Boeing 727-224
Service difficulty reports · 2,252
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 = '727224' 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 = '727224' 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 GAIA05033OPSwitch · out of adjustDURING CLIMB FROM 14,000 FEET THE (MAIN CARGO DOOR NOT CLOSED) LIGHT ILLUMINATED. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. ON DECENT THE LIGHT WENT OFF AT 12,000 FEET. AN UNEVENTFUL LANDING WAS MADE AT DEPARTURE. THE MAIN CARGO DOORSDR DHL2005747001Wire · chafedNR 1 GEN FAILED ON T/O ROLL DISCONECTED CSD RTO INFO OAT 16 C PA 4300 SPEED 45 KNOTS MODERATE BREAKING A/C WEIGHT 131,400 REV. THRUST MODERATE. DEFERRED IAW MEL 24-1CAT B CONTROL NR 23128 MC INATALS KPS. TRANSFERED TO DMI GREEN SHEET. C/W SPECIAL PROCEDURSDR DHL2005747002Smoke · detectedCOCKPIT FILLED WITH SMOKE, EVACUATED A/C. WITH ENGINE PNEUMATICS RAN BOTH A/C PACKS AND INSPECTED FOR SMOKE SOURCE, NO DEFECTS A/C OK FOR SERVICE IAW MM JRH 6.3.SDR FX7A200500010Switch · inoperativeASYMMETRY ON OUTBOARD FLAP, L/R NEEDLES DISAGREE, FLAPS AT 5 DEGREES. DUMPED FUEL AND FOLLOWED THE EMERGENCY PROCEDURES. MAINTENANCE FOUND RT OUTBOARD FLAP FOLLOW UP DRUM IS LOOSE IN THE INSIDE. MAINTENANCE REMOVED AND REPLACED ACTUATOR SWITCH, ALSO REMOVEDSDR DHL2005747511Bear Strap · corrodedCORROSION FOUND AFT PIT INTERNAL SKIN STA 990 STR 28R AFT OF BEAR STRAP DOUBLER. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER 20.25 X 15.5 INCH FROM 2024-T3 .160 IAW B737 SRM 53-30-3 FIG 3.SDR DHL2005747510Stringer · corrodedCORROSION FOUND ON STR 28R, STA 950F TO 970 AT SKIN ATTACHMENTS. REMOVED STR 28R FROM 950F TO 1010, FRAME STA 987 RT CLIPS AND ANGLE SUPPORT STA 950F, 985, 990. FABRICATED AND INSTALLED STR SPLICE 13.5 INCH FROM BAC1498-131, SPLICE 1.08 X .810 X .19R FROM 70SDR DHL2005747509Shear Web · corrodedCORRODED AFT CARGO INTERCOSTAL FROM STA 950F TO 970 STR 28R. REMOVED FLOOR SUPPORT CLIPS, REMOVED SHEAR WEB. FABRICATED AND INSTALLED NEW SHEAR WEB 19.5 X 7 INCHES FROM 7075-T6 .040 WEB, FLOOR SUPPORT CLIPS IAW B727 SRM 51-30-5, 51-10-2, 53-10-2 AND 51-30-2.SDR DHL2005747508Stringer Splice · corrodedCORRODED STRINGER SPLICE 28R IN AFT CARGO COMPT BS 1010. REMOVED CORRODED SPLICE. FABRICATED AND INSTALLED REPAIR STRINGER SPLICE 12.5 INCHES FROM BAC1498-131 IAW B727 SRM 51-30-2 AND DWG 65-16341.SDR DHL2005747507Attach Angle · corrodedCORROSION ON