Boeing 727-2M7
Service difficulty reports · 459
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 = '7272M7' 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 = '7272M7' 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 C7WA200300078Wire · shortedNR 1 PACK VALVE CIRCUIT BREAKER POPPED ON CLIMB-OUT, CIRCUIT BREAKER WOULD NOT RESET. TROUBLESHOOTING PERFORMED BY WD 21-61-02, FOUND WIRE SHORTED. ACCOMPLISHED REPAIR BY WIRE SPLICE, AIR COND SYSTEM. TESTED WITH BOTH PACKS ON TESTED GOOD. (M)SDR DHL2004750045Landing Gear · collapsedRIGHT MAIN LANDING GEAR DAMAGED AND WING DAMAGED DUE TO INCIDENT, AFTER TOUCHDOWN THE RIGHT HAND MAIN LANDING GEAR COLLAPSED. REPAIRED RT MLG & WING DAMAGE IAW JC NR000000001 WO 600012457SDR C7WA200400067Line · looseON CLIMB OUT THROUGH 16,000, NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE WAS 35 PSI AND DECREASING. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN IAW AOM. FOUND NR 3 ENGINE LOW OIL PRESSURE SWITCH OIL LINE LEAKING. REMOVED AND REINSTALLED LINE OPERASDR DHL2004750044Battery · inoperativeBOTH EMERGENCY EXIT LIGHTS INOP ON PREFLIGHT. REPLACED EMERGENCY EXIT LIGHTS BATTERIES, CKS GOOD NOW.SDR DHL2004750042Warning System · malfunctionedENGINE NR 3 STRUT OVERHEAT LIGHT ILLUMINATED MOMENTARILY AFTER T/O. LIGHT EXTINGUISHED BEFORE ABNORMAL PROCEDURE WAS BEGUN. INSPECTED AND RAN NR 3 IAW JRH 5.2 WITH NO DEFECTS NOTED 26-14-00.SDR DHL2004750041Lens · crackedDURING FLIGHT THE EMERGENCY EXIT SIGN OVER THE FORWARD ENTRY DOOR FELL TO THE FLOOR AND CRACKED ITS LENS. REMOVED AND REPLACED ENTRY OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY, OPS CHECKED GOOD IAW M/M 33-50-01.SDR DHL2004750024Bracket · crackedDURING -C- CHECK, NR 1 LEADING EDGE FLAP ACTUATOR BRACKETS TRUNNION SUPPORT CRACKS BOTH SIDES I/B & O/B. REMOVED AND REINSTALLED NR 1 L/E FLAP ACTUATOR IAW B727 MM 27-81-22. REMOVED BRACKETS FROM NR 1 L/E FLAP ACTUATOR IAW B727 SRM 51-30-2, 2EA LEFT & RIGHTSDR DHL2004750040Stringer · corrodedDURING -C- CHECK, STRINGER 19L CORRODED AT BS 720D & 10. REMOVED FASTENERS FOR ACCESS IAW 727 SRM 51-30-2. CUT OUT DAMAGED SECTION OF STRINGER AND FABBED FILLER FROM BAC 1498-144 PO 3357 92 DIM 3.5 INCH SPLICE FROM BAC 1498-125 PO 335792 DIM 15.125 IAW 727 SDR DHL2004750039Web · crackedDURING -C- CHECK, LWR VERTICLE LEADING EDGE LWR INTERNAL WEB CRACKS OUT AROUND BOLT FIN STA 55.9. REMOVED DAMAGED WEB AND FABBED NEW FROM 2024-T3 .032 PO 900534 DIM 12.75 X 12 INCH IAW 727 SRM 55-30-2 FIG 2. WEB TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALSDR DHL2004750038Frame · crackedDURING -C- CHECK, LT WING L/E CAVITY WBL 92 INT FRAME STIFFENER 2ND FROM SPAR HAS UPPER END CRACKED. CUT OUT DAMAGED AREA AND FABRICATED FILLER FROM 2024 T3 .032 PO 900534 DIM 3.75 X 