# Service difficulty reports: N118FE, cancelled Oct 31, 2002

A list on [N118FE, cancelled Oct 31, 2002](https://openairdocs.org/deregistered/N118FE-2002-10-31.md).

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

- [SDR 01FDEA00391](https://openairdocs.org/sdr/01FDEA00391.md): Stringer · cracked · May 29, 2001 · N118FE · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > AT BS 400 STR 1, 2R & 3L ARE CRACKED AT FASTENER COMMON TO STR AND FRAME. REMOVED AND REPLACED STRINGERS PER IAW FEDEX EA 7-5310-57956.
- [SDR 00FDEA00718](https://openairdocs.org/sdr/00FDEA00718.md): Valve · damaged · Oct 11, 2000 · N118FE · Boeing 72725C · Nose/Tail Landing Gear
  > RED GEAR DOOR LIGHT AND AMBER NOSE GEAR DOOR LIGHT REMAIN ON. ASSOCIATED AIR NOISE AND VIB FELT IN NOSE GEAR AREA. RED TAB PROC AND CYCLE GEAR. *S/D* REMOVED AND REPLACED NOSE STRUT CHARGING VALVE AND SERVICED WITH FLUID AND NITROGEN. PER GEAR RETRACTION
- [SDR 00FDEA00676](https://openairdocs.org/sdr/00FDEA00676.md): Valve · malfunctioned · Sep 22, 2000 · N118FE · Boeing 72725C · Engine Bleed Air System
  > AFT T/O BRING RT PACK ON, TURNED NR 3 BLD ON AND RT PACK ON. AFT COMING ON A LOUD BOOMING NOISE HEARD AND MOMENTARY PRESS SPIKE IN CABIN. *S/D* REMOVED AND REPLACED NR 3 ENG BLEED AIR SHUTOFF VALVE. REMOVED AND REPLACED NR 3 ENG HIGH PRESS MODULATING AND S
- [SDR 00FDEA00565](https://openairdocs.org/sdr/00FDEA00565.md): Control Cable · out of adj · Aug 22, 2000 · N118FE · Boeing 72725C · Landing Gear Position and Warning
  > ON T/O, LANDING GEAR SELECTED UP, GEAR CAME UP WITH VIB AFT GREEN/RED GEAR IND WENT OUT WITH THE EXCEPTION OF THE RED DOOR LIGHT ON FWD PNL (NOSE). COMPLIED WITH RED TABS. A/C RELEASED FOR SERVICE PER MEL. *S/D* ADJUSTED NOSE GEAR DOORS PER MM 32-22-1. AD
- [SDR 99FDEA00292](https://openairdocs.org/sdr/99FDEA00292.md): Connector · dirty · Jul 28, 1999 · N118FE · Boeing 72725C · Landing Gear Position and Warning
  > 99-177 - LEFT LANDING GEAR DOOR LIGHT IND UNSAFE. AFT CYCLING GEAR, RED LIGHT EXTINGUISHED. CK LEFT DOOR SWITCH ADJUSTMENT PER MM 32-62-011-4. CLEANED AND SECURED CONNNECTOR. DOOR AND LIGHT CHECK NORMAL.
- [SDR 99FDEA00071](https://openairdocs.org/sdr/99FDEA00071.md): Skin · cracked · Feb 21, 1999 · N118FE · Boeing 72725C · Fuselage Main, Plate/Skin
  > LEFT SIDE OF FUSELAGE BS 1150 3 ABOVE STR S4L SHEAR FASTENER HEAD AND SKIN CRACK. REPAIRED PER SRM 53-30-3 FIG 13A.
- [SDR 98FDEA00654](https://openairdocs.org/sdr/98FDEA00654.md): Skin · corroded · Oct 19, 1998 · N118FE · Boeing 72725C · Fuselage Main, Plate/Skin
  > NR 273 BULGING SKIN AT BS 340-342, RBL 18, WL 148. ** S/D ** REPAIRED SKIN AT BS 338, RBL 21, WL 148 IAW FEDEX SRM 53-30-03.
