# Service difficulty reports: N198FE, cancelled Aug 23, 2006

A list on [N198FE, cancelled Aug 23, 2006](https://openairdocs.org/deregistered/N198FE-2006-08-23.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 · 51 reports

- [SDR 06FDEA1565](https://openairdocs.org/sdr/06FDEA1565.md): Tee Fitting · corroded · Apr 21, 2006 · N198FE · Boeing 727100 · Wing, Landing Gear Attach Fittings
  > DURING EMBODIMENT OF SB 727-57A0132, CORROSION WAS FOUND AFFECTING THE OUTBOARD TEE FITTING ASSOCIATED WITH THE RT MLG. CORROSION WAS REMOVED BY REAMING TO 0.875 INCH AND INSTALLED A REPAIR BUSHING IN THE ADJACENT ATTACH FITTING AND REPAIR IS CLASSIFIED AS MA
- [SDR 05FDEA03870](https://openairdocs.org/sdr/05FDEA03870.md): Odor · detected · Nov 18, 2005 · N198FE · Boeing 727100 · Air Distribution System
  > PASSING FL 180 SMELLED FUMES IN THE COCKPIT. RAN SMOKE AND FUME CHECKLIST. RETURNED TO MEMPHIS. SMELLED LIKE BURNING RUBBER OR PLASTIC. FACT REPLACED BOTH CONDENSER BAGS AND FOUND BOTH RT AND LT AIR CYCLE MACHINES OUT OF OIL REPLACED BOTH ACM RAN BOTH PA
- [SDR 04FDEA00059](https://openairdocs.org/sdr/04FDEA00059.md): Warning Light · illuminated · Jan 6, 2004 · N198FE · Boeing 727100 · Door Warning System
  > MAIN CARGO DOOR LIGHT ILLUMINATED CLIMBING THRU FL270,.79 COMPLETED RED TABS AND LIGHT REMAINED ILLUMINATED. VISUALLY INSPECTED MCD, LATCHES AND ACTUATORS. OPERATED MCD FULL TRAVEL SEVERAL TIMES. MCD OPERATION IS NORMAL PER 727-100 AMM 52-34-009-0. CLEANE
- [SDR 04FDEA00060](https://openairdocs.org/sdr/04FDEA00060.md): Switch · defective · Jan 6, 2004 · N198FE · Boeing 727100 · Door Warning System
  > MAIN CARGO DOOR WARNING LIGHT ILLUMINATED PASSING FL 250, 315 KIAS, CABIN ALTITUDE SHOWED 2000 FEET COMPLETED RED TABS AND LIGHT REMAINED ON. FOUND DOOR WARNING SWITCH SH009 OUT OF ADJUSTMENT, ADJUSTED SWITCH PER M/M 52-70-009-5. ALSO FOUND FWD DOOR WARNING
- [SDR 03FDEA02055](https://openairdocs.org/sdr/03FDEA02055.md): Shear Tie · cracked · Dec 5, 2003 · N198FE · Boeing 727100 · Fuselage Main, Structure
  > CRACKED SHEAR TIE AT BS 336 WL 124 LBL 16 INSIDE TORQUE BOX. *S/D* REMOVED AND REPLACED SHEAR TIE AT BS 336, LBL 16, WL 124 PER SRM 51-20-1, 51-30-2, MM 51-20-021-7, 51-20-151-7.
- [SDR 03FDEA02054](https://openairdocs.org/sdr/03FDEA02054.md): Web · corroded · Dec 5, 2003 · N198FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > ON WEB AT BS 600 STR 26R. REMOVED CORROSION ON WEB & FOUND STR 26R OUT OF LIMITS. REPAIRED STR 26R AT BS 600 & WEB PER SRM 53-10-3 & 51-20-1.
