N752DH
Service difficulty reports · 115
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N752DH' AND registry_match = 'registration' 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 n_number = 'N752DH' AND registry_match = 'registration' 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 DHL2006752519Repair · noneFOUND NR 111054; ACCOMPLISH IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 410 & STR 24R. ACCOMPLISHED IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 410 & STR 24R. INSTALLATION PERFORMED IAW B727 SRM 53-30-3 FIG 1. VERIFIED SDR DHL2006752518Repair · noneFOUND NR 111053; ACCOMPLISH IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 305 & BETWEEN STR 8L - 11L (L1 DOOR UPPER HINGE CUTOUT). ACCOMPLISHED IDENTIFCATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 305 BETWEEN STR 8L - 11L (L1 DOOR UPSDR DHL2006752517Repair · noneFOUND NR 111052; ACCOMPLISH IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 205 & BETWEEN STR 19R-23R. ACCOMPLISHED IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 205 & BETWEEN STR 19R-23R. INSTALLATION PERFORMED IAW B727 SRM 5SDR DHL2006752516Repair · noneFOUND NR 111051; ACCOMPLISH IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 465 & STR 16R. ACCOMPLISHED IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 465 & STR 16R. INSTALLATION PERFORMED IAW B727 SRM 53-30-3 FIG 1. VERIFIED SDR DHL2006752510Skin · dentedDENT ON NR 1 SLAT UPPER SURFACE WSTA 720. CUTOUT SKIN SIZE 4 5/8 X 1 1/2 AND INNER SKINS SIZES 8 1/2 X 3 1/4 AND 8 1/2 X 3 1/2 IAW B727 SRM 57-50-3 FIG 1 AND FIG 44. FIBBED SKIN DOUBLERS FROM 2024 T3 .080 SIZE 8 1/2 BY 5 1/8 POX 9002459 AND INNER SKIN FROM 2SDR DHL2006572510Slat · dentedFOUND NR 111042; DENT ON NR1 SLAT UPPER SURFACE WSTA 720. CUTOUT SKIN SIZE 4.6250 X 1.5 AND INNER SKINS SIZES 8.5 X 3.25 AND 8.5 X 3.5 IAW SRM 57-50-3 FIG 1 AND FIG 4 FABBED SKIN DOUBLER FROM 2024 T3 .080 SIZE 8.5 X 5.1250 PO 9002459 AND INNER SKIN FROM 2024SDR DHL2006752509Skin · corrodedFWD CARGO FUSELAGE INNER SKIN AT STR 28L BS 580-600 HAS HEAVY CORROSION. CUT OUT DAMAGED AREA OF SKIN AT STR 28L BETWEEN BS 580-600 DIM 19" X 3". FABBED DOUBLER 2024-T3 .100 PO 9002507 29.75" X12.0" AND FILLER 2024T3 .090 18.0"X3.125" IAW B727 SRM 53-30-2 FISDR DHL2006572509Skin · corrodedDISCREPANCY FOUND NR 110979; FWD CARGP FUSELAGE INNER SKIN AT STR 28L BS 580-600 HAS HEAVY CORROSION. CUT OUT DAMMAGED AREA OF SKIN AT STR 28L BETWEEN BS 580-600 DIM 19 INCH X 3 INCH FABBED DOUBLER 2024-T3 .100 PO 9002507 29.75 INCH X 12.0 INCH AND FILLER 20SDR DHL2006752508Actuator · crackedNR 2 SLAT ACTUATOR I/B SUPPORT MOUNT CRACKED. REMOVED CRACKED NR 2 SLAT ACTUATOR I/B SUPPORT MOUNT IAW B727 SRM 51-30-2. FABBED DOUBLER PLATE MIL 5-5059 301 1/2 HD .100 7.4" BY 3" PO 9001425 IAW S/B 727-57-0130 