# Service difficulty reports: N945F, cancelled May 4, 2015

A list on [N945F, cancelled May 4, 2015](https://openairdocs.org/deregistered/N945F-2015-05-04.md).

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

Page 1 of 2 · 70 reports

- [SDR EIA2002019](https://openairdocs.org/sdr/EIA2002019.md): Battery · inoperative · Feb 10, 2002 · N945F · Doug DC933F · Battery/Charger System
  > DURING CRUISE AT FL 330, AT APPROX 2015Z, THE NR 1 NAV FAILED. SHORTLY AFTER THAT, THE CAPTAINS ADI TUMBLED THEN THE TRANSMITT FUNCTION OF THE RADIOS FAILED. REPLIES WERE MADE BY THE IDENT ON THE TRANSPONDER. ALL LIGHTS IN THE COCKPIT OTHER THAN THE MASTER
- [SDR 20000620SH020](https://openairdocs.org/sdr/20000620SH020.md): Web · corroded · Jun 20, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK FOUND CORROSION ON CUSP WEB BS 937 TO BS 965, RBL 44.5. CAUSE UNKNOWN. (X)
- [SDR 20000619SH016](https://openairdocs.org/sdr/20000619SH016.md): Web · cracked · Jun 19, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CRACKS AND CORROSION ON CUSP WEB BS 775 TO BS 897, RBL 44.5. CAUSE UNKNOWN. (X)
- [SDR 20000619SH015](https://openairdocs.org/sdr/20000619SH015.md): Floorbeam · misdrilled · Jun 19, 2000 · N945F · Doug DC933F · Fuselage Main, Floor Beam
  > DURING MAINTENANCE, THE FLOORBEAM AT BS 756, RBL 45, AND BS 737, RBL 45, WERE FOUND MISDRILLED. (X)
- [SDR 20000619SH013](https://openairdocs.org/sdr/20000619SH013.md): Bulkhead · cracked · Jun 19, 2000 · N945F · Doug DC933F · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND CRACK IN DOUBLER ON THE AFT PRESSURE BULKHEAD BS 996. CAUSE UNKNOWN. (X)
- [SDR 20000619SH012](https://openairdocs.org/sdr/20000619SH012.md): Skin · dented · Jun 19, 2000 · N945F · Doug DC933F · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND MULTIPLE DENTS IN FUSELAGE SKIN BS 351 TO BS 362, LONGERON 23R TO LONGERON 26R. CAUSE UNKNOWN. (X)
- [SDR 20000619SH011](https://openairdocs.org/sdr/20000619SH011.md): Web · cracked · Jun 19, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, TWO CRACKS WERE FOUND IN RHS CUSP WEB A BS 605 TO BS 617, RBL 44.5 TO RBL 60. CAUSE UNKNOWN. (INT)
- [SDR 20000619SH009](https://openairdocs.org/sdr/20000619SH009.md): Web · cracked · Jun 19, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND ELONGATED HOLES, CRACKS, AND CORROSION ON CUSP WEB AT BS 737 TO BS 756, RBL 44.5 AND RBL 60. (X)
- [SDR 20000619SH010](https://openairdocs.org/sdr/20000619SH010.md): Web · corroded · Jun 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND ELONGATED HOLES, CRACKS, AND CORROSION ON CUSP WEB AT BS 737 TO BS 756, RBL 44.5 AND RBL 60. (X)
- [SDR 20000615SH013](https://openairdocs.org/sdr/20000615SH013.md): Web · cracked · Jun 15, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CRACK IN CUSP WEB, BS 598, LBL 44.5. CAUSE UNKNOWN. (X)
- [SDR 20000619SH017](https://openairdocs.org/sdr/20000619SH017.md): Beam · cracked · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CRACK IN FORWARD CARGO DOOR HORIZONTAL BEAM, PN 9957663-13. CAUSED BY FASTENER TOOL. (X)
- [SDR 20000619SH014](https://openairdocs.org/sdr/20000619SH014.md): Seat Track · cracked · Apr 18, 2000 · N945F · Doug DC933F · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK, FOUND CRACK ON THE HORIZONTAL FLANGE OF SEAT TRACK, MAIN CABIN FLOOR. CAUSE UNKNOWN. (X)
