N640AE
Service difficulty reports · 282
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 = 'N640AE' AND registry_match = 'registration' 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 = 'N640AE' AND registry_match = 'registration' 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 HNAA2021083100403Skin · gougedCARGO DOOR LOWER INNER SKIN GOUGED AT JUNCTURE OF HB3 AND VB4. ACCOMPLISHED REPAIR ON CARGO DOOR INNER SKIN AT HB3 AND VB2 (LOCATION OF DAMAGE REVISED, SEE WIP #2) IAW SRM 52-30-01 STEP 12 FIGURE 213 AND EO1-52-21-0208.SDR HNAA2021083100402Skin · gougedCARGO DOOR LOWER INNER SKIN GOUGED AT HB4 FWD END. REPAIRED THE CARGO DOOR LOWER INNER SKIN AT HB4 FORWARD END IAW PIEDMONT EO1-52-21-0207SDR HNAA2021083100401Profile · corrodedCARGO DOOR LOWER PROFILE CORRODED AT FWD THREE PANEL SCREW HOLES. REMOVED AND REPLACED CARGO DOOR LOWER PROFILE IAW EMB145 SRM 51-40-02SDR HNAA2021083100400Bushing · crackedR/H ENG FWD PYLON LOWER YOKE FWD FITTING POSSIBLE CRACK. COMPLIED WITH FCD1-54-21-0017 RT PYLON REPLACEMENT OF FWD PYLON LINKAGE FITTINGS AND BUSHINGSSDR HNAA2021083100399Bushing · migratedRIGHT AILERON OTBD PCA ATTACHMENT FITTING HAS MIGRATED HAT BUSHING. REMOVED RH AILERON OTBD PCA ATTACHMENT FITTING HAT BUSHING FOUND FITTING TO HAVE ELONGATED HOLE IAW AMM 20-10-08. REMOVED RIGHT AILERON OUTBD PCA ATTACHMENT FITTING IAW SRM 51-40-02, AMM 20-1SDR HNAA2021083100398Rib · crackedRIGHT WING RIB 21 CRACKED INSIDE 651CB. PERFORMED DOUBLER REPAIR AT R/H WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM 4 FIGURE203 DET. C AND EO1-57-21-0213.SDR HNAA2021083100394Skin · crackedL/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVETS FR-77 IN THREE (3) PLACES. REPAIRED THE L/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVET AT FR-77 AT ONE (1) LOCATION IAW PIEDMONT EO1-53-21-0223, TWO (2) LOCATIONS FOUND NOT TO BE CRACKED,SDR HNAA2021083100393Skin · crackedL/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVETS FR-78 IN THREE (3) PLACES. REPAIRED THE L/H EXTERNAL FUSELAGE SKIN AROUND RIVET AT FR-78 AT ONE (1) LOCATION IAW EO1-53-21-0223, TWO (2) LOCATIONS FOUND NOT TO BE CRACKED,SDR HNAA2021083100392Support · crackedNLG LEG HYDRAULIC HOSE SUPPORT IS CRACKED ON FWD SIDE OF PRESSURE BULKHEAD. REMOVED AND BEGAN INSTALLATION OF NLG LEG HYDRAULIC HOSE SUPPORT ON FWD SIDE OF PRESSURE BULKHEAD IAW EMB 145 SRM 51-40-02.SDR HNAA2021030100064B-Nut · looseBLEED 1 LEAK WARNING MESSAGE AFTER TAKEOFF WITH HIGH THRUST SETTING. CREW REPORTED HIGH THRUST SETTING MESSAGE IS IN VIEW LOW THRUST SETTING MESSAGE CLEARS. TIGHTENED LOOSE B-NUT ON T FITTING. GROUND RAN A/C. OPS AND LEAK CHECK GOOD. OK FOR SERVICESDR HNAA2020111600328Autopilot Sys · malfunctionedCLOSE ON MISSED APPROACH MODERATE TURBULENCE CAUSED A/P FA IL EICAS WARNING. 