# N706DH: Boeing 727-22C, registration cancelled 2000-09-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 21, 2000 - Exported to: São Tomé and Príncipe - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-22C](https://openairdocs.org/model/boeing-727-22c) (registry code 138400F) - Serial number: 19192 - Type of aircraft: Fixed wing multi engine - Certificate issued: April 13, 1987 - Last registry action: April 20, 1999 - Mode S code: A96B2B - Owner when cancelled: [Dhl Airways Inc](https://openairdocs.org/faa-owner/DHL%20AIRWAYS%20INC) - Location: [Redwood City, CA](https://openairdocs.org/faa-place/CA/Redwood%20City) - Owner type: Corporation - Owner's area on the map: 37.5334° N, 122.2496° W: Placed by OpenAirDocs at the center of ZIP code 94065, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N706DH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=706DH - Page: https://openairdocs.org/deregistered/N706DH-2000-09-21 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 727-22C: https://openairdocs.org/model/boeing-727-22c.md ## Service difficulty reports (66, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DHL2000706005](https://openairdocs.org/sdr/DHL2000706005), Jun 22, 2000: INTERCOSTAL. CRACKED. FWD RT LAV FLOOR FRAME INTERCOSTAL HAS 2 LARGE CRACKS EMINATING FROM TOP, LOCATED I/B OF DUMP SHUTE BS 303.9, RBL 43. REMOVED WEB FOR REPLACMENT PER SRM 57-30-2 - [SDR DHL2000706006](https://openairdocs.org/sdr/DHL2000706006), Jun 21, 2000: ANGLE. BROKEN. AFT CARGO COMPT APPROX BS 950 AFT AREA, WL 195.0 & BBL 0.0 ANTI ICE DUCT HAS ANGLE SUPPORT BROKEN AT LOWER SECTION. REMOVED AND INSTALLED NEW ATTACH ANGLE SUPPO - [SDR DHL2000706004](https://openairdocs.org/sdr/DHL2000706004), Jun 21, 2000: THRESHOLD. CORRODED. FWD RT LAV FLOOR AT THRESHOLD HAS CORROSION ABOVE AND BELOW FLOOR BS 328, RBL 14. REMOVED THRESHOLD PER SRM 51-30-2. FABRICATED NEW THRESHOLD PER SRM 53-10-1. I - [SDR DHL2000706003](https://openairdocs.org/sdr/DHL2000706003), Jun 21, 2000: ATTACH ANGLE. CRACKED. FWD ENTRY DOOR PANEL (INTERIOR) AFT SUPPORT ATTCH ANGLE CRACKED SEVERAL PLACES. REMOVED AND REPLACED ANGLES PER SRM 51-30-2. TREATED AND PRIMED SUPPORT ANGLES P - [SDR DHL2000706002](https://openairdocs.org/sdr/DHL2000706002), Jun 21, 2000: FLOORBOARD. DAMAGED. FLOOR PANEL DAMAGED AT FWD LEFT CORNER AT BS 360 PANEL FROM RBL 24.0 TO 48.0. REMOVED FLOORBOARD, FABRICATED DOUBLERS PER SRM 53-20-1. ALODINED AND PRIMED PER S - [SDR DHL2000706001](https://openairdocs.org/sdr/DHL2000706001), May 27, 2000: FLUID. LEAKING. AFTER T/O, TOWER AND ANOTHER A/C REPORTED A SIGNIFICANT AMOUNT OF FLUID LEAKING FROM LFT WING. FUEL WAS DUMPED DOWN TO LANDING WT AND RETURNED TO SERVICE. INSPE - [SDR