Boeing 727-264
Service difficulty reports · 617
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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 = '727264' 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 = '727264' 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 K11A2012102529002Seat Track · corrodedMAIN DECK STA 380 TO STA 460 RBL 46 SEAT TRACK HAS CORROSION (NR 49057).SDR K11A2012100829001Seat Track · corrodedCORROSION ON SEAT TRACK AROUND NUT PLATE, 1X1 INCH (NR 49051).SDR DHLA200900034Battery Pack · malfunctionedDEFECT DESCRIPTION; ENTRY WAY EMERGENCY EXIT LIGHT FLICKERS AND IS DIM WHEN STDY BATTERY CHECK IS DONE. REMOVED AND REPLACED ENTRY EMERGENCY EXIT LIGHT BATTERIES IAW B727 M/M 33-50-01. OPS CK NORMAL, P/N-55-2713-1 2EA.SDR DHLA200800118Circuit Breaker · trippedDURING THE CLIMB-OUT OF KILN, EMERGENCY EXIT CONTROL RT C/B POPPED. COCKPIT EMERGENCY EXIT LIGHTS OPERATE NORMAL.SDR DHLA2000800117Cable Assy · noisyFLIGHT 935 - DURING CLIMBOUT HEARD LOUD NOISE SEEMING TO COME FROM NOSE GEAR AREA, MINUTES LATER RED DOORS LIGHT ON FWD PANEL & NOSE GEAR DOOR LIGHT ILLUM ON S/O PANEL. FELT VIBRATION. COMPLETED ABNORMAL PROCEDURE & RETURNED TO ILN. REPLACED BOTH NOSE GEAR SDR DHLA20087651016Casting · crackedUPON VISUAL INSPECTION FOUND THE NR 6 K-FLAP CENTER HINGE CASTING OUTBOARD SIDE AT THE ATTACH POINT FOR THE ACTUATOR ROD END CRACKED APPROX 2 INCHES IN LENGTH. K-FLAP IS TO BE CHANGED. REMOVED PART NUMBER IS 65-16227-18 SERIAL NUMBER BN1869. UNKNOWN IS THE SDR DHLA200800114Accessory Unit · failedON CLIMBOUT AT 300KIAS PASSING FL200 RED DOORS LIGHT ON FWD PANEL & NOSE GEAR DOOR LIGHT ON S/O'S PANEL ILLUMINATED. FELT HEAVY VIBRATION PERFORMED ABNORMAL PROCEDURE AFTER SLOWING TO 260KTS LIGHT WENT OUT /VIBRATION REMAINED. MX INSTRUCTED, CYCLE GEAR UPON SDR DHL2008F00000Pin · damagedSMALL DAMAGE ON NR (6) L/E SLAT AT IB GUIDE PIN EXISTING DOUBLER. DAMAGE WAS BLENDED SMOOTH LESS THAN 1 INCH X .100 MATERIAL LOSS, WORK ACCOMPLISHED IAW SRM 57-50-01. (K)SDR DHL2008764532Spar · crackedWHILE AT C CHECK, RT WING REAR SPAR J BEAM CRACKED WBL 126. FABRICATED AND REMOVED AND REPLACED IAW BOEING DWG 65-21655 AND ASTAR EC-00911-001.SDR DHL2008764531Spar · crackedWHILE AT C CHECK, LT WING REAR SPAR J BEAM CRACKED INDICATION WBL126. FABRICATED AND REMOVED AND REPLACED IAW BOEING DWG 65-21655 AND ASTAR EC-00910-001 MATERIAL BAC 1506-860 7075T6 DIM 81 INCH BY 5 1/2 INCH PO NR 815922.SDR DHL2008764533Attach Angle · crackedWHILE AT C CHECK, LT O/B MID FLAP I/B LOWER END CAP AND ATTACHMENT ANGLE CRACKED. REPAIRED IAW