2.5 INCH REPAIR ANGLE FROM 7075 T3 040 PO 900226 DIM 7 X 3.5 INCH IAW B727 SSDR DHL2004750037Stiffener · crackedDURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT WING L/E CAVITY WBL 92 INT FRAME INBOARD SIDE UPPER STIFFENER 1ST FWD OF SPAR HAS UPPER END CRACKED. CUT OUT DAMAGE AREA & FABRICATED DOUBLER FROM 2024 T3 .040 PO 900226, 7 X 1.5 X 1.5 INCH, FILLER FROM 2024T3 .0SDR DHL2004750026Rod End · crackedDURING C-CHECK, NR 7 SLAT AT ACT ROD END HAS INBOARD ATTACH FRAME CRACKED IN LOWER FWD RADIUS. REMOVED CRACKED RIB, LOCATED, DRILLED AND INSTALLED NEW RIB P/N 65-17310-3, PO 413646 IAW B727 SRM 51-30-2 FIG 1 & 2. ACCOMPLISHED L/E FLAPS OP'S CHECK FOUND OK IASDR C7WA200400003Warning Light · illuminatedLWR AFT CARGO FIRE LIGHT CAME ON AFTER TAKEOFF AND THEN EXTINGUISHED ON FINAL APPROACH BACK. ADDITIONALLY THE DUCT OVERHEAT LIGHT ON PILOTS OVERHEAD PANEL CAME ON AND REMAINED ON DURING FINAL APPROACH. TEMP PEGGED AT 250 DEGREES OR GREATER. OPS CHECK OF LOWSDR DHL2004750036Skin · dentedDURING -C- CHECK, RIGHT HORIZ STAB, I/B LEADING EDGE AT STAB STA 13.7 HAS A DENTED GOUGE. DENTED GOUGE OUT OF LIMITS IAW B727 SRM 55-10-1 FIG 2. CUT OUT DAMAGE AREA IAW B727 SRM 55-10-3 FIG 2. FABRICATED DOUBLERS FROM 2024 T3 .071 & FILLER FROM 2024 T3 .050SDR DHL2004750035Skin · dentedDURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT FUSELAGE HAS A DENT BS 720E BELOW STR 17L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA (1.9375 X 1.875 INCH) AND FABBED DOUBLER FROM2024-T3 100 PO 900484 DIM 12.25 X 8.75 INCSDR DHL2004750034Skin · dentedDURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT FUSELAGE HAS A DENT BS 1166 ABOVE STR 25L. DAMAGED FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGED AREA DIM (1.25 X .75 INCH) & FAB DOUBLER FROM 2024 T3 .071 PO 900484 DIM 10.125 X 6.5 INCH IAW BSDR DHL2004750033Skin · dentedDURING -C- CHECK, RT FUSELAGE HAS A DENT BS 1130 BELOW STR 21R. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1061. CUT OUT DAMAGED AREA 2.5 X 1.5 INCH AND FABBED REPAIR DOUBLER FROM 2024 T3 .071 PO 900484 DIM 12 X 7 INCH IAW 727 SRM 53-30-3 FIG 1 & 53-SDR DHL2004750032Skin · dentedDURING C-CHECK, RIGHT FUSELAGE HAS 3 DENTS BS 1090 BELOW STR 19R. ACTION AS FOLLOWS; DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-80-1 FIG 1. CUT OUT DAMAGED AREA DIM 2.75 X 2 INCH AND FABBED DOUBLER FROM 2024 T3 .071 PO 900484 DIM 13 X 7.75 INCH IAW 727 SDR DHL2004750022Frame · dentedDURING -C- CHECK, LEFT FUSELAGE HAS A DENT BS 1273 BELOW STR 14L. CUT OUT DAMAGED AREA DIM 1.875 X 1.25 INCH AND FABRICATED DOUBLER, MAT ID 2024T3 .071 PO 900484 DIM 8.25 X 10.875 IAW B727 SRM 53-30-3, TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED DOUSDR DHL2004750021Frame · dentedDURING C-CHECK, LT