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 DHL2006763001Accessory Unit · malfunctionedRAISED GEAR, L GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED AB PROC, L & R GEAR UNSAFE LIGHT & DOOR LIGHT ILLUMINATED. RII REQUIRED. REPLACED LANDING GEAR ACCESSORY UNIT AND OPS CHECK GOOD IAW 727 MM 32-09-121.SDR DHL2006764001Light · looseEMERGENCY EXIT LIGHT IN COCKPIT LOOSE AND REMAINS ILLUMINATED IN FLIGHT. RESECURED COCKPIT EMERGENCY EXIT LIGHT PACK. OPS CHECK GOOD IAW MM 33-50-71.SDR DHL2006764517Tab · dentedDENT ON R/WING OB AILERON TAB UPPER SURFACE. CUT OUT DENTED AREA ON RT OB AILERON TAB APPROX 1 INCH DIA FABRICATED FILLER APPROX 1 INCH DIA AND DOUBLER APPROX 3.7500 INCHES X 4 INCHES FROM 2024-T3 .010 PO NR 9912184CLEANED, PREPPED PRIMED, BONDED CLEANED TREATSDR DHL2006764516Skin · dentedNR 016062 LT WING IB AILERON UPPER SKIN HAS NUMEROUS DENTS. REMOVED AND REINSTALLED LH IB AILERON AND TAB IAW MM 27-10-01 AND MM 27-10-11. FABRICATED NEW SKIN USING MAT 2024T3 .040 PO NR 9003189 DIM 41 .2500 X 22.2500 INCH IAW SRM 57-50-2 FIG7 AND SRM 51-30-5SDR DHL2006764519Stiffener · crackedLT WING FRONT SPAR VERTICAL STIFFENER AT WS 90 SHOWS CRACK FROM BOTTOM END. REMOVED FASTENERS FOR ACCESS IAW SRM 51-30-2 HFEC AT ANGLE MARKED END OF CRACK NDT MAN PART6 51-00-00 FIG23 STOP DRILLED .250 END OF CRACK IAW SRM51-10-1 FAB REPAIR MAT USED 7075 T6 .SDR DHL2006765001Accessory Unit · warning lightRT MAIN (RED) GEAR LIGHT ILLUMINATED IN FLIGHT. EXTINGUISHED AFTER GEAR EXTENSION. COULD NOT DUPLICATE. REPLACED RT GEAR RED KORRY LIGHT ASSY. REPLACED LANDING GEAR ACCY UNIT IAW MM 32-09-21. JACKED A/C AND SWUNG GEAR. OPS NORMAL AT THIS TIME.SDR DHL2006764506Attach Fitting · crackedL/WING INSIDE NR 4 SLAT LE ACTUATOR ATTACH POINT FOUND CRACK ON INNER SKIN AT WS 410. CUTOUT AREA AT L/WING INSIDE NR 4 SLAT LE ON INNER SKIN AT WS 410 DIM 10.5"X 5.250" IAW B727 SRM 57-30-4 FIG 3. FABRICATED FILLER MAT USED 2024T3 .040 PO# 9002787 AND DIM. SDR DHL2006764515Rib · crackedREF ASTAR N/R 015815 DISCREPANCY: NR 6 SLAT OB ACT ROD END MOUNT RIB CRACKED REMOVED AND REPLACED RIB NR 6 SLAT OB ACT ROD END MOUNT PO NR 619549 P/N 65-17294-14 IAW B727 SRM 51-30-2.SDR DHL2006764512Attach Bracket · crackedLT WING INSIDE NR 4 SLAT LE ACTUATOR ATTACHED POINT IB AND OB RIB CRACKED. REMOVED RIBS AT LT WING NR 4 SLAT IB AND OB ACTUATOR ATTACHED POINT AND 1 CHANNEL IAW B727 SRM 51-30-5. TREATED AND PRIMED HOLES AND AREA IAW B727 SRM 51-10-2. INSTALED RIBS P/N 65-1SDR DHL2006764510Angle · crackedLEFT WING LE WBL117.0 CHORD ANGLE CRACKED TO FWD END. REMOVED CHORD ANGLE AT LEFT WING LE WS117 IAW B727 SRM 51-30-2. FABRICATED NEW ANGLE MATERIAL USED 7075T6 .063 PO# 9003002 DIM. 46"X 2" IAW B727 SRM 57-20-2 FIG 1 AND MAT