# Service difficulty reports: N193FE, cancelled Aug 10, 2006

A list on [N193FE, cancelled Aug 10, 2006](https://openairdocs.org/deregistered/N193FE-2006-08-10.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 · 77 reports

- [SDR 04FDEA03023](https://openairdocs.org/sdr/04FDEA03023.md): Fire Warning · false activation · Nov 5, 2004 · N193FE · Boeing 727100 · Fuel Heater
  > ENGINE FIRE INDICATION NR 2 ENGINE. RAN RED TABS, SHUT DOWN ENGINE, DID NOT FIRE BOTTLES. INDICATION EXTINGUISHED AFTER 10 SEC, BEFORE POWER LEVER WAS MOVED TO IDLE, INDICATION OCCURED DURING CLIMB ABOUT 7,000 FT, 90 PERCENT N1, EPR 1.85. ALSO ENGINE WAS W
- [SDR 04FDEA00033](https://openairdocs.org/sdr/04FDEA00033.md): Rib · cracked · Jan 5, 2004 · N193FE · Boeing 727100 · Elevator, Spar/Rib
  > STABILIZER- ELEVATOR HINGE SUPPORT RIB INSPECTION S/B 727-55A0091, COMPLY WITH EO 7-5510-7-5001 REV B1 POS PT2.
- [SDR 03FDEA01633](https://openairdocs.org/sdr/03FDEA01633.md): Power Supply · failed · Sep 25, 2003 · N193FE · Boeing 727100 · Fire Detection
  > ON CLIMBOUT PASSING ABOUT 3,000 FT FIRE WARNING BELL SOUNDED WITH NO ASSOCIATED LIGHTS. ALL SYSTEM INDICATIONS WERE IN THE GREEN. ALL ENGINE INST INDICATED NORMAL. LOWER CARGO SMOKE, CARGO SMOKE AND ENG AND WHEEL WELL FIRE DETECTIONS SYSTEM ALL TESTED WITH
- [SDR 01FDEA01027](https://openairdocs.org/sdr/01FDEA01027.md): Downlock Switch · faulty · Dec 4, 2001 · N193FE · Boeing 72722 · Landing Gear Position and Warning
  > 1-387 AFTER T/O UNSAFE GEAR LIGHT ILLUMINATED. R&R R/H LAND GEAR DOWNLOCK SWITCH & ACCESSORY UNIT PER MM 32-61-021-4, 32-09-111-4.
- [SDR 01FDEA00075](https://openairdocs.org/sdr/01FDEA00075.md): Light · inoperative · Feb 3, 2001 · N193FE · Boeing 72722 · Emergency Lighting
  > DURING MAINT TEST FLT FWD ENTRY DOOR EMERGENCY EXIT LIGHT FAILED TO EXTINGUISH IN EITHER DISARM OR OFF POS. REMOVED AND REPLACED LIGHT ASSY PER IAW FEDEX MM 33-50-00. OPS CK GOOD.
- [SDR 98FDEA00459](https://openairdocs.org/sdr/98FDEA00459.md): Splice · cracked · Jul 17, 1998 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CRACKED STRINGER SPLICE AT BS 440, STR 20 RT. *S/D* REPLACED STRINGER SPLICE, BS 440, STR 20 RT IAW FED-EX SRM 53-10-3.
- [SDR 98FDEA00435](https://openairdocs.org/sdr/98FDEA00435.md): Frame · cracked · Jul 6, 1998 · N193FE · Boeing 72722 · Fuselage Main, Frame
  > NR 866 001 - STA-PAE, CRACK IN RADIUS OF BS 480 FRAME B4 STR 27 RT. REPAIRED CRACK IN RADIUS OF BS 480 BY STR 27 RT PER FED-EX EA NR 7-5310-39851.
- [SDR 98FDEA00454](https://openairdocs.org/sdr/98FDEA00454.md): Chord · corroded · Jul 2, 1998 · N193FE · Boeing 72722 · Wing Miscellaneous Structure
  > STA-PAE - LOWER CHORD AT BS 740 IS CORRODED AT RBL 13 TO RBL 20. COMPLIED WITH EA 7-5710-39850 ACCESS BLENDED AND TREATED CORROSION ON LOWER CHORD 740, RBL 13 - RBL 20. RESTORED AREA IAW ER 98-2645.
