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 C8GA20050010Motor · leakingFLT 712 FROM TOL TO DEN. 10 MINUTES AFTER TAKE OFF AT FL190, CREW NOTICED LOSS OF SYSTEM A-HYDRAULIC FLUID FOLLOWED BY ILLUMINATION OF HYDRAULIC LOW PRESSURE LIGHTS. CREW DUMPED 600 LBS OF FUEL, RETURNED TO TOL, AND LANDED WITHOUT INCIDENT. FOUND RT OUTBOARDSDR 05FDEA01020Attach Fitting · corrodedCORROSION VERTICAL STAB TENSION TIE LT FWD FITTING IS CORRODED. REPAIRED PER EA 7-5530-86277.SDR 05FDEA01018Pump · malfunctionedTOTALLY LOST SYS A HYDRAULIC FLUID WHEN RAISING GEAR HANDLE ON DEPARTURE. SYSTEM A HYDRAULIC PUMPS RAN W/O FLUID. FLUID SHUTOFF SWITCHES OFF FOR APPROX 40 MIN HYDRAULIC LINE REPAIR AT RIGHT WHEEL WELL FAILED. MPN 65-17840-487 REPLACED NR 1 ENGINE HYDRAULISDR DHL2005741546Rib · chafedNR 1 SLAT ACTUATOR ROD END BOLT CHAFING AGAINST I/B SLAT RIB. REMOVED DAMAGED I/B RIB IAW B727 SRM 51-30-2. DRILLED, TREATED, PRIMED RIB AND AREA IAW B727 SRM 51-30-2 AND 51-10-2. INSTALLED I/B RIB IAW B727 SRM 51-30-2 PO 5096329 P/N 65-17327-3.SDR XNOA1231Selector Switch · burned outAFTER STARTING NR 3 ENGINE, AC FREQUENCY METER PEGGED OUT AND SMOKE POURED OUT OF FREQ (AC) SELECTOR SWITCH. REMOVED AND REPLACED AC FREQ METER SELECTOR SWITCH AND OPS CHECK OKAY IAW B727 MM 24-20-00.SDR DHL2005783512Rib · crackedNR 5 SLAT INTERIOR AT ACTUATOR ATTACHMENT INB RIB CRACK NOTED WS 410. REMOVED NR 5 LE SLAT ACTUATOR ASSY IAW 727 MM 27-81-32 AND 27-81-11. REMOVED CRACKED U-CHANNEL IAW 727 SRM 51-30-2 AND FABBED NEW FROM 2024T3 .071 PONR 9002193 DIM.15 INCH BY 3 1/8 INCH IASDR DHL2005782572Attach Fitting · crackedNR 5 SLAT ACTUATOR ATTACH POINT IS CRACKED INSIDE SLAT. DISCONNECTED NR 5 SLAT ACTUATOR FOR ACCESS IAW 727 MM 27-81-22. OPENED SLAT INNER SKIN IAW 727 SRM 51-30-2. REMOVED DAMAGED PART AND FABBED FROM 2024T3 .071 PO 9001978 DIM 12 X 4.5 INCH IAW 727 SRM 57-SDR 05FDEA00987Beam · corrodedCORROSION ON LT MLG BEAM LOWER SURFACE. REPAIRED PER EA 7-5710-86267.SDR DHL2005783509Skin · dentedC1 DOOR SKIN DENTED LOWER AFT CORNER. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 52-00-2 AND 53-30-1 FIG 1. CUT OUT DAMAGED AREA 5 INCH BY 3 1/8 INCH AND FABBED DOUBLER FROM 2024T3 PO NR 9001634 DIM. 10 1/4 INCH BY 8 1/2 INCH IAW SRM 52-00-3 FIG 3 AND 52-30-1 SDR DHL2005783508Skin · dentedC1 DOOR SKIN LOWER FORWARD CORNER DENTED. REMOVED AND REPLACED C1 DOOR LOWER FORWARD CORNER IAW 727 SRM 51-30-2, P/N 65-57146-4 PO NR 507979.SDR 05FDEA00870Fitting · damagedWING FITTING REQUIRED RESLEEVING DUE TO BLENDED DAMAGE OUT OF LIMITS. SO, THE BODY FITTING ALSO NEED TO BE RESLEEVED. REPAIRED LT 740 WING TERMINAL FITTING PER FED EX EA 7-5710-86260.SDR 05FDEA00869Fitting · damagedBLENDED DAMAGE IN WING TERMINAL FITTING OUT OF LIMITS. REPAIRED LEFT WING BODY FITTING PER FED EX EA 7-5340-86266.SDR DHL2005783503Clip · crackedRIGHT ELEV T/E UPPER & LWR ADJOINING CLIPS CRACKED AT ELEV STA 60 MARKED. REMOVED CLIP IAW B727 SRM 51-30-2, FAB'D CLIPS USING 2024T3 .032 PO 9002034 DIM 3 X .75 INCH IAW B727 SRM 55-20-2 FIG 1. ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2. REINSTALLED RISDR DHL2005783502Clip · crackedRT ELEV T/E UPPER AND LWR ADJOINING CLIPS CRACKED AT ELEV STA 106. REMOVED CLIP IAW B727 SRM 51-30-2. FABRICATED CLIPS USING 2024T3 .032 PO NR 2034 DIM 3 INCH BY 3/4 INCH IAW B727 SRM 55-220-2 FIG 1. ALODINE AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLEDSDR DHL2005783504Skin · dentedDENT ON RT UPPER RUDDER FS 1540 MARKED. CUT OUT DAMAGE AREA 0.750 INCH DIA IAW B727 SRM 55-20-3 FIG 1. FAB'D DOUBLER REPAIR FROM MAT 2024-T3 .032 PO NR 9002034 DIM 5 INCH BY 3 1/4 INCH IAW B727 SRM 55-20-3 FIG 1. ALODINED AND PRIMED DOUBLER REPAIR IAW B727 SDR DHL2005783501Skin · dentedLWR LT RUDDER DENTED MARKED. CUT OUT DAMAGE AREA 3/4 INCH DIA IAW B727 SRM 55-20-3 FIG 1. FAB'D DOUBLER REPAIR FROM MAT 2024-T3 .032 PO NR 9022034 DIM 5 INCH BY 3 INCH IAW B727 SRM 55-20-3 FIG 1. ALODINE AND PRIMED DOUBLER REPAIR IAW B727 SRM 51-10-2 AND INSDR DHL2005783500Clip · crackedRT ELEVATOR T/E UPPER AND LWR ADJOINING CLIPS CRACKED AT ELEV STA 116. REMOVED CLIP IAW B727 SRM 51-30-2. FABRICATED CLIPS USING 2024T3 032 PO NR 9002034 DIM 3 INCH BY 3/4 INCH IAW B727 SRM 55-20-2 FIG 1. ALODINE AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTSDR DHL2005783521Skin · gougedRT WING INBD FOREFLAP LE IS GOUGED AT OB END WBL 240. REMOVED EXISTING DOUBLER REPAIR IAW B727 SRM 51-30-2 FABRICATED DOUBLER USING 2024T3 .063 PO NR 9002149 DIM. 4 1/2" BY 4 1/2" IAW B727 SRM 57-50-2 AND 57-50-4 FIG 1. ALODINE AND PRIMED DOUBLER AND AREA IASDR DHL2005783520Skin · dentedRT WING AILERON UPPER SKIN IS DENTED, WING STA 436. CUT OUT DAMAGED AREA DIM 3 BY 1 1/4 IAW B727 SRM 57-50-5 FIG 2. FABRICATED DOUBLER FROM 2024T3 .032 PO NR 9002034 DIM. 5 1/8" BY 6 1/4" IAW B727 SRM 57-50-5 FIG 2. TREATED AND PRIMED IAW B727 SRM 51-10-2. SDR DHL2005783519Skin · dentedRT WING INBD AILERON UPPER SKIN IS DENTED, WING STA 436. CUT OUT DAMAGED AREA DIM 3" BY 1 1/4" IAW B727 SRM 57-50-5 FIG 2. FABRICATED DOUBLER FROM 2024T3 .032 PO NR 9002034 DIM. 5 1/8" BY 6 1/4" IAW B727 SRM 57-50-5 FIG 2. TREATED AND PRIMED IAW B727 SRM 51SDR DHL2005783518Skin · damagedBS 362 BELOW STR 17L FUSELAGE SKIN IS DENTED. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. REMOVED PREVIOUS REPAIR AT LOCATION FOR INCORPORATION IAW SRM 51-30-2. PREVIOUS CUT OUT DIM 2" BY 1 7/16", CUT OUT DAMAGE AREA DIM 4.500 BY 2.500 INCHESDR DHL2005783517Skin · delaminatedRT WING I/B FOREFLAP PREVIOUS REPAIR IS DISBONDED ON LOWER SURFACE WBL 220. REMOVED RT I/B TE FOREFLAP FOR REPAIR IAW B727 MM. REMOVED PREVIOUS REPAIR AND CUTOUT DAMAGE AREA APPROX 4 INCH DIAMETER IAW SRM. FABRICATED ONE FILLER APPROX 4 INCH ROUND AND ONE DSDR DHL2005783513Frame · crackedNR 2 ENGINE STRUT RT COWLING FRAME CRACKED AT 3RD CUTOUT (ENGINE SUPPORT STRUCTURE). ROUTED OUT DAMAGED AREA AND FABBED REPAIR ANGLE FROM 301 1/2HD .050 PO NR 90001233 DIM 7 3/4" BY 3 1/2" IAW 727 SRM 54-10-2 FIG 8 AND 51-40-3 FIG 1. REPAIR ANGLE TREATED, PRSDR DHL2005783507Skin · bulgedBS 675 STR 28R, FUSELAGE SKIN HAS BULGED SKIN WITH POPPED FASTENERS. CUT OUT CORRODED STRINGER SECTION (DIM. 5") FROM 28R STA 675 TO 680. CUT OFF CORRODED SHEAR TIE (DIM. 6") AT STA 680 BETWEEN S28R AND S27R IAW B727 SRM 53-10-3 FIG 1 AND 53-10-4 FIG 15. FASDR DHL2005783516Support Angle · crackedNR 6 SLAT ACTUATOR INBD SUPPORT ANGLE IS CRACKED AT BOTTOM, WING STA 519. REMOVED NR 6 SLAT ACT IAW 727 MM 27-81-32. REMOVED DAMAGED I/B SUPPORT IAW 727 SRM 51-30-2. FABBED NEW SUPPORT ANGLE FROM PN AND 10133-1401 PO NR 501952 DIM.10" BY 3 1/4" IAW 727 SRM SDR DHL2005783515Support · crackedNR 5 LE FLAP ACTUATOR SUPPORT IS CRACKED AT IB UPPER CORNER WING STA 224.5. REMOVED NR 5 LE FLAP ACT IAW B727 MM 27-81-22. UPON FURTHER EVAL, FOUND O/B SUPPORT CRACKED. REMOVED BOTH I/B AND O/B SUPPORTS IAW B727 SRM 51-30-2, FABRICATED SUPPORTS O/B AND I/B SDR DHL2005783506Skin · damagedLT OB AFT FLAP LOWER SURFACE, WBL 432 HAS A LARGE SMOOTH DENT. CUT OUT DAMAGED AREA APPROX 3 INCH DIAM L/W O/B FLAP LOWER SKIN IAW B727 SRM 51-40-20 FIG 31. FABRICATED ONE FILLER APPROX 3 INCH ROUND AND ONE DOUBLER APPROX 6 INCH ROUND USING 2024T3 .016 PO NRSDR DHL2005783505Support · crackedNR 6 LEADING EDGE FLAP ACTUATOR SUPPORT IS CRACKED AT INBD LWR CORNER WING STA 304. REMOVED NR 6 L/E FLAP ACT I/B SUPPORT IAW 727 SRM 51-30-2. FABBED NEW FROM 7075 T6 .063 PO NR 9001660 DIM 7 1/2 INCH BY 3 !/2 INCH IAW 727 SRM 57-10-25 FIG 3. SUPPORT TREATESDR DHL2005782566Web · crackedAFT AIRSTAIR AREA, FUSELAGE STA 12 30 WEB IS CRACKED. CUT OUT DAMAGE AREA AT AFT AIRSTAIR STA 1230 DIM 5" BY 3 1/4" IAW B727 SRM 51-40-2 FIG 1. FABRICATED DOUBLER REPAIR-MAT-USED 7075-T6 .040 PO NR 9001777 DIM 8" BY 6 1/4" IAW B727 SRM 53-10-2 FIG 6 AND 51-4SDR 05FDEA00734Intake · corrodedAPU AIR INTAKE HOUSING HAS CORROSION ON MOUNTING FLANGE ALONG LOWER SIDE.SDR DHL2005782571Fitting · corrodedSTRINGER 19 RT ATTACH FITTING CORRODED AT BS 1183. REMOVED & REPLACED FITTING AT STR 19 BS 1183 IAW B727 SRM 