N25705

Service difficulty reports · 111

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 = 'N25705' 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.

SDR CALA2023011300108Landing Gear · malfunctionedGEAR WOULD NOT RETRACT ON TO OUT OF RDU ACP ALTERNATE LANDING GEAR TEST REF AMM 32-31-51-400-801 AFTER CLOSING ALT GEAR EXTENSION ACCESS DOOR, ALTERNATE LANDING GEAR TEST CHECKED NORMAL. AIRCRAFT WAS JACKED AND LANDING GEAR WAS RETRACTED AND EXTENDED RETRACT Jan 13, 2023 · N25705 · Boeing 737724 · Landing Gear Retraction/Extension SystemSDR CALA2022110203016Stop Fitting · crackedPDA 3 LEFT PACK EXHAUST DIFFUSER DOOR STOP (L-ANGLE) CRACKED AND PARTIALLY MISSING.Nov 1, 2022 · N25705 · Boeing 737724 · Cabin Cooling SystemSDR CALA2022051801270Skin · crackedRIGHT WHEEL WELL VERTICAL PRESSURE DECK WEB CRACKED BETWEEN RBL 40.0 AND RBL 45.64 -- SEE PHOTO,S PHOTO ADDED -- CRACK IS APPROX 2" LONG ......IDT AC NEEDED TO VERIFY AND MARK ENDS OF CRACK REPAIR AS GIVEN IN REPAIR 3 NO MORE THAN 6000 FLIGHT CYCLES OR 24 MONMay 16, 2022 · N25705 · Boeing 737724 · Wing, Center BoxSDR CALA2021061400873Pcu · leakingSTANDBY RUDDER POWER CONTROL UNIT APPEARS TO BE LEAKING AT FORWARD LOWER "B" NUT OR UNION. SECURED B NUTS. CLEANED AREA. OPPERATED STANDBY HYDRAULICS AND CYCLED RUDDER SEVERAL TIMES. NO LEAKS NOTED.Jun 14, 2021 · N25705 · Boeing 737724 · Hydraulic System, MainSDR CALA2021052400708Window Frame · crackedSMALL CRACK NOTED ON L1 WINDOW FRAME WHILE AIRCRAFT WAS PRESSURIZED. SEE ATTACHED PICTURES ADDITIONAL PICS.CRACK LOCATED ON C-D POST.CRACK. MEASURES 0.9" LENGTH. IAW AVO#ESC210516-0705-1 R.A. PERFORMED HFEC INSPECTION ABOVE WELL AS DVI OF SAME AREA. CRACK INDMay 22, 2021 · N25705 · Boeing 737724 · Fuselage Main, StructureSDR CALA2021051700666Windshield · leakingREFERENCE LOG PAGE 6300515 COCKPIT AIR NOISE / LEAK. FOUND UPPER FWD EYEBROW WINDOW LEAKING FROM LOWER SEAL AREA.UPON PRESSURIZING ACFT, FOUND LH #4, LH #5, AND LH #2 SLIDING WINDOW LEAKING SEVERELY.#4 LH AND #5 LH WINDOW BLANKING PLATES REMOVED FOR INSPECTIONMay 15, 2021 · N25705 · Boeing 737724 · Flight Compartment WindowsSDR CALA2021033000402Latch · malfunctionedGEAR WOULD NOT RETRACT AFTERTAKEOFF FOUND ALT LANDING GEAR DOOR IN CP NOTLATCH. CLEANED LATCH AND SECURED DOOR CLOSED. PREFORMED CHECK PER AMM 32-35-00-820-801 ALL GEAR ACT WENT TO RAISED POSITION . AC OK FOR SERVICEMar 30, 2021 · N25705 · Boeing 737724 · Landing Gear Door Retract SectionSDR CALA2020010600107Fitting · crackedSHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED SUPPORT TASK 58458 36 REMOVED AND REPLACED SHEAR FITTINGS IAW B737-700. SRM 51-40-02 A ND DWG NO 111 A 2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION, 12/23/19Dec 23, 2019 · N25705 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2020010600033Fitting · crackedSHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED. SUPPORT TASK 5845 843 REMOVED AND REPLACED SHEAR FITTING. IAW B737-700. SRM 51-40-02, DWG NO. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSP ECTION U356089, 12/23/19Dec 23, 2019 · N25705 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2020010600001Fitting · crackedSHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED. SUPPORT TASK 5845 835 REMOVED AND REPLACED SHEAR FITTING. IAW B737200 SRM 51-40-02 AND DWG AND 111 A 2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL I NSPECTION U356089, 12/23/19Dec 23, 2019 · N25705 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2020010600032Fitting · crackedSHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED. SUPPORT TASK 5845 841 REMOVED AND REPLACED SHEAR FITTING. IAW B737-700. SRM 51-40-02 A ND DWG NO. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL I NSPECTION U356089, 12/23/19Dec 23, 2019 · N25705 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2020010600031Fitting · crackedSHEAR FITTING AT STA 540 LBL 32.40 IS CRACKED. SUPPORT TASK 5845 840 REMOVED AND REPLACED SHEAR FITTING. IAW B737-700. SRM 51-40-02 A ND DWG NO. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL I NSPECTION U356089, 12/23/19Dec 23, 2019 · N25705 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2020010600030Fitting · crackedSHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. SUPPORT TASK 5845 839 REMOVED AND REPLACED SHEAR FITTING. IAW B737-700. SRN 51-40-02 A ND DWG NO.111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL IN SPECTION U356089, 12/23/19Dec 23, 2019 · N25705 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2020010600029Fitting · crackedSHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED. SUPPORT TASK 58458 38 REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D DWG NO. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL IN SPECTION U356089, 12/23/19Dec 23, 2019 · N25705 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2020010600028Fitting · crackedSHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED. SUPPORT TASK 5845 837 REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D DWG NO 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INS PECTION U356089,12/23/19Dec 23, 2019 · N25705 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2020010600023Fitting · crackedSHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. SUPPORT TASK 5845 834 REMOVED AND REPLACED SHEAR FITTING. IAW B737-700. SRM 51-40-02 A ND DWG NO 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL U3 56089, 12/23/19Dec 23, 2019 · N25705 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2020010600022Fitting · crackedSHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED. SUPPORT TASK 58458 33 REMOVED AND REPLACED SHEAR FITTINGIAW B737-700. SRM 51-40-02 AND DWG NO. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INS PECTION U356089, 12/23/19Dec 23, 2019 · N25705 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2019092801658Spring · brokenENTRY DOOR PROBLEM REPORTED BY OPERATIONS UPDATED MAA CODE FIX USING VENDOR MAA SCREEN INSPECT THE ENTRY DOOR FOR ANY DEFECTS AND CONTACT TOMC LOCKED BY TOMC OCM FOUND 1L DOOR EXT HANDLE WILL NOT SPRING BACK INTO RECESSED POSITION. ADD EMP: MTC FERRY COMPLETEDSep 27, 2019 · N25705 · Boeing 737724 · Passenger/Crew DoorsSDR CALA2019020100193Landing Gear · malfunctionedON TAKEOFF GEAR DID NOT RETRACT. RAN GEAR DISAGREE CHECKLIST. NO