# Service difficulty reports: Boeing 727-29

A list on [Boeing 727-29](https://openairdocs.org/model/boeing-727-29.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 229 reports

- [SDR DHL2002712001](https://openairdocs.org/sdr/DHL2002712001.md): Battery · discharged · Jan 9, 2002 · N712DH · Boeing 72729 · Emergency Lighting
  > EMERGENCY EXIT LIGHT IN COCKPIT INOP. REMOVED AND REPLACED LT ASSY BATTERIES. OPS CHECK GOOD IAW MM 33-50-111.
- [SDR DHL2001712022](https://openairdocs.org/sdr/DHL2001712022.md): Connector · loose · Nov 9, 2001 · N712DH · Boeing 72729 · Smoke Detection
  > NR 1 SMOKE DETECTOR WON'T TEST. RESECURED LOOSE CONNECTOR ON NR 1 SMOKE DETECTOR. SYSTEM TESTS GOOD IAW B727 MM 26-17-000.
- [SDR DHL2001712021](https://openairdocs.org/sdr/DHL2001712021.md): Motor · failed · Oct 24, 2001 · N712DH · Boeing 72729 · Windshield/Door Rain/Ice Removal
  > CAPTAIN'S WIPER DOES NOT WORK ON ANY SPEED. REPLACED CAPTS (LT) WIPER MOTOR ASSY, OPS CHECK NORMAL PER M/M 30-42-01.
- [SDR DHL2001712020](https://openairdocs.org/sdr/DHL2001712020.md): Bracket · missing · Oct 24, 2001 · N712DH · Boeing 72729 · Fire Detection
  > THE NR 3 DETECTOR CIRCUIT GROUND LIGHT CAME ON AT FLT LEVEL 330 AND WOULD NOT GO OUT. FOUND TWO BRACKETS MISSING. INSTALLED BRACKETS AND RESECURED FIRE LOOP, OPS CHECKS SERVICEABLE PER B727 M/M REF 26-11-01.
- [SDR DHL2001712019](https://openairdocs.org/sdr/DHL2001712019.md): Fire Loop · out of position · Oct 23, 2001 · N712DH · Boeing 72729 · Fire Detection
  > NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED AFTER TAKEOFF. NR 3 FIRE LOOP REPOSITIONED AWAY FROM COWL. GROUND FAULT LIGHTS. OPS OK PER BMM 26-11-00.
- [SDR DHL2001712018](https://openairdocs.org/sdr/DHL2001712018.md): Clamp · loose · Oct 23, 2001 · N712DH · Boeing 72729 · Detection System
  > NR 3 CIRCUIT DETECTOR GROUND LIGHT ILLUMINATED IN FLIGHT. FOUND LOOSE GROUND CLAMP. RESECURED LOOSE CLAMP IAW B-M/M 26-14-000, OPS CHECK GOOD.
- [SDR DHL2001712017](https://openairdocs.org/sdr/DHL2001712017.md): Grommet · defective · Oct 20, 2001 · N712DH · Boeing 72729 · Fire Detection
  > NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED ON S/O PANEL AUXILIARY. REMOVED NR 3 FIRE LOOP CLAMP GROMMETS IAW B727 MM 26-11-00. OPERATIONAL CHECK SERVICEABLE.
- [SDR DHL2001712016](https://openairdocs.org/sdr/DHL2001712016.md): Fire Loop · broken · Oct 13, 2001 · N712DH · Boeing 72729 · Fire Detection
  > NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED INFLIGHT. NR 3 ENGINE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED DURING CLIMBOUT FROM MCI. IN CRUISE, LIGHT DIMMED BUT REMAINED ON. OPENED NR 3 ENGINE CHECKED ROUTING OF SENSOR LOOP SECURE CLAMP AND REPOSIT
- [SDR DHL2001712015](https://openairdocs.org/sdr/DHL2001712015.md): Wire · broken · Sep 28, 2001 · N712DH · Boeing 72729 · Flight Control System Wiring
  > ON WALK AROUND FOUND LT AILERON BUSS CABLE BROKEN, LT MLG W/W.R&R LT AILERON BUSS CABLE (CORRODED)R&R RT AILERON BUSS CABLE AS PRECUTION.