- [SDR 98FDEA00617](https://openairdocs.org/sdr/98FDEA00617.md): Chord · corroded · Oct 5, 1998 · N118FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > CORROSION (C-53-100-01,1) ON BS 351.2 FRAME BETWEEN STR 26 AND 27 LT. *S/D* REMOVED AND REPLACED BS 351.2 LOWER REINFORCEMENT CHORD PER FEDEX SRM 51-30-2.
- [SDR 98FDEA0583](https://openairdocs.org/sdr/98FDEA0583.md): Frame · corroded · Sep 17, 1998 · N118FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > PAE - NR 0546 - CORROSION (C53-100-010) ON E/E DOOR FRAME AT BS 423, RBL 4 - LBL 4, WL 148. (X)
- [SDR 98FDEA00583](https://openairdocs.org/sdr/98FDEA00583.md): Frame · corroded · Sep 17, 1998 · N118FE · Boeing 72725C · Fuselage Main, Frame
  > NR 546 CORROSION (C53-100-010) ON E&E DOOR FRAME AT BS 423, RBL 4-LBL 4, WL 148. ** S/D ** R&R E & E DOOR FRAME AT BS 423, WL 148 PER FEDEX SRM 51-30-2 & FEDEX SRM 51-10-1.
- [SDR 98FDEA00536](https://openairdocs.org/sdr/98FDEA00536.md): Beam · cracked · Aug 28, 1998 · N118FE · Boeing 72725C · Cargo/Baggage Doors
  > NR 0072 AFT CARGO DOOR #4 TRANSVERSE BEAM HAS CRACK INDICATION AT OUTBOARD FLANGE. *** S/D *** R&R #4 TRANSVERSE BEAM IN AFT CARGO DOOR IAW FEDEX SRM 51-30-2.
- [SDR 98FDEA00535](https://openairdocs.org/sdr/98FDEA00535.md): Skin · creased · Aug 27, 1998 · N118FE · Boeing 72725C · Cargo/Baggage Doors
  > FWD CARGO DOOR OUTER SKIN IS DENTED 17 AFT OF FWD EDGE AND 27 UP FROM BOTTOM. *S/D* REPAIRED FWD CARGO DOOR 17 AFT OF FWD EDGE AND 27 UP FROM BOTTOM, PER FEDEX SRM 52-00-3.
- [SDR 98FDEA00533](https://openairdocs.org/sdr/98FDEA00533.md): Channel · cracked · Aug 26, 1998 · N118FE · Boeing 72725C · Cargo/Baggage Doors
  > NR0424 FWD CARGO DOOR #4 TRANSVERSE BEAM (FROM BOTTOM) IS CRACKED IN OUTBOARD RADIUS. *** S/D ***R&R FWD CARGO DOOR #4 TRANSVERSE BEAM IAW FEDEX DRAWING 65-18620.
- [SDR 98FDEA00532](https://openairdocs.org/sdr/98FDEA00532.md): Shear Web · corroded · Aug 25, 1998 · N118FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > CORROSION (C53-224-08) ON SHEAR WEB BS 1166 TO 1174, LBL 37, WL 208. *S/D* REPAIRED SHEAR WEB AT BS 1166 TO 1174, LBL 37, WL 208 PER FED-EX SRM 51-40-2.
- [SDR 98FDEA00516](https://openairdocs.org/sdr/98FDEA00516.md): Skin · corroded · Aug 17, 1998 · N118FE · Boeing 72725C · Fuselage Main, Plate/Skin
  > BS 440 TO 680, STR 1 TO STR 3 LT SHOWS SIGN OF CORROSION DUE TO SKIN PILLOWING AND DISHED RIVET HEADS. *S/D* REMOVED AND REPLACED CROWN SKIN AT STA 440 TO 740, STR 4 LT- STR 4 RT PER FED EX EA 7-5330-42276.
