# Service difficulty reports: N497FE, cancelled Mar 19, 2013

A list on [N497FE, cancelled Mar 19, 2013](https://openairdocs.org/deregistered/N497FE-2013-03-19.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 · 52 reports

- [SDR 08FDEA02845](https://openairdocs.org/sdr/08FDEA02845.md): Stringer · cracked · Jul 12, 2008 · N497FE · Boeing 727232 · Wing, Longeron/Stringer
  > RT WING, STR 10 CRACKED AT WS 656.5, ITEM IS AD DRIVEN, IF CRACKS EXCEED LIMITS IN SECTION II, FIG 12, CONTACT FED EX STRUCTURES ENGINEERING FOR REPAIR INSTRUCTIONS PER WORK CARD E7-5710-7-4322. STOP DRILLED CRACK, VERIFIED CRACK TERMINATION AT STOP DRILL, LO
- [SDR 01FDEA00831](https://openairdocs.org/sdr/01FDEA00831.md): Line · loose · Sep 8, 2001 · N497FE · Boeing 727232 · Engine Thrust Reverser
  > NR 3 ENG STRUT O/H LIGHT ILLUM DURING CLIMBOUT. RAN ENG WITH BOTH PACKS AT HIG 5 MIN, NO O/H LIGHT. TIGHTENED LEAKING THRUST REVERSER FLEX LINE. OK FOR SERVICE.
- [SDR 01FDEA00815](https://openairdocs.org/sdr/01FDEA00815.md): Connector · dirty · Sep 8, 2001 · N497FE · Boeing 727232 · Overheat Detection
  > ON DEPARTURE NR 3 STRUT O/H LIGHT CAME ON. REMOVED, CLEANED NR 3 ENG LOOP CONNECTOR PER MM REF ATA 20. RESECURED STRUT PANELS.
- [SDR 01FDEA00015](https://openairdocs.org/sdr/01FDEA00015.md): Detector · activated · Jan 10, 2001 · N497FE · Boeing 727232 · Overheat Detection
  > 01-004 AT 5000 FT ON CLB OUT NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON. NO IRREGULARITIES NOTED. CLEANED OVERHEAT DETECTION ELEMENT. RAN NR 3 ENGINE IAW JET RUN HANDBOOK, NO LEAKS NOTED. OK FOR SERVICE.
- [SDR 00FDEA00878](https://openairdocs.org/sdr/00FDEA00878.md): Connector · contaminated · Dec 14, 2000 · N497FE · Boeing 727232 · Landing Gear Position and Warning
  > 00-359 LEFT GEAR DOOR WARN LIGHT. RED TAB ACCOMPLISHED. CLEANED CANNON PLUG WITH SOLVENT. OPS CK GOOD PER BOEING MM 32-62-00.
- [SDR 00FDEA00382](https://openairdocs.org/sdr/00FDEA00382.md): Module · malfunctioned · Jun 8, 2000 · N497FE · Boeing 727232 · Landing Gear Position and Warning
  > LT MG LIGHT WON''T EXTINGUISH AFT GEAR RAISED. RECYCLED GEAR PER RED TABS. GEAR LIGHT WENT OUT WITH GEAR DOWN. AMBER LIGHT ON 2ND OFF PNL WAS NOT ON WITH GEAR UP. *S/D* REMOVED AND REPLACED LG ELECTRICAL/ELECTRONIC MODULE PER MM 32-09-121-4. OPS TEST PER
- [SDR 00FDEA00354](https://openairdocs.org/sdr/00FDEA00354.md): Seat Track · corroded · May 23, 2000 · N497FE · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE BS 993, RBL 48, WL 208. *S/D* REPLACED PER FEDEX SRM 53-10-1, 51-20-2, 51-30-2.
- [SDR 00FDEA00313](https://openairdocs.org/sdr/00FDEA00313.md): Seat Track · corroded · May 1, 2000 · N497FE · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TOP OF EXPANSION JOINT FOUND AFT REMOVAL OF SEAT TRACK BS 758, LBL 25, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-30-02.
- [SDR 00FDEA00310](https://openairdocs.org/sdr/00FDEA00310.md): Floorbeam · corroded · May 1, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor Beam
  > LONGITUDINAL FLOORBEAM BS 760 - 848, LBL 45, WL 208. CORRODED AROUND NUT PLATES. *S/D* REMOVED AND REPLACED PART PER FEDEX SRM 51-30-02.
- [SDR 00FDEA00311](https://openairdocs.org/sdr/00FDEA00311.md): Beam · corroded · Apr 30, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON LONGITUDINAL BEAMS 816, RBL 25, WL 208 TO BS 848. *S/D* REMOVED AND REPLACED PART PER FEDEX SRM 51-30-02.
