# Service difficulty reports: N190FE, cancelled Mar 1, 2007

A list on [N190FE, cancelled Mar 1, 2007](https://openairdocs.org/deregistered/N190FE-2007-03-01.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 · 55 reports

- [SDR 05FDEA02689](https://openairdocs.org/sdr/05FDEA02689.md): Fitting · misdrilled · Aug 26, 2005 · N190FE · Boeing 72722 · Wing, Landing Gear Attach Fittings
  > LEFT AND RIGHT LOWER FORWARD TRUNNION TEE ATTACHED FITTINGS PART NUMBER 65-19257-6 /5/7/8, REQUIRES REWORK, REFERENCE:EO/7-5710-7-2314D PT-4. REWORKED LEFT AND RIGHT LOWER FORWARD TRUNNION ATTACH TEE FITTINGS PART NUMBERS 65-19257-5/6/7/8 IAW FEDEX EA 7-5710-
- [SDR 04FDEA01900](https://openairdocs.org/sdr/04FDEA01900.md): Intercostal · cracked · Jul 1, 2004 · N190FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT INTERCOSTAL IS CRACKED AT STRINGER 22R BS 572 THRU BS 580. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-1.
- [SDR 04FDEA01899](https://openairdocs.org/sdr/04FDEA01899.md): Skin · bulged · Jul 1, 2004 · N190FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > SKIN BULGE AT BS 1180 STRINGER 26L THRU STRINGER 23L. REPAIRED AREA IAW EA 7-5330-79539.
- [SDR 04FDEA01233](https://openairdocs.org/sdr/04FDEA01233.md): Warning Light · illuminated · May 12, 2004 · N190FE · Boeing 727100 · Landing Gear Position and Warning
  > NOSE GEAR DOWN LIGHT (GREEN) DID NOT ILLUMINATE WHEN GEAR LOWERED, CAME ON AFTER NOSE GEAR PIN INSTALLED. ADDITIONAL INFO FROM DEBRIEFING CREW. EXTREME PRECIPITATION LEAVING MSY UPON ARRIVAL INTO SHV, NOSE GEAR SHOWED UNSAFE. CYCLED HANDLE GREEN LIGHT ILLU
- [SDR 04FDEA00002](https://openairdocs.org/sdr/04FDEA00002.md): Connector · contaminated · Jan 1, 2004 · N190FE · Boeing 727100 · Landing Gear Position and Warning
  > UNSAFE NOSE GEAR INDICATION - NO GREEN LIGHT. RAN PROCEDURE PER QRH. RECYCLED GEAR. VIEWED NOSE GEAR PORT WITH A GEAR DOWN & LOCKED INDICATION NORMAL. NOSE GEAR GREEN LIGHT ILLUMINATED UPON FINAL APPROACH. AFTER JACKING A/C REMOVED CANNON PLUG FROM DOWNLO
- [SDR 99FDEA00465](https://openairdocs.org/sdr/99FDEA00465.md): Bellframe · damaged · Sep 27, 1999 · N190FE · Boeing 72722 · Fuselage Main, Frame
  > NR 685 - DENTS IN UPPER FLANGE RADIUS OF BELLFRAME AT BS 1050 ABOVE STR 26L IN AFT CARGO. CUT OUT DAMAGED AND INSTALL FILLER AND DOUBLER PER SRM 53-10-4 AND EA 7-5310-45407.
- [SDR 99FDEA00464](https://openairdocs.org/sdr/99FDEA00464.md): Stringer · corroded · Sep 22, 1999 · N190FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > STR 30 IS CORRODED BETWEEN BS 1148 AND 1166 IN AFT CARGO. REMOVED AND REPLACED STR 30 PER SRM 53-10-3.
- [SDR 99FDEA00478](https://openairdocs.org/sdr/99FDEA00478.md): Splice · corroded · Sep 21, 1999 · N190FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 118 - UPPER LOBE BS 344 LBL 45- LBL 60 CORROSION AROUND FLOORBOARD ATTACH HOLES UPPER LEG OF FLOORBEAM. INSTALLED UPPER CHORD SPLICE PER DRAWING SR 27-53-007 PG 14.