SKIN ATTACH ANGLE FS 990 FROM STR 27R TO STR 29R. REMOVED CORROSION OFF SKIN ATTACH ANGLE FS 990 STR 27R TO 29R. PERFORMED ULT INSP ON BLENDED AREA. ATTACH ANGLE BEYOND LIMITS IAW B727 SRM 51-20-1. FABRICATED AND INSTALLED NEW ATTACH ANGLE SKISDR DHL2005747506Shear Tie · corrodedCORROSION ON AFT PIT FRAME AT BS 970 STR 28R - 29R. REMOVED FLOOR SUPPORT AND VERTICAL STIFFENER BS 930 - 990. ANGLE SHEAR TIE FOUND 100 PERCENT MATERIAL LOSS. CUT OUT CORRODED AREA OF ANGLE SHEAR TIE. FABRICATED AND INSTALLED SHEAR TIE REPAIR 6 X 1 X 1 INSDR DHL2005746529Support · crackedAFT AIRSTAIR RT LWR TORQUE BOX HORIZONTAL SUPPORT IS CRACKED AT STA 1263 RBL 18 NDT VERIFIED. REMOVED CRACKED EXISTING REPAIR IAW B727 SRM 51-30-2. FABBED NEW ANGLE REPAIR MAT 15-5 PH SS .063 PO 315722 8"X 3 1/2" IAW B727 SRM 53-10-2 FIG 1, S/B 727-53-0129 &SDR DHL2005746528Skin · crackedC-CHECK NR 4 SLAT SKIN CRACKED AT I/B SLAT HOOK (ON RIVET). ROUTED OUT CRACKED SIZE 1/4" ON NR 4 SLAT AT I/B SLAT HOOK IAW B727 SRM 57-50-3 FIG 10. FABBED REPAIR PLATE FROM 2024T3 .125 SIZE 3 3/4"X 4 1/4" PO 9002329 IAW B727 SRM 57-50-3 FIG 10. TREATED AND SDR DHL2005747502Wedge · delaminatedLEFT WING INBD MID FLAP T/E WEDGE APPROX 61" FROM INBD END HAS AREA OF DELAMINATION ON BOTTOM SKIN. REPAIRED LEFT INBD MID FLAP T/E INNER BOTTOM SKIN AT APPROX 61" FROM INBD END IAW B-727 SRM 51-40-20 PAR 20-22 BY INSTALLING DOUBLER REPAIR.SDR DHL2005745010Odor · detectedAT FL 300 CREW NOTICED BURNING ODOR IN COCKPIT AND NOTED L-1 OVERHEAT LIGHT ILLUMINATED TURNED OFF L-1 OVERHEAT LIGHT BURNING ODOR WENT AWAY. TRANSFERRED TO DMI 21743 PER 727 MEL 30-15 CAT C PLACARDS INSTALLED. REF DMI CONTROL 21743 AT FL 300 CREW NOTICED SDR DHL2005747513Web · corrodedCORROSION ON WEB AT STR 27L STA 950 TO STA 950A. REMOVED CORROSION ON WEB AT STA. 950 TO 950A LONGERON 27L. FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 AND 51-10-6. REMOVED WEB AND INSTALLED NEW WEB P/N 69-44877-13, ALODINED AND PRIMED IAW B727 SRM 51-10-2, INSTSDR DHL2005747512Skin · gougedLT WING INBOARD TRAILING EDGE FORE FLAP OUTBOARD LOWER LEADING EDGE REPAIR DOUBLER IS GOUGED THRU. REMOVED EXISTING REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER 3.95 X 4.55 INCH FROM 2024-T3 .063 IAW B727 SRM 57-50-4. ALODINED AND PRIMED, INSTSDR DHL2005747503Skin · delaminatedLT WING INBD MID-FLAP T/E APPROX 61" FROM INBD END HAVE DELAMINATION. REPAIRED LT INBD MID FLAP T/E