B727 SRM 51-40-2, 51-20-1, 51-30-5 AND 57-50-2 FIG 6. REPAIR ANGLE MAT.7075 T6 .071" PO NR 9006522 DIM 4 INCH BY 4 INCH AND 3 INCH BY 2 INCH.SDR DHL2008764530Rib · crackedWHILE AT C CHECK, NR 5 K-FLAP ACTUATOR SIDE MOUNTING RIBS I/B AND O/B CRACKED. REPAIRED RIBS IAW BOEING DWG 65-16269 REVC MATERIAL 2024T3 .063" DIM 7" BY 6 1/8 INCH PO NR 9006773.SDR DHL2008764529Skin · bentWHILE AT C CHECK, L1 DOOR INNER SKIN BENT FWD LOWER CORNER. REPAIRED IAW B727 SRM 51-40-2 AND ASTAR EVA B52-00073 REV1.SDR DHL2008764528Keelbeam · crackedWHILE AT C-CHECK, CRACK AT BS 874 RIGHT KEEL BEAM LWR CHORD IN APU BAY. REPAIRED IAW S/B 727 53-02-08 MATERIAL 4130 STEEL .071" PO 610176.SDR DHL2008764527Frame · dentedWHILE AT C-CHECK, DENT AT MAIN FRAME BS 580 BETWEEN STR 16 AND 17R. REPAIRED IAW SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3, 7075T6 .050 DIM 7.125" X 6.25" PO 9006742.SDR DHL2008764526Stringer · corrodedWHILE AT C-CHECK, PILLOWING AT FASTENERS AT RIGHT LWR FUSELAGE AT BS 350, 4 INCHES FWD OF NOSE JACK PAD. REPAIRED IAW SRM 53-10-3 FIG 1 DETAIL 2. MATERIAL USED P/N 95-24786-10 GUSSET / CHANNEL, REPAIR FOR 21R BAC 1496-138 DIM 11" PO 815987, CHANNEL SPLICE FRSDR DHL2008764524Skin · delaminatedWHILE AT C-CHECK, LT WING O/B AILERON TAB LWR I/B SURFACE DELAM WBL 492. CUT OUT DELAMINATED AREA 1 INCH DIA AND APPLIED POTTING COMPOUND. FABRICATED DOUBLER 3 INCH DIA FROM.010" 2024-T3 PO 9003621. BONDED DOUBLER, CLEANED PRIMED AND SEALED IAW B727 SRM 51-SDR DHL2008764523Hinge · crackedWHILE AT C-CHECK, EXTERNAL FUSELAGE BS 650 MCD AFT HINGE SEGMENT HAS AFT 2 LOBES WITH SMALL CRACKS. REMOVED AND REPLACED MCD STA 650 AFT HINGE SEGMENT IAW AEI B727 M/M CH 52 PGS 17-20 P/N MS20001-16-7200 PO 9006913.SDR DHL2008764535Bulkhead · crackedCRACK INDICATION AT BS 870 IN RT W/WELL AT APU LOAD CONTROL VALVE CUT-OUT. TRIMMED OUT CRACKED MATERIAL, FABRICATED REPAIR PARTS, AND INSTALLED REPAIR AT BS 870 BULKHEAD PER B727 SRM 53-10-9 FIG 5, 51-10-6, 51-10-1, AND NDTM PT6, 51-00-00 FIG 23.SDR DHL2008764522Mount Bracket · crackedNR 1 K-FLAP ACTUATOR TRUNNION MOUNTING BRACKETS CRACK INDICATION WS 305. REMOVED NR 1 K-FLAP MOUNTING BRACKETS WS 305 IAW B727 SRM 51-30-2. FAB NEW BRACKETS WITH 2024-T3 .063", DIM 7.5" X 4" AND PO 9006027 IAW BOEING ENGINEERING DWG 65-16275.SDR DHL2008764521Frame · dentedDENTS ON MAIN CABIN FRAME BS 640 BETWEEN STR 16 AND 17R. CUT OUT DAMAGED AREA AT FRAME BS 640 BETWEEN STR 16 & 17 RT APPROX 7/8" X 1", FAB DOUBLER REPAIR WITH 7075-T6 .050", DIM 7" X 5" AND PO 9006742 IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1.SDR