Boeing 727-232
Service difficulty reports · 6,539
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 = '727232' 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 = '727232' 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 CALA9800002Hyd Line · rupturedTHE AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY DURING GEAR EXTENSION WHILE ON APPROACH TO IAH. ABNORMAL AND EMERGENCY PROCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT GEAR DOOR HYDRAULIC LINE RUPTURED. THE HYDRAULICSDR DL72S980728Battery Pack · dischargedLEFT OVERWING EMERGENCY LIGHT WAS INOP. FOUND THAT BATTERY PACK WAS DEAD. REPLACED BATTERY PACK WITH NEW, OPS NML.SDR DL72S980403Skin · crackedDURING SHOP INSPECTION, THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A REPAIR ANGLE.SDR DL72K972754Skin · inoperativeFOUND EXIT SIGN ABOVE SEAT ROW 3 NOT ILLUMINATED DURING TEST. REPLACED BATTERY PACK, OPS CKS OK.SDR CALA9701801Accessory Unit · inoperativeTHE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT IAW MM 32-09-121. OPERATION OF THE GEAR CHECKED GOOD.SDR DL72S972747Skin · crackedFOUND DURING D-2 LETTER CHECK, .75 INCH CRACK FUSELAGE SKIN AT MAIN ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED PER SRM 53-30-3 FIG 33.SDR DL72S972745Skin · holeNR 1 SLAT HAS HOLE IN TAI BAFFLE. REPAIRED PER MM 57-54-0 P. 804A.SDR DL72S972744Skin · crackedFOUND ON D2 LETTER CHECK, .75 INCH CRACK EXTENDING FROM ACCESS PANEL 9524 RT SIDE. REPAIRED PER MM 54-30-0.SDR DL72S972743Skin · crackedFOUND NON D2 LETTER CHECK, 1 INCH CRACK 'S' DUCT HOUSING LT SIDE STA 1243. REPAIRED PER MM 54-30-0.SDR DL72S980120Angle · damagedTEMPORARY REPAIR STA 1343 BL 0 AFT AIRSTAIR OPENING AFT EDGE LWR SIDE. REMOVED REPAIR, CHORD ANGLE, NR 2 ENG FIREWALL PNL. BEGAN DRILLED NEW CHORD AND SKIN. COMPLETED DRILLING CHORD. OK TO INST CHORD. BEGAN INSTALLING CHORD. FINISHED INSTALLING CHORD. CSDR DL72S972746Frame · cracked.25 INCH CRACK FROM UPPER END OF RADIUS BLOCK MLG UPLOCK 913 FRAME. REPAIRED PER M/M 53-11-0 P. 834.SDR DL72S972734Battery Pack · dischargedCENTER AISLE EMER EXIT LIGHT INOP. REPLACED BATTERY PACK, OPS NML.SDR DL72K972733Battery · dischargedFWD LT WING OUTSIDE EMERG LIGHT INOP. REPLACED BATTERY, CKS OK.SDR DL72K972727Light · inoperativeR2 EMERG SLIDE LIGHT INOP. REPLACED REFLECTOR, OPS CHKS GOOD.SDR DL72S972726Battery · dischargedEMERG LIGHT ABOVE AFT AIRSTAIRS INOP. REPLACED BATTS AND CKS GOOD.SDR DL72S980189Skin · wornDURING SHOP VISIT INSPECTION, THE MIDFLAP LEADING EDGE WAS FOUND WORN BEYOND SRM LIMITS AT THE IB END OF FLAP. THE