DHL99706001](https://openairdocs.org/sdr/DHL99706001), Nov 1, 1999: TEMP BULB. FAILED. NR 1 ENGINE OIL TEMP ROSE IN FLIGHT TO 131 REGARDLESS OF THRUST SETTING. ENGINE OIL TEMP WOULD NOT DECREASE. SHUT DOWN NR 1 ENGINE AFTER 15 MIN, TOTAL TIME TEMP - [SDR DHL98706003](https://openairdocs.org/sdr/DHL98706003), Jun 24, 1998: WHEEL. CRACKED. ON SERVICE CHECK, FOUND NR 4 WHEEL AND TIRE ASSY BROKEN LUGS HITTING BRAKE ASSY. INSPECTED, INNER WHEEL HALF CRACKED AND BROKEN. REMOVED AND REPLACED NR 4 MAIN - [SDR DHL9870646C](https://openairdocs.org/sdr/DHL9870646C), Jun 3, 1998: SEAT TRACK. CRACKED. AT C-CHECK, CABIN SEAT TRACK CRACKED AT STA 580 LBL 24. CUT OUT DAMAGED SECTION OF SEAT TRACK FROM BS 560 TO 620, INSTALLED NEW SEAT TRACK 5' LONG PER SRM 53-10 - [SDR DHL9870636C](https://openairdocs.org/sdr/DHL9870636C), May 22, 1998: RIB. CRACKED. AT C-CHECK, NR 5 SLAT I/B CLOSURE RIB IS CRACKED. REPLACED RIB PER SRM 51-30-2. N/R 2137. - [SDR DHL9870632C](https://openairdocs.org/sdr/DHL9870632C), May 21, 1998: FORGING. CRACKED. AT C-CHECK, FUSE FORGING BS 950 LT SIDE HAS 1 INCH CRACK AT SECOND ROW TOP NR 1 FASTENER. INSTALLED S/B REPAIR PER S/B 53-0126 PART VI. N/R 1701. - [SDR DHL9870635C](https://openairdocs.org/sdr/DHL9870635C), May 20, 1998: CENTER SECTION. CRACKED. AT C-CHECK, RT UPPER AT 70.5 WING CENTER SECTION HAS 2 CRACKS AT FWD LOWER HOLE. INSTALLED REPAIR AT RT WING LOWER I/B AND CENTER SECT PER S/B 57-0112. N/R 213. - [SDR DHL9870618C](https://openairdocs.org/sdr/DHL9870618C), May 20, 1998: RIB. CRACKED. AT C-CHECK, RT WING RIB AT STA 629 CRACKED AT STR 14 LOWER. STOP DRILLED CRACK, ACCOMPLISHED HFEC, INSTALLED DOUBLER PER SRM 51-30-2, 3 X 6'. N/R 2132. - [SDR DHL9870650C](https://openairdocs.org/sdr/DHL9870650C), May 19, 1998: BOB WEIGHTS. CRACKED. AT C-CHECK, RT ELEV TAB BOB WEIGHTS CRACKS AND DETERIORATED. REMOVED AND REPLACED WEIGHTS PER SRM 51-10-1 AND 51-30-2. N/R 4569. - [SDR DHL9870631C](https://openairdocs.org/sdr/DHL9870631C), May 19, 1998: CASTING. CRACKED. AT C-CHECK, NR 7 SPOILER CENTER HINGE CASTING CRACKED AT I/B LOWER END. REMOVED AND REPLACED CENTER CASTING PER 727 SRM 57-10-1. N/R 1698. - [SDR DHL9870617C](https://openairdocs.org/sdr/DHL9870617C), May 19, 1998: SKIN. CRACKED. AT C-CHECK, RIGHT WING UPPER SURFACE, HFEC REVEALED 3 CRACK INDICATIONS AT 3 FASTENER HOLES AT WING RIB UPPER CHORD AT 70.5 O/B HORIZ FLANGE. OVERSIZED HOLES, H - [SDR DHL9870611C](https://openairdocs.org/sdr/DHL9870611C), May 19, 1998: BOB WEIGHT. CRACKED. AT C-CHECK, LT ELEVATOR BOB WEIGHTS CRACKED AND DETORATED ON TAB. REMOVED AND REPLACED WEIGHTS PER SRM 51-30-2. N/R 4568. - [SDR DHL9870603C](https://openairdocs.org/sdr/DHL9870603C), May 18, 1998: COWLING. CRACKED. AT C-CHECK, NR 1 ENGINE FWD FIXED COWL AFT FRAME IS CRACKED AT LOWER END BY MOUNT BRACKET. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 4.5 X 2. N/R 6939. - [SDR DHL9870630C](https://openairdocs.org/sdr/DHL9870630C), May 17, 1998: STRINGER. CRACKED. AT C-CHECK, VENT STR S-14 CRACK LEFT WING RIB STA 686.5 UPPER. TRIMMED OUT DAMAGED AREA, INSTALLED REPAIR OF VENT PER SRM 57-10-5, L-ANGLE 14. N/R 1670. - [SDR DHL9870606C](https://openairdocs.org/sdr/DHL9870606C), May 17, 1998: STRINGER. CRACKED. AT C-CHECK, CRACKED VENT STRINGER 13 AT WS 629 LEFT WING. CUT OUT DAMAGED SECTION PER S/B 57-A159, INSTALLED ATTACH ANGLE PER S/B 57-A159, 12 LONG. N/R 1671. - [SDR DHL9870605C](https://openairdocs.org/sdr/DHL9870605C), May 17, 1998: RIB. CRACKED. AT C-CHECK, LEFT WING WS 686.5 RIB CRACK AT LOWER STR 9. STOP DRILLED CRACK, HFEC, INSTALLED DOUBLER REPAIR PER SRM 57-10-5, 9 X 4. N/R 1669. - [SDR DHL9870610C](https://openairdocs.org/sdr/DHL9870610C), May 16, 1998: STRAP. DISBONDED. AT C-CHECK, SKIN BONDED TEAR STRAP AT STA 380 STR 3L TO 1 HAS DISBONDED. CUT OUT TEAR STRAP AT STA 380 BETWEEN STR 1L TO STR 4. CLEANED INNER FUS SKIN , NO CORR - [SDR DHL9870649C](https://openairdocs.org/sdr/DHL9870649C), May 15, 1998: FLOORBEAM. CORRODED. AT C-CHECK, CORROSION ON FLOORBEAM AFT UPPER FLANGE LOWER SURFACE AT BS 560 LBL 48. CUT OUT DAMAGED SECTION AT STA 560 FROM LBL 24 TO O/B END. INSTALLED FLOORBE - [SDR DHL9870648C](https://openairdocs.org/sdr/DHL9870648C), May 15, 1998: ANGLE. CORRODED. AT C-CHECK, VERTICAL STAB LT STAINLESS STEEL RUB STRIP FOR THE HORIZ STAB RUB BLOCK IS BULGED. VERTICAL SUPPORT ANGLE CORRODED. INSTALLED NEW ANGLE PER SRM 55-3 - [SDR DHL9870647C](https://openairdocs.org/sdr/DHL9870647C), May 15, 1998: ANGLE. CORRODED. AT C-CHECK, VERT STAB RT STAINLESS STEEL RUB STRIP FOR THE HORIZ STAB RUB BLOCK IS BULGED. REMOVED STRIP AND FOUND VERT ATTACH SUPPORT ANGLE CORRODED. INSTALLED - [SDR DHL9870643C](https://openairdocs.org/sdr/DHL9870643C), May 15, 1998: FLOORBEAM. CORRODED. AT C-CHECK, CORROSION ON DOOR SILL FITTING BOTTOM SURFACE OF TOP FLANGE AT BS 560 LBL 60. CUT OUT DAMAGED SECTION OF CABIN FLOORBEAM UPPER CHORD STA 560 LBL 28, - [SDR DHL9870629C](https://openairdocs.org/sdr/DHL9870629C), May 15, 1998: RIB. CRACKED. AT C-CHECK, NR 1 SLAT INBD TRACK OUTBD RIB IS CRACKED AT FWD END. STOP DRILLED, HFEC, INSTALLED DOUBLER PER SRM 57-50-3, 1 X 4. N/R 1668. - [SDR DHL9870628C](https://openairdocs.org/sdr/DHL9870628C), May 15, 1998: RIB. CRACKED. AT C-CHECK, NR 4 SLAT INBD TRACK OUTBD RIB IS CRACKED PAST STOP DRILL. STOP DRILLED END OF CRACK, HFEC, FABRICATED RIB REPAIR PER SRM 57-50-3, 4 X 5. N/R 1667. - [SDR DHL9870627C](https://openairdocs.org/sdr/DHL9870627C), May 15, 