AT APPROX 61" FROM INBD END IAW B-727 SRM 51-40-20 PAR 20-22 BY INSTALLING DOUBLER REPAIR.SDR DHL2005747500Web · corrodedCORROSION ON WEB AFT CARGO BIN FS 950 TO FS 950A AT STR 27R. REMOVED CORROSION ON WEB IN AFT CARGO BIN FS 950 TO 950A AT STR 27R. FOUND OUT OF LIMITS. OPEN PANEL NR 3622 FOR ACCESS. REMOVED FLOOR SUPPORT SPLICE ANGLE SAT 950A TO 950B LONGERON 27R. REMOVEDSDR DHL2005746526Stiffener · crackedC-CHECK LOWER CARGO COMPT BS 1183 VERTICAL STIFFENER RBL 7.6 SHOWS CRACK FROM LOWER END IS ABOUT 3 INCHES LONG (NDT VERIFIED). REMOVED FASTENERS FOR ACCESS IAW S/B 727-53-0175. STOP DRILLED CRACK IAW B727 SRM 51-10-1. HFEC VERIFIED STOP DRILL IAW B727 NDT MSDR DHL2005746527Gusset · crackedBS 825 FRAME GUSSET ON RT SIDE I/B AT EDGE IS CRACKED. REMOVED GUSSET ON BS 825 FRAME ON RT SIDE I/B IAW B727 SRM 51-30-2. FABBED GUSSET FROM 7075 T6 .090 SIZE 4.3"X5.6" PO 9001777 IAW B727 S/B 53-0197 SRM 51-10-2. INSTALLED GUSSET IAW B727 S/B 53-0197 REV SDR DHL2005746525Skin · bulgedLT HORIZONTAL UPPER SURFACE REAR CHORD SKIN BULGING OFF FASTENERS STAB 188, MARKED. CUT HORIZONTAL STAB UPPER SKIN FOR ACCESS AT STAB 188 DIM 17 1/2" X 3" IAW B727 SRM 55-10-3 FIG 3. CUT OUT FWD FLANGE OF UPPER T/E SPAR CHORD IAW B727 SRM 55-10-5 FIG 1. REMSDR DHL2005746524Skin · crackedC-CHECK CRACK ON R/W TRAILING EDGE UPPER SURFACE AT NR 12 SPOILER NR 2 HINGE CUTOUT. STOP DRILLED CRACK AT NR 12 SPOILER CUTOUT IAW B727 SRM 57-30-04 FIG 10, C/W HFEC IAW NDT M PT6, 51-00-00 FIG 23, CRACK IS CONTAINED. FABBED REPAIR PLATE FROM .071 7075T6 POSDR DHL2005747505Skin · debondedRT WING INBD MID FLAP T/E APPROX 1/2" FROM INBD END IS DISBONDED. CUT OUT DELAM AREA, FAB FILLER AN DOUBLERS ON TRAVELER NR T-828368. CLEANED UP AN PREP REPAIR AREA AN PARTS FAB. BONDED REPAIR PARTS, TREATED AND PRIMED. COMPLETED REPAIR ON RT WING I/B MID SDR DHL2005747504Skin · crackedCRACK IN T/E FLAP LWR SKIN AT NR 3 ATTACH CUT OUT I/B SIDE LT WING. FABRICATED REPAIR DOUBLER, CHEM TREATED AND PRIMED AND INSTALLED REPAIR DOUBLER IAW B727 SRM 57-50-4,51-10-2 AN 51-20-0 PG 1 OF MM AT T/E FLAP LOWER SKIN NR 3 ATTACH CUTOUT I/B SIDE OF LT WINSDR DHL2005747501Skin · crackedCRACK IN T/E FLAP SHIM AT NR 2 ATTACH CUT OUT I/B SIDE LOWER SIDE LEFT WING. FABRICATED REPAIR DOUBLER, CHEM TREATED AN PRIMED AN INSTALLED REPAIR DOUBLER IAW B-727 SRM 57-50-4,51-10-2 AND 51-20-0 PG 1 OF B727 MM, AT T/E FLAP SKIN AT NR 2 ATTACH CUT OUT I/B