# Service difficulty reports: N897US, cancelled Jan 17, 2018

A list on [N897US, cancelled Jan 17, 2018](https://openairdocs.org/deregistered/N897US-2018-01-17.md).

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

- [SDR USAAF01061](https://openairdocs.org/sdr/USAAF01061.md): Fire Detector · malfunctioned · Jul 30, 2001 · N897US · Fokker F28MK0100 · Fire Detection
  > TRI - FLT 896 - EN ROUTE PIT-CLT, AT FL310, RECEIVED AN APU FIRE WARNING. THE FIRE EXTINGUISHING SYSTEM AUTOMATICALLY DISCHARGED. THE FLIGHT DIVERTED TO TRI AND LANDED SAFELY. MAINTENANCE INSPECTED THE APU ENCLOSURE AND THE TAIL COMPARTMENT. NO SIGNS OF A
- [SDR USAAF01051](https://openairdocs.org/sdr/USAAF01051.md): Extinguisher · discharged · Jul 24, 2001 · N897US · Fokker F28MK0100 · Fire Protection System
  > CLT-IND - FLT 476 - THE WATER FIRE EXTINGUISHER DISCHARGED INTO THE LAVATORY TRASH BIN IN FLIGHT. NO SMOKE OR FIRE WAS DETECTED. THE FLIGHT LANDED WITHOUT INCIDENT IN IND. MAINTENANCE REPLACED THE WATER BOTTLE EXTINGUISHER. OK FOR SERVICE. (M)
- [SDR USAAF01048](https://openairdocs.org/sdr/USAAF01048.md): Odor · detected · Jul 17, 2001 · N897US · Fokker F28MK0100 · Air Distribution System
  > STL-CLT - FLT 1249 - THE LAVATORY SMOKE ALARM BEGAN TO CHIME AND AN ODOR OF SMOKE WAS PRESENT IN THE AFT CABIN AREA DURING CLIMB. THE FLIGHT RETURNED TO FIELD IN STL AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN ENGINES AND APU. NO ODOR WAS DETECTED. THE TA
- [SDR USAAF01049](https://openairdocs.org/sdr/USAAF01049.md): Timer · malfunctioned · Jul 17, 2001 · N897US · Fokker F28MK0100 · Potable Water System
  > STL-PIT - FLT 9281 - SLIGHT FUMES WERE NOTICED COMING FROM BOTH LAVATORIES, AND SMOKE DETECTORS ACTIVATED FOR A BRIEF TIME DURING CRUISE FLIGHT. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT AND RIGHT LAVATORY FAUCET TIMERS. LEAK
- [SDR USAAF00069](https://openairdocs.org/sdr/USAAF00069.md): Strut · discharged · Sep 15, 2000 · N897US · Fokker F28MK0100 · Nose/Tail Landing Gear Strut/Axle
  > PIT-BNA - FLT 1532 - THE NOSE LANDING GEAR FAILED TO COME DOWN DURING APPROACH. RECEIVED A GEAR UNSAFE WARNING. THE FLIGHT PERFORMED A GO-AROUND AND CYCLED THE LANDING GEAR AGAIN. THE LANDING GEAR THEN OPERATED NORMALLY AND THREE GREEN LANDING GEAR INDICATI
- [SDR USAAF00043](https://openairdocs.org/sdr/USAAF00043.md): Brake Assy · malfunctioned · Jun 4, 2000 · N897US · Fokker F28MK0100 · Landing Gear Brake System
  > CMH-PHL - FLT 835 - ON LANDING ROLL, EXCESSIVE BRAKE PRESSURE REQUIRED TO STOP AIRCRAFT ON CAPTAINS SIDE. FIRST OFFICERS BRAKES SEEM NORMAL AT TAXI SPEED. MAINTENANCE INSPECTED PEDAL TORQUE TUBES, SPRINGS, AND ROD ENDS. OPERATIONALLY CHECKED BRAKES. LUBED
- [SDR USAAF00040](https://openairdocs.org/sdr/USAAF00040.md): Brake · malfunctioned · Jun 1, 2000 · N897US · Fokker F28MK0100 · Brake
  > BHM-CLT - FLT 1511 - DURING ROLL OUT, MUCH MORE THAN NORMAL BRAKE PEDAL FORCE SEEMED TO BE REQUIRED FOR NORMAL BRAKING EFFORT. MAINTENANCE BLED NR 3 AND NR 4 BRAKE ASSEMBLIES. LEAK AND OPS CHECKS OK. (M)
- [SDR USAAF00034](https://openairdocs.org/sdr/USAAF00034.md): Spring · broken · May 3, 2000 · N897US · Fokker F28MK0100 · Escape Slide
  > CLT - FOUND SERVICE DOOR GIRT BAR SLIDER HAS BROKEN SPRING. MAINTENANCE REPLACED THE SPRING IN SLIDER. CHECKS NORMAL. (M)
- [SDR USAA991233](https://openairdocs.org/sdr/USAA991233.md): Fitting · cracked · Nov 1, 1999 · N897US · Fokker F28MK0100 · Fuselage Miscellaneous Structure
  > PIT - DURING RON VISIT, FOUND 1.125 INCH CRACK IN T-FITTING (W/O JOGGLE) AT BOTTOM END OF T-FITTING AFT SIDE APBH BL 1027L. STOP DRILLED CRACK PER CD. REINSTALLED BLIND FASTENERS PER CD 53F00703. (M)
- [SDR USAAF99048](https://openairdocs.org/sdr/USAAF99048.md): Battery Pack · discharged · Sep 28, 1999 · N897US · Fokker F28MK0100 · Emergency Lighting
  > GSO - EMERGENCY LIGHT STRIP NEAR CENTER EXIT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)
