# Service difficulty reports: N301AE, cancelled Aug 14, 2008

A list on [N301AE, cancelled Aug 14, 2008](https://openairdocs.org/deregistered/N301AE-2008-08-14.md).

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

- [SDR SIMA200816502](https://openairdocs.org/sdr/SIMA200816502.md): Floor Support · corroded · Jun 6, 2008 · N301AE · Saab 340B · Fuselage Miscellaneous Structure
  > DURING A HMBV INSPECTION, A PREVIOUS REPAIR ON THE GALLEY FLOOR FRAME 258.0 WAS FOUND CORRODED WITH LEVEL TWO CORROSION. REMOVED THE DAMAGED FILLER TO REMOVED THE CORROSION. FABRICATED NEW ANGLE FILLER, DRILLED AND TREATED NEW PART. DONE IAW SAAB 340 SRM (
- [SDR SIMA200742301](https://openairdocs.org/sdr/SIMA200742301.md): Bleed Valve · malfunctioned · Nov 5, 2007 · N301AE · Saab 340B · Compressor Bleed Valve
  > BEFORE TAKEOFF CHECKLIST NOTED RIGHT BLEED VALVE NOT CLOSED FOUND CB H16 POPPED. CONTACTED MOC. ADVISED TO RESET CB. CB H16 POPPED A SECOND TIME. CREW ELECTED TO RETURN TO THE GATE. REMOVED AND REPLACED PRSO VALVE IAW SAAB340 AMM 36-11-05-02. OPS CK NORMA
- [SDR SIMA200629002](https://openairdocs.org/sdr/SIMA200629002.md): Warning Light · false indication · Oct 16, 2006 · N301AE · Saab 340B · Smoke Detection
  > LAVATORY SMOKE LIGHT ON CENTRAL WARNING PANEL. NO SMOKE NOTED IN LAVATORY, ISSUED MEL 26-2. (M)
- [SDR SIMA200620502](https://openairdocs.org/sdr/SIMA200620502.md): Windshield · failed · Jul 22, 2006 · N301AE · Saab 340B · Flight Compartment Windows
  > CAPT FORWARD WINDSHIELD OUTER PLY SHATTERED. (M)
- [SDR SIMA200530001](https://openairdocs.org/sdr/SIMA200530001.md): Odor · detected · Oct 24, 2005 · N301AE · Saab 340B · Air Distribution System
  > FOUND CREW REPORTED STRONG SMOKE SMELL IN COCKPIT AND FORWARD CABIN. FOLLOWED CHECKLIST AND COULD NOT DETERMINE SOURCE. INSPECTED AVIONICS RACK AIR DISTRIBUTION SYSTEM. PERFORMED OPERATIONAL CHECK OF THE BLEED AND AIR DISTRIBUTION SYSTEM WITH NO DISCREPANCI
- [SDR SIMA200520301](https://openairdocs.org/sdr/SIMA200520301.md): Line · ruptured · Jul 15, 2005 · N301AE · Saab 340B · Hydraulic System, Main
  > DISC, UPON GEAR SELECTION UP THE HYDRAULIC QUANTITY STARTED DROPPING TO -0-, MANUAL PUMP OVERRIDE FAILURE. REPLACED RUPTURED NOSE LANDING GEAR RETRACT/EXTENSION ACTUATOR HYDRAULIC LINE. LEAK AND OPS CHECK GOOD. AC RETURNED TO SERVICE. (K)
- [SDR SIMA200518608](https://openairdocs.org/sdr/SIMA200518608.md): Skin · chafed · Jun 29, 2005 · N301AE · Saab 340B · Nacelle/Pylon, Plate/Skin
  > THE LT IB NACELLE WAS FOUND CHAFED AT THE FILLET FAIRING SEAL CONTACT POINT. BLENDED THE DAMAGED AREA. FABRICATED AND INSTALLED A REPAIR DOUBLER. WORK DONE IAW SRM. (K)
- [SDR SIMA200518606](https://openairdocs.org/sdr/SIMA200518606.md): Floorbeam · corroded · Jun 23, 2005 · N301AE · Saab 340B · Fuselage Main, Floor Beam
  > FLOORBEAM AT STA 225.0 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. FABRICATED A FILLER, DOUBLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)
- [SDR SIMA200518605](https://openairdocs.org/sdr/SIMA200518605.md): Floorbeam · corroded · Jun 23, 2005 · N301AE · Saab 340B · Fuselage Main, Floor Beam
