Boeing 727-2M7
Service difficulty reports · 459
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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 = '7272M7' 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 = '7272M7' 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 DHL2008F00024Bracket · crackedLT WING NR 1 KRUEGER FLAP ACTUATOR INBOARD AND OUTBOARD ATTACH BRACKETS ARE CRACKED IN THE CORNERS. REMOVED BRACKETS (2 EACH) IAW B727 SRM 51-30-2. FABRICATED BRACKETS WITH 2024-T3 .036 3.5" X 7.5" PO 9006767 IAW BOEING ENGINEERING DOCUMENT 65-16275 AND B72 SDR DHLA200700093Overheat Loop · misroutedNR 1 STRUT OVERHEAT LIGHT AFTER T/O PERFORMED NORMAL SHUTDOWN NR 1 ENGINE PER PROCEDURE. FOUND 4 DUCT CONNECTIONS LEAKING ON DUCT FROM PRECOOLER TO THE ENG. REMOVED AND REINSTALLED DUCTS PER 727 M/M 36-00-01 (DUCTS WERE MIS-ALIGNED) ALSO FOUND NR 1 PYLON OVESDR DHLA200700085Latch · lack of lubeFWD ENTRY DOOR WILL NOT LOCK IN OPEN POSITION. CLEANED AND LUBED FWD ENTRY DOOR LATCH ASSY. OPS CHECK NORMAL IAW AMM 52-11-01.SDR DHLA200700078Rudder Control · malfunctionedLOWER RUDDER MOVED ON ITS OWN FAR TO THE LEFT AS COMPARED WITH THE UPPER RUDDER AS SEEN ON THE RUDDER POSITION INDICATORS DURING TAKEOFF ROLL. ACFT PULLED TO THE LEFT, UPPER RUDDER IND FAR RT. TRANSFERRED RUDDER POS IND TO DMI 31029 PER MEL 27-8 CAT C DDD12-SDR DHL2007750505Skin · dentedWHILE AT FLIGHTSTAR FOR AN A CHECK DISCREPANCY FUSELAGE REPAIR HAS BLIND FASTENERS INSTALLED AT STA 1203 STR22R AND DOUBLER IS DENTED. REMOVED PREVIOUS REPAIR IAW B727SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER FROM 2024-T3 .063" PO NR 9005089 DIM 11 1/2" BY SDR DHL2007750504Door Frame · corrodedC2 DOOR LWR AFT FRAME CORRODED. REMOVED DOOR AFT CORNER AND DISPLACED WEB TO GAIN ACCESS IAW B727 SRM 51-30-2. CUT-OUT DAMAGED SECTION OF FRAME DIM 13 1/2" BY 6" IAW B727 51-10-1 AND 51-40-3 FIG 1. FABRICATED NEW FRAME SECTION FROM 7075-T6 .063" PO NR 90053SDR DHL2007750503Web · dentedDURING A CHECK DISCREPANCY, LT TORQUE BOX UPPER WEB HAS 2 DENTS AT APPROX STA 1243. CUTOUT DAMAGED AREA TWO 4" DIM IAW B727 SRM 51-40-2 FIG 1. FAB REPAIR DOUBLERS TWO 7075-T6 .040 PO NR 9005551 6.5"DIA AND 4 NUT PLATE CHANNEL DIA 1" BY 6" IAW B727 SRM 51-40SDR DHL2007750502Support Angle · crackedAFT AIRSTAIRS BS 1243 LT UPPER SUPPORT ANGLE CRACKED INSIDE OF TORQUE BOX. REMOVED CRACKED ANGLE IAW B727 SRM 51-30-2 FIG7. FABRICATED NEW ANGLE 7075-0 .063 PO NR 9005314 29 1/4" BY 4 3/4" IAW B727 SRM 53-10-2 FIG 6 AND 51-20-1. HEAT TREATED NEW PART TO 707SDR DHL2007750001Shear Tie · corrodedWHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR AN A CHECK.REFERENCE ASTAR N/RS 093661,093687 DISCREPANCY: PILLOWING AT FASTENERS ON FUSELAGE SKIN BS 700 BETWEEN STRINGER 25R-26R. REMOVED SHEAR TIE AT BS 700 BETWEEN S25R-26R. REMOVED CORROSION ON INNER SKIN MAT LOSSDR DHL200776201Skin · crackedWHILE COMPLYING WITH VISUAL INSPECTION NOTICED NR 6 LE SLAT SKIN AT THE OUTBOARD TRACK ATTACH AREA WITH TWO CRACKS IN CORNERS.SDR DHL2007750002Duct · leakingNR 1 FIRE HANDLE INTERMITTENTLY GOES OFF AFTER TAKEOFF. FOUND SIX STAGE DUCT LEAKING AT FIREWALL ABOVE FIRELOOP REMOVED AND REPLACED DEFECTIVE DUCTING IAW B727 M/M 36-00-01. PERFORMED ENG RUN NO LEAKS NOTED IAW ASTAR JRHCHPT 7. REMOVED AND REPLACED FIRE LOOSDR DHL2006750001Apu · malfunctionedLOST APU BLEED AIR DURING ENGINE NR 2 START. PERFORMED EMERGENCY START MALFUNCTION CHECKLIST. APU CONTINUED TO RUN "HOT" (640 DEGREES) IN STATIC CONDITION (NO LOAD). SHUT DOWN APU. HOT/BURNING SMELL IN COCKPIT, DISSIPATED FOLLOWING APU SHUTDOWN. TRANSFERSDR C7WA200600010Coupling · brokenFLIGHT RETURN: LOSS OF ALL B-SYSTEM HYDRAULIC FLUID AND QUANTITY. REPLACED BROKEN HYDRAULIC QUICK DISCONNECT COUPLING TO NR1 B-SYSTEM HYDRAULIC PUMP. SYSTEM OPERATIONAL AND LEAK CHECKS GOOD IAW MM. (K)SDR 2006750001Wing · crackedWING CRACKED, REMOVED AND REPLACED LEFT WING.SDR DHL2006750522Skin · debondedL/WING I/B FOREFLAP, I/B CLOSE OUT BROKEN W/UPPER SKIN DISBONDED AT I/B END. REMOVED PREVIOUS REPAIR AND FABBED FILLER APPROX 3 3/4 BY 8 1/2 DOUBLER APPROX 5 1/4 BY 10 1/4 FROM 2024 T3 .016 PO 9003142. CLEANED, PREPPED, PRIMED, BONDED, CLEANED, TREATED, ANDSDR DHL2006750521Skin · gougedFOUND L WING I/B AILERON UPPER SKIN IS GOUGED AT WS 410. CUT OUT DAMAGED AREA DIM 2X2 AND FABBED REPAIR DOUBLER FROM MAT USE 2024 T3 .04 PO 9003055 AND DIM 5 1/3 BY 4 IAW B727 SRM 57-50-2 FIG NR 7 AND 57-50-5 FIG 5. TREATED AND PRIMED IAW B727 SRM 51-10-2. SDR DHL2006750518Frame · dentedFOUND FRAME DENTED AT BS 700 STR 24 R. CUT OUT DAMAGED AREA SIZE 1 BY 3/4 ON FRAME STA 700 AT STR 24R IAW B727 SRM 51-10-1. FABBED REPAIR ANGLE FROM 7075-0 .063 SIZE 8 3/4 BY 3 1/2 PO 9002827 IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. HEAT TREATED TSDR DHL2006750517Frame · dentedFRAME DENTED AT BS 680 AT STR 24R. CUT OUT DAMAGED AREA SIZE 1 X 3/4 ON FRAME STA 680 AT STR 24R IAW B727 SRM 51-10-1. FABBED REPAIR ANGLE FROM 7075 .063 SIZE 8 3/4 X 3 1/2 PO 9002827 IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. HEATED TO 7075 T6 .063 SDR DHL2006570519Frame · dentedFOUND FRAME DENTED AT BS 720A STR 25R. CUT OUT DAMAGED AREA SIZE 1 BY 1 ON FRAME STA 720A AT STR 25R IAW B727 