SUBSTUITION 51-20-1 FIG 2. LOCATSDR DHL2006764509Support Angle · crackedLEFT WING LE WBL117.0 LWR PANEL SUPPORT ANGLE SHOW CRACK BETWEEN FASTENER HOLES. NDT CONFIRM. REMOVED SUPPORT ANGLE AT LEFT WING LE WBL 117 LWR PANEL IAW B727 SRM 51-30-2. FABRICATED NEW ANGLE SUPPORT MATERIAL USED 7075T6 .050 PO# 9002787 DIM 18"X 1 3/4" IASDR DHL2006764518Panel · delaminatedNR 5 SPOILER UPPER TE CORNER IB SURFACE DELAMINATED CUT OUT DELAM AREA APPROX 13.2500 INCHES X 4.2500 INCHES AND VACUUM BAGGED FOR MOISTURE REMOVAL SRM 51-40-20 FABED REPAIR SKIN APPROX 13.2500 INCHES X 4.25 INCHES AND DOUBLER APPROX 16.2500 INCHES X 5.7500 INSDR DHL2006764511Skin · dentedLT HORIZ STAB UPPER SURFACE AT STAB STA 170 DENTED. MEASURED DENT AT LT HORIZ STAB UPPER SURFACE STA 170 IAW B727 SRM 55-10-1 FIG 1. FOUND WITHIN LIMITS A=.500 Y=.012 A/Y=41. NDT HFEC SHOWS SKIN CRACK PER MANUAL PT6 51-00-00 FIG 4. REMOVED DAMAGED AREA IAWSDR DHL2006764513Skin · dentedL/S UPPER RUDDER T/E DENTED (RED DOT). REMOVED AT L/S UPPER TRL ANGLE AS REQ IAW B727 SRM 51-30-2. FAB`D NEW RUDDER TRL ANGLE MAT USED 2024T3 .032 PO NR 53081 DIM 54 1/2" BY 7" IAW B727 SRM 55-40-2 FIG 2 AND 51-30-5. TREATED AND PRIMED AREA AND PART IAW B7SDR DHL2006764500Skin · chafedLT FUSELAGE EXTERIOR SKIN CHAFED AT STA 720E STR 20L, MARKED. REMOVED FASTENERS FOR ACCESS AT LT FUSELAGE STA 720E STR 20L IAW B727 SRM 51-30-2, CUT OUT DAMAGE AREA DIM 2.5" X 2.25" IAW B727 SRM 53-30-3 FIG 14. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .080 SDR DHL2006764503Skin · crackedLT WING NR 4 SLAT OB GUIDE CUTOUT ON FIXED LE, CRACKED AT OB AFT CORNER, MARKED. REMOVED FASTENERS FOR ACCESS AT LT WING NR 4 SLAT OB GUIDE CUTOUT IAW B727 SRM 51-30-2. STOP DRILLED CRACK .250 TERMINATED AT END OF CRACK IAW B727 SRM 51-10-1. NDT INSPECTED ASDR DHL2006764501Skin · crackedLT WING FIXED LE CRACKED AT NR 4 SLAT OB TRACK CUTOUT, MARKED. REMOVED FASTENERS FOR ACCESS AT LT WING FIXED LE AT NR 4 SLAT OB TRACK CUTOUT IAW B727 SRM 51-30-2. STOP DRILLED CRACK .250 TERMINATED AT END OF CRACK IAW B727 SRM 51-10-1, NDT ACCOMPLISHED 727 HSDR DHL2006764504Structure · crackedLT WING FIXED LE UPPER SURFACE CRACKED AT NR 3 SLAT OB GUIDE (HOOK) CUTOUT AFT OB CORNER, MARKED. REMOVED FASTENERS FOR ACCESS IAW B727 SRM 51-30-2. STOP DRILLED CRACK IAW B727 SRM 51-10-1, NDT INSPECTED PER 727 PT6 51-00-00 FIG 23 CRACK ENDS IN STOP HOLE. SDR DHL2006764508Rib · crackedLT WING INSIDE NR 2 SLAT LE ACTUATOR POINT IB AND OB RIBS HAVE EVIDENCE OF CRACKS, MARKED. HFEC INSP PER 727 PT6 51-00-00 FIG 23 CONFIRMED BOTH RIBS CRACKED. REMOVED AND REPLACED RIB ASSY OB P/N 65-17310-4 PO# 619582 AND IB P/N 65-17310-4 PO# 619577 ON LH WISDR DHL2006764507Rib · crackedLT WING INSIDE NR 3 SLAT LE ACTUATOR ATTACH