- [SDR 98FDEA00485](https://openairdocs.org/sdr/98FDEA00485.md): Longeron · corroded · Aug 4, 1998 · N118FE · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > STA-PAE: CORROSION ON LONGITUDINAL BS 836 AND 839, RBL 45, WL 208.1. *S/D* REMOVED DAMAGE LONG BEAM FROM BS 760-850, RBL 45, WL 208.1 AND REPLACED PER FEDEX DRAWING 65-34144.
- [SDR 98FDEA00470](https://openairdocs.org/sdr/98FDEA00470.md): Skin · delaminated · Jul 23, 1998 · N118FE · Boeing 72725C · Trailing Edge Flaps
  > NR 0455 005 STA-PAE: STEEL RUBSTRIP IS DISBONDED ON R/W I/B FOREFLAP I/B END. *** S/D *** REPAIRED R/W I/B FOREFLAP I/B END UPR & LWR SURFACES PER FEDEX SRM 51-40-6 & DRAWING 65-32738.
- [SDR 98FDEA00469](https://openairdocs.org/sdr/98FDEA00469.md): Fitting · cracked · Jul 23, 1998 · N118FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > NR 0478 STA-PAE - VISUAL DAMAGE, CRACK AND CORROSION INDICATION NOTED IN HOLES NR 1 THROUGH 5 OF ROW 2 BS 870 RIGHT TERMINAL FITTING. REPAIRED HOLES NR 1 - 5 OF ROW 2, BS 870 RIGHT TERMINAL FITTING PER FEDEX EA 7-5310-39911.
- [SDR 98FDEA00468](https://openairdocs.org/sdr/98FDEA00468.md): Fitting · cracked · Jul 23, 1998 · N118FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > NR 0421 STA-PAE - MECHANICAL DAMAGE NOTED IN HOLES NR 1 THROUGH 5 OF ROW 3 BS 870 LEFT TERMINAL FITTING. REPAIRED MECH DAMAGED HOLES IN LEFT TERMINAL FITTING AT BS 870 HOLE NR 1 THROUGH NR 5 OF ROW 3 PER EA NR 7-5310-39910.
- [SDR 98FDEA00467](https://openairdocs.org/sdr/98FDEA00467.md): Fitting · cracked · Jul 23, 1998 · N118FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > NR0420 STA-PAE - CRACKS NOTED BY NDI IN HOLE NR 1 AND NR 2 OF ROW 2 BS 870 LEFT TERMINAL FITTING. REPAIRED LEFT TERMINAL FITTING AT BS 870 HOLE NR 1 AND NR 2 OF ROW 2 PER EA NR 7-5310-39910.
- [SDR 98FDEA00466](https://openairdocs.org/sdr/98FDEA00466.md): Fitting · cracked · Jul 23, 1998 · N118FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > NR0479 STA-PAE - CRACK INDICATION NOTED IN HOLE NR 1 OF ROW 3, BS 870 RIGHT TERMINAL FITTING. REPAIRED HOLE NR 1 OF ROW 3, BS 870 RIGHT TERMINAL FITTING PER FEDEX EA 7-5310-39911.
- [SDR 97FDEA00690](https://openairdocs.org/sdr/97FDEA00690.md): Retract Mech · failed · Sep 26, 1997 · N118FE · Boeing 72725C · Leading Edge Slat Control System
  > AFTER TAKEOFF, NR 2 LEADING EDGE FLAP WOULD NOT RETRACT WHEN HANDLE MOVED FROM 5 TO 2. RED TABS WHERE FOLLOWED BUT PROBLEM STILL EXIST RETURNED TO ATL. CLEANED AND RESEATED CANNON PLUG NR 2 LEADING EDGE FLAP, OPERATIONAL CHECK NORMAL.
