Boeing 727-225
Service difficulty reports · 4,226
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 = '727225' 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 = '727225' 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 99ZZZM687Floorbeam · corrodedFUSELAGE INTERIOR STATION 380 RBL 62 TO LBL 62 FLOORBEAM HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-8. CUT OUT DAMAGED AREA IAW SRM 53-10-8. FABRICATED REPAIR PARTS IAW SRM 53-10-8. INSTALLED REPAIR PARTS, UPPER CHORD, 2 SUPPORT ANGLES, AND 2 REISDR 99ZZZM686Skin · crackedNR 3 ENGINE PYLON APRON UPPER SURFACE HAS SEVERAL CRACKS. DAMAGED AREAS REMOVED IAW SRM 51-40-2. FABRICATED REPAIRS IAW SRM 51-40-2. INSTALLED REPAIRS IAW SRM 51-40-2. (M)SDR 99ZZZM685Frame · corrodedFUSELAGE INTERIOR STATION 440 LBL 62 TO RBL 62 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 51-10-6. FABRICATED REPAIR PARTS IAW SRM 51-10-8. INSTALLED REPAIR PARTS, T-CHORD NR 2 AND NR 3 SUPPORT ANGLE, NR 4 AND NR 5. REINFORCEMENT STRAPS IAW SRM 53-10-8SDR 99ZZZM684Stringer · corrodedEXTERNAL FUSELAGE BULGE IN SKIN AT FS 1070R, STRINER 27R CORROSION OUT OF LIMITS. REMOVED STRINGER IAW SRM 53-10-1. FABRICATED NEW STRINGER, SPLICES, SHIMS, AND FILLERS IAW SRM 53-10-3. INSTALLED REPAIR PARTS IAW SRM 53-10-3. INSTALLED INTERCOSTAL AND SHEASDR 99ZZZM683Floorbeam · corrodedFUSELAGE LOWER LOBE INTERIOR RIGHT HORIZONTAL WALKWAY BEAM CHORD STATION 294 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED CHORD AND FRAME IAW SRM 53-10-4. FABRICATED BELT FRAME AND T-CHORD IAW SRM 53-10-4. INSTALLED BELT FRAME ANSDR 99ZZZM682Skin · dentedRIGHT SIDE EXTERIOR FUSELAGE BELOW FORWARD JACK POINT HAS A DENT DAMAGE OUT OF LIMITS IAW SRM 53-30-3. REMOVED DAMAGED AREA IAW SRM 53-30-3. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3. INSTALLED REPAIR DOUBLER AND FILLER IAW RM 53-30-3. (M)SDR 99ZZZM681Skin · damagedNR 3 ENGINE COWL UPPER HALF INBOARD SECTION BY NR 1, NR 2, AND NR 3 LATCH RECEPTICALS DAMGED SKIN. REPAIRED DAMAGED SKIN IAW SRM 51-10-1. FABRICATED DOUBLER IAW RM 53-10-4. INSTALLED DOUBLER IAW SRM 53-10-4. (M)SDR 99ZZZM680Skin · damagedNR 3 ENGINE COWL UPPER HALF INBOARD SECTION ALONG EDGE EXHIBITED DAMAGE TO INNER SKIN FROM FORWARD TO AFT IN MANY AREA. REMOVED DAMAGE IAW SRM 51-40-2. FABRICATED REPAIRS IAW SRM 51-40-2. INSTALLED REPAIRS IAW SRM 51-40-2. (M)SDR 99ZZZM679Track · crackedSTABILIZER RIGHT SIDE OUT OF TRAK AND IS CRACKED. RECEIVED NEW TRACK P/N 65-29389-16. INSTALLED NEW TRACK IAW SRM 51-30-2. (M)SDR 99ZZZM678Skin · separatedNR 1 ENGNE COWL LOWER HALF NR 3 LATCH RECEPTICAL EDGE SEPARATING. FABRICATED DOUBLERS IAW SRM 54-10-3. INSTALLED DOUBLERS IAW SRM 54-10-3. (M)SDR 99ZZZM677Skin · damagedNR 1 ENGINE COWL HALF OUTBOARD BY NR 2 LATCH RECEPTICAL EDGE IS DAMAGED. REMOVED DAMAGED ANGLE FROM COWL IAW SRM 54-10-3. FABRICATED REPAIR DOUBLER IAW SRM 54-10-3. INSTALLED DOUBLER IAW SRM 54-10-3. (M)SDR 99ZZZM676Rib · crackedNR 1 ENGINE