Boeing 727-264
Service difficulty reports · 617
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 = '727264' 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 = '727264' 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 DHL2008763518Seat Track · corrodedFOUND SEAT TRACK CORRODED AT BS 480-600, RBL 24. REMOVED, FABRICATED FROM BAC 1520-792, PO NR 9006020, 209" LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 1.SDR DHL2008763515Seat Track · corrodedSEAT TRACK DAMAGED BS 520 TO 540, LBL 45. REMOVED AND REPLACED SEAT TRACK SECTION WITH P/N 65-23637-53, PO NR 658565, 220 INCH LONG, PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 2.SDR DHL2008763526Seat Track · corrodedCABIN SEAT TRACK CORRODED AT BS 990 TO 1130, LBL 45.75. REMOVED, FABRICATED SEAT TRACK SECTION FROM BAC1520-792, 297.875" LONG, PO NR 9006020, AND INSTALLED PER B727 SRM 53-10-5 FIG 1, 53-10-1 FIG 7, AND 51-30-2.SDR DHL2008763508Rib · crackedPREVIOUS REPAIR ON L/WING O/B FORE FLAP UPPER SURFACE CHAFED, LWBL 400. REMOVED EXISTING REPAIR AND ASSOCIATED INTERNAL RIB. FABRICATED AND INSTALLED NEW REPAIR SKIN SECTION, 2024-T3 .050 INCH BY 14.125 INCH BY 5.875 INCH, PO NR 9005554; AND SPLICE, 2024-T3 SDR DHL2008763517Seat Track · corrodedSEAT TRACK CORRODED AT BS 1110-1130, LBL 24. REMOVED, FABRICATED FROM BAC 1520-792, PO NR 9006020, 297" LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 1 AT BS 958.5" TO BS 1139.SDR DHL2008763510Attach Angle · crackedR/WING L/E INTERIOR, CRACKED RIB ATTACH ANGLE AT RWS 125 (FRONT SPAR). FABRICATED AND INSTALLED REPAIR DOUBLER, 7075-T6 .050 INCH BY 10.5 INCH BY 2.5 INCH, PO NR 9006153, AND FILLER, 7075-T6 .040 INCH BY 3 INCH BY 2.5 INCH, PO NR 9006639, PER B727 SRM 51-40-3SDR DHL2008763512Support Angle · crackedRMLG BODY DOOR ACTUATOR HANGER SUPPORT ANGLE CRACKED AT BS 870. REMOVED, FABRICATED, AND INSTALLED SUPPORT ANGLE, 7075-T6 .100 INCH BY 3.75 INCH BY 3.375 INCH, PO NR 9005773, PER B727 SRM 53-10-2 51-20-1 AND 51-30-5.SDR DHL2008763516Seat Track · corrodedSEAT TRACK CORRODED AT BS 560-600, LBL 25. REMOVED, FABRICATED FROM BAC1520-792, PO NR 9006020, 209" LONG, AND REPLACED SEAT TRACK SECTION PER B727 SRM 53-10-1 FIG 7 AND 53-10-5 FIG 1.SDR DHL2008763514Seat Track · corrodedSEAT TRACK CORRODED BS 760 TO 850, RBL 25. REMOVED AND REPLACED SEAT TRACK SECTION WITH BAC1520-841 EXTRUSION, PO NR 810987, 95 INCH LONG, PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 2.SDR DHL2008763513Seat Track · corrodedSEAT TRACK CORRODED BS 760 TO 850, RBL 45. REMOVED AND REPLACED SEAT TRACK SECTION WITH BAC1520-841 EXTRUSION, PO NR 810987, 95 INCHES LONG, PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 2.SDR DHL2008763525Stringer Splice · corrodedAFT CARGO COMP AT BS 1010, STR 29R SPLICE CORRODED O/B SIDE. REMOVED, FABRICATED NEW SPLICE FROM BAC1498-131, 15" LONG, PO NR 9005686, AND INSTALLED PER B727 SRM 53-10-2 FIG 9, 53-10-3 FIG 1, AND 51-30-2.SDR DHL2008763522Frame · dentedFRAME DENTED AND GOUGED IN CARGO COMPT AT BS 660, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-30-2.SDR DHL2008763521Frame · dentedFRAME DENTED AND GOUGED IN CARGO COMPT AT BS 640, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-30-2.SDR DHL2008763520Frame · gougedFRAME GOUGED IN CARGO COMPT AT BS 600, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-30-2.SDR