- [SDR 97FDEA00050](https://openairdocs.org/sdr/97FDEA00050.md): Door Mechanism · not latched · Jan 17, 1997 · N118FE · Boeing 72725C · Passenger/Crew Doors
  > AIRCRAFT WOULD NOT HOLD PRESSURE ABOVE 2,000 FT GROUND LEVEL. PRESSURIZATION WOULD RESPOND IN MANUAL BUT ONLY TO 10,000 CABIN PRESSURE. THEN EVEN IN FULL MANUAL INCREASE CABIN WOULD CLIMB AT 1,500 TO 1,800 FT PER MINIMUM RATE OF CLIMB. FORWARD ENTRY DOOR WA
- [SDR 96FDEA01055](https://openairdocs.org/sdr/96FDEA01055.md): Hyd Line · leaking · May 30, 1996 · N118FE · Boeing 72725C · Hydraulic System, Main
  > HYDRAULIC SYSTEM-A FAILURE, QTY DROPPED TO ZERO, MANUALLY CRANKED GEAR DOWN. FLUID SHUTOFF VALVES OFF FOR 30 MINUTES PRIOR TO ENGINE SHUTDOWN. PARTS CATALOG 27-60-00 FIG 20 PG 1, FOUND HYD FLUID LEAKING FROM B-NUT TO T-FITTING NR 60 AND A SMALLER LEAK AT T-F
- [SDR 96FDEA00312](https://openairdocs.org/sdr/96FDEA00312.md): Forging · cracked · Feb 23, 1996 · N118FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > HFEC IND A CRACK IN LT STA 870 FORGING AT INTEGRAL RIB, BELOW CABIN FLOOR WL 190 ON TOP SIDE AT LOWER AFT FASTENER CRACK. ALSO, RUNNING UNDER RIB EXTENDING AFT. REMOVED INTEGRAL RIB FLUSH WITH WEB, PER ESO 11782. HFEC CONFIRMED NO CRACKS AFTER DAMAGE REMOVA
- [SDR 96FDEA00311](https://openairdocs.org/sdr/96FDEA00311.md): Floorbeam · corroded · Feb 20, 1996 · N118FE · Boeing 72725C · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM AT STA 950 IS CORRODED AROUND SCREW HOLES TOP AND BOTTOM OF BEAM FROM SEAT TRACK NR 3 TO NR 5. REMOVED CORROSION PER 51-10-06, OUT OF LIMITS. REPAIRED PER ESO 11782 AND FEDEX EA 7-5310-27477.
- [SDR 96FDEA00310](https://openairdocs.org/sdr/96FDEA00310.md): Bellframe · plugged hole · Feb 13, 1996 · N118FE · Boeing 72725C · Fuselage Main, Frame
  > STR 27L BELLFRAME 990 PLUGGED HOLE TOP NEAR EXISTING FASTENER HOLE. INSTALLED DOUBLER PER SRM 51-40-3.
- [SDR 96FDEA00309](https://openairdocs.org/sdr/96FDEA00309.md): Web · corroded · Feb 13, 1996 · N118FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > LOWER FUSE CENTER TANK REAR SPAR UPPER CHORD, 3 RIVETS HAD POPPED 2 RIVETS WORKING, SKIN WARP BULGE LBL 18 TO 30. INSTALLED DOUBLER AND TRIPLER TO CENTER TANK UPPER WEB PER ESO 11782 DATED 2-13-96, AWAITING FEDEX EA.
- [SDR 96FDEA00307](https://openairdocs.org/sdr/96FDEA00307.md): Stringer · cracked · Feb 6, 1996 · N118FE · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > UPPER LOBE MAIN CARGO INTERIOR STRUCTURE, STR 15L CRACKED AT FS 676. REMOVED DAMAGED SECTION OF STR 15L AND INSTALLED STR SPLICE REPAIR PER SRM 53-10-3 FIG 1 PG 3 TO 48.

## 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 = 'N118FE' AND deregistration_id = 'N118FE-2002-10-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N118FE-2002-10-31/reports

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