Boeing 727-233
Service difficulty reports · 3,034
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 = '727233' 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.
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 = '727233' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 96FDEA00616Frame · dentedDENT ON TOP FLANGE OF FRAME BS 660 LBL 42 WL 165. REPAIRED DENTED FRAME AT BS 660 LBL 42 WL 165 IAW FEDEX SRM 51-40-3.SDR 96FDEA00615Floor Beam · corrodedCORROSION ON FLOOR BEAM UPPER CHORD BS 1030 LBL 9 RBL 10 AND RBL 21 WL 208. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PARTS ON FLOOR BEAM UPPER CHORD BS 1030 RBL 10 WL 208 PER FEDEX SRM 53-10-8 FIG 8. REMOVED .011 OF ORIGINAL .125 AT LBL 9 AND .006 AT RSDR 96FDEA00614Skin · dentedTWO DENTS IN FUSELAGE SKIN BS 400 STR 17L. REPAIRED DENTS PER FEDEX SRM 53-30-03 FIG 1.SDR 96FDEA00613Riser Assy · corrodedWHILE WORKING ON TREAD REMOVAL FOUND CORROSION ON NR 1 RISER BEYOND LIMITS. REMOVED AND REPLACED NR 1 AIRSTAIR RISER, ALODINED, PRIMED AND PAINTED.SDR 96FDEA00612Skin · corrodedCORROSION ON SKIN AROUND BLIND FASTENERS UNDER FAIRING STRUCTURE AT BS 720A PLUS 10, 1 INCH BELOW STR 29L. REPAIRED SKIN AROUND BLIND FASTENERS UNDER FAIRING STRUCTURE AT BS 710, 1 INCH BELOW STR 28L PER FEDEX SRM 53-30-1, 53-10-1, 53-10-3 AND 51-20-1.SDR 96FDEA00606Riser · corrodedFOUND CORROSION ON NR 2 AIRSTAIR RISER WHILE REMOVING TREAD. REMOVED AND REPLACED NR 2 AIRSTAIR RISER, ALODINED, PRIMED AND PAINTED.SDR 96FDEA00560Shear Web · corrodedCORROSION (C53-224-04) ON SHEAR WEB BS 1139 RBL 25 TO 45 WL 208. REPAIRED SHEAR WEB AT BS 1139.SDR 96FDEA00559Seat Track · corrosionCORROSION (C53-224-01, 1) AROUND FASTENER THROUGH FLANGE OF SEAT TRACK AT BS 344 LBL 24 WL 208. REMOVED CORROSION ON UPPER SEAT TRACK FLANGE BS 344 LBL 24 WL 208 IN AN AREA 1 INCH BY .5 INCH BY .0135 INCH. ORIGINAL THICKNESS WAS .070, REMAINING MATERIAL THICSDR 96FDEA00558Seat Track · corrodedCORROSION AROUND FASTENER HOLES IN SEAT TRACK WELL FROM BS 760 TO 848 RBL 25 WL 208. REMOVED CORRODED SEAT TRACK WELL FROM BS 760 TO 848 RBL 25 WL 208 FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. INSTALLED NEW SEAT TRACK WELL AT BS 760 TO 848 RBL 25 WL 2SDR 96FDEA00557Frame · double drilledDOUBLE HOLE IN BS 760 FRAME BELOW STR 6L. REMOVED DAMAGE, FABRICATED REPAIR PART AND INSTALLED AT BS 760 FRAME BELOW STR 6L PER FEDEX SRM 53-10-4.SDR 96FDEA00556Frame · double drilledDOUBLE AND TRIPLE HOLES IN FRAME STA 1030 BETWEEN STR 8 AND 9 RT. ACCESSED AREA, TRIMMED OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED FASTENERS AT BS 1030 BETWEEN STR 8 AND 9 RT PER EWO NR 96-2135.SDR 96FDEA00611Web · gougedFWD ENTRY DOOR UPPER HINGE CASTING IN