FUSELAGE FRAME HAS A DENT BS 1283 BELOW STR 22L. CUT OUT DAMAGED AREA .75 X .375 INCH LEFT FUSELAGE BS 1287 BETWEEN STR 22L FAB DOUBLER 2024-T3 PO 300606 DIM 6.5 X 12 INCH IAW B272 SRM 57-30-2 FIG 3, 53-30-3 FIG 3. ALODINED AND PRIMED IAW SDR DHL2004750020Frame · dentedDURING -C- CHECK, LT FUSELAGE HAS A DENT BS 1070 BELOW STR 17L. REMOVED DAMAGE CUTOUT IS A 1.0 INCH CIRCLE IAW B727 SRM 53-30-3 FIG 1. FABRICATED DOUBLER FROM 2024T3 .090 PO 900103. DOUBLER IS 10.5 X 13.5 INCH IAW B727 SRM 53-30-3 FIG 1. TREATED AND PRIMESDR DHL2004750016Skin · dentedDURING -C- CHECK, LEFT L2 DOOR HAS DENT BS 1050 STR 16L. REMOVED DAMAGE, CUTOUT IS .65 X .50 INCH IAW B727 SRM 52-00-3 FIG 3. FABRICATED DOUBLER FROM 2024T3 .063 PO 900606. DOUBLER IS .063, 6.5 X 7.2 INCH IAW B727 SRM 52-00-3 FIG 3. TREATED AND PRIMED IAWSDR DHL2004750015Frame · dentedDURING -C- CHECK, LEFT FUSELAGE HAS A DENT BS 431 ABOVE STR 20L. CUT OUT DAMAGED AREA .75 INCH DIA AND FABBED FILLER, FROM 2024-T3 .063, PO 900606, DIA .75 INCH AND DOUBLER FROM 2024-T3, .071, PO 900484 DIA 3.25 INCH IAW B727 SRM 53-30-2 FIG 2 AND 53-30-3 FIGSDR DHL2004750013Frame · dentedDURING -C- CHECK, LEFT FUSELAGE HAS A DENT BS 1130 ABOVE STR 26L. DAMAGED FOUND TO BE OUT OF LIMITS IAW B-727-SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA SIZE 2 X 1.75 INCH AND FABRICATED DOUBLER FROM 2024-T3 .071 PO 900484 DIM 10 X 8.5 INCH STRUCTURAL FILLER FSDR DHL2004750031Bracket · crackedDURING C-CHECK, NR 6 L/E FLAP ACTUATOR TRUNNION BRACKETS SUPPORT BOTH I/B & O/B CRACKED WBL 304. REMOVED DAMAGED SUPPORTS AND FABBED NEW FROM 7075-T6, .063, PO 900226, DIM 7.5 X 3.5 INCH EA IAW B727 SRM 57-10-2 FIG 3. TREATED AND PRIMED IAW B727 SRM 51-10-2.SDR DHL2004750030Stiffener · crackedDURING C-CHECK, LEFT WING FRONT SPAR & WBL 92.8 VERTICAL STIFFENER CRACK INDICATION FROM BOTTOM END. REMOVED FASTENERS FOR ACCESS IAW B727 SRM 51-30-2, STOPDRILLED CRACK AT LEFT WING FRONT SPAR VERTICAL STIFFENER IAW B727 SRM 51-10-1, FABRICATED ANGLE REPAIR SDR DHL2004750029Stiffener · crackedDURING C-CHECK, LT WING L/E CAVITY WBL 92 INT FRAME STIFFENER 1ST FWD OF SPAR HAS LOWER END CRACKED THRU FASTENER. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 7075-T6 .040 PO 900226 DIM 5 X 2 X 2 INCH AND DOUBLER FROM 7075-T6 .050 PO 900489 DIM 7 X 2 X 2 INCHSDR DHL2004750028Attach Angle · crackedDURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT WING L/E CAVITY WS 130.7 INBOARD SIDE OF INT FRAME UPPER ATTACH ANGLE HAS 12 INCH CRACK IN RADIUS. REMOVED EXISTING ANGLE IAW B727 SRM 51-30-2. FABRICATED ANGLE FROM 2024-T3, .050, 7 X 2 INCH, PO 900641 IAW B727SDR DHL2004750025Bracket · crackedDURING -C- CHECK, NR 5 L/E FLAP ACTUATOR TRUNNION BRACKETS SUPPORT BOTH I/B & O/B ARE CRACKED WS 171. REMOVED AND REINSTALLED