CHANGE PERFORMED BITE ON PSEU AND FOUND NO CURRENT /EXISTING OR FAULT HISTORY. JACKED PLANE FOR GEAR SWING AND FOUND HE GER HANDLE NOT GOING PAST THE "OFF" POSITION. COULD NOT HEAR CONTROL LEVEJan 29, 2019 · N25705 · Boeing 737724 · Landing Gear Retraction/Extension SystemSDR CALA2017082102829Battery Pack · inoperativeCABIN EMERGENCY LIGHT MOUNTED ON OVERHEAD BIN ABOVE PAX SEAT ROW 24DEF INOPERATIVE. REMOVED AND REPLACED BATTERY PACK & CHARGER. OPS CHECKS NORMAL IAW WDM 33-51-14.Aug 21, 2017 · N25705 · Boeing 737724 · Emergency LightingSDR CALA2017022400442Battery Pack · weakRT WINDOW ESCAPE EMERGENCY EXIT LIGHT BATTERY WEAK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND PREFORMED OPS TEST NORMAL REF B737 AMM 33-51-06Feb 24, 2017 · N25705 · Boeing 737724 · Emergency LightingSDR CALA2017022400455Floorbeam · corrodedMAIN CABIN FLOOR STRUCTURE STA 328 BETWEEN RBL 46 AND RBL 53 HAS 2EA SPOTS OF CORROSION AT FLOOR SUPPORT BEAM UPPER FLANGE. REMOVED CORROSION FROM FLOORBEAM AT STA 328 RBL 46 AND 53 REF SRM 51-10-02 FOUND REWORKED AREA RBL 53 OUT OF LIMITS REF ECRA 5321-01330.Feb 22, 2017 · N25705 · Boeing 737724 · Fuselage Main, Floor BeamSDR CALA2017022400450Frame · dentedAFT CARGO COMPARTMENT FRAME AS BS 727E DENTED BETWEEN STR 24L AND 25L. PERFORM REPAIR TO STA 727E FUSELAGE LOWER FRAME PER MIA RES 2011833 WITHOUT DEVIATIONS THE APPLICABLE WORK INSTRUCTIONS AND REPAIR FIGURE FROM RES 2011833-46 ARE INCLUDED ON PAGES 3-6 OF ECFeb 22, 2017 · N25705 · Boeing 737724 · Fuselage Main, FrameSDR CALA2017022000419Skin · crackedCRACK FOUND AT RT HORIZONTAL STAB LOWER SKIN HSS 138.70 AND 26 INCHES FWD OF AFT SPAR. CRACK LENGTH .500 INCH. REPAIRED THE SKIN IAW SRM 55-10-01, REPAIR 11, FIGURE 204.Feb 18, 2017 · N25705 · Boeing 737724 · Horizontal Stabilizer, Plate/SkinSDR CALA2017021700411Structure · crackedR1 DOOR INTERNAL STRUCTURE AT BOTTOM GATE ACTUATING ROD PASS THRU HOLE CRACKED. REPAIRED IAW ECR A 5210-02805, FIGURE 3.Feb 17, 2017 · N25705 · Boeing 737724 · Service DoorsSDR CALA2017021700410Skin · crackedCRACK FOUND ON RT HORIZONTAL STAB LOWER SKIN. REPAIRED IAW SRM 55-10-01, FIGURE 204.Feb 17, 2017 · N25705 · Boeing 737724 · Horizontal Stabilizer, Plate/SkinSDR CALA2017021700409Frame · corrodedBS 303 BETWEEN STRINGERS 16 - 17L INBD FLANGE OF FRAME HAS CORROSION. REPAIRED IAW ECRA 5310-7073.Feb 17, 2017 · N25705 · Boeing 737724 · Fuselage Main, BulkheadSDR CALA2016112600972Sensor · faultyNOSE LANDING GEAR NOSE GEAR GREEN LIGHT DOES NOT GO OFF WITH LANDING GEAR LEVER AT UP, NOSE GEAR RED LIGHT ON NOSE GEAR UNSAFE INDICATION. REPLACED SENSOR PER AMM32-61-51-400-802. ACCOMPLISHED PSEU BITE CHECK NO FAULTS AND PERFORMED OPS TEST AMM32-61-51-710-Nov 26, 2016 · N25705 · Boeing 737724 · Landing Gear Position and WarningSDR CALA2016091400650Valve · damagedFL 390, CABIN ALTITUDE WARNING HORN AND LIGHT, PRECEDED BY RIGH T BLEED TRIP OFF LIGHT. PERFORMED NR 2 ENG HEALTH CHECK IAW AMM 36-11-00-700-803, REPLACED THE NR 2 ENG HIGH STAGE VALVE IAW AMM 36-11-06.Sep 14, 2016 · N25705 · Boeing 737724 · Pneumatic Distribution SystemSDR CALA2014072100948Intercostal · corrodedFOUND HEAVY INTERGRANULAR CORROSION ON