Boeing 727-2J0
Service difficulty reports · 220
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 = '7272J0' 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 = '7272J0' 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 P762004F00003Bracket · crackedLT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.SDR P762004F00002Bracket · crackedLT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.SDR P762004F00000Bracket · crackedLT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.SDR C7WA200400039Hydraulic Line · chafedAT FLIGHT LEVEL 20.0 A-SYSTEM QUANTITY AND PRESSURE WENT TO ZERO. REPLACED CHAFED HYDRAULIC HOSE AT NR 2 ENGINE DRIVEN HYDRAULIC PUMP OPERATIONAL AND LEAK CHECK NORMAL.SDR C7WA200400002Warning Light · illuminatedFLT RETURN, LT AND RT GEAR DOORS LIGHT ILLUMINATED. RECYCLED GEAR LIGHTS REMAINED ON. INSPECTED MAIN LANDING GEAR DOORS, NO DISCREPANCIES FOUND. RERACKED MAIN LANDING GEAR ACCESSORY UNIT. CYCLED DOORS SEVERAL TIMES MLG DOOR INDICATORS CHECKED NORMAL PER MMSDR DHL2004749003Start Valve · openNR 2 START VALVE OPEN ON TAKEOFF ROLL. TAKEOFF REJECTED PRIOR TO 80 KNOTS. AIRCRAFT WEIGHT = 149700 LBS, IAS = 70 KNOTS, OAT = 6 C, PA = 3740, BRAKE ENERGY ZONE NORMAL. REMOVED AND REPLACED START VALVE IAW M/M 80-10-00. GROUND RUN, FUNCTION CHECK OK. NOTESDR P9RA20040006Lamp · inoperativeDURING LINE CHECK, FOUND CENTER AISLE EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT IAW BMM 33-50-11.SDR GAIA04002OPValve · malfunctionedFLT 2872 - LAX-FWA - DURING CRUISE, THE FILGHT CREW NOTICED THAT THE NR 2 FUEL CROSS FEED VALVE APPEARED TO BE CLOSED. THE CREW DECIDED TO MAKE A PRECAUTIONARY LANDING IN PHX. OPENED THE NR 2 TANK TO ENGINE VALVE AND SAFETIED OPEN PER THE BOEING DISPATCH DEVSDR 2004F00328Light · dislodgedFOUND EMERGENCY LIGHTING STRIP IN FRONT OF AFT GALLEY IS PULLED LOOSE FROM FLOOR. SECURED EMERGENCY LIGHTING STRIP IAW SAFTGLO MM 33-60. (M)SDR 2004F00260Wire · brokenDEPARTING SJU, ON TAKEOFF ROLL, AFT AIRSTAIR LIGHT CAME ON. EXITED RUNWAY AND CYCLED AIRSTAIRS AND THE LIGHT EXTINGUISHED. CONTACTED DISPATCH FOR NEW RELEASE AND PROCEEDED NORMALLY. DURING FLIGHT TO SFB, LIGHT ON AFT AIRSTAIR BEGAN FLICKERING AND THEN REMAISDR 2003F00658Battery · inoperativeR2 ENTRY DOOR EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY SUPPLY IAW BMM 33-50-71. (M)SDR DHL2003749514Skin · dentedDURING C-CHECK, SKIN DENT LT WING LEADING EDGE AT LEADING EDGE STA 130 (ABOVE I/B EDGE OF NR 3 L/E FLAP). CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024 T3 .040 PO 90020 DIM 2.5 X 1.5 INCHES AND DOUBLER FROM 2024 T3 .050 PO 90096 DIM 6.5 X 6 INCHES IAW B-72SDR DHL2003749500Skin · dentedDURING C CHECK, SKIN DENT LT WING L/E AT LEADING EDGE STA. 130 ( ABOVE IB EDGE OF NR 3 LE FLAP ). CUT-OUT DAMAGED AREA AND FABBED FILLER FROM 2024 T3 .040 P.O. NR 90024 DIM 2.5 INCH X 1.5 INCH AND DOUBLER FROM 2024 T3 .050 P.O. NR 90096 DIM. 6.5 INCH X 6 INCHSDR DHL2003749511Floor Support · dentedDURING C-CHECK AT FLIGHTSTAR IN JACKSONVILLE, FL., AFT PIT FLOOR SUPPORT FROM STA 950E TO 990 LBL 6 HAS SEVERAL DENTS. REMOVED AFT PIT FLOOR SUPPORT FROM STA 950 E TO 990 LBL 6 IAW B727 SRM 51-30-2. DRILLED NEW FLOOR SUPPORT PO 328319, P/N BAC 1500-6199 DIM.SDR DHL2003749508Floor Support · dentedDURING C CHECK, PIT FLOOR SUPPORT FROM STA. (50 E TO STA. 990 LBL 14 HAS SEVERAL DENTS. REMOVED DAMAGED FLOOR SUPPORT FROM AFT. PIT STA. 950 E TO 990, LBL 14 I.A.W. B-727 SRM 51-30-2. DRILLED NEW FLOOR SUPPORT P.O. NR 328319, P/N BAC 1500-6199. 