- [SDR DHL2001712014](https://openairdocs.org/sdr/DHL2001712014.md): Fire Loop · out of position · Sep 15, 2001 · N712DH · Boeing 72729 · Fire Detection
  > NR 3 ENGINE FIRE DETECTOR CIRCUIT ARMED LIGHT ILLUMINATED FROM INITIAL CLIMB TO TOP OF DESCENT. OPEN COWLING FOUND FIRE LOOP DETECTOR LINE RUBBING COWLING. RE-ROUTED IAW B727 MM 26-11-000.
- [SDR DHL2001712013](https://openairdocs.org/sdr/DHL2001712013.md): Fire Loop · out of position · Sep 12, 2001 · N712DH · Boeing 72729 · Fire Detection
  > NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED NR 1 ENG REQ OIL SVS. TRANSFERRED TO DMI 7080 MEL REF 26-7 CAT-C PLACARD INSTALLED SERVICED NR 1 ENG OIL IAW B727 MM 12-13-01. INSPECTED AND REPOSITIONED NR 3 ENG FIRE LOOP AND TESTED IAW 727MM 26-11GROUND CHECK
- [SDR DHL2001712012](https://openairdocs.org/sdr/DHL2001712012.md): Spoiler · damaged · Sep 5, 2001 · N712DH · Boeing 72729 · Spoilers
  > NR 4 J-SCREW GEARBOX REQ CLEAN AND LEAK CK NR 10 SPOILER CRACK AT ACTUATION ROD ATTACH POINT. THRU BOLT EXCESSIVELY LOOSE 4" 6" DELAMINATION LOCATED UPPER SURFACE NR 4 SPOILER OUTBD FWD EDGE NR 2 SPOILER ACT HAS HYD FLUID ON BOTTOM NR 6 SPOILER CENTER HINGE P
- [SDR DHL2001712011](https://openairdocs.org/sdr/DHL2001712011.md): Battery · discharged · Sep 4, 2001 · N712DH · Boeing 72729 · Emergency Lighting
  > DURING STANDBY POWER CHECK EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERIES PER B727 MM 24-54-0. OPS CHECK GOOD.
- [SDR DHL2001712010](https://openairdocs.org/sdr/DHL2001712010.md): Switch · defective · Aug 28, 2001 · N712DH · Boeing 72729 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ARMING SWITCH DOES NOT OPERATE PROPERLY. REMOVED AND REPLACED SWITCH GUARD. OPS CHECKED GOOD.
- [SDR DHL2001712009](https://openairdocs.org/sdr/DHL2001712009.md): Switch · lack of lube · Aug 18, 2001 · N712DH · Boeing 72729 · Emergency Lighting
  > EMERGENCY EXIT ARMING SWITCH-GUARD DOES NOT MOVE SWITCH FROM ON TO ARMED WHEN GUARD IS CLOSED. LUBED SWITCH, OPS CHECKED GOOD IAW 727 MM 20-60-02.
- [SDR DHL2001712008](https://openairdocs.org/sdr/DHL2001712008.md): Fuel Control · Jul 10, 2001 · N712DH · Boeing 72729 · Power Lever
  > AT TOP IF DESENT #1 ENGINE WOULD NOT RESPOND TO THRUST LEVER MOVEMENTS, STAYED AT MIN OF 75% N1, PRECAUTIONARY ENG SHUTDOWN ACCOMPLISHED WITH UNEVENTFUL LANDING#1 ENG FUEL CONTROL R&R SEE ITEM 7M LOG PG. 224983.STATUS: CLOSED
- [SDR DHL2001712007](https://openairdocs.org/sdr/DHL2001712007.md): Pointer · out of position · Jun 20, 2001 · N712DH · Boeing 72729 · Rudder Control System
  > REQUIRED WRITE UP - AIRCRAFT REQUIRED 1.5 UNITS OF RIGHT TRIM ON RUDDER DURING CLIMBOUT. CRUISE AILERON TRIM 0. FOUND POINTER ON RUDDER TRIM KNOB JUMPED TRACK. CENTERED RUDDER, REINSTALLED TRIM KNOB PER 27-20-0 ADJ/TEST CKS GOOD.