LEADING EDGE WAS REPAIRED PER 727 MM 57-52-0 BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER.SDR DL72S980168Rib · crackedITEM: AT HMV2 FOUND R/W STA 656-5 UPPER STRINGER TO RIB ATTACH IS CRACKED LOC 2ND STRINGER FWD OF REAR SPAR. PLUGGED HOLE PER ERA 33125-14AD STOP DRILLED/REPAIR PART PER MM 57-13-0 FABD PART PER ERA.SDR DL72S980109Web · crackedNR 6 L/E SLAT INTERNAL WEB CRACKED ON O/B SIDE OF SLAT TRACK MT FITTING. REPAIRED PER MM 57-40-00.SDR DL72S980054Stringer · crackedITEM: LH WING HFEC INSP SHOWS CRACK INDICATION AT UPPER STRINGER-TO-RIB NO. 8 AT W.S. 546.5. CORRECTION: COMPLETED STEPS #1 THRU 4 PER MM 57-13-0 FIG 802. FINISHED DRILLING REPAIR ANGLES PER MM 57-13-0 FIG 802. OK TO INSTALL. BEGAN INSTALLING REPAIR PER MM 57SDR DL72S980052Stringer · crackedRIGHT WING STA 656.6 UPPER STRINGER TO RIB ATTACH IS CRACKED LOC AT FWD VENT BOX AFT LUG. PROVIDED CUTOUT IN VENT STRINGER FOR ACCESS AS PER DETAIL I M/M 57-13-0 PG 806. FORWARD ANGLE IN PLACE, NEED TO DRILL UP TO VENT BOX STRINGER. DRILLED UP FWD AND REPASDR DL72S980051Stringer · crackedRT WING HFEC INSP SHOWS CRACK INDICATION AT NO 13 STRINGER-TO-RIB HOLE AT WS 629.0. DRILLED ACCESS HOLE PER M/M 57-13-0. DRILLED REPAIR PARTS PER M/M 57-13-0. OK TO INSTALL. INSTALLED REPAIR PER M/M 57-13-0.SDR DL72S980030Stringer · crackedLEFT WING STA 601.5 UPPER STRINGER TO RIB ATTACH IS CRACKED. FIRST STRINGER FWD OF REAR SPAR. REPAIRED PER MM 57-13-0.SDR DL72S972713Web · crackedA 1 INCH CRACK IN LIGHTENING HOLE TORQUE BOX WEB RT SIDE STA 1223. REPAIRED PER MM 53-11-0 PG 828.SDR DL72K972719Structure · crackedTHE RT TORQUE BOX STRUCTURE IN THE VENTRAL STAIRWAY WAS FOUND TO THREE CRACKED MEMBERS. THE FS 1263 BEAM WAS FOUND WITH A 1.0 CRACK AND THE FS 1273 BEAM AND GUSSET WERE FOUND WITH 1.0 CRACKS. THE DAMAGED MEMBERS WERE REPLACED PER BAC S/B 727-53-0129 AS DOCUMSDR DL72S980108Web · crackedWEB CRACKED VERTICAL STAB INTERIOR, WEB CRACKED LT SIDE OF VERTICAL, APPROX STA 1303 ABOVE S-DUCT. REPAIRED PER SRM 53-10-4.SDR DL72S980107Web · crackedWEB CRACKED VERTICAL STAB INTERIOR, WEB CRACKED RT SIDE OF VERTICAL APPROX STA 1303. REPAIRED PER SRM 53-10-4.SDR DL72S980053Frame · crackedSTA 930 FRAME AT STR 14 FRAME CRACK AND VERTICAL SKIN STRAP CRACK AT SAME LOCATION. REMOVED FASTENERS AND CUT OUT REPAIR AREA PER SRM 53-10-4 PG 7. ALSO, PERFORMED DYE PENETRANT CHECK PER PS 900-6-3 NR 1. DYE CHECK OK. BEGAN DRILLING REPAIR ANGLES, FINISHSDR DL72S980050Web · crackedWEB CRACKED NR 1 SLAT ACTUATOR ATTACH HOUSING WEBS BOTH CRACKED I/B AND O/B SIDE. FABRICATED