Boeing 727-22

Service difficulty reports · 1,282

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = '72722'
  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 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 BeamSDR 95FDEA00218Floorbeam · damagedDOUBLE HOLE IN LOWER FLANGE OF FLOORBEAM BS 600 RBL 62 WL 208. REPAIRED LOWER FLANGE OF BS 600 FLOORBEAM RBL 62 PER FEDEX EA 7-5310-23941.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 95FDEA00217Floorbeam · corrodedCORROSION (71C209-02) BS 640 WL 200 RBL 6-13 IN NUTPLATE HOLES ON LOWER FLANGE OF FLOORBEAM. BLENDED OUT CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM STA 640 IAW FEDEX EA 7-5310-23908.Mar 10, 1995 · N190FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 95FDEA00192Frame · gougedGOUGE FOUND ON FRAME BS 660 BETWEEN STR 8 AND 9L WL 271. ACCOMPLISHED FRAME REPAIR BS 660 BETWEEN STR 8 AND 9L WL 271 PER FEDEX SRM 53-10-4.Feb 28, 1995 · N185FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00190Frame · damagedMECHANICAL DAMAGE ON FWD SIDE OF FRAME BS 540 BELOW STR 9R. REMOVED MECHANICAL DAMAGE ON FWD SIDE OF FRAME BS 540 BELOW STR 9R AND REPAIRED IAW FEDEX SRM 53-10-4.Feb 28, 1995 · N185FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00189Frame · damageMECHANICAL DAMAGE ON FWD SIDE OF FRAME BS 520 BELOW STR 9R. ACCOMPLISHED FRAME REPAIR AT BS 520, STR 9R IAW PER FEDEX SRM 53-10-4.Feb 28, 1995 · N185FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00194Clip · crackedNOTED CRACK AND/OR HOLE DAMAGE IN LEFT BS 870 TERMINAL FITTING ROW 1 HOLE NR 1. INVESTIGATED DAMAGE. DETERMINED BY HFEC THAT DAMAGE TO FRAME TO STRINGER CLIP TO BE MECHANICAL TOOLING DAMAGE. REMOVED AND REPLACED CLIP.Feb 27, 1995 · N190FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00191Seat Track · corrodedCORROSION FOUND ON SEAT TRACK BS 600-650 BL 0 WL 208. REMOVED CORRODED SEAT TRACK, INSTALLED FABRICATED SEAT TRACK BS 600-650 BL 0 WL 208 IAW FEDEX SRM 53-10-5 SEAT TRACK EXTRUSION REPAIR.Feb 27, 1995 · N185FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00188Clip · crackedCRACK FOUND IN STR CLIP BS 440 STR 16L. REMOVED STR CLIP AT BS 440 STR 16L THEN INSTALLED A STR CLIP.Feb 27, 1995 · N185FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00187Doublers · crackedAFT CARGO BAY BS 1050 RBL 3-9 WL 146. THE FRAME IS CRACKED. REMOVED DAMAGED AREAS RBL 3-9. FABRICATED DOUBLER AND TWO FILLERS AND INSTALLED PER FEDEX SRM 51-40-3 AT STA 1050.Feb 27, 1995 · N185FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00184Clip · damagedNOTED CRACK AND/OR HOLE DAMAGE IN LT BS 870 TERMINAL FITTING ROW 1, HOLE NR 1. INVESTIGATED DAMAGE. DETERMINED BY HFEC THAT DAMAGE TO FRAME TO STRINGER CLIP TO BE MECHANICAL TOOLING DAMAGE. REMOVED AND REPLACED CLIP.Feb 27, 1995 · N190FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00195Frame · gougedGOUGE ON FRAME AT BS 680 STR 14L. REMOVED DAMAGED AREA, REPAIRED PER FEDEX SRM 51-40-3.Feb 25, 1995 · N190FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00181Seat Track · corrodedCORROSION ON THE SEAT TRACK BS 480-482 WL 208 LBL 23.5. REMOVED CORRODED SEAT TRACK SECTION. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION USING EXISTING AS TEMPLATE.Feb 25, 1995 · N185FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00183Angle · corrosionCORROSION IN AFT CARGO BAY BS 960, RBL 20, WL 144 ON L-ANGLE STIFFENER (HORIZONTAL) FOR BULKHEAD. CORROSION OUT OF LIMIT PER FEDEX SRM 53-10-01 CUT OUT DAMGED. FABRICATED PARTS, REPAIRED PER FEDEX SRM 51-40-04.Feb 24, 1995 · N185FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00180Clip · crackedSTR CLIP DAMAGED BS 440 STR 8L. REMOVED DAMAGED STR CLIP AND INSTALLED NEW CLIP IAW SRM 51-30-2.Feb 24, 1995 · N185FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00182Web · damagedSEVERAL HOLES IN THE WEB DAMAGED WHILE REMOVING A STIFFENER AT BS 310, LBL 12 - RBL 12, WL 180. REMOVED DAMAGED AREA IN WEB BS 310, LBL12-RBL 12, WL 180. FABRICATED DOUBLER AND FILLERS, SCOTCH BRITED, ALODINED, PRIMED, INSTALLED AS PER FEDEX SRM 53-10-9.Feb 23, 1995 · N185FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00179Stringer · gougedGOUGE IN STR BS 440, STR 7L. ACCOMPLISHED STR REPAIR BS 440, STR 7L PER FEDEX SRM 53-10-3.Feb 23, 1995 · N185FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA00171Support · corrosionCORROSION ON FLOOR SUPPORT BS 334, LBL 30, WL 208. REMOVED CORRODED FLOOR SUPPORT THEN INSTALLED A NEW FLOOR SUPORT BS 334, LBL 30, WL 208.Feb 22, 1995 · N185FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00170Intercostal · corrosionCORROSION ON FLOOR SUPPORT BS 322, LBL 30, WL 208. REMOVED CORRODED FLOOR SUPPORT THEN INSTALLED A NEW FLOOR SUPPORT AT BS 322, LBL 30, WL 208.Feb 22, 1995 · N185FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00169Skin · gougedGOUGE IN EXTERNAL SKIN STA 390, STR 7 AND 8 SKIN THICKNESS .040 GOUGE .012, GOUGE OUT OF LIMITS AS PER FEDEX SRM 53-30-1. REPAIRED GOUGE WITH SKIN FLUSH REPAIR AT STA 390 STR 7 AND 8 PER FEDEX SRM 53-30-3 FIG 13.Feb 21, 1995 · N185FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 95FDEA00168Clip · crackedCRACK FOUND IN STR CLIP BS 440 STR 2R. REMOVED FASTENERS FROM CRACKED STR CLIP AT BS 440 STR 2R. THEN INSTALLED NEW STR CLIP IAW FEDEX SRM 51-30-2.Feb 21, 1995 · N485FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95ZZZX532Switch · dirtyCVG - AT 200 FEET AGL FINAL APPROACH, GPWS ACTIVATED WITH 'TOO LOW FLAPS' WARNING. FLAP POSITION WAS VERIFIED IN 30 DEGREE POSITION BY ALL THREE CREW MEMBERS. GO-AROUND WAS EXECUTED, NEXT APPROACH WAS UNEVENTFUL TO A NORMAL LANDING. CLEANED FLAP SWITCH. OPJan 5, 1995 · N707DH · Boeing 72722 · Ground Proximity System
Back to Boeing 727-22