28781 00 JDH. HISTORY: FACT 15NOV20 02:54 SBY. PERFORMED AUTOPILOT FUNCTIONAL TEST, IAW AMM 22-11-00. FUNCTIONAL TEST OK, OPERATIONS CHECK GOOD.SDR HNAA2020060200162Pressure Switch · defectiveBLEED 1 VALVE FAIL WHEN TAKEOFF POWER APPLIED. REJECTED TAKE OFF. R & R NR 1 PRESSURE SWITCH. SEE HA-300 SEQ NR 3 FOR WORK PERFORMED. OPS CK GOOD. AIRCRAFT OK FOR SERVICE AT THIS TIME. CLEAR MEL 36-1-1.SDR HNAA2020033100114Clamp · looseBLEED 1 VLV FAIL MSG FOLLOWED BY BLEED 1 LEAK MSG. INSPECTED BLEED VLV ONE AND FOUND LOOSE CLAMPS. TIGHTEND CLAMPS AND PERFORMED OPS CHECK IN REF TO 36-00-00-700-803A. NO MSGS ON EICAS OR PRESENT ON CMCSDR HNAA2020033110114Unknown · malfunctionedCAPT STEERING DISCONNECT SWITCH ON YOKE IS INOP. DISCREPANCY VERIFIED. R&R'D SWITCH IAW AMM 32-50-08. NO FIX. OPENED PANELS 223ELW AND 224 ERW AND SWAPPED RELAYS K0366 AND K0650.NO FIX. SWAPPED K0007 AND K0244.NO FIX. RETURNED RELAYS TO ORIGIONAL POSITION AND SDR HNAA2020010600003Uplock · crackedNDIS 640 33-20 0030560 03JAN20 MDT CLOSE
FRONT BEAM OF NLG UPLOCK BOX CRACKED
FACT 03JAN20 08:50 MDT
REMOVED FRONT BEAM OF NLG UPLOCK BOX. FABRICATED HOLES IN NEW BEAM AND INSTALLED HI-LOKS AND TOP ROW OF
RIVETS IRT STANDARD PRACTICES ANDSDR HNAA2019090900259Thermostat · malfunctionedPDIS 640 30-10 1826421 07SEP19 ART CLOSE DURING ICING, WG A/ICE FAIL MSG ON EICAS, CREW C/W QRH, MESSAGE CLEARED. FACT WING A/I LEAK MESSAGE ON CMC. FOUND BLEED PIPE BETWEEN PACK VLV #1 AND TEMP CONTROL VLV #1 TO BE LEAKING. R&R'D PIPE IRT AMM 21-60-0SDR HNAA2019062600183Display · malfunctionedFO,S PFD IS BLINKING WITH ODOR IN FLIGHT DECK. R & R COPILOTS PFD AS REQUIRED. OPS CHECK GOOD. IAW AMM 34-22-01 PERFORMED OPS CHECK IAW 34-22-00-700-80-1A, OK FOR SERVICE.SDR HNAA2019031100068Contactor · burnedPDIS 640 21-01 1934001 08MAR19 BDL CLOSE DURING CLIMB AT FL180 AND PERFORMING ICE PROTECTION TEST A BURNING ODOR WAS OBSERVED AND DID NOT DISSIPATE, WITH SLIGHT EYE IRRITATION. FACT 08MAR19 19:44 BDL FOUND WINDSHIELD HEAT NR 1 CONTACTOR BURNT, R\R WINSDR HNAA2019030600064Warning System · activatedPDIS 640 52-30 1933971 05MAR19 PHF ASSGN BAG DOOR OPEN WARNING EICAS INFLT HISTORY: NO, HISTORY: MEL 05MAR19 16:48 PHF C06409 52-3-2 BAGGAGE DOOR WARNING / POSITION WARNING.SDR HNAA2019012100020Thermostat · defectivePDIS 640 36-20 1858973 18JAN19 PHL CLOSE BLEED 1 OVERTEMP WARNING MESSAGE DISPLAYED WHEN ICING ENCOUNTERED. HISTORY: 07,17JAN FACT 19JAN19 18:21 PHL R&R FAN AIR THERMOSTAT, REF LP 1858982.SDR HNAA2018121800318Filter · not reportedPDIS 640 30-14 1858621 15DEC18 PHL CLOSE
SHORTLY AFTER TAKEOFF ICE COND - A/I INOP EICAS MSG, FOLLOWED BY BLD 1 OVTEMP.
