# Service difficulty reports: N313FL, cancelled Jun 2, 2005

A list on [N313FL, cancelled Jun 2, 2005](https://openairdocs.org/deregistered/N313FL-2005-06-02.md).

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

- [SDR F3LA200500018](https://openairdocs.org/sdr/F3LA200500018.md): Cover · missing · Apr 22, 2005 · N313FL · Boeing 7373L9 · Turbine Engine Oil System
  > AIR RETURN TO DEN, ON CLIMB-OUT, BOTH ENGINE OIL QUANTITY INDICATORS WENT TO ZERO. BOTH OIL PRESSURE INDICATORS WENT TO ZERO. BOTH LOW OIL PRESSURE LIGHTS ILLUMINATED. ENGINES OPERATED APPROXIMATELY 15 MINUTES IN THAT CONDITION UNTIL LANDING, WHICH WAS WITH
- [SDR F3L2005F00000](https://openairdocs.org/sdr/F3L2005F00000.md): Engine · leaking · Apr 22, 2005 · N313FL · Boeing 737300 · Turbine Engine Oil System
  > APPROX 11 MIN INTO CLIMB AT FL260, BOTH ENGINES BEGAN TO LOSE OIL QUANTITY. AFTER A SHORT PERIOD OF TIME, OIL QUANTITY ON NR 1 ENG WENT TO ZERO, FOLLOWED BY NR 2 ENG ALSO GOING TO ZERO. NR 1 ENG OIL PRESS THEN DROPPED TO ZERO, NR 2 ENG OIL PRESS DROPPED TO M
- [SDR F3LA200500008](https://openairdocs.org/sdr/F3LA200500008.md): Sill · corroded · Mar 9, 2005 · N313FL · Boeing 7373L9 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK INSPECTION, REPORTED L2 DOOR MOP SILL CORRODED. REPLACED L2 DOOR MOP SILL PER SRM 51-40-02.
- [SDR F3LA200500010](https://openairdocs.org/sdr/F3LA200500010.md): Strap · corroded · Mar 8, 2005 · N313FL · Boeing 7373L9 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT GALLEY PAN STRAP AT BS 1016, BETWEEN RBL 30 AND LBL 30. FOUND TO BE OUT OF LIMITS PER SRM 53-60-61, FIG 101, DETAIL VII. REMOVED PAN STRAP PER SRM 51-40-02. FABRICATED NEW STRAP AND INSTALLED PER EA 53-
- [SDR F3LA200500009](https://openairdocs.org/sdr/F3LA200500009.md): Intercostal · corroded · Mar 8, 2005 · N313FL · Boeing 7373L9 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK INSPECTION, REPORTED INTERCOSTAL AT BS 950, RBL 20 TO RBL 40, CORRODED. FOUND TO BE OUT OF LIMITS PER SRM 53-60-51. REPLACED INTERCOSTAL PER SRM 51-40-05, 51-40-02, AND 53-60-51.
- [SDR F3LA200500007](https://openairdocs.org/sdr/F3LA200500007.md): Sill · corroded · Mar 8, 2005 · N313FL · Boeing 7373L9 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK INSPECTION, REPORTED R2 DOOR MOP SILL CORRODED. REPLACED R2 DOOR MOP SILL PER SRM 51-40-02.
- [SDR F3LA200400091](https://openairdocs.org/sdr/F3LA200400091.md): Pressure Panel · cracked · Aug 20, 2004 · N313FL · Boeing 7373L9 · Fuselage Main, Bulkhead
  > FLIGHT CREW REPORTED ALTITUDE CABIN CLIMBED AT 150 FPM WITH BOTH PACKS IN AUTO AT CRUISE ALTITUDE. PRESSURIZED AIRCRAFT ON THE GROUND AND FOUND AN 8-INCH CRACK AT TOP OF RT WHEEL WELL, STA 664, RBL 37. REPAIRED PER SRM 53-60-51, FIGURE 203, DETAIL IV AND EA
- [SDR F3LA200400067](https://openairdocs.org/sdr/F3LA200400067.md): Control Module · inoperative · Jun 3, 2004 · N313FL · Boeing 7373L9 · Leading Edge Slat Control System
