Boeing 727-227
Service difficulty reports · 5,082
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 = '727227' 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 = '727227' 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 DHL2007783511Bracket · crackedNR 2 K-FLAP ACTUATOR SUPPORT ANGLES INBD AND OUTBD ARE CRACKED W/S 235. REMOVED NR 2 K-FLAP ACTUATOR TRUNNION SUPPORT ANGLES INBD AND OUTBD IAW B727 SRM 51-30-2. FABRICATED SUPPORT ANGLES FROM 7075T6, .071, 8.25 BY 6.25 IAW B727 SRM 57-20-2, FIG 1 AND 51-20-SDR DHL2007783502Web · crackedRT SIDE AIRSTAIRS WEB PANEL CRACKED AT LIGHTING HOLE BS 1243, WL 191, RBL 21. CUT OUT DAMAGED AREA DIM .5 BY .75 IAW B727 SRM 51-40-2, FIG 1. FABRICATED NEW DOUBLER REPAIR, MATERIAL USED 7075T6, 040, 4.50 BY 3.50 IAW B727 SRM 51-40-2, FIG 1 AND 53-10-2, FIG SDR DHL2007783501Web · crackedRT SIDE AIRSTAIRS WEB PANEL CRACKED AT LIGHTING HOLE BS 1233, WL 166, RBL 21. CUT OUT DAMAGED AREA DIM .5 BY .75 IAW B727 SRM 51-40-2, FIG 1. FABRICATED NEW DOUBLER REPAIR, MATERIAL USED 7075T6, 040, 3.50” BY 4.75 IAW B727 SRM 51-40-2, FIG 1 AND 53-10-2, FIGSDR DHL2007783520Stringer · corrodedLIGHT CORROSION AT STA 560, STR 27R FWD SIDE, FWD BILGE AREA. REMOVED CORROSION IAW B727 SRM 51-10-6, MATERIAL THICKNESS .090, MATERIAL REMAINING .058, FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. CUT OUT DAMAGED SECTION OF STRINGER 27R AT STA 560, 18 LONSDR DHL2007783510Doubler · wornFUSELAGE TO LT WING LE BS 720E, WBL 70.5, PREVIOUS REPAIR DOUBLER SHOW WORN OUT PATH, CHAFING WITH INBD L/E LEFT. REMOVED PREVIOUS REPAIR DOUBLER IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER FROM .040, 2024T3, 35.25 BY 14 IAW US AIR EA 7357. TREATED, PRISDR DHL2007783509Skin · wornFUSELAGE TO RT WING L/E BS 720E, WBL 70.5, PREVIOUS REPAIR DOUBLER SHOW WORN OUT PATH, CHAFING WITH INBD L/E WEDGE. REMOVED PREVIOUS REPAIR DOUBLER IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER FROM .040, 2024T3, 26 BY 10 IAW US AIR EA 7357. TREATED, PRIMSDR DHL2007783504Seat Track · corrodedCABIN SEAT TRACK CORRODED BETWEEN BS 760 TO BS 825, RBL 24. REMOVED SEAT TRACK SECTION BS 757.45 TO BS 852.45, RBL 45 IAW B727 SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK P/N BAC1520-841 IAW B727 SRM 51-30-5 AND 53-10-2, FIG 7. PART AND AREA TREATED, PRSDR DHL2007783503Seat Track · corrodedCABIN SEAT TRACK CORRODED BETWEEN BS 760 TO BS 825, RBL 45. REMOVED SEAT TRACK SECTION BS 757.45 TO BS 852.45, RBL 45 IAW