N202SR, cancelled Dec 14, 2020
Service difficulty reports · 49
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 = 'N202SR' AND deregistration_id = 'N202SR-2020-12-14' 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 = 'N202SR' AND deregistration_id = 'N202SR-2020-12-14' 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 NSVA2011385Tail Cone · misrepairedDOUBLER REPAIR TO UPPER LT TAIL CONE SKIN AT STA 793 IS NOT IN DAMAGE LOG OR ON FILE. THE RIVET PATTERN AROUND THE CUTOUT IS IRREGULAR AND DOES NOT HAVE A DOUBLE ROW AT BOTTOM EDGE OF CUTOUT. THE FORWARD EDGE OF THIS REPAIR IS AT THE SKIN SPLICE OF FRAME STASDR NSVA2011382Tail Cone · misrepairedDOUBLER/TRIPLER REPAIR TO RT UPPER TAIL CONE JUST BELOW VERTICAL STAB FAIRING NOT IN DAMAGE LOG OR ON FILE. THIS REPAIR IS MISSING MULTIPLE RIVETS IN THE FIELD. THERE IS A DENT IN THE AFT LOWER AREA OF THE PATCH AT STA 823. THE RIVET PATTERN AROUND THE CUTOSDR NSVA2011378Tail Cone · misrepairedDOUBLER/TRIPLER REPAIR TO RT UPPER TAIL CONE JUST BELOW VERTICAL STAB FAIRING NOT IN DAMAGE LOG OR ON FILE. THIS REPAIR IS MISSING MULTIPLE RIVETS IN THE FIELD. THERE IS A DENT IN THE AFT LOWER AREA OF THE PATCH AT STA 823. THE RIVET PATTERN AROUND THE CUTOSDR NSVA2011375Cargo Track · misrepairedPREVIOUS CARGO SEAT RAIL SPLICE LBL 18 FUSE STA 621 TO 687 NOT IN DAMAGE LOG, U-BEAM SPLICE DOES NOT HAVE SUFFICIENT NAS 1580 BOLT COUNT AND INCORRECT FASTENERS I/B AND O/B SEAT RAIL FLANGES. U-BEAM SPLICE IS NOT MINIMUM LENGTH PER TD 340-53-11-59. ACCEPTED SDR NSVA2011384Structure · damagedFWD RT FWD O/B ATTACH HOLE ELONGATED. CONTROL# 202-67 REFERENCE TD. 340-54-11-37 DATED 12/13/.SDR NSVA2011366Rivet · damagedPREVIOUS DOUBLER/TRIPLER REPAIR TO RT FUSELAGE AT STA 339 TO 363, SL1615 TO 1617 HAS ONE RIVET THAT IS MISSING THE SHOP HEAD. REFER TO SAAB STATEMENT SDS 023471, TD 340-53-11-98 AND MM409 #406962 FOR CORRECTIVE ACTION UNDER CONTROL #202-22.SDR NSVA2011367Frame · corrodedTHE AFT UPPER FLANGE ON THE BOTTOM FRAME AT ATA 258 HAS PREVIOUS REPAIR NOT IN DAMAGE LOG OR ON FILE. BOTH FORWARD AND AFT UPPER FLANGES HAVE SEVERE CORROSION FROM LBL 10.5 TO RBL 15.13. NUMEROUS RIVET HOLES IN THE VERTICAL WEB FROM THE PREVIOUS REPAIR ARE MSDR NSVA2011363Skin · corrodedCORROSION ON RT FUSELAGE SKIN JUST ABOVE WINDOW DOUBLER EDGE AT SL1607 FROM STA 583 TO 595.5 REFER TO SAAB STATEMENT 340SDS023472 PARA 1, DATED 12-16-2011, TD 340-53-11-06 AND MM409#406977 FOR REPAIR DETAILS UNDER CONTROL # 202-33 AREA 2.SDR NSVA2011362Skin · corrodedCORROSION ON RT FUSELAGE SKIN JUST ABOVE WINDOW DOUBLER EDGE AT SL1607 FROM STA 565.5 TO 621.5 REFER TO SAAB STATEMENT 340SDS023472 PARA 1 DATED 12-16-2011, TD 340-53-11-06 AND MM409#406977 FOR REPAIR DETAILS UNDER CONTROL # 202-33.SDR NSVA2011361Frame · crackedFUSELAGE BOTTOM FRAME AT STA 294 HAS MODERATE TO SEVERE CORROSION FROM LBL 25 TO RBL 10.5 AND A CRACK AT RBL 19.5. REFER TO SAAB STATEMENT 340SDS023466 