COWL TOP HALF AFT RIB DOUBLER BY BAYONET LATCH IS BENT AND CRACKED. FABRICATED BRACKET AND DOUBLER IAW SRM 54-10-3. INSTALLED REPAIR BRACKET AND DOUBLER IAW SRM 51-30-2. (M)SDR 99ZZZM675Support · corrodedFUSELAGE INTERIOR STATION 303 TO 350 LBL 45 FLOOR SUPPORT HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. FABRICATED REPAIR ANGLES IAW SRM 51-40-4. INSTALLED REPAIR ANGLES IAW SRM 51-30-2. (M)SDR 99ZZZM674Support · corrodedFUSELAGE INTERIOR STATION 420 TO 460 RBL 62 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 51-10-6. FABRICATED SUPPORT IAW SRM 53-10-2 AND SRM 53-10-8. INSTALLED FASTENERS AND SUPPORT IAW SRM 51-30-2. (M)SDR 99ZZZM673Floorbeam · corrodedFUSELAGE INTERIOR STATION 360 LBL 62 TO RBL 62 FLOORBEAM HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 51-10-6. REMOVED FLOORBEAM CAP IAW SRM 51-30-2. FABRICATED REPAIR IAW SRM 53-10-8. INSTALLED FLOORBEAM REPAIR IAW SRM 51-30-2. (M)SDR 99ZZZM672Floorbeam · corrodedFUSELAGE INTERIOR STATION 460 LBL 62 TO RBL 62 FLOORBEAM HAS CORROSION CORROSION OUT OF LIMITS IAW SRM 53-10-1. FABRICATED REPAIR PARTS IAW SRM 53-10-8. INSTALLED REPAIR PARTS T-CHORD, NR 2 AND NR 3 SUPPORT ANGLES, NR 4 AND NR 5. REINFORCEMENT STRAPS AND DOSDR 99ZZZM671Crossmember · corrodedSTATION 1030 LEFT BETWEEN BL 45.50 AND 24.75 EXHIBITS CORROSION ON CROSSMEMBER. CORROSION OUT OF LIMITS IAW SRM 51-10-6. REMOVED CROSSMEMBER IAW SRM 51-30-2. FABRICATED REPAIR PARTS IAW SRM 53-10-8. INSTALLED CROSSMEMBER IAW SRM 51-30-2. (M)SDR 99ZZZM670Skin · crackedLEFT WING INBOARD FLAP AFT FLAP AT MIDDLE OUTBOARD ATTACHMENT POINT CRACKED THROUGH STOP DRILL HOLE IN SKIN. FABRICATED REPAIR DOUBLER IAW SRM 57-50-4. INSTALLED REPAIR DOUBLER IAW SRM 57-50-4. (M)SDR 99ZZZM669Skin · gougedRT WING INBOARD FLAP FOREFLAP LEADING EDGE GOUGED INBOARD OF INBOARD TRACK. FABRICATED REPAIR DOUBLER IAW SRM 57-50-4. INSTALLED REPAIR DOUBLER IAW SRM 57-50-4. (M)SDR 99ZZZM668Skin · gougedRIGHT WING OUTBOARD FLAP FOREFLAP HAS GOUGE IN LEADING EDGE. FABRICATED REPAIR IAW SRM 57-50-4. INSTALLED REPAIR IAW SRM 57-50-4. (M)SDR USAA099902Charger · inoperativeFLT 6141 - BOS-LGA - EMERGENCY EXIT SIGN AT L-1 AND R-1 DOORS INOPERATIVE. REPLACED BATTERY PACK CHARGER, CHECKS OK. (M)SDR 20000515AP010Skin · tornFOUND LEFT WING NR 3 LEADING EDGE FLAP TORN AT TRAILING EDGE. BLENDED OUT DAMAGED AREA PER SRM 57-50-3. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-50-3 PAGE 10 AND 51-10-2 PAGE 1. (M)SDR SCNA99119Battery Pack · dischargedDURING A LINE MAINTENANCE CHECK, THE RIGHT FOWARD OVERWING EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. OPERATIONALLY CHECKS GOOD REF MM 335071.SDR 20000515AP041Light · inoperativeAFT AIRSTAIR UPPER EMERGENCY LIGHT DOES''NT WORK. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW MM 33-50-61 PAGE 403. (M)SDR 20000515AP039Ballscrew · corrodedNOSE LANDING GEAR MANUAL EXTENSION JACKSCREW HAS PITTING CORROSION. REMOVED AND REPLACED NLG MANUAL EXTENSION JACKSCREW IAW MM 32-34-1 PAGE 401, OPS CHECK GOOD IAW MM 32-34-0 PAGE 201. (M)SDR 99ZZZX3943Beam · crackedRIGHT WING J-BEAM HAS APPROXIMATELY .3750 INCH CRACK ABOVE NR 8 SPOILER ACTUATOR. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER STATED DESIGN FLAW OR WING FLEX CAUSE OF CRACK.SDR 99ZZZX3942Airstair · crackedAFT AIRSTAIRS, AREA AT RIGHT, STA 1263 JUST BELOW ACTUATOR ATTACH FITTING, AREA CRACKED. FOUND DURING C-MAINTENANCE CHECK. OPENING AND CLOSING OF STAIRS CAUSED AREA TO BE UNDER CONSTANT PRESSURE.SDR 99ZZZX3941Web · crackedCABIN FLOOR SUPPORT INTERCOSTAL WEB HAS APPROXIMATELY .25 INCH CRACK AT FORWARD END JUST AFT OF BS 400 AT BL ZERO. FOUND DURING C-MAINTENANCE CHECK. SUBMITTER SUGGESTED AREA EXPOSED TO HEAVY LOADS, STRESS.SDR 99ZZZX3940Frame · corrodedLEFT AFT EXIT HATCH FRAME HAS SIGNS OF CORROSION AT LOWER AFT CORNER. FOUND DURING SCHEDULED C-CHECK. SUBMITTER STATED AREA EXPOSED TO MOISTURE AND OTHER ELEMENTS.SDR 99ZZZX3939Stiffener · crackedONE INCH CRACK AT TOP OF STIFFENER INSIDE RIGHT WING LEADING EDGE AT INBOARD SIDE OF LEADING EDGE RIB WDL 92.0. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED AREA SUBJECTED TO STRESS LOADS AND FLEX.SDR 99ZZZX3938Web · crackedLEFT WING LEADING EDGE LBL 92.0 WEB CRACKED 1.5 INCHES DOWN FROM TOP AFT VERTICAL STIFFENER. ACCESS 6302. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED WING FLEX OR STRESS LOADS POSSIBLE CAUSE.SDR 99ZZZX3937Floorbeam · corrodedCABIN FLOORBEAM ST STA 1030, LBL 24 THROUGH RBL 25 HAS CORROSION. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER STATED AREA IS EXPOSED TO LIQUID SPILLS.SDR 99ZZZX3936Angle · corrodedCABIN AFT LAVATORY (LEFT SIDE) FLOOR SUPPORT ANGLE AT STA 1150 THROUGH STA 1180 LBL 24 HAS CORROSION. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED LIQUID SPILLS ARE POSSIBLE CAUSE FOR PROBLEM.SDR 99ZZZX3935Stiffener · crackedONE INCH CRACK AT TOP OF SECOND FROM AFT STIFFENER INSIDE RT WING LE AT INBOARD SIDE OF LEADING EDGE RIB WBL 92.0, ACCESS CUT-OUT 6402. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. AREA EXPOSED TO STRESS LOADS.SDR 99ZZZX3934Floorbeam · corrodedCABIN FLOORBEAM STA 400 RBL 12 TO RBL 12LT HAS CORROSION AND DAMAGE HOLE. FOUND DURING SCHEUDLED C-MAINTENANCE CHECK. AREA EXPOSED TO ENVIRONMENTAL CHANGES AS WELL AS LIQUID SPILLS, ETC.SDR 99ZZZX3933Skin · crackedAPPROXIMATELY .6250 INCH CRACK AT LEFT OUTBOARD FOREFLAP LOWER LEADING EDGE ABOVE NR 1 FLAP TRACK. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. AREA EXPOSED TO STRESS LOADS AS WELL AS BENDING LOADS.SDR 20000515AP009Skin · crackedFOUND LEFT INBOARD FORE FLAP LEADING EDGE HAS CUT AT CENTER SECTION. STOP DRILLED IAW SRM 57-50-4 HFEC, CRACK CONTAINED AT STOP DRILL PART 6 51-00-00, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-50-4 AND 51-30-2 PAGE 4. (M)SDR 20000515AP008Flap Track · corrodedFOUND NR 3 FLAP TRACK AFT ATTACH AREA TOP SURFACE CORRODED. ACCOMPLISHED REPAIR