# Service difficulty reports: N202SR, cancelled Dec 14, 2020

A list on [N202SR, cancelled Dec 14, 2020](https://openairdocs.org/deregistered/N202SR-2020-12-14.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR NSVA2011385](https://openairdocs.org/sdr/NSVA2011385.md): Tail Cone · misrepaired · Dec 30, 2011 · N202SR · Saab 340B · Aerodynamic Fairings
  > DOUBLER 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 STA
- [SDR NSVA2011382](https://openairdocs.org/sdr/NSVA2011382.md): Tail Cone · misrepaired · Dec 29, 2011 · N202SR · Saab 340B · Aerodynamic Fairings
  > DOUBLER/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 CUTO
- [SDR NSVA2011378](https://openairdocs.org/sdr/NSVA2011378.md): Tail Cone · misrepaired · Dec 29, 2011 · N202SR · Saab 340B · Aerodynamic Fairings
  > DOUBLER/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 CUTO
- [SDR NSVA2011375](https://openairdocs.org/sdr/NSVA2011375.md): Cargo Track · misrepaired · Dec 29, 2011 · N202SR · Saab 340B · Fuselage, Seat/Cargo Attach Fittings
  > PREVIOUS 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 NSVA2011384](https://openairdocs.org/sdr/NSVA2011384.md): Structure · damaged · Dec 28, 2011 · N202SR · Saab 340B · Engine Cowling System
  > FWD RT FWD O/B ATTACH HOLE ELONGATED. CONTROL# 202-67 REFERENCE TD. 340-54-11-37 DATED 12/13/.
- [SDR NSVA2011366](https://openairdocs.org/sdr/NSVA2011366.md): Rivet · damaged · Dec 28, 2011 · N202SR · Saab 340B · Fuselage Miscellaneous Structure
  > PREVIOUS 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 NSVA2011367](https://openairdocs.org/sdr/NSVA2011367.md): Frame · corroded · Dec 27, 2011 · N202SR · Saab 340B · Fuselage Main, Frame
  > THE 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 M
- [SDR NSVA2011363](https://openairdocs.org/sdr/NSVA2011363.md): Skin · corroded · Dec 26, 2011 · N202SR · Saab 340B · Fuselage Main, Plate/Skin
  > CORROSION 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 NSVA2011362](https://openairdocs.org/sdr/NSVA2011362.md): Skin · corroded · Dec 26, 2011 · N202SR · Saab 340B · Fuselage Main, Plate/Skin
  > CORROSION 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 NSVA2011361](https://openairdocs.org/sdr/NSVA2011361.md): Frame · cracked · Dec 26, 2011 · N202SR · Saab 340B · Fuselage Main, Frame
  > FUSELAGE 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 NSVA2011358](https://openairdocs.org/sdr/NSVA2011358.md): Skin · corroded · Dec 26, 2011 · N202SR · Saab 340B · Fuselage Main, Plate/Skin
  > FUSELAGE 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 NSVA2011355](https://openairdocs.org/sdr/NSVA2011355.md): Structure · cracked · Dec 23, 2011 · N202SR · Saab 340B · Fuselage Miscellaneous Structure
  > THE 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 NSVA2011354](https://openairdocs.org/sdr/NSVA2011354.md): Angle · corroded · Dec 23, 2011 · N202SR · Saab 340B · Fuselage Miscellaneous Structure
  > FLIGHT 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 NSVA2011349](https://openairdocs.org/sdr/NSVA2011349.md): Structure · corroded · Dec 23, 2011 · N202SR · Saab 340B · Fuselage Miscellaneous Structure
  > LT 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 NSVA2011347](https://openairdocs.org/sdr/NSVA2011347.md): Structure · damaged · Dec 23, 2011 · N202SR · Saab 340B · Fuselage Miscellaneous Structure
  > CARGO 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 NSVA20111223346](https://openairdocs.org/sdr/NSVA20111223346.md): Floorbeam · misrepaired · Dec 23, 2011 · N202SR · Saab 340B · Fuselage Main, Floor Beam
  > CARGO 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 LOCA
- [SDR NSVA2011372](https://openairdocs.org/sdr/NSVA2011372.md): Rivet · corroded · Dec 22, 2011 · N202SR · Saab 340B · Fuselage Miscellaneous Structure
  > RT 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 NSVA20111222370](https://openairdocs.org/sdr/NSVA20111222370.md): Floor Skin · corroded · Dec 22, 2011 · N202SR · Saab 340B · Fuselage Floor Panel
  > RIGHT COCKPIT FLOOR HAS MULTIPLE CORRODED RIVETS. REPAIRED.