  > ABORTED TAKEOFF. FLIGHT CREW REPORTED L/E FLAPS TRANSIT LIGHT ILLUMINATED WITH NR 2 SLAT ON OVERHEAD PANEL SHOWING INTRANSIT. TAKEOFF ABORTED AT 111 KIAS. REPLACED FLAP/SLAT MODULE PER MM 27-88-41. CHECKED TARGET TO EXTEND SENSORS ON NR 2, 3 AND 5 SLATS PE
- [SDR F3LA200300123](https://openairdocs.org/sdr/F3LA200300123.md): Snubber · inoperative · Aug 1, 2003 · N313FL · Boeing 7373L9 · Passenger/Crew Doors
  > DURING C-3 CHECK, INSPECTION REPORTED R-1 DOOR LOCK PIN INOPERATIVE. ADJUSTED SNUBBER ON R-1 DOOR PER MM 52-41-00, PAGE 504, STEP 5.
- [SDR F3LA200200370](https://openairdocs.org/sdr/F3LA200200370.md): Intercostal · corroded · Oct 24, 2002 · N313FL · Boeing 737300 · Fuselage Miscellaneous Structure
  > DURING C 2 CHECK, CORROSION WAS FOUND ON THE AFT CARGO PIT INTERCOSTAL SURFACE AND AROUND NUT PLATES BETWEEN STA 767 TO STA 794 AND RBL 21. NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-02, SRM 51-40-02 AND SOPM 20-41-02.
- [SDR F3LA200200363](https://openairdocs.org/sdr/F3LA200200363.md): Floor Support · corroded · Oct 24, 2002 · N313FL · Boeing 737300 · Fuselage Miscellaneous Structure
  > DURING C 2 CHECK, THE AFT CARGO COMPARTMENT FLOOR TRACK WAS FOUND CORRODED AT STA 727D AT RBL 13.8 THE CORRODED SECTION OF TRACK WAS REPLACED BETWEEN STA 727 AND STA 767 IAW SRM 51-40-02
- [SDR F3LA200200372](https://openairdocs.org/sdr/F3LA200200372.md): Floor Support · corroded · Oct 23, 2002 · N313FL · Boeing 737300 · Fuselage Miscellaneous Structure
  > DURING C 2 CHECK, CORROSION WAS FOUND OF THE AFT CARGO COMPARTMENT FLOOR TRACK AT STA 791, LBL 11.5. REMOVED AND REPLACED THE FLOOR TRACK IAW SRM 51-10-02 AND SRM 51-40-02, BETWEEN STA 727 AND STA 947 AT LBL 11.5.
- [SDR F3LA200200369](https://openairdocs.org/sdr/F3LA200200369.md): Floor Support · corroded · Oct 23, 2002 · N313FL · Boeing 737300 · Fuselage Miscellaneous Structure
  > DURING C 2 CHECK, AFT CARGO FLOOR TRACK WAS FOUND CORRODED AT STA 860, RBL 2. FLOOR TRACK WAS REPLACED BETWEEN STA 727 AND STA 947, RBL 2.5 IAW SRM 51-40-05 AND SRM 51-40-02.
- [SDR F3LA200200368](https://openairdocs.org/sdr/F3LA200200368.md): Skin · punctured · Oct 23, 2002 · N313FL · Boeing 737300 · Leading Edge Devices
  > DURING C 2 CHECK, IT WAS NOTED RT, IN BOARD FORE FLAP HAD A HOLE IN THE LOWER SURFACE. FLAP WAS REMOVED AND REPAIRED IAW SRM 51-70-10 AND REINSTALLED IAW BOEING 737 MM 27-51-07.
- [SDR F3LA200200366](https://openairdocs.org/sdr/F3LA200200366.md): Floor Support · corroded · Oct 22, 2002 · N313FL · Boeing 737300 · Fuselage Miscellaneous Structure
  > DURING C 2 CHECK, AFT CARGO FLOOR TRACK WAS FOUND CORRODED AT STA 860, LBL 3.0 FLOOR TRACK REPLACED BETWEEN STA 791 TO STA 860. LBL 3.0, IAW SRM 51-40-02
- [SDR F3LA200200371](https://openairdocs.org/sdr/F3LA200200371.md): Floor Panel · corroded · Oct 20, 2002 · N313FL · Boeing 737300 · Fuselage Floor Panel