DHL2008764520Bracket · crackedNR 2 K-FLAP ACTUATOR, TRUNNION MOUNTING BRACKETS CRACK INDICATION (WS 235 APPROX). REMOVED NR 2 K-FLAP TRUNNION MOUNTING BRACKETS FROM ACTUATOR WS 235 IAW B727 SRM 51-30-2. FAB NEW BRACKETS WITH 2024-T3 .063" DIM 9" X 6.5 AND PO 9006773 IAW BOEING ENGINEERINSDR DHL2008764519Skin · damagedSKIN DAMAGE ON LT WING T/E AT NR 2 SPOILER NR 3 HINGE CUTOUT. ROUTER OUT SKIN AT LT WING T/E NR 2 SPOILER NR 3 HINGE CUTOUT FOUND OUT OF LIMITS IAW B727 SRM 51-10-1 AND 57-20-1 FIG 2. FAB DOUBLER REPAIR WITH 7075-T6. DIMENSION: 4" X 7" AND PO 9006522 IAW B72SDR DHL2008764518Flap · crackedLEFT INBOARD FORE FLAP CRACK INDICATIONS AT L/E FWD OF SEQUENCE CAR ATTACH POINTS (FITTING) WBL 124/203. STOP DRILLED AT THE END OF CRACKS AT LEFT INBOARD FORE FLAP L/E WBL 124/203 IAW B727 SRM 51-10-1. FAB DOUBLER REPAIR WITH 2024-T3 .050" AND PO 9006457 I/SDR DHL2008764534Tab · bentLT ELEV TAB INBD CORNER DAMAGED, REMOVED DAMAGED AREA, FABRICATED REPAIR, AND INSTALLED BY BONDING IAW B727 SRM 51-40-20 PGS 12 THROUGH 62 AND SRM 51-80 FIG 2. NO FURTHER ACTION REQUIRED.SDR DHL2008764517Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK BS 1110-1130 LBL 24. REMOVED SEAT TRACK FROM MAIN CABIN BS 1110-1137 LBL 24 FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3 AND SRM 51-30-2. FAB NEW SEAT TRACK WITH BAC1520-792-7178-T6 DIM, 2'3" AND PO 9003797 IAW B727 SRM 5SDR DHL2008764516Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK BS 1110-1130 LBL 45. REMOVED CORRODED SEAT TRACK FROM BS1110 TO 1137 LBL 45 FOUND OUT OF LIMITS IAW B727 SRM 51-30-2 ZND 53-10-1 FIG 3. FAB NEW SECTION WITH BAC 1520-792-7178-T6 DIM. 2'3" AND P.O. 6295113 IAW B727 SRM 53-1SDR DHL2008764515Rib · crackedNR 6 K-FLAP ACTUATOR SUPPORT SIDE I/B AND O/B RIBS CRACKED WS 304. REMOVED INBOARD AND OUTBOARD RIBS AND FAB NEW RIBS WITH 2024-T3-.063 INCH DIM 7 1/2 INCH BY 4 INCH AND PO 9006773 IAW BOEING ENGINEER DWG NR 65-16275.SDR DHL2008764514Flap · crackedL/WING I/B MIDFLAP T/E CHORD CRACKED AT I/B CABLE DRUM, 2 PLACES. REMOVED DAMAGED AREA AT T/E CHORD ABOUT 51 INCHES. FABRICATED NEW SECTION WITH P/N 604754 7075-T6 DIM 51 INCH AND PO 815986 IAW B727 SRM 57-50-2 FIG 5 AND 51-40-1 FIG 1.SDR DHL2008765513Seat Track · corrodedCORRODED SEAT TRACK RBL 45 BS 1110-1135. SEAT TRACK AT RBL 45 BS 950 TO 1183 CORRODED OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. FAB NEW SECTION OF SEAT TRACK WITH BAC 1520-792-7178-T6 DIM 15'7 INCH AND PO 9006864 AND TWO ANGLES FOR SPLICES WITH BAC 1503-1001SDR DHL2008764512Seat Track · corrodedCORRODED SEAT TRACK