B727 SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK P/N BAC1520-841 IAW B727 SRM 51-30-5 AND 53-10-2, FIG 7. PART AND AREA TREATED, PSDR DHL2007783516Nose Cowl · out of toleranceNR 1 ENGINE NOSE COWL AT 11 O`CLOCK POSITION, 2 BLIND FASTENERS IMPROPERLY INSTALLED, NAC STA 81.5. REMOVED 2 BLIND FASTENERS ON NR 1 NOSE COWL AT 11 O`CLOCK POSITION IAW B727 SRM 51-30-2. FASTENERS HOLES OUT OF LIMITS AND OVER SIZE IAW B727 SRM 51-30-2. RESDR DHL2007783523Nose Cowl · gougedNR 1 ENG NOSE COWL 4 O`CLOCK POS EXISTING REPAIR DOUBLER AN ADJACENT SKIN GOUGED AT NAC STA 82.5. REMOVED DAMAGED DOUBLER ON NR 1 ENGINE NOSE COWL 9 O`CLOCK POSITION IAW B7627 SRM 51-30-2. REMOVED DAMAGED SKIN ADJACENT TO DOUBLER AREA ON NR 1 ENG NOSE COWL ISDR DHL2007783500Unknown · unknownDURING INBOUND TEST FLIGHT FOR C-CHECK MANUAL GEAR EXTENSION, UNABLE TO EXTEND RIGHT MAIN GEAR. PERFORMED SPECIAL PROCEDURES, RIGHT MAIN DOOR DAMAGE NOTED ON LANDING. AIRCRAFT WAS JACKED IN HANGER AND TRIED TO DUPLICATE PROBLEM. UNABLE TO DUPLICATE PROBLEM.SDR DHLA200700029Coalescer Bag · odorCHEMICAL/BURNING ODOR COMING FROM PACKS WHEN SUPPLIED BY ENGINE AIR MORE EVIDENT AT HIGH POWER SETTINGS. REMOVED AND REPLACED LEFT AND RT PACK WATER SEPARATOR COALESCER IAW M/M 21-55-51 P/N 22D10 RAN ALL ENGINES IAW JRH 5.2, NO ODORS OR DEFECTS NOTED.SDR 07FDEA01778Warning Horn · false activationREJECTED TAKEOFF AT 75 KTS, ACFT WEIGHT 130,000 DUE TO UNSCHEDULED AIRSPEED/MACH AURAL WARNING SYSTEM MEL 12MAY07 03:27, BFM R ACN RELEASED FOR SERVICE PER MEL/CDL: 34-04-03 CATEGORY: B EXPIRATION: 15MAY07. MEM R PERFORMED MACH AURAL WARN TEST IAW 727-200 M/SDR DHLA200700025Battery · inoperativeEMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY EXIT BATTERIES IAW B-MM 33-50-71, OPS CHECK GOOD.SDR DHL2007782515Skin · crackedEXT FUSELAGE BS 254 AT STR 10L HAS EDGE CRACKED TO FASTENER HOLE. CUT OUT DAMAGED SKIN, 1.5" 1", PER B727 SRM 53-30-3 FIG 29. FABRICATED FILLER FROM 2024-T3, .063" BY 1.5" BY 1", PO NR 9004670; AND DOUBLER FROM 2024-T3, .080" BY 14.5" BY 12.75", PO NR 71771SDR DHL2007782514Stringer · corrodedFOUND STR 28R AT BS 1183 TENSION TIE IS CORRODED. REMOVED CORRODED STRINGER SECTION, 24" LENGTH. FABRICATED NEW STR SECTION FROM BAC1498-147, PO NR 3345302, 24" BY 5.875" AND STR SPLICE FROM BAC1498-131, PO NR 9003505, 20" LONG, PER B727 SRM 53-10-3 FIG 1 ANSDR DHL2007782513Bracket · excess playRT INBD AFT FLAP CONTROL CABLE ACTUATOR ROD LOWER MOUNTING BRACKET LOOSE