- [SDR 00FDEA00303](https://openairdocs.org/sdr/00FDEA00303.md): Fitting · corroded · Apr 27, 2000 · N497FE · Boeing 727232 · Entrance Stairs
  > AFT AIRSTAIR LT AFT UPLOCK FITTING ON AIRSTAIR CORRODED. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-30-2.
- [SDR 00FDEA00302](https://openairdocs.org/sdr/00FDEA00302.md): Skin · cracked · Apr 27, 2000 · N497FE · Boeing 727232 · Fuselage Main, Plate/Skin
  > CRACK IND NOTED WITH HFEC INSP ADJACENT TO FASTENER IN LAP JOINT ROW OF FASTENERS BS 528, STR 4 RT. *S/D* REMOVED AND REPLACED PER EO 00-5117 & FEDEX SRM 53-30-3 FIG 5 AND FEDEX EA 7-5330-50061.
- [SDR 00FDEA00280](https://openairdocs.org/sdr/00FDEA00280.md): Floor Support · corroded · Apr 21, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > NR 325 CORROSION ON THE UNDERSIDE OF L/H FLOOR TO SIDEWALL SUPPORT AROUND THE STANCION SUPPORT, BS 500, WL 155, LBL 23 AT STR 26 L/H. ** S/D ** R&R PART PER SRM 51-10-1.
- [SDR 00FDEA00279](https://openairdocs.org/sdr/00FDEA00279.md): Floor Support · corroded · Apr 21, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > NR 328 CORROSION ON THE UNDERSIDE OF THE LT SIDEWALL TO FLOOR SUPPORT AROUND THE STANCION SUPPORT, BS 552 - 480, LBL 23, WL155. ** S/D ** REMOVED, DRILLED, & INSTALL PART PER SRM 51-30-2.
- [SDR 00FDEA00278](https://openairdocs.org/sdr/00FDEA00278.md): Floor Support · corroded · Apr 21, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > NR 330, CORROSION ON TOP OF LT FLOOR TO SIDEWALL SUPPORT AROUND NUTPLATES FROM BS 590 TO 650, LBL 23, WL 155 AT STR LH 26.** S/D ** R&R PER SRM 51-30-2 & 51-30-5, 51-30-1.
- [SDR 00FDEA00277](https://openairdocs.org/sdr/00FDEA00277.md): Stringer · cracked · Apr 21, 2000 · N497FE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > BS 720B+4, STR 15L, STRINGER CRACKED AT FASTENER HOLE. *S/D* REMOVED AND REPLACED STRINGER PER FEDEX 727 SRM 53-10-3 FIG 5 STEP 3 & SRM 53-10-3 FIG 1.
- [SDR 00FDEA00267](https://openairdocs.org/sdr/00FDEA00267.md): Floorbeam · corroded · Apr 18, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor Beam
  > NR 457 CORROSION ON FLOORBEAM LWR SURFACE OF UPPER FWD FLANGE BS 48, RBL 25, WL 208. ** S/D ** R&R FLOORBEAM.
- [SDR 00FDEA00265](https://openairdocs.org/sdr/00FDEA00265.md): Floorbeam · corroded · Apr 18, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor Beam
  > NR 1064, 1070 LOWER CHORD CORRODED AROUND NUTPLATES FROM RBL 25- LBL 25. ** S/D ** R&R PER SRM 53-1-1.
- [SDR 00FDEA00266](https://openairdocs.org/sdr/00FDEA00266.md): Channel · cracked · Apr 18, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > NR 1307 CRACKED FAIRING SUPPORT BRACKET AT BS 722, RBL 10, WL 140. ** S/D ** R&R PART PER 51-10-2., 51-30-1.
- [SDR 00FDEA00270](https://openairdocs.org/sdr/00FDEA00270.md): Stringer · cracked · Apr 18, 2000 · N497FE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > NR 470 BS 720B+4, STR 15R STRINGER CRACKED AT FASTENER HOLE. ** S/D ** R&R STR PER FEDEX SRM 53-10-3.
- [SDR 00FDEA00269](https://openairdocs.org/sdr/00FDEA00269.md): Frame · corroded · Apr 18, 2000 · N497FE · Boeing 727232 · Fuselage Main, Frame
  > NR 1103 TWO FASTENERS LOOSE AND CAUSED FRETTING CORROSION. ** S/D ** R&R PER SRM 51-30-2.