- [SDR 03FDEA02052](https://openairdocs.org/sdr/03FDEA02052.md): Splice · corroded · Dec 4, 2003 · N198FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > CORROSION ON STR 26R AFT OF SPLICE AT BS 486. REPAIRED STRINGER PER SRM 53-10-2, 51-30-5 & 51-30-2, 53-10-3
- [SDR 01FDEA01098](https://openairdocs.org/sdr/01FDEA01098.md): Actuator · failed · Dec 20, 2001 · N198FE · Boeing 72722 · Leading Edge Slat Actuator
  > DURING T/O, NR 7 LEADING EDGE FAILED TO RETRACT. REMOVED AND REPLACED SLAT ACT PER MM 27-81-032-4.
- [SDR 01FDEA00345](https://openairdocs.org/sdr/01FDEA00345.md): Skin · corroded · May 14, 2001 · N198FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > DURING ROUTINE INSP FUSELAGE SKIN FOUND BULGING and CORRODED FROM BS 1154 - 1180 AT STR 19L. *S/D* Removed and replaced PER IAW FEDEX EA 7-5710-57242.
- [SDR 01FDEA00344](https://openairdocs.org/sdr/01FDEA00344.md): Web · corroded · May 14, 2001 · N198FE · Boeing 72722 · Wing, Center Box
  > DURING ROUTINE INSP CTR WING BOX FOUND CORRODED AT BS 870 NEXT TO LWR SPAR CHORD. *S/D* REMOVED AND REPLACED PER IAW FEDEX EA 7-5710-57245.
- [SDR 01FDEA00346](https://openairdocs.org/sdr/01FDEA00346.md): Skin · corroded · May 14, 2001 · N198FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > DURING ROUTINE INSP FUSELAGE SKIN FROM BS 1166 - 1173 BETWEEN STR 20L & STR 21L FOUND BULGING AND CORRODED. *S/D* REMOVED AND REPLACED PER IAW FEDEX EA 7-5710-57242.
- [SDR 01FDEA00343](https://openairdocs.org/sdr/01FDEA00343.md): Angle · corroded · May 14, 2001 · N198FE · Boeing 72722 · Wing, Center Box
  > DURING ROUTINE INSP CTR WING BOX AFT SPAR LWR CHORD ANGLE FOUND CORRODED. R&R PER 727 SRM 57-10-1 FIG 3, 51-10-2.
- [SDR 01FDEA00334](https://openairdocs.org/sdr/01FDEA00334.md): Skin · cracked · May 7, 2001 · N198FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > DURING ROUTINE INSP FUSELAGE SKIN Found CRACKED AT BS 250.5 BELOW LT NR 3 COCKPIT. *S/D* Removed and replaced DAMAGE PER IAW FEDEX EA 7-5330-57544.
- [SDR 01FDEA00330](https://openairdocs.org/sdr/01FDEA00330.md): Intercostal · cracked · May 7, 2001 · N198FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > DURING ROUTINE INSP INTERCOSTAL EXTENTION FROM BS 440-460, STR 2L FOUND CRACKED AT 3RD FASTENER FROM AFT END UPPER ROW 12 O''CLOCK. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-30-2.
- [SDR 01FDEA00332](https://openairdocs.org/sdr/01FDEA00332.md): Rib · cracked · May 7, 2001 · N198FE · Boeing 72722 · Leading Edge Devices
  > DURING ROUTINE INSP NR 2 SLAT RIB AT SLAT BS 342 FOUND CRACKED. *S/D* REMOVED AND REPLACED NR 2 L/E SLAT PER IAW BAC 727 MM 27-81-011.
- [SDR 01FDEA00333](https://openairdocs.org/sdr/01FDEA00333.md): Rib · cracked · May 7, 2001 · N198FE · Boeing 72722 · Leading Edge Devices
  > DURING ROUTINE INSP NR2 SLAT RIB AT SLAT BS 347 FOUND CRACKED. *S/D* REMOVED AND REPLACED PER IAW BAC 727 MM 27-81-011.
- [SDR 01FDEA00336](https://openairdocs.org/sdr/01FDEA00336.md): Seat Track · cracked · May 7, 2001 · N198FE · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE INSP NR 2 MAIN CABIN SEAT TRACK FOUND CRACKED AT BS 870.