- [SDR 99FDEA00477](https://openairdocs.org/sdr/99FDEA00477.md): Cover · corroded · Sep 21, 1999 · N190FE · Boeing 72722 · Wing Miscellaneous Structure
  > NR 782 - RT WING RT STUB TANK PLATE LAND NEEDS RESIDUE REMOVED FWD SPAR ACCESS. CORROSION REMOVED AND REPLACED AREA PER EA NR 75710-45413 DATED 9-29-99 SEEN NR 782 AND JPF AREA ON REVERSE SIDE.
- [SDR 99FDEA00466](https://openairdocs.org/sdr/99FDEA00466.md): Casting · scored · Sep 21, 1999 · N190FE · Boeing 72722 · Fuselage, Wing Attach Fittings
  > NR 999 - LT WING BS 870 FWD AND AFT BOTTLE PIN CASTINGS ARE SCORED, AFT CASTING HAS 2 PREVIOUSLY BLENDED (DISHED OUT) AREAS (MARKED). REMOVED SCORING AND BLENDING. INSTALL TERMINAL PIN BUSHINGS IAW S/B 727-57-0175 NSC01, EA 7521045399 AND SRM 5240-1.
- [SDR 99FDEA00476](https://openairdocs.org/sdr/99FDEA00476.md): Keel Beam · cracked · Sep 20, 1999 · N190FE · Boeing 72722 · Fuselage Main, Keel
  > NR 794 - KEEL BEAM LWR LT CHORD CRACKED IN RADIUS AT BS 954. STOP DRILLED CRACK AND INSTALL DOUBLER PER EA NR7-531045391 DATED 15 SEP 99.
- [SDR 99FDEA00462](https://openairdocs.org/sdr/99FDEA00462.md): Bottle Pin · corroded · Sep 10, 1999 · N190FE · Boeing 72722 · Wing, Fuselage Attach Fittings
  > RT FWD BOTTLE BOLT (SPAR TERMINAL PIN) HAS CORROSION. REMOVED AND REPLACED NEW BOTTLE BOLT PIN SEALED.
- [SDR 99FDEA00067](https://openairdocs.org/sdr/99FDEA00067.md): Bulb · failed · Feb 18, 1999 · N190FE · Boeing 72722 · Landing Gear Position and Warning
  > LT MAIN LANDING GEAR LIGHT DID NOT COME ON WHEN GEAR LOWERED. COMPLIED WITH RED TABS. REPLACED BOTH BULBS IN LT MAIN GEAR IND PER CHAPTER 20 STANDARD PRACTICES. LIGHTS GROUND CK GOOD.
- [SDR 98FDEA00769](https://openairdocs.org/sdr/98FDEA00769.md): Valve · failed · Dec 29, 1998 · N190FE · Boeing 72722 · Landing Gear Retraction/Extension System
  > LOST ALL SYS A UPON GEAR RETRACT, SHUT OFF VALVES FOR 33 MIN. REMOVED AND REPLACED LEFT MAIN GEAR LOCK PER MM 32-32-031-4, A SYS RETURN FILTER PER MM 29-11, NR 1 AND NR 2 HYD PUMP CASE DRAIN FILTER ASSY PER MM 29-11. RAN NR 1 AND 2 ENG PER JET RUN HANDBOOK.
- [SDR 98FDEA00497](https://openairdocs.org/sdr/98FDEA00497.md): Computer · malfunctioned · Aug 11, 1998 · N190FE · Boeing 72722 · Stall Warning System
  > STICK SHAKER AFTER TAKEOFF DURING FIRST FLAP RETRACTION 165 KIAS. OCCURRED INTERMITTENTLY AT ALL ALTITUDES AND AIRSPEEDS UNTIL LANDING, PITCH APPROX 8 DEG UP. *S/D* REMOVED AND REPLACED STALL WARN COMP AND ANGLE ATTACK SENSOR RIGHT, TEST OK.