LSDR DHL2005746523Crossbeam · crackedE&E DOORS AFT CROSS MEMBER IN ENTRYWAY CRACKED INSIDE LIP 4.5 INCHES OFF CENTER RT SIDE (MARKED). REMOVED FASTENERS AND FRAME IAW B727 SRM 51-30-2. FABBED NEW FRAME 7075 T6 PO9001873 1050 24"X6" IAW B727 SRM 53-10-2 FIG 1. TREATED AND PRIMED PART IAW B727 SSDR DHL2005746521Structure · crackedC-CHECK VERTICAL FIN STA 133 LT STR 9 IS CRACKED AT ATTACH BOLT TO FRAME. REMOVE FASTENERS IAW B727 SRM 51-30-2, CUT OUT DAMAGE AREA DIM 9 1/2"X 3" AND FABBED FILLER FROM BAC15171367 PO 501963 DIM 9 1/2"X 3" AND ANGLE FROM 10134-1201 PO 501962 DIM 23"X 1 1/4"SDR DHL2005746522Structure · crackedVERTICAL STAB FIN STA 180 LT STR 9 IS CRACKED AT ATTACH BOLT TO FRAME. CUT OUT CRACKED SECTION OF STR 9 DI 4 1/2". FABBED FILLER P/N BAC1517-1367 PO 501963 4 1/2" 2EA ANGLE DOUBLERS P/N AND 10134-1201 PO 601952 18" IAW B727 SRM 55-30-4 FIG 1. TREATED AND PRSDR DHL2005746520Frame · dentedFRAME DENTED AT BS 700 STR 24R. REMOVED NESSARY FASTENERS IAW B727 SRM 51-30-2. REMOVED DAMAGED SEC FROM FRAME AT BS 700 STR 24R IAW B727 SRM 51-40-3 FIG 1, 51-30-2 FABBED DOUBLER FROM 7075 T6 .063 PO 900226 10" X 3.5" X .75" DRILLED, DEBURRED, TREATED & PRISDR DHL2005746512Angle · crackedAFT AIRSTAIRS RT TORQUE BOX ACTUATOR ANGLE SUPPORT FITTING STRUCTURE IS CRACKED ALONG RADIUS. REMOVED I/B WEB DOUBLER AND ANGLE AT AFT AIRSTAIR TORQUE BOX AREA IAW B727 S/B 727-53-0129. DRILLED, INSTALLED, TREATED AND PRIMED ANGLE IAW B727 S/B 727-53-0129. SDR DHL2005746519Skin · dentedC-CHECK DENT LT SIDE FUSELAGE SKIN STA 1090 BETWEEN STR. 26L & 27L. CUT OUT DAMAGE ON FUSELAGE SKIN AT STA 1090 BETWEEN STR 26L & 27L 1"X 1.5" IAW B727 SRM 53-30-3 FIG 1. FABRICATED REPAIR DOUBLER 7.5"X 9" 2024T3 .063 PO 9002199 IAW B727 SRM 53-30-3 FIG 1. SDR DHL2005746518Skin · dentedC-CHECK DENT RT SIDE FUSELAGE SKIN STA 1123 ABOVE STR 27R (MARKED). CUT OUT DAMAGE AREA OF SKIN AT STA 1123 ABOVE STR 27R DIMENSIONS 2.5"X 1", FABBED REPAIR DOUBLER FROM .063 2024T3 PO 9002199 IAW B727 SRM 53-30-2 FIG 2 & 53-30-3 FIG 1, DIMENSIONS 11.25"X 7.5SDR DHL2005746514Web · crackedPOSSIBLE CRACK IN UPPER TORQUE BOX WEB BS 1303 AT LWR RT CORNER ACCESS BY PNL 9504 MARKED RED. STOP DRILLED CRACK IAW B727 SRM 51-10-1. HFEC VERIFIED STOP DRILL IAW B727 NDT MANUAL PH 4 51-00-00 FIG 23. COMPLIED WITH COTNEY AEROSPACE EAZ04.3 07-26-05.SDR DHL2005746517Web · crackedC-CHECK POSSIBLE CRACK IN UPPER TORQUE BOX WEB BS 1303 AT