- [SDR 99FDEA00079](https://openairdocs.org/sdr/99FDEA00079.md): Torsion Links · worn · Feb 26, 1999 · N198FE · Boeing 72722 · Landing Gear Steering System
  > A/C SHAKES AND DRIFT RIGHT OF CENTER LINE. NOSE WHEEL STEER INOP. REMOVED AND REPLACED UPPER AND LOWER TORSION LINKS PER MM 32-21-021-4. NOSE GEAR STEERING OPER CK GOOD PER MM 32-51-000-5.
- [SDR 98FDEA00160](https://openairdocs.org/sdr/98FDEA00160.md): Switch · dirty · Mar 6, 1998 · N198FE · Boeing 72722 · Landing Gear Position and Warning
  > 98-0059 ON TAKEOFF, RIGHT MAIN GEAR DOOR LIGHT CAME ON AND WOULD NOT GO OFF. CYCLED GEAR, LIGHT WENT OUT. INSPECTED AND CLEANED RIGHT MAIN GEAR DOOR SWITCH. CYCLED DOOR SEVERAL TIMES. OPERATIONAL CHECK NORMAL.
- [SDR 96FDEA01170](https://openairdocs.org/sdr/96FDEA01170.md): Lug · corrosion · Jun 25, 1996 · N198FE · Boeing 72722 · Leading Edge Devices
  > MR 0681 AND NR 039. NR 2 K-FLAP HAS CORROSION AROUND OUTBOARD LUG UPPER BOLT HOLE. ****S/D*** REMOVED CORROSION FROM NR 2 K-FLAP, OUTBOARD LUG UPPER HOLE AND REPAIRED PER FEDEX DRAWING SR 27-57-010, REV B.
- [SDR 96FDEA01169](https://openairdocs.org/sdr/96FDEA01169.md): Angle · cracked · Jun 25, 1996 · N198FE · Boeing 72722 · Cargo/Baggage Doors
  > NR 0405 AND NR 038, AFT CARGO DOOR HAS CRACK INDICATION IN RADIUS OF NR 4 (FROM TOP) OUTBOARD L-ANGLE, 20 INCHES AFT OF FWD EDGE. *****S/D**** COMING.
- [SDR 96FDEA01164](https://openairdocs.org/sdr/96FDEA01164.md): Bonding Jumper · corroded · Jun 21, 1996 · N198FE · Boeing 72722 · Leading Edge Devices
  > NRO0684 AND 037, NR 2 K-FLAP HAS CORROSION AROUND I/B BONDING JUMPER UPPER AND LOWER ATTACH POINTS. *S/D* BLENDED CORROSION AND REPAIRED RIB IAW FEDEX SRM 57-50-3 AND FEDEX DRAWING SR 27-57-010 REV B.
- [SDR 96FDEA01149](https://openairdocs.org/sdr/96FDEA01149.md): Floor Beam · corroded · Jun 19, 1996 · N198FE · Boeing 72722 · Fuselage Main, Floor Beam
  > NR0354 AND 036, CORROSION (C53-224-01) ON FLOOR BEAM TOP CHORD BS 680 RBL 2 TO 25 WL 208. *S/D* REPAIRED TOP CHORD OF FLOOR BEAM AT BS 680 RBL 2 TO 25 WL 208.1 PER FEDEX SRM 53-10-8 FIG 3.
- [SDR 96FDEA01148](https://openairdocs.org/sdr/96FDEA01148.md): Stringer · cracked · Jun 19, 1996 · N198FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > NR0587 AND 035, WHILE WORKING NRO213 FOUND CRACK AND GOUGE IN STR 4R BS 600 IN U-CHANNEL. *S/D* REMOVED DAMAGE AT BS 600 STR 4R, REPAIRED PER FEDEX SRM 53-10-1 FIG 1.
- [SDR 96FDEA01138](https://openairdocs.org/sdr/96FDEA01138.md): Shear Tie · cracked · Jun 15, 1996 · N198FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 0321 AND NR 034. BS 1070, LBL 51, STR 22L SHEAR TIE IS CRACKED AT FASTENER. ****S/D**** REPAIRED SHEAR TIE AT BS 1070, LBL 51, STR 22L PER FEDEX SRM 53-10-4, FIG 11.
