# Service difficulty reports: N9332, cancelled Nov 19, 2013

A list on [N9332, cancelled Nov 19, 2013](https://openairdocs.org/deregistered/N9332-2013-11-19.md).

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

- [SDR 0602539968](https://openairdocs.org/sdr/0602539968.md): Boot · blown · Nov 28, 2006 · N9332 · Doug DC931 · Cabin Cooling System
  > DURING DESCENT FROM FL240, THE COCKPIT CREW NOTICED THAT THE CABIN ALTITUDE WAS CLIMBING AT 1,500 FEET PER MINUTE. AN EMERGENCY DESCENT TO 10,000 FEET WAS INITIATED. THE CABIN ALTITUDE REACHED AS HIGH AS 9,500 FEET BEFORE CONTROL WAS REGAINED AT ABOUT FL140.
- [SDR 0600739968](https://openairdocs.org/sdr/0600739968.md): Controller · malfunctioned · Apr 15, 2006 · N9332 · Doug DC931 · Cabin Pressure Controller
  > DURING A GRADUAL DESCENT OUT OF CRUISE THE CREW LOST CONTROL OF CABIN PRESSURIZATION. THE CABIN ALTITUDE CLIMBED TO 10,000 FT AT 9500 TO 1200 FPM. CREW INITIATED AN EMERGENCY DESCENT TO ATTEMPT REGAINING CONTROL OF CABIN PRESSURE AND PREVENT FURTHER CLIMB.
- [SDR 0500769968](https://openairdocs.org/sdr/0500769968.md): Cusp Web · cracked · Apr 14, 2005 · N9332 · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING "M" CHECK, FOUND CRACK IN RT CUSP WEB AT BS 834. REPAIRED PER EA 99-203527.
- [SDR 0100109968](https://openairdocs.org/sdr/0100109968.md): Valve · intermittent · Jan 7, 2001 · N9332 · Doug DC931 · Engine Anti-Icing System
  > DURING TAKEOFF ROLL, THE LEFT ENGINE LEFT ANTI-ICE VALVE LIGHT ILLUMINATED ABORTED TAKEOFF AT 100 KNOTS WITHOUT INCIDENT. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED AND OPERATED THE LEFT ENGINE LEFT ANTI-ICE VALVE. OPERAITONAL CHECK NORMAL.
- [SDR 0001469968](https://openairdocs.org/sdr/0001469968.md): Transceiver · failed · Apr 22, 2000 · N9332 · Doug DC931 · VHF Communications System
  > DURING CLIMB, THE NR 1 AND NR 2 RADIOS FAILED TO TRANSMIT AND HAD INTERMITTENT RECEPTION. AIRCRAFT RETURNED TO MSP AFTER A BRIEF RECEPTION FROM THE TOWER CLEARING THE FLIGHT TO LAND. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED BOTH VHF CONTROL PANELS AND AUD
- [SDR 9804929968](https://openairdocs.org/sdr/9804929968.md): Sensor · malfunctioned · Mar 22, 1998 · N9332 · Doug DC931 · Landing Gear Position and Warning
  > DURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CAPTAIN DECLARED AN EMERGENCY AND VERIFIED THROUGH PEEP HOLE THAT THE GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR PROXIMITY
- [SDR 9802369968](https://openairdocs.org/sdr/9802369968.md): Battery Pack · discharged · Feb 6, 1998 · N9332 · Doug DC931 · Emergency Lighting
  > DURING INSPECTION, THE FLIGHT ATTENDANT FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK OK.
- [SDR 9724229968](https://openairdocs.org/sdr/9724229968.md): Stall Warning · malfunctioned · Dec 23, 1997 · N9332 · Doug DC931 · Stall Warning System
  > STALL INDICATION FAILURE LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CROSS MONITOR PINS DOWN ON BOTH STALL WARNING COMPUTERS. RESET PINS. ALSO, REPLACED STALL WARNING TONE GENERATOR, OPERATIONA
- [SDR 9722739968](https://openairdocs.org/sdr/9722739968.md): Jamb · cracked · Nov 11, 1997 · N9332 · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING L-CHECK, FOUND CRACK IN LOWER RIGHT SIDE OF CABIN DOOR JAMB WEB FS 1010. REPAIRED PER EA 99-153348.
- [SDR 9722729968](https://openairdocs.org/sdr/9722729968.md): Pressure Web · cracked · Nov 7, 1997 · N9332 · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING L-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 110. REPAIRED PER EA 99-153337.