3) DIMENSIONSDR DHL2003749507Floor Support · dentedDURING C-CHECK, AFT PIT FLOOR SUPPORT FROM STA 950E TO STA 990 HAS SEVERAL DENTS IN UPPER FLANGE LBL 10. REMOVED ANGLES SUPPORT AFT PIT STA 950E TO 990 LBL 10 IAW B-727 SRM 51-30-2. COLD WORKING AREA AND RETURNED TO ORIGINAL COUNTOUR. NO CRACK NOTED IAW B-7SDR DHL2003749506Skin · crackedDURING C-CHECK, WS 464 UPPER LT WING L/E SURF IS CRACKED AT RIVET. REMOVED FASTENERS AS REQUIRED IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM 2.375 X 1.25 INCH AND FABBED DOUBLERS FROM 2024 T3 .050 INCH PO 90096 DIM 7.25 X 6 X 7.25 X 4.5 INCH AND FILLER FSDR DHL2003749501Skin · crackedDURING C-CHECK, WS 464 UPPER LT WING L/E SURFACE IS CRACKED AT RIVET (SKIN). REMOVED FASTENERS AS REQUIRED IAW B-727 SRM 51-30-2 AND CUT OUT DAMAGED AREA DIM 2.375 X 1.25 INCHES. FABBED DOUBLERS FROM 2024 T3 .050 PO 90096 DIM 7.25 X 6 INCHES AND 7.25 X 4.5 ISDR DHL2003749503Web · crackedDURING C CHECK, AFT AIRSTAIR TORQUE BOX VERTICAL WEB HAS A CRACK COMING FROM LIGHTNING HOLE AT STA. 1323 LT SIDE. STOP DRILLED CRACK IAW B-727 SRM 51-10-1. 2) NDT STOP DRILLED HOLE IAW B-727 N.D.T. PT-6 51-00-00 FIG. 23, CRACK STOPS AT HOLE. FABRICATED REPASDR GAIA03081OPLight · malfunctionedDURING CRUISE, THE CREW NOTICED THE COCKPIT EMERGENCY EXIT LIGHT CAME ON WITH THE SWITCH IN THE ARMED POSITION. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPS CHECK NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR C8GA20030021Pitot Tube · obstructedFLT 744 FROM TOL TO MEM. CLIMBING THROUGH 15,000 FT, THE ELEVATOR FEEL DIFFERENTIAL PRESSURE LIGHT CAME ON IN FLIGHT. ACCOMPLISHED THE APPROPRIATE CHECKLIST, RETURNED TO TOL AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND THE LEFT HAND ESDR GAIA03033SPStringer · crackedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 360 HAS WEB CRACKED AT STRINGER 16L FASI N/R 35753. FABRICATED REPAIR DOUBLER FROM MATERIAL 7075-T6 .063 PO NR 9911488 DIM 3.5 INCH BY 4 INCH. INSTALLED REPAIR IAW B727 SRM 51-40-2. (M)SDR GAIA03035SPStiffener · crackedDURING C-CHECK, FOUND LEFT WING FRONT SPAR STATION 475 VERTICAL STIFFENER CRACKED TWO FASI N/R 35923. FABRICATED STIFFENERS FROM MATERIAL 7075-T6 STRUT P/N 1505-29063, PO NR 3146124 DIM 10.125 INCH BY 2.25 INCH TWO EACH, INSTALLED IAW B727 SRM 51-30-2. (M)SDR GAIA03032SPFrame · dentedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 360 HAS DENTS INTO THE RADIUS BETWEEN STRINGER 15L AND 17L FASI N/R 35752. CUT OUT DAMAGES AREAS, FABRICATED REPAIR DOUBLER, MATERIAL USED 7075-T6 .063 PO NR 9912571 DIM 18.5 INCH BY 6.5 INCH. TWO ATTACH ANGLES P/N BSDR GAIA03039SPSkin · debondedDURING