DHL2008763502Seat Track · corrodedSEAT TRACK CORRODED AT FLANGE, BS 850-870, LBL 45. REMOVED TRACK SECTION, FABRICATED SECTION FROM BAC 1520-1466, PO NR 730788, 15.75 INCHES LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7, 53-10-5 FIG 1 AND 51-30-2.SDR DHL2008763501Seat Track · corrodedSEAT TRACK CORRODED AT FLANGE, BS 850-870, LBL 24. REMOVED TRACK SECTION, FABRICATED SECTION FROM BAC1520-1466, PO NR 730788, 15.75 INCHES LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7, 53-10-5 FIG 1 AND 51-30-2.SDR DHL2008763500Seat Track · corrodedSEAT TRACK CORRODED AT BS 850-870, RBL 45. REMOVED TRACK SECTION, FABRICATED SECTION FROM BAC1520-1466, PO NR 730788, 15.75" LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7, 53-10-5 FIG 1 AND 51-30-2.SDR DHL2008763524Shear Tie · corrodedFRAME SHEAR TIE CORRODED AT BS 1130, BETWEEN STR 28R AND 29R, AFT SIDE. REMOVED, FABRICATED SHEAR TIE FROM 7075-T6, .050" BY 6" BY 2.5", PO NR 9006153, AND INSTALLED NEW SHEAR TIE PER B727 SRM 53-10-4 FIG 4, 53-10-2, AND 51-30-2.SDR DHL2008763519Frame · dentedFRAME DENTED IN CARGO COMPT AT BS 580, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-30-2.SDR DHL2008763507Frame · dentedFRAME GOUGED AND DENTED AT BS 560, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6, .063 INCHES BY 7.25 INCHES BY 3.25 INCHES, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1.SDR DHL2008763506Frame · dentedFRAME GOUGED AND DENTED AT BS 540, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6, .063 INCH BY 7.25 INCH BY 3.25 INCH, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1.SDR DHL2008763505Frame · dentedFRAME GOUGED AND DENTED AT BS 520, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6, .063 INCH BY 7.25 INCH BY 3.25 INCH, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1.SDR DHL2008763504Frame · dentedFRAME GOUGED AND DENTED AT BS 500 ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6, .063 INCH BY 7.25 INCH BY 3.25 INCH, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1.SDR DHL2008763503Frame · dentedFRAME GOUGED AND DENTED AT BS 480, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6, .063 INCHES BY 7.25 INCHES BY 3.25 INCHES, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1.SDR DHL2008765033Rib · crackedDURING C CHECK, NR 2 SLAT INBOARD ACTUATOR SUPPORT RIB CRACKED. REMOVED INNER SKIN PANEL FOR ACCESS IAW SRM 51-30-2. REMOVED DAMAGE INBOARD RIB IAW SRM 51-30-2. LOCATED AND DRILLED NEW RIB IAW SRM 51-30-5 AND 51-40-1. TREATED AND PRIMED HOLES AND AREA IAWSDR DHL2008765020Skin · dentedDURING C CHECK, 2 EACH PROTRUDING DENTS ON RIGHT HORIZONTAL STABILIZER UPPER SURFACE 3" INBOARD OF PCU PANEL. REWORKED TO ORIGINAL CONTOUR IAW SRM 51-40-1, 2 EACH DENTS. C/W HFEC IAW NDTM PT 6 51-00-00 FIG 23, CRACK INDICATION. REMOVED DAMAGED DRILLED HOLE SDR DHL2008765015Structure · crackedDURING C CHECK, LEFT INBOARD MID FLAP LOWER TRAILING EDGE WBL 102 AT PUSH-ROD IS CRACKED, INBOARD. REMOVED INBOARD MID FLAP LOWER SKIN AND NR 3 TEAR DROP FOR ACCESS IAW SRM 51-30-2. FABRICATED NEW SECTION DIMENSION 57.5" LONG IAW SRM 53-30-5 AND 57-50-2 FIG SDR DHL2008765010Frame · gougedDURING C CHECK, FUSELAGE FRAME GOUGED AT BS 480 BELOW STRINGER 17L. BLENDED AREA AT BS 480 BELOW STRINGER 17L, ORIGINAL MATERIAL 0.150", MATERIAL