- [SDR 9716149968](https://openairdocs.org/sdr/9716149968.md): Controller · malfunctioned · Aug 23, 1997 · N9332 · Doug DC931 · Cabin Pressure Controller
  > AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE TESTED SYSTEM AND DISCREPANCY COULD NOT BE DUPLICATED ON GROUND. REPLACED CABIN PRESSURE CONTROLLER AND AMPLIFIER AS A PRECAUTION, OPERATIONAL CHECK
- [SDR 9707419968](https://openairdocs.org/sdr/9707419968.md): Battery Pack · discharged · Apr 8, 1997 · N9332 · Doug DC931 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND LEFT EXTERIOR NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.
- [SDR 9704359968](https://openairdocs.org/sdr/9704359968.md): Bulbs · failed · Feb 25, 1997 · N9332 · Doug DC931 · Landing Gear Position and Warning
  > DURING APPROACH, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH NOSE GEAR GREEN LIGHT BULBS, OPERATIONAL CHECK NORMAL ON
- [SDR 9702199968](https://openairdocs.org/sdr/9702199968.md): Power Supply · malfunctioned · Jan 30, 1997 · N9332 · Doug DC931 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL.
- [SDR 9701459968](https://openairdocs.org/sdr/9701459968.md): Batteries · discharged · Jan 25, 1997 · N9332 · Doug DC931 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EMERGENCY EXIT SIGN AT ROW 11 INOPERATIVE ON BOTH SIDES. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.
- [SDR 9701029968](https://openairdocs.org/sdr/9701029968.md): Batteries · discharged · Jan 19, 1997 · N9332 · Doug DC931 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.
- [SDR 9626979968](https://openairdocs.org/sdr/9626979968.md): Batteries · discharged · Dec 24, 1996 · N9332 · Doug DC931 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 5, 7 AND 9 INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL.
- [SDR 9626689968](https://openairdocs.org/sdr/9626689968.md): Batteries · discharged · Dec 19, 1996 · N9332 · Doug DC931 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 10 THROUGH 12 INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY. OPERATIONAL CHECK NORMAL.
- [SDR 9616199968](https://openairdocs.org/sdr/9616199968.md): Terminal Block · melted · Jul 22, 1996 · N9332 · Doug DC931 · Buffet/Galleys
  > FLIGHT ATTENDANT REPORTED THAT FORWARD GALLEY COFFEEMAKER HAD NO POWER. MAINTENANCE INSPECTED WIRING AND FOUND WIRING AND TERMINAL BLOCK TO COFFEEMAKER MELTED. DEFERRED COFFEEMAKER AND COLLARED CIRCUIT BREAKER. AWAITING PARTS FOR TERMINAL BLOCK REPLACEMENT.
- [SDR 9615539968](https://openairdocs.org/sdr/9615539968.md): Light Ballast · failed · Jul 17, 1996 · N9332 · Doug DC931 · Passenger Compartment Lighting
  > FLIGHT ATTENDANT REPORTED ELECTRICAL BURNING SMELL IN AFT CABN. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BALLAST FOR SIDEWALL LIGHTS AT ROW 16 RIGHT SIDE. DEFERRED LIGHTING PER MEL 33-2 AWAITING PARTS FOR REPLACEMENT OF
- [SDR 9615059968](https://openairdocs.org/sdr/9615059968.md): Batteries · discharged · Jul 11, 1996 · N9332 · Doug DC931 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.
- [SDR 9610189968](https://openairdocs.org/sdr/9610189968.md): Clips · out of adjust · May 4, 1996 · N9332 · Doug DC931 · Aerodynamic Fairings
  > DURING H-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE INTERIOR TAIL CONE HANDLE FROM THE CLIPS AND EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAIL CONE, SAME HANDLE. ADJUSTED THE CLIPS AND THE RELEASE SYSTEM PER MM 53-50-3, CHECKED OK.
- [SDR 9610099968](https://openairdocs.org/sdr/9610099968.md): Evac Slide · low pressure · May 4, 1996 · N9332 · Doug DC931 · Escape Slide
  > DURING LINE MAINTENANCE INSPECTION, FOUND THE TAILCONE EVACUATION SLIDE BOTTLE PRESSURE LOW. REPLACED SLIDE.
