Boeing 727-2Q9
Service difficulty reports · 830
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 = '7272Q9' 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 = '7272Q9' 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 DHL2005740018Seat Track · damagedMAIN CABIN SEAT TRACK BS 344 TO 480 LBL 24.75 DAMAGED. REMOVED AND REPLACED SEAT TRACK AT BS 344 TO BS 480 LBL 24.75 AND FABRICATED NEW SEAT TRACK P/N BAC1520-792 PO NR 9001465 DIM. 12 FT IAW B727 SRM 53-10-2 FIG1 AND 51-30-5 AND DWG NR 2902 VENTURA AEROSPACESDR DHL2005740017Floorbeam · corrodedMAIN CABIN FLOORBEAM TEE CAP DAMAGED AT BS 344 RBL 65.5 TO LBL 65.5. REMOVED AND REPLACED TEE CAP BS 344 RBL 65.5 TO 65.5 FROM P/N BAC1505-29222 PO NR 9001043 DIM 12 FT IAW B727 SRM 53-10-2 FIG 6, 51-30-5 AND DWG NR 2902 VENTURA AEROSPACE. TREATED AND PRIMEDSDR DHL2005740016Seat Track · damagedMAIN CABIN SEAT TRACK BS 344 TO 480 RBL 24.75 DAMAGED. REMOVED AND REPLACED NEW SEAT TRACK AT BS 344 TO BS 480 RBL 24.75 AND FABRICATED NEW SEAT TRACK P/N BAC1520-792 PO NR 9001767 DIM 12 FT IAW B727 SRM 53-10-2 FIG 1 AND 51-30-5 AND DWG NR 2902 VENTURA AEROSSDR DHL2005740015Seat Track · damagedMAIN CABIN SEAT TRACK BS 344 TO BS 480 RBL 45.5 DAMAGED. REMOVED SEAT TRACK FROM BS 344 TO 480 RBL 45.5 IAW B727 SRM 51-30-2. FABRICATED NEW SEAT TRACK P/N BAC1520-792 PO NR 9001329 DIM. 12 FT IAW B727 SRM 53-10-2 FIG 1 AND 51-30-5 AND DWG NR 2902, TREATED ASDR DHL2005740005Structure · dentedRT WING INBD AILERON TAB IS DENTED ON LOWER SURFACE WING STA 430 WBL 269. CUT OUT DENT AT RT WING INBD AILERON TAB LOWER SURFACE APPROX 1 INCH DIA. FABRICATED FILLER APPROX 1 INCH DIA AND DOUBLER APPROX 3 INCH DIA FROM .010 2024T3 PO NR 9912184, BONDED, CURESDR DHL2005740014Skin · delaminatedRT WING OB AILERON TAB IS DELAMINATED AT OB EDGE. CUT OUT DELAMINATED AREA AT RT WING OB AILERON TAB, FABRICATED FILLER AND DOUBLER, BONDED FILLER AND DOUBLER, CURED, CLEANED, PRIMED AND SEALED IAW B727 SRM 57-50-2 AND 51-40-20 FIG 30.SDR DHL2005740524Hinge · crackedFWD AND AFT SECTIONS OF MCD HINGE CRACKED. REMOVED AND REPLACED FWD AND AFT SECTIONS OF MAIN CARGO DOOR HINGE IAW S/B AEI01-01 REVB 10-26-01 P/N MS 2001-16-7200 PO NR 900733 DIM 6FT FWD AND AFT P/N MS 2001-16-7200 PO NR 90002150 DIM 6FT.SDR DHL2005740013Angle · crackedNOSE WW STA 259 LBL 3 L-ANGLE IS CRACKED ABOVE PRESSURE PANELS. REMOVE ANGLE AT NOSE WW STA 259 LBL 3 IAW B727 SRM 51-30-2. FABRICATED NEW ANGLE REPAIR MAT. USED 2024T3 .040 PO NR 9001938 DIM 7" BY 1 1/2" IAW B727 SRM 51-20-1 AND 53-10-2 FIG 1. ALODINED ANDSDR DHL2005740006Skin Panel · delaminatedRT WING LOWER TE PANEL AT WING STA 190 WBL 90 IS DELAMINATED ON UPPER SURFACE, BELOW APU EXHAUST DUCT. REMOVED RT WING LOWER TE PANEL AT WING STA 190 RBL 90 IAW B727 SRM 51-30-2. CUT OUT DELAMINATED AREA OF UPPER SURFACE APPROX 6" BY 