# Service difficulty reports: Boeing 727-82C

A list on [Boeing 727-82C](https://openairdocs.org/model/boeing-727-82c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 164 reports

- [SDR DHL2002709004](https://openairdocs.org/sdr/DHL2002709004.md): Light · inoperative · Jun 26, 2002 · N709DH · Boeing 72782C · Emergency Lighting
  > COCKPIT EMERGENCY EXIT LIGHT WILL NOT HOLD A CHARGE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY SYST, OPS CHECKED GOOD IAW B727 MM 33-50-00.
- [SDR DHL2002709003](https://openairdocs.org/sdr/DHL2002709003.md): Light · Jun 25, 2002 · N709DH · Boeing 72782C · Emergency Lighting
  > 1) FWD MAIN ENTRY DOOR EMERGENCY EXIT LIGHT VERY DIM.2) R/R EMERGENCY EXIT LIGHT ASSY IAW MM 33-50-00 OPS CK GOOD.
- [SDR DHL2002709002](https://openairdocs.org/sdr/DHL2002709002.md): Electrical Sys · malfunctioned · Jan 15, 2002 · N709DH · Boeing 72782C · Airborne Auxiliary Power Unit (APU) System
  > APU ELECTRICAL TRIPPED OFF. A FEW SECONDS LATER, LEFT PACK TRIP OFF LIGHT ILLUMINATED AND THEN COCKPIT FILLED WITH SMOKE. RAN APU IAW MM 49-00 & JRH 8.1. APU & AIR OPS CHECKS GOOD. APU ELECTRICS WILL NOT HOLD A LOAD.
- [SDR DHL2002709001](https://openairdocs.org/sdr/DHL2002709001.md): Windshield Wiper · out of adj · Jan 11, 2002 · N709DH · Boeing 72782C · Windshield/Door Rain/Ice Removal
  > F/O WINDSHIELD WIPER BLADE WILL NOT RUN IN LOW. ADJUSTED F/O'S WIPER IAW 727 MM CHP 30-42-01, OPS CHECK NORMAL AT THIS TIME.
- [SDR DHL2001709013](https://openairdocs.org/sdr/DHL2001709013.md): Fire Loop · out of position · Sep 15, 2001 · N709DH · Boeing 72782C · Fire Detection
  > NR 1 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED ON P6-3 GROUND FAULT. DEFERRED PER MEL 26-9 CAT-C CONTROL 7094. REPOSITIONED FIRE LOOP AND TESTED IAW 727 MM 26-11-0, OPS CHECK NORMAL AT THIS TIME. THIS CLEARS DMI 7094 PLACARD REMOVED.
- [SDR DHL2001709012](https://openairdocs.org/sdr/DHL2001709012.md): Switch · malfunctioned · Sep 11, 2001 · N709DH · Boeing 72782C · Landing Gear Position and Warning
  > ON FINAL NOSE GEAR INDICATION WENT FROM DOWN AND LOCKED 3 GREEN TO UNSAFE. VISUALLY CONFIRMED GEAR DOWN AND LOCKED. ON FINAL GEAR WENT FROM UNSAFE TO DOWN AND LOCKED. INSTALLED NEW NOSE GEAR LOCK AND POSITION CONTROL SWITCH IAW B-MM 32-61-01, OPS CHECK GOOD
- [SDR DHL2001709011](https://openairdocs.org/sdr/DHL2001709011.md): Fire Loop · out of position · Aug 25, 2001 · N709DH · Boeing 72782C · Fire Detection
  > NR 1 ENGINE FIRE DETECTOR CIRCUIT AND LIGHT ILLUMINATED. REPOSITIONED FIRE LOOP. OPS CHECKED GOOD IAW DHL 727 MM CH 26-11-00.
