N190FE, cancelled Mar 1, 2007

Service difficulty reports · 55

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 05FDEA02689Fitting · misdrilledLEFT 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-Aug 26, 2005 · N190FE · Boeing 72722 · Wing, Landing Gear Attach FittingsSDR 04FDEA01900Intercostal · crackedFWD CARGO COMPARTMENT INTERCOSTAL IS CRACKED AT STRINGER 22R BS 572 THRU BS 580. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-1.Jul 1, 2004 · N190FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 04FDEA01899Skin · bulgedSKIN BULGE AT BS 1180 STRINGER 26L THRU STRINGER 23L. REPAIRED AREA IAW EA 7-5330-79539.Jul 1, 2004 · N190FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 04FDEA01233Warning Light · illuminatedNOSE 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 ILLUMay 12, 2004 · N190FE · Boeing 727100 · Landing Gear Position and WarningSDR 04FDEA00002Connector · contaminatedUNSAFE 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 DOWNLOJan 1, 2004 · N190FE · Boeing 727100 · Landing Gear Position and WarningSDR 99FDEA00465Bellframe · damagedNR 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.Sep 27, 1999 · N190FE · Boeing 72722 · Fuselage Main, FrameSDR 99FDEA00464Stringer · corrodedSTR 30 IS CORRODED BETWEEN BS 1148 AND 1166 IN AFT CARGO. REMOVED AND REPLACED STR 30 PER SRM 53-10-3.Sep 22, 1999 · N190FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 99FDEA00478Splice · corrodedNR 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.Sep 21, 1999 · N190FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 99FDEA00477Cover · corrodedNR 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.Sep 21, 1999 · N190FE · Boeing 72722 · Wing Miscellaneous StructureSDR 99FDEA00466Casting · scoredNR 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.Sep 21, 1999 · N190FE · Boeing 72722 · Fuselage, Wing Attach FittingsSDR 99FDEA00476Keel Beam · crackedNR 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.Sep 20, 1999 · N190FE · Boeing 72722 · Fuselage Main, KeelSDR 99FDEA00462Bottle Pin · corrodedRT FWD BOTTLE BOLT (SPAR TERMINAL PIN) HAS CORROSION. REMOVED AND REPLACED NEW BOTTLE BOLT PIN SEALED.Sep 10, 1999 · N190FE · Boeing 72722 · Wing, Fuselage Attach FittingsSDR 99FDEA00067Bulb · failedLT 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.Feb 18, 1999 · N190FE · Boeing 72722 · Landing Gear Position and WarningSDR 98FDEA00769Valve · failedLOST 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. Dec 29, 1998 · N190FE · Boeing 72722 · Landing Gear Retraction/Extension SystemSDR 98FDEA00497Computer · malfunctionedSTICK 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.Aug 11, 1998 · N190FE · Boeing 72722 · Stall Warning SystemSDR 98FDEA00226Switch · failedMAIN CARGO DOOR LIGHT CAME ON SHORTLY AFTER TAKEOFF. REPLACED LOCK ROD SWITCH AND ADJUSTED PER MAINTENANCE MANUAL 52-70-09, OPERATIONAL CHECKS GOOD.Apr 1, 1998 · N190FE · Boeing 72722 · Door Warning SystemSDR 97FDEA00562Frame · crackedCRACK 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.Aug 18, 1997 · N190FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00536Frame · crackedNR 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.Aug 14, 1997 · N190FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00535Frame · damagedNR 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.Aug 14, 1997 · N190FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00534Fitting · corrodedNR 0271 005 - R/W I/B AILERON, I/B TAB FITTING CORRODED (AREA MARKED).Aug 14, 1997 · N190FE · Boeing 72722 · AileronsSDR 97FDEA00521Shear Tie · corrodedCORROSION (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.Aug 8, 1997 · N190FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00520Mid Flap · delaminatedRIGHT 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.Aug 8, 1997 · N190FE · Boeing 72722 · Trailing Edge FlapsSDR 97FDEA00504Skin · delaminatedNR 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.Aug 6, 1997 · N190FE · Boeing 72722 · Trailing Edge FlapsSDR 97FDEA00335Hyd Filter · dirtyON 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 DEPLOYJun 10, 1997 · N190FE · Boeing 72722 · Hydraulic Filter, MainSDR 96FDEA01307Sequence Valve · leakingLOSS 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 2Jul 31, 1996 · N190FE · Boeing 72722 · Landing Gear Retraction/Extension SystemSDR 95FDEA00230Frame · double holeAT 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.Mar 12, 1995 · N190FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00245Fitting · crackedUPPER RUDDER TAB ACTUATING ROD SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED CRACKED UPPER RUDDER TAB ACTUATING ROD SUPPORT FITTING.Mar 10, 1995 · N190FE · Boeing 72722 · Rudder, Tab StructureSDR 95FDEA00244Frame · gougedGOUGE ON FRAME AT BS 680 STR 14L. REMOVED AND REPLACED DAMAGED AREA PER FEDEX SRM 51-40-3.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00243Stringer Tie · crackedFRAME TO STRINGER TIE CRACKED AT BS 680 STR 11L. REMOVED, FABRICATED AND REPLACED STR TIE AT BS 680 STR 11L.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA00242Stringer · corrodedCORROSION (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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA00241Stringer · crackedSTR 25R IS CRACKED AT BS 420. REPAIRED STR 25R AT BS 420 IAW SRM 53-10-3 FIG 1 DETAIL II.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA00240Floor Beam · corrodedCORROSION (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-Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 95FDEA00239Seat Track · corrodedCORROSION (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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00238Seat Track · corrosionCORROSION ON SEAT TRACK BS 480 RBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 480-510 RBL 25 WL 208.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00237Seat Track · corrosionCORROSION 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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00236Seat Track · corrodedCORROSION (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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00235Seat Track · corrosionCORROSION 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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00234Bulkhead · dentedDENT 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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, BulkheadSDR 95FDEA00233Clip · damagedCRACK 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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00232Seat Track · wornF/E'S AFT SEAT TRACK IS WORN. REMOVED AND REPLACED F/E'S AFT SEAT TRACK.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00231Frame · double holeAT 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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00229Stringer · gougedBS 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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA00226Skin · damaged9503-11 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.Mar 10, 1995 · N190FE · Boeing 72722 · Horizontal Stabilizer, Plate/SkinSDR 95FDEA00225Fitting · crackedBS 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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00224Skin · corrodedGREATER 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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 95FDEA00223Skin · gougedGOUGES 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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 95FDEA00222Stiffener · corrodedCORROSION 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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00221Stringer · damagedMECHANICAL 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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA00220Stringer · crackedSTR 21R IS CRACKED AT BS 400. REPAIRED STR 21R AT BS 400 IAW FEDEX SRM 53-10-01.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA00219Floorbeam · corrodedCORROSION (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.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Floor Beam
Back to N190FE, cancelled Mar 1, 2007