REMAINING WAS APPROXIMATE 40% OF THICKNESS LEAVING 60% FOUND TO BE WITHIN LIMITS IAW EO NR OE-N765AT-1-25-08. TRSDR DHL2008765009Frame · damagedDURING C CHECK, 2 MISDRILLED HOLES IN FUSELAGE FRAME STRINGER 18L BS 480. REMOVED AND REINSTALLED HINGE ASSEMBLY AT FRAME, STRINGER 18 BS 480 IAW STC DRAWING 727021025-1, DRILLED THROUGH THE TWO HOLES AND INSTALLED MS20426AD6-6 RIVET FLUSH IAW DRAWING NR 7270SDR DHL2008765001Skin · misrepairedDURING C CHECK, EXISTING REPAIR HAS BLIND RIVETS INSTALLED IN DOUBLER SHOULD BE SOLID FASTENERS PER SRM AT BS 1185 STRINGER 17L. REMOVED EXISTING REPAIR IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER IAW SRM 53-30-3 FIG 26 AND 53-30-2 FIG 3. ZERO TIMING OF SDR DHL2008765024Skin · crackedDURING C CHECK, NR 4 SLAT UPPER SKIN CRACKED AT INBOARD HOOK MOUNT SCREW WS 390. STRIPPED AREA IAW B727 MM 51-20-1, C/S HFEC IAW B727 NDTM PT6 51-00-00 FIG 23. CRACKS TERMINATE IN STOP DRILL HOLES. FABRICATED REPAIR PLATE MATERIAL USED 7075-T6 0.125" PO NR SDR DHL2008765022Beam · damagedDURING C CHECK, REJECTED NR 105146 BECAUSE ORIGINAL FABRICATED 'J' BEAM WAS DAMAGED UPON INSTALLATION. RT WING TRAILING EDGE UPPER 'J' BEAM IS CRACKED AT WBL 118. REMOVED TRAILING EDGE PANEL FOR ACCESS AT RT WING IAW SRM 51-30-2. REMOVED 'J' BEAM AT RT SIDESDR DHL2008765016Beam · crackedDURING C CHECK, LT WING UPPER TRAILING EDGE PANEL SUPPORT 'J' BEAM WBL 124 IS CRACKED IN CUT OUT FORWARD OF NR 7 SPOILER ACTUATOR. REMOVED TRAILING EDGE UPPER PANEL FROM LT WING FOR ACCESS IAW SRM 51-30-2. REMOVED CRACKED 'J' BEAM IAW SRM 51-30-2. FABRICATESDR DHL2008765034Bulkhead · corrodedDURING C CHECK, BS 227.8 BULKHEAD FORWARD LOWER WEB AND STIFFENER IS CORRODED. REMOVED STIFFENERS AND ATTACHED PARTS IN AREA FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGED SECTION IAW SRM 51-40-4 FIG 1 AND 53-10-2 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-SDR DHL2008765014Structure · crackedDURING C CHECK: DISCREPANCY - RIGHT WING INBOARD FLAP, MID FLAP AFT IS CRACKED ON BOTH INBOARD AND OUTBOARD SIDE WBL 90.69 AND WBL 104.0. REMOVED NR 5 AND 6 TEAR DROP FAIRINGS AND RIGHT INBOARD MID FLAP LOWER SKIN TO GAIN ACCESS IAW SRM 51-30-2. REMOVED CRACSDR DHL2008765012Stringer · corrodedDURING C CHECK: DISCREPANCY - RT WHEEL WELL STRINGER 18A IS CORRODED AT WBL 70 ON FORWARD SIDE OF BS 880. REMOVED STRINGER 18A IAW SRM 51-30-2. FABRICATED STRINGER 18A IAW SRM 53-10-2 FIG 4, 51-10-3 AND 51-30-5. TREATED AND PRIMED PART AND AREA IAW SRM 51-1SDR DHL2008765011Support · crackedDURING C CHECK, RIGHT WHEEL WELL SUPPORT STRUCTURE HAS CRACK AT BS 880 RBL 26. REMOVED SUPPORT STRUCTURE AT RIGHT WHEEL WELL BS 880 RBL 26 IAW SRM 51-30-2. FABRICATED NEW SUPPORT STRUCTURE AT RIGHT WHEEL WELL BS 880 RBL 26 IAW SRM 53-10-2 FIG 4 AND 51-10-3. SDR DHL2008765003Torque Box · crackedDURING C CHECK, AFT STAIRWELL LIGHTENING HOLE CRACKED 5 O'CLOCK POSITION RIGHT SIDE BS 1265 (TORQUE BOX). CUT OUT DAMAGED AREA AT AFT STAIRWELL LIGHTENING HOLE DIMENSION 1" BY .75" IAW SRM 51-40-2 FIG 1. FABRICATED DOUBLER REPAIR IAW SRM 53-10-2 FIG 6 AND 51SDR DHL2008765021Hinge · crackedDURING C CHECK, MCD AFT HINGE SECTION IS CRACKED AT BS 612 STRINGER 4L. REMOVED AFT HINGE SECTION AT MAIN CARGO DOOR BS 612 STRINGER 4L IAW MM FIG 5201B REV E. FABRICATED HINGE SECTION IAW MM FIG 5201B REV