N191FE, cancelled May 2, 2007

Service difficulty reports · 147

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 = 'N191FE' AND deregistration_id = 'N191FE-2007-05-02'
  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 07FDEA00427Computer · malfunctionedCAPT STICK SHAKER ACTIVATED ON ROTATION. SHAKER SPEED WAS ABNORMALLY SLOW, ABOUT 1/3 NORMAL RATE DURING TEST. SHAKER CONTINUED FOR APPROX 3 MINUTES AND SLOWED GRADUALLY UNTIL IT STOPPED. AIRCRAFT FLEW NORMALLY. REMOVED AND REPLACED NR 1 STALL WARNING COMPUFeb 8, 2007 · N191FE · Boeing 72722 · Stall Warning SystemSDR 06FDEA0889Skin · crackedEXTERIOR FUSELAGE SKIN HAS A CRACK AT BS 352, LBL 18, WL 145. *S/D* REMOVED REPAIR BS 352, LBL 18, WL 145, REPAIRED IAW FED EX EA 7-5330-96595.Mar 2, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 06FDEA0844Skin · damagedDENT WITH ASSOCIATED GOUGE IN FUSELAGE SKIN, BS 590, BETWEEN STR 17 AND 18 RT. FOUND TO BE OUT OF SERVICE LIMITS, REPAIRED IAW SRM 53-30-3 FIG 13A.Feb 26, 2006 · N191FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 06FDEA0814Skin · debondedN01287 REWORK OF CARD N01229 REQUIRED. WHILE INSPECTING LT LOWER NOSE CHORD INSTALLATION, FOUND SKIN DISBONDED AND CORRODED AT BS 297, LBL 20, WL 148. REWORK REQUIRED BECAUSE REPAIR WAS INSTALLED IN A RESTRICTED AREA IAW SRM 53-30-3 FIG. 12. ** SD ** Feb 23, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 06FDEA0806Shear Tie · damagedWHILE REMOVING SKIN FOR ACCESS ON STR 27L REPAIR; FOUND SHEAR TIE AT BS 1143 STR 27L DAMAGED. REPAIRED SHEAR TIE PER SRM 53-10-4 FIG 15.Feb 22, 2006 · N191FE · Boeing 72722 · Fuselage Internal Mounting StructureSDR 06FDEA0578Stringer · corrodedWHILE WORKING N01286 FOUND STRINGER 27 LEFT CORRODED AT BS 1176. REMOVED AND REPLACED STR 27L, BS 1090 - 1183 IAW SRM 53-10-3, 51-10-2, AND 51-30-2.Feb 7, 2006 · N191FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 06FDEA0537Spar · tool damageRT WING FRONT SPAR LOWER CHORD PLATE HAS A MISSED DRILLED HOLE LOCATED DIRECTLY BELOW THE NR 4 K-FLAP ACTUATOR. REPAIRED MISSDRILLED HOLE IAW FED EX EA 7-5710-96565.Feb 3, 2006 · N191FE · Boeing 72722 · Wing SparSDR 06FDEA0467Angle · unknownCOMPLY WITH EA 7-5710-96564, RIGHT MAIN LANDING GEAR TRUNNION SUPPORT FITTING, -TEE ANGLE- HOLE LOCATION -E- REPAIR- AD 2004-18-08. COMPLIED WITH FED-EX EA 7-5710-96564, REFERENCE CUSTOMER CARD 7-5710-7-2314 PT 4.Feb 1, 2006 · N191FE · Boeing 727100 · Wing, Landing Gear Attach FittingsSDR 06FDEA0431Web · damagedWHILE WORKING FED EX CARD N00897 FOUND AN EXTRA HOLE ON WEB UNDER UPPER PANEL SUPPORT CHORD ON VERTICAL STAB AT FIN STA 247 UPPER RIGHT SIDE. *S/D* REPAIRED PANEL SUPPORT CHORD ON VERTICAL STAB IAW FED-EX EA 7-5530-96566.Jan 30, 2006 · N191FE · Boeing 727100 · Vertical StabilizerSDR 06FDEA0430Skin · unknownDURING ACCESS FOR STR 30 REPAIR, (CUSTOMER CARD N00999), UPON REMOVAL OF EXISTING REPAIR DOUBLER BS 1165 - 1183 RBL 12 - LBL 10 FOUND ORIGINAL SKIN HAS CUTOUT BS 1175 - 1183 RBL 1 - 6.5 AND BS 1183 LWR CHORD CUTOUT IN A 1 X 2 INCH AREA. ALL WORK WAS ACCOMPLISHJan 30, 2006 · N191FE · Boeing 727100 · Aircraft StructuresSDR 06FDEA0404Spar · corrodedRT WING FRONT SPAR HAS AREAS OF CORROSION AT LES 340-345. REPAIRED PER FED EX EA 7-5710-96562.Jan 27, 2006 · N191FE · Boeing 727100 · Wing SparSDR 06FDEA0405Trunnion · unknownWHILE WORKING E.O. 705710-7-2314 P4, FOUND BOTH "C" HOLES IN TRUNION ATTACH FITTING TO BE SPOTFACED ON INNER SURFACE AROUND HOLES. REPAIRED RT MLG FWD TRUNNION FITTING SPOT FACED AREAS AT "C" HOLE LOCATIONS IAW FED-EX EA 7-5710-96561. THIS IS A MAJOR REPJan 27, 2006 · N191FE · Boeing 727100 · Wing, Landing Gear Attach FittingsSDR 06FDEA0375Flap · corrodedNR 5 K-FLAP HAS CORROSION AT OB BULLNOSE TO K-FLAP BONDING WIRE BOTH ATTACH POINTS. REPAIRED NR 5 K FLAP BULLNOSE PER SR DRAWING SR 27-57-010 REV C.Jan 25, 2006 · N191FE · Boeing 727100 · Leading Edge DevicesSDR 06FDEA0374Stringer · corrodedAFT CARGO COMPARTMENT, CORROSION ON STR. 30 BS 1166 TO BS 1183 BL 0. REPAIRED STR 30 BS 1140 - 1183 IAW SRM 53-10-3, 51-10-2 AND 51-30-2.Jan 25, 2006 · N191FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 06FDEA0298Structure · corrodedWHILE WORKING N01170 FOUND CORROSION ON EXTERIOR FUSELAGE STRUCTURE AT BS 352, LBL 17, WL 145. REMOVED AND REPLACED STRUCTURE IAW SRM 53-10-1, 51-30-2.Jan 20, 2006 · N191FE · Boeing 727100 · Fuselage Main, StructureSDR 06FDEA0304Flap Track · corrodedCORROSION ON NR 2 FLAP TRACK, AFT O/B MOUNTING HOLE. NEW NR 2 FLAP TRACK WAS INSTALLED ON FED-EX W/C 27X5706-03.Jan 20, 2006 · N191FE · Boeing 727100 · Trailing Edge FlapsSDR 06FDEA0286Door Frame · corrodedCORROSION ON RIGHT FWD EMERGENCY EXIT HATCH EXTERIOR LWR EDGE FRAME UNDER PRESS SEAL. *S/D* RIGHT FWD EMERGENCY EXIT DOOR WAS OVERHAULED IAW WORK ORDER MR1382409.Jan 19, 2006 · N191FE · Boeing 727100 · Emergency ExitsSDR 06FDEA0214Stringer · crackedLT WING, STA 629.00 THIRD STRINGER FROM REAR SPAR IS CRACKED.Jan 16, 2006 · N191FE · Boeing 727100 · Wing, Longeron/StringerSDR 06FDEA0181Floorbeam · corrodedCORROSION STA 312 LBL 30 WL 208 CORROSION ON FLOORBEAM UPPER CHORD. *S/D* REPAIRED FLOORBEAM AT STA 312, LBL 30, WL 208 PER SRM 53-10-8, 53-10-1.Jan 13, 2006 · N191FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 06FDEA0180Floorbeam · corrodedCORROSION STA 328 LBL 30 AND LBL 40 WL 208 CORROSION ON FLOORBEAM UPPER CHORD. *S/D* REPAIRED FLOORBEAM AT BS 328, LBL 30 AND 40, WL 208 PER SRM 53-10-8, 53-10-1, 51-30-02.Jan 13, 2006 · N191FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 06FDEA0157Skin · crackedEXTERIOR FUSELAGE SKIN HAS A CRACK AT BS 352, LBL 18, WL 145. *S/D* REPAIRED SKIN IAW SRM 53-30-3.Jan 12, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 06FDEA0155Skin · dentedDENT IN EXTERNAL FUSELAGE SKIN AT BS 1163, STR 9L. *S/D* DENT IN FUSELAGE SKIN AT BS 1163, STR 9L REPAIRED IAW SRM 53-30-3.Jan 12, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 06FDEA0158Skin · crackedEXTERIOR FUSELAGE SKIN HAS A CRACK AT BS 352, LBL 18, WL 145.Jan 12, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 06FDEA0156Skin · crackedEXTERIOR SKIN HAS A CRACK AT FASTENER HOLE AT BS 352, RBL 18, WL 145. REPAIRED CRACK PER ER 06-1285 AND FED EX EA 7-5330-96592.Jan 12, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 