8". REMOVED INSERTS ANSDR DHL2005740565Skin · dentedVERT STAB ABOVE RT FIN STA 133 LOWER RUDDER SURF IS DENTED NEAR T/E. EVALUATED DENTED AREA AT VERT STAB ABOVE RT FIN STA 133 LOWER RUDDER SURF TRIM OUT DAMAGED SKIN SIZE 1/2" BY 3/4" IAW B727 SRM 55-30-3 AND 51-10-1. FABRICATED DOUBLER REPAIR SIZE 2" BY 2.5"SDR DHL2005740562Skin · crackedL/WING T/E UPPER SURFACE CRACKED AT NR 4 SPOILER HINGE CUTOUT (NR3). REMOVED FASTENER AT L/WING T/E UPPER AT NR 4 SPOILER HINGE CUTOUT NR 3 IAW B727 SRM 51-30-2, STOP DRILL CRACK .250 TERMINATED AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIRSDR DHL2005740523Torque Box · crackedRT AFT AIRSTAIR TORQUE BOX AT VENTRAL STAIR ACTUATOR SUPPORT REPAIR IS CRACKED AND DAMAGED AND WEB IS IMPROPERLY INSTALLED BS 1253 TO 1273. REPAIRED RT AFT AIRSTAIR TORQUE BOX AT VENTRAL STAIR ACTUATOR SUPPORT AND WEB BS 1253 TO 1283 IAW S/B 727-53-0129 REV 5SDR DHL2005740522Skin · dentedNR 1 SLAT EXTERNAL SKIN DENTED AT W STA 738. REMOVED PANELS AND WEB FROM SLAT NR 1 FOR ACCESS. CUTOUT DAMAGED AREA FROM EXT SKIN 3.25 INCH BY 3.125 INCH, TRIMMED OUT SKIN AND ACCESS TO DOUBLER IAW SRM. FAB PARTS FILLER 3 .125 INCH BY 3.0625 MAT 2024 2024 T3SDR DHL2005740516Support Angle · crackedLEFT WING ROOT FIXED LEADING EDGE HAS LOWER ANGLE SUPPORT CRACKED L/E STA 130. REMOVED FASTENERS FOR ACCESS AT LEFT WING ROOT FIXED EDGE L/E STA 130 STOP DRILLED CRACK .250 TERMINATED AT END OF CRACKED IAW B727 SRM 51-10-1 NDT HFEC INSP PER B727 NDT MAN PT6 5SDR DHL2005740012Rib · crackedNR 4 SLAT CRACKED AT ACTUATOR I/B RIB. REMOVED NR 4 SLAT TO FOM SHEET METAL REPAIR IAW B727MM 27-81-11, REMOVED ACCESS PANEL IAW B727 SRM 51-30-2, REMOVED FASTENERS FOR REPAIR AND RIBS IAW B727 SRM 51-30-2, FABRICATED NEW RIBS I/B AND O/B MAT USED 2024T3 .040SDR DHL200574011Skin · damagedNR 1 SLAT EXTERNAL SKIN DENTED AT WING STA 738. REMOVED PANELS AND WEB FROM SLAT NR 1 FOR ACCESS IAW B727 SRM 51-30-2 CUT OUT DAMAGE AREA FROM SKIN. TRIMMED OUT SKIN TO ACCESS DOUBLER IAW B727 SRM 57-30-3. FABBED FILLER. DOUBLER 3 PIECES IAW B727 SRM 57-50SDR DHL2005740010Rib · damagedNR 4 SLAT CRACKED AT ACTUATOR IB RIB. REMOVED NR 4 SLAT TO FOM SHEET METAL REPAIR IAW B727 MM 27-81-11. REMOVED ACCESS PANEL IAW B727 SRM 51-30-2. REMOVED FASTENERS FOR REPAIR AND RIBS IAW B727 SRM 51-30-2. FABRICATED NEW RIBS IB AND OB MAT USED 2024T3 .04SDR DHL2005740009Skin · damagedLT WING TE UPPER SURFACE CRACKED AT NR 4 SPOILER HINGE CUT OUT (NR2). REMOVED NR 4 SPOILER TO FACILITATE S/M WORK IAW B727 MM 27-62-1. REMOVED FASTENERS AT LT WING TE UPPER AT NR 4 SPOILER HINGE CUT OUT NR 2 IAW B727 SRM 51-30-2. STOP DRILLED CRACK .250 TERSDR DHL2005740008Skin · dentedLT WING OB AILERON UPPER SURFACE HAS DENT WBL 490. REMOVED FASTENER AND CUT OUT DAMAGED AREA IAW B727 SRM 51-30-2 AND 57-50-5. FABBED DOUBLER AND FILLER