Boeing 727-223
Service difficulty reports · 5,313
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 = '727223' 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 = '727223' 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 DHL2008753509Attach Angle · cracked"C" CHECK 1 ENG PYLON OB UPPER ATTACH ANGLE CRACKED AT SECOND HOLE, VERIFIED BY NDT. REMOVED DAMAGED ANGLE AT NR 1 ENGINE (PYLON) OB UPPER IAW B727 SRM 51-30-2. LOCATED HOLE, DRILLED AND DEBURRED ANGLE WITH P/N 69-16977-1 PO NR 738094 IAW B727 SRM 51-30-5 ANSDR DHL2008753508Beam · damaged"C" CHECK, LT WING UPPER T/E PANEL SUPPORT "J" BEAM WBL 124 HAS DOUBLER REPAIR. REMOVED "J" BEAM IAW B727 SRM 51-30-2. FABRICATED NEW "J" BEAM PER DRAWING 65-21655 REV J AND EC-00829-001 FROM BAC1506-860 7075T6 DIM.81" PO NR 738052. TREATED AND PRIMED IAW BSDR DHL2008753501Structure · crackedDURING "C" RT I/B MID FLAP LOWER T/E CHORD AT CUTOUT WBL 102 IS CRACKED. OPENED SECTION OF LOWER PANEL RT I/B MID FLAP T/E IAW SRM 51-30-2. REMOVED SEAL AND SEL RETAINER FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGE AREA AT CHORD APPROX 70 INCH. FAB NEW CHORD SDR DHL2008753502Support · crackedDURING "C" RT WING UPPER T/E WBL 124 "J" BEAM PANEL SUPPORT IS CRACKED FWD OF SPOILER ACTUATOR. REMOVED "J" BEAM IAW B727 SRM 51-30-2. FABRICATED NEW "J" BEAM PER DRAWING 65-21655 REV J AND EC-00829-001 FROM BAC1506-860 7075T6 DIM.81" PO NR 738738052. TREATSDR DHL2008752511Skin · crackedNR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1.SDR DHL2008753506Skin · cracked"C" CHECK LT WING L/E CRACKED AT NR 4 SLAT O/B TRACK CUTOUT. REMOVED PAINT LT WING L/E NR 4 SLAT O/B TRACK IAW MM 51-20-1. STOP DRILLED WITH .250 AT THE END OF THE CRACK IAW SRM 51-10-1. FAB DOUBLER REPAIR IAW SRM 57-30-4 FIG 11 AND SRM 51-20-1 FIG 7. TREASDR DHL2008752609Skin · crackedNR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1.SDR DHL2008753504Intercostal · corrodedDURING "C" CHECK FWD E/E COMPT BS 227.8 CORROSION ON WEB AND ANGLE BBL "0". REMOVED INTERCOSTAL DAMAGE, STIFFENER AND ANGLE FOR ACCESS IAW SRM 51-30-2. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. CUTOUT DAMAGED AREA APPROX 11 INCHES. FAB SDR DHL2008752509Flap · delaminatedRT INBD MIDFLAP HAS DELAM AT LOWER OUTBD TRAILING EDGE (AT WBL 238.0). CUT OUT DELAMINATED AREA ON RT I/B MIDFLAP APPROX 1.5 INCH DIAMETER APPLIED POTTING COMPOUND AND CURED AND SANDED SMOOTH. FABRICATED DOUBLER APPROX 3.5 DIAMETER FROM 7075T6 .020 PO NR 728SDR DHL2008752508Rib · crackedNR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW B727SRM 51-30-2 LOCATED, DRILLED