51-30-2.SDR DHL2005782565Web · crackedRT WING TIP WEB CRACKED AT THE UPPER AND LWR FLANGES. ON RT WING TIP REMOVED CRACKED WEB IAW B727 SRM 51-30-2. FAB NEW WEB FROM 7075T6 .040 PO NR 9001068 14" BY 9" IAW B727 SRM 57-20-2 FIG 3. TREATED AND PRIMED IAW B727 SRM 51-10-2 INST IAW B727 SRM 51-30-2SDR DHL2005782564Skin · damagedINSTALL B727 GPS ANTENNA DOUBLER AT BS 360-380 BETWEEN STR 1 AND 2R PER DECRANE AIRCRAFT EO NR 2757-3460-150 REV A. INSTALLED B727 GPS ANTENNA DOUBLER AT BS 370 BETWEEN STRINGERS 1 AND 2R PER DECRANE AIRCRAFT EO NR 2757-3460-150 IAW DWG NO 2757-3460-1045 REV SDR 05FDEA00634Intercostal · crackedWHILE WORKING BARRIER MOD FOUND STR 16 LT INTERCOSTAL CRACKED AT BS 354. REPAIRED PER SRM 51-40-3.SDR 05FDEA00633Floorbeam · damagedWHILE ACCESSING FOR BARRIER MOD FOUND REPAIR ON FLOORBEAM BL 0 NEEDS REWORK TO ACCOMPLISH INSTALLATION OF EXTENDED SEAT TRACK. REPAIRED PER SRM 53-10-8SDR DHL2005782563Skin · damagedREMOVED AND REPLACED FASTENER ON NR NR 82194, BELOW STA 19R SAT 680 NEED TO EVALUATE MATERIAL LOSS FROM BLEND OUT. MEASURED BLEND OUT AT STA 680 STR 19R AND FOUND OUT OF LIMITS A.6/Y.028=21.4 IAW B727 SRM 53-30-1 FIG 1. FABRICATED DOUBLER MATERIAL IDENTIFICASDR DHL2005782561Skin · delaminatedLT WING OB AFT FLAP OB TE CORNER DELAMINATED. REMOVED PREVIOUS REPAIR AND CUT OUT DELAMINATED AREA OF LOWER SKIN APPROX 7" BY 5" AT O/B CORNER AND VACUUM BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20 FIG 31. FABRICATED REPLACEMENT SKIN APPROX 7" BY 5" ASDR DHL2005782562Skin · dentedNR 2 LE SLAT EXTERNAL SKIN HAS DENT WS 684.3 (AREA MARKED). DENT AT WS 684.3 ON NR 2 SLAT SKIN OUT OF LIMITS A.9/Y.032=28.1 IAW B727 SRM 57-50-1 FIG 1. CUT OUT DAMAGE AREA SIZE 1" BY 1" IAW B727 SRM 57-50-1. FABRICATED DOUBLER REPAIR USING 2024T3 .080 PO NRSDR DHL2005782560Skin · damagedACCOMPLISH IDENTIFICATION OF EXISTING REPAIR ON RT ELEVATOR LOWER SKIN AT STAB STA 106 PER ASTAR J/C NR FCD500001-001B. REPAIR ON RT ELEVATOR LWR SKIN AT STAB STA 106 FOUND TO BE IN NON-COMPLIANCE IAW 727 SRM 55-20-3 FIG 5. REMOVED REPAIRS 2 EA FOR INCORPARASDR DHL2005782559Skin · debondedLT I/B T/E FOREFLAP DISBONDED AT T/E. CUT OUT DISBONDED AREA AT TE APPROX 4 1/2" BY 1 3/4". REMOVED DAMAGED CORE APPROX 4 1/2" BY 1 3/4" AND VACUUM BAGGED FOR MOISTURE REMOVAL FABRICATED REPLACEMENT SKIN APPROX 4 1/2" BY 1 3/4" EXTERNAL DOUBLER APPROX 3 1/2"SDR DHL2005782558Hinge · crackedL/WING T/E SURFACE CRACKED AT NR 3 SPOILER HINGE CUTOUT (3RD). REMOVED NR 3 SPOILER TO FACILITATE S/M WORK IAW 7727-61-0 STOP DRILL CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER USING7075 T6 .071 PO NR 9001737 DIM 6 1/4" BY 4" IAW B727 SRM 57-30-04 FIG 10. SDR