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 DHL2007740516Intercostal · crackedFWD PIT BETWEEN STA 680 AND STA 700 INTERCOSTAL AT LT STR 26 IS CRACKED AT TOP EDGE. REMOVED CRACKED INTERCOSTAL IAW SRM 51-30-2 AND FABRICATED A NEW INTERCOSTAL FROM 7075-T6 .050 PO NR 9004940, DIM 10.75" BY 9" IAW 727 SRM 51-20-1 AND 53-10-2 FIG 3. TREATEDSDR DHL2007740515Intercostal · damagedFWD PIT BS 683 BETWEEN STR'S 27R AND 28R INTERCOSTAL HAS 2 HOLES NEARBY 2 RIVETS. REMOVED INTERCOSTAL IAW 727 SRM 51-30-2. FABRICATED NEW INTERCOSTAL USING 7075-T6 .032 PO NR 9004940 DIM 18.50" BY 5.50" IAW 727 SRM 53-10-2 FIG 3. ALODINED AND PRIMED AND REISDR DHL2007740514Frame · corrodedAFT CARGO BS 1130 BETWEEN STR'S 27R AND 29L, FRAME HAS BARE METAL AND CORROSION. CORROSION REMOVAL OUT OF LIMITS PER B727 SRM 53-10-1 FIG 1. REMOVED AND FABRICATED 4 SHEAR TIE ANGLES FROM 7075-T6, .063" BY 6" BY 2.5" ( 4 EACH), PO NR 9004690. TREATED, PRIMSDR DHL2007740520Frame · corrodedWHILE IN "C" CHECK, AFT CARGO BS 1070 STR 28L-29L FWD FRAME FLANGE HAS CORROSION. REMOVED CORROSION IAW B727 SRM 51-10-6. REMOVED FASTENERS TO GAIN ACCESS TO AREA IAW B727 SRM 51-30-2. ORIGINAL MAT .063 IAW B727 SRM 53-10-2 FIG 5, MAT LOSS .008, REMAINING MASDR DHL2007740524Stringer · corrodedWHILE IN "C" CHECK, AFT CARGO COMPARTMENT, STRINGER 27L BETWEEN STA 950F AND 970 HAS CORROSION AROUND FASTENERS. REMOVED FASTENERS TO GAIN ACCESS IAW B727 SRM 51-30-2. REMOVED CORROSION IAW B727 SRM 51-10-6, CORROSION FOUND OUT OF LIMITS IAW B727 SRM 53-10-1SDR DHL2007740525Stringer · corrodedWHILE IN "C" CHECK, AFT CARGO COMPARTMENT, STRINGER 27L BETWEEN STA 950F AND 970 HAS CORROSION AROUND FASTENERS. REMOVED FASTENERS TO GAIN ACCESS IAW B727 SRM 51-30-2. REMOVED CORROSION IAW B727 SRM 51-10-6, CORROSION FOUND OUT OF LIMITS IAW B727 SRM 53-10-1SDR DHL2007740523Shear Tie · corrodedWHILE IN "C" CHECK, FWD PIT SKIN UNDER SHEAR TIE AT BS 580 BETWEEN STR 28L AND 28R IS GOUGED AND CORRODED. CUTOUT AREA AT BS 580 BETWEEN STR 28L AND 28R DIM 1"BY 5 1/2" IAW B727 SRM 53-30-3 FIG 1. FABRICATED DOUBLER FROM 2024T3 .100 PO NR 9005138 DIM 14 1/2"SDR DHL2007740503Torque Box · crackedWHILE IN "C" CHECK, NLG WW STA 294 RT LOWER TORQUE BOX WEB IS CRACKED. TRIMMED OUT CRACKED PORTION IAW B727 SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024T3 .063 PO NR 9005089 DIM 7 1/2 BY 8 1/4 IAW B727 SRM 53-10-2 FIG 2 AND 51-40-2 FIG 1. TREATED AND PRSDR DHL2007740509Skin · delaminatedRT O/B AFT FLAP WBL 417 HAS DELAMINATION AND SURFACE CORROSION ON AN NEAR T/E. REMOVED DAMAGED AREA APPROX 10" BY 20". CLEANED AN PREPPED AREA TO BE REPAIRED. FAB`D FILLER 10" BY 20" AN 2 DOUBLERS 3" BY 20" FROM .016" 2024-T3 PO NR 9004174. ANODIZED AN PRISDR DHL2007740531Shear Tie · crackedWHILE IN "C" CHECK, AFT CARGO COMPARTMENT