- [SDR 98FDEA00205](https://openairdocs.org/sdr/98FDEA00205.md): Tire · missing · Mar 18, 1998 · N193FE · Boeing 72722 · Tire
  > RIGHT OUTBOARD ANTI-SKID LIGHT BEGAN TO FLICKER DURING TAKEOFF ROLL, CAME ON SOLID AFTER ROTATION. ROC REPORTED, LOST THE RIGHT MAIN TIRE (OUTBOARD). FOUND NR 4 TIRE MISSING. REMOVED BRAKE TO INSPECT AXLE SLEEVE. REMOVED AND REPLACED AXLE SLEEVE AND INSPEC
- [SDR 96FDEA00283](https://openairdocs.org/sdr/96FDEA00283.md): Frame · double drilled · Feb 19, 1996 · N193FE · Boeing 72722 · Fuselage Main, Frame
  > BS 1090 FRAME HAS A DOUBLE HOLE BETWEEN STR 8 TO 9L. REPAIRED FRAME IAW FEDEX SRM 53-10-4.
- [SDR 96FDEA00275](https://openairdocs.org/sdr/96FDEA00275.md): Skin · cracked · Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND CRACK IN UPPER SKIN BS 1090 WL 140 RBL 25. REPAIRED DAMAGE SKIN BS 1090 WL 140 RBL 25 PER FEDEX EA 7-5330-27406.
- [SDR 96FDEA00274](https://openairdocs.org/sdr/96FDEA00274.md): Shear Tie · corrosion · Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1050 WL 146 RBL 1 TO 6, FOUND TO BE OUT OF LIMITS WHILE WORKING NR0053. REMOVED DAMAGED AREA AND INSTALLED REPAIR IAW FEDEX SRM 53-10-4.
- [SDR 96FDEA00273](https://openairdocs.org/sdr/96FDEA00273.md): Fail-Safe Chord · cracked · Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > BS 1010 CRACKED FAIL-SAFE CHORD AT RBL 45 WL 149, FOUND WHILE WORKING NR0053. REMOVED CRACKED FAIL-SAFE CHORD, INSTALLED NEW CHORD AND SPLICE IAW FEDEX SRM 51-40-3.
- [SDR 96FDEA00272](https://openairdocs.org/sdr/96FDEA00272.md): Shear Tie · corrosion · Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM OF SHEAR TIE BS 990 LBL 9 TO 13 WL 146, FOUND WHILE WORKING NR0053. REPAIRED SHEAR TIE WITH DOUBLER IAW FEDEX SRM 53-10-4.
- [SDR 96FDEA00270](https://openairdocs.org/sdr/96FDEA00270.md): Shear Tie · corrosion · Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1030 LBL 17 TO 22, FOUND WHILE WORKING NR0053 WL 146. REMOVED SHEAR TIE, REMOVED CORROSION, TREATED AND REINSTALLED IAW FEDEX SRM 53-10-1, 53-10-4.
- [SDR 96FDEA00269](https://openairdocs.org/sdr/96FDEA00269.md): Frame · corrosion · Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Main, Frame
  > CORROSION FOUND ON DOOR FRAME BS 1057.5 WL 162 RBL 25, WHILE WORKING NR0053. REMOVED AND REPLACED FRAME IAW DRAWING 65-20728.
- [SDR 96FDEA00268](https://openairdocs.org/sdr/96FDEA00268.md): Skin · corrosion · Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN BULGE AND RIVET HEAD DISHED AT BS 1108, 4.5 INCHES UP FROM BOTTOM OF SKIN LAP STR 26R, AT AFT CARGO DOOR CUTOUT LOWER AFT CORNER. REPAIRED DAMAGED SKIN AT BS 1108 STR 26 RT SKIN LAP PER FEDEX EA 7-5330-27406.
- [SDR 96FDEA00267](https://openairdocs.org/sdr/96FDEA00267.md): Hinge · corroded · Feb 16, 1996 · N193FE · Boeing 72722 · Leading Edge Devices
  > FIXED L/E FITTING PER NR 1 K-FLAP CENTER LUG IS CORRODED. REPAIRED CENTER HINGE FITTING WITH NEW.
- [SDR 96FDEA00258](https://openairdocs.org/sdr/96FDEA00258.md): Frame Splice · damaged · Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > FRAME SPLICE DAMAGE AT BS 1010 RT WL 157 RBL 41 BETWEEN STR 24 TO 25R. REMOVED DAMAGED FRAME SPLICE AT BS 1010 RT WL 157 RBL 14. FABRICATED NEW FRAME SPLICE AND INSTALLED.