- [SDR 20000619SH008](https://openairdocs.org/sdr/20000619SH008.md): Structure · misdrilled · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND MISLOCATED HOLES COMMON TO CUSP TEE AT BS 775, LBL 60. CAUSE UNKNOWN. (X)
- [SDR 20000615SH040](https://openairdocs.org/sdr/20000615SH040.md): Floorboard · cracked · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Floor Panel
  > DURING C-CHECK, FOUND FLOOR PANEL DENTED AND CRACKED IN TWO PLACES FROM BS 447 TO BS 452.5, BL ZERO. CAUSE UNKNOWN. (X)
- [SDR 20000615SH039](https://openairdocs.org/sdr/20000615SH039.md): Structure · misdrilled · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND MISLOCATED HOLES COMMON TO CUSP TEE AT BS 794, LBL 60. CAUSE UNKNOWN. (X)
- [SDR 20000615SH038](https://openairdocs.org/sdr/20000615SH038.md): Floorboard · punctured · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Floor Panel
  > DURING C-CHECK, FOUND PUNCTURE IN FLOOR PANEL AT RT BS 516.5, RBL 10-26. CAUSE UNKNOWN. (X)
- [SDR 20000615SH037](https://openairdocs.org/sdr/20000615SH037.md): Pan · damaged · Apr 18, 2000 · N945F · Doug DC933F · Passenger/Crew Doors
  > DURING C-CHECK, FOUND OVERSIZED FASTENER HOLE IN THE FORWARD ENTRANCE DOOR PAN AT LEFT BS 197.75 NEAR BEAM NR 1. CAUSE UNKNOWN. (X)
- [SDR 20000615SH036](https://openairdocs.org/sdr/20000615SH036.md): Longeron · misdrilled · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND DOUBLE DRILLED HOLES ON FLANGE OF LONGERON L30 AT BS 340. CAUSE UNKNOWN. (X)
- [SDR 20000615SH035](https://openairdocs.org/sdr/20000615SH035.md): Skin · misdrilled · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Main, Plate/Skin
  > DURING C-CHECK,, FOUND MISLOCATED HOLES IN FUSELAGE SKIN AT BS 951.8 TO BS 959.6, LONGERON L24. CAUSE UNKNOWN. (X)
- [SDR 20000615SH034](https://openairdocs.org/sdr/20000615SH034.md): Web · cracked · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND ELONGATED HOLES, CRACKS AND CORROSION ON CUSP WEB AT BS 775 TO BS 832, LBL 44.5. CAUSE UNKNOWN. (X)
- [SDR 20000615SH033](https://openairdocs.org/sdr/20000615SH033.md): Bulkhead · misdrilled · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND NUMEROUS HOLES MISLOCATED IN THE WEB AT RT BS 965 BETWEEN L7 AND L15. CAUSE UNKNOWN. (X)
- [SDR 20000615SH032](https://openairdocs.org/sdr/20000615SH032.md): Web · cracked · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND ELONGATED HOLES, CRACKS, AND CORROSION ON CUSP WEB AT BS 832 TO BS 897, LBL 44.5. CAUSE UNKNOWN. (X)
- [SDR 20000615SH031](https://openairdocs.org/sdr/20000615SH031.md): Longeron · corroded · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, CORROSION DAMAGE WAS FOUND ON L29L AND L30. CAUSE UNKNOWN.
- [SDR 20000615SH030](https://openairdocs.org/sdr/20000615SH030.md): Web · cracked · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND NUMEROUS CRACKS AND ELONGATED HOLES IN CUSP WEB AT BS 218 TO BS 237, LBL 44.5. CAUSE UNKNOWN. (X)
- [SDR 20000615SH029](https://openairdocs.org/sdr/20000615SH029.md): Web · cracked · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND NUMEROUS CRACKS AND ELONGATED HOLES IN CUSP WEB AT BS 237 TO BS 313. CAUSE UNKNOWN. (X)
- [SDR 20000615SH028](https://openairdocs.org/sdr/20000615SH028.md): Seat Track · misdrilled · Apr 18, 2000 · N945F · Doug DC933F · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK, FOUND MISLOCATED HOLES IN SEAT TRACK AT BS 266 TO BS 455, LBL 54.0. CAUSE UNKNOWN. (X)