AND INSTALLED FLAP TRACK IAW SB 727-57-0178. (M)SDR 20000515AP015Floorbeam · corrodedFOUND CABIN FLOORBEAM AT STATION 1110 RBL 18 THROUGH LBL 18 HAS CORROSION AT UPPER AND LOWER SURFACE. REMOVED CORROSION AT FLOORBEAM BETWEEN LBL 18 THROUGH RBL 16. REPAIRED FLOORBEAM AT RBL 17 IAW SRM 53-10-8 FIG 3. (M)SDR 20000515AP003Frame · crackedFOUND CRACK IN FORMER AT STATION 930 AND STRINGER 14L. REPAIRED FRAME IAW SB 727-53-0162, REVISION 1. (M)SDR 20000515AP007Bracket · damagedFOUND VERTICAL STABILIZER LEADING EDGE THROUGH PANEL 9502 UPPER RIGHT CORNER BRACKET AND WEB DAMAGED. REMOVED INNER PANEL, CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR IAW SRM 51-10-1 PAGE 4, 51-40-2 PAGE 2, 51-30-1 PAGE 1, 55-10-1 PAGE 6. (M)SDR 20000515AP040Beam · corrodedRIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE SKIN FROM NR 1 TO NR 3 ELEVATOR ATTACH HINGE AREA HAS SPOTS OF CORROSION. REMOVED TRAILING EDGE BEAM IAW SRM 51-30-2 PAGE 1. INSTALLED TRAILING EDGE BEAM IAW SRM 55-10-6 FIG 1, 51-30-2 PAGE 1. (M)SDR 20000515AP012Seat Track · corrodedFOUND CABIN FLOOR SEAT TRACK SUPPORT BASE HAS CORROSION AT STATION 1020 THROUGH 1130 LBL 25. REMOVED CORROSION, OUT OF LIMITS STATION 990-1130. REMOVED AND REPLACED SEAT TRACK STATION 990-1130 IAW SRM 53-10-30 PATE 20, 51-10-2 PAGE 1. (M)SDR 20000515AP028Frame · crackedLEFT HORIZONTAL STABILIZER INNER COMPARTMENT NR 5 INBOARD RIB HAS SUPPORT CHORD CRACKED. CUT OUT SKIN TO GAIN ACCESS TO SUPPORT CHORD 3 INCH BY 6 INCH. REMOVED SUPPORT CHORD. FABRICATED AND INSTALLED SUPPORT CHORD. INSTALLED DOUBLER REPAIR TO SKIN CUT OUT SDR 20000515AP027Angle · crackedFOUND VERTICAL STAB INNER COMPARTMENT RIB NR 9 RIGHT STRINGER NR 9 CRACKED AT ATTACH BOLT. REMOVED CRACKED AREA. NDT AREA FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-4 FIG 1, 55-30-5 FIG 1. (M)SDR 20000515AP026Angle · crackedFOUND VERTICAL STABILIZER INNER COMPARTMENT NR 8 RIGHT STRINGER NR 8 CRACKED AT ATTACH BOLT. REMOVED CRACKED AREA. NDT AREA FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-4 FIG 1, 55-30-5 FIG 1. (M)SDR 20000515AP025Angle · crackedFOUND VERTICAL STAB INNER COMPARTMENT NR 6 RIGHT SUPPORT WEB BETWEEN STRINGER NR 8 AND NR 9 CRACKED AT LOWER CORNER. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED ANGLE IAW SRM 51-40-3 PAGE 7. (M)SDR 20000515AP014Intercostal · corrodedFOUND CABIN FLOOR INTERCOSTAL AT STATION 1110 THROUGH 1130 AT BL 0 HAS CORROSION AT UPPER AND LOWER SURFACE. REMOVED INTERCOSTAL. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-30-2 PAGE 6, 51-20-1 PAGE 4. (M)SDR 20000515AP013Seat Track · corrodedFOUND CABIN FLOOR SEAT TRACK STATION 1060 RBL 24 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK AT STATION 1060 RBL 24 IAW SRM 53-10-5 PAGE 3, 51-10-2 PAGE 2. (M)SDR CA990907069Filter · contaminated(CAN) ENGINE OIL TEMPERATURE INCREASED FOLLOWED BY OIL FILTER BYPASS. FILTER FOUND CARBON CONGESTED. ENGINE BEING MONITORED.
Back to Boeing 727-225