IAW B727 SRM 57-50-51 AND 57-50-2. TREATED, PRIMED, AND INSTALLED DOUBLER AND FILLER AT L/WING OB AILEROSDR DHL2005740004Skin · damagedMAIN CARGO DOOR INNER SKIN DAMAGED (INTERNAL) AFT SECTION. REMOVED INNER SKIN IAW B727 SRM 51-30-2, LOCATED AND DRILLED INNER SKIN P/N AE727-1-032A-17 PO NR 508028 IAW DWG NR AE727-1-032A LTR "A" 4-28-99 AERONAUTICAL ENGINEER INC. TREATED AND PRIMED HOLES ANSDR DHL2005740003Skin · damagedMAIN CARGO DOOR INNER SKIN DAMAGED (INTERNAL) FWD SECTION. REMOVED INNER SKIN IAW B727 SRM 51-30-2, LOCATED AND DRILLED INNER SKIN P/N AE727-1-032A-17 PO NR 508028 IAW DWG NR AE727-1-032A LTR A 4-28-99 AERONAUTICAL ENGINEERS INC. TREATED AND PRIMED HOLES ANDSDR DHL2005740007Skin · crackedFWD ENTRY DOOR LOWER CUT OUT SKIN CRACKED. CRACKED CONFIRM BY HFEC NDT. REMOVED FASTENERS PER ACCESS AND CUT OUT DAMAGE AREA (DIM. 2.5 BY 1.5) IAW S/B 727 53A0198. ACCOMPLISHED NDT HFEC AROUND CUT OUT NO CRACKS NOTED IAW B727 NDT MAN. PART 6 51-00-00. FABBSDR DHL2005740548Frame · damagedREMOVED PREVIOUS REPAIR FUSELAGE FRAME BS 580 STR 16R AND 17R IAW B727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MAT USED 7075T6 .071 PO 9001737 DEM 6" BY 5" IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. ALODINED AND PRIMED AREA AND PART IAW B727 SRM 51-40-2.SDR DHL2005740510Structure · delaminatedCUT OUT DELAMINATED AREA AT RT WING OUTBOARD AILERON TAB APPROX 1 X 1 INCH, FABRICATED FILLER APPROX 1 X 1 X 1 INCH AND DOUBLER APPROX 2.5 X 3 INCH FROM .010 INCH 2024T3 PO9912184 BONDED FILLER AND DOUBLER, CURED, CLEANED, PRIMED AND SEALED IAW B727 SRM 57-50-SDR DHL2005740002Cover · dislodgedAFT EMERGENCY LIGHT COVER FELL OFF ON CLIMBOUT. RESECURED LIGHT ASSY AND OPS CHECKED GOOD IAW MM 33-50-01.SDR DHL2005741002Control Handle · malfunctionedAFTER TAKEOFF GEAR HANDLE WOULD NOT GO UP PAST OFF. PERFORMED ABNORMAL CHECKLIST, RAISED GEAR CONTINUED TO CVG WITHOUT FURTHER INCIDENT. PERFORM OPS CHECK OF LANDING GEAR CONTROL HANDLE PER B727 MM 32-31-11, OPS NORMAL. NO DEFECTS NOTED.SDR DHL2005740001Handle · looseOUTSIDE HANDLE ON FORWARD ENTRY DOOR SOMETIMES MOVES OUT INTO SLIPSTREAM AND ROTATES WHILE EN ROUTE. STOWED OUTSIDE HANDLE PER MM 52-11-01, OPS CHECK GOOD.SDR DHL2005741001Warning Light · illuminatedNR 3 THRUST REVERSER LIGHT ILLUMINATED PRIOR TO TAKEOFF ROLL PER ASTAR SAFETY REPORT. CREW CYCLED REVERSER SEVERAL TIMES AND RAN ENGINE UP. REVERSER LIGHT DID NOT COME ON AGAIN.SDR DHL2004741011Fire Loop · inoperativeDURING THE ENGINE FIRE PROTECTION TEST, FOUND NR 3 ENGINE SYS "B" LIGHT WON'T COME ON SYS "A" LT OK. FIRE DETECTION SYS ON NR 3 ENGINE SYS "B" DEFERRED IAW MEL 26-6 SYS "A" WORKS OK PLACARD INSTALLED CTRL NR 18526. WORKING DMI (18526) NR 3 ENGINE FIRE DET SSDR DHL2004741010Overheat Loop · malfunctionedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED CLIMBING THROUGH FL 160. RAN ABNORMAL PROCEDURE. RETURNED TO IAH. A/C SHUT DOWN AFTER LANDING AND TOWED TO PARKING. FOUND LT AFT BODY FIRE LOOP BREAKING DOWN DURING OPERATION OF ENGINES & SYSTEMS. REMOVED AND REPLSDR DHL2004741009Fire Loop · shortedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING DEPARTURE RAN ENTIRE ABNORMAL PROCEDURE TWICE LIGHT EXTINGUISHED ON RETURN TO IAH NR 2 THRUST LEVER AT IDLE FOR ENTIRE DECENT. FOUND SCREW TOUCHING FIRE LOOP IN AFT AIRSTAIR AREA LT SIDE REPOSITIONED FIRE LOOP,SDR DHL200474006Web · corrodedDURING A-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED. NOSE SECTION LWR LOBE INTERIOR BS 312 AND RT SIDE HORIZONTAL WALKING BEAM. CORROSION AT FRAME ATTACH CLIP; CUT OUT DAMAGED WEB SECTION (ATTACH CLIP) AT STA.312 AT HORIZ WALKWAY BEAM RT SIDE IAW SRM 51-SDR DHL200474005Spar · corrodedDURING AN (A) CHECK, INTERIM REPAIR INSTALLED ON LT WING STA.137.8 LOWER FRONT SPAR CHORD PLATE. REMOVED INTERM REPAIR AND TRIMMED OFF 3.7500 INCH IB END SECTION OF LT WING FRONT SPAR LWR CHORD PLATE FROM WS 136.00 T0 139.75 DUE TO CORROSION DAMAGE BEYOND ALLSDR DHL2004741007Light · inoperativeEMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR WON'T ILLUMINATE WITH LIGHT SWITCH ON THE PILOTS OVERHEAD PANEL TO ON. HOWEVER, POSITION THE SWITCH ON THE LIGHT ASSEMBLY TO ON AND LIGHT WORKS. REPLACED LIGHT ASSEMBLY AND TESTED GOOD PER M/M 33-50-00 PAGE 501.SDR DHL2004741006Door · out of adjustAT 260 MACH .78 A THUMPING NOISE WAS HEARD IN THE NOSE GEAR AREA ACCOMPANIED WITH RED DOORS LIGHT AND YELLOW NOSE DOOR LIGHT S/O'S PANEL ILLUMINATED. COMPLETED ABNORMAL, GEAR HANDLE MOVED TO UP POSITION THUMPING NOISE STOPPED. ADJUSTED NOSE GEAR WHEEL WELL DOSDR DHL2004741005Door · out of adjustON CLIMB OUT AT 330 KIAS A RATTLING SOUND CAME FROM THE NOSE GEAR AREA ACCOMPANIED BY RED (DOORS) LIGHT ON F/O'S PANEL AND (NOSE GEAR DOOR) LIGHT ON S/O'S PANEL. LIGHTS CYCLED ON AND OFF RAPIDLY IN SYNCHRONIZATION WITH THE BANGING SOUND. CREW PERFORMED THE (LASDR DHL2004740006Skin · crackedLOWER SURFACE OF NR 6 SPOILER PREVIOUS REPAIR CRACKED. REPLACED NR 6 SPOILER PANEL OPS CHECKED NORMAL IAW B727 M/M 27-60-0.SDR DHL2004740005Spar · damagedPER DER RECOMMENDATION, INSTALLED DOUBLER REPAIR'S AS REQ AT LWS 198, FWD SPAR, LOWER CHORD PLATE IAW AERONAUTICAL SOLUTIONS REPORT 04-004IK. FABRICATED REPAIR DOUBLER & TRIPLER, TREATED & PRIMED, AND INSTALLED PER AERONAUTICAL SOLUTIONS REPORT 04-004IR, DATESDR DHL2004740004Channel · corrodedCORROSION ON CHANNEL LOCATED IN RIGHT-HAND LEADING EDGE WING WELL STA 220 THRU STA 224. REMOVED DAMAGE, INSTALLED MINOR EXTRUDED REPAIR IAW B-727 SRM 51-40-4.SDR DHL2004740003Spar · corrodedSMALL AREA OF EXFOLIATION CORROSION AT FORWARD SPAR WING WELL STA 198 TO 210 LEFT-HAND WING. REMOVED CORROSION AT LEFT WING FORWARD