REV 3 DATED 4-24-03. FABBED SUPPORT MOUNT BAC SDR DHL2006752507Frame · crackedVERT STAB BS 1303 FRAME ABOVE ENG INLET PIPE HAS WEB WITH 1" CRACK ON RT LWR CORNER. STOP DRILLED CRACK AS REQUIRED IAW S/B 727-53-0094 REV 3 DATED 4-26-90 ACCOMPLISHED COTNEY AEROSPACE EA: EAZ04-5 REV IR W/8110-3 DATED: 1-12-06. THIS REPAIR IS CAT. "B" VISSDR DHL2006572508Actuator · crackedNR 2 SLAT ACTUATOR I/B SUPPORT MOUNT CRACKED. CORRECTIVE ACTION; REMOVED CRACKED NR 2 SLAT ACTUATOR I/B SUPPORT MOUNT IAW B727 SRM 51-30-2 FABBED DOUBLER PLATE MIL 5-5059 301 1/2 HD .100 7.4" X 3" PO 9001425 IAW S/B 727-57-0130 REV 3 DATED 4-24-03 FABBED SUPSDR DHL2006752506Grommet · deterioratedFOUND NR 110899; DB COOPER VANE STOP GROMMET, LT SIDE FUSELAGE SKIN IS DETERIORATED STA 1323 ABOVE STR 26L. REMOVED DB COOPER VANE STOP GROMMET IAW B727 SRM 51-30-2, FAB DOUBLER FROM 2024-T3 .063 PO 9002435 9.375 X 4.75 INCH IAW B727 SRM 53-30-3 FIG 1. TREASDR DHL2006572506Grommet · deterioratedDISCREPANCY FOUND NR 110899; DB COOPER VANE STOP GROMMET, LT SIDE FUSELAGE SKIN IS DETERIORATED STA 1323 ABOVE STR 26L. REMOVED VANE STOP GROMMET IAW SRM 51-30-2 FAB DOUBLER FROM 2024-T3 .063 PO 9002435 9 .3750 X 4.7500 IAW SRM 53-30-3 FIG1 TREATED AND PRIMEDSDR DHL2006752505Frame · misdrilledDISCREPANCY FOUND NR 110760; TOP FLANGE OF FRAME AT BS 520 STR 26R HAS MISDRILLED HOLE. FOUND PREVIOUSLY INSTALLED REPAIR DOUBLER DAMAGED. REMOVED ANGLE AT FRAME BS 520 STR 26R IAW B727 SRM 51-30-2 FABBED FROM 7075-T6 .063 SIZE 2" X 7" PO 9002827 IAW B727 SRMSDR DHL2006752504Frame · puncturedFOUND PUNCTURE HOLE ON UPPER SEGMENT OF FRAME AT BS 480 STR 26R (FWD PIT, UNDER FLOOR SUPPORT STAP). REMOVED TRANSMISSION PANEL IN FWD BAG RT FROM 480 TO 560 FOR ACCESS IAW SRM 51-30-2 CUT OUT DAMAGED AREA SIZE 1 INCH X .5 INCH IAW SRM 51-10-1 FABBED ANGLE RSDR DHL2006752524Attach Fitting · crackedFOUND RT WING NR 5 L/E SLAT ACT ROD END ATTACH FITTING, INTERNAL ANGLES INBOARD AND OUTBOARD ARE CRACKED. REMOVED INBOARD AND OUTBOARD RIBS ON RIGHT WING NR 5 SLAT ACT END ATTACH TO FITTING, IAW B727 SRM 51-30-2, FABRICATED 2 EA RIBS FROM 7075-0 .040 SIZE 16"SDR DHL2006752523Intercostal · bentFOUND BENT INTERCOSTAL BS 1030-1050, STR 25R. REMOVED INTERCOSTAL AT STA 1030-1050 AT STR 25R IAW B727 SRM 51-30-2. FABRICATED FROM 2024-T3 .050 SIZE 22" BY 5" PO> 503081 IAW B727 SRM 51-40-3 AND SRM 53-10-1. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 5SDR DHL2006752503Spar · corrodedDISCREPANCY FOUND NR 110621; RT/WING AT WS 170 APPRX L/E CAVITY FRONT SPAR LWR CHORD HAS CORROSION. REMOVED CORR ON RT/WING LWR SPAR AT WS 170 ORIGINAL THICKNESS .413 MAT REMOVED .109 MATL REMAINING IS .304 AND IS OUT OF LIMITS IAW SRM 57-10-1 FIG2 FABBED DSDR DHL2006752502Skin · crackedDISCREPANCY FOUND NR 110620; CRACK INDICATION ON NR 2 SLAT SKIN UPPER