RBL 24 BS 1110-1135. SEAT TRACK CORRODED FROM RBL 24 FROM BS 1070 TO 1136 IAW B727 SRM 51-30-2 AND 53-10-1 FIG 3. FAB NEW SECTION WITH BAC 1520-792-7178-T6 DIM 5'6" AND PO 9006020 IAW B727 SRM 53-10-5 FIG 1.SDR DHL2008764511Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK BS 480-600 LBL 45. SEAT TRACK CORRODED OUT OF LIMITS STA 480-590 IAW B727 SRM 51-20-2 FIG 21 AND 53-10-1 FIG 3. FAB NEW SECTION OF SEAT TRACK WITH BAC 1520-792-7178-T6511 DIM 9'2 INCH PO 9006020 IAW B727 SRM 53-10-2 FIG 1 ASDR DHL2008764510Shear Web · dentedDENT AND PUNCTURE HOLE ON MAIN CABIN SHEAR WEB BS 1140 RBL 24. CUT OUT DAMAGED AREA AT SHEAR WEB RBL 24 BS 1140 (2 EACH ) 3/4 INCH BY 3/4 INCH AND 1 INCH BY 1 INCH IAW B727 SRM 51-40-2 FIG 1. FAB DOUBLER REPAIR WITH 7075-T6 .071 INCH SIZE: 9 INCH BY 7 INCH ASDR DHL2008764509Floorbeam · corrodedCORROSION ON BS 1110 FLOORBEAM LBL 24 - LBL 45. CORROSION ON FLOORBEAM LBL 24-LBL 45 BS 111O FOUND OUT OF LIMITS AT LBL 33 IAW B727 SRM 51-10-6 AND 53-10-1 FIG 5. CUT OUT DAMAGED AREA, FAB ONE FILLER WITH 7075-T6 .125 INCH DIM 2 INCH BY 1 INCH PO 7371263. TSDR DHL2008764507Frame · gougedWHILE AT C CHECK REF N/R 097896, 4 EACH TOOLING MARKS/GOUGES ON MAIN CABIN FRAME BS 700 BETWEEN S7-8L. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MATERIAL 7075-O PO NR 9006027 HEAT TREATED FROM 7075-O TO 7075-T6 IAW FAS ENGINEERING REPORT NR 2-3715SDR DHL2008764506Frame · dentedWHILE AT C CHECK REF N/R 098177, DENT ON MAIN CABIN FRAME BS 600 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MATERIAL 7075-T6 .050 INCH DIMENSION 7 INCH BY 5 1/4 INCH PO NR 9006153.SDR DHL2008764505Frame · dentedWHILE AT C CHECK REF N/R 098175, DENT ON MAIN CABIN FRAME BS 540 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MATERIAL 7075-T6 .050 INCH DIM 7 1/8 INCH BY 6 INCH PO NR 9006742.SDR DHL2008764508Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK BS 480-620 RBL 45. SEAT TRACK CORRODED OUT OF LIMITS IAW B727 SRM 51-20-2 FIG 21 AND 53-10-1 FIG 3. FAB NEW SECTION WITH BAC 1520-792-7178T6 DIM 12'6 3/8 INCH AND PO 9006020 IAW B727 SRM 53-10-5 FIG 1 AND VENTURA AEROSPACE SDR DHL2008764504Frame · dentedWHILE AT C CHECK REF N/R 098180, DENT AT MAIN CABIN FRAME BS 680 BETWEEN STR 16 AND 17R. FABRICATED REPAIR IAW B727 SRM 51-40-3 FIG1 AND 53-10-2 FIG3 MATERIAL 7075-T6 .050 INCH DIM 7 1/8 INCH BY 5 1/4 INCH PO NR 9006742.SDR DHL2008764503Frame · dentedWHILE AT C CHECK REF N/R098179, DENT AT MAIN CABIN FRAME BS 660 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 DOUBLER MATERIAL 7075-T6 .050 DIM 7 1/8 INCH BY 5 1/4 