26905 00 DS
FACT 15DEC18 16:34 PHL
RNR FAN AIR VALVE FILTER ISDR HNAA2018121800321Lamp · inoperativeNDIS 640 33-51 0021060 14DEC18 RIC CLOSE
EMERGENCY LIGHT ON MAIN DOOR ENTRANCE CEILING DOES NOT ILLUMINATE
FACT 14DEC18 06:58 RIC
R&R MAIN DOOR ENTRANCE EMERGENCY CEILING LIGHT LAMP ISDR HNAA2018120500302Switch · malfunctionedPDIS 640 52-40 1720451 30NOV18 CLT CLOSE
FUEL DOOR OPEN EICAS IN FLT DOOR FOUND TO BE CLOSED
FACT 30NOV18 05:01 ROA
R/R'D FUELING DOOR MICRO SWITCH PER MM 52-78-01, OPS CK GOOD.SDR HNAA2018112000287Ground Wire · damagedPDIS 640 21-25 1720271 17NOV18 PHL CLOSE
AT 33000FT. AIRCRAFT SLOWLY LOST PRESSURIZATION WHILE IN AUTO-MODE. ON DESCENT PRESSURIZATION STABALIZED AT 10000FT.
28487 00 MM
FACT 19NOV18 01:4SDR HNAA2018102600268Door Sill · corrodedCARGO ENTRANCE SILL CORRODED. CLASSIFIED AS LEVEL 1 CORROSION PER MP&P SECTION 5.11.17 FIGURE 3. R&R CARGO ENTRANCE SILL IAW SRM 51-40-02.SDR HNAA2018102400264Skin · crackedDURING HEAVY CHECK MAINTENANCE FOUND CARGO DOOR HANDLE CUTOUT SKIN TO BE CRACKED ON AFT UPPER CORNER. CORRECTIVE ACTION WAS TO FABRICATE AND INSTALL DOUBLER, FILLER FOR REPAIR ON CARGO DOOR EXTERNAL SKIN HANDLE CUTOUT IAW ETD2018-145-110759.SDR HNAA2018102400267Fitting · crackedDURING HEAVY CHECK MAINTENANCE FOUND MACHINED FITTING BETWEEN FRAME 19 AND 20 AT STRINGER 3L TO BE CRACKED. CORRECTIVE ACTION WAS TO REMOVE CRACKED MACHINED FITTING AND INSTALL SERVICEABLE MACHINED FITTING P/N 145-24109-603 BETWEEN FRAME 19 AND 20 AT STRINGER SDR HNAA2018102400265Fitting · corrodedDURING HEAVY CHECK MAINTENANCE FOUND FR 65 SHEAR CLIP CORRODED AT LOWER FWD CORNER OF CARGO DOOR CUTOUT. CORRECTIVE ACTION DETERMINED CORROSION TO BE LEVEL 1, REMOVED DAMAGED FR 65 SHEAR CLIP, AND INSTALLED SERVICEABLE FR 65 SHEAR CLIP PN 145-25175-601 AT LOWESDR HNAA2018102400266Rib · crackedDURING HEAVY CHECK MAINTENANCE FOUND CRACK ON LEFT ELEVATOR INBOARD HINGE CUTOUT INBOARD NOSE RIB. CORRECTIVE ACTION WAS TO REMOVE AND REPLACE RIB WITH P/N 145-30264-601 IAW SRM 51-20-03 AND 51-40-02.SDR HNAA2018080210177Unknown · odorUNKNOWN BURNING SMELL DETECTED IN FLIGHT DECK AND CABIN IN CRUISE FLIGHT, WENT AWAY AFTER 3 MINUTES LATER. INSPECTED FLIGHT DECK AND CABIN FOR POSSIBLE DEFECTS. NONE