SURFACE 6 INCHES O/B OF ACTUATOR MARKED. CUT OUT DAMAGED AREA DIMENSION 4" X 2" AND FABBED NEW DOUBLER FROM MATERIAL USE 2024 T3 0.80 PO 9002459 IAW B727 SRM 57-50-3 FIG 1 TREATED AND PRIMESDR DHL2006752501Skin · dentedDISCREPANCY FOUND NR 110587; DENT LT SIDE FUSELAGE SKIN AT STA 373 STR. 24L (MARKED). DENT IS IN AREA NOT ALLOWED IAW SRM SPECIFICATIONS. CUT OUT DAMAGED AREA DIM 3INCHES X 1INCH FABBED FILLER 2024-T3 .050 PO 9002695 3.1 INCHES X 1.3 INCHES AND DOUBLER 2024-SDR DHL2006752500Hinge · crackedDISCREPANCY FOUND NR 110541; EXT FUSE BS 510 MCD FWD HINGE SECT HAS FWD LOBE CRACKED. REMOVED FWD SECTION OF MCD HINGE AT BS 510-530 AND REPLACED WITH NEW SECTION PO NR 9002527 P/N MS20001-16-7200 IAW B727 AEI M/M CHAPTER 52 FIG 5201B, REV F DATE 01-22-01SDR DHL2005752005Battery · inoperativeDURING STBY TEST EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERYS, OPS CK NORMAL IAW MM 33-50-101, P/N MISC-O62.SDR DHL2005752004Light · inoperativeDURING SBY PWR CHECK, FWD ENTRY DOOR EXIT LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED FWD ENTRY DOOR EXIT LIGHT IAW M/M 33-50-00, CKS NORMAL.SDR DHL2005752003Battery Pack · inoperativeENTRY DOOR EMERGENCY LIGHTS INOP. REPLACED PACK ASSY PER MM 3350, OP NML.SDR DHL2005752002Lock · malfunctionedCOCKPIT DOOR LOCKS WHEN CLOSED AND CAN`T BE OPENED FROM OUTSIDE. CYCLED COCKPIT DOOR SEVERAL TIMES NO AUTO LOCKING FEATURE NOTED, DOOR OPS CHECKS NORMAL IAW MM 52-50-10.SDR DHL2005752001Smoke Hood · damagedCREW PBE ON COCKPIT DOOR HAS RED BUTTON EXTENDED BEYOND BOX. REMOVED AND REPLACED CREW PBE IAW B-M/M 25-60-02.SDR DHL2004752010Stabilizer · damagedLEFT HORIZONTAL STAB AND ELEVATOR DAMAGED FROM TAXIING A/C TURNING INTO SPOT. A/C WAS PARKED. REPLACED LEFT ELEVATOR ASSY IAW BMM 27-30-01. RIG AND OPS CHECKED IAW BMM 27-30-01. REPLACED LT HORIZ STAB TIP ASSY IAW 55-10-11. NO FURTHER NOTED. OPS OK.SDR DHL2004752009Indicator · failedF/O'S A/S INDICATOR FAILED ON T/O ROLE AT 80KIAS INDICATED 60 KIAS AT 165,000, LBS 18 DEGREES C, PA 830 IN NORMAL BRAKE ENERGY ZONE NOTE: 0 KIAS INDICATION IS THE SAME AS 60 KIAS THERE WAS NO A/S INDICATION IE NEEDLE MOVEMENT ON THE CO-PILOTS SIDE A/S FAILED FSDR DHL2004752007Warning Horn · activatedTAKEOFF WARNING HORN SOUNDED WHEN T/O POWER WAS APPLIED FLAPS 15 DEG TRIM AT 5.0 ABORTED T/O AT LESS THAN 5 KNOTS GROUND SPEED. PERFORMED T/O WARNING SYSTEM TEST IAW B-727 M/M 31-26-1. NO DEFECTS FOUND. OK FOR FURTHER SERVICE.SDR DHL2004752006Accessory Unit · malfunctionedAFTER GEAR RETRACTION, RIGHT MAIN LANDING GEAR UNSAFE LIGHT AND DOOR LIGHT REMAIN ILLUMINATED. PERFORM ABNORMAL PROC ON 6.2.70. LANDING GEAR EXTENDED NORMALLY. REDISPATCHED TO KDAL AT 0811 PER JRM. REMOVED & REPLACED LGAU & OPS CK GOOD PER B727 MM 32-09-12SDR DHL2004752005Accessory Unit · malfunctionedAFTER T/O, LANDING