# Service difficulty reports: N916F, cancelled Dec 30, 2015

A list on [N916F, cancelled Dec 30, 2015](https://openairdocs.org/deregistered/N916F-2015-12-30.md).

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

- [SDR EIA2004042](https://openairdocs.org/sdr/EIA2004042.md): Battery · inoperative · Jun 11, 2004 · N916F · Doug DC915F · Emergency Lighting
  > EMERGENCY LIGHTS IN COCKPIT EXTREMELY DIM WHEN TURNED ON. REPLACED COCKPIT EMERGENCY LIGHT BATTERY PER DC9 MM 33-53-0, OPS CHECKED GOOD.
- [SDR EIA2003057](https://openairdocs.org/sdr/EIA2003057.md): Skin · cracked · Apr 11, 2003 · N916F · Doug DC915F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT LWR AFT CORNER OF MAIN DOOR JAMB CRACKED. REPAIRED PER DC9 SRM 53-05 FIG 103 PAGE 407-418 & 420. REPAIR IS CAT-B N5343 ASSIGNED INSP WITHIN 28,000 CYCLES PER SRM 51-10-5C (EDDY CURRENT).
- [SDR EIA2003055](https://openairdocs.org/sdr/EIA2003055.md): Crossbeam · cracked · Apr 8, 2003 · N916F · Doug DC915F · Passenger/Crew Doors
  > L1 DOOR CROSSBEAM 2ND FROM TOP.5 INCH CRACK AT FWD END IN RADIUS. REPAIRED L1 DOOR CROSSBEAM, BLENDED EDGE AO PART REF DC9 SRM 53-01 FIG 1, STOPPED DRILLED CRACK PER DC9 SRM 52-05 FIG 3, HF EDDY CURRENT PER DOUGLAS SOP 51-06-07, NO CRACKS NOTED.
- [SDR ERKR200100154](https://openairdocs.org/sdr/ERKR200100154.md): Frame · damaged · Aug 27, 2001 · N916F · Doug DC915F · Fuselage Main, Frame
  > FRAME HAS ELONGATED FASTENER HOLE, FS 303, L15 LEFT.
- [SDR ERKR200100153](https://openairdocs.org/sdr/ERKR200100153.md): Longeron · corroded · Aug 27, 2001 · N916F · Doug DC915F · Fuselage Main, Longeron/Stringer
  > LONGERON 30 CORROSION - FS 285.
- [SDR ERKR200100151](https://openairdocs.org/sdr/ERKR200100151.md): Doubler · cracked · Aug 27, 2001 · N916F · Doug DC915F · Passenger/Crew Doors
  > L1 DOOR UPPER FWD CORNER INNER DOUBLER CRACK.
- [SDR ERKR200100150](https://openairdocs.org/sdr/ERKR200100150.md): Pan · cracked · Aug 27, 2001 · N916F · Doug DC915F · Cargo/Baggage Doors
  > CRACKED INNER DOOR PAN ON AFT CARGO PIT DOOR (P/N: 5910157-5).
- [SDR ERKR200100149](https://openairdocs.org/sdr/ERKR200100149.md): Skin · damaged · Aug 24, 2001 · N916F · Doug DC915F · Cargo/Baggage Doors
  > UPPER CARGO DOOR OUTER SKIN DAMAGED.
- [SDR EIA2001238](https://openairdocs.org/sdr/EIA2001238.md): Doubler · cracked · Aug 1, 2001 · N916F · Doug DC915F · Fuselage Main, Structure
  > FOUND LEFT FORWARD ENTRANCE DOOR FORWARD UPPER CORNER INNER DOUBLER HAS TWO CRACKS FROM EDGE GOING FORWARD. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLERS AND FILLERS PER ECRA 916-53-030-2. (M)
- [SDR EIA2001234](https://openairdocs.org/sdr/EIA2001234.md): Frame · cracked · Jul 30, 2001 · N916F · Doug DC915F · Fuselage Main, Frame
  > MZJ - FOUND STATION 897 LEFT L17 FRAME CRACKED. REPAIRED PER SRM 51-30-05, 53-03, FIGURE 32, SHT 5, AND 51-10-2, 51-10-3. (M)
- [SDR EIA2001237](https://openairdocs.org/sdr/EIA2001237.md): Longeron · corroded · Jul 20, 2001 · N916F · Doug DC915F · Fuselage Main, Longeron/Stringer
  > MZJ - FOUND CORROSION ON LONGERON 30 NEAR STATION 290. FABRICATED AND INSTALLED REPAIR STRAP ON LONGERON 30 AT STATION 290 PER ECRA 916-53-033-2. (M)
- [SDR EIA2001015](https://openairdocs.org/sdr/EIA2001015.md): Engine · failed · Mar 14, 2001 · N916F · Doug DC915F · Engine (Turbine/Turboprop)