06FDEA0149Shear Tie · corrodedAFT CARGO COMPARTMENT, CORROSION ON SHEAR TIE BETWEEN STR 30 LT AND 29 LT BS 1110. *S/D* REMOVED FASTENERS COMMON TO SHEAR TIE, REMOVED CORROSION OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-4.Jan 11, 2006 · N191FE · Boeing 727100 · Fuselage Internal Mounting StructureSDR 06FDEA0148Skin · corrodedWHILE INSPECTING LT LOWER NOSE CHORD INSTALLATION FOUND SKIN DISBONDED AND CORRODED AT BS 297, LBL 20, WL 148.Jan 11, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 06FDEA0135Failsafe · crackedFAIL SAFE CHORD CRACKED BS 990 STR 25L. *S/D* CUT OUT AND REMOVED DAMAGED FAIL SAFE CHORD, FABRICATED AND INSTALLED REPAIR AND REPAIR SECTION PER SRM 51-40-3 FIG 1, IAW SRM 51-30-2.Jan 10, 2006 · N191FE · Boeing 727100 · Fuselage Main, StructureSDR 06FDEA0134Failsafe · crackedFAIL SAFE CHORD CRACKED BS 1030 STR 25L. *S/D* REMOVED FAIL SAFE CHORD, FABRICATED AND INSTALLED REPAIR AND REPAIRED SECTION PER SRM 51-40-3, 51-30-2.Jan 10, 2006 · N191FE · Boeing 727100 · Fuselage Main, StructureSDR 06FDEA0131Stringer · damagedAFT CARGO COMPARTMENT HOLE IN STR 23 LT B/S 965. REPAIRED AFT CARGO COMPARTMENT STR 23L AT BS 965, HOLE IN TOP OF STR IAW SRM 53-10-3.Jan 9, 2006 · N191FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 06FDEA0104Shear Tie · unknownAFT CARGO COMPARTMENT ON SHEAR TIE BETWEEN STR 30 LT AND 29 LT BS 1130. REPLACED SHEAR TIE IAW SRM 51-30-2.Jan 9, 2006 · N191FE · Boeing 727100 · Fuselage Internal Mounting StructureSDR 06FDEA0103Shear Tie · corrodedAFT CARGO COMPARTMENT, CORROSION ON SHEAR TIE BETWEEN STR. 28 LT AND 29 LT BS 1130. REPLACED SHEAR TIE IAW SRM 51-30-2.Jan 9, 2006 · N191FE · Boeing 727100 · Fuselage Internal Mounting StructureSDR 06FDEA0102Frame · corrodedWHILE WORKING ON ACCESSING FOR N00743, FOUND CORROSION ON LT MIDDLE NOSE CHORD AT BS 297-BS 352, WL 169, LBL 16. ** SD ** COMINGJan 9, 2006 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 06FDEA0060Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM UPPER FLANGE AROUND NUTPLATES AT BS 1130, LBL 10 TO RBL 29, WL 208. REPAIRED FLOORBEAM UPPER FLANGE BS1130, RBL 10, WL 208 IAW SRM 53-10-8.Jan 6, 2006 · N191FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 06FDEA00019Stringer · dentedDENTED STRINGER AT STA 493, STR 8RT. *S/D* REPAIRED STRINGER PER SRM 53-10-3.Jan 4, 2006 · N191FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 06FDEA0018Frame · tool damageAFT CARGO COMPARTMENT, DRILL STARTS IN FRAME AT STR 23 RT AND 27 LT BS 1148 ON INBOARD FLANGE. *S/D* ALL MAINTENANCE REQUIREMENTS FOR THIS CARD ACCOMPLISHED ON CARD N00986.Jan 4, 2006 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 06FDEA0015Stringer · crackedFOUND STR 26R CRACKED AT FASTENER HOLE O/B FLANGE BS 430. REPAIRED CRACKED FASTENER IAW SRM 53-10-03.Jan 3, 2006 · N191FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 06FDEA0013Skin · chafedFOUND SECTION SKIN IS CHAFED ABOVE RT LWR RAIN GUTTER, BS 1351. REPAIRED SKIN CHAFE OVER RT LWR RAIN GUTTER, BS 1351 PER SRM 54-30-3.Jan 3, 2006 · N191FE · Boeing 72722 · Nacelle/Pylon, Plate/SkinSDR 06FDEA0012Floorbeam · corrodedFOUND