  > THE GALLEY FLOOR FRAME AT STA 272 WAS FOUND CORRODED. BLENDED THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (K)
- [SDR SIMA200518604](https://openairdocs.org/sdr/SIMA200518604.md): Frame · damaged · Jun 23, 2005 · N301AE · Saab 340B · Fuselage Main, Frame
  > THE CARGO SIDEWALL FRAME AT STA 686.888 WAS FOUND BENT AND DENTED. RECONTOURED THE FRAME. PREPARED AND INSTALLED REPAIR SECTION OF NEW FRAME. REPAIR DONE IAW SRM. (K)
- [SDR SIMA200518603](https://openairdocs.org/sdr/SIMA200518603.md): Frame · damaged · Jun 22, 2005 · N301AE · Saab 340B · Fuselage Main, Frame
  > THE CARGO SIDEWALL FRAME AT STA 640 WAS FOUND DENTED. RECONTOURED THE DENT. FABRICATED AND INSTALLED REPAIR SECTION OF NEW FRAME. REPAIR DONE IAW SRM. (K)
- [SDR SIMA200518602](https://openairdocs.org/sdr/SIMA200518602.md): Frame · corroded · Jun 22, 2005 · N301AE · Saab 340B · Fuselage Main, Frame
  > THE RT SIDEWALL CARGO FRAME AT STA 677 WAS FOUND DENTED. RECONTOURED THE DENT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (K)
- [SDR SIMA200518601](https://openairdocs.org/sdr/SIMA200518601.md): Web · corroded · Jun 22, 2005 · N301AE · Saab 340B · Fuselage Miscellaneous Structure
  > THE REINFORCEMENT WEB AT STA 294 WAS FOUND CORRODED. BLENDED THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW REPAIR. (K)
- [SDR SIMA200518607](https://openairdocs.org/sdr/SIMA200518607.md): Floorbeam · damaged · Jun 21, 2005 · N301AE · Saab 340B · Fuselage Main, Floor Beam
  > THE CARGO FLOOR FRAME AT STA 710.0 WAS FOUND BENT IN 2 AREAS. RECONTOURED BOTH DENTS. FABRICATED AND INSTALLED 2 DOUBLERS AND 2 ANGLES. REPAIR DONE IAW SRM. (K)
- [SDR SIMA200536101](https://openairdocs.org/sdr/SIMA200536101.md): Battery Pack · discharged · Dec 22, 2004 · N301AE · Saab 340B · Emergency Lighting
  > EMERGENCY LIGHTS AT ROW 9 AND 10 WILL NOT ILLUMINATE DURING TEST. EXIT SIGN OVER SEAT 8A DOES NOT ILLUMINATE. REPLACED BATTERY PACK. IAW MM OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K)
- [SDR SIMA200111802](https://openairdocs.org/sdr/SIMA200111802.md): Light · inoperative · Apr 28, 2001 · N301AE · Saab 340B · Emergency Lighting
  > LAX - FLT 3067 - EMERGENCY ARMED LIGHT INOPERATIVE ON FLIGHT ATTENDANTS PANEL. REMOVED AND REPLACED BULB IAW AMM 23-30-00. (M)
- [SDR SIMA0622](https://openairdocs.org/sdr/SIMA0622.md): Warning Light · illuminated · Mar 3, 2001 · N301AE · Saab 340B · Brake Anti-Skid Section
  > DFW - FLT 3769 - ON APPROACH, WHEN GEAR WAS LOWERED CREW RECEIVED AN ANTI-SKID CAUTION INDICATION ON CWP. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR SIMA0503](https://openairdocs.org/sdr/SIMA0503.md): Power Supply · discharged · Feb 19, 2001 · N301AE · Saab 340B · Emergency Lighting
  > JFK - FLT 5013 - CREW REPORTED THE EMERGENCY LIGHT OVER CABIN DOOR IS DIM AND FLICKERS. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT 21LN. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR SIMA2914](https://openairdocs.org/sdr/SIMA2914.md): Light · malfunctioned · Oct 17, 2000 · N301AE · Saab 340B · Emergency Lighting