AFT CARGO INTERCOSTAL AT BS 847 BETWEEN STRINGERS 25L & 26L AT BASE OF BULKHEAD VERTICAL STANCHION. INSTALLED FABRICATED INTERCOSTAL IAW DWG 149A8102 REV B & SRM 51-40-02.Jul 17, 2014 · N25705 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2014072100946Skin · dentedRAMP DISCOVERED AFT CARGO DOOR DENT LOCATED 18.5 INCHES FROM AFT EDGE & 13.5 INCHES FROM TOP EDGE. INSPECTED DENT & FOUND TO BE OUT OF LIMITS, DEPTH IS .147 INCHES, MAX ALLOWED IS .125 INCHES. INSTALLED, SEALED & PAINTED REPAIR IAW SRM 52-00-01 REPAIR 2.Jul 16, 2014 · N25705 · Boeing 737724 · Cargo/Baggage DoorsSDR CALA2014071600935Pressure Panel · crackedCENTER WING BOX REAR SPAR VERTICAL PRESS WEB CRACKED BETWEEN LBL 40.00 & 45.64. INSTALLED REPAIR IAW SRM 57-10-10 REPAIR 3 & REPAIRED SECONDARY FUEL VAPOR BARRIER IAW AMM 28-11-00.Jul 14, 2014 · N25705 · Boeing 737724 · Fuselage Main, BulkheadSDR CALA2014071400913Retaining Clip · crackedLEFT WING TE CAVITY BULB SEAL RETAINER CRACKED WERE IT ATTACHED TO THE DEFLECTOR RIB. R & R CLIP 115A6260-1 IAW DWG 115A6260 & 737SRM 51-40-02.Jul 14, 2014 · N25705 · Boeing 737724 · Wing Miscellaneous StructureSDR CALA2014071400912Angle · corrodedLOWER RAIL ASSEMBLY AT STATION 500D FOR FBB AFT BULKHEAD CTR WALL PNL HAS CORROSION. R & R LOWER RAIL ASSEMBLY. PN 143A9485Y35 AT STATION 500D IAW SRM 51-40-02 & IPC 53-11-01-43.Jul 13, 2014 · N25705 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2014053000699Transmitter · faultyDIVERT TO LAX. ON APPROACH TO SNA WHEN EXTENDING FLAPS TO 1 THE FLAP INDICATOR NEEDLE STOPPED JUST PRIOR TO 1 BAND & LE FLAPS TRANSIT LIGHT ILLUMINATED. RAN QRH & THEN DIRECTED TO A MANUAL FLAP EXTENSION, USED ALT FLAP EXTENSION TO EXTEND FLAPS TO 15 IAW QRHMay 29, 2014 · N25705 · Boeing 737724 · Trailing Flap Position Indicating SystemSDR CALA2012100800649Frame · crackedCRACK INDICTION FOUND FRAME BS 400 MID FREQ ONLY. INBD FASTENER NOT EXTENDING INTO RADIUS ACCOMPLISHED REPAIR IAW ECRA 5310-05459.Oct 5, 2012 · N25705 · Boeing 737724 · Fuselage Main, FrameSDR Z6WR20120302003Panel · delaminatedCMM 78-31-37 REV 23 FIG 35 ITEM 40B. THE 315A2101-41 INNER WALL BONDED PANEL HAS AN AREA OF DISBOND (PERF SKIN TO CORE) THAT MEASURES 1.5 X 24.5". AFTER REMOVING THE DISBONDED PORTION OF THE SKIN IT WAS DISCOVERED THAT THE PERF SKIN WAS PERPARED INCORRECTLY Mar 2, 2012 · N25705 · Boeing 737724 · Engine Thrust ReverserSDR Z6WR20120301002Ring · wornTHE 315A2222-5 CASCADE RING HAS EXTENSIVE WEAR/DAMAGE CT THE AFT LWR ATTACHING BOLT LOCATION. HOLE SHOULD BE .3750 -.3754. ACTUAL IS ELONGATED TO APPROX .6210 WITH HEAVY WEAR/MISSING MATERIAL CT THE NUT SIDE. THE 315A2402-5 LATCH BEAM HAS A CORRESPONDING ELOMar 1, 2012 · N25705 · Boeing 737724 · Engine Thrust ReverserSDR CALA2012022400123Frame · corrodedSUPPORT TASK REF EA 5310-04716 REV C CRACK INDICATION FOUND FRAME 907L BOTH MID AND HIGH FREQ INB FASTENER NOT EXTENDING INTO RADIUS. REPAIRED PER ECRA 5310-05458.Feb 24, 2012 · N25705 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012021500100Frame · crackedSUPPORT TASK - REF EA 5310-04716 REV C CRACK INDICATION FOUND AT FRAME 440 L MID FREQ ONLY INBD FASTENER NOT EXTENDING INTO RADIUS