N187FE, cancelled Aug 16, 2004

Service difficulty reports · 75

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 = 'N187FE' AND deregistration_id = 'N187FE-2004-08-16'
  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 03FDEA02198Position Switch · inoperativeNLG DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. COMPLIED WITH QRH PROCEDURE. LIGHT REMAINED ON. CONFIRMED PROBLEM. NLG DOOR LIGHT ON ALL THE TIME. TROUBLESHOOT USING 727WDM 32-62-01. FOUND LT NLG DOOR POSITION SWITCH INOP. REPLACED LT NLG POSTION SWIDec 15, 2003 · N187FE · Boeing 727100 · Landing Gear Position and WarningSDR 02FDEA00382Module · shortedON TAKEOFF, AFTER RAISING THE GEAR HANDLE THE PRESS TO TEST & LIGHTS C/B (P6-3, LANDING GEAR) POPPED. 1ST & 2ND VERTI ROWS ON THE DOOR LIGHT PANEL LIGHT UP. ON RECOVERY, NONE OF THE GEAR LIGHTS WOULD LIGHT. M/GEAR EXT ACCOMP. F/O NOTICED A SPARK BEHIND 3 Jun 5, 2002 · N187FE · Boeing 727100 · Landing Gear Position and WarningSDR 01FDEA00501Battery · dischargedDURING ROUTINE INSP FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE LIGHT FOUND INOPERATIVE. *S/D* REMOVED AND REPLACED BATTERY PER IAW BAC 727 MM 33-50-121-2.Jun 26, 2001 · N187FE · Boeing 72722 · Emergency LightingSDR 01FDEA00500Skin · crackedN 318 DUR ROUTINE INSP FUSELAGE SKIN FOUND CRACKED AT BS 303.9 AT STR 4L LWR FASTENER HOLE. R&R FASTENER PER IAW BAC 727 SRM 51-30-2.Jun 26, 2001 · N187FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 01FDEA00499Bracket · crackedN 500 DUR ROUTINE INSP IB BRACKET ON THE #8 FLAP TRACK FOUND CRACKED. R&R & FAB BRACKET PER IAW BAC 727 SRM 51-20-1, 51-30-2.Jun 26, 2001 · N187FE · Boeing 72722 · Wing Miscellaneous StructureSDR 01FDEA00498Skin · crackedN 501 DUR ROUTINE INSP RH OB AILERON IB LE SKIN FOUND CRACKED. ** S/D ** R&R BRACKET PER IAW BAC 727 SRM 51-30-2.Jun 26, 2001 · N187FE · Boeing 72722 · AileronsSDR 99FDEA00302Fitting · crackedCRACK IN RIGHT HAND BS 740 FRAME FITTING. CRACK FOUND BEYOND REPAIRABLE LIMITS (EA 7-5310-40339 ISSUED) MAJOR REPAIR. *S/D* REPLACED FRAME (P/N 65C137724-92).Jul 31, 1999 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00680Casting · crackedNR 1034 HFEC IND CRACK AT BOTTOM FASTENER HOLE IN LT BS 870 CASTING, 2ND HOLE FROM BOTTOM, 1ST ROW FASTENERS BETWEEN STR 9L AND 10L. REPAIR ACCOMPLISHED PER EA 7-5310-29685.Oct 28, 1998 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00679Floorbeam · corrodedNR 924 CORROSION ON UPPER FLANGE OF FLOORBEAM 620 BL O TO LBL 25. CUT AND REMOVED DAMAGED PART OF FLOORBEAM AND INSTALLED UPPER CHORD REPAIR PER SRM 53-10-8 FIG 3.Oct 28, 1998 · N187FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00678Casting · crackedNR 1064 HFEC IND CRACK IN 1 FASTENER HOLE AT LT BS 870 CASTING 2ND HOLE FROM BOTTOM, 1ST ROW FASTENERS BETWEEN STR 10L AND 11L. REPAIR ACCOMPLISHED PER EA NR 7-5310-29685.Oct 28, 1998 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00677Casting · crackedNR 1066 HFEC IND 2 CRACKS EXTEND FROM NR 1 HOLE LT BS 870 SPLICE IN CASTING AT 11 O'CLOCK AND 7 O'CLOCK ROW 4. REPAIR ACCOMPLISHED PER EA 7-5310-29685.Oct 28, 1998 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00681Floorbeam · corrodedNR 136 UPPER LOBE BS 1130 HEAVY CORROSION UNDER UPPER AFT LIP OF FLOORBEAM AT RBL 55. REMOVED CORROSION, TREATED AND PRIMED AREA AND INSTALLED DOUBLER PER EA 7-5310-29681.Oct 27, 1998 · N187FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00676Floorbeam · corrodedNR 790 UPPER LOBE, CORROSION ON FLOORBEAM TOP SIDE OF UPPER FLANGE BS 1130, RBL 45 - RBL 65. REMOVED CORROSION, TREATED AND PRIMED AREA, INSTALLED DOUBLER PER EA 7-5310-29681.Oct 27, 1998 · N187FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00662Stringer · crackedSTR 25R, BS 480 CRACKED AT BRACKET ATTACHMENT. REPAIRED STR 25R AT BS 480 PER SRM 53-10-3.Oct 21, 1998 · N187FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 98FDEA00661Floorbeam · corrodedUPPER LOBE CABIN, CORROSION ON UPPER AND LOWER SIDE OF FWD TOP FLOORBEAM FLANGE AT BS 540 RBL 10, 5 INCHES FROM CENTER OF A/C. REMOVED CORROSION PER SRM 51-10-6, BEYOND LIMITS. INSTALLED DOUBLER, ACCOMP PER AARD 53-10-01-1 FIG 2.Oct 21, 1998 · N187FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00663Frame · crackedCRACK IN FRAME WEB BS 480, BELOW STR 26R. REPAIRED CRACK IN FRAME WEB BY STOP DRILL AND INSTALL OF DOUBLER PER SRM 53-10-4.Oct 20, 1998 · N187FE · Boeing 72722 · Fuselage Main, FrameSDR 98FDEA00641Floorbeam · corrodedCORROSION MAIN CARGO FLOORBEAM BS 620 AT LBL 45.5 AND 2 HOLES CORRODED BETWEEN LBL 45.5 AND LBL 24.75 FWD SIDE OF FLOORBEAM UPPER CHORD. NOTE: 2 HOLES BETWEEN LBL 24.5 AND LBL 45.5 ARE NOT MAJOR REPAIRS. REPAIR CORROSION DAMAGE AT LBL 45.5 BS 620 PER AARD 53Oct 6, 1998 · N187FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA01370Relay · dirtyCLIMBING OUT AT APPROX FLT LVL 250, HIGH PITCHED HOWL STARTED, FOLLOWED BY LOSS OF CABIN PRESS. UNABLE TO CONTROL CABIN PRESSURE USING BOTH PACKS. REMOVED AND REPLACED SAFETY RELAY, CLEANED AND OPS CK'D, OUTFLOW VALVES PER ENGINE RUN TO STEADY 4 PSI.Aug 15, 1996 · N187FE · Boeing 72722 · Cabin Pressure Control SystemSDR 96FDEA00733Strap · misdrilledWHILE WORKING 7-5310-7-3367B PT9, DISCOVERED FASTENER HOLES INTERFERED WITH RADIUS OF ANGLE AT BS 825.95 WL 207 TO 198 LBL 65, DUE TO INSTALLATION OF REPAIR STRAP. REPAIRED STRAP BS 825.95 WL 207 TO 198 LBL 65 PER FEDEX EA 7-5310-28184.Apr 3, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00732Web · corrosionUPON REMOVAL OF PRESSURE PAN, FOUND CORROSION ON WEB BS 760.95 WL 207 LBL 65 TO 68. REPAIRED BS 760.95 WEB WL 207 LBL 65-68 PER FEDEX EA 7-5310-28183.Apr 3, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00724Stringer · corrodedCORROSION (C53-113-01, 2) ON STR 27R AT BS 990 RBL 22 WL 142. INSTALLED STR SPLICE REPAIR PER SRM 53-10-3.Apr 1, 1996 · N187FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA00727Vertical Web · corrodedCORROSION (C53-113-01, 2) ON AFT BAY WEB SILL BS 1057 TO 1110 RBL 21 WL 148.5. FOUND UPON REMOVAL OF STRAP NR 0217. REMOVED AND REPLACED AFT BAY WEB SILL FROM BS 1057 TO 1110 RBL 21 WL 148.5.Mar 29, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00726Door Frame · corrosionCORROSION (C53-113-01, 2) ON DOOR FRAME AT BS 1057 RBL 30 WL 148 AT NUTPLATE HOLES. REPAIRED DAMAGE PER SRM 51-40-3.Mar 29, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00725Keel Beam · corrosionCORROSION (C53-113-01, 2) ON RT KEEL BEAM RBL 6 WL 140 BS 1020, 1030, 1042, 1056 AND 1085. REPAIRED KEEL BEAM IAW FEDEX EA 7-5310-28083.Mar 29, 1996 · N187FE · Boeing 72722 · Fuselage Main, KeelSDR 96FDEA00721Strap · corrodedWHILE WORKING EO 7-5310-7-3367B, FOUND REINFORCEMENT STRAP AND T-CLIP TO BE BADLY CORRODED AT BS 760 WL 206 LBL 