AND DEBURRED RIB P/N 65-17327U3 PO 7375239 IAW B727 SRM 51-30-5. FABRICATED CHANNEL USING 2024-T3 .071 PO 9005922 DIM 6.5 INSDR DHL2008752606Attach Fitting · crackedNR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW B727 SRM 51-30-2. LOCATED, DRILLED AND DEBURRED RIB P/N 65-17327U3 PO 7375239 IAW B727 SRM 51-30-5. FABRICATED CHANNEL USING 2024-T3 .071 PO 9005922 DIM 6.5SDR DHL2008752607Attach Fitting · crackedNR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW SRM 51-30-2. LOCATED, DRILLED AND DEBURRED RIB IAW SRM 51-30-5. FABRICATED CHANNEL IAW BDW NR 65-17327 AND SRM 51-20-01, 51-20-2, 51-30-5. INSTALLED RIB ANSDR DHL2008752506Frame · dentedAFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4 INCH BY 1/2 INCH IAW B727SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9" BY 4" IAW B727SDR DHL2008752512Angle · crackedRT WING I/B L/E AREA AT FSS 107.2 FWD WING SPAR TERMINAL JOINT ANGLE CRACK AT BOTTOM. STOP DRILLED CRACK DIM .250 IAW B727 SRM 51-10-1 HFEC VERIFIED THAT CRACK END ON STOP DRILL HOLE IAW B727 NDTM PT6 51-00-00 FIG 23. FABRICATED NEW ANGLE USING 7075-T6 .063 SDR DHL2008752505Frame · dentedAFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4 INCH BY 1/2 INCH IAW B727SRM 51-40-3 FIG1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9 INCH BY 4 INCH ISDR DHL2008752610Spar · crackedRT WING INBOARD L/E AREA AT FSS 107.2 FWD WING SPAR TERMINAL JOINT ANGLE CRACK AT BOTTOM. STOP DRILLED CRACK DIM .250 IAW B727 SRM 51-10-1. HFEC VERIFIED THAT CRACK END ON STOP DRILL HOLE IAW B727 NDTM PT6 51-00-00 FIG 23. FABRICATED NEW ANGLE USING 7075-T6SDR DHL2008752603Frame · dentedAFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4" BY 1/2" IAW B727 SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9 INCH BY 4 INCHES IAW BSDR DHL2008752604Frame · dentedAFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4" BY 1/2" IAW B727 SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9" BY 4" IAW B727 SRM 51SDR DHL2008749019Angle · corrodedDURING C CHECK, EXFOLIATION NOTED AT C2 DOOR CUT OUT, BS 990 (FRAME) BETWEEN STRINGERS 26R AND 27R. REMOVED CORROSION AT C2 DOOR CUT OUT BS 990 IAW SRM 51-10-6, ORIGINAL THICKNESS 0.100, MATERIAL LOSS 0.35, MATERIAL REMAINING 0.65, FOUND OUT OF LIMITS IAW SRMSDR DHL2008752510Skin · delaminatedLT OB AILERON TAB UPPER SURFACE HAS DELAMINATED AREA. CUTOUT DELAMINATED AREA 2 INCHES DIA ON LT O/B AIL TAB UPPER SURFACE. FABRICATED FILLER AND DOUBLER IAW B727SRM 57-50-2, BONDED FILLER AND DOUBLER IAW B727SRM 51-40-20.SDR DHL2008752507Structure · crackedLT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IS CRACKED FWD. REMOVED FASTENERS AT LT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IAW B727SRM 51-30-2. STOP DRILLED 0.250" DIA AT END OF CRACK IAW B727 SRM 57-30-4 FIG 1SDR DHL2008752608Skin · delaminatedLT OB AILERON TAB UPPER SURFACE HAS DELAMINATED AREA. CUTOUT DELAMINATED AREA 2 INCHES DIA ON LT O/B AILERON. TAB UPPER SURFACE FABRICATED FILLER AND DOUBLER IAW B727 SRM 57-50-2, BONDED FILLER AND DOUBLER IAW B727SRM 51-40-20.SDR DHL2008752605Skin · crackedLT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IS CRACKED FWD. REMOVED FASTENERS AT LT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IAW B727 SRM 51-30-2. STOP DRILLED 0.250" DIA AT END OF CRACK IAW B727 SRM 