INSIDE FLAP, RWBL 101.0. ACCESS GAINED TO AFFECT REPAIR; CUT OUT AFT FLAP L/E SECTION, 8.5" BY 14" PER B727 SRM 57-40-4 FIG 17. FABRICATED 2 REPAIR SPLICES FROM 2024-T3, .050" BY 5.5" BSDR DHL2007782512Skin · dentedLOWER HALF OF FUSELAGE EXTERIOR SURFACE RT, BS 351.0, DENTED BETWEEN STR 24R AND 25R. CUT OUT DAMAGED AREA 3.3" BY 3.5". FABRICATED, REPAIR DOUBLER FROM 2024-T3, .050" BY 12" BY 12", PO NR 9004174; REPAIR FILLER FROM 2024-T3, .063" BY 14" BY 2", PO NR 900364SDR DHL2007782511Shear Angle · corrodedE/E BAY FWD CRAWLWAY RT SIDE PRESENTS CRACK AND EXFOLIATION CORROSION AT BS 328.0 SHEAR TIE SUPPORT ANGLE BRACKET BETWEEN STR 26R AND 27R. CUT OUT DAMAGED AREA. FABRICATED NEW SHEAR TIE ATTACH ANGLE AND DOUBLER FROM 7075-T6, .050" BY 4.5" BY 2" (SHEAR TIE) ASDR DHL2007782510Frame · corrodedLARGE AREA OF CORROSION AT BS 320 APPROX, ON FRAME AND LOWER CHORD ANGLE, IN E-BAY FWD CRAWLWAY, RT SIDE BILGE AREA. LOWER NOSE CHORD CORRODED BEYOND LIMITS: REMOVED AND REPLACED LOWER RT NOSE CHORD ASSY PER B727 SRM 51-30-5, 51-30-2, AND 53-10-2 FIG 1. CUTSDR DHL2007782509Frame · corrodedFUSELAGE LOWER LOBE, BS 360 FRAME, BETWEEN STR 26R AND 27R, HAS EXFOLIATION CORROSION ON FWD SIDE. CUT OUT DAMAGED AREA 5" BY 1.5", FABRICATED 2 FILLERS FROM 7075-T6, .071" BY 5" BY 1.5", PO NR 9004150; DOUBLER FROM 7075-T6, .071" BY 7" BY 4.5", PO NR 9004150SDR DHL2007782508Skin · dentedNR 4 SLAT DENTED ON L/EDGE, LWS 380. CUT OUT DAMAGE, FABRICATED DOUBLER FROM 2024-T0, .080" BY 9" BY 4" (2 EA), PO NR 509622; FABRICATED FILLER FROM 2024-T3, .063" BY 4.75" BY 3.5", PO NR 9003641, PER B727 SRM 57-50-2 FIG 2 AND 57-50-3 FIG 1. HEAT TREATED 20SDR DHL2007782507Structure · corrodedCORROSION AT UPPER AND LOWER CHORD AND SPLICES, AIRSTAIR CUTOUT BS 1223 LBL22- RBL22, BELOW STEP. REMOVED FASTENERS AND UPPER AND LOWER SPLICES FOR ACCESS IAW B727 SRM 51-30-2. FOUND 3 SPLICES OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED CORROSION FROMSDR DHL2007782503Floorbeam · crackedCABIN FLOOR PANEL SUPPORT AT BS 760, BETWEEN LBL 44 AND LBL 66, IS CRACKED AT I/B ENDS. REMOVED FLOOR SUPPORT, FABRICATED REPAIR ANGLES FROM 7075-T6, .032" BY 6" BY 2" (2 EA.), PO NR 9004042, PER B727 SRM 51-10-3 AND 51-40-3 FIG 1. TREATED, PRIMED, AND INSTASDR DHL2007782502Pressure Panel · crackedCABIN PRESSURE WEB AT BS 740 TO 760, LT, IS CRACKED AT AFT HOLE. FABRICATED NEW PRESSURE WEB FROM 7075-T6, .040" BY 13.5" BY 9.5", PO NR 9004539, PER B727 SRM 53-10-3 FIG 7 AND 