C-CHECK, FOUND LEFT WING OUTBOARD AFT FLAP T/E DISBONDED AREAS BETWEEN WBW .348 AND WBL 442 FASI N/R 35939. CUT OUT DELAMINATED AREAS, FABRICATED FILLER FROM MATERIAL 2024-T3 .016, PO NR 209415 DIM 6.75 INCH BY 7 INCH. FABRICATED DOUBLER FROM MATERIALSDR GAIA03041SPSkin · dentedMAIN CABIN FRAME BS 580 DENTED BELOW STRINGER 8 RT FASI N/R 36052, FOUND DURING C-CHECK. CUT OUT DAMAGE 1 INCH BY 1.5 INCH, DOUBLER REPAIR 7075 T-6 IAW B-727 SRM 53-10-4 FIG 1. (M)SDR GAIA03040SPWeb · crackedDURING C-CHECK, FOUND LOWER FORWARD CARGO COMPARTMENT BS 620 FRAME WEB DOUBLER HAS PIECES BROKEN OFF FASI N/R 35707. REMOVED BROKEN PART, FABRICATED DOUBLER REPAIR FROM MATERIAL 7075-T6 .063 PO NR 991396 DIM 14 INCH BY 5.25 INCH. INSTALLED IAW B727 SRM 51-30-SDR GAIA03026SPFrame · dentedDURING C-CHECK, MAIN CABIN FRAME BS 720 HAS A DENT INTO THE RADIUS BELOW STRINGER 16R. REMOVED FASTENERS AND CUT OUT DAMAGED AREA OF FRAME, FABRICATED REPAIR DOUBLER IAW B727 SRM 53-10-4 FIG 1, MAT USED .050 7075-T6 P/O NR 9911488 DIM 10 INCH BY 5 INCH. INSTSDR GAIA03027SPFrame · dentedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 600 HAS A DENT INTO THE RADIUS AT STRINGER 16R. CUT OUT DAMAGED AREA OF FRAME. FABRICATED NEW SECTION OF FRAME, MAT USED 7075-T6 .050 P/O NR 991420 DIM 12 INCH BY 5 INCH, AND FILLER MAT USED 7075-T6 .050 P/O NR 9914SDR GAIA03024SPStringer · crackedDURING C-CHECK, FOUND AT MAIN CABIN FORWARD STATION 720B, STRINGER 15L IS CRACKED. CUT OUT CRACK FROM STRINGER 15L, IAW SRM 53-10-3 FIG 5, FABRICATED REPAIR PARTS ONE CHANNEL .040 7075-T6 DIM 4.7 INCH BY 3.2 INCH, TWO FILLRES .100 7075-T6 4.7 BY 8 IAW SRM 53-SDR GAIA03047SPSkin · chafedDURING C-CHECK, FOUND UPPER AND LOWER RUDDERS LEADING EDGES TEFLON ANTI-CHAFE PAINT WORN OUT, BOTH RUDDERS HAVE AREAS OF CHAFING. FOUND 6 AREAS ON LOWER RUDDER OUT OF LIMITS, FABRICATED 6 DOUBELRS, TWO 21.5 AND 14.25, TWO 15.25 BY 23.5, TWO 13.5 BY 15.5 ALL FSDR GAIA03046SPKeelbeam · crackedDURING C-CHECK, FOUND RIGHT WHEEL WELL BS 870 AND KEEL BEAM, VERTICAL STIFFENER CRACKED FASI N/R 35583. REPLACED VERTICLE ANGLE, P/N 65-18636-378 IAW B727 SRM 51-30-2. (M)SDR GAIA03045SPFrame · dentedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 580 HAS A DENT AT STRINGER 16 RT, FASI N/R 36051. CUT OUT DAMAGE 1 INCH BY 1.5 INCH, REPAIR DOUBLER 7075 T-6 INSTALLED IAW B-727 SRM 51-40-3 FIG 1. (M)SDR GAIA03048SPSkin · debondedDURING C-CHECK, FOUND RT WING LOWER TRAILING EDGE PANEL 8605 HAS DISBONDED SPOT OUTER SKIN. CUT OUT 3 INCHES BY 48 INCHES, FABRICATED FILLER 3 INCHES BY 48 INCHES, LOWER DOUBLER 3 INCHES BY 48 INCHES 2024 T-3 .016 UPPER DOUBLER 4.5 BY 50 INCHES 2024 T-3 .020,SDR GAIA03023SPStringer · crackedDURING C-CHECK, FOUND FASI NR 35734, AT MAIN CABIN FRAME 720B, STRINGER 15R IS CRACKED FORWARD OF THE WING LIGHT. CUT OUT CRACK FROM STRINGER 15R IAW SRM 53-10-3 FIG 5, FABRICATED REPAIR PARTS ONE CHANNEL .040 7075-T6 DIM 4.7 INCH BY 3.2 INCH, TWO FILLERS .10SDR GAIA03022SPSkin · corrodedDURING C-CHECK, FOUND FUSELAGE RIGHT SIDE STATION 675 STRINGER R19 HAS PILLOWING AT FASTENERS. CUT OUT DAMAGED