E. TREATED AND PRIMED PARTS AND AREA IAW SRM 51-10SDR DHL2008765032Rib · crackedDURING C CHECK, NR 2 SLAT OUTBOARD ACTUATOR SUPPORT RIB CRACKED. REMOVED ACCESS PANEL AT NR 2 SLAT IAW SRM 51-30-2. LOCATED AND DRILLED HOLES ON NEW RIB IAW SRM 51-30-5. INSTALLED NEW RIB AT NR 2 SLAT OUTBOARD ACTUATOR IAW SRM 51-30-2. INSTALLED ACCESS PANSDR DHL2008765030Rib · crackedDURING C CHECK, CRACK INDICATION ON NR 4 SLAT OUTBOARD ACTUATOR SUPPORT RIB. REMOVED ACCESS PANEL AT NR 4 SLAT IAW SRM 51-30-2. LOCATED AND DRILLED HOLES ON NEW RIB IAW SRM 51-30-5. INSTALLED NEW RIB AT NR 4 SLAT OUTBOARD ACTUATOR IAW SRM 51-30-2. INSTALLESDR DHL2008765025Skin · crackedDURING C CHECK, CRACKED ON NR 3 SLAT UPPER SURFACE AT INBOARD SLAT HOOK MOUNT SCREW WS 520. REMOVED HOOK FROM AREA IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-3 FIG 10. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR AT NR 3 SDR DHL2008765005Torque Box · crackedDURING C CHECK, AFT STAIRWELL LIGHTENING HOLE CRACKED 6 O'CLOCK POSITION RIGHT SIDE BS 1240 (TORQUE BOX). CUT OUT DAMAGED AREA AT AFT STAIRWELL LIGHTENING HOLES 6 O'CLOCK POSITION BS 1240 RT IAW SRM 51-40-2 FIG 1, DIMENSION 1.25" BY .5". FABRICATED DOUBLER RSDR DHL2008765004Torque Box · crackedDURING C CHECK, AFT STAIRWELL LIGHTENING HOLE CRACKED 12 O'CLOCK POSITION RIGHT SIDE OF STAIRWELL BS 1243 (TORQUE BOX). CUT OUT DAMAGED AREA AT AFT STAIRWELL LIGHTENING HOLE BS 1243 RIGHT DIMENSION 1.5" BY .5" IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR AT AFT SDR DHL2008765002Web · crackedDURING C CHECK, CUT OUT DAMAGED AREA AFT STAIRWELL LIGHTENING HOLE 10 O'CLOCK POSITION DIMENSION CUT OUT 1.5" BY .75" IAW SRM 51-40-2 FIG 1. FABRICATED DOUBLER REPAIR AT AFT STAIRWELL LIGHTNING HOLES 10 O'CLOCK POSITION IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1SDR DHL2008765006Cover · gougedDURING C CHECK, RT INBOARD AILERON UPPER INBOARD HINGE COVER HAS DEEP GOUGE. REMOVED COVER IAW SRM 51-30-2. FABRICATED NEW COVER IAW SRM 57-50-2 FIGURE 7 AND 51-20-1. TREATED AND PRIMED NEW COVER IAW SRM 51-10-2. INSTALLED NEW COVER AT RT WING INBOARD AILSDR DHL2008765031Rib · crackedDURING C CHECK, CRACK INDICATION ON PREVIOUS REPAIR OF NR 3 SLAT OUTBOARD ACTUATOR SUPPORT RIB. REMOVED NR 3 SLAT ACCESS PANEL IAW SRM 51-30-2. REMOVED CRACKED RIB IAW SRM 51-30-2. LOCATED AND DRILLED NEW RIB IAW SRM 51-30-5. INSTALLED NEW RIB IAW SRM 51-3SDR DHL2008765018Structure · gougedDURING C CHECK, RIGHT WING NR 6 SLAT TRAILING EDGE GOUGED AT HOOK FITTINGS WS 150 APPROXIMATE. REMOVED HOOK FITTING FROM ACCESS IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-3 FIGURE 10. TREATED AND PRIMED DOUBLER AND AREA IAW SRM 51-10-2. INSTASDR DHL2008765017Skin · crackedDURING C CHECK, RT WING NR 4 LEADING EDGE FLAP INNER SKIN CRACKED 3 PLACES AROUND RIVETS AT INBOARD IND WS 150. STOP DRILLED 3 EACH CRACKED PLACES AROUND RIVETS AT INBOARD END WS 150 (DIAMETER 0.190") IAW SRM 51-10-1 AND 57-50-3 FIGURE 12. HFEC C/W AROUND STSDR DHL2008765026Skin · crackedDURING C CHECK, NR 2 SPOILER NR 2 HINGE CUT OUT ON LT WING TRAILING EDGE CRACKED. REMOVED ON LT WING TRAILING EDGE SKIN SECTION AT NR 2 SPOILER DIMENSION 36" BY 2.5" IAW SRM 51-30-2. FABRICATED NEW SKIN SECTION IAW SRM 57-30-2 FIG 4 AND 51-20-1. TREATED AND
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