AND DRILLED I/B REPAIR PER M/M 57-54-0 FIG 804. FABRICATED AND DRILLED UP O/B REPAIR AS PER M/M 57-40-0 FIG 804. OK TO INSTALL. INSTALLED REPAIRS PER M/M 57-54-0 SDR DL72S980029Skin · crackedS-DUCT INTERIOR SKIN CRACKED AND BENT UPWARD FROM 10 O'CLOCK TO 1 O'CLOCK POSITION. REMOVED DAMAGED SECTION OF SKIN. FAB REPAIR DOUBLER AND FILLER PER ERA 331180-14. INSTALLED DOUBLER PER ERA 331180. INSTALLED TAPERED SHIM AND CLOSED OUTER SKIN PER ERA 331SDR DL72S972702Indicator · failedSMOKE IN THE COCKPIT, FLT DIVERTED TO BHM. MTC FOUND NR 3 ENG OIL QTY IND TO BE SOURCE OF SMOKE. REPLACED INDICATOR.SDR DL72K972717Stringer · crackedA 1.5 INCH CRACK IN LWR RADIUS OF STR 18A. REPAIRED PER MM 53-12-0 PG 820.SDR DL72K972708Rib · crackedFOUND ON B2 LETTER CHECK, 1.25 INCH CRACK IN RADIUS OF NOSE RIB I/B SIDE OF ACTUATOR ATTACH NR 7 SLAT. REPAIRED PER MM 57-54-0.SDR DL72K972707Skin · crackedFOUND ON B2 LETTER CK, SEVERAL .25 INCH CRACKS 'S' DUCT HOUSING FWD OF ACCESS PANEL 9501 RT SIDE. REPAIRED PER MM 54-30-0.SDR DL72K972706Bracket · crackedFOUND ON B2 LETTER CK, 1 INCH VISIBLE CRACK NR 1 SLAT ACTUATOR O/B ATTACH BRACKET. REPAIRED PER MM 57-20-21.SDR DL72K972705Skin · crackedFOUND DURING B-2 LETTER CHECK, 1.25 INCH CRACK FUSELAGE SKIN AT MAIN ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED PER SRM 53-30-3 FIG 33, TIME LIMITED.SDR DL72K972700Bracket · misinstalledWHILE ACCOMPLISHING INSPECTIONS MANDATED BY DAL SI 4-59271-12AD, MTC FOUND A .031 GAP BETWEEN THE NR 1 SLAT ACTUATOR AND THE SUPPORT FITTINGS. THE GAP WAS SHIMMED PER THE REQUIREMENTS OF BAC S/B 727-57-0130 AND DOCUMENTED IN ER/A 363526-14AD.SDR EISA97282Actuator · failedLANDING GEAR LOWERED IN TURN TO FINAL, NOSE GEAR WOULD NOT EXTEND, WINGS LEVEL DOWN WIND, GEAR EXTENDED NORMALLY. REPLACED NOSE GEAR ACTUATOR. DRAG BRACE, AND TRANSFER CYLINDER. GEAR SWING CHECKS GOOD PER MM 32-33-0. SYSTEM CHECK NORMAL. (X)SDR DL72S980056Stringer · crackedSTR 18L, INDICATIONS FOUND 3 EA ON TOP ROW, 2ND HOLE FROM FRONT. ON BOTTOM ROW 1ST AND 3RD HOLE FROM FRONT. REFERENCE SUPPLEMENTAL CARD - ATTACHMENT A OPN 250. CLEANED HOLES. REAMED HOLE IN STRINGER 2ND HOLE FROM FRONT ON BOTTOM TO 542. BEGAN DRILLING REPSDR DL72S980055Bracket · crackedBRACKET CRACKED, ACT ATTACH BRACKET NR 3 KRUEGER FLAP OUTBD SIDE. BEGAN MANUFACTURING ANGLE REPAIR DOUBLER AS PER M/M 57-20-21 FIGURE 807. FINISH MFG ANGLE REPAIR DOUBLER PER MM 57-20-21 FIG 807. OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER M/M 57-20-21 FISDR DL72S980028Frame · dentedFRAME DENTED FS 1050 BETWEEN STR 25L AND 