  > DURING C 2 CHECK, THE AFT CARGO COMPARTMENT FLOOR TRANSITION PANEL WAS FOUND CORRODED BETWEEN STA 787 AND STA 807. AFT CARGO COMPARTMENT FLOOR TRANSITION PANEL WAS REMOVED AND REPLACED BETWEEN STA 727 AND 947, LBL 20 IAW SRM 53-60-53 AND SRM 51-40-02.
- [SDR F3LA200200365](https://openairdocs.org/sdr/F3LA200200365.md): Tail Cone · dented · Oct 18, 2002 · N313FL · Boeing 737300 · Aerodynamic Fairings
  > DURING C 2 CHECK, A DENT WAS FOUND ON THE LT SIDE OF THE TAIL CONE, NEAR THE ELEVATOR ATTACH POINTS. DENT WAS REPAIRED AND PAINTED IAW MAINTENANCE MANUAL 737-300 MM 51-21-99 AND SRM 51-70-06.
- [SDR F3LA200200367](https://openairdocs.org/sdr/F3LA200200367.md): Skin · bird strike · Oct 17, 2002 · N313FL · Boeing 737300 · Horizontal Stabilizer, Plate/Skin
  > DURING C 2 CHECK, A BIRD STRIKE WAS FOUND ON THE RT LEADING EDGE OF THE STABILIZER BETWEEN STA 184.7 AND STA 189.2. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55-10-01.
- [SDR F3LA200200136](https://openairdocs.org/sdr/F3LA200200136.md): Control Cable · broken · May 8, 2002 · N313FL · Boeing 7373L9 · Aileron Control System
  > FLIGHT CREW REPORTED SIGNIFICANT RT ROLL TENDENCY ON FINAL APPROACH AND LANDING. CORRECTED ON TOUCHDOWN. FOUND AILERON BUS CABLE BROKEN. REMOVED RT AILERON CABLE ABSB-4 AND FABRICATED, INSTALLED, ADJUSTED AND TESTED REPLACEMENT CABLE PER MM 27-11-0, 27-09-1
- [SDR F3LA200200120](https://openairdocs.org/sdr/F3LA200200120.md): Video Unit · shorted · Apr 1, 2002 · N313FL · Boeing 7373L9 · Entertainment System
  > FLIGHT CREW REPORTED ENTERTAINMENT TAPE RECORDER SMOKING EN ROUTE TO DEN. DIVERTED TO SLC AND LANDED WITHOUT INCIDENT. ISOLATED ELECTRICAL SHORT IN TAPE PLAYER. PULLED AND COLLARED CIRCUIT BREAKER E7 ON P6-1 PANEL. REMOVED TAPE PLAYER FROM WALL ABOVE FWD F
- [SDR F3LA200200105](https://openairdocs.org/sdr/F3LA200200105.md): Actuator · inoperative · Mar 1, 2002 · N313FL · Boeing 7373L9 · Rudder Actuator
  > BLOCK TURNBACK. FLIGHT CREW REPORTED RUDDER WOULD NOT CENTER AFTER START UP AND TAXI. REPLACED RUDDER TRIM ACTUATOR AND CHECKED OKAY.
- [SDR F3LA200000259](https://openairdocs.org/sdr/F3LA200000259.md): Door · out of adj · Nov 28, 2000 · N313FL · Boeing 7373L9 · Door Warning System
  > DURING TAKEOFF, FLIGHT CREW REPORTED FORWARD ENTRY DOOR LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT 75 KIAS. MAINTENANCE ADJUSTED FORWARD ENTRY DOOR PER MM 52-11-0 AND PERFORMED ENTRY DOOR TEST. OPERATIONAL TEST AND LEAK CHECK OKAY. REPLACED NR 3 AND NR 4 MA
- [SDR F3LA200000260](https://openairdocs.org/sdr/F3LA200000260.md): Spring · unserviceable · Nov 24, 2000 · N313FL · Boeing 7373L9 · Aileron Control System
  > DURING C-7 CHECK TEST FLIGHT, FLIGHT CREW REPORTED AILERONS STIFF IN MANUAL REVERSION. REPLACED AILERON CONTROL SPRING AND CHECKED OKAY.

## 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 = 'N313FL' AND deregistration_id = 'N313FL-2005-06-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N313FL-2005-06-02/reports

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