NR 5 L/E FLAP ACTUATOR IAW B727 MM 27-81-22. REMOVED DAMAGED SUPPORT ANGLES 2EA AND FABBED NEW FROM 7075-T6, .063, PO 900226, DIM 8SDR DHL2004750023Floor Support · bentDURING -C- CHECK, FWD CARGO FLOOR SUPPORT IS BENT BS 600 RBL 3. CUT OUT DAMAGED AREA SIZE 1 X 4 INCH ON FWD CARGO FLOOR SUPPORT BS 600 RBL 3 IAW B727 SRM 51-10-1. FABRICATED FILLER FROM 2024T3 .063 SIZE 1 X 4 INCH PO 900606 AND ANGLE FROM BAC 1506-1080 SIZESDR DHL2004750019Rod End · crackedDURING -C- CHECK, NR 2 SLAT AT ACT ROD END ATTACH HAS INBOARD ATTACH FRAME CRACKED IN FWD LOWER RADIUS. REMOVED AND REPLACED AT NR 2 SLAT AT ACT ROD END ATTACH HAS INBOARD ATTACH FRAME BY FWD LOWER 2 EA RIB SUPPORT PO 413627 P/N 65-17310-4 AND PIL 413644 P/NSDR DHL2004750018Frame · crackedDURING -C- CHECK, NR 3 SLAT AT ACT ROD END HAS OUTBOARD ATTACH FRAME IS CRACKED IN AFT RADIUS. REMOVED AND REPLACED NR 3 SLAT AT ACT ROD AND OUTBOARD ATTACH FRAME AFT 2 EA RIB SUPPORT PO 4136-27 P/N 65-17294-13 AND PO 413643 P/N 65-17294-14 IAW B727 SRM 51-30SDR DHL2004750017Rib · crackedDURING -C- CHECK, DISCREPANCY AS FOLLOWS; NR 7 SLAT INTERIOR RIB O/B OF ACTUATOR ATTACH POINT CRACK INDICATION WS 640 NDT CONFIRMED. REMOVED CRACKED RIBS LOCATED, DRILLED AND INSTALLED NEW RIB P/N 65-17310-4, PO 410362 IAW B727 SRM 51-30-2, FIG 1 & 2.SDR DHL2004750027Frame · dentedDURING -C- CHECK, DISCREPANCY AS FOLLOWS; UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 540. CUT OUT DAMAGED AREA SIZE .75 X 1 INCH ON UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME AT BS 540 IAW B727 SRM 51-10-1, FABRICATED REPAISDR DHL2004750012Frame · dentedDURING -C- CHECK, UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 560. CUT OUT DAMAGE AREA SIZE .5 X 1 INCH ON UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME BS 560 IAW B727 SRM 51-10-1. FABRICATED, REPAIR ANGLE FROM 7075T6 .063 SSDR DHL2004750011Frame · dentedDURING -C- CHECK, UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 580. CUT OUT DAMAGED AREA 1 X .75 INCH AND FABBED REPAIR ANGLE FROM 7075-T6 .063 PO 900489 DIM 8 X 3.75 INCH IAW 727 SRM 53-10-2 FIG 1 & 51-40-3 FIG 1. PART TREATED & PRISDR DHL2004750010Frame · dentedDURING -C- CHECK, UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND STR 17R FRAME IS DENTED AT BS 600. CUT OUT DAMAGED AREA DIM 1 INCH X .75 INCH AND FABBED REPAIR ANGLE FROM 7075-T6 .053 PO 900489 DIM 8 X 3.75 INCH IAW 727 SRM 53-10-2 FIG 1 & 51-40-3 FIG 1. PART SDR DHL2004750008Frame · dentedDURING C-CHECK, UPPER CABIN RT SIDE BS 500 BETWEEN STR 17R AND 16R DENTED. CUT OUT DAMAGE AREA DIM 1 X .75 INCH IAW B727 SRM 51-40-3 FIG 1. FABRICATED DOUBLER REPAIR FROM MAT 7075-T6 .063 PO 900166 DIM 9 X 3.75 INCH IAW B727 SRM 51-40-3 FIG 1. TREATED AND PSDR DHL2004750007Frame · dentedDURING