- [SDR 98FDEA00226](https://openairdocs.org/sdr/98FDEA00226.md): Switch · failed · Apr 1, 1998 · N190FE · Boeing 72722 · Door Warning System
  > MAIN CARGO DOOR LIGHT CAME ON SHORTLY AFTER TAKEOFF. REPLACED LOCK ROD SWITCH AND ADJUSTED PER MAINTENANCE MANUAL 52-70-09, OPERATIONAL CHECKS GOOD.
- [SDR 97FDEA00562](https://openairdocs.org/sdr/97FDEA00562.md): Frame · cracked · Aug 18, 1997 · N190FE · Boeing 72722 · Fuselage Main, Frame
  > CRACK INDICATIONS NOTED (DAMAGED HOLE) BS 970, STR 27L AND 27R, AFT CARGO BAY LOWER LOBE. *S/D* REMOVED AREA OF DAMAGE.5 BY.5 BY.071 AT BS 970, STR 27L AND 27R, LOWER LOBE AND INSTALLED REPAIR DOUBLERS IAW FED-EX SRM 51-40-3.
- [SDR 97FDEA00536](https://openairdocs.org/sdr/97FDEA00536.md): Frame · cracked · Aug 14, 1997 · N190FE · Boeing 72722 · Fuselage Main, Frame
  > NR 0372 004 CRACK INDICATION NOTED AT TOOLING HOLE BS 1110, STR 26L AFT CARGO BAY LOWER LOBE. REMOVED.5 FT BY.3 FROM AREA AROUND TOOLING HOLE. REPAIRED IAW FED-EX SRM 51-40-3.
- [SDR 97FDEA00535](https://openairdocs.org/sdr/97FDEA00535.md): Frame · damaged · Aug 14, 1997 · N190FE · Boeing 72722 · Fuselage Main, Frame
  > NR 0370 006 WHILE WORKING EO 7-5310-7-2354E2 PT 2, FOUND DAMAGED HOLES ON FRAME BS 1090, LBL 17, WL 150. REMOVED DAMAGED AREA OF.425 BY.550 AND.500 BY.750 ON FRAME BS 1090, LBL 17, WL 150. FABRICATED AND INSTALLED REPAIR PARTS PER FED-EX SRM 51-40-3.
- [SDR 97FDEA00534](https://openairdocs.org/sdr/97FDEA00534.md): Fitting · corroded · Aug 14, 1997 · N190FE · Boeing 72722 · Ailerons
  > NR 0271 005 - R/W I/B AILERON, I/B TAB FITTING CORRODED (AREA MARKED).
- [SDR 97FDEA00521](https://openairdocs.org/sdr/97FDEA00521.md): Shear Tie · corroded · Aug 8, 1997 · N190FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION (C53-113-01, 2) BS 1168, AFT SHEAR TIE LBL 15 TO RBL 10 WL 164 BETWEEN STR 27R TO 27L. *S/D* REMOVED CORRODED SHEAR TIE AT BS 1168, LBL 15 TO RBL 10, WL 164. FABRICATED REPLACEMENT PART AND INSTALLED PER FED-EX SRM 51-10-1, 51-30-2.
- [SDR 97FDEA00520](https://openairdocs.org/sdr/97FDEA00520.md): Mid Flap · delaminated · Aug 8, 1997 · N190FE · Boeing 72722 · Trailing Edge Flaps
  > RIGHT WING I/B MID FLAP T/E WEDGE IS DELAMINATED AT 22 INCHES FROM I/B END. *S/D* REMOVED 9 BY 4 OF DAMAGED SKIN AND CORE, 22 INCHES FROM I/B END OF RIGHT WING I/B MIDFLAP TRAILING EDGE WEDGE. FABRICATED AND INSTALLED REPAIR PER FED-EX SRM 51-40-6.