DHL2005782557Skin · crackedL/WING T/E SURFACE CRACKED AT NR 4 SPOILER HINGE CUTOUT (3RD). STOP DRILLED CRACK SIZE .250 IAW B727 SRM 51-10-1. REMOVED NR 4 SPOILER IAW B727 MM 27-61-0. NDT AREA IAW B727 NDTM PART 6 51-00-00 FIG 23 CRACK TERMINATES AT STOP DRILL HOLE, FABRICATE DOUBLER SDR DHL2005782546Stringer · crackedVERT STAB STR 8L CRACKED AT FIN STA 180.6. REMOVED FASTENERS CUT OUT DAMAGED AREA FABBED NEW STIFFENER FROM BAC 1517-1367 PO NR 501953 DIM 4 5/8" BY 3" SPLICE FROM AND 10133-1401 PO NR 501952 DIM 19 1/8" BY 2" SPLICE FROM AND 10134-1201 PO NR 501952 DIM 19 1/SDR DHL2005782500Skin · debondedLEFT INBOARD T/E FOREFLAP DISBONDED AT /TE. CUT OUT DISBONDED AREA AT T/E APPROX 4.5 X 1.75 INCH, REMOVED DAMAGED CORE APPROX 4.5 X 1.75 INCH AND VACUUM BAGGED FOR MOISTURE REMOVAL. FABRICATED REPLACEMENT SKIN APPROX 4.5 X 1.75 INCH EXTERNAL DOUBLER 3.5 X 7.SDR DHL2005782556Rib · gougedRT NR 5 BALANCE PANEL I/B RIB GOUGED. REMOVED RT NR 5 BALANCE BAY I/B SEAT PLATED FOR ACCESS IAW 727 SRM 51-30-2. EVALUATED DAMAGED TO BE OUT OF LIMITS IAW SRM 55-10-1 FIG 1. REMOVED RT NR 5 BALANCE PANEL I/B RIB IAW B727 SRM 51-30-2 AND INSTALLED NEW RIB SDR DHL2005782555Skin · damagedACCOMPLISH IDENTIFICATION OF EXISTING REPAIR ON FUSELAGE SKIN AT A/C STA 406 STRINGER 24R PER ASTAR J/C NR FCD500001-001B. EXISTING REPAIR FOUND TO BE NON-COMPLIANCE IAW 727 SRM 53-30-3 FIG 1. REMOVED PREVIOUS REPAIR IAW 727 SRM 51-30-2. FABRICATED NEW DOUBSDR DHL2005782570Skin · crackedCRACK ON PREVIOUS REPAIR RADIUS AT STR 21 FUSELAGE STA 950. REMOVED INTERCOSTAL AT STR 21 FUSELAGE STA 950 LT IAW SRM 51-30-2, FABRICATED NEW INTERCOSTAL USING 7075T6 .080 PO 9002012 SIZE 16 X 6 INCH IAW B727 SRM 53-10-2 AND INSTALLED INTERCOSTAL IAW B727 SRMSDR DHL2005782554Stringer · corrodedFUSELAGE STRINGER 23R CORRODED BS 441-470. CORROSION ON STRINGER 23R BS 441 TO BS 470 OUT OF LIMITS IAW B727 SRM 53-10-1 TIS 1. REMOVED STRINGER SECTION 23 R BS 441 TO BS 490 IAW B727 SRM 51-30-2. FABRICATED NEW FROM BAC 1498-142 PO NR 9001078 DIM 48 INCH LSDR DHL2005782553Stringer · corrodedFUSELAGE STRINGER 22R CORRODED BS 441-470. CORROSION ON STR 22R BS 441-470 OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. REMOVED STRINGER 22R BS 441-490 IAW 727 SRM 51-30-2. FABBED NEW FROM BAC 1498-142 PO NR 9001078 DIM 48 INCH LONG IAW 727 SRM 53-10-2 FIG 9 NESDR DHL2005782552Stringer · corrodedFUSELAGE STRINGER 21 R CORRODED BS 441-490. CORROSION ON STR 21R BS 440 TO 490 OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED STR 21R BS 440 TO 490 IAW B727 SRM 51-30-2. FABBED NEW FROM BAC 1498-142 PO NR 9001078 DIM 48 INCH LONG IAW B727 SRM 53-10-2 FIG
Back to Boeing 727-227