- [SDR DHL2001712006](https://openairdocs.org/sdr/DHL2001712006.md): Transmitter · leaking · May 4, 2001 · N712DH · Boeing 72729 · Landing Gear Brake System
  > WITH PACKS OPERATING AFTER ABOUT 15 MINUTES ON THE GROUND DURING PREFLIGHT, SMOKE FILLED THE COCKPIT. TURNED OFF LEFT PACK TO STOP SMOKE.FOUND BRAKE PRESSURE XMITR IN RT MLG WHEEL WELL LEAKING. REPLACED DAMAGED O-RING SEAL. LEAKAGE FROM XMTR LEAKING ON APU DU
- [SDR DHL2001712005](https://openairdocs.org/sdr/DHL2001712005.md): Downlock Switch · out of position · Apr 29, 2001 · N712DH · Boeing 72729 · Landing Gear Position and Warning
  > DURING GEAR EXTENSION, NOSE GEAR INTRANSIT LIGHT AND GEAR DOWN LIGHT DID NOT ILLUMINATE. RAN ABNORMAL PROCEDURE 6.2 67 LIGHT STAYED OUT. VERIFIED NOSE GEAR DOWN THRU VIEWING PORT. AFTER GEAR WAS VERIFIED DOWN AND LOCKED, WHEN POWER WAS REDUCED, GEAR WARNING
- [SDR DHL2001712003](https://openairdocs.org/sdr/DHL2001712003.md): Igniter Box · failed · Mar 16, 2001 · N712DH · Boeing 72729 · Spark Plug/Igniter
  > DURING START ATTEMPT NR 1 ENGINE DID NOT OBTAIN LIGHT-OFF. RESET IGNITION C/B''S PER THE ABNORMAL PROCEDURE. ATTEMPTED A SECOND START AND STILL DID NOT OBTAIN LIGHT-OFF. REMOVED AND REPLACED IGNITOR BOX, OPS CHECKS GOOD IAW B727 MM 74-31-00 ENGINE RUN (CREW
- [SDR DHL2001712517](https://openairdocs.org/sdr/DHL2001712517.md): Fitting · cracked · Feb 15, 2001 · N712DH · Boeing 72729 · Spoilers
  > C-CHECK, LEFT WING T/E NR 4 SPOILER HOUSING FITTING WS 436.5 CRACKED 1.0 INCH. REMOVED FITTING CRACK IAW SRM 51-30-2, PAGE 1-2. PERFORMED ANTI-CORROSION TREATMENT AND PRIMED IAW SRM 51-10-2, PAGE 1 AND 2. INSTALLED NEW FITTING IAW SRM 51-30-2, PAGE 1 AND 2.
- [SDR DHL2001712516](https://openairdocs.org/sdr/DHL2001712516.md): Structure · cracked · Feb 15, 2001 · N712DH · Boeing 72729 · Spoilers
  > C-CHECK - RT WING NR 14 SPOILER LWR PART CRACKED 2.0 INCHES. CLEANED AND REPAIRED RT WING NR 14 SPOILER LOWER PART WITH POLYESTER RESIN AND CATALYST IAW SRM 51-20-3, FIG 2. (NON-ROUTINE CARD NR 1412).