- [SDR 97FDEA00504](https://openairdocs.org/sdr/97FDEA00504.md): Skin · delaminated · Aug 6, 1997 · N190FE · Boeing 72722 · Trailing Edge Flaps
  > NR 0011 001 R/W I/B FOREFLAP HAS DELAMINATION DENT APPROXIMATELY 48 I/B O/B END. REPAIRED R/W I/B FOREFLAP DELAMINATION DENT APX 48 I/B OF O/B END IAW FED-EX SRM 51-40-06.
- [SDR 97FDEA00335](https://openairdocs.org/sdr/97FDEA00335.md): Hyd Filter · dirty · Jun 10, 1997 · N190FE · Boeing 72722 · Hydraulic Filter, Main
  > ON TAKEOFF, FIRST OFFICER FELT THAT HYDRAULIC PRESSURE TO ELEVATOR WAS LOST DURING GEAR RETRACTION. SAME THING OCCURED ON LANDING IN BFM WHEN SPEED BRAKES WERE DEPLOYED. DURING TAXI IN WAS ABLE TO DUPLICATE BY PULLING BACK ON YOKE WHILE SIMULTANEOUSLY DEPLOY
- [SDR 96FDEA01307](https://openairdocs.org/sdr/96FDEA01307.md): Sequence Valve · leaking · Jul 31, 1996 · N190FE · Boeing 72722 · Landing Gear Retraction/Extension System
  > LOSS OF SYS A-HYD ON GEAR RETRACTION. A-PUMPS RAN FOR 7 MINUTES WITHOUT FLUID. REMOVED AND REPLACED NR 1 AND NR 2 ENG HYD PUMPS PER MM 29-11-33. REMOVED AND REPLACED NR 1 AND NR 2 ENG HYD PUMP CASE DRAIN FILTERS PER MM 29-11-41, S-SYS RETURN FILTER PER MM 2
- [SDR 95FDEA00230](https://openairdocs.org/sdr/95FDEA00230.md): Frame · double hole · Mar 12, 1995 · N190FE · Boeing 72722 · Fuselage Main, Frame
  > AT BS 970 STR 27R WL 157 THERE IS A DOUBLE HOLE IN THE FRAME. REPAIRED FRAME AT BS 970 STR 27R WL 157 PER FEDEX 51-40-3.
- [SDR 95FDEA00245](https://openairdocs.org/sdr/95FDEA00245.md): Fitting · cracked · Mar 10, 1995 · N190FE · Boeing 72722 · Rudder, Tab Structure
  > UPPER RUDDER TAB ACTUATING ROD SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED CRACKED UPPER RUDDER TAB ACTUATING ROD SUPPORT FITTING.
- [SDR 95FDEA00244](https://openairdocs.org/sdr/95FDEA00244.md): Frame · gouged · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Frame
  > GOUGE ON FRAME AT BS 680 STR 14L. REMOVED AND REPLACED DAMAGED AREA PER FEDEX SRM 51-40-3.
- [SDR 95FDEA00243](https://openairdocs.org/sdr/95FDEA00243.md): Stringer Tie · cracked · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > FRAME TO STRINGER TIE CRACKED AT BS 680 STR 11L. REMOVED, FABRICATED AND REPLACED STR TIE AT BS 680 STR 11L.
- [SDR 95FDEA00242](https://openairdocs.org/sdr/95FDEA00242.md): Stringer · corroded · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > CORROSION (72C237-02) ON STRINGER AT BS 1150-1160 STR 7L. FOUND CORROSION TO BE OUT OF LIMITS. REPAIRED STR AT BS 1150-1160 IAW SRM 53-10-3 AND 51-40-3.
- [SDR 95FDEA00241](https://openairdocs.org/sdr/95FDEA00241.md): Stringer · cracked · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > STR 25R IS CRACKED AT BS 420. REPAIRED STR 25R AT BS 420 IAW SRM 53-10-3 FIG 1 DETAIL II.