DATED 12-14-2011, TD 340-53-11-93 AND MM409#407125 FOR REPAIR DETAILS UNDER CONTROL# 202-25.SDR NSVA2011358Skin · corrodedFUSELAGE SKIN UNDER RT ICE SHIELD NR 8 HAS 15 SMALL AREAS OF PITTING CORROSION AND 1 SMALL AREA OF PITTING CORROSION UNDER ICE SHIELD NR 7. REFER TO SAAB STATEMENT 340SDS023481, PARA 1 DATED 12-16-2011, TD 3450-53-11-05 AND MM409#406963 UNDER CONTROL #202-24 SDR NSVA2011355Structure · crackedTHE COCKPIT FLOOR IS CORRODED AND OR CRACKED UNDER THE TWO SNAPS LOCATED OB OF THE AFT OB CORNER OF THE RT CONTROL COLUMN AND JUST AFT OF STA 186. REFERENCE TD 340-53-11-27 DATED 12-23-11 AND MM409# 407400 FOR REPAIR DETAILS UNDER CONTROL# 202-12.SDR NSVA2011354Angle · corrodedFLIGHT DECK ENTRANCE RISER AND THE ATTACHED FLOORBOARD MOUNT ANGLE AT STA 225 HAVE SEVERE CORROSION. REFERENCE TD 340-53-11-95 DATED 12-22-11 AND MM409#407174 UNDER CONTROL # 202-29 FOR CORRECTIVE ACTION.SDR NSVA2011349Structure · corrodedLT COCKPIT FLOOR CORROSION AT AND UNDER PREVIOUS DOUBLER REPAIRS AND SNAP FASTENERS IB, OB AND FORWARD OF CONTROL COLUMN. (REF ITEMS 1 THROUGH 5 & 7 THROUGH 9 OF CA-M268 FOR CONTROL #202-11) REFERENCE TD 340-53-11-27 AND MM409#407274 FOR REPAIR DETAILS.SDR NSVA2011347Structure · damagedCARGO FLOOR FRAME AT STA 694 IS KINKED FROM LBL 8.75 TO LBL 17. REF TO TD 340-53-11-92 AND MM409#407231 FOR REPAIR DETAILS UNDER CONTROL #202-14.SDR NSVA20111223346Floorbeam · misrepairedCARGO FLOORBEAM AT BS 694 IS KINKED FROM LBL 8.75 TO LBL 17. PREVIOUS REPAIRS NOT IN DAMAGE LOG OR ON FILE. BOTH REPAIRS ARE MISSING THE REINFORCEMENT ANGLES AND SHIMS PER SRM 53-70-30-206 AND HAVE CORROSION AT THE CENTER NUT PLATE. REPAIR 1 (ITEM 1) IS LOCASDR NSVA2011372Rivet · corrodedRT COCKPIT FLOOR HAS MULTIPLE CORRODED RIVETS, 3 PREVIOUS REPAIRS FORWARD OF STA 186 ARE NOT IN DAMAGE LOG. THE O/B MOST REPAIR DOES NOT TIE INTO THE RIVET ROW OF THE ADJACENT VERTICAL WALL PANEL. REFERENCE TD # 340-53-11-27 DATED 12-10-11, MM409#407280 FOR SDR NSVA20111222370Floor Skin · corrodedRIGHT COCKPIT FLOOR HAS MULTIPLE CORRODED RIVETS. REPAIRED.SDR NSVA2011353Seat Track · corrodedCONTROL # 202-61: LT FWD SEAT RAIL AT LBL 18.3 FROM STA 297-352 CORRODED. COMPLETED SEAT RAIL SPLICE REPAIR IAW TD 340-53-11-59.SDR NSVA2011352Frame · damagedCONTROL # 202-17: FRAME STATION 339 GOUGED AND KINKED. COMPLETED REPAIR IAW TD 340-53-11-09.SDR NSVA2011350Structure · corrodedLT COCKPIT FLOOR CORROSION UNDER SNAP FASTENERS AFT AND OB OF CONTROL COLUMN. (REF ITEM 10 OF CA-M268 FOR CONTROL #202-11) REFERENCE TD 340-53-11-27 AND MM409#407274 FOR REPAIR DETAILS.SDR NSVA2011348Angle · corrodedFLIGHT DECK ENTRANCE RISER AND THE ATTACHED FORWARD FLOORBOARD MOUNT ANGLE AT STA 225 HAVE SEVERE CORROSION REFERENCE TD 340-53-11-95 409#407174 CONTROL #202-29.SDR NSVA2011343Rib · crackedUPPER AND LOWER ENDS OF I/B AND O/B CLOSING RIBS ON RT WING I/B LEADING EDGE 611AR ARE CRACKED. REF TD 400-57-11-17 AND MM409# 