  > KFAR - RIGHT ENGINE FAILED IN FLIGHT. (M)
- [SDR EIA2000038](https://openairdocs.org/sdr/EIA2000038.md): Brake Assy · malfunctioned · Aug 12, 2000 · N916F · Doug DC915F · Landing Gear Brake System
  > STL - FLT 460 - WHEN CHECKING LEFT BRAKE SYSTEM DURING TAXI INTO STL, LEFT BRAKE PRESS GOES TO ZERO WHEN PEDALS DEFLECTED, AND REQUIRES PUMPING UP WITH PEDALS TO REACH 3000 PSI. REPLACED LEAKING SCHRADER VALVE AND SERVICED LT BRAKE ACCUM. (M)
- [SDR EIAA990181](https://openairdocs.org/sdr/EIAA990181.md): Seat · misinstalled · Jul 22, 1999 · N916F · Doug DC915F · Flight Compartment Equipment
  > MMV - DURING EVALUATION, FOUND THAT COURIER SEAT INSTALLED PER STC SA2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF FAR 25.561. COURIER SEAT IS DEACTIVATED PER EIA EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO 25-DC9-805-91, REV C. EO AP
- [SDR EIA980378](https://openairdocs.org/sdr/EIA980378.md): Connector · dirty · Dec 28, 1998 · N916F · Doug DC915F · Landing Gear Retraction/Extension System
  > ABQ - ON APPROACH TO KDEN, NO SAFE GEAR DOWN INDICATION, LOW APPROACH FLOWN AND TOWER REPORTED GEAR HANGING. RETURNED TO ABQ, EMERGENCY GEAR EXTENSION CHECKLIST RUN, ACCOMPLISHED LOW APPROACH AT ABQ, AND LANDED WITH 6000 LBS FUEL. CLEANED AND RESEATED DIMME
- [SDR EIAA970198](https://openairdocs.org/sdr/EIAA970198.md): Light · malfunctioned · Oct 10, 1997 · N916F · Doug DC915F · Emergency Lighting
  > STA - ABQ - LOG PAGE: F32459 - EMERGENCY EXIT LIGHTS INTERMITTENTLY ILLUMINATED IN-FLIGHT. COULD NOT DUPLICATE, CHECKED EMERGENCY BATTERY AND LIGHTS. (X)
- [SDR EIAA96103](https://openairdocs.org/sdr/EIAA96103.md): Skin · corroded · Dec 8, 1996 · N916F · Doug DC915F · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE SKIN AT BS 642, LONGERON 30, BL 0.0. AFFECTED AREA WAS TRIMMED TO REMOVE CORROSION. INSTALLED INTERNAL FINGER DOUBLERS AND EXTERNAL REPAIR DOUBLERS WET WITH SEALANT AND TOP COAT
- [SDR 97ZZZM180](https://openairdocs.org/sdr/97ZZZM180.md): Skin · corroded · Dec 8, 1996 · N916F · Doug DC915F · Fuselage Main, Plate/Skin
  > DURNG C-CHECK INSPECTION DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE EXTERNAL SKIN AT BS 642, LONGERON 30, BL 0. THE CORRODED AREA MEASURED 5.25 INCH IN LENGTH AND 4.9 IN WIDTH. AFFECTED AREA WAS TRIMMED TO REMOVE CORROSION. INSTALLED INTERNAL FI
- [SDR 97ZZZM179](https://openairdocs.org/sdr/97ZZZM179.md): Skin · corroded · Dec 8, 1996 · N916F · Doug DC915F · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE EXTERNAL SKIN AT BS 642, LONGERON 30, BL 0. THE CORRODED AREA MEASURED 5.25 INCH IN LENGTH AND 4.9 INCH IN WIDTH. AFFECTED AREA WS TRIMMED TO REMOVE CORROSION. INSTALLED INTERN
- [SDR EIAA9680](https://openairdocs.org/sdr/EIAA9680.md): Skin · corroded · Nov 1, 1996 · N916F · Doug DC915F · Fuselage Main, Plate/Skin
  > MZJ - EXFOLIATION CORROSION WAS FOUND ON THE LOWER FUSELAGE EXTERNAL SKIIN AT BS 642, LONGERON 30, AND BL 0.000. CORRODED AREA MEASURES 5.25 INCH LONG AND 4.90 INCH WIDTH. TWO EXTERNAL FINGER REPAIR DOUBLERS FABRICATED AND INSTALLED ON TRIMMED OUT AREA. AN

## 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 = 'N916F' AND deregistration_id = 'N916F-2015-12-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N916F-2015-12-30/reports

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