- [SDR DHL2001709010](https://openairdocs.org/sdr/DHL2001709010.md): Fire Loop · inoperative · Jul 19, 2001 · N709DH · Boeing 72782C · Fire Detection
  > NR 1 ENGINE FIRE DETECTION SYSTEM WILL NOT TEST NR 1 ENG FIRE WALL TEST INOP. INSTALLED OVERHAULED ENGINE SENSOR LOOP IAW WITH B-M/M 26-11-021 R&R FIRE SENSOR/RESPONDER IAW B-727 M/M 26-11-31 ON NR 1 ENG, OPS CHECK SERVICEABLE.
- [SDR 2001F00221](https://openairdocs.org/sdr/2001F00221.md): Hydraulic Line · leaking · Jul 4, 2001 · N528PC · Boeing 72782C · Hydraulic System, Main
  > TOTAL LOSS OF A SYSTEM HYDRAULICS. COMPLIED WITH EMERGENCY CHECKLIST OF HYDRAULIC SYSTEM FAILURE. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED SPOILER PRESSURE LINE AND RETURN LINE IN LEFT WING. SERVICED WITH SKYDROL. OPERAT
- [SDR 2001F00220](https://openairdocs.org/sdr/2001F00220.md): Hydraulic Line · leaking · Jul 4, 2001 · N528PC · Boeing 72782C · Hydraulic System, Main
  > TOTAL LOSS OF A SYSTEM HYDRAULICS. COMPLIED WITH EMERGENCY CHECKLIST OF HYDRAULIC SYSTEM FAILURE. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED SPOILER PRESSURE LINE AND RETURN LINE IN LEFT WING. SERVICED WITH SKYDROL. OPERAT
- [SDR 2001F00099](https://openairdocs.org/sdr/2001F00099.md): Element · malfunctioned · Jun 14, 2001 · N528PC · Boeing 72782C · Fire Detection
  > WHEEL WELL FIRE LIGHT ILLUMINATED 4 MINUTES AFTER TAKEOFF. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT WHEEL WELL FIRE SENSING ELEMENT. (M)
- [SDR DHL2001709009](https://openairdocs.org/sdr/DHL2001709009.md): Autopilot Sys · malfunctioned · Jun 14, 2001 · N709DH · Boeing 72782C · Autopilot System
  > AT FL350 WITH A/P ENGAGED AND ELEVATOR IN A OR B MODE, A/P PITCHES UP AND WILL NOT HOLD ALTITUDE. (BEGINS ALTITUDE OSCILLATION AND OVER CORRECTS WITH TRIM). AUTOPILOT DEFERRED PER DHL MEL 22-1 CAT B, DMI 6023 PLACARD INSTALLED. COULD NOT DUPLICATE ON GROUND
- [SDR DHL2001709008](https://openairdocs.org/sdr/DHL2001709008.md): Control Handle · broken · May 31, 2001 · N709DH · Boeing 72782C · Landing Gear Selector
  > GREEN GEAR NOSE LIGHT EXTINGUISHED AND RED GEAR LIGHT ILLUMINATED WITH GEAR LEVER DOWN. ABNORMAL PROCEDURES ACCOMPLISHED. FOUND ARM AND LINKAGE BROKEN AT APEX ATTACH POINT. REPLACED LEVERS WITH NEW AND INSTALLED IAW BMM 32-61-21. ALL TESTING CHECKED GOOD.
- [SDR DHL2001709007](https://openairdocs.org/sdr/DHL2001709007.md): Light · malfunctioned · May 18, 2001 · N709DH · Boeing 72782C · Landing Gear Position and Warning
  > LEFT GEAR WARNING LIGHT IN TRANSIT (RED) DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED. ALL GEAR LIGHTS TEST ARE NORMAL. MAIN LANDING GEAR LOCK SWITCHES TESTED PER MM 32-61-21 (4) CHKS OPS CHECK.
