N708AS, cancelled Oct 9, 2018
Service difficulty reports · 151
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 = 'N708AS' AND deregistration_id = 'N708AS-2018-10-09' 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 = 'N708AS' AND deregistration_id = 'N708AS-2018-10-09' 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 ASAA2017053020919Battery Pack · failedEMERGENCY EXIT LIGHTS ABOVE SEAT ROWS 1 - 11ABC FOUND INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED THE BATTERY PACK, OPS NORMAL IAW AMM 33-51-06-960-805.SDR ASAA2016110718677Fitting · corrodedAFTER REMOVAL OF OTBD FOREFLAP OTBD TORQUE TUBE, FOUND ATTACH FITTING FOR TORQUE TUBE CORRODED. ACFT GROUNDED. REMOVED & REPLACED THE FITTING IAW AMM 20-80-11-912-002, PG 6.SDR ASAA2016110718675Fitting · corrodedAFTER REMOVAL OF INBD FOREFLAP INBD TORQUE TUBE, FOUND ATTACH FITTING FOR TORQUE TUBE CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE FITTING IAW AMM 20-50-11-912-602 PG 6.SDR ASAA2016103118688Frame · crackedPAX CABIN FRAME CRACKED BS 827 BETWEEN STRINGERS 8 AND 9R. ACFT GROUNDED. REPAIRED THE FRAME IAW T/C AD20062609-400-53-107 REV 00.SDR ASAA2016103018772Floorbeam · crackedCABIN FLOORBEAM CRACKED AT BS 538 LBL 1 - 22. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-05-0G-0.SDR ASAA2016103018674Floor Support · corrodedFLOOR SUPPORT RBL 22 CORRODED AT BS 952. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-01-1, REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0.SDR ASAA2016103018673Floor Support · corrodedFLOOR SUPPORT LBL 42 BS 947 TO 967 CORRODED MULTIPLE AREAS. ACFT GROUNDED. REMOVED AND REPLACED DAMAGED FLOOR SUPPORT IAW SRM 51-40-02-0G-0.SDR ASAA2016103018672Floor Support · corrodedFLOOR SUPPORT LBL 22 CORRODED AT BS 952. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0W.SDR ASAA2016102918676Skin · chafedLT WING I/B EXHAUST GATE O/B UPPER CORNER SKIN IS CHAFED. GROUNDED - YES. REMOVED DAMAGE FROM UPPER SKIN REMAINING MAT. FOUND TO BE .0605, RESTORED FINISH IAW SRM 57-53-01-0G-0. REQUIRES A DETAILED VISUAL INSPECTION OF AREA AT EVERY 3000 FLT CYCLES OR EVERY 12SDR ASAA2016102818755Cargo Track · crackedAFT CARGO RT CARGO TRACK IS CRACKED IN RADIUS OF VERTICAL LEG AT BS 747. ACFT GROUNDEDS. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-2R-2 AND EA 400-53EA-18029.SDR ASAA2016102818708Cargo Track · crackedAFT CARGO BAY RT CARGO TRACK IS CRACKED IN THE RADIUS OF VERTICAL LEG AT BS 727C. ACFT GROUNDED. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-2R-2.SDR ASAA2016102818678Floorbeam · corrodedFLOORBEAM BS 312 HAS SPOT OF CORROSION AT LBL 14. ACFT GROUNDED. REPAIRED DMGE TO FLOOR BEAM UPPER CHORD IAW SRM 53-10-51-2R-5.SDR ASAA2016102818557Transition Panel · crackedAFT CARGO RIGHT TRANSITION IS CRACKED AT BS 727F. ACFT GROUNDED. REMOVED CRACKED TRANSITION PANEL AND REPLACED WITH NEW IAW SRM 51 40 02 0G 0.SDR ASAA2016081217684Arm · out of adjustL1 DOOR WILL NOT CLOSE. THERE WERE NO PRESSURIZATION ISSUES ON PREVIOUS FLIGHT SEGMENT. ACFT GROUNDED. ADJUSTED L1 DOOR GUIDE ARM, IAW AMM 52-11-00-705. ACCOMPLISHED L1 DOOR OPS TEST, IAW AMM 