  > PVD - FLT 5045 - CREW REPORTED EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY, SUSPECT BATTERIES RECHARGED DURING FERRY FLIGHT. EMERGENCY LIGHTS OPERATIONAL. CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR SIMA2552](https://openairdocs.org/sdr/SIMA2552.md): Bulb · inoperative · Sep 11, 2000 · N301AE · Saab 340B · Emergency Lighting
  > ALB - FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 7BC IS INOPERATIVE. MAINTENANCE REPLACED BULB IN FLOOR LIGHT AT SEAT 7BC. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR SIMA1611](https://openairdocs.org/sdr/SIMA1611.md): Control Panel · inoperative · Jun 9, 2000 · N301AE · Saab 340B · Elevator Control System
  > JFK - FLT 5069 - ABORTED TAKEOFF DUE TO CONFIGURATION WARNING, SPLIT PITCH, STANDBY UNCOMMANDED MOVEMENT. C/A - REPLACED TRIM CONTROL PANEL IAW SAAB340BA MM 27-32-05. GROUND OPS CHECKED GOOD. (X)
- [SDR SIMA1383](https://openairdocs.org/sdr/SIMA1383.md): Handle · inoperative · May 17, 2000 · N301AE · Saab 340B · Landing Gear Door Retract Section
  > JFK - FLT 5143 - RIGHT LANDING LIGHT DID NOT ILLUMINATE WHEN GEAR HANDLE WAS SELECTED DOWN. ABORTED APPROACH. AIRCRAFT WENT AROUND AND CREW PERFORMED LANDING GEAR CHECK LIST. GEAR CAME DOWN AND LOCKED, THREE GREEN. REMOVED AND REPLACED LANDING GEAR CONTROL
- [SDR SIMA0821](https://openairdocs.org/sdr/SIMA0821.md): Bulb · inoperative · Mar 22, 2000 · N301AE · Saab 340B · Emergency Lighting
  > DFW - FLT 3679 - EMERGENCY FLOOR LIGHT AT 9B INOPERATIVE. REMOVED AND REPLACED BULB AT 9B. OPS CHECK GOOD. (M)
- [SDR SIMA3641](https://openairdocs.org/sdr/SIMA3641.md): Connector · disconnected · Dec 28, 1999 · N301AE · Saab 340B · Landing Gear Position and Warning
  > DFW - FLT 3296 - UNSAFE RIGHT GEAR INDICATION. PERFORMED EMERGENCY PROCEDURES. PULLED EMERGENCY HANDLE FOR GEAR DOORS. AIRCRAFT LANDED WITHOUT EVENT. INSPECTED RIGHT GEAR ASSY AND FOUND MLG DRAG BRACKE CANNON PLUG DISCONNECTED. RECONNECTED CANNON PLUG, RE
- [SDR SIMA992652](https://openairdocs.org/sdr/SIMA992652.md): Wire · broken · Sep 22, 1999 · N301AE · Saab 340B · Light System Wiring
  > JFK - FLT 5006 - EMERGENCY OVERHEAD LIGHTS AT SEATS 8BC, 10BC, AND 12 BC DO NOT ILLUMINATE. REPAIRED BROKEN WIRES AT FUSE HOLDERS 71 AND 72 LN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR SIMA992231](https://openairdocs.org/sdr/SIMA992231.md): Brakes · req'd service · Aug 11, 1999 · N301AE · Saab 340B · Landing Gear Brake System
  > JFK - FLT 4925 - LEFT BRAKE GRABS EXCESSIVELY. RIGHT BRAKE DOES NOT GRAB AT ALL. INSPECTED AND BLED ALL FOUR BRAKES. LEAK AND FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR SIMA990893](https://openairdocs.org/sdr/SIMA990893.md): Angle · chafed · Mar 30, 1999 · N301AE · Saab 340B · Nacelle/Pylon Structure
  > ABI - DURING A MBV INSPECTION, FOUND CHAFE ON THE LEFT NACELLE INLET COMPARTMENT LOWER LONGERON. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED A REINFORCEMENT L ANGLE.090 THICK. APPLIED SURFACE T
- [SDR SIMA990892](https://openairdocs.org/sdr/SIMA990892.md): Skin · chafed · Mar 30, 1999 · N301AE · Saab 340B · Nacelle/Pylon, Plate/Skin
