# Service difficulty reports: N117FE, cancelled Aug 26, 2004

A list on [N117FE, cancelled Aug 26, 2004](https://openairdocs.org/deregistered/N117FE-2004-08-26.md).

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

- [SDR 00FDEA00895](https://openairdocs.org/sdr/00FDEA00895.md): Switch · failed · Dec 20, 2000 · N117FE · Boeing 72725C · Landing Gear Position and Warning
  > 00-374 ON LAND WHEN GEAR DOWN THE NOSE FAILED TO GIVE GREEN LIGHT. R&R NOSE GEAR LOCK SWITCH PER MM 32-61-21 401-405. OPS CK PER 32-61-21-502. OPS NORMAL. OK FOR SERVICE.
- [SDR 00FDEA00894](https://openairdocs.org/sdr/00FDEA00894.md): Switch · malfunctioned · Dec 20, 2000 · N117FE · Boeing 72725C · Landing Gear Position and Warning
  > 00-373 ON CLB OUT AFT LAND RETRACT THE RED DOORS LIGHT ON THE GEAR FLAP CONTROL LIGHT PANEL & FWD RT MLG LIGHT (YELLOW) CAME ON. R&R RMLG DOOR WARN SWITCH MM REF 32-62-11. OPS CK GOOD. OK FOR SERVICE.
- [SDR 00FDEA00383](https://openairdocs.org/sdr/00FDEA00383.md): Duct · damaged · Jun 13, 2000 · N117FE · Boeing 72725C · Pneumatic Distribution System
  > NR 1 ENGINE STRUT OVERHEAT CAME ON IN FLT (WITH ENG ANTI-ICE SELECTED). EXTINGUISH WHEN THROTTLES PULL BACK TO IDLE. *S/D* REMOVED AND REPLACED DUCT AS PER MM 36-11-051-4. NO LEAKS AND NO OVHT LIGHT. OK FOR SERVICE.
- [SDR 97FDEA0764](https://openairdocs.org/sdr/97FDEA0764.md): Switch · failed · Oct 14, 1997 · N117FE · Boeing 72725C · Landing Gear Position and Warning
  > WHEN LDG WAS EXTENDED THE GREEN NOSE GEAR LIGHT DID NOT ILLUMINATE. LIGHT TESTED GOOD, RAN RED TAB CHECKLIST AND RECYCLED GEAR. VERIFIED DOWN AND LOCKED MANUALLY. AT 200 FT BGL WHEN FLAPS WERE PLACED 25 FT NLG LIGHT ILLUMINATED. REMOVED AND REPLACED NOSE G
- [SDR 97FDEA00680](https://openairdocs.org/sdr/97FDEA00680.md): Connector · loose · Sep 24, 1997 · N117FE · Boeing 72725C · Landing Gear Position and Warning
  > UNSATISFACTORY NOSE GEAR LIGHT ON FINAL. RECYCLED HANDLE AND LIGHT CAME ON. FOUND POSITION SWITCH CANNON PLUG LOOSE REMOVED AND CLEANED. RESEATED CANNON PLUG. ALSO, REMOVED AND CLEANED LOCK SWITCH CANNON PLUG, ALL INDICATION NORMAL.
- [SDR 97FDEA00542](https://openairdocs.org/sdr/97FDEA00542.md): Gear Light · malfunctioned · Aug 14, 1997 · N117FE · Boeing 72725C · Landing Gear Position and Warning
  > AFTER TAKEOFF AND GEAR SELECTED UP, ALL THREE RED GEAR LIGHTS AND RIGHT MAIN GEAR LIGHT REMAINED ILLUMINATED. SECOND OFFICER'S PANEL DOOR LIGHTS WERE EXTINGUISHED AND SAME INDICATION PERSISTED AFTER GEAR WERE CYCLED.
- [SDR 97FDEA00017](https://openairdocs.org/sdr/97FDEA00017.md): Drage Brace · cracked · Dec 23, 1996 · N117FE · Boeing 72725C · Nose/Tail Landing Gear
  > NOSE GEAR DRAG BRACE SHELF CRACKED LT AFT LOWER CORNER. REMOVED AND REPLACED NLG DRAG BRACE SHELF PER S/B 727-53-108 AND SRM 51-10-1.
- [SDR 97FDEA00016](https://openairdocs.org/sdr/97FDEA00016.md): Pin Casting · cracked · Dec 23, 1996 · N117FE · Boeing 72725C · Wing Miscellaneous Structure
  > RT WING, THE FWD TERMINAL PIN CASTING AT STA 740 IS CRACKED IN INSIDE BORE ON I/B LWR SIDE OF BORE. REMOVED AND REPLACED THE RT WING FWD WING TO FUSE TERMINAL PIN CASTING AT STA 740 IAW EA 7-5710-28934, EA 7-5710-28952, BOEING DWG NR 62C29064, BOEING DEG 65-1