FOUND. BOTH ENGINES RUN UP AND BLEEDS SELECTED FOR BOTH ENGINES. RAN BOTH AC PACKS AND APU BLESDR HNAA2018071800153Warning System · false activationCARGO DOOR INDICATES OPEN AFTER PUSHBACK. CYCLED DOOR OPEN AND CLOSED. OPS CHECK GOOD DOOR INDICATION OKAY. OKAY FOR SERVICE.SDR HNAA2018071300150Inverter · inoperativeEMERGENCY LIGHT ON CEILING ABOVE ROW 1A AND BELOW COCKPIT DOOR INOP. REMOVED AND PLACED INVERTER 1 IAW AMM 33-50-11-000-801-A AND 33-50-11-400-801A. OPS CHECK GOOD.SDR HNAA2018071300149Fuse · inoperativeEMERGENCY LIGHT AT LT EMERGENCY EXIT (UPPER) INOP. REMOVED AND REPLACED PICO FUSE IN BATTERY NR 3 POWER SUPPLY REINSTALLED BATTERY NR 3 POWER SUPPLY ASSY IAW AMM 33-50-04-400-8-01A OPS CHECK GOOD.SDR HNAA2017121500389Power Supply · inoperativeNDIS 640 33-51 0013530 08DEC17 SBY CLOSE
FWD EMERGENCY EXIT LIGHT UNDER COCKPIT DOOR INOP.
FACT 08DEC17 13:29 SBY
SLAVED IN EMERGENCY EXIT LIGHT SIGN NO FIX. R&R EMER
GENCY BATT POWER SUPPLY 1 IAW AMM 33-50-04-000-SDR HNAA2017121100388Power Supply · inoperativeL/H AND R/H EXTERIOR OVER WING EMERGENCY LIGHTS INOP..........R&R #4 EMERGENCY BATTERY AND POWER SUPPLY ASSY WITH RETAINED HARDWARE AND SECURED OVERHEAD PANEL AND LIGHT COVER WITH RETAINED HARDWARESDR HNAA2017022200059Line · rupturedDURING CLIMB, AT APPROXIMATELY FL260, HYD 1 LOW QTY MESSAGE APPEARED. FOLLOWED BY AILERON SYSTEM 1 INOPERATIVE AND RUDDER SYS 1 INOPERATIVE MESSAGES. CREW FOLLOWED QRH. SELECTED NR 1 HYD ELECTRIC PUMP OFF AND ALTERNATE EXTENDED GEAR. FOUND RUPTURED LINE TO LSDR HNAA2016113000363Unknown · odorELECTRICAL ODOR AT ROW 11BC AND 12BC, NEAR SIDEWALL. MAINTENANCE INSPECTED. NO DAMAGE FOUND.SDR HNAA2016101400317Unknown · odorIN FLIGHT DURING APPROACH, A STRONG ODOR WAS DETECTED IN THE COCKPIT FOR 15 SECONDS AND SELF EXTINGUISHED. AFTER LANDING, FLIGHT ATTENDANT CONFIRMED ABNORMAL ODOR ON LEFT SIDE OF AIRCRAFT IN THE SAME PHASE OF FLIGHT. INSPECTED LEFT AND RIGHT RELAY PANELS, WISDR HNAA2016071800220Oil System · fluctuatesDURING TAKEOFF ROLL, FO REPORTED NR 1 ENGINE OIL PRESSURE ROSE INTO YELLOW. GROUND RAN AIRCRAFT PERFORMED PROPER ENGINE WARM UP PROCEDURE. SYSTEM PRESSURE AND TEMP STABILIZED AS REQUIRED IN ACCEPTABLE RANGE. ALL SYSTEMS OPS NORMAL AT THIS TIME OKAY FOR