- [SDR DHL2001709006](https://openairdocs.org/sdr/DHL2001709006.md): Light · inoperative · May 16, 2001 · N709DH · Boeing 72782C · Landing Gear Position and Warning
  > LT LANDING GEAR INTRANSIT UNSAFE LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION OR EXTENSION. ALL RED LIGHTS GROUND TEST NORMAL. FOUND LT MAIN GEAR RED LIGHT INOPERATIVE. (NO TEST) RELAMPED LIGHT. PERFORMED GEAR INDICATION WARNING TEST IAW B727 M/M 32-61-0
- [SDR DHL2001709005](https://openairdocs.org/sdr/DHL2001709005.md): Battery · discharged · Apr 28, 2001 · N709DH · Boeing 72782C · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED ALL DOOR EMER EXIT BATTERIES WITH SERVICABLE. OPS CHECK GOOD IAW MM 33-50-01.
- [SDR DHL2001709004](https://openairdocs.org/sdr/DHL2001709004.md): Control Unit · malfunctioned · Apr 18, 2001 · N709DH · Boeing 72782C · Autopilot System
  > ANYTIME THE AUTOPILOT ELEVATOR IS ENGAGED IN A SYSTEM MODE, THE AIRCRAFT PITCHES ERATICALLY UP AND DOWN. R / R PITCH CHANNEL CONTROL IAW MM 22-11-01. SECURITY CHECK IS GOOD. STATUS-CLOSED.
- [SDR DHL2001709003](https://openairdocs.org/sdr/DHL2001709003.md): Autopilot Sys · malfunctioned · Apr 17, 2001 · N709DH · Boeing 72782C · Autopilot System
  > WITH AUTOPILOT AND ALT HOLD ENGAGED, A/C GAINS ABOUT 300 FT AN HOUR IN BOTH A & B MODE AND WITH AUX 1 NORMAL AND AUX VGS SELECTED. TRANSFERRED ITEM TO DEFERRAL-ALT, SELECT MODE - DMI 5201 PER MEL 27-1-3, PLACARD INSTALLED. STATUS-OPEN
- [SDR DHL2001709002](https://openairdocs.org/sdr/DHL2001709002.md): Start Valve · malfunctioned · Feb 20, 2001 · N709DH · Boeing 72782C · Engine Start Valves/Controls
  > NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED ON TAXI-OUT. SHUT DOWN ENGINE AND CLOSED NR 3 BLEED. REMOVED AND REPLACED NR 3 ENGINE START VALVE (P/N 979254-1-1) (S/N 13835) OFF WITH (P/N 979254-1-1) (S/N P-1541) ON, PER M/M 80-11-11. OPS CHECK GOOD.
- [SDR 20010425AP003](https://openairdocs.org/sdr/20010425AP003.md): Bulb · burned out · Feb 18, 2001 · N528PC · Boeing 72782C · Smoke Detection
  > MAIN CABIN SMOKE DETECTOR HAS 1 BACKGROUND LIGHT INOPERATIVE. REMOVED AND REPLACED ONE BACKGROUND LIGHT IN MAIN CABIN SMOKE DETECTOR INDICATOR ON FLIGHT ENGINEERS PANEL. SYSTEM TEST NORMAL. (M)
- [SDR DHL2001709001](https://openairdocs.org/sdr/DHL2001709001.md): Harness · chafed · Feb 17, 2001 · N709DH · Boeing 72782C · Engine Start Valves/Controls
  > DURING TAXI-OUT, ENGINE NR 3 START VALVE OPEN LIGHT ILLUMINATED. TROUBLESHOT SYSTEM AND FOUND START VALVE LIGHT SWITCH CANNON PLUG WIRES CHAFING (BARE) AND WITHOUT STRAIN RELIEF. INSTALLED NEW PINS AND STRAIN-RELIEF BACKSHELL REFERENCE M/M 20-11-0. PERFORME
- [SDR DHL2001709064](https://openairdocs.org/sdr/DHL2001709064.md): Fairing · missing · Dec 28, 2000 · N709DH · Boeing 72782C · Trailing Edge Flap Control System
  > NR 8 FLAP JACKSCREW FAIRING MISSING. TRANS TO DMI 3788.