- [SDR 97FDEA00009](https://openairdocs.org/sdr/97FDEA00009.md): Fitting · corroded · Dec 23, 1996 · N117FE · Boeing 72725 · Fuselage, Wing Attach Fittings
  > FUSE STA 740 LT WING ATTACH FWD FITTING CORRODED, FOR LT FWD BOTTLE BOLT. REMOVED CORROSION BY REAMING BORE PER BOEING SRM 57-10-7 FIG 2, SHEET 1. FABRICATED AND INSTALLED SLEEVE PER SRM 57-10-7, FIG 2 SHEET 5.
- [SDR 97FDEA00003](https://openairdocs.org/sdr/97FDEA00003.md): Skin · corroded · Dec 23, 1996 · N117FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER FUSE SKIN STR 10 L STA 863 TO 875, FOUND DURING REPLACEMENT OF 870 CASTING. REMOVED CORROSION AND INST DOUBLER AND FILLER ON OUTSIDE OF FUSE PER EA 7-5330-28946 DOUBLER 2024 T 3.071.
- [SDR 97FDEA00002](https://openairdocs.org/sdr/97FDEA00002.md): Bulkhead Forging · cracked · Dec 23, 1996 · N117FE · Boeing 72725 · Fuselage Main, Bulkhead
  > LT FUSE 870 BULKHEAD FORGING. CRACKED BEYOND LIMITS OF SB 727-53-116, REF NR S001. INSTALLED NEW LT 870 FORGING PER FED EX EA 7-5310-28935, SB 727-53-116, SRM 51-30-2.
- [SDR 96FDEA01701](https://openairdocs.org/sdr/96FDEA01701.md): Spar Web · mis-manufactured · Dec 11, 1996 · N117FE · Boeing 72725C · Wing Spar
  > NR 1663 RT WING, FRONT SPAR WEB MILLED BEYOND DRAWING 65C29064 SPECIFICATIONS. FABRICATED NEW SPLICES AND INSTALLED SPICES PER EA 7-5710-28952DATED 12/10/96 AND ACCOMPLISHED REMAINING EA 7-5710-28952 DTD 12/10/96 INSTRUCTIONS.
- [SDR 96FDEA01700](https://openairdocs.org/sdr/96FDEA01700.md): Skin · oversized hole · Dec 11, 1996 · N117FE · Boeing 72725C · Fuselage Main, Plate/Skin
  > NR 1653 STRINGER 9L FASTENER HOLE IN FUSELAGE SKIN IS OVERSIZED AT STA 870 WING TO FUSE TERMINAL PIN CASTING. INSTALLED FREEZE PLUG AND DOUBLER PER EA 7-5330-28947A.
- [SDR FDEA01673](https://openairdocs.org/sdr/FDEA01673.md): Floorbeam · corroded · Nov 15, 1996 · N117FE · Boeing 72725C · Fuselage Main, Floor Beam
  > CORROSION ON VERTICAL WEB OF BS 640 FLOORBEAM RBL 52 THROUGH RBL 61 AFT SIDE UNDER TOP CHORD. REMOVED CORROSION FROM VERTICAL WEB OF BS 640 FLOORBEAM RBL 52 THROUGH RBL 61. AFT SIDE FABRICATED, REPAIR DOUBLER FOR BS 640 FLOORBEAM VERTICAL WEB 17 RBL 52 TO RB
- [SDR 96FDEA01680](https://openairdocs.org/sdr/96FDEA01680.md): Floorbeam · corroded · Nov 15, 1996 · N117FE · Boeing 72725C · Fuselage Main, Floor Beam
  > CORROSION ON UPPER FLANG OF FLOORBEAM STA 312 LBL 4. CUT OUT CORROSION ALONG WITH CORROSION AND DAMAGE FROM NR 0708 AND NR 1434 OF INST DOUBLER PER SRM 53-10-8 FIG 7 FROM LBL 29 TO RBL 9.
- [SDR 96FDEA01679](https://openairdocs.org/sdr/96FDEA01679.md): Fitting · cracked · Nov 14, 1996 · N117FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > UPPER LOBE; END FITTING CRACK FWD OF STA 870 STR 2R. REMOVED AND REPLACED STR 2R END FITTING FWD OF STA 870 PER 51-10-1 SRM.
- [SDR 96FDEA01678](https://openairdocs.org/sdr/96FDEA01678.md): Rib · cracked · Nov 14, 1996 · N117FE · Boeing 72725C · Horizontal Stabilizer, Spar/Rib
  > HORZ STAB RT SIDE RIB CRACKED, FWD UPPER CHORD, I/B SIDE STA 17.20. REMOVED AND REPLACED CHORD RIB PER EA 7-5510-20214.
- [SDR 96FDEA01672](https://openairdocs.org/sdr/96FDEA01672.md): Floorbeam · corroded · Nov 14, 1996 · N117FE · Boeing 72725C · Fuselage Main, Floor Beam
  > MAIN CARGO FLOORBEAM STA 640 RBL 45 TO 60 HAS CORROSION AND PREVIOUS REPAIR DOES NOT COVER DAMAGE AREA. REMOVED TOP CHORD OF BS 640 FLOORBEAM FROM RBL 19 TO RT OUTBOARD SKIN, FABRICATED NEW TOP CHORD AND REPAIR ANGLES AND STRAPS PER SRM 53-10-8 FIG 5.