- [SDR DHL2001712522](https://openairdocs.org/sdr/DHL2001712522.md): Fitting · cracked · Feb 13, 2001 · N712DH · Boeing 72729 · Auxiliary Gear (Tail Skid)
  > C-CHECK - AFT FUSELAGE LUG OF LOWER FITTING FROM TAIL SKID DRAG LINK DOOR CRACKED 3 INCHES. REMOVED DAMAGED FITTING, CLEANED, TREATED, AND PRIMED AREA AND INSTALLED NEW FITTING IAW SRM 51-30-2, PAGE 13; SRM 51-10-2 PAGE 1, 2. (NON-ROUTINE CARD 1498)
- [SDR DHL2001712520](https://openairdocs.org/sdr/DHL2001712520.md): Pressure Panel · cracked · Feb 9, 2001 · N712DH · Boeing 72729 · Fuselage Main, Bulkhead
  > C-CHECK, MLG WHEEL WELL TOP SURFACE SHOWS 6 CRACKS OF.75 INCH BETWEEN LBL 25 AND LBL 40, STA 900.000 AND STA 910.000. REMOVED FLOOR PANELS, BRACKETS, CLIPS, STRAPS IAW DWG 65-89360-3. PERFORMED STOP DRILL IAW DWG 65-89360. FABRICATED DOUBLER (ALCLAD 2024,
- [SDR DHL2001712521](https://openairdocs.org/sdr/DHL2001712521.md): Pressure Panel · cracked · Feb 8, 2001 · N712DH · Boeing 72729 · Fuselage Main, Bulkhead
  > C-CHECK, MAIN CARGO MLG WHEEL WELL TOP SURFACE SHOWS 4 CRACKS OF.5 INCH BETWEEN RBL 17 AND RBL 25, STA 910 AND STA 920. REMOVED FLOOR PANELS, BRACKETS, CLIPS, STRAPS DWG 65-89360-3. PERFORMED STOP DRILL IAW DWG 65-89360-3. FABRICATED DOUBLER (ALCLAD 2024,
- [SDR DHL2001712505](https://openairdocs.org/sdr/DHL2001712505.md): Seal · cracked · Feb 7, 2001 · N712DH · Boeing 72729 · Passenger/Crew Doors
  > C-CHECK - BASE OF LWR HINGE SEAL FROM FWD ENTRY DOOR CRACKED 1.0 INCH. REMOVED HINGE SEAL BASE IAW SRM 51-30-2, PAGE 13. PERFORMED STOP DRILL IAW SRM 51-40, PAGE 1. FABRICATED DOUBLER (ALCAD 2024, T3, 0.032 INCH IAW SRM 51-40, PAGE 1. CLEANED, TREATED, AND
- [SDR DHL2001712501](https://openairdocs.org/sdr/DHL2001712501.md): Skin · cracked · Feb 7, 2001 · N712DH · Boeing 72729 · Fuselage Main, Plate/Skin
  > SKIN EXTERIOR HAS 0.250 INCH CRACK AT STA 1102, STR 4L. CUT AFFECTED AREA IAW SRM 53-30-3, PAGE 24. FABRICATED FILLER WITH ALCLAD 2024 T3 0.040 INCH, SRM 53-30-3, PAGE 24. FABRICATED DOUBLER WITH ALCLAD 2024 T3 0.063 INCH IAW SRM 53-30-3 PAGE 24. TREATED A
- [SDR DHL2001712508](https://openairdocs.org/sdr/DHL2001712508.md): Angle · cracked · Feb 6, 2001 · N712DH · Boeing 72729 · Wing Miscellaneous Structure
  > C-CHECK - RT WING WINGLET FAIRING LWR PART SUPPORT ANGLES CRACKED 1.0 INCH. REMOVED SUPPORT ANGLES IAW SRM 51-30-2, PAGE 13. FABRICATED ANGLES (SUPPORT ANGLE) NEW WITH ALCLAD 2024, T3, 0.05 INCH IAW SRM 57-20-3, PAGE 1-3. TREATED AND PRIMED IAW SRM 51-10-2,
- [SDR DHL2001712506](https://openairdocs.org/sdr/DHL2001712506.md): Door Frame · damaged · Feb 6, 2001 · N712DH · Boeing 72729 · Fuselage Main, Structure
  > C-CHECK - MAIN CARGO DOOR JAMB CORNER DENTED AND BROKEN 1 INCH LWR PART STA 620.000. REMOVED CORNER IAW SRM 51-30-2, PAGE 1 AND 2. FABRICATED SUPPORT ANGLE WITH ALCLAD 2024, T3, 0.063 INCH IAW SRM 52-30-00, PAGE 4. FABRICATED CORNER COVER WITH ALCLAD 2024,