57-30-4 FIG SDR DHL2008752601Web · crackedLT SIDE OF AIRSTAIR WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA AT LT SIDE OF AIRSTAIR WEB SAT 1223 IAW B727 SRM 51-40-2 FIG1. FABRICATED DOUBLER MAT USED 7075T6 0.032 DIMENSION 2.5" BY 2.5" PO NR 9006457 IAW B727 SRM 51-40-2 FIG 1 AND B727 SRMSDR DHL2008752502Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024TSDR DHL2008752504Web · crackedLT SIDE OF AIRSTAIR WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA AT LT SIDE OF AIRSTAIR WEB SAT 1223 IAW SRM 51-40-2 FIG 1. FABRICATED DOUBLER MAT USED 7075T6 0.032 DIMENSION 2.5 INCH BY 2.5 INCH PO NR 9006457 IAW SRM 51-40-2 FIG 1 AND SRM 53-10SDR DHL2008752503Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT NR 5 L/E SLAT MATERIAL USED SDR DHL2008752501Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024TSDR DHL2008752570Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL SDR DHL2008752550Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL SDR DHL2008752500Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL SDR DHL2008749013Stringer · crackedAFT PIT STRINGER 29R CRACKED AT SPLICE AFT OF BS 950. REMOVED AFT PIT STRINGER 29R, LOCATED AND DRILLED NEW STRINGER 29L P/N 65-52441-8 PO NR 7370104. INSTALLED NEW STRINGER 29L FROM BS 950 TO BS 1010 IAW B-727 SB 727-53-0179.SDR DHL2008752602Web · crackedLT SIDE OF AIRSTAIR WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA AT LT SIDE OF AIRSTAIR WEB STA 1223 IAW SRM 51-40-2 FIG1. FABRICATED DOUBLER IAW SRM 51-40-2 FIG1 AND SRM 53-10-2 FIG 6. TREATED AND PRIMED AREA IAW SRM 51-10-2. INSTALLED DOUBLESDR DHL2008752600Slat · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024TSDR DHL2008752515Beam · crackedRT WING T/E UPPER "J" BEAM IS CRACKED AT WBL 118. ACCOMPLISHED REPAIR TO CRACKED RT WING T/E UPPER "J" BEAM WBL 118. REPLACED MATERIAL USED J BEAM P/N BAC1506-860 7075T6 DIM 80.625" IAW EC-00795-001, DWG NR 65-21655 REV J DATED 12/4/78, B727 SRM 51-30-2.SDR DHL2008752513Angle · crackedCRACK AT RT MLG WHEEL WELL STATION 870 FWD INBD LWR BULKHEAD 18: LEFT OF LOAD CONTROL VALVE 8 INCHES RIGHT OF CENTER. REMOVED AND REPLACED ANGLE AT RT MLG W/W STA 870 FWD I/B LOWER BULKHEAD IAW
B727SRM 51-30-2.SDR DHL2008752611Angle · crackedCRACK AT RT MLG WHEEL WELL STATION 870 FWD INBD LWR BULKHEAD 18: LEFT OF LOAD CONTROL VALVE 8" RIGHT OF CENTER. REMOVED AND REPLACED ANGLE AT RT MLG W/W STA 870 FWD INBOARD LOWER BULKHEAD IAW B727 SRM 51-30-2.SDR DHL2008780002Flap · cracked1 INCH CRACK ON I/B LOWER SIDE OF NR 3 K FLAP JUST ABOVE BULL NOSE.SDR DHL2008780001Flap · delaminatedLT WING I/B FORE FLAP DELAMINATED BEHIND I/B FLAP TRACK AREA 7 INCH BY 3 INCH.SDR DHL2008749009Angle · crackedRIGHT ELEVATOR LOWER SKIN INTERIOR SUPPORT ANGLE IS CRACKED ELEVATOR STATION 20 VIEW THROUGH ACCESS 9405. REMOVED ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 51-20-1, 51-20-2, 51-30-5, 55-20-2 FIGURE 7. ALODINE AND PRIMED ANGLE IAW SRM 51-10-2. INSSDR