70.5. REMOVED AND REPLACED STRAP AND CLIP AT BS 760 WL 206 LBL 70.5.Mar 28, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00689Frame · double drilledDOUBLE DRILLED HOLES ON NESTLED FLANGE OF FRAME AT BS 1166 LBL 20 WL 159. TRIMMED DAMAGE AND INSTALLED DOUBLER PER FEDEX SRM 51-40-3.Mar 25, 1996 · N187FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00688Keel Beam · corrodedCORROSION (C53-113-01, 2) ON LT KEEL BEAM AT LBL 6 WL 190 BS 979, 1013 AND 1030. ALSO, MATERIAL CHIPPED AWAY FROM BEAM AT 1031. FABRICATED REPAIR PARTS AND INSTALLED PER EA 7-5310-28043.Mar 25, 1996 · N187FE · Boeing 72722 · Fuselage Main, KeelSDR 96FDEA00687Stringer · corrodedUPON REMOVAL OF SPLICE AT BS 520, DISCOVERED CORROSION OF STR 27R BS 522 AND 517 TO BE OUT LIMITS. REMOVED AND REPLACED DAMAGED SECTION OF STR 27R.Mar 25, 1996 · N187FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA00686Skin · corrodedCORROSION (C53-132-02, 1) ON INNER SURFACE OF WING CENTER SECTION UPPER SKIN BS 870 RBL TO LBL 70 PLUS ON RT SURFACE LBL 55 TO 70. REMOVED CORROSION AND BLENDED AREA, WITHIN LIMITS PER EA 7-5710-28042.Mar 25, 1996 · N187FE · Boeing 72722 · Wing, Plate/SkinSDR 96FDEA00685Web · crackedUPON REMOVAL OF I/B FLOOR WEB AT BS 294 TO 344 WL 169 RBL 15 TO 27 FOUND TO BE CRACKED. REMOVED AND REPLACED FLOOR WEB AND INSTALLED ALL BRACKETS AND ANGLES REMOVED FOR INSTALLATION AT BS 294 TO 351 WL 169 RBL 15 TO 27. ALL WORK IAW BAC DRW NR 65-18915.Mar 25, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00684Web · crackedWHILE WORKING NR0498, FOUND O/B RT DOGHOUSE WEB TO BE CRACKED BS 294 TO 351 RBL 25 AND 26 WL 169. REMOVED AND REPLACED O/B DOGHOUSE WEB ALL WORK IAW BAC DRW NR 65-18915 AT BS 294 TO 351 RBL 25 TO 36 WL 169.Mar 25, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00691Skin · gougeBS 277.2 STR 21R WL 180, THERE IS A DEEP GOUGE IN SKIN. BLENDED GOUGE IN SKIN AT BS 277.2 STR 21R WL 180 ORIGINAL SKIN THICKNESS WAS .040, AREA REMOVED WAS .030. A 1 INCH BY .5 INCH AREA AND WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. DAMAGED AREA Mar 23, 1996 · N187FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00690Skin · dentedBS 660.3 STR 20R WL 181, THERE IS A DEEP GOUGE IN SKIN. BLENDED GOUGE AT BS 660.3 STR 20R WL 181 WAS OUT OF LIMITS PER FEDEX SRM 53-30-1. REMOVED 2.75 INCH BY 1.8 INCH OF DAMAGED SKIN, FABRICATED DOUBLE AND INSTALLED IAW FEDEX SRM 53-30-3.Mar 22, 1996 · N187FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA0539Frame · double drilledDOUBLE DRILLED HOLES ON THE NESTLED FLANGE OF FRAME AT BS 1110 LBL 19 WL 152. TRIMMED DAMAGE AND INSTALLED DOUBLER PER FEDEX SRM 51-40-3.Mar 18, 1996 · N187FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00602Tripler · corrodedNR 0074 AND 027, BS 1110 RBL 29 BETWEEN STR 25 TO 26R SKIN BULGE AROUND FASTENERS. REPAIRED DAMAGED SKIN IAW FEDEX EA 7-5310-28049.Mar 18, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00601Transverse Beam · crackedNR 0248 AND 028, FWD CARGO DOOR NR 4 FROM BOTTOM, TRANSVERSE BEAM IS CRACKED IN O/B RADIUS 12 INCHES AND 24 INCHES OF FWD EDGE. REMOVED AND REPLACED NR 4 TRANSVERSE BEAM ON FWD CARGO DOOR MM 52-31-61.Mar 18, 1996 · N187FE · Boeing 72722 · Cargo/Baggage DoorsSDR 96FDEA00600Web · crackedNR 0254 AND 029, AFT CARGO DOOR NR 4 FROM BOTTOM, TRANSVERSE BEAM IS CRACKED IN RADIUS 24 INCHES AFT OF FWD EDGE OF DOOR. REMOVED