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 DHL2004745534Skin · dentedDURING A C-CHECK, RT WING I/B FOREFLAP L/E HAS A DENT WS 335. DAMAGED FOUND TO BE OUT OF LIMIT IAW B727 SRM 57-50-1 FIG 3. CUT OUT DAMAGED AREA & FABBED FILLER FROM 2024 T3 .050 PO 900980 DIM 2.6875 INCH X 2.5 INCH & 2 EA DOUBLERS FROM 2024 T3 .063 PO 90079SDR DHL2004745533Skin · puncturedDURING A C-CHECK, RT WING INBD FOREFLAP L/E WS 224 HAS A PUNCTURE AND AT WS 335 L/E HAS ONE (1) DENT. REFER TO NR 96459 FOR DENT REPAIR. CUT OUT DAMAGED AREA AND FABBED FROM 2024 T3 .050 PO 9001189 DIM 4 X 4 INCH AND 2 EA DOUBLERS FROM 2024 T3 .063 PO 900790SDR DHL2004745532Skin · corrodedDURING A C-CHECK, LT LOWER FUSELAGE STA 675 STR 26L HAS SKIN PILLOWING WITH A POPPED FASTENER. REMOVED FASTENERS AT BS 675 STR 26L IAW B727 SRM 51-30-2, DUE TO THE FURTHER EVALUATION NO CORROSION FOUND ON SKIN. STRINGER 26L AT BS 670 TO BS 685 FOUND TO BE OUSDR DHL2004745531Skin · damagedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSELAGE SKIN PREVIOUS REPAIR HAS SKIN PILLOWING AT BS 1130-1144 ABOVE STR 26L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 53-30-1 FIG 1. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGED AREA 12.1250 INCHES X 8.SDR DHL2004745530Skin · damagedDURING A C-CHECK, RT FUSE HAS A CREASE IN THE SKIN BS 440 TO BS 520 BELOW STR 20R. REWORKED SKIN TO ORIGINAL CONTOUR AT BS 440-500 STR 20R-21R IAW 727 SRM 51-40-1. CUT OUT DAMAGED AREA BS 520 STR 20R-21R AND FABBED FILLER FROM 2024-T3 .050 PO 900980 DIM 5 X SDR DHL2004745529Stringer · corrodedDURING A C-CHECK, STR 21 RT IS CORRODED JUST FWD OF STA 740 BULKHEAD. CUT OUT DAMAGED SECTION OF STRINGER 730 TO 740 DIM 10 INCHES AND FABBED STR FROM BAC 149G-131 PO 3323107 DIM 10 INCHES & SPLICE FROM BAC 1498-142 PO 900878 DIM 14 INCHES IAW 727 SRM 53-10-3SDR DHL2004745528Stringer · corrodedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; STR 23 RT IS CORRODED AT 740 STA BULKHEAD M/R. CUTOUT SECTION OF STR 23R FROM STA 725-STA740 SIZE 15 INCHES IAW B727 SRM 51-10-3 FIG 1. FABRICATED STRINGER FROM BAC 1496-131 SIZE 15 INCHES PO NR 332SDR DHL2004745527Hinge · crackedDURING A C- CHECK, MAIN DECK CARGO DOOR HINGE AFT UPPER SECTION CRACKED. REMOVED & REPLACED DAMAGED HINGE SECTION P/N 20001-16-7200 PO 9912233 DIM 18 INCHES LONG PER S/B AEI 01-01 OPS CHECK ACCOMPLISHED ON NR 90350.SDR DHL2004745525Keelbeam · crackedDURING A C-CHECK, LT WHEEL WELL BS 870 & KEEL BEAM VERTICAL STIFFENER CRACK INDICATION NDT VERIFIED MED. REMOVED AND REPLACED LT W/W BS 870 KEEL BEAM VERTICAL STIFFENER IAW B727 SRM 51-30-2 PO 4274124, P/N 65-18636-377.SDR DHL2004745524Skin · dentedDURING A C-CHECK, LT FUSE HAS DENTS FWD BS 620 ABOVE STR 27L. DAMAGED AREA OUT OF LIMITS IAW B727 SRM53-30-1 FIG 1. CUT OUT DAMAGED AREA 14.125 X 4.75 INCH AND FABBED FILLER FROM 2024 T3 .050 PO 9001118 DIM 14.125 X 1.125 INCH AND DOUBLER FROM 2024 T3 .063 PSDR DHL2004745523Frame · dentedDURING A C-CHECK, AFT CARGO FRAME BS 1030 HAS A DENT INTO THE RADIUS ABOVE STR 25L. DAMAGED AREA OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED AREA DIM 1.75 X 1 INCH AND FABBED REPAIR ANGLE FROM 7075-T6 .071 PO 900489 DIM 11.75 X 4 INCHES IAW 727 SDR DHL2004745522Frame · dentedDURING A C-CHECK, AFT CARGO FRAME BS 1010 HAS A DENT INTO THE RADIUS ABOVE STR 26L TO STR 24L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. REMOVED EXISTING SPLICE, CUT OUT DAMAGED FRAME, FABBED NEW FROM 7075 T-6 .063 PO 900408 DIM 13.5 X 5.25SDR DHL2004745520Stiffener · crackedDURING A C-PICCOLO TUBE CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT WING IB L/E INT STIFFENER IB SIDE OF WBL 92 FRAME 12 INCHES FROM FWD SPAR IS CRACKED ON TOP. REMOVED DAMAGED ANGLE AND FABBED NEW FROM 7075-T6 .040 PO NR 900920 DIM 3.1250 INCH X2 INCHESDR DHL2004745521Panel · dentedDURING A C-CHECK, VERTICAL FIN BASE COMPOSITE PANEL LT SIDE BELOW AND FWD OF THE NR 2 ENGINE CHANGE FIXTURE CAVITY WITH DENTS. CUT OUT 3 EA SHARP DENTED AREAS APPROX 2.25 X .5 INCH, 2.25 X .5 INCH & 1 DIA. FABRICATED 2 EA FILLERS APPROX 2.25 X .5 INCH & 1 EASDR DHL2004745519Frame · crackedDURING A C-CHECK, NR 3 SLAT INT FRAME BOTTOM AFT WS 525 IS CRACKED IN RADIUS. REMOVED NR 3 SLAT FOR SHEET METAL ACCESS IAW B727 M/M 27-81-11. REMOVED CRACKED RIB ON NR 3 SLAT IAW B727 SRM 51-30-2. FABRICATED RIB FROM 7075-T6 .032 SIZE 15 X 5.5 INCHES PO 90SDR DHL2004745518Skin · delaminatedC-CHECK, LT OTBD AFT FLAP LOWER SURF WBL 400 HAS 2 AREAS OF DELAMINATION. CUT OUT DELAM AREA. FABBBED ONE FILLER AND ONE DOUBLER. CLEARED, PREPED, APPLIED ADHESHIVE PRIMER & ADHESIVE TO ALL MATING SURFACES. BONDED, CURED, SANDED, CLEANED, TREATED, PRIMED, SDR DHL2004745517Skin · crackedDURING A C-CHECK, FUSELAGE SKIN BS 1100 RT OF STR 1 CRACK INDICATION FROM FAST HOLE SKATE ANGLE SUPPORT NR 2 ENG NOSE COWL. NDT VERIFIED. CUT OUT CRACKED AREA SIZE .375 X .375 INCH AT STR 1 BS 1100 IAW S/B 727 53 02 04 AND SRM 53-30-3 FIG 3, FABRICATED DOUBSDR DHL2004745516Skin · delaminatedDURING A C-CHECK, LEFT I/B FORE FLAP LOWER SURF AT L/E WBL 124 HAS SKIN DELAMINATED. REMOVED LEFT I/B FORE FLAP IAW 727 MM 27-51-01, CUT OUT LWR SKIN 5.5 X 4.5 INCHES, FABBED FILLER 6.5 X 4.5 INCHES AND DOUBLER 9.5 X 6 INCHES FROM 2024-T3 .016 PO 900573 IAW 7SDR DHL2004745515Panel · delaminatedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT. WING IB LOWER MLG BEAM PANEL WBL114 OB SURF IS DELAMINATED SEVERAL PL. CUT OUT 2EA DELAMINATED AREAS DIM 3 INCH DIA & 4 INCH DIA FABBED FILLERS DIA 3 INCH DIA & 4 INCH DIA, DOUBLERS 2EA 6.5 INCH DISDR DHL2004745514Seat Track · damagedDURING A C-CHECK, IN MAIN CABIN SEAT TRACK LBL 60 135 495 TO BS 515 SCALLOP IS WARN. CUT OUT DAMAGE