CORROSION, STA 344 LBL 50 TO RBL 15 WL 208 CORROSION ON FLOORBEAM UPPER CHORD. REMOVED DAMAGED SECTION OF UPPER CHORD, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8.Jan 3, 2006 · N191FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 05FDEA04412Strap · corrodedN00310 CORROSION ON REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM AT BS 1130 RBL 63, WL 208. REMOVED AND REPLACED REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM AT BS 1130, RBL 63, WL 208, PER SRM 51-30-2.Dec 27, 2005 · N191FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 05FDEA04410Strap · corrodedN00312 CORROSION ON REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM BS 1130 LBL. 63, WL 208. REMOVED AND REPLACED REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM BS 1130, LBL 63, WL 208, IAW SRM 51-30-5, 51-30-2.Dec 27, 2005 · N191FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 05FDEA04414Skin · lightning strikeN00280 LIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1167, STR 13R. DETERMINED LIGHTNING STRIKE DAMAGE IN SKIN AT BS 1167, STR 13R TO BE OUT OF LIMITS, REPAIRED IAW SRM 53-30-3 FIG 13A.Dec 27, 2005 · N191FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 05FDEA04413Crease Beam · corrodedFOUND CORROSION ON CREASE BEAM ANGLE, BS 1120 TO BS 1130, LBL 65, WL 208.Dec 27, 2005 · N191FE · Boeing 727227 · Fuselage Main, StructureSDR 05FDEA04407Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 25 LT AND 27 LT BS 1050 ON IB FLANGE. REPAIRED DENTED FRAME BETWEEN STR 25LT AND 27LT, BS 1050 ON I/B FLANGE IAW SRM 51- 40-3.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04406Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 24 LT AND 27 LT BS 1030 ON IB FLANGE. REPAIRED IAW SRM 51-40-3.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04405Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 24 LT AND 27 LT BS 1010 ON IB FLANGE. REPAIRED PER 51-40-03 & 53-10-1.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04404Frame · dentedN00987 AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 26 LT AND 27 LT BS 1148 ON IB FLANGE ** SD ** COMING.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04403Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 26 RT AND 23 RT BS, 1148 IN IB FLANGE. AFT CARGO COMPARTMENT FRAME AT BS 1148 BETWEEN STR 23R, AND 26R WAS FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-40-3.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04402Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 25 LT AND 27 LT BS 990, ON IB FLANGE. REPAIRED FRAME PER SRM 51-40-3.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04395Structure · corrodedBS 297 CORROSION ON LT LOWER NOSE CHORD.Dec 21, 2005 · N191FE · Boeing 72722 · Fuselage Main, StructureSDR 05FDEA02932Indicator · inoperativeNR 2 KRUGER FLAP LED FAILED TO RETRACT ON SCHEDULE. KRUGER FLAP INDICATION INOP, FO'S AND SO'S PANEL REMOVED AND REPLACED NR 2 POS INDICATION SWITCH PER MM 27-82-001-4 SYS, OPS CHECK NORMAL.Sep 15, 2005 · N191FE · Boeing 72722 · Leading Edge Slat Position Indicating System
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