LWR LT CORNER ACCESS BY PNL 9504 (MARKED IN RED). STOP DRILLED IAW B727 SRM 51-10-1, HFEC VERFIED STOP DRILLED IAW B727 NDT MAN.PH.4 51-00-00 FIG 23. C/W COTNEY AEROSPACE EAZ04.3 DATED 7/26/05.SDR DHL2005746515Stringer · corrodedSTRINGER 27R CORRODED AT BS 700. CUT OUT DAMAGED SECTION OF STR 27R BS 700 3.5", REPLACED WITH FILLER MAT ID BAC1498-131 PO9001873 3.5" AND STR DOUBLER BAC1498-144 PO 335792 10.5" IAW B727 SRM 53-10-3 FIG 1. TREATED & PRIMED REPAIR PARTS IAW B727 SRM 51-10-2SDR DHL2005746513Splice · incorrectINCORRECT STRINGER SPLICE INSTALLED AT PREVIOUS REPAIR STR 28R STA 480. REMOVED INCORRECT STR SPLICE AT STR 28R STA 480 IAW B727 SRM 51-30-2. FABBED NEW STR SPLICE MAT USED BAC 1498-145 PO 422371 DIM 13" IAW B727 SRM 53-10-3 FIG 1 AND 53-10-20 FIG 9. TREATESDR DHL2005746511Skin · gougedRT WING LOWER WS 770 FWD HAS EDGE OF SKIN GOUGED. CUT OUT DAMAGED SECTION OF SKIN AT WS 770 LWR SKIN DIM 3/4"X 2.5" IAW B727 SRM 57-30-4 FIG 1. FABBED REPAIR DOUBLER FROM .080 2024 T3 PO 9002255 DIM 3 1/8" X 6 3/4" IAW B727 SRM 57-30-4 FIG 1. TREATED AND PRSDR DHL2005746510Retainer · crackedFWD CARGO DOOR LWR AFT CORNER CRACK. REMOVED AND REPLACED SEAL RETAINER (FRAME) AT C1 DOOR IAW B727 SRM 51-30-2 P/N 65-59948-502 PO522885, LEAK CHECK GOOD IAW B727 MM 21-31-0.SDR DHL2000746509Frame · brokenLWR AFT CORNER OF ATTACH FRAME INBOARD OF 1439 SLAT ATTACH POINT ON NR 5 SLAT BROKEN. REMOVED NR 5 SLAT TO REPAIR IAW B727 MM 27-81-1, REMOVED INNER PANELS AND I/B & O/B RIBS FOR REPLACEMENT IAW B727 SRM 51-30-2, DRILLED, TREATED AND PRIMED PARTS AND AREA IAWSDR DHL2005746508Seat Track · damagedMAIN CABIN SEAT TRACK DAMAGED AT BS 1110 TO 1130 LBL 45.5. CUT OUT DAMAGED SEAT TRACK FROM STA 1020 TO 1135 LBL 45.5 IAW B727 SRM 53-10-5 FIG 1, FABBED NEW SEAT TRACK DIM (117 1/2") MAT USED BSC 520-792 PO 900-203 SPLICE 7075 T6 0.25 PO 900-1189 DIM (9") 2 ANSDR DHL2005746507Seat Track · damagedSEAT TRACK DAMAGED AT BS 520 TO 560 RBL 24.75. REMOVED SEAT TRACK AT BS 480 TO 550 RBL 24.75 IAW B727 SRM 51-30-2, FABBED NEW SEAT TRACK MAT P/N BAC 1520-792 PO 9001320 SIZE 70" IAW B727 SRM 53-10-5 FIG 1 AND SRM 53-10-2 FIG 1, TREATED AND PRIMED SEAT TRACK ISDR DHL2005746506Seat Track · damagedMAIN CABIN SEAT TRACK DAMAGED AT BS 480 TO 580 RBL 45.5. REMOVED DAMAGED SEAT TRACK FROM 480-720 RBL 45.5 IAW B727 SRM 51-30-2 AND SRM 53-10-5 FIG 1, FABBED NEW SEAT TRIM 480-720 RBL 45.5 MAT USED BAC 1520-792 