DOOR, LOWER SUPPORT WEB IS GOUGED REQUIRING REPLACEMENT. REMOVED AND REPLACED LOWER SUPPORT WEB ON UPPER HINGE CASTING, FWD ENTRY DOOR.SDR 96FDEA00610Support Assy · damagedTRAMCO RESPONSIBILITY 9603-12, UPON REMOVAL OF FWD ENTRY DOOR UPPER HINGE CASTING IN DOOR, LOWER SUPPORT, UPPER HINGE SUPPORT ASSY WAS DAMAGED. REMOVED AND REPLACED DAMAGED UPPER HINGE SUPPORT ASSY.SDR 96FDEA00609Skin · crackedNR 3 CARGO DOOR INNER SKIN HAS A RIVNUT HOLE WITH THREE CRACKS EMANATING FROM IT 12 INCHES AFT OF THE FWD EDGE, 1.5 INCH FROM THE BOTTOM. FABRICATED AND INSTALLED EXTERNAL DOUBLER AFTER DAMAGED AREA WAS REMOVED.SDR 96FDEA00608Depressor Seal · crackedFOUND CRACK IN DEPRESSOR SEAL RT AFT SERVICE DOOR UPPER FWD CORNER REVEAL. REPLACED DEPRESSOR SEAL.SDR 96FDEA00580Seat Track · corroded(NR 0388 AND NR 075). CORROSION ON THE RIGHT SIDE OF SEAT TRACK AT BS 1160, RBL 45, WL 208. ****S/D**** REMOVED AND REPLACED SEAT TRACK FROM BS 1130 - 1173, RBL 45, WL 208 IAW FEDEX SRM 53-10-5.SDR 96FDEA00579Stringer Clip · corrodedNR0663 AND 076, CORROSION BS 700 STR CLIP NR 5L HAS CORROSION. *S/D* REMOVED STRINGER CLIP AT BS 700, STR CLIP 5L, REPLACED WITH NEW CLIP PER SRM 51-30-2.SDR 96FDEA00532Skin · delaminatedRT WING I/B AFT FLAP HAS A 2 INCH DELAMINATED DENT 14 INCHES FROM I/B END UPPER SURFACE. REPAIRED RT WING I/B AFT FLAP 14 INCHES FROM I/B END UPPER SURFACE IAW FEDEX SRM 51-40-6.SDR 96FDEA00528Skin · disbondedLEFT WING I/B AFT FLAP HAS DISBONDED DENT UPPER SURFACE AT 18 INCHES FROM I/B END. REPAIRED LEFT WING I/B AFT FLAP AT 18 INCHES FROM I/B END IAW FEDEX 51-40-6.SDR 96FDEA00531Keel Beam · crackedRT KEEL BEAM CRACKED AT BS 990 STR 29R, SPLICED IN NEW SECTION OF AFT RT KEEL BEAM. REPAIRED RT KEEL BEAM PER FEDEX CARD 7-5310-7-2356C PT 5 AND FEDEX EA NR 7-5310-27778.SDR 96FDEA00530Frame · damagedAT FRAME 500 ABOVE STR 24L HAS A 1 INCH BY .5 INCH HOLE TORN THROUGH TOP OF FRAME. REPAIRED PER FEDEX SRM 51-40-03.SDR 96FDEA00607Rib · chafingNR 3 ENG LOWER COWL HAS TWO AREAS OF CHAFING ON NR 5 RIB. REMOVED AND REPLACED NR 3 ENGINE LOWER COWL NR 5 RIB.SDR 96FDEA00529Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT BS 950C TO 950E PLUS 5 RBL 25 WL 208. REPLACED SEAT TRACK FROM BS 950 TO 950E PLUS 10 RBL 25 WL 208.SDR 96FDEA00499Web · gougedNR 0736, FORWARD ENTRY DOOR UPPER HINGE CASTING IN DOOR, LOWER SUPPORT WEB IS GOUGED REQUIRING REPLACEMENT. *S/D* REMOVED AND REPLACED LOWER SUPPORT WEB ON UPPER HINGE CASTING ON FORWARD ENTRY DOOR PER SRM 53-10-2.SDR 96FDEA00498Skin · dented(NR 0685) MAIN CARGO DOOR HAS TWO BULGES IN THE OUTER SKIN AT FORWARD AND AFT LIFT ACTUATORS. CORRECTIVE ACTION: REWORKED BULGES ON MCD OUTER SKIN AT FORWARD AND AFT LIFT ACTUATORS TO WITHIN LIMITS