- [SDR USAAF99044](https://openairdocs.org/sdr/USAAF99044.md): Battery Pack · discharged · Sep 13, 1999 · N897US · Fokker F28MK0100 · Emergency Lighting
  > IND - FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROW 12 THROUGH 17. MAINTENANCE REPLACED THE NR 7 BATTERY PACK. (M)
- [SDR USAAF99012](https://openairdocs.org/sdr/USAAF99012.md): Window · cracked · Mar 13, 1999 · N897US · Fokker F28MK0100 · Flight Compartment Windows
  > CLT - FLT 8076 - EN ROUTE TO CLT AT FL240, THE OUTER PANE OF THE LEFT COCKPIT SLIDING WINDOW CRACKED. FLIGHT WAS A NON-REVENUE FERRY FLIGHT. AIRCRAFT LANDED CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT SLIDING WINDOW. (M)
- [SDR USAAF00003](https://openairdocs.org/sdr/USAAF00003.md): Anti-Skid System · malfunctioned · Jan 7, 1999 · N897US · Fokker F28MK0100 · Brake Anti-Skid Section
  > CLT-BHM - FLT 1252 - ON TAXI OUT FOR TAKEOFF, WHEN BRAKES WERE APPLIED (20 KNOTS), ANTI-SKID WOULD RELEASED BRAKES, MAKING IT HARD TO SLOW DOWN. MAINTENANCE ACTION PENDING. AIRCRAFT WAS RELEASED ON MEL. (M)
- [SDR USAAF98093](https://openairdocs.org/sdr/USAAF98093.md): Bulb · failed · Nov 30, 1998 · N897US · Fokker F28MK0100 · Landing Gear Position and Warning
  > CRW - FLT 435 - ON APPROACH TO CRW WHEN LANDING GEAR WAS SELECTED DOWN, THERE WAS NO GEAR DOWN AND SAFE INDICATION. CREW RECYCLED LANDING GEAR BUT THERE WAS STILL NO GEAR SAFE INDICATION. PROBLEM APPEARED TO BE AN INDICATION PROBLEM. CAPTAIN DID NOT DECLARE
- [SDR USAAF98066](https://openairdocs.org/sdr/USAAF98066.md): Battery Pack · discharged · Aug 2, 1998 · N897US · Fokker F28MK0100 · Emergency Lighting
  > GSO - FORWARD EMERGENCY LIGHTS WEAK. MAINTENANCE REPLACED THE BATTERY PACK. (M)
- [SDR USAAF96026](https://openairdocs.org/sdr/USAAF96026.md): Bulb · failed · Feb 25, 1996 · N897US · Fokker F28MK0100 · Landing Gear Position and Warning
  > FLT 578 - CLT - RIGHT MAIN GEAR FAILED TO INDICATE DOWN AND GREEN. RECYCLED GEAR, CHANGED BULBS WITH NO CHANGE. LANDED NORMALLY, TAXIED WITH GEAR PINNED. PERFORMED BITE USING THE PSEU WITH NO DEFECTIVE SWITCHES OR TARGETS. INSPECTED INDICATION PACK ON FORW
- [SDR USAA950451](https://openairdocs.org/sdr/USAA950451.md): Lines · uninstalled · May 6, 1995 · N897US · Fokker F28MK0100 · Pitot/Static System
  > PIT - FLT 8554 - DURING TAKEOFF AT ROTATION, THE AC LOST ALL INSTRUMENTATION. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO PIT. MAINTENANCE REINSTALLED THE PITOT AND STATIC LINES. OPERATIONS CHECKED GOOD. (W)
- [SDR USAA950580](https://openairdocs.org/sdr/USAA950580.md): Stringer · cracked · May 5, 1995 · N897US · Fokker F28MK0100 · Fuselage Main, Longeron/Stringer
  > PIT - DURING SCHEDULED INSPECTION OF USAIR CD 53F00762 HFEC INSPECTION OF STRINGERS NR 6, 7, 68 AFT OF FRAME STATION 3870, FOUND.5 INCH CRACK (RADICAL) AT STRINGER NR 68 RT SIDE FRAME 3870. INSTALLED SPLICE REPAIR TO STRINGER 68 RT SIDE AFT OF FRAME STATION
- [SDR USAA950579](https://openairdocs.org/sdr/USAA950579.md): Stringer · cracked · May 5, 1995 · N897US · Fokker F28MK0100 · Fuselage Main, Longeron/Stringer
  > PIT - DURING SCHEDULED INSPECTION USAIR PCI 289 CD 53F00762, FOUND A.5 INCH CRACK IN STRINGER 68 RT SIDE AFT OF FRAME 3870. INSTALLED SPLICE REPAIR TO STRINGER 68 PER SRM 51-70-06. (M)
- [SDR USAA950232](https://openairdocs.org/sdr/USAA950232.md): Pump · inoperative · Mar 13, 1995 · N897US · Fokker F28MK0100 · Fuel Boost Pump
  > PIT - FLT 0141 - THE R1 FUEL BOOST PUMP FAULT LIGHT ILLUMINATED IN-FLIGHT. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTEANCE REPLACED THE R1 AND R2 BOOST PUMPS AND COCKPIT OVERHEAD PANEL. OPERATIONS CHECKED GOOD. (X)

## 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 = 'N897US' AND deregistration_id = 'N897US-2018-01-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N897US-2018-01-17/reports

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