- [SDR DHL2000709063](https://openairdocs.org/sdr/DHL2000709063.md): Switch · out of adj · Oct 20, 2000 · N709DH · Boeing 72782C · Trailing Edge Flap Control System
  > CONFIGURATION WARNING HORN SOUNDS WITH TAKEOFF POWER APPLIED. COFIGURATIONS NORMAL. ADJUSTED FLAP T/O WARNING SWITCH S 196. TESTED T/O WARNING SYS PER M/M 31-26-0, TEST OK.
- [SDR DHL2000709062](https://openairdocs.org/sdr/DHL2000709062.md): Csd · failed · Sep 23, 2000 · N709DH · Boeing 72782C · Alternator-Generator Drive
  > NR 1 CSD LOW OIL PRESS LIGHT ILLUM DURING TAXI. RETURNED TO BLOCKS IN TEMP 150 AND RISING. DEFERRED PER MEL 24-1 DMI NR 2496 CAT B PLACARD INSTALLED. THE CSD WAS REMOVED AND REPLACED PER M/M 24-10-61.
- [SDR DHL200070948D](https://openairdocs.org/sdr/DHL200070948D.md): Skin · dented · Aug 21, 2000 · N709DH · Boeing 72782C · Trailing Edge Flaps
  > RIGHT WING L/E SKIN HAS 3 DENTS OVER NR 4 L/E FLAP. REMOVED INNER SKIN FOR ACCESS PER SRM 51-30-2. REWORKED ALL 3 DENTS PER SRM 57-20-1. REINSTALLED INNER SKIN PER SRM 51-30-2.
- [SDR DHL200070937C](https://openairdocs.org/sdr/DHL200070937C.md): Skin · damaged · Aug 13, 2000 · N709DH · Boeing 72782C · Trailing Edge Flaps
  > DURING C CHECK INSPECTION, FOUND HOLE IN UPPER SURFACE OF RIGHT INBORD AFT FLAP APPROX 18 INCHES OF NR 6 AFT FLAP FAIRING. INSTALLED DOUBLER PER SRM 51-40-0. SIZE OF REPAIR 7.5 X 5 INCHES.
- [SDR DHL200070958D](https://openairdocs.org/sdr/DHL200070958D.md): Skin · delaminated · Aug 5, 2000 · N709DH · Boeing 72782C · Trailing Edge Flaps
  > LEFT WING O/B TRAILING EDGE FLAP AFT LOWER SURFACE OLD REPAIR IS DELAMINATED. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8. SANDED AND PAINTED PER SRM 51-20-0.
- [SDR DHL200070949D](https://openairdocs.org/sdr/DHL200070949D.md): Fitting · cracked · Aug 1, 2000 · N709DH · Boeing 72782C · Wing Miscellaneous Structure
  > RT WING UPPER FRONT SPAR CORNER FITTING AT RBL 70.5 IS CRACKED. REMOVED UPPER FRONT FITTING PER SRM 51-30-2. INSTALLED NEW FITTING PER SRM 51-30-2.
- [SDR DHL200070938C](https://openairdocs.org/sdr/DHL200070938C.md): Structure · corroded · Jul 31, 2000 · N709DH · Boeing 72782C · Trailing Edge Flaps
  > DURING D CHECK INSPECTION, FOUND RT WING I/B MID FLAP I/B FITTING CARRIAGE CAVITY CORRODED AT ACCESS PLATE 8508. REMOVED CORROSION. MATERIAL LOSS.050. OUT OF LIMITS PER SRM 57-30-1. INSTALLED 2 X 7 INCHES REINFORCED ANGLE.
- [SDR DHL200070936C](https://openairdocs.org/sdr/DHL200070936C.md): Panel · cracked · Jul 31, 2000 · N709DH · Boeing 72782C · Wing, Plate/Skin
  > DURING D CHECK INSPECTION, FOUND LT WING LOWER SURFACE PANEL NR 1 JACKSCREW FASTENER HOLE ATTACH TO UPPER FAIRING CRACKED. INSTALLED COMPOSITE REPAIR TO LEFT WING LOWER SURFACE PER MM 12-30-0 AND SRM 51-40-6. SIZE OF REPAIR 3 X 4.