DHL2008749008Attach Fitting · crackedRT WING NR 5 SLAT ACTUATOR ATTACH FITTING CRACKED AT INBOARD SIDE, INSIDE LEADING EDGE STRUCTURE. FABRICATED NEW RIBS (2 EACH) IAW SRM 57-50-2 FIGURE 2, 51-20-1 FIGURE 1 AND SRM 51-20-1 FIGURE 2. IAW ER 2-37163-801 REV A. INSTALLED NEW RIBS AT NR 5 SLAT ISDR DU4R2008191Skin · corrodedS/O 304002 N/R NR26444 CORROSION FWD CARGO BILGE AREA BS 660 S-28L - S-28R. REPAIRED BY CUTTING OUT CORRODED AREA BS 661 TO BS 664.5, NDT VERIFIED NO CRACKS IAW NPTM PT. 6 51-00-00 FIG. 23. FABRICATED AND INSTALLED REPAIR DOUBLER 11.6 INCH X 16.25 INCH FROM 2SDR DHL2008749018Angle · corrodedDURING C CHECK, EXFOLIATION AT FASTENER ON "L" ANGLE ON UPPER SURFACE OF LONGITUDINAL FRAME, BS 919 RWBL 70.5. FABRICATED NEW "L" ANGLE IAW SRM 51-30-5, 51-10-3 AND 53-10-2 FIG 4. INSTALLED IAW SRM 51-30-2. NR 033718SDR DHL2008749007Seat Track · corrodedMAIN CABIN SEAT TRACK CORRODED FROM BS 500 TO 520 LBL25. FABRICATED NEW SEAT TRACK SECTION FROM P/N BAC 1520-792 7178-T6 PO NR 9006152 APPROXIMATE LENGTH 210" IAW B-727 SRM 53-10-5 FIGURE 1 AND SRM 53-10-2 FIGURE 7. INSTALLED NEW SEAT TRACK SECTION USING PRESDR DHL2008749006Seat Track · corrodedSEAT TRACK CORRODED IN MAIN CARGO COMPARTMENT BS 480 - 620 LBL 45. FABRICATED NEW SEAT TRACK IAW SRM 53-10-2 FIGURE 7 AND SRM 53-10-5 FIGURE 1. INSTALLED NEW SEAT TRACK IAW SRM 53-10-5 FIGURE 1 USING PREVIOUS GOOD CONDITION SPLICE PARTS.SDR 08FDEA00132Connector · burnedAT ROTATION OFF FLAG IN CAPT'S ALTIMETER AND ALT SELECT WINDOW APPEARED. FOUND RACK CONNECTOR D609 CENTER SECTION, BEHIND NR 1 CADC BLACK FROM ELECTRICAL DAMAGE. INSTALLED WIRE NUMBERS W0007-162-22 AND W0007-9069-2 2 IN D609A PIN 12 PER BOEING HOOK UP LIST.SDR DHL2008749005Angle · crackedC-1 DOOR FORWARD FRAME REINFORCEMENT 3RD ANGLE CRACKED BS 500. REMOVED ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 51-20-2, 51-30-5 AND 52-30-1 FIGURE 4. ALODINE AND PRIMED ANGLE IAW SRM 51-10-2. INSTALLED ANGLE IAW SRM 51-30-2 AND 51-40-3 FIGURE 1SDR DHL2008749004Shear Tie · corrodedFORWARD CARGO COMPARTMENT SHEAR TIE CORRODED AT FORWARD SIDE OF BS 680 FRAME AND STRINGER 26R. REMOVED CORRODED SHEAR TIE IAW SRM 51-30-2. CLEANED AREA AROUND SHEAR TIE IAW SOPM 20-30-3. NO DEFECTS NOTED IAW SRM 51-10-6 PARA 3. FABRICATED NEW SHEAR TIE IAWSDR DHL2008749003Shear Tie · corrodedFORWARD CARGO COMPARTMENT SHEAR TIE AND FRAME CORRODED AT FORWARD SIDE OF BS 720F STRINGER 25L. REMOVED SHEAR TIE IAW SRM 51-30-2. CLEANED SKIN AREA IAW MM 12-40-00, NO CORROSION NOTED. FABRICATED NEW SHEAR TIE IAW SRM 53-10-2 FIGURE 3, 51-20-2 AND 53-10-4 SDR DHL2008749002Stringer Clip · corrodedFORWARD CARGO COMPARTMENT STRINGER CLIP CORRODED AT STRINGER 26L BS 740. REMOVED STRINGER CLIP IAW SRM 51-30-2. CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIGURE 1. CLEANED LOWER AREA IAW MM 12-40-00 NO CORROSION NOTED. FABRICATED NEW PART IAW SRM 53-10-2 FI
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