26L. REMOVED DAMAGE AND DYE-CHECKED PER SRM 53-10-4. NO CRACKS FOUND AROUND CUTOUT. DRILLED UP DOUBLER AS PER SRM 53-10-4 FIG 27. OK TO INSTALL, BEGAN INSTALLING REPAIR. INSTALLED PER SRM 53-10-4.SDR DL72S980027Support · crackedSUPPORTS CRACKED NR 6 L/E FLAP ACTUATOR SUPPORTS ARE CRACKED. VERIFIED CRACKS TO BE PRESENT PER PS 900-6-3. REMOVED CRACKED SUPPORTS FROM A/C. FABRICATED REPAIR PARTS PER M/M 57-20-32 FIG 807. OK TO TREAT AND PAINT TREATED AND PAINTED PER PS 900-3-6 ASSEMSDR DL72S972714Frame · dentedFRAME DENTED FS 1030 AT STR 26L. REPAIRED PER SRM 53-10-4 FIG 27.SDR CALA9701785Hyd Line · leakingTHE AIRCRAFT LOST A SYSTEM HYDRAULIC FLUID QUANTITY PRIOR TO LANDING AT EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE A SYSTEM HYDRAULIC PRESSURE LINE LEAKING. THE HYDRAULIC PRESSURE LINE WAS REMOVED AND REPLACED. THE HYDRAULIC SSDR CALA9701783Door · out of adjustTHE NOSE GEAR DOOR RED LIGHT REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANDING AT EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. NOSE GEAR DOORS WERE ADJUSTED IAW MM 32-22-1, PAGE 501. INDICATIONS AND OPERATION CHECKED GOOD.SDR DL72S980026Liner · crackedNR 2 ENG INLET ASSY (DOGHOUSE) ACCOUSTICAL LINER 12 O'CLOCK POS AFT CRACKED AND SEPARATING. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND FILLER AS PER SRM 54-10-3 FIG 13. BEGAN INSTALLATION OF REPAIR PER SRM 54-10-3 FIG 13. COMPLETE REPAIR PER SRM 54-10-3 FSDR DL72S972699Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT THE STRINGER 26L LAPSPLICE BETWEEN FS 575 AND 613. THE CORRODED AREA WAS CUTOUT AND A REPAIR DOUBLER INSTALLED. AREAS FWD AND AFT OF THE CUTOUT WERE INSPECTED TO ENSURE NO FURTHER CORROSION WAS PRESENT. THE REPAIR SDR DL72S972680Tube · brokenON TAXI OUT, -A- SYS HYD FAILED. REPLACED NR 2 L/E SLAT LINE.SDR DL72L972697Skin · corrodedTHE FUSELAGE SKIN A FS 705, BL 0 WAS FOUND WITH A SMALL AREA OF CORROSION. THE DAMAGE WAS REMOVED WITH A 1 DIA HOLE. THREE OTHER REPAIRS WERE IN THE GENERAL AREA OF THE CUTOUT. THEREFORE, THE SKIN WAS CUT AT FS 710 FROM S-26L TO S-26R AND A NEW SECTION OF SSDR DL72L972693Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT STA 1050, S-29R. THE SKIN WAS CUTOUT WITH A 1 X 4 CUTOUT. THE DAMAGE WAS ADJACENT TO A PREVIOUSLY INSTALLED SKIN REPAIR. THE EXISTING REPAIR WAS REMOVED AND A NEW DOUBLER INSTALLED TO INCORPORATE BOTH REPAIR ASDR DL72K972685Skin · crackedFOUND ON B2 LETTER CK, SEVERAL 1 INCH CRACKS 'S' DUCT HOUSING FWD OF ACCESS PANEL 9501 LT LOWER CORNER. REPAIRED PER MM 54-30-0.
Back to Boeing 727-232