- [SDR 9610979968](https://openairdocs.org/sdr/9610979968.md): Longeron · broken tab · May 1, 1996 · N9332 · Doug DC931 · Wing, Longeron/Stringer
  > DURING H-CHECK, FOUND A 1.25 INCH BY.75 INCH TAB BROKEN OFF THE LEFT WING TRAILING EDGE STR 28L AT WS 164. REPAIRED STRINGER (P/N 5912156-39) PER EA 99-109002.
- [SDR 9609809968](https://openairdocs.org/sdr/9609809968.md): Evac Slide · failed batt chk · May 1, 1996 · N9332 · Doug DC931 · Escape Slide
  > DURING PERIODIC CHECK, FORWARD SERVICE DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE.
- [SDR 9610959968](https://openairdocs.org/sdr/9610959968.md): Longeron · cracked · Apr 30, 1996 · N9332 · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING H-CHECK, FOUND A CRACK IN THE LONGERON 30 KEEL CAP AT FS 606. REPAIRED CAP (P/N 9915525-509) PER EA 99-108990.
- [SDR 9610949968](https://openairdocs.org/sdr/9610949968.md): Skin · corroded · Apr 30, 1996 · N9332 · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING H-CHECK, FOUND CORROSION ON THE UNDER WING KEEL SKIN FS 676. REPAIRED SKIN (P/N 5911418-9) PER EA 99-109434.
- [SDR 9610939968](https://openairdocs.org/sdr/9610939968.md): Press Dome T Cap · corroded · Apr 30, 1996 · N9332 · Doug DC931 · Fuselage Main, Bulkhead
  > DURING H-CHECK, FOUND CORROSION ON THE PRESSURE DOME T-CAP AT FS 604, LONGERON 30. REPAIRED T-CAP (P/N 5914865-29) PER EA 99-109435.
- [SDR 9608479968](https://openairdocs.org/sdr/9608479968.md): Sill · corroded · Apr 10, 1996 · N9332 · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING M-CHECK, FOUND CORROSION ON THE FORWARD CARGO DOOR JAMB LOWER SILL AT FS 340. REPAIRED SILL (P/N 5912494) PER EA 99-109426.
- [SDR 9608419968](https://openairdocs.org/sdr/9608419968.md): Fitting · corroded · Apr 9, 1996 · N9332 · Doug DC931 · Wing Miscellaneous Structure
  > DURING M-CHECK, FOUND CORROSION ON THE WING BOX FITTING AT FS 598 TO 617, LBL 50. REPLACED FITTING PER SRM 51-30-5.
- [SDR 9608409968](https://openairdocs.org/sdr/9608409968.md): Fitting · cracked · Apr 9, 1996 · N9332 · Doug DC931 · Passenger/Crew Doors
  > DURING M-CHECK, FOUND CRACKS ON THE AFT CABIN DOOR RIGHT SIDE BEAM FITTINGS; NR 3 AND NR 4 UPPER AND LOWER. REPLACED FITTINGS (P/N 9915565-161, 99-15563-157 AND 99-15565-155) PER SRM 51-30-2, -3.
- [SDR 9609539968](https://openairdocs.org/sdr/9609539968.md): Door Jamb · corroded · Apr 6, 1996 · N9332 · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING H-CHECK, FOUND CORROSION IN THE FORWARD CARGO DOOR LOWER JAMB PAN. REPAIRED PAN (P/N 5912494) PER EA 99-109426.
- [SDR 9608069968](https://openairdocs.org/sdr/9608069968.md): Fitting · corroded · Apr 6, 1996 · N9332 · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING M-CHECK, FOUND CORROSION ON THE LONGERON 23L FITTING AT FS 996. REPLACED FITTING (P/N 3914654-1D).
- [SDR 9602859968](https://openairdocs.org/sdr/9602859968.md): Strut · reqd service · Feb 4, 1996 · N9332 · Doug DC931 · Nose/Tail Landing Gear Strut/Axle
  > AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT RAISE ON GEAR RETRACTION, NOSE WHEEL WAS STEERABLE. THIS CAUSED THE AIRCRAFT TO REMAIN IN GROUND MODE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. EMERGENCY EQUIPMENT WAS CALLED OUT ON STANDBY AS A PRECAU
- [SDR 9521719968](https://openairdocs.org/sdr/9521719968.md): Batteries · discharged · Dec 27, 1995 · N9332 · Doug DC931 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EMERGENCY EXIT LIGHTS VERY WEAK. REPLACED BATTERIES. OPERATIONAL CHECK GOOD.