51-20-1. TREATED, PRIMED, AND INSTALLED PRESS WEB PER B727 SRM 51-10-2 AND 51-30-SDR DHL2007782501Pressure Panel · crackedCABIN PRESSURE WEB AT BS 740 TO 760, RT, IS CRACKED AT AFT HOLE. FABRICATED NEW PRESSURE WEB FROM 7075-T6, .040" BY 13.5" BY 9.5", PO NR 9003110, PER B727 SRM 53-10-2 FIG 3. TREATED, PRIMED, AND INSTALLED PRESS WEB PER B727 SRM 51-10-2 AND 51-30-2.SDR DHL2007782506Stringer · corrodedFOUND STR 27R AT BS 560 IS CORRODED. CUT OUT DAMAGED STRINGER APPROX LENGTH 16" IAW B727 SRM 53-10-3 FIG 1. FABBED NEW STRINGER REPAIR FROM P/N BAC1477075T-6 PO NR 5096200 AND P/N BAC 1496-1317075-T6 PO NR 9004539 APPROX DIM 22" IAW B727 SRM 53-10-3 FIG 1 ANSDR DHL2007782505Support Fitting · corrodedNLG LT TRUNNION SUPPORT FITTING LOWER CAP PRESENTS CORROSION. REMOVED CORROSION AT NLG LT TRUNNION SUPPORT FITTING ORG DIA 2.848" FINAL DIA 2.602 MAT. REMOVED WITHIN LIMITS IAW B727 SRM 53-40-1 FIG 2. CHAMFER BORE HOLE TO .6 BY 45 DEGREES IAW B727 SRM 53-40SDR DHL2007782504Support Fitting · corrodedNLG RT TRUNNION SUPPORT FITTING LOWER CAP PRESENTS CORROSION. REMOVED CORROSION AT RT TRUNNION BORE ORG DIA 2.488" FINAL DIA 2.587" MAT LOSS WITHIN LIMITS IAW B727 SRM 53-40-1 FIG 2. CHAMFER BORE HOLE TO .6 BY 45 DEGREES IAW B727 SRM 53-40-1 FIG 2, PENETRANT SDR 07FDEA01102Door · leakingAPPEARED TO LOOSE PRESSURIZATION PASSING 12,000' LEVELED AT 14,000' CABIN AT 9500, DESCENDED TO 10,000 AND WAS UNABLE TO GET PRESSURE IN CABIN BELOW 8,000. HEARD LOUD AIR NOISE, CHECKED MAIN CABIN DOOR, FOUND AIR LEAKING AROUND DOOR. RETURNED TO MEM. ADJUSSDR ASTAR20070011Rheostat · shortedFOUND STRONG ODOR ON FLT DECK IN FLT. FOUND S/O BACK GROUND LIGHTING RHEOSTAT SHORTED INTERNALLY AND CAUSING STRONG ODOR. REMOVED AND REPLACED RHEOSTAT, F/E'S BACK GROUND LIGHTING, OPS NORMAL IAW B-MM 33-10-01SDR 07FDEA00849Bolt · looseAFTER T/O LANDING GEAR FAILED TO RETRACT RAN THE "LANDING GEAR LEVER LATCH FAILED TO RELEASE" CHECKLIST TEST NR 1 FAIL, TEST 2&3 PASSED. RETURN TO MEMPHIS NORMAL LANDING. FOUND LEFT MAIN GEAR SAFETY SENSOR ACTUATOR CENTER PIVOT BOLT LOOSE AND NUT BACKED OFF SDR DHL2007781016Intercostal · crackedAFT CARGO COMPT AT BS 925, INTERCOSTAL WEB ATTACH TO STR 20L IS CRACKED. STOP DRILLED CRACK PER B727 SRM 51-10-1. CRACK CONTAINMENT VERIFIED BY HFEC METHOD. FABRICATED REPAIR ANGLE FROM 7075-T6, .080" BY 9" BY 2.25", PO NR 9003958, PER B727 SRM 53-10-2 FIG SDR DHL2007781015Nose Cowl · dentedNR 3 ENG NOSE COWL LOWER SIDE DENTED BETWEEN NAC