- [SDR 20000615SH027](https://openairdocs.org/sdr/20000615SH027.md): Floorboard · damaged · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Floor Panel
  > DURING C-CHECK, FOUND ELONGATED HOLES IN CABIN FLOOR PANEL NR 14, PN 5922429-37. CAUSE UNKNOWN. (X)
- [SDR 20000615SH026](https://openairdocs.org/sdr/20000615SH026.md): Floorbeam · misdrilled · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Main, Floor Beam
  > DURING C-CHECK, FOUND MIS-DRILLED HOLE IN UPPER CAP OF FUSELAGE FLOORBEAM AT BS 427, LBL 37. (X)
- [SDR 20000615SH025](https://openairdocs.org/sdr/20000615SH025.md): Floorboard · cracked · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Floor Panel
  > DURING C-CHECK, FOUND ELONGATED FASTENER HOLES AND CRACKS IN CAPTAIN''S FLOOR PANEL, PN 9910078-3. CAUSE UNKNOWN. (X)
- [SDR 20000615SH024](https://openairdocs.org/sdr/20000615SH024.md): Web · cracked · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND ELONGATED HOLES AND CRACKS IN CUSP WEB BS 756 TO BS 775, LBL 44.5. CAUSE UNKNOWN. (X)
- [SDR 20000615SH023](https://openairdocs.org/sdr/20000615SH023.md): Web · cracked · Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND ELONGATED HOLES, CORROSION, AND CRACKS IN CUSP WEB AT BS 756 TO BS 775, RBL 44.5. CAUSE UNKNOWN. (X)
- [SDR 20000615SH022](https://openairdocs.org/sdr/20000615SH022.md): Web · damaged · Apr 11, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND ELONGATED HOLES IN CUSP WEB AT BS 503 TO BS 598,RBL 44.5. CAUSE UNKNOWN. (X)
- [SDR 20000615SH021](https://openairdocs.org/sdr/20000615SH021.md): Floorbeam · corroded · Apr 11, 2000 · N945F · Doug DC933F · Fuselage Main, Floor Beam
  > DURING C-CHECK, FOUND CORROSION ON FLOORBEAM, PN 9958212-25 AT BS 756, APPROXIMATELY LBL 14.5. CAUSE UNKNOWN. (X)
- [SDR 20000615SH020](https://openairdocs.org/sdr/20000615SH020.md): Web · damaged · Apr 11, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND ELONGATED HOLES IN CUSP WEB AT BS 313 TO BS 389, RBL 44.5. CAUSE UNKNOWN. (X)
- [SDR 20000615SH019](https://openairdocs.org/sdr/20000615SH019.md): Web · damaged · Apr 11, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND ELONGATED HOLES IN CUSP WEB AT BS 389 TO BS 503, RBL 44.5. CAUSE UNKNOWN. (X)
- [SDR 20000615SH018](https://openairdocs.org/sdr/20000615SH018.md): Web · cracked · Apr 11, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND ELONGATED HOLES AND CRACKS IN CUSP WEB BS 218 TO BS 237, RBL 44.5. CAUSE UNKNOWN. (X)
- [SDR 20000615SH017](https://openairdocs.org/sdr/20000615SH017.md): Web · cracked · Apr 11, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND ELONGATED HOLES AND CRACKS IN CUSP WEB AT BS 237 TO BS 313, RBL 44.5. CAUSE UNKNOWN. (X)
- [SDR 20000615SH016](https://openairdocs.org/sdr/20000615SH016.md): Floorbeam · gouged · Apr 11, 2000 · N945F · Doug DC933F · Fuselage Main, Floor Beam
  > DURING C-CHECK, FOUND GOUGE IN FLOORBEAM WEB BS 100, RBL 10. CAUSE UNKNOWN. (X)
- [SDR 20000615SH015](https://openairdocs.org/sdr/20000615SH015.md): Door Frame · damaged · Apr 11, 2000 · N945F · Doug DC933F · Fuselage Main, Structure
  > DURING C-CHECK, FOUND OVERSIZED HOLE IN AFT CARGO DOOR JAMB AT BS 937. CAUSE UNKNOWN. (X)
- [SDR 20000615SH014](https://openairdocs.org/sdr/20000615SH014.md): Frame · tool damage · Apr 11, 2000 · N945F · Doug DC933F · Fuselage Main, Frame
  > DURING C-CHECK, FOUND HOLE AND DRILL MARKS IN FRAME BS 294 BETWEEN LONGERON L16 AND L18.