POINT RIB CRACKED, MARKED. REMOVED AND REPLACED INBOARD AND OUTBOARD ATTACH POINT ACTUATOR AT LT WING NR 3 SLAT LE PO NR 6195105 P/N 65-17294-14 AND PO NR 619578 P/N 65-17294-13 IAW B727 SRM 51-30-2.SDR DHL2006764505Stiffener · crackedLWR END OF VERTICAL STIFFENER CRACKED ON RT WING FIXED LE WSTA125. STOP DRILLED CRACK PER B727 SRM 51-10-1, HFEC STOP DRLL IAW B727 NDT MAN PT 6 51-00-00 FIG 23. FAB`D DOUBLER FROM 7075T6 .063 PO# 9002454 DIM. 25" BY 7" IAW B727 SRM 51-40-3 FIG 1 AND 57-20-2SDR DHL2006764502Rib · crackedNR 6 SLAT IB ACTUATOR ROD END MOUNT RIB CRACKED. REMOVED AND REPLACED RIB AT NR 6 SLAT IB ACTUATOR ROD MOUNT PO NR 619549 P/N 65-17294-13 IAW B727 SRM 51-30-2.SDR DHL2006764514Rib · crackedFOUND CRACK INDICATION ON NR 7 SLAT I/B ACTUATOR ROD END MOUNT RIB. REMOVED AND REPLACED RIB ASSY P/N 65-17310-3 PO NR 619595 AND P/N 65-17310-4 PO NR 61956. CHANNEL P/N 65-17310-7 PO NR 619596 IAW B727 SRM 51-30-5 AT NR 7 SLAT IB AND OB ACTUATOR ROD END MOUSDR DHL2007751514Frame · corrodedA/C IN C CHECK, AFT CARGO COMPT FRAME AT STA 950D IS CORRODED AT BOTTOM BETWEEN STR 29L-28L. REPLACED DAMAGED SHEER TIE AT BS 950D BETWEEN STRINGER 29L-28L. FABRICATED NEW PART 7075-0 .080 PO NR 9002619 IAW B727 SRM 53-10-4 FIG15 AND 53-10-2 FIG 5. HEAT TRESDR DHL2006763505Angle · gougedFWD CARGO S-27R AT BS 560 HAS EXFOLIATION CORROSION. CUT OUT CORRODED SECTION BS 568 - 547.2 S-27R. FABRICATED AND INSTALLED REPAIRS 3.150" X .090" X .800" FROM 7075-T6 .090, 20.800" X 3.00" X 1.250" FROM BAC1498-131 AND 1.650" X .825" X 1.40" FROM 7075-T6 .SDR DHL2006763503Cap · corrodedS/O 284007 N/R 031817 - FWD CARGO AFT DOOR OPENING FRAME CAP BS 620 S-26R HAS EXFOLIATION CORROSION. CUT OUT CORRODED SECTION OF FRAME CAP. FABRICATED AND INSTLLED FRAME CAP REPAIRS 14" X 1" AND 22" X 1" FROM 60-9101 7075-T6 IAW B727 SRM 51-40-4 FIG. 1 AND 5SDR DHL2006763517Skin · puncturedS/O 284007 N/R 032223 - RT INBD FORE FLAP PUNCTURED APPROX 4 FEET FROM INBD END. CUT OUT PUNCTURED AREA 1" X 3". FABRICATED AND INSTALLED REPAIR DOUBLER 3 X 6" FROM 2024-T3 .016" IAW SRM 51-40-20 FIG 8.SDR DHL2006763510Intercostal · corrodedS/O 284007 N/R 032047 - CORRODED SHEAR CLIP INTERCOSTAL, 6 INCHES FWD OF BS 990 OUTBD OF S-28R (BS 984). CUT OUT CORRODED SECTION. FABRICATED AND INSTALLED INTERCOSTAL 7-1/4" X 4-3/8" X 5-5/8" X 2" FROM 7075-T6 .050 IAW B727 SRM 53-10-4 FIG 11.SDR DHL2006763515Skin · chafedS/O 284007 N/R 032201 - RT INBD T/E FORE FLAP L/E SKIN CHAFED BEYOND LIMITS AT WBL 72 AND 166, 1.5" AND 96" INBD END. REMOVED 2 EA L/E PANELS THAT WERE OUT OF LIMITS. FABRICATED AND INSTALLED NEW PANELS 7" X 7-5/8" AND 15" X 15" FROM 2024-T3 .040 IAW B727 BOESDR DHL2006763516Skin · crackedS/O 284007 N/R 032203 - RT INBD T/E FORE FLAP L/E SKIN CRACKED ON LOWER SURFACE 53.5" FROM INBD END WBL 124. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER 8" X 6.375 FROM 2024-T3 .063" IAW SRM 57-50-4 FIG 1.SDR DHL2006763501Fitting · brokenS/O 284007 N/R 031639 - LT OUTBD AILERON TAB HAS EXCESSIVE PLAY. OPEN LT OUTBD AILERON SKIN, FOUND INTERNAL TAB MOUNT FITTING BROKEN. REMOVED AND REPLACED FITTING, BALANCED IAW B727 SRM 51-80-4 AND 51-30-2.SDR DHL2006763514Skin · chafedS/O 284007 N/R 032199 - LTOUTBD T/E FORE FLAP L/E SURFACE CHAFED BETWEEN IND AND CENTER HINGES WBL 367. TRIMMED OUT CHAFED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 6" X 4" FROM 2024-T3 .063" IAW B727 SRM 57-50-4 FIG 1.SDR DHL2006763518Frame · crackedS/O 284007 N/R 032154 - CRACK ABOUT 10 INCHES LONG ON FRAME WEB AT BS 1352 RT LOWER SIDE FROM 4 O'CLOCK POSITION TO 5 O'CLOCK AFT SIDE OF WEB. CUT OUT CRACKED AREA OF FRAME. FABRICATED AND INSTALLED REPAIR DOUBLER 27-7/8" X 3-3/8" AND FILLER FROM 7075-T6 .071SDR DHL2006763513Nut Plate · missingS/O 284007 N/R 032195 - LT OUTBD FLAP OUTBD ATTACH FITTING ATTACH POINT HAS MISSING NUTPLATE. REMOVED EXISTING REPAIR DOUBLER, CUT OUT SKIN FOR ACCESS, REMOVED AND REPLACED NUTPLATE. FABRICATED AND INSTALLED REPAIR DOUBLER 10.25" X 4" FROM 2024-T3 .063" IAW ISDR DHL2006763506Clip · corrodedS/O 284007 N/R 032039 - AFT CARGO CORROSION SHEAR CLIP 950D S-28L - 29L. REMOVED CORRODED SHEAR CLIP. FABRICATED AND INSTALLED REPAIR 3-1/2" X 6-1/4" FROM 7075-T6 .071" IAW B727 SRM 53-10-4 FIG. 11.SDR DHL2006763509Clip · corrodedS/O 284007 N/R 032042 - CORRODED SHEAR CLIP IN AFT CARGO COMPARTMENT BS 950F S-28L. REMOVED EXISTING CORRODED DOUBLER. FABRICATED AND INSTALLED DOUBLER 8" X 4" FROM 7075-T6 .071 IAW B727 SRM 53-10-4 FIG 13.SDR DHL2006763507Skin · corrodedS/O 284007 N/R 021040 - CORRODED FUSELAGE SKIN 4 INCHES AFT OF BS 950D O/B S-27 IN AFT CARGO COMPT. CUT OUT CORRODED SKIN. FABRICATED AND INSTALLED DOUBLER REPAIR 18-1/2" X 10-3/4" FROM 2024-T3 .160 IAW B727 SRM 53-30-3 FIG. 3.SDR DHL2006763512Torque Box · misrepairedS/O 284007 N/R 032151 - AFT AIRSTAIR AREA RT SIDE BELOW FLOOR LINE BS 1243 LOWER TORQUE BOX VERTICAL SKIN LIGHTNING HOLE HAS AN IMPROPER REPAIR, DOES NOT EXTEND TO CUT-OUT. REMOVED EXISTING DOUBLER. FABRICATED AND INSTALLED DOUBLER REPAIR 4.4" X 2.4" FROM 707SDR DHL2006763508Clip · corrodedS/O 284007 N/R 021041 - CORRODED SHEAR CLIP IN AFT CARGO COMPARTMENT BS 950F S-28L. REMOVED EXISTING CORRODED DOUBLER. FABRICATED AND INSTALLED DOUBLER 8" X 4" FROM 7075-T6 .071 IAW B727 SRM 53-10-4 FIG. 13.SDR DHL2006763511Stringer · corrodedS/O 284007 N/R 032080 - CORROSION ON S-28L IN AFT PIT OUTBD SIDE BETWEEN BS 970 - 990. CUT OUT CORRODED SECTION. FABRICATED AND INSTALLED STRINGER REPAIRS 5.5" X 3.6" FROM 