- [SDR 96FDEA00257](https://openairdocs.org/sdr/96FDEA00257.md): Frame · cracked · Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Main, Frame
  > CRACK AND MULTIPLE STOP DRILLS ON UNDERSIDE OF FRAME AT BS 930 BETWEEN STR 15 TO 14R. REPAIRED CRACK AND MULTIPLE STOP DRILLS ON UNDERSIDE OF FRAME AT BS 930, BETWEEN STR 15 TO 14R IAW FEDEX EA 7-5310-27450.
- [SDR 96FDEA00256](https://openairdocs.org/sdr/96FDEA00256.md): Keel Beam · corrosion · Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Main, Keel
  > EXTERIOR SKIN, BULGE IN SKIN AT KEEL BEAM STR 29L BS 1050 TO 1030. REMOVED CORROSION ON KEEL BEAM BS 1030 TO 1050 STR 29L, FOUND TO BE OUT LIMITS PER FEDEX SRM 53-10-1. REMOVED FRAMES BS 970, 990, 1010, 1050, 1070 AND 1030. REMOVED KEEL BEAM, INSTALLED NEW
- [SDR 96FDEA00240](https://openairdocs.org/sdr/96FDEA00240.md): Floorbeam · corroded · Feb 14, 1996 · N193FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01) ON UPPER CHORD OF BS 950 FLOORBEAM AT RBL 21 WL 208. CLEANED AND TREATED CORROSION ON UPPER CHORD OF BS 950 FLOORBEAM AT RBL 21 WL 208, FOUND TO BE WITHIN LIMITS PER FEDEX EA 7-5310-27447.
- [SDR 96FDEA00239](https://openairdocs.org/sdr/96FDEA00239.md): Shear Tie · corrosion · Feb 14, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM OF SHEAR TIE BS 970 RBL 8 TO 13 WL 146, FOUND WHILE WORKING NR0053. REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE IAW FEDEX SRM 53-10-4, CLEANED UP AREA AND INSTALLED SHEAR TIE.
- [SDR 96FDEA00236](https://openairdocs.org/sdr/96FDEA00236.md): Shear Tie · damaged · Feb 12, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > OBLONGED HOLE ON SHEAR TIE AT BS 1030 RBL 42 WL 165, FOUND WHILE WORKING NR 0053. CUT OFF DAMAGED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE AT BS 1030 RBL 42 WL 165 PER FEDEX SRM 53-10-4.
- [SDR 96FDEA00235](https://openairdocs.org/sdr/96FDEA00235.md): Shear Tie · corrosion · Feb 12, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION (C53-111-01,-3) AFT CARGO BAY, ON SHEAR TIE AT BS 1030 RBL 4 WL 138.5. REPAIRED SHEAR TIE AT BS 1030 RBL 4 WL 138.5 AS PER FEDEX SRM 53-10-4.
- [SDR 96FDEA00234](https://openairdocs.org/sdr/96FDEA00234.md): Floorbeam · corroded · Feb 12, 1996 · N193FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-06) ON FLOORBEAM AT BS 620 RBL 10 TO 43 WL 208. REMOVED DAMAGED SECTION OF FLOORBEAM, FABRICATED REPAIR PARTS, CLEANED, TREATED AND INSTALLED PARTS. ALL WORK ACCOMPLISHED IAW FEDEX SRM 53-10-8 AT BS 620 RBL 10 TO 43 WL 208.
- [SDR 96FDEA00271](https://openairdocs.org/sdr/96FDEA00271.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1030 RBL 17 TO 22 WL 146, FOUND WHILE WORKING NR0053. REMOVED SHEAR TIE, REMOVED CORROSION, TREATED AND REINSTALLED SHEAR TIE FEDEX SRM 53-10-1.
- [SDR 96FDEA00224](https://openairdocs.org/sdr/96FDEA00224.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM OF SHEAR TIE BS 1030 LBL 3 TO 4 WL 146, FOUND TO BE OUT OF LIMITS WHILE WORKING NR 0053. ACCOMPLISHED SHEAR TIE REPAIR AT BS 1030 LBL 3 TO 4 WL 146 IAW FEDEX SRM 53-10-4 FIG 15.