- [SDR NSVA2011353](https://openairdocs.org/sdr/NSVA2011353.md): Seat Track · corroded · Dec 22, 2011 · N202SR · Saab 340B · Fuselage, Seat/Cargo Attach Fittings
  > CONTROL # 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 NSVA2011352](https://openairdocs.org/sdr/NSVA2011352.md): Frame · damaged · Dec 22, 2011 · N202SR · Saab 340B · Fuselage Miscellaneous Structure
  > CONTROL # 202-17: FRAME STATION 339 GOUGED AND KINKED. COMPLETED REPAIR IAW TD 340-53-11-09.
- [SDR NSVA2011350](https://openairdocs.org/sdr/NSVA2011350.md): Structure · corroded · Dec 22, 2011 · N202SR · Saab 340B · Fuselage Miscellaneous Structure
  > LT 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 NSVA2011348](https://openairdocs.org/sdr/NSVA2011348.md): Angle · corroded · Dec 22, 2011 · N202SR · Saab 340B · Fuselage Miscellaneous Structure
  > FLIGHT 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 NSVA2011343](https://openairdocs.org/sdr/NSVA2011343.md): Rib · cracked · Dec 22, 2011 · N202SR · Saab 340B · Wing, Rib/Bulkhead
  > UPPER 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 NSVA2011340](https://openairdocs.org/sdr/NSVA2011340.md): Cargo Track · damaged · Dec 21, 2011 · N202SR · Saab 340B · Fuselage, Seat/Cargo Attach Fittings
  > CARGO 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 NSVA2011335](https://openairdocs.org/sdr/NSVA2011335.md): Structure · chafed · Dec 19, 2011 · N202SR · Saab 340B · Nacelle/Pylon Miscellaneous Structure
  > CONTROL # 202-50: RT ENGINE INLET COMPARTMENT CHAFED IN CENTER DECK AREA. COMPLETED REPAIR IAW TD 340-54-11-02.
- [SDR NSVA2011331](https://openairdocs.org/sdr/NSVA2011331.md): Rivet · missing · Dec 14, 2011 · N202SR · Saab 340B · Fuselage Miscellaneous Structure
  > WATER 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 T
- [SDR NSVA2011106](https://openairdocs.org/sdr/NSVA2011106.md): Oil System · low · May 10, 2011 · N202SR · Saab 340B · Turbine Engine Oil System
  > CREW 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 EXTINGU
- [SDR NSVA2011072](https://openairdocs.org/sdr/NSVA2011072.md): Strut · low pressure · Apr 4, 2011 · N202SR · Saab 340B · Landing Gear System
  > AFTER 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 SWINGS
- [SDR NSVA2011016](https://openairdocs.org/sdr/NSVA2011016.md): Autopilot Sys · malfunctioned · Feb 1, 2011 · N202SR · Saab 340B · Autopilot System
  > RETURNED 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 NSVA201085](https://openairdocs.org/sdr/NSVA201085.md): Battery Pack · discharged · May 27, 2010 · N202SR · Saab 340B · Emergency Lighting
  > FLOOR 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 NSV2008F00022](https://openairdocs.org/sdr/NSV2008F00022.md): Smoke Detector · false indication · Aug 27, 2008 · N202SR · Saab 340B · Smoke Detection
  > AVIONICS 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 NSV2008F00018](https://openairdocs.org/sdr/NSV2008F00018.md): Connector · unknown · Aug 10, 2008 · N202SR · Saab 340B · Smoke Detection
  > AVIONICS 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 NSV2008F00017](https://openairdocs.org/sdr/NSV2008F00017.md): Power Supply · discharged · Aug 7, 2008 · N202SR · Saab 340B · Emergency Lighting
  > MAIN 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 NSV2008F00015](https://openairdocs.org/sdr/NSV2008F00015.md): Connector · contaminated · Aug 5, 2008 · N202SR · Saab 340B · Fire Protection System Wiring
  > TAIL 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 NSV2008F00012](https://openairdocs.org/sdr/NSV2008F00012.md): Cowling · damaged · Jul 24, 2008 · N202SR · Saab 340B · Nacelle/Pylon, Main Frame
  > LT ENGINE INBOARD COWLING DAMAGED. REMOVED AND REPLACED LT INBOARD COWLING IAW SAAB MM 71-10-05-08. (A)
- [SDR NSVA20070230](https://openairdocs.org/sdr/NSVA20070230.md): Smoke Detector · loose · Sep 18, 2007 · N202SR · Saab 340B · Smoke Detection
  > CARGO COMPARTMENT SMOKE DETECTION SYSTEM DOES NOT TEST. FOUND SMOKE DETECTOR LOOSE RESECURED, OPS CHECK GOOD.