STA 70 AND 85. CUT OUT DAMAGED AREA OF COWL, 17.5" BY 9.5" APPROX, PER B727 SRM 54-30-3 FIG 3.FABRICATED; FILLER FROM 2024-T3, .040" BY 9" BY 18", PO NR 9004042; AND DOUBLER FROM 2024-T3, .050" BY 20.5" BY 6.5"SDR DHL2007781014Skin · gougedRT NR 5 BALANCE BAY (HORIZ STAB) UPPER SKIN GOUGED. REMOVED GOUGED PREVIOUS REPAIR DOUBLER. FABRICATED NEW DOUBLER FROM 7075-T0, .032" BY 6" BY 5", PO NR 44953 PER B727 SRM 55-20-3 FIG 3. HEAT TREATED REPAIR TO T6 CONDITION IAW FASI FORM FAS 0115. TREATED,SDR DHL2007781013Skin · corrodedFOUND SKIN AT BS 481, STR 28R, HAS CORROSION. FOUND CORROSION ON SKIN OUT OF LIMITS. CUT OUT DAMAGED SECTION OF SKIN, 9.75" BY 3". FABRICATED DOUBLER FROM 2024-T3, .100" BY 15.875" BY 10.375", PO NR 9003970; AND FILLER FROM 2024-T3, .090" BY 9.75" BY 3.125"SDR DHL2007781012Stringer · corrodedFOUND FWD CARGO, BS 690, STR 27R, HAS SMALL SPOT OF CORROSION IN CHANNEL. CORROSION OUT OF LIMITS PER B727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED PORTION OF STRINGER, 8" APPROX, FABRICATED, STR SPLICE OUT OF BAC1498-132, 20.5" LONG, PO NR 7114294; SHIM OUT OF 7SDR DHL2007781011Fitting · corrodedFOUND NLG DRAG BRACE FITTING HAS CORROSION ON BOTH DRAG BRACE ATTACH LUGS, IN LUG BORE'S AND ON LUG FACES. REMOVED CORROSION IN LUG BORES; MATERIAL REMOVED FOUND OUT OF LIMITS PER B727 SRM 53-40-1 FIG 1. REMOVED AND REPLACED NLG DRAG BRACE FITTING PER B727 SDR DHL2007781004Stringer · corrodedFOUND FWD CARGO BS 495, STR 28R HAS EXFOLIATING CORROSION. CUT OUT DAMAGED SECTION OF STR FROM BS 483 TO 515, FABRICATED REPAIR SPLICE FROM BAC1498-132, PO NR 6452106, APPROX LENGTH 12", AND FILLER FROM BAC1498-138, PO NR 7114324, APPROX LENGTH 34", PER B727 SDR DHL2007781010Trunnion · corrodedFOUND LT UPPER NLG TRUNNION BORE HAS PITTING CORROSION. REMOVED CORROSION ON TRUNNION BORE PER B727 SRM 53-40-1 FIG 2; ORIGINAL DIA 2.640", FINAL BORE DIA 2.7", MAX ALLOWABLE DIM 2.75", IS WITHIN LIMITS PER B727 SRM 53-40-1 FIG 2. TREATED AND PRIMED TRUNNIONSDR DHL2007781009Seat Track · corrodedFOUND LT CABIN, SEVERAL AREAS OF CORROSION ON SEAT TRACK AT BS 500-600, LBL48. REMOVED DAMAGED SEAT TRACK SECTIONS, BS 480-610. FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792, PO NR 9003797, 130" LONG, PER B727 SRM 53-10-5 FIG 1. FABRICATED REPAIR ANGLESDR DHL2007781008Seat Track · corrodedLT CABIN, SEVERAL AREAS OF CORROSION ON SEAT TRACK AT BS 500-600, LBL24. REMOVED DAMAGED SEAT TRACK SECTIONS, BS 