GEAR LEVER WOULD NOT MOVE PAST (OFF) POSITION. CONDUCTED ABNORMAL PROCEDURE T/O CONFIG WARNING HORN SOUNDED AT FLAPS 2 DEG. DIVERTED BACK TO KDAL IAW RE-RELEASE AT 0359Z (SR). REMOVED AND REPLACED LGAU IAW MM 32-09-121. OPS CK GOOD. LG HANSDR DHL2004752004Smoke Detector · malfunctionedIN FLIGHT LOWER CARGO FIRE DETECTION. FOUND SMOKE DETECTOR S/N: 8650, TO BE GIVING FALSE WARNING. REMOVED AND REPLACED ALL 5 FORWARD SMOKE DETECTORS IAW B727 M/M 26-16-01, REMOVED AND REPLACED CENTRAL CONTROL UNIT (CCU) IAW B727 M/M 26-16-20, OPS CHECKED SERSDR DHL2004752003Battery · dischargedAFTER T/O FORWARD FIRE LOWER CARGO INDICATION, AFTER SEVERAL MINUTES LIGHT EXTINGUISHED. DEFERRED FORWARD LOWER CARGO COMPARTMENT FIRE DETECTION PER MEL 26-19, COMPLIED WITH SPECIAL PROCEDURES (FORWARD PIT EMPTY). PLACARDS INSTALLED DMI 16604. WORKING DMI 1SDR DHL2004752002Compressor · stalledREJECTED TAKEOFF FOR INFORMATIONAL PURPOSES ONLY WT=152,000 LBS, TEMP=12.6, PRESS ALT=SEA LEVEL, AIRSPEED=60 KNOTS. SUSPECTED COMPRESSOR STALL WITH AN AUTO PACK TRIP. WIND WAS 89 AT CROSSWIND AT 10 KNOTS. ALSO FOR INFORMATIONAL PURPOSES ONLY. INSPECTED ENGSDR DHL2004752001Light · dislodgedCOCKPIT EMERGENCY EXIT LIGHT FELL DURING FLIGHT. RE-SECURED COCKPIT EMERGENCY EXIT LIGHT, CHECKED GOOD IAW B-727 M/M 33-50-101.SDR DHL2004752514Skin · bentDURING C-CHECK, RT AFT OVERWING EMERGENCY EXIT HATCH AT AFT TOP EXTERIOR SKIN EDGE IS BENT AND DENTED. CLEANED AREA AND FOUND SKIN TO BE CRACKED AND OUT OF LIMITS IAW B-727 SRM 52-00-02. CUT OUT DAMAGED AREA SIZE 1 X 1.5 INCH ON RIGHT AFT OVERWING EMERGENCY SDR DHL2004752510Skin · dentedDURING C-CHECK, FUSELAGE EXTERIOR AT BS 420, BETWEEN STR 23R AND STR 24R DENT IN SKIN. DAMAGE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA 1 INCH DIA AND FABBED FILLER FROM 2024-T3 .050 PO 900471 DIM 1 INCH AND DOUBLER FROM 2024-T3 .063 PSDR DHL2004752513Rib · damagedDURING C-CHECK, NR 5 SLAT AT ACTUATOR ATTACH HAS INBOARD ATTACH FRAME CRACKED. REMOVED AND REPLACED DAMAGED RIBS P/N 65-17276-9 PO 342198 AND 65-17276, PO 343446 IAW B-727 SRM 51-20-12 AND 51-30-2.SDR DHL2004752509Skin · crackedDURING C-CHECK, FUSELAGE SKIN CRACK AT FWD ENTRY DOOR LOWER HINGE CUT OUT, VERIFIED BY NDT INSP. CUT OUT DAMAGED AREA DIM 1.625 X 1 INCH AND FABBED FILLER FROM 2024-T3 .080 PO 900474 DIM 1.625 X 1 INCH AND DOUBLER FROM 301 1/2 HD .063 PO 900125 DIM 15.75 X 6 SDR DHL2004752512Panel · dentedDURING C-CHECK, LT WING UPPER T/E PANEL WBL 124 HAS ONE SMOOTH DENT OUTBOARD AND ONE SHARP DENT INBOARD. CUT OUT 2 DENTED AREAS ON LT WING UPPER T/E PANEL, 1 APPROX 1.75 INCH DIA & 2 APPROX 2.25 INCH DIA. FABRICATED FILLERS 1 APPROX 1.75 INCH & 2 APPROX 2.2SDR DHL2004752504Skin · delaminatedDURING C-CHECK, LT INBOARD FOREFLAP UPPER INBOARD SURFACE PREVIOUS REPAIR DELAMINATED. REMOVED