100232 FOR REPAIR DETAILS. CONTROL # 209-3.SDR NSVA2011340Cargo Track · damagedCARGO SEAT TRACK AT BL 0 WAS REPLACED FROM STA 631.5 TO 686.888. THIS REPAIR APPEARS TO CONFORM TO THE PRINCIPLES OF TD 340-53-11-59. REF TD 340-53-11-59 DATED 12-16-11 AND MM409 # 407314.SDR NSVA2011335Structure · chafedCONTROL # 202-50: RT ENGINE INLET COMPARTMENT CHAFED IN CENTER DECK AREA. COMPLETED REPAIR IAW TD 340-54-11-02.SDR NSVA2011331Rivet · missingWATER SERVICE RELOCATION MOD DOUBLER NOT ENTERED INTO DAMAGE LOG. DOUBLER IS LOCATED FROM STA 248 TO 262, BETWEEN SL1622 AND SL1636. 1.5" ABOVE SKIN SPLICE AT SL1622. REF SB 340-38-007. FOUND DOUBLER TO BE MISSING RIVETS AROUND INTERNAL DOUBLER PLATE. REF TSDR NSVA2011106Oil System · lowCREW RECEIVED RT ENG OIL PRESSURE MASTER WARNING DURING INITIAL CLIMB. ALL RT ENG INDICATIONS WERE NORMAL EXCEPT ENG OIL PRESSURE WHICH WAS FLUCTUATING FROM 50 PSI TO BOTTOM OF GREEN ARC (30 PSI) AND IN SOME CASES INTO YELLOW ARC. THEN MASTER WARNING EXTINGUSDR NSVA2011072Strut · low pressureAFTER TAKEOFF, CREW COULD NOT RAISE THE LANDING GEAR. THE AIRCRAFT RETURNED TO BGM AND LANDED SAFELY WITHOUT FURTHER INCIDENT. CREW CONFIRMED THAT GEAR PIN WAS NOT THE ISSUE. SERVICED STRUT, INSPECTED, LUBED AND RETORQUED INTERCONNECT, PERFORMED GEAR SWINGSSDR NSVA2011016Autopilot Sys · malfunctionedRETURNED TO GATE DUE TO PRE TAKEOFF FLIGHT CHECKS CREW FELT A BINDING IN THE YOKE. FOUND TO BE AUTO PILOT, MEL'D AUTO PILOT.SDR NSVA201085Battery Pack · dischargedFLOOR PROXIMITY ESCAPE PATH LIGHTS ARE DIM AT SEATS 5D AND 6D AND OVERHEAD EMERGENCY LIGHT IS DIM AT SEAT 6A. REMOVED AND REPLACED NR 3 EMERGENCY POWER SUPPLY BATTERY PACK.SDR NSV2008F00022Smoke Detector · false indicationAVIONICS SMOKE LIGHT ILLUMINATED. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR (PN 72-111211-000) SN A4091, SN ON A5414, DONE IAW 26-13-06-04, OPS CHECK GOOD. (K)SDR NSV2008F00018Connector · unknownAVIONICS SMOKE LIGHT CAME ON INFLIGHT FOR A FEW SECONDS. RESET CONNECTOR TO SMOKE DETECTOR IAW SAAB AMM 28-13-00. OPS CHECKED GOOD. (S)SDR NSV2008F00017Power Supply · dischargedMAIN EMERGENCY LIGHTS IN CABIN OUT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AT SEAT 5A CWC 33-50-026. OPS CHECK GOOD. P/N ON/OFF 60-1321-1, S/N: OFF 17486, S/N: ON 12291. (S)SDR NSV2008F00015Connector · contaminatedTAIL PIPE HOT LIGHT (RT) CAME ON AFTER TAKEOFF THEN WENT OUT AND STAYED OUT. CLEANED CONNECTORS AT DISCONNECTS WITH CONTACT CLEANER TO REMOVE MOISTURE, PERFORMED ENG RUN, NO FAULTS NOTED AMM 30-12-00. (S)SDR NSV2008F00012Cowling · damagedLT ENGINE INBOARD COWLING DAMAGED. REMOVED AND REPLACED LT INBOARD COWLING IAW SAAB MM 71-10-05-08. (A)SDR NSVA20070230Smoke Detector · looseCARGO COMPARTMENT SMOKE DETECTION SYSTEM DOES NOT TEST. FOUND SMOKE DETECTOR LOOSE RESECURED, OPS CHECK GOOD.SDR NSVA20070219Cooling Fan · failedAVIONICS VENT FAN LIGHT ILLUMINATED AND CB G-11 POPPED ACCOMPANIED