- [SDR DHL2001712509](https://openairdocs.org/sdr/DHL2001712509.md): Angle · cracked · Feb 5, 2001 · N712DH · Boeing 72729 · Fuselage Miscellaneous Structure
  > C-CHECK, MAIN CARGO COMPART CABLES PLACARD PROTECTIVE ANGLE CRACKED 0.50 INCH AT RBL 20 INCH BETWEEN STA 930.000 AND STA 940.000. PERFORMED STOP DRILL IAW SRM 51-10-1, PAGE 6B. FABRICATED DOUBLER (2024, T3, 0.032 INCH) IAW SRM 51-40, PAGE 1. CLEANED, TREATE
- [SDR DHL2001712515](https://openairdocs.org/sdr/DHL2001712515.md): Fitting · cracked · Feb 5, 2001 · N712DH · Boeing 72729 · Fuselage, Landing Gear Attach Fittings
  > C-CHECK - RT MLG FITTING TO ANGLE SPLICE CRACKED 1.0 INCH BS 945.000 TO BS 950.000, 5-18 RT. REMOVED CRACKED ANGLE IAW SRM 51-30-2, PAGE 66. FABRICATED TWO ANGLES WITH ALCLAD 2024, T3, 0.090 AND ALCLAD 2024, T3, 0.040 IAW SRM 53-40-1, PAGE 1-2. TREATED AND
- [SDR DHL2001712519](https://openairdocs.org/sdr/DHL2001712519.md): Structure · cracked · Feb 3, 2001 · N712DH · Boeing 72729 · Ailerons
  > C-CHECK, LT WING TRIM TAB L/E PART FROM EXTERNAL AILERON SHOWS CRACK.25 INCH. REMOVED LEADING EDGE FROM TRIM TAB IAW SRM 51-10-2, PAGE 1 AND 2. FABRICATED NEW LEADING EDGE WITH ALCLAD 2024, T3, 0.020 INCH IAW SRM 57-20-03, FIG 2. TREATED AND PRIMED IAW SRM
- [SDR DHL2001712518](https://openairdocs.org/sdr/DHL2001712518.md): Fitting · cracked · Feb 3, 2001 · N712DH · Boeing 72729 · Fuselage Miscellaneous Structure
  > C-CHECK, AFT CARGO COMPARTMENT NR 2 DOOR STOP CRACKED 1.0 INCH AT STA 1058.000 STR 23 RT. REMOVED SKIN TO GAIN ACCESS IAW SRM 51-30-2 PAGE 1 AND 2. REMOVED FITTING (STOP) CRACKED IAW SRM 51-30-2 PAGE 1 AND 2. REINSTALLED SKIN IAW SRM 51-30-2 PAGE 1 AND 2.
- [SDR DHL2001712512](https://openairdocs.org/sdr/DHL2001712512.md): Structure · damaged · Feb 3, 2001 · N712DH · Boeing 72729 · Engine Cowling System
  > C-CHECK - NR 1 ENGINE LWR COWLING 2/B DOUBLER BROKEN 2.0 INCHES (INTERIOR) AT STA 136.0. REMOVED DOUBLER IAW SRM 51-30-2, PAGE 1 AND 2. FABRICATED DOUBLER WITH ALCLAD 2024, T3, 0.050 INCHES IAW SRM 54-10-3, FIG 2. CLEANED, TREATED, AND PRIMED IAW SRM 51-10-
- [SDR DHL2001712513](https://openairdocs.org/sdr/DHL2001712513.md): Fairing · cracked · Feb 3, 2001 · N712DH · Boeing 72729 · Engine Thrust Reverser
  > C-CHECK - NR 3 ENGINE THRUST REVERSER FWD FAIRING 1.0 INCH CRACK AT 3 O CLOCK. PERFORMED STOP DRILL IAW SRM 51-10-1, PAGE 6B. INSPECTED DOUBLER WITH ALCLAD 2024, T3, 0.032 INCH IAW SRM 51-40, PAGE 1. TREATED AND PRIMED IAW SRM 51-10-2, PAGE 1 AND 2. INSTAL
- [SDR DHL2001712514](https://openairdocs.org/sdr/DHL2001712514.md): Fairing · cracked · Feb 2, 2001 · N712DH · Boeing 72729 · Engine Thrust Reverser
  > C-CHECK - NR 3 ENGINE RT REVERSE CASE FAIRING CRACKED 0.50 INCH AT STA 210, 9 O CLOCK POSITION. WELDED NR 3 ENGINE RT REVERSE CASE FAIRING WITH ALUMINIUM AGS WELDING.0625 INCH WITH TIG IAW OVERHAUL MANUAL 72-21-1, PAGE 402. (NON-ROUTINE CARD NR 1519).