- [SDR 95FDEA00240](https://openairdocs.org/sdr/95FDEA00240.md): Floor Beam · corroded · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CORROSION (72C235-2) ON 344 FLOOR BEAM RBL 15 WL 208 UNDER NUTPLATE HOLE. CORROSION PERMIATED THROUGH BEAM AND HAT CHANNEL OUT OF LIMITS PER FEDEX SRM 53-10-1 REMOVED, FABRICATED AND INSTALLED TOP CHORD OF FLOORBEAM BS 344 BLO TO RBL 60 IN IAW FEDEX SR 27-53-
- [SDR 95FDEA00239](https://openairdocs.org/sdr/95FDEA00239.md): Seat Track · corroded · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION (72C235-02) ON SEAT TRACK BS 740 LBL 25. CORROSION FOUND TO BE OUT OT LIMITS, REMOVED AND REPLACED SEAT TRACK FROM BS 710-740 IAW SRM 53-10-5.
- [SDR 95FDEA00238](https://openairdocs.org/sdr/95FDEA00238.md): Seat Track · corrosion · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BS 480 RBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 480-510 RBL 25 WL 208.
- [SDR 95FDEA00237](https://openairdocs.org/sdr/95FDEA00237.md): Seat Track · corrosion · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BS 470-484 LBL 45 WL 208. REPLACED SEAT TRACK FROM BS 480-510 LBL 45 WL 208 AND CLEANED CORROSION ON TRACK FLANGE AT BS 470 PER FEDEX SRM 53-10-5.
- [SDR 95FDEA00236](https://openairdocs.org/sdr/95FDEA00236.md): Seat Track · corroded · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION (72C235-02) ON SEAT TRACK BS 344-350 RBL 25. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-10-1.
- [SDR 95FDEA00235](https://openairdocs.org/sdr/95FDEA00235.md): Seat Track · corrosion · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BS 870 RBL 25 WL 208 OUT OF LIMITS PER SRM 51-10-01 1 INCH BY 1 INCH BY.035 ORIGINAL THICKNESS.090. REMOVED AND REPLACED SEAT TRACK BS 870-960 RBL 25 WL 208, EXISTING FACTORY SPLICE BS 870-960 RBL 25 WL 208.
- [SDR 95FDEA00234](https://openairdocs.org/sdr/95FDEA00234.md): Bulkhead · dented · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Bulkhead
  > DENT IN PRESSURE BULKHEAD BS 950 RBL 23 WL 153. REPAIRED DENT IN BS 950 CENTER BULKHEAD AT RBL 23 WL 153 PER FEDEX SRM 53-10-9 FIG 4.
- [SDR 95FDEA00233](https://openairdocs.org/sdr/95FDEA00233.md): Clip · damaged · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CRACK AND OR HOLE DAMAGE IN LEFT BS 870 TERMINAL FITTING ROW 1 HOLE NR 1. DETERMINED BY HFEC THAT DAMAGE TO FRAME TO STRINGER CLIP TO BE MECHANICAL TOOLING DAMAGE. REMOVED AND REPLACED CLIP.
- [SDR 95FDEA00232](https://openairdocs.org/sdr/95FDEA00232.md): Seat Track · worn · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings
  > F/E'S AFT SEAT TRACK IS WORN. REMOVED AND REPLACED F/E'S AFT SEAT TRACK.
- [SDR 95FDEA00231](https://openairdocs.org/sdr/95FDEA00231.md): Frame · double hole · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Frame
  > AT BS 990 STR 27R WL 148 THERE IS A DOUBLE HOLE IN THE FRAME. REPAIRED FRAME AT BS 990 STR 27R WL 157 PER FEDEX SRM 51-40-3.