SERVISDR SIMA20160414008Skin · corrodedSSI 53-30-07 CARGO UNDER FLOOR SKIN IS CORRODED ON BOTH SIDES OF FRAME 67, BETWEEN STRINGERS 21L - 21R. ACCOMPLISHED REPAIR TO CARGO UNDER FLOOR SKIN IAW ERS-EM-53MR-2017.SDR SIMA20160413007Hinge · corrodedPASSENGER DOOR UPPER NUTPLATE HOLES HAVE SURFACE CORROSION. ACCOMPLISHED PERMANENT REPAIR OF PAX DOOR UPPER NUTPLATE HOLES IAW ERS-EM-52MR-530.SDR SIMA20160411007Wire · brokenEMERGENCY LIGHT STRIP NR 3, BROKEN WIRE AT BASE ASSEMBLY. FOUND ON CLOSE UP. R & R EMER LIGHT STRIP NR 3 IAW AMM 33-50-12.SDR SIMA20160407003Floor Support · corrodedFOUND CORROSION ON LT OMEGA BEAM BETWEEN FRAME 33 & 34. REPAIRED LT OMEGA BEAM IAW SRM 53-00-10 FIGURE 202 SHEET 1.SDR SIMA20160407004Floor Support · corrodedFOUND CORROSION ON CTR OMEGA BEAM BETWEEN FRAME 33 & 34. REPAIRED CTR OMEGA BEAM IAW SRM 53-00-10 FIGURE 203 SHEET 1.SDR SIMA20160407005Floor Support · corrodedFOUND CORROSION ON LT OMEGA BEAM BETWEEN FRAME 28 & 29. INSTALLED DOUBLER, FILLER, SHIMS ON LT OMEGA BEAM IAW SRM 53-00-10 & 51-40-02.SDR SIMA20160407007Door Frame · corrodedSERVICE DOOR CUT OUT STRUCTURE LOWER AFT NUTPLATE HOLE PREVIOUS REPAIR HAS CORROSION. INSTALLED EXTERNAL DOUBLER, INTERNAL DOUBLER & FILLER FOR SERVICE DOOR CUT OUT STRUCTURE LOWER AFT NUTPLATE HOLE IAW SRM 53-00-04 FIG 208.SDR SIMA20160407006Floor Support · corrodedFOUND CORROSION ON CTR OMEGA BEAM BETWEEN FRAME 28 & 29. INSTALLED DOUBLER, EXTERNAL ANGLE, FILLER, SHIM ON CTR BEAM IAW SRM 53-00-10 & 51-40-02.SDR SIMA20160318009Rib · crackedLEFT WING SPAR NR 1 RIB 9, LOWER FLANGE CRACK AT FASTENER HOLE AREA. ACCOMPLISHED REPAIR TO LT WING SPAR NR 1 RIB 9, LOWER FLANGE AT FASTENER HOLE AREA IAW ERS-EM-57MR-605. SEE WIPS & TASK FOR DETAILS.SDR SIMA20160318010Structure · corrodedPASSENGER DOOR UPPER NUTPLATE HOLES HAVE SURFACE CORROSION. ACCOMPLISHED PERMANENT REPAIR OF PAX DOOR UPPER NUTPLATE HOLES IAW ERS-EM-52MR-530.SDR SIMA20160318011Floor Skin · corrodedSSI 53-30-07 CARGO UNDER FLOOR SKIN IS CORRODED ON BOTH SIDES OF FRAME 67, BETWEEN STRINGERS 21L - 21R. ACCOMPLISHED REPAIR TO CARGO UNDER FLOOR SKIN ON BOTH SIDES OF FRAME 67, BETWEEN STRINGERS 21L - 21R IAW ERS-EM-53MR-2017.
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