SKIN 3 INCHES BY 2.75 INCHES, ACCOMPLISHED DOUBLER REPAIR IAW B727 SRM 53-30-3 FIG 14. DOUBLER 2024 T-3, .071, FILLER 2024 T-3 .063. (M)SDR GAIA03043SPBeam · crackedDURING C-CHECK, FOUND VERTICAL BEAM BULKHEAD 1183 RBL 36.5 WL 249 INBOARD CHORD HAS A CRACK. REMOVED FASTENERS FOR ACCESS IAW 727 SRM 51-30-2. STOP DRILLED CRACK IAW B727 SRM 51-10-1. ACCOMPLISHED 727 HFEC INSPECTION. INSTALLED VERTICAL BEAM REPAIR IAW S/BSDR DHL2003749006Switch · malfunctionedON PRE-DEPARTURE CHECK LOWER AFT BODY OVERHEAT WOULD NOT TEST. TRANSFERRED TO DMI CONTROL 13029 PER MEL 26-10-2. PLACARD INSTALLED. SPECIAL PROCEDURES 26-10-2 COMPLIED WITH TO VERIFY SYSTEM OPERATION. REF DMI 13029 ON PRE-DEPARTURE CHECK LOWER AFT BODY OVERSDR COOSDR030023Skin · delaminatedLT WING, SPOILER NR 2, PN 65-17347-48, SN TIC-1693, WITH DELAMINATION.SDR COOSDR030021Skin · delaminatedLEFT WING, GROUND SPOILER NR 5, PN 65-17348-71, SN 139, WITH DELAMINATION.SDR COOSDR030020Skin · delaminatedLEFT WING, GROUND SPOILER NR 7, PN 65-17348-66, SN 196, WITH DELAMINATION.SDR COOSDR030019Skin · delaminatedRT WING, FLIGHT SPOILER NR 9, PN 65-17348-66, SN 22, WITH DELAMINATION.SDR COOSDR030017Skin · delaminatedLEFT WING, FLIGHT SPOILER NR 4, PN 65-17347-54, SN BN378 WITH DELAMINATION.SDR GAIA03001OPValve · malfunctionedFLT 884 - ONT-FWA - DURING CLIMB CREW DISCOVERED A PROBLEM WITH THE FUEL PANEL. THE NR 2 CROSSFEED VALVE WAS NOT OPEN. CREW DECLARED AN EMERGENCY AND DIVERTED TO PHX. DEFERRED NR 2 CROSSFEED VALVE PER MEL 28-7. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA02051STStringer · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STRINGER 15 LEFT IS CRACKED AT BS 720B PLUS 5. ACCOMPLISHED STRINGER REPAIR AT BS 720B PLUS 5 STRINGER 15 LEFT IAW B727 SRM 53-10-3 FIG 5. (M)SDR GAIA02052STStringer · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STRINGER 15 LEFT IS CRACKED AT BS 720B PLUS 15. ACCOMPLISHED STRINGER REPAIR AT BS 720B PLUS 15 STRINGER 15 LEFT IAW B727 SRM 53-10-3 FIG 5. (M)SDR GAIA02053STSeat Track · damagedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE MAIN CABIN SEAT TRACK RBL 24.75 IS DAMAGED SEVERAL DIFFERENT PLACES FROM BS 480-530. ACCOMPLISHED SEAT TRACK REPAIR AT BS 480-530 RBL 24.75 IAW B727 SRM 53-10-5 FIG 1. (M)SDR GAIA02054STStiffener · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE PRESSURE BULKHEAD BS 1183 VERTICAL BEAM LBL 36.9 CRACKED AT WL 245. ACCOMPLISHED BS 1183 VERTICAL BEAM REPAIR AT LBL 36.9 IAW S/B 727-53-0192. (M)SDR GAIA02055STSkin · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE SKIN IS CRACKED AT THE FORWARD ENTRY DOOR LOWER HINGE CUT OUT. ACCOMPLISHED FUSELAGE SKIN REPAIR AT THE FORWARD ENTRY DOOR LOWER HINGE CUT OUT IAW S/B 727-53-0198. (M)SDR GAIA02056STWeb · corrodedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STATION 1230 AFT FACE OF THE TAIL SKIN CAVITY BULKHEAD, CORROSION ON SUPPORT ANGLE AND WEB VISIBLE THROUGH AIRSTAIR CUT-OUT, AFT OF THE TAIL SKID. ACCOMPLISHED BS 1230 WEB AND T-ANGLE REPAIR IAW B727 SRM 51-
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