- [SDR 96FDEA01130](https://openairdocs.org/sdr/96FDEA01130.md): Floor Beam · corroded · Jun 14, 1996 · N198FE · Boeing 727225 · Fuselage Main, Floor Beam
  > NR0476 AND 033, CORROSION (53-111-01, -2) ON FLOOR BEAM STA 560 LBL 18 WL 198, FWD CARGO BAY.
- [SDR 96FDEA01129](https://openairdocs.org/sdr/96FDEA01129.md): Frame · corroded · Jun 14, 1996 · N198FE · Boeing 727225 · Fuselage Main, Frame
  > NR0312 AND 032, CORROSION (53-111-01) STA 970, LBL 24 ON TOP FLANGE OF FRAME UNDER STRAP. *S/D* REPAIRED FRAME AT BS 970 WL 147 RBL 24 PER FEDEX SRM 51-40-3.
- [SDR 96FDEA01128](https://openairdocs.org/sdr/96FDEA01128.md): Shear Tie · cracked · Jun 14, 1996 · N198FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > NR0645 AND 031, WHILE WORKING NRO348 AFTER REMOVAL OF RT LWR NOSE CHORD FOUND SHEAR TIE AT BS 303 WL 148 RBL 15 TO 19 TO BE CRACKED AND CORRODED AND OUT OF LIMITS PER SRM.
- [SDR 96FDEA01121](https://openairdocs.org/sdr/96FDEA01121.md): Beam · corrosion · Jun 13, 1996 · N198FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 0650 AND 028. CORROSION C53-221-01 ON 25G BEAM STA 268, LBL 2, WL 208. ****S/D**** REMOVED AND REPLACED 25 G-BEAM, STA 268, LB 2, WL 208 PER FEDEX SRM 51-10-1.
- [SDR 96FDEA01120](https://openairdocs.org/sdr/96FDEA01120.md): Web · corrosion · Jun 13, 1996 · N198FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR0610 AND 027, CORROSION (C53-224-01) UNDER WEB BETWEEN STA 234 TO 259 WL 227 LBL 48.
- [SDR 96FDEA01118](https://openairdocs.org/sdr/96FDEA01118.md): T-Fitting · corroded · Jun 13, 1996 · N198FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 0417 AND NR 025. T-FITTING AT BS 360, STR 20L IS CORRODED BEYOND LIMITS. ****S/D**** REMOVED AND REPLACED T-FITTING. REF: FEDEX SRM 51-30-2.
- [SDR 96FDEA01113](https://openairdocs.org/sdr/96FDEA01113.md): Chord · cracked · Jun 13, 1996 · N198FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR0545 AND 020, CRACK IN I/B FLANGE OF STR 18A REINFORCEMENT CHORD BS 914.5 RBL 63.7 WL 189. *S/D* REPAIRED CRACK IN I/B FLANGE OF STR 18A REINFORCEMENT CHANNEL BS 914.5 RBL 63.7 WL 189 FEDEX EA 7-5310-29176, FUNCTIONALLY TEST GOOD PER FEDEX MM 32-30-0.
- [SDR 96FDEA01105](https://openairdocs.org/sdr/96FDEA01105.md): Shear Tie · cracked · Jun 11, 1996 · N198FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR0671 AND 019, FOUND CRACKED SHEAR TIE BS 321 RBL 15 TO 19 WL 148. *S/D* REPAIRED CRACKED FRAME AND SHEAR TIE AT BS 321 RBL 15 TO 19 WL 148 IAW SRM 53-10-4.
- [SDR 96FDEA01104](https://openairdocs.org/sdr/96FDEA01104.md): Te Wedge · delaminated · Jun 11, 1996 · N198FE · Boeing 72722 · Trailing Edge Flaps
  > NR 0668 AND NR 018. L/W I/B MID FLAP LWR O/B T/E WEDGE DELAMINATED. ****S/D**** REPAIRED L/W I/B MID FLAP IAW FEDEX SRM 51-40-6.