- [SDR NSVA20070219](https://openairdocs.org/sdr/NSVA20070219.md): Cooling Fan · failed · Aug 27, 2007 · N202SR · Saab 340B · Air Distribution Fan
  > AVIONICS 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 NSVA20070110](https://openairdocs.org/sdr/NSVA20070110.md): Switch · malfunctioned · Apr 23, 2007 · N202SR · Saab 340B · Gust Lock Damper System
  > GUST 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 SERVICE
- [SDR NSVA20070088](https://openairdocs.org/sdr/NSVA20070088.md): Switch · malfunctioned · Apr 6, 2007 · N202SR · Saab 340B · Gust Lock Damper System
  > GUST 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 END
- [SDR NSVA20070039](https://openairdocs.org/sdr/NSVA20070039.md): Control Quadrant · unknown · Feb 14, 2007 · N202SR · Saab 340B · Engine Controls
  > CONFIG 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 R
- [SDR NSVA20070004](https://openairdocs.org/sdr/NSVA20070004.md): Smoke Detector · no test · Jan 7, 2007 · N202SR · Saab 340B · Smoke Detection
  > FOUND 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 NSVA200600228](https://openairdocs.org/sdr/NSVA200600228.md): Connector · loose · Dec 11, 2006 · N202SR · Saab 340B · Fire Protection System Wiring
  > FOUND FIRE TEST RIGHT SIDE FAILED. FOUND RT FIRE LOOP CONNECTOR LOOSE TIGHTENED AND SATISFIED IAW SAAB AMM CHP 26-11-05, NO DISCREPANCY.
- [SDR NSVA200600087](https://openairdocs.org/sdr/NSVA200600087.md): Wire · malfunctioned · Jun 21, 2006 · N202SR · Saab 340B · Engine Indicating System Wiring
  > AFTER 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. GRC
- [SDR NSVA200600076](https://openairdocs.org/sdr/NSVA200600076.md): Unknown · unknown · Jun 15, 2006 · N202SR · Saab 340B · Standard Practices/Structures
  > LT ENGINE ITT REACHED 942 DEGREES FOR ABOUT 5 SECONDS. PERFORMED CAPPED AND UNCAPPED RUNS. DELTA FOUND TO BE 4.92, OPS CHECK OK.
- [SDR 06052006A](https://openairdocs.org/sdr/06052006A.md): Turbine Blades · damaged · Jun 4, 2006 · N202SR · Saab 340B · Turbine Section
  > ON 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 O
- [SDR 05262006B](https://openairdocs.org/sdr/05262006B.md): Pressure Switch · faulty · May 24, 2006 · N202SR · Saab 340B · Engine Oil Pressure
  > LT ENGINE OIL PRESSURE LIGHT ON. R&R NR 1 ENGINE OIL PSI SWITCH PN 8346-501 OPS CHECK GOOD.
- [SDR 03012006C](https://openairdocs.org/sdr/03012006C.md): Warning System · malfunctioned · Feb 25, 2006 · N202SR · Saab 340B · Engine Oil Indicating System
  > NR 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 01252006B](https://openairdocs.org/sdr/01252006B.md): Indicator · inoperative · Jan 22, 2006 · N202SR · Saab 340B · Engine EGT/TIT Indicating System
  > LOST 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 11172005A](https://openairdocs.org/sdr/11172005A.md): Warning System · false activation · Nov 14, 2005 · N202SR · Saab 340B · Central Warning
  > ABORTED TAKEOFF DUE TO CONFIG WARNING DURING TAKEOFF. PERFORMED OPERATIONAL TEST OF TAKEOFF CONFIG WARNING. NO DEFECTS NOTED AT THIS TIME, OPS CHECK GOOD.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N202SR-2020-12-14/reports

---
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