1998: SPAR. CRACKED. AT C-CHECK, LEFT WING FRONT SPAR WS 115 LOWER END OF VERTICAL ANGLE CRACKED. STOP DRILLED END OF CRACK, HFEC, FABRICATED ANGLE REPAIR, 6 X 2 PER SRM 51-40-3. N/ - [SDR DHL9870621C](https://openairdocs.org/sdr/DHL9870621C), May 15, 1998: STOP. CRACKED. AT C-CHECK, RIGHT HAND AFT ENTRY DOOR STOP NR 7 IS CRACKED. REMOVED AND REPLACED STOP PER SRM 51-30-2. N/R 5802. - [SDR DHL9870620C](https://openairdocs.org/sdr/DHL9870620C), May 15, 1998: SKIN. CRACKED. AT C-CHECK, AFT ENTRY DOOR LEFT NR 7 DOORS TOP FITTING CUTOUT IS CRACKED. HFEC OF STOP DRILL, INSTALLED REPAIR PER S/B 53-055 AND DRAWING 65C15764. REPAIRS 22 X - [SDR DHL9870609C](https://openairdocs.org/sdr/DHL9870609C), May 15, 1998: SKIN. CRACKED. AT C-CHECK, AFT ENTRY DOOR RIGHT NR 7 DOOR STOP FITTING CUTOUT IS CRACKED. ACCOMPLISHED NDT, STOP DRILLED, INSTALLED REPAIR PER S/B 53-055 22 X 8.5 AND 13 X 7. - [SDR DHL9870604C](https://openairdocs.org/sdr/DHL9870604C), May 15, 1998: ANGLE. CRACKED. AT C-CHECK, NR 1 FLAP TRACK OUTBD COVE PANEL SUPPORT ANGLE CRACKED. REMOVED DAMAGED SUPPORT, FABRICATED AND INSTALLED ANGLE PER SRM 51-30-2. N/R 1652. - [SDR DHL9870645C](https://openairdocs.org/sdr/DHL9870645C), May 14, 1998: FRAME. CRACKED. AT C-CHECK, FWD CARGO DOOR FUS FRAME, FWD SIDE INNER SKIN HAS CRACK RUNNING FROM RIVET HOLE TO EDGE OF FRAME, JUST UNDER SECOND STOP FITTING. REMOVED DOUBLER, H - [SDR DHL9870644C](https://openairdocs.org/sdr/DHL9870644C), May 14, 1998: RIB. CRACKED. AT C-CHECK, RT UPPER RIB AT 70.5 WING CENTER SECTION HAS 2 CRACKS AT FWD LOWER HOLE. STOP DRILLED, HFEC, AND PERFORMED MODIFICATION PER S/B 57-0112. N/R 2073. - [SDR DHL9870642C](https://openairdocs.org/sdr/DHL9870642C), May 14, 1998: BULKHEAD FITTING. CORRODED. AT C-CHECK, CORROSION ON FITTING LOCATED ON AFT SIDE OF BULKHEAD AND KEEL BEAM FWD END LBL 15, WL 166. REMOVED AND REPLACED FITTING PER SRM 51-10-1. N/R 3580. - [SDR DHL9870641C](https://openairdocs.org/sdr/DHL9870641C), May 14, 1998: SEAT TRACK. CORRODED. AT C-CHECK, CORROSION AT NUT PLATE ON OUTBD FLANGE OF SEAT TRACK LBL 46 BETWEEN BS 480 AND 600. REMOVED SEAT TRACK, REMOVED CORROSION FROM CABIN FLOOR, WITHIN L - [SDR DHL9870640C](https://openairdocs.org/sdr/DHL9870640C), May 14, 1998: SKIN. CRACKED. AT C-CHECK, FWD ENTRY DOOR CUTOUT EXTERIOR SKIN JUST ABOVE UPPER FWD CORNER OF CUTOUT. STOP DRILLED CRACK, INSTALLED EXTERNAL DOUBLER PER S/B 53-186 21 X 50. N/ - [SDR DHL9870639C](https://openairdocs.org/sdr/DHL9870639C), May 14, 1998: ANGLE. CRACKED. AT C-CHECK, LOWER FWD CARGO DOOR INTERIOR CRACK INTO RADIUS OF ANGLE SUPPORT, INSIDE AFT CTR SIDE. REMOVED AND REPLACED ANGLE AT LEFT LOWER END PER SRM 52-30-1, - [SDR DHL9870638C](https://openairdocs.org/sdr/DHL9870638C), May 