7075-T6 .040 AND 25-1/4" X 11-1/4" FROM BAC1498-131 AT BS 950F + 9.25" - 984.5 S-28L IASDR DHL2006763504Stringer · corrodedS/O 284007 N/R 031818 - FWD CARGO S-27R AT BS 560 HAS EXFOLIATION CORROSION. CUT OUT CORRODED SECTION BS 568 - 547.2 S-27R. FABRICATED AND INSTALLED REPAIRS 3.150" X .090" X .800" FROM 7075-T6 .090, 20.800" X 3.00" X 1.250" FROM BAC1498-131 AND 1.650" X .825"SDR DHL2006763502Skin · crackedS/O 284007 N/R 031777 - CRACK IN L-1 DOOR UPPER HINGE CUTOUT IN FUSELAGE SKIN .300" LENGTH , FWD LOWER CORNER, CONFIRMED 10X VISUAL BS 303.7. CUT OUT CRACKED SECTION, FABRICATED AND INSTALLED DOUBLER REPAIR 16.5" X 5.4" FROM 301-1/2 HARD .063" AND 6.5" X 6.5"SDR DHL2005763005Warning Light · illuminatedMAIN CARGO DOOR WARNING LIGHT ILLUMINATED AT FL 250, NO LOSS OF PRESSURIZATION NOTED. PLACED DMI PER MEL 52-4-1 CAT B DDD 12/27/05 DMI 23781 PLACARDS INSTALLED DOOR IS VERIFIED CLOSED & LOCKED.SDR DHL2005765511Stringer · crackedFOUND FWD PIT STRINGER CRACKED STA 675 S-29L. CUT OUT CRACKED SECTION OF STRINGER AT STA 675 STR 29L. FABRICATED AND INSTALLED REPAIR STRINGER SECTION 20-5/8" FROM BAC1498-132 AND 5" FROM BAC1498-144 IAW B727 SRM 53-10-3 FIG 1.SDR DHL2005765502Channel · corrodedAFT CARGO PIT FLOOR SUPPORT CHANNEL IS CRACKED BEYOND STOP DRILL HOLES (6" FWD OF STA 950F, RBL 4). REMOVED FLOOR SUPPORT IAW B727 SRM 51-30-2. FABRICATED AND INSTALLED FLOOR SUPPORT CHANNEL 5'8" FROM BAC1500-6199 IAW B727 SRM 51-30-2, 51-10-2.SDR DHL2005751007Battery Pack · dischargedEMERGENCY EXIT LIGHTS INOPERATIVE. ALLOWED PACKS TO RE-CHARGE AND CHECKS SERVICE IAW MM 33-50-01.SDR DHL2005765507Hinge Fitting · corrodedFOUND LEFT HORIZ STAB T/E NR 1 ELEVATOR ATTACH HINGE LUGS INNER FACES HAS PITTING CORROSION. BLENDED CORROSION ON LUGS IAW TIMCO REO-983 REV IR DATED 12/01/05. FOUND LUGS TO BE WITHIN LIMITS, TREATED AND PRIMED IAW B727 SRM 51-20-1.SDR DHL2005765506Floor Support · corrodedAFT BAGGAGE PIT CORROSION ON FLOOR SUPPORT CHANNEL, LWR SIDE, BETWEEN STA 1030 AND 1050 RBL 12. REMOVED SECTION OF FLOOR SUPPORT STA 1030 - 1082. FABRICATED AND INSTALLED (3) REPAIR SPLICES 10.50" BY 1" BY 1" FROM BAC1490-2583, 10.50 BY .085" BY .085" FROM ASDR DHL2005765508Hinge Fitting · corrodedRT HORIZ STAB T/E NR 1 ELEVATOR ATTACH HINGE LUGS INNER FACES HAS PITTING CORROSION. BLENDED CORROSION ON LUGS IAW TIMCO REO-983 REV IR DATED 12/01/05. FOUND LUGS TO BE WITHIN LIMITS, TREATED AND PRIMED IAW B727 SRM 51-20-1.SDR DHL2005765518Frame · corrodedAFT CARGO COMPT BILGE, BS 1010 FRAME CORRODED AT LOWER FWD SIDE BETWEEN STR 29R - 30. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR 5.25" BY 5.25" BY 3.75" BY .75" FROM 7075-T6 .071 IAW B727 SRM 53-10-4 FIG 13.
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