SHEAR TIE AT BS 970 BETWEEN STR.25L AND 24L IS CRACKED AT LOWER END. REMOVED CRACKED SHEAR TIE "T" EXTRUSION IAW B727 SRM 51-30-2. FABRICATED NEW SHEAR TIE FROM BAC1505-100246 PO NR 650418 DIM 7" IAW B727 SRM 53-10-2SDR DHL2007740530Frame · dentedWHILE IN "C", FWD CARGO COMPT STA 600 +4" REINFORCEMENT FRAME IS DENTED ABOVE STR 24L. TRIMMED OUT DAMAGED (DIM.3" BY 1.25") IAW B727 SRM 51-10-1. FABRICATED REPAIR CHANNEL FROM 7075-0 .090 PO NR 7185240 (DIM 23" BY 5") IAW B727 SRM 53-10-4 FIG 1. HEAT TREASDR DHL2007740511Skin · brokenL-2 LOWER HINGE ARM SKIN IS BROKEN AT FWD END. REMOVED SKIN SECTION IAW B727 SRM 51-30-2. FAB`D NEW SKIN FROM 2024-T3 0.050" PO NR 9005049 DIM 9"BY 1 1/2" IAW B727 SRM 52-40-1 FIG 4 ANH 51-20-1. TREATED AND PRIMED NEW PART IAW B727 SRM 51-10-2 AND INSTALLEDSDR DHL2007740507Skin · brokenL-2 DOOR LOWER HINGE ARM SKIN IS BROKEN AT FWD END. REMOVED SKIN SECTION IAW B727 SRM 51-30-2. FABBED NEW SKIN FROM 2024-T3 0.050" PO NR 9005049, DIM 9" BY 1 1/2 " IAW B727 SRM 52-40-1 FIG 4 AND 51-20-1. TREATED AN PRIMED NEW PART IAW B727 SRM 51-10-2 AN INSDR DHL2007740500Shear Tie · crackedWHILE IN "C" CHECK, FRAME STA 480, SHEAR TIE AT FRAME IS CRACKED BETWEEN STR 16L AND STR 17L. REMOVED FASTENERS AND CRACKED ANGLE AT STA 480 BETWEEN STR 16L AND 17L IAW B727 SRM 51-30-2. FABRICATED ANGLE FROM 7075T6 .040 PO NR 9004940 APPROX DIM. 6" BY 2" IASDR DHL2007740510Frame · corrodedCORROSION ON FRAME SHEAR TIE BS 580 BETWEEN STR 28R-28L. FOUND CRACK IN SHEAR TIE IAW B727 SRM 51-10-1. FAB`D NEW SHEAR TIE FROM 7075-0 .071" PO NR 9004690. DIM 2 1/4" BY 5" IAW B727 SRM 53-10-4 FIG 15 AN B727 SRM 53-10-2 FIG 3. HEAT TREAT PART FROM 7075-0SDR DHL2007740529Pressure Panel · crackedWHILE IN "C" CHECK, NOSE LANDING GEAR WHEEL WELL LT WEB UPPER PLATE CRACKED AT OPENING (BS273). REMOVED WEB IAW B727 SRM 51-30-2. FABRICATED NEW WEB FROM 7075T6 .032 PO NR 9003110 DIM 11 1/2" BY 7" IAW B727 SRM 53-10-2 FIG 3 AND 51-10-3. TREATED AND PRIMED SDR DHL2007740504Rib · crackedLT WING NR 3 SLAT ACTUATOR ROD O/B ATTACH RIB CRACKED. REMOVED NR 3 SLAT ACTUATOR O/B RIB IAW B727 SRM 51-30-2. FABBED NEW RIB MAT. USED 7075 .040 PO NR 9003230 DIM 16" BY 6" BY 6" IAW B727 SRM 51-30-5 AND 57-50-2 FIG 2. HEAT TREATED MATERIAL TO T6 CONDITIOSDR DHL2007740501Shear Tie · crackedWHILE IN "C" CHECK, MAIN CABIN, LT BS 680 WL 210 FRAME PRESENTS CRACK (AT SHEAR TIE). CUTOUT DAMAGED AREA, FABRICATED FILLER FROM 7075T6 .040 PO NR 9004940 DIM 2 1/8 BY 1 AND DOUBLER FROM 7075T6 .050 PO NR 9004843 DIM 5 7/8 BY 3 1/4 IAW B727 SRM 51-40-3 FIG SDR DHL2007740528Bulkhead · crackedWHILE IN "C" CHECK, RT PRESSURE BULKHEAD WEB PRESENTS 3" CRACK AT BS 1180 RBL54 WL208. REMOVED CRACKED WEB IAW B727 SRM 51-30-2. FABRICATED NEW WEB FROM 2024T3 .026 .025 PO NR 9004384 DIM 16 1/2"BY 