUNT IS CRACKED FS 1021 LBL 45. R & R MATCH DRILLED TO FLOOR PANEL, FLOOR PANEL MOUNTING PATE AT FS 1021 LBC 45 IAW B767 SRM 51-40-02, 51-40-05, PN PLATE, CRACK LENGTH 1 INCH, PN 457T4101-2, SN NSN, LOCSDR ABXA20131101632Keelbeam · corrodedCORROSION ON FLAT PANEL IN WW AT STATION 973 LBL 6 & ON ANGLE AT STATION 977 LBL 6. REMOVED CORROSION IAW B767-200 SRM 53-50-12. COMPLIED WITH REA NR B653-60754-MR. PN 145T8612-1, PN KEEL BEAM WEB FS & BS LOC. ON A/C BS 973 TO BS 977, STRINGER & WS LOC. ON SDR ABXA20131101629Frame · corrodedFORWARD LOWER CARGO FUSELAGE STATION 478 AFT SIDE OF CHORD AT LBL 20 UNDERSIDE OF CHORD IS CORRODED AT NUTPLATE. REMOVED OLD CORD DRILLED NEW ONE IAW BOE 767 SRM 51-40-05 INSTALLED NEW CORD IAW BOE 767 SRM 51-40-02, OLD CORD WAS FOUND TO BE OUT OF LIMITS IAW SDR ABXA20131101628Frame · corrodedFORWARD LOWER CARGO FUSELAGE STATION 478 AFT SIDE OF CHORD AT LBL 38 UNDERSIDE OF CHORD IS CORRODED AT NUTPLATE. R & R CORD ON NR 0259. NEW CORD WAS DRILLED IAW BOE 767 SRM 51-40-05 ROLLER TRAYS WILL BE REINSTALLED ON NR 0250 ENTRY 4 CORD WAS OUT OF LIMITS ISDR ABXA20131031638Shear Tie · corrodedAREA BEHIND FWD LOWER CARGO AT FUSELAGE STATION 742 STRINGER 38L - STRINGER 39L SHEAR TIE CORRODED. INSTALLED SHEER TIE IN FWD LOWER CARGO AT STATION 742 BETWEEN 538L & 539L IAW B767 SRM 51-40-02. LEVEL 2 CORRODED, LOC FROM 742, LOC FROM 538L TO 539L, PN 140SDR ABXA20131031636Shear Tie · corrodedBEHIND FWD LOWER CARGO AFT SIDE OF FUSELAGE STATION 742 SHEAR TIE CORRODED BETWEEN STRINGER 35L - STRINGER 36L. INSTALLED NEW SHEET TIE IN FWD LOWER CARGO AT STATION 742 BETWEEN STRINGER 35L - STRINGER 36L IAW B767 SRM 51- 40-02. LEVEL 2, LOC FROM 742, LOC. SDR ABXA20131030631Floorbeam · corrodedFORWARD LOWER CARGO FUSELAGE STATION 720 LBL 41 UPPER & LOWER CHORD IS CORRODED & SEPARATING INCLUDING 3 INCHES OTBD ON LOWER SIDE. REPLACED T CHORD. LOCATED, DRILLED & INSTALLED IAW DRAWING 143T1213. LEVEL 2 CORROSION LOC FROM FS 720 LBL43 TO FS 720 RBL 43,SDR ABXA20131030630Intercostal · corrodedFORWARD LOWER CARGO FUSELAGE STATION 580 LBL 13 ON LOWER SIDE OF INTERCOSTAL CORRODED. REPLACED & INSTALLED NEW INTERCOSTAL AT STATION S80 LBL 13 IAW B767 SRM 51-40- 02 & IAW B767 SRM 53-00-04, INSTALLED PDO AT STATION 580 LBL 13 IAW B767 AMM 25-53- 0. LEVELSDR ABXA20131029640Panel · corrodedFORWARD LOWER CARGO FUSELAGE STATION 630 BILGE PANEL COVER CORRODED ON TOP AT LBL PO 0039309. LEVEL 2 CORROSION PN 143T5000-122, PN BILGE PANEL, SN NA. LOCATION FROM 632 TO 610 LOCATION FROM LBL 11 TO LNL 11. AIRCRAFT WAS GROUNDED.SDR ABXA20131029637Shear Tie · corrodedBEHIND FWD LOWER CARGO AFT SIDE OF FUSELAGE STATION 742 SHEAR TIE CORRODED BETWEEN STRINGER 38R - STRINGER 39R. R & R SHEAR TIE AT STATION 742 BETWEEN G38R & 39R IAW B767-200 SRM 51-40-02. LEVEL 2 CORROSION, PN 140T2102U254, PN SHEAR TIE, SN NSN, LOC FROM 74SDR ABXA20131029633Keelbeam · corrodedLEFT HAND KEEL CHORD UPPER FLANGE HAS CORROSION AT STATION 985 - 995 LBL 10.75. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION PN 145T8611-5, PN KEEL BEAM CHORD LT, SN NA, LOC FS 985 -FS 995, LBL 10.75 TO LSDR ABXA20131029626Keelbeam · corrodedCORROSION ON KEEL BEAM UPPER & LOWER SURFACE ADJACENT TO NUTPLATE AT STATION 801 LBL 9. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-6, PN KEEL BEAM CHORD, SN NA, LOC FS 801, LBL 9. AIRCRAFTSDR ABXA20131029625Keelbeam · corrodedSPOT OF CORROSION ON KEEL BEAM UPPER SURFACE AT STATION 814 RBL 9 ADJACENT TO NUTPLATE. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101. COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-5, PN KEEL BEAM CHORD, SN NA, LOC 814 RBL 9. AIRCRAFT WASDR ABXA20131029624Keelbeam · corrodedCORROSION ON KEEL BEAM AT STATION 827 LBL 11. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-5, PN KEEL BEAM CHORD LT, SN NA, LOC FS 827, LBL 11. AIRCRAFT WAS GROUNDED.SDR ABXA20131029623Keelbeam · corrodedCORROSION ON KEEL BEAM AT STATION 955 LBL 12. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-5, PN KEEL BEAM CHORD, SN NA, LOC FS 955, LBL 12. AIRCRAFT WAS GROUNDED.SDR ABXA20131029622Keelbeam · corrodedCORROSION ON KEEL BEAM AT STATION 951 RBL 12 LOWER SURFACE. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-65, PN KEEL BEAM CHORD, SN NA, LOC FS 951 RBL 12, AIRCRAFT WAS GROUNDED.SDR ABXA20131029621Keelbeam · corrodedCORROSION ON KEEL BEAM AT STATION 808 RBL 10 LOWER SURFACE. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-6, PN KEEL BEAM CHORD, SN NA, LOC STATION 808 RBL 10, AIRCRAFT WAS GROUNDED.
Back to N315AA, cancelled Mar 8, 2016