- [SDR DHL200070935C](https://openairdocs.org/sdr/DHL200070935C.md): Structure · corroded · Jul 31, 2000 · N709DH · Boeing 72782C · Trailing Edge Flaps
  > DURING D CHECK INSPECTION, FOUND RIGHT WING I/B MID FLAP I/B FITTING CARRIAGE CAVITY CORRODED AT ACCESS PLATE 8508. REMOVED CORROSION. MATERIAL LOSS.050. OUT OF LIMITS PER SRM 57-30-1. INSTALLED 2 X 7 INCH REINFORCED ANGLE.
- [SDR DHL200070923C](https://openairdocs.org/sdr/DHL200070923C.md): Bulkhead · cracked · Jul 23, 2000 · N709DH · Boeing 72782C · Fuselage Main, Bulkhead
  > AFT BULKHEAD BS 1183, BETWEEN RBL 12 TO RBL 26 DITCH PAN HAS CRACK. REMOVED DAMAGED DITCH PAN AND FABRICATED NEW PAN PER SRM 51-10-1, 51-10-2 AND 51-10-2. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED NEW PAN PER SRM 51-30-2.
- [SDR DHL200070929C](https://openairdocs.org/sdr/DHL200070929C.md): Bulkhead · cracked · Jul 22, 2000 · N709DH · Boeing 72782C · Fuselage Main, Bulkhead
  > AFT BULKHEAD FUSELAGE STA 1183 RT LOWER 20 IN FROM RT CORNER FOUND DITCH PAN CRACKED. (BETWEEN RBL 24.7 AND RBL 45.5). REMOVED PAN PER SRM 51-30-2. CLEANED AREA TREATED AND PRIMED PER SRM 51-10-2. INSTALLED NEW DITCH PAN PER SRM 51-30-2. TREATED AND PRIME
- [SDR DHL200070934C](https://openairdocs.org/sdr/DHL200070934C.md): Cover · worn · Jul 20, 2000 · N709DH · Boeing 72782C · Engine Mount Section
  > NR 2 ENGINE FIREWALL REAR MOUNT LOWER SURFACE FIBERGLASS COVER WORN. REMOVED COVER AND SENT TO FIBERGLASS SHOP FOR REPAIR PER M/M 54-30-0. INSTALLED FIBERGLASS REPAIR ON COVER PER SRM 51-40-8. INSTALLED MOUNT COVER PER M/M 54-30-0.
- [SDR DHL200070912C](https://openairdocs.org/sdr/DHL200070912C.md): Floor Panel · corroded · Jul 19, 2000 · N709DH · Boeing 72782C · Fuselage Floor Panel
  > MAIN CARGO COMPT FLOOR PANEL 1B CORRODED ON TOP AREA. REMOVED UPPER SKIN AND CORROSION FROM FLOOR PANEL PER SRM 51-10-6. MATERAL LOSS WITHIN LIMITS PER SRM 53-30-1. TREATED AND PRIMED PER SRM 51-10-2. FABRICATED AND INSTALLED NEW UPPER SKIN AT FLOOR PANEL
- [SDR DHL200070930C](https://openairdocs.org/sdr/DHL200070930C.md): Skin · cracked · Jul 19, 2000 · N709DH · Boeing 72782C · Trailing Edge Flaps
  > RIGHT WING I/B FLAP MID SECTION CRACK INDICATION (2) AT CUTOUT I/B EXTENSION MECHANISM. REMOVED FASTENERS PER SRM 51-30-2. STOP DRILLED AT END OF CRACK PER SRM 51-10-1. PERFORMED HFEC INSPECTION PER NDT MAN 51-00-00, NO CRACK PAST STOP DRILL. INSTALLED DOU
- [SDR DHL200070961D](https://openairdocs.org/sdr/DHL200070961D.md): Door Frame · cracked · Jul 18, 2000 · N709DH · Boeing 72782C · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR UPPER FRAME IS CRACKED AT INNER BLENDING RADIOUS AT 2 LOCATIONS AT FWD AND AFT STOP FITTINGS. REMOVED FASTENERS AT INNER SKIN AND REMOVED UPPER CENTER FRAME PER SRM 51-30-2. FABRICATED NEW UPPER FRAME PER SRM 52-30-1. ALODINED AND PRIMED PER
- [SDR DHL200070905C](https://openairdocs.org/sdr/DHL200070905C.md): Cover · broken · Jul 15, 2000 · N709DH · Boeing 72782C · Leading Edge Devices
  > RT WING NR 7 L/E SLAT ACTUATOR COVER BROKEN AND MISSING BOLT. REPLACED ANGLES SUPPORTS FROM ACTUATOR COVER PANEL PER SRM 51-40-4 FOR FWD ANGLE AND 51-40-3 FOR AFT ANGLE. INSTALLED WITH NEW FASTENERS PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-30-2.