LOWER CHORD. TREATED AND PRIMED PER B-727 SRM 51-10-6 & 51-10-2, MATERIAL REMOVED LESS THAN .080 CROSS SECTIONAL AREA REDUCED SDR DHL2004741004Intercostal · corrodedLT MLG WW SURFACE CORROSION AT STA 740 APPROXIMATELY INTERCOSTAL AREA OUTBOARD FUEL SHROUD. REMOVED SURFACE CORROSION APPROXIMATELY .001 INCH, WITHIN LIMITS. TREATED AND PRIMED WITH ZINC CHROMATE IAW SRM 51-10-6.SDR DHL2004741003Intercostal · corrodedSURFACE CORROSION AT RT MLG STA 740 THRU 760 OUTBOARD OF FUEL SHROUD UPPER INTERCOSTAL. REMOVED SURFACE CORROSION, APPROXIMATELY .001 INCH, WITHIN LIMITS. TREATED AND PRIMED WITH ZINC CHROMATE IAW SRM 51-10-6.SDR DHL2004740002Line · leakingB-SYSTEM BOTH LOW PRESSURE LIGHTS ILLUMINATED AT START OF TAKEOFF ROLL. PRESS DROPPED 200 LBS. OPENED BRAKE INTERCONNECT A-SYSTEM DROPPED TO 1 GALLON INTERCONNECT. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE NR 2 B-PUMP REF M/M 20-10-12, NO LEAKS NOTED. PSDR DHL2004741002Mount · crackedNR 6 LEADING EDGE K-FLAP ACTUATOR MOUNT ON SPAR APPEARS TO BE CRACKED AT INBOARD SIDE AT BASE OF TRUNNION CAP. REMOVED NR 6 LEADING EDGE K-FLAP ACTUATOR ASSEMBLY TO FOM. REMOVED INBOARD VERTICAL WEB SECTION OF NR 6 K-FLAP ACTUATOR MOUNT BOX, FABRICATED REPLASDR DHL2004740001Handle · lack of lubeMAIN ENTRY DOOR HANDLE DOESN'T WANT TO STAY FLUSH. LUBED HANDLE ASSEMBLY AND STOWED REF M/M 52-11-01.SDR DHL2004741001Switch · dirtyWITH GEAR HANDLE IN NEUTRAL RED DOORS LIGHT ILLUMINATED AND RT GEAR DOOR LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE, AND PLACED GEAR HANDLE IN UP POSITION. LIGHTS EXTINGUISHED. CLEANED RT GEAR DOOR SWITCH WITH CONTACT CLEANER. OPEN AND CLOSED DOOR SEVSDR DHL2003740009Control Valve · malfunctionedRTO - AIRCRAFT WEIGHT 143.1, AIRSPEED 5 KTS, OAT 01C, PRESSURE ALTITUDE 900 FT, BRAKE ENERGY CHART - NORMAL. BRAKES WOULD NOT RELEASE WITH 85 PERCENT N1 ON ALL 3 ENGINES FOR APPROX 6 SEC. AFTER REPLACING AUTO BRAKING CONTROL VALVE BRAKING OPS CHECKED GOOD. SDR DHL2003740007Bulb · burned outRTO DUE TO LOSS OF RIGHT MAIN GEAR DOWN & LOCKED INDICATION. REPLACED TWO BULBS, OPS CHECKED GOOD. T.O.W 159.6, IAS O K.T.S, O.A.T 8 C, BRAKE ENERGY ZONE - NORMAL. RELAMPED INDICATOR LIGHT IAW M/M 33-10-51, OPS CHECKED NORMAL.SDR DHL2003741012Structure · crackedLT WING INBOARD AFT FLAP HAS 3 INCH CRACK AT L/E. REMOVED AND REPLACED AFT FLAP ASSEMBLY IAW B727-200 M/M CHAPTER 27-51-02. OPS CHECK REQUIRED. PERFORMED OPS CHECK IAW B727-200 M/M CHAPTER 27-51-02. OPS CHECKED GOOD.SDR DHL2003741011Door · bindingDURING FLIGHT COCKPIT ENTRY DOOR BECOMES DIFFICULT TO OPEN. DOOR RUBS AGAINST DOOR JAMB. PROBLEM SEEMS TO IMPROVE AFTER AIRCRAFT IS ON THE GROUND, BUT STILL RUBS THE DOOR JAMB A LITTLE. CLEANED EXCESS PAINT FROM DOOR JAMB. LUBED DOOR AND LATCH ASSEMBLY PER
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