BY HOT ELECTRICAL ODOR. AVIONICS VENT FAN MEL'D, WILL BE REPLACED AT NEXT MAINTENANCE BASE VISIT.SDR NSVA20070110Switch · malfunctionedGUST LOCK LIGHT ON DURING FLIGHT CONTROL CHECK. REINSTALLED RUDDER GUST LOCK ACTUATOR IAW SAAB 340 AMM 27-72-10-04, OPS CHECK GOOD TS IAW AMM 72-27-00-00. FOUND WARNING SWITCH 3CF STICKING. REMOVED AND REPLACED GUST LOCK WARNING SW PN MS25348-1 WITH SERVICESDR NSVA20070088Switch · malfunctionedGUST LOCK LIGHT ILLUMINATED WHEN GUST LOCK IS RELEASED. TS TO QUADRANT GUST LOCK SWITCH QUADRANT REMOVED AND REPLACED IAW 76-10-05-09 OPS AND RIGGING KS STILL NEED TO BE DONE. CONTROL LEVERS, INSTALLED COTTER PINS ON BOTH CONTROL LEVERS AND GUST LOCK ROD ENDSDR NSVA20070039Control Quadrant · unknownCONFIG WARNING ON TAKEOFF ROLL. VERIFIED POWER TO RELAY 8 GA W PINX1. VERIFIED GROUND TO RELAY AT 8GA PIN X2.5. VERIFIED GROUNDS FROM RELAY 8GA PINS D1 AND A2. VERIFIED OPERATION OF L POWER LEVER QUADRANT SWITCH PINS 5 AND 6 AT P1. VERIFIED OPERATION OF RSDR NSVA20070004Smoke Detector · no testFOUND CARGO SMOKE TEST FAILED. REMOVED AND REPLACED CARGO AFT SMOKE DETECTOR, OM CARGO OM REF WITH SMM 26-13-15-4. OPS CHECK GOOD, PN ON/OFF CGAB1201-01, SN ON 981, SN OFF 1079.SDR NSVA200600228Connector · looseFOUND FIRE TEST RIGHT SIDE FAILED. FOUND RT FIRE LOOP CONNECTOR LOOSE TIGHTENED AND SATISFIED IAW SAAB AMM CHP 26-11-05, NO DISCREPANCY.SDR NSVA200600087Wire · malfunctionedAFTER TAKEOFF, NG FLUCTUATED ERRATICALLY BETWEEN 0-97% THEN DROPPED TO 0%. AUTO COARSEN HIGH LIGHT FLUCTUATED ON AND OFF ALSO. DURING LOW POWER SETTING NG NORMAL (LEFT NG GAUGE). REMOVED AND REPLACED CABLE ASSY (GREEN), P/N 6039T34P01, OPS CHECK GOOD. GRCSDR NSVA200600076Unknown · unknownLT ENGINE ITT REACHED 942 DEGREES FOR ABOUT 5 SECONDS. PERFORMED CAPPED AND UNCAPPED RUNS. DELTA FOUND TO BE 4.92, OPS CHECK OK.SDR 06052006ATurbine Blades · damagedON TAKEOFF 200 FEET OFF THE GROUND LT ENGINE SHUTDOWN. FOUND EXTENSIVE BLADE DAMAGE ON THE FIRST STAGE TURBINE IN THE HOT SECTION GOING AFT. FOUND DURING BORESCOPE INSPECTION. R&R LT ENGINE IAW 72-00-00 LEAK AND OPS CHECKED GOOD. PN ON/OFF 6058T83G01, SN OSDR 05262006BPressure Switch · faultyLT ENGINE OIL PRESSURE LIGHT ON. R&R NR 1 ENGINE OIL PSI SWITCH PN 8346-501 OPS CHECK GOOD.SDR 03012006CWarning System · malfunctionedNR 2 ENGINE CHIP DETECTOR LIGHT ON INTERMITTENTLY. PERFORMED INSPECTION IAW GE MM 72-00-00 PAGE 128-144 INSPECTION OF OIL SCREENS. PERFORMED OIL CHANGE ON NR 2 ENGINE PER DOM REQUEST.SDR 01252006BIndicator · inoperativeLOST ITT NEEDLE AND DIGITAL INDICATION ON TAKEOFF ROLL. REMOVED AND REPLACED ITT GAUGE IAW 77-20-05 PN ON/OFF 10227N01TOO SN ON 157A, SN OFF 124A, OPS CHECK GOOD.SDR 11172005AWarning System · false activationABORTED TAKEOFF DUE TO CONFIG WARNING DURING TAKEOFF. PERFORMED OPERATIONAL TEST OF TAKEOFF CONFIG WARNING. NO DEFECTS NOTED AT THIS TIME, OPS CHECK GOOD.
Back to N202SR, cancelled Dec 14, 2020