CABIN FRAME 440 L. REPAIRED IAW EA 5310-04716 REV C.Feb 14, 2012 · N25705 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012021500099Frame · crackedREF EA 5310-04716 REV C CRACK INDICATION FOUND FRAME 747L BOTH MID AND HIGH FREQ-NOT EXTENDING INTO RADIUS. REPAIRED PER EA 5310-04716 REV C.Feb 13, 2012 · N25705 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012021300098Frame · crackedSUPPORT TASK - REF EA 5310-04716REV C CRACK FOUND FRAME STA 727D R MID FREQ AND HIGH FREQ I/B FASTENER NOT INTO RADIUS. REPAIRED IAW EA 5310-04716 SEE ATTACHED 44.0008FOR ADDITIONAL WORK ACCOMPLISHED.Feb 13, 2012 · N25705 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012021300097Frame · crackedREF EA 5310-04716 REV C CRACK INDICATION FOUND FRAME 827L MID FREQUENCY INBD FASTENER NOT EXTENDING INTO RADIUS. REPAIRED FRAME AT STA 827L IN ACCORDANCE WITH EA 5310-04716 REV C.Feb 12, 2012 · N25705 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012021300095Frame · crackedSUPPORT TASK - REF EA 5310-04716 REV C OP1 CRACK INDICATION FOUND FRAME 747R BOTH MID AND HIGH FREQ INBD FASTENER NOT EXTENDING INTO THE RADIUS. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND INSTALLED PARTS AS PER EA 5310-04716 REV C.Feb 12, 2012 · N25705 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012021300094Frame · crackedSUPPORT TASK - REF EA5319-04716 REV C CRACK FOUND FRAME 787 R MI D FREQ AND HIGH FREQ I/B FASTENER NOT INTO RADIUS. REPAIRED STA 787 FRAME BETWEEN STR 8 AND STR 9 REF EA 5310-04716 REV C REF FORM 44.0008 FOR WORK DETAILS.Feb 12, 2012 · N25705 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012021300093Frame · crackedSUPPORT TASK - REF EA5310-04716 REV C CRACK FOUND FRAME STA 867L NOT INTO THE RADIUS. SHOULD BE A/C 705 ACCOMPLISHED PERMANENT REPAIR PER EA5310-04716 REV C .Feb 12, 2012 · N25705 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012021000084Frame · crackedSUPPORT TASK REF EA5310-04716 REV C CRACK INDICATION FOUND AT FRAME 827R, NO EXPENDING INTO THE RADIUS. REPAIRED PER EA5310-04716 REV C .Feb 10, 2012 · N25705 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012021300091Frame · crackedSUPPORT TASK - REF EA5310-04716 REV C CRACK FOUND FRAME STA867R M ID FREQ AND HIGH FREQ I/B FASTENER NOT INTO RADIUS. REPAIRED AS PER ECRA 5310-04716 REV C SEE FORM 44.0008 FOR WORK ACCOMPLISHED.Feb 10, 2012 · N25705 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012021000082Frame · crackedREF EA 5310-04716 REV C CRACK INDICATION FOUND FRAME 787L BOTH MID AND HIGH FREQ INBD FASTERNER NOT EXTENDING INTO RADIUS. REPAIRED FRAME AT STATION 787L PER EA 5310-04716 REV C SEE FORM 44.0008 FOR WORK PERFORMED.Feb 10, 2012 · N25705 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012021000081Skin · crackedSUPPORT TASK - C SCAN INSP OF RIGHT STAB PER EA 5510-01843 FOUND A CRACK INDICATION AT LOWER SKIN SURFACE STA 161.04 RIB 9 AND AFT OF FRONT SPAR APPROX 6". REPAIRED RT STAB LOWER SKIN PER SRM 55-10-01 REPAIR 11 SEE BL0 CK 42 AND ATTACHED 44.0008 FOR ALL PARTIFeb 9, 2012 · N25705 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
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