- [SDR 00FDEA00268](https://openairdocs.org/sdr/00FDEA00268.md): Stringer · cracked · Apr 18, 2000 · N497FE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > NR 473 BS 720B+16, STR 15L STRINGER CRACKED AT FASTENER. ** S/D ** R&R REPAIR PER FEDEX 727 SRM 53-10-3 FIG 5.
- [SDR 00FDEA00271](https://openairdocs.org/sdr/00FDEA00271.md): Seat Track · corroded · Apr 18, 2000 · N497FE · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BS 480 - 590, LBL 45, WL 208. *S/D* REMOVED AND REPLACED PER SRM 51-30-2, 51-10-2, 51-30-5 & 53-10-5.
- [SDR 00FDEA00257](https://openairdocs.org/sdr/00FDEA00257.md): Channel · corroded · Apr 17, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > NR 829 CORROSION (C53-111-01-1) BETWEEN STRAP & FLOOR STRUCTURE AT BS 302, LBL 46, WL 207 AT MISSING NUT PLATE. ** S/D ** R&R PER FEDEX SRM 51-30-2.
- [SDR 00FDEA00262](https://openairdocs.org/sdr/00FDEA00262.md): Stringer · corroded · Apr 17, 2000 · N497FE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > NR 1071, CORROSION ON STRINGER 28 RT AT BS 524 - 528. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3.
- [SDR 00FDEA00261](https://openairdocs.org/sdr/00FDEA00261.md): Stringer · cracked · Apr 17, 2000 · N497FE · Boeing 727232 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER STR 9 RT IS CRACKED WHERE IT ATTACHES TO RIB NR 7. *S/D* REMOVED AND REPLACED NEW STRINGER PER FEDEX SRM 55-30-04 PG 5.
- [SDR 00FDEA00260](https://openairdocs.org/sdr/00FDEA00260.md): Floorbeam · corroded · Apr 17, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM UPPER FLANGE BS 328, LBL 2 - 20, WL 208. *S/D* REMOVED AND REPLACED REPAIR PER SRM 53-10-1, 53-10-8, 51-20-1.
- [SDR 00FDEA00259](https://openairdocs.org/sdr/00FDEA00259.md): Skin · corroded · Apr 17, 2000 · N497FE · Boeing 727232 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERIOR SKIN OF FORWARD CARGO BAY AT BS 527, RBL 7, WL 147. *S/D* REPAIRED PER SRM 53-30-3 & FEDEX EA 7-5330-50044.
- [SDR 00FDEA00258](https://openairdocs.org/sdr/00FDEA00258.md): Skin · cracked · Apr 17, 2000 · N497FE · Boeing 727232 · Fuselage Main, Plate/Skin
  > NR 271 CRACKS IN EXTERNAL SKIN AT STRINGERFASTENERS, BS 524-528, RBL 6, STR 28. ** S/D ** REPAIRED PER SRM 53-30-3 & FEDEX EA 7-5330-50044.
- [SDR 00FDEA00237](https://openairdocs.org/sdr/00FDEA00237.md): Intercostal · cracked · Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > NR 1088, REMOVED AND REPLACED CRACKED INTERCOSTAL AT BS 358, LBL 67, WL 216. ** S/D ** R&R PART PER IAW FEDEX SRM 51-40-2, 51-30-2, 51-10-2 & 51-30-6.
- [SDR 00FDEA00240](https://openairdocs.org/sdr/00FDEA00240.md): Stringer Clip · cracked · Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > CRACKED STRINGER CLIP 10R, BL 700. *S/D* REMOVED AND REPLACED STR.
- [SDR 00FDEA00239](https://openairdocs.org/sdr/00FDEA00239.md): Stringer Clip · cracked · Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > BS 660, STR 7R STRINGER CLIP CRACKED. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-30-2.
- [SDR 00FDEA00238](https://openairdocs.org/sdr/00FDEA00238.md): Strap · cracked · Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > TIE STRAP AT BS 328, RBL 45, WL 200 IS CRACKED AT PREVIOUS REPAIR. *S/D* REPAIR STRAP PER FEDEX SRM 53-10-8 FIG 6.
- [SDR 00FDEA00234](https://openairdocs.org/sdr/00FDEA00234.md): Strap · corroded · Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > CORROSION (C53-224-04) ON STABILIZER STRAP BS 1070, LBL 25, WL 200. *S/D* REMOVED, FAB & INSTALL PER FEDEX SRM 53-10-8.
- [SDR 00FDEA00243](https://openairdocs.org/sdr/00FDEA00243.md): Strap · cracked · Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > TIE STRAP AT BS 344, RBL 25, WL 200 IS CRACKED AT PREVIOUS REPAIR. *S/D* STOP DRILL CRACK PER FEDEX SRM 51-10-1, 53-10-8 FIG 6.