PO 9002389 61" 100" & 109 1/2" 2 SPLICES P/N BAC SDR DHL2005746505Seat Track · damagedMAIN CABIN SEAT TRACK DAMAGED AT BS 760 TO 850 RBL 45.5. REMOVED SEAT TRACK AT BS 760 TO 850 RBL 45.5 IAW 727 SRM 53-10-1 FIG 3 AND 51-30-2. FABBED NEW SEAT TRACK P/N BAC 1520-841 DIM 8FT IAW 727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 2. TREATED AND PRIMED SEAT SDR DHL2005746504Skin · damagedPILLOWING AT STA 1208 STR 29R RT SIDE FUSELAGE SKIN (MARKED). REMOVED FASTENERS AT BS 1208 IAW B727 SRM 51-30-2. EVALUATED SKIN CREASES AREA BS 1208 IAW B727 SRM 53-30-1 FIG 1 AND 51-30-2. FOUND TO BE OUT OF LIMITS. SKIN REMOVED LWR SKIN BS 1208 TO BS 1225SDR DHL2005746503Skin · dentedPILLOWING AT STA 1213 BETWEEN STR 28L AND 29L LT SIDE FUSELAGE SKIN (MARKED). REMOVED FASTENERS AT STA 1213 STR 28L TO 29L IAW B727 SRM 51-30-2. EVALUATED AREA SKIN DAMAGED (CREASES) AND DENTS OUT LIMITS IAW B727 SRM 53-30-1 FIG 1. REMOVED LOWER SKIN BS 120SDR DHL2005746502Skin · dentedDENT LT FUSELAGE SKIN STA 1233 BETWEEN STR 23L AND 24L (MARKED). CUT OUT DAMAGE AREA FOUND OUT OF LIMITS DIM CUT OUT 1" BY 3/4" IAW B727 SRM 53-30-3 FIG 1. FABBED DOUBLER REPAIR MAT USED 2024 T3 .063 PO NR 9002199 DIM 8" BY 6" IAW B727 SRM 53-30-3 FIG 1 AND SDR DHL2005746501Skin · damagedPILLOWING AT AFT AIRSTAIR LT CUT OUT SKIN BETWEEN STA 1223 AND 1229 STR 27L (MARKED). REMOVED FASTENERS FROM AREA. REMOVED CORROSION FROM CHORD AT STR 27L MATT LOSS .017 ORIG THICKNESS .125 FABED NEW ANGLE FROM 7075 T6 .040 PO NR 9002219 27.3" X 1.25" X 3" ISDR DHL2005746500Skin · crackedFWD ENTRY DOOR LWR HINGE SUPPORT SKIN CRACKED. REMOVED FASTENERS & CUT OUT DAMAGED SKIN & DOUBLER IAW B727 SRM 51-30-2 AND S/B 727-53A0198 REV 2 FIG 3 SHEET 1 & 2 (3.75 X 1 .375 INCH). FABRICATED DOUBLER FROM 2024-T3, .100 PO 441290, 19.625 X 10.125 INCHES &SDR DHL2005745009Warning Switch · out of adjustAFTER GEAR RETRACTION RED DOOR LIGHT ILLUMINATED. S/O PANEL INDICATED RT GEAR DOOR. ACCOMPLISHED ABNORMAL PROCEDURE PLACE HANDLE UP POSITION DOOR LIGHTS OUT. ADJUSTED RT MAIN GEAR DOOR WARNING SWITCH IAW MM 32-62-11. OPS CHECK GOOD.SDR FX7A200500005Shaft · shearedENGINE FLAME OUT NR 1 DURING CRUISE. UPON TROUBLESHOOTING, MAINTENANCE FOUND THE NR 1 ENGINE FUEL PUMP SHAFT SHEARED, REMOVED AND REPLACED THE NR 1 ENGINE FUEL PUMP AS PER MAINTENANCE MANUAL REFERENCE 73-11-1, PERFORMED OPS/LEAK CHECK.
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