DELAMINATED PREVIOUS REPAIR. FABRICATED FILLER APPROX 13 INCH X 13 INCH AND DOUBLER APPROX 13 INCH X 5 INCH FROM 2024 T3 .016 PO 900291. CLEANED, PREPPED, APPLIEDSDR DHL2004752508Angle · crackedDURING C-CHECK, RT WING WBL 130.7 HAS CRACK IN L-ANGLE OF L/E FLAP AREA. STOP DRILLED CRACK IAW 727 SRM 51-10-1 & FABBED REPAIR ANGLE FROM 2024T3050 DIM 6 INCH X 2 INCH PO 900471 IAW 727 SRM 51-40-3 FIG 1. REPAIR TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALSDR DHL2004752505Stiffener · corrodedDURING C-CHECK, RT WING HAS L/E OF FRONT SPAR VERTICAL STIFFENER. REMOVED DAMAGED STIFFENER IAW B-727 SRM 51-30-2. FABBED NEW FROM BAC 1517-1406 PO 3448268 DIM 32 INCHES AND FILLER (SHIM) FROM 7075-T6 .190 PO 314676 DIM 27.5 X 1.5 INCH IAW B-727 SRM 57-10-2SDR DHL2004752506Skin · damagedDURING C-CHECK, FUSELAGE EXT SKIN BS 1090 STR 2312 IS CREASED. DAMAGE BELOW STRINGER OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024 T3 .063 PO 900355 DIM 9.3125 INCH X 3 INCH, 2 EACH SHIMS SAME MAT DIM 3.5 INCH X SDR DHL2004752501Stringer · dentedDURING C-CHECK, REPAIR AT BS 1130 BETWEEN STR 21R TO 24R DENTED AND ENDS ON STRINGER. REMOVED PREVIOUS REPAIR AND FOUND SKIN DENTED OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. REMOVED RT AFT SIDEWALL IN AFT PIT FOR ACCESS IAW B-727 MM 25-52-02. CUT OUT DAMAGSDR DHL2003752501Stringer · dentedDURING "C" CHECK, REPAIR AT BS 1130 BETWEEN STR 21 RT TO 24 RT DENTED AND ENDS ON STRINGER. REMOVED PREVIOUS REPAIR AND FOUND SKIN DENTED OUT OF LIMITS IAW SRM 53-30-1 FIG. 1.REMOVED RT AFT. SIDEWALL IN AFT. PIT FOR ACCESS IAW M.M. 25-52-02. CUT OUT DAMAGSDR DHL2004752511Skin · dentedDURING C-CHECK, FUSELAGE EXTERIOR ABOVE STR 28R BS 500 DENTED (PREVIOUSLY MAPPED). CUT OUT DAMAGED AREA DIM .5 X 5 INCH AND FABBED REPAIR DOUBLER FROM 2024 T3 .050 DIM 10 X 9 INCH PO 900414 IAW B-727 SRM 53-30-3 FIG 1. DOUBLER TREATED AND PRIMED IAW B-727 SSDR DHL2004752507Skin · corrodedDURING C-CHECK, FUSELAGE EXTERIOR BS 300 TO 294.5 ABOVE STR 25R AREAS OF SKIN BULGING AND DENTS. REMOVED RT WALKWAY HORIZ WEB FOR ACCESS, AREAS FOUND TO BE OUT OF LIMITS. CUT OUT 2 EA AREAS 5 INCH X 1.625 INCH + 2.75 INCH X 1.75 INCH. FABBED 2 FILLERS FROMSDR DHL2004752502Skin · dentedDURING "C" CHECK, FUSELAGE EXTERIOR NR 1 CARGO DOOR SKIN IS DENTED LOWER AFT SIDE. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 52-00-02. CUT OUT DAMAGED AREA DIM. 1.7500 INCHES X 1INCH AND FABRICATED DOUBLER REPAIR FROM MAT 2024-T3 .050 P.O.NR 900471 DIM. 7.250SDR DHL2004752503Skin · dentedDURING C-CHECK, FUSELAGE EXTERIOR BS 380.0 BETWEEN STR 22 AND 23R SKIN IS DENTED (PREVIOUSLY MAPPED). DENT FOUND TO BE OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024-.T3 .040 PO 90489 DIM 2.6875 INCH X 1.1875 INCH AND D
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