- [SDR 96FDEA00223](https://openairdocs.org/sdr/96FDEA00223.md): Frame · cracked · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Main, Frame
  > BS 1070 FRAME CRACK EMITTING FROM STOP DRILL HOLE AT BL 0 TO BL 10 WL 150, FOUND WHILE WORKING CUSTOMER CARD NR 0053. REMOVED DAMAGE FROM FRAME BS 1070 AT BL 0 AND LBL 10 WL 150, FABRICATED FILLERS AND INSTALLED IAW SRM 51-40-3 AND PREVIOUS REPAIR DOUBLER REI
- [SDR 96FDEA00221](https://openairdocs.org/sdr/96FDEA00221.md): Hinge · corroded · Feb 9, 1996 · N193FE · Boeing 72722 · Ailerons
  > CORROSION ON RT WING O/B AILERON NR 3 HINGE. REMOVED CORRODED NR 3 HINGE, INSTALLED A NEW HINGE AND REINSTALLED RT WING O/B AILERON IAW FEDEX MM 27-10-31, FUNCTIONAL TESTED IAW FEDEX MM 27-10-00.
- [SDR 96FDEA00220](https://openairdocs.org/sdr/96FDEA00220.md): Floorbeam · corroded · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM (C53-224-01(1), BS 344 WL 208 RBL 15 TO 50 AROUND NUT CLIP HOLES UPPER AND LOWER SURFACE. REMOVED UPPER CHORD OF FLOORBEAM BS 344 FABRICATED AND INSTALLED NEW UPPER CHORD OF FLOORBEAM PER FEDEX SR 27-53-007.
- [SDR 96FDEA00219](https://openairdocs.org/sdr/96FDEA00219.md): Stringer · damaged · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL BETWEEN BS 1130 AND 1149 HAS FASTENER PULLED THROUGH STR 6R. CUT OUT STR DAMAGE AREA FABRICATED STR SPLICES REPAIR AND INSTALLED REPAIR PARTS WITH FASTENERS PER FEDEX SRM 53-10-3 FIG 3 AT BS 1130 AND 1149 STR 6R.
- [SDR 96FDEA00218](https://openairdocs.org/sdr/96FDEA00218.md): Keel Beam · corrosioin · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Main, Keel
  > EXTERIOR SKIN BULGE IN SKIN AT KEEL BEAM STR 29L BS 1050 TO 1030.
- [SDR 96FDEA00217](https://openairdocs.org/sdr/96FDEA00217.md): Floorbeam · corroded · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-06), ON FLOORBEAM OF BS 600 RBL 10 TO 30 WL 208. REMOVED CORRODED SECTION OF FLOORBEAM FABRICATED REPAIR ANGLES AND INSTALLED ALL WORK DONE PER FEDEX SRM 53-10-8.
- [SDR 96FDEA00212](https://openairdocs.org/sdr/96FDEA00212.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1050 WL 146 RBL 1 TO 6, FOUND TO BE OUT OF LIMITS WHILE WORKING NR 0053.
- [SDR 96FDEA00211](https://openairdocs.org/sdr/96FDEA00211.md): Fail-Safe Chord · cracked · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > BS 1010 CRACKED FAIL-SAFE CHORD AT RBL 45 WL 149, FOUND WHILE WORKING NR 0053.
- [SDR 96FDEA00210](https://openairdocs.org/sdr/96FDEA00210.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM OF SHEAR TIE BS 990 LBL 9 TO 13 WL 146, FOUND WHILE WORKING NR 0053.
- [SDR 96FDEA00209](https://openairdocs.org/sdr/96FDEA00209.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 990 LBL 2 TO 4 WL 146, FOUND WHILE WORKING NR 0053. ACCOMPLISHED SHEAR TIE REPAIR AT BS 990 LBL 2 TO 4 WL 146 PER FEDEX SRM 53-10-4.
- [SDR 96FDEA00208](https://openairdocs.org/sdr/96FDEA00208.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM OF SHEAR TIE BS 970 RBL 8 TO 13 WL 146, FOUND WHILE WORKING NR 0053.
- [SDR 96FDEA00207](https://openairdocs.org/sdr/96FDEA00207.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM OF SHEAR TIE BS 970 LBL 8 TO 13 WL 146, FOUND WHILE WORKING NR 0053. ACCOMPLISHED SHEAR TIE REPAIR BS 970 LBL 8 TO 13 WL 146 IAW FEDEX SRM 53-10-4 FIG 15. REMAINING FASTENERS ON FLOOR SUPPORT BRACKET WILL BE INSTALLED ON NR 0053.