- [SDR 96FDEA01103](https://openairdocs.org/sdr/96FDEA01103.md): Shear Tie · cracked · Jun 11, 1996 · N198FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR0646 AND 017, WHILE WORKING NR0348 AFTER REMOVING R/LOWER NOSE CHORD, FOUND CRACKED AND CORRODED SHEAR TIE AT BS 328 WL 148 RBL 15 TO 18. *S/D* REMOVED DAMAGED SHEAR TIE AT BS 328 WL 148 RBL 15 TO 18 IAW FED EX SRM 53-10-4.
- [SDR 96FDEA01102](https://openairdocs.org/sdr/96FDEA01102.md): Frame · dented · Jun 11, 1996 · N198FE · Boeing 72722 · Fuselage Main, Frame
  > NR0494 AND 016, DENT IN FRAME AT BS 660 LBL 39 WL 162. *S/D* REPAIRED FRAME AT BS 660 LBL 39 WL 162 AS PER FED EX SRM 51-40-3.
- [SDR 96FDEA01101](https://openairdocs.org/sdr/96FDEA01101.md): Frame · dented · Jun 11, 1996 · N198FE · Boeing 72722 · Fuselage Main, Frame
  > NR0499 AND 015, DENT IN FRAME AT BS 620 RBL 39 WL 162. *S/D* REMOVED DENT IN FRAME AT BS 620 RBL 39 WL 162. FABRICATED REPAIR PARTS AND INSTALLED PER FED EX SRM 51-40-3.
- [SDR 96FDEA01100](https://openairdocs.org/sdr/96FDEA01100.md): Floor Beam · gouged · Jun 11, 1996 · N198FE · Boeing 72722 · Fuselage Main, Floor Beam
  > NR0481 AND 014, FOUND GOUGE IN FLOOR BEAM STA 560 RBL 6 WL 198, FWD BAY. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-8.
- [SDR 96FDEA01099](https://openairdocs.org/sdr/96FDEA01099.md): Floor Beam · corroded · Jun 11, 1996 · N198FE · Boeing 72722 · Fuselage Main, Floor Beam
  > NR0477 AND 011, CORROSION (C53-111-01, -2) ON FLOOR BEAM STA 600 RBL 2, 8, 13, 15, 18 WL 198, FWD BAY. *S/D* BLENDED AND INSTALLED REPAIR STRAP IAW FED SRM 53-10-1 AND 53-10-8.
- [SDR 96FDEA01098](https://openairdocs.org/sdr/96FDEA01098.md): Fitting · corroded · Jun 11, 1996 · N198FE · Boeing 72722 · Leading Edge Devices
  > NR 5 K-FLAP CENTER HINGE FITTING THAT ATTACHES TO FIXED L/E CORRODED. REMOVED AND REPLACED PER SRM.
- [SDR 96FDEA01097](https://openairdocs.org/sdr/96FDEA01097.md): Fitting · corroded · Jun 11, 1996 · N198FE · Boeing 72722 · Leading Edge Devices
  > NR 1 K-FLAP TO L/E MOUNT FITTING FOR THE CENTER HINGE IS CORRODED. REMOVED AND REPLACED PER SRM.
- [SDR 96FDEA01096](https://openairdocs.org/sdr/96FDEA01096.md): Fitting · corroded · Jun 11, 1996 · N198FE · Boeing 72722 · Leading Edge Devices
  > NR0376 AND 008, NR 2 K-FLAP TO L/E MOUNT FITTING FOR THE CENTER HINGE IS CORRODED (C57-562-01). *S/D* REMOVED AND REPLACED NR 2 K-FLAP TO LEADING EDGE MOUNT FITTING FOR THE CENTER HINGE IAW SRM 51-30-2.
- [SDR 96FDEA01095](https://openairdocs.org/sdr/96FDEA01095.md): Clip · gouged · Jun 11, 1996 · N198FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR0212 AND 007, DAMAGED RIVETS AND STR CLIP AT BS 720 STR 4R. *S/D* REMOVED AND REPLACED STRINGER CLIP AT BS 720, STR 4 RT PER SRM 53-10-8.