- [SDR DHL200070936D](https://openairdocs.org/sdr/DHL200070936D.md): Stringer · cracked · Jul 13, 2000 · N709DH · Boeing 72782C · Fuselage Main, Longeron/Stringer
  > RT W/W STR 18A HAS CRACK AT BS 940 SEEN FROM TOP OF WING. REMOVED FASTENERS FOR ACCESS PER SRM 51-30-2. REPAIRED PER DWG DHL MIA 60-00022H. HFEC INSPECTED AREA PER NDT MAN 51-00-00. CRACK RUNS INTO RADIOUS. STOP DRILLED CRACK PER SRM 51-10-1. HFEC INSPEC
- [SDR DHL200070935D](https://openairdocs.org/sdr/DHL200070935D.md): Fitting · corroded · Jul 13, 2000 · N709DH · Boeing 72782C · Main Landing Gear Attach Section
  > RT MAIN LANDING GEAR FWD TRUNNION ATTACH FITTING IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-2. REMOVED RT MLG FWD TRUNNION AS PER SRM 51-30-2. INSTALLED NEW TRUNNION PER SRM 53-10-2 AND 51-30-2. SEALED FASTENERS INSIDE FUEL TANK
- [SDR DHL200070928C](https://openairdocs.org/sdr/DHL200070928C.md): Stringer · corroded · Jul 11, 2000 · N709DH · Boeing 72782C · Fuselage Main, Longeron/Stringer
  > STRINGER 26R BETWEEN BS 360 AND 380 CORODED. REMOVED TIE FITTING PER SRM 51-30-2. REMOVED DAMAGED SECTION AND INSTALLED STRINGER REPAIRS AT STR 26R BETWEEN BS 360 AND 380 PER SRM 53-10-3. REINSTALLED TIE FITTING PER SRM 51-10-1.
- [SDR DHL200070919C](https://openairdocs.org/sdr/DHL200070919C.md): Housing · cracked · Jul 11, 2000 · N709DH · Boeing 72782C · Vertical Stabilizer
  > VERT STAB RT SIDE DUCT HOUSING STA 1307 APPROX HAS SEVERAL CRACKS (DUCT MATES TO VERT STAB FRONT SPAR). CUT OUT DAMAGED AREA PER SRM 51-40-2. INSTALLED EXTERNAL DOUBLER REPAIR PER SRM 55-30-3. ALODINED AND PRIMED PER SRM 51-10-2.