- [SDR 95FDEA00229](https://openairdocs.org/sdr/95FDEA00229.md): Stringer · gouged · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > BS 500 WL 190 STR 19R STR IS GOUGED ON LOWER SIDE CHANNEL. REMOVED GOUGED STR 19 BS 500 WL 190 AND INSTALLED NEW STR PER FEDEX SRM 53-10-3.
- [SDR 95FDEA00226](https://openairdocs.org/sdr/95FDEA00226.md): Skin · damaged · Mar 10, 1995 · N190FE · Boeing 72722 · Horizontal Stabilizer, Plate/Skin
  > 9503-11 LEFT HORIZONTAL STABILIZER INTERSPAR SKIN (LWR SURFACE) IS DAMAGED BETWEEN STAB STA 151.81 AND STAB 169.81. REPAIRED DAMAGED AREA ON LEFT HORIZONTAIL STAB LOWER SKIN IAW FEDEX SRM 55-10-3.
- [SDR 95FDEA00225](https://openairdocs.org/sdr/95FDEA00225.md): Fitting · cracked · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > BS 870 TERMINAL FITTING ROW 2 HOLES NR 3 AND NR 4 HAVE CRACK INDICATION NOTED RT SIDE. REPAIRED CRACK BETWEEN HOLES 3 AND 4, ROW 2 IN BS 870 TERMINAL FITTING RT SIDE IAW FEDEX EA 7-5310-23954.
- [SDR 95FDEA00224](https://openairdocs.org/sdr/95FDEA00224.md): Skin · corroded · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > GREATER THAN 10 PERCENT MATERIAL LOSS INDICATION NOTED AT BS 441 CIRCUMFERENTIAL SPLICE FWD SKIN PANEL BETWEEN STR 1920R. REPAIRED AFT UPR SKIN STA 440 STR 19 IAW FEDEX SRM 53-30-3 AND INITATED PART 5 OF 7-5330-7-2319G FOR BS 441 BETWEEN STR 19-20 FWD SKIN.
- [SDR 95FDEA00223](https://openairdocs.org/sdr/95FDEA00223.md): Skin · gouged · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > GOUGES IN SKIN AT F/O'S WINDSHIELD WIPER MOUNT AND JUST BELOW O/B SIDE OF NR 1 WINDOW. BLENDED GOUGE AT SKIN BELOW F/O'S WINDSHIELD WIPER. INSTALLED DOUBLER PER FEDEX EA NR 7-5330-23942.
- [SDR 95FDEA00222](https://openairdocs.org/sdr/95FDEA00222.md): Stiffener · corroded · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION IN E/E BAY ON FRAME STIFFENER AT BS 300 LBL 38 WL 169. PART OUT OF LIMIT REMOVED.070 BY.1250 BY.5 INCH CORROSION, REMOVED AND REPLACED STIFFENER STRAP.
- [SDR 95FDEA00221](https://openairdocs.org/sdr/95FDEA00221.md): Stringer · damaged · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > MECHANICAL DAMAGE ON STR 8L BS 802. REMOVED DAMAGED.5 INCH SECTION OF STR 8L FROM BS 802, FABRICATED AND INSTALLED PART PER FEDEX SRM 53-10-3.
- [SDR 95FDEA00220](https://openairdocs.org/sdr/95FDEA00220.md): Stringer · cracked · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > STR 21R IS CRACKED AT BS 400. REPAIRED STR 21R AT BS 400 IAW FEDEX SRM 53-10-01.
- [SDR 95FDEA00219](https://openairdocs.org/sdr/95FDEA00219.md): Floorbeam · corroded · Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CORROSION (71C709-02) IN NUTPLATE HOLES ON LOWER FLANGE OF FLOORBEAM AT BS 1110 RBL 3-47 WL 200. REPAIRED BS 1110 FLOORBEAM RBL 3-47 WL 200 AS PER FEDEX EA 7-5310-23951.

Next page: https://openairdocs.org/deregistered/N190FE-2007-03-01/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 = 'N190FE' AND deregistration_id = 'N190FE-2007-03-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N190FE-2007-03-01/reports

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