INCH PO NR 9006742.SDR DHL2008764502Frame · dentedWHILE AT C CHECK REF N/R 098174, DENT AT MAIN CABIN FRAME AT BS 520 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MAT, 7075-T6 .050" DIM 5 1/8 INCH BY 8 1/4 INCH PO NR 9006742.SDR DHL2008764501Frame · dentedWHILE AT C CHECK REF N/R 098173, DENT AT RT MAIN CABIN FRAME BS 480 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG1 AND 53-10-2 FIG3 MATERIAL DOUBLER 7075-T6 .050 INCH DIM 7 1/4 INCH BY 5 3/4 INCH PO NR 9006742.SDR DHL2008764500Skin · crackedWHILE AT C CHECK REF N/R 097599, RT I/B AFT FLAP LOWER SKIN WBL 203 CRACKED AT MOUNTING FITTING. REPAIRED IAW B727 SRM 57-50-4 FIG 11, SPLICE 2024T3 .050 DIM 5.5 INCH BY 11 INCH PO NR 9006742. FABBED FILLER 2024T3 .040 DIM 9 INCH BY 14 INCH PO NR 9006587.SDR DHL2008763530Floorbeam · corrodedEXFOLIATION FOUND ON FLT DECK FLOORBEAM UPPER CAP AT BS 266, BL 0. REMOVED AND REPLACED UPPER CHORD SECTION WITH P/N 65-17588-2, PO NR 8109233, PER B727 SRM 51-30-5, 51-30-2, AND BAC DWG 65-17588 REV D.SDR DHL2008763529Rib · crackedNR 5 L/E SLAT INB TRACK INTERIOR, O/B RIB IS CRACKED. REMOVED AND REPLACED RIB ASSY (I/B AND O/B) WITH P/N 65-17281-13, PO3 8109195, PER B727 SRM 51-30-2.SDR DHL2008763523Frame · dentedFRAME DAMAGED IN CARGO COMPT AT BS 347, ALONG STR 4L. CUT OUT DAMAGE, INSTALLED FRAME REPAIR PARTS, P/N AE727-2-360-11 AND AE727-2-360-12, PO NR 810972, PER B727 SRM 51-30-5, 51-30-2, AND AEI DWG AE727-2-360 REV G.SDR DHL2008763511Hinge · crackedMCD AFT HINGE SEGMENT AFT LOBE CRACKED. REMOVED AND REPLACED HINGE SEGMENT WITH MS 20001-16-7200 MATERIAL PO NR 9002527 PER AEI B727-200 FREIGHTER MM CH 52 FIG 5201A AND SRM 51-30-5.SDR DHL2008763509Skin · chafedRT I/B FORE FLAP I/B L/E CHAFED AT RWBL 73. DAMAGE BEYOND SERVICE LIMITS. REMOVED, FABRICATED, AND INSTALLED SKIN PANEL, 2024-T3 .050 INCH BY 14 INCH BY 14.5 INCH, PONR 9006586, PER B727 SRM 57-50-2 FIG 3, 51-20-1, AND 51-30-2.SDR DHL2008763528Support Fitting · crackedNR 6 K-FLAP ACTUATOR MOUNT SPT FITTING CRACKED AT WS 307.5. REMOVED ACTUATOR SUPPORT MOUNT ASSY. FABRICATED SUPPORT WEBS FROM 2024-T3, .063" BY 8" BY 3.5" (2 EA), PO NR 9006027, AND MOUNT DOUBLERS FROM 7075-T6, .125" BY 5" BY 2", (2 EA), PO NR 9005685, ASSEMSDR DHL2008763527Support Fitting · crackedNR 1 K-FLAP ACTUATOR MOUNT SPT FITTING CRACKED AT WS 307.5 AND 315.3. REMOVED ACTUATOR SUPPORT MOUNT ASSY, FABRICATED SUPPORT WEBS FROM 2024-T3, .063" BY 8" BY 3.5" (2 EA), PO NR 9006027, AND MOUNT DOUBLERS FROM 7075-T6, .125" BY 5" BY 2", (2 EA), PO NR 90056
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