SRM 51-10-1. FABBED REPAIR ANGLE FROM 7075-0 .063 SIZE 8 3/4 BY 3 1/2 PO 9002827 IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. HEAT TREATED TO SDR DHL2006570516Skin · corrodedCORROSION BULGE LT WING UPPER SURFACE PANEL 10" FWD OF NR 6 SPOILER WS 300. CUT OUT DAMAGED AREA 4 BY 2 1/2 IAW B727 SRM 51-10-1. FABBED DOUBLER FROM 2024 T3 .050 PO 53081 SIZE 9 BY 4 1/2 AND FILLER FROM 2024 T3 .080 PO 9002727 SIZE 1 BY 3 3/4 AND 2ND FILLERSDR DHL2006750513Skin · dentedLT T/E SIDE OF UPPER RUDDER DENTED AT RUDDER TAB COURT (2ND FROM BOTTOM). FOUND DENT TO BE OUT OF LIMITS, ROUTED OUT DAMAGED AREA SIZE 3/8 BY 3/4 IAW B727 SRM 51-10-01. FABBED DOUBLER FROM 2024 T3 SIZE 4 BY 6 PO 9002416 IAW B727 SRM 51-40-2 FIG 3. TREATED SDR DHL2006750512Web · bentVERT STAB FWD TENSION TIE SUPPORT WEB BENT/STRESSED RT SIDE. REMOVED SUPPORT WEB ON VERT STAB FWD TENSION TIE RT SIDE IAW B727 SRM 51-30-2. FABBED WEB FROM 7075 T6 .032 SIZE 24 1/4 BY 6 PO 9002507 IAW B727 SRM 51-20-1 AND SRM 55-30-2. TREATED AND PRIMED PARSDR DHL2006570514Skin · crackedL/WING INB FLAP, REAR SPAR LOWER CORE SHOWS CRACK AT INB AFT FLAP ACTUATING ROD CUT OUT. CUT OUT DAMAGED AREA AND FABBED REPAIR ANGLE FROM BAC 1503 100046 PO 617555 DIM 46 BY 2 AND SPLICE FROM BAC1503-100046 PO 617555 DIM 10 BY 2 IAW B727 SRM 51-40-4 FIG 1. SDR DHL2006750515Skin · gougedRT WING OTBD FORE FLAP LEADING EDGE IS GOUGED AT WBL 442. CUT OUT DAMAGED AREA DIM 1 5/8 BY 1, FABBED REPAIR DOUBLER FROM 2024T3 .063 PO 9003110 DIM 4 1/16 BY 4. TREATED PRIMED AND INSTALLED DOUBLER IAW B727 SRM 57-50-4 FIG 1 51-10-2 AND 51-30-2.SDR DHL2006750508Torque Box · crackedTORQUE BOX FIN REAR SPAR CHORD LWR LT SIDE APPEARS TO BE CRACKED PASSED STOP DRILL HOLE STA BS 1303 LBL 22. C/W HFEC ON BS 1303 FRAME WEB IAW B727 NDTM PT6 51-00-00 FIG 23. FOUND 1/4" CRACK EXTENDING FROM PREVIOUS STOP DRILL HOLE. TOTAL CRACK LENGTH 1". NOSDR DHL2006750509Skin · gougedNR 6 SLAT TRAILING EDGE IS GOUGED AT OUTBD HOOK. ROUTED OUT GOUGE .200 RADIUS BY 6" AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 2. FABBED REPAIR DOUBLER FROM 7075 T6 A125 PO5096301 DIM 8 1/2 BY 3 1/2 IAW B727 SRM 57-50-3 FIG10. TREATED AND PRIMESDR DHL2006750511Beam · crackedSTA 1183 BULKHEAD VERTICAL BEAM IS CRACKED AT AFT FLANGE INBD AND OUTBD SIDE RBL 36. STOP DRILLED 2 CRACKS IAW S/B 727-53-0192 REV 1 DATED MAY 30 1991. REMOVED GILLINER SUPPORT STRUCTURE FOR ACCESS IAW S/B 727-53-0192 REV 1 DATED MAY 30 1991. LOCATED AND DRSDR DHL2006750510Skin · dentedNR 6 SLAT UPPER SKIN IS DENTED AT WING STA 560. FOUND DENT TO BE OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 2. REMOVED 2 RIBS FOR ACCESS AND CUT OUT DAMAGE AREA SIZE 2 1/4 BY 3 1/2 IAW B727 SRM 51-30-2 AND 57-50-3 FIG 1. FABBED DOUBLER FROM 2024 T3 .080 SIZE 7 SDR DHL2006750507Structure · dentedFOUND C2 DOOR FWD LWR END DENTED. REMOVED C-2 DOOR LWR FWD CORNER DEPRESSOR IAW B727 SRM 51-30-2. LOCATED AND DRILLED HOLES IAW B727 SRM 51-30-2 FIG NR 2. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW PART IAW B727 SRM 51-30-1 FIG NR 8, PN 65-5994SDR DHL2006750506Support Bracket · crackedNR 1 LE FLAP ACTUATOR TRUNNION SUPPORT BRACKET IS CRACKED OUTBOARD END. CONFIRMED CRACK. REMOVED SUPPORT BRACKET AT NR 1 L/E FLAP ACTUATOR TRUNNION OUTBOARD END FABBED NEW SUPPORT BRACKET FROM 7075 T6 .040 PO 9002590 DIM 8 1/8 BY 3 3/4 AND TREATED PRIMED ANDSDR DHL2006750505Stiffener · crackedFOUND LEFT WING REAR SPAR VERTICAL STIFFENER AT WS 546 INB OF NR 2 SPOILER FITTING SUPPORT IS CRACKED FROM BOTTOM END. REMOVED AND REPLACED L WING REAR SPAR VERT STIFFENER AT WS 546 I/B OF NR 2 SPOILER FITTING SUPPORT IAW B727 SRM 51-30-2, LEAK CHECK GOOD IAWSDR DHL2006750504Frame · corrodedAFT CARGO COMPT FRAME ANS SHEAR TIE ARE CORRODED WITH EXFOLIATION AND BROKEN FASTENERS AT STA 1166 BETWEEN STR 28L AND 28R. REMOVED AUX STRUCTURE FROM STA 1166 BULKHEAD IAW B727 SRM 51-30-2, CLEANED AREA AND REMOVED CORROSION, FOUND OUT OF LIMITS, MATL.LOSS .SDR DHL2006750503Skin · corrodedAFT CARGO COMPARTMENT, VHF ANTENNA DOUBLER HAS HEAVY CORROSION BETWEEN STR 30-29R, BETWEEN STA 1030-1050. REMOVED VHF ANTENNA AND DOUBLER BETWEEN STR 30-29R, AT STA 1030-1050 IAW B727 SRM 51-30-2. FOUND FUSE CORRODED, CUT OUT DAMAGED AREA, SIZE 2 X 3.5 INCHESDR DHL2006750502Hinge · crackedMAIN CARGO DOOR AFT END HAS ONE LOBE CRACKED. REMOVED AFT HINGE SECTION AT MAIN CARGO DOOR IAW AEI M/M CHAPTER 52 REV.F DATED JANUARY 22,2001. FABRICATED AFT HINGE SECTION, MAT USED MS20001-16-72 PO 9002527 IAW AEI M/M CHAPTER 52 REV.F DATED JANUARY 22,2001.SDR DHL2006750501Rib · crackedR/W L/E STA171 PANEL SUPPORT RIB CRACKED AT LIGHTING HOLE. REMOVED DAMAGED RIB AT R/W L/E STA 171, O/B OF DEFUEL VALVE IAW B727 SRM 51-30-2. FABRICATED RIB FROM 2024-T3 0.40 SIZE 15" BY 7" PO 9002715, IAW B727 SRM 51-20-1, AND SRM 57-20-2. TREATED AND PRIMESDR C7WA200500116Indicator · inoperativeNOSE LANDING GEAR DOWN AND LOCKED INDICATOR LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. FOLLOWED ABNORMAL PROCEDURES, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NOSE LANDING GEAR GREEN LIGHT ASSEMBLY PER MM 33-10-51. OPS CHECKS GOOD. (M)SDR C7WA200500115Wire · shortedAIR TURNBACK, NR 3 ENGINE FIRE DETECTOR INOPERATIVE LIGHT