6" IAW B727 SRM 53-10-2 FIG 5 51-20-1. TREATED AND PRIMED NSDR DHL2007740502Skin · crackedWHILE IN "C" CHECK, RT WING LE CRACKED AT NR 5 SLAT OB HOOK CUTOUT. STOP DRILLED CRACK IAW B727 SRM 57-30-4 FIG 9 AND 51-10-1. FABRICATED REPAIR PLATE FROM 301 1/2HD .025 PO NR 9005090 DIM 7 1/4 BY 5 1/8, FILLER FROM 301 1/2HD .032 PO NR 614973 AND BACKING SSDR DHL2007740508Hook · gougedNR 3 SLAT GOUGED AT O/B SLAT HOOK. ROUTED OUT EDGE WITH MAT LOSS OF 0.192" FOUND OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 1. FAB`D DOUBLER REPAIR FROM 2024-T3 0.125" PO NR 645747 DIM 5" BY 3 1/2" IAW B727 SRM 57-50-3 FIG 10. TREATED AND PRIMED PARTS IAW B727 SDR DHL2007740506Skin · delaminatedLT I/B MID FLAP UPPER SURFACE DELAM 36" FROM O/B END. REMOVED DAMAGED AREA APPROX 6 3/4" BY 4" BY 4 1/4" CLEANED AN PREPPED AREA TO BOND, FABBED FILLER (6 3/4"X 4 1/4") AND FILLER 2 EACH 3" BY 4 1/4" FROM .016 7075-T6 PO NR 9003988, ANODIZED, PRIMED AN APPLIESDR DHL2007740505Rib · crackedNR 3 SLAT I/B ACTUATOR ROD ATTACH RIB IS CRACKED. REMOVED NR 3 RIB SLAT I/B ACTUATOR ROD CRACKED IAW B727 SRM 51-30--2. INSTALLED NEW RIB P/N 65-17294U13, PO NR 721255 AT SLAT I/B ACTUATOR ROD IAW B727 SRM 51-30-2.SDR DHL2007740512Hinge · crackedEXT FUSE MCD AFT MOST HINGE SEGMENT BS 650 IS CRACKED ON THE AFT LOBE. REMOVED HINGE SECTION IAW B727-200 AEI MM CHAP 52. FAB`D NEW HINGE SECTION FROM MS20001-16-7200 PO NR 9002527 DIM 17" LONG AN 11" LONG IAW B727 MM AEI CHAP 52 TREATED AN PRIMED AREA AN PASDR DHL2007740513Frame · corrodedAFT CARGO BS 1030, BETWEEN STR'S 28R AND 29R, AFT SIDE OF FRAME HAS CORROSION BELOW FAIL SAFE CHORD. CORROSION REMOVAL OUT OF LIMITS PER B727 SRM 53-10-1 FIG 1. CUT OUT SHEAR TIE, FABRICATED NEW SHEAR TIE FROM 7075-T6, .071" BY 6.75" BY 4", PO NR 9004940, TRSDR DHLA200700024Engine · power lossON TAKEOFF ROLL, BELOW 80 KTS NR 2 ENG N1 INDICATOR DROPPED TO 0 PERCENT. ALL OTHER ENGINE PARAMETERS NORMAL, 146,700LBS.;80 KTS IAS;26C PA-26FT.1. ENTERED ON DMI NR 28913 IAW MEL 77-2 CAT"B" PLACARD INSTALLED + SP-77-2.SDR DHL2006741004Skin · delaminatedRT WING OUTBD AFT FLAP TE HAS DELAMINATE SPOT AT WBL 445 APPROX (MARKED). CUT OUT DELAMINATED AREA APPROX 4" BY 2". FABRICATED FILLER APPROX 4"BY 2" AND DOUBLER APPROX 7" BY 3 1/2", MAT ID 7075T6 .016 PO NR 526029. PREPARED DAMAGED SURFACE, FILLER AND DOUBLSDR DHL2006741003Switch · out of adjustTRIM SET AT 3.1 APPLIED T/O THRUST AT 1.4 EPR T/O WARNING HORN. ADJUSTED UPPER STAB SWITCH S532 IAW MM 31-26-24. OPS CHECKED T/O. WARNING SYSTEM OK IAW 31-26-24.SDR DHL2006740003Light · inoperativeCOCKPIT EMERGENCY EXIT LIGHT INOP DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, OPS CK NORMAL IAW BMM REF 33-50-00.SDR DHL2006741002Warning Switch · out of adjustAFTER SELECTING THE LANDING GEAR HANDLE TO