- [SDR EIA990287](https://openairdocs.org/sdr/EIA990287.md): Skin · cracked · Sep 29, 1999 · N945F · Doug DC933F · Fuselage Main, Plate/Skin
  > SEA - DURING PREFLIGHT, FOUND 11 INCH CRACK IN LEFT SIDE OF AIRCRAFT AT STATION 89, ALSO, FOUND FUSELAGE FRAME CRACKED AT STATION 83, LEFT SIDE. REPAIRED DAMAGED SKIN AREA PER SRM 51-10-03 AND SRM 51-30-02. REMOVED AND REPLACED DAMAGED FRAME WITH NEW PART P
- [SDR 99ZZZM783](https://openairdocs.org/sdr/99ZZZM783.md): Frame · cracked · Sep 29, 1999 · N945F · Doug DC933F · Fuselage Main, Plate/Skin
  > SEA - DURING PREFLIGHT, FOUND 11 INCH CRACK IN LEFT SIDE OF AIRCRAFT AT STATION 89, ALSO, FOUND FUSELAGE FRAME CRACKED AT STATION 83, LEFT SIDE. REPAIRED DAMAGED SKIN AREA PER SRM 51-10-03 AND SRM 51-30-02. REMOVED AND REPLACED DAMAGED FRAME WITH NEW PART P
- [SDR EIA990188](https://openairdocs.org/sdr/EIA990188.md): Pedal · binding · Jul 26, 1999 · N945F · Doug DC933F · Rudder Control System
  > KSEA - ON FLIGHT 823, CRWE REPORTED THAT ON TAKEOFF ROLL AT ABOUT 100 KTS AIRCRAFT BEGAN PULLING TO THE RIGHT. CAPTAIN APPLIED HEAVY LEFT FOOT PRESSURE ON THE LEFT RUDDER AND HEARD AN AUDIBLE SNAP. CAPTAIN THEN RELEASED PRESSURE ON PEDAL AND AIRCRAFT IMMEDIA
- [SDR EIAA990186](https://openairdocs.org/sdr/EIAA990186.md): Seat · misinstalled · Jul 22, 1999 · N945F · Doug DC933F · Flight Compartment Equipment
  > MMV - DURING EVALUATION, FOUND COURIER SEAT INSTALLED PER STC SA2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF FAR 25.561. COURIER SEAT DEACTIVATED PER EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO 25-DC9-805-91. REV C. EO APPROVED BY 811
- [SDR EIA990187](https://openairdocs.org/sdr/EIA990187.md): Drive Link · broken · Jul 22, 1999 · N945F · Doug DC933F · Engine Thrust Reverser
  > AFTER LANDING AT PAJN, RIGHT ENGINE THRUST REVERSER WOULD NOT STOW. THRUST REVERSER DRIVE LINK P/N 5958782-503 FOUND BROKEN. (M)
- [SDR EIAA990004](https://openairdocs.org/sdr/EIAA990004.md): Retract Mech · malfunctioned · Feb 27, 1999 · N945F · Doug DC933F · Landing Gear Door Retract Section
  > DEN - ON DEPARTURE FROM DEN, THE FLIGHT CREW, UPON ATTEMPTING TO RAISE THE LANDING GEAR, RECEIVED THE GEAR DOOR OPEN LIGHT ILLUMINATION AND THREE RED GEAR UNSAFE LIGHTS. AFTER RECYCLING THE GEAR HANDLE TO THE DOWN POSITION THE CREW RECEIVED THREE GREEN LANDIN
- [SDR EIA980361](https://openairdocs.org/sdr/EIA980361.md): Strut · flat · Dec 3, 1998 · N945F · Doug DC933F · Main Landing Gear Strut/Axle/Truck
  > SEA - DURING POST FLIGHT WALK AROUND INSPECTION, THE RIGHT GEAR STRUT WAS FOUND COMPLETELY DEFLATED. DURING FURTHER INVESTIGATION IT WAS FOUND THAT THE GLAND NUT WAS COMPLETELY DISENGAGED FROM THE OUTER CYLINDER. (M)
- [SDR EIA980350](https://openairdocs.org/sdr/EIA980350.md): Retract Mech · dirty · Nov 20, 1998 · N945F · Doug DC933F · Trailing Edge Flap Control System
  > SEA - DURING APPROACH SET FLAPS INDICATED AS FOLLOWS 5 DEGREES, 9 DEGREES, 15, L 18 - R 16) 25 = 27.5, 40-45. CHECKED ADJUSTMENT OF CONTROL VALVE PUSHROD ARM PER MM 27-52-1, INSPECTED AND CLEANED DEBRIS (EXCESSIVE AND DIRTY LUBE) FROM FOLLOW-UP CABLES. (M)
- [SDR EIA980349](https://openairdocs.org/sdr/EIA980349.md): Valve · failed · Nov 19, 1998 · N945F · Doug DC933F · Trailing Edge Flap Control System
  > SEA - DURING APPROACH SET FLAPS TO 15 DEGREES (L FLAP 20R, R FLAP 15) FLAPS THEN BLEW BACK TO 10 DEGREE WHILE 15 SELECTED, SELECTED 25 GOT 30, SELECTED 40 GOT 45 INITIAL LANDED WITH 38 DEGREES. REPLACED FLAP CONTROL VALVE PER MM 27-51-1 SYSTEM CHECKED GOOD.
- [SDR EIAA980337](https://openairdocs.org/sdr/EIAA980337.md): Skin · cracked · Oct 31, 1998 · N945F · Doug DC933F · Passenger/Crew Doors
  > MZJ - DURING C4 CHECK, LEFT FORWARD DOOR SKIN AT FED LOWER CORNER IS CRACKED AT TWO PLACES. REPAIRED PER SRM 52-05 FIG 32. (M)

Next page: https://openairdocs.org/deregistered/N945F-2015-05-04/reports.md?page=2

## 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 = 'N945F' AND deregistration_id = 'N945F-2015-05-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N945F-2015-05-04/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.