AND REPLACED NR 4 TRANSVERSE BEAM ON AFT CARGO DOOR.Mar 18, 1996 · N187FE · Boeing 72722 · Cargo/Baggage DoorsSDR 96FDEA00597Skin · delaminatedNR 0411 AND 035, RT WING O/B AFT FLAP HAS AN AREA OF DELAMINATION ON LOWER SKIN 60 INCHES FROM I/B END. REPAIRED DAMAGED LOWER SURFACE SRM 51-40-6.Mar 18, 1996 · N187FE · Boeing 72722 · Trailing Edge FlapsSDR 96FDEA00595Frame · double drilledNR0473, DOUBLE DRILLED HOLES ON NESTLED FLANGE OF FRAME AT BS 1166 LBL 20 WL 159. *S/D* TRIMMED DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-3.Mar 18, 1996 · N187FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00594Frame · double drilledNR 0474 AND 038, DOUBLE DRILLED HOLES ON FRAME AT BS 1148 LBL 20 WL 156. REPAIRED DOUBLE DRILLED HOLES PER SRM 51-40-3.Mar 18, 1996 · N187FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00593Angle · crackedNR0500 AND 042, CRACK FOUND IN BS 740 SILL REINFORCEMENT ANGLE FWD WL 170 LBL 38. REPAIRED 740 SILL ANGLE PER SRM 51-20-1 AND 51-40-3.Mar 18, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00592Blkhd Web · corrodedNR 0518 AND 043, WHILE WORKING NR 0468 FOUND AFT BULKHEAD OF WING CENTER SECTION TO BE CORRODED BS 870 LBL TO RBL 65 WL 178. REMOVED DAMAGED WEB AND INSTALLED NEW WEB AT BS 870 WL 162 TO 188 RBL 65 TO LBL 65.Mar 18, 1996 · N187FE · Boeing 72722 · Fuselage Main, BulkheadSDR 96FDEA00590Angle · crackedNR 0540 AND 045, WHILE WORKING NR 0254 FOUND AFT CARGO DOOR NR 2 FROM BOTTOM, I/B L-ANGLE TO BE CRACKED IN RADIUS. REMOVED AND REPLACED L-ANGLE SRM 52-30-1.Mar 18, 1996 · N187FE · Boeing 72722 · Cargo/Baggage DoorsSDR 96FDEA00589Web · corrodedNR 0558 AND 047, UPON REMOVAL OF LT I/B DOGHOUSE WEB, FOUND IT TO BE OUT OF LIMITS AT BS 294 TO 344 LBL 15 TO 23 WL 159. REMOVED AND REPLACED LT I/B DOGHOUSE WEB AND REINSTALLED ALL DUCTS AND BRACKETS THAT WERE REMOVED FOR INSTALLATION AT BS 294 TO 351 LBL 15Mar 18, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00544Frame · crackedCRACK INDICATION NOTED HOLE 2 ROW 2 BS 870 LT. REMOVED ANGLE, STOP DRILLED CRACK, INSTALLED ANGLE PER SB 727-53-194 AND ER 031496LD2.Mar 18, 1996 · N187FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00543Frame · double drilledDOUBLE DRILLED HOLES ON FRAME AT BS 1050 LBL 20 WL 147. TRIMMED DAMAGED AREA AND REPAIRED FRAME PER FEDEX SRM 51-40-3 FIG 1.Mar 18, 1996 · N187FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00542Door Skin · dentedFWD ENTRY DOOR HAS 2 DENTS BY LOWER HINGE CUTOUT AFT SIDE OF DOOR ON EXTERNAL SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 52-00-3.Mar 18, 1996 · N187FE · Boeing 72722 · Passenger/Crew DoorsSDR 96FDEA00541Strap · corrodedCORROSION (C53-113-01) ON THRESHOLD VERTICAL WEB, BS 540 AND 560 RBL 21 WL 156. REMOVED AND REPLACED VERTICAL WEB SRM 53-10-1.Mar 18, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00540Frame · double drilledDOUBLE DRILLED HOLES ON THE NESTLED FLANGE OF A-FRAME AT 1130 LBL 19 WL 154. TRIMMED AND REPAIRED DOUBLE DRILLED HOLES ON NESTLED FLANGE OF A-FRAME AT 1130 LBL 19 WL 154 PER FEDEX SRM 51-40-3.Mar 18, 1996 · N187FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00538Frame · double drilledDOUBLE DRILLED HOLES ON FRAME AT BS 1070 LBL 20 WL 149. TRIMMED DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-3.Mar 18, 1996 · N187FE · Boeing 72722 · Fuselage Main, Frame
Back to N187FE, cancelled Aug 16, 2004