- [SDR 9520309968](https://openairdocs.org/sdr/9520309968.md): Schrader Valve · leaking · Dec 14, 1995 · N9332 · Doug DC931 · Nose/Tail Landing Gear Strut/Axle
  > DURING CLIMB, THE AIRCRAFT FAILED TO SHIFT INTO FLIGHT MODE. PULLED GROUND SHIFT CIRCUIT BREAKERS TO GET AIRCRAFT TO SHIFT INTO FLIGHT MODE. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND NOSE STRUT SCHRADER VALVE LEAKING. REPLACED VALVE AND SE
- [SDR 9520159968](https://openairdocs.org/sdr/9520159968.md): Tire · flat spot · Dec 12, 1995 · N9332 · Doug DC931 · Tire Tube
  > DURING CLIMB, AIRCRAFT FAILED TO GROUND SHIFT AND A VIBRATION WAS FELT FROM THE NOSE WHEEL. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. INSPECTED NOSE GEAR GROUND SHIFT MECHANISM. UNABLE TO FIND ANY MALFUNCTIONS IN GROUND SHIFT MECHANISM. FOUND A
- [SDR 9518969968](https://openairdocs.org/sdr/9518969968.md): Starter · failed · Nov 21, 1995 · N9332 · Doug DC931 · Engine Starter
  > ON START, THE NR 1 ENGINE STARTER EXPERIENCED AN UNCONTAINED FAILURE. THE STARTER AND ADJACENT LINES AND DUCTS DAMAGED BY THE FAILURE WERE REPLACED WITH SERVICEABLE PARTS.
- [SDR 9516229968](https://openairdocs.org/sdr/9516229968.md): Fitting · corroded · Oct 12, 1995 · N9332 · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING D-CHECK, FOUND CORROSION ON THE JACK SUPPORT FITTING. REPLACED FITTING PER SRM 51-01 AND DWG 59-17491.
- [SDR 9513249968](https://openairdocs.org/sdr/9513249968.md): Skin · cracked · Aug 25, 1995 · N9332 · Doug DC931 · Spoilers
  > DURING A-CHECK, FOUND A 7 INCH CRACK IN THE LEFT INBOARD SPOILER LOWER SKIN. REPLACED SPOILER. MFG. P/N 5910055-515.
- [SDR 9507389968](https://openairdocs.org/sdr/9507389968.md): Prbc Valve · malfunctioned · May 4, 1995 · N9332 · Doug DC931 · Compressor Bleed Valve
  > ON SINGLE ENGINE TAXI, THE NR 2 ENGINE COMPRESSOR STALLED WHEN POWER WAS INCREASED. THE ENGINE WAS SHUTDOWN, STARTED THE NR 1 ENGINE AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE PRBC VALVE. THE ENGINE WAS RUNUP AND TESTED OK. AIRCRAFT RETURNED TO SER
- [SDR 9502869968](https://openairdocs.org/sdr/9502869968.md): Press Amplifier · malfunctioned · Feb 19, 1995 · N9332 · Doug DC931 · Cabin Pressure Control System
  > AUTO CABIN PRESSURIZATION FAILED AFTER TAKEOFF. CABIN PRESSURE WENT TO FULL INCREASE RELIEVING PRESSURE AT 8.06 PSI AND SHOWING NEGATIVE CABIN ALTITUDE. NORMAL CABIN PRESSURE WAS REGAINED USING MANUAL CONTROL BUT VERY DIFFICULT TO MAINTAIN. FLIGHT RETURNED
- [SDR 9502919968](https://openairdocs.org/sdr/9502919968.md): Skin · cracked · Feb 18, 1995 · N9332 · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING LINE CHECK, FOUND ONE INCH CRACK IN FUSELAGE SKIN BETWEEN FS 427 - 446 AND LONGERONS 29R - 30. REPAIRED PER SRM 53-04, FIG 12B.
- [SDR 9501859968](https://openairdocs.org/sdr/9501859968.md): Rectifier · malfunctioned · Feb 1, 1995 · N9332 · Doug DC931 · DC Rectifier/Converter
  > LOSS OF RIGHT TRANSFORMER RECTIFIER OCCURRED AFTER TAKEOFF. DC LOAD WAS INDICATING ZERO. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT TRANSFORMER RECTIFIER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.

## 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 = 'N9332' AND deregistration_id = 'N9332-2013-11-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N9332-2013-11-19/reports

---
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