- [SDR DHL2001712511](https://openairdocs.org/sdr/DHL2001712511.md): Bulkhead · cracked · Feb 2, 2001 · N712DH · Boeing 72729 · Fuselage Main, Bulkhead
  > C-CHECK- AFT BAGGAGE RT AFT BULKHEAD PANEL CRACKED 2.0 INCHES AT STA 1166.0. CLEANED AND REPAIRED AFT BAGGAGE RT AFT BULKHEAD PANEL AT STA 1166.0 WITH FIBER GLASS CLOTH AND RESIN POLYSTER IAW SRM 51-20-03, FIG 2. (NON-ROUTINE CARD 0995).
- [SDR DHL2001712507](https://openairdocs.org/sdr/DHL2001712507.md): Skin · cracked · Feb 2, 2001 · N712DH · Boeing 72729 · Nacelle/Pylon, Plate/Skin
  > C-CHECK - NR 3 ENG UPPER COWLING SKIN, 0.125 INCH CRACKS. PERFORMED STOP DRILL IAW SRM 51-10-1, PAGE 6B. FABRICATED DOUBLER WITH ALCLAD 2024, T3, 0.050 INCH IAW SRM 54-10-3, FIG 5. INSTALLED DOUBLER IAW SRM 54-10-3, FIG 5. (NON-ROUTINE CARD 1177).
- [SDR DHL2001712502](https://openairdocs.org/sdr/DHL2001712502.md): Skin · cracked · Feb 2, 2001 · N712DH · Boeing 72729 · Leading Edge Devices
  > C-CHECK, FORE FLAP CRACKED 2.0 INCH AT WBL 440. PERFORMED STOP DRILL IAW SRM 57-50-4, FIG 1. FABRICATED DOUBLER (ALCLAD 2024, T3, 0.050 INCH) IAW 57-50-4, FIG 1. CLEANED, TREATED AND PRIMED IAW 51-10-2, PAGE 1 AND 2. INSTALLED DOUBLER IAW SRM 57-50-4, FIG
- [SDR DHL2001712510](https://openairdocs.org/sdr/DHL2001712510.md): Support Bracket · broken · Feb 1, 2001 · N712DH · Boeing 72729 · Wing Miscellaneous Structure
  > C-CHECK, NR 4 GROUND SPOILER AFT ACTUATOR HYDRAULIC TUBING ATTACH SUPPORT BROKEN. REMOVED BROKEN SUPPORT IAW SRM 51-30-2, PAGE 1-2. FABRICATED SUPPORT T-ANGLE (EXTRUDED 7075, T6) IAW SRM 51-20-2, FIG 6. CLEANED, TREATED, AND PRIMED IAW SRM 51-10-2, PAGE 1-2
- [SDR DHL2001712503](https://openairdocs.org/sdr/DHL2001712503.md): Intercostal · broken · Feb 1, 2001 · N712DH · Boeing 72729 · Fuselage Miscellaneous Structure
  > C-CHECK, FWD CARGO COMPARTMENT BEAM LOWER PART INTERCOSTAL BROKEN 1.0 INCH (CEILING) AT STA 540.000 LBL 43.0 INCH. PERFORMED STOP DRILL HOLE IAW SRM 51-10-1, PAGE 6. FABRICATED DOUBLER WITH ALCLAD 2024, T3, 0.032 INCH, 5 X 3 INCH IAW SRM 51-40, PAGE 1. TREA
- [SDR DHL2001712504](https://openairdocs.org/sdr/DHL2001712504.md): Door Frame · cracked · Feb 1, 2001 · N712DH · Boeing 72729 · Fuselage Main, Structure
  > C-CHECK - MAIN CARGO DOOR CORNER JAMB, LWR PART DENTED AND BROKEN 1.0 INCH AT STA 480. READIED LWR CORNER COVER IAW SRD 51-30-2 PAGE 1 AND 2. FABRICATED COVER SUPPORT ANGLE WITH ALCAD 2024, T3, 0.063 INCH IAW SRM 52-20-2, FIG 1. FABRICATED COVER CORNER WITH
- [SDR DHL2001712500](https://openairdocs.org/sdr/DHL2001712500.md): Frame · corroded · Feb 1, 2001 · N712DH · Boeing 72729 · Fuselage Main, Frame
  > C-CHECK - COMPARTMENT FRAME SHOWS CORROSION AT STA 110.000, STR 26 LT. CUT OUT DAMAGED AREA AT STA 110.000 STR 26L, AND FABRICATED FILLER AND CHANNEL (ALCLAD 707S.T6.0.063 INCH) IAW SRM 53-10-4 PAGE 3. CLEANED, TREATED AND PRIMED IAW SRM 51-10-2 PAGE 1 & 2.