- [SDR DHL200070933C](https://openairdocs.org/sdr/DHL200070933C.md): Panel · failed · Jul 10, 2000 · N709DH · Boeing 72782C · Fuselage Main, Plate/Skin
  > LOWER FUS FAIRING PANEL AROUND FWD CARGO AIR OUTFLOW VALVE, FS 685 - 700, RBL 10L - 10R, PANEL HAS MANY CORROSION HOLES. REMOVED LOWER FUSELAGE FAIRING PANEL FOR COMPOSIT REPAIR PER SRM 51-30-2. INSTALLED COMPOSIT REPAIR TO FAIRING PER SRM 51-40-6. INSTALLE
- [SDR DHL200070932C](https://openairdocs.org/sdr/DHL200070932C.md): Floorbeam · corroded · Jul 10, 2000 · N709DH · Boeing 72782C · Fuselage Main, Floor Beam
  > CORROSION ON AFT SIDE OF FLOORBEAM AT STA 1130. REMOVED SUB FLOOR AT RT SIDE FROM STA 1130 TO 1160 RBL 25 TO RBL 62 AS PER SRM 51-30-2. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-6. SANDED OUT LOOSE PAINT AND CLEANED RT AFT LAV AREA FLOOR
- [SDR DHL200070931C](https://openairdocs.org/sdr/DHL200070931C.md): Floorbeam · corroded · Jul 10, 2000 · N709DH · Boeing 72782C · Fuselage Main, Floor Beam
  > FWD RT CORNER OF FLOORBEAM AT STA 1130 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-6. TREATED AND PRIMED AREA PER SRM 51-6-2. FABRICATED ANGLE REPAIR PER SRM 51-10-6. INSTALLED REPAIR PER AVITAS EO AVHM-140RO-1.
- [SDR DHL200070926C](https://openairdocs.org/sdr/DHL200070926C.md): Frame · corroded · Jul 10, 2000 · N709DH · Boeing 72782C · Fuselage Main, Frame
  > CIRCUMFERENTIAL FRAME FWD WEB CORRODED AT STA 380 BETWEEN STRINGERS 27R AND 28R. CUT OUT DAMAGED AREA PER SRM 53-10-1. DID HFEC INSPECTION PER NDT M/M 51-00-00. FABRICATED AND INSTALLED ANGLE PER SRM 51-40-04. ALODINED AND PRIMED PER SRM 51-10-2.
- [SDR DHL200070913C](https://openairdocs.org/sdr/DHL200070913C.md): Floor Support · bent · Jul 10, 2000 · N709DH · Boeing 72782C · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE IS BENT AND CRACKED ON LOWER AFT CARGO COMPT STR 27R BS 1148 - 1166. REMOVED REAR SUPPORT DAMAGED ANGLE PER SRM 51-30-2. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-40-3. ALODINED AND PRIMED AREA PER SRM 51-10-2.
- [SDR DHL200070911C](https://openairdocs.org/sdr/DHL200070911C.md): Angle · corroded · Jul 10, 2000 · N709DH · Boeing 72782C · Fuselage Miscellaneous Structure
  > CIRCUMFERENTIAL FRAME REINFORCING ANGLE CORRODED AT STA 380 BETWEEN STRINGERS 27R AND 28R. CUT OUT DAMAGED AREA PER SRM 53-10-1. HFEC INSPECTED CUTOUT PER NDT M/M 51-00-00. NO CRACKS IND. INSTALLED ANGLE REPAIR PER SRM 51-40-04. TREATED AND PRIMED PER SRM
- [SDR DHL200070908C](https://openairdocs.org/sdr/DHL200070908C.md): Support Bracket · cracked · Jul 10, 2000 · N709DH · Boeing 72782C · Trailing Edge Flaps
  > NR 5 FLAP TRACK O/B AFT SUPPORT BRACKET CRACKED. REPLACED CRACKED BRACKET PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-30-2.
- [SDR DHL200070907C](https://openairdocs.org/sdr/DHL200070907C.md): Fairing · cracked · Jul 10, 2000 · N709DH · Boeing 72782C · Aerodynamic Fairings
  > NR 4 FLAP TRACK CANOE FAIRING, FWD L/E OF SKIN HAS CRACK IN EXISTING REPAIR. REMOVED AND REPLACED EXISTING REPAIR PER SRM 51-30-2.

Next page: https://openairdocs.org/model/boeing-727-82c/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = '72782C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-82c/reports

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