- [SDR 96FDEA00206](https://openairdocs.org/sdr/96FDEA00206.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 970 LBL 2 TO 6 WL 146, FOUND WHILE WORKING NR 0053. ACCOMPLISHED SHEAR TIE REPAIR AT BS 970 LBL 2 TO 6 WL 146 IAW FEDEX SRM 53-10-4 FIG 15. REMAINING FASTENERS ON FLOOR SUPPORT BRACKET WILL BE INSTALLED ON NR 0053.
- [SDR 96FDEA00205](https://openairdocs.org/sdr/96FDEA00205.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1030 RBL 17 TO 22 WL 146, FOUND WHILE WORKING NR0053. REMOVED SHEAR TIE AND CORROSION, TREATED AND REINSTALLED IAW FEDEX SRM 53-10-1 AND 53-10-4.
- [SDR 96FDEA00203](https://openairdocs.org/sdr/96FDEA00203.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1030 RBL 8 TO 13 WL 146, FOUND WHILE WORKING NR 0053. ACCOMPLISHED REPAIR ON SHEAR TIE BS 1030 RBL 8 TO 13 WL 146 IAW FEDEX SRM 53-10-4.
- [SDR 96FDEA00202](https://openairdocs.org/sdr/96FDEA00202.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON BOTTOM SIDE OF SHEAR TIE BS 1050 LBL 32 TO 38, FOUND TO BE OUT OF LIMITS WHILE WORKING NR 0053. CUT OUT DAMAGE AND REPAIRED PER FEDEX SRM 53-10-4.
- [SDR 96FDEA00201](https://openairdocs.org/sdr/96FDEA00201.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON BOTTOM SIDE OF SHEAR TIE BS 1050 WL 146 LBL 1 TO 6, FOUND TO BE OUT OF LIMITS WHILE WORKING NR 0053. REPAIRED CORRODED SHEAR TIE PER FEDEX SRM 51-10-4.
- [SDR 96FDEA00199](https://openairdocs.org/sdr/96FDEA00199.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1050 WL 146 RBL 16 TO 22, FOUND WHILE WORKING NR OO53, OUT OF LIMITS. CUT OFF DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE FROM HEAT TREATED MATERIAL, BACK DRILLED, ALODINED, PRIMED, PAINTED AND INSTALLED FASTENERS PER
- [SDR 96FDEA00198](https://openairdocs.org/sdr/96FDEA00198.md): Shear Tie · corrosion · Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1050 WL 146 LBL 7 TO 13, FOUND TO BE OUT OF LIMITS WHILE WORKING NR O0053. ACCOMPLISHED SHEAR TIE REPAIR AT BS 1050 WL 146 LBL 7 TO 13 PER FEDEX SRM 53-10-4.
- [SDR 96FDEA00222](https://openairdocs.org/sdr/96FDEA00222.md): Door Frame · corrosion · Feb 6, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON DOOR FRAME BS 1057.5 WL 162 RBL 25, WHILE WORKING NR 0053.
- [SDR 96FDEA00191](https://openairdocs.org/sdr/96FDEA00191.md): Skin · corrosion · Feb 5, 1996 · N193FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > LFEC INSP INDICATED A GREATER THAN 20 PERCENT MATERIAL LOSS AT BS 360, 2 INCHES BELOW STR 17L WL 203 TO 206. AREA MARKED IN RED AND IS VISIBLE ON THE SURFACE OF THE SKIN. REPAIRED AREA FROM BS 358 TO 360, BS 360 TO 362 AT STR 17L TO 18L IAW FEDEX EO 7-5330-7
- [SDR 96FDEA00189](https://openairdocs.org/sdr/96FDEA00189.md): Stringer · cracked · Feb 5, 1996 · N193FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > CRACK THROUGH FASTENER HOLE AT FAIL-SAFE STR INTERSECTION BS 890 STR 14R. REPAIRED CRACK THROUGH FASTENER HOLE AT FAIL-SAFE STR INTERSECTION BS 890 STR 14R AS PER FEDEX SRM 51-40-3.

Next page: https://openairdocs.org/deregistered/N193FE-2006-08-10/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 = 'N193FE' AND deregistration_id = 'N193FE-2006-08-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N193FE-2006-08-10/reports

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