C-CHECK, UPPER CABIN RT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 620. CUT OUT DAMAGED AREA DIM 1 X .75 INCH IAW B727 SRM 51-40-3 FIG 1, FABRICATED DOUBLER MAT 7075-T6 .063 PO 900489, DIM 3.75 X 7.625 INCH IAW B727 SRM 51-40-3 FIG 1, TREATED ASDR DHL2004750006Frame · dentedDURING C-CHECK, UPPER CABIN RT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 520. CUT OUT DAMAGE AREA DIM 1 X .75 INCH IAW B727 SRM 51-40-3 FIG 1, FABRICATED DOUBLER REPAIR FROM MAT 7075-T6 .063 PO 900166 DIM 9 X 3.75 INCH IAW B727 SRM 51-40-3 FIG 1, TRESDR DHL2004750014Skin · damagedDURING -C- CHECK, RIGHT FWD OVERWING EMERGENCY EXIT HATCH TOP EXTERIOR SKIN EDGE IS BENT OUT WITH RIVET HEADS PULLING THROUGH SKIN. REMOVED FASTENERS AS REQUIRED FOR ACCES IAW B727 SRM 51-30-2. CUT OUT DAMAGE AREA, DIMENSION: 9.75 X 1.375 INCH IAW B727 SRM 5SDR DHL2004750009Door Frame · dentedDURING -C- CHECK AT FLIGHTSTAR AIRCRAFT SERVICES IN JACKSONVILLE FLORIDA, DISCREPANCY AS FOLLOWS; C1 DOOR EXTERNAL HAS DENT IN BOTTOM CENTER OF DOOR U-CHANNEL. REMOVED DAMAGED ANGLE IAW B727 SRM 51-30-2, FABRICATED NEW ANGLE FROM BAC1496-383 PO 206631 DIM 44 SDR DHL2004750005Light · illuminatedEMERGENCY EXIT LIGHTS IN COCKPIT ILLUMINATES ON TOUCHDOWN, EVEN GENTLE ONES. RESECURED EMERGENCY EXIT LIGHT IN COCKPIT IAW B-727 M/M 33-50-101. OPS CHECKED GOOD.SDR DHL2004750003Light · inoperativeON P/F MAIN EXIT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT IAW 33-50-101. OPS CHECKED GOOD. (P/N ON: 10-0067-7, S/N ON: 23781)SDR DHL2004750004Light · inoperativeEXIT LIGHT OVER COCKPIT DOOR INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT IAW 33-50-101. OPS CHECKED GOOD. (P/N ON: 10-0067-7, S/N ON: 25899)SDR C7WA200400001Gyro · inoperativeABORTED TAKEOFF AT APPROX 80 KTS DUE TO FAILURE OF F/O DIRECTIONAL GYRO. REMOVED AND REPLACED VIRTICAL GYRO IAW MM.SDR DHL2004750002Light · inoperativeFOUND EMERGENCY EXIT LIGHT ASSEMBLY (LOCATED OVER ENTRY DOOR) ON ENTRY WAY FLOOR. REINSTALLED LIGHT ASSEMBLY, OPS CHECKED GOOD IAW B-727 M/M 33-50-01.SDR DHL2004750001Light · dislodgedFORWARD ENTRY EMERGENCY EXIT LIGHT FELL OUT OF ITS MOUNT. REPLACED AND SECURED EMERGENCY EXIT LIGHT IAW B-M/M 33-50-101. OPS CHECKED GOOD.SDR DHL2003750009Actuator · failedSTABILIZER JAMMED ONLY IN NOSE UP TRIM. NOSE DOWN TRIM WORKS NORMAL DURING DESCENT. PERFORMED ABNORMAL PROCEDURE WITH NO RESULT. FLAPS 15 DEGREES LANDING IN CVG. REMOVED AND REPLACED CRUISE TRIM ACTUATOR AND MAIN ELECTRIC STAB TRIM ACTUATOR IAW B-727 M/M 2SDR C7WA200300051Connector · looseFLIGHT RETURN, AFT BODY OVERHEAT LIGHT CAME ON IN FLIGHT. CLEANED AND RESEATED CONNECTOR AT LOWER AFT BODY OVERHEAT SENSING ELEMENT, OPS CHECK NORMAL IAW MM 20-60-01 AND 26-14-0. (M)
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