52-11-00-755. OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR ASAA2016051716786Latch · gougedAFT CARGO DOOR HANDLE RECESS IS GOUGED FROM MISSING HANDLE BUMPER. ACFT GROUNDED. REMOVED RIVETS FROM HOUSING, REF SRM 51-40-02. ALL HOLES PREVIOUSLY OVERSIZED TO NR 6 RIVETS EXCEPT 1 WHICH IS OVERSIZED TO .238. REMOVED AFT CARGO DOOR HANDLE, REF AMM 52-31-SDR ASAA2016041316391Controller · failedPROMPTLY AFTER LEVEL OFF AT FL 310 HEARD CABIN ALTITUDE WARNING HORN ACCOMPANIED BY VISUAL CABIN RED ANNUNCIATER LIGHT PERFORMED QRH CHECKLIST PROCEDURES & EXECUTED EMERGENCY DECENT TO 10000'. CABIN STABILIZED IN STANDBY MODE AT 10000 REMAINED OF FLIGHT. ACFSDR ASAA2015100513347Lamp · failedEMERGENCY LIGHT EXIT LOCATOR SIGNS AT LT FORWARD, LT AFT, AND RT AFT OVERWING EXITS HAVE MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. RELAMPED AND TESTED IAW MM 33-51-81-962-011. OPS NORMAL.SDR ASAA2015082012954Floor Support · bentAFT CARGO COMPARTMENT, LT FLOOR SUPPORT INTERCOSTAL BS 727A-727B IS BENT. ACFT GROUNDED. R & R FLOOR SUPPORT INTERCOSTAL AT BS 727A-727B IAW SRM 51-10-02, PARA NR 8 SRM 51-40-05 , DWG 69-16500 REV:D AND REAPPLIED CIC IAW AMM 51-21-91.SDR ASAA2015072912676Stiffener · crackedLEFT HORIZONTAL STABILIZER AT STABILIZER 129.5 RIB, STIFFENER CRACKED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-10-02, PARA 8 AND 51-40-02, AND DWG 65-47508, REV C.SDR ASAA2015072912675Stiffener · crackedLEFT HORIZONTAL STABILIZER AT STAB STA 129.5 RIB, STIFFENER, PN 65-47508-50 IS CRACKED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-10-02, PARA 8 AND 51-40-02, AND BAC DWG 65-47508, REV C.SDR ASAA2015072812940Frame · damagedFUSELAGE FRAME BS 727D HAS AN ENLONGATED HOLE AT LT LOWER Z ANGLE ATTACHMENT. ACFT GROUNDED. REPAIRED IAW EA 400-53EA-15683, REV NEW.SDR ASAA2015072812939Frame · damagedFUSELAGE FRAME 727F HAS AN ENLONGATED HOLE AT LT LOWER Z-ANGLE ATTACHMENT. ACFT GROUNDED. REPAIRED FRAME IAW EA 400-53EA-15684, REV NEW, STA 727F.SDR ASAA2015072312757Web · corrodedAFT CARGO DOOR SILL WEB IS CORRODED. ACFT GROUNDED. REMOVED CORRODED ORIG .045", REMAIN .040" LOSS OF .005", FOUND OUT OF LIMITS IAW SRM 53-60-16, NEW WEB IAW DWG 65-479.57 AND DWG A530001818L. DRILLED AND INSTALLED 2 EA DOUBLERS IAW DWG A5330001818L.SDR ASAA2015072212933Floor Support · corrodedAFT CARGO BAY LT FLOOR SUPPORT ANGLE IS CORRODED APPROXIMATELY BS 727+4 TO BS 760. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-60-53-1A-1, ORIGINAL MATERIAL THICKNESS WAS 0.040 IN REMAINING THICKNESS 0.000 IN ACCOMPLISHED SPSDR ASAA2015072212920Strip · corrodedAFT CARGO COMPARTMENT, RT CAP STRIP NR 4, AFT OF DOORWAY IS CORRODED. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS -.063. REMOVED -.012 REMAINING THICKNESS .051 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53, MAT ID 2024-T3, PSDR ASAA2015072212756Strip · corrodedAFT CARGO COMPARTMENT, RT CAPSTRIP NR 3, FWD OF DOORWAY IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL USING TOOL T82254 CAL DATE 11/25/2015, ORIGINAL THICKNESS .063", REMOVED .024" REMAINING THICKNESS .039" FOUND TO BE OUT OF ALLOWSDR ASAA2015072112937Frame · crackedCRACK INDICATIONS FOUND BS 520 ABOVE S-21L IN .500" HOLE, MARKED AT 7 & 9 O'CLOCK POSITION IN FWD PIT. ACFT GROUNDED. REPAIRED FRAME IAW EA 400-53EA-15603.SDR ASAA2015072112936Frame · crackedRIGHT BS 500B, .500" WIRE PENETRATION HOLE, ABOVE S-21R HAS CRACK INDICATION DUE TO NOISE. IN FWD PIT, MARKED. ACFT GROUNDED. CLEANED HOLE RT BS 500B, 500" WIRE PREPERATION, HOLE ABOVE S-21R IAW NDT MANUAL PART 6, 51-00-00 PROCEDURE 1, PARA 4, CRACK INDICATSDR ASAA2015072112934Strip · corrodedPARTS RACK, AFT CARGO FLOOR/SIDEWALL CAPSTRIP IS CORRODED. LT NR 2. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .020 REMAINING THICKNESS .049 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53 MATERIAL ID 2024-T3 PSDR ASAA2015072112933Strip · corrodedPARTS RACK, AFT CARGO FLOOR/SIDEWALL CAPSTRIP IS CORRODED, RT NR 3. ACFT GROUNDED. REMOVED CORROSION FROM PANEL, ORIGINAL THICKNESS .063. REMAINING THICKNESS .039 FOUND TO BE OUT OF LIMITS WITH MINIMUM THICKNESS REMAINING OF .057 IAW SRM 53-60-53, 10 PERCENTSDR ASAA2015072112694Support · corrodedAFT CARGO SIDEWALL CAPSTRIP IS CORROSION LT NR 1. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .022, REMAINING THICKNESS .041 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51SDR ASAA2015072112691Support · corrodedAFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063, REMOVED .031, REMAINING THICKNESS .032 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 53-6SDR ASAA2015072112690Support · corrodedAFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS 0.63, REMOVED .012, REMAINING THICKNESS .051 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10SDR ASAA2015072112689Support · corrodedAFT CARGO SIDEWALL CAPSTRIP IS CORRODED RT NR 1. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKESS .063, REMOVED .013, REMAINING THICKNESS .050 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10SDR ASAA2015072112688Support · corrodedAFT CARGO SIDEWALL CAPSTRIP IS CORRODED LT NR 4. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063 REMOVED .018. REMAINING THICKNESS .045 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51SDR ASAA2015072112674Support · corrodedAFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION. MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063. REMOVED .037, REMAINING THICKNESS .026. FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRMSDR ASAA2015072112673Support · corrodedAFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION. MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .011. REMAINING THICKNESS .052 FOUND TO BE PAST 10 PERCENT, ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM SDR ASAA2015072112672Support · corrodedAFT CARGO SIDEWALL CAPSTRIP IS CORRODED. ACFT GROUNDED. REMOVED CORROISON. MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .031. REMAINING THICKNESS .032, FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10SDR ASAA2015072112671Support · corrodedAFT CARGO SIDEWALL CAPSTRIP IS CORRODED. ACFT GROUNDED. REMOVED CORROISON. MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063, REMOVED .024. REMAINING THICKNESS .039. FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10-0SDR ASAA2015072012938Door Frame · gougedAFT CARGO DOOR, FWD DOOR FRAME, 2ND FROM UPPER DOOR STOP PIN FITTING GOUGED. APPROXIMATELY S-21R MARKED IN RED. DOT ATTACHED. ACT GROUNDED. R & R AFT CARGO DOOR FWD FRAME 2ND FROM UPPER STOP FITTING, BEAM B IAW SRM 51-40-02 AND 51-10-02, PARA 8, AND DWG 65-4SDR ASAA2015072012913Stop Fitting · gougedFORWARD CARGO DOOR, FWD DOOR FRAME, UPPER DOOR STOP PIN FITTING GOUGED DEEP. APPROXIMATELY S-20R, MARKED IN RED, DOT ATTACHED. ACFT GROUNDED. R & R CARGO DOOR FWD DOOR FRAME UPPER STOP PIN FITTING IAW SRM 51-10-02, PARA 8 AND 51-40-02, DWG 65-46921, REV K RESDR ASAA2015071812938Frame · crackedBS 500F RT FRAME IN FWD PIT, .500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 6 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. REPAIRED FUSELAGE FRAME AT BS 500F, S-20R-S-21R IAW EA 400-53EA-15605, REV: NEW.SDR ASAA2015071812919Frame · crackedBS 500B, LT FRAME IN FWD PIT, .500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 1 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. REPAIRED FUSELAGE FRAME AT BS 500B, S-20L TO S-21L IAW SRM 53-00-07-2R-B.SDR ASAA2015071812918Frame · crackedBS 500G, LT FRAME IN FWD CARGO BAY, A .500 INCH HOLE HAS CRACK INDICATION NOTED IN FRAME AT 10 O'CLOCK POSITION. REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. REPAIR FUSELAGE FRAME AT BS 500G LT SIDE S-20L TO S-21L IAW SRM 53-00-07-2SDR ASAA2015071812871Attach Bracket · gougedFWD CARGO DOORWAY FWD FRAME INTERNAL ATTACH BRACKET GOUGED, STREAMER ATTACHED, STR 24R. ACFT GROUNDED. R & R FWD CARGO DOORWAY, FW FRAME BACKUP FITTING IAW SRM 51-10-02, PARA 8 AND 51-40-02 AND BAC DWG 65-20722, REV B, REMOVED DOT N258 .SDR ASAA2015071812868Frame · crackedBS 500F STRINGERS 20 - 21L FRAME IN FWD CARGO BAY, A .500 HOLE HAS CRACK INDICATION NOTED IN FRAME AT 5 O'CLOCK POSITION. ACFT GROUNDED. REPAIRED THE FRAME IAW SRM 53-00-07-2R-13.SDR ASAA2015071812843Frame · crackedBS 500D LT FRAME IN FWD PIT, .500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 1 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. ACCOMPLISHED REPAIR BS 500D LT FRAME AT .500 HOLE AT STR 20L-STR 21L IAW SRM 53-00-07-2R-13SDR ASAA2015071812833Skin · crackedCRACK INDICATION ON LT HORIZONTAL STABILIZER LOWER SKIN, APPROXIMATELY STABILIZER BS 123, APPROXIMATELY 1" IN LENGTH, MARKED IN RED. ACFT GROUNDED. REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN IAW EA 400-55EA-15572, REV NEW AND REO-G19081, REV A.SDR ASAA2015071712915Hinge · crackedFORWARD SERVICE DOOR, LOWER HINGE HAS ONE FASTENER HOLE WITH A CRACK INDICATION. UNABLE TO DETERMINE LAYER. INDICATION POSITIONED AT 11 O'CLOCK IN HOLE, MARKED. ACFT GROUNDED. ACCOMPLISHED REPAIR TO FUSELAGE SKIN AND BEAR STRAP COMMON TO FORWARD GALLEY, R1, SDR ASAA2015071712869Fitting · crackedCRACK INDICATION ON LT UPPER, OTBD HORIZONTAL STABILIZER THRUST BEAM CORNER FITTING, APPROX 2" IN LENGTH. ACFT GROUNDED. ACCOMPLISHED REPLACEMENT OF LT SIDE HORIZONTAL STABILIZER THRUST BEAM CORNER FITTINGS IAW EA 400-55EA-15573, REV A.
Back to N708AS, cancelled Oct 9, 2018