THE OFF POSITION ON CLIMBOUT THE -DOORS- LIGHT AND THE -R GEAR DOOR- LIGHT ON S/O PANEL ILLUMINATED. COMPLETED THE ABNORMAL PROCEDURE RESULTING IN BOTH LIGHTS TO EXTINGUISH. INSP DOOR SWITCHING AND PERF ADJ AND TESTSDR DHL2006741001Warning System · malfunctionedSELECT GEAR DOWN, RED GEAR UNSAFE LIGHTS ILLUM. CYCLED GEAR UP & DOWN, OPS NORMAL EXC MISSED APPROACH GEAR ODS NORMAL, LANDING NORMAL. OPS CHECK ON GROUND, NO DEFECTS NOTED IAW MM 32-31-00.SDR DHL2006740002Battery · dischargedEMERGENCY EXIT LIGHTS INOP. REPLACED BATTERIES, OPS CK GOOD IAW MM 33-50-101. P/N MISC062.SDR DHL2006740001Engine · failedNR 2 ENGINE FAILED AT 16000 FT. ACCOMPLISHED ALL EMERGENCY ABNORMAL CHECKLIST. REMOVED AND REPLACED NR 2 ENGINE ASSY IAW B727 MTM 71.2 RII 8188SDR DHL05740019Switch · failedYELLOW (L GEAR DOOR) LIGHTON S/O PANEL FAILS TO ILLUMINATE ON GEAR RETRACT OR EXTENTION BUT DOES TEST.NO OTHER GEAR INDICATION ARE ABNORMAL. REMOVED AND REPLACED LT LANDING GEAR DOOR WARNING SWITCH IAW B-727 M/M 32-61-11.OPS CHECK GOOD P/N 1EN161-RB1SDR DHL2005741005Handle · malfunctionedAFTER T/O RED DOOR LIGHT, & AMBER RT GEAR DOOR LIGHTS ILLUMINATED WITH GEAR HANDLE IN OFF POSITION. ACCOMMPLISH AOM PROCEDURES, DOOR LIGHTS EXTINGUISHED WHEN GEAR HANDLE IN UP POSITION. PERFORMED OP'S CHECK OF RT GEAR DOOR, DUMMY RETRACTION, CHECK GOOD PER MSDR DHLA05740016Door · out of adjustNOSE GEAR DOOR LIGHT ILLUMINATED DURING DESCENT. PERFORMED ABNORMAL LIGHT REMAINED EXTINGUISHED WITH GEAR HANDLE IN UP POSTION. ADJUSTED NOSE GEAR DOORS, SWUNG NOSE GEAR, CK NORMAL PER MM 32-22-1SDR DHLA05740015Switch · out of adjustNOSE GEAR DOOR LIGHT ILLUMINATED DURING DECENT. ABNORMAL PROCEDURE WAS ACCOMPLISHED LIGHT WENT OUT WITH GEAR LEVER IN UP POSITION. ADJUSTED NOSEGEAR DOOR WARNING SWITCH IAW M/M 32-62-0 OPS CK NORMALSDR DHLA05740013Door · out of adjustNOSE GEAR DOOR LIGHT ILLUMINATED IN FLT. LIGHT REMAINED ILLUMINATED EVEN WITH GEAR HANDLE IN UP POSITION. LIGHT ILLUMINATED DURING DESCENT ONLY. LUBED NOSE GEAR DOOR UP WARNING SW 5398 & 5435 . ADJUSTED R&L NLG DOOR PER B727 MM 32-22-1 PG 504 & 505 . JACK A/CSDR DHL2005740011Warning Horn · activatedAURAL TAKEOFF WARNING ON TAKEOFF ROLL COMPLETED W/ RTO FLOW CHART A/C SPEED NOT ABOVE 10 KNOTS. LUBED FLAP TAKEOFF SWITCH, OPS CKS GOOD IAW MM 31-26-00.SDR DHL2005741004Warning Light · illuminatedAFTER TAKEOFF WHEN SELECTING GEAR HANDLE OFF, RIGHT GEAR DOOR LIGHT ILLUMINATED. COMPLIED WITH ABNORMAL PROCEDURE. LIGHT EXTINGUISHED. INSPECTED & CLEANED RT GEAR DOOR POSITION SWITCH. CYCLED GEAR DOOR SEVERAL TIMES, NO DEFECTS NOTED IAW MM 32-62-11 & 32-6SDR DHL2005741003Feel Unit · malfunctionedON TEST FLIGHT LOST A-SYSTEM HYDRAULICS ON APPROACH BACK INTO JAX, DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. LOST A-SYSTEM HYDRAULICS, ALL QUANTITY LOST ABNORMAL PROCEDURE COMPLETED HYD FLUID SHUT OFF VALVES CLOSE FOR ONLY 1.5 MINUTES (APPROXSDR DHL2005741597Computer · leakingDURING A HEAVY MAINTENANCE EXCEPTANCE FLIGHT, THE AIRCRAFT LOST A-SYSTEM HYDRAULICS, ALL QUANTITY LOST, ABNORMAL PROCEDURE COMPLETED, HYD FLUID SHUTOFF VALVE CLOSED FOR 1.5 MINUTES APPROX. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER IAW B727 MM 27-30-101, LEASDR DHL2005741611Skin · dentedRIGHT HORIZONTAL STABILIZER LOWER INTERSPAR SKIN AT STAB STA 109.97 IS DENTED. CUT OUT DAMAGED AREA TWO PLACES DIM 3.5 X 1.25 & 8.5 X 2 INCH IAW B727 SRM 55-10-3 FIG 3. FAB DOUBLER FROM 2024T3 .080 PO 9002555 DIM 15 X 101.5 INCH IAW B727 SRM 55-10-3 FIG 3. SDR DHL2005741610Skin · dentedDENT AT RIGHT FUSELAGE STA 1330 ABOVE STR 19R. CUT OUT DAMAGE AREA SIZE 1.75 X 2.75 INCH ON RIGHT FUSELAGE STA 1330 ABOVE STR 19R IAW B727 SRM 53-30-3 FIG 1. FAB'D DOUBLER FROM 2024-T3 0.63 SIZE 7.5 X 10.75 INCH PO 9001978. TREATED & PRIMED PART AND AREA IASDR DHL2005741609Doubler · crackedMAIN CARGO DOOR CUTOUT SURROUNDING EXTERNAL DOUBLER HAS 3EA CRACKS AT STA: 561 (MATING SURFACE FOR MCD HINGE) TRIMMED-OUT 3.45 INCH X .440 INCH SECTION OF AEI-38 EXTERNAL SURROUND DOUBLER AT STA 561 TO REMOVE ALL 3 CRACKS IAW AEI EO 1448 FABRICATED FILLER FOSDR DHL2005741608Duct · defectiveREPAIR OF NR 2 ENG S-DUCT INNER SKIN AREA. CUT OUT 5 EA HAT CHANNEL SECTION ON OUTER RING OF THE S-DUCT FOR ACCESS TO THE 5 REPAIRS WITH BLIND FASTENERS FROM BS 1223-1275 AND REPLACED WITH SOLID FASTENERS IAW B727 SRM 51-30-2 FIG 7. FABRICATED HAT CHANNEL RESDR DHL2005741607Floorbeam · corrodedFLOORBEAM AT BS 1110, BL-0, LWR CHORD IS EXFOLIATED. REMOVED WEB FOR ACCESS FROM STA 1110 BL 0 TO STA 1130 BL 0 IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA FLOORBEAM LOWER CHORD STA 1110 BL 0 SIZE 4.5 X 2 INCH IAW B727 SRM 53-10-8. FABRICATED REPAIR ANGLES FSDR DHL2005741589Web · crackedWEB CRACKED AT AFT ATTACH BRACKET HOLE OF C2 DOOR SNUBBER. ROUTED OUT CRACK ON WEB BY INSP HOLE ON INNER SKIN OF C-2 DOOR SNUBBER AREA IAW B727 SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER TO INNER WEB OF C-2 DOSDR DHL2005741600Rib · crackedNR 7 SLAT O/B OF ACTUATOR ROD HAS CRACKED RIB AT WS 650. REMOVED CRACK RIB, FABRICATED NEW RIB, MATL 2024-T3 .040 PO 9002248, 16 X 5 INCH IAW B727 SRM 51-30-2 AND 57-50-2 FIG 2. TREATED AND PRIMED RIB IAW B727 SRM 51-10-2, INSTALLED RIB IAW B727 SRM 51-30-2.SDR DHL2005741539Skin · chafedLWR RUDDER UPPER WEB FASTENERS AND SKIN CHAFED RUDDER STA 152. DAMAGED TO LWR RUDDER UPPER WEB FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-40-1 FIG 1. REMOVED WEB ON LWR RUDDER UPPER WEB IAW B727 SRM 51-30-2. FABRICATED WEB FROM 2024 T3 .040 SIZE 14.500 X 14.
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