- [SDR 96FDEA01669](https://openairdocs.org/sdr/96FDEA01669.md): Floorbeam · corrosion · Nov 5, 1996 · N117FE · Boeing 72725C · Fuselage Main, Floor Beam
  > MAIN CARGO COMPARTMENT STA 580 FLOORBEAM RBL 45 FROM C/L, UPPER CHORD OF BEAM CORRODED AFT SIDE AT FASTENERS ON FLOORBEAM. CORROSION REMOVED, THICKNESS LESS THAN ALLOWABLE LIMITS AFTER REPAIR. INSTALLED STRAP PER AARD 53-10-07-2 FIGURE 1. REPAIR INSTALLED A
- [SDR 96FDEA01676](https://openairdocs.org/sdr/96FDEA01676.md): Floorbeam · corroded · Nov 3, 1996 · N117FE · Boeing 72725C · Fuselage Main, Floor Beam
  > UPPER LOBE FLOORBEAM HAS CORROSION STA 400 RBL 27 TO RBL 35. INSTALLED REPAIR STRAP TO FLOORBEAM PER SRM 53-10-8.
- [SDR 96FDEA01677](https://openairdocs.org/sdr/96FDEA01677.md): Fitting · cracked · Nov 1, 1996 · N117FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > STR 4R END FITTING CRACKED AT STATION 870 FWD SIDE. REMOVED AND REPLACED STR END FITTING PER 51-10-01.
- [SDR 96FDEA01671](https://openairdocs.org/sdr/96FDEA01671.md): Frame · cracked · Oct 29, 1996 · N117FE · Boeing 72725C · Fuselage Main, Frame
  > STA 440 FRAME IS CRACKED AT STR 9 LT. TRIMMED OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-4 FIG 2 PAGE 7 TO 11.
- [SDR 96FDEA01675](https://openairdocs.org/sdr/96FDEA01675.md): Chord · corrosion · Oct 28, 1996 · N117FE · Boeing 72725C · Wing Miscellaneous Structure
  > CENTER WING AFT WEB UPPER CHORD BULGED AND CORROSION EMANTING FROM BETWEEN WEB AND CHORD AT STA 870 W/L 190 LBL 30. REMOVED CORRODED WEB AND UPPER CHORD STA 870 LBL 70 RBL 70. INSTALLED REPAIR PER ESO 11697 DATED 9-10-96, PER SRM 57-10-00.
- [SDR 96FDEA01674](https://openairdocs.org/sdr/96FDEA01674.md): Floorbeam · corroded · Oct 28, 1996 · N117FE · Boeing 72725C · Fuselage Main, Floor Beam
  > FUSELAGE UPPER LOBE; CORROSION ON FLOORBEAM BETWEEN LBL 0 TO LBL 26 SEAT TRACKS STA 560. REMOVED CORROSION PER SRM 51-10-6, ALODINED AND PRIMED AREA, FABRICATED AND INSTALLED STRAP REPAIR LBL 0 TO LBL 26 STA 560 AS PER EA 7-5310-78928. INSTALLED ADDITIONAL
- [SDR 96FDEA01670](https://openairdocs.org/sdr/96FDEA01670.md): Casting · corrosion · Oct 25, 1996 · N117FE · Boeing 72725C · Ailerons
  > LT AILERON NR 3 HINGE CASTING HAS CORROSION AT HINGE PIN AREA. REMOVED AND REPLACED CASTING PER 51-10-1 SRM.
- [SDR 96FDEA01668](https://openairdocs.org/sdr/96FDEA01668.md): Casting · corrosion · Oct 25, 1996 · N117FE · Boeing 72725C · Ailerons
  > NR 0932, LT OUTBOARD AILERON NR 2 HINGE CASTING HAS CORROSION AT LOWER HINGE HOLES. REMOVED AND REPLACED CASTING PER SRM 51-10-01, (P/N 5700200) HINGE ASSY.
- [SDR 96FDEA01681](https://openairdocs.org/sdr/96FDEA01681.md): Vert Stiffener · cracked · Oct 21, 1996 · N117FE · Boeing 72725C · Wing Miscellaneous Structure
  > VERTICAL STIFFINER ON CENTER WING AFT WEB AFT SIDED CRACKED APPROX 4 INCHES AT UPPER END STA 868 RBL 40 WL 190. REMOVED STIFFENER AND INSTALLED NEW STIFFENER PER SRM 51-10-1.

## 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 = 'N117FE' AND deregistration_id = 'N117FE-2004-08-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N117FE-2004-08-26/reports

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