- [SDR 96FDEA01094](https://openairdocs.org/sdr/96FDEA01094.md): Clip · gouged · Jun 11, 1996 · N198FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR0211 AND 006, MISSING FASTENERS FROM STR CLIP AT BS 660 STR 3R AND DAMAGED STR CLIP. *S/D* REMOVED AND REPLACED STRINGER CLIP AT BS 660, STR 3 RT PER SRM 53-10-8.
- [SDR 96FDEA01093](https://openairdocs.org/sdr/96FDEA01093.md): Clip · gouged · Jun 11, 1996 · N198FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR0210 AND 005, DAMAGED STR CLIP AT BS 660 STRS 4R. *S/D* REMOVED DAMAGED CLIP AND INSTALLED NEW STRINGER CLIP AT BS 660 STR 4 RT PER SRM 53-10-8.
- [SDR 96FDEA01092](https://openairdocs.org/sdr/96FDEA01092.md): Floor Beam · corroded · Jun 11, 1996 · N198FE · Boeing 72722 · Fuselage Main, Floor Beam
  > NR0352 AND 004, CORROSION (C53-224-01) ON FLOOR BEAM TOP CHORD BS 600 RBL 10 TO 47 WL 208. *S/D* REMOVED CORROSION ON FLOOR BEAM TOP CHORD BS 600 RBL 10 TO 47 WL 208. FOUND AREA AT RBL 10 TO 17 TO BE OUT OF LIMITS. REPAIRED FLOOR BEAM IAW SRM 53-10-08.
- [SDR 96FDEA01081](https://openairdocs.org/sdr/96FDEA01081.md): Web · corrosion · Jun 11, 1996 · N198FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 0624 (013) CORROSION (C53-221-01) UNDER WEB BETWEEN STA 219.8 TO 227.8, WL 227, LBL 43.
- [SDR 96FDEA01080](https://openairdocs.org/sdr/96FDEA01080.md): Floor Beam · double hole · Jun 11, 1996 · N198FE · Boeing 72722 · Fuselage Main, Floor Beam
  > NR 0514, 012 DOUBLE HOLE IN FLOOR BEAM TOP CHORD BS 1110, LBL 32, WL 208. *S/D* TRIMMED OUT DOUBLE HOLE IN FLOOR BEAM TO CHORD BS 1110 LB 32 WL 208. FABRICATED REPAIR ANGLES AND FILLER, ALODINED AND PRIMED FLOOR BEAM AND REPAIR ANGLES, INSTALLED PARTS PER F
- [SDR 96FDEA01079](https://openairdocs.org/sdr/96FDEA01079.md): Floor Beam · corrosion · Jun 10, 1996 · N198FE · Boeing 72722 · Fuselage Main, Floor Beam
  > NR 0353, 003 CORROSION (C53-224-01) ON FLOOR BEAM TOP CHORD BS 620, LBL 10 TO 21 AND RBL 2 TO 56 WL 208. *S/D* REPAIRED BS 620 FLOOR BEAM UPPER CHORD LBL 21 TO RBL 56 IAW FEDEX SRM 53-10-8.
- [SDR 96FDEA01075](https://openairdocs.org/sdr/96FDEA01075.md): Support Beam · corrosion · Jun 5, 1996 · N198FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 0647, (002) WHILE WORKING NR0348 AFTER REMOVING RT LWR NOSE CHORD FOUND DRAG BRACE SUPPORT BEAM TO BE CORRODED OUT OF LIMITS PER SRM AT BS 328 TO 345 WL 148 RBL 15. *S/D* REMOVED AND REPLACED DRAG BRACE SUPPORT T-BEAM AT BS 328 TO 345 WL 148 RBL 15, INSTAL

Next page: https://openairdocs.org/deregistered/N198FE-2006-08-23/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 = 'N198FE' AND deregistration_id = 'N198FE-2006-08-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N198FE-2006-08-23/reports

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