ILLUMINATED AND NR 3 ENGINE FIRE WARNING LIGHT AND BELL WENT OFF REPEATEDLY 7 TIMES. FOUND NR 3 ENGINE B-LOOP WIRE SHORTED. REPAIRED WIRE PER B727 MM 20-00-00. OPS CHECKS GOOD PER 26-11-01. (M)SDR C7WA200500117Transponder · inoperativeFLIGHT RETURN, NR 2 TRANSPONDER FAILED DURING FLIGHT. RETURNED TO KDAY PER ATC REQUEST. REMOVED AND REPLACED TRANSPONDER OPERATIONAL CHECKS GOOD PER B727 MM 34-43-10. (M)SDR DHL2005750004Servo · inoperativeCRUISE TRIM INOP NOSE DOWN. STAB TRIM INOP NOSE DOWN BELOW '0'. NO ABNORMAL APPLICABLE, RETURN TO SAN. RII REQUIRED. REMOVED AND REPLACED A/P STAB TRIM SERVO IAW B727 M/M 22-11-21. INSP ALL WIRING AND CONN ON STAB SERVO AND MAIN ELEC ACTUATOR AND JACKSCREWSDR DHL2005750003Indicator · malfunctionedPRIOR TO REACHING RUNWAY NR 3 OIL PRESS. WAS 25 PSI.REFERED TO ABNORMAL PROCEDURE AND SHUT DOWN ENGINE. R & R NR 3 OIL PRESSURE INDICATOR OPS CHECK GOOD WITH ENGINE RUN IAW ASTAR JRH 5.2 & MM CH 79-32-0.SDR C7WA0500109Line · looseAIR TURNBACK: ENGINE SHUTDOWN, NR 1 ENGINE OIL FILTER BYPASS LIGHT CAME ON AT 8000 FT, DURING CLIMB OUT. COMPLETED PRECAUTIONARY SHUTDOWN CHECKLIST. DURING INSPECTION OF NR 1 ENGINE, FOUND LOOSE LINE B-NUT AT OIL PRESSURE SWITCH. TIGHTENED B-NUT. OPERATIOSDR C7WA200500109Connector · looseAIR TURNBACK; ENGINE SHUTDOWN, NR 2 EGT FLUCTUATES AT FLIGHT LEVEL 27,000. OIL PRESSURE DROPPED TO ZERO, OIL QUANTITY FOLLOWED TO ZERO. DURING INSPECTION OF NR 2 ENGINE FOUND INLET CASE TUBE CONNECTOR ASSEMBLY LOOSE AND LEAKING. TIGHTENED LOOSE BOLTS. LEASDR DHL2005750002Uplock Sensor · out of adjustIN MODERATE CHOP AUDIBLE THUMP FROM NOSE GEAR WITH ASSOCIATED INTERMITTENT NOSE GEAR LIGHT ILLUMINATED. PLACING GEAR HANDLE UP MADE INDICATIONS NORMAL IF GEAR HANDLE REMAINED UP. JACKED NOSE GEAR PER MM 7-11-0-4A. PERFORMED NOSE GEAR OPERATIONAL CHECK PER MSDR DHL2005750001Switch · inoperativeLATCHES UNLOCKED LIGHT ON CARGO DOOR PANEL OUT WITH DOOR OPEN. REMOVED AND REPLACED Q-TUBE LATCH LOCK SWITCH IAW B-727-200 FRIEGHTER M/M CHAPTER 24 PG 28, 29. P/N 914CE1-3 INSTALLED, OPS CHECK SERVICEABLE.SDR 2005F00010Attach Fitting · damagedPORK CHOP FITTING RT MLG DAMAGED AND MISALIGNED.SDR 2005F00013Attach Fitting · deformedRT WING LG TRUNNION HALVES BENT AND GOUGED.SDR 2005F00012Rib · damagedOUTBOARD RT WING RIBS DAMAGED.SDR 2005FA0000007Bulkhead · gougedRIGHT STA 950 BULKHEAD GOUGED.SDR 2005F00011Attach Fitting · gougedRT MAIN LANDING GEAR TRUNNION ATTACH HOLES DAMAGED AND GOUGED.SDR 2005F00014Beam · gougedRIGHT WING MAIN LANDING GEAR SUPPORT BEAM GOUGED AND CORROSION.
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