SEAT TRACK IAW B727 SRM 53-10-2 FIG 7. FABRICATED SEAT TRACK DIM: 29.5 FROM PART NUMBER BAC 1520-841 PO 416740 IAW B727 SRM 53-10-2. TREATED & PRIMED ALL PARSDR DHL2004745537Spar · crackedDURING A C-CHECK, 4 INCH CRACK ON DOUBLER FWD OF FWD EDGE OF UPPER MAIN SPAR LOCATED ABOVE NR 5 FLAP ACTUATOR AFT END RWS 147 (RIGHT WING). CUT OUT SKIN SPLICE SIZE 10.25 X 2.5 INCH ON L/E SKIN ABOVE NR 5 FLAP ACTUATOR AFT END RWS 147 IAW B727 SRM 51-10-1. FSDR DHL2004745513Skin · crackedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LEADING EDGE SKIN AT CUTOUT FOR NR 6 SLAT HAS BROKEN FASTENERS AND SHARP EDGES RW5-525. REMOVED NR 6 L/E SLAT IAW MM 27-81-11. REMOVED DAMAGED FASTENERS IAW SRM 51-30-2 REMOVED SHARP EDGES AT NR 6 SLATSDR DHL2004745512Window Frame · damagedDURING A C-CHECK, THE FOLLOWING DESCREPANCIES WERE NOTED; RT "F-N" WINDOW POST CROCK INDICATION AT POINT N MOST OB BOLT HOLE TOP FRAME WINDOW NR 5 MARKED NDT X-RAY FINDING. INSTALLED RT WINDOW POST REPAIR KIT PN65635282-8 PO NR 427441 IAW S/B 727-53-0086 REV SDR DHL2004745560Seat Track · wornDURING A C-CHECK, COCKPIT F/E AFT TRACK HAS WORN OUT INDICATION LOCK HOLES ARE SCRATCHED. REMOVED & REPLACED DAMAGED TRACK P/N 806019-401 PO 427462 IAW 727 SRM 51-30-2.SDR DHL2004745503Skin · dentedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT FUSE HAS A DENT AFT BS640 ABOVE STR 23R. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGE DIM 2.5 INCH X 2.2500 INCH AND FABBED DOUBLER FROM 2024 T3 .080 PO NR 9001135 DIM 11.SDR DHL2004745511Skin · dentedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT FWD BS 380 BELOW STR 17L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 2 INCH X 1 INCH AND FABBED DOUBLER FROM 2024 T3 .071 PO NR 9007903 DIM SDR DHL2004745510Skin · dentedDURING A C-CHECK, LT FUSE HAS A DENT AFT BS 560 ABOVE STR 27L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA 57/8 X 21/4 AND FABBED FILLER FROM 2024 T3 .040 PO NR 9001030 DIM 57/8 X 1 AND DOUBLER FROM 2024 T3 .063 PO NR SDR DHL2004745509Skin · dentedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT FWD BS 580 ABOVE STR 27 LT. CORRECTIVE ACTION; DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 2.8750 INCH X 1.7500 INCH AND FABBED FILLER FROM 2SDR DHL2004745508Skin · dentedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT BS 1010 ABOVE STR 21L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024 T3 .063 PO NR 900732 DIM 2.5 INCHES X 2.5 INCHES ASDR DHL2004745507Skin · dentedDURING A "C" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT AFT BS 1030 STR 25L. DAMAGED FWD TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1; FABRICATED DOUBLE (10.2500 INCH X 7.7500 INCH) 2024 T3 0.71 PO NR 900790, FILLER (2.1250 INCH X 1.7500 SDR DHL2004745506Skin · dentedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS DENTS FWD BS 1090 ABOVE STR 18L. DAMAGED AREA OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 10 INCHES X 8 INCHES IAW SRM 53-30-3 FIG 1. DOUBLER TREATED AND PRIMED IAW SRM 51-SDR DHL2004745505Skin · dentedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT FWD BS1090 BELOW STR 19L. DAMAGED AREA OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1; CUT OUT DAMAGED AREA AT STR 18L BS 1084 DIMENTION (1INCH DIA) AND FABRICATED DOUBLER (4.2500 INCH DIASDR DHL2004745504Skin · dentedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT FUSE HAS A DENT AFT BS 640 ABOVE STR 23 RT. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGE DIM 2.5 INCHES X 2.2500 INCHES AND FABBED DOUBLER FROM 2024 T3 .080 PO NR 9001135SDR DHL2004745502Skin · dentedDURING A (C) CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED;R/H FUSE HAS A DENT AT BS 480 BELOW STR 23R. DAMAGE OUT OF LIMITS IAW B727 SRM 53-30-1,FIG.1,CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024-T3 .050 P.O.900980 DIM. 1.8750 INCH X 1.7500 INCH AND DOUBLSDR DHL2004746005Brake · malfunctionedBRAKES DRAGGING UNABLE TO DISENGAGE. T/S BRAKE SYST FOUND PNEUMATIC BRAKE HANDLE SLIGHTLY OFF DETENT STILL SAFETIED, BLED BRAKES, SAFETIED PNEUMATIC BRAKE HANDLE SYST. OPS CKD GOOD IAW MM 32-41-0.SDR DHL2004745501Skin · dentedDURING A C-CHECK AT THE FOLLOWING DISCREPANCIES WERE NOTED; RT FUSE HAS A DENT AT BS 380, BELOW STR 20R. DAMAGE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG.1 CUT OUT DAMAGED AREA DIM 1.7500 X 1.5 INCH AND FABBED DOUBLER FROM 2024 T3, .050,P.O. 900980. DIM 9.1250SDR DHL2004745559Bracket · crackedDURING A C-CHECK, LT WING LOWER WBL 203 NR 3 FLAP TRACK ANGLE SUPPORT FWD FAIRING HAS CRACK OVER PREVIOUS REPAIR O/B OF TRACK. FAB ANGLE SUPPORT ON LT WING NR 3 FLAP TRACK FROM 2024T3 .063 PO 900781 SIZE 9 X 1.5 INCH IAW B727 SRM 51-40-3. ALODINED & PRIMEDSDR DHL2004745558Skin · debondedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT IB MID FLAP TE TOP SKIN DEBONDED AREA WBL 203. CUT OUT DAMAGED AREA OF L/W IB MID FLAP UPPER SKIN APPROX 4.2500 INCHES X 5.7500 INCHES IAW SRM 51-40 -20 FIG 30 FABRICATED ONE FILLER APPROX 4.2500 ISDR DHL2004745554Skin · debondedDURING A C-CHECK, RT INBOARD MID FLAP T/E UPPER SKIN SHOW DISBONDED AREAS WBL 160 TO OUTBOARD. CUT OUT DELAMINATED ARE OF RW I/B MIDFLAP T/E UPPER SKIN APPROX 6.5 X 4.25 INCHES & 2 EA DOUBLERS APPROX 3 X 4.5 INCHES FROM 2024-T3 .016 PO 900962 IAW B727 SRM 57SDR 2004F00174Line · crackedDURING FINAL APPROACH HYDRAULIC SYSTEM A QUANTITY DROPPED TO ZERO LANDED SAFELY WITHOUT INCIDENT. FOUND NR 2 ENGINE SUPPLY LINE CRACKED REPLACED SAME PER MM 29-00. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVIEC WITHOUT FURTHER INCIDENT. (M)SDR GAIA04079OPTube · brokenFLT 6007 - SEA-KTN - DURING DEPARTURE, ENGINE NR 2 N2 AT 102 PERCENT AND EGT AT RED LINE ON CLIMB-OUT, EPR AT 1.89. AIRCRAFT RETURNED. LANDING WEIGHT 142000, NORMAL LANDING AND BRAKING. LANDING WAS MADE WITHOUT INCIDENT. INSPECTED NR 2 ENGINE AND FOND BROKSDR DHL2004745018Engine · shutdownNR 2 ENGINE SHUTDOWN AFTER START COMPLETED. VALVE INTRANSIT LIGHT REMAINED ILLUMINATED DURING START. RESTART NR 2 ENGINE AND MAINTAINED ENGINE PARAMETERS. NR 2 ENGINE START AND OPS CHECKED OK PER B727 M/M 80-11-0. DUE TO WRITE UP ON LOG PAGE 008250 ON FUELSDR GAIA04076AOPIndicator · smokeBOS - AFTER PUSH-BACK, FLIGHT CREW INDICATED SMOKE COMING FROM RADAR INDICATOR. REMOVED AND REPLACED RADAR INDICATOR. OPS CHECK AND SELF TEST GOOD ON GROUND. THIS CLEARS DMI NR 1855. PLACARD REMOVED. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA04076OPIndicator · malfunctionedAFTER PUSH-BACK, FLIGHT CREW INDICATED SMOKE COMING FROM RADAR INDICATOR. INSPECTED RADAR SYSTEM, FOUND BAD RADAR INDICATOR, TRANSFERRED TO DMI NR 1855 IAW MEL 34-21, CAT (C) DUE.SDR GAIA04074OPActuator · leakingNOTED ELEVATOR LOW PRESSURE LIGHT CAME ON, HYDRAULIC SYSTEM (A) QUANTITY INDICATED ZERO, SYSTEM (A) ENGINE PUMP LOW PRESSURE LIGHTS BLINKING. FLIGHT DIVERTED MAINTENANCE BASE WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND BROKEN INSERT IB TRUNNION FITTING SDR DHL2004746004Indicator · malfunctionedMACH AIRSPEED WARNING ACTIVATED AT 90 KTS DURING TAKE-OFF ROLL. T/O REJECTED AT 110 KTS, 145.200 TOW, TEMP +19 C, PA 100', RWY 36L, AND BRAKE ENERGY CAUTION ZONE. TRANSFERRED TO DMI NR 16523 IAW ASTAR MEL 34-4-3 MACH AIRSPEED WARNING SYSTEM DEACTIVATED FOR FSDR FX72004F00000Valve · defectiveNR 2 ENGINE SHUT-DOWN DURING FLIGHT DUE TO HIGH OIL TEMP IN YELLOW ARC. TROUBLESHOT AND FOUND FUEL HEAT VALVE OPEN. CLOSED MANUALLY AND SAFETY WIRED SHUT. RAN ENGINE ALL PARAMETERS NORMAL AND AIRCRAFT RETURNED TO SERVICE WITH FUEL HEAT VALVE ON DMI. NO FURSDR DHL2004745017Fire Loop · misroutedNR 1 ENGINE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED. TRANSFERRED TO DMI 16463 IAW MEL 26-9 PLACARD INSTALLED. REF DMI NR 16463 NR 1 ENG DETECTION CIRCUIT GROUNG LIGHT ILLUMINATED. FOUND ENG FIRE LOOP TOUCHING CASE, REROUTED FIRE LOOP, OPS CHECKS GOOD ISDR DHL2004745016Warning System · malfunctionedLANDING GEAR DOOR LIGHT ILLUMINATED, WHEN LANDING GEAR HANDLE WAS SELECTED TO OFF. DOOR ANNUNCIATOR PANEL INDICATED RIGHT GEAR DOOR PLACED GEAR HANDLE IN UP POSITION PER ABNORMAL PROCEDURE AND RED DOOR LIGHT EXTINGUISHED. CYCLED GEAR HANDLE SEVERAL TIMES WITSDR GAIA04055OPAccessory Unit · malfunctionedFLT 772 - DTW-FWA - NOSE GEAR RED LIGHT ON GEAR ANNUNCIATOR PANEL CAME ON AFTER GEAR RETRACTION. RERACKED LANDING GEAR ACCESSORY UNIT. CYCLED GEAR NUMEROUS TIMES. NO DEFECTS NOTED. OPS CHECK OK. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
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