- [SDR 00FDEA00241](https://openairdocs.org/sdr/00FDEA00241.md): Seat Track · corroded · Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-04) ON SEAT TRACK FLANGE BS 1070, RBL 45, WL 208. *S/D* REMOVED AND REPLACED, ALODINED, PRIMED PER FEDEX SRM 53-10-1 FIG 3, 51-30-5 FIG 1 & 2, 51-10-2.
- [SDR 00FDEA00242](https://openairdocs.org/sdr/00FDEA00242.md): Floorbeam · corroded · Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM UPPER FLANGE AND NUT PLATE HOLE BS 312, LBL 19, WL 208.
- [SDR 00FDEA00233](https://openairdocs.org/sdr/00FDEA00233.md): Floorbeam · corroded · Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM UPPER FLANGE BS 620, LBL 45 TO RBL 25, WL 208.
- [SDR 00FDEA00232](https://openairdocs.org/sdr/00FDEA00232.md): Strap · cracked · Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > TIE STRAP AT BS 312, RBL 45, WL 200 IS CRACKED AT PREVIOUS REPAIR.
- [SDR 00FDEA00231](https://openairdocs.org/sdr/00FDEA00231.md): Stringer Clip · cracked · Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > CRACKED STRINGER CLIP AT BS 700, STR 7L.
- [SDR 00FDEA00222](https://openairdocs.org/sdr/00FDEA00222.md): Floorbeam · corroded · Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor Beam
  > CORROSION ON LWR CHORD FLOORBEAM BS 1130, RBL 16-34 AROUND FASTENER HOLES. ** S/D ** R&R CORROSION FND TO BE OUT OF LIMITS PER ER 005113.
- [SDR 00FDEA00223](https://openairdocs.org/sdr/00FDEA00223.md): Stringer Clip · corroded · Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > NR 0847, CORROSION ON STRINGER CLIP BS 1148, STR 22L, LBL 49, WL 170. ** S/D ** R&R CORROSION FND OUT OF LIMITS IAW SRM 53-10-1. R&R STR CLIP PER IAW SRM 51-30-5, 51-30-2.
- [SDR 00FDEA00230](https://openairdocs.org/sdr/00FDEA00230.md): Floorbeam · corroded · Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM UPPER FLANGE BS 680, BL 0 TO LBL 45, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-8 FIG 3.
- [SDR 00FDEA00229](https://openairdocs.org/sdr/00FDEA00229.md): Skin · misdrilled · Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Main, Plate/Skin
  > SKIN REPAIR BS 1123, STRINGER 9L. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-30-3.
- [SDR 00FDEA00227](https://openairdocs.org/sdr/00FDEA00227.md): Floorbeam · corroded · Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-04) AROUND FASTENER HOLE BS 950F, LBL 11, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-8 FIG 8 & FEDEX SRM 53-10-2 FIG 7 SHEET 2, 24.
- [SDR 00FDEA00228](https://openairdocs.org/sdr/00FDEA00228.md): Floorbeam · corroded · Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM UPPER FLANGE BS 620, LBL 45 TO RBL 25, WL 208.
- [SDR 00FDEA00226](https://openairdocs.org/sdr/00FDEA00226.md): Stringer Clip · cracked · Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > BS 560, STR 10R STRINGER CLIP IS CRACKED.
- [SDR 00FDEA00225](https://openairdocs.org/sdr/00FDEA00225.md): Stringer Clip · cracked · Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > BS 720B, STR 7R STRINGER CLIP CRACKED.
- [SDR 00FDEA00224](https://openairdocs.org/sdr/00FDEA00224.md): Splice · corroded · Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > CORROSION ON FRAME DOUBLER ABOVE STR 24R, BL 1070, RBL 45.
- [SDR 97FDEA00827](https://openairdocs.org/sdr/97FDEA00827.md): Skin · cracked · Nov 11, 1997 · N497FE · Boeing 727232 · Fuselage Main, Plate/Skin
  > CRACK IN SKIN AT LOWER FORWARD CORNER OF CUTOUT, BS 1323, STR 16 LEFT. *S/D* CUT OUT DAMAGED AREA AT BS 1323, STR 16, LT AND FABRICATED FILLERS AND REPAIR DOUBLERS. DRILLED UP ALODINED, PRIMED AND INSTALLED WET WITH SEALANT ALL IAW FED-EX SRM 53-30-3, 51-30

Next page: https://openairdocs.org/deregistered/N497FE-2013-03-19/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 = 'N497FE' AND deregistration_id = 'N497FE-2013-03-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N497FE-2013-03-19/reports

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