480-610. FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792, PO NR 9003797, 130" LONG, PER B727 SRM 53-10-5 FIG 1. FABRICATED REPAIR ANGLES FROM SDR DHL2007781007Seat Track · corrodedFOUND RT CABIN, SEVERAL AREAS OF CORROSION ON SEAT TRACK AT BS 500-600, RBL 24. REMOVED DAMAGED SEAT TRACK SECTIONS, BS 480-690. FABRICATED 2 NEW SEAT TRACK SECTIONS, 1 AT BS 480-610, AND 2 AT 610-690, FROM BAC1520-792, PO NR 9003797, 128.5" AND 80" LONG, PESDR DHL2007781006Seat Track · corrodedRT CABIN, SEVERAL AREAS OF CORROSION ON SEAT TRACK AT BS 500-600, RBL 48. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION FROM BAC1520-792, PO NR 9003797, 111.5" LONG, PER B727 SRM 53-10-5 FIG 1. FABRICATED REPAIR SPLICE FROM BAC1503-10122, PO NRSDR DHL2007781005Attach Angle · crackedFOUND UPPER OTBD NR 3 PYLON ATTACH ANGLE CRACKED AT HOLE "P" AT ENG BL 28, REF B727 SB 54A0010. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE FROM P/N 4130 ANNEALED, .100" X 20.5" X 3", PO NR 7114153, PER B727 SRM 54-10-2 FIG 3, 51-30-2, AND 51-30-5. HEAT TREASDR 07FDEA00540None · noneNACELLES AND PYLONS MINOR DEVIATION TO SRM S DUCT HOUSING SKIN REPAIR. COMPLIED WITH EA 7-5410-102026 THIS ITEM CLEARED BY REPAIR PER SRM 54-10-3 FIG 4 WITH MINOR DEVIATION DOCUMENTED BY THIS EA.SDR 07FDEA00537Oil System · unknownNR 1 ENG OIL QUANTITY BEGAN TO DECREASE SHORTLY AFTER T/O WITH ASSOCIATED NOTICEABLE DECREASE IN OIL TEMP, (OUT OF LIMITS) PRECAUTIONARY ENGINE SHUTDOWN. OIL QTY DECREASED TO BELOW 1 GAL. AFTER SHUTDOWN OIL QTY ROSE AGAIN TO 4 GALS. DUE TO THE FACT THAT THESDR DHL2007781003Stringer · corrodedFWD CARGO COMPT, BS 555, AND BS 562, STR 28R, HAS EXFOLIATED CORROSION. CORROSION OUT OF LIMITS PER B727 SRM 53-10-1 FIG 1. GAINED ACCESS AS REQ TO FOM. CUT OUT DAMAGED MATERIAL APPROX 9", FABRICATED REPAIR SPLICE FROM BAC1498-131, 22" IN LENGTH, PO NR 9005SDR 07FDEA00480Engine · damagedAFTER TAKEOFF AT 1000 FT, CREW FELT A VERY PRONOUNCED THUMP ACCOMPANIED BY A LOUD NOISE. AUTO PACK TRIP ILLUMINATED. ENGINE INSTRUMENTS CHECKED NORMAL. WHILE TROUBLESHOOTING THE PROBLEM AND CLIMBING THROUGH 18,000FT. ANOTHER LOUD THUMP AND NOISE OCCURRED SDR DHL2007781002Skin · crackedFWD ENTRY DOOR UPPER AFT CORNER OF EXTERIOR SKIN, WORKING RIVETS, BS 314. REMOVED FASTENERS ON L1 DOOR, AFT UPPER CORNER PER B727 SRM 51-30-2, CRACK FOUND ON EXISTING DOUBLER. FABRICATED DOUBLER FROM 2024-T3, .050" X 4.5" X 3.5", PO 9004042, TREATED, PRIMED,
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