  > ABI - DURING A MBV INSPECTION, FOUND CHAFE ON THE LEFT NACELLE OUTBOARD INNER SKIN. BLENDED THE CHAFE AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED A REINFORCEMENT DOUBLER.025. APPLIED SEALANT TO THE CONTACT SURFAC
- [SDR SIMA990891](https://openairdocs.org/sdr/SIMA990891.md): Skin · dented · Mar 30, 1999 · N301AE · Saab 340B · Fuselage Main, Plate/Skin
  > ABI - DURING A MBV INSPECTION, FOUND DENTS ON RIGHT FUSELAGE SKIN PANEL STATION 327.5 BETWEEN SL 1620 AND 1622. CLEANED AREA, CUT OUT DAMAGE, AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATION OF CRACKS. DEBURRED AND APPLIED ALODINE TO THE CUT OUT E
- [SDR SIMA983121](https://openairdocs.org/sdr/SIMA983121.md): Engine · malfunctioned · Nov 8, 1998 · N301AE · Saab 340B · Engine (Turbine/Turboprop)
  > ALB - FLT 4812 - EN ROUTE TO JFK FROM YUL, THE LEFT ENGINE OIL PRESSURE STARTED DROPPING. WHEN IT GOT TO THE BOTTOM OF THE GREEN ARC, THEY SHUT DOWN THE ENGIEN AND DIVERTED TO ALB. ENGINE REQUIRED OVER FIVE QUARTS OF OIL. REMOVED AND REPLACED THE LEFT ENGIN
- [SDR SIMA980862](https://openairdocs.org/sdr/SIMA980862.md): Bulb · failed · Mar 27, 1998 · N301AE · Saab 340B · Emergency Lighting
  > DFW - FLT 3935 - WHITE FLOOR LIGHT NEAR ROW 10 INOP MEL'D PER 33-15-2. RETURNED A/C TO SERVICE. RAID BULB AT ROW 10 ON THE FLOOR PROX LIGHTING. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M)
- [SDR SIMA980102](https://openairdocs.org/sdr/SIMA980102.md): Connector · loose · Jan 10, 1998 · N301AE · Saab 340B · Emergency Lighting
  > DFW - FLT 3775 - LEFT OVERWING EMERGENCY LIGHT IS INOP. MAINTENANCE FOUND CONNECTOR PIN HAD BACKED OUT IN CONNECTOR AT LIGHT ASSY. REINSTALLED PIN IN CONNECTOR, PERFORMED OPERATIONAL CHECK AND RETURNED TO A/C TO SERVICE. (M)
- [SDR SIMA952661](https://openairdocs.org/sdr/SIMA952661.md): Engine · seized · Sep 23, 1995 · N301AE · Saab 340B · Engine (Turbine/Turboprop)
  > DFW - FLT NR 3503 - DURING TAKEOFF ENGINE NR 2 LOST POWER, TAKEOFF ABORTED. MAINTENANCE FOUND FIRST STAGE ROTOR DAMAGED. MAINTENANCE REPLACED NR 2 ENGINE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR SIMA952341](https://openairdocs.org/sdr/SIMA952341.md): Smoke Detector · malfunctioned · Aug 22, 1995 · N301AE · Saab 340B · Smoke Detection
  > SGF - FLT NR 4186 - DURING TAKEOFF ROLL, THE AFT SMOKE DETECTOR LIGHT ILLUMINATED, THE TAKEOFF WAS ABORTED AND THE AFT CARGO FIRE BOTTLE WAS DISCHARGED. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF HEAT OR FIRE, REPLACED AFT SMOKE DETECTOR AND FIRE BOTTLE.
- [SDR SIMA950991](https://openairdocs.org/sdr/SIMA950991.md): Hmu · malfunctioned · Apr 9, 1995 · N301AE · Saab 340B · Fuel Controlling System
  > ORD - FLT 4351 - DURING CRUISE FLIGHT, PILOT UNABLE TO CONTROL ENGINE NR 2 TORQUE WITH POWER LEVER, TORQUE WAS FIXED AT 8046. TORQUE MOTOR LOCK-OUT NO EFFECT. FLIGHT TURNED BACK TO ORD. NR 2 ENGINE SHUT DOWN IN FLIGHT. EMERGENCY DECLARED, AIRCRAFT LANDED W

## 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 = 'N301AE' AND deregistration_id = 'N301AE-2008-08-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N301AE-2008-08-14/reports

---
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