14, 1998: SKIN. CORRODED. AT C-CHECK, LOWER FWD CARGO DOOR EXT SKIN HAS BULGE AT LWR FWD AREA. CUT OUT DAMAGED AREA, HFEC, INSTALLED EXTERNAL DOUBLER PER SRM 52-00-3, 7 X 6. N/R 3558. - [SDR DHL9870637C](https://openairdocs.org/sdr/DHL9870637C), May 14, 1998: SEAT TRACK. CORRODED. AT C-CHECK, FWD CARGO RT SEAT TRACK STR 27R HAS CORROSION AT TOP AND BOTTOM BS 480 TO 510. N/R 3550. - [SDR DHL9870626C](https://openairdocs.org/sdr/DHL9870626C), May 14, 1998: ANGLE. CRACKED. AT C-CHECK, LEFT WING L/E, NR 2 SLAT OUTBD TRACK, INBD SUPPORT RIB AFT VERTICAL DOUBLER HAS A VERTICAL CRACK AT BOTTOM. REMOVED AND REPLACED ANGLE SUPPORT PER S - [SDR DHL9870625C](https://openairdocs.org/sdr/DHL9870625C), May 14, 1998: RIB. CRACKED. AT C-CHECK, LT UPPER RIB AT 70.5 WING CENTER SECTION HAS 2 CRACKS AT FWD UPPER HOLE AND 3 CRACKS AT FWD LOWER HOLE. STOP DRILLED CRACKS, HFEC, INSTALLED REPAIR - [SDR DHL9870619C](https://openairdocs.org/sdr/DHL9870619C), May 14, 1998: SKIN. DENTED. AT C-CHECK, L/E OF AFT BAGGAGE BIN DOOR IS DENTED IN SEVERAL PLACES. REPLACED SKIN AT AFT CARGO DOOR PER SRM 52-30-02, 48 X 52.5. N/R 3549. - [SDR DHL9870615C](https://openairdocs.org/sdr/DHL9870615C), May 14, 1998: PLATE. CRACKED. AT C-CHECK, RT WING BELOW NR 13 SPOILER REMOVED AND REPLACED CORRUGATE PLATE AT RT WING PER SRM 57-20-1. N/R 2090. - [SDR DHL9870614C](https://openairdocs.org/sdr/DHL9870614C), May 14, 1998: BRACKET. CRACKED. AT C-CHECK, RT WING I/B SPOILER NR 11 HAS PANEL VERTICAL BRACKET CRACKED, ATTACHED TO SUPPORT ROD LOWER END. REMOVED AND REPLACED BRACKET PER SRM 51-10-1. N/R 2 - [SDR DHL9870613C](https://openairdocs.org/sdr/DHL9870613C), May 14, 1998: PLATE. CRACKED. AT C-CHECK, RT WING I/B PANEL SUPPORT CORRUGATED PLATE HAS CRACK AND LOOSE FASTENERS BETWEEN LOWER WING SPAR AND LOWER WING SKIN WS 350. REMOVED AND REPLACED SU - [SDR DHL9870602C](https://openairdocs.org/sdr/DHL9870602C), May 14, 1998: COWLING. TORN. AT C-CHECK, NR 1 ENGINE COWL SKIN TORN BETWEEN NR 2 AND NR 3 LATCH. REMOVED DAMAGED AREA, INSTALLED DOUBLER REPAIR PER RM 54-10-3 6 X 3. N/R 6871. - [SDR DHL9870601C](https://openairdocs.org/sdr/DHL9870601C), May 14, 1998: COWLING. CORRODED. AT C-CHECK, NR 1 ENG LOWER COWL HAS AN AREA OF CORROSION ON SKIN. CUT OUT DAMAGED SECTION, INSTALLED REPAIR PER SRM 54-10-3 FILLER 29 X 4.5 DOUBLER, 18.5 X 18.5 - [SDR DHL9870634C](https://openairdocs.org/sdr/DHL9870634C), May 13, 1998: STIFFENER. CRACKED. AT C-CHECK, RT WING LEADING EDGE FRONT SPAR OUTBD VERTICAL STIFFENER CRACKED AT LOWER END, NR 6 SLAT OUTBD. REPLACED VERTICALS STIFFENER PER SRM 51-10-1. N/R 20 All 66: https://openairdocs.org/deregistered/N706DH-2000-09-21/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.