- [SDR DHL200171208C](https://openairdocs.org/sdr/DHL200171208C.md): Angle · cracked · Jan 30, 2001 · N712DH · Boeing 72729 · Aerodynamic Fairings
  > AT C-CK; RT WING FAIRING SUPPORT ANGLE CRACKED.5 INCH AT STA 330.000. PERFORMED STOP DRILL IAW SRM 51-10-1, PG 6B, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-10-2, PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-40, PG 1-2.
- [SDR DHL200171207C](https://openairdocs.org/sdr/DHL200171207C.md): Intercostal · cracked · Jan 30, 2001 · N712DH · Boeing 72729 · Fuselage Miscellaneous Structure
  > AT C-CK; FWD CARGO COMPT BEAM LOWER PART INTERCOSTAL CRACKED 2 INCHES (CEILING) AT STA 720.000 LBL 46. PERFORMED STOP DRILL IAW SRM 51-10-1 PG 6B, CLEANED TREATED AND PRIMED IAW SRM 51-10-2 PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-40 PG 1.
- [SDR DHL200171206C](https://openairdocs.org/sdr/DHL200171206C.md): Intercostal · cracked · Jan 30, 2001 · N712DH · Boeing 72729 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE BIN INTERCOSTAL CRACKED 1 INCH STA 640.000 UPPER PART LT BETWEEN STR 18 AND 19 LT. STOP DRILLED PER SRM 51-10-1, FABRICATED DOUBLER PER SRM 51-40 PG 1, CLEANED, TREATED AND PRIMED PER SRM 51-10-2. INSTALLED DOUBLER PER SRM 51-40 PG 1.
- [SDR DHL200171205C](https://openairdocs.org/sdr/DHL200171205C.md): Frame · cracked · Jan 30, 2001 · N712DH · Boeing 72729 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT FRAME CRACKED 1.5 INCH BETWEEN S25 AND S26 LT STA 680.000. STOP DRILLED PER SRM 51-10-1, FABRICATED DOUBLER PER SRM 53-10-4, CLEANED, TREATED AND PRIMED PER SRM 51-10-2, INSTALLED DOUBLER PER SRM 53-10-4.
- [SDR DHL200171204C](https://openairdocs.org/sdr/DHL200171204C.md): Floor Support · cracked · Jan 30, 2001 · N712DH · Boeing 72729 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE FLOOR SUPPORT ANGLE CRACKED BETWEEN STRINGER 26 TO 27 RT STA 670.000 RT SIDE. STOP DRILLED PER SRM 51-10-1. FABRICATED DOUBLER PER SRM 51-40 PG 1. CLEANED, TREATED AND PRIMED PER SRM 51-10-2, INSTALLED DOUBLER PER SRM 51-40 PG 1.
- [SDR DHL200171203C](https://openairdocs.org/sdr/DHL200171203C.md): Floor Support · broken · Jan 30, 2001 · N712DH · Boeing 72729 · Fuselage Miscellaneous Structure
  > MAIN CARGO FLOOR SUPPORT ANGLE BROKEN.25 INCH AND CRACKED.25 INCH AT STA 760.95. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED DOUBLER PER SRM 51-40 PG 1. CLEANED, TREATED AND PRIMED PER SRM 51-10-2, INSTALLED DOUBLER PER SRM 51-40 PG 1.
- [SDR DHL200171202C](https://openairdocs.org/sdr/DHL200171202C.md): Floor Support · deformed · Jan 30, 2001 · N712DH · Boeing 72729 · Fuselage Miscellaneous Structure
  > MAIN CARGO FLOOR SUPPORT ANGLE DEFORMED AT TRACK 2 AND 3. REMOVED FLOOR SUPPORT ANGLE PER SRM 51-30-2. FABRICATED NEW SUPPORT ANGLE PER SRM 53-10-5. CLEANED, TREATED AND PRIMED PER SRM 51-10-2. INSTALLED NEW ANGLE PER SRM 51-30-2.

Next page: https://openairdocs.org/model/boeing-727-29/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 = '72729'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-29/reports

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