AS PER DRAWING 52FX1435. ADJUSTED CLEARANCES BETWEEN MCD OUSDR 96FDEA00496Floor Beam · corrosion(NR 0626) CORROSION C53-224-01, BS 344 FLOOR BEAM FROM LBL 60 TO RBL 30 WL 208. CORRECTIVE ACTION: *** S/D*** REMOVED DAMAGED FLOOR BEAM, BS 344, LBL 1 - 60, WL 208 AND REPLACED WITH NEW IAW FEDEX STANDARD REPAIR DRAWING SRM 27-53-007.SDR 96FDEA00493Skin · corrosion(NR 0168) CORROSION (C53-111-02-(2)), NR 3 CARGO DOOR INNER SKIN HAS CORROSION AROUND A RIVNUT 12 INCHES FROM THE AFT, EDGE 10 INCHES FROM THE BOTTOM. ***S/D *** REMOVED CORROSION FROM NR 3 CARGO DOOR INNER SKIN AROUND RIVNUTS. FOUND TO BE OUT OF LIMITS SDR 96FDEA00503Skin · missing(NR 0751) CORROSION ON SKIN AROUND BLIND FASTENERS UNDER FAIRING STRUCTURE AT BS 720A + 10, 1 INCH BELOW STR 29/L. CORRECTIVE ACTION: ***S/D*** REPAIRED SKIN AROUND BLIND FASTENERS UNDER FAIRING STRUCTURE AT BS 710, 1 INCH BELOW STR 28L PER FEDEX SRM'S 53-SDR 96FDEA00501End Cap · corroded(NR 0748) FT AIRSTAIR FORWARD END CAP IS CORRODED BEYOND LIMITS, REQUIRES REPLACEMENT. CORRECTIVE ACTION: ***S/D*** REMOVED AND REPLACED AFT AIRSTAIR FORWARD END CAP PER FEDEX SRM 51-40-2.SDR 96FDEA00484Skin · lightning strikeSNRM (0709). LIGHTNING STRIKER AT BS 349 (BETWEEN STR 3 AND STR 4 LT). BS 360 (BETWEEN STR 3 AND STR 4 LT), BS 376, STR 3 LT, BS 374 LT, BS 439, STR 4 LT. *** S/D *** COMING.SDR 96FDEA00483Support · corrodedSNRM (0709). CORROSION (53-224-01 (3), (53-224-04) FLOOR BOARD SUPPORT B.S. 1068, LBL 25, WL 208. ORIGINAL THICKNESS, .091 INCH. REMAINING .072 INCH OUT OF LIMITS PER FEDEX SRM 53-10-1, FIG 1 DETAIL VI. *** S/D *** COMING.SDR 96FDEA00482Centering Block · gougedSNRM (0690). MAIN CARGO DOOR AFT CENTERING IS GOUGED. C/A REMOVED GOUGED MAIN CARGO DOOR AFT CENTERING BLOCK, INSTALLED ONE EACH NEW BLOCK IAW FEDEX 727 SRM 51-10-1.SDR 96FDEA00481Clip · crackedSNRM (0663). BS 700, STRINGER 7R IS CRACKED (CLIP). ***S/D** COMING.SDR 96FDEA00480Stringer Clip · corrodedSNRM 0663, BS 700 STRINGER CLIP NR 5 HAS CORROSION. *S/D* REMOVED STRINGER CLIP AT BS 700 STRINGER CLIP NR 5 LT, REPLACED WITH NEW CLIP PER SRM 51-30-2.SDR 96FDEA00479Clip · damagedSNRM (0649). BS 380, STRINGER 7L, STRINGER CLIP IS DAMAGED. ***S/D** COMING.SDR 96FDEA00477Skin · crackedSNRM (0270). NR 4 SLAT, 01B GUIDE HOOK CUT-OUT, CRACKED. C/A STOP DRILLED CRACK AND FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 57-30-4.SDR 96FDEA00476Window · heat damageFIRST OFFICER'S NR 4 WINDOW IS DAMAGED BEYOND LIMITS (HEAT DAMAGE). *****S/D **** REMOVED AND REPLACED THE F/O'S NR 4 WINDOW PER FEDEX MM 56-11-31.SDR 96FDEA00475Window · gougedSNRM (0141). F/O'S NR 3 WINDOW IS DAMAGED BEYOND LIMITS, GOUGED. *** S/D *** COMING.SDR 96FDEA00474Window · delaminatedSNRM (0139). CAPTAIN'S NR 5 WINDOW IS DAMAGED BEYOND LIMITS, DELAMINATED. *** S/D *** REMOVED DAMAGED NR 5 WINDOW AND REPLACED WITH NEW PER FEDEX MM 56-11-41. SEAL WILL BE APPLIED ON CARD NR NR0134. PERFORMED FUNCTIONAL TEST OF CAPT'S WINDOW IAW FEDEX MM SDR 96FDEA00473Window · heat damagedSNRM (0139). CAPTAIN'S NR 4 WINDOW MIDDLE PANE IS HEAT DAMAGED. *** S/D *** REMOVED AND REPLACED THE CAPT'S NR 4 WINDOW PER FEDEX MM 56-11-31.SDR 96FDEA00472Window · heat damagedSNRM (0133). FIRST OFFICER'S NR 5 WINDOW IS DAMAGED BEYOND LIMITS (HEAT DAMAGED). *** S/D *** REMOVED AND REPLACED THE F/O'S NR 5 WINDOW PER FEDEX MM 56-11-41.SDR 96FDEA00471Fairing · gougedSNRM (0509). GOUGE ON FAIRING 3340, 22 INCHES FROM BOTTOM AND 12 INCHES AFT OF PANEL. C/A REMOVED DAMAGED AREA 3 INCHES BY 5 INCHES, .040 INCH, AND REPAIRED PER FEDEX SRM 51-40-2.SDR 96FDEA00461Position Switch · out of adjustON DEPARTURE WHEN FLAPS RETRACTED TO 2 DEGREES, THE NR 2 LEADING EDGE DEVICE REMAINED EXTENDED. WHEN FLAPS WERE RETURNED TO 5 DEGREES THE LEADING EDGE DEVICES WERE NORMAL. C/A: FOUND NR 2 LEADING EDGE FLAP POSITION SWITCH OUT OF ADJUSTMENT. ADJUSTED NR 2 FSDR 96FDEA00462Web · crackedCRACK IN WEB AT BS 950A + 17, BL ZERO, WL 203.5. ****S/D***** AT BS 950A + 17, BL ZERO, WL 203.5, REMOVED DAMAGED AREA. FABRICATED REPAIR WEB AND INSTALLED PER FEDEX SRM 51-40-2.SDR 96FDEA00455Floor Beam · corrodedCORROSION ON FLOOR BEAM UPPER CHORD, BS 1030, LBL 9, RBL 10 AND 21, WL 208. *** S/D **** REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS ON FLOOR BEAM UPPER CHORD BS 1030, RBL 10, WL 203 PER FEDEX SRM 53-10-8, FIG 8. REMOVED .011 INCH OF ORIGINAL .12SDR 96FDEA00454Frame · damagedDOUBLE HOLE IN BS 760 FRAME BELOW STR 6L. *S/D* REMOVED DAMAGE, FABRICATED REPAIR PART AND INSTALLED AT BS 760 FRAME BELOW STR 6L PER SRM 53-10-4.SDR 96FDEA00453Floor Beam · gougedFLOOR BEAM AT BS 277, LBL 15, WL 208, IS GOUGED. **** S/D **** REMOVED DAMAGE, FAB AND INSTALLED REPAIR PARTS PER FEDEX SRM 51-40-4, FIG 1.SDR 96FEA00424Seat Track · corrodedCORROSION ALONG SEAT TRACK FLANGE AND AROUND FASTENERS IS OUT OF LIMITS BS 480 TO 680 LBL 45 WL 208. *S/D* REMOVED AND REPLACED SEAT TRACK AT BS 480 TO 680 LBL 45 WL 208 SRM 53-10-5.SDR 96FDEA00658Intercostal · corrodedINTERCOSTAL, WL 208, BS 256 - BS 277, LBL 14, IS CORRODED BEYOND LIMITS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 51-40-4, FIG 1.SDR 96FDEA00451Flap · corrodedNR 4 K-FLAP OUTBOARD LOWER BONDING JUMPER IS CORRODED AT UPPER ATTACH POINT. MATERIAL REMOVED DURING REWORK EXCEEDS LIMITS PER FEDEX SR 27-57-010, REV B. ****S/D*** COMING. C/A REMOVED CORRODED AREA AND REPAIRED OUTBOARD LOWER BONDING JUMPER ATTACH POINT
Back to Boeing 727-233